N701GS

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 75,091 hrs · 45,939 cycles

AFT EMERGENCY OUTBOARD FLASH LIGHT STRAP BROKEN. / R&R STRAP PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,531 hrs · 45,593 cycles

LT 156 AFT EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 74,528 hrs · 45,589 cycles

R1 DOOR FORWARD UPPER SIDE FUSELAGE SKIN AND BEAR STRAP CRACKED AT BS. 295, 10" ABOVE HINGE CUTOUT. REPAIRED SKIN BEAR STRAP PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,528 hrs · 45,589 cycles

R1 DOOR UPPER FORWARD FRAME STUB FRAME CRACKED. R&R STUB FRAME PER SRM AND EA.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 74,399 hrs · 45,501 cycles

L2 EXTERIOR EMERGENCY EXIT LIGHT INOP. FOUND CONTACTS TO BE DIRTY. CLEANED CONTACTS. RELAMPED LIGHT IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19R. R&R GUSSET IAW DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 21R. / R&R GUSSET IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

FORWARD PIT RT Z-ANGLE SPOTS CORRODED BETWEEN BS. 500A TO BS. 500D. R&R RT Z ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

FORWARD PIT RT Z-ANGLE HAD SPOTS OF CORROSION, BETWEEN BS. 500 TO BS. 500A. REPAIRED Z-ANGLE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

PASSENGER CABIN SEAT TRACK CROWN CORRODED AT BS. 727, LBL 24. REPAIRED SEAT TRACK IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

FORWARD PIT AFT BULKHEAD LOWER SUPPORT CORRODED AT BS. 500D BETWEEN STR. 24L TO STR. 24R. R&R LOWER SUPPORT IAW DWG AND SRM.

Part: SHEAR TIE — CORRODED (BS 907) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT STA 907 BL 0 TO RBL 5 SHEAR TIE CORRODED ON THE AFT SIDE. / REPAIRED FRAME IAW SRM AND EA.

Part: WEB — CORRODED (BS 794-814) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED BETWEEN BS. 794 TO BS. 814. / R&R WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 934-947) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT CORRODED BETWEEN BS. 934 TO BS. 947, RBL 13. R&R FLOOR TRACK IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

AFT PIT RT Z-ANGLE HAD SPOTS OF CORROSION BETWEEN BS. 727D TO BS. 767. R&R Z ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 848) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED AT BS. 848, LBL 17. / R&R INTERCOSTAL IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

AFT PIT FLOOR SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+6, RT. REPAIRED SHIELD IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 510) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE CORRODED AT FASTENER HOLES BS. 510, LBL 24.5. / REPAIRED "Z" ANGLE IAW SRM.

Part: CARGO TRACK — CORRODED (BS 727E) · airframe 74,399 hrs · 45,501 cycles

AFT PIT STA FLOOR SUPPORT RAIL CORRODED AT BS. 727E+3, LBL 12. / REPAIRED RAIL IAW SRM.

Part: ANGLE — CORRODED (BS 450) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT L/H SIDE Z-ANGLE AT FASTENER HOLE CORRODED AT BS. 450, LBL 24.5. / REPAIRED "Z" ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 926-947) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT CORRODED BETWEEN BS. 926 TO BS. 947, LBL 3. / R&R FLOOR SUPPORT IAW DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

AFT PIT FLOORBEAM CORRODED AT BS. 727E+3, LBL 3. REPAIRED FLOORBEAM IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT SIDEWALL BULKHEAD FRAME CORRODED AT BS. 500D, BETWEEN STR. 24R TO STR. 25R. R&R FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 926) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT CORRODED AT BS. 926, RBL 8. / REPAIRED FLOOR BOARD SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (BS 867) · airframe 74,399 hrs · 45,501 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT ANGLE CORRODED AT BS. 867, RBL 10. REPAIRED ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 500A-500B) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS. 500A TO BS. 500B, LBL 23, AT FASTENER HOLES. REPAIRED "Z" ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 500) · airframe 74,399 hrs · 45,501 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE AT FASTENER HOLE CORRODED AT BS. 500+7, LBL 23. / REPAIRED Z ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 74,399 hrs · 45,501 cycles

PRESSURE WEB CRACKED AT BS. 663, LBL 38. REPAIRED WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 74,399 hrs · 45,501 cycles

