N695SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,462 hrs · 54,212 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,463 hrs · 54,212 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,463 hrs · 54,212 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,402 hrs · 54,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 12, STR 23. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,402 hrs · 54,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,402 hrs · 54,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,402 hrs · 54,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 23L. REPAIRED SKIN PER EA.

Part: LUG — CORRODED (RT MLG) · airframe 70,402 hrs · 54,167 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG LOWER FITTING LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: SKIN — CRACKED (BS 947 S25R) · airframe 69,410 hrs · 53,422 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, STR 17R. REPAIRED FRAME PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25L CORRODED BETWEEN BS 343 AND BS 355. REPAIRED STRINGER PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1006, LBL 10. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947.5, RBL 48. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULE 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 44. REPAIRED FLOOR BEAM PER ER.

Part: FITTING — CORRODED (GIRT BAR) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 27L CORRODED AT BS 1006. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 15. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25L CORRODED AT BS 988. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLAP — DEBONDED (RT WING) · airframe 69,205 hrs · 53,271 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP INBOARD END DISBONDED. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 68,197 hrs · 52,505 cycles

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

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 68,163 hrs · 52,479 cycles

ON APPROACH CREW REPORTED AN ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,833 hrs · 52,223 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 375 S8L) · airframe 67,512 hrs · 51,966 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 8L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 67,267 hrs · 51,771 cycles

WITH THE GEAR HANDLE IN THE OFF POSITION AND AIRBORNE THE RIGHT MLG EXTENDED. RETRACTED NORMALLY AND STAYED STOWED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,091 hrs · 51,642 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 425 AND BS 435, LBL 2 TO RBL 3. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,634 hrs · 51,278 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 66,192 hrs · 50,904 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,133 hrs · 50,856 cycles

FUSELAGE SKIN CRACKED AT BS 787, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 763 S24L) · airframe 65,702 hrs · 50,535 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT TE FLAP) · airframe 65,702 hrs · 50,535 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP UPPER OUTBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: HYDRAULIC LINE — LEAKING (NLG W/W) · airframe 64,575 hrs · 49,666 cycles

AIR TURNBACK, DURING CLIMB NLG WOULD NOT RETRACT WHEN LANDING GEAR HANDLE LEVER RAISED TO THE UP POSITION. REMOVED AND REPLACED NLG ACTUATOR DOWNLOCK LINE PER MM.

Part: SHEAR TIE — CORRODED (BS 827 S27L-27R) · airframe 63,514 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT OVERWING LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: KEELBEAM — CORRODED (BS 523) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 523. REPAIRED KEEL BEAM PER SRM.

Part: STRAP — CRACKED (FLOORBEAM) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM STABILIZER STRAP CRACKED AT BS 344, LBL 11. REMOVED AND REPLACED STABILIZER STRAP SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 400 S13-14L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 400, STR 13L TO 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 727C S26L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S28L-28R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L TO 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S15R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GIRT BAR — CRACKED (ESCAPE SLIDE) · airframe 63,914 hrs · 49,120 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CORRODED (BS 460 S13-14L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 13L TO 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB FITTING FWD LUG FACE CORRODED. REMOVED AND REPLACED VERTICAL STAB FITTING PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND PRESSURE DOME WEB CRACKED AT BS 1016, THIRD FASTENER FROM DOME CAP. REPAIRED WEB PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.

Part: STRINGER — CORRODED (BS 540) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27R CORRODED AT BS 540. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB FITTING AFT LUG FACE CORRODED. REMOVED AND REPLACED VERTICAL STAB FITTING PER SRM.

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.

Part: STRINGER CLIP — CORRODED (BS 927 S26R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (BS 500 S22R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 22R CORRODED AT BS 500. REPAIRED STRINGER PER SRM.

Part: SKIN — CHAFED (BS 860-887) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 860 TO BS 887, BETWEEN STR 2L AND STR 2R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (BS 727E S26L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S14R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 400 S13R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S26R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 807 S26L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S13L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 747 S26R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 348 S15L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 727C S27L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT FORE FLAP) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S26L) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 874, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 795, STR 18L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S14R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S24R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S23R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FWD GIRT BAR HOOK PER SRM.

Part: SKIN — CRACKED (BS 735E S21R) · airframe 63,914 hrs · 49,126 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735E, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 518) · airframe 63,307 hrs · 48,660 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 14R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 518 S14R) · airframe 63,288 hrs · 48,652 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 14R. REPAIRED SKIN PER SWA EA AND SRM.

