N614SW

Part: HINGE FITTING — BROKEN (LT NR 4 SPOILER) · airframe 66,341 hrs · 52,819 cycles

LEFT WING NR 4 GROUND SPOILER INBD HINGE BROKEN. R & R SPOILER ASSY IAW MM.

Part: AXLE — CRACKED (NLG) · airframe 66,101 hrs · 52,661 cycles

NLG LT AXLE CRACKED AT CHROME. R & R NLG INNER AXLE ASSY IAW MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 65,851 hrs · 52,499 cycles

FORWARD ENTRY EXIT SIGN LENS BROKEN. REPAIRED THE LENS IAW EA.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 65,834 hrs · 52,490 cycles

FORWARD GALLEY EMERGENCY LIGHT COVER FELL OFF. INSTALLED THE COVER IAW SIP.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,619 hrs · 52,352 cycles

FLOORBEAM TIE STRAP CRACKED AT BS 344, BL 0. REPAIRED STRAP IAW SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 65,410 hrs · 52,212 cycles

L1 DOOR EXIT SIGN COVER MISSING. INSTALLED THE COVER IAW SIP.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 65,375 hrs · 52,189 cycles

R1 DOOR EMERGENCY SLIDE LOOSE. REINSTALLED SLIDE IAW MT.

Part: COVER — DEFECTIVE (COCKPIT) · airframe 65,222 hrs · 52,085 cycles

OVERHEAD PANEL COCKPIT CABIN EMERGENCY EXIT LIGHT SWITCH COVER INOPERATIVE. R & R COVER IAW MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 65,187 hrs · 52,065 cycles

RIGHT WING NR 4 SLAT DELAMINATED ON UPPER OUTBOARD END. R&R THE NR 4 SLAT ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 65,167 hrs · 52,049 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: LOCK — OBSTRUCTED (GIRT BAR) · airframe 64,780 hrs · 51,805 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOCK STUCK. REMOVED OBSTRUCTION OF LOCK IAW SIP.

Part: ATTACH ANGLE — CRACKED (TE FLAP) · airframe 64,204 hrs · 51,409 cycles

RIGHT WING NR 6 INBD FLAP, OTBD TRACK FAIRING, OTBD FWD LOWER PANEL ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (LT MLG) · airframe 64,204 hrs · 51,409 cycles

LEFT WING REAR SPAR MLG BEAM FITTING CRACKED. R & R FITTING IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 64,204 hrs · 51,409 cycles

RIGHT MLG AFT SUPPORT FITTING NR 5 HOLE CRACKED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (LT MLG) · airframe 64,204 hrs · 51,409 cycles

LEFT MLG AFT SUPPORT FITTING NR 5 HOLE CRACKED. R & R FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 238. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING, SKIN CRACKED TE 2ND FROM AFT FASTENER HOLE, AT RSS 245. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE 3RD FROM AFT FASTENER HOLE AT RSS 164. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 253. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 284. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT UPPER WING SKIN CRACKED TE AFT FASTENER HOLE AT RSS 249. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT UPPER WING SKIN TE, AFT FASTENER HOLE, CRACKED AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT WING, UPPER WING SKIN, TE EDGE AFT FASTENER HOLE AT RSS 269 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT UPPER WING SKIN TE, AFT FASTENER HOLE, AT RSS 264 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT UPPER WING SKIN TE, 2ND FROM AFT FASTENER HOLE, CRACKED AT RSS 213. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT UPPER WING SKIN, E AFT FASTENER HOLE, AT RSS 266 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT UPPER WING SKIN TE AFT FASTENER HOLE CRACKED AT RSS 256. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 221. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 221. REPAIRED WEB IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT WING LOWER SPLICE PLATE, WAFFLE BOARD, CRACKED AT RSS 27.3. REPAIRED SPLICE PLATE IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (CARGO DOOR) · airframe 64,204 hrs · 51,409 cycles

AFT CARGO, AFT CORNER SCUFF PLATE, CRACKED AT AFT CORNER. REPAIRED SCUFF PLATE IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,204 hrs · 51,409 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,204 hrs · 51,409 cycles

FORWARD GALLEY DOOR CUT OUT LOWER AFT CORNER SKIN CRACKED AT BS. 328+4, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 64,204 hrs · 51,409 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 64,204 hrs · 51,409 cycles

