N657SW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 96,405 hrs · 59,563 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: HYDRAULIC LINE — BROKEN (NLG WW) · airframe 96,395 hrs · 59,556 cycles

AIR TURN BACK, DECLARED EMER. NLG WOULD NOT RETRACT AFTER TAKEOFF, ALL LG PINS ABOARD. FOUND RETRACT PRESS LINE BROKEN. R & R LINE IAW MM.

Part: SPAR — CRACKED (RT WING) · airframe 95,330 hrs · 58,722 cycles

RIGHT WING UPPER REAR SPAR CHORD FASTENER HOLE IN WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 95,330 hrs · 58,722 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 222. REPAIRED CHORD IAW ER & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,175 hrs · 58,608 cycles

LEFT OVERWING EMER EXIT LOWER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,767 hrs · 58,293 cycles

SKIN CRACKED BETWEEN BS 908 TO 917, STRINGER 15L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 94,421 hrs · 58,068 cycles

RIGHT WING FIXED FAIRING UPPER INBD ANGLE CRACKED AFT OF INBD GND SPOILER. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP DAMAGED AT BS 986 STRINGER 19R. R & R CLIP IAW DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP DAMAGED AT BS 986 STRINGER 20R. R & R CLIP IAW DWG.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP DAMAGED AT BS 986 STRINGER 19L. R & R CLIP IAW DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

LONGITUDINAL FLOORBEAM STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639 LBL 45.5. R & R CLIP IAW DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP CORRODED AT BS 747 STRINGER 26R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP CORRODED AT BS 947, STRINGER 19L. R & R CLIP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

AFT CARGO BAY INTERCOSTAL CRACKED AT BS 947 STRINGER 21L. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

INTERCOSTAL CRACKED BETWEEN BS 747T TO 767, BETWEEN STRINGER 24R TO 25R. R & R INTERCOSTAL IAW DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668 BL 0. REPAIRED BEAM IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER SPLICE CRACKED AT BS 910 STRINGER 4R . R & R SPLICE IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME CRACKED AT BS 947.5 STRINGER 20L. R & R FRAME IAW SRM & DWG.

Part: PANEL — DELAMINATED (RT WING) · airframe 93,832 hrs · 57,655 cycles

RIGHT WING TE PANEL 8501 DELAMINATED AT CORNER. R & R PANEL IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 93,832 hrs · 57,655 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

LEFT MAIN WW ON VERTICAL ANGLE CORRODED AT BS 717, LBL 62. REPAIRED ANGLE IAW SRM & DWG.

Part: DOOR — DELAMINATED (LT MLG) · airframe 93,832 hrs · 57,655 cycles

LEFT MLG CTR GEAR DOOR DELAMINATED. R & R DOOR IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME OUTER CHORD CRACKED BS 616 STRINGER 16L. REPAIRED CHORD IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

SKIN CORRODED BETWEEN BS 270 TO 276 STRINGER 22R. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME CRACKED AT BS 947 RBL 13. REPAIRED FRAME IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD AFT END OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B-3 RBL 24.8. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME CORRODED AT BS 747 BETWEEN STRINGER 27L TO 27R. R & R FRAME IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP CORRODED AT BS 787 STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

PRESSURE BULKHEAD WEB CORRODED AT BS 1016, LBL 6. REPAIRED WEB IAW ER & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME SHEAR TIE CORRODED AT BS 847 BETWEEN STRINGER 27L TO 27R. R & R FRAME SECTION IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

STRINGER CLIP CORRODED AT BS 767 STRINGER 26R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 93,832 hrs · 57,655 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT LOWER AFT FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 93,832 hrs · 57,655 cycles

RIGHT WING TE, UPPER MOST INBD NO STEP PANEL INBD SUPPORT ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.

Part: STRAP — FRAYED (CABIN) · airframe 93,832 hrs · 57,655 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP FRAYED. R & R STRAP IAW AMM.

Part: BULKHEAD — CUT (FUSELAGE) · airframe 92,693 hrs · 56,812 cycles

PRESS DOME SKIN CUT AT BS 1016, RBL 2. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 92,693 hrs · 56,812 cycles

STIFFENER CRACKED AT BS 1016.5, RBL 1. REPAIRED STIFFENER IAW ER & EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 92,693 hrs · 56,812 cycles

EXTERNAL POWER DOOR CUT OUT INTERNAL DOUBLER CRACKED FWD EDGE BELOW LOWER HINGE. REPAIRED CUT OUT IAW EA & ER.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 92,693 hrs · 56,812 cycles

FORWARD SIDE OF AFT PRESS BULKHEAD WEB CORRODED AT BS 1017, RBL 2. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 91,157 hrs · 55,736 cycles

R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. R & R DOOR IAW AMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 88,296 hrs · 53,623 cycles

AFT GALLEY DOOR LOWER HINGE CUTOUT HAS .300 CRACK ON DOOR FRAME. COMPLIED WITH EA 1-352-1292.

