N685SW

Part: LENS — LOOSE (EXIT SIGN) · airframe 91,220 hrs · 67,862 cycles

FORWARD DOOR EMER EXIT SIGN LOOSE. SECURED LENS IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 91,100 hrs · 67,778 cycles

FORWARD LOWER EMER EXIT LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW AMM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 91,100 hrs · 67,778 cycles

AFT CEILING EMER LIGHT BATTERY PACK. R & R BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,100 hrs · 67,778 cycles

R2 DOOR LOWER EMER LIGHT ASSEMBLY INOPERATIVE. REPAIRED LIGHT IAW WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,100 hrs · 67,778 cycles

FORWARD GALLEY LOWER EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 91,099 hrs · 67,777 cycles

L2 DOOR EXIT LIGHT LOOSE. SECURED SIGN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,837 hrs · 67,599 cycles

SKIN CRACKED AT BS 342, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: LUG — BROKEN (LT SPOILER) · airframe 90,303 hrs · 67,202 cycles

LEFT WING INBD NR 4 GND SPOILER HINGE LUG BROKEN. R & R NR 4 GND SPOILER IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 89,634 hrs · 66,724 cycles

RIGHT EMER BULLNOSE LIGHT LENS LOOSE AT ROW 8. INSTALLED LENS IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 89,634 hrs · 66,724 cycles

RIGHT WING UPPER PYLON ACCESS PANEL 5836R, AFT SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 89,606 hrs · 66,705 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR BRACKET LOOSE. R & R BRACKET ASSEMBLY IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 88,901 hrs · 66,210 cycles

R2 DOOR EXIT SIGN LIGHT COVER LOOSE. SECURED LIGHT ASSEMBLY IAW SIP.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 88,901 hrs · 66,210 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 88,813 hrs · 66,148 cycles

L1 DOOR EMER SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 88,853 hrs · 66,179 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 88,738 hrs · 66,097 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 88,716 hrs · 66,081 cycles

RIGHT OVERHEAD EMER EXIT LIGHT LENS LOOSE AT ROW 8. SECURED LENS IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF LT OVERWING DOOR. R & R BATTERY CHARGER PACK ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF L2 DOOR. R & R BATTERY CHARGER PACK ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF L1 DOOR. R & R BATTERY CHARGER PACK ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF RT OVERWING DOOR. R & R BATTERY CHARGER & REPAIRED ELEC WIRING IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF L2 DOOR. R & R BATTERY CHARGER & REPAIRED ELEC WIRING IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,602 hrs · 66,007 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER AREA OF R2 DOOR. R & R BATTERY CHARGER & REPAIRED ELEC WIRING IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FORWARD CARGO BAY AFT DOOR FRAME CLOSE OUT WEB CRACKED AT BS 492 AT LOWER END. R & R WEB IAW DWG & SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

COVER PLATE CRACKED AT BS 348 BETWEEN STRINGER 16L TO 17L. R & R PLATE IAW DWG & SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

LEFT KEEL BEAM BRACKET CRACKED AT BS 633.2, WL 153.5. R & R BRACKET IAW SRM & DWG.

Part: LENS — MISSING (CABIN) · airframe 88,567 hrs · 65,982 cycles

AFT GALLEY CTR EMER LIGHT MISSING LENS. INSTALLED LIGHT LENS IAW MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STUB BEAM FRAME INNER WEB CORRODED BELOW FWD & AFT SIDE AT BS 695, WL 190, LT SIDE. R & R WEB IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STUB BEAM FRAME WEB CORRODED ON FWD & AFT SIDE AT BS 695, BELOW WL 190, RT SIDE. R & R WEB IAW DWG & SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

BRACKET CRACKED AT BS 670, RBL 6.5. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FUSELAGE SKIN BEAR STRAP CRACKED AT STATION 340, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

SHEAR TIE CRACKED BETWEEN BS 351 TO 360 BETWEEN STRINGER 19R TO 20R. R & R SHEAR TIE IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

INTERCOSTAL WEB CRACKED BETWEEN BS 1006 TO 1016, LBL 18. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FRAME CRACKED AT BS 947 STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

T CLIP CORRODED AT BS 638, RBL 8. REPAIRED T CLIP IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

T CLIP CORRODED AT BS 654, RBL 8. REPAIRED T CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. R & R SPLICE IAW SRM & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FRAME CRACKED AT BS 663 STRINGER 3L. REPAIRED FRAME IAW ER & EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

PAN ATTACH ANGLE CRACKED AT BS 530, STRINGER 28R. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

SUPPORT ANGLE CRACKED AT BS 334, BETWEEN STRINGER 22R TO 23R. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FUSELAGE SKIN CRACKED AT STATION 951 BETWEEN STRINGERS 14L & 16L. REPAIRED SKIN IAW EA & EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

LEFT INBD T CHORD ANGLE CRACKED AT BS 727. R & R T CHORD IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

BS 1016 BULKHEAD PRESS CHANNEL ANGLE CORRODED AT STATION 1016, WL 191, RBL 7 TO LBL 7. REPAIRED WEB IAW SRM & ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

Z STIFFENER CRACKED AT BS 1016, STRINGER 15L. REPAIRED Z STIFFENER IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 685, STRINGER 5L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 747, STRINGER 5R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 727E, STRINGER 5R. R & R CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

BS 1016 BULKHEAD PRESS CHANNEL ANGLE CORRODED AT STATION 1016, WL 191, RBL 1 TO LBL 1. REPAIRED WEB IAW SRM & ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 727B, STRINGER 5R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 685 STRINGER 4L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 685, STRINGER 7R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 520, STRINGER 7L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 520, STRINGER 5L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 685 STRINGER 6L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 639, STRINGER 2R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 559, STRINGER 9R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

