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FLYAWAY CONDITIONS ARE MET (AIRSPEED, ALTITUDE AND ATTITUDE).
ADDITIONAL CONSIDERATIONS EXIST FOR NIGHT/IFR CATAPULT
LAUNCHES. AIRCRAFT ACCELERATION AND THE LACK OF EXTERNAL VISUAL
CUES WILL CAUSE THE AIRCREW TO SENSE THAT THE NOSE IS HIGHER THAN
ACTUAL AND CAN RESULT IN SPATIAL DISORIENTATION. UNDER THESE
CONDITIONS, A VIGILANT INSTRUMENT SCAN IS REQUIRED TO ENSURE THAT
THE PROPER ATTITUDE IS MAINTAINED THROUGHOUT THE LAUNCH AND
SUBSEQUENT CLIMBOUT. //
BT
________________________________________________________________________
CNO 181806Z NOV98 Page 1 of 1 NA 01-F14AAD-1 IC 20
PTAUZYUW RUENAAA7311 3221825-UUUU--RULSTGP.
ZNR UUUUU
P R 181806Z NOV 98 ZYB PSN 667712M29
FM CNO WASHINGTON DC//N889//
TO ALL TOMCAT AIRCRAFT ACTIVITIES//
INFO RUCTPOH/NAVOPMEDINST PENSACOLA FL//06//
RULSTGP/COMNAVWARDEVCOM DIV WASHINGTON DC//NATOPS//
BT
UNCLAS //N03711//
MSGID/GENADMIN/N889//
SUBJ/INTERIM CHANGE TO F-14D AIRCRAFT NATOPS FLIGHT MANUAL//
REF/A/DOC/NAVAIR/01FEB97//
REF/B/MSG/CNO WASH DC/231304ZOCT98//
NARR/REF A IS NAVAIR 01-F14AAD-1 (F-14D NATOPS FLIGHT MANUAL (NFM)),
AND REF B IS INTERIM CHANGE NUMBER 19 (EJECTION SEAT AIRCREW WEIGHTS)
TO REF A.//
RMKS/1. THIS IS INTERIM CHANGE NUMBER 20 TO REF C (F-14D NFM).
2. SUMMARY. CORRECTS ERROR IN IC 19 (REF B) TO F-14D NFM (REF A).
REF B INCORRECTLY REPLACED THE FIRST THREE SENTENCES OF FIRST
PARAGRAPH OF PARA 2.38.1. THIS MESSAGE RESTORES ORIGINAL WORDING OF
THE FIRST PARAGRAPH AND CHANGES THE SECOND PARAGRAPH.
3. CHANGE REF A (F-14D NFM), CHAPTER 2, PAGE 2-243, PARAGRAPH 2.38.1
EJECTION SEAT, AS FOLLOWS:
A. FIRST PARAGRAPH OF PARAGRAPH 2.38.1. IF IC 19 NOT YET
INCORPORATED INTO FIRST PARAGRAPH, PROCEED TO PARAGRAPH 3.B BELOW.
IF IC 19 ALREADY INCORPORATED INTO FIRST PARAGRAPH, PROCEED AS
FOLLOWS:
(1) DELETE FIRST THREE SENTENCES, AS FOLLOWS:
AFTER EJECTION HAS BEEN INITIATED, TWO PITOT HEADS MOUNTED
NEXT TO THE PARACHUTE CONTAINER ARE DEPLOYED. AIRSPEED AND
ALTITUDE ARE PROVIDED TO THE BATTERY-OPERATED ELECTRONIC
SEQUENCER MOUNTED UNDER THE PARACHUTE CONTAINER. THE
SEQUENCER USES THE INFORMATION TO DETERMINE THE RELEASE TIME
FOR THE DROGUE BRIDLES, THE DEPLOYMENT TIME FOR THE
PARACHUTE, AND RELEASE TIME FOR THE HARNESS LOCKS.
