Owner Declared AMP with EASA Minimum Inspection …camo.zweefportaal.nl/CAMO/ARC/D-KXYZ invulvoorbeeld... · Web viewEASA MINIMUM INSPECTION PROGRAM PIK-20 E D-KXYZ sn 20XYZ LBA Kennblatt

CAMO KNVVL Template AMP, EASA Owner self declared AMP + MIP, aug 2017

Aircraft Maintenance Programme ELA-1 glider, not complex, no commercial use only.

Aircraft identification

1 Registration(s): D-KXYZ

EnginePropellor

Type: PIK-20E

Rotax: 501Hoffman: HO 11F-127B92

Serial No (s): xyz

Serial No.: 1234Serial No.: 1234

Basis for the Maintenance Programme

2 This Aircraft Maintenance Programme complies with : M.A.302(h)

(Only possible for ELA1 aircraft not used in commercial operations)

For Aircraft Maintenance Programmes complying with M.A.302(h) the following data is used:

Minimum Inspection Programme as detailed in the latest revision of AMC M.A.302(i)

Design Approval Holder Maintenance Data (not applicable if using Minimum Inspection Programmes)

3

Not applicable if using Minimum Inspection ProgrammesAttached to annex A is a table with all valid source docs. The alternative is to add this date here in section 3

Additional maintenance requirements not covered above (applicable to all Aircraft Maintenance Programmes, regardless of whether they are based on Design Approval Holder Data or Minimum Inspection Programmes)

Indicate if any of the following additional maintenance requirements are applicable (when replying ‘YES’, list the specific requirements in Appendix B to this Aircraft Maintenance Programme)

Yes No

DKXYZOP-KNVVL######-yymmdd-1 Page 1 of 3

copy EXACTLY from certificate of registration

section 2 for ELA1 non commercial and MIP ONLY

MIP is published by EASA for glider, Turbo, Self-launch and TMG, check annually for current version MA 302(i)

SEE AMC material for MA 302If Annual (periodic) Inspection is based on MIP only, no source docs need to be listed under 3.NOTE: the MIP according MA302(i) still requires design holder data as reference documents to perform maintenance and inspections.

fill out : Yes/ No and add details in Appendix B,NO = OK when covered by MIP


4

Maintenance related to specific equipment and modifications ---- NO

Maintenance related to repairs implemented in the aircraft ---- NO

Maintenance related to life-limited components ---- NO

Maintenance related to Mandatory Continuing Airworthiness Information (ALs, CMRs, specific requirements in the Type Certificate Data Sheet (TCDS, SAS), etc.), rudder cables in case of PIK

YES ----

Maintenance related to repetitive Airworthiness Directives TOST, Hotelliers, K-6 Rudder YES ----

Maintenance related to specific operational/airspace directives/requirements (altimeter, compass, transponder, etc.)

----- NO

Maintenance related to the type of operation or to operational approvals such as Reduced Vertical Separation Minima (RVSM), Minimum Navigation Performance Specification (MNPS), Basic Area Navigation (B-NAV). Does not apply to (powered) gliders, TMG

----- NO

5 Indicate if there are any specific maintenance recommendations made in Service Bulletins, Service Letters, etc, that are applicable (when replying ‘YES’, list all the specific recommendations and any deviations in Appendix B to this Aircraft Maintenance Programme)

SIB for Rotax engine applies

Yes ----


No, is detailed in Bedrijfstijden lijst/ Betriebszeiten Übersicht

Bestandsnaam:registratie-OP-KNVVL lidnummer- datum- versie


Pilot-owner maintenance ( sailplanes, powered-sailplanes)

6

Does the Pilot-owner perform Pilot-owner maintenance (ref. Part-M, M.A.803)?

