Revision: 17a Date: 04/16/2012 DEPARTMENT OF ... rev 17a.pdfSAAB SF-340 SAAB-340A, SAAB-340B, SAAB-340B+, SAAB-340WT Gary L. Larsen, Chairman Flight Operations Evaluation Board Federal

Revision: 17a Date: 04/16/2012 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION WASHINGTON, D.C. MASTER MINIMUM EQUIPMENT LIST SAAB SF-340 SAAB-340A, SAAB-340B, SAAB-340B+, SAAB-340WT Gary L. Larsen, Chairman Flight Operations Evaluation Board Federal Aviation Administration Flight Standards Division Aircraft Evaluation Group, SEA-AEG 1601 Lind Ave. S.W. Renton Washington 98057-3356 Telephone: (425)-917-6600 FAX: (425)-917-6638

FEDERAL AVIATION ADMINISTRATION Page: I Revision: 17a MASTER MINIMUM EQUIPMENT LIST Date: 04/16/2012 SF-340 Table of Contents

SYSTEM NO. SYSTEM PAGE

-- Table of Contents I, -- Control Page II -- Highlights of Change III -- Definitions IV, V, VI, VII -- Definitions VIII, IX, X, XI -- Preamble XII, XIII 21 Air Conditioning 21-1 THRU 12 22 Auto Flight 22-1 THRU 2 23 Communications 23-1 THRU 11 24 Electrical Power 24-1 THRU 7 25 Equipment/Furnishings 25-1 THRU 17 26 Fire Protection 26-1 THRU 3 27 Flight Controls 27-1 THRU 5 28 Fuel 28-1 THRU 4 29 Hydraulic Power 29-1 THRU 3 30 Ice and Rain Protection 30-1 THRU 15 31 Indicating/Recording Systems 31-1 THRU 8 32 Landing Gear 32-1 THRU 18 33 Lights 33-1 THRU 8 34 Navigation 34-1 THRU 19 35 Oxygen 35-1 36 Pneumatic 36-1 THRU 11 38 Water/Waste 38-1 49 Airborne Auxiliary Power 49-1 52 Doors 52-1 56 Windows 56-1 61 Propellers 61-1 73 Engine Fuel & Control 73-1 74 Ignition 74-1 75 Bleed Air 75-1 76 Engine Controls 76-1 THRU 3 77 Engine Indicating 77-1 79 Engine Oil 79-1

FEDERAL AVIATION ADMINISTRATION Page: II Revision: 17a MASTER MINIMUM EQUIPMENT LIST Date: 04/16/2012 SF-340 Control Page

Cover Page 17a 04/16/2012 Table of Contents 17a 04/16/2012 Control Page 17a 04/16/2012 Highlights of Change 17a 04/16/2012 Definitions 11 09/11/2006 Preamble 2 06/14/1989 ATA 21 17a 04/16/2012 ATA 22 17 02/28/2011 ATA 23 17 02/28/2011 ATA 24 17 02/28/2011 ATA 25 17 02/28/2011 ATA 26 17 02/28/2011 ATA 27 17 02/28/2011 ATA 28 17 02/28/2011 ATA 29 17 02/28/2011 ATA 30 17 02/28/2011 ATA 31 17 02/28/2011 ATA 32 17 02/28/2011 ATA 33 17 02/28/2011 ATA 34 17a 04/16/2012 ATA 35 17 02/28/2011 ATA 36 17 02/28/2011 ATA 38 17 02/28/2011 ATA 49 17 02/28/2011 ATA 52 17 02/28/2011 ATA 56 17 02/28/2011 ATA 61 17 02/28/2011 ATA 73 17 02/28/2011 ATA 74 17 02/28/2011 ATA 75 17 02/28/2011 ATA 76 17 02/28/2011 ATA 77 17 02/28/2011 ATA 79 17 02/28/2011

FEDERAL AVIATION ADMINISTRATION Page: III Revision: 17a MASTER MINIMUM EQUIPMENT LIST Date: 04/16/2012 SF-340 Highlights of Change

EFFECTIVE ABOVE DATE, Interim Revision 17a to the SF-340 Master Minimum Equipment List has been published. This Revision makes minor typographical corrections to two MMEL Items: Item 21-50-1, Supplemental Air Conditioning System, installed IAW STC SA7971SW, and Item 34-11-2, Standby Pitot Static System. Operators which do not have Item 21-50-1 installed as an option, and/or operators which have correctly interpreted the intent of Item 34-11-2, need not incorporate this revision. ATA 21 – AIR CONDITIONING: Item 21-50-2 Supplemental Air Conditioning Systems Item Title changed and Sub-Items added to provide relief for both optional Supplemental Air Conditioning Systems: Sub-Item 1) for Single Condensor Systems installed IAW STC No. SA7971SW; and Sub-Item 2) for Dual Condensor Systems installed IAW STC No. SA3667SW. ATA 34 - NAVIGATION: Item 34-11-2 Standby Pitot Static System: Number Required for Dispatch which has been corrected to “0.”

FEDERAL AVIATION ADMINISTRATION Page: IV Revision: 11 MASTER MINIMUM EQUIPMENT LIST Date: 09/11/2006 SF-340 Definitions

For the Master Minimum Equipment List, Definitions addendum, refer to the current FAA Policy Letter PL-25, “Policy Concerning MMEL Definitions,” as-well-as the current FAA Policy Letter PL-70, “Definitions Required in MELs,” as found in FAA Order 8900.1 - Flight Standards Information Management System (FSIMS), under “Publications – MMEL & AEG Guidance Documentation – MMEL Policy Letters.” http://fsims.avs.faa.gov/fsims/fsims.nsf/actpubs?openview&count=-1&RestrictToCategory=MMEL%20Policy%20Letters

FEDERAL AVIATION ADMINISTRATION Page: V Revision: 2 MASTER MINIMUM EQUIPMENT LIST Date: 09/11/2006 SF-340 Preamble

For the Master Minimum Equipment List, Preamble addendum, refer to the current FAA Policy Letter PL-34, “MMEL and MEL Preamble,” for operations under 14 CFR Parts 121, 125, 129, and 135, as found in FAA Order 8900.1 - Flight Standards Information Management System (FSIMS), under “Publications – MMEL & AEG Guidance Documentation – MMEL Policy Letters.” http://fsims.avs.faa.gov/fsims/fsims.nsf/actpubs?openview&count=-1&RestrictToCategory=MMEL%20Policy%20Letters

U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION

AIRCRAFT: REVISION NO : 17a PAGE:

SF-340 DATE: 04/16/2012 21-1

2. NUMBER INSTALLED SYSTEM & 1. SEQUENCE ITEM NUMBER

3. NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING

4. REMARKS OR EXCEPTIONS

20-1 Recirculation Fans C 2 0 May be inoperative provided: a) Associated Air Conditioning

Pack(s) operate normally, and b) Remaining Recirculation Fan is

only run when associated Air Conditioning Pack(s) are on-line.

NOTE: With Recirculation Fan(s) inoperative, Air Conditioning System performance and associated thermal comfort will be degraded.

1) All-Cargo

Airplanes (Saab SB # 340-25-280 Installed)

C 1 0 May be inoperative provided associated Air Conditioning Pack(s) operate normally. NOTE: With Recirculation Fan inoperative, Air Conditioning System performance and associated thermal comfort will be degraded.



