N359SW

Part: WEB — CRACKED (BS 349-352) · airframe 76,644 hrs · 63,582 cycles

LOWER INBOARD FASTENER HOLE CLOSE OUT WEB CRACKED BETWEEN BS 349 - 352, BETWEEN STRINGERS 15 - 17L. R & R THE WEB IAW DWG & SRM.

Part: PAN — CRACKED (FUSELAGE) · airframe 76,644 hrs · 63,582 cycles

LEFT WATER SERVICE DOOR PAN CRACKED AT BS 985, STR 26L. REPAIRED DOUBLER IAW ER AND EA.

Part: BEAR STRAP — CRACKED (BS 345) · airframe 76,644 hrs · 63,582 cycles

L1 DOOR LOWER AFT CORNER BEARSTRAP CRACKED AT BS 345, WL 210. REPAIRED THE BEAR STRAP IAW SRM.

Part: BLOWER — INOPERATIVE (CABIN) · airframe 76,493 hrs · 63,474 cycles

DECLARED EMERGENCY ON FINAL, 20NM TO 30NM, F/A CALLED AND SAID THEY SMELLED FUMES, NO SMOKE, IN AFT GALLEY AREA. THE ODOR SPREAD THRU CABIN TO FLIGHT DECK. THE EQUIPMENT COOLING LIGHT, IN NORMAL, CAME ON, SWITCHED TO ALT AND, OFF, LIGHT WENT OUT. ODOR ALSO PRESENT IN ELECTRONIC EQUIPMENT BAY. R & R NORMAL ELECTRONIC EQUIPMENT BLOWER IAW MM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 75,372 hrs · 62,707 cycles

L1 DOOR GIRT BAR LOOSE. SECURED CLIPS IAW SIP.

Part: LIGHT — LOOSE (CABIN) · airframe 75,069 hrs · 62,489 cycles

RIGHT LUMINESCENT FLOOR STRIP LOOSE AT ROW 8. SECURED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

SKIN CRACKED AT BS 361.5, STRINGER 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 360) · airframe 74,570 hrs · 62,128 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 3 - 4R. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CRACKED, BETWEEN BS 500 - 500B, STRINGER 8L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CRACKED AT BS 500B, STRINGER 8R. REPAIRED STRINGER IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 291, STRINGER 8R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CLIP CRACKED AT BS 907, STRINGER 10R. R & R CLIP IAW SRM.

Part: SUPPORT CHANNEL — CORRODED (BS 727) · airframe 74,570 hrs · 62,128 cycles

NUMBER 3 VHF LOWER ANTENNA SUPPORT U-CHANNEL CORRODED AT STATION 727D+7, LBL 2. R & R CHANNEL IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 5R. R & R SPLICE IAW ER & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER SPLICE CRACKED AT BS 360+2, STRINGER 4R. R & R SPLICE IAW ER & EA.

Part: FRAME — CRACKED (BS 360) · airframe 74,570 hrs · 62,128 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 20R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 727C - 727D, WL 208 LT SIDE. R & R WEB IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 74,570 hrs · 62,128 cycles

RIGHT OVERHEAD BULLNOSE BIN EMER LIGHT LENS MISSING AT ROW 2. INSTALLED LENS IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 74,570 hrs · 62,128 cycles

AFT CTR EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CLIP CRACKED AT BS 500B, STRINGER 8R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 8R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CLIP CRACKED AT BS 500D, STRINGER 8R. R & R CLIP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

SEAT TRACK WEB UPPER RADIUS CRACKED AT BS 727B+1.5, RBL 45.5. REPAIRED SEAT TRACK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

LEFT SIDE FUSELAGE SKIN CRACKED AT STATION 289, WL 254. REPAIRED SKIN IAW EA.