FORWARD CARGO AFT CORNER SCUFF PLATE CRACKED ON FWD & AFT. REPAIRED SCUFF PLATE IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,193 hrs · 51,402 cycles

RT WING INBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 64,193 hrs · 51,402 cycles

RT EMERGENCY EXIT LIGHT COVER BROKEN. R&R COVER PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,833 hrs · 51,159 cycles

R1 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: LENS — MISSING (CABIN) · airframe 63,411 hrs · 50,872 cycles

L1 DOOR LOWER EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: LENS — MISLOCATED (CABIN) · airframe 63,275 hrs · 50,771 cycles

FORWARD ENTRY EMER EXIT BULKHEAD LIGHT LENS MISS LOCATED. R & R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 62,986 hrs · 50,569 cycles

L2 DOOR EMER LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 62,915 hrs · 50,514 cycles

L1 DOOR EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 62,840 hrs · 50,466 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — MISSING (ROW 2 ABC) · airframe 62,652 hrs · 50,337 cycles

EMERGENCY BULLNOSE LIGHT LENS MISSING AT 2 ABC. INSTALLED LENS IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 62,454 hrs · 50,202 cycles

R1 DOOR SLIDE BUSTLE SLIDE LOOSE. SECURED BUSTLE IAW SOPM.

Part: WIRE — BROKEN (CABIN) · airframe 62,454 hrs · 50,202 cycles

RIGHT OVERWING EMER EXIT LIGHT WIRE BROKEN. REPAIRED WIRE IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

LONGITUDINAL FLOORBEAM CTR WING BOX UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED AT STATION 550, LBL 52. R & R INTERCOSTAL IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

TIE CLIP CRACKED AT STATION 947.5, STRINGER 24L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 2L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 5L. R & R CLIP IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 62,454 hrs · 50,202 cycles

LEFT WING NR 2 LE SLAT DELAMINATED AT OTBD EDGE. REPAIRED SLAT IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

RIGHT CREASE BEAM CRACKED AT STATION 460 - 480. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

AFT GALLEY DOOR CUTOUT LOWER FORWARD CORNER CRACKED. REPAIRED IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,454 hrs · 50,202 cycles

NOSE LANDING GEAR WW LT PANEL WEB CRACKED AT BS 259.5. REPAIRED WEB IAW SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 62,454 hrs · 50,202 cycles

OVERHEAD CTR CABIN EMER EXIT LIGHT LENS OUT OF POSITION AT BS 907. REPOSITIONED LIGHT ASSEMBLY IAW AMM.

Part: COVER — UNSECURE (CABIN) · airframe 62,402 hrs · 50,161 cycles

FORWARD BULKHEAD EMER EXIT LIGHT LENS COVER FELL OFF. ATTACHED COVER IAW SIP.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,069 hrs · 49,937 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: COVER — MISSING (CABIN) · airframe 61,937 hrs · 49,849 cycles

FORWARD GALLEY EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 61,846 hrs · 49,792 cycles

OVERHEAD ENTRY DOOR EMER EXIT SIGN INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 60,705 hrs · 49,022 cycles

RIGHT INBD TE MID FLAP WEDGE PANEL DELAMINATED TOP SURFACE. R & R WEDGE IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,643 hrs · 48,972 cycles

AFT PRESS BULKHEAD STIFFENER ANGLE CORRODED AT BS 1016 BL 0. REPAIRED ANGLE IAW SRM & EA.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 60,643 hrs · 48,972 cycles

L1 DOOR FRAME STOP FITTING CRACKED AT BS 348.2 STRINGER 16L. R & R FITTING IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 59,294 hrs · 48,019 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: MOUNT BRACKET — BROKEN (R2 DOOR) · airframe 58,999 hrs · 47,812 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT SIDE MOUNT BRACKET BROKEN. R & R BRACKET IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,960 hrs · 47,788 cycles

LEFT EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,960 hrs · 47,788 cycles

RT EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,909 hrs · 47,752 cycles

RT AFT WING TO BODY EMERGENCY LIGHT INOPERATIVE. RE LAMPED LIGHT IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,277 hrs · 46,587 cycles

LT WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 57,274 hrs · 46,586 cycles

LT WING AILERON MID INBD HINGE ANGLE CRACKED AT FWD INBD SIDE AT APPROXIMATELY RSS 545. R&R ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,271 hrs · 46,585 cycles

