Miscellaneous

Question 1

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

Answer 1

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.

Question 2

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

Answer 2

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

Question 3

Minimum idle speed:
Hartzell

McCauley

Answer 3

Hartzell : 1180 RPM

McCauley: 1100 RPM

Question 4

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

Answer 4

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

Question 5

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

Answer 5

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

Question 6

Propeller Deice Ammeter
Green Arc (Normal Operating Range)

Answer 6

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

Question 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

Answer 7

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

Question 8

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation
Operation with Yaw Damp System Inoperative

Answer 8

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

Question 9

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

Answer 9

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