RT WING REAR SPAR AFT NUTPLATE ATTACH ANGLE FOR PANEL 661AB CRACKED INBOARD SIDE. R&R ANGLE IAW DWG AND SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 74,399 hrs · 45,501 cycles

CRACK IN DOOR HANDLE BOX LOWER ATTACH BEAM AT INBOARD ATTACH BOLT HOLE IN INSPECTION AREA. R&R THE #4 BEAM IN THE R1 DOOR IAW DWG AND CCO.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 74,399 hrs · 45,501 cycles

VERTICAL STABILIZER FUSELAGE STA. 1018, 8" ABOVE FUSELAGE SKIN, LBL AND RBL 10", LATERAL SUPPORT RIB STIFFENER AT STRAIN RELIEF RADIUS, CRACKED ON BOTH ENDS. / R&R STIFFENER IAW SRM AND DWG.

Part: RIB — CRACKED (RT WING) · airframe 74,399 hrs · 45,501 cycles

RT WING ANGLE ATTACHED TO INBOARD SIDE OF DEFLECTOR RIB CRACKED. R&R DEFLECTOR RIB IAW SRM AND DWG.

Part: SLIDE — LOOSE (ENTRY DOOR) · airframe 74,310 hrs · 45,442 cycles

SLIDE LOOSE. TIGHTENED SCREWS IAW SIP.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 73,664 hrs · 45,030 cycles

AFT SERVICE DOOR ESCAPE SLIDE IS COMING OUT OF HOUSING. STRAIGHTENED SLIDE GIRT BAR INTO COMPARTMENT PER CMM 25-00-00

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 73,186 hrs · 44,739 cycles

L1 DOOR SLIDE LIGHT INOP. R&R FUSE PER AMM.

Part: SLIDE — STRETCHED (R1 DOOR) · airframe 73,120 hrs · 44,695 cycles

R1 DOOR WITH SLIDE ARMED, STRECTED OUT OF CONTAINER MORE THAN NORMAL. SLIDE DID NOT DEPLOY. SECURED SLIDE PER AMM.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 72,965 hrs · 44,603 cycles

DIVERSION/DECLARED EMERGENCY, F1945 SAN/MSY DIVERTED TO AUS DUE TO NR 1 ENGINE OIL QUANTITY. R&R GARLOC SEAL PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,732 hrs · 44,455 cycles

L1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 71,830 hrs · 43,867 cycles

L2 DOOR EMERGENCY EXIT SIGN MISSING COVER. INSTALLED LENS COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,553 hrs · 42,400 cycles

LT EMERGENCY HATCH LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: COVER — CRACKED (RT AILERON TAB) · airframe 68,555 hrs · 41,763 cycles

RT AILERON TRIM TAB OUTBOARD HINGE COVER CRACKED. R&R COVER IAW AMM.

Part: STRINGER SPLICE — CORRODED (BS 887) · airframe 67,962 hrs · 41,382 cycles

STRINGER SPLICE 26L CORRODED AT BS 887. R & R THE STRINGER SPLICE IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 887) · airframe 67,962 hrs · 41,382 cycles

STRINGER SPLICE 25L CORRODED AT BS 887. REPAIRED THE STRINGER SPLICE IAW SRM.

Part: STRINGER — CORRODED (BS 375) · airframe 67,962 hrs · 41,382 cycles

STRINGER 28L CORRODED AT BS 375. REPAIRED THE STRINGER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 67,962 hrs · 41,382 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 380 TO 400, RBL 10. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 67,962 hrs · 41,382 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 380 TO 400, BL 0. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: ANGLE — CORRODED (BS 320) · airframe 67,962 hrs · 41,382 cycles

OUTER ANGLE CORRODED AT BS 320, BETWEEN STRINGER 21L TO 23L. REMOVED THE ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (BS 312-325) · airframe 67,962 hrs · 41,382 cycles

INTERCOSTAL CORRODED BETWEEN BS 312 TO 325, STRINGER 23L. R & R THE INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (BS 344-360) · airframe 67,962 hrs · 41,382 cycles

INTERCOSTAL CORRODED BETWEEN BS 344 TO 360, STRINGER 23L. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 259.5) · airframe 67,962 hrs · 41,382 cycles

BULKHEAD WEB CRACKED AT BS 259.5, STRINGER 12L. REPAIRED THE BULKHEAD WEB IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,962 hrs · 41,382 cycles

AFT POTABLE WATER DRAIN MAST CUTOUT CORRODED. R&R CUTOUT PER SRM AND DWG.

