N399WN

Part: MOUNT BRACKET — LOOSE (L2 DOOR) · airframe 68,304 hrs · 54,825 cycles

L2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET LOOSE. R&R BRACKET PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,304 hrs · 54,825 cycles

LT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,536 hrs · 54,296 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED THE LENS IAW EA.

Part: COVER — LOOSE (L1 DOOR) · airframe 67,506 hrs · 54,275 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW SIP.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 794, RBL 21. R & R INTERCOSTAL IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 67,221 hrs · 54,076 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 15R. R & R THE STRINGER CLIP IAW EA.

Part: SHEAR TIE — CRACKED (BS 277) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CRACKED AT BS 277, BETWEEN STRINGERS 13 - 14R. REPAIRED THE SHEAR TIE IAW ER & EA.

Part: INTERCOSTAL — CRACKED (BS 279) · airframe 67,221 hrs · 54,076 cycles

INTERCOSTAL WEB CRACKED AT BS. 279, STR. 14R. R & R THE INTERCOSTAL IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

CREASE WEB CORRODED BETWEEN BS 867 TO BS 887, LBL 65. R&R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

CREASE WEB CORRODED BETWEEN BS 460 TO BS 480, RBL 65. R&R WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

CREASE WEB CORRODED BETWEEN BS 420 TO BS 440, RBL 65. R&R WEB PER SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

FRAME SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHIELD — CORRODED (BS 847-867) · airframe 67,221 hrs · 54,076 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS 847 - 867, STRINGER 25R. R & R THE SHIELD IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 67,221 hrs · 54,076 cycles

MAIN WHEEL HORIZONTAL PRESSURE DECK BEADED WEB CRACKED AT BS 665, RBL 39. REPAIRED WEB PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 67,221 hrs · 54,076 cycles

LEFT WING, RIB LOWER CHORD AT WBL 135.5 CRACKED AT RADIUS BETWEEN S-2 AND S-3. REPAIRED CHORD IAW EA.

Part: MOUNT BRACKET — CORRODED (L1 DOOR) · airframe 67,221 hrs · 54,076 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR MOUNT BRACKET CORRODED. R&R BRACKET PER SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

RIGHT MOP SILL FORWARD ATTACH DOUBLER CORRODED BETWEEN BS 294 TO BS 312. R & R DOUBLER IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

RT MOP SILL AFT ATTACH DOUBLER ANGLE CORRODED. R&R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

FLOORBEAM CHORD CRACKED AT BS 312, RBL 22, UPPER FLANGE. REPAIRED CHORD IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 67,221 hrs · 54,076 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 10R. R & R THE STRINGER CLIP IAW ER & EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR WEB CRACKED AT BS 986, LBL 35. R & R WEB IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

STRINGER CLIP CORRODED AT BS 807, STR 26R. R&R CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 28R - 28L. REPAIRED THE SHEAR TIE IAW EA.

Part: STRINGER CLIP — CORRODED (BS 927) · airframe 67,221 hrs · 54,076 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 927, STRINGER 26R. R & R THE STRINGER CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26 TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 67,221 hrs · 54,076 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 787, STRINGER 27R. R & R THE STRINGER CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (BS 867) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STRINGERS 25 - 26R. REPAIRED THE SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

FRAME SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: GUSSET — CORRODED (BS 727E) · airframe 67,221 hrs · 54,076 cycles

AFT CARGO BAY ANTENNA GUSSET CORRODED AT BS 727E, RBL 1. R & R GUSSET IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26 TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26 TO STR 27R. R&R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 907) · airframe 67,221 hrs · 54,076 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 907, STRINGER 26R. R & R THE STRINGER CLIP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, LBL 3. REPAIRED INTERCOSTAL PER DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 27 TO STR 28R. R&R SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 27 - 28L. REPAIRED THE SHEAR TIE IAW ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 67,221 hrs · 54,076 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 27 - 28R. REPAIRED THE SHEAR TIE IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,221 hrs · 54,076 cycles

INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. R&R INTERCOSTAL PER DWG & SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 67,221 hrs · 54,076 cycles

RT WING INBOARD NO STEP PANEL INBOARD AFT ATTACH POINT ANGLE CRACKED. REPAIRED ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 67,221 hrs · 54,076 cycles

NOSE WHEEL WELL RT SIDE WEB CRACKED BETWEEN BS 247 - 248, RBL 16. REPAIRED THE WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT AILERON) · airframe 67,221 hrs · 54,076 cycles

RIGHT WING AILERON WIPER WEB SUPPORT ANGLE CRACKED AT RSS 547. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 67,221 hrs · 54,076 cycles

LT WING INBOARD NO STEP PANEL INBOARD AFT ATTACH POINT ANGLE CRACKED IN CUTOUT RADIUS. REPAIRED ANGLE IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (LT AILERON) · airframe 67,221 hrs · 54,076 cycles

LEFT WING AILERON WIPER WEB ATTACH ANGLE CRACKED AT RSS 547. R & R ANGLE IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 67,221 hrs · 54,076 cycles

FLIGHT COMPARTMENT RT NR 1 WINDOW UPPER FRAME ASSEMBLY OUTBOARD RADIUS CRACKED. REPAIRED SKIN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

STRAP ANGLE CORRODED, BETWEEN BS 967 - 981, STRINGER 21R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

ANGLE CORRODED, BETWEEN BS 943 - 955, STRINGER 21R. R & R ANGLE IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

R2 DOOR MOP SILL INNER CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

INTERCOSTAL CRACKED, BETWEEN BS 927 - 947, STRINGER 21R. R & R INTERCOSTAL IAW DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

STUB FRAME CORRODED AT BS 992, BETWEEN STRINGER 17R - 21R. R & R STUB FRAME IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

FORWARD BUTT STRAP STRINGER CORRODED AT BS 908, STRINGER 21R. R & R STRINGER IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,815 hrs · 53,795 cycles

AFT RT OVERHEAD BIN EMER LIGHT INOPERATIVE AT ROW 12. RELAMPED LIGHT IAW AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,815 hrs · 53,795 cycles

STRINGER CORRODED, BETWEEN BS 907 - 1000, STRINGER 21R. R & R STRINGER IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,814 hrs · 53,794 cycles

STRINGER CORRODED AT BS 902, STRINGER 23R. R & R STRINGER IAW SRM.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 66,022 hrs · 53,271 cycles

DECLARED EMER, DURING APPROACH WITH GEAR & FLAPS 30, MASTER CAUTION & HYD LIGHTS ILLUMINATED. INDICATIONS WERE A SYS HYD LOW PRESS, BOTH ENG & ELEC, LIGHTS & ZERO A SYS QTY. R & R A ELEC MOTOR DRIVEN PUMP IAW AMM.

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 65,992 hrs · 53,252 cycles

AIR TURN BACK, DECLARED EMER & A SYS HYD PRESS WENT TO 1200 PSI ON CLIMB OUT, THEN TO 200 PSI BY LANDING, EMER DECLARED. FOUND O RING ON A HYD SYS TRANSMITTER LEAKING. REPLACED A SYS PRESS TRANSMITTER O RING IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 65,825 hrs · 53,139 cycles

RIGHT WING NR 5 SLAT DELAMINATED AT 66" FROM INBD SIDE. R & R NR 5 SLAT IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 65,825 hrs · 53,139 cycles

LEFT WING NR 3 SLAT TE DELAMINATED AT INBD END. R & R NR 3 SLAT IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 65,825 hrs · 53,139 cycles

LEFT WING NR 2 SLAT TE INBD END DELAMINATED. R & R NR 2 SLAT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,520 hrs · 52,912 cycles

