Term
|
Definition
|
|
Term
| max takeoff and landing altitude |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Land as soon as possible in terms of... |
|
Definition
(FTWT)
Facilities
Time
Weather
Terrain |
|
|
Term
|
Definition
| 2 pilots and any NATOPS qualified crewmember |
|
|
Term
| Oxygen limits at 30 deg C |
|
Definition
Max 1900 psi
Min 1440 psi
(chart on page 4-3) |
|
|
Term
| maximum allowable in-flight difference between pilot and copilot altitude displays |
|
Definition
|
|
Term
| maximum allowable on-the-ground altitude display difference between pilot and copilot altitude displays |
|
Definition
50 feet (from sea level to 5,000 feet)
60 feet (from 5,001 feet to 10,000 feet) |
|
|
Term
The maximum allowable on-the-ground difference between pilot and copilot altitude displays and field elevation
for RVSM operation |
|
Definition
|
|
Term
| Anytime IDG loads in excess of ___ % are required during ground operations, advance thrust to a minimum of __% N1 |
|
Definition
|
|
Term
| Maximum Altimeter differences |
|
Definition
Chart on page 4-4
(at FL250 the max is 100 ft) |
|
|
Term
| Min engine oil quantity (overland) |
|
Definition
|
|
Term
| Min engine oil quantity (overwater) |
|
Definition
| 60% (12quarts) or 7 quarts plus 1 quart per total flight hour, whichever is higher |
|
|
Term
| Do not exceed __ during each start attempt. A minimum of __ is required between start attempts |
|
Definition
|
|
Term
| Do not try to engage the starter while N2 is more than |
|
Definition
|
|
Term
|
Definition
| Two consecutive extended motorings (2 to 15 min) with a minimum of 2 minutes between. Subsequent extended motorings are limited to 5 min starter operation with a 10 min cool off period in between |
|
|
Term
|
Definition
| 950 deg C (5 min/10 min for SE) |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
104.7% (20 sec)
104.0% (continuous) |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
140-155 (45 min)
140 (continuous) |
|
|
Term
| Engine idle time prior to shutdown |
|
Definition
|
|
Term
| Engine ignition shall be set to ___ if moderate or heavy rain, hail, or sleet is encountered |
|
Definition
|
|
Term
| Engine ignition shall be set to ___ if severe turbulence is encountered |
|
Definition
|
|
Term
| Assumed temperature takeoffs shall not be used when... |
|
Definition
1. runway is contaminated
2. antiskid is inop |
|
|
Term
| requirements for TO with EECs in alternate mode |
|
Definition
1. Both EECs shall be in ALT
2.Fixed derate and/or Assumed Temp TO is not allowed
3. Do not use FMC Takeoff N1
4. Use of A/T for TO is prohibited |
|
|
Term
| Reverse Thrust shall not be utilized for backing due to... |
|
Definition
| risk of foreign object ingestion |
|
|
Term
| Max sonobuoy deployment airspeed |
|
Definition
|
|
Term
| Max landing gear extend speed |
|
Definition
|
|
Term
| Max landing gear retract speed |
|
Definition
|
|
Term
| Max landing gear extended speed |
|
Definition
|
|
Term
| Symmetric G limits (clean wing or Pylons Installed, Flaps UP) |
|
Definition
|
|
Term
| Unsymmetric G limits (clean wing or Pylons Installed, Flaps UP) |
|
Definition
|
|
Term
| G limits with Landing Gear DOWN or in Transition (Symmetric and Unsymmetric) |
|
Definition
Symmetric
Max 1.8
Min 0.5
Unsymmetric
Max 1.5
Min 0.7 |
|
|
Term
| Max Taxi/Towing weight (MTW) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max Zero Fuel Weight (MZFW) |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
Active tank feeding engine: 59 deg C
Active tank feeding APU: 59 deg C
Tank not feeding APU or ENG: 62 deg C |
|
|
Term
| Fuel Temp OVHT light illuminates when fuel reaches |
|
Definition
| 57 deg C when tank feeding ENG OR 60 deg C for main tank not feeding ENG |
|
|
Term
|
Definition
3 deg C above the freezing point of the fuel
OR
-43 deg C, whichever is higher |
|
|
Term
| Max lateral fuel imbalance between main tanks 1 and 2 for ground and flight operations |
|
Definition
|
|
Term
|
Definition
|
|
Term
| During flight execution, a MODF of ___ may be used if unanticipated conditions affect fuel burn (after OFFTASK) |
|
Definition
|
|
Term
|
Definition
MODF of 6000 lbs
OR
10% of planned fuel load, whichever is higher |
|
|
Term
| If destination or alternate field OAT is forecast to be __ deg C or above, plan to increase MODF |
|
Definition
39
Note: Does not apply to EODF |
|
|
Term
| Emergency On Deck Fuel (EODF) |
|
Definition
|
|
Term
| Min fuel for ground operation of electric motor-driven pumps |
|
Definition
| 1675 lbs in related main tank |
|
|
Term
| Hydraulic quantity limits |
|
Definition
|
|
Term
| Max APU altitude (elec only) |
|
Definition
|
|
Term
| Max APU altitude (bleed only) |