STRINGER CLIP CRACKED AT STATION 500C, STRINGER 7R. R & R CLIP IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

BS 1016 BULKHEAD PRESS WEB CORRODED AT STATION 1016, STRINGER 22L TO 25L. REPAIRED WEB IAW SRM & ER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

LEFT FUSELAGE SKIN DAMAGED AT STATION 304.5, WL 238. REPAIRED SKIN IAW EA & EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

STRINGER CORRODED AT BS 1006, STRINGER 2R. REPAIRED STRINGER IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

INTERCOSTAL WEB FILLER CRACKED AT STATION 358.5, STRINGER 16L. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 88,567 hrs · 65,982 cycles

RIGHT WING LOWER RIB CRACKED AT WBL 135.5, BETWEEN STRINGER 2 TO 3. REPAIRED RIB IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

FLOORBEAM UPPER SURFACE CHORD CORRODED AT BS 1016, BETWEEN LBL 45 TO RBL 45. REPAIRED CHORD IAW ER & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

WEB CORRODED BETWEEN BS 1016 TO 1030, BETWEEN LBL 2 TO 21. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 88,567 hrs · 65,982 cycles

FLOORBEAM CORRODED AT STATION 986, LBL 46 TO RBL 46. REPAIRED FLOORBEAM IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,566 hrs · 65,982 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EA & ER.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 88,045 hrs · 65,586 cycles

RIGHT ELEVATOR LOWER SURFACE DELAMINATED. R & R ELEVATOR IAW AMM & EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 88,045 hrs · 65,586 cycles

L1 DOOR INNER SKIN CRACKED FWD SIDE OF LOWER HINGE CUT OUT VERTICAL FRAME. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 87,921 hrs · 65,490 cycles

RIGHT WW CEILING PRESS DECK WEB CRACKED AT BS 665, RBL 40. REPAIRED WEB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 87,921 hrs · 65,490 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 87,873 hrs · 65,452 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,136 hrs · 64,920 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 87,035 hrs · 64,854 cycles

AFT CARGO DOOR HANDLE CUT OUT CRACKED. R & R CUT OUT IAW SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 86,677 hrs · 64,601 cycles

L2 WINDOW ARCED. R & R L2 WINDOW, PIGTAIL & HEAT CONTROLLER IAW AMM

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 86,650 hrs · 64,582 cycles

AFT INBD EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 86,305 hrs · 64,338 cycles

R1 DOOR ASSIST HANDLE ATTACH STRUCTURE CRACKED. R & R HANDLE ASSEMBLY IAW SRM.

Part: COVER — CRACKED (CABIN) · airframe 86,305 hrs · 64,338 cycles

RT EMERGENCY EXIT LIGHT LENS COVER CRACKED. R & R COVER IAW AMM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 86,305 hrs · 64,338 cycles

R1 DOOR EXTERIOR SKIN CRACKED AT FWD LOWER EDGE. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,298 hrs · 64,332 cycles

FRAME CRACKED AT 500D BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,298 hrs · 64,332 cycles

FRAME CRACKED AT 500B BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,298 hrs · 64,332 cycles

FRAME CRACKED AT 500B BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,664 hrs · 63,842 cycles

RT FWD OVER WING EMERGENCY EXIT HANDLE LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,664 hrs · 63,842 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT L547 INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,544 hrs · 63,743 cycles

RT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE AT ROW 16. R&R BULB IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,544 hrs · 63,743 cycles

SKIN CRACKED AT BS 500C+3.5, STRINGER 8L. R&R SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,544 hrs · 63,743 cycles

SKIN CRACKED AT BS 500C+2.5, STRINGER 8R. REPAIRED SKIN IAW ER & EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,524 hrs · 63,724 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: TERMINAL — DEFECTIVE (CABIN) · airframe 84,537 hrs · 62,995 cycles

FORWARD ENTRY LOWER ENTRY LIGHT INOP. REMOVED AND REPLACED GROUND AND POWER TERMINAL LUGS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 84,537 hrs · 62,995 cycles

CABIN GALLEY G4 EMERGENCY LIGHT INOP. REPAIRED LIGHT WIRING PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 84,537 hrs · 62,995 cycles

CABIN GALLEY G4 EMERGENCY LIGHT INOP. REPAIRED WIRE PER SWPM & MM.

Part: LIGHT — LOOSE (OVERWING EXIT) · airframe 84,013 hrs · 62,610 cycles

EMERGENCY EXIT LIGHT ASSY AT LEFT OVERWING LOOSE. SECURED LIGHT ASSY PER M/M.

Part: LOGIC CARD — FAULTY (E&E BAY) · airframe 83,922 hrs · 62,549 cycles

AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED IN THE UP POSITION THE RED GND GREEN NOSE GEAR LIGHTS WERE ILLUMINATED AT THE SAME TIME. AFTER CYCLING THE GEAR UP AND DOWN THE SAME INDICATIONS WERE NOTED. REMOVED AND REPLACED M983 LOGIC CARD FOR TROUBLESHOOTING IAW AMM. P/N: 65-58250-29 S/N OFF: WN0009 S/N ON: D00159 M983

Part: SPINDLE — CORRODED (LE SLAT) · airframe 83,903 hrs · 62,532 cycles

LEFT NR 1 O/B FLAP CARRIAGE SPINDLE HAS MISSING THERMAL COATING WITH EVIDENCE OF CORROSION. REMOVED AND REPLACED NR 1 LEFT /OB FLAP CARRIAGE SPINDLE ASSY, PER M/M 27-51-34 & MT 327-51-07 & MT 327-51-06.

