N605SW

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 67,013 hrs · 53,532 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE IAW MT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

FLOOR STRUCTURE ANGLE CRACKED AT BS 727B, BL 0. R&R ANGLE IAW SRM AND DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT PLATE CRACKED AT BS 492, BETWEEN STR 19R TO STR 25R. R&R PLATE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

FRAME CORRODED AT BS 500A, BETWEEN STR 28R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 66,718 hrs · 53,333 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING) · airframe 66,718 hrs · 53,333 cycles

RIGHT WING FIXED LEADING EDGE SKIN CRACKED AT WS 208. REPAIRED THE SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 66,718 hrs · 53,333 cycles

LT WING REAR SPAR LOWER CHORD SUPPORT ANGLE CRACKED ON WS 537.806. R&R ANGLE IAW SRM AND DWG.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 66,718 hrs · 53,333 cycles

LT WING INBOARD FLAP OUTBOARD TRACK NR 3 FAIRING DELAMINATED. REPAIRED FAIRING IAW SRM.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 66,718 hrs · 53,333 cycles

FLOOR PROXIMITY PHOTO LUMINESCENT LIGHT STRIP BROKEN STRIP. R&R STRIP IAW AMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

CHANNEL CRACKED BETWEEN BS 328 TO BS 344, LBL 45.6. R&R CHANNEL IAW SRM AND DWG.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 66,718 hrs · 53,333 cycles

LT WING NR 4 FLAP TRACK FAIRING DELAMINATED. REPAIRED FAIRING IAW SRM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 66,718 hrs · 53,333 cycles

AFT GALLEY AREA FLASHLIGHT SAFETY STRAP BROKEN. R&R STRAP IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

STUB FRAME CRACKED AT BS 294.5, STR 8R. R&R STUB FRAME IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

FLOOR STRUCTURE WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 277-291) · airframe 66,718 hrs · 53,333 cycles

R1 DOOR CUTOUT ANGLE CRACKED BETWEEN BS 277 TO 291.5, STRINGERS 9 -15R. REPAIRED THE ANGLE IAW EA.

Part: FRAME — CRACKED (BS 277) · airframe 66,718 hrs · 53,333 cycles

FRAME CRACKED AT BS 277, STRINGER 15R. REPAIRED THE FRAME IAW EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,718 hrs · 53,333 cycles

FORWARD GALLEY AREA EMERGENCY EXIT SIGN LENS BROKEN. R & R THE LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,718 hrs · 53,333 cycles

L1 DOOR LOWER AFT CORNER SKIN CRACKED BETWEEN BS 326 TO BS 355, BETWEEN STR 14L TO STR 18L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (BS 312-344) · airframe 66,718 hrs · 53,333 cycles

FORWARD GALLEY DOOR SKIN CUTOUT CRACKED BETWEEN BS 312 TO 344, BETWEEN STRINGERS 15 TO 18R. REPAIRED THE SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 66,718 hrs · 53,333 cycles

LT WING TRAILING EDGE STRUCTURE ANGLE CRACKED AT WS 537. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,718 hrs · 53,333 cycles

RT WING OUTBOARD AFT FLAP LOWER EXTERNAL SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: MOUNT — CORRODED (R1 DOOR) · airframe 66,718 hrs · 53,333 cycles

R1 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNT ASSEMBLY CORRODED. R&R MOUNT ASSEMBLY IAW AMM.

Part: FRAME — CRACKED (BS 794) · airframe 66,718 hrs · 53,333 cycles

AFT CARGO BAY FRAME CRACKED AT BS 794, BETWEEN STRINGERS 16 - 27R. R & R THE FRAME SECTION IAW SRM & DWG.

Part: BULKHEAD — CRACKED (BS 664) · airframe 66,718 hrs · 53,333 cycles

LEFT MAIN WHEEL WELLS COMPARTMENT PRESSURE DECK CRACKED AT BS 664, LBL 8. REPAIRED THE BULKHEAD IAW EA.

Part: BULKHEAD — CRACKED (BS 664) · airframe 66,718 hrs · 53,333 cycles

LEFT MAIN WHEEL WELL COMPARTMENT PRESSURE DECK CRACKED AT BS 664, LBL 17. REPAIRED THE BULKHEAD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 66,718 hrs · 53,333 cycles

RT MAIN WHEEL WELL COMPARTMENT PRESSURE DECK CRACK WEB CRACKED BETWEEN BS 664 TO BS 675, BETWEEN 31 TO RBL 48. REPAIRED WEB IAW EA.

Part: SEAT TRACK — BROKEN (BS 807-827) · airframe 66,718 hrs · 53,333 cycles

SEAT TRACK BROKEN BETWEEN BS 807 TO 827, LBL 24.75. REPAIRED THE SEAT TRACK IAW EA.

Part: LATCH — STUCK (COCKPIT) · airframe 65,672 hrs · 52,663 cycles

F/O EMERGENCY ESCAPE ROPE LATCH STUCK. FREED LATCH IAW AMM.

Part: CIRCUIT CARD — FAULTY (LANDING GEAR) · airframe 65,359 hrs · 52,455 cycles

LANDING GEAR DOWN INDICATION 3 GREEN LIGHTS, 2 RED LIGHTS FOR MAIN GEAR CYCLED GEAR & GOT ONLY 3 GREEN. R & R CARD IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 64,885 hrs · 52,149 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,830 hrs · 52,106 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED, AT FASTENER JUST OTBD OF ACT. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING NR 8 SPOILER TOP SURFACE DELAMINATED. R & R NR 8 SPOILER IAW MM.

Part: HINGE BRACKET — CRACKED (LT SPOILER) · airframe 64,828 hrs · 52,105 cycles

LEFT WING NR 4 GND SPOILER PANEL SUPPORT HINGE BRACKET, CRACKED ON UPPER OTBD FWD OTBD END. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING UPPER SKIN, AT REAR SPAR HOLE CRACKED, AT RSS 232.5, FWD ROW. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING BRACKET CRACKED AT RSS 234. R & R BRACKET IAW SRM & DWG.

