N358SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,615 hrs · 63,982 cycles

SKIN CRACKED BETWEEN BS 478.5 TO BS 478.7, BETWEEN STR 3R TO STR 2R. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 76,105 hrs · 63,595 cycles

R1 DOOR EXIT SIGN LIGHT LENS BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 75,715 hrs · 63,346 cycles

L1 DOOR EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 75,698 hrs · 63,335 cycles

L1 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

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

Part: HINGE — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

R1 DOOR LOWER HINGE STRUCTURE CRACKED. R & R HINGE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 7R. R & R CLIP IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STRINGER CLIP CRACKED AT STATION 348.2, STRINGER 16L. R & R CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FUSELAGE FRAME CORRODED AT STATION 360, BETWEEN STRINGER 28L & 28R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

SHEAR TIE CORRODED AT STATION 360, BETWEEN STRINGER 27R & 28R. REPAIRED SHEAR TIE IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

AFT PIT STRAP ON TOP OF FRAME CORRODED, AT BS 847, STRINGER 26R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FRAME CRACKED AT BS 291.5, STRINGER 10R. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

AFT PIT FRAME CORRODED AT BS 747, BETWEEN STRINGER 27L - 26L. REPAIRED FRAME IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

RIGHT CREASE BEAM CRACKED AT STATION 616. REPAIRED CREASE BEAM IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

CLIP CRACKED AT BS 908, STRINGER 1L. R & R CLIP IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

AFT CARGO DOOR THRESHOLD WEB CORRODED AT STATION 794 - 847. REPAIRED WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STRINGER SPLICE CRACKED AT STATION 360, STRINGER 4R. R & R SPLICE IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 23R. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STRINGER SPLICE CRACKED AT STATION 360, STRINGER 3R. R & R SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 6L. R & R SPLICE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

CLIP CRACKED AT BS 908, STRINGER 1R. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FORWARD GALLEY SERVICE DOOR CUT OUT UPPER FWD CORNER SKIN CRACKED, BETWEEN BS 277 - 313, BETWEEN STRINGER 6R - 15R. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FLOOR SUPPORT CORRODED AT STATION 950 - 990, WL 208. R & R SUPPORT IAW SRM.

Part: BRACKET — WORN (R2 DOOR) · airframe 75,252 hrs · 63,058 cycles

R2 DOOR SLIDE MOUNTING NUTPLATE FWD & AFT WORN. R & R BRACKETS IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

STIFFENER CRACKED AT MAIN CABIN BELOW FLOOR, AT STATION 727, RBL 46. R & R STIFFENER IAW SRM.

Part: BRACKET — WORN (L2 DOOR) · airframe 75,252 hrs · 63,058 cycles

L2 DOOR SLIDE MOUNTING NUTPLATE FWD & AFT AREA WORN. R & R BRACKET ASSEMBLY IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FUSELAGE FRAME CRACKED AT STATION 500D, STRINGER 20L - 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FORWARD CARGO PIT FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L - 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,252 hrs · 63,058 cycles

FUSELAGE FRAME CRACKED AT STATION 500D, BETWEEN STRINGER 20L & 21L. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 75,252 hrs · 63,058 cycles

MAIN WW PRESS DESK WEB CRACKED, AT BS 673.25, LBL 30.50. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,105 hrs · 62,952 cycles

FUSELAGE SKIN CRACKED AT BS 500B+3, STRINGER 2R. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,879 hrs · 62,795 cycles

R2 DOOR FWD FUSELAGE CUT OUT FRAME CRACKED. R & R FRAME IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 74,630 hrs · 62,594 cycles

LEFT HORIZONTAL STABILIZER LOWER SURFACE, INSPAR SKIN CRACKED, BETWEEN FASTENERS AT REPAIR SPAR STABILIZER STATION 89. REPAIRED SKIN IAW EA.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 74,580 hrs · 62,560 cycles

AFT PRESS BULKHEAD CREASED AT BS 1016+4, BETWEEN RBL 1 TO LBL 1. REPAIRED BULKHEAD IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 74,580 hrs · 62,560 cycles