SF-340 DATE: 04/16/2012 21-2



21 AIR CONDITIONING


20-2 Avionic Rack Fan C 1 0 (M)(O)May be inoperative provided: a) Both Air Conditioning Packs operate normally, b) Non-required or redundant navigation equipment is deactivated and alternate procedures are established and used,

c) DPU Fans and MPU Fan (if installed) operate normally, And

d) Avionic Rack Door is removed if cabin temperatures exceed 75 degrees F (24 degrees C) on the ground.

NOTE: Depending on navigational

requirements and company procedures, non-required or redundant navigational equipment could include: one DME (if two installed), one ADF (if two installed), HF Radio, ACARS, one VHF Radio (if three installed and Radio is not powered by an Emergency Bus), MFD, Area Nav.



SF-340 DATE: 04/16/2012 21-3



21 AIR CONDITIONING


20-3 Avionic Rack Fan Failure Indication (AVIONICS VENT on CWP)

C 1 0 (M)(O)May be inoperative provided: a) Both Air Conditioning Packs operate normally, b) Non-required or redundant navigation equipment is deactivated and alternate procedures are established and used, c) DPU fans and MPU fan (if installed) operate normally, And

d) Avionics Rack Door is removed if cabin temperatures exceed 75 degrees F (24 degrees C) on the ground.

NOTE: Depending on navigational

requirements and company procedures, non-required or redundant navigational equipment could include: one DME (if two installed), one ADF (if two installed), HF Radio, ACARS, one VHF Radio (if three installed and Radio is not powered by an Emergency Bus), MFD, Area Navigation.

20-4 Ambient Air Intake

System

Deleted, Revision 16.



SF-340 DATE: 04/16/2012 21-4



21 AIR CONDITIONING


31-1 Cabin Pressure Control Systems

B 2 0 (M)(O)Both Manual and Automatic Cabin Pressure Control Systems may be inoperative provided:

a) Primary Outflow Valve is, either, removed, or secured open by a procedure endorsed by Saab,

b) If operating normally, PRESS DUMP Switch (on Emergency Panel) is ON, and

c) Flight is conducted in an Accepted unpressurized configuration.

1) Manual

Pressurization Control System

B 1 0 (O)May be inoperative provided: a) Automatic Pressurization

Control System operates normally, and

b) Pressure Dump System is verified to operate normally.

31-2 Pressure Dump System

B 1 0 (M)(O)May be inoperative provided: a) Primary Outflow Valve is,

either, removed, or secured open by a procedure endorsed by Saab, and

b) Flight is operated in an Accepted unpressurized configuration.



SF-340 DATE: 04/16/2012 21-5



21 AIR CONDITIONING


31-3 Outflow Valves

B 2 0 (M)(O)May be inoperative provided: a) Primary Outflow Valve is, either, removed, or secured open by a procedure endorsed by Saab,

b) If operating normally, PRESS DUMP Switch (on Emergency Panel) is ON, and

c) Flight is operated in an Accepted unpressurized configuration.

33-1 CABIN RATE Indicator

C 1 0 (O)May be inoperative provided: a) Automatic Pressurization Control System operates normally, and b) Cabin Differential Pressure (DIFF PRESS) Indicator and Cabin Altitude (CABIN ALT) Indicator are verified to operate normally.

B 1 0 (O)May be inoperative provided: a) If operating normally, PRESS DUMP Switch (Emergency Panel) is ON, and b) Flight is operated in an Accepted unpressurized configuration.



SF-340 DATE: 04/16/2012 21-6



21 AIR CONDITIONING


33-2 Cabin Altitude (CABIN ALT)

Indicator

C 1 0 (O)May be inoperative provided: a) Cabin Differential Pressure (DIFF PRESS) Indicator operates normally, and b) A chart is readily available to the crew to convert cabin differential pressure to cabin altitude.

B 1 0 (O)May be inoperative provided:

a) If operating normally, PRESS DUMP Switch (Emergency Panel) is ON, and b) Flight is operated in an Accepted unpressurized configuration.

33-3 Cabin Differential

Pressure (DIFF PRESS) Indicator

C 1 0 (O)May be inoperative provided: a) Cabin Altitude (CABIN ALT) Indicator operates normally, and b) A chart is readily available to the crew to convert cabin altitude to differential

pressure.

B 1 0 (O)May be inoperative provided: a) If operating normally, PRESS DUMP Switch (Emergency Panel) is ON, and b) Flight is operated in an

Accepted unpressurized configuration.

33-4 Cabin Altitude/ Differential

Pressure (CABIN PRESS) Warning System on CWP

B 1 0 (O)May be inoperative provided: a) If operating normally, PRESS

DUMP Switch (Emergency Panel) is ON, and

b) Flight is operated in an Accepted unpressurized configuration.



SF-340 DATE: 04/16/2012 21-7



21 AIR CONDITIONING


40-1 Cabin Auxiliary *** Ground Heating

System (Installed IAW STC No. SA8114SW)

1) Heating Units

D D

1 3

0 1

(M)May be inoperative provided: a) System is deactivated by

pulling and collaring the associated Circuit Breaker,

b) Cabin Auxiliary Ground Heating System (AUX HEAT) Switch remains OFF, and

c) Associated Supplemental Air Conditioning is considered inoperative and Supplemental Air Conditioning (SUPP A/C) Switch remains OFF.

NOTE: Deactivation of the Cabin

Auxiliary Ground Heating System also deactivates the Supplemental Air Conditioning System.

(M)Two individual Heating Units may be inoperative, and the Cabin Auxiliary Ground Heating used, provided affected Heating Unit(s) are deactivated by removal of the associated Current Limiter(s).



SF-340 DATE: 04/16/2012 21-8



21 AIR CONDITIONING


50-1 Air Conditioning Packs (Mod. 2305 installed)

B 2 1 (M)(O)One may be inoperative provided:

a) Avionics Fan is verified to operate normally,

b) If right Air Conditioning Pack is inoperative, all Windshield Heaters operate normally,

c) Ambient Air (Ram Air) Intake is extended,

d) Associated Bleed Valve (BLD VALVE) Switch remains CLOSED,

e) Associated Recirculation (L/R RECIRC) Fan remains OFF,

f) Flight time is limited to 2 hours or less, and aircraft is not dispatched if ground or flight temperatures are above ISA +20 deg C, or below ISA -20 deg C,

g) Airplane is not operated in known or forecast icing conditions,

h) MEA's on planned route of flight are 8,000 feet MSL, or less, and

i) Alternate Abnormal Procedures for loss of a second Air Conditioning Pack are established and used.

NOTE: Icing Conditions exist any time weather conditions meet visibility and temperature Limits specified in the AFM for operation of Wing and

Stabilizer De-Icer Boots, and any time airplane ice

accretion is known or is predicted to occur.



SF-340 DATE: 04/16/2012 21-9



21 AIR CONDITIONING


50-2 Supplemental Air *** Conditioning Systems

1) Single Condensor Systems installed IAW STC No. SA7971SW

2) Dual Condensor Systems installed IAW STC No. SA3667SW

D D

- -

0 0

(M)May be inoperative provided:

a) System is deactivated by pulling and collaring the associated Circuit Breaker,

b) Supplemental Air Conditioning (SUPP A/C) Switch remains OFF, and

c) Associated Cabin Auxiliary Ground Heating System is considered inoperative and associated AUX HEAT Switch remains OFF.

NOTE: Deactivation of the

Supplemental Air Conditioning System also deactivates the Cabin Auxiliary Ground Heating System.

