2015- 07- 03

Saab Aircraft AB Handled by

Date

Your date Reference

Your reference Matilda Krig

OFIC- 0- 2015- 0008
Saab AB, Aeronautics

Int + 46 13 18 20 00 Int + 46 13 18 44 95 S- 581 88 LINKÖPING Postal address Saab Aircraft AB Telephone Telefax Nat 013 - 18 20 00

SWEDEN Nat 013 - 18 44 95 Saab AB Page 1 (1) To: All holders of an Airplane Flight Manual AFM 340 B, code 010.

Subject: Revision No. 28 Date: Mar 27/1 5

Page Code Reason for change
1- 4 010 Revised to reflect changes in this revision. 1- 5 010 - ”- . 1- 6 010 - ”- . 1- 7 010 - ”- . 2- 9 010 Eastman Turbo Oils (ETO) added as approved oils for engine and propeller gearbox. The ETOs are identical to the corresponding BP Turbo Oils (e.g. ETO 2380 is identical to BP Turbo Oil 2380). 2- 15 010 Mod. No. corrected. Previously 3313, now 3530. 2- 16 010 Limitation regarding flap setting for landing with TIMER master caution together with the STAB light not illuminating (indicating a faulty ST AB boot system) added. 4- 4 010 AOM Alert Operations Bulletin (AOB) No. 12 regarding “Ruptured de- ice boots” implemented in AFM. General information from AOB: There has been reported events with ruptured de- ice boots on the horizontal tail. Recently an event with a ruptured de- ice boot resulted in slight vibrations starting at a speed of approximately 220 KIAS, with a gradual increase in vibrations with decreasing speed. With flap 15 selected, a further increase in vibrations was noted. Selection of flap 20 resulted in a repetitive nose down pitch every 3 to 4 seconds together with rumbling and shaking of the flight controls. The nose down pitch was counteracted by pilot input and a go- around was initiated. The aircraft made a flap- less (flap 0) landing with only slight vibrations felt in the flight controls. The following recommendation from AOB added in Abnormal Procedure: Should a TIMER master caution together with the STAB light not illuminating - indicating a faulty STAB boot system - be experienced during flight, the landing shall be performed as a flap 0 landing. 6- 2.11 010 A parenthesis added to clarify that the demonstrated crosswind values include gust.

REVISIONS TO SUPPLEMENTS List of Supplements Date changed to reflect this revision.
Supplement Page Reason for change

No. 16, Operation on narrow runways All This supplement does not meet Australia’s current guidance material in CAAP 235- 1(0) minimum Runway width and is therefore cancelled. REVISIONS TO APPENDICES List of Appendices Date changed to reflect this revision.

With kind regards, Saab AB



### Matilda Krig

### Airplane Flight Manual

RECORD OF REVISIONS - AFM 340B 010

Rev. No. Date By Rev. No. By Rev. No. By

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15 Jan 12/96

Jan 30/96

Mar 22/96

Jun 26/96

Oct 16/96

Nov 12/96

Jun 02/97

Dec 05/97

Mar 31/98

Mar 12/99

Oct 01/99

Nov 03/00

Jun 01/01

Dec 03/01

Jan 31/03 Date Date

16 Dec 05/03

17 Nov 10/04

18 Feb 25/05

19 Jan 05/07

20 Oct 05/07

21 Nov 30/07

22 Aug 20/08

23 Feb 26/10

24 Feb 17/11

25 Aug 31/12

26 Nov 22/13

27 Aug 14/14

28 Mar 27/15

### GENERAL Airplane Flight Manual 

# WT

AFM 340B Page 1- 4 Code 010 

### LIST OF EFFECTIVE PAGES The following pages comprise the Airplane Fli ght Manual for SAAB 340B airplanes with Mod. No. 2571 - Extended Wing Tips - installed, whose registration authority accepts/approves the use of the EASA/FAA standard version m anual for flight operations.



