N385SW

Part: LIGHT — LOOSE (CABIN) · airframe 70,278 hrs · 56,730 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT LENS ASSEMBLY LOOSE. SECURED LIGHT PER AMM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 70,278 hrs · 56,730 cycles

R2 DOOR AFT SLIDE MOUNT BRACKET CRACKED. R&R BRACKET PER DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 70,278 hrs · 56,730 cycles

AFT GALLEY AREA PHOTO LUMINESCENT STRIP DAMAGED. R&R STRIP PER AMM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 70,212 hrs · 56,678 cycles

CENTER PEDESTAL OVERHEAD PANEL EMERGENCY EXIT LIGHTS INOP. R&R LIGHT PER SIP.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 69,690 hrs · 56,357 cycles

L1 DOOR SLIDE GIRT BAR OUT OF ADJUST. R & R THE GIRT BAR IAW MT.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 69,637 hrs · 56,319 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED ON THE INBOARD TRAILING EDGE OF THE FLAP. R & R AFT FLAP IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 68,697 hrs · 55,697 cycles

LEFT OVERHEAD BIN EMER EXIT SIGN LOOSE AT ROW 2. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,571 hrs · 55,610 cycles

RIGHT EMER EXIT HATCH BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,571 hrs · 55,610 cycles

FORWARD GALLEY A LAVATORY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: LINK ASSY — CORRODED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING LINK ASSEMBLY CORRODED ON RSS 135.24. REPAIRED LINK ASSEMBLY IAW CMM.

Part: RIB — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING RIB CRACKED EXISTING FILLER INTERNAL AREA ON WBL 114.00, STRINGER 2R UPPER CHORD REAR SPAR. REPAIRED RIB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING INSPAR UPPER SKIN TE CRACKED AT REAR SPAR RSS 290. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INBD FORE FLAP CRACKED ON LOWER SURFACE TE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT FASTENER HOLE UPPER REAR SPAR RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT UPPER REAR SPAR RSS 253. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT UPPER REAR SPAR RSS 249. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 168. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT RSS 152. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT UPPER REAR SPAR RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT UPPER REAR SPAR RSS 248.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 229.75. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 256. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INSPAR UPPER SKIN TE CRACKED AT UPPER AT RSS 238.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 263. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 250.25. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 164. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 269. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER SKIN CRACKED AT RSS 261. REPAIRED SKIN IAW EA.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 5 FLAP TRACK SUPPORT ATTACH FITTING CORRODED. REPAIRED FITTING IAW EA.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 68,571 hrs · 55,610 cycles

RIGHT MAIN WW CTR WING SECTION, SUPPORT ANGLE STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING INBD FORE FLAP INTERNAL UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FAIRING INBD FLAP, OTBD TRACK SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FAIRING SUPPORT ANGLE CRACKED, ON INBD FLAP OTBD TRACK INTERNAL AREA, UPPER POSITION LT SIDE. REPLACED ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FAIRING INBD FLAP, OTBD TRACK STIFFENER CRACKED ON INTERNAL AREA. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FAIRING, FWD EDGE INBD FLAP, OTBD TRACK SUPPORT CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FAIRING INBD FLAP, OTBD TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

LEFT WING INBD FLAP, OTBD TRACK 3 FAIRING ANGLE CRACKED, UPPER POSITION INTERNAL AREA. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 68,571 hrs · 55,610 cycles

LEFT WING NR 3 INBD FLAP, OTBD TRACK STIFFENER CRACKED. R & R STIFFENER IAW DWG & SRM.

Part: SPLICE — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING SPAR UPPER CHORD SPLICE CRACKED AT RSS 221.5. REPAIRED SPLICE IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 218.5. REPAIRED WEB IAW EA.

Part: SPLICE — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON FASTENER HOLE RSS 221.5. REPAIRED SPLICE IAW EA.

Part: STRIP — DETERIORATED (CABIN) · airframe 68,571 hrs · 55,610 cycles

EEPLS STRIP DETERIORATED AT RT SIDE. R & R STRIP IAW MM.

