Limitations Flashcards
Maximum Takeoff and Landing Tailwind Component
15 Knots
Maximum Speeds
Observe Vmo Pointer and Gear/Flap Placecards
Turbulent Airspeed
280 Konts / .76 Mach
Minimum Runway Width
98 feet
Flight Deck Door Access System
Verify that an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day
Passenger Evacuation
Cabin occupants >1, all doors must be armed and verified prior to taxi, takeoff and landing.
0 Cabin occupants, forward doors only required to be armed and verified prior to taxi, takeoff and landing
(On flights with one or more occupants in the cabin, all entry door evacuation slides must be armed and engagement of the girt bar with door still verified prior to taxi, takeoff, or landing. On flights with no occupants in the cabin, only the two forward escape slide retention bars (girt bars) must be installed during taxi, takeoff, and landing.)
HF Radios/Fueling
Do not operate HF Radios durning Refueling
Flaps Certified for Takeoff
Flaps 1,5,10,15,25
Cabin Altitude Briefing
As part of the takeoff briefing before engine start for the first flight of the day or following any change of either flight crew member, the PIC shall ensure the CABIN ALTITUDE WARNING indications and procedures are briefed in accordance with normal procedures of this manual. If a CABIN ALTITUDE WARNING LIGHT is installed, this briefing is not required.
Engine Anti-Ice System
Must be on:
All ground and flight operations when:
Icing conditions exist or are anticipated, except climb and cruise with SAT -40 deg C or greater.
Must be on prior to and during decent in icing conditions including temperatures below -40 deg C
(The engine anti-ice system must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when SAT is below -40 deg C. Engine anti-ice must be on prior to and durning decent in icing conditions, including temperatures below -40 deg C.)
Wing Anti-Ice System
Do not use wing anti-ice as a substitute for ground deicing/ anti-icing and inspection procedures that are necessary to comply with TEM deicing manual procedures. Do not operate wing anti-ice on the ground when the OAT is above 10 deg C (50 deg F)
Aileron Trim with Autopilot Engaged
Prohibited
Autopilot takeoff engagement altitude
400 feet AGL or greater.
Single Channel Approach - Autopilot mandatory disengagement altitude
50 feet AGL
Do not use Level Change on final approach below what altitude
1000 feet AFE
Maximum takeoff EGT
950 deg C
Maximum Continuous EGT
925 deg C
Maximum Start EGT
725 deg C
Maximum Altitude for Flap Extension
20,000 feet pressure altitude
In flight, do not extend the speed brake lever beyond…
The flight detent
Avoid rapid and large alternating control, inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. Large side slip angles) as they may result in structural failure at any speed, including below….
VA
Holding in Icing conduction with Flaps extended
is PROIBITED
Do not apply speed brakes in flight at flap settings greater then
Flaps 10
Do not deploy speed brakes at radio altitude less than
1000 feet
Flap 15 landings may be performed when required by a non-normal procedure. When is flaps 15 not authorized
Normal landings
Vertical Situation Display
When installed, all non-ILS/ non-precision approaches, the PM must have the Vertical Situation Display (VSD) selected to on to enhance ground/ terrain situational awareness
Fuel pump circuit breaker
Do not reset
Maximum Fuel Temperature
49 deg C
Minimum fuel temperature
Fuel freeze point of fuel being used +3 deg C or -43 deg C, whichever is higher (warmer)
Operating Center Tank Pump on ground
Must not be positioned to ON unless center tank fuel quantity exceeds 1000 pounds, except when refueling or transferring fuel
Center Tank Fuel Pumps must not be ON unless
Personel are available in the flight deck to monitor low pressure lights
Center tank fuel pumps must be OFF when…
< 5000 pounds and when the aircraft is readied for initial taxi
<1000 pounds during climb
<3000 pounds durning decent and landing
Operation with assumed temperature reduced takeoff thrust is no permitted with
Anti-Skip Inoperative
Runway Slope
+/- 2%
Maximum Flight Operating Latitude
82 deg North and 82 deg South
Maximum Operating Altitude
41,000 feet
Maximum Takeoff and Landing Altitude
8,400 feet pressure altitude
Flight Maneuvering Load Acceleration Limits
Flaps Up: +2.5g to -1.0g
Flaps Down: +2.0g to 0.0g
B737 certificated in the Transport Category
14 CFR, Part 25 and Part 36
B737 Kind of Airplane Operations
Both day and Night, when required equipment is installed and approved in accordance with the applicable FAR
VFR
IFR
Icing Conditions
Extended Over-water
Flight Crew
Pilot and CoPilot
Photoluminescence Floor Emergency Lighting System
PL Floor Emergency Lighting must be charged in accordance with approved procedures. Refer to AFM Supplements Chapter for Aircraft Specific Procedures.
Brake Cooling
Observe minimum ground time shown on the Recommended Brake Cooling Schedule chart in the Performance Inflight section the QRH
Maximum Taxi Weight
174,700 lbs
Maximum Takeoff Weight
174,200 lbs
Maximum Landing Weight
146,300 lbs
Maximum Zero Fuel Weight
138,300 lbs
Maximum Cabin Differential
9.10 psi
Maximum allowable cabin differential pressure for takeoff and landing
0.125 psi
Maximum Time Limit for Takeoff Thrust
5 Mins
Maximum N1 RPM
104%
Maximum N2 RPM
105%
Minimum Oil Pressure
13 psi
Maximum Fuel Temperature
49 deg C
Fuel Tanks
No.1 and No.2
1288 gallons per tank
9144 lbs per tank
Fuel tanks
Center
4081 Gallons
28,803 lbs
Fuel Tanks
Total usable quantity
6,875 gallons
46,063 lbs
