N362SW

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 76,778 hrs · 63,680 cycles

R2 DOOR EMERGENCY SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW AMM.

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 76,668 hrs · 63,583 cycles

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. SECURED THE LAMP IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 76,668 hrs · 63,583 cycles

R1 DOOR EXIT SIGN COVER LENS LOOSE REPLACED THE LENS IAW AMM.

Part: DOOR — DELAMINATED (RT MLG) · airframe 76,400 hrs · 63,367 cycles

RT MAIN LANDING GEAR OUTER GEAR DOOR DELAMINATED AT LOWER FORWARD EDGE. R&R DOOR PER AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 76,400 hrs · 63,367 cycles

RT PHOTO LUMINESCENT STRIP DAMAGED AT ROW 10. R&R STRIP PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,332 hrs · 63,319 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,332 hrs · 63,319 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 76,332 hrs · 63,319 cycles

LEFT WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF THE PYLON INBOARD ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,332 hrs · 63,319 cycles

SKIN CRACKED BETWEEN BS 913.5 TO BS 915.5, STR 4L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,332 hrs · 63,319 cycles

SKIN CRACKED BETWEEN BS 423.5 TO BS 424.5, STR 2R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,332 hrs · 63,319 cycles

SKIN CRACKED BETWEEN BS 412.5 TO BS 414.5, STR 1L. REPAIRED SKIN IAW ER AND EA.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 75,716 hrs · 62,904 cycles

LOWERED LANDING GEAR, GOT LT GEAR REV LIGHT INDICATION, NO GREEN LIGHT INDICATIONS. RAISED ALL GEAR NORMALLY RAN CHECK LIST. MANUALLY EXTENDED LT GEAR NORMALLY. R & R DOWNLOCK ACTUATOR IAW AMM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 75,716 hrs · 62,904 cycles

LOWERED LANDING GEAR, GOT LT GEAR REV LIGHT INDICATION, NO GREEN LIGHT INDICATIONS. RAISED ALL GEAR NORMALLY RAN CHECK LIST. MANUALLY EXTENDED LT GEAR NORMALLY. R & R UPLOCK ACTUATOR IAW AMM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 74,669 hrs · 62,191 cycles

FORWARD CARGO DOOR FRAME, CRACKED FRAME AT THE EXTERNAL UPLOCK ASSEMBLY. R & R DOOR IAW AMM.

Part: ATTACH BRACKET — CRACKED (LT SPOILER) · airframe 74,669 hrs · 62,191 cycles

LEFT WING INBD GND SPOILER, INBD ACTUATOR CASTING ATTACH BRACKET CRACKED. REPAIRED BRACKET IAW DWG & SRM.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN CRACKED, APPROX 3.0" FWD OF REAR SPAR, LOCATED FWD OF FWD TRUNNION OF MLG, APPROX RSS 179. R & R SKIN IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

CREASE BEAM WEB CRACKED AT BS 360, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

R1 DOOR CUT OUT FWD OF UPPER HINGE, OTBD INTERCOSTAL ATTACH ANGLE CRACKED ON AFT END. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

R1 DOOR UPPER HINGE CUT OUT CRACKED AT BS 290 RT, WL 257. REPAIRED CUT OUT IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING AFT SPAR WING SPAR, UPPER CHORD TO BODY BATH TUB FITTING AT RSS 70.85 CRACKED. R & R FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 239.5 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

FORWARD ENTRY DOOR UPPER HINGE CUT OUT, CRACKED AT BS 304.4, LT WL 258.5. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 237 RT, FASTENER HOLE 1 INCH FROM AFT EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 255.5 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 238 RT, FASTENER HOLE 1INCH FROM AFT EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN AT APPROX RSS 236 RT, FASTENER HOLE 1" FROM AFT EDGE CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 251 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

FORWARD ENTRY DOOR UPPER HINGE CUT OUT CRACKED AT BS 304.4, LT WL 257. REPAIRED CUT OUT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

FRAME WEB CRACKED AT BS 360, STRINGER 20R. R & R WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING REAR SPAR WEB FASTENER HOLE COMMON TO UPPER CHORD, CRACKED AT RSS 220. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,858 hrs · 62,318 cycles