Part: STRIP — DETERIORATED (CABIN) · airframe 68,571 hrs · 55,610 cycles

LEFT CABIN EEPLS STRIP DETERIORATED. R & R STRIP IAW MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

FORWARD ENTRY SURROUND STRUCTURE ATTACHMENT CLIP CRACKED AT BS 360, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

ELECTRONIC EQUIP COMPARTMENT STRAP CRACKED, BETWEEN BS 312 - 344, BL 0. R & R STRAP IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT HORIZ STAB) · airframe 68,571 hrs · 55,610 cycles

RIGHT HORIZONTAL STABILIZER ATTACH ANGLE CRACKED, AFT SIDE OF THE UPPER CHORD ON CTR SECTION IN TAIL COMPARTMENT. REPLACED ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

ZEE ANGLE CORRODED, BETWEEN BS 947.5 - 986, STRINGER 17R. R & R ZEE ANGLE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT HORIZ STAB) · airframe 68,571 hrs · 55,610 cycles

RIGHT HORIZONTAL STABILIZER ATTACH ANGLE CRACKED, FWD SIDE OF THE UPPER CHORD ON TAIL COMPARTMENT. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

FUSELAGE SKIN CRACKED AT BS 332-3.5, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

FORWARD GALLEY DOOR INNER CHORD CORRODED, BETWEEN BS 312 - 360, STRINGER 17R. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

FORWARD ENTRY DOOR, INNER CHORD CORRODED, BETWEEN BS 312 - 344, STRINGER 17L. R & R CHORD IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

FLOOR STRUCTURE STIFFENER CRACKED AT BS 328, LBL 45.5. R & R STIFFENER IAW DWG & SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 10R. R & R CLIP IAW EA.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 5 FLAP TRACK BEAM CRACKED. R & R NR 5 TRACK IAW AMM.

Part: PLATE — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING TE PLATE CRACKED AT WBL 208.60 ON LOWER SURFACE. R & R PLATE IAW SRM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 68,571 hrs · 55,610 cycles

AFT GALLEY AREA FLASHLIGHT BASE BROKEN. R & R FLASHLIGHT IAW CMM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 68,571 hrs · 55,610 cycles

FORWARD GALLEY AREA FLASHLIGHT BASE BROKEN. R & R FLASHLIGHT IAW CMM.

Part: PLATE — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING PLATE CRACKED ON TE AT WBL 85.85. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING TE ANGLE CRACKED ON WBL 84. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

AFT CARGO COMPARTMENT, CHANNEL CORRODED AT BS 859, RBL 3. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

AFT CARGO COMPARTMENT, LOWER FLANGE ON FRAME CORRODED, AT BS 747, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING ANGLE CRACKED AT RSS 537.806, APPROX IN TE. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FLAP TRACK) · airframe 68,571 hrs · 55,610 cycles

LEFT WING TE, NR 3 FLAP TRACK FAIRING CLIP ASSEMBLY, CRACKED ON RSS 270. R & R CLIP ASSEMBLY IAW SRM.

Part: BRACKET — CRACKED (LT SPOILER) · airframe 68,571 hrs · 55,610 cycles

LEFT WING NR 4 GND SPOILER INBD SUPPORT FITTING BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED, AT BS 859, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING, INBD SIDE SUPPORT ANGLE CRACKED AT WBL 183.40, TE. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — DETERIORATED (R2 DOOR) · airframe 68,571 hrs · 55,610 cycles

R2 DOOR EMER EVAC SLIDE FLOOR MOUNTED HARDWARE PLATE BRACKET DETERIORATED. R & R BRACKET IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 68,571 hrs · 55,610 cycles

RIGHT WING INSPAR UPPER SKIN TE CRACKED AT WBL 171. REPAIRED SKIN IAW EA.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 68,571 hrs · 55,610 cycles

AFT CARGO COMPARTMENT, TRACK CRACKED AT BS 787, LBL 17.24. REPAIRED TRACK IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

AFT CARGO COMPARTMENT, LOWER FLANGE OF FRAME CORRODED, AT BS 747, BETWEEN STRINGER 27L - 26L. REPAIRED FRAME IAW SRM.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 68,571 hrs · 55,610 cycles

TAIL CONE EXTERNAL SKIN DELAMINATED AT TAIL CONE. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 68,571 hrs · 55,610 cycles

