N356SW

Part: SLIDE — LOOSE (L2 DOOR) · airframe 79,068 hrs · 66,405 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BUSTLE LOOSE. REPACKED SLIDE PER MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 79,067 hrs · 66,405 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BUSTLE LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,575 hrs · 66,019 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: SKIN — CRACKED (RT WING LE) · airframe 78,296 hrs · 65,810 cycles

RIGHT WING LEADING EDGE COMPOSITE SKIN JUST ABOVE NR 6 SLAT INBOARD AUX TRACK CURTAIN CRACKED. REPAIRED THE SKIN IAW EA AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,296 hrs · 65,810 cycles

LT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 2. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: ESCAPE ROPE — LOOSE (CABIN) · airframe 78,296 hrs · 65,810 cycles

RT EMERGENCY EXIT OPENING ROPE LOOSE. SECURED ROPE IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,250 hrs · 65,785 cycles

L1 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. R & R CHARGER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,250 hrs · 65,785 cycles

R1 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: BULB — FAULTY (NR 1 ENG TEMP) · airframe 77,986 hrs · 65,608 cycles

INFLIGHT SHUTDOWN, DECLARED EMERGENCY, NR 1 ENGINE OIL TEMP INDICATED TOP OF YELLOW ARC. COMPLIED WITH QRH PROCEDURE AND SHUT DOWN ENGINE. R & R THE NR 1 ENGINE OIL TEMPERATURE BULB PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,910 hrs · 65,556 cycles

R1 DOOR EMERGENCY EVAC SLIDE LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,910 hrs · 65,556 cycles

OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R PACK ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,487 hrs · 65,274 cycles

AFT LT SIDE EMER LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SPOILER — LEAKING (LT WING) · airframe 77,242 hrs · 65,116 cycles

LEFT WING NR 4 GND SPOILER OTBD LEAKED. R & R NR 4 GND SPOILER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,966 hrs · 64,910 cycles

FRAME CRACKED AT BS 328, STRINGER 21R. R & R FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,966 hrs · 64,910 cycles

FRAME ANGLE CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,906 hrs · 64,866 cycles

EMERGENCY LIGHT POSITION M1135 INOPERATIVE AT ROW 5. R & R BATTERY POWER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,906 hrs · 64,866 cycles

R2 DOOR EMER LIGHT M1133 INOPERATIVE. R & R BATTERY POWER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,720 hrs · 64,740 cycles

R1 DOOR SLIDE EXTERIOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 76,172 hrs · 64,354 cycles

R1 DOOR AFT EMER EXIT LIGHT INOPERATIVE. R & R FUSE IAW SIP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,946 hrs · 64,195 cycles

FOUND AFT EMER EXIT SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,728 hrs · 64,021 cycles

SKIN CRACKED AT BS 749.75, STRINGER 11R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,729 hrs · 64,021 cycles

FUSELAGE SKIN CRACKED AT BS 949.75, STRINGER 11L. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 74,959 hrs · 63,453 cycles

AFT CTR EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,944 hrs · 63,443 cycles

L2 DOOR EMER EXIT SIGN LIGHT INOPERATIVE. R & R BATTERY IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,944 hrs · 63,443 cycles

R2 DOOR EMER EXIT SIGN LIGHT INOPERATIVE. R & R BATTERY IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB CRACKED AT BS 520+8, BETWEEN STRINGER 22L - 24L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 1006, STRINGER 17A LT. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SKIN CRACKED AT BS 303.9, BETWEEN STRINGER 10L - 11L. R & R SKIN IAW SRM & DWG.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 74,944 hrs · 63,443 cycles

LEFT MLG LINK ASSEMBLY CORRODED. R & R LINK ASSEMBLY IAW SRM.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 74,944 hrs · 63,443 cycles

RIGHT MLG LINK ASSEMBLY CORRODED. R & R LINK ASSEMBLY IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

LEFT WING NR 3 FLAP TRACK CORRODED ON UPPER SURFACE. R & R NR 3 FLAP TRACK ASSEMBLY IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

LEFT WING CORRODED ON HOLES UPPER SURFACE THAT ATTACH FLAP TRACK TRANSMISSION NR 3 LT WING. R & R FLAP TRACK IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 380, BETWEEN STRINGER 26L - 18L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 867, STRINGER 27L. R & R TIE CLIP IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 74,944 hrs · 63,443 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 222. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 540, STRINGER 22L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT INBD EDGE LOWER SKIN. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 - 291.5, BETWEEN STRINGER 12R - STR 11R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 21R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, STRINGER 22L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 22R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 685, STRINGER 2R. R & R TIE CLIP IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 215.97+6.5. REPAIRED CHORD IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SPLICE CHANNEL CRACKED AT BS 360, STRINGER 7R. REPAIRED CHANNEL IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SPLICE ANGLE CRACKED AT BS 540 BETWEEN STRINGER 20L - 21L. R & R ANGLE IAW SRM & EA.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING NR 8 FAIRING TRACK INTERNAL SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CHORD SPLICE ANGLE CRACKED AT BS 540, BETWEEN STRINGER 21R - 22R. R & R ANGLE IAW SRM & EA.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT CARGO TRACK TIE DOWN CRACKED AT BS 747, RBL 13.80. REPAIRED TIE DOWN IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CRACKED AT BS 727E, STRINGER 25R. REPAIRED SUPPORT ZEE IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING INBD FORE FLAP DELAMINATED AT OTBD EDGE UPPER SKIN. REPAIRED FORE FLAP IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT FRAME DOUBLER CORRODED AT BS 787, BETWEEN STRINGER 26R - 27R. R & R DOUBLER IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,944 hrs · 63,443 cycles