Part: FITTING — CORRODED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING REAR SPAR, INBD BATH TUB FITTING AT UPPER CHORD CORRODED, AT RSS 136, INBD FASTENER HOLE. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,828 hrs · 52,105 cycles

LEFT WING REAR SPAR, WEB AT MLG AFT SUPPORT FITTING, 2ND HOLE FROM INBD, HOLE NR 4 CRACKED. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,828 hrs · 52,105 cycles

LEFT WING REAR SPAR, UPPER CHORD AT MLG AFT SUPPORT FITTING, 2ND HOLE FROM INBD NR 4 HOLE CRACKED. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING REAR SPAR, AFT SUPPORT FITTING AT UPPER CHORD, UPPER ROW HOLE NR 5 RSS 222.34 OF GROUP OF 12 HOLES CRACKED, INDICATION AT 7 O CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR AFT SUPPORT FITTING AT UPPER CHORD, UPPER ROW HOLE NR 5, RSS 222.34 OF GROUP OF 12 HOLES, CRACKED AT 5 O'CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LT WING MAIN LANDING GEAR SUPPORT FORWARD FITTING CRACKED AT STA RSS 224.14. REMOVED AND REPLACED FITTING IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR WEB, UPPER FWD WING ROOT FITTING, CRACKED AT INBD HOLE AT RSS 139, FWD EDGE OF HOLE AT 7 O CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING REAR SPAR WEB UPPER FWD WING ROOT FITTING INBD HOLE AT RSS 139, FWD EDGE OF HOLE AT 7 O CLOCK POSITION CRACKED. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR WEB, LOWER CHORD LOWER HOLE AT RSS 224.75, CRACKED AT 6 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING UPPER SKIN, AT REAR SPAR HOLE AT RSS 263.34, AFT FASTENER ROW CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING UPPER SKIN AT REAR SPAR HOLE, AT RSS 241.5, 3RD FASTENER ROW FWD 3.5" FROM TE. CRACKED INDICATION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING UPPER SKIN AT REAR SPAR HOLE, AT RSS 255.34, AFT FASTENER ROW CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN HOLE CRACKED, AT RSS 248.875, 4TH ROW FROM AFT, 4.75" FROM TE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN CRACKED AT RSS 239.34, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN CRACKED AT RSS 249.5, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN HOLE CRACKED, AT RSS 269, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN HOLE CRACKED AT RSS 268, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN HOLE CRACKED, AT RSS 230.34, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN HOLE CRACKED, BETWEEN RSS 239 - 257, AFT FROM TE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN CRACKED AT RSS 255.375, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN CRACKED, AT RSS 257, AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING UPPER SKIN CRACKED, AT RSS 251, AFT ROW. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR UPPER CHORD, AT MLG AFT SUPPORT FITTING UPPER ROW, 4TH FROM OTBD FASTENER HOLE H CRACKED. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING REAR SPAR, UPPER CHORD, LOWER ROW OTBD FASTENER HOLE SPLICE CRACKED. REPAIRED SPLICE IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING REAR SPAR, UPPER CHORD AT MLG, AFT SUPPORT FITTING LOWER ROW 2ND FROM OTBD FASTENER HOLE CRACKED. REPAIRED SPLICE IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING REAR SPAR, UPPER CHORD AT MLG AFT SUPPORT FITTING, UPPER INBD FASTENER HOLE CRACKED. REPAIRED SPAR IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,828 hrs · 52,105 cycles

RIGHT WING REAR SPAR, UPPER CHORD, UPPER ROW 3RD FROM INBD FASTENER HOLE CRACKED. REPAIRED SPLICE IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,827 hrs · 52,105 cycles

LEFT WING REAR SPAR UPPER CHORD, UPPER ROW, 4TH FROM INBD, FASTENER HOLE CRACKED. REPAIRED CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR WEB AT MLG, AFT SUPPORT FITTINGS UPPER ROW, 5TH FROM OTBD, FASTENER HOLE CRACKED. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,827 hrs · 52,105 cycles

RIGHT WING REAR SPAR, UPPER CHORD UPPER ROW, 4TH FROM INBD FASTENER HOLE CRACKED. R & R SPAR IAW EA.

Part: BRACKET — CRACKED (LT MLG DOOR) · airframe 63,483 hrs · 51,161 cycles

LEFT MLG MID DOOR AFT ATTACHMENT TO STRUT BRACKET CRACKED. R & R DOOR BRACKET IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 62,816 hrs · 50,719 cycles

R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,806 hrs · 50,713 cycles

FORWARD SERVICE DOOR EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM.

Part: SLAT — CRACKED (RT WING) · airframe 62,806 hrs · 50,713 cycles

RIGHT WING NR 5 SLAT LOWER LE 2 INCHES FROM INBD END CRACKED. REPAIRED NR 5 SLAT IAW SRM.

Part: BATTERY PACK — DAMAGED (CABIN) · airframe 62,806 hrs · 50,713 cycles

LEFT EMER BATTERY PACK POWER SUPPLY CEILING OVERHEAD DAMAGED AT BS 967. R & R BATTERY PACK IAW AMM.

Part: SLAT — CRACKED (RT WING) · airframe 62,806 hrs · 50,713 cycles

RIGHT WING NR 5 SLAT LOWER LE 40 INCHES FROM OTBD END CRACKED. REPAIRED NR 5 SLAT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STRINGER 28R TO 28L. R & R SHEAR TIE IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOOR STRUCTURE UPPER INTERCOSTAL ANGLE CRACKED BETWEEN BS 927 TO 947, BL 0. INSTALLED ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 767 TO 787. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO 500C. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 380 - 400. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO 420. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO 420. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO 380. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500C TO 500D. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 747 TO 767. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO 787+6. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 440 TO 460. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 807 TO 827. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO 500B. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO 480. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO 400. R & R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBOARD SUPPORT STRUCTURE CORRODED BETWEEN BS 770 TO 775, RBL 8. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 770 TO 775, RBL 3. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 770 TO 775, LBL 8. REPAIRED SUPPORT IAW EA & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBOARD SUPPORT CORRODED BETWEEN BS 770 TO 775, LBL 3. REPAIRED SUPPORT IAW EA & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FRAME LOWER ANGLE SHEAR TIE CORRODED AT BS 520, BETWEEN STRINGER 28R & 28L. R & R SHEAR TIE IAW DWG & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 667 TO 671, RBL 24.8. REPAIRED BEAM IAW ER & EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBEAM STABILIZING STRAP CRACKED AT BS 328, BL 10. REPAIRED STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FLOORBEAM STABILIZING STRAP AT CRACKED AT BS 328, BL 0. REPAIRED STRAP IAW SRM

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 660, LBL 24.8. REPAIRED BEAM IAW ER & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

STRINGER TIE CLIP CRACKED AT BS 328, STRINGER 20L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