(M)May be inoperative provided:

a) System is deactivated by pulling and collaring the associated Circuit Breaker, and

b) FWD and AFT Supplemental Air Conditioning Switches remains OFF.

||||||||||||||||||||||||||||||



SF-340 DATE: 04/16/2012 21-10



21 AIR CONDITIONING


60-1 Compressor/Duct Overtemperature (L/R DUCT OV TEMP) Caution Indicators on Overhead Air Conditioning Panel (Mod. 2305 installed)

B 2 1 (M)(O)One may be inoperative provided:

a) Avionics Fan is verified to operate normally,

b) If Right Air Conditioning Pack is inoperative, all Windshield Heaters operate normally,

c) Ambient Air (Ram Air) Intake is extended,

d) Associated Bleed Valve (BLD VALVE) Switch remains CLOSED,

e) Associated Recirculation (L/R RECIRC) Fan remains OFF,

f) Flight time is limited to 2 hours or less, and aircraft is not dispatched if ground or flight temperatures are above ISA +20 deg C, or below ISA -20 deg C,

g) Airplane is not operated in known or forecast icing conditions,

h) MEA's on planned route of flight are 8,000 feet MSL, or less, and i) Alternate Abnormal Procedures for loss of a second Air Conditioning Pack are established and used.



SF-340 DATE: 04/16/2012 21-11



21 AIR CONDITIONING


NOTE: Icing Conditions exist any time weather conditions meet visibility and temperature Limits specified in the AFM for operation of Wing and

Stabilizer De-Icer Boots, and any time airplane ice accretion is known or is predicted to occur.

60-2 Cabin and Flight

Deck Automatic (AUTO) Temperature Control Systems

C 2 0 (O)May be inoperative provided: a) Associated Manual Temperature

Control System(s) operate normally,

b) Cabin Temperature Indicator, and L DUCT Temperature Indicator (if installed) operate normally,

c) Associated Recirculation Fan(s) operate normally, and their respective L/R RECIRC Switches remain ON, and

Alternate manual heating and cooling procedures are established and used.

60-3 Cabin and Flight

Deck Manual Temperature Control Systems

C 2 0 (O)May be inoperative provided associated Automatic (AUTO) Temperature Control System(s) operate normally.



SF-340 DATE: 04/16/2012 21-12



21 AIR CONDITIONING


60-4 CABIN Temperature, and, for Aircraft Serial No 139 and above, L DUCT Temperature

Indicator

C 1 0 May be inoperative provided Cabin and Flight Deck Automatic (AUTO) Temperature Control Systems operate normally. NOTE: The CABIN sensing position is

installed on the Temperature Indicators of all aircraft. Aircraft Serial Number 139, and above, also have an L DUCT sensing position on the Temperature Indicator.


AIRCRAFT: REVISION NO : 17 PAGE:

SF-340 DATE: 02/28/2011 22-1



22 AUTO FLIGHT


10-1 Autopilot System (Single or Dual Flight Director)

B 1 0 May be inoperative provided operational procedures and/or approach minimums do not require its use.

10-2 Autopilot System (Dual Flight Director)

Included in item 10-1, Rev. 4

10-3 Yaw Damper System B 1 0 May be inoperative provided:

a) Autopilot is considered inoperative, and b) Operational procedures and/or approach minimums do not require its use.

10-4 Autopilot Control Wheel Disengage Switches

C 2 1 One may be inoperative provided: a) Autopilot is not used below

1500 feet AGL, and b) Approach minimums do not

require use of Autopilot System.

B 2 0 Both may be inoperative provided:

a) Autopilot is considered inoperative, and b) Operational procedures and/or approach minimums do not require its use.



SF-340 DATE: 02/28/2011 22-2



22 AUTO FLIGHT


10-5 Autopilot Disconnect Aural Alert

B 1 0 May be inoperative provided: a) Autopilot is considered inoperative, and b) Operational procedures and/or approach minimums do not require its use.



SF-340 DATE: 02/28/2011 23-1



23 COMMUNICATIONS


10-1 Communications System (VHF and UHF)

D - - (M)Any in excess of those required by FAR may be inoperative provided: a) Radio is not powered by an Emergency Bus, and is not required for emergency procedures, and b) Inoperative Radio(s)are deactivated. NOTE: HF Communications System(s) moved to 23-10-4 Revision 16.

1) VHF Comm Control Units a) Transfer Buttons b) Frequency Selector Knobs c) Frequency Displays

C C C

- - -

0 2 2

10-2 Selective Call System(s) (SELCAL) *** 1) Individual Channels

C D C D

- - - -

0 0 0 0

(O)May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use. (O)May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.



SF-340 DATE: 02/28/2011 23-2



23 COMMUNICATIONS


10-3 Dual Tone *** Multifrequency Microphone (DTMF) (Telephone Dialing Feature)

C - 0 May be inoperative provided: a) Voice Mode operates normally, and b) Alternate communication procedures are established and used.

D - 0 May be inoperative provided:

a) Voice Mode operates normally, and b) Procedures do not require its use.

10-4 HF Communications *** System(s)

D - - (M)Any in excess of those required by FAR may be inoperative provided inoperative HF Radio(s) are deactivated.

22-1 ACARS System(s) ***

C D

- -

0 0

(M)(O)May be inoperative provided: a) Inoperative System(s) are deactivated, and b) Alternate procedures are established and used. (M)May be inoperative provided: a) Inoperative System(s) are deactivated, and b) Procedures do not require its use.



SF-340 DATE: 02/28/2011 23-3



23 COMMUNICATIONS


23-1 Tropospheric *** Airborne Meteorological Data Recording System (TAMDAR) (Installed IAW STC No. ST00545DE)

C 1 0 (O)May be inoperative provided alternate procedures are established and used.

1) Automatic Flight Time Reporting (OUT/OFF/ON/IN)

C 1 0 (O)May be inoperative provided alternate flight time recording and transmission procedures are established and used.

2) Weather Data Acquisition and Transmission

D 1 0 May be inoperative provided operational procedures are not dependant on its use.



SF-340 DATE: 02/28/2011 23-4



23 COMMUNICATIONS


30-1 Passenger Address System (PA) 1) Passenger Configuration a) Lavatory

Speaker

B C C

1 1 1

0 0 0

(O)May be inoperative provided: a) Alternate normal, abnormal, and emergency procedures, and/or operating restrictions are established and used, and b) Flight Attendant Alerting System (Audio and Visual) operates normally. NOTE: Any station function(s) that operate normally may be used. (O)May be inoperative provided: a) PA is not required by FAR, and b) Flight Attendant Alerting System (Audio and Visual) operates normally. NOTE: Any station function(s) that operate normally may be used. (O)May be inoperative provided alternate procedures are established and used. (Continued)



SF-340 DATE: 02/28/2011 23-5



23 COMMUNICATIONS


30-1 Passenger Address System (PA) (Cont'd) 2) Cargo Configuration a) Lavatory Speaker

C D C D

- - - -

0 0 0 0

(O)May be inoperative provided alternate normal, abnormal, and emergency procedures, and/or operating restrictions are established and used. May be inoperative provided procedures do not require its use. (O)May be inoperative provided alternate procedures are established and used. May be inoperative provided procedures do not require its use.

