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PAGES ARE REQUIRED. NAVAIR 4.1.1.1 POC IS LCDR SCOTT PORTER, AT DSN
757-7017 OR COMM (301)757-7017, OR EMAIL PORTERSD@NAVAIR.NAVY.MIL.
6. THIS MESSAGE AND ALL OTHER NATOPS INTERIM CHANGES WILL BE POSTED
ON THE NATEC WEBSITE, WWW.NATEC.NAVY.MIL, WITHIN 15 DAYS OF THE
RELEASE OF THIS MESSAGE. IF UNABLE TO VIEW THIS MESSAGE AT THE
NATEC WEBSITE, PLEASE INFORM THE CNO NATOPS OFFICE AT DSN 288-5797
OR COMM (202)433-5797.//
BT
_______________________________________________________________________
CNO 051758Z APR01 Page 1 of 9 NA 01-F14AAA-1 IC 147
NA 01-F14AAA-1B IC 103
NA 01-F14AAP-1 IC 45
NA 01-F14AAP-1B IC 29
NA 01-F14AAD-1 IC 25
NA 01-F14AAD-1B IC 14
RAAUZYUW RUENAAA0915 0951755-UUUU--RUEASUU.
ZNR UUUUU
R 051758Z APR 01 ZYB ZYW
FM CNO WASHINGTON DC//N789J//
TO ALL TOMCAT AIRCRAFT ACTIVITIES
INFO NAVOPMEDINST PENSACOLA FL
BT
UNCLAS //N04790//
MSGID/GENADMIN/N789//
SUBJ/INTERIM CHANGES TO F-14 AIRCRAFT NATOPS FLIGHT PUBLICATIONS
/SAFETY OF FLIGHT//
REF/A/DOC/NAVAIR/YMD:19970201//
REF/B/DOC/NAVAIR/YMD:19970201//
REF/C/DOC/NAVAIR/YMD:19970201//
REF/D/DOC/NAVAIR/YMD:19970201//
REF/E/DOC/NAVAIR/YMD:19970201//
REF/F/DOC/NAVAIR/YMD:19970201//
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-F14AAA-1B (F-14A
NATOPS POCKET CHECKLIST (PCL)) DTD 15MAY95 W/CHG-1 01FEB97. REF C IS
NAVAIR 01-F14AAP-1 ((F-14B NATOPS FLIGHT MANUAL (NFM)) DTD 15MAY95
W/CHG-1 01FEB97. REF D IS NAVAIR 01-F14AAP-1B ((F-14B NATOPS POCKET
CHECKLIST (PCL)) DTD 15MAY95 W/CHG-1 01FEB97. REF E IS NAVAIR 01-
F14AAD-1 ((F-14D NATOPS FLIGHT MANUAL (NFM)). REF F IS NAVAIR 01-
F14AAD-1B ((F-14D NATOPS POCKET CHECKLIST (PCL)).//
RMKS/RMKS/1. THIS IS INTERIM CHANGE (IC) NUMBER 147 TO REF A (F-14A
NFM),
IC NUMBER 103 TO REF B (F-14A PCL), IC NUMBER 45 TO REF C (F-14B
NFM), IC NUMBER 29 TO REF D (F-14B PCL), IC NUMBER 25 TO REF E
(F-14D NFM), AND IC NUMBER 14 TO REF F (F-14D PCL).
2. SUMMARY. ADDS RUDDER HARDOVER PROCEDURE, REVISES CONTROLLABILITY
CHECK PROCEDURE, AND MODIFIES UNCOMMANDED ROLL AND/OR YAW PROCEDURE
IN REFS A THROUGH F.
3. CHANGE REF A (F-14A NFM), REF B (F-14B NFM), AND REF C (F-14D
NFM) AS FOLLOWS:
A. CHAPTER 14, F-14A PAGES 14-29 AND 14-30/F-14B PAGES 14-32 AND
14-33/F-14D PAGES 14-35 AND 14-36, PARAGRAPH 14.11.7
CONTROLLABILITY CHECK:
(1) DELETE EXISTING PARAGRAPH.
