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96 Cards in this Set
- Front
- Back
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Maximum Taxi
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836,000
(AOM 101-5) |
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Maximum Takeoff (Stage 2,3)
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833,000 pounds
(AOM 101-5) |
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Maximum Landing (Stage 3)
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630,000 pounds
(AOM 101-5) |
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Maximum Landing, Flaps 30 (Stage 3)
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630,000
(AOM 101-5) |
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Maximum Zero Fuel Weight
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590,000 pounds
(AOM 101-5) |
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Maximum Inflight Landing Flaps
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650,000 pounds
(AOM 101-5) |
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Maximum Fuel Transfer Weight
(Reserve 1 & 4) |
703,000 pounds
(AOM 101-5) |
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Tire rating
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Rated for 235 MPH and 55,700#
(AOM 101-5) |
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CABIN DIFFERENTIAL PRESSURE
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8.9 psi normal, 9.4 psi maximum
(AOM 101-7) |
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OPERATION WITH PACKS OFF
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Not above 110°F (44°C) up to 2,000 feet above takeoff or landing airport
(AOM 101-7) |
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PACK OPERATION AT TEMPERATURE OF 110 °F (44 °C) OR LESS
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PACKS OFF operation is limited to 2,000 feet above takeoff or landing airport.
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PACK OPERATION AT TEMPERATURE ABOVE 110 °F (44 °C)
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To ensure adequate pre-cooling, operate 2 or more packs prior to taxi. When pack #2 is operated during takeoff, with bleed air furnished by APU, the above limitations do not apply. Do not turn on packs #1 or #3 prior to reaching 400 feet AGL. Either pack #1 or #3 may be turned on above 400 feet AGL if four engines are operating. If engine failure occurs, turn on packs #1 and #3 only after minimum gross height for obstacle clearance has been reached.
(AOM 101-7) |
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TAKEOFF WITH APU SUPPLYING PACK #2 OPERATION
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If engine failure occurs, do not change air conditioning bleed configuration until minimum height for obstacle clearance has been achieved.
(AOM 101-7) |
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AILERON TRIM
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Use of aileron trim with the autopilot engaged is prohibited.
(AOM 101-7) |
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ALTITUDE SELECT
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Do not use if rate of descent is greater than 5,000 feet per minute.
(AOM 101-7) |
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AUTOLAND
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Not approved.
(AOM 101-7) |
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Autopilot Engaged – Minimum Altitudes
•Enroute •Non-precision approaches •Precision (Coupled Approaches) |
ENROUTE (including climb)
1200 feet AGL NON PRECISION APPROACHES 50 feet below MDA COUPLED APPROACHES (Single Autopilot) 50 feet below DH but not less than 75 feet AGL (AOM 101-7) |
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ALTERNATING CURRENT (AC) SPECIFICATIONS
•Volts •Freq's |
Voltage: 115 ±5 Volts AC
Frequency: 400 ±5 Hertz (AOM 101-8) |
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Generator Load-
•Isolated •3 or 4 generators paralleled •2 generators paralleled |
ISOLATED:
54 kilowatts (81 kilowatts for 5 minutes) 3 or 4 GENERATORS PARALLELED: 51 kilowatts each 2 GENERATORS PARALLELED: 81 kilowatts total (AOM 101-8) |
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DIRECT CURRENT (DC) SPECIFICATIONS
•Battery & TR •APU Battery •Battery Minimum |
Battery and T/R: 25 to 32 Volts DC
APU Battery: 25 to 36 Volts DC Battery Minimum: 22 Volts DC (AOM 101-8) |
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MAX TR LOAD
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54 Amperes per T/R with Equipment Cooling “No Airflow” light on.
75 Amperes continuous. 93 Amperes for 30 minutes. 113 Amperes for 5 minutes. (AOM 101-8) |
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MAX AUXILIARY LOAD (APU OR EXTERNAL)
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250 Amperes.
115 ± 5 Voltage 400 ± 5 Frequency (AOM 101-8) |
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UPPER DECK ESCAPE SLIDE
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The upper deck escape slide must be in the forward locked position whenever personnel occupy the upper deck cabin during taxi, takeoff and landing.