30-2 Crewmember Interphone System(s) 1) Passenger Configuration Flight Deck- to-Cabin, Cabin-to-Flight Deck Function(s)

B D

- -

0 0

(O)May be inoperative provided alternate communications procedures between affected flight attendant station(s) are established and used. NOTE: Any station function(s) that operate normally may be used. May be inoperative provided procedures do not require its use. NOTE: Any station function(s) which operate normally may be used. (Continued)



SF-340 DATE: 02/28/2011 23-6



23 COMMUNICATIONS


30-2 Crewmember Interphone System(s) (Cont’d) 1) Passenger Configuration Flight Deck- to-Cabin, Cabin-to-Flight Deck Function(s) (Cont’d)

a) Flight Deck Handset System

C D

- -

0 0

(O)May be inoperative provided: a) Headset Function of Flight Deck to Cabin Crewmember Interphone System operates normally, and b) Alternate procedures are Established and used. May be inoperative provided procedures do not require its use.

b) Crewmember Interphone Alerting System (Audio/Visual) 1) Flight Deck Deck Call, Visual Alerting System

B

1

0

May be inoperative provided Flight Deck Audio Alerting System operates normally. NOTE: Flight Deck Audio Alerting System must always operate normally. (Continued)



SF-340 DATE: 02/28/2011 23-7



23 COMMUNICATIONS



b) Crewmember Interphone Alerting System (Audio/Visual) (Cont’d)

2) Flight Attendant Call, Visual Alerting System

B 1 0 (O)May be inoperative provided: a) Passenger Address (PA) System operates normally, and b) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Flight Attendant Call System is considered Non-Essential Equipment and Furnishings (NEF). NOTE 2: Any Visual Alerting System Function(s) that operates Normally may be used.

(Continued)



SF-340 DATE: 02/28/2011 23-8



23 COMMUNICATIONS



b) Crewmember Interphone Alerting System (Audio/Visual) (Cont’d)

3) Flight Attendant Call, Audio Alerting System

B 1 0 (O)May be inoperative provided: a) Passenger Address (PA) System operates normally, and b) Alternate procedures for contacting flight attendants are established and used. NOTE 1: Passenger to Flight Attendant Call System is considered Non-Essential Equipment and Furnishings (NEF). NOTE 2: Any Audio Alerting System Function(s) that operates Normally may be used.

(Continued)



SF-340 DATE: 02/28/2011 23-9



23 COMMUNICATIONS


30-2 Crewmember Interphone System(s) (Cont’d)

2) Cargo Configuration - Flight Deck-to- Cabin, Cabin- To-Flight Deck Function(s)

a) Flight Deck Handset System

C D C D

- - - -

0 0 0 0

(O)May be inoperative provided alternate normal, abnormal and emergency communications procedures are established and used. NOTE: Any station function(s) which operate normally may be used. May be inoperative provided procedures do not require its use. NOTE: Any station function(s) which operate normally may be used. (O)May be inoperative provided: a) Headset Function of Flight Deck to Cabin Crewmember Interphone System operates normally, and b) Alternate procedures are Established and used. May be inoperative provided procedures do not require its use.

b) Crewmember Interphone Alerting System (Audio/Visual)

1) Flight Deck Call, Visual

Alerting System

B D

- -

0 0

May be inoperative provided Flight Audio Alerting System operates normally. May be inoperative provided procedures do not require its use.



SF-340 DATE: 02/28/2011 23-10



23 COMMUNICATIONS


30-3 Automated *** Passenger Address System

C D

1 1

0 0

(O)May be inoperative provided: a) Passenger Address System operates normally, and b) Alternate normal, and, as appropriate, abnormal and emergency procedures are established and used. May be inoperative provided procedures do not require its use.

35-1 Active Noise *** Control System

D 1 0 (M)May be inoperative provided system is deactivated.

50-1 Audio Selector Panels

Deleted, Rev. 4.

50-2 Cockpit Loudspeakers

C 2 0 (O)May be inoperative provided: a) Pilot to Pilot Intercom System is verified to operate normally before departure, and b) Pilots wear operative headsets throughout flight.

50-3 Ground-To-Cockpit *** Intercom System

C D

- -

0 0

(O)May be inoperative provided alternate ground-cockpit communication procedures are established and used. May be inoperative provided procedures do not require its use.

50-4 Ground-To-Cockpit *** Intercom System Chime

C D

- -

0 0

(O)May be inoperative provided alternate ground-cockpit communication procedures are established and used. May be inoperative provided procedures do not require its use.



SF-340 DATE: 02/28/2011 23-11



23 COMMUNICATIONS


50-5 Boom Microphones A - 0 May be inoperative provided: a) Normally operating Hand-Held Microphone(s) are installed on affected side(s), b) Flight Data Recorder (FDR) operates normally, and c) Repairs are made within three flight days.

60-1 Static Dischargers Deleted Revision 16.

NOTE: Allowances and procedures for broken or missing Static Dischargers are contained in the Configuration Deviation List (CDL).

70-1 Cockpit Voice Recorder (CVR)

A 1 0 May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days.



SF-340 DATE: 02/28/2011 24-1



24 ELECTRICAL POWER


21-1 AC Generators

B 2 1 (M)(O)One may be inoperative provided: a) Associated AC Generator is visually inspected to verify there are no indications of damage or oil leakage, b) Associated AC GEN Switch on ENGINE Panel remains in OFF/R, and c) Airplane is not operated in known or forecast icing conditions as defined in the AFM pertaining to activation of Engine Inlet Anti-Icing.

22-1 AC GEN Caution Lights

B 2 1 (O)One may be inoperative provided: a) Associated AC Generator is verified to operate normally before departure, b) Associated L/R INTAKE Caution and associated L/R ENG ANTI-ICE Status Lights are verified to operate normally before departure, c) Engine Air Intake Anti-Ice Systems are verified to operate normally before departure, and d) Alternate procedures are established and used during flight to assure that Engine Air Intake Anti-Ice is verified to operate normally prior to operations in temperatures of +10 degrees C, or less. NOTE: Not required for an inoperative AC Generator.



SF-340 DATE: 02/28/2011 24-2



24 ELECTRICAL POWER


24-1 Main AC Inverter(s) 1) Mod. 2024 Not Installed (System with Single Main AC Inverter and a 26V AC Standby Inverter) a) TAWS/GPWS Installed

A

1

0

(O)May be inoperative provided: a) Standby 26 V AC Inverter is verified to operate normally before departure, b) Standby VOR/ILS Indicator operates normally, c) Weather Radar is not required, d) Flight is conducted in day-VMC conditions, e) Alternate VOR/ILS navigation procedures are established and used for in-flight loss of Standby 26V AC Inverter, f) TAWS/GPWS is considered inoperative, and alternate procedures for loss of TAWS/GPWS are established and used, and g) Repairs are made within two flight days. NOTE: Subsequent loss of 26 V AC Standby Inverter will result in loss of VOR/ILS course information on both EHSI's and RMI's. Standby VOR/ILS Indicator will not be affected. (Continued)



SF-340 DATE: 02/28/2011 24-3



24 ELECTRICAL POWER


24-1 Main AC Inverter(s) (Cont'd) 1) Mod. 2024 Not Installed (System with Single Main AC Inverter and a 26V AC Standby Inverter) (Cont'd) b) TAWS/GPWS Not Installed

B

1

0

(O)May be inoperative provided: a) Standby 26 v AC Inverter is verified to operate normally before departure, b) Standby VOR/ILS Indicator operates normally, c) Weather Radar is not required, d) Flight is conducted in day-VMC conditions, e) Alternate VOR/ILS navigation procedures are established and used for in-flight loss of Standby 26 V AC Inverter. NOTE: Subsequent loss of 26 V AC Standby Inverter will result in loss of VOR/ILS course information on both EHSI's and RMI's. Standby VOR/ILS Indicator will not be affected. (Continued)



SF-340 DATE: 02/28/2011 24-4



24 ELECTRICAL POWER


24-1 Main AC Inverter(s) (Cont'd) 2) Mod. 2024 Installed (System with Two Main 115/26 V AC Inverters)

B

2

1

(O)One may be inoperative provided: a) Standby VOR/ILS operates normally, and b) Alternate VOR/ILS navigation procedures are established and used in event of in-flight loss of remaining 115/26 V AC Inverter. NOTE: Subsequent loss of 115/26 V AC Main Inverter will result in loss of VOR/ILS course Information on both EHSI's and RMI's. Standby VOR/ILS Indicator will not be affected.