FORWARD PRESSURE BULKHEAD LOWER STRAP CORRODED AT BS 1016, BETWEEN STRINGER 27L - 27R. REPAIRED STRAP IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 74,580 hrs · 62,560 cycles

AFT CARGO BAY, FWD FRAME STRAP CORRODED AT BS 1003, STRINGER 27R. REPAIRED STRAP IAW SRM & EA.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 74,580 hrs · 62,560 cycles

PRESSURE WEB SKIN CORRODED AT BS 1016, BETWEEN STRINGER 26L - 27L. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,580 hrs · 62,560 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,571 hrs · 62,554 cycles

LEFT OVERWING EMER EXIT AISLE LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 74,396 hrs · 62,434 cycles

FRONT RT EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 74,094 hrs · 62,219 cycles

FORWARD ENTRY DOOR EXIT SIGN COVER BROKEN. REPAIRED COVER IAW SIP.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,961 hrs · 62,123 cycles

LEFT WING OTBD AFT FLAP DELAMINATED APPROX 78" FROM OTBD EDGE. R & R AFT FLAP IAW AMM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 73,228 hrs · 61,557 cycles

AIR TURN BACK LE FLAP TRANSIT LIGHT ILLUMINATED. NR 1 SLAT TRANSIT LIGHT ILLUMINATED ON OVERHEAD PANEL. DURING LANDING LIGHT EXTINGUISHED WHEN SELECTING BETWEEN FLAPS 5 - 15. R & R NR 1 SLAT ACTUATOR IAW MM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 73,228 hrs · 61,557 cycles

AIR TURN BACK LE FLAP TRANSIT LIGHT ILLUMINATED. NR 1 SLAT TRANSIT LIGHT ILLUMINATED ON OVERHEAD PANEL. DURING LANDING LIGHT EXTINGUISHED WHEN SELECTING BETWEEN FLAPS 5 - 15. R & R NR 2 SLAT ACTUATOR IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 73,219 hrs · 61,546 cycles

LEFT WING NR 1 SLAT UPPER OTBD TE DELAMINATED. R & R NR 1 SLAT IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,219 hrs · 61,546 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,219 hrs · 61,546 cycles

LEFT WING OTBD FORE FLAP TE DELAMINATED. R & R FORE FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,219 hrs · 61,546 cycles

RIGHT EMER EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT ASSEMBLY IAW MM.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 72,435 hrs · 60,990 cycles

AFT EMER FLASHLIGHT INOPERATIVE. RESEATED FLASHLIGHT IN BASE IAW SIP.

Part: LENS — BROKEN (EXIT SIGN) · airframe 72,358 hrs · 60,939 cycles

L1 DOOR SLIDE EMER EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,751 hrs · 59,075 cycles

LT EMERGENCY EXIT DOOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

SUPPORT TEE CHORD ANGLE CRACKED AT BS 540, LT AIR CONDITIONING BAYS COMPARTMENT. R & R ANGLE IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 69,751 hrs · 59,075 cycles

AFT CARGO DOOR CROSS BEAM CRACKED AT AFT END. REPAIRED BEAM IAW SWA EA.

Part: LIGHT — CRACKED (CABIN) · airframe 69,751 hrs · 59,075 cycles

AFT EEPLS CRACKED. R & R EEPLS IAW AMM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 69,751 hrs · 59,075 cycles

LT WING FLAP TRACK FAIRING BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

BUTT STRAP CRACKED AT BS 360, STRINGER 4R. R & R BUTT STRAP IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 69,751 hrs · 59,075 cycles

AFT CARGO DOOR FWD END OF THE CROSS BEAM AT THE T CHORD CRACKED. REPAIRED T CHORD IAW EA & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FUSELAGE FRAME OUTER CHORD CRACKED APPROXIMATELY STATION 348.2, STRINGER 16L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FUSELAGE FRAME CRACKED AT STATION 348.2 INNER CHORD, STRINGER 17L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FUSELAGE FRAME OUTER CHORD CRACKED APPROXIMATELY STATION 348.2, 0.5 INCHES. BELOW STRINGER 16L. REPAIRED FRAME IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

SKIN CRACKED AT BS 360, BETWEEN STRINGER 3L TO STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