Part: ATTACH ANGLE — CORRODED (BS 326) · airframe 74,570 hrs · 62,128 cycles

ATTACH ANGLE CORRODED AT BS 326.7, STRINGER 28L. R & R ANGLE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

FLOOR TRACK FLOOR SUPPORT ANGLE, CRACKED AT BS 380, STRINGER 27R. R & R FLOOR TRACK IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

INTERCOSTAL CORRODED, BETWEEN BS 727A - 727B, BETWEEN STRINGER 27R TO 26R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

INTERCOSTAL CORRODED, BETWEEN BS 847 - 867, STRINGER 27R. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

AFT CARGO COMPARTMENT, FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727D - 727E, BETWEEN STRINGER 26R - 27R. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 787, BETWEEN STRINGER 26L - 27R. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

INTERCOSTAL CORRODED, BETWEEN BS 727A - 727B, BETWEEN STRINGER 25L - 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

AFT CARGO COMPARTMENT, SIDEWALL SUPPORT AROUND FASTENER HOLES, CORRODED AT BS 727D, BETWEEN STRINGER 25R - 27R. R & R ANGLE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

FORWARD CARGO DOOR THRESHOLD SILL WEB CORRODED. R & R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,570 hrs · 62,128 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 500C - 500D, BETWEEN STRINGER 26R - 25R. R & R SUPPORT IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 74,570 hrs · 62,128 cycles

LEFT EMER EXIT AISLE LIGHT COVER MISSING AT ROW 10. INSTALLED COVER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 74,570 hrs · 62,128 cycles

LEFT OVERHEAD BIN EMER LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 74,370 hrs · 61,977 cycles

RIGHT OVERWING EMER EXIT SIGN INOPERATIVE. R & R BATTERY CHARGER IAW AMM.

Part: INDICATOR — MISSING (CABIN) · airframe 73,020 hrs · 60,988 cycles

OVERHEAD EMER LIGHTS INDICATOR LIGHT MISSING. INSTALLED INDICATOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,020 hrs · 60,988 cycles

RIGHT FRAME OTBD CHORD CRACKED AT BS 727. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,346 hrs · 61,234 cycles

FUSELAGE MAIN FRAME CRACKED AT LT STATION 727. REPAIRED FRAME IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 71,882 hrs · 60,208 cycles

FORWARD CARGO DOOR FRAME MIDDLE SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 71,882 hrs · 60,208 cycles

LEFT EMER EXIT CUT OUT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SPRING ASSY — OUT OF ADJUST (R1 DOOR) · airframe 70,951 hrs · 59,508 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR SECURE SPRING OUT OF ADJUSTMENT. ADJUSTED SPRING ASSEMBLY IAW SIP.

Part: FITTING — DAMAGED (RT PYLON) · airframe 70,553 hrs · 59,244 cycles

RIGHT PYLON STRUT FITTING OTBD LUG BORE DAMAGED AT ENG MOUNT CROSSBEAM ATTACH POINT. REPAIRED FITTING IAW EA.

Part: SKIN — WRINKLED (LE SLAT) · airframe 70,500 hrs · 59,213 cycles

RIGHT WING NR 4 SLAT LOWER SKIN WRINKLED & LOOSE FASTENERS AT ACTUATOR. R & R SLAT ASSEMBLY IAW AMM.

Part: HINGE — LOOSE (RT AILERON) · airframe 70,500 hrs · 59,213 cycles

RIGHT WING AILERON TAB OTBD HINGE & BEARING LOOSE. R & R HINGE ASSEMBLY IAW CMM.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 70,823 hrs · 59,421 cycles

LEFT WING INBD FLAP OTBD TRACK FAIRING INBD LOWER SURFACE DELAMINATED. REPAIRED FAIRING IAW EA.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 70,181 hrs · 58,979 cycles

RT WING TRAILING REAR SPAR ATTACH BRACKET CRACKED AT REAR SPAR STATION 238. R & R BRACKET IAW SRM.

Part: HINGE — LOOSE (RT AILERON TAB) · airframe 70,181 hrs · 58,979 cycles

RT WING AILERON TAB OTBD HINGE LOOSE. R & R TAB IAW MM.