If yes, enter the name of the pilot-owner(s) or the alternative procedure described in AMC M.A.803 point 3:

Pilot-owner name: Piet Vlieger Licence Number: NL.FC.SPL.2016-0****

Signature: _______________________________________________ Date: 31 december 2016

If yes, list in Appendix B to this Aircraft Maintenance Programme the deviations to the list of Pilot-owner maintenance tasks contained in the AMC to Appendix VIII to Part-M (tasks which are not performed by the Pilot-owner and additional tasks performed)

YES / NO

YES

Record of periodic reviews of the Aircraft Maintenance Programme (in accordance with M.A.302(g) or M.A.302(h)5, as applicable)

7

Describe whether the review has resulted or not in changes to the Aircraft Maintenance Programme (any changes introduced will be described in field 8 below)

Name, signature, date

Revision control of the Aircraft Maintenance Programme

8

Rev. No Content of revision Name, signature, date

1 Initial version valid per 01-01-2017 Piet Vlieger



Approval/Declaration of the Maintenance Programme (select the appropriate option)

9 Declaration by owner:

‘I hereby declare that this is the maintenance programme applicable to the aircraft referred to in field 1 and I am fully responsible for its content and, in particular, for any deviations from the Design Approval Holder’s recommendations’:

Name (given and family name):

Piet Vlieger

Signature:

Date:

31 December 2016

Certification statement

10 ‘I will ensure that the aircraft is maintained in accordance with this maintenance programme and that the maintenance programme will be reviewed and updated as required’

Signed by the person/organisation responsible for the continuing airworthiness of the aircraft according to M.A.201:

Owner - Lessee

Name of owner/lessee: Piet Vlieger

Address: Nimbuslaan 6, NL5555 AA, Basisdorp, Netherlands

Telephone/fax: +31 123456789

E-mail: [email protected]

Date: 31 December 2016

Signature:

11 Appendices attached:

— Appendix A YES MIP adopted for PIK 20E (red= added, strike through does not apply), table with source docs issued by TCDS holders added

— Appendix B YES


If EASA MIP is used. Thick YES. 2 situations apply:1. EASA MIP suffices you do not

need to add the MIP to the file.2. EASA is modified (like in this

example) then you must add the MIP

Yes when you have items in table 4, 5, 6 answered with YES

mailto:[email protected]


Appendix A ‘Minimum Inspection Programme’ (only applicable if a Minimum Inspection Programme different from the one described in AMC M.A.302(i) is used)

Detail the tasks and inspections contained in the Minimum Inspection Programme being used.

Attached appendix A == EASA MIP.

Adopted for PIK-20 E



Appendix B ‘Additional Maintenance Requirements’ and ‘Pilot-owner maintenance’ (include only if applicable) (see Sections 4, 5 and 6 above)

Task Description References Interval

Maintenance related to specific equipment and modifications

Not applicable -- --

Maintenance related to repairs implemented in the aircraft


Maintenance related to life-limited components


Maintenance related to Mandatory Continuing Airworthiness Instructions (ALIs, CMRs, specific requirements in the TCDS, etc.)

Rudder cables on condition Current EASA SAS document for PIK-20 E annually

Maintenance related to repetitive Airworthiness Directives

Overhaul Tost Aero Tow Coupling,

Aero tow is not practiced. Annual check for operation is performed.

Current Tost manual, LTA 1989-18/3 date May 2002 2000 Launches or 10000 activations

Inspection of Hotellier Couplings Replace at 3000 hours or excessive wear

Actual instructions of L-Hotellier, LTA 1993-001/3 L’HotellierLTA 1994-001/2

Annually, advise to replace at 3000 hours

Inspection of fuel clamps, tighten screws, replace clips or hoses when necessary

LTA 1983-187 Annually or 25 engine hours

Propeller hub bolt, Re-torque every 25 motor hours

LTA 1998-322 Annually or 25 engine hours

Maintenance related to specific operational/airspace directives/requirements (altimeter, compass, transponder, etc.)


Fill out Annex B when you have items in table 4, 5, 6 answered with YES.

In Annex be you specify the difference in your AMP with respect to manufacturers suggestions.

Also specify consequences of AD’s, BLA, LTA and AL (Airworthiness Limitation).



Maintenance related to the type of operation or operational approvals

Not applicable --- --

Appendix B ‘Additional Maintenance Requirements’ and ‘Pilot-owner maintenance’ (include only if applicable) (see Sections 4, 5 and 6 above),

Task Description Recommended interval

Indicate:

‘Adopted’, or‘Not adopted’, or‘Adopted with deviations’

Alternative inspection/task (if adopted with deviations)

Amended interval (if adopted with deviations)

Maintenance recommandations contained in Service Bulletins, Service Letters, etc.