MAIN WW SUPPORT ANGLE TEE CRACKED AT BS 727, BETWEEN STRINGER 21R TO STRINGER 26R. R & R TEE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

ANGLE CRACKED BETWEEN BS 887 TO BS 907. R & R ANGLE IAW SRM & DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, BL 0. REPAIRED CHANNEL IAW EA.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

L1 DOOR CUTOUT RETAINER FWD LOWER CORNER CRACKED. R & R RETAINER IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FUSELAGE FRAME CRACKED AT STATION 348.2, STRINGER 17L. REPAIRED FRAME IAW SWA EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 15R. R & R TIE CLIP IAW SRM & DRAWING.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

L1 DOOR CUTOUT RETAINER FWD UPPER CORNER CRACKED. R & R RETAINER IAW SRM & DRAWING.

Part: BRACKET — BROKEN (TE FLAP) · airframe 69,751 hrs · 59,075 cycles

RT WING INBD MIDFLAP BRACKET BROKEN. R & R BRACKET ASSEMBLY IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FUSELAGE FRAME CRACKED AT STATION 951, STRINGER 6R. REPAIRED FRAME IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 947.5, LBL 52.5. REPAIRED CHORD IAW EA.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

L1 DOOR CUTOUT RETAINER CRACKED BETWEEN STRINGER 8L TO STRINGER 9L. R & R RETAINER IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

STRAP CRACKED BETWEEN BS 294.5 TO BS 312, STRINGER 4L. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

FWD ENTRY DOOR CUTOUT ANGLE CRACKED AT BS 312, STRINGER 15L. R & R ANGLE IAW SRM & DRAWING.

Part: PANEL — CRACKED (NLG WW) · airframe 69,751 hrs · 59,075 cycles

NLG WW PANEL CRACKED AT BS 243.7+2.5, RBL 16. REPAIRED PANEL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 69,751 hrs · 59,075 cycles

LT WING SUPPORT ANGLE CRACKED AT TE WING STATION 537.806. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

WEB CRACKED BETWEEN BS 947.5 TO BS 967, LBL 21. R & R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

LT NLG WW WEB CRACKED AT BS 259, WL 169.1+8.5. REPAIRED WEB IAW SRM.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

L1 DOOR CUTOUT AFT LOWER CORNER RETAINER CRACKED. R & R RETAINER IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 312, STRINGER 4L. R & R WEB IAW SRM & DRAWING.

Part: PANEL — CRACKED (NLG WW) · airframe 69,751 hrs · 59,075 cycles

NLG WW PANEL CRACKED AT BS 243+3.5, RBL 16. REPAIRED PANEL IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

WEB CRACKED LOCATED BETWEEN BS 348.2 TO BS 351.2, STRINGER 16L. R & R WEB IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 12. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 69,751 hrs · 59,075 cycles

RT WING SUPPORT ANGLE CRACKED BETWEEN RSS 517 TO RSS 534. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

SKIN CRACKED AT BS 362, STRINGER 1R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

R1 DOOR UPPER HINGE CUTOUT SKIN CRACKED AT BS 947.5, STRINGER 11R. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,751 hrs · 59,075 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+1, BETWEEN RBL 45.5 TO RBL 24.5. REPAIRED DECK IAW SRM.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 69,751 hrs · 59,075 cycles

LT MAIN WW CHORD CRACKED AT BS 680.75. R & R CHORD IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

LT SIDE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,751 hrs · 59,075 cycles

RT SIDE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,751 hrs · 59,075 cycles

LT WING LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,612 hrs · 58,975 cycles

FRAME CRACKED AT BS 500B BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW SWA EA.

Part: LENS — BROKEN (CABIN) · airframe 69,004 hrs · 58,552 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,889 hrs · 57,698 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 67,889 hrs · 57,698 cycles

LEFT EMERGENCY LIGHT LENS COVER LOOSE AT ROW 21. SECURED COVER IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,374 hrs · 57,343 cycles

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

Part: BALLAST — INOPERATIVE (CABIN) · airframe 67,022 hrs · 57,089 cycles

LEFT EMERGENCY OVERWING EXIT SIDEWALL LIGHT IS INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,022 hrs · 57,089 cycles

A 1.2 INCH CRACK LOCATED AT BS 500D+10 RIGHT SIDE OF STR 1. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,646 hrs · 56,823 cycles

LEFT OTBD AFT FLAP IS SEPARATED ON T/E OTBD CORNER. REPAIRED LEFT OTBD T/E OTBD CORNER IAW SRM 51-70-10- 2R-0.