Part: WINDOW — CRACKED (COCKPIT) · airframe 83,815 hrs · 62,475 cycles

R1 OUTER PANE ARCED AND CRACKED. R & R R1 WINDOW IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 83,796 hrs · 62,464 cycles

EMERGENCY EXIT LIGHT AT FWD AT LOWER LEVEL CRACKED. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LENS — MISSING (COCKPIT) · airframe 83,778 hrs · 62,452 cycles

FAA REPORTS EMERGENCY EXIT LIGHT (ARROW) LENS MISSING CAPTS SIDE. REPLACED LEFT FWD OVERWING EMERGENCY EXIT LIGHT ASSY PER M/M. CL 92378 CLOSING LP 8783148

Part: SPACER — CRACKED (RT WING) · airframe 83,587 hrs · 62,327 cycles

CRACK ON SPACER BETWEEN WBL 181.15 TO 184.63 INTERNAL STRUCTURE OF TRAILING EDGE AREA RIGHT WING. REPLACED SPACER IAW SRM AND DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK OUTBOARD TEE LOCATED AT BS 727 AT LEVEL STR 27L AFT CARGO COMPARTMENT. REPLACED OUTBOARD TEE LOCATE AT BS 727 AT LEVEL STR 27L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 AND DWG 65-46547

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACKS LOCATED ON UPPER FLANGE OF SEAT TRACK BS 727B LBL 45.5 AFT PAX CABIN. REPAIRED SEAT TRACK LOCATED BS 727B AND LBL 45.5 IN AFT PAX CABIN IAW B737-300 SRM 53-00-52 REPAIR 4 FIG 201.

Part: WEB — CRACKED (NLG WW) · airframe 83,587 hrs · 62,327 cycles

CRACK ON RIGHT SIDE PANEL WEB AT A RIVET HOLE WL 169.1 AND BS 243.7 +2.4. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 83,587 hrs · 62,327 cycles

CRACK ON RIGHT SIDE PANEL WEB AT A RIVET HOLE WL 169.1 AND BS 243.7+3.4. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 83,587 hrs · 62,327 cycles

CRACK ON RIGHT SIDE PANEL WEB AT A RIVET HOLE WL 169.1 AND BS 243.7+4.4. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON FUSELAGE SKIN ALONG THE CHEM-MILL STEP ABOVE STR 5R AND BS 967+2.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK IN THE FUSELAGE SKIN ALONG CHEM MILL STEP AT ABOVE STR 5R AND BS 967+6. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON ANGLE LOCATED AT BS 294.5 AND AT STR 13L FWD ENTRY DOOR SURROUND STRUCTURE. REPLACED ANGLE LOCATED AT BS 294.5 AND STR 13L FWD ENTRY DOOR SURROUND STRUCTURE IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON STRAP LOCATED BETWEEN BS 312 TO BS 328 LBL 13 FLOOR CABIN STRUCTURE. REPLACED STRAP LOCATED BETWEEN BS 312 TO BS 328 LBL 13 FLOOR CABIN STRUCTURE IAW SRM B737-300 51-40-02 AND 51-10-02 ITEM 8 AND DWG

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON STRAP LOCATED BETWEEN BS 312 TO BS 348 BL 0 FLOOR CABIN STRUCTURE. REPLACED STRAP LOCATED BETWEEN BS 312 TO BS 348 BL 0 FLOOR CABIN STRUCTURE IAW SRM B737-300 51-40-02 AND 51-10-02 ITEM 8 AND DWG

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON STRAP LOCATED BETWEEN BS 312 TO BS 348 RBL 32 FLOOR CABIN STRUCTURE. REPLACED STRAP LOCATED BETWEEN BS 312 TO 348 RBL 32 FLOOR CABIN STRUCTURE IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DWG

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON TIE CLIP LOCATED BS 380 AT STR 22L IN E/E COMPARTMENT. REPLACED TIE CLIP LOCATED BS 380 AT STR 22L IN E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON FRAME LOCATED BS 344 BETWEEN STR 21L TO STR 22L IN E/E COMP. REPLACED FRAME LOCATED BS 344 BETWEEN STR-21L TO STR 28L IN E/E COMP IAW SRM B737-300 51-10-02 PART 8, 51-40-02 AND DWG 65-45815.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE OF WEB CRACKED AT BS 294.5, STR 24L. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 83,587 hrs · 62,327 cycles

CRACK ON ANGLE LOCATED AT AFT INBOARD CORNER OF RIGHT STRUT ENGINE 2. REPLACED REPAIR ANGLE LOCATED AT AFT INBOARD CORNER OF RIGHT STRUT ENGINE 2 IAW DWG SRM 737-300 51-40-02, 51-10-02 PART 8.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT BS 380 E/E COMPARTMENT. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT BS 312, LBL 23 IN E/E COMPARTMENT. REMOVED AND REPLACED IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 328 AND LBL 50 IN E/E COMPARTMENT. REPLACED SUPPORT ANGLE LOC BS 328 AND LBL 50 IN E/E COMPARTMENT IAW DRAWING AND SRM B737-300 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

FUSELAGE SKIN CRACKED AT BS 947.5+16.5, STR 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

FUSELAGE SKIN CRACKED AT BS 967+6, STR 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

FUSELAGE SKIN CRACKED AT BS 967+13, STR 5R. REPAIRED SKIN IAW SRM.