(AOM 101-8) |
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SMOKE BARRIER DOOR
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The smoke barrier door must be closed during taxi, takeoff, flight and landing in aircraft upper deck.
(AOM 101-8) |
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MAXIMUM OPERATING LIMIT SPEED
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The maximum operating limit speed (VMO) shall not be deliberately exceeded in any regime of flight.
(AOM 101-8) |
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MAXIMUM AIRSPEED, RVSM AIRSPACE
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For all operations in RVSM airspace, M0.90 is not to be exceeded.
At gross weights less than 520,000 pounds between FL290-340; M0.87. (AOM 101-8) |
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Flap Speeds
•1 •5 •10 •20 •25 •30 |
275 KIAS
255 KIAS* 238 KIAS 231 KIAS 205 KIAS 180 KIAS *Flap 5 placard speed for N752SA and N753SA is 250 KIAS. (AOM 101-8) |
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Speed brakes with Flaps Extended
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NOT AUTHORIZED
(AOM 101-8) |
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ALTERNATE FLAP EXTENSION
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The extended speed from position 25° to 30° is 160 KIAS.
(AOM 101-8) |
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MAX ALTITUDE FOR FLAP EXTENSION
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20,000 feet.
(AOM 101-8) |
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AUTOMATIC SPEEDBRAKES
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Do not arm automatic speed brakes at ambient temperatures of -42 °F (-41 °C) and below.
If hydraulic pressure in system #1 and #4 is lost, deactivate auto speed brakes. (AOM 101-8) |
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FUEL FREEZE POINT
•Jet A •Jet B |
Jet A: -40° C.
Jet B: -50° C. (AOM 101-9) |
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FUEL IMBALANCE – MAXIMUM WEIGHT
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Between Main Tanks 1 and 4:
1500 pounds. Between Main Tanks 2 and 3: 1500 pounds Between Wing Tanks: 3000 pounds. (AOM 101-9) |
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Low Fuel Quantity Operation
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Do not exceed 8° nose up body angle with any MAIN TANK containing 2,000 pounds or less.
(AOM 101-10) |
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Fuel Loading- RESERVE TANKS
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Reserve tanks 1 and 4 must be full at or above 703,000 pounds.
(AOM 101-10) |
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Fuel Loading- CWT
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•The CWT quantity indication system must be operative to dispatch with CWT mission fuel.
•The CWT may be emptied normally in an emergency fuel jettison. •The CWT fuel may be used in a low fuel situation. (AOM 101-11) |
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Fuel Loading- General
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Each main tank must contain a sufficient fuel quantity for engine start, taxi, takeoff and landing.
Tanks may be loaded simultaneously and in any sequence. Main and reserve tanks must be loaded so that the resulting fuel load is symmetrical about the airplane centerline. (AOM 101-10) |
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CWT LIMITATION, CONDITION 1
CWT fuel quantity between 4,000 pounds and 17,000 pounds prior to engine start: |
Pumps OFF until stabilized cruise, then-
pumps ON. pumps to OFF at the FIRST OCCURRENCE of the following: 3,000 pounds OR Pump Low Pressure light on, then- Scavenge rest. (AOM 101-11) |
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CWT LIMITATION, CONDITION 2
CWT fuel quantity greater than or equal to 17,000 pounds but less than 50,000 pounds prior to engine start: |
Pumps ON in climb to 7,000 pounds, then-
Pumps OFF until STABILIZED CRUISE, then- Pumps ON pumps to OFF at the FIRST OCCURRENCE of the following: 3,000 pounds OR Pump Low Pressure light on, then- scavenge rest. (AOM 101-11) |
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CWT LIMITATION, CONDITION 3
CWT fuel quantity greater than 50,000 pounds prior to engine start: |
Pumps ON in climb AND cruise, then-
pumps to OFF at the FIRST OCCURRENCE of the following: 3,000 pounds OR Pump Low Pressure light on, then- Pumps OFF, scavenge rest. (AOM 101-10) |
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Tripped Fuel Pump Circuit Breaker
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Pump damage may be accompanied by tripped circuit breakers.
