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Flashcards in Miscellaneous Deck (9)
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1

Propeller Autofeather for airplanes equipped with Hartzell propellers, the propeller autofeather system must be operable for ____ ______ and must be armed for ______, ______, ______, and _______.

Propeller Autofeather for airplanes equipped with Hartzell propellers, the propeller autofeather system must be operable for:

All flights and
must be armed for takeoff, climb, approach, and landing.

2

Cabin Differential Pressure Gauge
Green Arc (Normal Operating Range) ............. ____________
Red Line (Maximum Operating Limit).............. ____________

Green Arc (Normal Operating Range) .....................0 to 6.6 psi
Red Line (Max Operating Limit) ............6.6 psi to end of scale

3

Minimum idle speed:
Hartzell
McCauley

Hartzell : 1180 RPM
McCauley: 1100 RPM

4

Pneumatic Gauge
Green Arc (Normal Operating Range)
Red Line (Maximum Operating limit)

Green Arc (Normal Operating Range) ....................12 to 20 psi
Red Line (Maximum Operating limit)...............................20 psi

5

Gyro Suction Gauge
Narrow Green Arc
Wide Green Arc
35K marked on face of gauge at?
15K marked on face of gauge at?

Narrow Green Arc..............................................2.8 to 4.3 in. Hg Wide Green Arc..................................................4.3 to 5.9 in. Hg
35K marked on face of gauge at ................................ 3.0 in. Hg
15K marked on face of gauge at ................................ 4.3 in. Hg

6

Propeller Deice Ammeter
Green Arc (Normal Operating Range)

Green Arc (Normal Operating Range) .......... 18 to 24 amperes

7

Weight Limits

Maximum Ramp Weight
Maximum Take-off Weight:
All Except 14 CFR Part 135 Operations
Maximum Landing Weight
Maximum Zero Fuel Weight

Maximum Weight in Baggage Compartment:
When Equipped with Fold-up Seats
When Not Equipped with Fold-up Seats

Maximum Ramp Weight ..................................... 12,590 pounds

Maximum Take-off Weight:
All Except 14 CFR Part 135 Operations............ 12,500 pounds Maximum Landing Weight ................................. 12,500 pounds Maximum Zero Fuel Weight............................... 11,000 pounds

Maximum Weight in Baggage Compartment:
When Equipped with Fold-up Seats ...................... 510 pounds
When Not Equipped with Fold-up Seats ............... 550 pounds

8

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation
Operation with Yaw Damp System Inoperative

Normal Operation ......................................................35,000 feet Operation with Yaw Damp System Inop..................17,000 feet

*The yaw damper is no longer a requirement for flight up to the ceiling capability of the airplane when it is equipped with the Raisbeck Engineering Dual Aft Body Strakes

9

MAXIMUM OUTSIDE TEMPERATURE LIMITS
Sea Level to 25,000 feet pressure altitude
Above 25,000 feet pressure altitude

Sea Level to 25,000 feet pressure altitude .............. ISA + 37°C
Above 25,000 feet pressure altitude ........................ ISA + 31°C