Part: PLATE — CRACKED (RT PYLON) · airframe 83,587 hrs · 62,327 cycles

CRACK ON PLATE LOCATED LOWER SURFACE OF WING RIGHT AT LEVEL WBL 198 AND 5.10 OF STRUT AREA MOD. PERFORMED REPAIR ON PLATE PER EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON H-STRAP AT LEVEL OF LOWER HINGE ENTRY DOOR S-13L BS 303.9. REPLACED H-STRAP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

FUSELAGE SKIN CRACKED AT BS 967+2.5, STR 5R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

FUSELAGE SKIN CRACKED AT BS 967+6, STR 5R. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON INTERCOSTAL WEB AT STA 12L BETWEEN BS 294.5 AND BS 303.9. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DWG.

Part: RETAINER — CRACKED (RT WING) · airframe 83,587 hrs · 62,327 cycles

CRACK ON SEAL RETAINER AT LEVEL WBL 184 FIXED TRAILING EDGE RIGHT WING. REMOVED AND REPLACED RETAINER IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

LOWER FLANGE OF FRAME CRACKED AT BS 787 BETWEEN STR 26R TO 27R. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (EMERGENCY EXIT) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT INTERNAL AREA OF THE LT EMERGENCY EXIT HATCH STRUCTURE. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — BENT (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

BENT SHEAR TIE LOCATED ON BS 947.5 AND BETWEEN STR 19L TO STR 20L AFT CARGO COMPARTMENT. REPLACED SHEAR TIE LOCATED ON BS 947.5 AND BETWEEN S 19L TO S 20L AFT CARGO COMPARTMENT IAW SRM B737- 300 51-10-02 ITEM 8 SRM B737-300 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

LOWER FLANGE OF FRAME CORRODED AT BS 827, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CRACK ON STIFFENER LOCATED AT BSTA 727 LEVEL STR 27L AFT CARGO COMPARTMENT. REPLACED STIFFENER (TEE) LOCATED AT BS 727 LEVEL STR 27L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 AND DWG 65-46547.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CORROSION ON STRINGER SPLICE LOCATED AT BSTA 907 STR 24L AFT CARGO COMPARTMENT. REPLACED STRINGER SPLICE LOCATED AT BS 907 STR 24L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02-0G-0 SRM B737-300 51-10-02-0G-0 ITEM 8 AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

BRACKET CRACKED AT BS 727 BETWEEN STR 27L TO 27R. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT T/E INTERNAL CAVITY AREA OF FLAP TRACK FAIRING NR 3 LEVEL WBL 193.40 LEFT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SKIN CRACKED AT BS 951, STR 11R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT BS 947.5 AND BL 0. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

CORROSION ON STRINGER 26R LOCATED AT BSTA 907+4" AFT CARGO COMPARTMENT. REPAIRED STRINGER 26R AT BSTA 907+4" TO BS 927+10" AFT CARGO COMPARTMENT IAW SRM B737-300 53-00-03 REPAIR I DETAIL VII.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT WBL 70.85 FRONT SPAR LOWER SURFACE OF THE LT WING. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 83,587 hrs · 62,327 cycles

STIFFENER CRACKED AT I/N SIDE OF FLAP TRACK FAIRING NR 6 TRAILING EDGE AREA RIGHT WING. REMOVED AND REPLACED TIFFENER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (EMERGENCY EXIT) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT INTERNAL AREA OF THE LT EMERGENCY EXIT HATCH STRUCTURE. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BRACKET — CRACKED (EMERGENCY EXIT) · airframe 83,587 hrs · 62,327 cycles

CRACK ON BRACKET LOCATED ON DOOR LINER 2393 OF RIGHT EMERGENCY ESCAPE HATCH. REPLACED BRACKET LOCATED ON DOOR LINER 2393 OF RIGHT EMERGENCY ESCAPE HATCH IAW B737-300 SRM 51-40-02 51-10-02 ITEM 8 AND DRAWING 65- 791308.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

WEB CRACKED BETWEEN BS 787 TO 807, RBL 16. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

RETAINER CRACKED BETWEEN BS 698 TO BS 727, STR 22R. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT OVAL HOLE BS 661 AND RBL 24.5 CENTER WING BOX. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727A+17, LBL 45.5. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 83,587 hrs · 62,327 cycles

CRACK ON WEB LOCATED BETWEEN BS 227.8 TO BS 251.6 BL 0 NOSE LANDING GEAR BAY. REPLACED WEB LOCATED BETWEEN BS 227.8 TO BS 259.12 BL 0 NOSE LANDING GEAR BAY IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 ACO 7820-53 AND DRAWING

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,587 hrs · 62,327 cycles

SUPPORT ANGLE CRACKED AT LOWER EDGE FRAME OF ENTRY DOOR POSITION. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLAP — CHAFED (LT WING) · airframe 82,739 hrs · 61,699 cycles

LEFT WING O/B FORE FLAP CHAFED. REMOVED AND REPLACED FORE FLAP PER AMM.

Part: SLIDE — LOOSE (CABIN) · airframe 82,431 hrs · 61,469 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 81,684 hrs · 60,887 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE IAW MT.