RIGHT MID CABIN EMER EXIT LIGHT AT ESCAPE HATCH INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,227 hrs · 52,716 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,138 hrs · 52,656 cycles

RIGHT WING OTBD AFT FLAP TE INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING NR 6 INBD FLAP OTBD TRACK FAIRING TO STRUT OTBD FRAME ATTACH ANGLE CRACKED AT BS 363.65. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING FORWARD MAIN LANDING GEAR FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING REAR SPAR LOWER CHORD RSS 225, LOWER CHORD FWD ATTACH FLANGE, AFT CHORD TO SKIN ATTACH FASTENER HOLE CRACKED. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING UPPER SKIN CRACKED IN FASTENER HOLE AFT OF REAR SPAR, NEAR RSS 251. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING UPPER SKIN CRACKED INDICATION IN FASTENER HOLE AFT OF REAR SPAR, NEAR RSS 192. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING UPPER SKIN CRACKED IN FASTENER HOLE AFT OF REAR SPAR NEAR RSS 267. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE ON TE NEAR RSS 239. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AFT OF REAR SPAR, NEAR RSS 288. REPAIRED SKIN IAW EA & ER.

Part: FITTING — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING RSS 222.25 UPPER SIDE FASTENER HOLE COMMON TO REAR SPAR WEB & MAIN LANDING GEAR FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: FRAME — CORRODED (BS 794) · airframe 65,014 hrs · 52,570 cycles

FUSELAGE FRAME CORRODED AT BS 794.3, STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 209 IN TOP FASTENER HOLE IN UPPER CHORD OF SPAR. REPAIRED WEB IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 211 IN TOP FASTENER HOLE IN UPPER CHORD OF SPAR. REPAIRED WEB IAW SRM.

Part: STRUCTURE — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING RSS 219, WING CHORD CRACKED AT THE FASTENER HOLE UPPER INBOARD SIDE OF AFT FITTING. REPAIRED CHORD IAW SRM & EA.

Part: WEB — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING RSS 219 WEB CRACKED RACK INDICATION AT UPPER FASTENER HOLE AT AFT FITTING INBOARD SIDE. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING STATION RSS 220 AFT FITTING, FASTENER HOLE UPPER INBD SIDE CRACKED. R & R FITTING IAW DWG & SRM.

Part: FITTING — CRACKED (LT WING) · airframe 65,014 hrs · 52,570 cycles

LEFT WING REAR SPAR RSS 222, UPPER FASTENER HOLE INBD SIDE OF FITTING CRACKED. R & R FITTING IAW DWG.

Part: FITTING — CRACKED (RT WING) · airframe 65,014 hrs · 52,570 cycles

RIGHT WING UPPER CHORD STATION RSS 220 UPPER FASTENER HOLE ON INBD SIDE OF AFT FITTING CRACKED. REPAIRED CHORD IAW EA.

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 65,014 hrs · 52,570 cycles

STRINGER CLIP CORRODED AT BS 787, STRINGER 26R. R & R THE STRINGER CLIP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 65,014 hrs · 52,570 cycles

INTERCOSTAL AT CREASE BEAM INNER CORD CORRODED AT BS 808 ABOVE DOOR CUT OUT. R & R FRAME IAW DWGS & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,014 hrs · 52,570 cycles

AFT CARGO DOOR CUTOUT FWD FRAME CLOSE OUT WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,950 hrs · 52,523 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,372 hrs · 51,442 cycles

RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,372 hrs · 51,442 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE AREA. REPAIRED SKIN IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 63,225 hrs · 51,329 cycles

R1 DOOR SIDEWALL EXIT SIGN LIGHT ASSEMBLY LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 62,954 hrs · 51,130 cycles

L2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FRAME WEB AT CRACKED AT BS 695 BETWEEN LBL 61 TO 62. REPAIRED WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FORWARD CARGO DOOR CUT OUT WEB CORRODED AT BS 490, STRINGER 18R TO 19R. REPAIRED WEB IAW SRM & DWG.

