N674AA

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,707 hrs · 55,983 cycles

FUSELAGE SKIN CRACKED AT BS 817, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,281 hrs · 55,638 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,281 hrs · 55,638 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503L, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,281 hrs · 55,638 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,281 hrs · 55,638 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 775, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,217 hrs · 55,632 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26L. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 65,535 hrs · 55,055 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,283 hrs · 54,871 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 21R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,277 hrs · 54,866 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERIES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,111 hrs · 53,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,111 hrs · 53,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742E, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,111 hrs · 53,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 23L. REPAIRED SKIN PER SWA EA.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 252, RBL 8. REPAIRED PANEL PER ACO.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 11 DEF. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SHEAR TIE — CORRODED (BS 827) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, RBL 3. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 303 S17L) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, STR 17L. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: STRINGER — CRACKED (BS 304 S4L) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER WEB CRACKED AT BS 304, STR 4L. REMOVED AND REPLACED STRINGER WEB PER SRM.

Part: STRINGER — CORRODED (BS 503A S28L) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28L CORRODED AT BS 503A. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 500B S27R) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 27R CORRODED AT BS 500B. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 446) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT AT BS 446, BL 0. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 500B S27R) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 26. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S6L) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 987, RBL 19. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 1016, LBL 9. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 16L CRACKED AT BS 358. REPAIRED STRINGER PER ACO.

Part: SKIN — CRACKED (BS 505D S15R) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 766 S24L) · airframe 63,487 hrs · 53,510 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 63,487 hrs · 53,510 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,798 hrs · 52,181 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 869, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,798 hrs · 52,181 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 785, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 934) · airframe 61,627 hrs · 52,045 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727C) · airframe 60,963 hrs · 51,513 cycles

DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727E) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (BS 500D) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (BS 765) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 22R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (BS 764) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 4R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (BS 762) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 762, BETWEEN STR 22R TO STR 23R. REPAIRED SKIN PER BFG ER.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,139 hrs · 50,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 59,922 hrs · 50,701 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,814 hrs · 50,612 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER INTERFERING WITH RECYCLE BIN COMPARTMENT DOOR. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,814 hrs · 50,612 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,352 hrs · 50,237 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 16, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 59,352 hrs · 50,237 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY BULLNOSE LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,235 hrs · 50,141 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,639 hrs · 49,651 cycles

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

Part: LIGHT — BROKEN (R2 DOOR) · airframe 58,567 hrs · 49,586 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY & BATTERY PACK PER MM.

Part: GCU — FAULTY (NR 2) · airframe 58,434 hrs · 49,482 cycles

AIR TURNBACK - DECLARED EMERGENCY. OBSERVED SMOKE FROM BEHIND F/O'S SEAT. NR 2 GCU FAILED. REMOVED AND REPLACED NR 2 GCU PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,409 hrs · 49,462 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,409 hrs · 49,462 cycles

DURING SCHEDULED C4 CHECK, FOUND CRACKED STRINGER AT BS 443, STR 25L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 49,456 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 26L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 58,399 hrs · 49,456 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED ON OUTBOARD EDGE LOWER SKIN. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,548 hrs · 48,752 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 786, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: GATE — CRACKED (R2 DOOR) · airframe 56,613 hrs · 48,120 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,609 hrs · 48,116 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, STRINGER 19R AND BS 727D, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,609 hrs · 48,116 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,723 hrs · 47,408 cycles

DURING SCHEDULED C1 CHECK, FOUND STRINGER 19R AT BS 735, CRACKED. REPAIRED STRINGER PER SRM.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 55,688 hrs · 47,381 cycles