STRINGER TIE CLIP CRACKED AT BS 320, STRINGER 20L. R & R TIE CLIP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

STRINGER CRACKED AT BS 360, STRINGER 2L. R & R STRINGER IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

STRINGER SPLICE CORRODED AT BS 360, STRINGER 24L. R & R SPLICE IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FORWARD CARGO LT KEEL BEAM LOWER CHORD CORRODED AT BS 500D. REPAIRED CHORD IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 62,806 hrs · 50,713 cycles

LEFT WING RSS 553 WIPER WEB ATTACH CLIP CRACKED. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

CAPTAIN'S NR 1 WINDOW C - D POST FUSELAGE SKIN CRACKED AT UPPER END SIDE. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 709 TO 712, RBL 24.75. REPAIRED BEAM IAW EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,806 hrs · 50,713 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 667, LBL 24.8. REPAIRED CHORD IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 62,806 hrs · 50,713 cycles

RIGHT WING SEAL SUPPORT ANGLE CHORD CRACKED ON OTBD SIDE OF NR 2 PYLON JUST AFT OF UPPER TE PANEL. REPAIRED CHORD IAW ACO & EA.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 62,806 hrs · 50,713 cycles

RIGHT WING RSS 553 WIPER WEB ATTACH CLIP CRACKED. R & R CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL FLOORBEAM CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

FIRST OFFICER'S NR 1 WINDOW C - D WINDOW POST UPPER END SIDE FUSELAGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 62,806 hrs · 50,713 cycles

RIGHT HORIZONTAL STABILIZER REMOVABLE LE 3RD RIB OTBD OF INBD END CRACKED. REPAIRED RIB IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LONGITUDINAL BEAM UPPER CHORD CRACKED BETWEEN BS 667 TO 671, RBL 24.8 AT FWD LOWER CORNER & UPPER AFT CORNER. REPAIRED CHORD IAW ER & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LEFT OTBD CHORD CRACKED AT BS 727, STRINGER 18A LOWER FWD HOLE CRACKED FWD & AFT SIDE OF HOLE. REPAIRED CHORD IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

LOWER FUSELAGE SKIN CRACKED AT OPENING FOR GND SERVICE AIR CONDITIONING ACCESS DOOR. REPAIRED CUT OUT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

INTERCOSTAL CHANNEL CRACKED AT BS 540, STRINGER 25L. R & R INTERCOSTAL IAW SRM.

Part: SKIN — BROKEN (FUSELAGE) · airframe 62,806 hrs · 50,713 cycles

RIGHT SIDE GND SERVICE AIR CONDITIONING ACCESS DOOR CUT OUT FUSELAGE SKIN BROKEN. REPAIRED CUT OUT IAW SRM.

Part: RETAINING CLIP — BROKEN (EXIT LIGHT) · airframe 62,747 hrs · 50,674 cycles

FORWARD ENTRY EMER EXIT LIGHT COVER RETAINING CLIPS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,884 hrs · 50,049 cycles

LEFT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 61,532 hrs · 49,809 cycles

B HYD QTY GAUGE SHOWED 1/2 FULL. ON APPROACH ENG 2 LOW PRESS LIGHT FLICKERED TWICE. R & R B SYS ELEC HYD PUMP PRESS LINE IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,579 hrs · 49,145 cycles

LT WING OTBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,555 hrs · 49,129 cycles

RT WING INBD AFT FLAP OTBD EDGE LOWER SURFACE DELAMINATED. R & R AFT FLAP IAW MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,555 hrs · 49,129 cycles

STRINGER CORRODED AT BS 1016, STRINGER 25L. R & R STRINGER IAW DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 60,555 hrs · 49,129 cycles

STIFFENER CHANNEL CORRODED AT BS 1016, LOWER HOLE IN RT 186. REPAIRED STIFFENER IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,555 hrs · 49,129 cycles

AFT CARGO COMPARTMENT FWD SIDE OF DOOR CUTOUT CLOSE OUT WEB CRACKED. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 60,555 hrs · 49,129 cycles

AFT BULKHEAD CORRODED AT BS 1016, BL 0. REPAIRED BULKHEAD IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,555 hrs · 49,129 cycles

FWD CARGO DOOR CUTOUT, AFT FRAME INBD FLANGE CRACKED AT INNER RADIUS ADJACENT TO INBD LOWER CORNER OF BOTTOM STOP FITTING. R & R FRAME IAW ACO.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 60,511 hrs · 49,100 cycles

FWD CARGO DOOR LOWER AFT CORNER MODIFICATION ANGLE CRACKED AT FASTENER. R & R DOOR IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 60,096 hrs · 48,828 cycles

RT HORIZONTAL LOWER STAB SKIN AT AFT SPAR CRACKED. MEASURES 1.9 INCHES & IS 60 INCHES OTBD OF FUSELAGE. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 59,401 hrs · 48,350 cycles

R1 DOOR EMERGENCY EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 59,401 hrs · 48,350 cycles

L1 DOOR EMERGENCY EXIT SIGN TAB BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 59,202 hrs · 48,200 cycles

R1 DOOR LIGHT SIGN MISSING. INSTALLED SIGN IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 59,149 hrs · 48,159 cycles

R1 DOOR EMERGENCY EXIT LENS FELL OFF. INSTALLED LENS IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 59,013 hrs · 48,058 cycles

FWD GALLEY EMERGENCY EXIT SIGN LOOSE. R&R SIGN IAW MM.

Part: BLOWER — OVERHEATED (AC BAY) · airframe 58,991 hrs · 48,044 cycles

PLASTIC SMELL IN COCKPIT & NORMAL EQUIP BLOWER CIRCUIT BREAKER TRIPPED. R&R EQUIP COOLING BLOWER IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,952 hrs · 48,012 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL DOWN FROM CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SIGN — MISSING (CABIN) · airframe 58,796 hrs · 47,879 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 58,660 hrs · 47,777 cycles

FWD ENTRY EMERGENCY EXIT LEN BROKEN OFF. R & R LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,612 hrs · 47,735 cycles

FWD OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,946 hrs · 47,240 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: MOUNT — BROKEN (CABIN) · airframe 57,941 hrs · 47,239 cycles

EMERGENCY EXIT LIGHT ON GALLEY G-1 MOUNTING BASE IS BROKEN. REMOVED & REPLACED BASE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,940 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 480 AT S-8L FOUND CRACKED. REMOVED AND REPLACED CLIP IAW SRM BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

STRINGER CLIP AT STA 986, STR 2L IS CRACKED. REMOVED AND REPLACED CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

STRINGER CLIP AT STA 1006, STR 2.5R IS CRACKED. REMOVED AND REPLACED CLIP IAW BAC DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,940 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 400 S-7R FOUND CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