FORWARD E & E COMPARTMENT FRAME FAIL SAFE CHORD CRACKED AT BS 360, STRINGER 20R. REPAIRED FRAME IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 74,646 hrs · 62,173 cycles

FORWARD LAVATORY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

MAIN CABIN PRESS DECK GUSSET CRACKED, BETWEEN BS 540 - 549, LBL 57. R & R GUSSET IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 787, STRINGER 24R. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 500, STRINGER 16L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 480, STRINGER 16L. R & R CLIP IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

SHEAR TIE CORRODED AT STATION 747, STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 887, STRINGER 9L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 14R. R & R CLIP IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

LEFT CREASE BEAM CORRODED AT STATION 360 - 380. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

RIGHT CREASE BEAM CORRODED AT STATION 360 - 380. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

MAIN CABIN STRINGER CLIP CRACKED AT BS 500A, STRINGER 16L. R & R CLIP IAW DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

AFT SEAT TRACK FLOORBEAM INBD & OTBD TRACK MOUNT FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIRED FLOORBEAM IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

SHEAR TIE CORRODED AT STATION 747, STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

RIGHT CREASE BEAM CORRODED AT STATION 727C - 727C. REPAIRED BEAM IAW SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 727D - 727E, STRINGER 17L. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 460 - 480. R & R WEB IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING NR 6 FLAP TRACK AFT ATTACH POINT CORRODED, AT AFT OTBD WING TO TRACK MATING SURFACE. R & R TRACK IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

SHEAR TIE CORRODED AT STATION 847, STRINGER 27R - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

AFT CARGO BAY TIE DOWN FLOOR SUPPORT CORRODED AT BS 945, RBL 13. R & R SUPPORT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,646 hrs · 62,173 cycles

SHEAR TIE CORRODED AT STATION 927, STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,645 hrs · 62,173 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8, INBD OF SEAT TRACK. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 74,646 hrs · 62,173 cycles

RIGHT WING REAR SPAR, UPPER CHORD CRACKED AT RSS 222. REPAIRED CHORD IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,588 hrs · 62,128 cycles

R2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,238 hrs · 61,855 cycles

SKIN CRACKED AT BS 520+3, STRINGER 6L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,238 hrs · 61,855 cycles

FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.

Part: WIRE — LOOSE (LT MLG) · airframe 74,164 hrs · 61,804 cycles

LEFT MAIN GEAR RED LIGHT ILLUMINATED & THERE WAS NO GREEN LIGHT AFTER A FLY BY. WHILE RUNNING CHECKLIST THE GREEN LIGHT CAME ON & RED LIGHT WENT OUT. FOUND LOOSE GND WIRE. SECURED GND WIRE IAW AMM.

Part: CIRCUIT CARD — FAULTY (COCKPIT) · airframe 74,094 hrs · 61,755 cycles

ON APPROACH WHEN LANDING GEAR SELECTED DOWN, LT MLG INDICATED RED & NO GREEN CYCLED GEAR ALL GREEN INDICATIONS. R & R LANDING GEAR LOGIC CARD IAW MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,918 hrs · 61,627 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R CHARGER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,761 hrs · 61,507 cycles

FUSELAGE SKIN CRACKED AT BS 356, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,571 hrs · 61,360 cycles

RIGHT OVERWING EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,079 hrs · 60,974 cycles

M1137 EMER EXIT BATTERY PACK INOPERATIVE AT BS 968R. R & R BATTERY PACK IAW AMM.

Part: HINGE — BROKEN (RT SPOILER) · airframe 72,218 hrs · 60,352 cycles

NUMBER 5 GND SPOILER OTBD HINGE BROKEN. R & R SPOILER ASSEMBLY IAW MM.

Part: ATTACH FITTING — MISSING (R2 DOOR) · airframe 71,466 hrs · 59,832 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR FLOOR ATTACH POINTS MISSING. INSTALLED ATTACH POINTS IAW AMM.

Part: ATTACH FITTING — MISSING (L2 DOOR) · airframe 71,466 hrs · 59,832 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR FLOOR ATTACHMENT POINTS MISSING. INSTALLED ATTACHMENT POINTS IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

CHORD CRACKED AT BS 727 BETWEEN STRINGER 18L TO STRINGER 27L. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

CHORD CRACKED AT BS 727 BETWEEN STRINGER 18R & STRINGER 27R. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,438 hrs · 58,360 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75 LBL 7. REPAIRED WEB IAW EO & EA.