Part: CASTING — BROKEN (SPOILER) · airframe 66,207 hrs · 56,515 cycles

RIGHT WING NR 5 GROUND SPOILER UPPER ACTUATOR HINGE BEARING CASTINGS BROKEN. REMOVED AND REPLACED NR 5 GROUND SPOILER PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,179 hrs · 56,490 cycles

FUSELAGE SKIN CRACKED AT BS 430+3, STR 1. REPAIRED SKIN IAW AAR EA AND EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,036 hrs · 54,883 cycles

DAMAGED EEPLS TRACK LIGHTING. REPLACED EEPLS IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,036 hrs · 54,883 cycles

LT WING I/B FORE FLAP UPPER SKIN I/B END DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP LOCATED BS 380 AT LEVEL STR 26L IN E/E COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP AT BS 867, STR 23L AFT CARGO COMPARTMENT CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: STRUCTURE — CRACKED (RT WING) · airframe 64,036 hrs · 54,883 cycles

RT WING CRACKED ON UPPER CHORD LOCATED AT WBL 114, STR 2. REPAIRED CHORD IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP LOCATED BS 787 AT LEVEL STR 23R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP LOCATED AT BS 867 STR 21L AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP LOCATED AT BS 727D AND STR 23L AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP AT BS 847, STR 23L AFT CARGO COMPARTMENT CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP LOCATED BS 787 AT LEVEL SRT 20R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP AT BS 827, STR 22L AFT CARGO COMPARTMENT CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK TIE CLIP LOCATED BS 787 AT LEVEL STR 21R IN AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26L. REPAIRED TIE CLIP IAW EO AND EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON STIFFENER AT BS 727, STR 27L AFT CARGO COMPARTMENT. REPLACED STIFFENER IAW BAC DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP BS 727A, STR 26L AFT CARGO COMPARTMENT. REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 64,036 hrs · 54,883 cycles

LEFT WING CRACKED ON UPPER CHORD LOCATED AT WBL 114, STR 2. REPAIRED CHORD IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP AT BS 827, STR 23L AFT CARGO COMPARTMENT CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN’T FIND ORIGINAL CONTROL NUMBER.)

Part: STRINGER CLIP — CRACKED (BS 947.5 S25R) · airframe 64,036 hrs · 54,883 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REPLACED TIE CLIP IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON TIE CLIP AT BS 727C STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON ATTACHMENT CLIP BS 360, STR 10L FWD CABIN. REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

WEB CRACKED AT BS 710, LBL 3. REPLACED WEB IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,036 hrs · 54,883 cycles

LT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON ATTACHMENT CLIP AT BS 639 AND RBL 45.5 LONGITUDINAL FLOORBEAM. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON STUB FRAME AT BS 294.5, STR 10R INTERNAL CUT OUT FWD GALLEY DOOR. REPLACED STUB FRAME LOCATED IAW SRM AND DWG.

Part: SKIN — CRACKED (BS 294.5 S17R) · airframe 64,036 hrs · 54,883 cycles

R1 DOOR CUTOUT CRACKED ON EXTERNAL SKIN AT BS 294.5, STR 17R. REPAIRED EXTERNAL SKIN IAW SRM AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

SHEAR TIE CRACKED AT BS 597, STR 17R. REMOVED AND REPLACED SHEAR TIE IAW SRM, DWG, AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON EXTERNAL FUSELAGE WINDOW SKIN AT BS 211.8, STR 9L. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON STRAP LOCATED BETWEEN BS 312 TO BS 328 LBL 45.6. REPLACED STRAP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,036 hrs · 54,883 cycles

CRACK ON LONGITUDINAL FLOORBEAM AT BS 660 AND RBL 0.07 UPPER CHORD. REPAIRED CHORD IAW SI.