FORWARD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 9L. R&R CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER SPLICE FITTING CRACKED AT STATION 908, STRINGER 4L. R&R FITTING IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

SKIN CRACKED AT STATION 380, STRINGER 14L. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER CRACKED AT STATION 727 +10, STRINGER 1. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

SKIN CRACKED AT STATION 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER CRACKED AT STATION 500D, STRINGER 8R. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT FS SKIN CRACKED AT BS 767+ 10, LOWER FWD CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 3,4,6,& 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT FS SKIN CRACKED AT BS 727B+ 10, UPPER AFT WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLE #4,5, & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT BS 727+10 LOWER FORWARD WINDOW SKIN CUT OUT CRACKED AT HOLE NR 6 & NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 847+10, UPPER AFT PAX WINDOW CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 827+ 10, LOWER FWD CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 3,4,5,6,8,9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT FS SKIN CRACKED AT BS 827+10, UPPER AFT PAX WINDOW CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 4,5,10,11,12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 807+10 LOWER FORWARD WINDOW SKIN CUT OUT CRACKED AT HOLES 3 & 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT BS 807+10 LOWER FORWARD WINDOW SKIN CUT OUT CRACKED AT HOLES 2,3,4,6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT FS SKIN CRACKED AT BS 727B+ 10, LOWER FWD WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 887+10, UPPER AFT PAX WINDOW CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 2,5,6,7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 867+ 10, UPPER AFT CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 847+ 10, LOWER FWD CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT FS SKIN CRACKED AT BS 747+ 10, UPPER AFT WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 787+ 10, UPPER AFT CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 787+ 10, LOWER FWD CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER CLIP DAMAGED AT BS 827, STRINGER 9R. R&R STRINGER CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 827+ 10, UPPER AFT CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

LT FS SKIN CRACKED AT BS 767+ 10, UPPER AFT CORNER OF PAX WINDOW CUTOUT. REPAIRED SKIN IAW SB & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,271 hrs · 46,585 cycles

STRINGER CRACKED AT STATION 727E, STRINGER 6L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,271 hrs · 46,585 cycles

RT WING NR 5 SLAT LE CRACKED JUST OTBD OF INBD TRACK. REPAIRED SKIN IAW SRM.

Part: CRADLE — FAULTY (COCKPIT) · airframe 57,075 hrs · 46,451 cycles

ON LANDING ROLL STRONG ELECTRICAL BURNING SMELL IN COCKPIT--OPC RADOME CIRCUIT BREAKER POPPED. OPC CHARGING CRADLE FOUND TO BE CAUSE. R&R OPC CRADLE IAW MM.

Part: COWLING — DELAMINATED (NR 1 ENGINE) · airframe 56,986 hrs · 46,381 cycles

NR 1 INBD FAN COWL DELAMINATED AT LOWER AFT CORNER. R & R COWL IAW SRM.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

UPPER CLEET CRACKED AT BS 727, RBL 19.5 BULKHEAD VERTICAL STIFFENER. REMOVED AND REPLACED CLEET PER SRM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

OUTER CHORD DAMAGED AT STA 291, STR 16R. REPAIRED CHORD IAW EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,986 hrs · 46,381 cycles

RIGHT FWD EMERGENCY EXIT LIGHTS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

STRINGER CORRODED AT BS 1016, STR 24R. REMOVED AND REPLACED STRINGER PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REMOVED AND REPLACED WEB PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FITTING CORRODED AT BS 1016, STR 24R. / REMOVED AND REPLACED FITTING PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

UNDERSIDE OF NUT PLATE HOLE CORRODED AT BS 807+6, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, RBL 11. REMOVED AND REPLACED TRACK PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, LBL 2. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, LBL 11. REPAIRED BEAM PER EA.

Part: INTERCOSTAL — SHEARED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT SIDE INTERCOSTAL WEB SHEARED AT BS 947, FWD SIDE OF FRAME UNDER RIGHT TRANSITION ANGLE. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, LBL 7. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 858, RBL 8. REMOVED AND REPLACED TRACK PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

RIGHT INTERCOSTAL WEB CORRODED BETWEEN BS 927 TO BS 947. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

STRINGER CORRODED AT BS 996, STR 25L. REPAIRED STRINGER PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM CRACKED AT BS 663, LBL 24.8. REMOVED AND REPLACED ANGLE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FLOOR CHANNEL CORRODED AT BS 727D+6, LBL 3. REPAIRED CHANNEL PER EA.