Part: ANGLE — CRACKED (BS 663) · airframe 67,962 hrs · 41,382 cycles

ANGLE CRACKED AT BS 663, RBL 60. R & R THE ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (BS 807-827) · airframe 67,962 hrs · 41,382 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 807 TO 827, STRINGER 17R. R & R THE WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 67,962 hrs · 41,382 cycles

STRINGER CLIP 8R CRACKED AT BS 360. R & R THE STRINGER CLIP IAW SRM.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 67,962 hrs · 41,382 cycles

DOUBLER ANGLE CHAFED AT BS 360, STR 8R. R&R ANGLE IAW SRM AND EA.

Part: STRAP — CORRODED (CABIN) · airframe 67,962 hrs · 41,382 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP CORRODED. R&R STRAP PER AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 67,962 hrs · 41,382 cycles

REAR SPAR BULKHEAD VAPOR BARRIER WEB CRACKED AT BS 663, RBL 30. REPAIRED WEB PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,962 hrs · 41,382 cycles

FLOOR SUPPORT CRACKED AT BS 663, BETWEEN RBL 45 TO RBL 65. R&R SUPPORT IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 67,962 hrs · 41,382 cycles

UPPER PRESSURE DECK CRACKED AT BS 664, RBL 42. REPAIRED DECK IAW EA AND ER.

Part: SKIN — CRACKED (LE SLAT) · airframe 67,962 hrs · 41,382 cycles

RT WING NR 5 SLAT SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 67,962 hrs · 41,382 cycles

RT WING NR 4 SLAT SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 67,962 hrs · 41,382 cycles

LEFT WING NR 1 SLAT SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED IAW SRM.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 67,962 hrs · 41,382 cycles

LEFT WING NR 2 SLAT SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED THE SKIN IAW SRM.

Part: GIRT BAR — LOOSE (L2 DOOR SLIDE) · airframe 67,249 hrs · 40,960 cycles

L2 DOOR SLIDE GIRT BAR LOOSE. R & R THE STRAP IAW SIP.

Part: CHARGER — FAILED (CABIN) · airframe 66,980 hrs · 40,809 cycles

RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R&R CHARGER PER MM.

Part: CHARGER — FAILED (CABIN) · airframe 66,980 hrs · 40,809 cycles

LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R&R CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,980 hrs · 40,809 cycles

CABIN EMERGENCY EXIT LIGHTS BULBS INOP. RELAMPED LIGHT IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,980 hrs · 40,809 cycles

CABIN EMERGENCY LIGHT BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM.

Part: MOUNT — CRACKED (L2 DOOR SLIDE) · airframe 66,978 hrs · 40,808 cycles

L2 DOOR SLIDE FWD MOUNT CRACKED. R & R THE MOUNT IAW MM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 66,978 hrs · 40,808 cycles

RIGHT MLG WHEEL WELL FWD BULKHEAD STIFFENER CRACKED AT BS 663, RBL 25. R & R THE STIFFENER IAW SRM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 66,122 hrs · 40,333 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 64,945 hrs · 39,643 cycles

AFT LT EMERGENCY BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: RIB — CRACKED (RT WING) · airframe 64,945 hrs · 39,643 cycles

RIGHT WING T/E FIXED PANEL SUPPORT BRACKET CRACKED. R & R RIB IAW DWG.

Part: BEAM — CRACKED (RT WING) · airframe 64,945 hrs · 39,643 cycles

RIGHT WING T/E FIXED PANEL SUPPORT BRACKET CRACKED. R & R BEAM IAW DWG.

Part: TRANSMITTER — FAULTY (LT WING TE FLAPS) · airframe 62,866 hrs · 38,430 cycles

TE FLAPS ASYMMETRY INDICATION. DECLARED AN EMERGENCY. R & R LT TE FLAPS POSITION TRANSMITTER IAW MM.