(2) ADD (INSERT):
THE NACES SEAT (FIGURE 2-126) IS PROVIDED WITH A ROCKETDEPLOYED
6.5 METER (20-FOOT), AEROCONICAL, STEERABLE
PARACHUTE THAT IS PACKED WITH A RIBBON EXTRACTION DROGUE IN A
CONTAINER BEHIND THE SEAT OCCUPANT'S HEAD. THE SEAT BUCKET
HOLDS THE SURVIVAL KIT AND ALSO HAS THE SEAT FIRING HANDLE
AND OTHER OPERATING CONTROLS. THE PARACHUTE RISERS ATTACH TO
THE CREWMWMBER'S TORSO HARNESS BY MEANS OF SEAWATER-ACTIVATED
RELEASE SWITCHES.
B. SECOND PARAGRAPH:
(1) DELETE THIRD SENTENCE:
THE SEQUENCER, WHICH ALSO RECEIVES STATIC PRESSURE, USES THE
INFORMATION TO DETERMINE THE PROPER SEQUENCING OF DEPLOYMENT
OF THE SEAT DROGUE AND PARACHUTE AND RELEASE OF THE HARNESS
LOCKS.
(2) ADD (INSERT) REPLACEMENT THIRD SENTENCE:
THE SEQUENCER USES THE INFORMATION TO DETERMINE THE RELEASE
TIME FOR THE DROGUE BRIDLES, THE DEPLOYMENT TIME FOR THE
PARACHUTE, AND RELEASE TIME FOR THE HARNESS LOCKS.//
BT

_______________________________________________________________________
CNO 231304Z OCT98 Page 1 of 5 NA 01-F14AAA-1 IC 142
NA 01-F14AAP-1 IC 40
NA 01-F14AAD-1 IC 19
PTAUZYUW RUENAAA6845 2961414-UUUU--RULSTGP.
ZNR UUUUU
P R 231304Z OCT 98 ZYB PSN 532084M22
FM CNO WASHINGTON DC//N889//
TO ALL TOMCAT AIRCRAFT ACTIVITIES
INFO RUCTPOH/NAVOPMEDINST PENSACOLA FL//06//
RULSTGP/COMNAVWARDEVCOM DIV WASHINGTON DC//NATOPS//
BT
UNCLAS //N03711//
MSGID/GENADMIN/N889//
SUBJ/INTERIM CHANGES TO F-14 AIRCRAFT NATOPS FLIGHT MANUALS//
REF/A/DOC/NAVAIR/01FEB97//
REF/B/DOC/NAVAIR/01FEB97//
REF/C/DOC/NAVAIR/01FEB97//
NARR/REF A IS NAVAIR 01-F14AAA-1 (F-14A NATOPS FLIGHT MANUAL (NFM))
DTD 15MAY95 WITH CHG-1 01FEB97, REF B IS NAVAIR 01-F14AAP-1 (F-14B
NATOPS FLIGHT MANUAL (NFM)) DTD 15MAY95 WITH CHG-1 01FEB97, AND REF C
IS NAVAIR 01-F14AAD-1 (F-14D NATOPS FLIGHT MANUAL (NFM)).//
RMKS/1. THIS IS INTERIM CHANGE NUMBER 142 TO REF A (F-14A NFM),
INTERIM CHANGE NUMBER 40 TO REF B (F-14B NFM), AND INTERIM CHANGE
NUMBER 19 TO REF C (F-14D NFM).
2. SUMMARY. ADDS WARNINGS ABOUT EJECTION SEAT INJURY RISKS TO
PAGE 02 RUENAAA6845 UNCLAS
EACH NFM.
3. CHANGE REF A (F-14A NFM), AS FOLLOWS:
A. CHAPTER 2, PAGE 2-159, PARAGRAPH 2.35 EJECTION SYSTEM, WARNING
AFTER SECOND PARAGRAPH:
(1) DELETE: NA
(2) ADD (INSERT) NEW FIRST BULLET INTO WARNING:
WARNING
　
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