Part: BRACKET — CRACKED (LT WING) · airframe 70,181 hrs · 58,979 cycles

LT WING REAR SPAR BRACKET CRACKED AT WING STATION 243. INBD OF INBD GND SPOILER OTBD HINGE BRACKET. R & R BRACKET IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,460 hrs · 58,500 cycles

LT BULLNOSE EMERGENCY EXIT LIGHT BULB INOPERATIVE AT ROW 21. R & R BULB IAW AMM.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 69,460 hrs · 58,500 cycles

LT WING NR 3 FLAP TRACK INTERNAL AREA STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

ANGLE CRACKED AT BS 348.2, STRINGER 14L. R & R ANGLE IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

ATTACHMENT CLIP CRACKED AT BS 348.2, STRINGER 14L. R & R CLIP IAW SRM & DRAWING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

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

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 69,460 hrs · 58,500 cycles

RT WING INBD MID FLAP CARRIAGE CORRODED ON AFT HOLE INBD ARM. REPAIRED MID FLAP IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 69,460 hrs · 58,500 cycles

RT WING OTBD MID FLAP CARRIAGE CORRODED ON AFT HOLE INBD ARM. REPAIRED MID FLAP IAW CMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FWD GALLEY DOOR STOP FRAME CRACKED. R & R STUB FRAME IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, RBL 4.5. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, AT RBL 3.5. REPAIRED WEB IAW SRM.

Part: PLATE — BROKEN (TE FLAP) · airframe 69,460 hrs · 58,500 cycles

RT WING INBD MID FLAP INTERNAL STRUCTURE PLATE BROKEN. R & R PLATE IAW CMM.

Part: STRIP — CRACKED (FLAP TRACK) · airframe 69,460 hrs · 58,500 cycles

RT WING NR 6 FLAP TRACK STRIP CRACKED. R & R STRIP IAW SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

BEAM UPPER CHORD CORRODED AT BS 344, LBL 7. REPAIRED CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLOOR BEAM UPPER CHORD AT THE AFT PAX CABIN FLOOR STRUCTURE CORRODED AT BS 967, BETWEEN RBL 7 & LBL 7. REPAIRED CHORD IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 69,460 hrs · 58,500 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

WEB CRACKED AT BS 328+2, LBL 45. R & R WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FWD GALLEY DOOR CUTOUT SURROUND INTERNAL STRUCTURE ATTACHMENT ANGLE CRACKED AT BS 291.5, BETWEEN STRINGER 8R & STRINGER 9R. R & R ANGLE IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLOOR BEAM CORRODED AT BS 328, BL 0. REPAIRED BEAM IAW SRM.

Part: STRAP — CRACKED (LT WING) · airframe 69,460 hrs · 58,500 cycles

LT WING TE AREA STRAP CRACKED BETWEEN WBL 71.24 TO WBL 86. R & R STRAP IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R WEB IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 69,460 hrs · 58,500 cycles

LT WING NR 3 FAIRING INBD SIDE FLAP TRACK STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 967, LBL 27.5. REPAIRED CHORD IAW SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 69,460 hrs · 58,500 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLOOR BEAM CORRODED AT BS 986.5, BETWEEN BL 0 & RBL 4. REPAIRED BEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLIGHT DATA RECORDER SUPPORT STRUCTURE IN THE AFT PAX CABIN ANGLE CRACKED AT BS 967, LBL 18. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 69,460 hrs · 58,500 cycles

LT WING FIXED TE STRUCTURE ANGLE CRACKED AT RSS 533. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (LT WING) · airframe 69,460 hrs · 58,500 cycles

LT WING TE AREA PLATE CRACKED ON WBL 86. R & R PLATE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FWD GALLEY DOOR CUTOUT INTER SURROUND STRUCTURE ATTACHMENT WEB ANGLE CRACKED AT BS 291.5, BETWEEN STRINGER 12R & STRINGER 13R. R & R WEB IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 69,460 hrs · 58,500 cycles

LT WING SUPPORT ANGLE INTERNAL STRUCTURE OTBD SIDE OF FLAP TRACK CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN BL 0 & LBL 44. REPAIRED BEAM IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 69,460 hrs · 58,500 cycles

RT WING REAR SPAR AREA ANGLE CRACKED AT RSS 545. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FWD ENTRY DOOR SURROUND STRUCTURE ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (CARGO DOOR) · airframe 69,460 hrs · 58,500 cycles

FWD EDGE INTERNAL AREA OF AFT CARGO DOOR WEB CRACKED AT LOWER EDGE. R & R WEB IAW SRM & DRAWING.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

LT SPLICE CRACKED AT BS 663.5. R & R SPLICE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FUSELAGE SKIN CRACKED AT BS 420 + 12, STRINGER 2R. REPAIRED SKIN IAW EO & EA.