Part: FUSE — BLOWN (CABIN) · airframe 69,438 hrs · 58,360 cycles

FWD RT GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. R & R FUSE IAW CMM.

Part: BRACKET — BROKEN (CARGO DOOR) · airframe 69,438 hrs · 58,360 cycles

FWD CARGO COMPARTMENT DOOR HOOK BRACKET BROKEN. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — BROKEN (R2 DOOR) · airframe 69,438 hrs · 58,360 cycles

R2 DOOR EMERGENCY EVAC SLIDE SUPPORT BRACKET BROKEN. R & R BRACKET IAW DRAWING & SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

TIE CLIP CRACKED AT BS 440 STRINGER 2R. R & R TIE CLIP IAW SRM & DRAWING.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 69,438 hrs · 58,360 cycles

LT WING NR 4 FLAP TRACK CRACKED. R & R FLAP TRACK IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 69,438 hrs · 58,360 cycles

LT WING MLG STABILIZER BEAM OTBD AFT CORNER OF ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

TIE CLIP CRACKED AT BS 440 STRINGER 1. R & R TIE CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5 STRINGER 10R. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

SUPPORT ANGLE CRACKED AT BS 360 STRINGER 17L. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

PLATE CRACKED AT BS 344 LBL 48. R & R PLATE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

STIFFENER CRACKED AT BS 1016. REPAIRED STIFFENER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2 LBL 63. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 LBL 61. REPAIRED CHORD IAW EO & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

SHEAR TIE CRACKED AT BS 967 STRINGER 7L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

LINING CUTOUT CRACKED AT BS 992.5 STRINGER 15R. R & R CUTOUT IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

STIFFENER CRACKED AT BS 1016 STRINGER 5R. REPAIRED STIFFENER IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

LINING CRACKED AT BS 332.1 STRINGER 16. REPAIRED LINING IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 LBL 61. REPAIRED CHORD IAW EO & EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

BRACKET CRACKED BETWEEN BS 348.2 TO BS 351.0 STRINGER 16L. R & R BRACKET IAW SRM & DRAWING.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

SKIN ACCESS PANEL CRACKED AT BS 716 BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 9R TO STRINGER 10R. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9 STRINGER 12L. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 11L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5 STRINGER 13R. R & R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

STRAP CRACKED AT BS 302 STRINGER 4L. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 69,438 hrs · 58,360 cycles

RT WING ANGLE CRACKED AT RSS 533+12" FIXED TE. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FUSELAGE SKIN CRACKED AT BS 908 STRINGER 3R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

L1 DOOR CUTOUT REVEAL ANGLE CRACKED AT BS 312. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 12R TO STRINGER 13R. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 11R TO STRINGER 12R. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

WEB CRACKED AT BS 303.9 STRINGER 4L. R & R WEB IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2 LBL 63. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 LBL 59. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FWD ENTRY DOOR REVEAL ANGLE CRACKED AT BS 344 BETWEEN STRINGER 9L TO STRINGER 10L. R & R ANGLE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

STRINGER CRACKED AT BS 1006+4 STRINGER 5R. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,438 hrs · 58,360 cycles

RT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

TIE CLIP CRACKED AT BS 277 STRINGER 10R. R & R TIE CLIP IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FLOOR BEAM CORRODED AT BS 328 BETWEEN LBL 3 TO RBL 16. REPAIRED BEAM IAW SRM.

Part: LENS — DAMAGED (CABIN) · airframe 69,438 hrs · 58,360 cycles

NR 4 GALLEY EMERGENCY EXIT LENS DAMAGED. R & R LENS IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,438 hrs · 58,360 cycles

LT WING NR 1 SLAT SKIN CRACKED BETWEEN STATION 333 TO STATION 348. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

ANGLE CRACKED AT BS 727 BETWEEN STRINGER 22L TO STRINGER 25L. R & R ANGLE IAW SRM & DRAWING.

