N742SW

Part: TRAY — BENT (CABIN) · airframe 72,104 hrs · 42,964 cycles

PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY TRAY BENT AT BS. 322, RBL 7. / R&R BATTERY IAW AMM.

Part: PLATE — CRACKED (L/H WING) · airframe 72,104 hrs · 42,964 cycles

L/H WING TRAILING EDGE AFT OF PYLON SAIL TAIL WIGGLE PLATE LOOSE/CRACKED. / R&R WIGGLE PLATE IAW SRM.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO FLOOR SUPPORT RAIL REPAIR CORRODED AT BS. 767+6, LBL 8, ON INSIDE OF ANGLE. / REPAIRED FLOOR SUPPORT RAIL IAW EA.

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO STRINGER CLIP CORRODED AT BS. 847, STR. 27L, ON INBOARD FLANGE. / R&R STRINGER CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO FLOOR SUPPORT RAIL REPAIR CORRODED AT BS. 767+6, LBL 12.5 ON INSIDE OF ANGLE. / R&R ANGLE IAW SRM AND EA.

Part: ANGLE — CORRODED (BS 767) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO FLOOR SUPPORT RAIL REPAIR CORRODED AT BS. 767+6, LBL 3, ON INSIDE OF ANGLE. / R&R FLOOR SUPPORT RAIL INSIDE ANGLE (CHANNEL) IAW SRM AND EA.

Part: ATTACH ANGLE — CRACKED (BS 827) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO ATTACH ANGLE CRACKED AT BS. 827, RBL 19, IN UPPER RADIUS, COMMON TO FRAME AND LOWER DOOR SILL LATERAL WEB. / R&R ANGLE IAW SRM AND DWG. / R&R ATTACH ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (BS 767) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO LONGITUDINAL DOOR SILL WEB CORRODED BETWEEN BS. 767+3 TO BS. 767+8, RBL 19, ON UPPER AND LOWER SURFACE OF FREE FLANGE. / R&R WEB IAW SRM AND DWG.

Part: HINGE ARM — CRACKED (R1 DOOR) · airframe 72,104 hrs · 42,964 cycles

R1 DOOR LOWER HINGE CRACKED. / R&R HINGE ARM IAW AMM.

Part: FITTING — CRACKED (BULKHEAD SUPPORT) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO JUST AFT OF AFT BULKHEAD SUPPORT ANGLE FITTING CRACKED AT BS. 947+1, LBL 10.1, COMMON TO LOWER LONGITUDINAL BULKHEAD SUPPORT ANGLE. / R&R FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS. 727D+5, LBL 3, ON LOWER SURFACE AROUND NUT PLATES. / REPAIRED RAIL IAW EA & SRM.

Part: ANGLE — CORRODED (BS 767) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO FLOOR SUPPORT RAIL REPAIR CORRODED AT BS. 767+6, RBL 8, ON INSIDE ANGLE. / R&R FLOOR SUPPORT RAIL INSIDE ANGLE (CHANNEL) IAW SRM AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 72,104 hrs · 42,964 cycles

AFT CARGO Z-ANGLE CORRODED ON UPPER AND LOWER SURFACE BETWEEN BS. 747+15 TO BS. 847, LBL 21. / R&R L/H Z ANGLE FROM IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 72,104 hrs · 42,964 cycles

R/H HORIZONTAL STABILIZER STAB. STA. 120.3 RIB CRACKED AT VERTICAL STIFFENER, 3RD FROM THE FORWARD SIDE. / REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,104 hrs · 42,964 cycles

R/H HORIZONTAL STABILIZER STAB. STA. 120.3 RIB CRACKED AT VERTICAL STIFFENER. 4TH FROM THE FORWARD SIDE. / REPAIRED RIB IAW SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 71,623 hrs · 42,662 cycles

OVERWING OVERHEAD EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REINSTALLED LENS COVER PER SIP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 71,127 hrs · 42,350 cycles

OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. RELAMPED SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 71,127 hrs · 42,350 cycles

OVERWING CEILING EMERGENCY EXIT SIGN LIGHTS INOP. RELAMPED SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 71,127 hrs · 42,350 cycles

R1 DOOR EMERGENCY EXIT SIGN LIGHTS INOP. RELAMPED SIGN PER MM.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 70,666 hrs · 42,054 cycles

EMERGENCY LIGHT BUTTON COVER DAMAGED AT AFT ATTENDANT PANEL. / R&R EMERGENCY LIGHT BUTTON PER AMM.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 69,152 hrs · 41,103 cycles

R1 DOOR EVAC SLIDE HAD OBJECT STICKING OUT FROM UNDER COVER. R&R SLIDE PER MT.

