N7712G

Part: PROCESSOR — FAULTY (FUEL QTY) · airframe 48,395 hrs · 23,915 cycles

DIVERSION, FUEL IMBALANCE APPROXIMATELY 1200 LBS. LEFT WING HEAVY FUEL IN WING TANKS ONLY. R&R FUEL QUANTITY PROCESSOR AS PER MM.

Part: COVER — UNSECURE (CABIN) · airframe 46,875 hrs · 22,973 cycles

EXIT LIGHT COVER FELL OFF NEAR FORWARD FLIGHT ATTENDANT JUMPSEAT. R&R LIGHT COVER ASSEMBLY IAW AMM.

Part: BEARING — DAMAGED (COCKPIT WINDOW) · airframe 46,688 hrs · 22,850 cycles

AIR TURNBACK, FIRST OFFICERS WINDOW CAME UNSEALED AFTER TAKE OFF - AIRCRAFT WOULD NOT PRESSURIZE. / FOUND 2 SLIDING WINDOW TO NOT BE CLOSED INSPECTED WINDOW AND INSTALLED FORWARD BEARING IN REFERENCE TO AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,332 hrs · 22,635 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,332 hrs · 22,635 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,332 hrs · 22,635 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 45,747 hrs · 22,282 cycles

RT 'EXIT SIGN FELL OFF' NEAR SEAT 12. SECURED SIGN PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,597 hrs · 21,596 cycles

EMERGENCY LIGHT BATTERY PACK INOP AT LOCATION M2335. R&R BATTERY PACK PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,597 hrs · 21,596 cycles

EMERGENCY LIGHT BATTERY PACK INOP AT LOCATION M2335. R&R CHARGER PER AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,597 hrs · 21,596 cycles

SEAT TRACK CORRODED BETWEEN BS 727B TO BS 888, RBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 44,597 hrs · 21,596 cycles

R1 DOOR BEAM NR 4 CRACKED. REPAIRED DOOR PER CMM & SRM.

Part: STRIP — DELAMINATED (CABIN) · airframe 44,339 hrs · 21,425 cycles

LT FLOOR EGRESS STRIPS BY AFT WHEELCHAIR CLOSET DELAMINATED. R&R EGRESS STRIPS PER DWG.

Part: STRIP — DELAMINATED (CABIN) · airframe 44,339 hrs · 21,425 cycles

RT FLOOR EGRESS STRIPS BY AFT WHEELCHAIR CLOSET DELAMINATED. R&R EGRESS STRIPS PER DWG.

Part: LIGHT — LOOSE (CABIN) · airframe 43,946 hrs · 21,202 cycles

AFT GALLEY ENTRY DOOR EXIT SIGN ON WALL LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 42,506 hrs · 20,347 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 42,506 hrs · 20,347 cycles

RT WING INBOARD AFT FLAP OUTBOARD TRACK AFT ATTACH POINT LOOSE. R&R FLAP TRACK AMM.

Part: BATTERY — FAILED (CABIN) · airframe 42,506 hrs · 20,347 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: PLATE — CRACKED (RT WING) · airframe 42,506 hrs · 20,347 cycles

RT WING LOWER TRAILING EDGE SHELF PANEL OUTBOARD NR 6 X-MISSION FORWARD WIGGLE PLATE CRACKED. R&R WIGGLE PLATE PER SRM..

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 42,506 hrs · 20,347 cycles

RT WING INBOARD AFT FLAP INBOARD TRACK AFT ATTACH POINT LOOSE. R&R FLAP TRACK PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 42,506 hrs · 20,347 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 42,506 hrs · 20,347 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 39,884 hrs · 18,827 cycles

NR 2 ENGINE WOULD NOT DEVELOP CLIMB THRUST OUT OF 10,000 FEET, RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE FUEL PUMP IAW MT.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 39,884 hrs · 18,827 cycles

NR 2 ENGINE WOULD NOT DEVELOP CLIMB THRUST OUT OF 10,000 FEET, RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MT.

Part: COVER — WRONG PART (EMERGENCY LIGHT) · airframe 39,329 hrs · 18,513 cycles

L1 DOOR EMERGENCY LIGHT COVER MISSING RED ARROW. R & R THE COVER IAW MM.

Part: COVER — WRONG PART (EMERGENCY LIGHT) · airframe 39,329 hrs · 18,513 cycles

R1 DOOR EMERGENCY LIGHT COVER MISSING RED ARROW. R & R COVER IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 38,264 hrs · 17,895 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PER AMM.