### REVISION No. 28 DATE: Mar 27/15 APPROVED BY EASA under approval No. 10053909 on 2nd 

### Jul 2015. ACCEPTED by FAA in letter No. ANM- 116- 15- 335.

PAGE CODE DATE PAGE CODE DATE PAGE CODE DATE

TITLE

1

INTRO 0 1 2 3

SECTION 1

1 2 3 R 4 R 5 R 6 R 7 8

SECTION 2

1 2 3 4 5 6 7 8 R 9 10 010

010 010 010

010 010 010 010 010 010 010 010

010 010 010 010 010 010 010 010 010 010 Nov 30/95

Nov 30/95 Feb 26/10 Nov 30/95

Jun 01/01 Jan 05/07 Nov 30/95 Mar 27/15 Mar 27/15 Mar 27/15 Mar 27/15 Aug 14/14

Feb 26/10 Feb 26/10 Feb 26/10 Feb 26/10 Feb 26/10 Aug 31/12 Feb 26/10 Feb 26/10 Mar 27/15 Feb 17/11 SECTION 2

11 12 13 14 15 R 16 17 18 19 20

SECTION 3

1 2 3 4 5 6 7 8

SECTION 4

1 2 3 R 4 5 6 (CONT)

010 010 010 010 010 010 010 010 010 010

010 010 010 010 010 010 010 010

010 010 010 010 010 010 Feb 17/11 Aug 14/14 Feb 26/10 Feb 26/10 Feb 17/11 Mar 27/15 Feb 26/10 Feb 26/10 Feb 26/10 Feb 26/10

Nov 30/95 Nov 30/95 Dec 05/03 Feb 26/10 Nov 30/95 Nov 30/95 Dec 03/01 Nov 30/95

Aug 31/12 Nov 30/95 Nov 30/95 Mar 27/15 Aug 31/12 Nov 30/95 SECTION 5

1 2 3 4 5 6 7

SECTION 6

0

1 2 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 2.10 R 2.11 2.12 2.13 2.14 2.15 2.16 010 010 010 010 010 010 010

010

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 Feb 26/10 Nov 30/95 Aug 14/14 Feb 17/11 Aug 14/14 Feb 26/10 Feb 26/10

Nov 30/95

Dec 05/97 Nov 30/95 Dec 05/97 Nov 30/95 Dec 05/97 Nov 30/95 Nov 30/95 Feb 17/11 Feb 17/11 Feb 17/11 Nov 30/07 Nov 30/95 Mar 27/15 Nov 03/00 Nov 30/95 Nov 30/95 Feb 25/05 Nov 30/95 R=REVISED (to be replaced) D=DELETED (to be removed) N=NEW (to be introduced) (TR = Temporary Revision)

Mar 27/15 EASA Approved

### GENERAL Airplane Flight Manual 

# WT

AFM 340B Page 1- 5 Code 010 

### LIST OF EFFECTIVE PAGES (Cont’d)

PAGE CODE DATE PAGE CODE DATE PAGE CODE DATE

SECTION 6

2.17 2.18 2.19 2.20 2.21 2.22 2.23 2.24 2.25 2.26 2.27 2.28 2.29 2.30 2.31 2.32 2.33 2.34 2.34 2.35 2.35 2.36 2.36 2.37 2.37 2.38 2.38 2.39 2.39 2.40 2.40 2.41 2.42 2.43

3 3.1 3.2 3.3 3.4 3.5 (CONT)

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 030 010 030 010 030 010 030 010 030 010 030 010 030 010 010 010

010 010 010 010 010 010 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Aug 20/08 Nov 30/95 Nov 30/95

Nov 30/95 Nov 30/95 Nov 30/95 Feb 17/11 Feb 17/11 Nov 30/95 SECTION 6

3.6 3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14 3.15 3.16 3.17 3.18 3.19 3.20 3.21 3.22 3.23 3.24 3.25 3.26 3.27 3.28 3.29 3.30 3.31 3.32 3.33 3.34

4 4.1 4.2 4.3 4.4 4.5 4.6 4.7 4.8 4.9 4.10 (CONT)

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010

010 010 010 010 010 010 010 010 010 010 010 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Dec 05/97 Nov 30/95 Jan 05/07 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 22/13 Jun 02/97 Jun 02/97

Nov 10/04 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Dec 05/97 Dec 05/97 SECTION 6