Part: SWITCH — FAULTY (CABIN) · airframe 68,444 hrs · 40,649 cycles

RT OVERWING EMERGENCY EXIT LIGHT FAULTY. R&R SWITCH PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 68,088 hrs · 40,411 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 67,686 hrs · 40,156 cycles

RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. R&R AFT FLAP PER AMM.

Part: TIRE — FAILED (NR 2 WHEEL) · airframe 67,091 hrs · 39,789 cycles

AIR TURNBACK AND DECLARED AN EMERGENCY, THE NR 2 TIRE BURST ON TAKE-OFF. LOSS OF A SYSTEM PRESSURE AND QUANTITY. ANTI SKID LIGHT ON, SWITCHED OFF. A ELECTRIC LOW PRESSURE NEVER ILLUMINATED. R & R THE NR 2 MAIN WHEEL WELL ASSEMBLY IAW AMM.

Part: TIRE — FAILED (LT MLG) · airframe 67,091 hrs · 39,789 cycles

AIR TURNBACK AND DECLARED AN EMERGENCY, THE NR 2 TIRE BURST ON TAKE-OFF. LOSS OF A SYSTEM PRESSURE AND QUANTITY. ANTI-SKID LIGHT ON, SWITCHED OFF. THE ELECTRIC LOW PRESSURE NEVER ILLUMINATED. R & R THE NR 1 MAIN WHEEL WELL ASSEMBLY IAW AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 66,781 hrs · 39,590 cycles

LT MAN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 66,781 hrs · 39,590 cycles

RT MAN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 66,781 hrs · 39,590 cycles

RT MAN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 66,781 hrs · 39,590 cycles

LT MAN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,577 hrs · 39,465 cycles

BATTERY PACK M1669 FAILED AN EMERGENCY LIGHT CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,577 hrs · 39,465 cycles

BATTERY PACK M1672 FAILED EMERGENCY LIGHT CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,259 hrs · 39,266 cycles

RT OVERWING EXT EMERGENCY LIGHT INOP. SECURED LOOSE LIGHT CONNECTION PER SIP.

Part: BATTERY PACK — DISCONNECTED (CABIN) · airframe 65,675 hrs · 38,910 cycles

R1 DOOR EGRESS LIGHT INOP. RECONNECTED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCONNECTED (CABIN) · airframe 65,675 hrs · 38,910 cycles

RT EMERGENCY EXIT STOWBIN LIGHTS INOP BETWEEN ROW 3 TO ROW 6. RECONNECTED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCONNECTED (CABIN) · airframe 65,675 hrs · 38,910 cycles

G1 GALLEY EMERGENCY EXIT LIGHT INOP. RECONNECTED BATTERY PACK PER AMM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

FORWARD CARGO INTERCOSTAL BAFFLE CRACKED BETWEEN BS 440 TO BS 460, STR 26L. R&R BAFFLE ASSEMBLY IAW DWG & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 65,675 hrs · 38,910 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 86.66 ALONG RADIUS AT LOWER AFT SIDE. R&R RIB IAW SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

AFT E&E BAY BILGE AREA L ANGLE BRACKET CORRODED AT BS 351, LBL 8. R&R SPLICE IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

R1 DOOR UPPER STUB FRAME CRACKED AT BS 295.5, STR 9R. REPAIRED STUB FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

R1 DOOR LOWER STUB FRAME CUTOUT ANGLE CRACKED AT BS 294.5, STR 17R. R&R ANGLE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

R1 DOOR INTERNAL DOUBLER CRACKED BETWEEN BS 291.5 TO BS 294.5, STR 9R. REPAIRED SKIN IAW EA.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 65,675 hrs · 38,910 cycles

UPPER FUSELAGE VERTICAL STABILIZER FIN PANEL 322B BOTTOM DELAMINATED. REPAIRED PANEL IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 727B+12 TO BS 727D+16, LBL 45.5. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 597) · airframe 65,675 hrs · 38,910 cycles