STRINGER CLIP AT STA 927, STR 2R IS CRACKED. REMOVED AND REPLACED CLIP IAW BAC DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,940 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 380 S-8L FOUND CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 500D S3R DAMAGED. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 440 S2R DAMAGED. REMOVED AND REPLACED CLIP AT IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 500 S3R DAMAGED. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 500 AT STRINGER S3L DAMAGED. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP STA 500B S-3R DAMAGED. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN STRINGER CLIP AT STA 360 AT STRINGER S1 DAMAGED. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN - DAMAGED STRINGER CLIP AT BS 727E S3L. REMOVED & REPLACED CLIP IAW SRM & BAC DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN -- DAMAGED STRINGER CLIP AT BS 727E S2R. REMOVED AND REPLACED STR CLIP IAW B737 -300 SRM 51-40-02 & BAC DWG 65C25230 REV J.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN -- DAMAGED STRINGER CLIP AT BS 867 STRINGER 1. REMOVED AND REPLACED STR CLIP IAW B737 -300 SRM 51-40-02 & BAC DWG 65C46555 REV G.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

MAIN CABIN -- DAMAGED STRINGER CLIP AT BS 827 STRINGER 1. REMOVED & REPLACED STR CLIP IAW B737 -300 SRM 51-40-02 & BAC DWG 65C46552 REV H.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED SKIN CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 500+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 9. REPAIRED RIGHT 500+40 UPPER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2, SECTION 3 B3 PER TASK CARD 10073, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 460+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 7. REPAIRED LEFT BS 480+10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3BB PER TASK CARD 10072. STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 400+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 2. REPAIRED RIGHT BS 400 +10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2, SECTION 3B3. PER TASK CARD 10073, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 6, 7. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 3, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 4, 6, 7. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 440+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 440+10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3 B3 PER TASK CARD 10072 REV 3 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 380+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED LEFT BS 380+10 UPPER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3 B3 PER TASK CARD 10072 REV 3 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CORNER HAS HFEC CRACK INDICATION AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 380+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED RIGHT BS 380+10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2, SECTION 3B3, PER TASK CARD 10073, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED SKIN CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 827+10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3 B3 AND TASK CARD 10075 FIGURE 9. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 727+10 UPPER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLES 2, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 727E+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED INDICATION AT HOLE NR 2. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 867 +10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 AND TASK CARD 10075 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CORNER HAS HFEC CRACK INDICATION AT HOLE NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 767+10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3 B3 AND TASK CARD 10075 FIGURE 9.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED SKIN CUTOUT IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED SKIN CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 787+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 787+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3 AND TASK CARD 10075 FIGURE 9. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 747+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 827+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3.B3. AND TASK CARD 10075 FIGURE 9. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED RIGHT BS 827 +10 UPPER AFT WINDOW CORNER IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED RIGHT BS 867 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 3. REPAIRED LEFT BS 807+10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3 B3 AND TASK CARD 10075 FIGURE 9. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED SKIN CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,941 hrs · 47,239 cycles

LEFT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED INDICATION AT HOLES 3, 7. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (RT WING) · airframe 58,195 hrs · 47,428 cycles

UPPER RIGHT WING TRAILING EDGE PANEL 5835R CRACKED IN RADIUS. REPAIRED PANEL IAW SRM.

Part: SIGN — SHORTED (CABIN) · airframe 57,567 hrs · 46,985 cycles

FWD LAV MOUNTED EMERGENCY EXIT SIGN BULBS FAIL TO ILLUMINATE. REPLACED SHORTED FWD MOUNTED EMERGENCY EXIT SIGN IAW AMM 33-51-81-332-044-002. OPS CHECK NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 57,567 hrs · 46,985 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR HAS BULBS THAT FAIL TO ILLUMINATE. REPLACED FUSE IN THE M1675 EMERGENCY EXIT LIGHT BATTERY PACK IAW WDM 33-51-12. OPS CHECKS GOOD IAW AMM 33-51-11-402-007 ITEM 4.D(1)(A).

Part: LATCH — CRACKED (LT WING) · airframe 57,567 hrs · 46,985 cycles

LEFT WING FUEL BOOST PUMP LATCH ASSEMBLIES CRACKED. REMOVED AND REPLACED 5 EACH LEFT WING FUEL BOOST PUMP LATCH ASSEMBLIES ON BOOST PUMP ACCESS PANELS IAW SOPM 20-50-01.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CORROSION FOUND ON STR CLIP 23 RT STA 947. REMOVED AND REPLACED STR CLIP STA 947 STR 23 WITH FABRICATED CLIP ON BACK SHOP WORK ORDER 26285/1600/0005 IAW SPM 57-40-02 AND DW 65-46560.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN: SHEAR TIE AT STA 947 BETWEEN STR 24L AND 26L IS CORRODED ALL THE WAY THROUGH ON I/B SIDE. REMOVED AND REPLACED SHEAR TIE AT STA 947 STR 24L - 26L IAW SRM 51-40-02 AND DWG 65-46560.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN: STRINGER CLIP AT STA 947 STR 25R WAS FOUND CRACKED. ACCOMPLISHED ON NON ROUTINE ITEM 7 LOCATION STA 947 STR 25R FOR INSTALLATION STR CLIP REMOVED & LOCATED IAW SRM 51-40-05 A TAG# A25782.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN STRINGER CLIP AT STA 947 STR 24L FOUND CORRODED. REMOVED AND REPAIRED STRINGER CLIP AT5 STA 947 STR 24L WITH FABRICATED CLIP ON BACKSHOP WORK ORDER 26285/1600/0006 IAW SRM 51-40-02 AND DWG 65-46560.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AFT CARGO PIT FRAME CLIP AT STA 807 RBL 20 IS CRACKED. REPLACED AFT CARGO PIT FRAME CLIP AT STA 807 RBL 20 WITH NEW CLIP IAW SRM 51-40-02 CIC'D CLIP IAW SRM 51-20-01 & DWG 65-47957 REV B.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

INTERCOSTAL SUPPORT CLIP AT STA 947 STR 24L CRACKED. REMOVED AND REPLACED CLIP IAW SRM AND BOEING DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 767+5, RBL 3, LONGITUDINAL FLOOR SUPPORT CORRODED AT FASTENER HOLE. REMOVED AND REPLACED SUPPORT IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 767+5, LBL 3, LONGITUDINAL FLOOR SUPPORT CORRODED AT 2EA FASTENER HOLES. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN: AFT PIT STA 794, RBL 8, LONGITUDINAL FLOOR SUPPORT LOWER SURFACE, 1EA FASTENER HOLE, EXFOLIATED. REPAIRED LONGITUDINAL FLOOR SUPPORT AT STA 794 RBL 8 IAW SRM 53-00-53-2R-1 & EA 1-A53-2021 REV 7 WITH A NESTED ANGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 727A+4, RBL 3, LONGITUDINAL FLOOR SUPPORT CORRODED AROUND 1EA FASTENER HOLE. REPAIRED SUPPORT IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