Part: TRACK — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO COMPARTMENT FLOOR TRACK NUT PLATE HOLES CORRODED AT STA 727D+6, LBL 17. REMOVED AND REPLACED TRACK PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FLOOR CHANNEL CORRODED AT BS 727D+6, RBL 3. REPAIRED CHANNEL PER EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

AFT CARGO COMPARTMENT INTERCOSTAL UNDER RIGHT TRANSITION ANGLE CORRODED BETWEEN BS 747 TO BS 767. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STR 18L. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 705, BBL .07. REPAIRED WEB PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 712.5, RBL 24.8. REPAIRED WEB PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, BBL .07. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STR 18R. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 714, LBL 24.8. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707.5 TO BS 710.25, LBL 24.8. REPAIRED WEB PER EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FLOOR SUPPORT STRAP CORRODED AT BS 782. REMOVED AND REPLACED STRAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FRAME CRACKED AT BS 727, OUTBOARD CHORD FORWARD FLANGE, RIGHT LOWER ROW. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

FRAME CRACKED AT BS 727, STR 18L. REPAIRED FRAME IAW EA.

Part: FLAP TRACK — CRACKED (LT WING) · airframe 56,986 hrs · 46,381 cycles

NR 1 FLAP TRACK CRACKED APPROX 15" FROM FWD END ON LOWER I/B FLANGE. REMOVED AND REPLACED NR 1 FLAP TRACK PER MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 712, LBL 24.8. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, RBL 24.8. REPAIRED WEB PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, BBL .07. REPAIRED WEB PER EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,986 hrs · 46,381 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, BBL .07. REPAIRED WEB PER EA.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

RIGHT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 19. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 21. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 6. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

RIGHT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 8. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 17. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 56,986 hrs · 46,381 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 13. REMOVED AND REPLACED LENS PER MM.

Part: STRIP — PEELING (CABIN) · airframe 56,809 hrs · 46,259 cycles

LEFT EMERGENCY EXIT LIGHT STRIP PEELING AWAY AT 8. REMOVED AND REPLACED EEPLS PER AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 56,196 hrs · 45,844 cycles

R-1 DOOR ESCAPE SLIDE HAS EXCESSIVE GIRT EXPOSED OUT OF CASE. RE-SECURED SLIDE PER M/M.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 56,196 hrs · 45,844 cycles

L-1 DOOR ESCAPE SLIDE HAS EXCESSIVE GIRT EXPOSED OUT OF CASE. RE-SECURED SLIDE PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,052 hrs · 45,729 cycles

FOUND INDICATION OF 2" SUBSURFACE FUSELAGE SKIN CRACK AT BS 727C+9" ABOVE STR 4R. ACCOMPLISHED SKIN REPAIR IAW ATS ER 12-03715 AND EA 1-353-21258.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,052 hrs · 45,729 cycles

LEFT FWD FUSELAGE IS CRACKED 1.5" AT STA 500D+7.0" AND ABOVE STR 10L MOD. REPAIRED FUSELAGE SKIN CRACKED AT BS 500D+7 ABOVE STR 10L IAW ER 12-03718 & EA 1-353-21251.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,052 hrs · 45,729 cycles

FOUND INDICATION OF 1" SUBSURFACE FUSELAGE SKIN CRACK AT BS 727D+12" ABOVE STR 4R. ACCOMPLISHED SKIN REPAIR IAW ATS ER 12-03715 AND EA 1-353-21258 TLD T032451 ACCOMPLISHED ON CUSTOMER CARD T175656.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,052 hrs · 45,729 cycles

FOUND INDICATION OF 1" SUBSURFACE FUSELAGE SKIN CRACK AT BS 727C+7" ABOVE STR 4L. REPAIRED SKIN CRACK AT BS 727C+7 ABOVE STR 4L IAW EA 1-A53-5808.