Part: LUG — CORRODED (LT WING) · airframe 62,250 hrs · 50,601 cycles

LEFT WING NR 4 FLAP TRACK AFT ATTACH POINT, OTBD LUG, OTBD FACE CORRODED ADJACENT TO BUSHING. REPAIRED LUG IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

L1 DOOR FWD FRAME CLIP CRACKED AT BS 348 STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

RIGHT INBD EXHAUST ATTACH WEB CRACKED AT BS 662. R & R WEB IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

STUB BEAM CRACKED AT BS 616 RT. R & R STUB BEAM IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

CLIP CRACKED AT BS 348.20 STRINGER 16L. R & R CLIP IAW DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGER 14L TO 15L. R & R SHEAR TIE IAW SRM.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

L1 DOOR STOP FITTING CRACKED AT BS 348 STRINGER 16L. REPAIRED FITTING IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FORWARD ENTRY DOOR L ANGLE CRACKED AT BS 348 STRINGER 15L AT DOOR STOP FITTING, CRACK INDICATIONS AT LOWER OTBD HOLE. R & R L ANGLE IAW DWG & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 62,250 hrs · 50,601 cycles

L1 DOOR FRAME INNER CHORD CRACKED AT BS 348 WL 208. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — BUCKLED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

LEFT CREASE BEAM WEB BUCKLED BETWEEN BS 360 TO 380 STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

RIGHT FRAME INNER CHORD CRACKED AT BS 616 WL 200. REPAIRED CHORD IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

SEAT TRACK CRACKED AT BS 727B RBL 24. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

SKIN CRACKED AT BS 727E BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867. REPAIRED WEB IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

RIGHT CREASE BEAM INNER CHORD CRACKED AT BS 639 WL 208. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,250 hrs · 50,601 cycles

MAIN WW PRESS DECK CRACKED AT BS 666, LBL 39.5. REPAIRED DECK IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

AFT CARGO BAY ANGLE CLIP ATTACHED TO INTERCOSTAL CRACKED AT BS 947.5, STRINGER 24L. R & R CLIP IAW SRM & DWG.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 62,250 hrs · 50,601 cycles

AFT CARGO DOOR AFT END CROSSBEAM T CHORD CRACKED INDICATION COMING FROM SECOND AFT FASTENER HOLE COMMON WITH STOP FITTING OTBD FASTENERS. R & R AFT CARGO DOOR IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 727B RBL 24.8. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — LOOSE (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FLOORBEAM UPPER CHORD LOOSE AT BS 727B RBL 24.8. R & R CHORD IAW EA.

Part: ATTACH BRACKET — CRACKED (FLAP TRACK) · airframe 62,250 hrs · 50,601 cycles

LEFT WING TE NR 3 FLAP TRACK FAIRING INTERIOR STRUCTURE RT SIDE FLAP DOOR SPRINGS ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

FORWARD GALLEY DOOR CUT OUT STRUCTURE OTBD OF FWD UPPER LATCH FITTING CRACKED. R & R STUB FRAME IAW DWG & SRM.

Part: ACCESS PANEL — DELAMINATED (LT WING) · airframe 62,250 hrs · 50,601 cycles

LEFT WING LE ACCESS PANEL 6231 DELAMINATED AT FWD INBD CORNER. REPAIRED PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,529 hrs · 50,815 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,250 hrs · 50,601 cycles

RIGHT FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 61,973 hrs · 50,408 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,823 hrs · 50,295 cycles

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

Part: SLIDE — LOOSE (L2 DOOR) · airframe 61,720 hrs · 50,221 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 60,523 hrs · 49,431 cycles

DIVERSION DECLARED EMERGENCY. AT CRUISE SMOKE SMELL BEGAN TO FILL CABIN, GASPER FAN WAS TURNED OFF & IT EASED THE SMELL. R & R GASPER FAN IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 60,321 hrs · 49,290 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: SPOILER — DELAMINATED (LT WING) · airframe 60,115 hrs · 49,117 cycles

