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CIVIL AVIATION AUTHORITY OF BANGLADESH AIR NAVIGATION ORDERS

AIRWORTHINESS REQUIREMENTS

PART A – AIRWORTHINESS CERTIFICATION

CHAPTER A.1 DESIGN STANDARDS AND ISSUE OF CERTIFICATE OF TYPE APPROVAL OF AIRCRAFT

Section No. Title 1. GENERAL 2. DEFINITIONS 3. PRIMARY DESIGN STANDARDS-AIRCRAFT, ENGINES AND

PROPELLERS 4. PRIMARY DESIGN STANDARDS – AERONAUTICAL

PRODUCTS 5. CERTIFICATE OF TYPE APPROVAL

Appendix - 1 TECHNICAL AND AIRWORTHINESS DATA Appendix - 2 FORM AWS – 17

1. GENERAL

1.1 This Order prescribes airworthiness design standards for aircraft, engines and propellers

and the design standard acceptable for aircraft materials, parts, processes and appliances, and the requirements for issue of a Certificate of Type Approval to be issued by the Chairman in respect of a complete aircraft.

2. DEFINITIONS

2.1 For the purpose of this Order, the definitions as mentioned under the Rule 2, 183 and

234 of the Civil Aviation Rules, 1984 shall apply. Where a particular definition is not given under the rules, the under mentioned definitions shall apply:

(a) "Aircraft appliances/components" means a major assembly of a complete

aircraft, engine or propeller and includes for example wings, flight control surfaces, landing gears, generators, fuel pumps, actuators, avionic components etc.

(b) "Aircraft parts" means, a sub-assembly of an aircraft component and standard

items including fasteners, rivets, nuts, bolts, rigging cable and electrical wire.

(c) “Certification compliance book (check list)” means the book compiled by the respective manufacturer(s) to show means of compliance with the applicable Design Standard of the aircraft.

Issue 4 17 September 2009

Page 2 ANO A.1

(d) “Certificate of type approval” in respect of an aircraft means, the action taken by the Chairman, as an alternative to issuing CAAB’s own Type Certificate (TC), in accepting a Type Certificate including the Type Certificate Data Sheet (TCDS) issued by any other contracting State which meets the design standard of the CAAB as specified in this Order.

(e) "Country of origin" means, the country having airworthiness responsibility for the

design approval; usually this is the country in which the aeronautical product is manufactured or assembled.

(f) “EASA CS” means European Aviation Safety Agency Certification

Specification as determined by the aviation safety agency formed by the member states of European Union.

(g) “FARs” means aviation regulations issued by Federal Aviation Administration

(FAA) of USA.

(h) “Large aero plane” means an aero plane of a maximum certified take-off mass of over 5700 kg.

(i) "Model of aircraft" means, a particular version of an aircraft type, such as

would be distinguished from another version of the same type by a change of sufficient effect on the weight and balance, structural strength, operational characteristics, or other characteristics as would require a separate entry on the type certificate identifying and approving the particular version as distinct from the identification and approval of other version, (e.g. Boeing 747-400 model of aircraft).

(j) “Small aero plane” means an aero plane of a maximum certified take-off mass

of 5700 kg or less.

(k) "Type of aircraft" means, a design and make of aircraft and refers to group of essentially similar aircraft, which although possibly existing in different models, stem from a common basic design (e.g. Boeing 747 aircraft).

(l) “Very light aero plane (VLA)” means aero planes with a single engine (spark

or compression-ignition) having not more than 2 (two) seats, with a maximum certified take-off mass of not more than 750 kg and certified as per EASA CS VLA design standard..

(m) “Very light rotorcraft (VLR)”means rotorcrafts (helicopters) with maximum

certified take-off mass not exceeding 600 kg which are: (i) of a simple design.; (ii) designed to carry not more than two occupants; (iii) not powered by turbine and/or rocket engines; and (iv) restricted to VFR day operations.

2.2 A term or abbreviation used in a design standard shall, unless otherwise specified by

the Chairman, CAAB be interpreted as having the meaning defined or applied therein.


Page 3 ANO A.1

3. PRIMARY DESIGN STANDARDS - AIRCRAFT, ENGINES AND PROPELLERS

3.1 Unless otherwise specified by the Chairman, the primary airworthiness design

standards in respect of aircraft, engines and propellers are:

3.1.1 Normal, Utility, Acrobatic and Commuter (Small or Light Aero plane)

: FAR part 23 or EASA CS – 23 or CS-VLA as applicable

3.1.2 Transport category aero planes (Large Aero plane)

: FAR part 25 or EASA CS - 25

3.1.3 Small rotorcraft (Normal or Light category):

: FAR part 27 or EASA CS - 27 or CS-VLR as applicable

3.1.4 Large rotorcraft (transport category) : FAR part 29 or EASA CS – 29 3.1.5 Engines : FAR part 33 or EASA CS- E 3.1.6 Propellers : FAR part 35 or EASA CS - P 3.1.7 Auxiliary power unit : EASA CS –APU 3.1.8 Sailplanes or Powered sailplanes : FAR part 23 or EASA CS - 22 3.1.9 Manned free balloons : FAR part 31 3.1.10 Hot Air Balloons : EASA CS -31 HB

3.2 The design standard used as the basis of certification for the importation of a

complete aircraft or for assembly of a complete aircraft or complete engine or propeller shall be recorded with the respective airworthiness or engineering documents and notified to the CAAB, and that standard shall thereafter be used as the basis of approval for all modifications and repairs to that aircraft or engine or propeller.

3.3 For aircraft or engine or propellers having more than one basis of certification, the

standard adopted by the country of Manufacture shall apply, provided it conforms to the requirements of the section 3.1 of this Order.

3.4 At the time of issue of Certificate of Airworthiness by the CAAB, applicable design

standard of an aircraft as mentioned in the paragraph 3.1 of this Order shall also be mentioned in the “Category” block of the Certificate of Airworthiness of the individual aircraft.

4. PRIMARY DESIGN STANDARDS – AERONAUTICAL PRODUCTS

4.1 Unless otherwise specified, the primary airworthiness design standard for aeronautical

products i.e. aircraft materials, part, processes and appliances are:

(a) Technical standard order (TSO) issued by FAA (FAR part 21, sub-part - 0) of the USA; or

(b) European Technical Standard Orders (CS- ETSO) issued by EASA; or

(c) Other standard that may be acceptable to the Chairman.


Page 4 ANO A.1 Note: For list of TSOs, reference should be made to the AC 20-36 published by FAA and

the TSO indices published by EASA. 4.2 Aircraft parts and/or class III products as defined in the FAR part 21.321 are

acceptable for installation on aircraft registered in Bangladesh if produced and approved under: (a) Parts manufacturing approval (PMA) issued under the FAR 21, sub-part K; or

(b) Production certificate (PC) issued under the FAR 21, sub-part G.

5. CERTIFICATE OF TYPE APPROVAL

5.1 Either the holder of the original Type Certificate (TC) or the prospective operator

for the aircraft type may apply to the Chairman for issue of a Certificate of Type Approval (CTA) in respect of a type certificated aircraft, which meets the design standard mentioned in the paragraph 3.1 provided Certificate of Type Approval has not been issued earlier by the Chairman in respect of that type of Aircraft or model of the aircraft. The Certificate of Type Approval shall be issued in respect of the aircraft type itself and not the applicant.

5.2 The Chairman may issue a Certificate of Type Approval in respect of a Type

Certificate on acceptance of original Type Certificate issued by the National Aviation Authority (NAA) of the country of manufacture, provided the TC conforms with the requirements of the section 3.1 of this Order. Certificate of Type Approval shall not be issued on the basis of Certificate of Validation of a TC issued by a contracting State.

5.3 The applicant shall submit an application on AWS- 17, as shown in Appendix-2 of

this order and shall submit the preliminary technical data as mentioned in the Appendix-1 of this order.

5.4 If accepted, the applicant will be asked to submit further technical data (as identified

by an asterisk (*) in the Appendix-1 to this order for examination by the Airworthiness and Engineering Licensing Division of the CAAB. The examination will normally include: (a) An assessment of the adequacy of the code of design standards applied and

their amendment status to ensure that no hazardous characteristics exist in the design and construction of the aircraft;

(b) An assessment of acceptability of any waivers or variations granted by the State of Design;

(c) An assessment of suitability of any special conditions specified and Certified by the State of Design; and

(d) An assessment of adequacy of type design in regard to specified requirements, operating conditions and airworthiness requirements of the CAAB.

5.5 The remaining further technical data/documents may be supplied later on, but

invariably be submitted by the operator along with application for issue of Certificate of Airworthiness for the first aircraft.


TECHNICAL AND AIRWORTHINESS DATA

APPENDIX-1 ANO.A1

Preliminary Technical Data (Para 5.3 of the Order)

1. Type Certificate and Type Certificate Data Sheet. 2. Certification Compliance Book or Certification Basis Book

Further Technical Data (Para 5.4 of the Order)

1. (*) Master equipment list. 2. (*) Maintenance Review Board (MRB) Report or equivalent document. 3. (*) Aircraft Flight Manual (AFM). 4. Flight Crew Operating Manual (FCOM). 5. Master Minimum Equipment List (MMEL). 6. MMEL Procedures Manual. 7. Configuration Deviation List (CDL). 8. Aircraft Maintenance Program/Schedule. 9. Aircraft Maintenance Planning Document (MPD). 10. List of Certification Maintenance Requirements (CMR) items published in applicable

document, as may be stated or referred in the TCDS. 11. Manufacturers’ (Aircraft/Engine/Propeller) Maintenance Manual, Weight and Balance

Manual, Overhaul Manual, Structural Repair Manual and Illustrated Parts Catalog. 12. Electrical Load Analysis covering all services of the aircraft. 13. Airworthiness Directives. 14. Service Bulletins. 15. Life Limited Critical Parts (Airworthiness Limitations) having retirement/scrapped life

and which are subject to fatigue. (if this information is not provided elsewhere in the above mentioned data).

16. Additional data and descriptive information that may be needed by the Authority to issue Acceptance Type Certificate in respect of the product.

Supply Of Continuing Airworthiness Data (Para 5.7 of the Order)

1. Amendments to the documents/manuals listed above and other documents/manuals

necessary for airworthiness support of the aircraft. 2. Airworthiness Directives. 3. Service Bulletins (SBs)

Note (*): Please refer the paragraph 5.4 of the ANO (AW), A.1.

Issue 4 Page 1 of 1 17 September 2009

AWS-17 ISSUE-1

APPENDIX-2 ANO A.1

CIVIL AVIATION AUTHORITY OF BANGLADESH Airworthiness & Engineering Licensing Division

APPLICATION FOR ISSUE OF CERTIFICATE OF TYPE APPROVAL.

1. Name of the organization :

2. Name of the applicant :

3. Address :

4. Contact person of the organization

: :

5. Telephone :

6. Fax :

7. E-mail :

8. Product identification: Type Certificate Supplemental Type Certificate Others

9. Information on payment of fees: The fee has been deposited in the account STD-16, Sonali Bank, Kurmitola, Dhaka-1229 as mentioned below:

Deposit slip No. Date

Amount Tk (in words)

10(a) Fixed wing aircraft

Large Aeroplanes (CS-25/FAR-25) Over 5,700 kgs

Small/Light Aeroplanes (CS-23/FAR-23. CS-22, CS- VLA) Over 5,700 kg up to 8,620 kg (incl. commuter) over 1000 kg up to 5,700 kg up to 1000 kg VLA, powered sailplanes, sailplanes

10(b) Rotorcraft Transport category (CS-29/FAR-29)

Normal category (CS-27/FAR-27)

Light category (CS-VLR)

10(c) Power plant Engines (CS-E/FAR-33) Reciprocating Turboprop Turbojet

10(d) Propeller (CS-P/FAR-35)


AWS-17 ISSUE-1

APPENDIX-2

ANO A.1 11. Type and Model of the

Aircraft

12.

(a) TC No.

(b) TCDS No.

13. Restriction (if applicable)

14. List of documents enclosed

(a) Type Certificate

(b) Type Certificate Data Sheet

(c) Certification Compliance Book or Certification of Basis Books

(d) Others (to be specified)

15. Applicant’s declaration

I do hereby state that the information contained herein is correct and complete. Moreover, I agree to pay the fees levied by the Chairman in respect of the issuance of a Type Certificate/Restricted Type Certificate or approval of a derivative and am aware of the consequences of non-payment.

16. Signature

Date Name Signature

This application should be sent by regular mail to: CHAIRMAN, CAAB HEADQUARTERS, KURMITOLA, DHAKA-1229, ATTENTION: AELD

Note- Application for Type Certificate of restricted Type Certificate will be charged as mentioned in the ANO (AW) A.10.


ANO A.2



PART A- AIRWORTHINESS CERTIFICATION

CHAPTER A.2 IMPORT PROCEDURES OF AIRCRAFT AND ISSUE AND RENEWAL OF CERTIFICATE OF AIRWORTHINESS

Section No. Title

1. GENERAL 2. DEFINITIONS 3. PROCEDURE FOR IMPORT OF AIRCRAFT UNDER

PURCHASE AGREEMTNT OR DRY LEASE 4. PROCEDURE FOR IMPORT OF AIRCRAFT UNDER WET

LEASE 5. AIRCRAFT TYPE DATA 6. ISSUANCE OF CERTIFICATE OF AIRWORTHINESS 7. RENEWAL OF CERTIFICATE OF AIRWORTHINESS 8. AIRWORTHINESS FLIGHT TEST 9. SURVEY INSPECTION OF AIRCRAFT 10. SUSPENSION AND CANCELLATION OF C OF A

APPENDIX-1 Form CA – 182C, Issue-5 APPENDIX-2 Form CA – 25, Issue-3 APPENDIX-3 Form CA-182C-1, Issue-4 APPENDIX-4 Form CA – 26, Issue-3 APPENDIX-5 Form AWS – 16, Issue-2 APPENDIX-6 Compliance Checklist-Aircraft Documentation, Issue-1

1. GENERAL

1.1 This Order prescribes the procedures for import of an aircraft, issue and renewal

of Certificate of Airworthiness of aircraft to be registered in Bangladesh, and also issue and renewal of aircraft registered in Bangladesh.

1.2 Persons considering import of an aircraft into Bangladesh should consult with

the Airworthiness and Engineering Licensing Division (AELD) of Civil Aviation Authority, Bangladesh to ensure that the airworthiness and design standards required to qualify for a Certificate of Airworthiness are clearly understood before importing aircraft.

Issue -5 Page-1 05 April, 2011

ANO A.2

2. DEFINITIONS

2.1 For the purpose of this Order, the definitions as mentioned under the Rule 2, 183 and 234 of the Civil Aviation Rules, 1984 shall apply. Where a particular definition is not given under the rules, the under mentioned definitions shall apply:

(a) “Recent data” in respect of issue/renewal of C of A means, the data

applicable within the preceding period not exceeding 30 (thirty) days from the date application for the purpose.

(b) “Used aircraft” means an aircraft which is 5 (five) years of age or have

accumulated at least 5000 (five thousand) hours or both since manufacture.

3. PROCEDURE FOR IMPORT OF AIRCRAFT UNDER PURCHASE

AGREEMTNT OR DRY LEASE.

3.1 In connection with import of any aircraft into Bangladesh, applicable rules of the Ministry of Commerce of the Government of the Peoples Republic of Bangladesh must be followed by an applicant or importer.

3.2 On the date of application, all aircraft to be procured under any type of Leasing

or Purchase agreements or in combination of both, must meet the requirements of:

(a) The ANO (AW) A.1; and

(b) The ANO (AW) B.21

3.3 In additionally, the aircraft to be acquired/ imported as applicable shall have at

least 30% (thirty percent) of time (hours or one year of calendar time) left for the next “C” check or Equivalent check, as per the MRB interval applicable for the aircraft, since last ‘C’ check or Equivalent check accomplished. In case the remaining time is less than 30% (thirty percent or less than of calendar time) then, at least a fresh “C” check or an “Equivalent” check including bridge-in- inspection as may be applicable, shall be accomplished within a period not exceeding 90 (ninety) days prior to positioning the aircraft in Bangladesh.