Part: WEB — CRACKED (LT MLG WW) · airframe 55,911 hrs · 45,629 cycles

MAIN WHEEL WELL CEILING BEADED WEB CRACKED STA 664 LBL 32 VERIFIED WITH HFEC AND MARKED. REPAIRED DAMAGE IAW SRM 53-60-51-2R-4. PERFORMED LEAK CHECK WITH NO DEFECTS NOTED REF M/M 99992.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,505 hrs · 45,349 cycles

BULLNOSE EMERGENCY LIGHT AT ROW 6 ABC INOP. RELAMPED BULLNOSE EMERGENCY LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 54,159 hrs · 44,314 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 54,160 hrs · 44,314 cycles

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

Part: STRAP — CRACKED (BS 794 FRAME) · airframe 53,468 hrs · 43,792 cycles

AFT CARGO DOOR CUTOUT FWD FRAME STRAP CRACKED AT BS 794, WL 165. REMOVED AND REPLACED STRAP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,468 hrs · 43,792 cycles

AFT CARGO DOOR CUTOUT, FWD LWR CORNER CRACKED AT WEB. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,468 hrs · 43,792 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND 21L. REPAIRED FRAME IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,822 hrs · 42,551 cycles

LT EMERGENCY EXIT LIGHT SWITCHED INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,822 hrs · 42,551 cycles

RT EMERGENCY EXIT LIGHT SWITCHED INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULE 16Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 827, STR 26R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CRACKED AT BS 520+6, STR 11L. REPAIRED SKIN PER EO AND EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING AFT FLAP DELAMINATED INBOARD OF LOWER SURFACE. REPAIRED AFT FLAP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 787, BETWEEN STR 25L TO STR 24L. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 887, STR 24L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 986.5 TO BS 1006, STR 21R. REPAIRED STRINGER PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 345, STR 8L. REMOVED AND REPLACED ANGLE PER SRM. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOOR WEB CORRODED BETWEEN BS 767 TO BS 787, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 8 TO RBL 43. REPAIRED CHORD PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727C+6, RBL 3. REPAIRED CHANNEL PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, BULKHEAD WEB SPLICE CRACKED AT BS 1016, RBL 2.5. REPAIRED SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOOR WEB CORRODED BETWEEN BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 332, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOOR WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOOR WEB CORRODED BETWEEN BS 747 TO BS 767, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 360, STR 3L. REMOVED AND REPLACED SPLICE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,433 hrs · 42,261 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,259 hrs · 42,121 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT EMERGENCY FLASHLIGHT BATTERIES INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: ENGINE — MAKING METAL (NR 2) · airframe 49,804 hrs · 41,018 cycles

INFLIGHT SHUT DOWN/ AIR TURNBACK. NR 2 ENGINE LOUD BANG; EGT 900 DEGREES, SHUT DOWN ENGINE. FOUND METAL DEBRIS IN TAILPIPE AND OIL LEAKAGE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,110 hrs · 40,469 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT O/B FLOORBEAM CRACKED AT BS 316. REPAIRED BEAM PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 48,381 hrs · 39,903 cycles

OUTER PANE OF L1 WINDOW SHATTERED AT 33,000 ARCED BEFORE SHATTERED. REMOVED AND REPLACED L1 WINDOW AND CONTROLLER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FWD FRAME CRACKED AT BS 440, AT NR 5 STOP PAD FITTING. REMOVED AND REPLACED FRAME PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,294 hrs · 39,830 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 47,679 hrs · 39,362 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,679 hrs · 39,362 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 1001, STR 5R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,679 hrs · 39,362 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 47,679 hrs · 39,362 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 47,679 hrs · 39,362 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT I/B END UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 47,679 hrs · 39,362 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,608 hrs · 39,309 cycles

DURING SCHEDULED MV2 CHECK, FOUND NR 3 VHF ANTENNA SKIN CRACKED AT BS 727E, BL 0. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 46,982 hrs · 38,844 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,321 hrs · 37,612 cycles

DURING SCHEDULED CV CHECK, FOUND RT WING TRAILING EDGE I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 44,450 hrs · 36,989 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B LEADING EDGE SKIN DELAMINATED. INSTALLED SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,450 hrs · 36,989 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,449 hrs · 36,989 cycles

LT FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 44,363 hrs · 36,935 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,846 hrs · 36,567 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,846 hrs · 36,567 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,846 hrs · 36,567 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,846 hrs · 36,567 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE SKIN CUTOUT CRACKED AT BS 305, WL 257. REPAIRED SKIN PER PAE ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 43,846 hrs · 36,567 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,358 hrs · 36,206 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 41,197 hrs · 34,601 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,166 hrs · 34,575 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, LBL 1.5. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CONTROL ROD — WORN (LT AILERON) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, LT AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,136 hrs · 34,554 cycles