FLOOR SUPPORT STRAP UPPER SURFACE CORRODED AT BS 811, RBL 20. REPLACED STRAP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 727B+3, LBL 3, LONGITUDINAL FLOOR SUPPORT CORRODED AROUND 1EA FASTENER HOLE. REPAIRED SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 727A+7 TO +17, RBL 23, INTERCOSTAL FLOOR SUPPORT CORRODED AT 4EA FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND BOEING DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

INTERCOSTAL FLOOR SUPPORT UPPER FLANGE CORRODED BETWEEN BS 927 TO BS 947, RBL 22. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 794 TO BS 867, RBL 14. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 767+5, LBL 8, LONGITUDINAL FLOOR SUPPORT CORRODED AT 2EA FASTENER HOLES. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 767+5, LBL 12, LONGITUDINAL FLOOR SUPPORT CORRODED AT 2EA FASTENER HOLES. REPAIRED SUPPORT IAW SRM AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT FRAME AT BS 947 CORRODED LOWER SIDE BETWEEN STR 25R AND 26R. REMOVED AND REPLACED IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN SI# 11972-53. FORWARD ENTRY DOOR SURROUND BS 348 STR 16L FRAME ATTACH ANGLE CRACKED. REF P/N 69-26555-3. REPLACED FWD ENTRY DOOR SURROUND STA 348 STR 16L FRAME ATTACH ANGLE IAW SRM 51-40-02 AND DWG 65-17685.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 727D+5, RBL 8, LONGITUDINAL FLOOR SUPPORT CORRODED AT FASTENER HOLE. REMOVED AND REPLACED SUPPORT IAW SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

SHEAR TIE AT STA 747 BETWEEN STR 27L AND 27R CORRODED. REMOVED AND REPLACED IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

SEAT TRACK, LBL 45, STA 500D + 9" IS CORRODED. REPAIRED PASSENGER CABIN SEAT TRACK AT BS 500 D+9 LBL 45 WITH 1EA SEAT TRACK SEGMENT AND 2 EA RADIUS FILLERS ALL INSTALLED IAW SRM 53-00-52-2R-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

FLOOR SUPPORT RAIL BETWEEN STA 847 AND 867 RBL 3 CORRODED. REMOVED AND REPLACED RAIL IAW SRM.

Part: SEAL — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

RIGHT HORIZ STAB TO FUSELAGE LOWER SLIDING SEAL CRACKED. REMOVED AND REPLACED SEAL IAW MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

FLOOR SUPPORT RAIL BETWEEN STA 847 AND 867 RBL 8 CORRODED. REMOVED AND REPLACED RAIL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

SEAT TRACK, LBL 24, STA 500D+ 9" IS CORRODED. REPAIRED SEAT TRACK IN PASSENGER CABIN, BS 500D+9", LBL 24 WITH 1 EA REPLACEMENT SEGMENT AND 2EA RADIUS FILLERS .125" ALL INSTALLED IAW SRM 53-00-52-2R-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

SEAT TRACK, LBL 45, STA 840, IS CORRODED. REPAIRED PASSENGER CABIN SEAT TRACK AT BS 840, LBL 45 WITH 1 EA SEAT TRACK SEGMENT, 1 STAINLESS STEEL SPICE AND 2 RADIUS FILLERS ALL INSTALLED IAW SRM 53-00-52-2R-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

FLOOR SUPPORT RAIL AT STA 727D +5 RBL 3 CORRODED. REMOVED AND REPLACED RAIL IAW EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO PIT DOOR THRESHOLD TO FLOORBEAM PLATE CORRODED ON BACK. REMOVED AND REPLACED PLATE IAW SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT BEAR STRAP CORRODED AT BS 947 BETWEEN STR 26L AND 27L AND AT BS 967. REPAIRED STRAP IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT SHEAR TIE AT BS 947 BETWEEN STR 26L AND 27L CORRODED. REMOVED AND REPLACED SHEAR TIE IAW BOEING AND SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

STA 348, STR 15L, FRAME ATTACH CLIP CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT SHEAR TIE AT BS 907 BETWEEN STRINGERS 26R AND 27R CORRODED. REMOVED AND REPLACED SHEAR TIE IAW MM.

Part: STRAP — CORRODED (CARGO BAY) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP CORRODED AT BS 727D. REMOVED AND REPLACED STRAP IAW SRM.

Part: PANEL — DELAMINATED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING PANEL 6526R DELAMINATED AT SLAT TRACK CUTOUT. FOUND EDGE BAND DELAMINATED ON RIGHT WING PANEL 6526R, BONDED EDGE BAND BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.

Part: PANEL — DELAMINATED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING PANEL 6541R CORNER CRUSHED. FOUND EDGE BAND DELAMINATED AND PULLED BACK ON PANEL 6541R, BONDED EDGE BAND BACK TO PANEL USING EA934NA/A60511 IAW SRM 57-41-01-2R-8.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AFT CARGO COMPARTMENT EQUIPMENT BAY BILGE BS 967 STRINGER 26L CORRODED AD DRIVEN. STR 27 WAS CORRODED 100% THROUGH MATERIAL, REMOVED DAMAGED AREA IN STR AT STA 967. INSTALLED NEW STR REPAIR IAW EA 121408 STEP 17 COMPLETE & SRM 53-00-03-1A-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN AFT CARGO COMPARTMENT FRAME AT BS 947 CORRODED BETWEEN STRINGERS 25R AND 26R. REMOVED AND REPLACED FRAME WITH NEW AT BS 947 51-12-32L-23R IAW SRM 51-40-02 AND BOEING DWG 65-46560.

Part: SKIN — CRACKED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING LEADING EDGE SKIN CRACKED AT UPPER EDGE OF NR 6 SLAT INBOARD AUXILIARY TRACK CUTOUT. REPAIRED DAMAGE AT RIGHT WING LEADING EDGE NR 6 SLAT AUXILARY TRACK CUTOUT IAW EA 1-A57-273 REV 1.