Part: GIRT BAR — CORRODED (L2 DOOR) · airframe 87,893 hrs · 53,330 cycles

L2 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR CORRODED. REMOVED AND REPLACED FITTING IAW AMM.

Part: GROUND STUD — BROKEN (CABIN) · airframe 87,893 hrs · 53,330 cycles

FORWARD LAV WALL EMERGENCY EXIT LIGHT ASSEMBLY GROUND STUD BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 87,893 hrs · 53,330 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW AMM.

Part: SHEAR TIE — BUCKLED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

SHEAR TIE BUCKLED AT BS 312, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

FLOORBEAM CRACKED AT BS 294, RBL 53. REPAIRED "T" CAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

UPPER FLANGE LOWER SIDE OF SUPPORT STRUCTURE CORRODED AT BS 338, STR 23L. REMOVED AND REPLACED STRUCTURE IAW DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

STRINGER CORRODED AT BS 325, BL 0. REMOVED AND REPLACED STRINGER IAW SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 87,893 hrs · 53,330 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

R1 DOOR FWD FRAME CUTOUT CRACKED AT BS 294.5, WL 208. REPAIRED FRAME IAW SRM AND DWG.

Part: SILL — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

R1 DOOR LOWER SILL WEB CORRODED BETWEEN BS 294 TO BS 328. REMOVED AND REPLACED WEB IAW DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

KEEL BEAM INBOARD CLIP CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED CLIP IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

R1 DOOR CREASE BEAM CHORD CORRODED. REMOVED AND REPLACED BEAM IAW DWG AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

BULKHEAD CHORD CRACKED AT BS 664, BL 0. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

FORWARD ENTRY DOOR FORWARD CUTOUT WEB CRACKED AT BS 303.9. REPAIRED WEB PER ACO.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 87,893 hrs · 53,330 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH POINT UPPER SURFACE CORRODED. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 87,893 hrs · 53,330 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH POINT CORRODED. REMOVED AND REPLACED GIRT BAR IAW SRM AND DWG.

Part: WIRE — BROKEN (CABIN) · airframe 87,893 hrs · 53,330 cycles

L1 DOOR EMERGENCY EXIT LIGHT WIRE BROKEN. REMOVED AND REPLACED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

R1 DOOR FUSELAGE SKIN CRACKED AT UPPER FORWARD CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO 28R. REMOVED AND REPLACED SHEAR TIE IAW DWG AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

WEB CRACKED AT STA 986.5, STR 9R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

FLOORBEAM T-CAP CORRODED AT BS 967, BETWEEN LBL 33 TO RBL 31. REPAIRED T-CAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

FORWARD CARGO COMPARTMENT DOOR AFT CUTOUT ENCLOSURE WEB CRACKED AT BS 490, STR 25R. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW DWG AND SRM.

Part: WEB — CRACKED (R1 DOOR) · airframe 87,893 hrs · 53,330 cycles

FORWARD GALLEY DOOR WEB CRACKED AT BS 294.5, STR 9R. REMOVED AND REPLACED L-ANGLE IAW SRM AND DWG.

Part: SPOILER — DELAMINATED (RT WING) · airframe 87,893 hrs · 53,330 cycles

RIGHT WING NR 6 SPOILER UNDER SIDE INBOARD OF ACTUATOR ATTACH CUT OUT DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER IAW AMM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

STRINGER CLIP CORRODED AT BS 727A, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 665, LBL 24.8. REPAIRED CHORD IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

LEFT KEEL BEAM CORRODED AT BS 500D+10, LBL 6.5. REPAIRED BEAM IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 87,893 hrs · 53,330 cycles

RIGHT KEEL BEAM CORRODED AT BS 500D+9. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 87,750 hrs · 53,219 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 86,867 hrs · 52,546 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 86,867 hrs · 52,546 cycles

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

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 86,642 hrs · 52,371 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 86,208 hrs · 52,032 cycles

RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW MM.