SEAT TRACK CORRODED AT BS 597+18, RBL 45. R & R THE SEAT TRACK IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 15. REPAIRED ANGLE IAW EA.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 65,675 hrs · 38,910 cycles

VERTICAL STIFFENER CRACKED AT BS 663, LBL 25. R & R THE STIFFENER IAW DWG & SRM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 65,675 hrs · 38,910 cycles

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

Part: STRIP — MISSING (R2 DOOR) · airframe 65,675 hrs · 38,910 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE COVER MISSING AFT SECTION OF BUMP STRIP. INSTALLED BUMP STRIP IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 65,675 hrs · 38,910 cycles

INTERCOSTAL AFT ATTACH CLIP CRACKED AT BS 500B, STR 26L. R&R CLIP IAW DWG AND SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 65,675 hrs · 38,910 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, LBL 33.5. REPAIRED WEB IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 665-672) · airframe 65,675 hrs · 38,910 cycles

PRESSURE BULKHEAD WEB CRACKED BETWEEN BS 665 TO 672, RBL 41. REPAIRED THE BULKHEAD WEB IAW EA.

Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 65,675 hrs · 38,910 cycles

LT OVERWING EMERGENCY EXIT HATCH LIFT HANDLE STRAP FRAYED. R&R STRAP IAW SOPM.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,675 hrs · 38,910 cycles

RT WING NR 8 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR FITTING. REPAIRED SKIN IAW SRM.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 65,675 hrs · 38,910 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP LATCH CORRODED. R&R PASS STRAP IAW AMM.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 65,675 hrs · 38,910 cycles

RT EMERGENCY EXIT HATCH ESCAPE STRAP CORRODED. R&R STRAP IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,675 hrs · 38,910 cycles

LT WING NR 1 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR FITTING. REPAIRED SKIN IAW SRM.

Part: HOUSING — LOOSE (CABIN) · airframe 65,675 hrs · 38,910 cycles

LT STOWBIN BULLNOSE EMERGENCY EXIT LIGHT HOUSING LOOSE BETWEEN ROW 4 TO ROW 5. SECURED LIGHT IAW SOPM.

Part: STRAP — DISCONNECTED (FLASHLIGHT) · airframe 65,081 hrs · 38,540 cycles

AFT INBOARD EMERGENCY FLASHLIGHT PLASTIC STRAP DISCONNECTED. R&R STRAP PER AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,630 hrs · 38,247 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,630 hrs · 38,247 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY CHARGER PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,630 hrs · 38,247 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LIGHT COVER MISSING. INSTALLED THE LENS IAW AMM.

Part: WINDOW — ARCED (L1) · airframe 64,173 hrs · 37,976 cycles

L1 WINDOW OUTER PAN ARCED IN UPPER LEFT CORNER. ACFT DIVERTED. R & R THE L1 WINDOW IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,736 hrs · 37,122 cycles

AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED LONG TEST. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,736 hrs · 37,122 cycles

FORWARD LT EMERGENCY LIGHTING BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

FORWARD CARGO BILGE FLOOR CHANNEL CORRODED, BETWEEN BS 500A - 515. R & R CHANNEL IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

L1 DOOR INNER CHORD CORRODED, BETWEEN BS 294 - 344. REPAIRED CHORD IAW EA.

Part: CHANNEL — CORRODED (L1 DOOR) · airframe 59,838 hrs · 35,427 cycles

L1 DOOR Z CHANNEL CORRODED. R & R CHANNEL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 46. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

FLOORBEAM UPPER CHORD, REPAIR DAMAGED DUE TO INTERFERENCE WITH INTERCOSTAL WITH GALLEY & LAVATORY SUPPORT HARD POINT FITTINGS, AT BS 986, BETWEEN RBL 45.5 - 24.75. REPAIRED CHORD IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: MOUNT — CORRODED (CABIN) · airframe 59,838 hrs · 35,427 cycles

L1 DOOR SLIDE GIRT BAR FWD FLOOR MOUNT CORRODED. R & R MOUNT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 59,838 hrs · 35,427 cycles

MAIN LANDING GEAR WW PRESS WEB CRACKED AT STATION 663, RBL 28. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 32. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

R1 DOOR CHORD ATTACH ANGLE CORRODED. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 46. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

INTERCOSTAL CRACKED, BETWEEN BS 294 - 312, RBL 16. R & R INTERCOSTAL IAW DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 24.75. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,838 hrs · 35,427 cycles