EXTERNAL SKIN LOWER AREA AT TAIL CONE DELAMINATED, BETWEEN 5 & 6 O CLOCK. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 68,571 hrs · 55,610 cycles

LEFT WING FIXED LE SKIN AT KRUEGER FLAP SEAL DOOR CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 68,571 hrs · 55,610 cycles

RIGHT MAIN WW CTR WING SECTION, STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 66,956 hrs · 54,540 cycles

RIGHT SIDEWALL EXIT LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,359 hrs · 54,120 cycles

LEFT WING NR 4 SLAT INBD TE LOWER SKIN DELAMINATED. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,352 hrs · 54,114 cycles

NUMBER 4 LE SLAT, INBD TE LOWER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 66,056 hrs · 53,924 cycles

RIGHT PHOTO LUMINESCENT STRIPS CRACKED AT ROW 1. R & R STRIP IAW MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 66,056 hrs · 53,924 cycles

LEFT PHOTO LUMINESCENT STRIPS CRACKED AT ROW 1. R & R STRIP IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,972 hrs · 53,859 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 65,659 hrs · 53,660 cycles

RIGHT WING NR 7 FLAP TRACK AN ARM FOR FAIRING CRACKED IN ARM. R & R NR 7 AFT FLAP TRACK IAW CMM.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 65,659 hrs · 53,660 cycles

LEFT WING NR 1 FLAP TRACK AFT OTBD BOLT HOLE SUPPORT FITTING CORRODED. R & R FITTING IAW DWG & SRM.

Part: DOWNLOCK SENSOR — FAULTY (RT MLG) · airframe 64,704 hrs · 53,000 cycles

DECLARED EMER RT MLG UNSAFE EXTEND LIGHT INDICATOR. R & R RT MLG DOWN LOCK SENSOR IAW MM.

Part: DOWNLOCK SENSOR — FAULTY (RT MLG) · airframe 64,727 hrs · 53,021 cycles

DECLARED EMER RT MLG GEAR WOULD NOT INDICATE DOWN WITH NORMAL OR MANUAL EXTENSION. R & R RT MLG DOWN LOCK SENSOR IAW MM.

Part: CONTROL VALVE — FAILED (LE SLAT) · airframe 65,653 hrs · 52,957 cycles

AIR TURN BACK ON CLIMB OUT LE TRANSIT LIGHT STAYED ON. LE SLATS FAILED TO RETRACT. R & R AUTO SLAT CONTROL VLV IAW MM.

Part: CONTROL VALVE — FAULTY (LE SLAT) · airframe 64,634 hrs · 52,943 cycles

AIR TURN BACK, DURING FLAP RETRACTION OTBD SLAT REMAINED EXTENDED. R & R LE DEVICE CONTROL VLV IAW MM.

Part: CIRCUIT CARD — FAULTY (COCKPIT) · airframe 64,611 hrs · 52,925 cycles

AIR TURN BACK RT MLG UNSAFE LIGHT INDICATION. R & R M981 & M982 PC CARD IAW MMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,450 hrs · 52,800 cycles

R2 DOOR EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,288 hrs · 52,680 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 64,049 hrs · 52,504 cycles

LEFT WING INBD NR 4 SPOILER DELAMINATED. R & R NR 4 SPOILER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,005 hrs · 52,468 cycles

RIGHT OVERWING EMER EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BRACKET — LOOSE (R2 DOOR) · airframe 63,560 hrs · 52,158 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK BRACKETS LOOSE. SECURED BRACKETS IAW MT.

Part: LENS — MISSING (CABIN) · airframe 63,322 hrs · 51,980 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,060 hrs · 51,778 cycles

RT EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT BS 986.5. R & R BATTERY PACK IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,060 hrs · 51,778 cycles

RIGHT WING TE OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,060 hrs · 51,778 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,060 hrs · 51,778 cycles

VERTICAL UPPER PRESS PANEL CRACKED AT BS 663, BETWEEN RBL 45.5 TO RBL 60. R & R PANEL IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

MAIN DECK FLOOR STRUCTURE FWD CARGO COMPARTMENT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R & R CHANNEL IAW SRM & DWG.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

DOOR STOP FITTING CRACKED SKIN AT BS 303.9, STRINGER 7L. R & R FITTING IAW SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

L1 DOOR CUT OUT FWD UPPER CORNER REVEAL CRACKED. R & R REVEAL IAW SRM & DWG.