Part: WEB — CRACKED (NLG WW) · airframe 69,460 hrs · 58,500 cycles

LT SIDE NLG WW WEB CRACKED AT BS 243.7+3, WL 169.1. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 69,460 hrs · 58,500 cycles

RT WING LE INBD FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 663+1.5, BBL 0.07. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

SKIN CRACKED BETWEEN BS 460 TO BS 500, BETWEEN STRINGER 3R & STRINGER 4R. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,460 hrs · 58,500 cycles

FWD PRESSURE BULKHEAD CRACKED AT BS 178, LBL 5.7. REPAIRED BULKHEAD IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,291 hrs · 58,386 cycles

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

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 68,845 hrs · 58,040 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE IAW MT.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 68,445 hrs · 57,751 cycles

MLG WW BEADED WEB CRACKED AT STATION 663, BETWEEN LBL 25-LBL 45. REPAIRED WEB IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,307 hrs · 57,645 cycles

AFT GALLEY DOOR CUTOUT CLOSEOUT FRAME BETWEEN THE FWD UPPER STOP PAD AND THE UPPER CAM PLATE CRACKED. R&R FRAME SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,611 hrs · 57,142 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,611 hrs · 57,142 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,389 hrs · 56,993 cycles

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

Part: ACTUATOR — FAULTY (RT MLG) · airframe 66,615 hrs · 56,448 cycles

LOWER L GEAR RT FAILED TO EXTEND (NO SCREEN LIGHT AND RED GEAR UNSAFE LIGHT ON RECYCLED WITH SAME RESULT. REMOVED AND REPLACED RIGHT ACTUATOR PER AMM.

Part: LUG — BROKEN (RT SPOILER) · airframe 65,910 hrs · 55,924 cycles

RIGHT WING NR 5 GROUND SPOILER LUGS BROKEN. REMOVED AND REPLACED NR 5 GROUND SPOILER PER AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,593 hrs · 55,694 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW M/M.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,197 hrs · 55,393 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,031 hrs · 55,272 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 441 TO BS 445, STR 1L. REPAIRED SKIN IAW EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,031 hrs · 55,272 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 431 TO BS 435, STR 1L. REPAIRED SKIN IAW EA AND SRM.

Part: FAN — FAULTY (A/C BAY) · airframe 64,198 hrs · 54,647 cycles

AT FL 360, 15 MILES FROM TOP OF DESCENT, CABIN REPORTED STRONG BURNING ODOR IN THE VICINTY OF ROW 22. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

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

CRACKED STRINGER SPLICE BS 908, STR 4R. REPLACED SPLICE IAW SRM AND DWG.

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

CRACKED STRINGER SPLICE AT BS 908, STR 4L. REPLACED STRINGER SPLICE IAW SRM AND DWG.

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

CRACK ON ANGLE LOCATED ON UPPER LEFT SIDE E/E COMPARTMENT. REPLACED ANGLE IAW SRM AND DRAWING.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 22R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 64,109 hrs · 54,583 cycles

RT STABILIZER HORIZONTAL LOWER CHORD CRACKED AT STA 138.7. REPLACED CHORD IAW EA AND EO.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,109 hrs · 54,583 cycles

RT WING LEADING EDGE NR 4 SLAT SKIN CRACK. REPAIRED SKIN IAW SRM.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 18R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 18R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

CORROSION ON CREASE BEAM WEB BETWEEN BS 380 TO BS 400, STRINGER 17R. REPLACED WEB IAW SRM AND DWG

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

CORROSION ON SHEAR TIE AT BS 344 STR 27R. REMOVED AND REPLACED SHEAR TIE IAW DWG.

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

CRACK ON TIE CLIP LOCATED B 294.5 AND STR 11L. REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

CORROSION ON FRAME AT BS 344, STR 27R. REPAIRED FRAME IAW SRM.

Part: LIGHT — WORN (CABIN) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS WORN. REMOVED AND REPLACED EEPLS PER MM.

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

CRACK ON TIE CLIP LOCATED ON BS 947.5 STR 25R. REPLACED TIE CLIP IAW SRM AND DRAWING 65-46560.