LT WING SPOILER DELAMINATED. R &R NR 2 SPOILER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 59,915 hrs · 48,967 cycles

FWD CABIN CEILING EMERGENCY EXIT LIGHT AT ROW 2 MISSING LENS. INSTALLED LENS ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,915 hrs · 48,967 cycles

LT SIDEWALL EMERGENCY EXIT LIGHT BULB INOPERATIVE. R&R LAMP IAW MM.

Part: WIRE HARNESS — FAULTY (COCKPIT) · airframe 59,287 hrs · 48,478 cycles

CAPT SLIDING WINDOW SPARKED AT THE CONNECTOR PLUG. R & R PIG TAIL IAW MM.

Part: TRANSMITTER — FAULTY (COCKPIT) · airframe 58,246 hrs · 47,741 cycles

DIVERT/DECLARED EMERGENCY -- DURING APPROACH WE SELECTED FLAPS 5. FLAPS STOPPED AT LEFT -0, RIGHT -1. LED'S WERE UP AS NORMAL. C/W ASSYMETRICAL FLAP CHECKLIST. LED'S WERE EXTENDED W/ALTERNATE METHOD AND WENT TO FULL EXTEND. APPROACH AND LANDING WERE NORMAL. R & R TRANSMITTER AMM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 58,151 hrs · 47,672 cycles

RT AILERON BAY L-ANGLE CRACKED AT NR 2 HINGE. REMOVED AND REPLACED L-ANGLE PER SRM 51-40-02.

Part: ANGLE — CRACKED (NR 2 AILERON) · airframe 58,151 hrs · 47,672 cycles

LEFT WING VERTICAL ANGLE INBOARD OF NR 2 AILERON HINGE CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-02. REMOVED AND RE-INSTALLED PANEL'S 7103L AND 7218L PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,258 hrs · 47,022 cycles

L1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,258 hrs · 47,022 cycles

R1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY IAW WDM & AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,257 hrs · 47,022 cycles

STRINGER CLIP CRACKED AT BS 867, STR 1. REMOVED & REPLACED CLIP IAW SRM & BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

STRINGER CLIP CRACKED AT BS 480, STR 8L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 WINDOW FORGING UPPER FORWARD CORNER CRACKED. REMOVED AND REPLACED SKIN IAW BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807 +10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787 +10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500A +10 UPPER FORWARD WINDOW CORNER CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767 +10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED BS 500C +10 UPPER FORWARD WINDOW CORNER CTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500 +10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360 +10 LOWER AFT WINDOW CORNER CUTOUT. EPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460 +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C +10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 47,022 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: COVER — MISSING (CABIN) · airframe 56,702 hrs · 46,595 cycles

AFT CENTER EEPLS COVER MISSING. INSTALLED COVER IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: FITTING — CORRODED (L1 DOOR) · airframe 56,702 hrs · 46,595 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING ASSY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

R1 DOOR EXTERNAL SKIN CRACKED AT LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW EO AND EA.

Part: FITTING — CORRODED (R1 DOOR) · airframe 56,702 hrs · 46,595 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTING ASSY IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 671, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

SKIN CRACKED AT BS 520+2, STR 28L. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

FRAME CORROED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

FRAME CORRODED AT BS 500D, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

SHEAR TIE CORRODED AT BS 500 BETWEEN, STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

TIE CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

FRAME CORRODED AT BS 727D, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,702 hrs · 46,595 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,702 hrs · 46,595 cycles

RIGHT WING INBOARD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 56,644 hrs · 46,552 cycles

R1 DOOR ESCAPE SLIDE HAS EXCESSIVE GIRT OUT OF CASE. RE-INSTALLED SLIDE PER M/M.