Part: SLAT — DELAMINATED (RT WING) · airframe 69,438 hrs · 58,360 cycles

RT WING NR 5 SLAT INBD EDGE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,438 hrs · 58,360 cycles

LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 69,438 hrs · 58,360 cycles

NR 1 GALLEY EMERGENCY EXIT LIGHT CRACKED. R & R LIGHT IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 69,438 hrs · 58,360 cycles

FWD LAVATORY EMERGENCY EXIT LENS CRACKED. R & R LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FUSELAGE SKIN CRACKED AT BS 420+3.750 STRINGER 1. REPAIRED SKIN IAW EO & EA.

Part: ACCESS PANEL — CRACKED (LT NACELLE) · airframe 69,438 hrs · 58,360 cycles

LT NACELLE STRUT ACCESS PANEL 5764 CRACKED. REPAIRED PANEL IAW EO & EA.

Part: ACCESS PANEL — CRACKED (LT HORIZ STAB) · airframe 69,438 hrs · 58,360 cycles

LT HORIZONTAL STABILIZER NR 9126 ACCESS PANEL CRACKED. R & R PANEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 69,438 hrs · 58,360 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75+1.5 RBL 24.5+13. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FUSELAGE SKIN CRACKED AT BS 420+14 STRINGER 1. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,438 hrs · 58,360 cycles

LT WING NR 3 SLAT LE SKIN CRACKED. R & R NR 3 SLAT IAW AMM.

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 69,438 hrs · 58,360 cycles

L1 EMERGENCY EXIT DOOR UPPER COVER HANDLE CRACKED. R & R HANDLE IAW AMM.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 69,438 hrs · 58,360 cycles

HORIZONTAL STABILIZER ACCESS PANEL 9226R ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 69,438 hrs · 58,360 cycles

AFT CARGO COMPARTMENT DOOR FRAME LOWER FWD CORNER CRACKED. R & R FRAME IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

CTR WING BOX SUPPORT ANGLE CRACKED AT BS 727 LBL 45.5. R & R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

STRAP CRACKED AT BS 908 STRINGER 3R. R & R STRAP IAW EA & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 705 TO BS 715 LBL 24.8. REPAIRED WEB IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

CHORD CRACKED AT BS 727 BETWEEN STRINGER 18R TO STRINGER 27R. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

FUSELAGE SKIN CRACKED AT BS 420+4 STRINGER 1. REPAIRED SKIN IAW EO & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,438 hrs · 58,360 cycles

CHORD CRACKED AT BS 727 BETWEEN STRINGER 18L TO STRINGER 27L. REPAIRED CHORD IAW EO & EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,240 hrs · 57,438 cycles

EMERGENCY LIGHT BATTERY PACK ASSEMBLY INOPERATIVE. R&R EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,190 hrs · 57,396 cycles

RT AFT EMERGENCY LIGHT INOPERATIVE. R&R BATTERY PACK IAW AMM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 68,182 hrs · 57,388 cycles

PHOTOILLUMINESCENT STRIP ON CABIN FLOOR AT ROW 8 LOOSE. SECURED STRIP IAW AMM.

Part: CAP — CRACKED (LE SLAT) · airframe 67,914 hrs · 57,160 cycles

LEFT WING NR 4 SLAT OTBD TAI DUCT END CAP CRACKED. R & R END CAP IAW AMM.

Part: CAP — CRACKED (LE SLAT) · airframe 67,914 hrs · 57,160 cycles

RT WING NR 6 SLAT OTBD END CAP CRACKED. R & R END CAP IAW AMM.

Part: ACTUATOR — BROKEN (RT SPOILER) · airframe 67,759 hrs · 57,036 cycles

RT WING GROUND SPOILER OUTBOARD ACTUATOR BROKEN. R & R ACTUATOR IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 67,586 hrs · 56,913 cycles

EXTERNAL POWER RECEPTACLE CUTOUT INTERNAL DOUBLER LIP CRACKED. REPAIRED DOUBLER PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,586 hrs · 56,913 cycles

FORWARD RIGHT EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 67,586 hrs · 56,913 cycles

RIGHT WING I/B NO-STEP PANEL O/B ANGLE CRACKED AT THE AFT END. REPAIRED ANGLE PER EA.