3.4 After compliance with the requirements as mentioned in the paragraph 3.3

above, and before signing any agreement for procurement and import of any aircraft into Bangladesh, the Operator or the Applicant must obtain permission i.e. Technical Clearance (TC). Application for TC of the aircraft is to be made through duly filled in form CA-182C/CA-182C-1 (refer Appendix-1/Appendix-3 of this order) along with the supporting documents. The TC will be issued on completion of the required inspection of the aircraft by the Airworthiness official(s) of the CAAB. The inspection shall be arranged after completion of all maintenance of the aircraft, during which the aircraft and its records will be inspected.

Issue-5 Page-2 05 April, 2011

ANO A.2

3.5 The TC issued in respect of the aircraft shall be valid for a period of 90 (ninety)

days from the date of issue of Technical Clearance. Within this 90 days period the followings are to be completed by the importer:

(a) Import Permit;

(b) If applicable, an application for Issue of Certificate of Registration; and

(c) If applicable, an application for Issue of Certificate of Airworthiness.

3.6 In case of failure to complete any or all of the above requirements within 90 (ninety) days of issue of the Technical Clearance, a new Technical Clearance is to be sought by submitting a fresh application for compliance with the requirements mentioned para-3, subpara-3.4.

3.7 Depending upon formal notification by the Applicant, either a Temporary C of R

as per the ANO (AW) A.5 and C of A as per the ANO (AW) A.2 will be issued or formal Letter of Authorisation will be issued for positioning the aircraft in Bangladesh based on the C of R and C of A of the country in which the aircraft is registered.

3.8 Application for the issue of a Certificate of Airworthiness for an aircraft located

outside Bangladesh shall be made on applicable forms (refer appendix-2 of this order) and must be submitted with a receipt for the appropriate fee at least prior to 30 (thirty) days of the desired date of issue of C of A.

3.9 After survey inspection at the site of the aircraft by airworthiness official(s), a

provisional Certificate of Airworthiness endorsed with the restriction "Issued for non-revenue ferry flight and valid only until the first landing at a customs Airport in Bangladesh" will be issued with restriction (if any) as may be required by CAAB.

3.10 The Certificate of Airworthiness for Export issued by the State of Export, should

have been issued not earlier than 30 (thirty) days and not more than 50 (fifty) flight hours prior to the date of application and shall meet additional requirements of the CAAB, if notified any.

3.11 Where the exporting country does not issue a Certificate of Airworthiness for

Export, or equivalent, the Chairman may accept in lieu of Export C of A, the current valid Certificate of Airworthiness of the State of Export and issue CAAB’s own Provisional C of A.

3.12 Issue of a Provisional Certificate of Airworthiness for an imported aircraft shall

be subject to compliance with all relevant Rules of the CARs 1984 and Air Navigation Orders issued by the Chairman.

3.13 All cost of travels for overseas investigation in connection with inspection of the

aircraft, records and issue of appropriate certificates will be borne by the applicant as per the Rule 213 of the Civil Aviation Rules, 1984.


ANO A.2

3.14 For aircraft imported by means other than air, issue of a Certificate of Airworthiness will be effected in Bangladesh in accordance with normal procedures as specified in this Order.

4. PROCEDURE FOR IMPORT OF AIRCRAFT UNDER WET LEASE

4.1 The procedures stated in the MOCAT gazette no. wecg/wmG-2/cvm-3/2003-

542, ZvwiL 26-11-2007 shall be followed.

4.2 On the date of application, all aircraft to be procured under any type of Leasing or Purchase agreements or in combination of both, must meet the requirements of:

(a) The ANO (AW) A.1; and (b) The ANO (AW) B.21.

4.3 For aircraft imported under wet lease agreement only the form CA-182C-1,

Issue-4 (Appendix-3) form filled up and shall be submitted to AELD at least 30 (thirty) days earlier before import of the aircraft along with the leased agreement (two copies). Following satisfactory inspection of the aircraft at the main maintenance base by the Airworthiness Official(s) of the CAAB, the instructions of placing the aircraft will be made.

4.4 In wet leases the lessor normally exercises operational control of the aircraft. A

wet lease situation therefore means that an aircraft will be operated under an AOC issued by the State of the lessor. In this case the State of the Operator may also be the State of Registry of the leased aircraft.

5. AIRCRAFT TYPE DATA

5.1 For each aircraft that is the first of its type for issue of Certificate of

Airworthiness in Bangladesh, the Technical Data mentioned in the ANO (AW) A.1, shall be submitted to the Chairman.

6. ISSUANCE OF CERTIFICATE OF AIRWORTHINESS

6.1 Certificate of Airworthiness shall be issued only in respect of the aircraft having a

Certificate of Registration issued by the Chairman.

6.2 The qualified applicant shall submit an official letter along with appropriate fee for issue of Certificate of Airworthiness and Noise Certificate as mentioned in ANO (AW) A.10 titled Fees/Charges for Airworthiness Services, to the Chairman on CAAB’s following forms with “recent” data, at least 30 (thirty) days prior to intended issue date of the provisional Certificate of Airworthiness:


ANO A.2

(a) Technical Data for issue of Certificate of Airworthiness on the Form CA- 182C (Issue -5, refer Appendix -1 of this Order);

(b) Application for issue of Certificate of Airworthiness on the Form CA-25,

(Issue -3, refer Appendix -2 of this Order);

(c) Compliance check list- Aircraft documentation (Issue-1, refer to Appendix -6, of this Order);

(d) Copy of letter from the manufacturer of the (i) Aircraft, (ii) Engine and

(iii) Propeller (if applicable) or Paid Order form confirming that the Applicant (Operator) has subscribed for the required Continuing Airworthiness Data as mentioned in the ANO (AW) A.1, titled “Design Standards and Issue of Certificate of Type Approval of Aircraft”; and

(e) Application for issue of noise certificate, Form AWS-18.

6.3 The applicant should make the aircraft available, at a time and place (maintenance

facility) acceptable to the AELD, for such checks and inspections considered necessary by the AELD.

6.4 It shall be the responsibility of the applicant to provide personnel and equipment

so that these checks and inspections may be satisfactorily carried out;

6.5 All work required to be done on the aircraft for the issuance of a Certificate of Airworthiness shall be carried out under the supervision of an organization approved by, or acceptable to, the AELD and be carried out in a proper manner and in conformity with the requirements, specifications, drawings and instructions relating to the approved design of the subject aircraft.

6.6 Full particulars of the work done should be entered in the appropriate log books

and a Maintenance Release shall be issued before issue of Provisional Certificate of Airworthiness as per the ANO (AW) B.3 titled Maintenance Certification Systems.

6.7 The organization referred to in the paragraph 5.5 of this Order should provide a

certification that the aircraft is fit to fly as far as can be reasonably determined from inspections of the aircraft and its records and manuals, and that all applicable Airworthiness Directives and mandatory modifications and inspections of the State of Design and the CAAB have been carried out or certified to have been carried out.

6.8 Automatic Data Processed (ADP) records or Computerized Print-out shall contain

signature of authorised person(s) of both the immediate last Operator or the Manufacturer and authorised person (s) of the Applicant seeking C of A.

Note: The AELD may, from time to time, stipulate special requirements to be met

before a Certificate of Airworthiness is issued. These should be listed as special conditions and communicated to the applicant.


ANO A.2

6.9 Documents for examination: The applicant shall make available Documents, Log Books, Inspection and Maintenance Records of the Aircraft, for examination by the AELD preferably in the standard format as described in the Appendix-6 titled Compliance Checklist-Aircraft Documentation and shown in the Appendix-6 of this Order.

6.9.1 Maintenance Programme including the following:

(a) Corrosion Prevention and Control Programme (CPCP); and

(b) Structural Integrity Programme.

6.9.2 Maintenance Task Identification Codes (HT, CM, OC, LU, SV, OP, RS, DS etc. as appropriate to the aircraft maintenance programme).

6.9.3 Manufacturer’s Master Change (MC) list, Kit Change Notice (KCN),

Supplemental Type Certificate (STC).

6.9.4 Log Books of the (i) Aircraft, (ii) Engine, (iii) Propeller and (iv) Auxiliary Power Unit (APU) as applicable.

6.9.5 Modification Log Books or Records of the (i) Aircraft, (ii) Engine, (iii) Propeller

and (iv) Auxiliary Power Unit (APU) as applicable.

[{

6.9.6 Historical Records of all components and aircraft parts containing the followings:

(i) Part Numbers, Nomenclature and Serial Numbers (if applicable) of Installed items;

(ii) Time Controlled Components (Flight Hours/Flight Cycle or Landings/

Calendar periods) having Time Between Overhaul (TBO), Restoration (RS), On Condition (OC); and

(iii) Life Limited Components / Parts having discard (DS) life.

6.9.7 Airworthiness Directives compliance records.

6.9.8 Major Repairs and Alteration records.

6.9.9 Service Bulletins compliance records.

6.9.10 Report of the recent “C” check or equivalent check.

6.9.11 Recent weighing and weight & mass balance report.

6.9.12 Recent Flight Test report on performance and handling qualities of the aircraft including the Avionics Systems in accordance with the Flight Test Schedules approved by the CAAB.

6.9.13 Any additional requirements of the CAAB.


ANO A.2

6.10 Additionally, in case of used aircraft and depending upon the AELD’s assessment of the adequacy of the previous State of Registry’s airworthiness code, the applicant may be required to submit a statement from the airworthiness authority of the State of Design certifying that deviation/departures (if any) made by the previous operator(s) are acceptable.

6.11 Documents for retention: The applicant shall submit the documents as

mentioned in the ANO (AW) A.1 and the following customized Manuals and Documents for retention by the AELD:

(a) A copy of the Type Certificate and the Type Certificate technical data

sheets or acceptable equivalent documents.

(b) A copy of the Export Certificate of Airworthiness issued by the State of Manufacture, and the current Certificate of Airworthiness.

(c) A copy of the flight manual or acceptable equivalent document.

(d) A copy each of the manufacturer’s maintenance, overhaul and repair

manuals and illustrated parts catalogues.

(e) A complete set of all manufacturer’s service bulletins or equivalent documents issued in respect of the aircraft.

(f) A copy of the flight crew operating manual.

(g) A copy of the mass and balance report.

(h) A flight test report for the avionics systems.

(i) A flight test report for the aircraft.

(j) A copy of the maintenance review board report for the aircraft type.

(k) An electrical load analysis covering all services.

(l) Unless held by the applicant and available for examination, a complete set of wiring diagrams covering all electrical and radio installations.

(m) Where applicable, a copy of the master minimum equipment list (MMEL).

(n) Customized Maintenance Programme.

(o) Customized MEL.

(p) Noise Certificate (issued by the country of export) and

(q) Any other documents as may be necessary.


ANO A.2

6.12 Supply of Continuing Airworthiness Data: The applicant shall be required to make the necessary renewal arrangements with Aircraft, Engine and Propeller (if applicable) manufacturers for continuous and un-interrupted amendments/revision service of the manuals as mentioned in the ANO (AW) A.1.

Note: The applicant(s)/operator(s) procuring used aircraft from another operator is/are

particularly reminded to ensure positive and confirmed supply of the required Continuing Airworthiness Documents/Publications from the manufacturer and also from the Seller of the aircraft where applicable.

7. RENEWAL OF CERTIFICATE OF AIRWORTHINESS

7.1 An official letter forwarding application for renewal of C of A should be

completed and appropriate fee for renewal of Certificate of Airworthiness as mentioned in ANO (AW) A.10 titled Fees/Charges for Airworthiness Services shall be submitted to the AELD on CAAB’s following forms with “recent” data at least 30 (thirty) days prior to intended renewal date of the Certificate of Airworthiness:

(a) Application on the Form CA–26, (Issue-3, refer Appendix-4 of this

Order); and

(b) Certificate of Inspection for renewal of C of A on the Form AWS-16 (Issue-2, refer Appendix-5 of this Order);

7.2 The applicant should be required to make the aircraft available, at a time and

place acceptable to the AELD, for Survey Inspection and such checks as required by the AELD.

7.3 The applicant should be required to provide the necessary personnel and

equipment so that required checks and inspections may be satisfactorily carried out by CAAB;

7.4 All work for the maintenance of airworthiness of the aircraft should be carried out

under the supervision of appropriately licensed aircraft maintenance personnel or by an organization approved by, or acceptable to, the AELD and should be carried out in a proper manner and in conformity with the requirements, specifications, drawings and instructions relating to the approved design of the subject aircraft.

7.5 Full particulars of the work accomplished should be entered in the appropriate log

book and a maintenance release should be issued as per the ANO (AW) B.3 titled Maintenance Certification Systems, if applicable.

7.6 Documents for examination: The applicant shall make available Documents,

Log Books, Inspection and Maintenance Records of the Aircraft since issue or last renewal of the C of A, for examination by the AELD. This shall include the followings but not limited to:


ANO A.2

(a) The documents mentioned in the section 6.9 of this Order; and

(b) Certificate of currency in respect of the Aircraft Flight Manual by an authorised signatory.

7.7 Documents for retention: The following Documents shall be retained by the

AELD:

(a) A copy of the aircraft weighing and mass & balance report;

(b) A copy of the Recent Flight Test report;

(c) Certificate on Revision Status of AFM and MEL; and

(d) Any other documents as may be necessary.

8. AIRWORTHINESS FLIGHT TEST

8.1 Flight tests — Issuance of a Certificate of Airworthiness

8.1.1 When an application is made for the issuance of a Certificate of Airworthiness, flight tests should have been completed in the Country of Export to a flight test schedule acceptable to the AELD to establish compliance with:

(a) The airworthiness requirements of the Country of Export/CAA of

Bangladesh.

(b) Such other conditions prescribed by the AELD as special conditions for the issuance of a Certificate of Airworthiness;

(c) In certain circumstances the AELD may require special flight tests to be

carried out to determine conformity with the national airworthiness requirements. If this procedure is necessary, the applicant should be notified and should arrange the same for AELD;

(d) The flight test schedules for the special test should be prepared by the

applicant and should require the approval of the AELD; and

(e) The applicant should submit to the AELD the results of the special tests in a flight test report acceptable to the AELD.

8.2 Flight tests — Renewal of a Certificate of Airworthiness

8.2.1 When an application is made for the renewal of a Certificate of Airworthiness,

flight tests should have been completed to a flight test schedule acceptable to the AELD and as per the interval mentioned in the Operator’s Maintenance Control Manual to establish compliance with:


ANO A.2

(a) Flight tests associated with the renewal of a Certificate of Airworthiness should be conducted in accordance with an airworthiness flight test schedule prepared for the aircraft type and approved by the AELD. The flight tests are required to ensure that the aircraft’s flight characteristics and its functioning in flight do not differ significantly from the normal performance for the type. Flight performance should be checked against the appropriate sections of the flight manual which is fully amended to current standards.

(b) At the conclusion of an airworthiness flight test in connection with

renewal of the Certificate of Airworthiness, the test report should be prepared in a manner acceptable to the AELD and should include the results of tests specified in the airworthiness flight test schedule, as well as a statement of observed performance versus flight manual performance for the same configuration and atmospheric conditions.

(c) Airworthiness flight test reports should be submitted to the AELD. If any

phase of the tests needs to be repeated, the AELD should give notification of requirements.

9. SURVEY INSPECTION OF AIRCRAFT

9.1 Each aircraft for which application is made for Issue and Renewal of a Certificate

of Airworthiness shall be subject to a survey inspection, the extent and conduct of which will be determined by the Chairman.

9.2 Where an aircraft has been adequately inspected within the preceding 30 (thirty)

days, the required survey inspection may be waived when renewing the Certificate of Airworthiness.

9.3 In cases where the AELD is not familiar with the aircraft type, the CAAB may

delegate responsibility of the survey inspection to an appropriately approved maintenance organization where the inspection is to be accomplished in the presence of CAAB’s Airworthiness Inspector(s).

9.4 Where a survey inspection is delegated to an approved maintenance organization,

a report of the inspection shall be submitted to the CAAB by that organisation.

9.5 All costs of the survey inspection at a location(s) other than at the main base of the Operator, associated with issuance and renewal of certificate of Airworthiness of aircraft shall be borne by the applicant as per the rule 213 of the CARs 1984.

9.6 Where an aircraft is to be surveyed by a CAAB airworthiness inspector, the

maintenance engineer or the organization responsible for the aircraft shall ensure that the aircraft is clean and that all the cowlings and access panels are removed prior to the time agreed for the inspection.


