737 Limits / EPs Flashcards
Max Operating Pressure Altitude
41,000’
Maximum Takeoff / Landing
TAILWIND component
15 KIAS
Recommended Severe Turbulence Penetration Speed
Cruise : Turbulance N1 Setting from Cruise Page
Climb & Decent : 280 KIAS / .76 Mach
TAKEOFF Crosswind Component
Blended Winglet :
RCC 6 - 34 Knots
RCC 5 - 25 Knots
Split Semitar Winglet:
RCC 6 - 33 Knots
RCC 5 - 25 Knots
LANDING Crosswind Component
Blended Winglet :
RCC 6 - 40 Knots
RCC 5 - 40 Knots
Split Semitar Winglet:
RCC 6 - 37 Knots
RCC 5 - 37 Knots
Icing Conditions on Ground & for Take Off
Outside Air Temp 10 Degrees or Below
Icing Conditions Exist in flight when :
10 Degrees of below
Minimum Altitude for use of AUTOPILOT on APPROACH
ILS/GPS Coupled Approaches
- No Autoland +50’ AGL
NON-Precision Approaches
-No Autoland 50’ Below MDA/DA
Auto Flight Parameters
DO NOT USE “LVL CHG” on the final approach below 1000’ AGL
Flap Extension Altitude
20,000’
APU FIRE
- APU FIRE SWITCH….CONFIRM…PULL, ROTATE & HOLD
(Rotate to the stop & hold 1 Second) - APU SWITC H…….OFF
LOSS OF THRUST IN BOTH ENGINES
- Engine Start Switchs (Both)………..FLT
- Engine Start Levers (Both)………….CUTOFF
- When EGT Decreases: Engine Start Levers…..IDLE
RUN-AWAY STABILIZER
- Control Column………………………………HOLD FIRMLY
- Auto Pilot………………………………………..DISENGAGE
- Auto Throttle…………………………………..DISENGAGE
- Control Column & Thrust Levers……..
CONTROL AIRPLANE, PITCH, ALTITUDE, & AIR SPEED - Main Electric Stabilizer Trim…………….
REDUCE CONTROL
RUN-AWAY STABILIZER
- Control Column………………………………HOLD FIRMLY
- Auto Pilot………………………………………..DISENGAGE
- Auto Throttle…………………………………..DISENGAGE
- Control Column & Thrust Levers……..
CONTROL AIRPLANE, PITCH, ALTITUDE, & AIR SPEED - Main Electric Stabilizer Trim…………….
REDUCE CONTROL COLUMN FORCES - Choose one:
@ The Runaway stops after auto pilot is disengaged:
1. DO NOT RE-ENGAGE AUTO PILOT / THROTTLES
@The Runaway continues
1. STAB TRIM CUTOUT SWITCHES…(BOTH)….CUTOUT
2. STAB TRIM WHEEL….. GRASP & HOLD
Engine Fire
Engine Sever Damage
Engine Separation
- Auto Throttle (affected eng)………….DISENGAGE
- Thrust Lever (affected eng)……………CLOSE