DECLARED EMERGENCY/DIVERSION, NR 1 ENGINE A SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG UPLOCK HYDRAULIC LINE PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,189 hrs · 46,980 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 727 + 14, LBL 9, STRINGER 27L, CORRODED. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT KEEL BEAM AT BS 767 TO BS 773, RT KEEL BS 727 + 13, AND RT BS 500D TO BS 540, CORRODED. REPAIRED KEEL BEAM PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES AT RT KEEL BEAM BS 727E INBOARD, BS 727E OUTBOARD, BS 767 OUTBOARD, CRACKED. REPAIRED SHEAR TIES PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 727, RT AND LT KEEL BEAM VERTICAL STIFFENERS CRACKED. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY LIGHT PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT WEB AT BS 840, BETWEEN STRINGERS 25L AND 26L, CORRODED. REMOVED AND REPLACED WEB SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED AT STRINGER 9L, BS 887, BS 847, BS 827, BS 787, BS 727E. REPAIRED FRAMES PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 420, STR 25L TO STR 26L. REPAIRED FRAME PER ER AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT STRINGER 9R, BS 807, BS 867, BS 827. REPAIRED FRAMES PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 460, STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, OUTBOARD OF RT KEEL BEAM. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 492, STR 24R-STR 25R, AND BS 616, RBL 65, WL 202. REPAIRED FRAMES PER ER AND SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 480, STR 26L. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE LT KEEL BEAM CORRODED AT BS 500D TO BS 540. REPAIRED KEEL BEAM SECTION PER ER.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT IN SPAR STA 125. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (KEELBEAM) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 500D, LT AND RT KEEL BEAM, AND BS 520, LT KEELBEAM. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (BULKHEAD) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BLKHD UPPER CHORD CRACKED AT WL 234, LBL 25. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND BS 188 FRAME CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (LOWER FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA LOWER FUSELAGE SHEAR TIES CORRODED AT BS 500D, LBL 6 TO LBL 10, AND BS 847, RBL 5. REPAIRED SHEAR TIES PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND CRACK INDICATION AT BS 1016 BULKHEAD, STR 15L. REPAIRED BULKHEAD PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CRACKED AT BS 520. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACES CORRODED AT BS 344, LBL 10 TO LBL 65, BS 328, RBL 15 TO RBL 50, AND BS 312, LBL 8 TO RBL 49. REPAIRED FLOORBEAMS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1016, LBL 5, WL 190.5. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 25L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION, LEFT AND RIGHT AFT SPAR CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 727D, STR 7R, AND BS 727C, STR 7R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE 4L CRACKED AT BS 360. REMOVED AND REPLACED SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 551,887 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 727B+. REPAIRED RT CREASE BEAM PER SRM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA LONGITUDINAL FLOORBEAMS CRACKED AT LBL 26, BS 708, BL 0, BS 710, AND RBL 25, BS 712. REPAIRED BEAMS PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, BETWEEN STRINGERS 26L AND 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,970 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 188, LT AND RT SIDES, WL 208. REPAIRED FRAMES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,188 hrs · 46,978 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,869 hrs · 46,685 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN HAS CRACK AT 727D STRINGER 23R. REPAIRED CRACK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,868 hrs · 45,910 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 520, STR 12L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,868 hrs · 45,910 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG AT BS 927, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,961 hrs · 45,160 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 747 AT STR 23R AND BS 970 AT STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,992 hrs · 43,631 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 50,258 hrs · 43,026 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: MECHANISM — WORN (ELEVATOR TAB) · airframe 49,821 hrs · 42,688 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB LOCKOUT MECHANISM AND LT ELEVATOR TAB PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 49,810 hrs · 42,675 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,465 hrs · 42,419 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 6, STR 24R. REPAIRED SKIN PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 49,465 hrs · 42,419 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT DOUBLER STRAP CRACKED AT BS 303, STR 13L. REPAIRED DOUBLER STRAP PER SWA RA.

Part: PANEL — DELAMINATED (T/E FLAP) · airframe 47,599 hrs · 40,882 cycles

DURING SCHEDULED C4 CHECK, FOUND T/E INBOARD MIDFLAP WEDGE PANEL DELAMINATED AT OUTBOARD UPPER SURFACE. REMOVED AND REPLACED WEDGE PANEL PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,278 hrs · 40,625 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SPOILER — DELAMINATED (LH WING) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND # 3 SPOILER DELAMINATED. R&R SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,278 hrs · 40,626 cycles

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

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. R&R EVAC SLIDE PER MM.

Part: SPOILER — DELAMINATED (RH WING) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND # 7 SPOILER DELAMINATED. R&R SPOILER PER MM.

Part: FITTING — LOOSE (CABIN) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH ENTRY DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTINGS LOOSE. R&R ATTACH FITTING FASTENERS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,278 hrs · 40,626 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 18 ABC. RELAMPED EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,907 hrs · 40,326 cycles

EEPLS INOP AT ROW 20. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 46,907 hrs · 40,326 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 5 DEF. INSTALLED EXIT LIGHT LENS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 46,900 hrs · 40,317 cycles

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

Part: WIRE — EXPOSED (CABIN) · airframe 46,523 hrs · 39,973 cycles

EEPLS WIRES EXPOSED AT ROW 9. SECURED EEPLS WIRES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,125 hrs · 39,640 cycles

DURING SCHEDULED SERV CHECK FOUND 2 CRACK IN FUSELAGE SKIN AT BS 727E, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,795 hrs · 39,351 cycles

DURING SCHEDULED C2 CHECK, FOUND 3 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 767, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,795 hrs · 39,351 cycles

DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 760, STR 18R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,234 hrs · 38,119 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,234 hrs · 38,119 cycles

DURING SCHEDULED SPECIAL VISIT FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 749, STR 18R. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (LT & RT WING) · airframe 44,197 hrs · 38,080 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT MLG WALKING BEAM HANGAR SUPPORT FITTINGS CORRODED. REMOVED AND REPLACED LT AND RT FITTINGS PER SRM.

