M. (1) DELETE (CHANGE): RENUMBER EXISTING STEP 4 TO NEW STEP 5
WITHOUT CHANGING VERBIAGE.
N. (1) DELETE: NA
(2) ADD (INSERT): STATEMENT AFTER NEW STEP 5 TO
READ: "IF INDICATIONS OF A FUEL LEAK EXIST:"
O. (1) DELETE: NA
(2) ADD (INSERT): NEW STEP 6 AFTER STATEMENT TO READ:
"6. REFER TO FUEL LEAK PROCEDURE (PAGE 126A)."
6. CHANGE REF F (F-14B NFM), CHAPTER 14, PAGE 14-20A, PARAGRAPH
14.6.6 AS FOLLOWS:
A. (1) DELETE: STATEMENTS UNDER FIRST WARNING: "DURING AB
OPERATIONS, NORM SHALL BE SELECTED. FWD OR AFT COULD DEPLETE THE
SUMP TANKS."
(2) ADD (REPLACE WITH): "AB OPERATION IS NOT RECOMMENDED WITH
A FUEL IMBALANCE OR WITH INDICATIONS OF VENTING FUEL."
B. (1) DELETE: NA
(2) ADD (INSERT): NOTE PARAGRAPH BEFORE THE EXISTING
NOTE PARAGRAPH AT THE BEGINNING OF THE PROCEDURE TO READ:
"FUEL QUANTITY BALANCING IS NOT REQUIRED PRIOR TO COMPLETION OF
WING/EXTERNAL TANK TRANSFER OR UNTIL ONE FUSELAGE TAPE DROPS BELOW
4,500 POUNDS."
C. (1) DELETE: NA
(2) ADD: STATEMENT IN CAPITAL ITALICS, PRIOR TO STEP 1, TO
READ: "WITH A FUEL STATE BELOW 4500 POUNDS IN A SINGLE FEED GROUP
AND A FUEL SPLIT GREATER THAN 1500 POUNDS BETWEEN THE AFT/LEFT AND
FWD/RIGHT FEED GROUPS:"
D. (1) DELETE: NA
(2) ADD (INSERT): NOTE PARAGRAPH IMMEDIATELY AFTER STEP 2
TO READ: "IF PRACTICAL, OBTAIN A VISUAL INSPECTION FOR VENTING
FUEL.DO NOT DELAY EXECUTION OF EMERGENCY PROCEDURES FOR VISUAL
INSPECTION."
E. (1) DELETE: NA
(2) ADD (INSERT): NOTE PARAGRAPH AFTER PRECEEDING (INSERTED)
NOTE PARAGRAPH, BUT PRIOR TO THE EXISTING WARNING PARAGRAPH TO READ:
"INDICATION OF FUEL BALANCING SHOULD APPEAR WITHIN 3 MINUTES OF
SELECTING THE HIGH FUSELAGE TAPE SIDE."
F. (1) DELETE: ENTIRE WARNING THAT BEGINS WITH "AIRCRAFT
ATTITUDE WILL HAVE A SIGNIFICANT INFLUENCE..."
(2) ADD: NA
G. (1) DELETE: NA
(2) ADD (MOVE): FIRST NOTE PARAGRAPH OF EXISTING PROCEDURE
THAT BEGINS, "WITH A HIGH QUANTITY...", TO A POSITION IMMEDIATELY
FOLLOWING THE SECOND ADDED NOTE PARAGRAPH BETWEEN STEPS 2 AND 3.
UPDATE THE NOTE PARAGRAPH TO READ: "WITH A HIGH QUANTITY IN THE
FWD/RT FUEL SYSTEM, THE GREATER STATIC HEAD PRESSURE, PARTICULARLY
IN NOSE-UP ATTITUDES CAN CAUSE OVERFILLING OF THE AFT/LT FUEL SYSTEM
AND SUBSEQUENT FUEL VENTING. TO PREVENT THIS, THE FEED SWITCH
SHOULD BE RETURNED TO NORM BEFORE THE AFT/LT TAPE REACHES 6,200
POUNDS. OVERFILLING IS INDICATED BY A QUANTITY OF 6,600 POUNDS OR
GREATER IN THE FWD/RT SYSTEM OR 6,200 POUNDS OF GREATER IN THE
AFT/LT SYSTEM."
H. (1) DELETE: STATEMENT IMMEDIATELY PRECEDING STEP 3 THAT
READS: "IF FUEL IMBALANCE INCREASES:"
NAVAIR 212005Z JUL04 Page 6 of 11 A1-F14AAA-1 IC 150
A1-F14AAA-1B IC 106
A1-F14AAP-1 IC 48
A1-F14AAP-1B IC 32
A1-F14AAD-1 IC 28
A1-F14AAD-1B IC 17
Summary of Contents for F-14B
Page 10: ......
