曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

RHMFIUU/NAVOPMEDINST PENSACOLA FL//06//
BT
UNCLAS SECTION 01 OF 03
MSGID/GENADMIN/N789J//
SUBJ/INTERIM CHANGES TO F-14ABD AIRCRAFT NATOPS FLIGHT PUBLICATIONS/
SAFETY OF FLIGHT//
REF/A/DOC/NAVAIR 01-F14AAA-1/YMD:19970201//
REF/B/DOC/NAVAIR 01-F14AAP-1/YMD:19970201//
REF/C/DOC/NAVAIR 01-F14AAD-1/YMD:19970201//
REF/D/DOC/NAVAIR 01-F14AAA-1B/YMD:19970201//
REF/E/DOC/NAVAIR 01-F14AAP-1B/YMD:19970201//
REF/F/DOC/NAVAIR 01-F14AAD-1B/YMD:19970201//
REF/G/LTR/VF-101/YMD:20010719//
NARR/REF A IS NAVAIR 01-F14AAA-1 (F-14A NATOPS FLIGHT MANUAL (NFM))
DTD 15MAY95 W/CHG-1 01FEB97. REF B IS NAVAIR 01-F14AAP-1 (F-14B
NATOPS FLIGHT MANUAL (NFM)) DTD 15MAY95 W/CHG-1 01FEB97. REF C IS
NAVAIR 01-F14AAD-1 ((F-14D NATOPS FLIGHT MANUAL (NFM)). REF D IS
NAVAIR 01-F14AAA-1B (F-14A NATOPS POCKET CHECKLIST (PCL)) DTD
15MAY95 W/CHG-1 01FEB97. REF E IS NAVAIR 01-F14AAP-1B ((F-14B
NATOPS POCKET CHECKLIST (PCL)) DTD 15MAY95 W/CHG-1 01FEB97. REF F
IS NAVAIR 01-F14AAD-1B ((F-14D NATOPS POCKET CHECKLIST (PCL)).
REF G IS VF-101 LTR 3711 SER 20/1479; SUBJ: F-14 NATOPS REVIEW
CONFERENCE REPORT.//
RMKS/1. THIS IS INTERIM CHANGE (IC) NUMBER 148 TO REF A (F-14A NFM),
IC NUMBER 46 TO REF B (F-14B NFM), IC NUMBER 26 TO REF C (F-14D
NFM), IC NUMBER 104 TO REF D (F-14A PCL), IC NUMBER 30 TO REF E
(F-14B PCL), AND IC NUMBER 15 TO REF F (F-14D PCL).
2. SUMMARY. THIS IC MSG DIRECTS ENTRY OF THE ADVANCE CHANGE ITEMS
FROM THE 19-22JUN01 F-14A/B/D NATOPS REVIEW CONFERENCE WHICH MODIFY
EMERGENCY PROCEDURES FOR DOUBLE GENERATOR FAILURE, UNCOMMANDED ROLL
AND/OR YAW, AND SPOILER MALFUNCTION/SPOILER STUCK UP IN REFS A
THROUGH F.
3. CHANGE REFS A, B, AND C, WITH ALL PREVIOUS IC'S INCORPORATED, AS
FOLLOWS:
A. LIST OF ACRONYMS AND ABBREVIATIONS.
(1) DELETE: NA
(2) ADD (INSERT) ABBREVIATION FOR INBOARD ON PAGE 46 OF REF A,
AND ON PAGE 44 OF REFS B AND C, RESPECTIVELY, AS FOLLOWS:
INBD. INBOARD.
(3) ADD (INSERT) ABBREVIATION FOR OUTBOARD ON PAGE 47 OF REF A,
AND ON PAGE 46 OF REFS B AND C, RESPECTIVELY, AS FOLLOWS:
OUTBD. OUTBOARD.
