N678AA
Registered owner: WINGS OVER TEXAS HOLDINGS LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
217 reports on file, 1995-02-14 – 2008-12-28.
Part: SKIN — CRACKED (BS 444-446 S17L) · airframe 72,221 hrs · 61,562 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 444 TO BS. 446, STR 17L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 947 S21R) · airframe 72,221 hrs · 61,562 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,949 hrs · 61,375 cycles
DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 15L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,949 hrs · 61,375 cycles
DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA.
Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 967, STR 27R AND STR 26R. REPAIRED SKIN PER SWA EA.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 767, STR 26R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND MLG W/W BS 663 VERTICAL STIFFENER CRACKED AT LBL 6.15. REMOVED AND REPLACED STIFFENER PER ACO.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND LT FWD KEEL BEAM CORRODED AT BS 500D. REMOVED AND REPLACED KEEL BEAM PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 767, STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CORRODED AT BS 785, STR 26R. REPAIRED STRINGER PER SRM.
Part: SHEAR TIE — CORRODED (BS 767 S27L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 767 S26R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 500A S28L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 500 S28R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CORRODED (BS 492 S27R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 492, STR 27R. REPAIRED SKIN PER SWA EA.
Part: FRAME — CRACKED (BS 328 S20R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (NR 1 SLAT) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.
Part: STRINGER — CORRODED (BS 492-500 S28R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28R CORRODED AT BS 492 TO BS 500. REPAIRED STRINGER PER SRM.
Part: SKIN — CRACKED (BS 967 S26R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 967, STR 26R. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CORRODED (BS 767 S25L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25L. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CORRODED (BS 967 S27R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CORRODED (BS 947) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 947, RBL 16. REPAIRED FRAME PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CRACKED AT BS 485, STR 28R. REPAIRED STRINGER PER SRM.
Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 71,464 hrs · 61,012 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP DAMAGED AT BS 767, STR 25R AND STR 26R. REPAIRED PER SWA EA.
Part: STRINGER — CRACKED (BS 506D S16L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16L CRACKED AT BS 506D. REPAIRED STRINGER PER SRM.
Part: SKIN — CRACKED (BS 505D S15L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 15L. REPAIRED SKIN PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 747 S26R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CORRODEED AT BS 747, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 520 S16R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SHEAR TIE — CRACKED (BS 500D S15L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 63,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,407 hrs · 63,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: STRINGER SPLICE — CORRODED (BS 360 S27L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 15R. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500D,STR 15R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SHEAR TIE — CORRODED (BS 360 S28L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (BS 303) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, BETWEEN WL 233 AND WL 238. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 291) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, BETWEEN WL 260 AND WL 350. REPAIRED SKIN PER SWA EA.
Part: BULKHEAD — CRACKED (BS 1016 S6L) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM.
Part: SKIN — CRACKED (BS 466 S16R) · airframe 71,407 hrs · 60,967 cycles
DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,404 hrs · 60,240 cycles
R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,024 hrs · 59,957 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: WEB — CRACKED (NLG W/W) · airframe 69,751 hrs · 59,735 cycles
DURING SCHEDULED BRDG CHECK, FOUND NOSE W/W RIGHT UPPER CEILING PANEL WEB CRACKED AT OUTBOARD END. REPAIRED WEB PER ER.
Part: FLAP — DELAMINATED (LT WING) · airframe 69,751 hrs · 59,735 cycles
DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.
Earlier reports · 1995–2007 · 166 reports
2007
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,961 hrs · 58,368 cycles
DURING MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405.5, STR 17L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 578 S10L) · airframe 67,746 hrs · 58,203 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 410) · airframe 67,746 hrs · 58,203 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT BS 410, LBL 3. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,280 hrs · 57,826 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,280 hrs · 57,826 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,280 hrs · 57,826 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 15L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 780 S19L) · airframe 66,276 hrs · 57,064 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER SRM.
2006
Part: SKIN — CRACKED (BS 765 S19L) · airframe 65,276 hrs · 56,289 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19L. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (R WING FORE FLAP) · airframe 65,276 hrs · 56,289 cycles
DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 64,425 hrs · 55,611 cycles
DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: LAMP — INOPERATIVE (CABIN) · airframe 64,312 hrs · 55,514 cycles
DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT L2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,090 hrs · 55,348 cycles
FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: MOTOR — FAULTY (TE FLAPS) · airframe 63,952 hrs · 55,226 cycles
AIR TURNBACK, FLAPS WOULD NOT RETRACT AFTER TAKEOFF. TRAILING EDGE FLAP DRIVE A/C CIRCUIT BREAKER TRIPPED DURING ALT EXTENSION. REMOVED AND REPLACED FLAP HYDRAULIC MOTOR PER MM.