LEFT WING NR 2 SLAT OTBD EDGE UPPER SURFACE DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,944 hrs · 63,443 cycles

LEFT WING OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,944 hrs · 63,443 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT OTBD EDGE. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SKIN CRACKED AT BS 727D+14, BETWEEN BL 0 TO LBL 1. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

LEFT FRAME WEB CRACKED AT BS 235.8, BETWEEN WL 220 - WL 230. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53.50. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FUSELAGE FRAME CRACKED AT STATION 947.5, STRINGER 19R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 1006, STRINGER 21L+5. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 380, STRINGER 23L. REPAIRED FRAME IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

OUTBOARD CHORD CRACKED AT BS 188, LT SIDE AT LEVEL OF THE FLOOR FLIGHT CREW COMPARTMENT. REPAIRED CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19R. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT CLIP CRACKED AT BS 947.5, STRINGER 22R. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FUSELAGE FRAME CRACKED AT STATION 1006, STRINGER 21L. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

OUTBOARD CHORD CRACKED AT BS 188 RT SIDE AT LEVEL OF FLOOR FLIGHT CREW COMPARTMENT. REPAIRED CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 21R - 22RL. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

ANGLE CRACKED BETWEEN BS 927 - 947.5, BETWEEN STRINGER 14R - 15R. R & R ANGLE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD CARGO COMPARTMENT CLIP CRACKED AT BS 540, BETWEEN STRINGER 28R - 28L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD SERVICE DOOR LOWER HINGE CUT OUT CRACKED AT BS 291.5, STRINGER 13R. REPAIRED CUT OUT IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 22R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 787, STRINGER 22R. R & R TIE CLIP IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

LEFT WING INBD FLAP, INBD FLAP TRACK AFT ATTACHMENT, OTBD LUG CORRODED. REPAIRED FLAP TRACK IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

SUPPORT BRACKET CRACKED AT BS 380, STRINGER 20L. R & R BRACKET IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

STRINGER SPLICE CRACKED AT BS 727, STRINGER 23R. R & R SPLICE IAW SRM & EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 420 - 440, STRINGER 17L. REPAIRED WEB IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB CRACKED BETWEEN BS 787 - 807, RBL 17.5. R & R WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 360, STRINGER 14R. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB CORRODED BETWEEN BS 460 - 480, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 16R. R & R TIE CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB CRACKED BETWEEN BS 188 - 196.5, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 500A, STRINGER 16R. R & R TIE CLIP IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CHANNEL CRACKED BETWEEN BS 294.5 - 312, BETWEEN STRINGER 27L - 26L. R & R CHANNEL IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CLIP CRACKED AT BS 807, STRINGER 25R. R & R CLIP IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING INBD FLAP, INBD TRACK AFT ATTACHMENT LUG CORRODED. REPAIRED FLAP TRACK IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT WEB CRACKED AT BS 847, BETWEEN STRINGER 24R - 25R. R & R WEB IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB SHEAR TIE CRACKED BETWEEN BS 188 - 196.5, STRINGER 17L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 380, STRINGER 23L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

VERTICAL STIFFENER ANGLE CRACKED BS 727, BETWEEN LBL 45 TO LBL 52. R & R ANGLE IAW SRM & DWG.

Part: STANCHION — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

STANCHION CRACKED AT BS 294.5+5, STRINGER 27R. R & R STANCHION IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT STRINGER CHANNEL CRACKED AT BS 727, STRINGER 23L. R & R CHANNEL IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT WEB CRACKED AT BS 794.3, BETWEEN STRINGER 24R - 25R. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 74,944 hrs · 63,443 cycles

RIGHT EMER LIGHT ASSEMBLY ON AFT GALLEY AREA CUT OUT BROKEN. R & R LIGHT ASSEMBLY IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,978 hrs · 63,466 cycles

FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 21R - 22R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING TE AREA ANGLE CRACKED AT LEVEL WBL 71.24. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FLOORBEAM WEB CRACKED AT BS 639+1.5, RBL 45.5. REPAIRED WEB IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 74,944 hrs · 63,443 cycles

LEFT WING NR 2 SLAT INBD EDGE UPPER SURFACE DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WEB CRACKED BETWEEN BS 616 - 639, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

WING TO BODY FAIRING AREA TEE CHORD CRACKED AT BS 727, BETWEEN STRINGER 22R TO 26R. R & R TEE CHORD IAW SRM & DWG.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT CARGO COMPARTMENT SUPPORT CHANNEL CORRODED BETWEEN BS 727D - 727E, BETWEEN STRINGER 27L - 27R. REPAIRED CHANNEL IAW EA.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 74,944 hrs · 63,443 cycles

RIGHT WING NR 8 SPOILER UPPER EXTERNAL SURFACE DELAMINATED. R & R SPOILER IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, STRINGER 23L. REPAIRED WEB IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

STRAP CRACKED BETWEEN BS 294.5+13 TO 360+5, RBL 46. R & R STRAP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

STRAP CRACKED BETWEEN BS 294.5+13 - 344+5, RBL 34. R & R STRAP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

STRAP CRACKED BETWEEN BS 294.5+13 TO 344+5, BL 0. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD AREA OF WING TO BODY FAIRING ANGLE CRACKED AT BS 540, STRINGER 24L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