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

CRACK ON WEB AT LBL 2 AND BS 711. REPLACED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FRAME CORRODED AT BS 867 BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

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

CORROSION ON STRINGER 27R BETWEEN BS 827 TO BS 847. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FLOORBEAM LOWER SURFACE UPPER CHORD CORRODED AT BS 986.3 AND LBL 34. REPAIRED CHORD IAW EO AND EA.

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

CRACK ON TIE CLIP LOC BS 727C AT LEVEL STR 28R. REPLACED TIE CLIP IAW SRM DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,109 hrs · 54,583 cycles

LEFT WING LOWER SURFACE OF O/B AFT FLAP DELAMINATED AT I/B END OF T/E. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

CORROSION ON FRAME LOCATED BS 727C BETWEEN, STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

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

CRACK ON TIE CLIP LOC BS 747 AT LEVEL STR 18R. REPLACED TIE CLIP IAW SRM DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FRAME CORRODED AT BS 827 BETWEEN, ST 27L TO STR 27R. REMOVED AND REPLACED FRAME PER EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FRAME CORRODED AT BS 827, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER EO AND EA.

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

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 531.5 TO BS 534, STR 28L. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FRAME CORRODED AT BS 867 BETWEEN, ST 27L TO STR 27R. REPAIRED FRAME IAW SRM.

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

STIFFENER CRACKED AT BS 727, RBL 6. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DRAWING.

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

CRACK ON TIE CLIP LOC BS 639 RBL 45.5. REPLACED TIE CLIP IAW SRM DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FLOORBEAM LOWER SURFACE UPPER CHORD CORRODED AT BS 986.3 AND RBL 45. REPAIRED CHORD IAW EO AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

CORROSION ON WEB AT 17R BETWEEN BS 400 TO BS 420. REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

FRAME CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME IAW EO AND EA.

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

CRACK ON TIE CLIP LOCATED AT BS 420, STR 28L. REPLACED TIE CLIP IAW DWG AND SRM.

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

CRACK INDICATION WAS FOUND IN THE FRAME BTW STR 20R AND STR 21R BS 520. REPAIRED FRAME IAW SRM.

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

CRACKED FUSELAGE SKIN AT BS 259.5, BETWEEN STR 21L AND STR 22L. REPAIRED SKIN IAW EO AND EA.

Part: ADC — FAULTY (COCKPIT) · airframe 62,809 hrs · 53,614 cycles

AIR TURNBACK - AT ROTATION ON TAKEOFF FIRST OFFICER'S FLIGHT INSTRUMENTS BECAME UNRELIABLE. AIRSPEED INDICATOR FROZEN AT 132. ALTIMETER CLIMBED TO FL 23D. NO FLAGS AT ANY TIME. REMOVED AND REPLACED AIR DATA COMPUTER PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 62,734 hrs · 53,553 cycles

LT WING NR 0 FLIGHT SPOILER T/E DELAMINATED. REMOVED AND REPLACED SPOILER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,028 hrs · 52,023 cycles

DURING SCHEDULED MV2 CHECK FOUND, RT OVERHEAD BIN EMERGENCY LIGHTS INOP AT ROW 12 TO 19. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,028 hrs · 52,023 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT OVERHEAD BIN EMERGENCY LIGHTS INOP AT ROW 13 TO 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 61,897 hrs · 52,933 cycles

L1 COCKPIT WINDOW OUTER PANE ARCED AND CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,559 hrs · 52,688 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,419 hrs · 52,584 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,403 hrs · 51,811 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

DURING SCHEDULED 18Y CHECK, FOUND PRESSURE BULKHEAD CHORD SPLICE CRACKED AT BS 727, RBL 45. REMOVED AND REPLACED SPLICE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

DURING SCHEDULED 18Y CHECK, FOUND PRESSURE BULKHEAD CHORD SPLICE CRACKED AT BS 727, LBL 45. REMOVED AND REPLACED SPLICE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 58,369 hrs · 50,233 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 668, LBL 24.5. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,339 hrs · 50,209 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 58,217 hrs · 50,117 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 55.5 TO STA 116. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 58,215 hrs · 50,116 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL LOWER SKIN CRACKED BETWEEN STA 55.5 TO STA 103. REPAIRED SKIN PER EA.