Therefore, a tripped fuel pump circuit breaker SHOULD NOT BE RESET. (AOM 101-10) |
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Center tank pump switch is ON, with a continuous low pressure indication present
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Do not cycle the center pump switch OFF and then back ON.
(AOM 101-11) |
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HYDRAULIC PRESSURE
•Normal: |
2800-3200 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•ADP on at: |
2600 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•Pump Low Pressure Light On at: |
1200 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•Pressure Relief at: |
3450-3650 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•Brake Accumulator Air Charge: |
750 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•Electric pump on at: |
1800-3200 psi
(AOM 101-12) |
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HYDRAULIC PRESSURE
•Hydraulic pump output above 3200psi |
Inflight, any hydraulic pump whose output pressure is above 3,200 psi should be depressurized.
However, if output pressure is not in red band range, the pump may be turned on for landing. (AOM 101-12) |
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HYDRAULIC SYSTEM
•Minimum Quantities |
Minimum for dispatch is all quantities in the green band, or 7 gallons, No. 1 and No. 4 and 4 gallons, No. 2 and 3.
(7,4,4,7) (AOM 101-12) |
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HYDRAULIC SYSTEM
•Low Fuel Considerations |
On the ground, EDP & ADP must not be operated for more than 15 MINUTES when the fuel quantity is below the following quantity.
Tanks 1 & 4, 2500 pounds. Tanks 2 & 3, 5300 pounds. Same rule applies to #4 Electric pump and (if installed) #1 Electric Pump. (AOM 101-12) |
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HYDRAULIC SYSTEM
•Low Qty Light On at: |
1.5 gallons (1 & 4)
2.5 gallons (2 & 3) (AOM 101-12) |
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ICE AND RAIN PROTECTION
Window Heat |
Window heat to both No. 1 windows and both No. 2 windows must be on for all normal flight conditions.
The window heaters may be inoperative on one No. 1 or one No. 2 window provided operation is not predicated on flights into known or forecasted icing; windshield air (anti-fog system) are operative and remaining No. 1 and No. 2 window heaters are operative. (AOM 101-13) |
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ICE AND RAIN PROTECTION
Nacelle Anti Ice |
Nacelle anti-ice must be on when icing conditions exist or are anticipated, except during climb and cruise when temperature is below -40° SAT.
Nacelle anti-ice must be on prior to and during descent in all icing conditions. (AOM 101-13) |
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Icing conditions present when:
•In Flight •On Ground |
Inflight:
TAT 10° C or below and visible moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). On the ground and for takeoff: OAT 50° F (10° C) or below with visible moisture in any form present (clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals) and where surface snow, ice, standing water or slush may be ingested by the engine or freeze on engine, nacelle or engine sensor probes. (AOM 101-13) |
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MINIMUM N1 RPM FOR OPERATING IN ICING CONDITIONS, EXCEPT FOR LANDING
•At or above 10,000' •Below 10,000' •No High Stage Bleed available |
50% N1 at or above 10,000 feet.
45% N1 below 10,000 feet. 70% N1 if no high stage bleed available. (AOM 101-13) |
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ANTI-ICE WITH INOPERATIVE ENGINE(S)/BLEEDS
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3 engines/bleeds operating: Max 2 packs on.
2 engines/bleeds operating: Max 1 pack on. (AOM 101-13) |
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LANDING GEAR
•Body Gear Steering |
Body Gear Steering must be deactivated for takeoff and landing.
(AOM 101-13) |
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LANDING GEAR
•Tires |
Ply rating: 34 Ply
Speed rating: 235 MPH (AOM 101-13) |
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LANDING GEAR
•Operating Speeds |
Extend: 270 knots / M 0.82
Retract: 250 knots / M 0.82 Extended: 320 knots / M 0.82 (AOM 101-13) |
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OXYGEN PRESSURE
•Crew •Passengers •Walk around portable bottle |
Crew (“C” needle):
800 psi; 1200 psi with jumpseat occupied. Personnel (“P” needle) (when on board): 1400 psi Walk around portable bottle: 1500 psi (AOM 101-13) |
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OXYGEN REQUIREMENTS FOR UPPER DECK OCCUPANTS
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An adequate quantity of oxygen for sustenance must be provided for each occupant for flight at 25,000' CABIN ALTITUDE to the nearest suitable airport.
