-
DC-8-62 limited to normal landing flaps of _____
35
-
Runway slope limits
+/- 2%
-
Altitude limits for takeoff and landing
-1000 to 8500 ft
-
-
Max demonstrated crosswind (-62)
Takeoff
Landing
Landing with aileron unpowered and lateral control spoilers available
-
Max demonstrated crosswind (-70)
Takeoff
Landing
Landing with aileron unpowered and lateral control spoilers available
-
Max operating speed Vmo (sea level) and Mmo
339/.88
-
Maneuvering speed
(sea level and above 35,000 ft)
-
If overspeed warning occurs below Mach ____, deactivate the system and operate at a speed below _____.
-
If the wing slot disagreement light remains ON after flap retraction, the aircraft may be operated to a max speed of _______ and/or Mach _____.
If the aircraft is operated with a slot or slots open at speeds above _____, a complete inspection of slots must be made.
280/.80
230/.46
-
Wing landing light max speeds
Vmo/Mmo
-
Altimeter Limits - non RVSM
Altimeter/Field elevation difference - within 75 ft
-
Altimeter Limits - RVSM
- Altimeter/Field elevation difference - within 75 ft
- Primary altimeter differences (any altitude) - within 200 ft of each other
NOTE: All aircraft require 2 altitude reporting sources and DADC must be operational prior to entry into RVSM airspace.
-
Do not use recirc fans while using _________.
ground ACM
-
When operating only recirc fans on the -62, _____________.
2 fans must be operated
-
Do not turn on a Recirc Fan unless ____________________, except when _____________.
- 2 or more generators are operating in parellel
- External Power
-
NASI Pneumatic Flow Control System
For cockpit temp control, the temp diverter valve must be actuated operating on the ______only.
RH flow control system
-
NASI Pneumatic Flow Control System
Do not initiate use of cabin ram air with cabin pressure above ______.
1.0 PSI
-
NASI Pneumatic Flow Control System
Never exceed delivery duct temp of _______.
100* C
-
NASI ACM
Max duct temp
100* C
-
NASI ACM
Max compressor temp
175* C
-
NASI ACM
Max turbine temp
100* C
-
NASI ACM
Max altitude for dispatch with one Flow Control Valve inop
25,000 ft
-
NASI ACM
If ACM's are not OFF below _____, max cabin differential pressure may be unattainable
4* C RAT
-
NASI Flight Deck Floor Heat
Cockpit floor heat should not be used whenever OAT is above ______.
11* C, 50* F
-
Air Conditioning System Limitations - 70 Series
Max altitude dispatch with one pack inop:
25,000 ft
-
Max cabin differential available from auto control
8.77 PSID
-
Cabin pressure safety relief valve begins to open at _____ and fully open at _____.
-
For unpressurized flight the _______ must not be used and the ______ must be operative.
Forward cargo compartment
Radio Rack Blower
-
If the Radio Rack Blower fails during upressurized flight and a Cabin Press Diff of ___PSI cannot be maintained, turn OFF the _____, ______, and ______.
2
weather radar, ATC transponder, HF radios
-
The Autopilot must not be operated while on _______ or _________.
manual aileron or rudder control
-
Max speed for autopilot operation
Vmo/Mmo
-
On aircraft equipped with a pitot cutoff switch, prior to placing the switch to the off position:
disengage autopilot and DO NOT re-engage the autopilot until the pitot cutoff switch is returned to the ON position.
-
Minimum altitude with autopilot engaged
En route:
600 ft AGL
-
Minimum altitude with autopilot engaged
Non-precision approches:
50 ft below MDA but not less than 600 AGL
-
Minimum altitude with autopilot engaged
Coupled approaches
70 ft AGL
-
Do not use approach coupler for ____________
back course approaches on any localizer
-
Prior to entering RVSM airspace, ______ and ______ must be operational.
Autopilot
- DADC
- NOTE: if DADC fails altitude hold function will be lost.
-
CSD Oil temp rise
Normal
Max
0*-11* C
17* C
-
CSD Outlet Oil temp
Normal
Max
20*-132* C
146* C
-
AC Load Meter normal ground ops
1.0
-
Normal Batt volts
26 +/- 4
-
Ignition Inverter
Normal
Allowable
-
Generator overload ratings
- 1.5 for 5 min
- over 1.5 for 5 sec
-
Do not ______ or _______ with main cargo door unlatched
tow or taxi
-
The Main Cargo Door may be opened to the ____ degree or ____ degree position with max wind velocity of ____ kts (steady)
86, 166
40 kts
-
If wind velocities from ____ to _____ anticipated, the main cargo door may be opened to the ____ position if airplane parked with wind direction against right side.