Part: COVER — LOOSE (CABIN) · airframe 57,442 hrs · 49,543 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR UPPER SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,694 hrs · 48,970 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,668 hrs · 48,948 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,158 hrs · 48,572 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 55,324 hrs · 47,962 cycles

LT OVERHEAD BULLNOSE LIGHT COVER MISSING AT ROW 16. INSTALLED COVER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 24L TO STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 EMERGENCY EVACUATION DOOR SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727, STR 9R. REPAIRED STRINGER PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. R&R STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT BS 129. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOORBEAM CHORD CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10, WL 208. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 348 S16L) · airframe 54,961 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 294, BETWEEN STR 2R TO STR 3R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8R. REPAIRED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED AT BS 707, LBL 25. REPAIRED BEAM PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 390, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 639, LBL 45, WL, 206. REPAIRED STUB FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 732, STR 4R. REPAIRED FRAME PER SWA ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BETWEEN BS 188 TO BS 197 STR 17R. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME PER PAE EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,962 hrs · 47,685 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 53,523 hrs · 46,642 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,493 hrs · 46,616 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,493 hrs · 46,616 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT FWD FRAME LOWER CORNER CRACKED. REPAIRED FRAME PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND BELT FRAME CRACKED AT BS 277, STR 16R. REPAIRED BELT FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR CUTOUT LOWER STOP FITTING CUTOUT CRACKED AT STA 303. REMOVED AND REPLACED WEB PER SRM.

Part: FITTING — CORRODED (FLAP TRACK) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (FLAP TRACK) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947, LBL 5. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,433 hrs · 46,572 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,326 hrs · 46,493 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 46,087 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 10L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,916 hrs · 45,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS INOP AT ROW 8 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,916 hrs · 45,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (ROW ABC) · airframe 51,916 hrs · 45,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,172 hrs · 44,059 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED UPPER AFT END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,171 hrs · 44,058 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 4. REPAIRED SKIN PER SB AND SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 50,171 hrs · 44,058 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 846, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,171 hrs · 44,058 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 25L. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,305 hrs · 53,759 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 373, RBL 67 TO RBL 69. REMOVED AND REPLACED WEB PER SRM.

Part: DUCT — LOOSE (KEELBEAM) · airframe 43,185 hrs · 36,763 cycles

DECLARED EMERGENCY, CABIN PRESS WARNING HORN SOUNDED. FOUND A/C DISTRIBUTION KEEL BEAM DUCT BOOT CLAMP LOOSE. SECURED DUCT CLAMP PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,725 hrs · 43,729 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STA 125. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 48,694 hrs · 42,954 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER END. REPAIRED FLAP PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 48,694 hrs · 42,954 cycles

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

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 48,694 hrs · 42,954 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT AND BUSHING PER MM.

Part: FITTING — CORRODED (RT WING) · airframe 48,970 hrs · 42,931 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG WALKING BEAM OUTBOARD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 48,970 hrs · 42,931 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM OUTBOARD STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 47,269 hrs · 41,842 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 45,987 hrs · 40,841 cycles

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

Part: SKIN — CRACKED (BS 500D) · airframe 45,518 hrs · 40,481 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 45,008 hrs · 40,069 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,008 hrs · 40,069 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA EA.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,592 hrs · 39,743 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,527 hrs · 39,689 cycles

DURING SCHEDULED RON CHECK, AFT CABIN EMERGENCY LIGHTS WOULD NOT TURN OFF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 43,179 hrs · 38,568 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIP BETWEEN ROWS 1 ABC AND 2 ABC, DAMAGED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 42,292 hrs · 37,874 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,875 hrs · 37,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT COCKPIT C-D WINDOW POST, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 41,875 hrs · 37,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN AT BOTTOM HINGE CRACKED. REPAIRED DOOR SKIN PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,875 hrs · 37,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE BULKHEAD WEB AT BS 178, LBL 11, LBL 12 AND RBL 8.5, WL 234. REPAIRED BULKHEAD WEB PER SRM.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 41,875 hrs · 37,529 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER CORNER CRACKED. REPAIRED DOOR FRAME UPPER HINGE CUTOUT PER EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 41,875 hrs · 37,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENRTY DOOR SKIN AT UPPER AND LOWER HINGES CRACKED. REPAIRED DOOR SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,875 hrs · 37,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,321 hrs · 37,082 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 & R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 & R1 DOOR EVAC SLIDES PER MM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 40,434 hrs · 36,374 cycles