(AOM 101-13) |
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APU
•Inflight use (As placarded) |
Below 15,000 feet (20,000 feet for inflight start – if placarded).
Not permitted in icing conditions. Electrical Power: Not Permitted inflight except up to 15,000 feet with all engines generators inoperative. |
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APU EGT
•Starting •Continuous |
Starting:
900° C or 990° C if a 1000° C gauge is installed. Continuous: 670° C or 657° C if a 1000° C gauge is installed. (AOM 101-14) |
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APU STARTER
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1 minute “ON,” 5 minutes “OFF,” 3 attempts per hour.
61 seconds to 90 seconds “ON,” 15 minutes “OFF,” 2 attempts per hour. (1/5/3 or 1.5/15/2) (AOM 101-14) |
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WIND LIMITS FOR NOSE AND SIDE CARGO DOOR
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Door opened: 65 knots.
Door operating: 40 knots. (AOM 101-14) |
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FULL FLIGHT REGIME AUTO THROTTLE SYSTEM (FFRATS)
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Do not use the auto throttle system to set thrust with engine intermix.
Do not re-engage auto throttle system on the approach if it has automatically disengaged. (AOM 101-14) |
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TAT/N1 LIMIT SYSTEM
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Do not use TAT/N1 Limit System with engine intermix.
(AOM 101-14) |
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LITTON 92 INS
•SIDS/STARS limitation |
SID(DP)s or STARs derived from MANUAL ENTRY of the waypoints, or generated from a PC, are NOT APPROVED FOR USE.
INS cannot be used as the sole source of navigation for STARs unless updated minimum 1 hour prior to commencing the STAR. All approved SID(DP) and STAR procedures are coded by a unique name and are found contained in the Jeppesen Manual. (AOM 101-15) |
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PENNY & GILES ENGINE INSTRUMENT DISPLAY SYSTEM (EIDS)
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The “compacted” view (reversion mode) is approved for takeoff only when engine digital mode is selected on the other display.
The system requires two fully working Display Units, with no major bit errors occurring. If any major bit errors occur prior to takeoff, TAKEOFF IS PROHIBITED. Takeoff will not be initiated if the engine instruments display any engine exceedance. (AOM 101-16) |
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GE CF6 ENGINES
•Max EGT Start |
750 °C (900 °C allowed for up to 40 seconds)
(AOM 101-16) |
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GE CF6 ENGINES
•Max EGT Continuous |
910° C
(AOM 101-16) |
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GE CF6 ENGINES
•Max EGT Takeoff |
945° C (5 Minutes)
(AOM 101-16) |
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GE CF6 ENGINES
•Max EGT Acceleration |
960°C (2 Minutes) *
(operation in the 945° to 960 °C range will not normally require crew action during the 2 minute acceleration limit.) (AOM 101-16) |
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GE CF6 ENGINES
•6 conditions requiring IGNITION |
EITHER System 1 or System 2 FLT START for the following conditions:
•Landing. •Heavy rain. •Severe turbulence. •Volcanic dust (Use System 1 and System 2). •Icing conditions. •Standing water or slush on runway. (AOM 101-16) |
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GE CF6 ENGINES
•Reverse Thrust |
Ground operation only
(AOM 101-16) |
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GE CF6 ENGINES
•Oil Pressures |
Normal oil pressure range: Green band.*
Minimum: Yellow band. *Cold weather starting may exceed 90 psi until oil viscosities are reduced by increasing oil temperature. LIMIT TO IDLE POWER until oil pressure normal. (AOM 101-16) |
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GE CF6 ENGINES
•Oil Quantity |
ENROUTE: Minimum oil quantity per engine for dispatch: 1/2 full, as appropriate.