(2) ADD (INSERT) REPLACEMENT PARAGRAPH:
14.11.7 CONTROLLABILITY CHECK. THERE ARE SEVERAL MALFUNCTIONS THAT
MAY SIGNIFICANTLY AFFECT THE HANDLING CHARACTERISTICS IN THE CRUISE
AND LANDING CONFIGURATIONS. THESE MALFUNCTIONS INCLUDE, BUT ARE NOT
LIMITED TO:
A. SPOILER MALFUNCTION*
B. FLAP/SLAT ASYMMETRY*
C. STRUCTURAL DAMAGE
D. UNCOMMANDED SAS INPUTS*
E. RUDDER MALFUNCTION (HARDOVER)*
F. WING SWEEP ASYMMETRY*
G. JAMMED FLIGHT CONTROLS
H. (DFCS ONLY) ARI FAILURE*
* THESE MALFUNCTIONS, WHICH HAVE UNIQUE NATOPS PROCEDURES SPECIFIC
_______________________________________________________________________
CNO 051758Z APR01 Page 2 of 9 NA 01-F14AAA-1 IC 147
NA 01-F14AAA-1B IC 103
NA 01-F14AAP-1 IC 45
NA 01-F14AAP-1B IC 29
NA 01-F14AAD-1 IC 25
NA 01-F14AAD-1B IC 14
TO A PARTICULAR FAILURE MODE, SHOULD BE PERFORMED BEFORE BEGINNING
A CONTROLLABILITY CHECK.
NATOPS PROCEDURES CANNOT ACCOUNT FOR EVERY POTENTIAL MALFUNCTION.
IT IS ABSOLUTELY IMPERATIVE THAT THE AIRCREW THOROUGHLY AND SAFELY
EVALUATE THE DEGRADED HANDLING CHARACTERISTICS OF THE DAMAGED OR
MALFUNCTIONING AIRCRAFT PRIOR TO CONTINUED FLIGHT AND LANDING.
THIS CHECK DOES NOT TAKE PRIORITY OVER EXISTING EMERGENCY
PROCEDURES.
UPON ENCOUNTERING A PROBLEM THAT ALTERS THE HANDLING QUALITIES OF
THE AIRCRAFT, THE AIRCREW SHOULD REALIZE THAT THE AIRCRAFT MAY NO
LONGER BE A STABLE AIRFRAME, ESPECIALLY IN THE LANDING
CONFIGURATION. IN ADDITION, THE FLIGHT CHARACTERISTICS MAY RAPIDLY
DEGRADE OR EVEN BECOME UNCONTROLLABLE WHEN NORMAL CONFIGURATION
CHANGES ARE INTRODUCED OR DURING AIRSPEED CHANGES. INCREASED
AWARENESS OF FLIGHT PARAMETERS SHOULD PREVAIL FOLLOWING A
MALFUNCTION UNTIL THE AIRCRAFT IS SAFELY ON DECK.
EVEN THOUGH THE AIRCRAFT MAY POSSESS SIGNIFICANTLY DIFFERENT OR
EVEN HAZARDOUS FLYING QUALITIES, THE PILOT AND RIO HAVE NUMEROUS
CUES AVAILABLE TO THEM TO WARN OF POTENTIAL PROBLEMS. SOME OF THESE
CUES INCLUDE:
A. TURN NEEDLE AND BALL POSITION
B. AOA
C. BUFFET
D. YAW STRING POSITION
E. FLIGHT CONTROL POSITIONS
F. TRIM SETTINGS
G. ROLL-OFF
H. RATE OF DESCENT
ALL CUES SHOULD BE VERY CLOSELY MONITORED SINCE THEY TELL THE
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F-14D 飞行手册 Flight Manual 1(5)