Part: SKIN — DELAMINATED (NR 8 SPOILER) · airframe 85,354 hrs · 51,397 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 8 SPOILER DELAMINATED. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR, BS 290.50, WL 235.50 ON LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,975 hrs · 36,738 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,236 hrs · 49,790 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR BEAM CHORD CRACKED AT BS 344, BETWEEN LBL 47 TO LBL 49. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, LBL 50. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 793, LBL 8. REPAIRED SUPPORT PER EA.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING AILERON TAB UPPER SURFACE DELAMINATED. REPAIRED TAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: CARRIAGE — CRACKED (TE FLAP) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING O/B TRAILING EDGE FLAP CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED NR 8 FLAP CARRIAGE PER MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, RBL 8. REPAIRED SUPPORT PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED SUPPORT PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, RBL 3. REPAIRED SUPPORT PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,526 hrs · 49,263 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 904 TO BS 907, LBL 12. REMOVED AND REPLACED SUPPORT PER EA.

Part: HANDLE — DIRTY (COCKPIT) · airframe 82,139 hrs · 48,959 cycles

ON APPROACH GEAR INDICATED 3 GREEN AND 3 RED. CYCLED LT GEAR. FOUND LANDING GEAR HANDLE STICKING OUT WHEN PUT IN "DOWN" DETENT CLEANED HANDLE PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 81,025 hrs · 48,122 cycles

AFTER REQUESTING "LANDING GEAR DOWN" HAD NORMAL INDICATIONS FOR NOSE AND LEFT MAIN BUT RED RIGHT GEAR AND NO GREEN LIGHT. RECYCLED LANDING GEAR ALL INDICATIONS NORMAL. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 25R. REMOVED AND REPLACED SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17L. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 516B, STR 22L. REPAIRED STRINGER PER SRM AND ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 952, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (RT WING) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING UPPER SURFACE SKIN CORRODED AT WBL 16.5. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 912, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 363, STR 17L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 360 TO BS 380, STR 25R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 928, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BS 420, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 827 TO BS 847, STR 17L. REMOVED AND REPLACED BEAM PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND ANGLE CORRODED BETWEEN BS 967 TO BS 980, STR 21R. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992.8, STR 20R. REPAIRED FRAME PER SRM.

Part: SPOILER — BULGED (LT WING) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND NR 3 SPOILER PANEL BULGED BETWEEN CENTER HINGE POINTS. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE INTERNAL SKIN DOUBLER CORRODED AT BS 970 TO BS 993, STR 20R TO STR 25R. REPAIRED SKIN DOUBLER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV, FOUND SHEAR TIE CORRODED AT BS 907, STR 17R TO STR 18R. REMOVED AND REPLACED SHEAR TIE PER SRM & BAC DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV, FOUND STRINGER 23L CORRODED AT BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV, FOUND STRINGER 18L CRACKED AT BS 520. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN BUTT JOINT CORRODED AT BS 908, STR 22L TO STR 23L. REPAIRED SKIN PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 520, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND FAIL SAFE ANGLE CORRODED AT BS 907, STR 21L TO STR 22L. REPAIRED ANGLE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED CLIP PER SI.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 23L TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BS 360. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,924 hrs · 48,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 80,211 hrs · 47,521 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 80,211 hrs · 47,521 cycles

DURING SCHEDULED SPV CHECK, RT FWD EMERGENCY LIGHT BATTERY PACK FAILED CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,250 hrs · 47,554 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP BETWEEN ROW 12 TO ROW 21. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 79,973 hrs · 47,336 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 79,726 hrs · 47,142 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (L2 DOOR) · airframe 79,645 hrs · 47,087 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR UPPER SKIN CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 79,645 hrs · 47,087 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT VERTICAL STAB FITTING LUG FACES AT AFT SPAR CORRODED, STA 1088. REPAIRED FITTING PER SWA EA.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 79,645 hrs · 47,087 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER AFT SPAR CORRODED AT STA 209.90. REMOVED AND REPLACED VERTICAL STABILIZER PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 79,645 hrs · 47,087 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: ATTACH FITTING — WORN (VERTICAL STAB) · airframe 79,645 hrs · 47,087 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT VERTICAL STABILIZER AFT FAIL SAFE ATTACH LUG WORN. REPAIRED LUG PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,643 hrs · 47,086 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER SKIN CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 78,845 hrs · 46,486 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,558 hrs · 46,293 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 77,930 hrs · 45,858 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,887 hrs · 45,830 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD NOSE COMPARTMENT LOWER BILGE CHORD CORRODED AT BS 227, BETWEEN RBL 8 TO LBL 6. REPAIRED CHORD PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,887 hrs · 45,830 cycles

DURING SCHEDULED BRDG CHECK, FOUND LOWER SKIN CORRODED AT BS 227, BETWEEN RBL 8 TO LBL 6. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (BS 727E) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 727E, STR 10L. REPAIRED STRINGER PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 77,648 hrs · 45,658 cycles

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

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM L ANGLE CRACKED AT BS 727B, LBL 45, WL 206. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT FRAME INNER CHORD WEB CRACKED AT BS. 639, WL 209. REPAIRED WEB PER PAE ER.