B. DOUBLE GENERATOR FAILURE:
(1) DELETE:
REF A (F-14A NFM), DFCS SUPPLEMENT, PAGE 14-4X,
PARAGRAPH 14.7.2 (DOUBLE GENERATOR FAILURE),
REF B (F-14B NFM), DFCS SUPPLEMENT, PAGE 14-4X,
_______________________________________________________________________
CNO 041749Z SEP01 Page 2 of 6 NA 01-F14AAA-1 IC 148
NA 01-F14AAP-1 IC 46
NA 01-F14AAD-1 IC 26
NA 01-F14AAA-1B IC 104
NA 01-F14AAP-1B IC 30
NA 01-F14AAD-1B IC 15
PARAGRAPH 14.7.2 /(DOUBLE GENERATOR FAILURE), AND/OR
REF C (F-14D NFM), DFCS SUPPLEMENT, PAGE 14-4X,
PARAGRAPH 14.7.2 (DOUBLE GENERATOR FAILURE):
(2) ADD (REPLACE WITH) IN EACH NFM:
14.7.2 DOUBLE GENERATOR FAILURE.
1. BOTH GENERATOR SWITCHES -- CYCLE.
WHEN OPERATING ON EMERGENCY GENERATOR, THE FOLLOWING
IMPORTANT SYSTEMS ARE INOPERATIVE:
A. EMERGENCY FLIGHT HYDRAULICS.
B. OUTBOARD SPOILER MODULE AND
EMERGENCY FLAPS ACTIVATION.
C. OBOGS CONCENTRATOR HEATER (F-14D ONLY)
(OBOGS MAY STILL FUNCTION AT A
REDUCED, BUT ADEQUATE LEVEL).
2. IF TEMPORARY LOSS OF COMBINED SYSTEM PRESSURE CAUSES
EMERGENCY GENERATOR TO SHIFT TO 1-KVA MODE:
EMERG GENERATOR SWITCH -- CYCLE.
CAUTION
A SHIFT TO 1-KVA MODE WILL CAUSE LOSS OF ALL DFCS
FUNCTIONS AND SPOILERS WITHOUT ILLUMINATION OF
CAUTION LIGHTS. IF THE 5-KVA MODE IS REGAINED, A
MASTER RESET WILL BE REQUIRED TO REGAIN SAS,
SPOILER, AUTHORITY STOP, AND ARI FUNCTIONS.
NOTE
DFCS SYNCHRONIZATION CAN TAKE UP TO 2 SECONDS
FOLLOWING A POWER INTERRUPT. IF THE MASTER RESET
PUSHBUTTON IS DEPRESSED DURING THE SYNCHRONIZATION
TIME, AN ADDITIONAL DEPRESSION OF THE MASTER RESET
PUSHBUTTON WILL BE REQUIRED TO RESTORE SPOILER
FUNCTIONALITY.
3. LAND AS SOON AS PRACTICABLE.
C. UNCOMMANDED ROLL AND/OR YAW:
(1) DELETE:
REF A (F-14A NFM), CHAPTER 14, PAGE 14-31, PARAGRAPH 14.12.1
(UNCOMMANDED ROLL AND/OR YAW),
REF B (F-14B NFM), CHAPTER 14, PAGES 14-33 AND 14-34,
PARAGRAPH 14.12.1 (UNCOMMANDED ROLL AND/OR YAW), AND/OR
REF C (F-14D NFM), CHAPTER 14, PAGE 14-37, PARAGRAPH 14.12.1
(UNCOMMANDED ROLL AND/OR YAW):
(2) ADD (REPLACE WITH) IN EACH NFM:
14.12.1 UNCOMMANDED ROLL AND/OR YAW.
NOTE
IF UNCOMMANDED ROLL AND/OR YAW OCCURS DURING
HIGH-AOA MANEUVERING (ABOVE 15 UNITS), ASSUME
DEPARTURE FROM CONTROLLED FLIGHT AND APPLY
APPROPRIATE DEPARTURE AND/OR SPIN RECOVERY
PROCEDURES.
NOTE
FAILURES THAT MAY CAUSE UNCOMMANDED ROLL AND/OR
YAW INCLUDE, BUT ARE NOT LIMITED TO:
A. ENGINE FAILURE.
B. STUCK UP SPOILER.
C. ASYMMETRIC FLAPS AND/OR SLATS.
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 1(2)