Term
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Definition
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Term
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Definition
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Term
| OIL PX annunciator with PCL above idle |
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Definition
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Term
| OIL PX annunciator with PCL at idle |
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Definition
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Term
| turbine output shaft speed |
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Definition
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Term
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Definition
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Term
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Definition
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Term
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Definition
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|
Term
| PMU managed minimum above 10K |
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Definition
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|
Term
| ignition and boost pump deactivated during auto start |
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Definition
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Term
| fuel pressure switch limit, turns on BP |
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Definition
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Term
| normal wing tank capacity |
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Definition
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Term
|
Definition
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|
Term
| SPR refueled full fuel load |
|
Definition
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|
Term
| over wing refueled full fuel load |
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Definition
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|
Term
| (for 2 minutes) imbalance where FUEL BAL annunciator illuminated |
|
Definition
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Term
|
Definition
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|
Term
| L or R FUEL LO annunciator illuminated |
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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Term
|
Definition
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|
Term
|
Definition
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|
Term
| min hydraulic pressure to operate NW steering, gear, flaps, speed brake |
|
Definition
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|
Term
| fuel pressure supplied by engine driven low pressure fuel pump |
|
Definition
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|
Term
| fuel pressure supplied by engine driven high pressure fuel pump |
|
Definition
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|
Term
| hydraulic pressure relief valve opens |
|
Definition
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|
Term
| EHYD PX LO annunciator illuminates |
|
Definition
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|
Term
| HYDR FL LO annunciator illuminates |
|
Definition
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|
Term
| normal gear extension/retraction time |
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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|
Term
| speed brake deflection when deployed |
|
Definition
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|
Term
| TAD active with no weight on wheels |
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
| 0’/0 KIAS to 35,000’/370 KIAS |
|
|
Term
| CKPT ALT annunciator illuminated |
|
Definition
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|
Term
| CKPT PX annunciator illuminated |
|
Definition
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|
Term
| DUCT TEMP annunciator illuminated |
|
Definition
|
|
Term
|
Definition
| > +30*/-20* pitch or 65* roll |
|
|
Term
| Full EADI presentation reappears after unusual attitude |
|
Definition
| < +25*/-15* pitch and 60* roll |
|
|
Term
| FDR annunciator illuminates |
|
Definition
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|
Term
| AUX BAT test light will not illuminate |
|
Definition
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|
Term
| OBOGS TEMP annunciator illuminates |
|
Definition
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|
Term
|
Definition
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|
Term
|
Definition
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|
Term
| Minimum main gear strut extension |
|
Definition
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|
Term
| Minimum nose gear strut extension |
|
Definition
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|
Term
|
Definition
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|
Term
| altitude lost during airstart procedure (at 125 KIAS glide) |
|
Definition
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|
Term
| time to complete airstart sequence |
|
Definition
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|
Term
| airstart envelope (above 15,000 feet MSL) |
|
Definition
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|
Term
| airstart envelope (at or below 15,000 feet MSL) |
|
Definition
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|
Term
| _____ indicate a steady state spin |
|
Definition
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|
Term
| engine feed fuel pressure below causes boost pump to automatically engage |
|
Definition
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|
Term
| auto fuel balancing keeps fuel balance within |
|
Definition
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|
Term
| fuel imbalance for two minutes triggers FUEL BAL light (fault in auto system) |
|
Definition
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|
Term
| EHYD PX LO light illuminates below |
|
Definition
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|
Term
| HYDR FL LO light illuminates below |
|
Definition
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|
Term
| max descent rate for 125 KIAS glide, 4-6% torque, clean. |
|
Definition
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|
Term
| FUEL PX light illuminates |
|
Definition
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|
Term
|
Definition
| <40 psi above idle or 15 psi at idle |
|
|
Term
| OBOGS TEMP light illuminates |
|
Definition
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|
Term
| altitude loss during six turn, steady-state spin |
|
Definition
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|
Term
| Recommended turbulence/t-storm penetration airspeed |
|
Definition
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