Specifications

SECTION V
MODEL 560 ABNORMAL PROCEDURES
ELECTRIC TRIM INOPERATIVE
1. PITCH TRIM Circuit Breaker (LH panel) - CHECK IN.
IF STILL INOPERATIVE
2. Manual Elevator Trim - AS REQUIRED.
NOTE
Do not attempt to use the autopilot if the electric trim is inoperative. The autopilot will
not be able to trim out servo torque, and disengaging the autopilot could result in a
significant pitch upset.
JAMMED ELEVATOR TRIM
TRIM JAMMED AT CRUISE SETTING
1. AP TRIM DISC Button - PRESS and RELEASE.
2. Maintain trim speed as long as practical until speed reduction is required for approach.
3. Flaps - UP (0°). Do not extend flaps for approach or landing. Refer to Abnormal Procedures,
FLAPS INOPERATIVE APPROACH and LANDING.
TRIM JAMMED AT TAKEOFF OR GO-AROUND SETTING
1. Throttles - REDUCE as required to maintain 120 KIAS or less.
2. Flaps - DO NOT MOVE.
3. Landing Gear - DOWN. Do not retract.
4. Airspeed - V
REF
for full flaps, V
APP
for 15° flaps, or V
REF
+ 12 KIAS for 7° flaps or V
REF
+ 15
KIAS for 0° flaps.
5. Flap Override Switch - GPWS FLAP OVRD ON (amber) if landing with flaps other than FULL.
6. Speed Brakes - RETRACT (50 feet AGL and below).
7. Yaw Damper Switch - OFF.
8. Land as soon as practical.
CAUTION
AVOID LANDINGS WITH TAILWINDS OR DOWNHILL RUNWAY GRADIENTS OR AT
FIELD ELEVATIONS ABOVE 10,000 FEET MSL WITH FLAPS 15°, 5000 FEET MSL
WITH FLAPS 7°, OR 3000 FEET MSL WITH FLAPS 0°.
NOTE
f Do not attempt to use the autopilot if the electric trim is inoperative. The autopilot will
not be able to trim out servo torque, and disengaging the autopilot could result in a
significant pitch upset.
f Multiply landing distance by 1.4 with flaps 15°, 1.5 for flaps 7°, and 1.6 for flaps 0°.
AUTOPILOT OUT OF TRIM (AP ROLL MISTRIM OR AP PITCH MISTRIM CAUTION LIGHT ON)
1. Control Wheel - Hold firmly with both hands.
2. AP TRIM DISC Button - PRESS and RELEASE (if elevator trim not in motion).
(Continued Next Page)
I
56OMB-01 Configuration AA 5-15