N513SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,793 hrs · 60,995 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847+ 51/2, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,793 hrs · 60,995 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,793 hrs · 60,995 cycles

DURING SCHEDULED OTS CHECK, FOUND RT INBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,793 hrs · 60,955 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,793 hrs · 60,955 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 769.5 TO BS 771.7, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,793 hrs · 60,955 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 762, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,793 hrs · 60,955 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK ON SKIN STA 960, BELOW STR 21. REPAIRS SKIN CRACK PER EA.

Part: LENS — PUNCTURED (CABIN) · airframe 64,704 hrs · 60,902 cycles

LT EMERGENCY EXIT LIGHT LENS PUNCTURED AT ROW 11. REMOVED AND REPLACED LENS IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 64,657 hrs · 60,874 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 6. SECURED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,175 hrs · 60,559 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT R1 DOOR. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: ADAPTER — FAULTY (FUEL SYSTEM) · airframe 63,451 hrs · 60,082 cycles

WITH FUEL IN CENTER TANK AND WITH ALL PUMP SWITCHES ON, FUEL TRANFERS TO RT MAIN TANK AT RATE OF 20 LBS PER MIN. REMOVED AND REPLACED NR 1 AND NR 2 SHUTOFF VALVE ADAPTER HOUSING ASSY PER MM. REMOVED AND REPLACED NR 2 TANK COUPLER O-RING.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,401 hrs · 60,042 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE IAW MT.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 63,249 hrs · 59,935 cycles

AFTER LEVEL AT FL 350, NOTICED ODOR IN COCKPIT AND CABIN. TURNED OFF GASPER FAN, ODOR CONTINUED. TURNED OFF RECIRC FAN ODOR STOPPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 63,021 hrs · 59,779 cycles

RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 62,961 hrs · 59,740 cycles

DURING SCHEDULED HC1 CHECK FOUND, LT EMERGENCY EXIT LIGHT INOP AT ROW 15. RECONNECTED WIRE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FWD CORNER. REPAIRED SKIN PER EA.

Part: ANGLE — CRACKED (ELEVATOR) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT ELEVATOR L/E STABILIZER ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 927 TO BS 947.5, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663, RBL 24.5. REPAIRED BEAM PER EA.

Part: RIB — CRACKED (LT WING) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB CHORD PER ACO.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 4 SLAT I/B END UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLIGHT DECK FLOOR WEB CUTOUT HOLE CRACKED AT BS 246.6+2.5, RBL 22.5. REPAIRED WEB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 658, RBL 24.5. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND CHANNEL CORRODED AT BS 727B+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B AFT FLAP O/B SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 658, LBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING FORE FLAP UPPER SKIN DELAMIINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP O/B SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING T/E AILERON CONTROL TAB DELAMINATED. REPAIRED TAB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, LBL 24.5. REPAIRED BEAM PER EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLIGHT DECK FLOOR WEB CUTOUT HOLE CRACKED AT BS 246.6+2.5, RBL 17. REPAIRED WEB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20YCHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REMOVED AND REPLACED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20YCHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3.0. REMOVED AND REPLACED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732B, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 28L TO BS 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 27R TO BS 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 25R TO BS 26R. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 1006 TO BS 1016, STR 26R. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 913 TO BS 954, BETWEEN STR 22R TO STR 27R. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 727, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 807, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 767, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BRACKET — BROKEN (EVAC SLIDE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 747, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: RIB — CRACKED (HORIZ STAB) · airframe 62,189 hrs · 59,207 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER L/E CRACKED RIB AT STA 263.3. REMOVED AND REPLACED RIB PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,185 hrs · 59,206 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: FUSE — BLOWN (CABIN) · airframe 61,995 hrs · 59,070 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 61,432 hrs · 58,677 cycles

LT OVERWING EMERGENCY EXIT SIDEWALL EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: CONTROL UNIT — FAULTY (CARGO BAY) · airframe 60,944 hrs · 58,331 cycles

AIR TURNBACK, ON CLIMBOUT FROM BDL AFT CARGO COMPARTMENT FIRE LIGHT ILLUMINATED, ALONG WITH FIRE BELL. PER QRH DISCHARGED BOTTLE. APPROX 4 MINUTES AFTER DISCHARGING BOTTLE, FIRE LIGHT EXTINGUISHED. OVERHEAD FIRE CONTROL PANEL SHOWS SCU FAULT WITH AMBER LIGHT. REMOVED AND REPLACED SCU.