RIGHT MAIN WW CUT OUT SUPPORT ANGLE CRACKED AT BS 663.75+17. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 20L - 21L. REPAIRED FRAME IAW EA.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

LEFT DRAG ANGLE INTERNAL FWD AREA OF WING TO BODY FAIRING BETWEEN BS 520 - 540 CRACKED. REPAIRED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706+1.5, LBL 24.8. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,978 hrs · 63,466 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 19L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

LEFT CREASE BEAM INNER CHORD CRACKED AT BS 616, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706+1.5, RBL 24.8.ON BS 706 + 4.75. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (BS 727) · airframe 74,948 hrs · 63,445 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT AT FWD LOWER FASTENER HOLE. REPAIRED FRAME IAW EA & EO.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 74,944 hrs · 63,443 cycles

L1 DOOR AFT LOWER CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

FORWARD LOWER FASTENER HOLE OTBD CHORD CRACKED AT BS 727, STRINGER 18A RT. R & R CHORD IAW EA.

Part: DOOR — CRACKED (FUSELAGE) · airframe 74,944 hrs · 63,443 cycles

GROUND AIR CONDITIONING ACCESS DOOR CRACKED AT LOWER OTBD FUSELAGE. R & R DOOR IAW DWG & SRM.

Part: SPAR — CRACKED (LT WING) · airframe 74,948 hrs · 63,443 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED AT RSS 222 MLG AFT SUPPORT FITTING COMMON AREA. REPAIRED CHORD IAW EO & EA.

Part: SPAR — CRACKED (RT WING) · airframe 74,948 hrs · 63,445 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED, FASTENER HOLE LOCATED AT RSS 215.97+6.5. REPAIRED CHORD IAW EO & EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,532 hrs · 63,136 cycles

AFT GALLEY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: WIRE — DAMAGED (CABIN) · airframe 74,510 hrs · 63,121 cycles

AFT GALLEY OVERHEAD EMER LIGHTING WIRE DAMAGED. REPAIRED WIRE IAW WDM.

Part: WIRE — DAMAGED (CABIN) · airframe 74,510 hrs · 63,121 cycles

AFT GALLEY OVERHEAD EMER LIGHT WIRE DAMAGED AT BS 960. REPAIRED WIRE IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 74,510 hrs · 63,121 cycles

AFT GALLEY OVERHEAD EMER LIGHT WIRE DAMAGED AT BS 975. REPAIRED WIRE IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 74,510 hrs · 63,121 cycles

AFT GALLEY OVERHEAD EMER LIGHT WIRE DAMAGED AT -1' FROM CONNECTOR D2966. REPAIRED WIRE IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 74,510 hrs · 63,121 cycles

AFT GALLEY OVERHEAD EMER LIGHTING WIRE DAMAGED AT BULLNOSE EXIT SIGN. REPAIRED WIRE IAW WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,510 hrs · 63,121 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (LT WING) · airframe 73,842 hrs · 62,675 cycles

LEFT WING UPPER SKIN CORRODED AT STATION 198 TE. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,669 hrs · 62,537 cycles

RIGHT WING OTBD AFT FLAP INBD CORNER EDGE DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 73,506 hrs · 62,424 cycles

LEFT WING NR 4 GND SPOILER OTBD ATTACH LUG BROKEN. R & R SPOILER IAW MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 73,409 hrs · 62,342 cycles

AFT CARGO DOOR LOWER FRAME CRACKED. R & R DOOR IAW AMM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 73,409 hrs · 62,342 cycles

RUDDER LE STATION 131, CTR BALANCE WEIGHT CORRODED BETWEEN MOUNT FLANGE & WEIGHT. R & R RUDDER IAW AMM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 73,026 hrs · 62,057 cycles

AFT CABIN EXIT DOOR EMER LIGHTS FAULTY. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 72,821 hrs · 61,904 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — DETACHED (CABIN) · airframe 72,806 hrs · 61,888 cycles

LEFT OVERWING EXIT LIGHT LENS DETACHED. INSTALLED LENS IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 72,190 hrs · 61,471 cycles

INTERCOSTAL ATTACH ANGLE CRACKED AT BS 348, STRINGER 15L. REPAIRED ANGLE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,190 hrs · 61,471 cycles

SKIN CRACKED AT THE TWO HOLES AT THE 2ND STOP FITTING FROM BOTTOM OF BS 348.2, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,190 hrs · 61,471 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 972 TO BS 973, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,190 hrs · 61,471 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 972 TO BS 973, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 72,190 hrs · 61,471 cycles

LEFT WING NO STEP ANGLE CRACKED AT THE AFT END. R & R ANGLE IAW DWG & SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 72,190 hrs · 61,471 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR BETWEEN STAB STATION 92.7 & 101.9. REPAIRED SKIN IAW EA.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 72,095 hrs · 61,405 cycles

LEFT WING NR 1 SPOILER HYD ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 71,642 hrs · 61,086 cycles

R1 DOOR AFT LOWER FRAME GUSSET CRACKED AT LOWER AFT CORNER STOP FITTING. R & R DOOR IAW AMM.

Part: ANGLE — CRACKED (LT AILERON) · airframe 71,642 hrs · 61,086 cycles

LT WING AILERON COVE PANEL AT RSS 533 LOWER ANGLE CRACKED. R & R ANGLE IAW DRAWING.