Part: FLOORBEAM — CRACKED (BS 352) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 352, LBL 50, WL 195. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (BS 303) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS. 303, WL 234. REPAIRED SKIN PER PAE ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM WEB CORRODED AT BS 710, BETWEEN LBL 6 TO RBL R. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 17.7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 304) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 303) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS. 303 WL 236. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BBL 0. REMOVED AND REPLACED SHEAR TIE PER SRM..

Part: SKIN — CRACKED (BS 305) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 305, WL 238. REPAIRED SKIN PER PAE ER.

Part: CREASE BEAM — CRACKED (BS 616-639) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BETWEEN BS 639 TO BS 667, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (BS 304) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 235. REPAIRED SKIN PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO AFT BULKHEAD FRAME CORRODED AT BS 1006, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,648 hrs · 45,658 cycles

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

Part: FRAME — CRACKED (BS 639) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT FRAME OUTER CHORD WEB CRACKED AT BS 639, WL 209. REPAIRED WEB PER PAE ER.

Part: FLOORBEAM — CORRODED (BS 639) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT STUB FLOORBEAM CORRODED AT BS 639, RBL 70, WL 137. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 708) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS. 708, RBL 24, WL 202. REPAIRED WEB PER PAE ER.

Part: SKIN — CRACKED (BS 303) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 303, WL 258. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (BS 712-713) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BETWEEN BS 712 TO BS 713, BL 0, WL 202. REPAIRED WEB PER PAE ER.

Part: FLOORBEAM — CRACKED (BS 706) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, BL 0, WL 140.5. REPAIRED WEB PER PAE ER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE O/B END LOWER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500A, LBL 17. REPAIRED FRAME PER SRM.

Part: FASTENER — LOOSE (GIRT BAR HOOK) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR ESCAPE SLIDE FWD LOWER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FASTENER — LOOSE (GIRT BAR HOOK) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR ESCAPE SLIDE FWD LOWER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED SKIN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BBL 0. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727B, STR 18R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,648 hrs · 45,658 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 76,397 hrs · 44,755 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 76,397 hrs · 44,755 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,481 hrs · 44,082 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 829, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,481 hrs · 44,082 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 849, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,481 hrs · 44,082 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 792, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,476 hrs · 44,079 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 849, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,476 hrs · 44,079 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 829, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,746 hrs · 44,079 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 792, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — WORN (T/E FLAP) · airframe 74,934 hrs · 43,701 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 7 T/E AFT FLAP TRACK WORN. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS INOP AT ROW 18 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,934 hrs · 43,701 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 74,934 hrs · 43,701 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND MLG BULKHEAD CORRODED AT BS 663.75, LBL 2 TO LBL 4. REPAIRED BULKHEAD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 344, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 427, LBL 1.2. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,933 hrs · 43,700 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 74,718 hrs · 43,547 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,871 hrs · 42,918 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 73,804 hrs · 42,861 cycles

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

Part: CYLINDER — FAILED (LT MLG AXLE) · airframe 73,772 hrs · 42,833 cycles

LEFT MLG NR 1 AXLE INNER CYLINDER DAMAGED DUE TO NR 1 WHEEL BEARING FAILURE. REMOVED AND REPLACED INNER CYLINDER PER MM.

Part: DRAG BRACE — CORRODED (LT MLG) · airframe 73,761 hrs · 42,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG LOWER DRAG BRACE BUSHING AND TEE FITTING CORRODED. REMOVED AND REPLACED DRAG BRACE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 72,160 hrs · 41,557 cycles

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

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 71,959 hrs · 41,396 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED OUTBOARD T/E END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FITTING — BROKEN (NR 4 SPOILER) · airframe 71,959 hrs · 41,396 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SHEAR TIE — CRACKED (BS 380 S16L) · airframe 71,457 hrs · 41,034 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 16L. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,359 hrs · 40,955 cycles

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

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 71,202 hrs · 40,835 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT 13 ABC. CLEANED LIGHT SOCKET. OPS CK GOOD.