24-2 Standby 26V AC Inverter (Mod. 2024 not Installed – System with Single Main AC Inverter and a 26V AC Standby Inverter)

B 1 0 (O)May be inoperative provided: a) Main 115 V AC Inverter operates normally, b) Standby VOR/ILS Indicator operates normally, and c) Alternate VOR/ILS navigation procedures are established and used for in-flight loss of Main AC Inverter. NOTE: Subsequent loss of 115/26 V AC Main Inverter will result in loss of VOR/ILS course Information on both EHSI's and RMI's. Standby VOR/ILS Indicator will not be affected.

31-1 DC Generator Functions

Deleted Revision 1.



SF-340 DATE: 02/28/2011 24-5



24 ELECTRICAL POWER


32-1 DC L GEN, R GEN Caution Lights

Deleted Revision 16.

32-2 DC GEN OV TEMP Caution Lights

Deleted Revision 16.

32-3 DC Voltmeter Deleted Revision 5 32-4 DC Ammeter Deleted Revision 1. 34-1 Batteries Deleted Revision 1. 34-2 L BAT, R BAT Caution Lights

C 2 1 (O)One may be inoperative provided: a) Associated Battery Ventilation System operates normally, b) Associated BAT HOT Indication is verified to operate normally before departure, and c) Before departure, DC Voltmeter is used to verify that affected Battery is being supplied by associated Generator.

34-3 BAT HOT Caution Lights

C 2 1 (M)(O)May be inoperative provided: a) Associated Battery Ventilation System operates normally, b) Associated BAT Caution Light operates normally, c) Associated BAT TEMP Indicator operates normally, d) Automatic Battery Temperature Disconnect (71 degrees C Switch) is verified to operate normally, e) Procedures are established and used to assure associated Battery Temperature is monitored throughout the flight, and f) Alternate Battery Hot Abnormal Procedures are established and used.



SF-340 DATE: 02/28/2011 24-6



24 ELECTRICAL POWER


35-1 DC Emergency Power Supply

Deleted, Revision 16.

36-1 Battery Ventilating Systems

C 2 0 (O)May be inoperative provided: a) Associated BAT HOT Caution Light(s) and L BAT/R BAT Caution Light(s) operate normally, b) Battery Temperature Indicator operates normally, c) When Ground Power is in use, associated Battery (BAT) Switch(es) are not selected to OVRD, d) During ground Engine Operations of more than 30 Minutes, with aircraft stationary, associated Battery (BAT) Switch is selected OFF, and e) Alternate procedures are established and used to assure that affected Battery (BAT) Switch(es) are selected ON prior to takeoff.

37-1 Battery Temperature Indicator

C 2 0 (M)(O)May be inoperative provided: a) Battery Ventilation Systems operate normally, b) BAT HOT Cautions Lights are verified to operate normally, c) Adequate Battery Charge is verified on the associated Battery before departure, and d) OAT at takeoff is above -20 Degrees C.

40-1 External Power System

C 1 0 (O)May be inoperative provided alternate procedures are established and used.



SF-340 DATE: 02/28/2011 24-7



24 ELECTRICAL POWER


52-1 DC Utility Bus C 1 0 May be inoperative provided the following equipment is considered inoperative: Galley Hot Water Pots & Oven (if installed), Passenger Reading Lights, Passenger Cabin Attendant Call, Tail Compartment Shutoff Valve (if Mod. 1991 installed), Lavatory Water Heater (if installed), Pilot Footwarmer (if installed), Flight Attendant Seat Heater (if installed), Active Noise Control (if installed), Heating for Tropospheric Airborne Meteorological Data Recording System (TAMDAR)(if installed).



SF-340 DATE: 02/28/2011 25-1

2. NUMBER INSTALLED SYSTEM & 1. SEQUENCE ITEM NUMBER 3. NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHINGS


00-1 Crewmember Shoulder Harness

Deleted Revision 4

21-1 Flight Attendant Seat Assembly

A 1 0 (M)(O)May be inoperative provided: a) Affected Seat is not occupied, b) Flight Attendant displaced by inoperative Seat Assembly occupies the Passenger Seat most accessible to the inoperative Flight Attendant Seat Assembly, c) Alternate procedures are established and used and published in the crew members' manuals, d) Folding type Seat is stowed or secured in the retracted position, e) Passenger Seat assigned to Flight Attendant is placarded "FOR FLIGHT ATTENDANT USE ONLY", and f) Repairs are made within two(2) flight days. (Continued)



SF-340 DATE: 02/28/2011 25-2




21-1 Flight Attendant Seat Assembly (Cont'd)

NOTE 1: An automatically folding Seat that will not stow automatically is considered inoperative. NOTE 2: A Seat with an inoperative or missing Restraint System (Seat Belt and Shoulder Harness) is considered inoperative. NOTE 3: The above provisos apply only to required flight attendant seats. Individual operators, when operating with inoperative Flight Attendant Seat Assemblies, shall consider location and combination of Seats to ensure that FAR proximity to Exits and distribution requirements are met. (Continued)



SF-340 DATE: 02/28/2011 25-3




21-1 Flight Attendant Seat Assembly (Cont'd)

D - - (M)May be inoperative provided: a) Flight Attendant Seat is not

required by FAR, b) Affected Seat or Seat Assembly

is not occupied, and c) Folding type Seat or Seat

Assembly stows automatically or is secured in the retracted position.

NOTE 1: An automatically folding Seat that will not stow automatically is considered inoperative. NOTE 2: A Seat with an inoperative or missing Restraint System (Seat Belt and Shoulder Harness) is considered inoperative.

21-2 Cabin Emergency Flashlight Holder/ Flashlight 1) Flashlight(s) 2) Flashlight Holder(s) 3) Aircraft in All- Cargo Configuration

C C D

- - -

0 0 0

(O)May be inoperative or missing provided the crewmember assigned to the associated seat has an approved flashlight of equivalent characteristics readily available. (M)(O)May be inoperative or missing provided alternate storage procedures are established and used.