Part: ANGLE — CRACKED (LT AILERON) · airframe 71,642 hrs · 61,086 cycles

LT WING AILERON COVE PANEL AT RSS 507 LOWER ANGLE CRACKED. R & R ANGLE IAW DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,979 hrs · 59,813 cycles

INTERCOSTAL CRACKED AT PYLON PANEL 5857R AFT UPPER EDGE AT HILOK FASTENER. R&R INTERCOSTAL IAW SRM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 69,702 hrs · 59,618 cycles

RIGHT WING NR 6 SPOILER ACTUATOR LEAKED. R & R NR 6 SPOILER IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 69,159 hrs · 59,229 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,159 hrs · 59,229 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CHANNEL ASSY CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.7. REMOVED AND REPLACED CHANNEL ASSY IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

TIE CLIP LOCATED CRACKED ATSTA 440, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT BRACKET — CRACKED (R2 DOOR) · airframe 69,159 hrs · 59,229 cycles

R2 DOOR EMERGENCY EVAC SLIDE SUPPORT BRACKETS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

FRAME CRACKED AT BS 360, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 69,159 hrs · 59,229 cycles

AFT CARGO COMPARTMENT DOOR SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SILL — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SILL WEB CRACKED AT STA 328+7", STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CHANNEL CRACKED AT STA 540, BL 0 TO LBL 24.7. REMOVED AND REPLACED CHANNEL PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SUPPORT ZEE ANGLE AT STA 847 AND BETWEEN STR 24L AND STR 25L CRACKED. REMOVED AND REPLACED ZEE ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

STRINGER CLIP CRACKED AT STA 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON TIE CLIP AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON TIE CLIP AT BS 380 AT LEVEL STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON TIE CLIP AT BS 380 AT LEVEL STR 22L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SKIN CRACKED AT BS 958.5, BETWEEN STRINGER 16L AND STRINGER 17L. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

WEB CRACKED BETWEEN BS 927 TO BS 947.5+5, BETWEEN STR 10R TO STR 15R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (NACELLE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON RUBSTRIP ON NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1. REMOVED AND REPLACED RUBSTRIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

STRINGER SPLICE CRACKED AT STA 348.2 TO STA 367, STR 15L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 69,159 hrs · 59,229 cycles

CRACK ON ANGLE LOCATED ON AREA OF RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9226R. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON STRAP BETWEEN BS 303 TO BS 344+5, LBL 12.5. REMOVED AND REPLACED STRAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SUPPORT CLIP CRACKED AT STA 294.5, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

ANGLE ATTACH CLIP AT STA 348.2, STR 15L CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON WEB BETWEEN BS 344+8.5 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SUPPORT ANGLE AT STA 312, STR 21L E/E COMPARTMENT CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: DUCT — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

DUCT ASSY CRACKED BETWEEN BS 294.5 TO BS 312, BETWEEN STR 26R TO STR 26L. REPAIRED DUCT ASSY IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,159 hrs · 59,229 cycles

RIGHT WING INBOARD FIXED LEADING EDGE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 69,159 hrs · 59,229 cycles

RIGHT WING LEADING EDGE SKIN CRACKED AT FS 542. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SHEAR TIE CORRODED AT STA 344 BETWEEN STR 26R & STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON WEB BETWEEN BS 328 TO BS 344, LBL 47. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 69,159 hrs · 59,229 cycles

RIGHT WING INBD FIXED CRACKED AT L/E ANGLE AT STA 190. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

ANGLE CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SUPPORT ANGLE CRACKED AT BS 312+9, STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

UPPER CHORD OF FLOORBEAM AT BS 312, BETWEEN BL 0 AND RBL 28 CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

STRINGER SPLICE CRACKED AT STA 360 TO STA 367, STR 15L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SUPPORT ANGLE CRACKED AT STA 328+9", STR 21L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

STRINGER CLIP CRACKED AT STA 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

STRINGER CLIP CRACKED AT STA 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

FUSELAGE SKIN CRACKED AT STA 947.5+ 14, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

FUSELAGE SKIN CRACKED AT STA 360, STR 2R. REPAIRED SKIN PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

TIE CLIP CRACKED AT STA 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON CLIP LOCATED ON BS 380 AND STR 26L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: RUB STRIP — CRACKED (NR 2 PYLON) · airframe 69,159 hrs · 59,229 cycles

CRACK ON RUBSTRIP LOCATED ON STRUT ACCESS PANEL 58720R ENGINE NR 2. REMOVED AND REPLACED RUBSTRIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON WEB LOCATED BETWEEN BS 500 TO BS 500A AND STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 69,159 hrs · 59,229 cycles

LEFT WING T/E ANGLE CRACKED AT RS STA 535. REMOVED AND REPLACED ANGLE PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

TIE CLIP CRACKED AT BS 400, STR 26L. REMOVED AND REPLACED CLIP IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 69,159 hrs · 59,229 cycles

CRACK ON SUPPORT ANGLE LOCATED WBL 204.40 TRAILING EDGE AREA OUTBOARD SIDE FLAP TRACK FAIRING NR 6 RIGHT WING. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

CRACK ON ANGLE LOCATED BETWEEN BS 927 TO BS 947.5 AND BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,159 hrs · 59,229 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+9, LBL 42.5. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,159 hrs · 59,229 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+1, LBL 39.5. REMOVED AND REPLACED WEB IAW SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 69,159 hrs · 59,229 cycles