Part: BOLT — WORN (RT ELEVATOR) · airframe 70,070 hrs · 39,967 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT INBOARD ELEVATOR TAB HINGE BOLT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 69,430 hrs · 39,458 cycles

R1 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: INDICATOR — FALSE INDICATION (MLG) · airframe 68,358 hrs · 38,633 cycles

WITH MLG HANDLE IN DOWN POSITION-3 RED & 3 GREEN INDICATOR LIGHTS ILLUMINATED. RECYCLED GEAR HANDLE, ALL INDICATIONS RETURNED TO NORMAL. CHECKED OPERATION OF MLG HANDLE & SWITCH. INSPECTED MLG ASSY, ALL INDICATIONS NORMAL.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT T/E INBD LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 3 L/E SLAT T/E LOWER SKIN CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SPLICE — CRACKED (BS 359) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CRACKED (BS 359) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (BS 344) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 18L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 312) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (BS 727) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEELBEAM CORRODED AT BS 727, LBL 7. REPAIRED KEELBEAM PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 957) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17R. REPAIRED SKIN PER SRM.

Part: POST — CRACKED (COCKPIT) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM.

Part: NUT PLATE — CRACKED (R2 DOOR) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT ANCHOR NUT PLATE CRACKED. REMOVED AND REPLACED NUT PLATE PER MM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31 & RBL 39. REPAIRED BEADED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 67,269 hrs · 37,772 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 67,117 hrs · 37,652 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,094 hrs · 37,629 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 259 TO BS 312, STR 14L. REPAIRED SKIN PER BFG ER.

Part: HINGE — BROKEN (R1 DOOR) · airframe 66,794 hrs · 37,380 cycles

R1 DOOR UPPER HINGE ASSY BROKEN. REMOVED AND REPLACED UPPER HINGE ASSY PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN AT BS 1016 TO BS 1088, FROM STR 26L TO STR 26R. REMOVED AND REPLACED BELLY SKIN SECTION PER BFG ER.

Part: STRAP — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME STRAP AT BS 360, FROM RBL 14 TO LBL 14. REPAIRED FRAME PER BFG ER & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 259 TO BS 305, STR 19L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 540 TO BS 727, STR 10L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON LOWER FUSELAGE SKIN AT BS 350 TO BS 360, BL 0. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 540 TO BS 727, STR 10R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 290 TO BS 360, STR 4R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 16L. REPAIRED SKIN PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE FRAME ASSY AT BS 500, FROM STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME SHEAR TIE AT BS 360, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN AT BS 907 TO BS 1016, FROM STR 26L TO STR 26R. REMOVED AND REPLACED BELLY SKIN SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 4L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP AT BS 1016 TO BS 1088, STR 16R. REPAIRED SKIN PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME AT BS 1088, FROM LBL 13 TO RBL 15. REPAIRED FRAME PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 24R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 986 TO BS 1016, STR 14L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 19R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 360 TO 500C, STR 19R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 24R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 1016, STR 4R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 907 TO BS 1016, STR 20R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 360 TO BS 500C, STR 26R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 727C TO BS 907, STR 25R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 950, STR 10L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 24L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 727D TO 951, STR 20L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 907 TO 1016, STR 14R. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 350 TO 500C, STR 19L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 950, STR 14L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO 360, STR 14L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 727C TO BS 907, STR 25L. REPAIRED SKIN PER PAE ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 360 TO BS 500D, STR 26L. REPAIRED SKIN PER PAE ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 178 TO BS 259, STR 19R & STR 24R. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 188, LBL 29, WL 208. REPAIRED FRAME PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER SPLICE AT BS 362, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER AT BS 1010, STR 26R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER BETWEEN BS 967 TO BS 1016, STR 25L. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN BEAR STRAP BETWEEN BS 947 TO BS 967, BETWEEN STR 23L TO STR 27R. REPAIRED BEAR STRAP SECTION PER SRM.

Part: WEB — CRACKED (COCKPIT) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FLOOR WEB CRACKED RT SIDE BETWEEN BS 188 & BS 196, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA OUTBOARD CHORD CRACKS AT BS 188, LBL 29 & RBL 29, WL 207. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 344, LBL 8-12, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE BETWEEN BS 350 & BS 370, STR 28R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE AT BS 358, STR 27R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 380, LBL 5 TO RBL 5, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,059 hrs · 36,781 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,420 hrs · 35,451 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM.

Part: TEE FITTING — CRACKED (FWD CARGO DOOR) · airframe 64,420 hrs · 35,451 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER TEE CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,420 hrs · 35,451 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,613 hrs · 34,804 cycles

DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 7 TO LBL 8, CRACKED. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,580 hrs · 34,778 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN BELOW L1 DOOR BS 335, LT LOWER SIDE, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,576 hrs · 34,774 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 28R, CORRODED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,576 hrs · 34,774 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,196 hrs · 34,470 cycles

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

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 63,077 hrs · 34,369 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW 14 DEF. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — DISLODGED (FWD ENRTY DOOR) · airframe 61,712 hrs · 33,321 cycles

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

Part: MODULE — FAULTY (LE FLAP/SLAT) · airframe 60,917 hrs · 32,669 cycles

ABORTED TAKEOFF, WARNING HORN SOUNDED ASSOCIATED WITH L/E INDICATOR LIGHTS. REMOVED AND REPLACED L/E FLAP/SLAT POSITION IND MODULE PER MM.