Part: LENS — LOOSE (CABIN) · airframe 60,777 hrs · 58,209 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 60,666 hrs · 58,134 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,280 hrs · 57,170 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,280 hrs · 57,170 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 59,280 hrs · 57,170 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 59,280 hrs · 57,170 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR CRACKED AT LOWER FWD CORNER, APPROX LENGTH OF CRACK, 2.5 INCHES. REMOVED AND REPLACED L1 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,248 hrs · 57,152 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 932, STR 21L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,248 hrs · 57,152 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482B, BETWEEN STR 20L TO STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,128 hrs · 57,067 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 793 TO BS 795, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,980 hrs · 56,967 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS LOOSE AT ROW 20. SECURED EEPLS PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 58,360 hrs · 56,594 cycles

R2 DOOR EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,720 hrs · 56,174 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 762, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,720 hrs · 56,174 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 499, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,396 hrs · 55,974 cycles

EMERGENCY EXIT BULLNOSE LIGHT OUT OF POSITION AT ROW 5. SECURED LIGHT PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,806 hrs · 55,602 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR LOWER AFT EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 739A, RBL 23, WL 208. REPAIRED BEAM PER AAR EA.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT ELEVATOR TAB LOWER SURFACE O/B END DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 661, BETWEEN RBL 1 TO LBL 1, WL 208. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 663, RBL 24, WL 207. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727A, RBL 23, WL 208. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 661, BBL 0, BETWEEN WL 208 TO WL 207. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 25, WL 207. REPAIRED BEAM PER SWA EA.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND MLG WHEEL WELL AFT BULKHEAD SUPPORT BEAM CRACKED AT BS 728, LBL 47. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,217 hrs · 55,197 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FLOORBEAM VERTICAL WEB CRACKED AT BS 710.5, BBL 0, WL 203. REPAIRED WEB PER SI.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,995 hrs · 55,024 cycles

DURING SCHEDULED HC1 CHECK, FOUND PRESSURE DECK ATTACHMENT WEB CRACKED AT BS 665, WL 204, RBL 41. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 54,456 hrs · 53,775 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 54,505 hrs · 53,807 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. R&R LENS PER MM.

Part: STRINGER CLIP — CRACKED (BS 277 S10L/R) · airframe 54,456 hrs · 53,775 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 328 S20R) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 328, STR 20R. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE RT SIDE. REPAIRED FLAP PER SRM.

Part: SKIN — DELAMINATED (LT WING LE SLAT) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: CREASE BEAM — CORRODED (BS 424 S17L) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 424, STR 17L. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, RBL 32. R&R TEE CASP PER SRM.

Part: FRAME — CRACKED (BS 291 S17R) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND STUB FRAME CRACKED AT BS 291, STR 17R. REPAIRED FRAME PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG WW RT CEILING WEB CUTOUT CRACKED. REPAIRED WEB PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG WW LT CEILING WEB CUTOUT CRACKED. REPAIRED WEB PER ACO.

Part: CREASE BEAM — CORRODED (BS 434 S17L) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 434, STR 17L. REPAIRED CREASE BEAM PER SRM.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 54,456 hrs · 53,775 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,320 hrs · 53,675 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,320 hrs · 53,675 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,732 hrs · 53,297 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,077 hrs · 53,482 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,430 hrs · 52,992 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,401 hrs · 52,968 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,269 hrs · 52,855 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,222 hrs · 52,812 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 53,062 hrs · 52,693 cycles

FLIGHT DECK L1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,755 hrs · 52,423 cycles

DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 52,362 hrs · 52,664 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER T/E. REPAIRED SLAT PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 52,257 hrs · 51,962 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,257 hrs · 51,962 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,122 hrs · 50,880 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 22L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,576 hrs · 49,415 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER ER AND SB.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 14R, CRACKED AT BS 420. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: WIRE — LOOSE (CABIN) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. FOUND WIRE W1150 LOOSE, SECURED WIRE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,570 hrs · 49,414 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5R) · airframe 49,570 hrs · 49,412 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S4L) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S10L) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S3L) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S10L) · airframe 49,570 hrs · 49,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 48,728 hrs · 48,534 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,002 hrs · 47,735 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,557 hrs · 47,255 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY INOP. R&R BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,211 hrs · 46,910 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CABIN EMERGENCY EXIT LIGHT LOOSE AT ROW 6 ABC. SECURED LIGHT PER MM.

Part: FRAME — CRACKED (BS 300) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 300, STR 10L. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT AFT LOWER CORNER DOOR STOP CUTOUT. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663, LBL 0.07. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 482B) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482B, STR 20R. REPAIRED FRAME PER SWA EA.

Part: SPLICE — CRACKED (BS 360) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: CHANNEL — CRACKED (BS 360) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CHANNEL CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER CHANNEL PER SRM.

Part: FRAME — CRACKED (BS 613) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 613, RBL 65. REPAIRED FRAME PER SWA SRM.

Part: FRAME — CRACKED (BS 613) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 613, LBL 65. REPAIRED FRAME PER SWA TRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (BS 665) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LT SIDE. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 452) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, BS 452, STR 24R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 482A) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 482A) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20R. REPAIRED FRAME PER SWA EA.