Part: WINDOW — ARCED (COCKPIT) · airframe 63,310 hrs · 54,737 cycles
AIR TURNBACK, R2 COCKPIT WINDOW ARCED & SHATTERED. REMOVED AND REPLACED R2 COCKPIT WINDOW & HEAT CONTROLLER PER MM.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING LT AND RT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED SIGN PER MM.
Part: BEAR STRAP — CORRODED (BS 794) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 794, RBL 8, WL 149. REPAIRED SKIN PER BFG ER.
Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER BFG ER.
Part: STRINGER — CORRODED (BS 348) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 348, STR 25R. REPAIRED STRINGER PER SRM.
Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.
Part: SHEAR TIE — CORRODED (BS 360) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, LBL 14, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CORRODED (BS 847) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT AFT CARGO DOOR CUTOUT, BS 847, RBL 34 TO RBL 40, WL 162. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FWD CARGO) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO BAY CUTOUT, LOWER OUTBOARD CORNER, NR 5 STOP FITTING. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (BS 1007) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1007, LBL 28, WL 208. REPAIRED FLOORBEAM PER BFG ER & SRM.
Part: FRAME — CRACKED (BS 188) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (BS 827) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (BS 188) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 360) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CRACKED (BS 947) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LBL 53, WL 208. REPAIRED FLOORBEAM PER BFG ER.
Part: SPLICE — CORRODED (BS 907) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 907, STR 25R. R & R SPLICE PER SRM.
Part: SHEAR TIE — CORRODED (BS 500D) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (BS 947) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. R & R CLIP PER SRM.
Part: BEAM — CRACKED (LT MLG WW) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 680, LBL 68, WL 170. REMOVED AND REPLACED VERTICAL BEAM PER SRM.
Part: CREASE BEAM — CORRODED (BS 746) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 746, WL 208. REPAIRED CREASE BEAM PER SRM.
Part: FRAME — CRACKED (BS 727D) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SRM.
Part: FLOOR PANEL — CRACKED (COCKPIT FLOOR) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, WL 207. REPAIRED WEB PER SRM.
Part: FRAME — CRACKED (BS 294) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, RBL 56, WL 208. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM.
Part: SHEAR TIE — CORRODED (BS 867) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 867, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: CREASE BEAM — CORRODED (BS 778) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 778, RBL 68, WL 208. REPAIRED WEB PER SRM.
Part: SPLICE — CRACKED (BS 360) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED AT BS 360, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.
Part: CREASE BEAM — CORRODED (BS 737A) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 737A, LBL 65, WL 208. REPAIRED WEB PER SRM.
Part: FRAME — CRACKED (BS 787) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME PER SRM.
Part: CREASE BEAM — CORRODED (BS 913) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 913, LBL 60, WL 208. REPAIRED WEB PER SRM.
Part: STRINGER — CORRODED (BS 892) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 892, STR 24L. REPAIRED STRINGER PER SRM.
Part: FRAME — CRACKED (BS 907) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME PER SRM.
Part: SPLICE — CRACKED (BS 360) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.
Part: FRAME — CRACKED (BS 847) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9L. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (BS 500C) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (BS 767) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 9R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 807) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9L. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 380) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (BS 927) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (BS 847) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (BS 887) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 9L. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (BS 1010) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1010, STR 4R. REPAIRED SKIN PER SRM.
Part: SHEAR TIE — CORRODED (BS 500A) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (BS 747) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (BS 787) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 16L. REMOVED AND REPLACED CLIP PER SRM.
Part: SHEAR TIE — CORRODED (BS 500B) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 500C) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.
Part: CREASE BEAM — CORRODED (BS 737A) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 737A, LBL 65, WL 208. REPAIRED CREASE BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 2R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727A, BETWEEN STR 5R TO STR 7R. REMOVED AND REPLACED CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (BS 616) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 767) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727A, BETWEEN STR 7L & STR 8L. REMOVED AND REPLACED CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (BS 767) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 5R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 616) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 578) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 597) · airframe 63,213 hrs · 54,666 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.
2005
Part: SKIN — CRACKED (BS 356) · airframe 63,101 hrs · 54,577 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 356, STR 18R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 727E) · airframe 62,663 hrs · 54,225 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 790) · airframe 62,522 hrs · 54,117 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 795) · airframe 62,522 hrs · 54,117 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 795, STR 18L. REPAIRED SKIN PER SRM.