Part: WEB — CRACKED (BS 181) · airframe 81,684 hrs · 60,887 cycles

FLIGHT DECK WEB CRACKED AT BS 181, LBL 20. REPAIRED WEB IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 81,637 hrs · 60,853 cycles

CHORD CORRODED AT BS 227, BETWEEN RBL 1 TO RBL 3. REMOVED AND REPLACED CHORD IAW SRM, ER, AND EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 81,637 hrs · 60,853 cycles

FRAME DAMAGED AT BS 220, STR 24R. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 81,637 hrs · 60,853 cycles

FRAME DAMAGED AT BS 220, STR 24R. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,637 hrs · 60,853 cycles

SKIN DAMAGED AT BS 220, STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,175 hrs · 60,511 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,175 hrs · 60,511 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 80,557 hrs · 60,049 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EEPLS LENS BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 80,501 hrs · 60,013 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,650 hrs · 59,358 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,647 hrs · 59,357 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 79,647 hrs · 59,357 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 79,647 hrs · 59,357 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 500A, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (L2 DOOR) · airframe 78,412 hrs · 58,427 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 767 TO BS 787, STR 26L. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 708, RBL 24.5. REPAIRED BEAM PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRDED BETWEEN BS 787 TO BS 807, STR 26L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 194.3 TO BS 849. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 78,465 hrs · 58,466 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 EMERGENCY LIGHT INOP. REPOSITIONED LIGHT IN CHARGER PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 17R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR4 SPOILER DELAMINATED. REPAIRED SPOILER PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRDED AT BS 793.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SPOILER — DELAMINATED (LT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REPAIRED SPOILER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 18L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 294.5+13, STR 18L. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FORWARD CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 18R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 639 TO BS 663.75, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB DOME CRACKED AT BS 1016, STR 15L. REPAIRED DOME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 3R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 6R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 727A TO BS 727B, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 24R. REPAIRED FRAME PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT SIDEWALL LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD WEB DOME CRACKED AT BS 1016, STR 7R. REPAIRED DOME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 19R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 500 TO BS 520, STR 28R. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 23R TO STR 24R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 909, STR 18L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CRACKED BETWEEN BS 559 TO BS 578, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEB BS 727B TO BS 727C, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727B, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 760, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: WIRE — BROKEN (CABIN) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT FWD EEPLS BROKEN. REMOVED AND REPLACED WIRE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500B, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 24.5. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 514C, STR 28L. REPAIRED SKIN PER EA.

Part: HOLDER — OUT OF POSITION (EVAC SLIDE) · airframe 78,417 hrs · 58,430 cycles

L2 SLIDE DIFFICULT TO REMOVE FROM GIRT BAR. REPOSITIONED SLIDE HOLDER PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500C, STR 9R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB DOME CRACKED AT BS 1016, STR 15R. REPAIRED DOME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 380, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,412 hrs · 58,427 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,382 hrs · 62,172 cycles

R1 DOOR UPPER FWD CORNER AT FASTENER HOLE L=0.250" APPROX RIGHT, UPPER FWD CORNER OF R1 DOOR RIGHT BETWEEN BS 294.5 AND BS 312, BETWEEN STR 6R AND STR 8R ON FUSELAGE SKIN AND BEAR STRAP CRACKED. REPAIRED PER EO AND EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 77,056 hrs · 57,381 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,056 hrs · 57,381 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,056 hrs · 57,381 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 77,056 hrs · 57,381 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 76,665 hrs · 57,067 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 76,491 hrs · 56,932 cycles

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

Part: SPINDLE — CRACKED (TE FLAP) · airframe 76,490 hrs · 56,932 cycles

DURING SCHEDULED MV2 CHECK, FOUND T/E FLAP NR 2 SPINDLE CRACKED. REMOVED AND REPLACED NR 2 SPINDLE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 76,220 hrs · 56,733 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 76,220 hrs · 56,733 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: COVER — BROKEN (CABIN) · airframe 75,958 hrs · 56,530 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,940 hrs · 56,519 cycles

L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 75,865 hrs · 56,463 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 75,830 hrs · 56,440 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 75,661 hrs · 56,321 cycles

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

Part: LIGHT — SHORTED (CABIN) · airframe 75,528 hrs · 56,218 cycles

AIR TURNBACK / DECLARED EMERGENCY - SMOKE IN CABIN LIGHT OVER ROW 14D SHORTED OUT. RETURNED TO SEA. SMELL WAS ELECTRICAL, BLACK RESIDUE AT LIGHT BULB CONNECTION. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 75,321 hrs · 56,070 cycles

DURING SCHEDULED MV2 CHECK, FOUND O/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — CRACKED (CABIN) · airframe 75,090 hrs · 55,904 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT LENS CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,636 hrs · 55,570 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: LENS — MISSING (CABIN) · airframe 74,197 hrs · 55,256 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 9. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 73,145 hrs · 54,462 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE R1 DOOR LOWER AFT CORNER SKIN CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 279, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS COVERS BROKEN. REMOVED AND REPLACED EEPLS PER SWA DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD E & E BAY STRINGER CORRODED BETWEEN BS 310 TO BS 312, LBL 27. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 278, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED WEB PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BL 0. REPAIRED BEAM PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 SLAT O/B END T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,971 hrs · 54,337 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 72,797 hrs · 54,217 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,660 hrs · 54,124 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867 STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,625 hrs · 54,100 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 272, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,606 hrs · 54,088 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 272, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,914 hrs · 53,599 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,914 hrs · 53,599 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER AAR EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,914 hrs · 53,599 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,914 hrs · 53,599 cycles

DURING SCHEDULED SPV CHECK, FOUND LT LOWER NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,914 hrs · 53,599 cycles

DURING SCHEDULED SPV CHECK, FOUND NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,912 hrs · 53,598 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, BETWEEN STR 17R TO STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 71,912 hrs · 53,598 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN RIB STA 147 TO RIB STA 157. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,912 hrs · 53,598 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, BETWEEN STR 18R TO STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 71,912 hrs · 53,598 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 161.9. REPAIRED SKIN PER EA.

