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NFM'S), AND INTERIM CHANGE NUMBER 1 TO REFS G AND H (F-14D FCFCL'S).
REFS F AND H ARE CURRENTLY AT PRINTER AND, WHEN DISTRIBUTED, WILL
SUPERSEDE REFS E AND G, RESPECTIVELY.
2. SUMMARY. MODIFIES FUNCTIONAL CHECKFLIGHT PROCEDURES IN REFS A
THROUGH I. ALPHABETICAL SUFFIXES ARE USED BELOW WITH STEP NUMBERS
WHEN INSERTING ADDITIONAL STEPS TO AVOID RENUMBERING SUBSEQUENT STEPS
(E.G., STEP 11A INDICATES AN INSERTED STEP WHICH FOLLOWS CURRENT STEP
11 AND WILL BE NUMBERED AS STEP 12 IN NEXT UPDATE OF THE PUBLICATION,
WHILE STEP 11.A INDICATES SUBSTEP A OF STEP 11.)
3. CHANGE REF A (F-14A NFM), CHAPTER 10, AS FOLLOWS:
A. PAGE 10-1, PARAGRAPH 10.2:
(1) DELETE EXISTING PARAGRAPH.
(2) ADD:
10.2 CHECKFLIGHT PROCEDURES. A FLIGHT PROFILE HAS
BEEN ESTABLISHED FOR EACH CHECKFLIGHT CONDITION AND IS
IDENTIFIED BY THE LETTER CORRESPONDING TO THE PURPOSE FOR
WHICH THE CHECKFLIGHT IS BEING FLOWN (A, B, C, AS SHOWN IN
_______________________________________________________________________
CNO 191427Z MAR98 Page 2 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
FIGURE 10-1). THE APPLICABLE LETTER IDENTIFYING THE
PROFILE PRECEDES EACH ITEM IN THE FUNCTIONAL CHECKFLIGHT
CHECKLIST (NAVAIR 01-F14AAA-1F). POSTMAINTENANCE
CHECKFLIGHT PROCEDURES ARE SPECIFIC AND ARE TO BE
PERFORMED IN CONJUNCTION WITH NORMAL NATOPS OPERATING
PROCEDURES (PART III). CHECKFLIGHT PERSONNEL SHALL
FAMILIARIZE THEMSELVES WITH THE PROFILE REQUIREMENTS
BEFORE EACH FLIGHT. A DAILY INSPECTION IS REQUIRED BEFORE
EACH CHECKFLIGHT. AN AIRCRAFT IS CONSIDERED HIGH GROSS
WEIGHT FOR PROFILE PURPOSES IF OVER 56,000 POUNDS TOTAL
WEIGHT. AIRCREW SHALL BE COGNIZANT OF THE AIRCRAFT'S
CONFIGURATION AND THE CUMULATIVE NEGATIVE EFFECTS OF
WEAPONS RAILS AND EXTERNAL STORES ON AIRCRAFT STABILITY.
NOTE
SHIPBOARD CONSTRAINTS CAN PRECLUDE COMPLETION OF SOME
ITEMS ON THE APPLICABLE FLIGHT PROFILE CHECKLIST.
10.2.1 GENERAL CONDUCT. THOROUGH, PROFESSIONAL
CHECKFLIGHTS ARE A VITAL PART OF THE SQUADRON MAINTENANCE
EFFORT. CHECK CREWS PERFORM A VALUABLE SERVICE TO THE
MAINTENANCE DEPARTMENT BY CARRYING OUT THIS FUNCTION. THE
QUALITY OF SERVICE PROVIDED BY CHECK CREWS REFLECTS
DIRECTLY IN THE QUALITY OF MAINTENANCE AND SUBSEQUENTLY
ENHANCES FLIGHT OPERATIONS. THE COMMANDING OFFICER SHALL
ENSURE THAT THOROUGHNESS, PROFESSIONALISM, AND SAFETY ARE
OBSERVED THROUGHOUT THE CHECKFLIGHT EVOLUTION AND THAT
CHECK CREWS STRICTLY ADHERE TO THE PROFILE CHECKLIST.
SAFETY IS A PRIMARY CONSIDERATION DURING ALL CHECKFLIGHTS.
B. PAGE 10-19, PARA 10.3.12, STEP 70 (NEGATIVE ALPHA MCB/FOD
CHECK):
(1) DELETE STEP 70.
(2) ADD:
70. DELETED
C. PAGE 10-21, PARA 10.3.12, AFTER STEP 72.M:
(1) DELETE: NA
(2) ADD:
ABC 72A. NEGATIVE ALPHA/MCB/FOD CHECK (20,000 FEET, 300
KIAS).
WARNING
IT IS IMPERATIVE THAT THE PROCEDURES IN
THIS CHECK BE FOLLOWED EXACTLY AND
NEGATIVE-G MANEUVERING AT HIGH GROSS
WEIGHT (OVER 56,000 POUNDS) SHOULD BE
AVOIDED BECAUSE OF THE HIGH PROBABILITY
OF ENGINE STALLS AND/OR AIRCRAFT
DEPARTURES.
NOTE
THIS CHECK VERIFIES THE PROPER OPERATION
OF EACH MCB WITH APPROXIMATELY 4 DEGREES
NEGATIVE ALPHA AS SENSED BY THE AICS
SENSOR PROBES, AND IS RELATIVELY
INDEPENDENT ON THE AMOUNT OF NEGATIVE G
APPLIED.
A. THROTTLES -- MIL
B. RAISE NOSE TO 10 DEGREES ABOVE HORIZON,
ROLL INVERTED (ENSURE WINGS LEVEL).
_______________________________________________________________________
CNO 191427Z MAR98 Page 3 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
C. SMOOTHLY APPLY FORWARD STICK PRESSURE (NOT
TO EXCEED -1.0 G). MCB TEST LIGHTS SHOULD
ILLUMINATE (COORDINATE WITH RIO).
D. CHECK FOR NORMAL ENGINE OPERATION AND FOD OR
LOOSE GEAR.
E. RELEASE FORWARD STICK AND PERFORM
COORDINATED ROLL TO UPRIGHT WINGS LEVEL
ATTITUDE. CHECK MCB TEST LIGHTS OUT AT
+1.0 G.
D. PAGE 10-24, PARA 10.4.4, STEP 19 (MCB TEST LIGHTS):
(1) DELETE STEP 19.
(2) ADD:
AB 19. REFUEL PROBE CHECK:
A. MCB TEST LIGHTS -- ILLUMINATED WITH PROBE
EXTENDED/OFF WHEN RETRACTED (COORDINATE
WITH PILOT).
E. PAGE 10-24, PARA 10.4.5 FIFTEEN THOUSAND-FOOT CHECKS:
(1) DELETE STEPS 23 THROUGH 25.
(2) ADD:
AB 23. ECS CHECK
A. SET WCS SWITCH TO STBY BEFORE PILOT ECS
CHECK.
ABC 24. HIGH AOA MACH LEVER/AUTO MAN DEVICES/MCB CHECKS
A. ALPHA COMP CB (7C8) -- IN.
B. CONFIRM ROLL SAS OFF AND THROTTLES IDLE.
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F-14D 飞行手册 Flight Manual 1(22)