Part: NUT PLATE — CRACKED (LT WING) · airframe 63,060 hrs · 51,778 cycles

LEFT WING NUT STRIPS CRACKED AT WBL 198.6, STRINGER 11L. R & R NUT STRIPS IAW SRM.

Part: NUT PLATE — CRACKED (LT WING) · airframe 63,060 hrs · 51,778 cycles

LEFT WING NUT STRIPS CRACKED BETWEEN WBL 191.0 TO WBL 183.4, BETWEEN STRINGER 11L TO STRINGER 12L. R & R NUT STRIPS IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 63,060 hrs · 51,778 cycles

RIGHT WING REAR SPAR UPPER RIB CHORD CRACKED AT WING STATION 198.6, STRINGER 5. REPAIRED RIB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R & R TIE CLIP IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

SUPPORT ANGLE CRACKED AT BS 312+8, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 23L. R & R TIE CLIP IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

STRINGER CRACKED AT BS 325.3, STRINGER 21R. REPAIRED STRINGER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 32. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R & R WEB IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

STIFFENER CRACKED AT BS 727, LBL 45.5. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

SUPPORT ANGLE CRACKED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

SUPPORT ANGLE CRACKED AT BS 328+8, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

AFT FACE OF PRESS BULKHEAD STIFFENER CRACKED AT BS 727, STRINGER 27L. R & R STIFFENER IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 887 TO BS 907, RBL 45.5. R & R ANGLE IAW SRM.

Part: FASTENER — CORRODED (EVAC SLIDE) · airframe 63,060 hrs · 51,778 cycles

R1 DOOR EMERGENCY EVAC SLIDE HARDWARE CORRODED. R & R HARDWARE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

AFT FACE OF PRESS BULKHEAD STIFFENER CRACKED AT BS 727, STRINGER 27R. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

STIFFENER CRACKED AT BS 727, RBL 45.5. R & R STIFFENER IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

WEB CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R & R WEB IAW SRM & DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FUSELAGE STIFFENER CORRODED AT STATION 1016, BL 0. REPAIRED STIFFENER IAW EA.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 63,060 hrs · 51,778 cycles

AFT CARGO COMPARTMENT DOOR T CHORD CRACKED. REPAIRED T CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 312, RBL 20. REPAIRED FLOORBEAM IAW SRM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 63,060 hrs · 51,778 cycles

RIGHT WING NR 8 CARRIAGE A FRAME CRACKED. R & R A FRAME IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 63,060 hrs · 51,778 cycles

RT WING NR 7 MOVABLE FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 63,060 hrs · 51,778 cycles

AFT CARGO COMPARTMENT DOOR T CHORD CRACKED AT AFT END OF CROSSBEAM E OF THE AFT CARGO COMPARTMENT DOOR. REPAIRED T CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 500D TO BS 520 & BL 0. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (BS 303) · airframe 63,060 hrs · 51,778 cycles

L1 DOOR SKIN CUT OUT CRACKED AT BS 303.9+6, STRINGER 6L+3. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FRAME CORRODED AT BS 787, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

TIE CLIP CRACKED AT BS 727D, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: ACCESS PANEL — CRACKED (RT HORIZ STAB) · airframe 63,060 hrs · 51,778 cycles

RIGHT HORIZONTAL STABILIZER PLATE ACCESS PANEL 9226R CRACKED. R & R PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FORWARD CARGO COMPARTMENT CLIP ANGLE CRACKED AT BS 500D & STRINGER 19R. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FLOOR STRUCTURE FWD CARGO COMPARTMENT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R & R CHANNEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FWD CARGO ANGLE CRACKED AT STATION 500C, STRINGER 26R. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,060 hrs · 51,778 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL 9224R PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FWD CARGO ANGLE CRACKED AT STATION 380, STRINGER 26R. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 63,060 hrs · 51,778 cycles

VERTICAL STABILIZER TE WEB CRACKED AT FIN STATION 81.80. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 21L TO STRINGER 22L. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 63,060 hrs · 51,778 cycles

