Specifications

SECTION V
ABNORMAL PROCEDURES
MODEL 560
ENGINE VIBRATION (ENG VIB L OR R ADVISORY LIGHT ON) (Continued)
IF VIBRATION EXISTS
ON GROUND
2. Correct prior to flight.
IN FLIGHT
2. Engine - MONITOR for other evidence of malfunction. Consider reducing RPM.
3. ENGINE SYNC Knob - OFF.
4. Throttle (affected engine) - REDUCE THRUST (as required).
5. Land as soon as practical.
IF VIBRATION INCREASES OR OTHER EVIDENCE OF ENGINE MALFUNCTION IS PRESENT
6. Consider the possibility of shutting down the engine. Refer to Abnormal Procedures ENGINE
FAILURE/PRECAUTIONARY SHUTDOWN and SINGLE-ENGINE APPROACH AND LANDING.
CAUTION
IF SIGNIFICANT VIBRATION CONTINUES WITH THE ENGINE RUNNING, ENGINE
FAILURE MAY RESULT.
FUEL GAUGING SYSTEM FAULT (FUEL GAUGE L OR R CAUTION LIGHT ON)
Indicates that a fault has been detected in the respective fuel gauging system. Monitor the respective
fuel gauge for proper indication. Consider the possibility that the tank contains less fuel than the
opposite tank. This fault may also be the result of improper fuel capacitance. Check fuel after
landing.
1. BATT SWITCH - BATT (until B.I.T.E. control box indications are checked by appropriate
personnel; record fuel quantity in each tank at time of fault.)
SINGLE GENERATOR FAILURE (GEN OFF L OR R CAUTION LIGHT ON)
1. Electrical Load - DECREASE if required.
2. A/C COMPRESSOR Switch - OFF or FAN.
3. Failed GEN Switch - RESET and GEN.
NOTE
The air conditioner compressor will not automatically load-shed on the ground.
IF UNABLE TO RESET
4. Failed GEN Switch - OFF.
I 5-10 Configuration AB 56OMB-01