Part: CARGO TRACK — CRACKED (BS 727-747) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO BAY, CARGO TRACK CRACKED BETWEEN BS 727 TO 747, RBL 13.8. R & R THE CARGO TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

RT SIDE INNER CREASE BEAM CORRODED AT BS 727A, STR 17R. REPAIRED CREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (BS 706) · airframe 38,197 hrs · 17,855 cycles

R/H CREASE BEAM CORRODED AT BS 706. REPAIRED THECREASE BEAM IAW EA.

Part: CREASE BEAM — CORRODED (BS 685-727) · airframe 38,197 hrs · 17,855 cycles

LEFT CREASE BEAM CORRODED AT BS 685 TO 727. REPAIRED THE CREASE BEAM IAW SRM.

Part: ANGLE — CORRODED (BS 727-757) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 727 TO 757, LBL 21. R & R THE ANGLE IAW SRM.

Part: WEB — CORRODED (BS 685) · airframe 38,197 hrs · 17,855 cycles

RIGHT CREASE BEAM WEB LOWER SIDE CORRODED AT BS 685+13. R & R THE WEB IAW DWG AND SRM.

Part: WEB — CORRODED (BS 709-727) · airframe 38,197 hrs · 17,855 cycles

R/H LOWER CREASE BEAM WEB CORRODED BETWEEN BS 706 TO 727. R & R THE WEB IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT FLOOR WEB ATTACH ANGLE CORRODED BETWEEN BS 767 TO BS 792, RBL 22. R&R ANGLE IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 792-847) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO BAY CARGO TRACK CORRODED BETWEEN BS 792 TO 847, RBL 12. R & R THE CARGO TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

RT CREASE BEAM CORRODED FORWARD AND AFT OF BS 706. R&R CREASE BEAM IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT FLOOR WEB SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 17. R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

INTERCOSTAL CORRODED BETWEEN BS 260 TO BS 270, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19R. R&R CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 38,197 hrs · 17,855 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.30, 2ND STIFFENER FROM THE FORWARD SPAR. REPAIRED THE RIB IAW SRM & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 767 TO BS 792, RBL 21. R&R WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT Z ANGLE CORRODED AT RT BS 727D. R&R Z ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 38,197 hrs · 17,855 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.30, 3RD STIFFENER FROM THE FORWARD SPAR. REPAIRED THE STIFFENER IAW EA.

Part: CREASE BEAM — CORRODED (BS 706) · airframe 38,197 hrs · 17,855 cycles

LEFT CREASE BEAM CORRODED AT BS 706. REPAIRED THE CREASE BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19L. R&R CLIP IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT LOWER DOOR CUTOUT FLOOR THRESHOLD WEB UPPER SURFACE CORRODED. REPAIRED WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 727 TO BS 767, RBL 21. REPAIRED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 757-847) · airframe 38,197 hrs · 17,855 cycles

AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 757 TO 847, LBL 21. R & R THE ANGLE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500B, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (BS 344) · airframe 38,197 hrs · 17,855 cycles

GIRT BAR FITTING SUPPORT ANGLE CORRODED AT BS 344, LBL 60. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

CABIN FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 9 TO RBL 7. REPAIRED SUPPORT IAW SRM AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,197 hrs · 17,855 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE RT SIDE SHIELD Z ANGLE CORRODED BETWEEN BS 490 TO BS 500A. R&R Z ANGLE IAW BAC DWG.

Part: FLOOR SUPPORT — CRACKED (BS 278-294) · airframe 38,197 hrs · 17,855 cycles

CABIN FLOOR SUPPORT IS CRACKED BETWEEN BS 278 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW DWG & SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 38,197 hrs · 17,855 cycles

LT WING TRAILING EDGE LOWER BULB SEAL BRACKET CRACKED ON FORWARD SIDE. R&R BRACKET IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 38,197 hrs · 17,855 cycles

RT WHEEL WELL VERTICAL PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB IAW SRM.

Part: COVER — BROKEN (L1 DOOR) · airframe 35,472 hrs · 16,323 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LIGHT COVER BROKEN. R & R COVER IAW MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 35,472 hrs · 16,323 cycles

R1 DOOR EMER EVAC SLIDE BOTTLE PRESS LOW. R & R SLIDE IAW MT & AMM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 34,272 hrs · 15,639 cycles

R2 DOOR EMER EXIT SIGN LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 31,446 hrs · 14,106 cycles

L2 DOOR SLIDE LOOSE. SECURED SLIDE ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 31,446 hrs · 14,106 cycles

R2 DOOR SLIDE LOOSE. SECURED SLIDE ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 31,446 hrs · 14,106 cycles