NOTE : List all the applicable maintenance recommendations, even those for which it has been decided not to accomplish the task or to accomplish it with deviations.

Rotax 501 maintenance and overhaul

See SB-505-010 Adopted with deviations

Check piston rings for play and conditionFuel /oil spills / leaksPower / run-up rpm

Based on operational hours.

No limits on calendar years

PZL Airspeed indi-cator, maintenance

No instructions Not adopted Leaktest and operational check against specs.

Bi-Annually

Safety Belt overhaul every 12 years

Annual inspec-tion, 12 year renewal of webbing

Adopted with deviations

Annual inspection, on condition use till 16 years

Annual inspection

Task Description (Pilot-owner maintenance)

Pilot-owner maintenance tasks contained in AMC to Appendix VIII to Part-M which are not performed by the Pilot-owner:

Not applicable. Owner holds valid ICAO / Part 66 Maintenance license

Pilot-owner maintenance tasks performed by the Pilot-owner additional to those contained in AMC to Appendix VIII to Part-M

Engine maintenance, inspections and repairs according to Rotax documentation. Excluding complete overhaul.

Propeller maintenance, inspections and repairs according to Hoffmann documentation. Excluding complete overhaul.


Owner may use alternative method and interval. When no AD or AL apply.

Owner may limit or expand scope of POM.Make sure you are only listing items that meet your capabilities.

EASA MINIMUM INSPECTION PROGRAM PIK-20 E D-KXYZ sn 20XYZ LBA Kennblatt 814

Minimum Inspection Programme for ELA1 sailplanes and ELA1 powered sailplanes not involved in commercial operations

To be performed: every annual / 100 h interval (for Touring Motor Gliders (TMG)), whichever comes first; or

every annual interval (for other than TMGs).

A tolerance of one month or 10 h, as applicable, may be applied. However, the next interval shall be calculated from the date/hours originally scheduled (without the tolerance).

Note 1: Use the manufacturer’s maintenance manual to accomplish each task/inspection .

Note 2: In the case of TMGs, it is acceptable to control the hours of use of the aircraft, engine and propeller as separate entities. Any maintenance check to be done between two consecutive annual/100 h inspections may be performed separately on the aircraft, engine and propeller depending on when each element reaches the corresponding hours. However, at the time of the annual / 100 h inspection, all the elements must be covered.

Note 3: Proper operation of backup or secondary systems and components should be included for every instance where a check is performed for improper installation/operation.

ELA1 sailplanes and ELA1 powered sailplanes not involved in commercial operations

Strike through == not applicable , Red == additional to MIP

System/component/area Task & Inspection detail

GENERAL

General — all tasks The aircraft must be clean prior to inspection. Inspect for security, damage, wear, integrity, drain/vent holes clear, signs of overheating, leaks, chafing, cleanliness and condition as appropriate to the particular task. Whilst checking composite structures, check for signs of impact or pressure damage that may indicate underlying damage.

Lubrication/servicing Lubricate and replenish fluids in accordance with the manufacturer’s requirements.

Markings Check that side and under-wing registration markings are correct. If applicable, check that an exemption for alternate display is approved. Identification plate for National Aviation Authority registered aircraft is present. Other identification markings on fuselage in accordance with local (national) rules.

Weighing: Review weighing record to establish accuracy against installed equipment.

Weigh the aircraft as required by the Part-NCO rules.

AIRFRAME

Fuselage paint/gel coat, including registration markings

Inspect external surface and fairings, gel coat, fabric covering or metal skin, and paintwork. Check that registration marks are correctly applied.

document.docx Page 1 of 8

Note1 below: A list of valid and actual documents is added. Although a is not required, it is helpful to prove maintenance is performed based on proper documents


Fuselage structure Check frames, formers, tubular structure, skin, and attachments. Inspect for signs of corrosion on tubular framework.

Nose fairing Inspect for evidence of impact with ground or objects.