Part: FASTENER — SHEARED (L1 DOOR) · airframe 62,736 hrs · 38,354 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR AFT RETAINER CLIP SHEARED. R & R FASTENER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,452 hrs · 38,191 cycles

INTERIOR EMER EXIT LIGHT BULB AT OVERWING EXIT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,452 hrs · 38,191 cycles

R1 DOOR EMER SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

STRINGER CLIP CRACKED AT BS 807, STRINGER 27R. R & R CLIP IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

R1 DOOR CUT OUT FWD LOWER STUB BEAM CRACKED AT BS 295, WL 209. REPAIRED STUB BEAM IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CRACKED, BETWEEN BS 294.5 - 312, RBL 14. REPAIRED INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 312 - 328, LBL 12. R & R SUPPORT IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 62,452 hrs · 38,191 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT RBL 40. REPAIRED WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

R1 DOOR THRESHOLD SUPPORTS CORRODED. R & R FWD SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 328 - 344, LBL 12. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CRACKED, BETWEEN BS 927 - 947, BL 0. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

FLOORBEAM UPPER SURFACE AROUND FASTENER HOLE CORRODED AT BS 986, RBL 45. REPAIRED FLOORBEAM IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,452 hrs · 38,191 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

FLOOR SUPPORT CORRODED, BETWEEN BS 312 - 328, RBL 12. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 48. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 30. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CRACKED, BETWEEN BS 277 - 294.5, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL CORRODED AT BS 727+4, LBL 4. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727C+18 TO 767, RBL 22. R & R SUPPORT IAW SRM.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 62,452 hrs · 38,191 cycles

LEFT WING INBD OF DEFLECTION ROLLER, RIB WEB ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

INTERCOSTAL WEB CORRODED, BETWEEN BS 787 - 794, STRINGER 19R - 20R. R & R INTERCOSTAL IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,452 hrs · 38,191 cycles

STRINGER CLIP CORRODED AT BS 787, STRINGER 19R. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,452 hrs · 38,191 cycles

RIGHT WING LOWER SURFACE OF THE LE, NR 7 SLAT NOSE SKIN, CRACKED AT SLAT BS 322.71. REPAIRED SKIN IAW SRM.

Part: ENGINE — LEAKING (RIGHT) · airframe 61,957 hrs · 37,893 cycles

DIVERTED & DECLARED EMER. ENG OIL QTY DROPPED TO 0. OIL PRESS REMAINED ABOVE LIMITS UNTIL SHORT FINAL, THEN FLASHED YELLOW. FOUND FWD SUMP DRAIN LINE LEAKING OIL. R & R NR 2 ENG IAW MT. ENG PN OFF, SN OFF 874109, ENG PN ON CFM56-7B24G22 & SN ON 874714.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,011 hrs · 37,393 cycles

FUSELAGE SKIN CRACKED AT BS 879, STRINGER 27L. REPAIRED SKIN IAW EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 60,833 hrs · 37,290 cycles

LEFT WING INBD MAIN FLAP TE WEDGE DELAMINATED. R & R WEDGE IAW SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 60,833 hrs · 37,290 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOOK LOOSE. R & R HOOK IAW SRM.

Part: FAN — FAULTY (AC BAY) · airframe 60,524 hrs · 37,115 cycles

DESCENDING ON ARRIVAL, FLIGHT ATTENDANT REPORTED ODOR AROUND MID-CABIN. R & R RECIRCULATION FAN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,372 hrs · 36,458 cycles

R1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LATCH — DIRTY (GIRT BAR) · airframe 58,707 hrs · 36,060 cycles

L1 DOOR FLOOR LATCH FOR GIRT BAR INOPERATIVE. REMOVED DEBRIS FROM UNDERNEATH FLOOR LATCH MECHANISM IAW SIP.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 57,088 hrs · 35,106 cycles

FORWARD FLASHLIGHT LIGHT MISSING. INSTALLED FLASHLIGHT IAW MM.

Part: OVERHEAT SENSOR — FAULTY (MLG WW) · airframe 57,016 hrs · 35,060 cycles

MLG WW FIRE WARNING LIGHT INDICATION. R & R MLG WW OVERHEAT SENSOR IAW MM.

Part: FLAP TRACK — LOOSE (LT WING) · airframe 56,526 hrs · 34,766 cycles

LT WING OTBD AFT FLAP INBD TRACK LOOSE AT BEARING ATTACH POINT. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — LOOSE (LT WING) · airframe 56,526 hrs · 34,766 cycles

LT WING OTBD AFT FLAP, OTBD TRACK LOOSE AT BEARING ATTACH POINT. R & R FLAP TRACK IAW AMM.