SF-340 DATE: 02/28/2011 25-4




21-3 Overhead Storage Bin(s)/Cabin and Galley Storage Compartment(s)/ Closet(s) 1) Airplanes with GEN I Interiors

C

-

-

(M)(O)May be inoperative provided: a) Doors of inoperative Bin(s), Compartment(s), and Closet(s) are either secured closed, or removed, b) Inoperative Bin(s), Compartment(s), and

Closet(s) are prominently placarded “DO NOT USE,” and are not used for storage except for items permanently affixed, c) Emergency Equipment located in inoperative Bin(s), Compartment(s), and Closet(s) which are secured closed, is considered inoperative, and associated MEL relief provisions are applied, d) Procedures are established and used to alert crewmembers and passengers of inoperative Bin(s), Compartment(s), and Closet(s), e) Passengers are briefed that inoperative Bin(s), Compartment(s), and Closet(s) are not to be used for storage. (Continued)



SF-340 DATE: 02/28/2011 25-5




21-3 Overhead Storage Bin(s)/Cabin and Galley Storage Compartment(s)/ Closet(s) 1) Airplanes with GEN I Interiors (Cont’d)

C

-

-

NOTE 1: If no partitions are installed in Overhead Storage Bin(s), the entire unit is considered one Storage Bin. NOTE 2: Accessible Emergency Equipment located in inoperative Overhead Storage Bin(s), Galley Storage Compartment(s), and Closet(s) which are not secured closed, is available for use. (Continued)



SF-340 DATE: 02/28/2011 25-6




21-3 Overhead Storage Bin(s)/Cabin and Galley Storage Compartment(s)/ Closet(s) (Cont’d)

2) Aircraft with GEN II, or GEN III Interiors

C

-

-

(M)(O)May be inoperative provided: a) Doors of inoperative Overhead Storage Bin(s) are removed, b) Doors of inoperative Galley Storage Compartment(s), and Closet(s) are either removed, or secured closed, c) Inoperative Bin(s), Compartment(s), and Closet(s) are prominently placarded “DO NOT USE,” and are not used for storage except for items permanently affixed,

d) Emergency Equipment located in inoperative Bin(s), Compartment(s), and Closet(s) which are secured closed, is considered inoperative, and associated MEL relief provisions are applied, e) Procedures are established and used to alert crewmembers and passengers of inoperative Bin(s), Compartment(s), Closet(s), and f) Passengers are briefed that inoperative Bin(s), Compartment(s), and Closet(s) are not to be used for storage. (Continued)



SF-340 DATE: 02/28/2011 25-7




21-3 Overhead Storage Bin(s)/Cabin and Galley Storage Compartment(s)/ Closet(s) (Cont’d)

2) Aircraft with GEN II, or GEN III

Interiors (Cont’d)

NOTE 1: If no partitions are installed in Overhead Storage Bin(s), the entire unit is considered one Storage Bin. NOTE 2: Accessible Emergency Equipment located in inoperative Overhead Storage Bin(s) is available for use.



SF-340 DATE: 02/28/2011 25-8




23-10 Flight Deck Door Surveillance System(s)

1) Electronic Flight Deck Door Surveillance System ***

a) Cargo Configuration

A C D C D

1 1 1 1 1

0 0 0 0 0

(O)May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

(O)May be inoperative provided: a) Flight Deck Door Viewing Port is Installed and operates normally, and b) Alternate procedures are established and used. May be inoperative provided procedures do not require its use. May be inoperative provided Courier/Supernumerary Compartment (if installed) remains unoccupied. May be inoperative provided procedures do not require its use. (Continued)



SF-340 DATE: 02/28/2011 25-9




23-10 Flight Deck Door Surveillance System(s) (Cont’d)

2) Viewing Port *** a) Cargo

Configuration

A C C D

1 1 1 1

0 0 0 0

(O)May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days.

(O)May be inoperative provided: a) Electronic Flight Deck Door Surveillance System is installed and operates normally, and b) Alternate procedures are established and used. May be inoperative provided Courier/Supernumerary Compartment (if installed) remains unoccupied. May be inoperative provided procedures do not require its use.

41-1 Exterior Lavatory Door Ashtray

A 1 0 May be missing provided it is replaced within 3 calendar days.



SF-340 DATE: 02/28/2011 25-10




60-1 Emergency *** Locator Transmitter (ELT)

1) Survival Type ELT(s) ***

2) Fixed ELT(s) ***

D A A D D

- - - - -

- 0 0 - -

Any in excess of those required by FAR may be inoperative or missing. (M)May be inoperative provided; a) System is deactivated, and b) Repairs are made within 90 calendar days May be missing provided repairs are Made within 90 calendar days. (M)Any in excess of those required by FAR may be inoperative provided system is deactivated. Any in excess of those required by FAR may be missing.



SF-340 DATE: 02/28/2011 25-11




60-2 Observer Seat (Including Associated Equipment)

A A

1 1

0 0

May be inoperative provided: a) A Passenger Seat in the Passenger Cabin is made available to an FAA inspector for the performance of official duties, and b) Repairs are made within two flight days. May be inoperative provided: a) Required minimum safety equipment (Seat Belt with Shoulder Harness, Oxygen) is available, b) Seat is acceptable to the FAA Inspector for the performance of official duties, and c) Repairs are made within two flight days.

NOTE 1: These provisions are

intended to provide for occupancy of the above Seats by an FAA Inspector when the minimum safety equipment (seat belt with shoulder harness, oxygen) operates normally, and the Inspector determines that the conditions are acceptable. NOTE 2: The Pilot-in-Command will determine if the minimum safety equipment is functional and satisfactory for occupancy of other persons authorized to occupy the Observers Seat.



SF-340 DATE: 02/28/2011 25-12




60-3 Passenger Seats D - - May be inoperative provided: a) Affected Seat(s) do not block an Emergency Exit, b) Affected Seat(s) do not restrict any passenger from access to the main aircraft aisle, and

c) Affected Seat(s) are blocked and placarded "DO NOT OCCUPY". NOTE 1: A seat with inoperative Seat Belt is considered inoperative. NOTE 2: Inoperative Seats do not affect the required number of Flight Attendants. NOTE 3: Affected Seat(s) may include Seat(s) behind and/or adjacent to outboard Seats.

1) Recline Mechanism(s)

D D

- -

- -

(M)May be inoperative, and the Seat(s) occupied, provided affected Seat Back(s) are secured in the full up-right position. May be inoperative, and Seat(s) occupied, provided affected Seat Back(s) are immovable in the full upright position. (Continued)



SF-340 DATE: 02/28/2011 25-13




60-3 Passenger Seats (Cont'd) 2) Underseat Baggage Restraining Bars 3) Armrests a) Non-GEN III Interiors (Serial # prior to 359)

C D

- -

- -

(O)May be inoperative provided: a) Baggage is not stowed under Seat(s) with inoperative Restraining Bar(s), b) Associated Seat(s) are placarded "DO NOT STOW BAGGAGE UNDER THIS SEAT," and c) Procedures are established and used to alert Cabin Crew of inoperative Restraining Bar(s) May be inoperative or missing, and associated Seat occupied, provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the main aircraft aisle, and c) For an Armrest on a Seat with a Recline Mechanism, Seat is secured in the full upright position. (Continued)



SF-340 DATE: 02/28/2011 25-14




60-3 Passenger Seats (Cont'd) 3) Armrests (Cont’d) b) GEN III Interiors (Serial # 359 And after)

D

-

-

May be inoperative in the full-down position, and associated Seat occupied, provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the main aircraft aisle, and c) For an Armrest on a Seat with a Recline Mechanism, Seat is secured in the full upright position. NOTE: Per affixed Placard, Arm Rests

on aircraft with GEN III Interiors must be down for takeoff.

60-4 "FASTEN SEAT BELT WHILE SEATED" Signs and Placards

C - - One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is readable from each occupied Passenger Seat.