Part: RETAINER — CRACKED (RT WING) · airframe 67,586 hrs · 56,913 cycles

RIGHT WING LOWER T/E SEAL RETAINER JUST O/B OF THE NR 2 PYLON CRACKED. REPAIRED RETAINER IAW EA.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 66,814 hrs · 56,363 cycles

NR 8 FLAP SPINDLE IS RUSTED & THERMAL COATING IS MISSING. REMOVED AND REPLACED IAW MT 327-51-08 & MT 327-51-06. P/N OFF:65-46481-145 S/N OFF:B5240R P/N ON:65-46481-155WN S/N ON:B4172R

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 66,210 hrs · 55,915 cycles

VERTICAL STAB STA 127.10 AT REAR SPAR LEFT TRIANGLE STIFFENER CRACKED. (HFEC VERIFIED) REPAIRED GUSSET PER SRM 51-70-11.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 66,210 hrs · 55,915 cycles

VERTICAL STAB STA 127.10 AT REAR SPAR RIGHT TRIANGLE STIFFENER CRACKED (HFEC VERIFIED). REPAIRED GUSSET PER EA1-355-1743 AND SRM 51-70-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,131 hrs · 55,856 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,076 hrs · 55,817 cycles

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

Part: LIGHT — ARCED (CABIN) · airframe 65,971 hrs · 55,741 cycles

ELECTRICAL SMELL IN AFT GALLEY AREA. REMOVED AND REPLACED AFT GALLEY CEILING LIGHT ASSY PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 65,933 hrs · 55,712 cycles

RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE DELAMINATED. REMOVED & REPLACED NR 5 SLAT IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 64,102 hrs · 54,374 cycles

LT WING L/E SKIN CRACKED AT STA 196.8. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

ANGLE CRACKED BETWEEN BS 312 TO BS 328, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

STRINGER CORRODED AT BS 328, STR 28R. REMOVED AND REPLACED STRINGER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

ANGLE CRACKED BETWEEN BS 328 TO BS 344, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REPLACED ANGLE IAW SRM AND DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 64,102 hrs · 54,374 cycles

LT PHOTOLUMINESCENT TRACK LIGHTING DAMAGED. REMOVED AND REPLACED LIGHT IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 500C, STR 26L. REPLACED TIE CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 947.5 S27L) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 947.5, STR 27L. REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 64,102 hrs · 54,374 cycles

LT HORIZONTAL STABILIZER VERTICAL ANGLE CRACKED AT STA 83.5+10. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 64,102 hrs · 54,374 cycles

RT PHOTOLUMINESCENT TRACK LIGHTING DAMAGED. REMOVED AND REPLACED LIGHT IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,102 hrs · 54,374 cycles

EMERGENCY EXIT LIGHT ON WALL FWD LAVATORY AT FWD AREA GALLEY DAMAGED. REMOVED AND REPLACED LIGHT IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW EO AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

SUPPORT ANGLE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 787 S20R) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 787, STR 20R. REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 64,102 hrs · 54,374 cycles

LT WING CRACKED ON SUPPORT ANGLE AT WS 537.806. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

FLOORBEAM UPPER CHORD LOWER SURFACE CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

STRINGER SPLICE CRACKED AT BS 360, 15L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 727A S26L) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP IAW RM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 787 TO BS 807, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REPLACED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 727A S26R) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 26R. REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767, STR17L. REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 400, STR 27L. REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 727A S25L) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 25L. REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 727C TO BS 727D, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26R. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (BS 294.5 S10L) · airframe 64,102 hrs · 54,374 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 400, STR 25R. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 420, STR 22L. REPLACED CLIP CRACK IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 420 S21L) · airframe 64,102 hrs · 54,374 cycles

STRINGER CLIP CRACKED AT BS 420, STR 21L. REPLACED STRINGER CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 400, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

SKIN CRACKED AT BS 951, BETWEEN STR 14L TO STR 15L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

FRAME INNER CHORD CRACKED AT BS 616 AND WEB, STR 17R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 500B, STR 25L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

FRAME INNER CHORD CRACKED AT BS 616, BETWEEN STR 15R AND 18R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, RBL 24.5. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 520, STR 22L. REPLACED TIE CLIP IAW SRM AND DWG AND SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

TIE CLIP CRACKED AT BS 420, STR 23L. REPLACED TIE CLIP IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,102 hrs · 54,374 cycles

