4. Reverse thrust: Inflight use of reverse thrust is prohibited. Reverse thrust is limited to max continuous thrust except in an emergency situation (when up to takeoff EPR is authorized).
(Continued)
5. The following limitations are applicable when the airplane is using
reverse thrust for powerback: Do not apply more than 1.3 EPR during powerback. (Thrust values in excess of 1.2 EPR should be limited to a momentary power application to initiate powerback.)
Ramp slope limit range is +1% to -2%.
Thrust reversers on both engines must be operating.
Application of brakes while backing is prohibited.
Powerback is not authorized when ice, snow, or slush is on the
ramp, or during periods of heavy rain.
6.
Engine synchronization must be off below..................1500 feet AGL (Operate in cruise flight only.)
7.
The automatic reserve thrust (ART) system must be off when using the Takeoff Flex mode of the thrust rating indicator.
8.
Autothrottles must be disconnected if engine surge (stall) is detected during takeoff.
9.
The minimum altitude for thrust cutback during takeoff is 500 feet AGL.
10.
The engine ignition must be turned to OVRD, SYS A or SYS B, or GRD START & CONTIN for takeoff or landing in standing water or slush.
Operating Parameters
1. Ignition duty:
4 position switch (SYS A, SYS B, BOTH, OVRD)
Normally, 10 minutes on, 10 minutes off. May be used in 10 minute alternating cycles.
2 position switch (OVRD, GND START & CONT)
Override - 2 min on, 3 min off, 2 min on, 23 min off. Ground start and continuous - no duty cycle.
(Continued)
2. Engine starter duty cycle:
Standard 90 seconds on* 5 minutes off 30 seconds on 5 minutes off 30 seconds on Alternate 90 seconds on* 10 minutes off 60 seconds on 10 minutes off 60 seconds on
Sequence may continue Sequence may continue
* May consist of 3 normal start cycles of 30 seconds
each with engine allowed to stop turning between
starts.
3.
Reduced EPR takeoff is not authorized under the following conditions:
Auto ground spoilers inoperative (landing mode)
Inboard ground spoilers system inoperative
Right engine hydraulic pump inoperative
Approach idle control system fails to high idle
The ART switch in AUTO
219 + 217 Engine intermix
Low altimeter setting (less than 29.72)
After application of de-ice / anti-ice fluid
Reported or suspected windshear
Standing water, slush, snow, or ice on runway
Combination of wet runway and tailwind.
4.
An entry should be made in the maintenance log if oil consumption reaches 1 quart or more per hour.
LIST OF EFFECTIVE PAGES
PAGE DATE
TOC-1 01/01/00
TOC-2 01/01/00
* 1 12/01/00
2 01/01/00
* 3 12/01/00
4 01/01/00
5 05/15/95
6 05/15/95
7 05/15/95
8 12/01/97
* 9 12/01/00
* 10 12/01/00
* 11 12/01/00
12 05/15/95
13 05/15/95
14 05/15/95
15 05/15/95
16 01/01/97
17 01/01/97
18 08/01/98
19 08/01/98
20 08/01/98
21 01/01/00
22 01/01/00
* 23 12/01/00
24 08/01/98
25 08/01/98
* 26 12/01/00
* LEP-1 12/01/00
* LEP-2 12/01/00
PAGE DATE PAGE DATE
FAA APPROVED
DON KLOS Principal Operations Inspector
* Asterisk indicates page(s) revised or added by the current revision.
INTENTIONALLY LEFT BLANK
EMERGENCY PROCEDURES
TABLE OF CONTENTS
AIR CONDITIONING/PRESSURIZATION
Air Conditioning Smoke Checklist .....................................................63
Air Conditioning Smoke Expanded Checklist.....................................65
Cockpit Smoke Removal (Unpressurized Flight) Checklist ................67
Cabin Smoke/Fume Removal Checklist............................................69
Cabin Smoke/Fume Removal Expanded Checklist ...........................71
Emergency Descent Procedure........................................................85
Emergency Descent Profile...............................................................87
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 1(18)