4.11 4.12 4.12A 4.13 4.13A 4.14 4.14A 4.15 4.16 4.17 4.18 4.19 4.20 4.21 4.21A 4.22 4.23 4.23 4.24 4.25 4.25 4.26 4.27

5 5.1 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 5.10 5.11 5.12 5.12A 5.13 5.13A 5.14 (CONT)

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 030 010 010 030 010 010

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 Dec 05/97 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Aug 31/12 Nov 30/95 Nov 30/95 Feb 17/11 Feb 17/11 Nov 10/04 Nov 10/04 Nov 10/04 Feb 17/11 Feb 17/11 Feb 17/11 Nov 10/04 Nov 10/04

Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95

Mar 27/15 EASA Approved

### GENERAL Airplane Flight Manual 

# WT

AFM 340B Page 1- 6 Code 010 

### LIST OF EFFECTIVE PAGES (Cont’d)

PAGE CODE DATE PAGE CODE DATE PAGE CODE DATE

SECTION 6

5.14A 5.15 5.16 5.17 5.18 5.19 5.20 5.21 5.21A

6 6.1 6.2 6.3 6.4 6.5 6.6 6.7 6.8 6.9 6.10 6.11 6.12 6.12A 6.13 6.13A 6.14 6.14A 6.15 6.16 6.17 6.18 6.19 6.20 6.21 6.21A

7 7.1 7.2 (CONT)

010 010 010 010 010 010 010 010 010

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010

010 010 010 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Aug 31/12 Nov 30/95 Nov 30/95 Feb 17/11 Feb 17/11

Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Aug 31/12 Mar 22/96 Mar 22/96 Feb 17/11 Feb 17/11

Jan 12/96 Jan 12/96 Jan 12/96 SECTION 6

7.3 7.4 7.5 7.6 7.7 7.8 7.9 7.10 7.11 7.12 7.12A 7.13 7.13A 7.14 7.14A 7.15 7.16 7.17 7.18 7.19 7.20 7.21 7.21A

8 8.1 8.2 8.3 8.4 8.4A 8.5 8.5 8.6 8.6 8.7 8.7 8.8 8.8 (CONT)

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010

010 010 010 010 010 010 010 030 010 030 010 030 010 030 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Jan 12/96 Aug 31/12 Jan 12/96 Jan 12/96 Feb 17/11 Feb 17/11

Nov 03/00 Feb 17/11 Nov 03/00 Nov 30/95 Nov 30/95 Nov 30/95 Dec 03/01 Jun 01/01 Feb 17/11 Feb 17/11 Dec 03/01 Jun 01/01 Dec 03/01 Jun 01/01 SECTION 6

9 9.1 9.2 9.3

10 10.1 10.2 10.2 10.3 10.3 10.4 10.4 10.5 10.5 10.6 10.6 10.7 10.7 10.8 10.8 10.9 10.9 10.10 10.11

11 11.1 11.2 11.2 11.3 11.3 11.4 11.4 11.5 11.5 11.6 11.6 11.7 11.7 (CONT)

010 010 010 010

010 010 010 030 010 030 010 030 010 030 010 030 010 030 010 030 010 030 010 010

010 010 010 030 010 030 010 030 010 030 010 030 010 030 Feb 26/10 Nov 30/07 Nov 30/07 Nov 30/07

Nov 30/95 Nov 30/95 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Feb 17/11 Feb 17/11 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Feb 17/11 Feb 17/11 Nov 03/00 Jun 01/01 Nov 30/95 Nov 30/07

Nov 30/95 Nov 30/95 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Feb 17/11 Feb 17/11 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01 Nov 03/00 Jun 01/01

Mar 27/15 EASA Approved

### GENERAL Airplane Flight Manual 

# WT

AFM 340B Page 1- 7 Code 010 

### LIST OF EFFECTIVE PAGES (Cont’d)

PAGE CODE DATE PAGE CODE DATE PAGE CODE DATE

SECTION 6

11.8 11.8 11.9 11.9 11.10 11.11

12 12.1 12.2 12.3 12.4 12.5 12.6 12.7 12.8 12.8A 12.9 12.9A 12.10 12.10A 12.11 12.12 12.13 12.14 12.15 12.16 12.17 12.17A 12.18 12.18A (CONT)