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

Part: FRAME — CRACKED (BS 400 S8L) · airframe 41,136 hrs · 34,554 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,273 hrs · 33,130 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: SKIN — DAMAGED (BS 362 S17L) · airframe 38,087 hrs · 32,188 cycles

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 362, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 36,635 hrs · 31,045 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT INBOARD LOWER T/E. REPAIRED L/E SLAT PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,621 hrs · 28,699 cycles

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

Part: SKIN — CORRODED (BS 787) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 787, RBL 10. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (BS 494) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 494, FWD CARGO DOOR NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 616) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RBL 65, WL 202. REPAIRED FRAME CHORD PER BFG ER.

Part: FLOORBEAM — CRACKED (BS 294.5) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 53. REPAIRED FLOORBEAM UPPER CHORD PER SRM.

Part: FRAME — CORRODED (BS 846) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 846, BETWEEN STR 24R & STR 25R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 787) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: GIRT BAR — CORRODED (BS 344) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR FITTING CORRODED AT BS 344. REMOVED AND REPLACED AFT GIRT BAR FLOOR FITTING PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CORRODED (R2 DOOR) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND R2 DOOR CUTOUT, FWD LOWER FRAME CORRODED AT BS 956, WL 208. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 270-328) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 270 TO BS 328. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 328, RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 947, BETWEEN BL 0 TO LBL 45, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: CREASE BEAM — CRACKED (BS 616) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 65. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L & STR 8R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 294-390) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 294-390. REPAIRED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 35 TO RBL 45, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BL 0 & RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 270) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, RBL 11 TO LBL 11, WL 208. REPAIRED Z-CHORD PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN BL 0 TO RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L TO STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L TO STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (BS 807) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 33,621 hrs · 28,699 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER RT T/E ANGLE CRACKED AT RS 23.37. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,037 hrs · 28,239 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378, BL 0. REPAIRED SKIN PER SWA EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,747 hrs · 27,191 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR LOWER HINGE BOX PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,846 hrs · 26,478 cycles

DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE BETWEEN ROWS 22 AND 23. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 30,661 hrs · 26,333 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 29,429 hrs · 25,326 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: LENS — BROKEN (EMERGENCY SIGN) · airframe 28,987 hrs · 24,973 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LOWER SIGN LENS BROKEN. REMOVED AND REPLACED SIGN LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 28,791 hrs · 24,820 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING RT OUTBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 28,147 hrs · 24,320 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 26,876 hrs · 23,299 cycles

AIR TURNBACK, DECLARED EMERGENCY, FWD CARGO FIRE DETECTION LIGHT ILLUMINATED, DISCHARGED BOTTLES. REMOVED AND REPLACED FOLLOWING, NR 1 AND NR 2 FIRE BOTTLES, CONTROL CABIN FIRE DETECTION PANEL, CARGO FIRE SYSTEM METERING VALVE, FIRE DETECTORS NR 1, NR 2, NR 3 AND NR 4 AND DIVERTER VALVE PER MM. AWAITING ENGINEERING INVESTIGATION TO DETERMINE ACTUAL CAUSE.

Part: ACTUATOR — FAULTY (LT WING TE FLAP) · airframe 25,996 hrs · 22,563 cycles

AIR TURNBACK - LEFT OUTBOARD L/E FLAP REMAINED EXTENDED DURING FLAP RETRACTION. REMOVED AND REPLACED LEFT OUTBOARD L/E FLAP ACTUATOR PER MM.

Part: SENSOR — OUT OF ADJUST (RT MLG W/W) · airframe 25,271 hrs · 21,992 cycles

AIR TURNBACK, LANDING GEAR LEVER WOULD NOT GO UP PAST THE OFF POSITION. TAKEOFF WARNING HORN SOUNDED. MX FERRY TO MDW, AND ADJUSTED GROUND SHIFT AIR SENSOR CABLE ASSY PER MM.

Part: SOLENOID — INOPERATIVE (COCKPIT) · airframe 25,271 hrs · 21,992 cycles

AIR TURNBACK, LANDING GEAR LEVER WOULD NOT MOVE UP PAST THE OFF POSITION. LANDING GEARS WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR LEVER LOCK SOLENOID PER MM.