R1 DOOR SLIDE LOOSE. SECURED SLIDE ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,446 hrs · 14,106 cycles

AFT ENTRY EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,446 hrs · 14,106 cycles

L1 DOOR EXTERNAL EMER SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

LONGITUDINAL BEAM FWD SEAT TRACK INBD FLANGE AFT & FWD HOLES & OTBD FLANGE AFT HOLE ARE CRACKED AT BS 727B, LBL 24. REPAIRED BEAM IAW EA, REPAIRED BEAM IAW ER & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 31,446 hrs · 14,106 cycles

LEFT HORIZONTAL STAB RIB AT RIB STATION 92.7 2ND STIFFENER AFT CRACKED. REPAIRED RIB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. R & R SUPPORT IAW SRM.

Part: RETAINING CLIP — BENT (L1 DOOR) · airframe 31,446 hrs · 14,106 cycles

L1 DOOR EMER EVAC SLIDE COVER FWD GIRT BAR RETAINER CLIP BENT. R & R RETAINER CLIP IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 31,446 hrs · 14,106 cycles

RIGHT WING TE ORSS 261, WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

STRINGER SPLICE CRACKED AT BS 727C, STRINGER 2L. REPAIRED SPLICE IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

CAPTAIN`S NR 3 WINDOW FRAME CRACKED, FWD SIDE OF FRAME, SECOND FROM BOTTOM FASTENER. REPAIRED FRAME IAW ACO.

Part: ATTACH BRACKET — CRACKED (TE FLAP) · airframe 31,446 hrs · 14,106 cycles

RIGHT WING TE FLAP CAM TRACK ARM, INBD ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 31,446 hrs · 14,106 cycles

VERTICAL STABILIZER HORIZONTAL STIFFENER CRACKED LT & RT SIDES JUST AFT & ABOVE VERTICAL STAB FWD ATTACH POINTS. R & R STIFFENER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

FIRST OFFICER'S NR 1 WINDOW FRAME CRACKED AT THE OTBD UPPER CORNER. REPAIRED FRAME IAW EO.

Part: SHEAR TIE — CRACKED (RT WING) · airframe 31,446 hrs · 14,106 cycles

RIGHT WING WW INBD OF BOOST PUMP SHEAR TIE CRACKED. R & R SHEAR TIE IAW SOPM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

LONGITUDINAL BEAM FWD SEAT TRACK INBD & OTBD FLANGE AFT HOLES CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

SKIN CRACKED AT BS 540 STRINGER 22L. REPAIRED SKIN IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

LONGITUDINAL BEAM INTERIOR FWD SEAT TRACK INBD FLANGE AFT & FWD HOLES & OTBD FLANGE FWD HOLE CRACKED AT BS 727B, RBL 24. REPAIRED BEAM IAW ER & EA.

Part: BRACKET — BENT (R1 DOOR) · airframe 31,446 hrs · 14,106 cycles

R1 DOOR EMER EVAC SLIDE LATCH BRACKET ASSEMBLY UPPER LINK IN CHAIN BENT. REMOVED & REPLACED BRACKET IAW SOPM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

LONGITUDINAL BEAM FWD SEAT TRACK INBD FLANGE AFT HOLE CRACKED AT BS 727B, RBL 45. REPAIRED BEAM IAW ER & EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 31,446 hrs · 14,106 cycles

L1 DOOR SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

RIGHT FLOOR CREASE BEAM CORRODED AT BS 616 RBL 64. REPAIRED BEAM IAW ER & EA.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 31,446 hrs · 14,106 cycles

L1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

RIGHT FLOOR CREASE BEAM AT FLOOR ATTACH FASTENER HOLES CORRODED BETWEEN BS 570 TO 624, RBL 64. REPAIRED CREASE BEAM IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 31,446 hrs · 14,106 cycles

RIGHT HORIZONTAL STABILIZER RIB AT RIB STATION 129.5 3RD STIFFENER AFT CRACKED. REPAIRED RIB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

RIGHT FLOOR CREASE BEAM UPPER SURFACE CORRODED BETWEEN BS 698 TO 707, RBL 64. REMOVED CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

RIGHT CREASE BEAM AT FLOOR ATTACH FASTENER HOLES CORRODED BETWEEN BS 639 TO 663, RBL 64. REPAIRED CREASE BEAM IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO RBL 25. R & R SUPPORT IAW SRM.

Part: GUSSET — CRACKED (RT WING) · airframe 31,446 hrs · 14,106 cycles

RIGHT WING TE U/S FIXED TE PANEL GUSSET CRACKED. R & R GUSSET IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,446 hrs · 14,106 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.