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CNO 091944Z JUN00 Page 1 of 2 NA 01-F14AAP-1 IC 44
NA 01-F14AAP-1F IC 10
NA 01-F14AAD-1 IC 24
NA 01-F14AAD-1F IC 3
PAAUZYUW RUENAAA4544 1612054-UUUU--RUENNSN.
ZNR UUUUU
P R 091944Z JUN 00 ZYB
FM CNO WASHINGTON DC//N889//
TO ALL TOMCAT AIRCRAFT ACTIVITIES
INFO RUDJABF/NAVWARCOL NEWPORT RI//213//
RUCTPOH/NAVOPMEDINST PENSACOLA FL//06//
BT
UNCLAS //N03711//
MSGID/GENADMIN/N889//
SUBJ/INTERIM CHANGES (IC'S) TO F-14B AND F-14D AIRCRAFT NATOPS FLIGHT
/PUBLICATIONS//
REF/A/DOC/NAVAIR/01FEB97//
REF/B/DOC/NAVAIR/01FEB97//
REF/C/DOC/NAVAIR/01FEB97//
REF/D/DOC/NAVAIR/01FEB97//
REF/E/MSG/CNO/311705ZMAY00//
NARR/REF A IS NAVAIR 01-F14AAP-1 (F-14B NATOPS FLIGHT MANUAL (NFM))
DTD 15MAY95 W/CHG-1 01FEB97. REF B IS NAVAIR 01-F14AAP-1F (F-14B
NATOPS FUNCTIONAL CHECKFLIGHT CHECKLIST (FCFCL)). REF C IS NAVAIR
01-F14AAD-1 (F-14D NATOPS FLIGHT MANUAL (NFM)). REF D IS NAVAIR
01-F14AAD-1F (F-14D NATOPS FUNCTIONAL CHECKFLIGHT CHECKLIST
(FCFCL)). REF E ISSUED DFCS IC'S AS F-14B NFM IC 42, F-14B FCFCL
IC 9, F-14D NFM IC 22, AND F-14D FCFCL IC 2.//
RMKS/1. THIS IS IC NUMBER 44 TO REF A (F-14B NFM), IC NUMBER 10 TO
REF B (F-14B FCFCL), IC NUMBER 24 TO REF C (F-14D NFM), AND IC
NUMBER 3 TO REF D (F-14D FCFCL).
2. SUMMARY. EXPANDS FUNCTIONAL CHECKFLIGHT ENGINE RUNUP CHECK
PROCEDURES IN REFS A THROUGH D (F-14B AND F-14D NFM'S AND FCFCL'S).
THESE CHANGES HAVE ALREADY BEEN INCORPORATED INTO PMCF CARDS FOR DFCS
AIRCRAFT AS PART OF REF E. THEREFORE, CHANGES CONTAINED IN THIS MSG
NEED BE MADE ONLY TO F-14B AND F-14D AIRCRAFT PUBS WITH AFCS, AND
SHALL NOT BE INCORPORATED INTO F-14B AND F-14D NATOPS PUBS WITH DFCS.
IF NATOPS PUBS HAVE REF E INCORPORATED, RETAIN THIS IC MSG, BUT HOLD
ENTRY OF IC'S IN THIS MSG IN ABEYANCE AND MAKE ENTRY ON EACH PUB
INTERIM CHANGE SUMMARY PAGE AS "ALREADY INCORPORATED BY CNO 311705Z
MAY00".
3. CHANGE REF A (F-14B NFM), CHAPTER 10, PAGES 10-11 AND 10-12,
PARAGRAPH 10.3.5 ENGINE RUNUP, STEP 48 AS FOLLOWS:
A. DELETE STEP 48.
B. ADD (INSERT) REPLACEMENT STEP:
AB 48. ENGINE RUNUP -- CHECK.
WARNING
ENGINE CHECKS SHALL NOT BE PERFORMED IN TENSION
AND SHALL BE PERFORMED WITH THE SHUTTLE FORWARD
OF THE LAUNCH BAR.
CAUTION
SHIPBOARD USE OF MRT AND MINIMUM AB IS RESTRICTED
TO A MAXIMUM OF 30 SECONDS TO PREVENT DAMAGE TO
THE JBD. JBD COOL DOWN REQUIRES BOTH THROTTLES
AT IDLE FOR 30 SECONDS, AND MAY BE NECESSARY
DURING THESE CHECKS.
CAUTION
ABOARD SHIP, EXCESSIVE ASYMMETRIC THRUST MAY
DAMAGE THE HOLDBACK BAR.
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CNO 091944Z JUN00 Page 2 of 2 NA 01-F14AAP-1 IC 44
NA 01-F14AAP-1F IC 10
NA 01-F14AAD-1 IC 24
NA 01-F14AAD-1F IC 3
A. VERIFY HOOK STOWED AND RATS LIGHT OUT.
B. BOTH ENGINE MODES -- SEC.
C. BOTH THROTTLES -- MIL.
NOTE ACCELERATION TIME (LESS THAN 10 SECONDS).
NOTE
ASHORE, CHECKS MUST BE PERFORMED WITH THE
OPPOSING ENGINE AT IDLE FOR THE BRAKES TO HOLD.
D. BOTH ENGINE MODES -- PRIMARY.
RECORD ENGINE PARAMETERS (READ IN FOUR COLUMNS).
ENGINE LEFT RIGHT
PARAMETER ENGINE ENGINE LIMITS
--------------- ------ ------ -----------------
NOZ POSITION . . . . . . 3 TO 10 - NOMINAL
(PERCENT) (CLOSED)
(AT MIL)
OIL (PSI) . . . . . . 25 TO 65
RPM (PERCENT) . . . . . . 95 TO 104 NOMINAL
(107.7 MAXIMUM)
EGT (DEGREES C) . . . . . . 935
FF (PPH) . . . . . . 9,000 TO 12,000
E. HOOK -- DOWN.
VERIFY RATS LIGHT AND 3 TO 6 PERCENT RPM DECAY.
F. RIGHT THROTTLE -- MIN AB.
VERIFY RPM INCREASES 3 TO 6 PERCENT.
G. RIGHT THROTTLE -- MIL.
H. LEFT THROTTLE -- MIN AB.
VERIFY RPM INCREASES 3 TO 6 PERCENT.
I. LEFT THROTTLE -- MIL.
J. THROTTLE MODE SWITCH -- MAN.
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