Release hook(s) Inspect TOST semi gravity aero-tow release hook and controls. Check operational life. Carry out operational test. If more than one release hook or control is fitted, check operation of all release hooks from all positions.

Pot pitot/ventilator Check alignment of probe, check operation of ventilator.

Pitot/static system Inspect pitot probes, static ports and all accessible tubing for security, damage, cleanliness, and condition. Drain any water from condensation drains.

Bonding/vents drains Check all bonding leads and straps. Check that all vents and drains are clear from debris.

CABIN AND COCKPIT

Cleanliness/loose articles

Check under cockpit floor/seat pan and in rear fuselage for debris and foreign items.

Canopy, locks and jettison

Inspect canopy, canopy frame and transparencies for cracks, unacceptable distortion, and discolouration. Check operation of all locks and catches. Carry out an operational test of the canopy jettison system from all positions.

Seat/cockpit floor Inspect seat(s). Check that all loose cushions are correctly installed and, as appropriate, energy absorbing foam cushions are fitted correctly. Ensure that all seat adjusters fit and lock correctly.

Harness(es) Inspect all harnesses for condition and wear of all fastenings, webbing, and fittings. Check operation of release and adjustments.

Rudder pedal assemblies Inspect rudder pedal assemblies and adjusters.

Flight control circuits/stops

Inspect flight controls rods/cables. Check that control stops are secure and make contact. Pay particular attention to wear and security of liners and cables in ‘S’ tubes. SEE TCDS: Rudder cable is on condition.

Inspect self-connecting control devices. See LTA/Instructions on L-Hotelliers.

Instrument panel assemblies

Inspect instrument panel and all instruments/equipment. Check instrument readings are consistent with ambient conditions. Check marking of all switches, circuit breakers, and fuses. Check operation of all installed equipment, as possible, in accordance with the manufacturer’s instructions.

Check markings of instruments in accordance with the Flight Manual.



Oxygen system Inspect oxygen system. Check bottle hydrostatic test date expiry in accordance with the manufacturer’s recommendations. Ensure that the bottle is not completely empty (13,8 bars/200 psi minimum) and refill with aviator’s oxygen only. Clean masks and regulators with suitable cleaning wipes.

Ensure that the oxygen installation is recorded on weight and C of G schedule. CAUTION: OBSERVE ALL SAFETY PRECAUTIONS.

Colour-coding of controls

Ensure that controls are colour-coded and in good condition, as follows:

Tow release: yellow

Air Brakes: blue

Trimmer: green

Canopy normal operation: white

Canopy jettison: red

Other controls: clearly marked but not using any of the above colours.

Equipment stowed in centre section

Check for security and condition. Check validity of any safety equipment. Check the manufacturer’s and the NAA’s (if required) data plates.

Speed/weight/ manoeuvre placard

Check that the placard is correct and legible and accurately reflects the status of the aircraft.

LANDING GEAR

Front skid/nose wheel and mounts

Inspect for evidence of hard/heavy landings. Check skid wear. Inspect wheel, tyre, and wheel box. Check tyre pressure.

Main wheel and brake assembly

Check for integrity of hydraulic seals and leaks in pipe work. Check life of hydraulic hoses and components if specified by the manufacturer. Remove brake drums, check brake lining wear. Check disk/drum wear. Refit drum. Check brake adjustment. CAUTION: BRAKE DUST MAY CONTAIN ASBESTOS.

Check operation of brake. Check level of brake fluid and replenish if necessary . Check tyre pressure. CAUTION: CHECK TYPE OF BRAKE FLUID USED AND OBSERVE SAFETY PRECAUTIONS.

Undercarriage suspension

Check springs, bungees, shock absorbers, and attachments. Check for signs of damage.

Service strut if applicable.

Undercarriage retract system and doors

Check retraction mechanism and controls, warning system if fitted, gas struts, doors and linkages/springs, over-centre/locking device. Perform retraction test.

Tail skid/ wheel Inspect for evidence of hard/heavy landings. Check skid wear . Inspect wheel, tyre, and wheel box. Check bond of bonded skids. Check tyre pressure.

Wheel brake control circuit

Inspect wheel brake control rods/cables. If combined with air brake, ensure correct rigging relationship . Check parking brake operation if fitted.