010 030 010 030 010 010

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 Feb 17/11 Feb 17/11 Nov 03/00 Jun 01/01 Nov 30/95 Nov 30/07

Jun 26/96 Dec 05/97 Nov 30/95 Nov 30/95 Nov 30/95 Dec 05/97 Dec 05/97 Dec 05/97 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Nov 30/95 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 Mar 22/96 SECTION 6

12.19 12.19A 12.20 12.21 12.22 12.23 12.24 12.25 12.26 12.26A 12.27 12.27A 12.28 12.28A 12.29 12.30 12.31 12.32 12.33 12.34 12.35 12.35A 12.36 12.36A 12.37 12.37A (CONT)

010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 010 Mar 22/96 Mar 22/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 Jun 26/96 SECTION 6

13 13.1 13.2 13.3 13.4 13.5 13.6 13.7

SECTION 7

SUPPLEMENTS

SECTION 8

APPENDICES (CONT)

010 010 010 010 010 010 010 010 Mar 31/98 Dec 05/97 Dec 05/03 Feb 26/10 Dec 05/97 Feb 25/05 Feb 25/05 Dec 05/03

Mar 27/15 EASA Approved

### LIMITATIONS Airplane Flight Manual 

# WT

AFM 340B Page 2- 9 Code 010 

### OIL SYSTEM

Approved types of oil (engine and propeller gearbox)

Type I oils: Type II oils: BP Turbo Oil 2389 Aero Shell Turbine Oil 500 ETO 2389 Castrol 205 Exxon Turbo Oil 2389 BP Turbo Oil 2380 Castrol 325 ETO 2380 Exxon Turbo Oil 2380 Mobil Jet II Stauffer Jet II Approved types of oil (engine only)
Type I oils: Type II oils: Mobil Jet 254

NOTE It is not allowed to mix Mobil Jet 254 oil with other approved oils.

NOTE 1. Minimum oil temperature for engine start with type II oil is - 40 oC (- 40 o F). 2. Mixing of type I and II oils is allowed but not recommended.



### FUEL SYSTEM
The total quantity of usable fuel is 5690 lbs (2580 kg) at a fuel density of 6.7 lbs/US gal. (0.802 kg/L). Fuel remaining in the tanks when the fuel quantity indicators read zero in level flight cannot be safely used in all flight conditions. Fuel anti- ice additives meeting specification Mil 27686E or Mil 85470B are authorized for use. Concentration shall be 0.06 % min to 0.15 % max by volume.

cont’d...

EASA Approved Mar 27/15These speeds already include an increment for maneuvering up to 30 degrees of bank. 

### LIMITATIONS Airplane Flight Manual 

# WT

AFM 340B Page 2- 15 Code 010 

### AIRSPEEDS (Cont’d)

MINIMUM AIRSPEEDS FOR ICING CONDITIONS The minimum airspeeds below must be used for operation in icing conditions and, with Mod. No. 3530 installed (improved stall warning system) whenever the blue ICE SPD status light is illuminated.

Definitions
VCLEAN = Final climb speed in accordance with Final Climb charts in section 6- 4. Maneuvering = A bank angle in excess of 15 degrees in a coordinated turn.

General 10 knots shall be added to the speeds below for maneuvering with bank angles between 15 and 30 degrees. At higher bank angles, increase speed by 10 knots for each 10 degrees of bank above 30.
For all- engines operating climb below minimum sector altitude (MSA): Maintain a minimum speed of “Enroute Climb Speed - with residual airframe and propeller ice” (VCLEAN +13) after transitioning to the Enroute Climb configuration (after initial power reduction from Take- off power).
For all- engines operating climb above minimum sector altitude (MSA), cruise, descent, holding and approach: Flaps 0 160 KIAS

............ Flaps 7 150 KIAS

............ Flaps 15 145 KIAS

............ Flaps 20 140 KIAS

............ Flaps 35 130 KIAS

............
If a lower airspeed must be used to exit the icing conditions, “Enroute Climb Speed - with residual airframe and propeller ice” (VCLEAN +13) may also be used for flaps 0 climb.
For single- engine climb after transitioning to the Enroute Climb configuration (after initial power reduction from Take- off power) and for driftdown: Flaps 0 “Enroute Climb Speed - with residual airframe and propeller ice” (VCLEAN +13).