Part: SPLICE — CRACKED (BS 360) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CHANNEL CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 47,041 hrs · 46,718 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR FWD LOWER FRAME CRACKED AT DOOR STOP. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (BS 844) · airframe 46,704 hrs · 46,355 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 844, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 944) · airframe 46,469 hrs · 46,096 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 46,369 hrs · 45,967 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT UPPER T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,531 hrs · 45,090 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,994 hrs · 44,509 cycles

EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 1. SECURED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN) · airframe 44,669 hrs · 44,162 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 & L1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: BOTTLE — LOW (L1 DOOR SLIDE) · airframe 44,317 hrs · 43,810 cycles

L1 DOOR EVAC SLIDE INDICATION, LOW PRESSURE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 43,870 hrs · 43,407 cycles

AFT SERVICE DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REINSTALLED SCREWS PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 43,747 hrs · 43,282 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,584 hrs · 43,133 cycles

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

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 43,584 hrs · 43,133 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT LENS DETACHED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,871 hrs · 42,376 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,171 hrs · 41,681 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT, LOWER FORWARD CORNER, CRACKED. REPAIRED SKIN PER EA.

Part: GATE — CRACKED (R1 DOOR) · airframe 42,171 hrs · 41,681 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR UPPER GATE CRACKED. REMOVED AND REPLACED R1 DOOR UPPER GATE PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 42,160 hrs · 41,672 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,091 hrs · 41,596 cycles

EEPLS LIGHT AT ROW 8 DEF LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,958 hrs · 41,463 cycles

DURING SCHEDULED RON, FOUND NOSE W/W WEB AT LT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,163 hrs · 40,729 cycles

DURING SCHEDULED A1 CHECK, FOUND STRINGER 24L, AT BS 807 CRACKED. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,506 hrs · 39,169 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 15 ABC. SECURED BULLNOSE LIGHT PER MM.

Part: SKIN — CRACKED (LH HORIZ STAB) · airframe 38,564 hrs · 38,281 cycles

DURING SCHEDULED C3 CHECK, FOUND LH HORIZ STAB CRACKED ON LOWER SKIN FWD OF AFT SPAR RIVET LINE AT STA 135. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 35,969 hrs · 35,843 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 35,849 hrs · 35,732 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 34,153 hrs · 34,126 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT FLAP DELAMINATED AT LOWER SURFACE INBD END. R&R FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND EEPLS INOP IN SEVERAL LOCATIONS. RELAMPED EEPLS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND FLOORBEAM CORRODED AT BS 980, FROM RBL 22 TO OUTBOARD END. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CANNING (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND EXTERNAL FUSELAGE SKIN OIL CANNED AT PREVIOUS REPAIR, BS 370, BETWEEN STR 24R & 25R. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (RT WING) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND RT MLG BEAM ATTACH FITTING. REMOVED AND REPLACED MLG BEAM FITTING PER SWA RA.

Part: FITTING — CORRODED (RT WING) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND RT MLG SUPPORT BEAM STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 BS FWD BULKHEAD VERTICAL BEAM WEB CRACKS AT BS 184, RBL 17.1. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 FWD BULKHEAD VERTICAL BEAM WEB CRACKS BETWEEN BS 179 & BS 183, RBL 17.1. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND 2 CRACKS AT FWD BULKHEAD VERTICAL BEAM WEBS BS 180, LBL 17.1 & BS 179.5, LBL 5.7. REPAIRED VERTICAL BEAM WEBS PER SWA RA.

Part: FITTING — CORRODED (LT MLG) · airframe 32,102 hrs · 32,117 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND LT MLG BEAM FITTING CORRODED. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,102 hrs · 32,117 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 32,101 hrs · 32,116 cycles

DURING SCHEDULED D-CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 9 & 11 DEF. SECURED LIGHT ASSY''S PER MM.

Part: COVER — BROKEN (CABIN) · airframe 30,623 hrs · 30,613 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS FWD TRACK COVER BROKEN. REMOVED AND REPLACED TRACK COVER PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 29,811 hrs · 29,787 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED C2 CHECK, FOUND AFT EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ONE AFT EMERGENCY FLOOR TRACK LIGHT INOP. REPLACED LIGHT TRACK ASSEMBLY PER BOEING MM, OPS CK GOOD.

Part: ENGINE — FAILED (NR 2)

NUMBER 2 ENGINE OIL QUANTITY DROPPED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO ONT AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M.

Part: ANGLE — CRACKED (BS 290)

DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 290, BETWEEN S10 AND S11R. REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 311)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM STABILIZING STRAPS CRACKED AT BS 311, BL ZERO, RBL 32, AND AT LBL 14. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOOR CUTOUT)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD SERVICE DOOR CUTOUT CRACKED AT LOWER CORNER AT FASTENER HOLE AND Z-ANGLE. REPAIRED PER BOEING SRM.

Part: STRAP — BROKEN (E/E COMPT)

DURING SCHEDULED B/C CHECK, FOUND RIGHT O/B FLOORBEAM STRAP AT FWD END OF E AND E COMPT BROKEN. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.