NR 1 ENG AFT STRUT ACCESS PANEL 5752L SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FUSELAGE FRAME CHORD CRACKED AT LT STATION 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

FUSELAGE FRAME CHORD CRACKED AT RT STATION 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,060 hrs · 51,778 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75+1.0, RBL 24.5+14.5. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,060 hrs · 51,778 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+1, LBL 24.5+15. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,060 hrs · 51,778 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 38. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,060 hrs · 51,778 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5. REPAIRED CHORD IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 63,023 hrs · 51,754 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 62,959 hrs · 51,709 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS ASSEMBLY IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 62,835 hrs · 51,622 cycles

FWD SERVICE DOOR EMERGENCY LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: ACTUATOR — CRACKED (LT SPOILER) · airframe 62,144 hrs · 51,154 cycles

DECLARED EMERGENCY HYDRAULIC A FAILURE. FOUND LT OTBD GROUND SPOILER ACTUATOR CRACKED. R & R BOTH FILTERS & SPOILER ACTUATOR IAW AMM.

Part: SPINDLE — DAMAGED (LT WING) · airframe 60,930 hrs · 50,230 cycles

LEFT WING NR 2 SPINDLE HAS CHIPPED/FLANKED THERMAL COATING ON LOWER SURFACE. R & R NR 2 SPINDLE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 60,024 hrs · 49,589 cycles

EMERGENCY EXIT LIGHT NEAR FORWARD F/A JUMPSEAT BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,729 hrs · 48,665 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITIONING. REPOSITIONED SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 58,456 hrs · 48,440 cycles

LEFT WING LEADING EDGE NR 3 SLAT CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: COVER — MISSING (CABIN) · airframe 58,456 hrs · 48,440 cycles

L2 DOOR LOWER EMERGENCY LIGHT COVER MISSING. INSTALLED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 58,456 hrs · 48,440 cycles

AFT GALLEY DOOR LOWER EMERGENCY LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,211 hrs · 47,503 cycles

LT OVERWING EMERGENCY EXIT LIGHT FORWARD BULB IS INOP. RELAMPED BULB IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,211 hrs · 47,503 cycles

RT WING AFT T/E FLAP DELAMINATED JUST AFT AND INBOARD OF THE NR 2 AFT FLAP TRACK. REPAIRED FLAP PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

R2 DOOR BEAR STRAP SKIN CUTOUT CRACKED AT FORWARD LOWER CORNER. REMOVED AND REPLACED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

MLG WHEEL WELL UPPER PRESS DECK CRACKED AT BS 540+1.5, LBL 33, WL 204.5. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

LT FRAME INNER CHORD CRACKED AT BS 616. REMOVED AND REPLACED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

RT STUB FRAME INNER CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

Z-ANGLE CORRODED AT BS 727E, RBL 24. REPAIRED Z-ANGLE IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,211 hrs · 47,503 cycles

RT WING I/B AFT FLAP DELAMINATED AT T/E ON FORWARD AND AFT SIDE. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: HINGE — BROKEN (NR 5 SPOILER) · airframe 57,211 hrs · 47,503 cycles

RT WING NR 5 SPOILER ACTUATOR HINGE BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

FRAME INNER CHORD ANGLE CRACKED AT BS 616, LBL 67. REMOVED AND REPLACEMENT FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

R2 DOOR SKIN CRACKED, FORWARD LOWER CORNER, UNDER SILL PLATE. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,211 hrs · 47,503 cycles

FRAME WEB CRACKED AT BS 639, STR 16L. REPAIRED WEB IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 57,211 hrs · 47,503 cycles

LT EMERGENCY EXIT LIGHTS LOOSE. REMOVED AND REPLACED LENS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 57,157 hrs · 47,464 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,929 hrs · 47,304 cycles