MAINTENANCE STATION: Full. (AOM 101-16) |
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GE CF6 ENGINES
•Oil Consumption |
If the oil consumption of any engine is more than 1/2 quart per hour, enter in aircraft logbook.
(AOM 101-16) |
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GE CF6 ENGINES
•Oil Temperature |
Maximum Continuous: Green Band.
Maximum 15 minutes: Yellow Band. Maximum: Red Radial. (AOM 101-17) |
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GE CF6 ENGINES
•Starter Duty Cycle |
5 minutes ON, 30 seconds OFF for each minute of operation.
10 minutes cooling after 2 consecutive 5 minute cycles. N2 must be ZERO before restart attempt. (In flight 20% N2 minimum) (AOM 101-17) |
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P&W JT9D
•Max EGT Start |
535° C
(AOM 220C-4) |
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P&W JT9D
•Max EGT Continuous |
620°C
(AOM 220C-4) |
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P&W JT9D
•Max EGT Takeoff |
685° C (5 minutes)
(AOM 220C-4) |
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P&W JT9D
•Max EGT Acceleration |
660°C (2 minutes)
(AOM 220C-4) |
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P&W JT9D
•Max N1 RPM |
106.2%/ 105.8%*
*N1 gages showing 105.8% limit markings may be used, provided that gage limit is observed. (AOM 220C-4) |
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P&W JT9D
•Max N2 RPM |
103.5%
(AOM 220C-4) |
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P&W JT9D
•5 conditions requiring IGNITION |
BOTH System 1 and System 2 on for the following conditions:
•Heavy Rain •Severe Turbulence •Volcanic dust •Icing condition •Standing water or slush on runway. (Not required for T/O & Landing as in GE engines) (AOM 220C-4) |
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P&W JT9D
•Oil Pressure |
Normal oil pressure: 40-60 psi *
Minimum: 35 psi *Cold weather starting may exceed 60 psi until oil viscosities are reduced by increasing oil temperature. LIMIT TO IDLE POWER until oil pressure normal. (AOM 220C-5) |
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P&W JT9D
•Oil Consumption |
If the oil consumption of any engine is more than 1 QUART PER HOUR, enter in aircraft logbook.
(AOM 220C-5) |
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P&W JT9D
•Starter Duty Cycle |
0-5 Minutes ON, no cooling required but N2 must drop to zero prior to re-engagement.
5-10 Minutes ON, 10 minutes COOLING 10-15 minutes ON, 15 minute COOLING (AOM 220C-5) |
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P&W JT9D
•Oil Quantity |
ENROUTE: Minimum oil quantity per engine for dispatch: 1/2 full, as appropriate.
MAINTENANCE STATION: Full. (AOM 220C-5) |
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FUEL- MAXIMUM TEMPERATURE
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+54.5 °C (130 °F)
+43 °C (110 °F) JP-4. (AOM 101-9) |
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MAXIMUM CABIN DIFFERENTIAL FOR TAKEOFF AND LANDING
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220 feet below field pressure altitude (0.11 psi)
(AOM 101-7) |
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FUEL- MINIMUM TEMPERATURE
|
Fuel freeze point +3 °C above the freezing point of the fuel being used.
(AOM 101-9) |
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11 conditions requiring
MAX THRUST TAKEOFF |
•When ambient TEMPERATURE is BELOW -47°F (-44°C).
•When takeoff runway is OTHER THAN DRY (A grooved runway is considered dry when there is no standing water or other clutter). •When HEADWIND ADJUSTMENT has been used to increase allowable takeoff gross weight. •When takeoff is to be made with a TAILWIND. •When ANY BRAKES are DEACTIVATED. •When SPARE ENGINE is carried. •When an N1 (GE) or EPR (P&W) INDICATOR INOPERATIVE. •When available runway length is LESS THAN 7000 feet. •When DDPG weight or performance PENALTIES are applied •When the probability of WINDSHEAR exists •When the aircraft has been DE-ICED. (Cold WX Manual 4.1-15) (QRH; PP-6) (T-174; 4.1-15) |