WING AND CENTRE SECTION

Centre section fairing Inspect for security, damage, and condition.

Wing attachments Inspect the wing structural attachments. Check for damage, wear, and security. Check for rigging damage. Check condition of wing attachment pins.

Aileron control circuit/stops

Inspect aileron control rods/cables. Check that control stops are secure and make contact.

Inspect self-connecting control devices. ref. LTA / L-Hotellier instructions

Air brake control circuit Inspect air brake control rods/cables. Check friction/locking device (if fitted). Inspect self-connecting control devices. ref. LTA / L-Hotellier instructions

Wing struts/wires Inspect wing struts for damage and internal corrosion. Re-inhibit wing struts internally every three years or in accordance with the manufacturer’s instructions.

Wings including underside registration markings

Check mainplane structure externally and internally as far as possible. Check gel coat, fabric covering, or metal skin . Check that registration marks are correctly applied.

Ailerons and controls Inspect aileron and flaperon assemblies, hinges, control connections, springs/bungees, tapes, and seals. Ensure that seals do not impair full range of movement.

Air brakes/spoilers Inspect air brake/spoiler panel(s) operating rods, closure springs, and friction devices as fitted.

Flaps Check flap system and control. Inspect self-connecting control devices. ref. LTA / L-Hotellier instructions

Control deflections and free play, and record on worksheets

Check and record range of movements and cable tensions, if specified, and check free play. See flight / maintenance manual for details and allowable play

EMPENNAGE

Tailplane and elevator With tailplane de-rigged, check tailplane and attachments, self-connecting and manual control connections. Check gel coat, fabric covering, or metal skin. ref. LTA / L-Hotellier instructions

Rudder Check rudder assembly, hinges, attachments, balance weights.

Rudder control circuit/ stops

Inspect rudder control rods/cables. Check that control stops are secure and make contact. Pay particular attention to wear and security of liners and cables in ‘S’ tubes. ref TCDS: rudder control cable is on condition.

Elevator control circuit/stops

Inspect elevator control rods/cables. Check that control stops are secure and make contact.Inspect self-connecting control devices. ref. LTA / L-Hotellier instructions

Trimmer control circuit Inspect trimmer control rods/cables . Check friction/ locking device.



Control deflections and free play, and record on worksheets

Check and record range of movements and cable tensions, if specified, and check free play. See flight / maintenance manual for details and allowable play

AVIONICS AND ELECTRICS

Electrical installation/fuses

Check all electrical wiring for condition. Check for signs of overheating and poor connections. Check fuses/trips for condition and correct rating.

Battery security and corrosion

Check battery mounting for security and operation of clamp. Check for evidence of electrolyte spillage and corrosion. Check that the battery has correct the main fuse fitted.

It is recommended to carry out battery capacity test on gliders equipped with radio, used for cross-country, controlled airspace, or competition flying.

Radio installations and placards

Perform an Operational Check radio installation, microphones, speakers, headsset and intercom, if fitted . Check that the call sign placard is installed. Carry out ground function test. Record radio type fitted.

Altimeter datum Check barometric sub-scale. Maximum error 2 hPa (mBar).

Pitot-static system Perform operational check.

Transponder & Flarm Perform operational check., update FLARM software when necessary.

MISCELLANEOUS

Removable ballast Check removable ballast mountings and securing devices (including fin ballast if applicable) for condition. Check that ballast weights are painted with conspicuous colour. Check that provision is made for the ballast on the loading placard.

Drag chute and controls Inspect chute, packing and release mechanism. Check packing intervals.

Water ballast system Check water ballast system, wing and tail tanks as fitted. Check filling points, level indicators, vents, dump and frost drains for operation and leakage. If loose bladders are used, check for leakage and expiry date as applicable.

POWERPLANT (when applicable)

Engine pylons and mountings

Inspect engine and pylon installation. Check engine compartment and fire sealing.

Gas strut Check gas strut.

Pylon/engine stops Check limit stops on retractable pylons. Check restraint cables. Must be under tension when extracted

Electric actuator / starter

Inspect electric actuator, motor, spindle drive, and mountings.