Part: VALVE — FAULTY (CABIN PRESSURE) · airframe 60,643 hrs · 32,451 cycles

AIR TURNBACK, UNABLE TO PRESSURIZE CABIN. REMOVED AND REPLACED CABIN PRESSURE RELIEF SAFETY VALVE PER MM.

Part: MOTOR — OVERHEATED (GASPER FAN) · airframe 60,581 hrs · 32,399 cycles

DIVERSION TO BOI, BURNING ODOR IN CABIN. REMOVED AND REPLACED GASPER AIR FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,142 hrs · 32,049 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 60,142 hrs · 32,049 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT OUTBOARD UPPER T/E WEDGE DELAMINATED. REPAIRED NR 5 L/E SLAT PER SRM.

Part: DOUBLER — MISSING (L/E SLAT) · airframe 59,973 hrs · 31,911 cycles

A 4 X 6 INCH PREVIOUS REPAIR MISSING AT NR 3 L/E SLAT UPPER SURFACE. REMOVED AND REPLACED NR 3 L/E SLAT PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 59,620 hrs · 31,631 cycles

DURING SCHEDULED C1 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER SWA SI AND MM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 58,724 hrs · 30,886 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB CONTROL ROD END BEARING AND BUSHING PER MM.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 58,664 hrs · 30,843 cycles

AIR TURNBACK, NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED HYDRAULIC HOSE TO NLG LOCK ACTUATOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,061 hrs · 30,349 cycles

DURING SCHEDULED RON, FOUND AFT OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: HINGE — WORN (RT ELEVATOR) · airframe 57,008 hrs · 29,487 cycles

DURING SCHEDULED C2 CHECK, FOUND EXCESSIVE AXIAL PLAY AT RT AND LT ELEVATOR TABS. REMOVED AND REPLACED NR 1 TAB HINGES PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 56,542 hrs · 29,103 cycles

DURING WALK AROUND INSP, FOUND NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM.

Part: LENS — MISSING (CABIN) · airframe 56,144 hrs · 28,799 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 56,144 hrs · 28,799 cycles

DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN CEILING EMERGENCY EXIT LIGHT INOP. RECONNECTED WIRING AND OPS CHECK GOOD PER MM.

Part: CONTROL UNIT — ERRATIC (CARGO BAY) · airframe 54,763 hrs · 27,660 cycles

CARGO COMP FIRE INDICATION DURING FLIGHT LASTED ONLY 2 TO 3 SECONDS, REMAINDER OF FLIGHT NORMAL. REMOVED AND REPLACED CCU PER MM.

Part: SLAT — CRACKED (LH WING) · airframe 54,196 hrs · 27,184 cycles

DURING SCHEDULED C3 CHECK, FOUND # 1 & # 3 L/E SLATS TRAILING EDGE SKINS CRACKED ON AFT ROW OF RIVETS. REPAIRED SLATS PER SWA RA.

Part: INDICATOR — FAILED (COCKPIT) · airframe 52,910 hrs · 26,106 cycles

DIVERSION, STANDBY ADI FAILED DURING CRUISE. RESET C/B, NO HELP. ALL OTHER SYSTEMS NORMAL. REMOVED AND REPLACED STANDBY HORIZON PER MM, OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 52,326 hrs · 25,650 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EGRESS LIGHT LENS MISSING AT ROW 17ABC. INSTALLED LENS PER MM.

Part: LIGHT — MALFUNCTIONED (ESCAPE SLIDE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LIGHT DIM WHEN TESTED. REMOVED AND REPLACED LIGHT ASSY PER WDM, OHM & MM.

Part: SKIN — CRACKED (OVERWING DOOR) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND RT OVERWING EXIT DOOR SKIN CRACKED AT FASTENER HOLE, BS 637, WL 245. REPAIRED SKIN PER ER 00-1219.

Part: STRINGER — CORRODED (A/C BAY) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR ATTACH FITTING CORRODED AFT SIDE OF BS 727 BULKHEAD, STR 27L. REPAIRED STR PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WBL 135.0, BETWEEN S2 & S3. REPAIRED RIB ER 00-1172.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD, LOWER SURFACE, CORRODED AT BS 986.5, LBL 14.5, WL 207.5. REMOVED AND REPLACED ENTIRE UPPER CHORD SECTION PER ER 00-1204.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND BS 663 VERTICAL PRESSURE WEB CORRODED AT RBL 38, WL 197. REPAIRED PRESSURE WEB PER ER 00-1203.