FORWARD CARGO DOOR SKIN CRACKED BETWEEN BS 415+7" TO BS 437+2". REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,159 hrs · 59,229 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75, LBL 39. REMOVED AND REPLACED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,159 hrs · 59,229 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+9, LBL 40. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,159 hrs · 59,229 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+9, LBL 41.5. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

ANGLE CRACKED AT BS 380 TO BS 400, BL 0, FWD CARGO COMPARTMENT. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

SKIN CRACKED AT BS 958.5 BETWEEN STRINGER 16L AND STR 17L. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, BBL 0.07. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,159 hrs · 59,229 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, BBL 0.07. REPAIRED CHORD IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 69,159 hrs · 59,229 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW DWG AND AMM.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 69,159 hrs · 59,229 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING DAMAGED. REMOVED AND REPLACED FITTING IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,129 hrs · 59,211 cycles

FORWARD FUSELAGE CROWN SKIN HAS 2.75" SURFACE CRACK AT STA 440 + 3.0" BELOW STR 2R. INSTALLED INTERIM REPAIR PER EA 1-353-21761.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,041 hrs · 59,150 cycles

VERY AFT O/H EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT LEFT EMERGENCY EXIT BATT CHARGER & BATT. OPS CHECK GOOD PER MM

Part: FAN — FAULTY (AC BAY) · airframe 68,856 hrs · 59,017 cycles

DIVERSION -- REACHING CRUISE, F/A'S REPORTED HAZY SMOKE & FIRE SMELL IN CABIN. IMMEDIATELY TURNED RECIRC FAN OFF. NO FIRE INDICATIONS. LANDED OVERWEIGHT 117,500 LBS SMOOTH GENTLE TOUCHDOWN. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: ACTUATOR — LEAKING (NR 6 SPOILER) · airframe 68,483 hrs · 58,758 cycles

NR 6 SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR PER M/M LEAK CHECK GOOD. RAR # 37974 P/N OFF 65-44561-14 P/N ON 65-44561-15 S/N OFF 3193A S/N ON 10380

Part: COVER — LOOSE (CABIN) · airframe 67,043 hrs · 57,657 cycles

FWD ENTRY LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW M/M.

Part: ENGINE — POWER LOSS (RIGHT) · airframe 66,598 hrs · 57,315 cycles

INFLIGHT SHUT DOWN, AIR TURNBACK, DECLARED EMERGENCY. NR 2 ENGINE ROLLED BACK TO SUB IDLE. DURING DESCENT NO ABNORMAL INDICATIONS. RESTATED NR 2 ENG. COMPLIED WITH NR 2 ENGINE INSPECTION. NO DEFECT FOUND. OPS CHECKED GOOD. REMOVED AND REPLACED FUEL SUPPLY LINE AND SPAR VALVE AS PRECAUTION PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 66,083 hrs · 56,935 cycles

RT WING L/E SKIN CRACKED O/B OF PYLON ABOVE MID SPAR FITTING. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,812 hrs · 55,961 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,915 hrs · 55,285 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,915 hrs · 55,285 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT SERVICE EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, KEEL BEAM WEB CRACKED BS 626, LBL 6.50. REPAIRED BEAM PER EO.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, LT WING O/B AFT FLAP T/E DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT LBL 24.5 BS 727B. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, SKIN CRACKED AT BS 430+4, STR 1L. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FWD GALLEY EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, ANGLE CRACKED BETWEEN BS380 AND BS400, LB 0. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 727D BETWEEN S-25L AND S-26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 747, BETWEEN STR 26R TOP STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 727D BETWEEN S-26R AND S-27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CORROSION ON FRAME, LOCATED BS 827 BETWEEN STR 27L TO STR 27R IN AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CORROSION ON FRAME LOCATED AT BS 807, BETWEEN STR 27R TO STR 27L AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACKED STRINGER CLIP LOCATED AT BS 747 AND S-18L AFT CARGO COMPARTMENT. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FLOOR BEAM CORRODED AT LOWER FLANGE LOCATED ON BS 986.5 AND BETWEEN RBL 27 TO RBL 46.5 UNDER FLOOR OF AFT GALLEY. R&R "T" CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACK AT CROWN SKIN BS 420+3" LT SIDE OF STR 1. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACKED ON LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND FASTENER LOCATED AT RBL 45.5 AND BS 727B. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACK AT CROWN SKIN BS 440+2" LT SIDE OF STR 1. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FOREFLAP) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACKED ON UPPER SKIN OF OUTBOARD FORE FLAP AND WBL 353.5 LT WING. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK FOUND, CRACKED ON LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND FASTENER HOLE LOCATED AT RBL 24.5 AND BS 727B IN PAX CABIN. REPAIRED BEAM PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,339 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT TIE CLIP CRACKED, BS 727B AND S-25L. REPAIRED CHANNEL PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,339 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT TIE CLIP CRACKED, BS 727D AND S-25L. REPAIRED CHANNEL PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727+5, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,339 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPARTMENT TIE CLIP CRACKED BS 400 AND 27L. REPAIRED CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR INNER CHORD LOWER SILL CORRODED. REMOVED AND REPLACED SILL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,339 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND CORROSION ON CHANNEL IN AFT CARGO COMPARTMENT, BS 727, RBL 8.10. REPAIRED CHANNEL PER DOC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,669 hrs · 55,092 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,917 hrs · 54,532 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 520, STR 8L. REPAIRED SKIN PER EA.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 62,974 hrs · 54,575 cycles