Part: LINK — BROKEN (RT MLG) · airframe 70,685 hrs · 52,696 cycles

RIGHT MLG LOWER TORSION LINK BROKEN. REMOVED AND REPLACED TORSION LINK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,631 hrs · 52,663 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,301 hrs · 52,411 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,123 hrs · 52,278 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 18R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 70,070 hrs · 52,239 cycles

DURING SCHEDULED PM CHECK, FWD CABIN EMERGENCY EXIT LIGHTS REMAIN ON. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 68,606 hrs · 51,114 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 67,387 hrs · 50,101 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (RT FOREFLAP) · airframe 67,357 hrs · 50,080 cycles

DURING SCHEDULED OTS CHECK, FOUND RIGHT WING INBOARD FORE FLAP CRACKED AT CENTER GUIDE TRACK FITTING. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 66,781 hrs · 49,647 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, LBL 23, WL 193. REPAIRED WEB PER BOEING SB AND SRM.

Part: FRAME — CRACKED (BS 639 S15R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 15R. REPAIRED FRAME PER ER AND BOEING SB.

Part: SHEAR TIE — CORRODED (BS 360 S28R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S4L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 430) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA. CUTOUT BS 430, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 450) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA . CUT OUT BS 450, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 410) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA. CUT OUT BS 410, BL 0. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR UPPER FRAME CRACKED AT PULLEY BRACKET LOCATION. REMOVED AND REPLACED DOOR FRAME PER SRM & BAC DRAWING.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 65 TO RBL 65. REPAIRED FLOORBEAM PER ER.

Part: SKIN — CRACKED (BS 291) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, NEXT TO R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR LOWER FRAME CRACKED AT PULLEY BRACKET LOCATION. REMOVED AND REPLACED DOOR FRAME PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (BS 303) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303.9, WL 259.88 NEXT TO L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 996, LBL 65 TO RBL 65. REPAIRED FLOORBEAM PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT KEEL BEAM CORRODED BETWEEN BS 500C & BS 510. REPAIRED KEEL BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT CREASE BEAM CORRODED AT BS 948. REPAIRED CREASE BEAM PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 706-712) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 706 TO BS 712, BL 0. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOOR SUPPORT — CRACKED (BS 707) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 707, LBL 25. REPAIRED FLOORBEAM PER BFG ER & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 538, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 277, STR 24R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 500A S15R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 66,780 hrs · 49,645 cycles

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

Part: FLOORBEAM — CORRODED (BS 328) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, LBL 28 TO RBL 57. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 2L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1006, LBL 41. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STA 101. REMOVED AND REPLACED L/E RIB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, BL 0 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 66,780 hrs · 49,645 cycles

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

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 66,780 hrs · 49,645 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT ELEVATOR TAB SKIN DELAMINATED AT UPPER SURFACE. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD STIFFENER CRACKED AT BS 1016, RBL 17, WL 209. REPAIRED STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 390, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727D, LBL 8. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT 935, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 26L TO 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (TE FLAPS) · airframe 66,780 hrs · 49,645 cycles

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

Part: STRINGER CLIP — CRACKED (BS 559 S7R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 559 S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 66,780 hrs · 48,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E LOWER SURFACE DISBONDED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639 S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S7R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S5R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S5R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S9R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S2R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S6R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 559 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 559 S10R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 747 S25L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S7R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S3R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S6R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S5R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S5R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S3R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 66,780 hrs · 49,645 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727C S5R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S27R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S7R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD AFT FLAP LOWER T/E SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S4R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S3R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S9R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S10R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S10R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD AFT FLAP INBOARD T/E LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500 S9R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S10R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S7L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S9L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACD STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S6L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S9L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 66,780 hrs · 49,645 cycles

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

Part: STRINGER CLIP — CRACKED (BS 907 S3R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S8L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S7L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 500B S27L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S28L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 767 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R-8L) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R AND 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 475) · airframe 66,780 hrs · 49,645 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 10R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733D, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,539 hrs · 49,445 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 881, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 66,042 hrs · 49,070 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 66,042 hrs · 49,070 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING L/E NR 2 SLAT UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 65,860 hrs · 48,940 cycles

EMERGENCY EXIT LIGHT COVER BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,680 hrs · 48,804 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 869 TO BS 871, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,680 hrs · 48,804 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 902 TO BS 905, STR 24R. REPAIRED SKIN PER SRM.

Part: SIGN — DISLODGED (CABIN) · airframe 65,570 hrs · 48,715 cycles

LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM.

Part: DUCT — CRACKED (A/C BAY) · airframe 65,413 hrs · 48,587 cycles

DIVERSION, CABIN PRESSURIZATION FAILED AT FL 350, MODE CONTROL TO MANUAL AND CLOSED VALVE DID NOT CHANGE STATUS. REMOVED AND REPLACED APU SUPPLY DUCT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,362 hrs · 48,544 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 961, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,256 hrs · 48,456 cycles

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

Part: TAB — CRACKED (RT ELEVATOR) · airframe 65,201 hrs · 48,411 cycles

DURING SCHEDULED C1 CHECK, FOUND RT ELEVATOR CONTROL TAB CRACKED AT NR 1 HINGE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,018 hrs · 48,252 cycles

EMERGENCY EXIT LIGHTS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,018 hrs · 48,252 cycles

EMERGENCY EXIT LIGHT BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,891 hrs · 48,154 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD CABIN LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULBS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,837 hrs · 48,111 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,346 hrs · 47,708 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,346 hrs · 47,708 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 64,346 hrs · 47,708 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SKIN — CRACKED (BS 395-397) · airframe 64,346 hrs · 47,708 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 395 TO BS 397, STR 10R. REPAIRED SKIN PER BFG ER.

