Term
| Torque limit applies within range of _______to______propeller RPM(N2). Below______propeller RPM, torque is limited to______. |
|
Definition
|
|
Term
| Cruise torque values vary with______ and_____ |
|
Definition
|
|
Term
| To account for power setting accuracy and steady state fluctuations, inadvertent torque excursions up to_____ are time limited to______ |
|
Definition
|
|
Term
| Sustained propeller overspeeds faster than_____ indicate failure of the primary governor. Flight may be continued at propeller overspeeds up to________ provided torque is limited to_______. Sustained propeller overspeeds faster than_______ indicate failure of bothe the primary and secondary governor and such overspeeds are not approved. |
|
Definition
| 1700 rpm, 1768 rpm, 96%, 1768rpm |
|
|
Term
| The propeller autofeather system must be operable for all flights and must be armed for __________, _________, _______, and ________. |
|
Definition
| Takeoff, Climb, Approach, Landing |
|
|
Term
| Normal oil pressure is ____ to ____ psi at gas generator speeds above _____%. With engine torque below ____%, minimum oil pressure is ______psi at normal oil temperature (______ to _____ degrees C). |
|
Definition
| 90, 135, 72, 62, 60, 60, 70 |
|
|
Term
| Oil pressures under_______psi are undesireable. Under emergency conditions, to complete a flight, a lower oil pressure limit of ____psi is permissible at a reduced power level not to exceed_____% torque. |
|
Definition
|
|
Term
| Oil presssures below _____psi are unsafe and require that either the engine be shut down or a landing be made at the nearest suitable airport, using the ___________________ to sustain flight. Fluctuations of plus or minus ______psi are acceptable. |
|
Definition
| 60, minimum power required, 10 |
|
|
Term
| During extremely cold starts, oil pressure may reach_____psi. In flight, oil pressure above_____psi but not exceeding ____psi are permitted only for the duration of the flight. A minimum oil temperature of____degrees C is recommeded for fuel heater operation at takeoff power. |
|
Definition
|
|
Term
| Oil temperature limits are _____ and ____. However, temperatures between ____ to _____ are limited to a maximum of ______. |
|
Definition
| -40 C, 110C, 99C, 110C, 10 min |
|
|
Term
| Do not takeoff if fuel quantity gauge indicates less than______ of fuel in each wing system. Do not put any fuel into the auxilliary tanks unless the main tanks are ____. |
|
Definition
|
|
Term
| Operation of either engine with its corresponding fuel pressure annunciator illuminated is limited to_____before overhaul and replacement of the __________fuel pump. Windmillin time_____________________against this limit. |
|
Definition
|
|
Term
| Maximum weight in baggage comparment. |
|
Definition
|
|
Term
| Maximum cabin pressure differential. |
|
Definition
|
|
Term
|
Definition
| Operational for all flights |
|
|
Term
| Sustained flight in icing conditions with flaps extended is_____________ except for________and__________ |
|
Definition
| prohibited, approach, landing |
|
|
Term
| Engine anti-ice shall be ____for operations in ambient temperatures of_____ or below when flight free of visible moisture cannot be assured, and shall be_____for takeoff operations in ambient tmeperatures of above_______. |
|
Definition
| on, 5 deg C, off, 10 deg C |
|
|