Part: BATTERY — FAILED (CABIN) · airframe 63,071 hrs · 48,482 cycles

DURING SCHEDULED C4 CHECK, R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT FAILED TIME TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FAN — FAULTY (CABIN AIR) · airframe 62,357 hrs · 47,933 cycles

DIVERSION/DECLARED EMERGENCY. STRONG BURNING ODOR IN CABIN. FOUND GASPER FAN WITH STRONG BURNED ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: HINGE — BROKEN (RT WING SPOILER) · airframe 62,249 hrs · 47,840 cycles

NR 5 GROUND SPOILER ATTACHMENT HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 410) · airframe 62,047 hrs · 47,682 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 2 RADIO ALTIMETER ANTENNA CUTOUT, BS 410, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500D) · airframe 62,047 hrs · 47,682 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500D) · airframe 62,047 hrs · 47,682 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 940) · airframe 62,047 hrs · 47,682 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: FASTENER — MISSING (L2 DOOR SLIDE) · airframe 62,047 hrs · 47,682 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE COVER ATTACH BRACKET MISSING FASTENER. INSTALLED FASTENER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,015 hrs · 47,656 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD & AFT ENDS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 61,921 hrs · 47,582 cycles

FWD CABIN BULLNOSE LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (BS 732B-736B) · airframe 61,771 hrs · 47,463 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732B TO BS 736B, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730B-733B) · airframe 61,771 hrs · 47,463 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 730B TO BS 733B, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 811-814) · airframe 61,771 hrs · 47,463 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 811 TO BS 814, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 735D) · airframe 61,633 hrs · 47,359 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 435-465) · airframe 61,633 hrs · 47,359 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, BS 455 AND BS 465, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 328) · airframe 61,633 hrs · 47,359 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 472) · airframe 61,633 hrs · 47,359 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 472, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750) · airframe 61,633 hrs · 47,359 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 61,098 hrs · 46,924 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE OTBD UPPER CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (BS 960) · airframe 61,098 hrs · 46,924 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 885) · airframe 60,826 hrs · 46,703 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 24R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,717 hrs · 46,619 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 22L. REPAIRED SKIN PER SWA EA & SRM.

Part: SIGN — BROKEN (CABIN) · airframe 60,599 hrs · 46,524 cycles

L1 DOOR EMERGENCY EXIT LOWER SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,736 hrs · 45,798 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 730, STR 23L & STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — PEELING (ROWS 7-9) · airframe 59,351 hrs · 45,522 cycles

FWD END OF EEPLS AT ROW 7 TO ROW 9 PEELING. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,152 hrs · 45,365 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 924R, STR 21R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 59,152 hrs · 45,365 cycles

DURING SCHEDULED C4 CHECK, FOUND CORROSION ON FUSELAGE STRINGER AT BS 344, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 59,060 hrs · 45,291 cycles

R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,030 hrs · 45,264 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 4R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,030 hrs · 45,264 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 867, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,030 hrs · 45,264 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482 + 2, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,839 hrs · 45,115 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 312, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,839 hrs · 45,115 cycles

FUSELAGE SKIN AT BS 500B, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,821 hrs · 45,096 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 58,036 hrs · 44,518 cycles

EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 DEF, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,824 hrs · 44,356 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 57,406 hrs · 44,026 cycles

AIR TURNBACK, AFTER TAKEOFF GEAR LEVER SELECTED TO UP, ALL GEARS RETRACTED NORMAL. WHEN LEVER SELECTED TO OFF RT MLG CAME DOWN. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,252 hrs · 43,901 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 972, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,252 hrs · 43,901 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 24L STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 57,078 hrs · 43,750 cycles

R2 DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO STOW AND REMOVE FROM CONTAINER. ADJUSTED GIRT BAR STOW CLIP HOOKS AT CONTAINER PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 56,947 hrs · 43,639 cycles

R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE INTO CONTAINER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,884 hrs · 43,582 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,785 hrs · 43,503 cycles

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

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 56,553 hrs · 43,320 cycles

R1 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,412 hrs · 43,208 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,630 hrs · 42,565 cycles

DURING SCHEDULED 1/4D CHECK, FOUND ROW 6 ABC BULLNOSE EMERGENCY EXIT ESCAPE AISLE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 500D, STRINGER 28L. REPAIRED CHORD PER SRM.

