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WITHIN THESE PARAMETERS SUBJECTS THE OCCUPANT TO
INCREASED RISK OF INJURY.
1. GENERAL INJURY RISKS:
A. EJECTION SEAT STABILITY IS DIRECTLY RELATED TO OCCUPANT
RESTRAINT. ALL OCCUPANTS SHOULD BE PROPERLY RESTRAINED
IN THE SEAT BY THEIR TORSO HARNESS FOR OPTIMUM
PERFORMANCE AND MINIMUM INJURY RISK.
B. INERTIA REEL PERFORMANCE MAY BE DEGRADED FOR OCCUPANTS
OUTSIDE OF THE QUALIFIED WEIGHT RANGE. LIGHTER
OCCUPANTS MAY BE INJURED DURING THE HAULBACK, AND BOTH
LIGHT AND HEAVY OCCUPANTS MAY EXPERIENCE POOR EJECTION
POSITIONS, RESULTING IN AN INCREASED RISK OF INJURY
DURING EJECTION.
2. INJURY RISKS FOR AVIATORS WITH NUDE WEIGHTS LESS THAN 136
POUNDS:
_______________________________________________________________________
CNO 231304Z OCT98 Page 5 of 5 NA 01-F14AAA-1 IC 142
NA 01-F14AAP-1 IC 40
NA 01-F14AAD-1 IC 19
A. THE CATAPULT WAS DESIGNED FOR THE EJECTION SEAT
QUALIFIED WEIGHT RANGE. LIGHTER WEIGHT OCCUPANTS ARE
SUBJECT TO A HIGHER RISK OF INJURY FROM THE CATAPULT
DUE TO GREATER ACCELERATION.
B. LIGHTER WEIGHT OCCUPANTS ARE AT A GREATER RISK OF
INJURY DURING EJECTIONS ABOVE 300 KIAS DUE TO
INSTABILITY DURING DROGUE DEPLOYMENT.
C. LIGHTER WEIGHT OCCUPANTS ARE AT A GREATER RISK OF
INJURY DURING EJECTIONS NEAR THE UPPER END OF MODE 1
(APPROACHING 300 KIAS) DUE TO HIGH PARACHUTE OPENING
SHOCK.
3. INJURY RISKS FOR AVIATORS WITH NUDE WEIGHTS GREATER THAN
213 POUNDS:
A. LARGER OCCUPANTS MAY NOT ATTAIN SUFFICIENT ALTITUDE FOR
PARACHUTE FULL INFLATION IN ZERO-ZERO CASES OR AT
EXTREMELY LOW ALTITUDES AND VELOCITIES.
B. LARGER OCCUPANTS MAY NOT ATTAIN SUFFICIENT ALTITUDE TO
CLEAR THE AIRCRAFT TAIL STRUCTURE.
THE ESCAPE SYSTEM WILL FUNCTION UP TO 0.9 IMN OR 600 KIAS,
WHICHEVER IS GREATER. HOWEVER, HUMAN LIMITATIONS ARE MORE
RESTRICTIVE AS INDICATED BELOW:
1. ZERO TO 250 KIAS -- SAFE EJECTION (INJURY IMPROBABLE)
2. 250 TO 600 KIAS -- HAZARDOUS EJECTION (APPRECIABLE FORCES
ARE EXERTED UPON THE BODY, MAKING INJURY PROBABLE)
3. ABOVE 600 KIAS -- EXTREMELY HAZARDOUS EJECTION (EXCESSIVE
FORCES ARE EXERTED UPON THE BODY, MAKING SERIOUS INJURY OR
DEATH HIGHLY PROBABLE).
(3) RETAIN OLD LAST PARAGRAPH. //
BT

DEPARTMENT OF THE NAVY
NAVAL AIR SYSTEMS COMMAND
47123 8”SE ROAD. “Nrr “IPT
PATUXENT RIVER. MD 20670-I 547 IN “CCL. IIPEm IO
3711
Ser AIR-t.3P/7.0098
17 Jul98
From: Commander, Naval Air Systems Command
To: Distribution
Subj: INTERIM CHANGE TO F-14A/B/D NATOPS PUBLICATIONS
P.& (a) 01-F-14AAA-I. F-14A NATOPS Flight Manual dtd 15 May 95 with Change 1.01 Feb 97.
(b) 01-F-14AAP-1. F-14B NATOPS Flight Manual dtd 15 May 95, with Change 1.01 Feb 97.
c-3 01-F-14AAD-1. F-14D NATOPS Flight Manual dtd 01 Feb 97.
Encl: (1) F-14A Interim NATOPS Change Number 141
(2) F-14B Interim NATOPS Change Number 39.
(3) F-14D Interim NATOPS Change Number 18.
1. The following F-14 Aircrall Interim NATOPS Changes are hereby issued:
a. F-14A Interim NATOPS Change Number 141 to reference (a).
b. F-14B Interim NATOPS Change Number 39 IO reference (b).
c. F-14D Interim NATOPS Change Number 18 to reference (c).
2. Make the following moditications to the F-14A, F-14B. and F-14D NATOPS Manuals:
a. Cross through NATOPS Manual page 4-14 with a pen and write “superseded”
b. Insert change pages 4-14a and 4-14b into the NATOPS Manual from the following enclosures:
(1) F-14A: enclosure (1)
(2) F-14B: enclosure (2)
(3) F-14D: enclosure (3)
c. At the bottom of page J-15, cross through “figure 2 of 2” with a pen, and write “figure 3 of 3” in its
place.
d. Enter the following on page 5, in the front of the appropriate NATOPS Manual,:
Interim Chance Oricinator/Date Pages Affected Remar!&Pwwse
@gn&
F-14A 141 CNASUl7 Jol98 4-14akl Rolling Maneuvering Limits
F-14B 39 CNASCIl7 Jul98 4-14a/b Rolling Maneuvering Limits
F-14D 18 CNASCI17 Jul98 4-14&l Rolling Maneuvering Limits
w
HARRY LEHMAN
By direction
Subj: DFFER~M CHANGE TO F-14tVB/D NATOPS PUBLICATIONS
Distribution:
AIR-4.1.1
AIR-I.4.1
COMNAVAIRLANT, NORFOLK VA (N422C24)
COMNAVAJBJ’AC. SAN DIEGO. CA (N422CTPL)
NAVAIRPRA, ATSUGI, JA
VF-2 (QAXTPL)
VP-I 1 (CTPL UNIT 25504. QATPL)
VF-14 (QAXTPL)
VF-3 I (QA/CTPL)
VF-32 (QAAXF’L)
V-F-41 (QA/CTPL)
VP-IO1 DET KEY WEST (QiXTPL)
VF-10 1 (QA/CTPL)
VF-102 (QA/CTPL)
VF-103 (QAAX-PL)
V-F-143 (QAAX-PL)
VF-154 (QA/CTPL)
VF-201 (QAXTPL)
VF-211 (QA/CTPL)
W-2 13 (QA/CTF’L)
VK-9 DET PT MUGU. CA
　
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