Part: COFFEEMAKER — DEFECTIVE (CABIN) · airframe 56,209 hrs · 46,208 cycles

F/A REPORTS BURNING SMELL AFT CABIN. TURNED GALLEY POWER OFF, ODOR WENT AWAY. FOUND NR 1, COFFEEMAKER HOT PLATE WIRES MELTED. REMOVED AND REPLACED NR 1 COFFEEMAKER PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 55,715 hrs · 45,837 cycles

R1 DOOR, EMERGENCY EXIT LENS COVER BROKEN. REMOVED & REPLACED LENS ASSY PER MM.

Part: PCU — LEAKING (LT MLG WW) · airframe 55,749 hrs · 45,863 cycles

AIR TURNBACK - A-SYSTEM QUANTITY DROPPED TO 1/4 INFLIGHT. FOUND HYDRAULIC LEAK IN NR 1 WHEEL WELL. REMOVED AND REPLACED "A" SYSTEM AILERON PCU IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,911 hrs · 45,207 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727D+12, STR 4R. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 54,853 hrs · 45,164 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 22. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,853 hrs · 45,164 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 23. RELAMPED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 54,147 hrs · 44,614 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: CSD — FAULTY (NR 1 ENGINE) · airframe 53,946 hrs · 44,460 cycles

AIR TURNBACK - NR 1 BUS FALLS OFF THE LINE WHEN POWER IS ADVANCED BEYOND MID RANGE. NR 1 BUS FALLS OFF WITH APU RUNNING. REMOVED AND REPLACED NR 1 ENGINE CSD AND A/C GENERATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,898 hrs · 44,422 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 360+10, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,898 hrs · 44,422 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 360+9, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,898 hrs · 44,422 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 360+12, STR 4R. REPAIRED SKIN IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 53,710 hrs · 44,275 cycles

L1 DOOR LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,154 hrs · 43,845 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK CRACKED AT BS 644, FWD OF AILERON BODY QUADRANT SHAFT. REPAIRED DECK PER SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 53,151 hrs · 43,844 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT EMERGENCY EXIT SIGN LIGHT LENS LOOSE AT ROW 23. SECURED LENS PER MM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 51,940 hrs · 42,940 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER MM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BRACKET CORRODED AT BS 344, LBL 62. REMOVED AND REPLACED BRACKET PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR FWD CUTOUT FRAME CRACKED AT BS 947, WL 254. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, BETWEEN LBL 10 TO RBL 2. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN RBL 17 TO RBL 20. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED CLIP PER EA.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BRACKET CORRODED AT BS 312, LBL 57. REMOVED AND REPLACED BRACKET PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26R. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: WEB — CRACKED (NLG WW) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL LT WEB BELOW UPPER PRESSURE DECK CRACKED AT BS 259. REPAIRED WEB PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 26R. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, RBL 20. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN BL 0 TO RBL 7. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 13. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 13. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 807 TO BS 827, LBL 65. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, LBL 65. REPAIRED FRAME PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ANGLE CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRAP — CRACKED (BS 949 S11L) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRAP CRACKED AT BS 949, STR 11L. R & R STRAP IAW SRM AND MANUFACTURER DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER WEB OF L2 DOOR CUTOUT CRACKED AT BS 949, WL 253. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND LOWER SILL WEB CORRODED AT BS 300, RBL 57. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, RBL 67. REPAIRED WEB PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 294.5, RBL 60. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 51,595 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. R & R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 51,595 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S27L/R) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747, RBL 65. REPAIRED WEB PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ATTACHMENT ANGLE CRACKED AT BS 639, RBL 45. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND PRESSURE DECK FLOOR CRACKED AT BS 540, LBL 0. REMOVED AND REPLACED DECK PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 51,695 hrs · 42,736 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STA 2 TO STA 3. REPAIRED CHORD PER ACO.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,431 hrs · 42,529 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 51,431 hrs · 42,529 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER T/E CRACKED. REPAIRED SLAT PER SRM.