............ For final approach:
VREF +10 Increase landing distance for the 10- knot speed increment applied to the reference speed in accordance with the performance data in Section 6 of this manual.
For missed approach/go- around: Maintain a minimum speed of “Approach Climb Speed - with residual airframe and propeller ice” until above minimum sector altitude (MSA), then the speeds specified above.

EASA Approved Mar 27/15

### LIMITATIONS Airplane Flight Manual 

# WT

AFM 340B Page 2

− 16 Code 010 

### SYSTEMS Cabin Pressurization Maximum Differential Pressure 7.5 psi (52.0 kPa)

.............. Auto Mode Schedule 7.1 psi (50.0 kPa)

.......................

Flight Director Use of flight director information in go

− around mode during take

− off is not authorised.

Autopilot

− In icing conditions, as defined in the “ICING CONDITIONS” section for adherence to autopilot/flight director limitations, if the flight director and/or autopilot are engaged in a vertical mode during climb, IAS mode must be used

.

− Following an engine failure it is required to disconnect the autopilot and re

−trim the aircraft before re

− engagement of the autopilot.

−Minimum Use Heights (MUH):

 During take

− off or go

− around: 200 ft AGL (Above Ground Level) For aircraft operating under LFV approval, the following additional limitations apply: (Not required for operation according to FAA regulations)

−Minimum Use Heights (MUH):

 During cruise: 500 ft AGL

 During coupled approach: 50 ft AGL

 During non

− coupled approach: 100 ft AGL.

Yaw Damper Yaw Damper Operation is notauthorised for:

−Take

− off

−Go around

−Landing.

Flaps

−Flaps may only be extended on ground and during take off, low altitude holding, approach and landing, up to

a maximum altitude of 14000 ft.

−Landing Flap to be selected before 300 ft radio height during normal landing. During flight with Master Caution (ICE PROT) and Timer light illuminated and green STAB light not illuminating, Flaps 0 must be used for landing (required by AD). For landing procedure see Section 4 Abnormal Procedures, Ice Protection Fault.

cont’d...

EASA Approved Mar 27/15

### ABNORMAL PROCEDURES Airplane Flight Manual 

# WT

AFM 340B Page 4

−4 Code 010 

### RUDDER LIMITER LIGHT ON

Reduce speed until light goes out but not below 140 kts. If light still is ON at 140 kts, select the rudder limiter switch to OVERRIDE. Max speed with the rudder limiter in OVERRIDE is 180 KIAS. Avoid large rudder deflections above 150 KIAS. If rudder limiter light is on below 140 KIAS, use if possible a runway with less than 10 kts crosswind for landing.



### HYDRAULIC WARNING
Switch off the hydraulic pump.

− If both emergency and main pressures are low, extend the landing gear and land at the nearest suitable airport. Leave flaps in present position; use hand pump if brake pressure needs to be restored.

− If only emergency pressure low, use hand pump for landing gear, flap and brake operation.

− If only main pressure is low, set the hydraulic pump to OVERRIDE; if main pressure increases, switch between OVERRIDE and OFF so as to maintain pressure. If there is no increase in pressure during override, set the pump to OFF and use the hand pump for landing gear, flap and brake operation.

− If main pressure and hydraulic quantity are low, pull emergency landing gear handle for gear extension. Leave flaps in present position and use hand pump if brake pressure needs to be restored.

− If all pressures are normal, use hand pump for landing gear, flap and brake operation.



### AC GENERATOR FAULT
Try to reset the generator once. If it will not reset, set the generator switch to OFF/R and leave icing conditions if possible.



