Limitations Flashcards
Reinforced cockpit door
A check of the remote access system must be performed once each flight day.
Reduced Thrust Operation
Not authorized on…
The operator must have a means to verify availability of takeoff thrust to ensure engine does not exceed authorized limits
Not authorized on runaways with standing water, slush, loose or compact snow or wet ice, can do it on a wet runway with wet runway numbers
Not permitted if items affecting performance cause a significant increase in crew workload, line inop engine guages, anti-skid inop, or non standard takeoff technique is required.
Evac system
Slide girt bars must be inserted into the floor fittings prior to departure, and until arrival at the passenger loading ramp.
The emergency handle on the aft pressure bulkhead must be exposed, and the normal handle covered, prior to departure from the pax loading ramp until arrival at pax offloading ramp
Circuit breakers
Do not reset: Hydraulic auxillary pump Fuel pump Fuel qty indicating system Lav flush motor Galley power
Emergency lights
Must be armed for all flight operations
Wing landing lights
Cycles
Ambient
Cool did 1.5 minutes after initial extension or retraction, and 3.5 minutes after each subsequent one.
Do not have lamps on in ambient air for periods over 10 minutes.
Max weights Taxi Takeoff Landing ZFW
115,000(119,000)
114,000(118,000)
110,000
100,500
Maneuvering limit load Factors
Flaps/slats retracted 2.5 to -1.0 G
Either extended 2.0 to 0.0G
Runway slope
Tailwind
Vmo
Mmo
1.7 to -2.0%
10kts
340kts up to 26,000ft
.82 above 26,000ft
Engine crosswind minutes
40 kts
For tailwinds > 10kts or crosswinds >40kts limited to 50% N1 and taxi and ground handling only
Max altitude
37,000ft
ACARS
Limited to messages which do not create unsafe conditions if;
- Message is delayed or not received
- Message is delivered to wrong recipient
- Message content may be frequently corrupt
Windshield heat
Windshield anti ice must be on for all flight operations except:
1. Do not operate on a cracked windshield
2. Do not exceed 315kts below 10,000ft if windshield heat is inop on any window
Cracked window limits below 10,000ft are
315kts outer glass
235kts inner glass
Cabin pressurization
Max cabin diff 7.86
Max emergency relief is 8.27
If manual mode takeoff and land unpressurized
Air conditioning
FLOW switch must be in NORM for takeoff if air conditioning is used