DURING SCHEDULED C2 CHECK, FOUND LT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: CABLE — LOOSE (R2 DOOR) · airframe 40,434 hrs · 36,374 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE LOOSE. SECURED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 34,105 hrs · 31,266 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB DELAMINATED ON T/E. REPAIRED RT ELEVATOR TAB PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 33,916 hrs · 31,120 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN REAR SPAR LT AND RT CLEVIS LUGS CORRODED. REPAIRED LUGS AND INSTALLED BUSHINGS PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT END OF EQUIPTMENT COOLING EXHAUST HOLE, BS 378.5 AT LBL 3.5. REPAIRED SKIN PER BFG ER.

Part: WIRE — BROKEN (COCKPIT) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT EMERGENCY FLOOD LIGHT INOP. REPAIRED BROKEN WIRE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 8R AND 9R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR'S 8R AND 9R. REPAIRED FRAME PER BFG ER..

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8R AND 9R, BS'S 787 AND 827. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR'S 8L AND 9L, BS'S 727D AND 787. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) AT STR 8R, BS'S 360, 400 AND 440. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,679 hrs · 30,731 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STR 8L, BS'S 380 AND 400. REPAIRED FRAMES PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 277 AND STR 11L, BS 360 AND STR 8R, BS 400 AND STR 1, BS 500C AND STR 16R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT STR 8L, BS 380, 400 AND 500A. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SPOILER — DELAMINATED (RH WING) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND NR 5 T/E GRD SPOILER DELAMINATED ON UPPER SURFACE 3.75 INCHES AFT OF FWD END. REPAIRED NR 5 T/E SPOILER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,845 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, BETWEEN STR'S 2R AND 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,576 hrs · 30,854 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,846 hrs · 30,272 cycles

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL POWER DOOR CUT OUT .25 INCH LONG ON AFT SECTION. REPAIRED SKIN PER SWA RA.

Part: BULB — FAULTY (NR 2 ENGINE) · airframe 32,592 hrs · 30,067 cycles

DIVERSION, DURING CRUISE NR 2 ENG OIL TEMP CLIMBED TO YELLOW MARKING. TO MAINTAIN TEMP IT WAS NECESSARY TO REDUCE POWER TO 69 PERCENT N1. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB AND CHECKED CHIP DETECTORS. OPS CHECKED GOOD PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,461 hrs · 29,785 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (6 EA) AT BS 178, BETWEEN LBL 1 & RBL 1. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,957 hrs · 29,554 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 4 EA ) AT BS 178, RBL 17.1 & LBL 17.1, WL 176 TO WL 230. REPAIRED WEBS PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,957 hrs · 29,554 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17.1 & WL 220. REPAIRED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,689 hrs · 29,327 cycles

DURING SCHEDULED A2 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AT RT AFT FUSELAGE. RELAMPED EXIT LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 31,552 hrs · 29,206 cycles

EEPLS COVER LOOSE AT OVERWING EMERGENCY EXIT. SECURED EEPLS COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 31,552 hrs · 29,206 cycles

EEPLS COVER LOOSE AT OVERWING EMERGENCY EXIT. REINSTALLED EEPLS COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 31,487 hrs · 29,145 cycles

EEPLS LOOSE AT ROW 11. SECURED EEPLS PER MM.

Part: TRIM TAB — WORN (ELEVATOR) · airframe 31,058 hrs · 28,789 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVATOR CONTROL TAB MECHANISM PER MM.

Part: TAB — WORN (ELEVATOR) · airframe 30,998 hrs · 28,735 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND ELEVATOR TAB CONTROL MECHANISM PER MM.

Part: CONTROL ROD — WORN (ELEVATOR) · airframe 31,058 hrs · 28,789 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. Removed and replaced ELEVATOR INPUT ROD PER MM.