Part: FRAME — CORRODED (BULKHEAD) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CHORD FORWARD OF THE PRESSURE BULKHEAD AT BS 1016, STRINGER 27R CORRODED. REMOVED AND REPLACED CHORD SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500D, BETWEEN STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: TAB — CRACKED (ELEVATOR) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD ATTACHMENT FITTING. REMOVED AND REPLACED TAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CHANNEL STIFFENERS CORRODED AT BS 1016, BL 0, WL 198. REPAIRED PER ACO AND AD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKS AT THE FOLLOWING, BS 585, BS 692, BS 700, BS 703, ALL AT STRINGER 4L. REPAIRED SKIN PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,329 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 770, STRINGER 26R, BS 770, STRINGER 27L AND BS 770 STRINGER 27R. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,629 hrs · 42,564 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACK AT BS 920, BETWEEN STRINGERS 24R AND 25R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 55,528 hrs · 42,497 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING, RT INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,516 hrs · 42,493 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STRINGER 10R. REPAIRED SKIN CRACK PER SRM.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 55,528 hrs · 42,497 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED T/E WEDGE PANEL PER MM.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 55,516 hrs · 42,493 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE UPPER INBOARD SURFACE DELAMINATED. REPAIRED SLAT WEDGE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,535 hrs · 41,739 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E - 2, ABOVE STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 53,224 hrs · 40,697 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 52,938 hrs · 40,455 cycles

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

Part: HYDRAULIC LINE — CRACKED (LT MLG) · airframe 52,281 hrs · 39,938 cycles

AIR TURNBACK, DECLARED EMERGENCY, DURING DEPARTURE LOSS 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE. FOUND, LT MLG UPLOCK ACTUATOR LINE CRACKED. REMOVED AND REPLACED UPLOCK ACTUATOR LINE PER MM.

Part: FITTING — CORRODED (LT/RT MLG) · airframe 51,447 hrs · 39,279 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LEFT AND RIGHT MLG FWD WALKING BEAM FITTINGS PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 51,365 hrs · 39,224 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,787 hrs · 38,768 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,787 hrs · 38,768 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,111 hrs · 38,236 cycles

DURING SCHEDULED SERVICE CHECK, FOUND TWO BULBS INOP AT AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 49,882 hrs · 38,052 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED ABOVE AND INBD OF LOWER STOP. REMOVED AND REPLACED SVC DOOR PER MM.

Part: TARGET — OUT OF ADJUST (RT MLG) · airframe 49,008 hrs · 37,345 cycles

AIR TURNBACK, DURING DEPARTURE GEAR HANDLE WOULD NOT GO TO UP POSITION. FOUND AIR SAFETY SENSOR TARGET GAP AND GROUND SPOILER INTERLOCK CABLE OUT OF ADJUSTMENT. ADJUSTED TARGET GAP AND INTERLOCK CABLE PER MM.

Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 48,392 hrs · 36,865 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — BROKEN (SERVICE DOOR) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHTS BROKEN AT AFT ENTRY DOOR AND FWD SVC DOOR. REMOVED AND REPLACED EXIT LIGHTS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CABIN FLOORBEAM CRACKED AT BS 665, BBL 0. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CRACKED AT BS 727B, RT OUTBOARD. REPAIRED FLOORBEAM PER DLF XEA & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED IN FWD CABIN AT BS 294.5, LBL 11. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND 2 Z-FRAMES CRACKED, STR 9R, BS 807 AND BS 887. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 309.9, LBL 11, FWD CABIN. REPAIRED FLOORBEAM PER SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND LT ELEVATOR TAB DELAMINATED AT INBOARD CORNER. REPAIRED TAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND Z-FRAMES CRACKED AT BS 807 & BS 867, STR 9L. REPAIRED Z-FRAMES PER SRM.

Part: SKIN — CRACKED (RH HORIZ STAB) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND RH HORIZ STAB LOWER SKIN CRACKED AT REAR SPAR AT ELEV STA 83. REPAIRED SKIN PER BOEING S.B.

Part: RIB — CRACKED (LH HORIZ STAB) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB RIB CRACKED AT L/E, STA 161.04, # 11 RIB. R&R RIB PER SRM.