Part: DOOR FRAME — CRACKED (AFT CARGO) · airframe 64,346 hrs · 47,708 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, AFT FRAME NR 1 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 64,225 hrs · 47,612 cycles

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

Part: SKIN — CRACKED (BS 519D) · airframe 64,225 hrs · 47,612 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730E) · airframe 64,225 hrs · 47,612 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23L. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,061 hrs · 47,495 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY OUT OF ADJUST BY PROVISIONING. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (GALLEY) · airframe 60,116 hrs · 44,400 cycles

DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: SKIN — CRACKED (BS 744) · airframe 63,097 hrs · 46,734 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,699 hrs · 45,610 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 23R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,580 hrs · 45,523 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,291 hrs · 45,286 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,291 hrs · 45,286 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 904, STR 25R. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 61,102 hrs · 45,142 cycles

L2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED WINDOW & HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,700 hrs · 44,836 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,337 hrs · 44,557 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,337 hrs · 44,557 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,882 hrs · 44,221 cycles

DURING SPV, FOUND 2 EACH STRINGER CLIPS AT BS 620, BS 616, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,414 hrs · 43,873 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 21R AND BS 727E, STRINGER 21L. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,414 hrs · 43,873 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,414 hrs · 43,873 cycles

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM AT BS 500D, CORRODED. REPAIRED KEEL BEAM PER EA.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 58,302 hrs · 42,940 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED STIFFENER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,302 hrs · 42,940 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 664, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,302 hrs · 42,940 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,302 hrs · 42,940 cycles

DURING SCHEDULED 1/4D CHECK, FOUND H-STRAP AT FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REPAIRED STRAP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,302 hrs · 42,940 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT LT BS 616, WL 208, CRACKED. REPAIRED FRAME SECTION PER T1-153-018.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,457 hrs · 42,256 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,421 hrs · 40,625 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D PLUS 2 AT STR 23L AND BS 943 AT STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,637 hrs · 39,990 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 3, STR 18R. REPAIRED SKIN PER SRM.

Part: MODULE — LEAKING (RT MLG WW) · airframe 54,627 hrs · 39,980 cycles

DIVERSION, DECLARED EMERGENCY. A SYSTEM HYDRAULICS FAILED, PRESSURE / QUANTITY ZERO. REMOVED AND REPLACED A SYSTEM MODULE O-RING AND REMOVED AND REPLACED CASE DRAIN FILTERS PER MM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 54,309 hrs · 39,731 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,819 hrs · 39,333 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,819 hrs · 39,333 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 52,932 hrs · 38,611 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 52,447 hrs · 38,238 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,154 hrs · 37,992 cycles

DURING SCHEDULED PM CHECK, FOUND CAPTIAN'S UPPER WINDOW POST SKIN CRACKED IN UPPER RADIOUS. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 52,069 hrs · 37,919 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 51,995 hrs · 37,853 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENSES LOOSE AT BOTH LEFT AND RIGHT OVERWING EXITS. SECURED LENSES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 51,150 hrs · 37,173 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 51,106 hrs · 37,137 cycles

DURING SCHEDULED C2 CHECK, FOUND NLG W/W UPPER LT PANEL OPENING CRACKED AT AFT INBD CORNER. MX FERRY TO DAL FOR REPAIR. REPAIRED WEB PER SWA RA AND SWA T1.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 51,040 hrs · 37,080 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,960 hrs · 37,013 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 4, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,329 hrs · 36,492 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FIRE DETECTOR — FAULTY (CARGO BAY) · airframe 49,970 hrs · 36,202 cycles

DECLARED EMERGENCY, AFT CARGO COMPT FIRE WARNING LIGHT ILLUMINATED AND FIRE BOTTLE WAS DISCHARGED. AFTER LANDING NO SIGN OF SMOKE OR FIRE FOUND. DEFERRED CARGO FIRE SYS AND INOP BOTH CARGO COMPTS PER MEL. LATER ON DURING RON REMOVED AND REPLACED BOTH FIRE BOTTLES. REMOVED AND REPLACED DIVERTED VALVE. REMOVED AND REPLACED OVERHEAD CARGO FIRE PANEL, AND REMOVED AND REPLACED CCU'S MODULE PER MM. AFTER DOWN LOADING CCU FOUND 3 EA AFT CARGO COMPT FIRE DETECTORS FAULTY. REMOVED AND REPLACED SAME PER MM. OPS CK GOOD.

Part: CONTROL UNIT — FAULTY (CARGO BAY) · airframe 49,966 hrs · 36,198 cycles

AFT CARGO COMPT FIRE WARNING BELL SOUNDED AND DISCHARGED FIRE BOTTLE IN AFT CARGO COMPT. C/W WITH INSPECT AND FOUND NO INDICATION OF OF SMOKE OR FIRE DAMAGE. DEFERRED SYS AND INOP BOTH CARGO COMPT'S PER MEL. LATER DURING RON, REMOVED AND REPLACED BOTH FIRE BOTTLES AND DIVERTER VALVE ASSY. REMOVED AND REPLACED FWD SMOKE DETECTOR, AND REMOVED AND REPLACED CCU PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED, BS 480, BS 807, BS 827, BS 867, AND BS 887, BETWEEN STRINGERS 8R AND 9R. REPAIRED FRAMES PER ER 01-5457 AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND 9 EA FUSELAGE FRAMES CRACKED, BS 747, BS 480, BS 767, BS 807, BS 827, BS 847,BS 867, BS 887, AND BS 907, BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAMES PER ER 01-5457 AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 357, STR 16L. REMOVED AND REPLACED WEB PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,186 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED (2 EA) AT BS 727A, WL 208, LBL 44 AND RBL 23. REPAIRED BEAM PER BFG ER.