Part: LENS — MISSING (CABIN) · airframe 30,678 hrs · 28,468 cycles

DURING RON FOUND EEPLS FLOOR TRACK HAD LENS MISSING. REPLACED LENS PER MM.

Part: ACTUATOR — CRACKED (SPOILER) · airframe 30,663 hrs · 28,452 cycles

AIR DIVERSION, A HYDRAULIC SYSTEM FAILED DURING FLIGHT. R&R NR 1 GRD SPOILER ACTUATOR PER MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 30,103 hrs · 27,984 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR SKIN CUTOUT 2 INCH CRACK AT LOWER FWD CORNER. REPAIRED SKIN DOUBLER PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 30,103 hrs · 27,984 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 29,950 hrs · 27,863 cycles

EEPLS FLOOR TRACK LOOSE AT EMERGENCY EXIT ROW. SECURED EEPLS TRACK PER MM.

Part: SLIDE — DISLODGED (FWD ENTRY) · airframe 29,157 hrs · 27,188 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER. REPOSITIONED SLIDE ASSY PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 28,776 hrs · 26,860 cycles

DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EMERGENCY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,969 hrs · 26,185 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT.

Part: WIRE — BROKEN (LE FLAP) · airframe 27,969 hrs · 26,185 cycles

DIVERSION, NR 4 L/E FLAP TRANSIT LIGHT ILLUMINATED. REPAIRED BROKEN WIRE AT NR 4 L/E FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,259 hrs · 25,573 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RESECURED WIRING AND OPS CHECK GOOD PER MM.

Part: LENS — LOOSE (CABIN) · airframe 27,259 hrs · 25,573 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 26,936 hrs · 25,293 cycles

FWD ENTRY DOOR EMERGENCY LIGHT LENS BROKEN. R&R LENS ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 9 EACH PLACES. REPAIRED BULKHEAD PER DALFORT XEA X2-53-267.

Part: CHORD — CRACKED (FUSELAGE NOSE)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 SIDE CHORD CRACKED, LT SIDE, WL 207. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: STRAP — BROKEN (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND FWD EMERGENCY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP ASSY PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EEPLS LIGHT LENS MISSING ON AFT END. REPLACED LENS AND CAP PER MM.

Part: SLIDE — FAILED (GALLEY DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY DOOR EVACUATION SLIDE GAUGE READING BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FITTING — LOOSE (NR 1 ENGINE)

AIR TURNBACK DUE TO LOSS OF SYSTEM A ENGINE PUMP AND SYSTEM FLUID UPON GEAR RETRACTION AFTER TAKEOFF. USED ALTERNATE GEAR EXTENTION TO LAND. FOUND NR 1 ENG HYD RETURN LINE FITTING LOOSE. REMOVED AND REPLACED FITTING AND O RING ASSY. INSPECTED RETURN FILTER FOR CONTAMINATION, ALL LEAK AND OPS CK GOOD.

Part: SLIDE — DISENGAGED (PAX DOOR)

DURING OVERNIGHT CHECK, FOUND FWD ENTRY DOOR SLIDE POPPED OUT OF RETAINER. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: CONTROLLER — MALFUNCTIONED (CONTROL CABIN)

AFTER T/O AT APPROX 1500 FT SMOKE STARTED COMING FROM PRESSURE CONTROLLER. CREW SWITCHED TO STBY AND IMMEDIATELY RETURNED FOR LANDING AT DAL DOWNWIND. LANDING WEIGHT WAS 109000 APPROX WITH NORMAL BRAKING. SMOKE STOPPED SOMETIME AFTER SWITCHING TO STBY. INSPECTED PRESSURE CONTROL PANEL WIRING AND CONNECTOR, NO DEFECTS NOTED. REMOVED AND REPLACED PRESSURE CONTROL PANEL PER M/M. PRESSURIZED ACFT ON GROUND, NO ABNORMALTIES NOTED. OP CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP ROWS 12 TO 15. RELAMPED AND RECONFIGURED PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTING INOP. REMOVED AND REPLACED AFT LT BATTERY PACK EMERGENCY LIGHTING PER BOEING MM. OPS CK GOOD.