SUB FRAME CORRODED, BETWEEN BS 967 - 986, RBL 18.25. R & R SUB FRAME IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FLOORBEAM SUPPORT BRACKET CRACKED AT BS 727B, RBL 45. R & R BRACKET IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

LEFT SEAT TRACK CORRODED BETWEEN BS 639+16 TO 639+20, LBL 46. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

RIGHT SEAT TRACK CORRODED IN BOTTOM OF CTR CHANNEL AROUND TWO FASTENERS AT BS 727E, RBL 46. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

SEAT TRACK CORRODED BETWEEN BS 727A TO 727A+3, LBL 46. REPAIRED SEAT TRACK IAW SRM.

Part: FLAP — CRACKED (LT WING) · airframe 58,557 hrs · 34,664 cycles

LEFT WING NR 1 KRUEGER FLAP CRACKED AT RIB FLANGE, 26" FROM OTBD EDGE OF FLAP & 2.5" FROM FLAP TE. REPAIRED FLANGE IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

STRINGER CLIP CRACKED AT BS 480, STRINGER 9L. R & R CLIP IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 58,557 hrs · 34,664 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, LOWER FWD STIFFENER. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

RIGHT SIDE FWD UPPER CLIP WEB FITTING FLANGE CRACKED AT STRINGER 18A. R & R FITTING IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 58,557 hrs · 34,664 cycles

RIGHT NR 3 WINDOW FRAME CRACKED AT 3RD FROM LOWEST FASTENER HOLE ALONG THE E - F POST. R & R FRAME IAW SRM & DWG.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 56,789 hrs · 33,671 cycles

LEFT WING UPPER TE SHELF PANEL OTBD OF NR 6 GND SPOILER, OTBD ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,614 hrs · 32,981 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 55,183 hrs · 32,736 cycles

R2 DOOR EMER EXIT SIGN COVER LOOSE. R & R LIGHT BASE ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,424 hrs · 31,708 cycles

LT WING NR 2 SLAT LOWER SURFACE SKIN CRACKED AT ACTUATOR ATTACH POINT RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,424 hrs · 31,708 cycles

FUSELAGE SKIN CRACKED AT STATION 540, STRINGER 22L. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,424 hrs · 31,708 cycles

FUSELAGE SKIN CRACKED AT STATION 540, STRINGER 22R. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,381 hrs · 31,073 cycles

FRAME CRACKED AT STATION 727B STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,381 hrs · 31,073 cycles

LT WING OTBD AFT FLAP INBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM & MM.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 50,247 hrs · 29,813 cycles

ELECTRICAL FAILURE ON ARRIVAL NR 2. REMOVED AND REPLACED NR 2 ENGINE IDG PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,952 hrs · 29,626 cycles

1 EACH BATTERY PACK POSITION M01675 FAILED CAPACITY CHECK. REMOVED AND REPLACED 1 EACH BATTERY PACK POSITION M01675 PER SSM-M/M.

Part: COVER — DETACHED (CABIN) · airframe 49,879 hrs · 29,582 cycles

FWD SERVICE DOOR EMERGENCY EXIT LENS IS DETACHED FROM LIGHTED PANEL. RE-INSTALLED LENS COVER, ALL CHECKS OK PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 49,449 hrs · 29,323 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,940 hrs · 28,979 cycles

CAPTAINS L1 WINDOW POST FRAME CRACKED. REMOVED AND REPLACED FRAME IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,940 hrs · 28,979 cycles

PRESSURE BULKHEAD CRACKED AT BS 663, LBL 42. REPAIRED BULKHEAD IAW ER.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,940 hrs · 28,979 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: RING ASSEMBLY — WORN (THRUST REVERSER)