RT AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 56,581 hrs · 47,057 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500C+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500C+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 360+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 827+10, LOWER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 847+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10 LOWER FWD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 867+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 867+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10 UPPER FWD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10 LOWER FWD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 847+10 LOWER FWD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULE SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 440+10 UPPER FWD CORNER. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, RT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 500C+10 UPPER FWD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 767+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 400+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 360+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 400+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 847+10 UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 47,007 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 380+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,324 hrs · 46,861 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 21 TO ROW 23. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,324 hrs · 46,861 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727B+10, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW SKIN CRACKED AT BS 360+10, UPPER FWD CORNER. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED SPV CHECK FOUND, CROWN SKIN OIL CAN CRACKED BETWEEN BS 727B TO BS 747+4, BETWEEN STR 3R TO STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED SPV CHECK FOUND, SKIN CRACKED AT BS 727A+10, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED SPV CHECK FOUND, CROWN SKIN OIL CAN CRACKED BETWEEN BS 847+10 TO BS 867, BETWEEN STR 3R TO STR 4R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 1. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 1. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 1. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,822 hrs · 46,471 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 55,602 hrs · 46,295 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, LT WING NR 3 SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FITTING — BROKEN (SPOILER) · airframe 55,602 hrs · 46,295 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND, RT WING NR 5 GROUND SPOILER O/B FITTING ASSY LUG BROKEN. REPAIRED FITTING PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,585 hrs · 46,273 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,585 hrs · 46,273 cycles

FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 55,578 hrs · 46,273 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,262 hrs · 46,022 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 807+6.5 TO +8, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,262 hrs · 46,022 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 807+7.5 TO +10, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,709 hrs · 45,609 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 530, STR 4R. REPAIRED SKIN PER AAR EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,679 hrs · 45,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,238 hrs · 45,255 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 795, STR 4R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 622, BETWEEN STR 1 TO STR 2R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 986.5 TO BS 1006, STR 24L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 827 TO BS 847, BETWEEN STR 1 TO STR 2R. REPAIRED SKIN PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.8. REPAIRED BEAM PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 24L. REPAIRED FRAME PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500B TO BS 500C, STR 1. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 420 TO BS 440, STR 1L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 526, STR 11L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 739C, STR 4L. REPAIRED SKIN PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 807 TO BS 827, LBL 3.00. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 847 TO BS 867, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 732D, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CRACKED AT BS 947.2, LBL 53.50. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 735E, STR 4R. REPAIRED SKIN PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 927 TO BS 947, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 487, STR 4R. REPAIRED SKIN PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 767 TO BS 787, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 727C TO BS 727D, RBL 3.00. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 500D TO BS 540, STR 11L. REMOVED AND REPLACED STRINGER PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 447, STR 4R. REPAIRED SKIN PER EO.

Part: PLATE — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO PLATE CORRODED AT BS 787, STR 25R. REMOVED AND REPLACED PLATE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 907 TO BS 927, LBL 3.00. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED BETWEEN BS 787 TO BS 807, LBL 3.00. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 692, RBL 24.5. REPAIRED BEAM PER EO.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 767 TO BS 787, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT LOWER SURFACE CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAD DWG.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732D, RBL 3. REPAIRED CHANNEL PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B END OF O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM AND BAD DWG.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BS 732B, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727E TO BS 747, LBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 25L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 827, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BS 732B, LBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 18R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 596, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD CORRODED AT BS 986.5, RBL 43. REMOVED AND REPLACED CHORD PER BAC DWG.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR FRAMING CRACKED AT BS 956, STR 11L. REMOVED AND REPLACED DOOR FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,132 hrs · 44,385 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: WIRE — LOOSE (CABIN) · airframe 52,811 hrs · 44,137 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXIT LIGHT INOP. SECURED EXIT LIGHT TERMINAL END WIRE PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,664 hrs · 44,040 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,520 hrs · 43,930 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 52,521 hrs · 43,930 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,477 hrs · 43,893 cycles

DURING SCHEDULED MV2D CHECK, FOUND SKIN CRACKED AT BS 840, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,477 hrs · 43,893 cycles

DURING SCHEDULED MV2D CHECK, FOUND SKIN CRACKED AT BS 512A, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 552,455 hrs · 43,879 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 897 TO BS 900, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 552,455 hrs · 43,879 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 778 TO BS 782, STR 4R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,982 hrs · 43,522 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,982 hrs · 43,522 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 737B, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,982 hrs · 43,522 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 737C, STR 4R. REPAIRED SKIN PER EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 51,202 hrs · 42,942 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,084 hrs · 42,106 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 49,568 hrs · 41,754 cycles