### ICE PROTECTION SYSTEM FAULT
Reset affected switch once. If the airframe or powerplant de

− icing/anti

− icing system is not restored, leave icing conditions if possible. During landing with iced

− up or inflated de

− ice boots, use the following flap settings and speeds:

Wing fault: Flaps 20 and V REF20+10 KIAS or Flaps 35 and VREF35+ 10 KIAS Stabilizer fault, or Wing and stabilizer fault: Flaps 20 and V REF20+ 10 KIAS

During landing with Master Caution (ICE PROT) and TIMER light illuminated and green STAB light not illuminating, use the following flap settings and speeds (required by AD) :
Flaps 0 and VREF20+ 30 KIAS



### ALTERNATE EXTENSION OF LANDING GEAR

Select landing gear down and use the hand pump to extend the landing gear. Hand pump selector must be set to LDG GR position. If an emergency extension has to be made, pull the emergency landing gear handle, then set landing gear handle to DOWN.

EASA Approved Mar 27/15

### PERFORMANCE DEFINITIONS AND

GENERAL DATA 

### Airplane Flight Manual 

# WT

AFM 340B Page 6- 2.11 Code 010 

### WIND COMPONENTS

Wind Components The conversion of reported wind velocities to headwind, tailwind and crosswind components is illustrated by the wind components chart on the following page.
Maximum Demonstrated Crosswind Component Maximum Demonstrated Crosswind Component is 35 knots (including gust). This was demonstrated on a dry runway and was not found to be limiting.
Example Entering the chart with a reported wind velocity which has a speed of 35 knots at a direction of 40 

###  relative to the runway: the crosswind component is 22.5 knots the headwind component is 26.8 knots.

EASA Approved Mar 27/15

### SUPPLEMENTS Airplane Flight Manual 

# WT

AFM 340B Section 7 Code 010 EASA Approved Mar 27/15 

### LIST OF SUPPLEMENTS APPLICABLE TO AFM 340B 010
The following Supplements may/must be used as a complement to this AFM:



### Approved by EASA under approval No. 10053909 on 2 nd 

### Jul 2015. DATE: Mar 27/15 

### Accepted by FAA in letter No. ANM- 116- 15- 335.

No. Supplements Latest Revision Approval date

2 Omega/VLF Operation with Ferry Flight Kit 2 Oct 16/96

4 CAT II Operation 3 Oct 16/96

12 Operation on unpaved runways (Australian CAA standard) 3 Aug 31/12

13 Traffic alert and Collision Avoidance System (TCAS II) 8 Dec 15/14

16 Operation on narrow runways (Australian CAA standard) 1 Deleted

17 Freon Air Conditioning 1 Oct 16/96

18 Ferry GPS Kit 1 Oct 16/96

19 HF Com Ferry Flight Kit 1 Oct 16/96

24 ITT Exceedance during take- off or go- around 2 Oct 16/96

39 Search and Rescue - 200 (SAR- 200)* 7 Nov 15/13

43 Operation with increased T/O speeds and high airfield performance 4 Feb 17/11

46 Operation with Autocoarsen inoperative 1 Oct 01/99

48 Extended operation with JP- 4 fuel* 1 Feb 27/98

49 Precipitation Covered and Low Friction Runway Operation (JAA standard)* First Issue Dec 05/97

53 Airborne Collision Avoidance System (ACAS II) 1 Dec 03/01

54 Landing with tailwind above 10 knots* 1 Nov 13/09

57 GPS Based FMS Non Precision Approach 1 May 05/04

59 P- RNAV Operation* 4 Aug 14/14

62 ADS- B Surveillance (ADS- B- NRA) First Issue Feb 20/12

* Distribution limited to particular operators.

### APPENDICES Airplane Flight Manual 

# WT

AFM 340B Section 8 Code 010 

### LIST OF APPENDICES APPLICABLE TO AFM 340B 010
The following Appendices may be used as a complement to this AFM:



### Approved by EASA under approval No. 10053909 on 2 nd 

### Jul 2015

. DATE: Mar 27/15 Accepted by FAA in letter No. ANM- 116- 15- 335.

Appendices Latest Revision Approval date
Configuration Deviation List 12 Nov 22/13
Operation with Derated Power on the CT7- 9B, Simplified method (WT) 3 Dec 03/01
Operation with Reduced Take- off Power (WT) 6 Dec 05/03

EASA Approved Mar 27/15