Specifications

SECTION V
ABNORMAL PROCEDURES
MODEL 560
SINGLE-ENGINE APPROACH AND LANDING (Continued)
12. Pressurization - CHECK ZERO DIFFERENTIAL PRIOR TO LANDING.
13. Landing Gear - DOWN.
14. ANTI-SKID Switch - CHECK ON.
15. Landing Lights - AS DESIRED.
16. Airspeed - V
APP.
17. Speed Brakes - RETRACT (50 feet AGL and below).
18. Flaps - LAND (35°).
19. Airspeed - V
REF
.
20. Autopilot and Yaw Damper - OFF (400 feet AGL and below).
21. Refer to Abnormal Procedures, SINGLE ENGINE REVERSING and SINGLE ENGINE GO-
AROUND.
SINGLE-ENGINE REVERSING
1. Throttle - IDLE.
2. Brakes - APPLY.
3. Speed Brakes - EXTEND.
4. Thrust Reverser - DEPLOY (after nose wheel on ground).
5. Thrust Reverser Indicator Lights - CHECK ILLUMINATION of ARM, UNLOCK and DEPLOY
LIGHTS.
6. Thrust Reverser - REVERSE POWER ON UNAFFECTED ENGINE.
7. Thrust Reverser - REVERSER LEVER TO IDLE REVERSE AT 60 KIAS.
NOTE
Reverse thrust may need to be reduced during crosswind landings on wet or icy run-
ways to prevent airplane from being forced to runway edge.
SINGLE-ENGINE GO-AROUND
1. Throttle (operating engine) - SET Takeoff N
1
.
2. Airplane Pitch Attitude - 10° (Go-around mode on flight director for reference).
3. Flaps - T.O. & APPR (15°).
4. Climb Speed - V
APP
.
5. Landing Gear - UP (when positive rate-of-climb is established).
6. If Anti-ice REQUIRED, R WINDSHIELD BLEED AIR Knob - OFF.
NOTE
The landing gear warning horn cannot be silenced if the landing gear is retracted prior
to the flaps reaching the TAKEOFF and APPROACH position.
7. Flaps (when clear of obstacle) - RETRACT at 1500 feet and V
APP
+ 10 KIAS and accelerate to
V
ENR
.
8. Throttle (operating engine) - SET Maximum Continuous N
1
.
I 5-32 Configuration AA 56FMB-01