Electrical wiring Inspect all electrical wiring. Pay special attention to wiring that is subject to bending during extension and retraction of engine/pylon.



Limit switches Check operation of all limit switches and strike plates. Make sure that they are not damaged by impact.

Fuel tank(s) Check fuel tank mountings and tank integrity. Check fuel quantity indication system if fitted.

Fuel pipes and vents Check all fuel pipes especially those subject to bending during extension and retraction of engine/pylon. Check that vents are clear. Make sure that overboard drains do not drain into engine compartment. Check self-sealing.see LTA: retighten screw clamps every 25 hours or annually.

Fuel cock or shut off valve

Check operation of fuel cock or shut-off valve and indications.

Fuel pumps and filters Clean or replace filters as recommended by the manufacturer. Check operation of fuel pumps for engine supply or tank replenishment. Check fuel pump controls and indications. Replace filters every 25 hours.

Decompression valve Inspect decompression valve and operating control.

Spark plugs Carry out spark plug service. It is recommended to replace spark plugs at annual intervals. Replace annually. Gap: 0,4-0,6 m, Torque 28 Nm

Harnesses and Magneto Inspect low-tension and high-tension wiring, connectors, spark plug caps. Check magneto to engine timing. Check impulse coupling operation.

Propeller bolts, assembly, mounting, torquing & drive belt

Inspect propeller (cracks according Hoffman Instructions), hub, folding mechanism, brake, pitch change mechanism , stow sensors. See flight / maintenance manual for details:> prop track 10 cm from tip, trailing edge < 3mm difference> belt: tension 60 N, +/- 2,5 mm in centre, check edges for wear> NO PLAY PROP-HUB- BEARING (Note: nut = left thread)> bolts: torque with 15-17 Nm / use lock wire (every 25 hours)

Doors Check engine compartment doors, operating cables, rods, and cams.

Safety springs Check all safety and counterbalance springs.

Extension and retraction Check that extension and retraction operation times are within limits specified by manufacturer. Check light indications and interlocks for correct operation.

Exhaust Inspect exhaust system, silencer, shock mounts, and links. Retorque exhaust manifold screws every 50 hours

Engine installation Inspect engine and all accessories. Carry out compression test and record results.

Compression test results (should be 10,5 +/- 0,5):

No1 (left/front):

No2 (right/rear):

Lubrication Change engine oil and filter. Replenish oil and additive tanks.

Engine instruments Inspect all engine instruments and controls. Check control unit, mounts, bonding and connections. Carry out internal self-test if fitted.



Flexible vibration dampers

Check for poor condition and deterioration.

Engine battery If separate from airframe battery, inspect battery and mountings. If the main fuse is fitted, check rating and condition. Perform an functional operational test.

Placards Check that all placards are in accordance with flight manual and legible.

Oil and fuel leaks With the engine fully serviced, check the fuel and oil system for leaks.



Ref Note 1: Overview of valid documents for D-KXYZ per October 2016

Document Published by Revision Date

Airframe and components

SAS PIK 20E EASA 02 28-04-2011

Flight Manual EIRI KY 03 02-01-1980

Betriebs & Wartungshandbuch EIRI KY 02 02-01-1980

LTA 1993-001/3 L’Hotellier LBA 03 09-04-1998

Radio, ATR833 OLED FUNKE 3.01 24-11-2014

Transponder VT-01, doc 01.0200.11E Garrecht 1.3 14-02-2007

Winter Altimeter 4 FGH20 Winter -- Mrt 2016

PZL Speed indicator Not available

Compass Not available

Autoflug Belts AutoFlug 15-08-1989

11-01-1978

Tost G-73 Tost 3 Mrch 2001

LTA 1989-018/3 on Tost couplings LBA 3 02-05-2002

Rotax 501 sn 1234

TCDS E.208 EASA 01 26-02-2010

Motorhandbuch Rotax 501 Rotax Austria - Dec 1978

Repairmanual Rotax 501 and 505 Rotax Austria - Jan. 1993

Tillotson HR Carburettor 177 B Tillotson Ireland - -

Rotax SB-505-010 Rotax Austria 01 05-09-2006

Propeller Hoffman sn 1234HO11F-127B92Geräte Nr 32.110/1Operation and maintenance manual No.E 0110.74

Hoffman, Rosenheim

08 Feb. 2002


TABLE on this page (in blue just to distinct it from the EASA MIP)

An overview of valid and actual documents is added.