DECLARED EMERGENCY. AFT COFFEE MAKER STARTED SMOKING, SHUTOFF GALLEY POWER. REMOVED AND REPLACED AFT COFFEE MAKER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,539 hrs · 54,243 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,539 hrs · 54,243 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,539 hrs · 54,243 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED CHANNEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,006 hrs · 53,850 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 11L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,006 hrs · 53,850 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 11R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 62,050 hrs · 53,878 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,988 hrs · 53,836 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 61,853 hrs · 53,727 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 61,146 hrs · 53,185 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 23. RELAMPED PER MM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WHEEL WELL BULKHEAD WEB FWD AND ABOVE SPOILER CONTROL VALVE CRACKED. REPAIRED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,068 hrs · 53,125 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — WORN (CABIN) · airframe 60,490 hrs · 52,663 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS WORN AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: PIN — FAULTY (FIRE LOOP) · airframe 59,977 hrs · 52,282 cycles

MOMENTARY FIRE WARN LIGHT/BELL FOLLOWED ABOUT 15MIN. LATER WITH FIRE BELLS. SYSTEM CHECK NORMAL, NO OTHER INDICATIONS. ALL OCCURRED ABOUT 45 MINS INTO FLT. NO OTHER INDICATIONS. REMOVED AND REPLACED APU FIRE LOOP PIN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,532 hrs · 51,942 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER ER.

Part: LENS — LOOSE (CABIN) · airframe 59,031 hrs · 51,577 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,896 hrs · 51,479 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT ASSY INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 58,896 hrs · 51,479 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,380 hrs · 51,079 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED AT O/B EDGE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,352 hrs · 51,062 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BULBS INOP. RELAMPED PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 58,109 hrs · 50,891 cycles

LT EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 58,109 hrs · 50,891 cycles

LT EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,671 hrs · 49,873 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF POSITION. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,601 hrs · 49,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AFT ENTRY EEPLS LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,601 hrs · 49,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT ENTRY EEPLS LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,350 hrs · 48,930 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. R&R LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,350 hrs · 48,930 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,350 hrs · 48,930 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 FLIGHT SPOILER DELAMINATED AT INBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 807, STR 23L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED 20Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — WORN (RUDDER) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED 20Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 400. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,297 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 520 S10L) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 379 S15R) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 379. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S4L) · airframe 55,278 hrs · 48,874 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 767 TO BS 787, RBL 65, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 311. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 7L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULE SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULE SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STIFFENER — CRACKED (LT WING) · airframe 55,296 hrs · 48,891 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING VERTICAL STIFFENER CRACKED AT RIB WBL 542. REPAIRED STIFFENER PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,856 hrs · 48,538 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 25L. REPAIRED SKIN PER SRM.

Part: TRANSMISSION — LOOSE (T/E FLAP) · airframe 54,402 hrs · 48,204 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 FLAP TRANSMISSION JACK SCREW LOOSE AT TRANSMISSION. REMOVED AND REPLACED TRANSMISSION AND JACK SCREW PER MM.

Part: SKIN — DELAMINATED (RT FORE FLAP) · airframe 54,391 hrs · 48,195 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 518D S12R) · airframe 54,357 hrs · 48,167 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 518D S12R) · airframe 54,352 hrs · 48,163 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 374 S4L) · airframe 54,352 hrs · 48,163 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, S4L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 54,352 hrs · 48,163 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 729E S22L) · airframe 54,269 hrs · 48,095 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727E S23-24L) · airframe 54,219 hrs · 48,055 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E + 2.5 TO BS 727E + 17, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 727D S22-24L) · airframe 54,219 hrs · 48,055 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D + 16 TO BS 727D + 17, BETWEEN STR 22L TO STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 727E S22-23L) · airframe 54,219 hrs · 48,055 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E + 2 TO BS 727E + 3, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 727E S22R) · airframe 54,219 hrs · 48,055 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 2, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727E S18L) · airframe 54,219 hrs · 48,055 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 13, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,194 hrs · 48,038 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,906 hrs · 47,827 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,697 hrs · 47,654 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,627 hrs · 47,604 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (R1 DOOR) · airframe 53,427 hrs · 47,444 cycles

DURING SCHEDULED MV1 CHECK, R1 DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LANDING GEAR — UNLOCKED · airframe 53,424 hrs · 47,443 cycles

DIVERSION / DECLARED EMERGENCY. AFTER TAKEOFF FROM SMF, GEAR HANDLE WOULD NOT MOVE FROM UP TO OFF POSITION. DIVERTED INTO OAK. FOLLOWED QRH AND MANUALLY LOWERED GEAR. GEAR CONFIRMED DOWN AND LOCKED BY THREE GREEN LIGHTS, VISUAL THROUGH VIEWER, AND TOWER FLY-BY. UPON LANDING, THE NLG RETRACTED. DISCOVERED RIGHT MLG WAS ALSO UNLOCKED.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,559 hrs · 46,796 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,235 hrs · 46,555 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,504 hrs · 45,981 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 178 S20R) · airframe 51,368 hrs · 45,873 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, STR 20R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,018 hrs · 44,812 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 517D TO BS 518D, STR 12L TO STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E COOLING DUCT EXHAUST PORT, BS 378.5, LBL 2. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 20R & STR 21R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 947, LBL 4. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, RBL 36. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 947, RBL 1. REPAIRED FLOORBEAM PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT LOWER INBD FLANGE, BS 616, STR 17L. REPAIRED BELTFRAME PER TRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. R&R CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,542 hrs · 44,448 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 730B, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 49,271 hrs · 44,228 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 49,077 hrs · 44,086 cycles