Part: FLAP — CRACKED (RT WING) · airframe 25,271 hrs · 21,992 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING T/E OUTBD FORE FLAP LOWER SKIN CRACKED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 23,414 hrs · 20,446 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY'S OUT OF ADJUST. ADJUSTED BOTH FWD SLIDES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,595 hrs · 19,763 cycles

OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 20 DEF. RELAMPED LIGHT PER MM.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 19,867 hrs · 17,502 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 18,920 hrs · 16,695 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBD AFT T/E FLAP DISBONDED AT RT LOWER SIDE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 18,429 hrs · 16,280 cycles

DECLARED EMERGENCY, FL 330, R1 WINDOW OUTER PANE CRACKED AND ARCED. PRESSURIZATION REMAINED NORMAL. REMOVED AND REPLACED R1 WINDOW AND RT FRONT WINDOW HEAT CONTROLLER (P/N 531-2) PER MM. OPS CHECK GOOD.

Part: INDICATOR — DISCONNECTED (COCKPIT) · airframe 17,663 hrs · 15,635 cycles

AIR TURNBACK, A/C HAD NO INDICATION OF CABIN PRESS AFTER TAKEOFF. FOUND QUICK DISCONNECT NOT CONNECTED ON BACK OF DIFFERENTIAL PRESSURE GAUGE. SECURED CONNECTION PER MM.

Part: LENS — LOOSE (CABIN) · airframe 17,612 hrs · 15,593 cycles

FWD ENTRY WALL EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS.

Part: BLEED VALVE — ERRATIC (APU) · airframe 17,248 hrs · 15,289 cycles

AIR TURNBACK, DURING CLIMBOUT LT DUCT PRESSURE WENT FROM 51 PSI TO 5 PSI & IN CRUISE IDLE LEFT DUCT PRESSURE WENT FROM 26 PSI TO 3 - 5 PSI. REMOVED AND REPLACED APU BLEED AIR VALVE AND APU BLEED AIR PRESS REG (P/N 108032-8) PER MM.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT ELEVATOR I/B RIB CRACKED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR INBOARD RIB CRACKED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHTING PACK AT BS 603, WL 213, RBL 68 INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT GUSSET ATTACH HOLE, LOWER CORNER. REPAIRED DOOR PER SRM & BAC DRAWING.

Part: GUSSET — CRACKED (SERVICE DOOR) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT LWR CORNER GUSSET CRACKED. REPAIRED DOOR PER SRM.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STUB FRAME AT FWD ENTRY LOWER DOOR OPENING, BS 294.5. REPAIRED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CLIP NUT HOLE CORRODED AT BS 947, FLOORBEAM, RBL 42. REPAIRED FLOORBEAM PER RA 1-353-2363.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STUB FRAME CRACKED BS 294.5 LT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,229 hrs · 15,274 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED AT BS 947, LBL 12 - LBL 28. REPAIRED BEAM PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 17,053 hrs · 15,119 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — MISINSTALLED (PAX DOOR) · airframe 16,870 hrs · 14,965 cycles

FWD ENTRY DOOR EVACUATION SLIDE NOT PROPERLY STOWED. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 16,495 hrs · 14,651 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY (GIRT BAR IMPROPERLY STOWED). REINSTALLED SLIDE ASSY.

Part: COVER — LOOSE (CABIN) · airframe 16,117 hrs · 14,316 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS LOOSE AT ROWS 13 - 14. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,000 hrs · 14,216 cycles

FOUR EEPLS INOP. REPAIRED WIRING BY OVERWING EXIT ROW. OPS CHECK GOOD PER MM.

Part: LENS — MISSING (CABIN)

EEPLS LENS MISSING AT ROW 3. INSTALLED MISSING LENS PER MM.

Part: BATTER PACK — DISCHARGED (CABIN)

EEPLS INOP BETWEEN ROWS 14 AND 19. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — TORN (PAX DOOR)

DURING SCHEDULED SPECIAL VISIT FOUND, AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY TORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: TRANSFER RELAY — FAILED (NR 1)

DIVERTED TO PHX DUE TO STANDBY POWER OFF LIGHT ILLUMINATING. \N\NR&R #1 TRANSFER RELAY R3 PER M/M