Part: WEB — CRACKED (NLG) · airframe 50,583 hrs · 41,887 cycles

DURING SCHEDULED OTS, FOUND RT NLG W/W WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,474 hrs · 41,808 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT BELOW SIGN INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,183 hrs · 41,587 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 50,132 hrs · 41,548 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,044 hrs · 41,488 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — CORRODED (LT WING) · airframe 49,833 hrs · 41,334 cycles

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

Part: CASTING — CRACKED (SPOILER) · airframe 48,221 hrs · 40,117 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING INBOARD GROUND SPOILER ACTUATOR CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM.

Part: LENS — MISSING (CABIN) · airframe 47,932 hrs · 39,907 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,932 hrs · 39,907 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 47,861 hrs · 39,855 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: LATCH — DEFECTIVE (R1 DOOR) · airframe 47,646 hrs · 39,694 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ENCLOSURE. REMOVED AND REPLACED LATCH PER MM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 47,367 hrs · 39,495 cycles

LEFT EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 430, BL 0. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY AISLE LIGHT INOP AT ROW 13. REPLACED LAMP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRNGER CLIP CRACKED AT BS 827, STR 6. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING SLAT I/B UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,403 hrs · 38,819 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 44,869 hrs · 37,689 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,220 hrs · 17,197 cycles

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

Part: SKIN — DEBONDED (TE FOREFLAP) · airframe 43,345 hrs · 36,530 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP INBOARD T/E DISBONDED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,345 hrs · 36,530 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — FAULTY (OIL TEMP) · airframe 42,183 hrs · 35,614 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH OIL TEMP INDICATION. REMOVED AND REPLACED OIL TEMP BULB AND INDICATOR PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 41,654 hrs · 35,187 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 L/E SLAT INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 41,654 hrs · 35,187 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLAP — CRACKED (RT WING) · airframe 41,654 hrs · 35,186 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP CRACKED. REPAIRED FLAP PER SRM.

Part: LINE — RUPTURED (HYDRAULIC SYS) · airframe 40,963 hrs · 34,661 cycles

DECLARED EMERGENCY, LOSS OF HYDRAULIC B-SYSTEM ON APPROACH. REMOVED AND REPLACED B-SYSTEM MODULE LINE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,479 hrs · 34,296 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD RIGHT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,658 hrs · 33,679 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: O-RING — BURNED (COCKPIT) · airframe 39,625 hrs · 33,656 cycles

AIR TURNBACK, PASSING FL 200 CAPTAINS L1 WINDOW UPPER LT CORNER CAUGHT FIRE. TURNED OFF WINDOW HEAT SWITCH FIRE EXTINGUISHED. REMOVED AND REPLACED L1 WINDOW O-RINGS IAW MM.

Part: FIRE DETECTOR — FAULTY (APU) · airframe 38,372 hrs · 32,699 cycles

APU FIRE WARNING LIGHT ILLUMINATED AND WARNING HORN SOUNDED DURING FLIGHT, PULLED FIRE HANDLE AND DISCHARGED FIRE BOTTLE. LIGHT EXTINGUISHED AND CIRCUIT CHECKED GOOD. REMOVED AND REPLACED APU FWD TAILPIPE FIRE DETECTOR AND HARNESS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,063 hrs · 32,458 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 37,272 hrs · 31,844 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 37,272 hrs · 31,844 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERWING UPPER EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: WIRE HARNESS — FAULTY (APU BAY) · airframe 36,571 hrs · 31,307 cycles

DECLARED EMERGENCY. APU FIRE HANDLE LIGHT ILLUMINATED & FIRE WARNING BELL SOUNDED. APU FIRE EXTINGUISHER BOTTLE DISCHARGED. REMOVED AND REPLACED APU TAILPIPE FIRE LOOP HARNESS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 36,241 hrs · 31,049 cycles