40-65 kts
86 degree
-
Emergency exit lights must be _____ for all flight ops
armed
-
Photoluminescent Aisle Path Marking System
The pilot must verify that the system is ______ prior to flight.
fully charged
-
Photoluminescent Aisle Path Marking System
Max length of night flight ops without recharging the system
NOTE: flight duration not limited if _________
6.5 hours
overhead ceiling lighting is operated in the "ON" and "BRIGHT" or "HIGH" setting.
-
No cargo or baggage may be carried in the lower cargo compartments if the ______ on the CDU is not illuminated.
"SYS OK" light
-
Airplane must lande within ______ following discharge of lower cargo compartment suppression system (COMBI only).
180 minutes
-
Aileron and Rudder power must be _____for all takeoffs.
ON
-
Stall warning must be _____ for all flight ops.
ON
-
If PTC malfunctions inflight, place switch to _____, pull the CB's and observe following speed limits:
Overide
Vmo/.78
-
Max altitude with PTC inop (except all-cargo config)
39,000 ft
-
Fuel dum chute operation speed range:
Min
Max
-
Max flap setting for dump chute ops
- 23/25
- Landing gear up or down
-
Prior to retracting fuel dump chute after dumping, dump chutes must be place in the _____ position for ______.
-
Fuel dump actuator limits
70 sec on, 5 min off
-
Hydraulic system pressure
Normal
System Relief
2800-3300 PSI
3300-3500 PSI
-
-
Engine anti-ice ground warm-up
JT3D
80% N2 for 20 seconds, repeat every 10 min
-
Engine anti-ice ground warm-up
CFM-56
Min power setting is 24% N1 when anti-ice turned on
-
Place windshield heat to FULL POWER during descent from cruise altitude when _____
OAT is below ISA standard day temp
-
Max speed with windshield heat inop
Center Pane:
Side Pane:
260 kts below 10,000 ft
285 kts below 10,000 ft
-
Max speed for cracked center or side windshield.
Affected window must be ______.
235 kts below 10,000 ft
OFF
-
Minimum desired pneumatic manifold temp during deicing:
190* C
-
Minimum pneumatc manifold air pressure for Rain Removal
15 PSI
-
Rain Removal system must not be turned on while pneumatic system is being supplied with High pressure and High Temp air above _____ from a ground pneumatic source.
200* F
-
Max tire ground speed
195 kts (225 mph)
-
Max brake wear limit
1/2 inch
-
Walk-Around O2 bottle pressure
1620 PSI +/- 35 PSI, for +/- 10 degrees deviation from 70* F (4 cubic ft)
-
Manifold Air Temp
Min
Normal
Max
182* C
214* - 242* C
258* C
-
Manifold Pressure, CFM-56
Min
Normal
Max
12.5 PSI
38 PSI
53 PSI
-
Manifold Pressure, JT3D
Min
Normal
Max
12.5 PSI
38 PSI
48 PSI
-
-
-
-
-
Oil Temp limits, CFM-56
Min
Max, (____ permitted for ____ minutes)
5* C
135* C, (145* C permitted for 10 minutes)
-
Oil Temp limits, JT3D
Min
Max, (____ permitted for ____ minutes)
N/A
132* C, (143* C permitted for 15 minutes)
-
Max oil consumption (70 series)
.4 gallons/hr
-
Max oil consumption (60 series)
- 1.6 quarts/hr (no external oil leakage).
- Max oile consumption is 2 quarts/hr
-
Engine starter limits, CFM-56
Max starter engagement speed inflight
20% N2
-
Engine starter limits, CFM-56
Max consecutive start attempts allowed
3
-
Engine starter limits, CFM-56
Required cooling period between start attempts
30 seconds
-
Engine starter limits, CFM-56
Starter duty limits
3 attempts/5 min on, then 10 min off
After 2 cycles: 30 min off
-
Engine starter limits, JT3D
N2 starter disengagement speed
Normal
Max
35%
40%
-
Engine starter limits, JT3D
N1 starter disengagement speed
Normal
Max
15%
20%
-
Engine starter limits, JT3D
Starter duty cycles
1 min on, 1 min off, 1 min on, 5 min off
Motoring only: 2 min on, 5 min off
NOTE: if starting or motoring sequence interrupted, starter button must not be pressed again until N2 indicates zero.
-
Thrust Reverser restrictions
After touchdown do not use power settings beyond reverse detent until ________
nose wheel is on the ground
-
Thrust Reverser restrictions
Wing flaps _______ for all in-flight reverser ops
must be completely retracted
-
Except in an emergency, all reverse levers should be at reverse idle detent or forward idle at speeds below ______
60 kts
-
RVSM min equipment list
Autopilot (DADC must also be operational for altitude/pitch hold)
Transponders (requires TWO separate sources of altitude information)
Altimeters - BOTH altimeters must be operative in External and Self-Sensing Mode
Altitude Alert System
TCAS
-
Altimeter allowance/differences for RVSM
Altimeter/field elevation differences within 75 ft
Primary altimeter differences (at any altitude) within 200 ft of each other
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