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

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 49,077 hrs · 44,086 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD UPPER T/E SKIN DELAMINATED. REPAIRED SLAT PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 49,077 hrs · 44,086 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,077 hrs · 44,086 cycles

DURING SCHEDULED C4 CHECK, FOUND RH HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STA 120.30. REPAIRED HORIZONTAL STAB SKIN PER SRM.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 49,077 hrs · 44,086 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (BS 732E) · airframe 49,077 hrs · 44,086 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732E, STR 25L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 48,163 hrs · 43,352 cycles

PHOTOLUMINESCENT STRIP COVER MISSING BETWEEN ROW 5 TO ROW 7. REMOVED AND REPLACED STRIP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 48,119 hrs · 43,317 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,129 hrs · 42,514 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,129 hrs · 42,514 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6L. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM..

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 47,129 hrs · 42,514 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: TIRE — SEPARATED (RT MLG WHEEL) · airframe 46,601 hrs · 42,102 cycles

DURING T/O, NR 4 MAIN TIRE TREAD SEPARATED. FOUND RT WING INBOARD AFT T/E FLAP, MIDFLAP, FOREFLAP & GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 4 MLG TIRE/WHEEL ASSY. MX FERRY TO PHX, RERMOVED AND REPLACED RT FOREFLAP, AFT FLAP & GROUND SPOILER ASSY PER MM. REPAIRED RT MIDFLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,265 hrs · 41,832 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 25L. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,562 hrs · 41,279 cycles

DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,573 hrs · 41,288 cycles

EEPLS STRIP AT ROWS 6 ABC AND 7 ABC, LOOSE. SECURED EEPLS STRIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,573 hrs · 41,288 cycles

EMERGENCY EXIT LIGHT AT FWD F/A'S SEAT, LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,972 hrs · 39,992 cycles

DURING SCHEDULED SERVICE, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,545 hrs · 39,663 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 42,704 hrs · 38,977 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L2/R2 DOORS) · airframe 42,704 hrs · 38,977 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES PER MM.

Part: CABLE — BROKEN (RT WING) · airframe 41,658 hrs · 38,123 cycles

DURING CLIMBOUT NOTICED UNUSUAL VIBRATION. VIBRATION DECREASED WHEN AIRSPEED LESS THAN 250 KNOTS. FOUND MIDFLAP BOOM CABLE BROKEN. REMOVED AND REPLACED BOOM CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,503 hrs · 38,023 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,530 hrs · 38,023 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FLOORBEAM CRACKED AT BS 747, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 41,442 hrs · 37,956 cycles

ON FINAL LOSE OF RT HYDRAULIC QUANTITY AND PRESSURE. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR PER MM. LK CHECK OK PER MM.

Part: DOOR SEAL — DAMAGED (CARGO DOOR) · airframe 40,144 hrs · 36,880 cycles

AIR TURNBACK, UNABLE TO PRESSURIZE CABIN. REMOVED AND REPLACED AFT CARGO DOOR SEAL AND LOWER OVER PRESSURE SAFETY VALVE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 39,864 hrs · 36,649 cycles

LEFT FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED LT FWD EMERGENCY FLASHLIGHT BATTERY PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 39,315 hrs · 36,204 cycles

EMERGENCY EXIT LIGHT LENS FELL OFF AT LT MID CABIN. REINSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,854 hrs · 35,858 cycles

L1 DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED THE L1 ESCAPE SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,816 hrs · 35,843 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR LOWER FWD FUSELAGE SKIN CUT OUT CRACKED .750 INCHES LONG. REPAIRED SKIN PER SWA EA AND SRM.

Part: FIRE LOOP — FAULTY (APU BAY) · airframe 38,590 hrs · 35,642 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB APU FIRE WARNING LIGHT ILLUMINATED AND FIRE ALARM SOUNDED, DISCHARGED APU FIRE BOTTLE. APU WAS NOT RUNNING. REMOVED AND REPLACED APU FIRE DETECTION HARNESS AND FIRE BOTTLE PER MM.

Part: SKIN — CRACKED (WINDOW POST) · airframe 36,973 hrs · 34,346 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 COCKPIT WINDOW POST SKIN CRACKED AT UPPER LT CORNER. REPAIRED WINDOW POST SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 36,459 hrs · 33,948 cycles

DURING SCHEDULED RON, FOUND LT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED LT ELEVATOR TAB INBD HINGE BUSHING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 380, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, STR'S 19R & 19L R&R STR CLIPS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17 & WL 230. REPAIRED WEB PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 39 & WL 208. REPAIRED FLOORBEAM PER SRM & SWA RA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND BEAR STRAP CORRODED AT BS 844, RBL 15 TO RBL 18, WL157. REPAIRED BEAR STRAP PER BFG ER.