DURING SCHEDULED C1 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,444 hrs · 29,564 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 33,502 hrs · 28,839 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED BOTH HINGE BOX FITTINGS PER MM & SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 54, CRACKED. REPAIRED FLOORBEAM SECTION PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN RBL 47 TO LBL 47, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 379, EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER ER.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB REAR SPAR BODY RT AND LT DRAG BRACES CORRODED. REMOVED AND REPLACED DRAG BRACES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND CAPTAINS NR 1 C-D WINDOW POST UPPER CORNER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 727D TO RIGHT BS 727E, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB RT T/E BEAM AT STATION 79, CRACKED. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 827, BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 8R AND STRINGER 8L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CORRODED AT RT BS 727C TO 727D AND LT BS 847 TO BS 867. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS AT BS 400, LT AND BS 344 RT, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 991, BETWEEN LBL 37 AND LBL 41, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN LBL 18 TO RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 33,157 hrs · 28,579 cycles

FWD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY SIGN PER MM.

Part: FRAME — CRACKED (BS 400) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500D, LBL 16 TO LBL 21, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1006, LBL 4 TO RBL 4, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD AND AFT FLOOR ATTACH FITTINGS CORRODED. REMOVED AND REPLACED FWD ENTRY DOOR GIRT BAR FITTINGS PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, FROM LBL 4 TO LBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,154 hrs · 28,577 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 33,095 hrs · 28,533 cycles

RT FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,700 hrs · 28,199 cycles

DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,887 hrs · 27,539 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 30,965 hrs · 26,767 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 30,933 hrs · 26,742 cycles

DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 30,912 hrs · 26,723 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 28,243 hrs · 24,576 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 26,800 hrs · 23,424 cycles

AIR TURNBACK, DURING CRUISE, NR 2 ENGINE HYDRAULIC PUMP LOW PRESS LIGHT ILLUMINATED, QUANTITY DECREASED TO 1/4. REMOVED AND REPLACED B-SYSTEM HYDRAULIC LINE AT ACOUSTIC FILTER TO PRESS MODULE PER MM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 24,850 hrs · 21,852 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 4 HINGE. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 24,557 hrs · 21,610 cycles

DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM..

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,497 hrs · 20,728 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORD ANGLES CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD ANGLES PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 23,497 hrs · 20,728 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, LBL 5 AND RBL 5. REPAIRED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,169 hrs · 19,608 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: INDICATOR — OVERHEATED (COCKPIT) · airframe 21,560 hrs · 19,080 cycles

DURING DESCENT DETECTED ELECTRIAL BURNING SMELL IN COCKPIT. R&R CAPT HORIZ SIT IND PER MM.

Part: LENS — MISSING (CABIN) · airframe 20,910 hrs · 18,520 cycles

DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT LIGHT SIDEWALL LENS MISSING. INSTALLED LENS PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FAME CRACKED ON AFT LOWER GUSSET. REPAIRED FRAME PER BOEING DRAWING.

Part: BRACKET — CORRODED (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: SLIDE — OUT OF ADJUST (DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: LIGHT — LOOSE (ROW 10)

DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS LOOSE AT ROW 10. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LIGHTING LOOSE. SECURED LIGHTING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EEPLS BATTERY PACK INOP, RT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMER EXIT)

DURING SCHEDULED C2 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT LENS PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE FELL OUT. REPACKED SLIDE ASSY PER MM.

Part: PUMP — LEAKING (NR 1 ENGINE)

AIR TURNBACK DUE TO LOSS OF SYSTEM 'A' HYD FLUID AT CRUISE, 25 MIN AFTER TAKEOFF. REPLACED 'A' SYSTEM HYD PUMP AND CASE DRAIN FILTER PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND FLOOR EMERGENCY TRACK LIGHTING IS COMING UP. REWIRED EMERGENCY TRACK LIGHTS PER BOEING MM.