ANO A.2

9.7 A survey inspection may include any or all of the following:

(a) Weighing of the aircraft;

(b) Inspection of the structure for corrosion, cracks and distortion;

(c) Inspection of the fabric and skin for deterioration and distortion; (d) Duplicate inspection of flight controls;

(e) Inspection of systems for condition and functioning; (f) Cabin pressurization check;

(g) Instrument serviceability check; (h) Compass swing;

(i) Inspection of the radio station for condition, conformity and functioning; (j) Inspection of safety equipment for condition;

(k) Verification that all applicable airworthiness directives, modifications and engineering records are implemented and meet acceptable standards; and

(l) Intermediate stage inspections during the progress of any work associated

with issue, validation or renewal of a Certificate of Airworthiness.

10. SUSPENSION AND CANCELLATION OF C OF A

10.1 The Chairman may suspend summarily any Certificate of Airworthiness if he

considers such action necessary to ensure compliance with the Civil Aviation Rule 1984, or in the interest of safety, or if it is ascertained that the holder of the Certificate has given false information for the purpose of obtaining the Certificate.

10.2 A Certificate of Airworthiness which has been cancelled or suspended in

accordance with the rule 10(5) of the CARs 1984 shall be returned to the Chairman forthwith.

10.3 Where an aircraft suffers damage, does not have a valid Maintenance Release, or

develops a defect which cannot normally be remedied by the flight crew, the Certificate of Airworthiness shall be deemed to be suspended.

9.4 A Certificate of Airworthiness which has been suspended in accordance with the

rule 187 of the CARs 1984, is deemed to be reinstated when as per the rule 203 of the CARs 1984, the Maintenance Release is revalidated or when a new Maintenance Release is issued.

10.5 Where the Certificate of Registration for an aircraft is cancelled, the Certificate

of Airworthiness shall also be cancelled, and the two certificates shall be returned to the Chairman forthwith.


APPENDIX-1 ANO A.2

Form: CA-182C Issue: 5


(TECHNICAL DATA FOR AIRCRAFT TECHNICAL CLEARANCE

IN RESPECT OF AIRCRAFT TO BE REGISTERED IN BANGLADESH)

All data shall be recent data i.e. must be no older than 30 days from the date of application

1. Aircraft Type and Model: TAT:

as on (date):

Manufacturer: TAC:

as on (date): MSN (Fuselage No.): MCTM;

*Date of Manufacture: Max. Passengers capacity

*Age of the aircraft: *Cycle of the aircraft:

*Note (1): Refer to the ANO (AW) B.21 Note (2): Evidence on the date of manufacture (e.g. if mentioned on the C of R, Aircraft Log book, Aircraft delivery document, any other official document etc.) to be enclosed.

2. Design standard of the aircraft:

*Design Standard TCDS No. issued by FAA or EASA: Remarks (if any)

*Note (1): Refer to the ANO (AW) A.1 Note (2): A copy of the TC (in case of new aircraft) and TCDS is to attached

3. Engine

Type and Model: No. of Engines:

Manufacturer: Power Rating:

Engine Position / Module name

Serial Number TSN / CSN as on (date):

TSO / CSO as on (date):

Note: In case of modular engines the required information shall be enclosed on separate page.

Issue-5 Page 1 of 9 05 April, 2011

APPENDIX-1 ANO A.2


4. APU

Type and Model: Aircraft Manufacturer:

5. Propeller / Rotor

Type and Model: Manufacturer:

Propeller Position



6. Special performance certification

Special performance Tick below against the

appropriate authorisation Reference of Certification documents and issuing authority

IFR

RVSM

BRNAV

RNP

ETOPS

ILS / AUTO LAND

MNPS

OTHERS (if any)

Note: (i) A copy of the current Operation Specification of to be enclosed in support of the Special Performance.

Note: (ii) Copy of the certification documents to be enclosed.

7. Aircraft equipment and instruments (cross out the ineligible equipment or instruments

Sl. No. Equipment / System No. of units or

Systems. Manufacturer and Model or Part number (as may be applicable)

7.1 ACAS I / ACAS II 7.2 FDR Type I / FDR Type

II / FDR IIA


APPENDIX-1 ANO A.2


7.3 CVR 7.4 EGPWS / GPWS 7.5 HF 7.6 VHF 7.7 SELCAL 7.8 Weather Radar 7.9 Attitude Indicator

(Artificial Horizon)

7.10 Heading Indicator (Directional Gyro)

7.11 Flight Director Systems (FMC / FMS / AHRS / ). Note: Specific system installed must be mentioned.

7.12 Auto Pilot 7.13 Altimeter 7.14 Sensitive altimeter

( with counter drum pointer or equivalent)

7.15 Stand by altimeter 7.16 INS / INU 7.17 Remote reading compass 7.18 Standby compass 7.19 APU 7.20 Automatic ELT 7.21 ELT (any type) 7.22 ELT (survival) 7.23 Life raft 7.24 Life jackets / Floatation

devices

7.25 Portable fire extinguishers

7.26 Passenger seats 7.27 Flight crew seats 7.28 Cabin crew seats 7.29 First aid kits 7.30 Emergency medical kits


APPENDIX-1 ANO A.2


7.31 Emergency escape path lightings

7.32 Galley 7.33 ULD containers (if any) 7.34 Toilets 7.35 Marking of break-in

points on fuselage

Note: If required, the information is to be provided in separate page.

8. Information regarding the current approved Maintenance Programme / Schedule:

AMP based on MRB report number and Revision number issued on

AMP based on the manufacturer MPD number and Revision number issued on

9. Information on Current Maintenance Check Cycles.

Scheduled maintenance Checks cycles

Check Interval (FH or/and Calendar Period as applicable)

Last performed on (date and TAT)

10. Operation and Maintenance history/status of the aircraft during last 12 months starting from current month to backward (for the period to ).

Month and Year Hours Flown

during the month

Type of Maint. Check Accomplished

Date and TAT at which the Check was accomplished


APPENDIX-1 ANO A.2


11. Information on last “C” check or equivalent check (large aircraft) or annual inspection

(small aircraft only) performed:

Date Type of Check

Check performed at/on (DT/TAT/TAC)

FH operated and days elapsed since the check

Remaining FH and Days for the next same check

12. Information on (i) Life Limited Parts (LLP) i.e. parts having scrap/retirement life / Time

Limited Works/Tasks (TLW) / Structural Inspection Programme (SIP) as on (date): .

Current AMP reference.

Name of the LLP / TLW / SIP Tasks

Approved life (LLP) or TLW

interval

Last Installed or

accomplished

Remaining life or Time

Next due time (DT/FH/CYC)

Note (1): The required information is to be enclosed on separate page in any format containing the above data which is to be certified by the current operator (in case used aircraft only).

Note (2): At the time of delivery/acceptance of an USED aircraft, the Bangladeshi operator must ensure complete receipt (100%) of all maintenance and historical documents/records (Serviceable Tags, Authorised Released Certificates for traceability, installation documents etc.) of (i) LLPs and TLW Items or Inspection from the Seller of the aircraft duly certified and sealed by the authorised person(s) and also duly verified by the authorised and competent person(s) of the Bangladeshi Operator and (ii) records of installed parts.

Note (3) In case of New aircraft, the Bangladeshi operator must ensure complete receipt (100%) of complete list on installed structural parts containing industry accepted data (parts name, part number, serial number, position installed, etc), maintenance and historical documents/records (Serviceable Tags, Authorised Released Certificates for traceability, installation documents etc.) duly certified and sealed by the authorised representative of the Manufacturer and also verified by the authorised and competent person(s) of the Bangladeshi Operator.


APPENDIX-1 ANO A.2


13. Information on past accidents (if any)

Date Aircraft TAT Brief details of damage and repair

Note: If required, the information may be provided in separate page.

14. Information on AOC and AMO (A copy each be submitted)

Name and address of the AOC holder and AOC No.

Name of the AMO for maintenance of the aircraft and Location of the AMO

E-mail address: E-mail address;

Note: A copy of the current Certificate of Approval of the AMO is to be enclosed. 15. Certificate of Registration

Current Regular C of R No. Issuing Authority

Note: A copy of the current valid certificate is to be enclosed. 16. Certificate of Airworthiness

Current Regular C of A No. Issuing Authority

Note: A copy of the current valid certificate is to be enclosed. 17. Noise Certificate:

Noise Certificate No. Issuing Authority

Note: A copy of the current valid certificate or equivalent document is to be enclosed.


APPENDIX-1 ANO A.2


18. Radio Station Operating Licence / Certificate:

Radio station licence no. Issuing Authority

Note: A copy of the current valid certificate or equivalent document is to be enclosed.

19. AD Status of the aircraft/Engine/Propeller/Appliances up to (date):

AD No. and Rev. No.

Subject in brief

Applicability status (Yes / No / Repetitive)

Initial Compliance (DT/TAT/TAC)

Next Due (DT/TAT/TAC)

Terminating action (Mod etc.) (DT/TAT/TAC)

Note: The required information is to be enclosed on similar or equivalent format

20. Information on Classification of Operation (Rule 105 of the CARs 1984) in which the aircraft is to be engaged by the Bangladeshi Lessee during the lease period:

21. Information regarding procurement of the aircraft (Tick or write as applicable) :

Out right purchase Dry lease Dry lease cum purchase agreement

Others (to be mentioned below)

Note (1): Refer to the Rule of the CARs 1984.

Note (2): Two copies of the agreement (draft or signed) to be enclosed.

22. Information in respect of the Lessor (The items in serial no. 22 through 24 are applicable for procurement of aircraft under Dry Lease agreement):

Lessor’s Name and Business address Nationality Immediate contact address

Tel: Cell: E-mail:


APPENDIX-1 ANO A.2


23. In case of lease agreement, the proposed duration of lease period:

From (date) To (date) Total period (in months)

24. Information regarding the Lessor (Tick against the appropriate statement):

(i) by a citizen of Bangladesh;

(ii) by a body corporate established under any Bangladesh law for the time being in force;

(iii) by a company registered in Bangladesh and carrying on business in Bangladesh;

(iv) by a company registered elsewhere than in Bangladesh but having its principal place of business in Bangladesh and having as its Chairman a citizen of Bangladesh;

(v) by a foreign company that has secured business or a contract in Bangladesh from the

Government that such business or contract is not, in the opinion of the Chairman, likely to be completed in less than six months;

(vi) by a foreign company that has secured business or a contract in Bangladesh from a

Bangladeshi Company and such business or contract is not, in the opinion of the Chairman, likely to be completed in less than six months.

(vii) Others if any (To be specified)

25. Insurance responsibility of the Bangladeshi AOC holder during operation of the aircraft:

Insurance Coverage Name of the party responsible

Maximum amount of liability

Hull and War risk (if any)

Passengers, mail, baggage, cargo etc.

Third Party liability

Any Other

Note: A copy of the Insurance Certificate is to be enclosed


APPENDIX-1 ANO A.2


26. Latest weighing report and Flight Test Schedule (must be within 90 days):

Last weighing report Last Flight Test Schedule

27. DECLARATION:

I do hereby declare that the above particulars are true in every respect, the mentioned recent data are applicable within the preceding period of not more than 30 (thirty) days from the date of this declaration and that nothing has been concealed or withheld by me. I also understand that in case any submitted data is found incorrect, then Technical Clearance, if issued by the Chairman, is liable to be withdrawn / cancelled by the Chairman. It is further stated that I am familiar with the current Civil Aviation Rules, 1984 and relevant Air Navigation Orders (Airworthiness Requirements) and shall abide by them.

Signature

Name:

Designation of the authorised Person:

Postal Address:

Telephone: Cell:

Fax: E-mail:

27. Countersigned by the CEO

Signature

Name of the CEO (Seal of the Company)

Telephone:

Cell:


APPENDIX-2 Form: CA-25

3 Issue: 3

ANO A.2


APPLICATION FOR ISSUE OF CERTIFICATE OF AIRWORTHINESS (C of A)

The application, when completed, should be forwarded to the Chairman, Civil Aviation Authority of Bangladesh (Attention: Deputy Director, AELD) and must be accompanied by the appropriate charges and documents.

1. Application for : (strike out items not applicable)

a) Certificate of Airworthiness b) Certificate of Airworthiness for ferry purpose

2. Name of the registered owner

3. a. Address (in full) of the registered owner

b. Telephone Number

a.

b. 4. a. Name and address of applicant

(if other than the owner) b. Telephone Number

a. b.

5. Registration Marks (Bangladesh or Foreign as applicable)

Current or allotted

Foreign (where known)

S2- 6. Description of Aircraft

(official nomenclature only) a. New or Used

b. Type/Designation/Series

c. Manufacturer of aircraft

d. Manufacturer’s Serial No. (MSN)

e. Date/Year of manufacture

f. Country of Manufacture

g. Engine-Make & Model

h. Number of engines fitted

i. Propeller-Make & Model

j. Seating accommodation (Including Crew)

k. Radio systems installed (Com, Nav &

Pulse)- Make & Model

a.

b.

c.

d.

e.

f.

g.

h.

i.

j.

k.

7. Design Standards and airworthiness requirements, according to which the aircraft type was certificated

Note: If required, a separate appendix may be attached

Page 1 of 4

APPENDIX-2 ANO A.2 Form: CA-25

Issue: 3

8. Maximum Certified Take-off Mass

9. Category and Sub-division required

Category : Sub-division :

10. Reference No. of Maintenance Schedule and AELD’s Approval No.

11. a. Reference No. of Type Certificate (TC) and Type Certificate Data Sheet (TCDS).

b. Current C of A, date of issue and the

Country of issue.

c. Export C of A, date of Issue and the Country of issue (To be enclosed)

a.

b.

c.

12. Is the aircraft undergoing –

a. Overhaul

b. Repair

c. Modification

a.

b.

c.

13. a. Total Airframe Time (TAT) of the aircraft

b Total Engine hours and cycle since

overhaul

c. Total propeller hours since overhaul (where applicable)

a. b. No. 1:

No. 2: No. 3: No. 4:

c. No. 1:

No. 2: No. 3: No. 4:

Page 2 of 4

Form: CA-25 Issue: 3

APPENDIX-2 ANO A.2

AIRCRAFT SYSTEMS, INSTALLATIONS AND EQUIPMENT

14. All items should be completed as appropriate and in cases where they are not

relevant, the words ‘Not Applicable’ should be entered. NO ITEM TO BE LEFT BLANK.

Aircraft Type:

Serial No.:

Registration Marks:

Owner:

SYSTEM, INSTALLATION AND EQUIPMENT

MANUFACTURER, TYPE AND QTY INSTALLED 1. AIRFRAME SYSTEMS

1.1 Pressurization system 1.2 Pneumatic system’s compressor 1.3 Hydraulic system’s pump 1.4 Portable fire extinguishers 1.5 Wheel assembly 1.6 Brake assembly

2. POWER PLANT 2.1 Auxiliary Power Unit 2.2 Fuel Control Unit 2.3 Propeller Control Unit (if applicable)

3. ELECTRICAL INSTALLATION 3.1 D. C. Generators

Nominal voltage and power rating 3.2 A.C. Generators

Nominal voltage and power rating Frequency control

3.3 Batteries NI-cad or lead acid Number/Nominal voltage/capacity

3.4 Emergency Lighting 3.5 Anti-Collision lights

4. INSTRUMENT SYSTEM 4.1 Stall detection & Warning 4.2 Fuel quantity Indicating

Total fuel quantity 4.3 Oxygen : Portable system

: Installed system 4.4 Inertial Navigation system 4.5 Flight Data Recorder

5. COMPASSES 5.1 D.R. Type 5.2 Remote type

Page 3 of 4

APPENDIX-2 ANO A.2 Form: CA-25

Issue: 3

SYSTEM, INSTALLATION AND EQUIPMENT

MANUFACTURER, TYPE AND QTY INSTALLED 6. AUTOMATIC-PILOTS

6.1 Radio Coupled/Non-Radio Coupled auto

pilot 6.2 Auto-Stabilizer 6.3 Flight Director

7. RADIO INSTALLATION

7.1 Communication System 7.2 Navigation System 7.3 Pulse & FM System 7.4 Cockpit Voice-Recorder 7.5 Ground Proximity Warning System

8. GENERAL

8.1 Safety harness: For Pilots’ seat

: For Passengers’ seat 8.2 Life Jackets 8.3 Life rafts

9. MISCELLANEOUS

10. PUBLICATIONS (FOR AELD. USE)

10.1 Flight-Manual or equivalent 10.2 Operation Manual 10.3 Maintenance Manual (aircraft) 10.4 Maintenance Manual (Engine) 10.5 Maintenance Manual (Propeller)

11. DECLARATION: I do here by declare that the particulars entered on this application are true and accurate in every respect.