FWD FLT ATTENDANT O/B FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 49,506 hrs · 41,714 cycles

DURING SCHEDULED HC2 CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,507 hrs · 41,714 cycles

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

Part: COVER — MISSING (CABIN) · airframe 49,507 hrs · 41,714 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER MISSING AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,507 hrs · 41,714 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,357 hrs · 41,605 cycles

FWD O/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 48,573 hrs · 41,060 cycles

DIVERSION, UNIDENTIFIED ODOR IN PAX CABIN AT ALTITUDE. INSPECTED FOUND GASPER C/B POPPED. INSPECTED AREA, NO DAMAGE NOTED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,274 hrs · 40,855 cycles

FOUND FWD O/B EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 348, 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER PAE EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 360 TO BS 380 AT STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,159 hrs · 40,763 cycles

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

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 47,523 hrs · 40,277 cycles

FLIGHT CREW REPORTED ELECTRICAL SMOKE SMELL. R&R GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,415 hrs · 40,202 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: SIGN — LOOSE (CABIN) · airframe 46,575 hrs · 39,600 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 43,983 hrs · 37,546 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP INBOARD T/E DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,502 hrs · 36,388 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,410 hrs · 36,311 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 24L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S24R) · airframe 42,410 hrs · 36,311 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,264 hrs · 36,208 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF TO ROW 5 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,380 hrs · 35,502 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 41,326 hrs · 35,460 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 41,326 hrs · 35,460 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 39,997 hrs · 34,413 cycles

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

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 38,353 hrs · 33,108 cycles

DURING SCHEDULED RON CHECK, L2 DOOR EMERGENCY EXIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 38,174 hrs · 32,970 cycles

ELECTRICAL SMELL FROM AFT COFFEEMAKER. REMOVED AND REPLACED AFT COFFEEMAKER PER MM.

Part: LENS — MISSING (CABIN) · airframe 36,855 hrs · 31,893 cycles

LEFT LOWER OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT RIGHT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 867, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM AND BAC DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB AT BS 467, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1040, STRINGER 23R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,970 hrs · 29,606 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 986, LBL 38, BS 1002, RBL 41, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 33,889 hrs · 29,538 cycles

EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,611 hrs · 29,305 cycles

EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,354 hrs · 29,091 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT LENS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 32,895 hrs · 28,749 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY LIGHT LENS COVER CRACKED. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,895 hrs · 28,749 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,368 hrs · 28,316 cycles

R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: LINE — SPLIT (HYD SYSTEM) · airframe 31,435 hrs · 27,563 cycles

AIR TURNBACK, DECLARED EMERGENCY, A-HYD SYSTEM FAILURE ON GEAR RETRACTION. FOUND LT MLG ACTUATOR HYD UP LINE SPLIT, REMOVED AND REPLACED HYD UP LINE AND ALL 'A' HYD SYSTEM FILTERS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,133 hrs · 26,519 cycles

DURING SCHEDULED C3 CHECK, FOUND R-1 COCKPIT WINDOW POST SKIN CRACKED AT UPPER OTBD CORNER. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 29,821 hrs · 26,270 cycles

DURING WALK ROUND INSPECTION, FOUND LT OTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT OTBD T/E FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,444 hrs · 25,175 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 28,318 hrs · 25,079 cycles

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

Part: BEARING — WORN (CONTROL COLUMN) · airframe 28,132 hrs · 24,921 cycles

DURING SCHEDULED RON, FOUND AILERONS BINDING DURING PREFLIGHT CONTROL CK. REMOVED AND REPLACED CONTROL COLUMN BEARINGS PER MM.

Part: BEARING — WORN (RT MLG W/W) · airframe 28,093 hrs · 24,883 cycles

NOTICABLE BINDING IN AILERON CONTROL WHEEL. MX FERRY TO PHX. REMOVED AND REPLACED BEARINGS AT AILERON FEEL CENTERING UNIT AND F/O'S CONTROL YOKE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,809 hrs · 24,664 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 25,645 hrs · 22,896 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPTIAN'S WINDOW POST CRACKED BETWEEN NR 1 AND NR 2 WINDOWS. REPAIRED WINDOW POST PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,645 hrs · 22,896 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 233 & RBL 17.1. R&R WEB PER SRM.

