Term
|
Definition
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|
Term
|
Definition
| Observe VMO, MMO, gear and flap placards |
|
|
Term
| Maximum operating altitude |
|
Definition
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|
Term
| Maximum takeoff and landing altitude |
|
Definition
|
|
Term
| Maximum demonstrated takeoff and landing crosswind (dry runway) |
|
Definition
|
|
Term
| Maximum demonstrated takeoff and landing crosswind (wet runway) |
|
Definition
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|
Term
| Maximum takeoff headwind component |
|
Definition
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|
Term
| Maximum takeoff and landing tailwind component |
|
Definition
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|
Term
| Altimeters - max allowable in-flight difference |
|
Definition
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|
Term
| Altimeters - max on-ground difference (pilot to co-pilot) |
|
Definition
50 feet (sea level to 5k)
60 feet (5k to 10k) |
|
|
Term
| Altimeters - max on-ground difference (display and field elevation) |
|
Definition
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|
Term
| Anytime IDG loads in excess of __% are required during ground operations, advance thrust to a minimum of __% N1 |
|
Definition
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|
Term
| Minimum engine oil quantity (overland operations) |
|
Definition
|
|
Term
| Minimum engine oil quantity (overwater operations) |
|
Definition
60% full (12 quarts)
OR
7 quarts plus 1 quart per flight hour |
|
|
Term
| Do not exceed __ minutes during each start attempt. A minimum of __ seconds is required between start attempts. |
|
Definition
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|
Term
| Do not try to engage the starter while N2 is more than __%. |
|
Definition
|
|
Term
| Engine ignition shall be set to ___ for takeoff and landing. |
|
Definition
|
|
Term
| Engine ignition shall be set to ___ for anti-ice operation or if moderate or heavy rain, hail, or sleet is encountered. |
|
Definition
|
|
Term
| Engine ignition shall be set to ___ if severe turbulence is encountered. |
|
Definition
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|
Term
| List limits for takeoff associated with EECs in alternate mode. |
|
Definition
1. Both EECs shall be in alternate mode.
2. Derate or assumed temperature reduced takeoff thrust is not allowed
3. Do not use FMS takeoff N1 or V-speed values.
4. Use of autothrottle for takeoff is prohibited. |
|
|
Term
| Reverse thrust shall not be utilized for backing due to ____. |
|
Definition
| the risk of foreign object ingestion. |
|
|
Term
| Max speed - landing gear extend |
|
Definition
|
|
Term
| Max speed - landing gear retract |
|
Definition
|
|
Term
| Max speed - landing gear extended |
|
Definition
|
|
Term
| Max speed - sonobouy deployment |
|
Definition
|
|
Term
| Max speed - opening/closing weapon bay |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max fuel imbalance between 1 and 2 (all phases of flight) |
|
Definition
|
|
Term
| Min fuel for ground operation of electric hydraulic pumps (for cooling) |
|
Definition
| 1675 pounds in related main tank |
|
|
Term
| Max altitude APU - bleed plus electrical (in flight) |
|
Definition
|
|
Term
| Max altitude APU - bleed plus electrical (on ground) |
|
Definition
|
|
Term
| Max altitude APU - bleed only (on ground or in flight) |
|
Definition
|
|
Term
| Max altitude APU - electrical load only (on ground or in flight) |
|
Definition
|
|
Term
| With the exception of engine start, APU bleed valve shall be closed when: |
|
Definition
1. Ground air connected and isolation valve open
2. Engine 1 bleed valve open
3. Isolation and engine 2 bleed valve open |
|
|
Term
| APU generator output above 32,000 feet is restricted to maximum __% |
|
Definition
|
|
Term
| Authorized flap settings for takeoff are ___ |
|
Definition
|
|
Term
| Maximum altitude flap extension |
|
Definition
|
|
Term
| Do not deploy speedbrakes in flight at radio altitudes less than ___ ft. |
|
Definition
|
|
Term
| Do not operate in icing conditions for more than __ minutes. |
|
Definition
|
|
Term
| Use of ___ with the autopilot engaged is prohibited. |
|
Definition
|
|
Term
| Do not engage the autopilot for takeoff below __ ft AGL. |
|
Definition
|
|
Term
| During approach, the autopilot shall not remain engaged below __ ft AGL. |
|
Definition
|
|
Term
| Max speed - EO/IR extended |
|
Definition
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