Part: FITTING — CORRODED (LT MLG) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG BEAM STABILIZING LINK FITTING CORRODED. REMOVED AND REPLACED LINK FITTING PER ER 00-1220P1 AND DRW 65-45321.

Part: SPLICE — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 905, STR 14L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 906, LBL 69, WL 230. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR 14L CRACKED AT BS 905. REPAIRED STR PER SRM.

Part: SUPPORT BRACKET — CORRODED (MLG) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING MLG SUPPORT BEAM CORRODED AT 3 FASTENER HOLES. REPAIRED MLG SUPPORT PER ER 00-1175 AND SRM.

Part: FRAME — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, LBL 59, WL 270. REPAIRED FRAME PER TR-A51-002 AND ER 00-1179.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB UPPER SURFACE AT BS 953, RBL 56, WL 208. REMOVED AND REPLACED DAMAGED WEB PER DWG 65-45855 AND SWA T1-A51-002.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT RBL 60, WL 270, BS 807 AND 827. REPAIRED FRAMES PER ER 00-1179 AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, LBL 52, WL 283. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT LBL 60, WL 270, BS 747, 807, 827, 847 AND 867. REPAIRED FRAMES PER ER 00-1179 AND SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR AFT BRACKET FLOOR FITTING CORRODED. REMOVED AND REPLACED CORRODED GIRT BAR BRACKET FITTING.

Part: FRAME — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 907, WL 270, RBL 60. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 5R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FASTENER HOLES CORRODED AT BS 874 AND 877.5, LBL 64, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: WEB — CORRODED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND WEB CORRODED AT BS 727D, LBL 69, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND CHORD CORRODED ON APU TORQUE BOX, BS 1088, RBL 21, WL 245. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 294.5 STR 7L, BS 559 STR 11L, BS 578 STR 11L, BS 597 STR 11L, BS 907 STR 15L AND BS 986 STR 5L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: WEB — CORRODED (CREASE BEAM) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 991, LBL 47.5, WL 208. FABRICATED NEW WEB PER SRM.

Part: ANGLE — CORRODED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM ANGLE CORRODED AT BS 991, LBL 49.5, WL 208. FABRICATED ANGLE PER DRWG 69-41226 AND INSTALLED PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG BEAM STAB LINK FITTING CORRODED. DRILLED STAB LINK FITTING PER DWG 65-82770 AND REPLACED FITTING PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND SKIN CREASED AT BS 839, STR 25R AND 26R. REPAIRED SKIN PER SRM.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZ STAB AFT SPAR LOWER ATTACH LUG AFT FACE CORRODED. REPAIRED AFT SPAR LOWER ATTACH FACE AND REMOVED AND REPLACED BUSHINGS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 663 STR 10L, BS 887 STR 15L AND 14L AND BS 578 STR 11R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FITTING — CORRODED (RT WING) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND RT MLG SUPPORT BEAM STAB LINK FITTING CORRODED. REMOVED AND REPLACED LINK FITTING PER MM.

Part: FITTING — CORRODED (LT WING) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG STAB LINK FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 52,139 hrs · 25,489 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED ABOVE AND BELOW WL 207. REMOVED AND REPLACED SIDE CHORDS PER ACO 7338-53 & 7342-53.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 52,139 hrs · 25,483 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR FLOOR BRACKET ATTACHMENT PLATES CORRODED AT BS 312 & 344, LBL 50.

Part: TIRE — FAILED (NLG) · airframe 51,212 hrs · 24,693 cycles

ABORTED TAKE-OFF. NR 1 NLG TIRE TREAD SEPARATED DURING TAKE-OFF ROLL AT APPROX 130 KNOTS, DAMAGING NLG SAFETY SENSOR ASSY AND WIRING, ALSO DAMAGING THE E&E COMPT DOOR. R&R BOTH NLG TIRES AND NLG SAFETY SENSOR ASSY / WIRING AND R&R E&E COMPT DOOR PER MM.

Part: HYD SYS — REQD SERVICE (LOWER MID FUSE)

HYD LOW PRESSURE A-SYSTEM INDICATON, QTY DECREASED TO 1/4 FULL. PREVIOUSLY REMOVED AND REPLACED NR 1 ENG T/R ISOLATION VALVE AND SUSPECT AIR IN SYSTEM. SERVICED HYD A-SYSTEM, ACTUATED FLIGHT CONTROLS AND NR 1 ENG T/R. ALL INDICATIONS CHECKED GOOD.