Part: BRACKET — BROKEN (AFT SVC DOOR) · airframe 25,645 hrs · 22,896 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET BROKEN. R&R MOUNT BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 25,591 hrs · 22,844 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,889 hrs · 22,265 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT SEVERAL LOCATIONS. RELAMPED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 24,581 hrs · 21,989 cycles

EEPLS COVER MISSING. INSTALLED EEPLS COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 24,535 hrs · 21,948 cycles

EEPLS MISSING COVER. REPLACED EEPLS COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,519 hrs · 21,100 cycles

EEPLS TRACK COVER MISSING AT ROW 11. INSTALLED TRACK COVER PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 22,974 hrs · 20,679 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 9, 16, 18, 19 & 21. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,231 hrs · 20,049 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 CRACKS AT BS 178 BULKHEAD, WL 201 - 201.5, RBL 5.7 & LBL 5.7. REPAIRED BULKHEAD PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 22,029 hrs · 19,880 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING AFT INBD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 21,600 hrs · 19,511 cycles

EEPLS LOOSE AND DAMAGED AT ROW 21. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: LIGHT COVER — LOOSE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 13. SECURED TRACK COVER PER MM.

Part: WIRE — DISCONNECTED (ROW 12)

EEPLS INOP. RECONNECTED WIRING AT ROW 12 PER MM.

Part: LIGHT — INOPERATIVE (ROW 14)

EEPLS INOP AT ROW 14. REPAIRED WIRING PER MM.

Part: HORZ IND — INOP (COCKPIT)

STANDBY HORIZON INDICATOR INOP. (PHX TO ONT). REMOVED AND REPLACED STATIC INVERTER AND STANDBY HORIZON INDICATOR.

Part: LIGHT — INOP (ROW 15)

EEPLS INOP AT ROW 15. RECONNECTED PULLED WIRES PER MM.

Part: WIRE — LOOSE (ROW 14&15)

EEPLS LIGHT OUT OF TRACK AND INOP AT ROWS 14 AND 15. REINSTALLED AND RECONNECTED WIRES ON LIGHT ASSY PER MM. OPS CK GOOD.

Part: LENS — MISSING (CABIN)

EEPLS LIGHT MISSING RED LENS AT MID CABIN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (ROW 12-14)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT INOP, ROWS 12 TO 14. REPAIRED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS FWD TRACK LIGHT OUT OF TRACK. INSTALLED NEW TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (ROW 11-12)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP BETWEEN ROWS 11 AND 12. RECONNECTED WIRE AT ROWS 11-12 PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A CRACK AT BULKHEAD, BS 178 , LBL 13. REPAIRED BULKHEAD PER SRM.

Part: LENS — MISSING (ROW 3ABC)

DURING SCHEDULED C4 CHECK, FOUND FLOOR EMERGENCY LIGHT MISSING LENS AT ROW 3 ABC. REPLACED LENS PER MM.

Part: LAMPS — FAILED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTING WITH SEVERAL LIGHTS INOP. RELAMPED PER BOEING M/M.

Part: SKIN — DENTED (BS 354-360)

DURING SPV CHECK, FOUND GOUGED SKIN AND DENTED AT BS 354-360, 3 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM.

Part: SPLICE — DAMAGED (BS 360)

DURING SPV CHECK, FOUND CIRCUMFERENTIAL BUTT SPLICE DOUBLER DAMAGED AT BS 360, 2 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 360)

DURING SPV CHECK, FOUND FRAME SHEAR TIE DAMAGED AT BS 360, 2 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 360)

DURING SPV CHECK, FOUND SKIN GOUGED AND DENTED AT BS 360 TO 378 STR 19 RT, 5 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING C1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L1 DOOR. RELAMPED PER BOEING M/M.

Part: BELTFRAME — CRACKED (BS 807)

DURING SCHEDULED C2 CHECK, FOUND BELTFRAME CRACKED AT BS 807, AT S29-28R. REPAIRED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED B/C CHECK, FOUND RIGHT SIDE EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M.