Part: ATTACH BRACKET — LOOSE (L2 DOOR) · airframe 56,526 hrs · 34,766 cycles

L2 DOOR EMERGENCY EVAC SLIDE UPPER FWD ATTACH BRACKET LOOSE. R & R BRACKET IAW SRM.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 56,461 hrs · 34,716 cycles

WING TO BODY FAIRING 195CL CRACKED. REPAIRED FAIRING IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 56,461 hrs · 34,716 cycles

WING TO BODY FAIRING PANEL 195CR CRACKED AT AFT LOWER EDGE. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,461 hrs · 34,716 cycles

FUSELAGE SKIN CRACKED AT STATION 540, STRINGER 22L. REPAIRED SKIN IAW SRM & SWA EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 56,461 hrs · 34,716 cycles

PASSENGER CABIN FLOOR PANEL 241BF DELAMINATED ON UPPER SURFACE & EDGE DAMAGE ON LOWER SURFACE AT AFT END. R & R PANEL IAW DRAWING & EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 56,461 hrs · 34,716 cycles

PASSENGER CABIN FLOOR PANEL 242AF DELAMINATED ON UPPER SURFACE. R & R PANEL IAW SRM & DRAWING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 56,461 hrs · 34,716 cycles

PASSENGER CABIN FLOOR PANEL 242BF DELAMINATED ON UPPER SURFACE & EDGE DAMAGE ON LOWER SURFACE. R & R PANEL IAW DRAWING & EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 56,461 hrs · 34,716 cycles

PASSENGER CABIN FLOOR PANEL 241AF DELAMINATED ON UPPER SURFACE. REPAIRED PANEL IAW SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 55,676 hrs · 34,241 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED SLIDE IAW MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

RT NR 1 WINDOW FRAME & WINDSHIELD ASSEMBLY CRACKED. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

LT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R&R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 727A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

LT NR 1 WINDOW FRAME CRACKED AT FASTENER HOLE AT UPPER OTBD CORNER. R&R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 907, STRINGER 8L. REPAIRED FRAME IAW AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 907 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

FRAME CRACKED AT STATION 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

RT FS FRAME WEB CRACKED AT STATION 259.5, STRINGER 9R. REPAIRED WEB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME AT E-F POST CRACKED AT SECOND LOWER CORNER FASTENER HOLE. R&R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,605 hrs · 34,198 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME AT E-F POST CRACKED AT SECOND LOWER CORNER FASTENER. CRACK EXTENDS THROUGH BOTH SIDES OF HOLE. R&R FRAME IAW SRM & DRAWING.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,825 hrs · 33,731 cycles

RIGHT EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 54,825 hrs · 33,731 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT PER AMM.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 54,713 hrs · 33,657 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,674 hrs · 33,627 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,674 hrs · 33,627 cycles

SEAT TRACK JUST CRACKED AT BS 727B, LBL 24.75. REPAIRED TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,674 hrs · 33,627 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,674 hrs · 33,627 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED TRACK IAW AAR EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,674 hrs · 33,627 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED TRACK IAW AAR EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,369 hrs · 33,430 cycles

R2 DOOR SLIDE GIRT BAR IS ADRIFT AFTER SECURING DOOR. RE-INSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 54,000 hrs · 33,194 cycles

AFT SERVICE SLIDE DISLODGED WHILE DOOR WAS OPENED. REPOSITIONED SLIDE IN AFT SERVICE DOOR COMPARTMENT PER MT 325-61-06. OK TO CONTINUE SERVICE.

Part: SLAT — CRACKED (LT WING) · airframe 52,869 hrs · 32,490 cycles

LEFT WING NR 1 SLAT CRACKED. REMOVED AND REPLACED NR 1 SLAT PER AMM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 52,869 hrs · 32,490 cycles

RIGHT WING INBOARD AFT FLAP LOWER SKIN PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 52,869 hrs · 32,490 cycles

RIGHT WING LEADING EDGE NR 8 SLAT CRACKED. REMOVED AND REPLACED NR 8 SLAT PER AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,869 hrs · 32,490 cycles

RIGHT WING O/B AFT FLAP DELAMINATED AT THE INBOARD CORNER. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SLAT — CRACKED (RT WING) · airframe 52,869 hrs · 32,490 cycles

RIGHT WING LEADING EDGE NR 6 SLAT CRACKED. REMOVED AND REPLACED NR 6 SLAT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,642 hrs · 31,730 cycles

OVERWING EEPLS INOP BETWEEN ROWS 9 TO ROW 11. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,687 hrs · 31,169 cycles

CENTER RIGHT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,687 hrs · 31,169 cycles

AFT RIGHT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,687 hrs · 31,169 cycles

FWD LEFT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,010 hrs · 30,754 cycles

EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,390 hrs · 30,408 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT FOR POSITION M1674 INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,458 hrs · 29,872 cycles

DURING SCHEDULED HC2 CHECK FOUND, R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 48,410 hrs · 29,843 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN COVER LENS LOOSE. SECURED LENS PER MM.