SF-340 DATE: 02/28/2011 25-15




60-5 Non-Essential Equipment & Furnishings (NEF)

- 0 May be inoperative, damaged, or missing, provided that the item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to flight crew and included in the operator’s appropriate document. NOTE 1: EXTERIOR LAVATORY DOOR ASHTRAYS ARE NOT CONSIDERED CONVENIENCE ITEMS. NOTE 2: Trolley Turn Buttons, which secure Galley Cart(s), are not considered Passenger Convenience Items.

60-6 9-G Cargo Restraining Net(s) (Cargo Airplanes)

C - - (M) May be inoperative, or missing provided associated compartment(s) remains empty.

60-7 Galley Waste Receptacle Access Doors/Covers

C - - (M)(O)May be inoperative provided: a) Associated Waste Receptacle(s) remain empty, b) Access to affected Waste Receptacle(s) is secured to prevent introduction of waste, and c) Procedures are established and used to ensure that a sufficient, operative Galley Waste Receptacles are available to accommodate all waste generated on the flight.



SF-340 DATE: 02/28/2011 25-16




60-8 Cargo Restraint Systems

A C

- -

- -

(M)May be inoperative, or missing, provided: a) Acceptable cargo loading limits from Approved source, i.e., an Approved Cargo Loading Manual, Approved Cargo Handling Manual, or Approved Weight and Balance Manual, are observed, and b) Repairs are made prior to completion of the next heavy maintenance visit.

May be inoperative, or missing, provided cargo compartment remains empty.

62-10 Emergency Medical Kit (EMK), and/or Associated Equipment

A D

- -

0 -

(O)May be inoperative provided: a) Inoperative Emergency Medical Kit(s) remaining aboard the airplane are resealed in a manner that clearly identifies them such that they cannot be mistaken for serviceable EMK’s, and b) Repairs or replacement is made within three flight cycles.

(O)Emergency medical Kits (EMK)’s in excess of those required by FAR may be missing, incomplete, or inoperable, provided, inoperable EMK(s) remaining aboard the airplane are resealed in a manner that clearly identifies them such that they cannot be mistaken for serviceable EMK’s.



SF-340 DATE: 02/28/2011 25-17




62-10 Automatic External Defibrillator (AED) and/or Associated Equipment

A - 0 (O)May be missing or inoperative provided: a) Inoperative Automatic External Defibrillator’s (AED’s) remaining aboard the airplane are resealed in a manner that clearly identifies them such that they cannot be mistaken for serviceable AED’s, and b) Repairs or replacement is made

within three flight cycles.

D - - (O)Automatic External Defibrillator

(AED)’s in excess of those required by FAR may be missing or inoperative, provided, inoperative AED’s remaining aboard the airplane, are resealed in a manner that clearly identifies them such that they cannot be mistaken for serviceable AED’s.



SF-340 DATE: 02/28/2011 26-1



26 FIRE PROTECTION


11-1 Engine Fire Detection System

Deleted Revision 1.

11-2 Engine Fire Warning Lights (Secondary Warnings on CWP)

B 2 0 (O)May be inoperative provided Associated ENG Fire Pull Handle Light(s), and Synthetic Fire Bell are verified to operate normally before departure.

11-3 Engine Fire Pull Handle Lights

Deleted Revision 1.

11-4 Synthetic Fire Bell Deleted Revision 1. 13-1 Lavatory Smoke Detection System

1) Passenger Configuration

2) Cargo Configuration

C D

1 -

0 0

May be inoperative provided: a) Lavatory Waste receptacle remains empty, b) Associated Lavatory Door is locked closed, and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. NOTE: These provisos are not intended to prohibit Lavatory use or inspection by crewmembers.



SF-340 DATE: 02/28/2011 26-2



26 FIRE PROTECTION


13-2 Cargo Compartment Smoke Detection System (Passenger and All Cargo Airplanes)

C - 0 (O)May be inoperative provided procedures are established and used to ensure the associated compartment remains empty, or is verified to contain only empty cargo handling equipment, ballast (ballast may be loaded in ULDs, and /or fly away kits. NOTE: Operator MEL's must define which items are approved for inclusion in the Fly Away Kits, and which materials can be used as ballast.

13-3 Avionic Rack Smoke Detection System

B 1 0 (M)May be inoperative provided the Avionic Rack Door is removed.

21-1 Engine Fire Extinguishing System

Deleted Revision 1.



SF-340 DATE: 02/28/2011 26-3



26 FIRE PROTECTION


22-1 Portable Fire Extinguisher(s)

D - - (O)Any in excess of those required by FAR may be inoperative, or missing, provided: a) Inoperative Portable Fire Extinguisher(s) remaining aboard the airplane are tagged “INOPERATIVE,” removed from their installed location(s), and secured out of sight such that they cannot be mistaken for functional Units, and. b) Required distribution of operative Portable Fire Extinguishers is maintained.

22-2 Lavatory Fire Extinguisher System

1) Passenger

Configuration C C

- -

0 0

May be inoperative provided associated Lavatory Smoke Detection System operates normally. (M)(O)May be inoperative provided: a) Lavatory Waste Receptacle remains empty, b) Associated Lavatory Door is locked closed, and placarded, "INOPERATIVE - DO NOT ENTER", and c) Lavatory is used only by crewmembers. NOTE: These provisos are not intended to prohibit Lavatory use or inspection by crewmembers.

2) Cargo Configuration

D - 0



SF-340 DATE: 02/28/2011 27-1



27 FLIGHT CONTROLS


12-1 Aileron (ROLL) Trim Systems

B 2 1 (M)(O)One may be inoperative provided: a) Before departure, qualified pilot(s) or maintenance personnel visually verify that Rudder (YAW) Trim operates Normally through full range of travel, and b) Associated Trim Tab is secured in the Neutral position. NOTE 1: Aileron (ROLL) Trim adjustment will be limited. NOTE 2: Autopilot may be used.

13-1 Aileron (ROLL) Trim Indicators

C 2 1 (O)One may be inoperative provided: a) Affected Aileron (ROLL) Trim Operates normally, b) Before departure, qualified pilot(s) or maintenance Personnel visually verify that Aileron (ROLL) Trim operates Normally through full range of travel, and c) Before Takeoff, qualified pilot(s) or maintenance Personnel visually verify that affected Aileron Trim Tab is in the Neutral position. NOTE: Autopilot may be used.



SF-340 DATE: 02/28/2011 27-2



27 FLIGHT CONTROLS


21-1 Rudder Limiter C 1 0 (M)(O)May be inoperative provided: a) Rudder Limiter System is deactivated, b) Rudder Limiter Switch remains in OVRD, c) Before departure, qualified pilot(s) or maintenance personnel visually verify that Rudder operates normally through full range of travel, d) Airspeed remains at or below 180 KIAS, e) Procedures are established and used to assure that large Rudder deflections are avoided above an airspeed of 150 KIAS, and f) For airplanes without Modification 2310 installed, 25-30% torque is maintained when De-ice Boot inflation is required. NOTE: RUDDER LIMIT Caution will remain illuminated.

22-1 Rudder Trim System Deleted Revision 1. 23-1 Rudder (YAW) Trim Indicator

C 1 0 (O)May be inoperative provided: a) Rudder (YAW) Trim operates normally, b) Before departure, qualified pilot(s) or maintenance personnel visually verify that Rudder (YAW) Trim operates normally through full range of travel, and c) Before Takeoff, qualified pilot(s) or maintenance Personnel visually verify that Rudder Trim Tab is in the Neutral position.