Date: ………................ Signature of the Applicant ……………..……...….

Page 4 of 4

Form: CA-182C-1 Issue: 4

APPENDIX-3 ANO A.2


APPLICATION FOR AIRCRAFT TECHNICAL CLEARANCE

IN RESPECT OF WET LEASED AIRCRAFT TO BE OPERATED BY BANGLDESHI AOC HOLDERS

Note: All data shall be recent data i.e. must be current and shall NOT be older than 30 days from

the date of application

1. Aircraft

Type and Model: TAT: as on (date):

Manufacturer: TAC: as on (date):

MSN (Fuselage No.): MCTM:

*Date of Manufacture: Max. Passengers capacity:

*Age of the Aircraft: *Cycle of the Aircraft: *Note (1): Refer to the ANO (AW) B.21 Note (2): Evidence regarding the date of manufacture (e.g. if mentioned on the C of R, Aircraft Log book, Aircraft delivery document, any other official document etc.) to be enclosed.

2. Design standard of the aircraft:

*Design Standard TCDS No. issued by FAA or EASA Remarks (if any)

*Note (1): Refer to the ANO (AW) A.1 Note (2): A copy of the TCDS is to attached

3. Engine

Type and Model: No. of Engines: Manufacturer: Power Rating: Engine Position / Module name

Serial Number TSN / CSN as on (date)

TSO / CSO as on (date)

Note: In case of modular engines, the required information shall be attached on separate page.

Issue-4 05 April, 2011 Page 1 of 7

APPENDIX-3 ANO A.2 Form: CA-182C-1

Issue: 4

4. APU

Type and Model Aircraft Manufacturer

5. Propeller / Rotor

Propeller / Rotor Type and Model: Manufacturer: Propeller Position



6. Special performance certification

Special performance Tick below against the appropriate authorisation

Remarks (if any)

ACAS I / ACAS II EGPWS / GPWS IFR RVSM BRNAV RNP ETOPS ILS / AUTO LAND MNPS OTHERS (if any)

Note: (i) A copy of the current Air Operator Certificate (AOC) along with Operation Specification is to be enclosed in support of the Special Performance Authorisation.

7. Information regarding the current approved Maintenance Programme / Schedule

AMP based on MRB report number and Revision number issued on

AMP based on the manufacturer MPD number and Revision number issued on



Issue: 4

8. Information on Current Maintenance Check

Scheduled maintenance Check Check Interval (FH or/and Calendar Period as applicable)

Last performed on (date and TAT)

9. Operation and Maintenance history/status of the aircraft during last 12 months starting

from current month to backward (for the period to ).

Month and Year Hours Flown during the month

Type of Maint. Check accomplished

Date and TAT at which the Check accomplished

10. Information on past accidents (if any)

Date Aircraft TAT Brief details of damage and repair

Note: If required, the information is to be provided in separate page.



Issue: 4

11. Information on AOC and AMO:

Name of the AOC holder and AOC No. Name of the AMO for maintenance of the aircraft and Location of the AMO

E-mail address: E-mail address:

Note (1): A copy of the current Certificate of Approval of the AMO is to be attached.

12. Certificate of Registration

Current Regular C of R No. Issuing Authority

Note: A copy of the current valid certificate is to be attached.

13. Certificate of Airworthiness

Current Regular C of A No. Issuing Authority

Note: A copy of the current valid certificate is to be attached.

14. Noise Certificate:

Noise Certificate No. Issuing Authority

Note: A copy of the current valid certificate or equivalent document is to be attached.

15. Radio Station License

Radio Station License No. Issuing Authority

Note: A copy of the current valid certificate or equivalent document is to be attached.

16. AD Status of the aircraft/Engine/Propeller/Appliances up to (date):

AD No. and Rev. No.

Subject in brief Applicability status (Yes/No/Repetitive)

Initial Compliance (DT/TAT/TAC)

Next Due (DT/TAT/TAC)

Terminating action (MOD etc.) (DT/TAT/TAC)

Note: The required information is to be attached on similar or equivalent format



Issue: 4

17. Information on Classification of Operation (Rule 105 of the CARs 1984) in which the aircraft is to be engaged by the Bangladeshi Lessee during the lease period:

18. Proposed duration of lease period:

From (date) To (date) Total period (in months)

19. Information regarding the Lessor:

Name of the Lessor and business address Nationality Immediate contact address

Tel:

Cell:

E-mail:

20. Submission of 2 (two) copies draft agreement for procurement of the aircraft:

YES (Reference no. and date or Copies to be enclosed NO

21. Responsibilities of the Lessee and Lessor

Type of Responsibility Name, Designation and immediate contact address (Tel, Cell and E-mail) of the designated officials of the Lessor and Lessee responsible for the control

Maintenance Control Name:

Designation

Tell: Cell: Operational Control Name:

Designation

Tell: Cell: Commercial Control Name:

Designation

Tell: Cell: Others Name:

Designation

Tell: Cell:



Issue: 4

22. Insurance responsibility (Lessor or Lessee) during the lease operation:

Insurance Coverage Name of the party responsible

Maximum amount of liability

Hull and War risk (if any)

Passengers, mail, baggage, cargo etc.

Third party liability

Any Other

Note: A copy of the Insurance Certificate is to be attached

23. Information on signing of MOU (in case the lease period is more than 6 months):

(Confirmation through the Lessor that the CAA of the lessor carrier is willing to accept the leasing operation and sign an MOU with the CAAB as per the Article 83 bis of the Chicago Convention)

YES NO If required mention on a separate page

24. Information on official statement by the CAA of the Lessor (carrier) on Maintenance and Operations Surveillance Responsibility, in case the lease period is 6 months or less):

(Confirmation through the Lessor: (Confirmation through the Lessor that the CAA of the lessor carrier is willing to accept the leasing operation and will provide the Statement to the Chairman CAAB as required under the applicable ANO of the CAAB).

YES NO If required mention on a separate page



Issue: 4

25. Latest weighing report and Flight Test Schedule (must be within 90 days):

Last weighing report Last Flight Test Schedule

26. DECLARATION:

I do hereby declare that the above particulars are true in every respect, the mentioned recent data are applicable within the preceding period of not more than 30 (thirty) days from the date of this declaration and that nothing has been concealed or withheld by me. I also understand that in case any submitted data is found incorrect, then Technical Clearance, if issued by the Chairman, is liable to be withdrawn / cancelled by the Chairman. It is further stated that I am familiar with the current Civil Aviation Rules, 1984 and relevant Air Navigation Orders (Airworthiness Requirements) and shall abide by them.

Signature

Name: Designation of the authorised Person:

Postal Address:

Telephone:

Cell:

Fax:

E-mail:

27. Countersigned by the CEO

Signature

Name of the CEO: (Seal of the Company)

Telephone: Cell:



CIVIL AVIATION AUTHORITY OF BANGLADESH

Airworthiness & Engineering Licensing Division

APPENDIX-4 ANO A.2

APPLICATION FOR RENEWAL OF CERTIFICATE OF AIRWORTHINESS

This application must be filled in complete and put tick [√] where appropriate. The Certificate of Inspection (as per ANO A.2) and the renewal fees must be accompanied with the application.

1. AIRCRAFT TYPE ……………………………...…..2. REGISTRATION MARKS: S2-………......................

3. MAINTENANCE SCHEDULE REFERENCE: ……………………………………...………….......................

4. CERTIFICATE OF AIRWORTHINESS NO: …….…………….. 5. DATE OF EXPIRY: ……......................

6. CATEGORY OF OPERATION: ………………………………………..……………………...........................

7. MAX. CERTIFIED TAKE-OFF MASS OF THE AIRCRAFT………........………..……………………KGS

8. NAME AND ADDRESS OF THE REGISTERED OWNER: ………………………………............................

………………………………..…………………..…………………………………..………….........................

……………………………………………………..………………….…………………………........................

9. NAME AND ADDRESS OF THE APPLICANT:……………………………..……………….........................

…………………………………………………………...…….. TELEPHONE: …………...……....................

10. BANK DEPOSIT SLIP NO. : …………………………….…….........................................................................

..............................................DATE ……………………….…………..……......................................................

11. PLACE WHERE THE AIRCRAFT WILL BE AVAILABLE FOR INSPECTION: .........................................

………...............................................................…………………………..………….........................................

12. DATE FROM WHICH AIRCRAFT IS AVAILABLE : ………….…………………..……............................

13. a. UTILIZATION DURING THE LAST TWELVE (12) MONTHS ……………..……………………..….....

b. TAT (ON THE DATE OF APPLICATION)....................................................................................................

14. LIST OF THE DOCUMENTS READY FOR INSPECTION (MENTION DATE):

A. AIRCRAFT LOG BOOK [ ] B. AIRCRAFT MODIFICATION RECORD BOOK [ ] C. ENGINE LOG BOOK [ ] D. ENGINE MODIFICATION RECORD BOOK [ ] E. PROPELLER LOG BOOK [ ] F. PROPELLER MODIFICATION RECORD BOOK [ ] G. APU LOG BOOK [ ] H. ROTABLE COMPONENT HISTORY CARD [ ] I. FLIGHT MANUAL [ ] J. MINIMUM EQUIPMENT LIST [ ] K. AD CONTROL CARD [ ]

15. DECLARATION: I do hereby declare that the above particulars are true in every respect. The aircraft has

been maintained as per the CAAB approved Maintenance Schedule and no unapproved modifications have been embodied on the aircraft. Further, all Service Bulletins affecting safety have been incorporated. All applicable mandatory modifications / inspections and ADs have been incorporated and the aircraft is in airworthy condition.

Date …………………….…. Signature of the Applicant ………………….….………..……............................

Name and designation ………….…………………………...………………………………..............................

Page 1 of 4


APPENDIX-4 ANO A.2

FOR USE OF CAAB

1. NAME OF THE AELD OFFICIAL(S) ENTRUSTED WITH AIRWORTHINESS

SURVEILLANCE INSPECTION.

A. MR. ……………………………………………………………………………………….…........

B. MR ……………………………………………………………………………………………......

C. MR. …………………………………………………..……………………………………….......

D. MR. …………………………………………………………..……………………………….......

2. DOCUMENTS CHECKED BY ……………………………………………………...…………........

DATE ………………………………………………………………………………………….….......

3. FEE’S RECEIVED BY ……………………………………..…………………………………..........

ENTRY NO…………………………..……………..……..DATE …………...……………...............

Page 2 of 2

Form: AWS-16 Issue: 2

APPENDIX-5 ANO A.2


CERTIFICATE OF INSPECTION FOR RENEWAL OF

CERTIFICATE OF AIRWORTHINESS

1. Aircraft Type :

2. Aircraft Registration No. :

3. Aircraft Serial No. :

4. Aircraft Hours (a) TAT :

(b) TAC :

(c) Since last renewal : TAT TAC

5. Engine status as on the (Specify date)

Position Serial No. TSN TSO TBO (RS)

6. Propeller status as on (Specify date)

Position Serial No. TSN TSO TBO (RS)

7. Details of Scheduled Maintenance since last renewal of the certificate:

S/L Type of Check A/C Hrs./Calendar period

Place Date

8. Record of work: Major Repair and Modification carried out since last C of A renewal:

Brief description of Work / Major/ Repair / Modification

SB/Repair Order No. Accomplished on (Specify date)

9. List of all AD(s) and CAAB mandatory inspection complied with since last C of A renewal:

AD No. and Rev. No. Brief description Date Accomplished

Page 1 of 2

APPENDIX-6 ANO A.2


Issue: 2

10. List of all non-applicable AD(s) [with brief reason of non-applicability]:

ANO A.2

AD No. and Rev. No. Brief description Reason of non-applicability

11. List of all outstanding AD(s) [with brief reason]:

AD No. and Rev. No. Brief description Reason

12. List of all SB(s) incorporated since last C of A renewal:

SB No. and Rev. No. Brief description Date accomplished

13. Record of major component (AMP/AMS items) change since last C of A renewal:

Nomenclature AMS / AMP task /item no. Scheduled or Un-scheduled Remarks

14. Abnormal occurrence if any (Overweight Landing, Lightning Strike etc.):

Brief description Flight No. and date Place of occurrence

15. Flight Test: (a) Last done on: (b) Next due on:

16. Weighing: (a) Last done on: (b) Next due on:

17. Declaration:

I / We, hereby certify that the statements are based on official records maintained in the Engineering Department, are correct and have been verified.

Prepared by:

Authorised Signatory Maintenance/Engineering Records

Checked by: Authorised Signatory Inspection and QA/QC

Page 2 of 2

APPENDIX-6 ANO A.2



COMPLIANCE CHECK LIST - AIRCRAFT DOCUMENTATION

Notes: (1) The operator has to submit “Documents (records) of the aircraft” to establish the national regulation of the State (Lessor)/ (Seller) under which the maintenance and operation of the aircraft has been carried out. This should also include, where applicable, details of any deviations form, or exemption issued against, those regulations. (2) A standard method of presenting the records as mentioned below is encouraged, which should be compiled into a book, preferably a 3 rings binder, with an index in the front and divider pages suitably marked in between each section. This will help in shortening the review time of the records by the CAAB and in turn will be beneficial to the Operator. Instructions: The column no. 3 and 4 shall be filled by the Head of the Quality Control Department or an Authorsied official and shall be forwarded along with forwarding letter for approval lease agreement.

(1) Sl. No.

(2) Description

(3) Related section and page no. of the Lease agreement

(4) Signatur

e

SEC. 1 STATUS SUMMARY AND DATA CERTIFICATION - This section should begin with a statement of certification from the transferring operator or owner that the information presented is true and correct, including.

(a) Airworthiness certificate basis and status.

(i) TC & TCDS

(ii) Acceptance by the Chairman

(iii) STCs

(b) A general statement of the current status of non- repetitive ADs, such as: “All applicable airworthiness directives through (Issue number, date, etc.) have been incorporated as listed on the (specify name of operator) airworthiness directive summary as enclosed in the Section 11 of this Document Folder, (specify date) with the exception of those directives requiring initial or repetitive action.”

(c) A general statement of the current status of repetitive Ads, such as: “All airworthiness directives listed on the (specify operator) airworthiness directive control summary as enclosed in the Section 11 of this Document Folder, dated (specify date) require initial or repetitive action at the date, time or cycles listed.”


APPENDIX-6 ANO A.2


Sl. No.

Description Related section and page no. of the Lease agreement

Signature

(d) A statement of the extent of the operator’s direct operational and maintenance control of the aircraft and a list of major repairs accomplished during that time, such as: “This aircraft has been under the direct operational and maintenance control of (specify operator) since (specify date). During this time the aircraft underwent the following major repairs in accordance with approved technical data documented in the aircraft records. (List all major repairs).”

(e) A statement of the extent of the operator’s direct operational and maintenance control of the aircraft and a list of SBs and Modifications accomplished during that time, such as: “This aircraft has been under the direct operational and maintenance control of (specify operator) since (specify date). During this time the aircraft underwent incorporation of the following SBs and Modifications in accordance with approved technical data documented in the aircraft records. (List all SBs and Modifications).”

(f) A statement regarding the accomplishment of the last major inspection, such as: ‘‘The last (specify type of major inspection) was accomplished by (specify operator/maintenance Organisation) between (specify date) and (specify date) at (specify operator/maintenance organization) maintenance facility in (specify city, State). Airframe total hours and total cycles were _ .”

(g) A statement regarding the current status of the installed engines and any spare engines, such as: ‘‘The following engines are currently installed on the aircraft with the total accumulated and remaining hours and cycles listed for each (list engines.) The (specify operator) life-limited parts report has been prepared using the (list manufacturer’s controlling document), and reflect accurate times and cycles of the life-limited parts as of the engine time/cycles noted above.’’

(h) A statement regarding the current component status, such as: ‘‘The components/inspection times listed on the (specify operator) component control summary represent the latest component installation information as of (specify date).’’