L2 DOOR FRAME STRUCTURE CRACKED AT THE LOWER HINGE AREA. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — DELAMINATED (CABIN) · airframe 63,649 hrs · 54,050 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS DELAMINATED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 63,064 hrs · 53,621 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 60,493 hrs · 51,655 cycles

AIR TURNBACK, AT 5,000 FT DESCENDING TO HOU THE PRESSURE CONTROLLER GAVE AUTO FAIL AND STANDBY LIGHT. REMOVED AND REPLACED PRESSURE CONTROL PANEL PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,568 hrs · 50,967 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,783 hrs · 50,357 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,783 hrs · 50,357 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 671, LBL 24.5. REPAIRED BEAM PER AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 58,782 hrs · 50,357 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING I/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,783 hrs · 50,357 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,783 hrs · 50,357 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,849 hrs · 49,675 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,035 hrs · 48,311 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LOWER LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT UPPER LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 17, LT SIDE. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,035 hrs · 48,311 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21, RT SIDE. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 360, STR 16R. REPAIRED SKIN PER ER.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND DOUBLER CORRODED BETWEEN BS 987 TO BS 1008, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED DOUBLER PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 729A TO BS 737A, STR 14R. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 897, STR 14L. REPAIRED STRINGER PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, STINGER CLIP CRACKED AT BS 787, STR 22R. R&R CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 360, BETWEEN STR 3R TO STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 360, BETWEEN STR 3L TO STR 4L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 16L TO STR 17L. R&R SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 22L. R&R CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. R&R CLIP PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 24L. R&R CLIP PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 14R TO STR 15R. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER WA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER WA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REPAIRED CLIP PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,035 hrs · 48,311 cycles

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

Part: GASPER FAN — FAULTY (CABIN) · airframe 55,128 hrs · 47,678 cycles

DURING DESCENT THERE WAS A STRONG SULPHER SMELL. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,502 hrs · 47,240 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR SIDEWALL LAMP INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LENS — MISSING (CABIN) · airframe 54,502 hrs · 47,240 cycles

FOUND LT OVERWING EMERGENCY EXIT LENS MISSING. REPLACED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,948 hrs · 46,857 cycles

DURING SCHEDULED MV2 CHECK, FOUND LOWER LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 55. REPAIRED CHORD PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT FWD END. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, RBL 12 TO RBL 48. R&R CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,438 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, BL0 TO RBL 3, WL 148. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,437 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, BETWEEN BL 0 AND RBL 3. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,437 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,437 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,437 hrs · 46,469 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,437 hrs · 46,469 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,286 hrs · 46,352 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,277 hrs · 46,348 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,646 hrs · 45,888 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 24L. REPAIRED SKIN PER SWA EA.

Part: TORQUE TUBE — FAILED (RT ELEVATOR) · airframe 50,360 hrs · 44,149 cycles

DURING SCHEDULED BRDG CHECK, LT AND RT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: PANEL — CRACKED (BS 714) · airframe 50,360 hrs · 44,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM STRESS PANEL CRACKED AT BS 714, STR 27R. REPAIRED PANEL PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 50,359 hrs · 44,148 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STAB FITTING FWD AND AFT CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER ER.

Part: SKIN — DELAMINATED (NR 7 SPOILER) · airframe 50,359 hrs · 44,148 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 7 SPOILER DELAMINATED AT UPPER SURFACE. REPAIRED SPOILER PER SRM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 49,121 hrs · 43,217 cycles

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

Part: HINGE FITTING — BROKEN (LT WING SPOILER) · airframe 48,956 hrs · 43,104 cycles

DURING SCHEDULED A1 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: BOLT — CORRODED (LT MLG) · airframe 48,476 hrs · 42,717 cycles

DURING SCHEDULED SPV CHECK, FOUND LT MLG TEE BOLT ASSY CORRODED. REMOVED AND REPLACED TEE BOLT ASSY PER MM.