Part: GIRT BAR — WORN (ESCAPE SLIDE) · airframe 42,971 hrs · 37,019 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY WORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF POSITION (ESCAPE SLIDE) · airframe 42,971 hrs · 37,019 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EEPLS LIGHT LENS ASSY MISSING AND LIGHT INOP. REPLACED LENS AND LIGHT BULB PER MM.

Part: FASTENER — LOOSE (GIRT BAR)

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT BAR RETAINING BRACKET FASTENERS LOOSE. REMOVED AND REPLACED BRACKET FASTENERS PER SRM.

Part: COVER — LOOSE (CABIN)

EEPLS TRACK COVERS LOOSE. SECURED TRACK COVERS PER MM.

Part: SLIDE — LOOSE (SERVICE DOORWAY)

FWD SERVICE DOOR EVACUATION SLIDE LOOSE AT DOOR. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 500)

DURING RON CHECK, FOUND FUSELAGE SKIN CRACKED APPROX BS 500C+5, STRINGER 15L. REPAIRED SKIN PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A .25 INCH CRACK AT BULKHEAD BS 178 WEB, LBL 12, WL 234. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 629)

DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BOTTOM RIVET FWD SIDE OF LT BS 629, WL 202. REPAIRED FRAME PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT BS 178 BULKHEAD WEB, LBL AND RBL 1, WL 187. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 326 BL 0. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 277)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT T-CAP NUT PLATE HOLES ON BS 277, LBL 30, LBL 38, AND LBL 49. REPAIRED PER SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 663, STRINGERS 10L AND 10R. REMOVED AND REPLACED CLIPS PER SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT STA 178, LBL 29, WL 207. REMOVED AND REPLACED CHORD ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 328 AROUND SCREW HOLES, RBL 25 TO RBL 43. REPAIRED PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND THRU NDT INSPECTION 2 CRACKS ON PRESS BULKHEAD WEB AT BS 178, LBL 5 AT WL 211.5 AND 201 (CRACKS ARE APPROX 1.5 INCHES LONG). REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 340)

DURING SCHEDULED 1/2D CHECK, FOUND CRACK IN SKIN AFT LWR CORNER OF FWD SERVICE DOOR CUTOUT. HFEC INSPECTION VERIFIED. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 294.5, RBL 20-RBL 57. REPAIRED BEAM PER SRM.

Part: WEB — CRACKED (BS 664)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT STA 664, LBL 32. REPAIRED PER SWA RA NR 1-353-2029.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND 4 CRACKS AT BULKHEAD WEB BS 178, RBL 7 WL 201, WL 213 AND RBL 5, WL 213, WL 198. REPAIRED PER SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND STUB FRAME CRACKED AT UPPER FWD CORNER OF SERVICE DOOR, BS 294.5. REPAIRED PER SRM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CORROSION BULGING DAMAGE AT BS 727 AT S14R. REPAIRED PER SWA RA 1-353-2014.

Part: SKIN — CORRODED (BS 500 & 540)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CORROSION DAMAGE AT BS 540, 500C, 500D AT S28L. REPAIRED PER SWA RA 1-353-2015.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND INSPECTION, FOUND 1 RED FLOOR EMERG LIGHT INOP. REPLACED LENS ASSEMBLY PER BOEING M/M.

Part: INDICATOR — MALFUNCTIONED (NR 2 ENGINE)

AFTER TAKEOFF, NR 2 ENGINE OIL LOW PRESSURE DROP AND TEMP RISE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED OIL TRANSMITTER AND INDICATOR PER BOEING M/M.

Part: SKIN — CRACKED (BS 787)

DURING BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, BETWEEN S22 AND 23. REPAIRED PER BOEING SRM.

Part: SENSOR — FAILED (NLG)

AFTER TAKEOFF, NOSE GEAR RED AND GREEN LIGHTS ILLUMINATED WITH GEAR IN UP POSITION. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED POSITION SENSOR, PC CIRCUIT CARD, AND PERFORMED GEAR RETRACT TEST PER BOEING M/M.

Part: PULLEYS — LACK OF LUBE (AILERONS)

CREW REPORTED AILERONS BINDING. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. INSPECTED AILERON CONTROL SYSTEM, NO DEFECTS. LUBED AILERON PULLEYS PER BOEING M/M.

Part: STRAP — CRACKED (BS 328)

DURING SCHEDULED C1 CHECK, FOUND TIE STRAP CRACKED AT BS 328, LOWER E & E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.