Part: DUCT — BROKEN (AC SYSTEM) · airframe 48,288 hrs · 29,782 cycles

DURING DESCENT NOTICED A SLIGHT SMELL IN CABIN AND COCKPIT. FOUND DISTRIBUTION DUCT BROKEN. REMOVED AND REPLACED DUCT PER MM.

Part: GASPER FAN — MALFUNCTIONED (CARGO BAY) · airframe 47,253 hrs · 29,194 cycles

GASPER FAN CAUSED ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,253 hrs · 29,194 cycles

RT EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 46,894 hrs · 28,993 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — BROKEN (CABIN) · airframe 45,863 hrs · 28,394 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT BASE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,977 hrs · 27,889 cycles

RT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 43,682 hrs · 27,141 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND STIFFENER CRACKED AT BS 540, LBL 33. REPAIRED STIFFENER PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER AAR EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND BULKHEAD VERTICAL BEAM CRACKED AT BS 727, RBL 35.5. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 43,122 hrs · 26,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,122 hrs · 29,791 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 42,831 hrs · 26,602 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,991 hrs · 26,096 cycles

DURING SCHEDULED HC1 CHECK, OVERWING EMERGENCY EXIT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,991 hrs · 26,096 cycles

DURING SCHEDULED HC1 CHECK, LT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 40,838 hrs · 25,371 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS STRIP BROKEN BETWEEN ROW 3 TO ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,738 hrs · 24,687 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BUSHING — MISSING (NR 1 ENGINE) · airframe 39,631 hrs · 24,625 cycles

AIR TURNBACK/DECLARED EMERGENCY. DURING CLIMB NR 1 ENG POPPED AND BANGED AT 10,000 FT. FOUND RT VSV ACTUATOR BELLCRANK TO 3RD STG ARM NUT BUSHING MISSING. INSTALLED BUSHING & HARDWARE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,548 hrs · 23,329 cycles

DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,548 hrs · 23,329 cycles

DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 36,782 hrs · 22,850 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 34,924 hrs · 21,784 cycles

R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: SIGN — MISSING (CABIN) · airframe 33,411 hrs · 20,918 cycles

FWD CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EMERGENCY EXIT SIGN PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 32,683 hrs · 20,495 cycles

DURING SCHEDULED HC1 CHECK, RIGHT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BRACKET — LOOSE (R2 DOOR GIRT BAR) · airframe 32,244 hrs · 20,227 cycles

R2 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,419 hrs · 18,644 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM UPPER CAP CORRODED AT BS 986.5. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 27,963 hrs · 17,812 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 27,278 hrs · 17,425 cycles

DURING SCHEDULED MV2 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT LENS BROKEN AT R1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 27,047 hrs · 17,305 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 19,786 hrs · 13,197 cycles

DURING SCHEDULED RON, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY HOUSING PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,843 hrs · 12,149 cycles

DURING SCHEDULED 5Y CHECK, FOUND EMERGENCY LIGHT BATTERY PACK AT FWD GALLEY LT CEILING INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: RETAINER — LOOSE (L1 DOOR.) · airframe 17,666 hrs · 12,034 cycles

FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE GIRT BAR FWD RETAINER CLIP FASTENER SHEARED. INSTALLED RETAINER CLIP FASTENER PER MM AND SRM.

Part: TAB — WORN (ELEVATOR) · airframe 12,342 hrs · 8,937 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: FAN — OVERHEATED (A/C BAY) · airframe 12,179 hrs · 8,837 cycles

DURING CRUISE FUMES ODOR IN COCKPIT AND FWD CABIN. TURNED OFF RECIRC FAN, AIR CLEARED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 12,060 hrs · 8,764 cycles

EEPLS TRACK LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 11,932 hrs · 8,680 cycles

EEPLS TRACK WIRES EXPOSED AT ROW 6. SECURED EEPLS WIRES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 11,325 hrs · 8,299 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 8, 9, 12, 19, 20 & 23. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 11,021 hrs · 8,117 cycles

EEPLS WIRING EXPOSED. INSTALLED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 10,217 hrs · 7,637 cycles