Part: BOLT — CRACKED (LT MLG) · airframe 48,476 hrs · 42,717 cycles

DURING SCHEDULED SPV CHECK, FOUND LT MLG TEE BOLT FITTING CRACKED. REMOVED AND REPLACED TEE BOLT FITTING PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,476 hrs · 42,717 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,883 hrs · 41,466 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 46,883 hrs · 4,166 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,059 hrs · 40,847 cycles

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

Part: SKIN — CRACKED (BS 291) · airframe 46,024 hrs · 40,819 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, BETWEEN STR 13R TO STR 14R. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 46,016 hrs · 40,808 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS DISCOLORED. REMOVED AND REPLACED LENS PER MM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 46,016 hrs · 40,808 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD WEB CRACKED BETWEEN LBL 15 TO RBL 10, WL 218. REPAIRED WEB PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 45,421 hrs · 40,310 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 44,903 hrs · 39,901 cycles

EEPLS TRACK COVER MISSING AT ROW 17 ABC. INSTALLED COVER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,494 hrs · 39,581 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,494 hrs · 39,581 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, STR 10R. REPAIRED SKIN PER SWA EA.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,380 hrs · 39,485 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,061 hrs · 39,223 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY SERVICE DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FUSELAGE CUTOUT AT LOWER AFT CORNER, FUSELAGE CRACKED. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT, LOWER FWD STOP FITTING, WEB DOUBLER CRACKED AT BS 303.9, STRINGER 16L. REMOVED AND REPLACED FRAME CUTOUT WEB DOUBLER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN, CRACKED. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME LOWER SECTION CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM AND BAC DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP AT BS 1016, RBL 1, CRACKED. REPAIRED BULKHEAD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 37,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, FLOORBEAM LT ATTACH POINT CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 41,887 hrs · 37,520 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LT SIDE WEB CRACKED AT BS 203.8. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,334 hrs · 37,055 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR CUTOUT WEB BELOW THE UPPER HINGE, CRACKED. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,334 hrs · 37,055 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 523, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,460 hrs · 36,332 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,460 hrs · 36,332 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COMPARTMENT EQUIPMENT COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,475 hrs · 35,561 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,588 hrs · 34,839 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, ABOVE STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,588 hrs · 34,839 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 38,588 hrs · 34,839 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVACUATION SLIDE RELEASE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,728 hrs · 34,133 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 35,290 hrs · 32,192 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,846 hrs · 31,009 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, WL 160 AND RBL 36. REPAIRED FRAME PER BFG ER.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 987, WL 208 AND LBL 21.5 TO 25.5. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8L AND 9L, AT BS'S 400, 440 AND 480. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED BETWEEN STR'S 8R AND 9R, AT BS'S 360, 400 AND 440. REPAIRED FRAMES PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 AND S-3. REPAIRED CHORD PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,002 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,845 hrs · 31,008 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER MM.

Part: LENS — MISSING (CABIN) · airframe 33,734 hrs · 30,916 cycles

EEPLS RED LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 32,342 hrs · 29,793 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: CONTROLLER — FAULTY (MLG W/W) · airframe 31,632 hrs · 29,189 cycles

AILERONS HEAVY AND WOULD NOT RETURN TO NORMAL. REMOVED AND REPLACED SPOILER MIXER AND AILERON CENTERING CAM BEARING PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 31,563 hrs · 29,129 cycles

DURING SCHEDULED C4 CHECK, FOUND TWO EEPLS INOP AT OVERWING EXIT. SECURED WIRES PER MM.

Part: TRACK — BROKEN (CABIN) · airframe 31,515 hrs · 29,083 cycles

EEPLS LENS MISSING AT MID CABIN AND FLOOR TRACK BROKEN. REMOVED AND REPLACED EEPLS LENS AND FLOOR TRACK SEGMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,939 hrs · 28,590 cycles

EEPLS INOP AT OVERWING EXIT. REPAIRED EEPLS PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 30,895 hrs · 28,548 cycles

EEPLS INOP & COVER BROKEN AT ROW 12. R&R EEPLS COVER & RELAMPED PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,659 hrs · 27,535 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CREASES, 5 TO 6 INCHES LENGTH, AT BS 440 & 470, BETWEEN STR 25R & 26R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,651 hrs · 27,529 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS LOOSE THROUGHOUT CABIN. INSTALLED EEPLS SPACERS PER MM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 29,559 hrs · 27,449 cycles

EEPLS DAMAGED. REPAIRED DAMAGED EEPLS CONNECTIONS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,548 hrs · 27,441 cycles

EEPLS WIRING EXPOSED AND BULBS INOP AT ROW 11 &12. SECURED EEPLS TRACK AND RELAMPED 2 BULBS PER MM.