Part: SHEAR TIE — CRACKED (BS 380) · airframe 62,502 hrs · 54,098 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 380, ABOVE STR 15L. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (BS 376) · airframe 62,502 hrs · 54,098 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, BETWEEN STR 14L AND STR 15L. REPAIRED SKIN PER SWA EA.
Part: LATCH — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 60,704 hrs · 52,581 cycles
DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE RELEASE MECHANISM OUT OF ADJUST. ADJUSTED RELEASE MECHANISM PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,704 hrs · 52,581 cycles
DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SKIN — CRACKED (L2 DOOR) · airframe 60,704 hrs · 52,581 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 60,704 hrs · 52,581 cycles
DURING SCHEDULED C1 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: GASPER FAN — OVERHEATED (E & E BAY) · airframe 60,147 hrs · 52,149 cycles
DIVERSION, DECLARED EMERGENCY. F/A REPORTED A BURNING ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,916 hrs · 51,981 cycles
DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,768 hrs · 51,864 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 482B, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA.
2004
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,749 hrs · 51,054 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,689 hrs · 51,003 cycles
DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA.
Part: TORQUE TUBE — WORN (TAIL) · airframe 57,902 hrs · 50,402 cycles
DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE, AFT BUSHING AND BEARING PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,831 hrs · 49,529 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STRINGER 16L. REPAIRED FUSELAGE SKIN PER SRM.
2003
Part: CARRIAGE — CORRODED (LT WING TE FLAP) · airframe 56,046 hrs · 48,915 cycles
DURING SCHEDULED C4 CHECK, FOUND NR 1 T/E FLAP SPINDLE CORRODED AT SHAFT UNDER THRUST BEARING. REMOVED AND REPLACED NR 1 T/E FLAP CARRIAGE ASSY PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 55,467 hrs · 48,452 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BS 460, ABOVE STR 14L AND BS 400 BETWEEN STR 14R AND STR 13R. REPAIRED FRAMES PER SRM.
Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 55,422 hrs · 48,411 cycles
DURING SCHEDULED 1/4D CHECK, FOUND CENTER FLOORBEAM CRACKED AT BS 663.75, BL 0. REPAIRED FLOORBEAM PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,422 hrs · 48,411 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,422 hrs · 48,411 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, STR 28R TO STR 28L. REPAIRED SHEAR TIE SECTION PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 55,422 hrs · 48,411 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN STR 28R AND STR 28L. REPAIRED FRAME PER SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,422 hrs · 48,411 cycles
DURING SCHEDULED 1/4D CHECK, FOUND RT KEELBEAM CORRODED BETWEEN BS 500D AND BS 520,STR 28R. REPAIRED KEEL BEAM PER SWA EA.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,558 hrs · 47,723 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,558 hrs · 47,723 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,558 hrs · 47,723 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, BELOW STR 14L. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,053 hrs · 47,339 cycles
DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 506, STR 14L & BS 510, STR 10R. REPAIRED SKIN PER SRM.
2002
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,134 hrs · 46,612 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 625 AND BS 713. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,429 hrs · 45,258 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, ABOVE STR 4L. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 49,942 hrs · 44,066 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
2001
Part: TORQUE TUBE — WORN (LH ELEVATOR) · airframe 48,772 hrs · 43,180 cycles
DURING SCHEDULED C4 CHECK, LH ELEVATOR FAILED FREE PLAY CHECK. R&R ELEVATOR BUSS ASSY OUTPUT TORQUE TUBE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 48,764 hrs · 43,174 cycles
DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED 4.4 INCHES LONG AT BS 498, STR 10R. REPAIRED SKIN PER SWA RA 1-353-2641.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,728 hrs · 42,304 cycles
DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS INOP, AT ROW 9 DEF AND ROWS 7 AND 11 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 11, WL 218. REPAIRED BULKHEAD WEB PER SRM.
Part: BEAM — CRACKED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL BEAM PER SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 616 FRAME SUPPORT ANGLE CRACKED AT WING TERMINAL ATTACHMENT POINT. REPAIRED ANGLE PER SWA TI-153-018.
Part: LENS — CRACKED (CABIN) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT OVERWING EMERGENCY LIGHT LENSES CRACKED. REMOVED AND REPLACED LENSES PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT, FWD CORNER. REPAIRED SKIN PER SRM.