Note: Section 1 should be signed by the senior airline official responsible for aircraft maintenance record- keeping.


APPENDIX-6 ANO A.2


Sl. No.

Description Related section and page no. of the Lease agreement

Signature

SEC.2 AIRCRAFT LEASE/SALE AGREEMENT - This section should contain a copy of the lease or sale agreement or Bill of Sale attested by a Notary Public. Economic or monetary information may be deleted for the purposes of this presentation.

SEC.3 OPERATING AUTHORITY - This page should contain a copy of the operating authority (AOC) issued by the responsible regulatory authority of the last operator. This is used to establish the rules under which the aero plane was operated and maintained.

SEC.4 EXPORT C of A / C of A - This section should contain a copy of the export certificate of airworthiness (if any)

SEC.5 LAST WEIGHT & BALANCE REPORT A copy of the Weight and Balance report shall be enclosed.

SEC.6 NOISE CERTIFICATE A copy of the Noise Certificate shall be enclosed.

SEC.7 RADIO STATION LICENSE A copy of the Radio Station License shall be enclosed.

SEC.8 CURRENT INSP. STATUS SUMMARY - This page should give a summary of the current inspection status of the aircraft at the time of transfer. It should list:

(a) the aircraft total time; (b) the aircraft total cycles or landings; (c) the time and landings since the last major scheduled

maintenance or inspection; (d) the scheduled major inspection intervals and the time

remaining to the next inspection; and (e) The power plants by position and serial number.

Note: The listing should show the time since new, cycles since new and the time and/or cycles remaining to the next life-limited part removal for each power plant.

SEC.9 SUMMARY OF CURRENT STATUS OF LIFE- LIMITED (Retirement Life) PARTS – A listing of all the airframe and power plant life-limited (retirement life) parts and components installed on the aircraft at the time of transfer containing following information shall be enclosed: (a) the name of the component/part; (b) the component/part number; (c) the installed location or position of the component/part; (d) the component/part serial number; (e) the required retirement time of the component/part; (f) the total number of hours or accumulated cycles; and (h) The number of hours or cycles remaining before the required retirement time of the component/part is reached. Note: In Case of change of ownership of the aircraft, the authorsied release certificates of the installed parts and components are to be enclosed with the respective Control Cards.


APPENDIX-6 ANO A.2


Sl. No. Description Related section

and page no. of the Lease agreement

Signature

SEC.10 SUMMARY OF CURRENT STATUS OF ROTABLE COMPONENTS (Components and Parts having Restoration or Overhaul life) - This section should contain a listing of all the Components and Parts having Restoration (RS) or Overhaul (OH) life installed on the aircraft at the time of transfer. The listing should contain: (a) The name of the component/part; (b) The component/part number; (c) The installed location or position of the

component/part; (d) The component/part serial number; (e) The required RS or OH time of the

component/part; (f) The total number of hours or accumulated cycle

or Calendar Period; and (h) The number of hours or cycles or calendar

period remaining before the required RS or OH of the component/part is reached.

Note: In Case of change of ownership of the aircraft, the authorsied release certificates of the installed parts and components are to be enclosed with the respective Control Cards.

SEC.11 CURRENT STATUS OF ADs - This section should contain a listing of each AD applicable to the aero plane, power plants, components and appliances. Recurring ADs should be listed separately. The listing should contain:

(a) The AD number and revision date;

(b) A concise description of the required action;

(c) The method of compliance;

(d) The time in service and the date of AD accomplishment; and

(e) For ADs having requirements for recurring

actions the date of AD accomplishment and when the next recurring action is due (date, hours, cycles, etc.).


APPENDIX-6 ANO A.2


Sl. No. Description Related section and page no. of the Lease agreement

Signature

SEC.12 AIRCRAFT MAINTENANCE PROGRAMME INTEGRATION - If the maintenance/inspection programme is to be changed for the aircraft, the integration or prorating plan for the two programmes should be presented here. For an integration plan, a listing of each scheduled maintenance/inspection item under both the old and new programme should be shown along with the method of transfer or bridging from one to the other.

SEC.13 CERTIFICATE FOR FITNESS TO FLIGHT: Certification that the aircraft is fit to fly as far as can be reasonably determined from inspections of the aircraft and its records and manuals and that all applicable Airworthiness Directives and mandatory modifications and inspections of the State of Design and the Chairman have been carried out or certified to have been carried out. Reference: Paragraph 5.7 of the ANO (AW) A.2

SEC.14 FLIGHT TEST REPORT – A copy of the aircraft performance Flight Test report, including aircraft Radio systems is to be enclosed.

SEC.15 Others

Signature:

Name:

Designation:

Head of Quality Control of the Operator.



AIR NAVIGATION ORDERS


PART A - AIRWORTHINESS CERTIFICATION

CHAPTER A.3 EXPORT CERTIFICATE OF AIRWORTHINESS

Section No. Title 1. GENERAL 2. DEFINITION 3. ELIGIBILITY 4. APPLICATION

APPENDIX-1 FORM AWS-15

1. GENERAL

1.1 This Order prescribes conditions for the issue of Export Certificate of Airworthiness for aircraft, aircraft engines and propellers being exported from Bangladesh.

2. DEFINITION

2.1 For the purpose of this Order, the definitions as mentioned under the Rules 2, 183 and 234 of the Civil Aviation Rules, 1984 shall apply. Where a particular definition is not given under the Rule, the under mentioned definition shall apply:

(a) "Export Certificate of Airworthiness of aircraft" means a document issued

by the Civil Aviation Authority, Bangladesh in respect of a complete aircraft including engine(s) and propeller(s) as applicable for the aircraft, being exported from Bangladesh, which attests that the aircraft, with exceptions (if any stated on the certificate), meets on the date of issue of the Certificate, the airworthiness and design standards established by the CAAB, but which is neither a Certificate of Airworthiness nor an authorisation for flight.

3. ELIGIBILITY

3.1 An Export Certificate of Airworthiness shall be issued only in respect of a product of

the following types when such a product is to be exported from Bangladesh:

(a) A complete aircraft, including engine(s) and propeller(s);

Issue - 3 17 September 2009

Page 2

ANO A.3

(b) A single complete engine; and

(c) A single complete propeller. 3.2 An Export Certificate of Airworthiness shall not be issued unless the Chairman is

satisfied that at the time of issue, with any stated exceptions, the aircraft, engine, or propeller:

(a) Conforms to the Certificate of Type Approval or Type Certificate for the

product as accepted by the CAAB under the ANO (AW) A.1;

(b) Complies with all pertinent Civil Aviation Rules, Air Navigation Orders and Airworthiness Directives;

(c) Complies with additional requirements as specified by the importing State (if

notified to the CAAB); and

(d) Is airworthy and in a condition for safe operation. 3.3 In respect of a complete aircraft, to be eligible for issue of an Export Certificate of

Airworthiness, the aircraft shall:

(a) Have in force a valid Bangladesh Certificate of Airworthiness, or satisfy the requirements for issue of a Bangladesh Certificate of Airworthiness.

(b) Have been submitted for survey to an approved maintenance organisation in

accordance with the ANO (AW) A.2 of these Orders within the preceding 30 (thirty) days, except that if the aircraft has been maintained in accordance with an approved continuous airworthiness programme, the Chairman may waive the inspection and survey requirements following assessment of the aircraft maintenance records.

4. APPLICATION

4.1 An application for issue of an Export Certificate of Airworthiness shall be made on

the Form AWS – 15 (refer Appendix 1 of this Order) at least 30 (thirty) days before the required date.

4.2 The applicant shall provide the following documents, as applicable, to the purchaser

of each product for which an Export Certificate of Airworthiness is issued:

(a) The aircraft must have been maintained under CAAB approved Continuing Airworthiness Maintenance Programme (CAMP) or should have undergone an annual type inspection and be approved for return to service. The annual type inspection should have been performed and properly documented within 30 (thirty) days before the application is made for an Export Certificate of Airworthiness;

Issue - 3 17 September 2009



Airworthiness & Engineering Licensing Division

APPENDIX-1 ANO A.3

APPLICATION FOR ISSUE OF EXPORT CERTIFICATE OF AIRWORTHINESS

1. Instructions: a. This application is to be submitted to the AELD (one copy) when the product(s) to be exported is (are)

presented for inspection. b. Application is made for an Export Certificate of Airworthiness to cover the aircraft described below,

which is a used aircraft. c. For complete aircraft, execute items 2 through 11 as applicable. 2. Name and address of exporter 3. Name and address of foreign purchaser 4. Country of destination

5. Description of the product (if necessary mention on the reverse side)

Type

Make and model

FSN / MSN

Serial numbers

TCDS No. Operating time (hours)

Time Since New (TSN)

Cycles Since New (CSN)

a) Aircraft

b) Engine(s)

c) Propeller(s)

6. The aircraft was given a satisfactory flight test on (date):

7. Does the product comply with all applicable CAAB regulations, Airworthiness Directives and other requirements of AELD? Yes No (explain in “Remarks”)

8. Have applicable special requirements of the importing country been complied with? Yes No (explain in “Remarks”)

9. Has proper preventive treatments been applied to products susceptible to rapid corrosion? Yes No (explain in “Remarks”)

10Remarks:

11Special requirements (if any) of the importing country. Note: Additional pages may be enclosed

12Exporter’s certification:

I do hereby certify that the above statements are true and that the product(s) described here is (are) airworthy and in condition for safe operation except as may be noted under item 10 “Remarks”, above.

Date: Signature of the authorized person, name & designation

Issue – 3 Page 1 of 1 17 September 2009




CHAPTER A.4 CLASSIFICATION OF AIRCRAFT AND AIRCRAFT OPERATION

Sections Title

1 GENERAL

2 CATEGORIES OF AIRCRAFT

3 CLASSIFICATION OF AIRCRAFT OPERATION

1. GENERAL

1.1 This Order prescribes the categories of aircraft which maybe entered on Bangladesh Certificate of Airworthiness, and the type of operation for which each category qualifies.

2. CATEGORIES OF AIRCRAFT

2.1 Every aircraft in respect of which a Certificate of Airworthiness is in force will be

classified on that Certificate for operation in one of the following categories.

(a) Private.

(b) Aerial work.

(c) Charter.

(d) Scheduled public transport.

3. CLASSIFICATION OF AIRCRAFT OPERATION

3.1 Unless otherwise stated on Its Certificate of Airworthiness, aircraft classified in the following categories may be obliged respectively for:

(a) Private category - operations prescribed In Rule 105(1) of the Civil Aviation Rules

1984, where the aircraft is flown other than for hire or reward.

( b) Aer ia l work categor y - oper at io ns pr escr ibed in Rule 105(2) o f t he CAR 1984, but excluding carr iage o f cargo or passenger s I n charter or public transport operatio ns.

Issue 2 Page-1 01 August, 1990

ANO A.4

( c) Charter categor y - oper at io ns prescr ibed in Rule 105( 3) o f t he CAR.

( d) 1984, and fo r any ot her pur pose aut hor ised by t he Chair man.

( e) S cheduled public t ransport categor y - oper at io ns pr escr ibed in Ru le 105(4) o f t he CAR 1984 and for any ot her pur pose aut hor ised by t he Chair man.

I ssued in pur suance o f t he Civil Aviat io n Rules 1984, Rule 4, Rule 105, Rule 106 and Rule 107.

(Sd/-) Air Cdre (Retd) Moinul Islam

Chairman Civil Aviation Authority of Bangladesh

Issue-2 Page-2 01 August, 1990


AIRWORTH INESS REQUIREMENTS


CHAPTER A.5 REGISTRATION OF AIRCRAFT

Sections Title

1 GENERAL

2 REGISTRATION PROCEDURE

3 REGISTRATION OUTSIDE OF BANGLADESH

4 AIRCRAFT IMPORTED OTHER THAN BY AIR

5 CHANGE OF OWNERSHIP

6 DEREGISTRATION OF AIRCRAFT

1. GENERAL

1.1 This Order prescribes the requirements and procedures for registration, deregistration and

change of ownership of aircraft.

(a) Proof of foreign registration cancellation. (b) Bill of sale or conditional sales contract. (c) Insurance Certificate. (d) Import permit. (e) A Bangladesh customs clearance certificate. (f) Any other documentation as may be required by the Chairman.

2. REGISTFITION PROCEDURE

2.1 Application for aircraft registration shall be made on Form CA -27C not later than 30 days

before the desired date of registration.

2.2 The application shall be submitted to the CAAB along with a receipt for the appropriate fee, and with a copy of each of the following documents, as applicable

2.3 The requirements of insurance certificate for aircraft owned and operated by the

Bangladesh Government, shall be as per the current policy of the Ministry of Finance.

Issue 2 Page-1 01 August, 1990

ANO A.5

2.4 When all requirements have been satisfied, the Chairman may issue a Certificate of Registration to the owner and, except as provided in the CAR 1984, Rule 120, that Certificate shall be carded in the aircraft at all times.

3. REGISTRATION OUTSIDE BANGLADESN

3.1 An aircraft being imported into Bangladesh by air shall only be flown into the country

provided the aircraft is:

(a) On the register of, and with a Certificate of Airworthiness of, another country.

(b) On the Bangladesh register and with a Bangladesh Certificate of airworthiness.

3.2 Where an imported aircraft is flown to Bangladesh on the civil register of another

country, on the regulations of that country concerning the Certificate of Airworthiness, maintenance and flight crew licensing shall apply, and in such cases the Bangladesh Certificate of Registration will be processed and issued in accordance with the procedures prescribed in section2 of this Order upon arrival of the aircraft in Bangladesh.

3.3 Application for the issue of a Certificate of Registration for an aircraft outside

Bangladesh shall be made on Form C.A.-27C and submitted with a receipt for the appropriate fee not later than 30 days prior to the desired date of Issue.

3.4 If acceptable, a temporary Certificate of Registration endorsed with the restriction "Issued

for ferry flight and valid only until the first landing at a Customs Airport in Bangladesh" will be provided by the CAAB.

3.5 In accordance with the CAR 1984, Rule 213, airworthiness representatives of CAAB

shall be present in the country from where the aircraft is to be exported to issue the Certificate of Registration.

3.6 A permanent Certificate of Registration will be issued by the Chairman when he is

satisfied that all conditions affecting the registration of the aircraft have been compiled with, and when a customs clearance has been obtained.

4. AIRCRAFT IMPORTED OTHER THAN BY AIR

4.1 For aircraft imported by means other than air, issue of a Certificate of Registration will be

effected in Bangladesh in accordance with normal procedures specified in section 2 of this Order.

5. CHANGE OF OWNERSHIP

5.1 Where there is a change of ownership of an aircraft registered in Bangladesh, through

sale or otherwise, the registered owner of the aircraft shall immediately provide written notice of the change and surrender the Certificate of Registration to Chairman after completing the relevant portion on the back of the Certificate,


ANO A.5

5.2 The new owner shall submit a new application aircraft on Form C.A. -27C and the following:

(a) An affidavit from the previous owner which has been auth6.1tIcated by a notary,

together with a statement that the aircraft has been sold or transferred to a new owner.

(b) The existing Certificate of Registration, discharged in favor of the new owner by

completing the relevant portion, if not already provided by the registered owner.

(c) A receipt for the appropriate fee.

6. DEREGISTRATION OF AIRCRAFT

6.1 When the aircraft has been destroyed or permanently withdrawn from service, the registered owner of the aircraft shall, within 15 days, request the Chairman in writing and return the Certificate of Registration after completing the relevant portion of the Certificate.

6.2 An aircraft for which a Certificate of Airworthiness has not been renewed for two

successive years shall be removed from the Bangladesh register of civil aircraft.

6.3 Reinstatement to the register may be effected when the owner or operator applies for renewal of the Certificate of Airworthiness, complies with any requirements specified by the Chairman for renewal of the Certificate, and when the aircraft has been inspected in accordance with Chapter A.2 of these Orders and found to be satisfactory.

Issued in pursuance of the Civil Aviation Rules 1984, Rules 4, 120, 171 and 174.







CHAPTER A.6 FLIGHT MANUALS

Sections Title

1 GENERAL

2 DEFINITION

3 REQUIREMENT

4 APPROVAL OF FLIGHT MANUALS

5 CONTENTS OF FLIGHT MANUALS

6 AMENDMENT OF FLIGHT MANUALS

1. GENERAL

1.1 This Order prescribes the requirements for the carriage, approval, amendment and contents

of aircraft flight manuals.

