曝光台 注意防骗
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ABOVE.
D. RENAME PAGE III-10-25, PARA 10.4.9 DESCENT AS:
10.4.9 DESCENT/20,000-FOOT CHECKS
E. PAGE III-10-26, AFTER SUBSTEP 23.E:
(1) DELETE: NA
(2) ADD STEP 23A (NEGATIVE ALPHA/FOD CHECK) AS IN PARA 7.E(2)
ABOVE.
9. CHANGE REF G (F-14D FCFCL DTD 15MAY95) AS FOLLOWS:
A. PART 1, PILOT CHECKLIST:
(1) PAGE 1-19, STEP 68 (NEGATIVE ALPHA/FOD CHECK):
(A) DELETE STEP 68.
(B) ADD:
_______________________________________________________________________
CNO 191427Z MAR98 Page 8 of 8 NA 01-F14AAA-1 IC 139
NA 01-F14AAA-1F IC 7
NA 01-F14AAP-1 IC 37
NA 01-F14AAP-1F IC 8
NA 01-F14AAD-1 IC 17
NA 01-F14AAD-1F IC 1
68. DELETED
(2) PAGE 1-24, AFTER SUBSTEP 77.G(2):
(A) DELETE: NA
(B) ADD STEP 77A (NEGATIVE ALPHA/FOD CHECK) AS IN PARA
7.C(2) ABOVE.
B. PART 2, RIO CHECKLIST:
(1) PAGE 2-5, AFTER STEP 22 (ENGINE INSTRUMENTS) TABLE:
(A) DELETE: DESCENT
(B) ADD: DESCENT/20,000-FOOT CHECKS
(2) PAGE 2-6, AFTER SUBSTEP 23.E:
(A) DELETE: NA
(B) ADD STEP 23A (NEGATIVE ALPHA/FOD CHECK) AS IN
PARAGRAPH 7.E(2) ABOVE.
10. WHEN RECEIVED, CHANGE REF H (F-14D FCFCL DTD 01FEB97) AS FOLLOWS:
A. PART 1, PILOT CHECKLIST:
(1) PAGES 1-22 AND 1-23, STEP 76 (NEGATIVE ALPHA/FOD CHECK):
(A) DELETE STEP 76.
(B) ADD:
76. DELETED
(2) PAGE 1-23, AFTER SUBSTEP 77.G(2):
(A) DELETE: NA
(B) ADD STEP 77A (NEGATIVE ALPHA/FOD CHECK) AS IN PARA
7.C(2) ABOVE.
B. PART 2, RIO CHECKLIST:
(1) PAGE 2-5, AFTER STEP 22 (ENGINE INSTRUMENTS) TABLE:
(A) DELETE: DESCENT
(B) ADD: DESCENT/20,000-FOOT CHECKS
(2) PAGE 2-6, AFTER SUBSTEP 23.E:
(A) DELETE: NA
(B) ADD STEP 23A (NEGATIVE ALPHA/FOD CHECK) AS IN
PARAGRAPH 7.E(2) ABOVE. //
BT
NAVAIR OI-Fl4AAD-I
SUMMARY OF APPLICABLE TECHNICAL DIRECTIVES
Information relating to thefollowing recent technical directives has been incorporated in this manual.
CHANGE
NUMBER
AFC 793
AFC 795
AYC 832
AFC 843
DESCRIPTION
Standard Central Air Data Computer
Radar Warning Receiver Modification
Incorporation of Unmodified OBOGS
Monitor
BOL Chaff Incorporation
DATE INC.
IN MANUAL
30 sep 94
30 sep 94
15 May95
1 Feb 97
VlSUAL
IDENTlFlCATlON
None
None
Panel size increasedo n pilot’s
right console
5A BOL PWR circuit breakers
at 219,211O
Information relating to thefollowing applicable technical directives will be incorporated in ofuhwe change.
I CHANGE
I
DESCRIPTION
NUMBER
VISUAL
IDENTIFICATION
7 (ReverseB lank) ORIGINAL
NAVAIR 01.F14AAD-1
RECORD OF CHANGES
Change No. and
Date of Change
Date of Page Count Verified by
Entry (Signature)
I
9 (ReverseB lank) ORIGINAL
NAVAIR Ol-F14AAD-1
F-14D NATOPS FliQht Manual
CONTENTS
PART I -THE AIRCRAFT
CHAPTER 1 -AIRCRAFT AND ENGINE
1.1 AIRCRAFT . . . . . . . . . .
1.1.1 Aircraft Weight. . . . . . . . .
1.1.2 Cockpit . . . . . . . . . . . .
1.1.3 ElectronicNomenclature . .
1.1.4 TecbnicalDirectivea . . . . . .
1.1.5 Block Numbers . . . . . . . .
CHAPTER 2 -SYSTEMS
.
. .
. .
. .
.
. .
. . * .
. . . .
. . .
. . . .
. . . .
. . . .
2.1
2.1.1
2.1.2
2.1.3
2.1.4
. . . .
. . . .
. . . .
. . . .
. . .
. . . . .
. . . . .
. . . . .
. . . . .
. . . .
2.2
2.2.1
2.2.2
. . . .
. . . .
. . . .
. . . .
. . . .
. . . . .
2.3
2.3.1
2.3.2
2.3.3
. . . .
. . . .
. . . .
. . . .
. . . . .
. . * . .
. . . . .
. . . . .
2.4
2.4.1
2.4.2
2.4.3
2.4.4
2.4.5
2.4.6
AIR INLET CONTROL SYSTEM ..........
Normal AICS Operations ...............
AICS Test .......................
AICS Failure Modes of Operation. ..........
AICS Anti-Ice .....................
ENGINE.. ......................
Engine Control .....................
Variable Exhaust Nozzle ...............
FATIGUE ENGINE MONITORING SYSTEM ...
FEMS Functional Description .............
FEMS Operation ....................
FEMS and OBC ....................
ENGINE FUEL SYSTEM ..............
Motive Flow Fuel Pump ................
Engine Fuel Boost Pump. ...............
Main Fuel Pump ....................
Main Engine Control .................
Afterburner Fuel Pump ................
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