Part: PANEL — DELAMINATED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING PANEL 6541R CORNER DELAMINATED AT SLAT ACTUATOR CUTOUT. FOUND EDGE BAND ON RIGHT WING PANEL 6541R DELAMINATED AT SLAT ACTUATOR CUTOUT, BONDED EDGE BAND BACK TO PANEL USING EA934NA/A16511 IAW SRM 57-41-01-2R-8.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

CARGO COMPARTMENT FAIL SAFE CHORD AT BS 947 CORRODED. REMOVED AND REPLACED IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

AD DRIVEN SI # 11972-53. FORWARD ENTRY DOOR SURROUND, STATION 348, STRINGER 16L, FRAME ATTACH CLIP CRACKED AT RADIUS - MARKED. REPLACED FRAME ATTACH CLIP AT FWD ENTRY DOOR SURROUND STA 348 STR 16L WITH NEW CLIP IAW SRM 51-40-02 AND DWG 65-1768.

Part: PANEL — DELAMINATED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING PANEL 6531R DELAMINATED AT SLAT TRACK CUTOUTS. FOUND EDGE BAND DELAMINATED ON RIGHT WING PANEL 6531R, BONDED EDGE BAND BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.

Part: PANEL — DELAMINATED (LT WING) · airframe 57,567 hrs · 46,985 cycles

LEFT WING PANEL 6231L DELAMINATED AT CORNERS OF TRACK CUTOUTS. FOUND EDGE BAND DELAMINATED ON LEFT WING PANEL 6231C, BONDED EDGE BACK TO PANEL USING EA934/A60511 IAW SRM 57-41-01-2R-8.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

BS 312 LBL 12 PASSENGER CABIN FLOOR STRUCTURE SUPPORT STRAP CRACKED. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: PANEL — DELAMINATED (LT WING) · airframe 57,567 hrs · 46,985 cycles

LEFT WING PANEL 6223L DELAMINATED AT SLAT TRACK CUTOUT. FOUND EDGE BAND ON LEFT WING PANEL 6223L DISBONDED. BONDED EDGE BAND BACK TO PANEL USING EA934NA/A60511 IAW SRM 57-41-01-2R-8.

Part: LENS — BROKEN (CABIN) · airframe 57,567 hrs · 46,985 cycles

EMERGENCY EXIT LIGHT ON CENTER CEILING PNL BETWEEN STOWBINS 2ABC AND 2DEF EXIT LENS IS BROKEN. REPLACED EMERGENCY EXIT LIGHT LENS ON CENTER CEILING PANEL BETWEEN STOWBINS 2ABC AND 2DEF IAW AMM 33-51-11-402-007.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,567 hrs · 46,985 cycles

BS 500B LEFT SIDE FRAME CRACKED AT GENERATOR FEED THRU HOLE. REMOVED AND REPLACED FRAME IAW SRM.

Part: COVER — BROKEN (EMERGENCY EXIT) · airframe 57,567 hrs · 46,985 cycles

RIGHT EMERGENCY EXIT HATCH, PULL HANDLE COVER IS BROKEN. REMOVED & REPLACED RIGHT EMERGENCY EXIT PULL HANDLE PULL COVER IAW AMM 25-21-12-004-001 AND AMM 52-21-12-404-008.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 57,567 hrs · 46,985 cycles

LEFT HORIZONTAL STABILIZER FAIRING 9124L SLIDING SEAL CRACKED. REMOVED & REPLACED SLIDING SEAL ON LEFT HORIZONTAL STABILIZER FAIRING 9124L IAW BOEING 737 SRM 51-40-02-0G-0.

Part: SEAL DEPRESSOR — CRACKED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING FIXED TRAILING EDGE DEFLECTOR RIB UPPER SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED SEAL IAW SRM AND BOEING DRAWING.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 57,567 hrs · 46,985 cycles

RIGHT WING TRAILING EDGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND BOEING DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,461 hrs · 46,915 cycles

SKIN CRACKED AT BS 500A+9, STR 10R. REPAIRED SKIN IAW EA.

Part: DUCT — BROKEN (AC BAY) · airframe 57,053 hrs · 46,621 cycles

CREW REPORTED A HOT SMELL IN CABIN. FOUND DISTRIBUTION BAY DUCT BROKEN. REMOVED AND REPLACED DUCT PER MM.

Part: SIGN — UNSECURE (CABIN) · airframe 56,894 hrs · 46,507 cycles

MAIN CABIN DOOR LOWER EMERGENCY EXIT SIGN COVER FELL OFF. REMOVED AND REPLACED SIGN IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,200 hrs · 45,988 cycles

CREASE BEAM CHORD CRACKED BS 639, LBL 60. REMOVED AND REPLACED CHORD IAW SRM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 56,130 hrs · 45,940 cycles

RIGHT ELEVATOR CONTROL TAB FAIRING CRACKED. REMOVED AND REPLACED TAB PER DWG.

Part: FDU — FAULTY (COCKPIT) · airframe 55,517 hrs · 45,449 cycles

FIRE WARNING LIGHTS (2 EA.) CAME ON AT 1500' ON FINAL APPROACH WITH FIRE BELL AND NO OTHER INDICATIONS. STAYED ON AFTER LANDING THOUGH TAXI TO GATE. RELAMPED BOTH GLARE SHIELD FIRE WARNING LIGHTS & REPLACED FIRE DETECTION UNIT PER M/M.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 55,245 hrs · 45,251 cycles

LT ELEVATOR TAB IS DELAMINATED ON INBOARD TRAILING EDGE. REMOVED AND REPLACED TAB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 55,245 hrs · 45,251 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 55,967 hrs · 45,052 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,442 hrs · 44,656 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 683, STR 13R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 515A, LBL 4.87. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULEDA 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 0. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 500C, BETWEEN STR 27L TO STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 847 TO BS 867. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED. REPAIRED WEB PER ACO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE KEEL BEAM, OUTBOARD LWR CHORD CORRODED AT STA 721, LBL 6.30. REMOVED CORROSION AND REPAIRED KEEL BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED IN AFT BILGE AREA STA 767, BETWEEN STR 25L AND 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND CRACK AT LT SIDE PASSENGER CABIN STRINGER CLIP AT SPLICE STA 360, STR 4L. REPLACED SPLICE PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN BL 0 TO STR 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727E TO BS 727D, BETWEEN LBL 2 TO RBL 2. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON AFT PIT SHEAR TIE STA 767 BETWEEN STR S27L AND S27R. REPAIRED FRAME PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT FRAME FAIL-SAFE CHORD STA 767, BETWEEN STR 26L AND 26R. REMOVED AND REPLACED FAIL-SAFE CHORD PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 787, STR 8L. REPAIRED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, RBL 3-6. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 986.5. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB BETWEEN BS 787 TO BS 807 CORRODED. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,384 hrs · 43,052 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LENS — LOOSE (CABIN) · airframe 51,870 hrs · 42,679 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 51,870 hrs · 42,679 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,870 hrs · 42,679 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B END UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 51,870 hrs · 42,679 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,870 hrs · 42,679 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OVERHEAD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,435 hrs · 40,873 cycles