2. DEFINITION

2.1 For the purpose of this Order, "flight manual" is defined as a manual approved by the Chairman which Is associated with the Certificate of Airworthiness for an aircraft, and which provides aircraft limitations, and information and procedures as required by ICAO Annex 8 for the safe operation of the aircraft by the flight crew.

2. REQUIREMENT

3.1 No Bangladesh aircraft shall be flown unless:

(a) There is an approved flight manual or equivalent carried on board,

(b) The pilot-in-command complies with all operation requirements, procedures and

limitations set out in the flight manual for that aircraft.

4. APPROVAL OF FLIGHT MANUALS

Issue 2 Page-1 01 August 1990

ANO A.6

4.1 The Chairman may approve a flight manual, and any subsequent amendments to that manual, which has been:

(a) Previously approved by the civil aviation authority of the country of origin.

(b) Prepared by or on behalf of the manufacturer, owner or operator of the aircraft, in

accordance with the prescribed standards.

4.2 For an imported aircraft, evidence that the data contain in the flight manual has been approved by the civil aviation authority of a contracting state shall be provided.

4.3 Where performance data for an aircraft is not available, the Chairman may require flight

tests.

4.4 Approval of a flight manual shall be indicated on the document by the signature of an authorised representative of the CAAB, or by a Certificate of Validation issued by an authorised representative of the CAAB.

4.5 The flight manual may be incorporated into the same document as the Certificate of

Airworthiness.

5. CONTENTS OF FLIGHT MANUAL

5.1 A Flight Manual shall contain all the related data specified by airworthiness requirements and such other data as may be specified by the Chairman.

5.2 Except where not applicable to a particular aircraft, a Flight Manual shall contain at least

the following information:

(a) General - Engine - Manufacturer, type and number - Propeller - Manufacturer, type, diameter, pitch settings - Fuel - Grade, capacity, total, usable - Oil - Specification, capacity

(b) Operating limitations: - Operational restriction relating to IFR and night

- Operation and flight in icing conditions - Airspeed - limitations - Maneuvers - permitted - Weight and centre of gravity limitations - Flight load factors - Power plant limitations - Total occupants/minimum crew - Smoking restrictions - An explanation of instrument markings and - Placards.


ANO A.6

(c) Emergency procedures

(d) Normal procedures - Fuel system :management - Stalls - Spinning

(e) Performance: - Information necessary to meet CAAB aircraft - Performance requirements - Stalling speeds - Maximum demonstrated cross wind component.

5.3 The Chairman may require supplements to be added to the flight manual of a particular

aircraft to amend the data contained therein when a modification is incorporated.

5.4 Except as provided in paragraph 5.5 of this Order, all flight data shall be given in the following units:

Weight - Kilograms and Pounds Temperature - Degrees Celsius Short distance - Meters and Feet Long distance - International Nautical Miles Height - Feet Pressure - Kilopascals and Pounds per Square Inch Liquid Quantity - Litters and Imperial Gallons or Pints Speed - Knots

5.5 Where a flight manual adopted in accordance with paragraph 4.1 of this Order does not provide data in the above units, conversion tables shall be incorporated.

6. AMENDMENT OF FLIGNT MANUALS

6.1 An amendment shall not be incorporated into the flight manual unless it has been approved by the Chairman.

6.2 Upon obtaining approval for an amendment, the Owner/Operator of the aircraft shall

ensure that it is incorporated In accordance with the Instructions provided unless otherwise directed by the Chairman.

6. 3 Approved amendments shall be incorporated wit hin the per iod stated by the

Chair man, or in the absence of, such a statement, prior to the next flight.


ANO A.6

NOTE: The amendment process in Bangladesh nor mally fo llowing approval o f the amendment by the regulatory author it y o f the countr y o f origin o f the aircraft , which or iginally appro ved t he flight ma nual.

I ssued in pur suance o f t he Civil Aviat io n Rules 1984, Rule 4 and Rule119.







CHAPTER A.7 MEDIFICATON AND REPAIR DESIGN DATA APPROVAL

Sections Title 1 GENERAL 2 DEFINITION 3 APROVEDD TECHNICAL DATA 4 APPLICATION FOR APPROVAL OF MODIFICATION AND REPAIR 5 ISSUE OF APPROVAL 6 RETENTION OF SUBSTANSIATING 7 RESPONSIBILITY OF THE MODIFICATION AND REPAIR

APPROVAL HOLDER Appendix-1 CRITERIA FOR THE CLASSIFICATION OF MAJOR

REPAIRSERTIFICATE Appendix-2 CRITERIA FOR THE CLASSIFICATION OF MAJOR AND MINOR

MODIFICATIOS AND REPAIRS

1. GENERAL

1.1 This Order specifies the approved technical data, which is required for the embodiment of any modification and Repair on an aircraft Registered in Bangladesh.

1.2 Typical modifications and repairs are listed in the Appendix-1 of this orders as guidance to

assist in determining whether a Particular modification of repair is "major" or "minor" incase a proposed modification on repair is not listed in tire Appendix-1, then the guidance presented in the Apendix-2 of this order should be used as criteria for the classification of major and minor modifications and repairs.

2. DEFINITIONS

2.1 For the purpose of this 0rder, (the definitions as mentioned under the Rules 2 and 183 of

the Civil Aviation Rules, 1984 shall apply, where a particular definition under the rule. under mentioned definitions shall apply.

(a) "Modification" of an aeronautical product Means, a subordinate Change to the original

type design which is not a repair. In this ANO modification and alteration are intended to be synonymous. Modification is further classified into:

Issue 2 Page-1 28 February, 2002

ANO A.7

(1) Major: A major modification means a type design change not listed ill the aircraft, engine propeller specifications.

(i) That might appreciably affect the mass and balance limits, Structural

strength, performance, power plant operation. Flight characteristics other qualities affecting airworthiness or environmental characteristics: or

(ii) that will be embodied in the product according to nonstandard practices.

(2) Minor: A minor modification means a modification other than a major

modification.

(b) "Repair" means a design change intended to restore an aeronautical product to an airworthy condition after it has been damaged or subjected to wear. Repair is further classified into:

(1) Major: A major repair means a design change, which is intended to

restore an aeronautical product to an airworthy condition:

(i) where the damage being repaired might appreciably affect the structural strength performance, power plant operation, flight characteristics, or other qualities affecting airworthiness or environmental characteristics: or

(ii) that will be embodied in the product using nonstandard practices.

(2) Minor: A minor repair means a repair other than a major repair.

(c) "Design approval representative" means a representative of an aeronautical product manufacturer or the engineering department of an approved airline operator who has been delegated authority by the Chairman to approve the drawings and technical data required to substantiate the airworthiness of a design, modification or repair of an aeronautical product.

Note: A Design Approval Representative (DAR) will normally be a professional

aeronautical engineer who, by reason of training, knowledge and experience in aeronautics, is capable of exercising professional responsibility in relation to his delegated authority.

(d) "Aircraft Maintenance Engineer (AME)" means a person who is the holder of a

valid license Issued under the Civil Aviation Rules, 1984, which delegates authority to that person to exercise certain privileges with respect to the maintenance and certification of aircraft, as set out in Part D entitled "Licensing- Aircraft Maintenance Engineer's" of these Orders.

(e) "Compliance Program" means the document that lists each discrete standard,

which must be satisfied, the method used in determining compliance (e.g. test,

Issue -2 Page-2 28 February, 2002

ANO A.7

analysis, and inspection) and the signature of a qualified person confirming findings of compliance.

(f) "Component" means a major assembly of a complete aircraft, engine, or

propeller, and includes, for example, wings, empennage, landing gear, power transmissions, control surfaces, generators, pumps, actuators and avionics products.

(g) "Part" means a sub assembly of an aircraft component including pulleys, gears,

blades, carburetor floats and bell cranks, and standard items including fasteners, rivets, nuts, bolts, rigging cable and electrical wire.

(h) "Material" means a raw product, which has undergone a quality program to

ensure that it conforms to aeronautical standards, and is traceable to the source of supply.

2. APPROVED TECHNICAL DATA

3.1 Approved technical data for a modification or repair shall comprise all drawings,

instructions or other data necessary for embodiment.

3.2 Subject to conformity with the applicability, limitations and conditions prescribed therein, the following technical data are acceptable for the modification or repair of aircraft or components.

(a) Data contained in an approved (regulatory authority) repair manual, overhaul

manual, or/and equivalent provided by:

(1) an aircraft, engine, or propeller manufacturers.

(2) an aircraft component manufacturer, if the manufacturer of the aircraft, engine, or propeller of which the component forms part specifies the document for use; that is, by listing in the prime manufacturer's component maintenance manual.

Note: The use of radio manufacturer's installation manuals is not normally specified by

the aircraft manufacturer, and is therefore not normally approved under this subparagraph; however, such data may be submitted as descriptive data for an application for approval made under section 4 of this Order.

(b) Structural repair methods contained in the FAA AC 43.13-1 A "Acceptable

Methods, Techniques and Practices-Aircraft Inspection and Repair" or the U.K. CAP 562" Civil Aircraft Airworthiness Information and Procedures", provided that any limitations on the use of these data specified by the aircraft or component manufacturer are observed.


ANO A.7

Note: This approval does not extend to the FAA AC 43.13-2A; however, AC 43.13- 2A may be used in support of an application for approval of a design change under Section 4 of this Order.

(c) Instructions contained in manufacturer's service bulletins, including component

manufacturer's service bulletins, provided the .maintenance manual for the component is specified for use by the prime manufacturer.

(d) Airworthiness Directives or equivalent, issued by the Civil Aviation Authority

of the country of origin of the aircraft, engine, or propeller, where these give specific instructions for modification or repair.

(e) Where provided for in an approved company General Engineering Manual,

drawings and methods issued and approved by a Design Approval Representative (DAR). However, copies of all such drawings, calculations, tests, and reports shall be subsequently submitted to the Chairman for confirmation, together with a certificate containing the approval number and signature of the DAR.

(f) Type Certificate Data Sheets and Supplemental Type Certificate STC) data as

applicable to the item for Modification or Repair.

(g) Airworthiness Directives (AD)

3.3 Prior approval is required for any amendments to Aircraft Maintenance Manuals (AMM), Aircraft Maintenance Schedules (AMS), Aeroplane Flight Manuals (AFM) or other approved documents resulting from modifications or repairs embodied in accordance with these data.

3.4 Data provided by a component manufacturer are not approved to the extent that they

conflict with data provided by the aircraft or component assembly manufacturer of which the component is to form a part.

3.5 The Chairman may require the owner of an aircraft repaired or modified in accordance

with data approved under this section to provide Type Certification Data to ensure compliance with Chapter A.2 of these Orders.

4. APPLICATION FOR APPROVAL OF MODIFICATION AND REPAIR

4.1 The CAAB may accept application for approval of Major Modification and Major Repair

provided the proposed modification and/or repair is based on approved technical data as mentioned in the section 3 of this Order.

4.2 Any Major Modification or Major Repair that is not based on approved technical data

shall require substantiation or recommendation from the Type Certificate (TC) holder of the aeronautical product.


ANO A.7

4.3 Minor modification and minor repair not based on above mentioned (section 3 of this Order) approved technical data might be considered for approval by the CAAB.

4.4 Application for approval of a Modification shall be made on the form CA-186 and

application for approval of Repair be submitted on Company letterhead.

4.5 An application for approval of Modification shall be accompanied by two sets of all drawings and other applicable descriptive data, including approved technical data, as mentioned below:

(a) a master document list detailing the individual drawings (B.S.S. 308 or

equivalent) and specifications, which define the design change;

(b) Drawings instructions necessary for the installation of the design change in the product;

(c) Compliance program;

(d) Engineering program which contain the analysis, calculations and the test results

used to make the determination that the modified product complies with the approval basis;

(e) a record of change in the mass and moment arm when the design change is

installed in the aeronautical product;

(f) a record of change in the electrical load when the design change is installed in an aircraft;

(g) a supplement to the following documents/manuals as may be appropriate in each

case:

(1) Flight manual; (2) Aircraft maintenance manual; (3) Component maintenance manual; (4) Structural repair manual; and (5) Instructions for continuing airworthiness.

4.6 An application for approval of Repair shall be accompanied by two sets of all drawings and

other applicable descriptive data, including approved technical data, as mentioned below:

(a) Compliance program;

(b) Master drawing or drawing list, production drawings, (B.S.S. 308 or equivalent) installation instructions;

(c) Engineering reports (static strength, fatigue, damage tolerance, fault analysis, etc.);

(d) Flight test program and results;

(e) Mass and Moment change data;


ANO A.7

(f) A supplement to the following documents/manuals as may be appropriate in each case:

(1) flight manual;

(2) Aircraft maintenance manual;

(3) Component maintenance manual;

(4) Structural repair manual; and

(5) Instructions for continuing airworthiness.

5. ISSUE OF APPROVAL

5.1 The Chairman may approve the modification or authorize approval when:

(a) the applicant satisfies the Authority that the aeronautical product, with the design change installed complies:

(1) the approval basis:

(2) the requirements of the Authority for the provision of engineering data and documentation; and

(b) in the opinion of the Authority the design has no unsafe features.

5.2 The Chairman may approve the repair or authority/approval when:

(a) the applicant satisfies the Authority that the aeronautical product, with the

proposed repair scheme complies with:

(1) the approval basis:

(2) the requirements of the Authority for the provision of engineering data and documentation;

(3) the restoration of the type design characteristics; and

(b) In the opinion of the Authority the repair has no unsafe feature.

5.3 In approving the modification or repair, the Chairman may prescribe such limitations

and conditions, as he considers necessary in the interests of safety.

6. RETENTION OF SUBSTANTIATING DATA

6.1 To show that the modified or repaired aeronautical product complies with the appropriate design standards reports on analyses and tests should be prepared. The CAAB requires that the holder of the approval shall:


ANO A.7

(a) retain the records of the analyses and tests performed to demonstrate compliance until the aircraft modified or repaired in conformity with the approved modification or repair are permanently withdrawn from service;

(b) make the records available to it upon request; and

(c) ensure that no person destroys or otherwise disposes of any record referred to

above without its prior permission.

7. RESPONSIBILITY OF THE MODIFICATION AND REPAIR APPROVAL HOLDERS

7.1 The person or organization responsible for design of the modification or repair shall:

(a) furnish at least one set of any amendment or supplement to a flight manual,

maintenance manual or instruction for continuing airworthiness produced in obtaining approval of the design to each intended user and make available to any user subsequent changes to such documents;

(b) if service experience shows a safety deficiency in the modification or repair:

(1) advise the airworthiness authority of the deficiency immediately:

(2) prepare appropriate design changes and make them available to the authority for mandatory continuing airworthiness action; and

(3) make available the descriptive data concerning the changes to all operators

of products affected by the mandatory action. Descriptive data concerning changes to a modification or repair would normally is published in the form of a service bulletin. The approval holder's responsibility includes the need to advise operators of any vendor bulletins for equipment included in a modification.

This Order is issued in pursuance of the Rules 4, 184, 193 and 196 of the Civil Aviation Rules 1984. The ANO is a complete re-issue and supersedes the Issue 1, dated August 1, 1990.

Air Cdre Lutfur Rahman ndu, psc



APPENDIX-1 ANO A.7

TYPICAL MAJOR MODIFICATIONS AND MAJOR REPAIRS

1. Major Modifications

1.1 Typical major modifications are listed below:

a) Airframe major modifications

Modification of the following parts/types, when not listed in the aircraft specifications, arc generally classified as airframe major alterations:

(1) Wings;

(2) Empennage

(3) Fuselage:

(4) Engine pylons;

(5) Flight control system;

(6) Landing gear;

(7) Hull or floats;

(8) (9)

Elements of an airframe including spars, ribs, fittings,

absorbers, bracing, cowling, fairing and balance mass;

Rotor blades;

shock

(10) Changes to the empty mass or empty- balance which result in an increase in the maximum certificates mass or center of gravity limits of the aircraft: changes to the basic design of the: -fire protection system -avionics flight control system -electrical power system - environmental control system - fuel system -pneumatic system -water and waste system -oxygen system - ice and rain protection system

(11) Auxiliary power unit;

(12) Changes to the wing or to fixed or movable control surfaces, which

affect flutter and vibration characteristics.