Part: BEARING — WORN (ELEVATOR) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND RT ELEVATOR PUSH ROD ATTACH BEARING WORN. REMOVED AND REPLACED BEARING AND SLEEVE PER MM.

Part: BEARING — WORN (TAIL) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND BOTH LH & RH ELEVATOR TORQUE TUBE PUSH ROD ATTACH BEARINGS WORN. R&R PUSH ROD BEARINGS PER OHM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND WEB CRACKED AT BS 665, BBL O. REPAIRED WEB PER BOEING SB & SWA RA.

Part: RIB — CRACKED (LH HORIZ STAB) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB L/E, # 11 RIB CRACKED. R&R RIB PER SRM.

Part: SLAT — CRACKED (LH WING) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND #1 L/E SLAT LOWER SURFACE SKIN CRACKED AT OTBD END. REPAIRED SLAT PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. R&R STR SPLICE PER SRM.

Part: SLAT — CRACKED (LH WING) · airframe 47,192 hrs · 35,861 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND # 1 L/E SLAT LOWER SKIN CRACKED AT OTBD END. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,497 hrs · 34,481 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 7 BS 178 BULKHEAD WEB CRACKS BETWEEN WL 210 - 218 & RBL 6.5 - LBL 9.5. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,497 hrs · 34,481 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED AT WL 207, LBL 26. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 45,294 hrs · 34,324 cycles

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

Part: COVER — MISSING (CABIN) · airframe 45,294 hrs · 34,324 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 4. INSTALLED TRACK COVER PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE) · airframe 43,377 hrs · 32,687 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP NEAR FWD GALLEY. RELAMPED PER MM.

Part: FMCS — MALFUNCTIONED (COCKPIT)

AIR TURNBACK, AFTER TAKEOFF, FIRST OFFICER'S AIR SPEED, ALTIMETER, AND VERTICAL SPEED INDICATORS FAILED. STICK SHAKER CAME ON FOR APPROX 1 MINUTE. PERFORMED DFCS AND FMCS BITE PER MM. INSPECTED AIRCRAFT AND TESTED SYSTEM PER MM. OPS CHECKED NORMAL.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND APPROX A 3 INCH LONG CRACK AT FUSELAGE SKIN, BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 2 VERTICAL CRACKS, BS 178 BULKHEAD WEB WL 188 BL 0. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD CRACKED AT BS 178, RBL 10. REPAIRED PER SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/4D CHECK, FOUND LT WHEEL WELL PRESSURE DECK CRACKED AT BEADED WEB, BS 663.75, LBL 30 TO LBL 33. REPAIRED PER DALFORT XEA NR X2-53-238.

Part: CONNECTOR — CHAFED (COCKPIT)

DURING SCHEDULED RON CHECK, NOTED ELECTRICAL SMELL IN COCKPIT, FOUND CHAFED AND BURNT WIRING AT CONNECTOR D00440. REPAIRED WIRING PER BOEING MM.

Part: SKIN — GOUGED (BS 727-747)

DURING SCHEDULED SERVICE CHECK, FOUND GOUGE IN ACFT SKIN ON RT SIDE BETWEEN BS 727 AND 747 BETWEEN STR 24R AND 23R. REPAIRED PER BOEING SRM.

Part: SLIDE — REQD SERVICE (PAX DOOR)

DURING WALKAROUND CHECK, FOUND FRONT ENTRY DOOR SLIDE NEEDS TO BE REPACKED. REPAIRED PER BOEING MM.

Part: SENSOR — MALFUNCTIONED (LT MLG)

FLIGHT ROUTED FROM TPA TO ABQ DIVERTED TO DAL WITH THE LEFT GEAR RED LIGHT ILLUM IN FLIGHT, BUT WENT OUT WHEN THE GEAR WAS LOWERED FOR LANDING. MADE AN UNEVENFUL LANDING. REMOVED AND REPLACED THE GEAR POSITION SENSOR AND C/W RETRACT CHECK WITH NO DISCREPANCY NOTED PER BOEING MM.

Part: FAN BLADES — BENT (NR 1 ENGINE)

DURING TAKEOFF AT GEAR RETRACTION NOTICED LOUD AIR NOISE AND VIBRATION ON NR 1 ENGINE. RETURNED TO PVD AND MADE AN UNEVENTFUL LANDING. INSPECTED ENG, FOUND THREE FAN BLADES BENT DUE TO BIRD STRIKE. REPLACED FAN SET OF BLADES PER BOEING MM.

