
737 Flight Crew Operations Manual
Performance Inflight
Text
737-8/LEAP-1B27
FAA
CATB
MN-FLT-OH-201
PI.18.5
Te
m
po
ra
ry
R
ev
is
io
n
One Thrust Reverser Inoperative
Wet runway takeoff performance presented for all brakes operating is
based on the use of one thrust reverser during deceleration. When
operating with a thrust reverser inoperative, the runway/obstacle limited
takeoff weight and V1 speed must be reduced to account for the reduced
deceleration capability.
A simplified method which conservatively accounts for this is to reduce
the normal wet runway/obstacle limited weight by 1250 kg and the V1
associated with the reduced weight by two knots.
If the resulting V1 is less than V1(MCG), takeoff is permitted with V1 set
equal to V1(MCG) provided the accelerate stop distance available
corrected for wind and slope exceeds approximately 1400 m.
Anti-Skid Inoperative
When operating with anti-skid inoperative, the field limit weight and V1
must be reduced to account for the effect on accelerate-stop performance.
Anti-skid inoperative is only allowed on a dry runway. A simplified
method which conservatively accounts for the effects of anti-skid
inoperative is to reduce the normal dry field/obstacle limited weight by
8700 kg and the V1 associated with the reduced weight by the amount
shown in the table below.
If the resulting V1 is less than V1(MCG), takeoff is permitted with V1 set
equal to V1(MCG) provided the dry accelerate-stop distance available
adjusted for wind and slope exceeds approximately 2000 m.
Detailed analysis for the specific case from the Airplane Flight Manual
may yield a less restrictive penalty.
Takeoff %N1
To find Max Takeoff %N1 based on normal engine bleed for air
conditioning packs on, enter Takeoff %N1 Table with airport pressure
altitude and airport OAT and read %N1. Apply %N1 adjustments as
provided when applicable.
ANTI-SKID INOPERATIVE V1 ADJUSTMENTS
FIELD LENGTH (M)
V1 ADJUSTMENT (KIAS)
2000
-22
2500
-19
3000
-16
3500
-14
4000
-12
October 26, 2021
Содержание 737-8
Страница 12: ...737 MAX Flight Crew Operations Manual Preface Introduction 0 2 6 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 146: ...737 MAX Flight Crew Operations Manual Normal Procedures Amplified Procedures MN FLT OH 201 NP 21 10 March 1 2021...
Страница 1008: ...737 MAX Flight Crew Operations Manual Electrical System Description 6 20 18 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1074: ...737 MAX Flight Crew Operations Manual Fire Protection System Description 8 20 10 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1118: ...737 MAX Flight Crew Operations Manual Flight Controls System Description 9 20 28 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1714: ...737 MAX Flight Crew Operations Manual Fuel Table of Contents 12 TOC 2 MN FLT OH 201 March 1 2021 Intentionally Blank...
Страница 1726: ...737 MAX Flight Crew Operations Manual Fuel Controls and Indicators 12 10 12 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1732: ...737 MAX Flight Crew Operations Manual Fuel System Description 12 20 6 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1734: ...737 MAX Flight Crew Operations Manual Hydraulics Table of Contents 13 TOC 2 MN FLT OH 201 October 26 2021 Intentionally Blank...
Страница 1740: ...737 MAX Flight Crew Operations Manual Hydraulics Controls and Indicators 13 10 6 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1750: ...737 MAX Flight Crew Operations Manual Landing Gear Table of Contents 14 TOC 2 MN FLT OH 201 March 1 2021 Intentionally Blank...
Страница 1770: ...737 MAX Flight Crew Operations Manual Landing Gear System Description 14 20 10 MN FLT OH 201 Intentionally Blank March 1 2021...
Страница 1826: ...737 MAX Flight Crew Operations Manual Warning Systems System Description 15 20 38 MN FLT OH 201 Intentionally Blank March 1 2021...