|
Definition
|
|
Term
| Max APU altitude (bleed + elec) |
|
Definition
|
|
Term
| Max on ground APU altitude (bleed + elec) |
|
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 No. 1 bleed valve open
3. Isolation and engine No. 2 bleed valves open |
|
|
Term
| Do not advance thrust levers past ___ with the dual bleed light on |
|
Definition
|
|
Term
| APU generator output above ___ feet is restricted to a maximum of___ |
|
Definition
|
|
Term
| Authorized flap settings for TO |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Do not deploy the speedbrakes in flight at radio altitudes less than |
|
Definition
|
|
Term
| Authorized flap settings for non-terminal, tactical maneuvering are |
|
Definition
|
|
Term
| In flight, do not extend the SPEED BRAKE lever... |
|
Definition
|
|
Term
| When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow __ after releasing the switch before moving the switch again |
|
Definition
|
|
Term
| After a complete extend/retract cycle using ALTERNATE FLAPS (i.e., 0 to 15 and back to 0) allow __ cooling |
|
Definition
|
|
Term
| With engine bleed air switchs ON, ,do not operate the air conditioning packs in ___ for ____ |
|
Definition
HIGH
TO, approach, or landing |
|
|
Term
|
Definition
OAT <10 deg C
Visible moisture (clouds/fog with vis <1sm)
OR
When operating on ramps, taxiway, runways where snow, slush, etc may be ingested |
|
|
Term
| Do not operate in continuous moderate or severe icing for more than |
|
Definition
|
|
Term
| Max bank angle while in icing or with suspected ice accumulation on the aircraft |
|
Definition
|
|
Term
| Use of ___ with the autopilot engaged is prohibited |
|
Definition
|
|
Term
| Do not engage the autopilot for TO below |
|
Definition
|
|
Term
| Do not use HDG SEL or ROLL CWS north of ___ or south of ___ |
|
Definition
|
|
Term
| The autopilot may be engaged on instrument approaches to no lower than |
|
Definition
| 50 feet below DH/MDA, but in no case lower than 100 feet AGL |
|
|
Term
| Use of autopilot dual channel capability is prohibited in... |
|
Definition
|
|
Term
| Maneuvering with autopilot roll axis in CWS at bank angles in excess of ___ may result in excessive altitude, vertical velocity, and normal acceleration excursions |
|
Definition
|
|
Term
| Air Data Inertial Reference Unit (ADIRU) alignment should not be attempted at latitudes greater than |
|
Definition
|
|
Term
| Do not use the look-ahead terrain alerting and terrain display functions within ___ of TO, approach, or landing at an airport not contained in the EGPWS database |
|
Definition
|
|
Term
| All stores stations loaded with weapons shall be charged to a min of ____ prior to takeoff to ensure emergency jettison is possible |
|
Definition
|
|
Term
| Max fully loaded sonobuoy storage rack weight |
|
Definition
|
|
Term
| On TO, initiate smooth continuous rotation to ___ pitch attitude |
|
Definition
|
|
Term
| After liftoff, the flight director commands pitch to maintain an airspeed of |
|
Definition
| V2 + 20, until another pitch mode is engaged |
|
|
Term
| If LNAV was selected or armed before TO, LNAV guidance becomes active |
|
Definition
| at 50 feet AGL if the active leg is within 3.0nm and 5 deg of rwy heading |
|
|
Term
|
Definition
1) 15 KIAS
2) 500 fpm vsi
3) 5 deg pitch change
4) 1 dot displacement on glideslope
5) Unusual thrust lever position
6)"WINDSHEAR" aural warning
7) Red WINDSHEAR message on PFD |
|
|
Term
| Flap maneuver speeds provide approx. ____ knots above the minimum maneuvering speed for each flap setting |
|
Definition
|
|
Term
| Stabilized Approach Criteria |
|
Definition
CCCCSST
1) Correct flightpath (C)
2) Small changes required to maintain flightpath (C)
3)Speed < Vref+20 but greater than Vref (S)
4) Correct landing configuration (C)
5) Sink rate < 1000 fpm (S)
6) Thrust setting appropriate (T)
7) Checklists and briefs complete (C)
With an ILS: within 1 dot of the glideslope and localizer
Circling approach: wings level on final by 300 feet AGL |
|
|
Term
| Maximum takeoff crosswind (flaps 1, 5, DRY) |
|
Definition
|
|
Term
| Maximum takeoff crosswind (flaps > 5, DRY) |
|
Definition
|
|
Term
| Maximum takeoff crosswind (all flaps, WET) |
|
Definition
|
|
Term
| Maximum landing crosswind (all flaps, DRY) |
|
Definition
|
|
Term
| Maximum landing crosswind (all flaps, WET) |
|
Definition
|
|
Term
| Maximum takeoff and landing crosswind (all flaps, CONTAMINATED) |
|
Definition
|
|
Term
| Maximum takeoff and landing tailwind component |
|
Definition
|
|
Term
| Touch-and-go not recommended with crosswinds above__ |
|
Definition
|
|
Term
| Flaps 40 not recommended with crosswind in excess of __ |
|
Definition
|
|