DURING SCHEDULED MV4 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 17. REMOVED AND REPLACED BULB PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 48,564 hrs · 40,232 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT KEEL BEAM PANEL CRACKED AT BS 700. REPAIRED KEEL BEAM PER EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 48,564 hrs · 40,232 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND EEPLS STRIPS DAMAGED. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 48,393 hrs · 40,111 cycles

LEFT FWD WINDSHIELD DELAMINATED. ARCED AND CRACKED DURING FLIGHT AT FL 340. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 48,227 hrs · 39,988 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS DELAMINATED FROM ROW 6 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: CAP — MISSING (COCKPIT) · airframe 48,085 hrs · 39,884 cycles

EMERGENCY EXIT KORRY LIGHT CAP MISSING. INSTALLED LIGHT CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,919 hrs · 39,757 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 2R TO STR 3R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 706, BETWEEN STR 2L TO STR 3L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT AT BS 304, WL 238. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,712 hrs · 38,850 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: GASPER FAN — FAULTY (A/C COMPT) · airframe 46,132 hrs · 38,434 cycles

UPON APPROACH INTO STL (APPROX 1000') FA'S CALLED, INFORMING CAPT OF ELECTRICAL SMELL. PILOT'S BEGAN SMELLING FAINT ELECTRICAL SMELL AT THAT TIME. NO LIGHTS OF INSTRUMENT FAILURES NOTED NOR POPPED CB'S. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 45,445 hrs · 37,943 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 45,445 hrs · 37,943 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,531 hrs · 37,288 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,531 hrs · 37,288 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,459 hrs · 37,237 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,735 hrs · 36,681 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 43,716 hrs · 36,667 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,716 hrs · 36,667 cycles

DURING SCHEDULED HC1 CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 43,716 hrs · 36,667 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,032 hrs · 36,143 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ROLLER — WORN (NLG W/W) · airframe 42,898 hrs · 36,040 cycles

MANUAL GEAR EXTENSION REQUIRED. ALL GEAR SAFE AND UNSAFE LIGHTS ILLUMINATED. FERRIED AIRCRAFT TO DAL FOR MAINTENANCE. FOUND LANDING CABLE OUT OF RIG, RIG CABLE PER MM. REMOVED AND REPLACED MANUAL RELEASE MECHANISM ROLLER ON NOSE GEAR PER MM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 42,071 hrs · 35,417 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 907) · airframe 42,071 hrs · 35,417 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 907, LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 40,793 hrs · 34,399 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 40,586 hrs · 34,216 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SPOILER DELAMINATED AT INBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: VENT — CLOGGED (HYD RESERVOIR) · airframe 39,100 hrs · 33,059 cycles

AIR TURN BACK/DECLARED EMERGENCY, DURING CLIMB F/A REPORTED A BURNING ODOR IN CABIN, THAT SEEMED TO BE GETTING STRONGER. NO VISIBLE SMOKE REPORTED, ODOR SEEMED TO BE IN FWD CABIN. MX FERRY TO PAE FOR REPAIRS. FOUND MAIN HYDRAULIC RESERVOIR PRESSURIZATION MODULE VENT CAPS CLOGGED. CLEANED 3 EACH VENT CAPS PER MM.

Part: STRINGER — CRACKED (BS 303 S16L) · airframe 69,450 hrs · 66,046 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16L CRACKED AT BS 303.9. REPAIRED STRINGER PER ER.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,143 hrs · 32,332 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — BROKEN (EMERGNECY LIGHT) · airframe 36,387 hrs · 30,963 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 35,467 hrs · 30,282 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HOOK — LOOSE (L2 DOOR SLIDE) · airframe 35,467 hrs · 30,282 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: HANDLE — FAULTY (MLG) · airframe 34,884 hrs · 29,804 cycles

DURING MLG EXTENTION, 3 GREEN & 3 RED LIGHTS ILLUMINATED. RECYCLED GEAR HANDLE, RED LIGHTS EXTINGUISHED. LUBED GEAR HANDLE PER MM. OPS CHECKED OK.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 34,606 hrs · 29,585 cycles

AIR TURNBACK, NR 1 ENGINE HAD UNCOMMANDED ACCELERATION. REMOVED AND REPLACED NR 1 ENGINE MEC & PMC PER MM.

Part: ENGINE — POWER LOSS (NR 1) · airframe 34,571 hrs · 29,558 cycles

NR 1 ENGINE WOULD NOT DEVELOP FULL POWER ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 34,551 hrs · 29,538 cycles

INFLIGHT SHUTDOWN/DIVERSION. NR 1 ENGINE FAILED FOR 5 SECONDS, THEN SURGED & RE-STARTED ITSELF. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUT-OFF VALVE, NR 1 ENGINE FUEL PUMP & NR 1 ENGINE MEC PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 794, RBL 14, WL 156. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON 2 EA SHEAR TIES AT BS 787, RBL 2 & RBL 11. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME WEB AT BS 847, RBL 20, WL 160. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767, RBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 907, RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, RBL 18. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DRAG ANGLE — CORRODED (VERTICAL STAB) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LT & RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727 C, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LT & RT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB BETWEEN BS 480 & BS 500, STR 17L. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON 2 EA SHEAR TIES AT BS 767, RBL 2 & RBL 18. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTINGS PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 188, WL 208, LT & RT SIDE. REMOVED AND REPLACED FRAMES PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED FITTINGS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 867 TO BS 887, LBL 67, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 360 & BS 787, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LBL 29 & RBL 29, WL 208. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND RT VERTICAL FIN T/E BEAM CRACKED 4 BELOW NR 1 RUDDER HINGE. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 727C TO BS 727E, RBL 67, WL 208. REPAIRED BEAM PER SRM.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, OUTBOARD MAIN TRACK, LOWER SURFACE CORRODED. REPAIRED TRACK PER OHM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR CREASE BEAM WEB CORRODED BETWEEN BS 312 TO BS 344, LBL 63, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA TYPICAL REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,665 hrs · 28,812 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 363, STR 17R. REPAIRED WEB PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 31,683 hrs · 27,238 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 31,683 hrs · 27,238 cycles

DURING SCHEDULED C4 CHECK, FOUND CENTER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (AFT SVC DOOR) · airframe 28,862 hrs · 25,043 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SKIN — DELAMINATED (NR 5 LE SLAT) · airframe 28,862 hrs · 25,043 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: SKIN — DELAMINATED (OUTBD TE FLAP) · airframe 28,862 hrs · 25,043 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OUTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED LT OUTBD T/E FLAP PER MM.

