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C. OBSERVE MANEUVER DEVICES EXTENDED AT 10.5
UNITS AOA.
D. MCB TEST LIGHTS ILLUMINATED AFTER 16 UNITS
AOA (COORDINATE WITH PILOT).
E. CONFIRM RPM INCREASE AT 18+/-1 UNITS AOA
(GREATER THAN 80 PERCENT).
F. OBSERVE MANEUVER DEVICES RETRACT AT 8 UNITS
AOA.
G. ALPHA COMP CB -- OUT.
AB 25. AICS/MCB CHECK
A. AICS CB'S (7E1 AND 7E2) -- PULL.
B. MCB TEST LIGHTS -- ILLUMINATED.
C. AICS CB'S -- RESET.
D. MCB TEST LIGHTS -- OFF.
ABC 25A. STRUCTURAL INTEGRITY CHECK
A. ANTI-G VALVE OPERATION
F. PAGE 10-24, PARA 10.4.6, AFTER STEP 27 (WCS SWITCH -- STBY):
(1) DELETE: NA
(2) ADD:
AB 27A. AT 0.85 IMN WITH THROTTLES LESS THAN MIL, MCB
TEST LIGHTS -- CHECK OFF (COORDINATE WITH
PILOT).
G. PAGE 10-25, PARA 10.4.7, AFTER STEP 28 (ENGINE INSTRUMENTS)
TABLE:
(1) DELETE: NA
(2) ADD:
AB 28A. MACH LEVER AND MCB CHECK
A. MCB TEST LIGHTS -- ILLUMINATED AT IDLE
(COORDINATE WITH PILOT).
H. PAGE 10-25, PARA 10.4.7: STEP 32 (MCB TEST LIGHTS):
_______________________________________________________________________
CNO 191427Z MAR98 Page 4 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
(1) DELETE STEP 32.
(2) ADD:
32. DELETED
I. RENAME PAGE 10-25, PARA 10.4.8 DESCENT AS:
10.4.8 DESCENT/20,000-FOOT CHECKS
J. PAGE 10-27, PARA 10.4.8, STEP 34 (MCB CHECK):
(1) DELETE ALL.
(2) ADD:
ABC 34. MCB CHECK
A. GUN ARMED POWER CB (8C3) -- PULL (RIO).
B. CONFIRM WEAPONS SELECT -- GUN.
C. CONFIRM MASTER ARM SWITCH -- ON.
D. CONFIRM THROTTLES -- STABILIZED ZONE 2
(APPROXIMATELY 2.4 NOZZLE POSITION).
E. CONFIRM TRIGGER -- SQUEEZE.
F. VERIFY NOZZLE POSITION INCREASE.
G. MCB TEST LIGHTS -- ILLUMINATED. (COORDINATE
WITH PILOT)
H. VERIFY NOZZLES RETURN TO THE ORIGINAL
POSITION.
I. CONFIRM MASTER ARM SWITCH -- OFF.
J. CONFIRM GUN -- DESELECTED
K. GUN ARMED POWER CB (8C3) -- RESET.
ABC 34A. 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. CONFIRM THROTTLES -- MIL.
B. AFTER PILOT RAISES NOSE TO 10 DEGREES ABOVE
HORIZON AND ROLLS INVERTED WINGS LEVEL (NOT
TO EXCEED -1.0 G), CONFIRM MCB TEST LIGHTS
ILLUMINATED.
C. CHECK FOR FOD OR LOOSE GEAR.
D. AS AIRCRAFT ROLLS UPRIGHT TO WINGS LEVEL
ATTITUDE, CHECK MCB TEST LIGHTS OUT AT
+1.0 G.
4. CHANGE REF B (F-14A FCFCL) AS FOLLOWS:
A. PART 1, PILOT CHECKLIST:
(1) PAGE 1-19, STEP 70 (NEGATIVE ALPHA MCB/FOD CHECK):
(A) DELETE STEP 70.
(B) ADD:
70. DELETED
_______________________________________________________________________
CNO 191427Z MAR98 Page 5 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
(2) PAGE 1-21 AFTER STEP 72.M:
(A) DELETE: NA
(B) ADD STEP 72A (NEGATIVE ALPHA/MCB/FOD CHECK) AS IN
PARAGRAPH 3.C(2) ABOVE.
B. PART 2, RIO CHECKLIST:
(1) CHANGE PAGE 2-4, STEP 19 (MCB TEST LIGHTS) AS IN PARAGRAPHS
3.D(1) AND 3.D(2) ABOVE.
(2) CHANGE PAGE 2-5, STEPS 23 THROUGH 25A, AS IN PARAGRAPHS
3.E(1) AND 3.E(2) ABOVE.
(3) PAGE 2-5, AFTER STEP 27 (WCS SWITCH -- STBY):
(A) DELETE: NA
(B) ADD STEP 27A (AT 0.85 IMN WITH THROTTLES....) AS IN
PARAGRAPH 3.F(2) ABOVE.
(4) PAGE 2-5, AFTER STEP 28 (ENGINE INSTRUMENTS) TABLE:
(A) DELETE: NA
(B) ADD STEP 28A (MACH LEVER AND MCB CHECK) AS IN
PARAGRAPH 3.G(2) ABOVE.
(5) PAGE 2-6, STEP 32 (MCB TEST LIGHTS):
(A) DELETE STEP 32.
(B) ADD:
32. DELETED
(6) PAGE 2-6, DESCENT HEADING (AFTER STEP 32):
(A) DELETE: DESCENT
(B) ADD: DESCENT/20,000-FOOT CHECKS
(7) CHANGE PAGE 2-8, STEP 34 (MCB CHECK), AS IN PARAS 3.J(1)
AND 3.J(2) ABOVE.
5. CHANGE REF C (F-14B NFM), CHAPTER 10, AS FOLLOWS:
A. CHANGE PAGE 10-1, PARA 10.2 AS IN PARAS 3.A(1) AND 3.A(2)
ABOVE, EXCEPT REPLACE REFERENCE TO 01-F14AAA-1F WITH
01-F14AAP-1F.
B. PAGE 10-20, PARA 10.3.8, STEP 73 (NEGATIVE ALPHA/FOD CHECK):
(1) DELETE STEP 73.
(2) ADD:
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F-14D 飞行手册 Flight Manual 1(23)