EEPLS TRACK LOOSE AT FORWARD SECTION. SECURED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 9,996 hrs · 7,491 cycles

LT SIDE, ROW 2, EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 9,989 hrs · 7,485 cycles

EEPLS WIRES LOOSE AT ROW 2. RELAMPED (P/N 0L3071BPL5GPL) AND SECURED EEPLS WIRES PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 9,379 hrs · 7,117 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED GIRT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 8,928 hrs · 6,871 cycles

EEPLS TRACK COVER SECTION LOOSE. RESECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (KRUGER FLAP) · airframe 8,597 hrs · 6,655 cycles

DURING SCHEDULED A1 CHECK, FOUND NR 1 KRUEGER FLAP CRACKED AT CENTER SECTION. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (WING LE) · airframe 8,394 hrs · 6,536 cycles

DURING SCHEDULED BC1 CHECK, FOUND BOTH LT AND RT WING O/B KRUEGER FLAPS HAVE .25 INCH CRACKS ON INNER SKIN ACROSS T/E OF VERTICAL STIFFENER RIB. REMOVED AND REPLACED BOTH KRUEGER FLAPS PER MM.

Part: WINDOW — UNLATCHED (COCKPIT) · airframe 7,952 hrs · 6,268 cycles

ABORTED TAKE-OFF - FIRST OFFICERS COCKPIT SLIDING WINDOW OPENED 95 KNTS INTO THE TAKE-OFF. INSPECTED AND OPERATED FIRST OFFICERS SLIDING WINDOW PER MM. OPS CK GOOD. NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (ROW 18 - 20) · airframe 7,869 hrs · 6,221 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOPERATIVE AT ROWS 18 - 20. REPAIRED WIRING PER MM.

Part: LIGHT — INOP (ROW 17-19)

EEPLS INOP BETWEEN ROWS 17-19. REPAIRED LIGHT SYSTEM PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK LOOSE AT FWD END. REINSTALLED TRACK ASSY PER MM.

Part: WIRE — LOOSE (ROW 20)

EEPLS WIRING LOOSE AT ROW 20. SECURED WIRING AND TRACK PER MM.

Part: WIRE — BROKEN (CABIN)

FWD SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHTING DAMAGED. REPAIRED BROKEN WIRE PER MM.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE)

HEAVY AIRFRAME VIBRATION AT 35000 FT FLIGHT LEVEL, 260 KNOTS, 92 PERCENT N1. VIBRATION GOES AWAY WHEN POWER REDUCED. REMOVED AND REPLACED NR 2 ENGINE HMU PER MM.

Part: COVER — LOOSE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING COVER LOOSE AND MISSING LENS. REFASTENED COVER AND REMOVED AND REPLACED LENS PER MM.

Part: HMU — CONTAMINATED (NR 2 ENGINE)

INFLIGHT SHUT DOWN, NR 2 ENGINE ROLLED BACK AT 31,000 FEET AND 87 PERCENT N1, WINDMILLED AND APU RESTART UNSUCCESSFUL AT 25,000 FEET, 280 KNOTS. APU RESTARTED AT 19,000 FEET 280 KNOTS, ENGINE RAN FOR APPROXIMATE 20 MINUTES AND ROLLED BACK AGAIN AT 12,000 FEET, 35 PERCENT N1 (ENGINE FLAMED OUT). REMOVED AND REPLACED NR 2 HMU AND FUEL PUMP (SUSPECT CONTAMINATION), OPS AND LEAK CHECKED GOOD PER MM. PUMP (P/N 828300-3), (S/N YA010103-F).

Part: BATTERY — DISCHARGED (ROW 16 & 19)

DURING SCHEDULED BC3 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 16ABC AND 19ABC INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER BOEING M/M.

Part: PITOT ADM — INOP (NR 2)

DIVERTED TO LAS DUE TO AIRSPEED INDICATOR 10 KTS LOW AT 35,000 FT ON SHORT FINAL, INDICATOR 17 KTS SLOWER THAN CAPT AND PNEUMATIC A/S INDICATOR. DURING ADIRU BITE FOUND FAULT CODES 34-21007 AND 34-210032 AND 34-210033. TROUBLESHOT SYSTEM PER 34-21-00-2. FOUND NR 2 PITOT ADM BAD (M01753). REMOVED AND REPLACED SAME. SYS NOW OPS GOOD PER M/M.