Part: LENS — OUT OF POSITION (CABIN) · airframe 63,915 hrs · 54,800 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LENS PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 63,515 hrs · 54,501 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,000 hrs · 54,103 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 414, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,000 hrs · 54,103 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,198 hrs · 52,723 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 170. REMOVED AND REPLACED SKIN PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,198 hrs · 52,723 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 170. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,329 hrs · 52,070 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 727D, STR 27L. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,471 hrs · 51,406 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,471 hrs · 51,406 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 58,889 hrs · 50,955 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,875 hrs · 50,942 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 57,946 hrs · 50,257 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: SPOILER — CRACKED (LT WING) · airframe 57,946 hrs · 50,257 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING T/E NR 4 GROUND SPOILER CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: TAB — DELAMINATED (AILERON) · airframe 57,946 hrs · 50,257 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING AILERON TAB DELAMINATED AT AFT CORNER. REPAIRED TAB PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,946 hrs · 50,257 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER SURFACED CRACKED. REMOVED AND REPLACED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,946 hrs · 50,257 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL L ANGLE CRACKED AT FWD SIDE OF FRAME BS 727B. REPAIRED L ANGLE PER SRM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 57,904 hrs · 50,230 cycles

DIVERSION, AT FLT 370 CABIN ALT WARNING HORN SOUNDED, CABIN ALT SHOWED 10,000FT. IN MANUAL MODE CABIN CONTINUED CLIMB TO 12, 000 FT. EMERGENCY DESCENT INITIATED. REMOVED AND REPLACED MAIN OUTFLOW VALVE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,234 hrs · 49,743 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,189 hrs · 49,708 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,189 hrs · 49,708 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER CORNER CUTOUT. REPAIRED SKIN PER AAR EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,189 hrs · 49,708 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS INOP BETWEEN ROW 15 TO ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,189 hrs · 49,708 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (TE FLAP) · airframe 57,189 hrs · 49,708 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE SKIN CRACKED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,150 hrs · 49,676 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 55,780 hrs · 48,685 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 55,718 hrs · 48,638 cycles

DECLARED EMERGENCY. ON DESCENT FL 260, CABIN ALTITUDE WARNING, HORN SOUNDED. MASKS MANUALLY DEPLOYED. NO WARNING INDICATIONS. DESCENDED TO 10,000 IN MANUAL CONTROL. REMOVED AND REPLACED PRESSURE CONTROLLER, PRESSURE CONTROL PANEL AND PERFORMED PACK CONFIDENCE CHECK, ALL OPS CHECK GOOD PER MM.

Part: STRIP — WORN (CABIN) · airframe 54,986 hrs · 48,123 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 8. R&R EEPLS PER MM.

Part: STRIP — WORN (CABIN) · airframe 54,986 hrs · 48,123 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: ATTACH BRACKET — LOOSE (L1 DOOR) · airframe 54,986 hrs · 48,123 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR AFT SLIDE ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: STRIP — WORN (CABIN) · airframe 54,986 hrs · 48,123 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 18. REMOVED AND REPLACED EEPLS PER MM.

Part: STRIP — WORN (CABIN) · airframe 54,986 hrs · 48,123 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 21. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 53,941 hrs · 47,364 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,600 hrs · 47,118 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 2L. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 32 TO RBL 41. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, BL 0 TO RBL 4. REPAIRED CHORD PER SRM.

Part: SLAT — DEBONDED (RT WING) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND RH WING #6 L/E SLAT INBOARD END DISBONDED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER ER.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, RBL 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, LBL 3 TO RBL 1. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,393 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 447, RBL 1. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (BS 380 S15L) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 855 S14L) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 14L CRACKED AT BS 855. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (BS 500) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BETWEEN LBL 1 AND RBL 4, WL 148. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (BS 188) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 188, RBL 10. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 312, LBL 13 TO RBL 13. REMOVED AND REPLACED CHORD PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S14L) · airframe 53,392 hrs · 46,960 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 344, LBL 29 TO RBL 2. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 11L. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 947.5, STR 4L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1016, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,392 hrs · 46,960 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,282 hrs · 46,875 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 25L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 52,771 hrs · 46,512 cycles

EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 6 DEF. INSTALLED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,638 hrs · 46,404 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732E AND BS 727E, STR 21L AND STR 22L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,339 hrs · 45,391 cycles

FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ENGINE — DAMAGED (NR 1) · airframe 50,519 hrs · 44,735 cycles

INFLIGHT SHUTDOWN / AIRTURN BACK / DECLARED EMERGENCY. NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMB. PER QRH REDUCED POWER, OIL LIGHT STILL INTERMITTENT, SHUT DOWN ENGINE PER QRH. FOUND FOD AT OIL SCAVENGE FILTER. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,066 hrs · 44,372 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 50,014 hrs · 44,331 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LIGHT — DIRTY (FUSELAGE) · airframe 50,002 hrs · 44,320 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. CLEANED LIGHT SOCKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,002 hrs · 44,320 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 204 LT SIDE. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,002 hrs · 44,320 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 204 RT SIDE. REPAIRED FRAME PER SRM.

Part: CONTROL ROD — WORN (LT AILERON) · airframe 50,002 hrs · 44,320 cycles

DURING SCHEDULED 14Y CHECK, LEFT AILERON FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED LEFT AILERON CONTROL ROD ASSY.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 49,683 hrs · 44,064 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 49,653 hrs · 44,041 cycles

LT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 49,612 hrs · 44,011 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BOLT AND SPACER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,019 hrs · 42,782 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOUSING — FAULTY (BATTERY PACK) · airframe 47,833 hrs · 42,628 cycles

AFT CABIN EMERGENCY EXIT LIGHTS FLASHED INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED AFT BATTERY HOUSING PER MM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 47,821 hrs · 42,621 cycles

AFT CABIN EMERGENCY EXIT LIGHTS INTERMITTENT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEARING — WORN (T/E FLAP) · airframe 47,489 hrs · 42,361 cycles

NOISE AND VIBRATION SENSED AT MID CABIN DURING FLAP RETRACTION AND EXTENSION, BETWEEN FLAP POSITION 1 AND FLAP POSITION 10. REMOVED AND REPLACED LT INBOARD FORE FLAP INBOARD ROLLER BEARINGS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,342 hrs · 42,241 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT LT LOWER FUSELAGE. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 46,890 hrs · 41,916 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 46,013 hrs · 41,250 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVE AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (BS 944) · airframe 45,486 hrs · 40,852 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FWD CARGO) · airframe 45,486 hrs · 40,852 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,864 hrs · 40,333 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STRIP — WORN (EMERGENC LIGHT) · airframe 44,864 hrs · 40,333 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK STRIP WORN AT ROW 23 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 44,455 hrs · 39,995 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,016 hrs · 39,653 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378, LBL 2. REPAIRED SKIN PER SWA EA.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 43,090 hrs · 38,909 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED UPPER & LOWER BUSHINGS, PUSHROD BOLT & TAB MECHANISM LINKS PER MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,682 hrs · 38,587 cycles

DURING SCHEDULED RON, FOUND FLOOR PANEL SUPPORT ANGLE AT BS 270, FROM LBL 9.5 TO RBL 9.5, CORRODED. REPAIRED FLOOR SUPPORT PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,670 hrs · 38,578 cycles

DURING SCHEDULED RON, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET HAS A CRACK AT RADIUS. REMOVED AND REPLACED NLG GUSSET FITTING PER SRM.

Part: CABLE — MISROUTED (L2 DOOR GIRT BAR) · airframe 42,094 hrs · 38,140 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,572 hrs · 37,715 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,572 hrs · 37,715 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER HINGE, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,572 hrs · 37,715 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 732E TO 735E, STRINGER 25L AND BS 742E TO 745E, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 727E) · airframe 41,572 hrs · 37,715 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, BETWEEN LBL 3 TO RBL 8 CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,572 hrs · 37,715 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727E, LBL 14, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: TIRE — BLOWN (RT MLG) · airframe 40,803 hrs · 37,072 cycles

AIR TURNBACK / DECLARED EMERGENCY. NR 3 MAIN TIRE BLEW ON TAKEOFF. BLOWN TIRE DAMAGED RT WING INBOARD, GROUND SPOILER, INBOARD MID FLAP, INBOARD FORE FLAP, INBOARD T/E FLAP, INBOARD MID FLAP AND FUSELAGE SKIN AT BS 382, STRINGER 14L. REMOVED AND REPLACED NR 3 MAIN TIRE/WHEEL ASSEMBLY PER MM. REPAIRED RT WING, INBOARD MID FLAP, INBOARD T/E FLAP, INBOARD GROUND SPOILER, INBOARD FORE FLAP, AND SKIN PER MM AND SRM.