Part: SKIN — DELAMINATED (OUTBD T/E FLAP) · airframe 28,862 hrs · 25,043 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OUTBD T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED RT OUTBD T/E FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,762 hrs · 24,959 cycles

EMERGENCY FLASHLIGHT INOP IN FWD CABIN. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: FITTING — CORRODED (BOTH MLG) · airframe 25,562 hrs · 22,428 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT WALKING BEAMS PER MM.

Part: FITTING — CORRODED (BOTH MLG) · airframe 25,562 hrs · 22,428 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD STABILIZER BAR SUPPORT FITTINGS CORRODED. REPAIRED FITTINGS PER SWA EA'S.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 25,331 hrs · 22,222 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 25,272 hrs · 22,168 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,968 hrs · 21,100 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS PER SWA ACO.

Part: WINDOW — CRACKED (COCKPIT) · airframe 22,147 hrs · 19,624 cycles

R1 WINDOW BEGAN ARCING, WINDOW HEAT TURNED OFF, R1 CONTINUED TO PROPAGATE CRACKS IN THE OUTER PANE. PRESSURIZATION NORMAL. R&R R1 WINDOW PER MM.

Part: SLIDE — OUT OF POSITION (AFT DOORS) · airframe 21,704 hrs · 19,219 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED BOTH EVAC SLIDES PER MM.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 18,580 hrs · 16,584 cycles

EMERGENCY EXIT LIGHTS SWITCHES INOP. ADJUSTED STUD 6D1220 AND REPLACED AFT F/A EMERGENCY LIGHT SWITCH PER MM.

Part: MODULE — ERRATIC (CABIN) · airframe 18,060 hrs · 16,136 cycles

OVERHEAD EMERGENCY EXIT REAR AND SIDE LIGHTS ILLUMINATED AFTER ACFT SHUT DOWN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY MODULE PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,045 hrs · 15,287 cycles

DURING SCHEDULED HALF -D- CHECK, FOUND EEPLS WOULD ONLY TURN OFF ONLY WITH IN ARMED POSITION. R&R AFT BATTERY CHARGER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,040 hrs · 15,282 cycles

DURING SCHEDULED HALF D CHECK, FOUND THRU ULTRASONIC INSPECTION BS 178 CRACKED, LBL 5 AND RBL 5. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (DOOR FRAME) · airframe 17,040 hrs · 15,282 cycles

DURING SCHEDULED HALF D CHECK, FOUND STUB FRAME CRACKED AT FWD SERVICE DOOR FWD CUTOUT, STRINGER 17 RT. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,040 hrs · 15,282 cycles

DURING SCHEDULED HALF D CHECK, FOUND BS 787 FLOOR BEAM CRACKED, RBL 14. REPAIRED FLOOR BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,040 hrs · 15,282 cycles

DURING SCHEDULED HALF D CHECK, FOUND BS 986.5 FLOORBEAM CORRODED ON UPPER SURFACE, LBL 44. REPAIRED BEAM PER RA 1-A53-2037.

Part: ENGINE — MALFUNCTIONED (NR 2)

ABORTED TAKEOFF, NR 2 ENG FAILED TO ACCELERATE DURING TAKEOFF AT 30 KNOTS, MAX N1 IND 48 PERCENT. REMOVED AND REPLACED NR 2 ENG. SUSPECTED NR 3 BEARING OIL/AIR SEAL FAILURE.

Part: ENGINE — VIBRATION (NR 2)

DIVERSION, IN FLIGHT ENGINE SHUT DOWN, NR 2 ENGINE SHUT DOWN DURING FLIGHT DUE TO HIGH VIBRATION (4.5 TO 5.0). ENGINE WOULD NOT RESTART. DIVERTED TO BWI. REMOVED AND REPLACED NR 2 ENGINE PER MM. (SUSPECT NR 3 BRG OIL-AIR SEAL FAILURE).

Part: FRAME — CRACKED (BS 807)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED, BS 807, BETWEEN STRINGERS 27L-28L. REPAIRED FRAME PER SRM.

Part: BRACKET — LOOSE (CABIN)

FWD ENTRY DOOR EVACUATION SLIDE LEFT GIRT BAR HOLDER LOOSE. TIGHTENED HOLDER PER MM.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING LOOSE AT FWD END. RESECURED TRACK LIGHTING PER MM.

Part: COVER — MISSING (CABIN)

FLOOR TRACK LIGHTING COVER MISSING AT ACROSS OVERWING DOOR. REPLACED COVER PER MM.

Part: LIGHT — LOOSE (ROW 14 ABC)

DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS LOOSE AT ROW 14ABC. RESECURED AND OP CHECKED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY FOR RT OVERWING EMERGENCY LIGHT PER M/M. OP'S CHECK NORMAL. (P/N 61-0479-1) OFF, (P/N 61-0478-9) ON, (S/N WN0020) ON.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND CABIN EMERGENCY EXIT TRACK LIGHTS WIRES EXPOSED AND DAMAGED AT ROW 14. REPAIRED WIRES AND REPLACED TRACK COVER PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND 2 SECTIONS OF CABIN FLOOR TRACK LIGHTING INOP. REPAIRED WIRING PER BOEING M/M.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND FWD CABIN EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (FWD SERV DOOR)

DURING SCHEDULED C1 CHECK, FOUND FORWARD SERV DOOR OUTER SKIN CRACKED ABOVE SNUBBER AT L/E FORWARD SIDE. REPAIRED PER SWA RA 1-352-0252.

Part: BEARING — FAILED (NR 1 MLG WHEEL)

WHILE TAXIING, CREW NOTED A BRAKE DRAGGING SENSATION, AIRCRAFT RETURNED TO GATE. INSPECTED AND FOUND DAMAGE TO LEFT MAIN GEAR AXLE AND NUMBER 1 WHEEL AND BRAKE ASSEMBLY. REPLACED LEFT MAIN GEAR INNER CYLINDER, NUMBER 1 AND 2 WHEEL/BRAKE ASSEMBLIES AND ANTI-SKID TRANSDUCERS PER BOEING M/M.