Part: BRACKET — LOOSE (SERVICE DOOR)

AFT GIRT BAR BRACKET LOOSE AT RT AFT SERVICE DOOR. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE DOOR — LOOSE (SERVICE DOOR)

DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY SLIDE LOOSE. REINSTALLED FWD SERVICE DOOR EMERGENCY SLIDE PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 879)

DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 879, LBL 2.5, WL 166. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CORRODED (BS 325)

DURING SERVICE CHECK, FOUND CORRODED UPPER CHORD AT BS 325, LBL 9 TO 14, WL 155. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 877)

DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 877 TO 907, STR 14 LEFT WL 230. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 432)

DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 432, RBL 45, WL 164. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 794)

DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUT PLATE AT BS 794, LBL 2.5 WL 158. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 954)

DURING SERVICE CHECK, FOUND CRACKED FWD SIDE OF FWD DOOR FRAME AFT SERVICE DOOR CUTOUT AT BS 954, RBL 55, WL 265. REMOVED PER BOEING SRM.

Part: WEB — CRACKED (BS 352)

DURING SERVICE CHECK, FOUND CRACKED WEB AT BS 352, RBL 1, WL 135. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 359)

DURING SERVICE CHECK, FOUND INTERCOSTAL SUPPORT ANGLE HAS ELONGATED FASTENER HOLES AT BS 359, BL 0, WL 149 TO 154. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 827.5)

DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL UPPER FWD CORNER AT BS 827.5 RBL 5.5 WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (RT TE FOREFLAP)

DURING SERVICE CHECK, FOUND RIGHT WING INBOARD FOREFLAP HAS A GOUGE AT LOWER SURFACE NEXT TO BULL NOSE 49 FROM I/B END 12 FROM T/E. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (LT TE FOREFLAP)

DURING SERVICE CHECK, FOUND LEFT O/B FOREFLAP 24.5 FROM I/B END DENTED AND PUNTURE ON LWR T/E SURFACE. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING SERVICE CHECK, FOUND NR 2 PYLON I/B AND O/B ACCESS CUTOUT PANEL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: STIFFENER — DAMAGED (CARGO DOOR)

DURING SERVICE CHECK, FOUND STIFFENER BETWEEN NR 2 AND NR 2 RIB ON FWD CARGO DOOR DAMAGED AREA. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CORRODED (BS 312)

DURING SERVICE CHECK, FOUND CORRODED FRAME AT BS 312, LBL 50, WL 182 ABOVE STR 20L. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SERVICE CHECK, FOUND CRACKED UPPER FWD INNER SKIN FRAME BETWEEN STOP FITTINGS NR 2 AND NR 3 ON FWD CARGO DOOR. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 294.5-310)

DURING SERVICE CHECK, FOUND CORRODED INTERCOSTAL WEB AT BS 294.5 TO 310, LBL 41 TO 46, WL 161. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 438)

DURING SERVICE CHECK, FOUND CRACKED EZ-4 RACK SUPPORT ANGLE AT BS 438, LBL 6 TO 28, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SERVICE CHECK, FOUND CRACKED STRINGER CLIP AT FWD CARGO BAY BS 500C, STR 23L, LBL 45, WL 164. REMOVED AND REPLACED PER BOEING SRM.

Part: PRESS PANEL — CORRODED (BS 663)

DURING SERVICE CHECK, FOUND CORRODED AT BS 663, RBL 47, WL 197 ON WHEEL WELL BULKHEAD. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT ANGLE — DAMAGED (BS 352-360)

DURING SERVICE CHECK, FOUND INTERCOSTAL SUPPORT ANGLE HAS ELONGATED FASTENER HOLES AT BS 352 TO 360, RBL 1, WL 149. REMOVED AND REPLACED DAMAGE INTERCOSTAL SUPPORT ANGLE PER BOEING SRM.

Part: BULKHD SUPPORT — WRINKLED (BS 380)

DURING SERVICE CHECK, FOUND WRINKLED SIDE BULKHEAD SUPPORT AT BS 380, STR 25L TO 19L, LBL 29 TO 55, WL 194 TO 160. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DENTED (BS 500)

DURING SERVICE CHECK, FOUND DENTED FLOORBEAM AT BS 500B, WL 150. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 813)

DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUT PLATE LOCATIONS AT BS 813 AND 825, LBL 2.5 WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 868-873)

DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN AT BS 868-873 ABOVE STR 24 RT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED CHECK, FOUND DENTED SKIN AT BS 500BT17, LBL 41, WL161. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 904/938)

DURING SCHEDULED TRAN CHECK, FOUND DENTED SKIN AT BS 904 2 ABOVE STR 21 RT; AND BS 938 3.5 ABOVE STR 24 RT. REPAIRED PER BOEING SRM.