(b) Propulsion system major modifications

The following alterations of a power plant, when not listed in the engine specifications, are power plant major alterations:

Issue-2 Page-1 28 February, 2002

APPENDIX-1 ANO A.7

(1) conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios, number of working stages, number of rotating airfoils, stators or the substitution of major engine parts which require extensive rework and testing of the engine;

(2) changes to the engine by replacing aircraft engine structural parts

with parts not supplied by the original manufacturer or parts not specifically approved by the CAA:

(3) installation of an accessory, which is not approved for the engine:

(4) removal of accessories that are listed as required equipment on the aircraft or engine specification;

(5) installation of structural parts other than the type of parts approved

for the installation: and

(6) conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specification.

(c) Propeller major modification

The following alterations of a propeller when not authorized in the propeller specification arc propeller major alterations;

(1) changes in blade design;

(2) changes in hub design;

(3) changes in the governor or control design;

(4) installation of a propeller governor or feathering system;

(5) installation of propeller de-icing system; and

(6) installation of parts not approved for the propeller.

(d) Equipment major modification

Alterations of the basic design not made in accordance with Airworthiness Directives are equipment major alterations. In addition, changes in the basic design of communication and navigation systems, flight management systems approved under type certification or approved specifications that have an effect of the performance of the equipment are


APPENDIX-1 ANO A.7

also major alterations.

2. Major Repairs

2.1 Typical major repairs are listed bellow:-

(a) Airframe Major Repairs. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing splicing and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting, bonding or welding, are airframe major repairs:

(1) box beams: (2) honeycomb panels; (2) Monocoque or Semimonocoque wings or control surface: (3) Wing skins, stringers or chord members; (4) Spars: (5) Pressure bulkheads, doors, hatches and windows; (6) Spar flanges; (7) Members of truss-type beams; (8) Thin sheet webs of beams; (9) Keel and chine members of boat hulls or floats; (10) Corrugated sheet compression members, which act as flange (12)

material of wings or tail (11)surface: Wing mam ribs and compression members;

(13) engine pylons; (14) engine mounts: (15) fuselage longerons; (16) members of the side truss, horizontal truss or bulkheads; (17) main seat support branches and brackets; (18) landing gear brace struts; (19) axles: (20) wheels (21) skis and ski pedestals: (22) parts of the control system such as control columns, pedals, shafts,

brackets or (23)horns: (24) repairs involving the substitution of material; (25) the repair of portions of skin sheets by making additional

seams; the splicing of skin sheets; (27) the repair of three or more adjacent wing or control surface ribs or

the leading edge of wings and control surfaces between such adjacent ribs; repair of fabric covering involving an area greater than that required to repair two adjacent ribs;

(28) replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers and control surfaces; and

(29) repairing of removable or integral fuel tanks and oil tanks.


APPENDIX-1 ANO A.7

(b) Power-Plant Major Repairs: Repairs of the following parts of an engine and Repairs of the following types are power-plant major repairs:

(1) - fan and shaft

- fan thrust bearing

- intermediate pressures and low-pressure turbines

- intermediate or pressure compressors

- combustor lever

(2) separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger;

(3) separation or disassembly of a crankcase or crankshaft of a

reciprocating engine equipped with other than spur-type propeller reduction gearing;

(4) removal, repair or replacement of external gear box; and

(5) special repairs to structural engine parts by welding, plating, metalizing or other methods.

(c) Propeller Major Repairs: Repairs of the following types to a propeller

are propeller major repairs.

(1) any repairs to or straightening of steel

(2) blades: repairing or machining of steel hubs:

(3) shortening of blades;

(4) repairs to wood or composition blades;

(5) repair of propeller governors;

(6) overhaul of controllable pitch propellers;

(7) repairs to deep dents, cuts, scars, nicks, etc., and straightening aluminum blades: and

(8) the repair or replacement of internal elements of blades.

(d) Equipment Major Repairs: Repairs of the following types to

equipment are considered major repairs:

(1) Repair and calibration of flight and navigation system installments and equipment;


APPENDIX-1 ANO A.7

(2) complete disassembly of complex hydraulic and pneumatic power valves:

(3) overhaul of pressure type carburetors and pressure type fuel, oil and

hydraulic pumps; and

(4) overhaul of fuel control systems.


APPENDIX-2 ANO A.7

CRITERIA FOR THE CLASSIFICATION OF MAJOR AND MINOR MODIFICATIONS AND REPAIRS

1. GENERAL

1.1 As mentioned in the paragraph 1.2 of this order, the following criteria outline the decisions

needed in assessing a modification or repair as major or minor. For each issue, it must be determined whether or not the proposed change will have other than a negligible effect. The questions require "yes" or "no" responses. An affirmative answer (yes) to any individual question indicates that the modification or repair should be classified as "major", on the other hand a negative answer (no) to any individual question indicates that the modification or repair should be classified as "minor". The examples and tests listed are for illustration only and not intended to be all encompassing.

2. CRITERIA

2.1 General

2.1.1 Is the change being accomplished as an alternative means of compliance with an airworthiness

directive or equivalent?

2.2 Mass and balance

(a) Does the change involve a revision in the approved mass limitations or center of gravity range limits?

(b) Does the change require the installation of ballast or other methods to maintain the

center of gravity within the approved limits?

2.2.3 Performance and flight characteristics

2.2.3.1 Does the change involve alterations to the configuration of the aircraft which may:

(a) increase drag;

(b) alter the thrust or power;

(c) affect stability or controllability:

(d) induce flutter or vibration; or

(e) alter the stalling characteristics to an extent which necessitates analysis or test?

2.4 Structural strength


APPENDIX-2 ANO A.7

(a) Does the change involve a principal component of the aircraft structure such as a frame,

stringer, rib, spar or safe evaluation?

(b) Does the change involve a structural element which is addressed as part of a damage tolerance or fatigue/failsafe evaluation?

(c) Is a pressure vessel penetration or change involved?

(d) Does the change involve the installation of an item of mass necessitating structural re-

evaluation?

(e) Does the change involve the installation or alteration of a containment or restraint system intended for the stowage of item of significant mass?

(f) Does the change involve repairs or modification to the load-bearing structure of seats’

harnesses or their means of attachment or any other occupant restraint equipment?

(g) Does the change involve the substitution of materials?

2.5 Power plant operation 2.5.1 Does the change significantly affect the power plant or propeller or their accessories?

2.6 Other qualities affecting airworthiness

2.6.1 Does the change involve equipment for which there is no performance standard which has been

approved or accepted by the airworthiness authority? 2.6.2 Does the change affect the probability of failure conditions which could impair or preclude

continued safe flight or landing? 2.6.3 Does the change affect the pilot's visibility or impair the pilot's capability to control the aircraft?

2.6.4 Does the change invoke alterations to the interior arrangement or cabin materials?

2.6.5 Does the change involve systems for cabin pressurization or the provision of breathing oxygen?

2.6.6 Does the change involve flight controls or an autopilot?

2.6.7 Does the change involve critical or essential components of the electrical system such as

generators, alternators, inverters, batteries, distribution busses, or bus protection and control devices?

2.6.8 Does the change affect installments, indicators or their subsystems which provide navigation

information? 2.6.9 Does the change affect instruments, indicators or their subsystems which provide essential or


APPENDIX-2 ANO A.7

critical information concerning the aircraft status''

2.6.10 Does the change affect regulated placard'.'

2.6.1 1 Does the change affect any approved information contained in the flight manual or equivalent document?

2.7 Other qualities affecting environmental characteristics

2.7.1 Docs the change alter the aircraft noise or emission characteristics?

2.8 Non-standard practices

2.8.1 Does the change involve practices or techniques which are novel or unproven in the proposed

application?





CHAPTER A.8 ASSIGNMENT OF MODES ADDRESS AND GROUND TESTING OF ACAS TRANSPONDERS

Sections Title

1 GENERAL

2 DEFINITIONS

3 ALLOCATION OF ADDRESS

4 APPLICATION PROCEDURES FOR ALLOCATION OF

5 ACAS TRANSPONDER GROUND TESTING COSI DERATION

6 RELATED AIRWORTHINESS

1. GENERAL

1.1 Aircraft are required to be equipped with, and operate, Mode S transponder equipment in certain segments of airspace within the USA, European Airspace and Indian Airspace. ICAO has also notified (Annex 6, Part I) that in future specific performance classes of aeroplanes are required to be equipped with ACAS II and shall operate in accordance with relevant provisions of Annex 10. Therefore, prior to operating in the designated airspace, where aeroplanes are required to be equipped with Mode S transponder, the aircraft must have a unique address code assigned by the aircraft's State of Registry.

2. DEFINITIONS

2.1 For the purpose of this Order, the definitions as mentioned under the Rule 2 and 183 of the

Civil Aviation Rules, 1984 shall apply. Where a particular definition under the rule, the under mentioned definitions shall apply:

(a) "ACAS" means an Airborne Collision Avoidance System (ACAS) based on

secondary surveillance radar (SSR) transponder signals which operate independently of ground-based equipment to provide advice to the pilot on potential conflicting aircraft that are equipped with SSR transponders.

Issue 1, Page-1 28 February,2002

ANO A.8

(b) "ACAS I" means an Airborne Collision Avoidance System which provide information as an aid to "see and avoid" action but does not include the capability for" generating resolution advisories (RAs).

(c) "ACAS II" means an Airborne Collision Avoidance System that utilizes

interrogations of, and replies from airborne radar beacon transponders and provides traffic advisories and resolution advisories in the vertical plane.

(d) "ACAS III" means an Airborne Collision Avoidance System, which provides

vertical and horizontal resolution advisories (RAs) in addition to traffic advisories (TAs)

(e) "Aircraft Address" means a unique combination of twenty-four bits available for

Assignment to an aircraft for the purpose of air-ground communications, navigation and surveillance.

(f) "Mode A" transponder equipment means, a transponder capable to elicit

transponder replies for identity and surveillance.

(g) "Mode C" transponder equipment means, a transponder capable to elicit transponder replies for automatic pressure-altitude transmission and surveillance

(h) "Inter mode A/C/S all-call" transponder equipment means, a transponder capable

to elicit replies for surveillance of Mode A/C transponders and for the acquisition of Mode S transponders.

(i) "Inter mode A/C- all-call" transponder means, a transponder capable to elicit

replies for surveillance of Mode A/C transponders. Mode S transponders do not reply.

(j) "Mode S" transponder equipment means a transponder, which meets the

requirements of FAA TSO-C88 or equivalent standard acceptable to the Chairman and be capable replying to:

(i) Mode A/C interrogations with the code specified by ATC (ii) Inter mode (iii) Mode S interrogations

(k) "Resolution advisory (RA)" means an indication given to the flight crew

recommending:

(i) a manoeuvre intended to provide separation from all threats; or

(ii) a manoeuvre restriction intended to maintain existing separation

(l) "Traffic advisory (TA)" means an indication given to the flight crew that a certain intruder is a potential threat.


ANO A.8

Note: (1) Mode A/C transponders are suppressed by Mode S interrogations and do not reply.

(2) The SSR Mode S address consisting of twenty-four bit aircraft address

allocated by ICAO to the State of Registry and assigned as prescribed in the Chapter 9, Part I, Volume III, Annex-10.

3. ALLOCATION OF ADDRESS CODE

3.1 In accordance with the fundamental concept of SSR Mode S operations, each Bangladesh

registered aircraft required to operate in the transponder Mode S-mandatory airspace, is assigned a unique 24 bit SSR Mode S address codes by the Chairman.

3.2 Aircraft addresses are assigned in accordance with the following principles-

(a) at the one time, no address shall be assigned to more than one aircraft;

(b) only one address shall be assigned to an aircraft, irrespective of the number of transponders on board;

(c) the address shall be not changed, except under an exceptional circumstance, and

shall not be changed in flight;

(d) when an aircraft changes State of Registry, the previously assigned address shall be relinquished and a new address shall be assigned by the new State of Registry or registering authority;

(e) the address serves only a technical role for addressing and identification of

aircraft and shall not be used to convey any specific information such; and

(0) the address composed of 24(twenty four) ZEROS and 24(twenty four) ONEs shall not be assigned to aircraft;

3.3 Under Annex 10 Volume 1, ICAO allocates blocks of SSR Mode S addresses to each State

of Registry. The first 12 bits of the address as allocated by the ICAO comprise the national identification code. For Bangladesh, the state code is be 0111 00 000 010.

3.4 The remaining (second) 12 bits provide the individual aircraft address codes, which for each

Bangladesh registered aircraft, comprise the binary form of the aircraft identification number assigned from CAAB data base or record maintained by the Airworthiness and Engineering Licencing Division. On application, the CAAB will allocate the remaining (second) 12 bits on the basis of binary value, which matches the order of assignment in ascending sequential order. Example of a complete address of the first aircraft allocated mode S code (registered as S2- ACO) is 0111 00 000 010 00 00 0000 0001. Similarly the mode S code allocated for the next aircraft (registered as S2- ACP) is 0111 00 000 010 00 00 0000 0010.


ANO A.8

4. APPLICATION PROCEDURES FOR ALLOCATION OF MODE S CODE

4.1 An application for allocation of a Mode S transponder code to a civil aircraft registered in Bangladesh shall be submitted to the Chairman by the Owner/Operator through letter. The following aircraft information must be supplied by the applicant-

(a) make; (b) model; (c) Serial number; and (d) for an aircraft already on the Bangladesh Register of Aircraft, the aircraft

registration marks.

4.2.1 Aircraft that are not currently registered in Bangladesh, but intended to be registered in

future in Bangladesh, cannot be allocated a Mode S code. Owner/Operator of such aircraft must forward their application to the appropriate authority in the aircraft's State of Registry.

5. ACAS TRANSPONDER GROUND TESTING CONSIDERATION

5.1 Recognizing that ACAS aircraft operate by interrogating operational transponders, it is

apparent that they will elicit replies from transponder equipped aircraft on the ground if they are in range and the equipment switched on.

5.2 This, therefore, presents the possibility that a ground operated transponder may trigger a

nuisance advisory on an ACAS equipped aircraft operating in the close vicinity. If the ground target is providing altitude data the ACAS logic should declare the aircraft to be on the ground and ought not to generate an advisory. If no altitude data is provided the ACAS will generate a TA if the threat criteria are met. If the ground is providing altitude data other than surface altitude, as may happen with a defective altitude encoder, or if a test pressure is being applied to the altitude encoder, the ACAS may generate both a TA and RA if the threat criteria met.

5.3 It is considered that nuisance advisories may be cause to any ACAS equipped aircraft flying

in the vicinity of transponders, which are being tested, this may also include aircraft passing overhead at medium altitudes. The problem may be more noticeable where ground testing of transponders takes place at airfields located beneath Terminal Control Areas or in the vicinity of Control Areas and Zones where are traffic movements are likely to be numerous.

5.4 Maintenance organization and personnel who are involved in the ground testing of

transponders and ACAS equipment are required to follow specific procedures given by the manufacturer of the equipment and take precautions to ensure that the risks of causing nuisance advisories are recognized and kept to a minimum.

5.5 Where no specific procedures are given by the manufacturer of the equipment, the

following procedures be followed by the maintenance personnel to minimize the possibility of causing nuisance advisories to ACAS equipped aircraft when ground testing transponders and/or ACAS:


ANO A.8

(a) when not required ensure that transponders are selected to 'OFF' or 'Standby'.

(b) for transponders under test, when equipped for altitude reporting, set the control to 'Mode A/C and select Altitude Reporting 'ON’.

(c) where possible, carry out testing inside a hangar to take advantage of any shielding properties it may provide.

(d) always use the antenna transmission absorption covers when these are provided

with the test set.

(e) when testing Mode C operation that requires the altitude to be increased, radiate directly into the ramp test via the prescribed attenuator.

(f) in between test parameters, select the transponder to the standby mode.

(g) the simulation of ACAS operation by the radiation from an antenna located on, or

remotely based from a workshop, is not permitted.

6. RELATED AIRWORTHINESS REQUIREMENT

6.1 The operators' attention is also drawn to the ANO (airworthiness) E.6 on aircraft equipment, system and instruments regarding the requirements of installation of an ACAS II (minimum performance level) on aircraft registered in Bangladesh.

This order is issued in pursuance of the Rules 4, 89 and 107 of the Civil Aviation Rules, 1984.