SF-340 DATE: 02/28/2011 27-3



27 FLIGHT CONTROLS


32-1 Elevator (PITCH) Trim Synchronizer System

B 1 0 (M)(O)May be inoperative provided: a) Elevator (PITCH) Trim Synchronizer System is deactivated and secured, b) Before departure, Main Pitch Trim System (MAIN PITCH) on Control Yoke and Standby Pitch Trim System (STBY PITCH) on Center Pedestal, are verified to operate normally through full range of travel, c) Before departure, Elevator (MAIN PITCH/STBY PITCH) Trim Indicators on Trim Indicator are verified to operate normally through full range of travel, d) Procedures are established and used to assure that maximum split between MAIN PITCH and STBY PITCH Indications remain within one unit during flight at speeds greater than 180 KIAS, and e) If Autopilot is used, procedures are established and used to assure that Autopilot and Yaw Damper are disengaged if yellow "EL" annunciation appears on EADI.

NOTE 1: Pilots should be prepared

for possible pitch mistrim when Autopilot is disengaged following annunciation of yellow EL on EADI. NOTE 2: PITCH TRIM Caution will be illuminated when Pitch Trim Synchronizer System is deactivated.



SF-340 DATE: 02/28/2011 27-4



27 FLIGHT CONTROLS


33-1 Elevator Trim Indicators (MAIN PITCH/STBY PITCH)

C 2 1 (O)Either the MAIN PITCH, or the STBY PITCH Indicator may be inoperative provided: a) Elevator (PITCH) Trim Synchronizer System operates normally, b) Before departure, qualified pilot(s) or maintenance personnel visually verify that Associated Elevator (PITCH) Trim Tab operates normally through full range of travel, c) Before departure, qualified pilot(s) or maintenance personnel visually verify that Elevator Trim Tabs are synchronized, and d) Procedures are established and used to assure that, in the event of an in-flight failure of the Elevator (PITCH) Trim Synchronizer System and illumination of the PITCH TRIM Caution, airspeed remains at or below 180 KIAS.

35-1 Stall Warning System Deleted Revision 1. 35-2 Stall Identification System (Stick Pusher)

Deleted Revision 1.

35-3 Stick Pusher System Status Indications (PUSH1/PUSH2)

C 4 2 (O)One Status Indication for each System (PUSH1, and/or PUSH2) may be inoperative, provided normal operation of the Stick Pusher System is verified before departure.



SF-340 DATE: 02/28/2011 27-5



27 FLIGHT CONTROLS


53-1 Flap Position Indications (Pointer Needles)

C 2 1 (O)One Pointer Needle may be inoperative provided Flap System is verified to operate normally through full range of travel.

72-1 Gust Lock System Deleted, Rev. 8.



SF-340 DATE: 02/28/2011 28-1



28 FUEL


21-1 Single Point Pressure Refueling System

C 1 0 (M)May be inoperative provided overwing fueling is used.

21-2 Defuel Valve C 1 0 (M)May be inoperative deactivated

Closed.

21-3 Pressure Fueling Cap C 1 0 22-1 Standby DC Pumps (A Model Only)

Deleted Revision 5.

22-2 L/R STBY PRESS Lights

B 2 1 (O)One may be inoperative provided: a) L/R MAIN PUMP Lights are verified to operate normally b) Associated Standby Pump

Automatic Control Mode operates normally,

c) XFEED ON Caution Light operates normally, d) Interconnect Valve and CONN VLV OPEN Caution Light operate normally, and e) Associated Standby Pump is verified to operate normally before departure.

22-3 Interconnect Shutoff Valve

C 1 0 (M)May be inoperative provided: a) Interconnect Valve is deactivated CLOSED, b) L/R STBY PRESS Lights operate normally, c) Cockpit Fuel Quantity Indicators operate normally, and d) Both Standby Pumps are verified to operate normally.



SF-340 DATE: 02/28/2011 28-2



28 FUEL


22-4 CONN VLV OPEN Caution Light

C 1 0 (M)May be inoperative provided: a) Interconnect Valve is deactivated Closed, b) L/R STBY PRESS Lights operate normally, c) Cockpit Fuel Quantity Indicators operate normally, and d) Both Standby Pumps are verified to operate normally.

22-5 Crossfeed Valve Deleted Revision 1. 22-6 XFEED ON Caution Light

C 1 0 (O)May be inoperative provided: a) L/R STBY PRESS Lights operate normally, and b) Crossfeed Valve is verified to operate normally before departure.

22-7 Standby Pump (STBY PUMP) Automatic Control Modes

C 2 0 (O)May be inoperative provided: a) L/R STBY PRESS Lights operate normally, b) L/R Standby Pumps are verified to operate normally, and c) Affected STBY PUMP Switch(es) remain in OVRD for Engine Start, Takeoff, Approach and Landing.

41-1 Cockpit Fuel Quantity Indicators

C 2 1 (M)One may be inoperative provided: a) Associated LOW LEVEL Caution is verified to operate normally, b) Fuel Flow Indicators operate normally, and c) Fuel quantity in associated tank is verified by an accepted procedure before departure.



SF-340 DATE: 02/28/2011 28-3



28 FUEL


41-2 Fueling Panel Fuel Quantity Indicators

C 2 0 (M)May be inoperative provided fuel quantity in associated tank(s) is verified by an accepted procedure before departure.

41-3 L/R LOW LEVEL Caution Lights

C 2 1 (M)May be inoperative provided associated Cockpit Fuel Quantity Indicator is verified to operate normally.

41-4 Fuel Quantity Test Function

C 1 0 (M)May be inoperative provided both Cockpit Fuel Quantity Indicators are verified to operate normally.

41-5 FUELING Status Light (on Ground Status Panel)

C 1 0 (M)(O)May be inoperative provided: a) Defuel Valve is deactivated Closed, and DE-FUEL Switch remains CLOSED. b) Single point refueling is not used, c) Acceptable alternate means of fueling is used, and d) Wing FUEL Panel Control Switch and both Fuel Tank FUEL LEVEL Switches are verified OFF before departure.

41-6 L/R VALVE CLOSED Caution Lights (Firewall Shutoff Valves)

C 2 0 (M)May be inoperative provided normal Firewall Shutoff Valve operation is verified once each flight day.

42-1 Dipsticks C 2 0 (M)May be inoperative provided fuel

quantity in associated Fuel Tank(s) is verified by an accepted procedure before departure.



SF-340 DATE: 02/28/2011 28-4



28 FUEL


44-1 Fuel Temperature Indication System

C 1 0 (O)May be inoperative provided: a) Departure fuel temperature is determined to be within AFM Temperature Limitations, and b) Flight is conducted at altitudes at which OAT and SAT are within AFM Fuel Temperature Limitations.



SF-340 DATE: 02/28/2011 29-1



29 HYDRAULIC POWER


10-1 Electric Driven Hydraulic Pump

Deleted, Rev. 1.

10-2 Automatic Hydraulic Pump Control

Documents

Revision: 17a Date: 04/16/2012 DEPARTMENT OF ... rev 17a.pdfSAAB SF-340 SAAB-340A, SAAB-340B, SAAB-340B+, SAAB-340WT Gary L. Larsen, Chairman Flight Operations Evaluation Board Federal