Part: BRACKET — BROKEN (SERVICE DOOR) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET BROKEN. R&R BRACKET PER MM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 46 TO LBL 15. REPAIRED FLOORBEAM PER SWA T1.
Part: BRACKET — CORRODED (CABIN) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR MOUNT BRACKETS CORRODED ON CABIN FLOOR. R&R BRACKETS PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, RBL 14 & RBL 28. REPAIRED FLOORBEAM PER SRM.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STR 24L CORRODED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 6.8, WL 201. REPAIRED BULKHEAD WEB PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 294, BL 0 TO LBL 19. REPAIRED FLOOR BEAM PER SWA T1.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STR 27R CORRODED BETWEEN BS 1006 & 1016. REPAIRED STR PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL 10 TO RBL 10. REPAIRED FLOOR BEAM PER SWA T1.
Part: FLAP — CRACKED (RT WING) · airframe 47,452 hrs · 42,077 cycles
DURING SCHEDULED 1/2D CHECK, FOUND RT WING AFT FLAP DELMINATED AT INBD EDGE & CRACKED AT FWD EDGE IN FRONT OF FIRST SET OF FLIGHT BEARINGS. R&R AFT FLAP PER MM.
Part: WIRE — LOOSE (COCKPIT) · airframe 47,093 hrs · 41,795 cycles
AIR TURNBACK - DURING CRUISE, R1 COCKPIT WINDOW OVERHEAT LIGHT ILLUMINATED AND C/B TRIPPED. RETURNED TO PHX DUE TO DESTINATION WEATHER. FOUND R1 WINDOW OVERHEAT SENSOR WIRE LOOSE. SECURED WIRE PER MM.
Part: INDICATOR — OUT OF TOLERANCE (EVAC SLIDE) · airframe 47,059 hrs · 41,767 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.
2000
Part: STRAP — CRACKED (FUSELAGE) · airframe 46,032 hrs · 40,909 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 STRAP CRACKED AT WL 188, BL 0. REPAIRED STRAP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 45,952 hrs · 40,855 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT CHORD CRACKED AT WL 207. REMOVED AND REPLACED CHORD PER AC 7342-53.
Part: FRAME — CRACKED (FUSELAGE) · airframe 45,952 hrs · 40,855 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT CHORD CRACKED AT WL 207. REMOVED AND REPLACED LT SIDE CHORD PER ACO 7338-53.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,952 hrs · 40,855 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD 3 CRACKS AT FASTENER HOLES WL 234, LBL 11 - RBL 10. REPAIRED BULKHEAD PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 45,900 hrs · 40,804 cycles
DURING SCHEDULED C1 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 510, STR 12L. REPAIRED SKIN PER SRM.
Part: BRACKET — LOOSE (GIRT BAR) · airframe 44,095 hrs · 39,273 cycles
DURING SCHEDULED C 3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR AFT ATTACH FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.
Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 44,095 hrs · 39,273 cycles
DURING SCHEDULED C 3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR LOW. R & R SLIDE ASSY PER MM.
Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 44,005 hrs · 39,206 cycles
AFT SERVICE DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: GIRT BAR — DAMAGED (ESCAPE SLIDE)
FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO STOW IN CONTAINER. ADJUSTED GIRTBAR SLIDE BRACKET PER MM.
Part: CONTROLER — ERRATIC (CABIN PRESSURE)
DIVERSION, DURING CRUISE, FLIGHT LEVEL AT 37,000 FEET, CABIN ALTITUDE CLIMBED 10,000 FEET, SETTING OFF THE WARNING HORN. INITIATED EMERGENCY DESCENT USING THE MANUAL CONTROLLER. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM.
Part: KEEL BEAM — CORRODED (BS 540)
DURING SCHEDULED C2 CHECK, FOUND RT KEEL BEAM OUTBOARD CHORD CORRODED FWD OF BS 540. REPAIRED KEEL BEAM PER SWA RA NR 1-353-2203.
1999
Part: SWITCH — INOP (LT LE FLAP)
AIR TURNBACK DUE TO NR 2 KRUEGER FLAP AND LEADING ENG LIGHT FLASHING ON PANEL. REPLACED PROXIMITY SWITCH PER MM.
1998
Part: LIGHT — INOP (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND ONE FLOOR TRACK LIGHT INOPERATIVE. RELAMPED PER BOEING MM.
Part: BATTERY — DISCHARGED (CABIN)
DURING WALKAROUND, FOUND EMERGENCY EXIT LIGHTING PARTIALLY INOP IN FORWARD CABIN AREA. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.