Part: WEB — CORRODED (CABIN) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 616 TO BS 639. REPAIRED WEB SECTION PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND LT OUTBD T/E FOREFLAP DELAMINATED ON BOTH SURFACES NEAR INBD END. REPAIRED FLAP PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND 13 EA STRINGER CLIPS CRACKED, STR 10R, BS 663 AND BS 787, STR 2R, BS 639 AND BS 787, STR 3L, BS 727D AND BS 747, STR 2L, BS 639, STR 3R, BS 767, STR'S 4L AND 4R, BS 639, STR 6R,BS 500C, STR'S 1 AND 5L, BS 520. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND LT VERTICAL STIFFENER CRACKED AT BS 663.75, WL 165. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON UPPER SURFACE INBD END. REPAIRED T/E FLAP PER MM..

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 780 AND BS 873 AND CRACKED AT BS 641. REPAIRED CREASE BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 206 AND RBL 1.5, WL 234 AND RBL 8. REPAIRED WEB PER SWA ACO.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 33,623 hrs · 33,726 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN RBL 8 AND LBL 8, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 64 AND WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0, WL 225 TO 230. REPAIRED WEB PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 & WL 238. REPAIRED WEB PER SWA RA.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 727B TO BS 857, WL 208 LBL 68. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (6 EA) AT BS 500D, STR 7R, 8R, 2R, 8L, 6L & 5L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,957 hrs · 36,189 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 14 EA ) AT BS 520, STR 7R, 6R, 7L & 8L, BS 578, STR 8L & 8R, BS 597, STR 8L, BS 616, STR 4R, BS 727B, STR 3L & 3R, BS 727C, STR 3L, BS 727E, STR 3L, 3R & 2R. R&R STR CLIPS PER SRM.

Part: FLAP — DELAMINATED (RH WING) · airframe 49,425 hrs · 35,729 cycles

DURING SCHEDULED C4 CHECK, FOUND RH WING OUTBD AFT T/E FLAP DELAMINATED AT LOWER SURFACE NEAR OUTBD END. R&R FLAP ASSY PER MM.

Part: BATTERY — OVERHEATED (E&E COMP) · airframe 49,015 hrs · 35,390 cycles

ELECTRICAL FUMES IN CABIN. R&R BATTERY CHARGER PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 48,529 hrs · 34,977 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,480 hrs · 34,931 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: COVER — LOOSE (ENTRY DOOR) · airframe 47,486 hrs · 34,129 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER HOOKS LOOSE. REMOVED AND REPLACED EVAC SLIDE COVER ASSY PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 47,486 hrs · 34,129 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMEGRENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (PAX DOOR) · airframe 47,243 hrs · 33,938 cycles

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

Part: RETAINER — LOOSE (PAX DOOR SLIDE) · airframe 46,513 hrs · 33,346 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD ATTACH HOOK LOOSE. REMOVED AND REPLACED RIVETS PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 44,929 hrs · 32,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 44,451 hrs · 31,608 cycles

ABORTED TAKE-OFF --- 80 KNTS INTO THE TAKE-OFF CAPTAINS AIRSPEED INDICATOR DISPLAYED RED FLAG AND ERRATIC. R&R CAPT''S AIRSPEED INDICATOR PER MM

Part: ASI — INOPERATIVE (COCKPIT)

ABORTED TAKEOFF, CAPT'S AIR SPEED IND FAILED 80 KNOTS INTO THE TAKEOFF. RAN SYSTEM AND LRU TESTS, RESET AIR SPEED IND C/B. OPS CK GOOD PER MM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHTS DIM WITH SWITCH OFF POSITION. REMOVED AND REPLACED AFT BATERRY CHARGER PER MM.

Part: SLIDE — OUT OF ADJUST (SRVCE DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED BOTH SLIDES PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH HFEC INSPECTON A 1.5 INCH LONG CRACK ON BS 178 BULKHEAD AFT SIDE, RBL1. REPAIRED BULKHEAD PER SRM.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E FLAP INBOARD EDGE DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND LEFT SIDE CHORD CRACKED, BS 178, LBL 29. REPAIRED CHORD PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-53-2143.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT FWD ENTRY DOOR AFT LOWER CORNER CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2144.

Part: FRAME — CRACKED (CARGO COMPT)

DURING SCHEDULED C3 CHECK, FOUND CRACK ON FWD CARGO FWD FRAME 6.625 INCHES ABOVE LOWER END. REPAIRED PER SWA RA NR 1-353-2059.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND CRACK ON OUTER FUSELAGE SKIN COMING OUT OF AFT SERVICE DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2058 AND SRM.

Part: KEEL BEAM — CORRODED (BS 525)

DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM LOWER CHORD DAMAGED AT B.S. 525 BY CORROSION. DAMAGE LENGTH APPROX 5 OF I/B SIDE OF 'T' EXTRUSION. MAX DAMAGE DEPTH AFTER CLEANING APPROX 0.070. REPAIRED PER SWA RA 1-353-1974.

Part: SKIN — CRACKED (NR 3 LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER SKIN IS CRACKED 15 O/B OF O/B ACTUATOR STOP PAD 1 LONG. REPAIRED PER SWA RA 1-357-0616.

Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND DOOR UPLATCH INTERCOSTAL CRACKED. REPAIRED PER BOEING MM.

Part: CLIPS — CRACKED (BS 807/827)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIPS CRACKED AT BELTFRAME BS 807, S14R AND BS 827, S14R. REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 1020)

DURING SCHEDULED 1/2 D-CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 1020, RBL 38, AT FLOOR LEVEL. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 25, LBL 24.75 AND AT LBL 46. REPAIRED PER ACO 3198-53.

Part: FLOORBEAM STRAP — CRACKED (E/E COMP)

DURING SCHEDULED C1 CHECK, FOUND RIGHT I/B FLOORBEAM STRAP CRACKED IN E AND E COMPT. REPAIRED PER BOEING SRM.