Part: FRAME — CRACKED (FWD CARGO DOOR) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUT OUT CRACKED AT BS 492, RBL 37, WL 160. REPAIRED FRAME PER BOEING SERVICE BULLETIN.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMED CRACKED BETWEEN STR 8L & 9L, BS 787, BS 827 & BS 867, BETWEEN STR 8R & 9R, BS 747. REPAIRED FRAMES PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 294, RBL 16 WL 208. REPAIRED FLOORBEAMS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64 & WL 201. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, RBL 68 & WL 208. REPAIRED WEB PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 706, STRINGER 11L. REPAIRED TIE CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 294, RBL 55 & WL 208, BS 440 BETWEEN STRINGERS 8R & 9R, BS 480 BETEWWN STRINGERS 8L & 9L. REPAIRED FRAMES PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 737.5, LBL 12 & WL 157. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AFT CARGO, BS 767, WL 157, RBL 7.5 TO LBL 17. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM E&E COMP, AT BS 312, WL 208, LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 8L HAS SEVERAL CRACKS AT BS 500D TO BS 524. REPAIRED STR PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO AT BS 727D TO BS 847, WL 157, LBL 7.5 TO RBL 2.5. REPAIRED FLOORBEAMS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, WL 148 & RBL6. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8-9 LH.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, STR 6R & BS 559, STR 11R. REPAIRED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8-9R, BS 827, BS 867 & BS 727D. REPAIRED FRAMES PER BFG ER.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 33,430 hrs · 31,474 cycles

DURING SCHEDULED D-CHECK, FOUND STR TIE CLIPS CRACKED AT BS 663, STR 10R & 10L, BS 520, STR 8L. Removed and replaced TIE CLIPS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,834 hrs · 30,111 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 5 EA. CRACKS AT BS 178 BULKHEAD WEB BETWEEN RBL 6.5 & RBL 17.1. REPAIRED BULKHEAD PER SRM & XEA X2-53-285.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,834 hrs · 30,111 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT & RT SIDE CHORDS CRACKED. R&R SIDE CHORDS PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,834 hrs · 30,111 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT UPPER WEB CRACKED. REPAIRED BULKHEAD PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,834 hrs · 30,111 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT SVC DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (SERVICE DOOR) · airframe 31,834 hrs · 30,111 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT SERVICE DOOR EMERGENCY EXIT DOOR LIGHT BATTERY LOW. R&R BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 31,802 hrs · 30,078 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 31,802 hrs · 30,078 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT FWD SECTION THRESHOLD. SECURED LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 31,562 hrs · 29,867 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING T/E FLAP DELAMINATED, MID SPAN, APPROX 18 LONG, 6 WIDE. REMOVED AND REPLACED T/E FLAP PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LOOSE FWD OF FWD SERVICE DOOR. SECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: SKIN — CRACKED (NR 3 LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND 3 EA CRACKS AT NR 3 L/E SLAT LOWER SKIN AROUND ACTUATOR CUT OUT. REPAIRED SLAT PER SWA RA NR 1-A57-0691.

Part: SKIN — CRACKED (NR 3 LE SLAT)

DURING SCHEDULED C3 CHECK, FOUND NR 3 LE SLAT LOWER SKIN CRACKED ON AFT RIVET ROW, 5 INCHES FWD OF ACTUATOR ATTACH POINT. REPAIRED SLAT ASSY PER SWA RA NR 1-357-0685.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THRU ULTRASONIC INSPECTION, 4 CRACKS AT BULKHEAD, BS 178, BETWEEN LBL 7 AND RBL 11 WL 198 TO 218. REPAIRED PER SRM.

Part: WINDOW — CRACKED (RT COCKPIT)

F/O NR 1 WINDOW ARCED AND CRACKED IN FLT (ALTITUDE APPROX 31,000). REMOVED AND REPLACED F/O NR 1 WINDOW PER MM, NO LEAKS NOTICED AT THIS TIME. AIRCRAFT OK FOR SERVICE. AIRCRAFT RECERTIFIED TO CAT IIIA STATUS, DO TO REMOVAL AND REPLACEMENT OF MCP TO FACILITATE OTHER MAINTENANCE.

Part: LAMP — BROKEN (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT FLOOR LEVEL LIGHT AT RT OVERWING EXIT BROKEN. REMOVED AND REPLACED LAMP ASSEMBLY PER BOEING MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED RON CHECK, FOUND ONE EGRESS LIGHT AT ROW 5 INOPERATIVE. REPLACED BULB PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND BULLNOSE EMERG LIGHT NOT SECURE AT 21 ABC AND 7 ABC. RESECURED EMERG LIGHT ASSY PER BOEING MM.

Part: ANGLE — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED BC1 CHECK, FOUND NR 6 LE SLAT ACTUATOR DOOR FWD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER SWA RA 1-363-11763.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUT-OUT CRACKED. REPAIRED PER SWA RA 1-353-1763.

Part: WEB — DENTED (BS 847)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT WEB DENTED AT BS 847 RBL 26 WL 156. REPLACED WITH NEW SECTION PER BOEING SRM.

Part: WEB — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT AFT CARGO DOOR CUTOUT AT BS 787, RBL 26, WL 156. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHANNEL — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND U-CHANNEL CRACKED AT BULKHEAD PANEL SUPPORT BS 727, RBL 5, WL 160. REPLACED PER BOEING SRM.

Part: MOPSILL — CORRODED (BS 270-360)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 270 TO 360 RBL 51 TO 64 WL 208. REPAIRED PER BOEING SRM.

Part: FLOOR — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BL ZERO, AND LBL 7. REPAIRED PER TI -A53-014 AND BOEING SRM.

Part: WHEEL — DAMAGED (NR 2)

NUMBER 2 WHEEL DAMAGED. REMOVED AND REPLACED NUMBERS 1 AND 2 TIRE/WHEEL ASSEMBLIES PER BOEING M/M.