Part: SLIDE — LOW PRESS (AFT ENTRY)
DURING SCHEDULED A1, FOUND AFT ENTRY EMERGENCY SLIDE PRESSURE BELOW SERVICEABLE LIMIT. REPLACED PER BOEING M/M.
1997
Part: FAN — FAILED (AC BAY)
NOTED A HOT RUBBER SMELL WAS NOTED WHEN GASPER FAN WAS SWITCHED ON, AND DISSIPATED WHEN SWITCHED OFF. REPLACED FAN PER BOEING M/M.
Part: SKIN — CRACKED (PAX DOORWAY)
DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOORWAY UPPER HINGE CUTOUT CRACKED .25. REPAIRED PER BOEING SRM.
1996
Part: PROX SWITCH — FAILED (LANDING GEAR)
AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RISE PAST THE OFF POSITION. CREW USED OVERRIDE TO RAISE GEAR. WARNING HORN SOUNDED WITH FLAPS UP, PRESSURIZATION AND ALL OTHER INDICATIONS NORMAL. DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. FOUND DEFECTIVE AIR/GROUND SENSING PROXIMITY SWITCH. REPLACED SWITCH AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M.
Part: SKIN — DENTED (BS 956)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 956, 1 BELOW S19R. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — DAMAGED (BS 277)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE DAMAGED AT BS 277, BETWEEN S23 AND 24R. REPAIRED PER BOEING SRM.
Part: FRAME — CORRODED (BS 294)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AROUND GROUNDING WIRES AT BS 294, LBL 56, WL 219. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AFT SIDE AT RBL 1, WL 189. REPAIRED PER BOEING SRM.
Part: BULKHEAD ANGLE — CRACKED (BS 729)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 729, BL 0, WL 164. REPLACED CRACKED SECTION PER BOEING SRM.
Part: FRAME — CRACKED (BS 827)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 827, LBL 32, WL 163. REPAIRED PER BOEING SRM.
Part: CLIPS — CRACKED (BS 663/867)
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663 S10L ,S10R AND AT BS 867 S9L. REPLACED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED AT RBL 5.7, WL 193 TO 202, AT LBL 5.7, WL 195 TO 202, AT RBL 10 TO 5.7 AND LBL 5.5, WL 207 TO 214. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 455/500)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 455, S17 TO 18L AND AT BS 500A PLUS 15 BETWEEN S14 AND 15L. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 474)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 474, S22 TO 23L. REPAIRED PER BOEING SRM.
Part: SUPPORT — CRACKED (BS 540)
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT FASTENER HOLE BS 540, LBL 1, WL 208. REPLACED PER BOEING SRM.
Part: FRAME — CORRODED (BS 219)
DURING SCHEDULED D-CHECK, FOUND UPPER SIDE OF FRAME CORRODED AT AFT SIDE OF LOWER NOSE COMPARTMENT, BS 219 WL 165 LBL 7. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (BS 639)
DURING SCHEDULED D-CHECK, FOUND WEB CRACKS AT BS 639, RBL 65, WL 221 AND AT BS 616, RBL 65, WL 221. REPLACED PER BOEING SRM.
Part: SPLICE — CRACKED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4R AND S4L. REPLACED PER BOEING SRM.
Part: STRAP — CRACKED (BS 315)
DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TENSION STRAP CRACKED AT BS 315, WL 200, RBL 30. REPAIRED PER BOEING SRM.
Part: SUPPORT — CORRODED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BETWEEN BS 277 AND BS 294. ALSO, BETWEEN BS 294 AND BS 312, LBL 12. REPAIRED PER BOEING SRM.
Part: MOP SILL — CORRODED (BS 312/322)
DURING SCHEDULED D-CHECK, FOUND MOP SILL CORRODED BETWEEN BS 312 AND BS 322, WL 208. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (GALLEY DR CUTOUT)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF FORWARD GALLEY DOOR CUTOUT. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 570)
DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 45 TO 48 WL 170. REPLACED PER BOEING SRM.
Part: SKIN — DENTED (BS 298/315)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 298 BETWEEN S28R AND L AND AT BS 315 BETWEEN S28L AND R. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 1075-1080)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AND GOUGED AT BS 1075 TO 1080, BETWEEN S18L AND 16L. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 996)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AFT OF AFT ENTRY DOOR JUST BELOW LIGHT AT BS 996 LEFT SIDE S12. REPAIRED PER BOEING SRM.
1995
Part: DOOR FRAME — CRACKED (FS 787)
DURING SCHEDULED B1 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT BS 787. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.