Part: GROUND WIRE — LOOSE (CABIN) · airframe 40,787 hrs · 37,058 cycles

THREE AFT EMERGENCY EXIT DOOR LIGHTS FLICKERED DURING FLIGHT. SECURED LOOSE GROUND WIRE PER MM.

Part: BUSHING — WORN (ELEVATOR) · airframe 40,347 hrs · 36,713 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PUSHROD BUSHINS PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 40,347 hrs · 36,713 cycles

DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY EXIT HATCH LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 39,471 hrs · 36,018 cycles

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

Part: BATTERY PACK — FAULTY (CABIN) · airframe 38,968 hrs · 35,617 cycles

AFT EMERGENCY EXIT LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED BOTH AFT EMERGENCY LIGHT BATTERY PACKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,843 hrs · 35,520 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 LONG CRACK AT FUSELAGE SKIN, BS 727E, STR 24R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,768 hrs · 35,457 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED (3 EA) AT LBL 1, WL 187, RBL 1, WL 187, AND RBL 5, WL 213. REPAIRED WEB PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 38,408 hrs · 35,166 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (SERVICE DOOR) · airframe 37,975 hrs · 34,814 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 37,587 hrs · 34,503 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 37,559 hrs · 34,489 cycles

DURING SCHEDULED RON, FOUND AFT CABIN LOWER EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 37,487 hrs · 34,423 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT CORNER OF HANDLE SPRING FLIP DOOR. REPAIRED SKIN PER SWA EA.

Part: PLATE — BROKEN (CABIN) · airframe 36,102 hrs · 33,310 cycles

LT EMERGENCY OVERWING EXIT DOOR HANDLE COVER PLATE BROKEN. REPAIRED COVER PLATE.

Part: LENS — MISSING (SERVICE DOOR) · airframe 47,228 hrs · 45,395 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LOWER LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,849 hrs · 31,460 cycles

DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT FWD SVC DOOR CUT OUT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR CUTOUT BEAR STRAP CORRODED FROM BS 780 TO BS 796, STR 26R. REPAIRED BEAR STRAP PER BFG ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR HINGE CUTOUT BEAR STRAP CRACKED AT BS 303, WL 238.5 TO WL 258.5. REPAIRED BEAR STRAP PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND 9R, AT BS'S 360, 400, 827 AND 907. REPAIRED FRAMES PER BFG ER AND SRM.

Part: FRAME — CRACKED (RT MLG W/W) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 680, WL 177 AND RBL 63. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L AND 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SKINS. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM.

Part: FLAP — DEBONDED (RT WING) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT INBOARD AFT T/E FLAP DEBONDED 37 INCHES OUTBOARD OF INBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,272 hrs · 30,972 cycles

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

Part: STIFFENER — CRACKED (FWD CABIN) · airframe 33,272 hrs · 30,972 cycles

DURING SCHEDULED D CHECK, FOUND STIFFENER CRACKED AT BS 328, WL 199 AND LBL 50. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,963 hrs · 29,854 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT OUTBOARD CHORD ANGLE CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD PER SWA ACO 7342-53.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,963 hrs · 29,845 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, LBL 5, WL 198 & WL 201. REPAIRED WEB PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,963 hrs · 29,854 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,963 hrs · 29,854 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 3 EA ) AT BS 178, LBL 17.1 & WL 229, BS 185, RBL 17.1 & WL 232, BS 178, RBL 17.1 & WL 220. R&R VERTICAL BEAMS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,963 hrs · 29,854 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178,WL 234, LBL 12 & RBL 9. REPAIRED WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 31,398 hrs · 29,367 cycles

EEPLS COVER LOOSE AT OVERWING EXIT. INSTALLED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,152 hrs · 29,148 cycles

DURING SCHEDULED C4 CHECK, FOUND LOWER AND FWD LEFT OVERWING EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: TRANSMISSION — FAILED (T/E FLAP) · airframe 30,700 hrs · 28,754 cycles

AIR TURNBACK, T/E FLAPS WOULD NOT RETRACT PAST 5 DEGREES DURING CLIMBOUT. REMOVED AND REPLACED NR 4 FLAP TRANSMISSION PER MM.