Part: LENS — MISSING (CABIN) · airframe 29,485 hrs · 27,386 cycles

EEPLS LENS MISSING AT OVERWING EXIT. REMOVED AND REPLACED TRACK COVER ASSY PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 29,347 hrs · 27,279 cycles

EEPLS WIRING EXPOSED AT MID CABIN. REINSTALLED EEPLS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 28,843 hrs · 26,867 cycles

EEPLS DAMAGED AT OVERWING EXIT. R&R EEPLS TRACK COVER PER MM.

Part: ACTUATOR — FAILED (LT MLG) · airframe 28,798 hrs · 26,824 cycles

DECLARED EMERGENCY DURING APPROACH, LT MLG DID NOT EXTEND FULLY AND RED UNSAFE LIGHT ILLUMINATED. EXTENDED GEAR MANUALLY, ALL GEAR LIGHTS SHOWED GREEN. MX FERRY TO MDW, R&R LT MLG ACTUATOR.

Part: LIGHT — MISSING (CABIN) · airframe 28,791 hrs · 26,818 cycles

EEPLS LENS & BULB MISSING AT OVERWING EXIT. R&R LENS & BULB PER MM.

Part: BULB — BURNED OUT (CABIN) · airframe 28,360 hrs · 26,480 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 15A. RELAMPED AND RECONNECTED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (ROW 9 - 16) · airframe 27,731 hrs · 25,944 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT ROWS 9 - 16. RECONNECTED EEPLS WIRES PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 27,238 hrs · 25,522 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (CABIN)

EEPLS WIRING SHOWING AT ROW 12. REPOSITIONED WIRING UNDER TRACK COVER PER MM.

Part: FIRE DETECTOR — MALFUNCTIONED (APU BAY)

AIR TURNBACK/DECLARED EMERGENCY. APU FIRE LIGHT ILLUMINATED JUST AFTER TAKEOFF. PULLED FIRE HANDLE AND DISCHARGED FIRE BOTTLE. INSPECTED APU. NO INDICATION OF FIRE FOUND. DEFERRED APU.

Part: SLIDE — LOOSE (CABIN)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 SIDE CHORD CRACKED, RBL 26. REPAIRED CHORD PER SRM.

Part: LIGHT — INOP (ROWS 23/24)

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROWS 23 AND 24. REPAIRED LIGHT WIRES PER MM.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD FLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: COVER — MISSING (ROW 11)

EEPLS TRACK COVER MISSING AT ROW 11. REPLACED COVER ASSY PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED, AND LATER ON FELL OUT OF THE CONTAINER IN SLC. REMOVED AND REPLACED SLIDE ASSY, AND REINSTALLED SLIDE ASSY AT SLC PER MM.

Part: LIGHT — INOPERATIVE (ROW 18ABC)

EMERGENCY EXIT LIGHT INOP AT ROW 18 ABC. REPAIRED CONNECTOR PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND AFT SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK AND HOUSING ASSY.

Part: LAMP — INOP (ROW 18 ABC)

DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY TRACK LIGHT INOP AT ROW 18ABC. RELAMPED PER BOEING MM.

Part: LAMP — INOP (ROW 18ABC)

DURING SCHEDULED BC2 CHECK, FOUND CABIN EMEGENCY TRACK LIGHTING INOP AT SEAT ROW 18ABC. RELAMPED PER BOEING M/M.

Part: WARNING — ACTIVATED (SPEED BRAKES)

AIRCRAFT ABORTED TAKEOFF. INFO ONLY TAKEOFF POWER ADVANCED AND T/O WARNING HORN SOUND. SPEED BRAKE HANDLE CYCLED AND WARNING HORN DID NOT RETURN. ALL SYSTEMS CHECKED NORMAL.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FWD POST OF FWD GALLEY DOOR FRAME CRACKED AT FWD CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 219.8/927)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 219.8 AND AT BS 927, BETWEEN S24 AND 23L. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (SERV DOOR STOP)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD SERVICE DOOR RT FWD ANGLE CRACKED FWD OF NR 2 DOOR STOP BELOW S10R. REPAIRED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PACK PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

AT GATE, FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.