Air Cdre Lutfur Rahman ndu, psc



- 1 -

ANO A.9

CIVIL AVIATION AUTHORITY, BANGLADESH AIR NAVIGATION ORDERS AIRWORTHINESS

REQUIREMENTS


CHAPTER A.9 AIRCRAFT NOISE CERTIFICATE

SECTIONS

1. GENERAL 5. ISSUE/VALIDATION OF NOISE 2.

DEFINITIONS

6.

CERTIFICATE VALIDITY PERIOD OF NOISE

CERTIFICATE

3.

APPLICABILITY

7.

SUSPENSION/CANCELLATION OF NOISE CERTIFICATE

4.

NOISE STANDARD

APPENDIX 1 - NOISE CERTIFICATE

1. GENERAL

1.1 ICAO Standard and Recommended Practices for operation of aircraft engaged in

international operations requires that all aircraft as mentioned in section 3 of this order shall carry a document attesting noise certification.

1.2 The Rule 276(1) of the Civil Aviation Rules, 1984 states that an aircraft registered in

Bangladesh shall not be engaged in international air navigation unless it holds a Noise Certificate issued or validated by the Chairman.

2. DEFINITIONS 2.1 For the purpose of this Order, the definitions as mentioned under the Rule 2 of the

Civil Aviation Rules, 1984 shall apply. Where a particular definition is not given under the Rule, the under mentioned definitions apply:

(a) "Acoustic change" means, any change in the type design of an aircraft that

may increase the noise level of that aircraft.

(b) "Subsonic aeroplane" means, an aeroplane for which the maximum operating limit speed does not exceed a Mach number of 1.

(c) “Annex” means ICAO Annex-16, Volume 1.

Issue 3 05 May 2009

- 2 - ANO A.9

3. APPLICABILITY

3.1 This Order applies to all such categories of aircraft as are specified in the ICAO Annex16, Volume 1 and registered in Bangladesh. It is also applicable to all foreign registered aircraft operated by the operators under Air Operator Certificate (AOC) issued by the Chairman.

3.1.1 Subsonic Jet Aeroplanes:

(i) Application for Certificate of Airworthiness for the prototype

accepted before 6 October 1977.

The standards given in Chapter 2 of the Annex shall be applicable to all subsonic jet aeroplanes and their derived versions for which the application for certification of a change in type design was accepted or another equivalent procedure was carried out by the certificating authority on or after 26th November 1981.

3.1.2 (a) Subsonic Jet Aeroplanes:


accepted on or after 6 October 1977 and before 1 January 2006.

(b) Propeller-driven Aeroplanes over 5700 Kg:


accepted on or after 1 January 1985 and before 17 November 1988.

(c) Propeller-driven Aeroplanes over 8618 Kg:


accepted on or after 17 November 1988 and before 1 January 2006.

The standards given in Chapter 3 of the Annex shall be applicable to the above stated aeroplanes.

3.1.3 (a) Subsonic Jet Aeroplanes:


accepted on or after 1 January 2006.

Issue 3 05 May 2009

- 3 - ANO A.9

(b) Propeller-driven Aeroplanes over 8618 Kg:


accepted on or after 1 January 2006.


3.1.4 Propeller-driven Aeroplanes over 5700 Kg:


accepted before 1 January 1985.


3.1.5 Propeller-driven Aeroplanes not exceeding 8618 Kg:


accepted before 17 November 1988.


3.1.6 Propeller-driven STOL Aeroplanes:

Guidelines provided in Chapter 7 of the Annex are used for noise certification of propeller-driven STOL aeroplanes.

3.1.7 Helicopters:

(i) All helicopters for which the ICAO Annex 16, volume I, Para

8.1.2, 8.1.3 and 8.1.4 apply, except those designated exclusively for agricultural, fire fighting or external load carrying purpose.

Guidelines provided in Chapter 8 of the Annex are used for noise certification of applicable helicopters.

3.1.8 Installed Auxiliary Power Units (APU) and Associate Aircraft Systems

during ground operations.

Guidelines provided in Chapter 9 of the Annex are used for noise certification of installed APU and associated aircraft systems.

Issue 3 05 May 2009

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3.1.9 Propeller-driven Aeroplanes not exceeding 8618 Kg:

(i) Application for Certificate of Airworthiness for the prototype or

derived version accepted on or after 17 November 1988.


3.1.10 Helicopters not exceeding 3175 kg maximum certificated take-off mass:

Guidelines provided in Chapter 11 of the Annex are used for noise certification of applicable helicopters.

3.1.11 Supersonic aeroplanes:

The guidelines will be developed later on.

3.1.12 Tilt – Rotor aircraft:

The guidelines will be developed later on.

4. NOISE STANDARD

4.1 All aircraft operated under AOC issued by the Chairman CAAB shall comply with at

least any one of the noise standards as mentioned below:

(a) ICAO Annex-16, Volume 1; or (b) FAR / JAR Part 36

4.2 Noise Certificate from CAAB is issued on the basis of noise certificate issued by

National Aviation Authority (NAA) of the ICAO contracting States responsible for issue of Type Certificate (TC) in compliance with ICAO Annex 16 noise standards or equivalent noise standards, or Noise Certificate issued by the NAA(s) responsible for issue/renewal of Certificate of Airworthiness and Noise Certificate of the aircraft or information/data contained in the NAA approved Flight Manual or Advisory Circular (AC) 36-1 issued by the Federal Aviation Administration (FAA) of the USA.

5. ISSUE/VALIDATION OF NOISE CERTIFICATE

5.1 An operator/owner is to submit the following documents to CAAB requiring issue of

Noise Certificate by the Chairman:

(a) Original copy of the Noise Certificate issued by the NAA responsible for issue of type certificate of the aircraft type; or

Issue 3 05 May 2009

Page 1 of 1 APPENDIX 1 ANO A.9

Noise Certificate No.

Civil Aviation Authority Of Bangladesh Airworthiness and Engineering Licencing Division

NOISE CERTIFICATE

FORM AWS-5 ISSUE - 3

Nationality and Regn. Marks Manufacturer and Designation of Aircraft Aircraft serial number

Engine make and model Maximum certificated take-off mass Propeller make and model

Approved maximum noise levels in – (Unit of measurement) Take off/flyover Side line Approach

Additional modification incorporated to comply noise complaints

The conditions to be satisfied with the above-mentioned requirement, as well as the noise level data appear in the following document Document title and No.: Page: Chapter/Section: Appendix:

Basis of issue of the Noise Certificate

------------------------- The Noise Certificate is issued in pursuance to the Rule 277 of the Bangladesh Civil Aviation Rules 1984, in respect of above-mentioned aircraft, which is considered to comply with the relevant noise requirements when maintained, overhauled and repaired in accordance with the Civil Aviation Rules 1984, operated according to the Approved Flight Manual. The certificate is valid in conjunction with the Certificate of Airworthiness issued for the aircraft by CAAB. The relevant noise requirements are those of the Annex 16 to the convention on International Civil Aviation Organization (ICAO). Thus the above-mentioned aircraft complies with the standards of Part II, Chapter , Volume 1, of the ICAO Annex 16. Unless suspended or cancelled in accordance with the ANO (Airworthiness) A.9, this certificate shall remain in force continually from the date of issue. Dated:

for Chairman CIVIL AVIATION AUTHORITY

This Certificate should be carried in the aircraft whenever it is in flight.

No entries or endorsements may be made on this Certificate except by the Civil Aviation Authority for the purpose. If this certificate is lost the Civil Aviation Authority should be informed at once. Any person finding this certificate should forward it immediately to the Civil Aviation Authority, Airworthiness & Engineering Licencing Division, CAAB Headquarters, Kurmitola, Dhaka-1229.

Issue 3 5 May 2009

CAAB ANO (AW) A.10

Issue 2 December 2016

[

CIVIL AVIATION AUTHORITY, BANGLADESHAIR NAVIGATION ORDERS



CHAPTER A.10 - FEES/CHARGES FOR AIRWORTHINESS SERVICES

This order specifies fees/charges for services related to airworthiness provided by Civil AviationAuthority, Bangladesh.

The followings are fees/charges for the type of services rendered by Airworthiness & EngineeringLicensing Division of CAAB:

Sl No. Type of Services

01 Certificate of Registration (Restricted). 20,000/=

02. Issue of Certificate of Registration.

a) Glider: 25,000/=

b) Small A/C: 1,00,000/=

c) Large A/C: 2,00,000/=

03.Allocation of Provisional Registration Marks (foreach extension).

10,000/=

04. Certificate of Airworthiness (Restricted). 20,000/=

05. Issue / Renewal of Certificate of Airworthiness.

a) Glider: 3,000/= for each 1,000 Kg or partthereof for aircraft MTOW.

b) Small Aeroplane & Helicopter: 15,000/=.

c) Aeroplane MTOW between 5,700Kg to1,00,000 Kg: 1,500/= for each 1,000 Kgor part thereof.

d) Aeroplane MTOW above 1,00,000 Kg:1,000/= for each 1,000 Kg or part thereof.

06.Re-issue / Duplicate of Certificate of Registration(change).

20,000/=

07. Change of Ownership 50% of the initial issue of C of R

08. Noise Certificate 10,000/=

09.De-registration of aircraft on operators / ownersrequest

a) Glider: 5,000/=

b) Aeroplane below 5,700Kg or Helicopterbelow 3,175 kg: 25,000/=

c) Aeroplane above 5,700Kg or Helicopterabove 3,175 kg: 50,000/=

Fees/Charges (Taka)

-2- CAAB ANO (AW) A.10



10.Re-issue / Duplicate Certificate of Airworthiness(change).

20,000/=

11.Permit to fly (Special Ferry flight permission) with /without Certificate of Airworthiness.

30,000/=

12. Export Certificate of Airworthiness.

Having Valid C of ASmall A/C: 30,000/=Large A/C: 1,00,000/=

Without Valid C of ASmall A/C: 50,000/=Large A/C: 2,00,000/=

13. Initial / re-issue approval of Aircraft MaintenanceSchedule / Programme.

Small aircraft: 25,000/=

Large aircraft: 50,000/=

14.Approval of amendments to the approved AircraftMaintenance Schedule / Programme.

25% of the initial approval.

15.Initial / Re-issue Approval of Maintenance ControlManual / MOE / CAME.

1,00,000/=

16.Approval of amendments to the MaintenanceControl Manual / MOE / CAME.

25% of the initial approval.

17. Issuance / change of Instructor approval. 5,000/=

18. Basic / type examination for each Module or type. 4,000/=

19. Type Course approval for each course 20,000/=

20.Issue / renewal / change/Duplicate of AircraftMaintenance Engineer Licence.

5,000/=

21. Application for Technical clearanceSmall aircraft: 25,000/=Large aircraft: 50,000/=

22. Issuance of NOC (Each Case) 10,000/=

23. Approval of Major Modification / Repair 20,000/=

24. Approval of Modification / Repair other than Major 5,000/=

25.Application fee for Validation of foreign AMElicence.

10,000/=

26. Certificate of Approval for design organization.Small A/C: 5,00,000/=Large A/C: 10,00,000/=

27.Certificate of Approval for manufacturingorganization.

Small A/C: 5,00,000/=Large A/C: 10,00,000/=

28.Issue of Certificate of Approval as AircraftMaintenance Organization (AMO) for the AOCholder.

Small A/C: 1,00,000/=Large A/C: 2,00,000/=

29.Renewal of Certificate of Approval as AircraftMaintenance Organization (AMO) for the AOCholder.

50% of the initial approval

30.Issue of Certificate of Approval for Foreign AMO /MRO.

1,00,000/=

31.Renewal of Certificate of Approval for ForeignAMO / MRO.


Fees/Charges (Taka)

-2- CAAB ANO (AW) A.10



32.Change of the AMO scope for additional rating(Airframe & Engine)

20,000/= for each item

33.Change of the AMO scope additional componentrating

10,000/= for each item

34.Issue of Aircraft Maintenance Training Instituteapproval.

1,00,000/=

35.Renewal / change of Aircraft Maintenance TrainingInstitute approval.


36.Issue of Aircraft Maintenance Training Instituteapproval (Foreign).

75,000/=

37.Renewal / change of Aircraft Maintenance TrainingInstitute approval (Foreign).


38.Grant of approval / renewal for technicalcertification of Bangladesh registered aircraft byforeign agency for each location.

20,000/=

This order is issued in pursuance of the Rules 4, 56, 171, 186 and 190 of Civil Aviation Rules, 1984. ThisANO supersedes Issue 1, dated 10 January 2005.

Air Vice Marshal Ehsanul Gani ChoudhuryGUP, ndc, psc

ChairmanCivil Aviation Authority, Bangladesh

-3-

Fees/Charges (Taka)

CIVIL AVIATION AUTHORITY, BANGLADESH AIR NAVIGATION ORDERS AIRWORTHINESS

REQUIREMENTS


CHAPTER A.1 1 PROCEDURE FOR AMENDMENTS OF AIR NAVIGATION ORDERS – AME LICENSE & AIRWORTHINESS RELATED

SECTIONS

1. GENERAL 4. PROCEDURE FOR ISSUE AND

SUBSEQUENT REVISIONS

2. DEFINITIONS 5. CAAB WEB SITE

3. RESPONSIBILITY FOR ISSUE AND REVISION OF ANOs - AIRWORTHINESS

1. GENERAL 1.1 The Air Navigation Orders (ANOs) are issued under the authority of the rule of the

Civil Aviation Rules 1984 Aircraft Rules, which specify various requirements and standards for civil aircraft registered in Bangladesh.

1.2 This Order describes the procedure of issue of ANO (Airworthiness Requirements),

its amendments / revisions and its circulation to the various operators.

2. DEFINITIONS 2.1 For the purpose of this Order, the definitions as mentioned under the Rules 2, 183

and 234 of the Civil Aviation Rules (CARs), 1984 shall apply.

3. RESPONSIBILITY FOR ISSUE AND REVISION OF ANOs – AIRWORTHINESS

3.1. The Air Navigation Orders are promulgated under the authority of CARs 1984 for

the purpose of giving effect to the Rules stated therein and specify the detailed requirements for compliance.

3.2 The promulgation and implementation of ANOs are to meet the duties and

obligations of Bangladesh as a Contracting State under the Chicago Convention including the International Standards contained in the Annexes.

Issue 1 17 May 2009

- 2 - ANO A.11

3.3 Head of the Airworthiness and Engineering Licensing is responsible for:

3.3.1 Processing amendment of existing ANOs or Issue of New ANOs (Airworthiness

Requirements), under the following circumstances:

(i) Whenever a new Rule is incorporated in the CARs 1984 or

(ii) Whenever an existing rule is amended / revised and

(iii) Whenever an amendment to ICAO annexes are issued which necessitates revision of any ANOs or Issue of an ANO.

3.3.2 Maintain up-to-date compliance Check List in respect of the under mentioned

Annexes and Chapters thereof for which the AELD responsible:

(a) Annex 1 (Aircraft maintenance – Technicians/Engineers/Mechanics);

(b) Annex 6, following Chapters:

(i) Chapter 5 – Aeroplane performance operating limitations; (ii) Chapter 6 – Aeroplane instruments, equipment and flight documents; (iii) Chapter 7 – Aeroplane communication and navigation equipment; (iv) Chapter 8 – Aeroplane maintenance; and (v) Chapter 11 – Manuals, logs and records.

(c) Annex 7, 8, 13 and 16.

(d) Identify differences with ICAO Annexes and notify difference, if any to Director F.S. & R for informing ICAO through AT Division.

3.4 Required issue and/or revision of the applicable ANO(s) shall be issued within a

period not exceeding 30 (thirty) days of effective date of the specific Rule of the CARs 1984 or effective date of the specific amendment number of the Annex.

4. PROCEDURE FOR ISSUE AND SUBSEQUENT REVISIONS

4.1. When an ANO is issued, the first page indicates the Issue number and the date of issue

on the date of issue on the bottom left hand corner and the bottom right hand corner of each page respectively. The initial issue is numbered as Issue 1, and the subsequent Revision as Issue 2 and so on.

4.2 Pages which are not affected by the revision will contain initial date of issue only.

All revisions to the ANO will be indicated by a sideline on the left side of the affected pages indicating the change/ revision to the ANO.

Issue 1 17 May 2009