Page 22: ......
Page 32: ...NAVAIR 01 F14AAP 1B 10 16...
Page 44: ...NAVAIR 01 F14AAP 1B 22 28 EJECT EGRESS...
Page 46: ...NAVAIR 01 F14AAP 1B 24 30...
Page 50: ...NAVAIR 01 F14AAP 1B 28 34 ELECT...
Page 52: ...NAVAIR 01 F14AAP 1B 30 36...
Page 66: ...NAVAIR 01 F14AAP 1B 44 50 ENG...
Page 68: ...NAVAIR 01 F14AAP 1B 46 52...
Page 92: ...NAVAIR 01 F14AAP 1B 70 76...
Page 130: ...NAVAIR 01 F14AAP 1B 106b 114...
Page 144: ...NAVAIR 01 F14AAP 1B 120 128 FUEL...
Page 146: ...NAVAIR 01 F14AAP 1B 122 130...
Page 158: ...NAVAIR 01 F14AAP 1B 130 140...
Page 166: ...NAVAIR 01 F14AAP 1B 136b 148...
Page 176: ...NAVAIR 01 F14AAP 1B 146 158 LAND LAND GEAR...
Page 178: ...NAVAIR 01 F14AAP 1B 148 160...
Page 194: ...NAVAIR 01 F14AAP 1B 162b 176...
Page 201: ...NAVAIR 01 F14AAP 1B 169 183 EMERGENCY FIELD ARRESTMENT GUIDE SHEET 2 169 SE...
Page 202: ...NAVAIR 01 F14AAP 1B 170 184 SE...
Page 204: ...NAVAIR 01 F14AAP 1B 172 186...
Page 215: ...NAVAIR 01 F14AAP 1B 183 197 2 TO...
Page 216: ...NAVAIR 01 F14AAP 1B 184 198 TO...
Page 218: ...NAVAIR 01 F14AAP 1B 186 200...
Page 222: ...NAVAIR 01 F14AAP 1B 190 206...
Page 226: ...NAVAIR 01 F14AAP 1B 190d 210...
Page 244: ...NAVAIR 01 F14AAP 1B 206 220...
Page 246: ...NAVAIR 01 F14AAP 1B 208 222...
Page 302: ...NAVAIR 01 F14AAP 1B 332...
Page 316: ...NAVAIR 01 F14AAP 1B 276 300 276 Change 3...
Page 319: ...NAVAIR 01 F14AAP 1B 279 295 AC RIGHT MAIN CIRCUIT BREAKER PANEL LEFT AFT PANEL NO 2...
Page 320: ...NAVAIR 01 F14AAP 1B 280 296 AC ESSENTIAL NO 2 PHASE A CIRCUIT BREAKER PANEL LEFT PANEL NO 3...
Page 323: ...NAVAIR 01 F14AAP 1B 283 299 DC ESSENTIAL NO 1 CIRCUIT BREAKER PANEL RIGHT SIDE PANEL NO 6...
Page 326: ...NAVAIR 01 F14AAP 1B 286 302 DC MAIN CIRCUIT BREAKER PANEL RIGHT AFT PANEL NO 8 UPPER SEGMENT...
Page 327: ...NAVAIR 01 F14AAP 1B 287 303 DC MAIN CIRCUIT BREAKER PANEL RIGHT AFT PANEL NO 8 LOWER SEGMENT...
Page 331: ...NAVAIR 01 F14AAP 1B 291 307 AIRCRAFT SERVICING LOCATIONS...
Page 334: ...NAVAIR 01 F14AAP 1B 294 310 AIRCRAFT SERVICING DATA SHEET 3...
Page 335: ...NAVAIR 01 F14AAP 1B 295 311 AIRCRAFT SERVICING DATA SHEET 4...
Page 336: ...NAVAIR 01 F14AAP 1B 296 312 AIRCRAFT SERVICING DATA SHEET 5 296 Change 2...
Page 337: ...NAVAIR 01 F14AAP 1B 297 313 AIRCRAFT SERVICING DATA SHEET 6...
Page 338: ...NAVAIR 01 F14AAP 1B 298 314 AIRCRAFT SERVICING DATA SHEET 7...
Page 339: ...NAVAIR 01 F14AAP 1B 299 315 AIRCRAFT SERVICING DATA SHEET 8 299 300 blank...
Page 340: ...NAVAIR 01 F14AAP 1B 300 316...