Part: ENGINE — BIRD STRIKE (NR 1)

RETURNED TO PVD AND MADE AN UNEVENTFUL LANDING DUE TO BIRDSTRIKE TO NUMBER 1 ENGINE. PERFOMED BIRDSTRIKE INSPECTION, FOUND 3 ENGINE FAN BLADES BENT. REMOVED AND REPLACED COMPLETED SET OF FAN BLADES PER BOEING M/M, WITH A BORESCOPE SCHEDULED WITHIN 10 CYCLES .

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED 1 INCH ON OUTER SKIN. REPAIRED PER BOEING SRM.

Part: OIL SYSTEM — OVERSERV (RT PACK)

DURING PREFLIGHT CHECK, CABIN BEGAN FILLING WITH SMOKE AFTER TURNING ON RIGHT PACK. \N\NINSPECTED AND FOUND RIGHT PACK OVERSERVICED WITH OIL. DESERVICED TO PROPER LEVEL. OPERATED PACK FOR ONE HOUR, NO DISCREPANCIES

Part: SENSOR — FAILED (NLG)

NOSE GEAR INDICATES UNSAFE ON APPROACH, CYCLED GEAR, NO HELP. VISUALLY CONFIRMED GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT AT LAX. REPLACED NOSE GEAR LOCK SENSOR 5846 AND RETRACTION TESTED GEAR PER BOEING M/M.

Part: DOWNLOCK SENSOR — FAILED (NLG)

ON APPROACH, NOSE GEAR INDICATED UNSAFE RED LIGHT. CYCLED GEAR HANDLE, NO HELP. VISUALLY COMFIRMED GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. FERRY FLEW AIRCRAFT NOSE GEAR DOWN TO PHX. REMOVED AND REPLACED NOSE GEAR DOWNLOCK SENSOR, RIGGED, AND RETRACTION TESTED OK PER BOEING M/M.

Part: SKIN — DENTED (BS 372)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE DENTED AT BS 372, BETWEEN S17 ABD 18R. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 793)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED FORWARD OF AFT CARGO DOOR CUTOUT AT BS 793, RBL 30, WL 161. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 494)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, S18R. REPAIRED PER BOEING SRM.

Part: CLIPS — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS DAMAGED AT BS 747 S4L, BS 994 S6L, BS 663.75 S4L, BS 520 S4R, BS 578 S4L, BS 616 S4L, BS 460 S4R, BS 480 S4L, BS 500A 4R AND BS 500B S4L. REPLACED ALL PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK IN AFT SIDE OF PRESSURE BULKHEAD FWD CHORD TO VERTICAL STIFFENER AT BS 178 WL 184 LBL 5.7 AND AT WL 184 LBL 5.7. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 183)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 183 RBL 21 WL 184. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 282/290)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 282 AND AT 290, JUST BELOW S22R. REPAIRED BOTH PER BOEING SRM.

Part: STRINGER — PUNCTURED (BS 995)

DURING SCHEDULED D-CHECK, FOUND STRINGER HAD .25 PUNCTURE ON LOWER SIDE AT BS 995, S12L. REPAIRED PER TRAMCO EWO 96-0483.

Part: FLOOR BEAM — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM LOWER FLANGE CRACK AT BS 827, S20L, WL 176. REPAIRED PER BOEING SRM.

Part: SKIN — OIL CANNING (BS 390)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 390, BETWEEN S20 AND 21R. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 793)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED FWD OF AFT CARGO DOOR CUTOUT AT BS 793 RBL 30 WL 161. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — DAMAGED (BS 987)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM DAMAGED AT BS 987 RBL 44 WL 208 FWD SIDE OF UPPER FLANGE. REPAIRED BOTH PER BOEING SRM.

Part: FLOOR BEAM — DAMAGED (BS 987)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM AT BS 987 WL 208.1 LBL 44 DAMAGED ON FWD SIDE OF UPPER FLANGE. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 494/916)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 494, S18R, S18R AND AT BS 916, BETWEEN SS15 AND 16L. REPAIRED BOTH PER BOEING SRM.

Part: SKIN — DENTED (BS 372)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 372, BETWEEN S17 AND 18R. REPAIRED PER BOEING SRM.