Part: LENS — LOOSE (CABIN) · airframe 30,233 hrs · 28,372 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BRACKET — LOOSE (CABIN) · airframe 30,233 hrs · 28,372 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 28,397 hrs · 26,707 cycles

FWD SERVICE DOOR EVACUATION SLIDE PULLED OUT OF CONTAINER. SECURED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 27,702 hrs · 26,146 cycles

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

Part: MODULE — FAILED (E/E BAY) · airframe 27,325 hrs · 25,836 cycles

DECLARED EMERGENCY. APU FIRE BELL AND LIGHT ACTIVATED AND DISCHARGED FIRE BOTTLE. FOUND SHORT ON D4816J CONNECTOR AND FOUND INTERNAL FAILURE IN M279 MODULE. REMOVED AND REPLACED D4816J HARNESS AND M279 MODULE PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SWA RA NR 1-353-2176.

Part: BEAM — CORROSION (AFT CARGO COMPT)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 860, RBL 8. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: BATTERY PACK — DISCHARGED (ROW 12-17)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP, ROW 12 THROUGH 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (ROW 17-12)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS LIGHTS INOP AT ROWS 17-12. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED AFT ENTRY DOOR LIGHT ASSY AND BATTERY PACKS AT BS 330 AND 730 LT PER MM.

Part: BATTERY CHARGER — INOPERATIVE (LT EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHT ABOVE LT WING INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SOCKET — SHORTED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND CENTER SECTION OF FLOOR TRACK LIGHTS INOP. FOUND SHORTED SOCKET. REMOVED AND REPLACED TRACK ASSY PER MM.

Part: CONNECTOR — FAILED (AFT GALLEY)

DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY CENTER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CANNON PLUG AT BATTERY PACK AND REPAIRED WIRING PER BOEING M/M. OPS CK GOOD PER MM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN LIGHTS INOP. REPAIRED WIRE TO BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (L2 DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND .875 INCH CRACKED FUSELAGE SKIN AT LOWER HINGE CUTOUT OF L2 DOOR. REPAIRED PER SWA RA 1-353-1930 AND TI-353-070.

Part: BATTERY BASE — INOPERATIVE (LT OVERWING)

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK BASE PER BOEING MM.

Part: REGULATOR — FAILED (NR 2 ENGINE)

RETURNED TO DAL DUE TO NOT BEING ABLE TO MAINTAIN CABIN PRESSURE. REPLACED NR 2 ENGINE BLEED AIR REGULATOR PER BOEING M/M.

Part: SUPPORT — CORRODED (BS 294-312)

DURING D CHECK, FOUND FLOOR SUPPORT CORROSION AT BS 294-312, RBL 11, WL 208. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 43, RBL 26 TO 37, WL 208. REPAIRED PER T1-A53-014 AND BOEING SRM.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND A CRACKED STUB FRAME ATTACH BRACKET AT BS 294, RBL 54. REPAIRED PER TRAMCO EWO 97-0440 AND BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND A CRACK INDICATION AT BS 178, AT WL 217 TO 217.5 AND AT 201.5 TO 202. REPAIRED BOTH PER TI-353-036 AND BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND INSPECTION, FOUND AFT BULKHEAD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M.

Part: AIR DISTR — ODOR (AFT GALLEY)

JUST AFTER PUSHBACK, PASSENGER AND F/A NOTED A BURNING SMELL AT AFT GALLEY AREA. OPENED AND INSPECTED AFT AREA PLUS, RAN ENGINES, AND TURNED OFF APU. SMELL DISSIPATED, CONTINUED UNDER MEL.

Part: SLIDE — LOW PRESSURE (FWD SERV DOOR)

DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.