Although a is not required by EASA, it is helpful to prove maintenance is performed based on proper documents.

For ARI & AMPI’s of CAMO NL MG 0065: This table is similar to the famous table 4 in the common AMP’s / OHP’s for PH-registered gliders (Brondocumenten / source documents)

Checklist for annual inspection of PIK-20 E, D-KXYZ

Reference: AMP Pik 20 E, D-KXYZF & Flight Manual, Maintenance Manual, January 1980

Flaps DeflectionWölbklappenaussläge

mm mm or °Gemessen / measured

+ 16° ± 1° Flap root/ KlappenwürzelAileron root/ Querruder würzel

46 ± 2,5 30 ± 1,8

L R

+ 0° ± 1° Flap root/ KlappenwürzelAileron root/ Querruder würzel

0 ± 2,5 0 ± 1,8

L R

- 12° ± 1° Flap root/ KlappenwürzelAileron root/ Querruder würzel

35 ± 2,5 22,5 ± 1,8

L R

Play in flaps, stick and flap handle fixed

Flap to flapFlap to aileronBoth flaps up / down

± 5 ± 2.5± 2.5

Hotellier Ref LTA Hotellier 2 mm jig: <0,1 mm ball:

L R

Aileron DeflectionQuerruderaussläge

Mm or °Gemessen / measured

+ 16° flaps mmUp: 13° - 1° + 2°

Flap root/ KlappenwürzelAileron root/ Querruder würzel

38 +5 -2,5 24,5 +3,8- 1,8

L R

Down: 12,5° - 1° + 2°


36 +5 -2,5 23,5+3,8- 1,8

L R

+ 0° flaps mmUp: 12° - 1° + 2°


35 +5 -2,5 22,5 +3,6- 1,8

L R

Down: 11° - 1° + 2°


31 +5 -2,5 21,0 +3,6- 1,8

L R

-12° flaps mmUp: 11° - 1° + 2°


32 +5 -2,5 21 +3,6- 1,8

L R

document.docx 1 of 2

Checklist for annual inspection of PIK-20 E, D-KXYZ

Down: 9,5° - 1° + 2°


27 +5 -2,5 18 +3,6- 1,8

L R

ElevatorHöhenruderaussläge


2 x + 20° ± 1° Symmetry planeSymmetrie ebene

± 47 ± 2,5

Play with stick fixedwith pushrod in tail fixed

+/- 3 mm+/- 1 mm

Hotellier Ref LTA Hotellier 2 mm / <0,1 mm

Jig: Ball:

RudderSeitenruderaussläge


2 x + 33° ± 2° Symmetry planeSymmetrie ebene

± 179 ± 11

L R

Wings Symmetry Tie down hole in wing tip to

TE-tube point on tail left

cm

right cm

Resonance frequency At wing tip with clock Number/ minute

Air brakes, Hotellier Ref LTA Hotellier 2 mm jig: <0,1 mm ball:

L R

Play in individual bearings and connectors max. 0,1 mm

Engine, See Rotax SB-505-010 Annual

Ground runEngine rpm

2000 – 5700 on ground>> 5600 take off rpm

Annual

Contact points, condensersIgnition timing

0,35-0,45 mm open2,07 mm +/- 0,25 bt

50 hrsReplace 150 hours

Charching coil resistance, 280 – 330 ohm

50 hrs

Cilinder head nuts Torque 20 Nm 25 hours

Carburettors Clean and overhaul , new membranes, main jets

100 hours

Inspect piston rings for free movement

See repair manual 150 hours

Remarks

All Items checked and OK Name + Signature Date:

document.docx 2 of 2

Documents

Owner Declared AMP with EASA Minimum Inspection …camo.zweefportaal.nl/CAMO/ARC/D-KXYZ invulvoorbeeld... · Web viewEASA MINIMUM INSPECTION PROGRAM PIK-20 E D-KXYZ sn 20XYZ LBA Kennblatt