REF: CMM 78-31-37, 01MAR2012, REV 023 INSPECTION FINDING OF (2) MISSING BACB30LE6K29 BOLTS (FIGURE 12, ITEM 100) NOTES THE FOLLOWING RELATED DISCREPANCIES. A) FIGURE 12, ITEM 115 AREA OF MATERIAL WEAR MEASURING .9240 LONG X .2125 WIDE X .0465 DEEP ON THE 315A2222-5 CASCADE RING ASSY LOWER OTBD SURFACE. B) FIGURE 12, ITEM 115 AREAS OF MATERIAL WEAR / GOUGING MEASURING .677 X .650 X .030 DEEP WITHIN THE 315A2222-5 RING ASSY OTBD RADIUS. C) THE (2) .375/.379 HOLE LOCATIONS FOR BACB30LE6K29 BOLTS (FIGURE 12, ITEM 100) C/T THE 315A2222-5 CASCADE RING ASSY ARE ELONGATED AS FOLLOWS: AFT MOST = .4101 X .3919 FWD MOST = .4234 X .3905 D) CORRESPONDING .375 / .379 HOLE LOCATION FOR THE FWD MOST BACB30LE6K29 BOLT C/T THE 315A2402-1 LATCH BEAM FITTING (FIG 21, ITEM 305) IS ELONGATED MEASURING .4021 X .3990. THERE IS ALSO AN .790 DIA X .008 TO .009 DEEP AREA OF WEAR (RESEMBLING A COUNTERBORE) AROUND THE FWD HOLE LOCATION C/T THE -5 BEAM INBD SURFACE. E) CORRESPONDING .4040 / .4160 HOLE LOCATION FOR THE AFT MOST BACB30LE6K29 BOLT C/T THE 315A2402-1 LATCH BEAM FITTING (FIG 21, ITEM 305) IS ELONGATED MEASURING .4155 X .4270. THERE IS ALSO AN .760 DIA X .0065 TO .0175 DEEP AREA OF WEAR (RESEMBLING A COUNTERBORE) AROUND THE FWD HOLE LOCATION C/T THE -5 BEAM INBD SURFACE.

Part: LIGHT — BROKEN (CABIN) · airframe 48,225 hrs · 28,555 cycles

FWD GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 47,971 hrs · 28,394 cycles

L1 DOOR SLIDE DROPPING FROM CASE. RE-INSTALLED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,746 hrs · 27,658 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN BULB INOP. RELAMPED PER MM.

Part: GAUGE — OUT OF POSITION (EVAC SLIDE) · airframe 41,743 hrs · 24,668 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF POSITION. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,701 hrs · 24,634 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 41,514 hrs · 24,513 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B AFT FLAP I/B END UPPER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 41,497 hrs · 24,502 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SENSOR — FAULTY (TE FLAP) · airframe 40,539 hrs · 23,924 cycles

DIVERSION - ON APPROACH TO MDW TRIED TO EXTEND FLAPS, FOR LANDING INDICATOR SHOWED SPLIT FLAPS AND WOULD NOT MOVE, RT STUCK AT 0 AND LT INDICATOR BETWEEN 1 AND 0. LANDED USING ALT FLAP METHOD. REMOVED AND REPLACED NR 4 FLAP SKEW SENSOR PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,531 hrs · 23,918 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 711 TO BS 715. REPAIRED BEAM PER ER.

Part: CONNECTOR — LOOSE (CABIN) · airframe 40,531 hrs · 23,918 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT CONNECTOR LOOSE. REMOVED AND REPLACED CONNECTOR PER WDM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,531 hrs · 23,918 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,531 hrs · 23,918 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 351.2, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME PER SRM.

Part: LENS — MISSING (CABIN) · airframe 39,526 hrs · 23,270 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,122 hrs · 23,017 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 39,073 hrs · 22,990 cycles

L2 COCKPIT WINDOW ARCED ON DESCENT AT 14,000FT. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,524 hrs · 22,663 cycles

DURING SCHEDULED CV CHECK, FOUND L/H BALLAST EMERGENCY EXIT LIGHT INOP BETWEEN ROW 5 TO ROW 10. R&R LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 37,590 hrs · 22,119 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 35,394 hrs · 20,788 cycles

R2 DOOR EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 34,739 hrs · 20,113 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 30,008 hrs · 17,530 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 43 TO RBL 40. REPAIRED FLOORBEAM PER SWA EA.

Part: TRANSMITTER — FAULTY (RT WING FLAP) · airframe 25,780 hrs · 15,075 cycles

DIVERSION / DECLARED EMERGENCY. T/E FLAPS WOULD NOT EXTEND PAST POSITION 1. REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,738 hrs · 15,054 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,365 hrs · 14,851 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 25,051 hrs · 14,696 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 24,128 hrs · 14,146 cycles

LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: ACTUATOR — FAULTY (MLG WW) · airframe 23,894 hrs · 14,019 cycles

AIR TURNBACK/DECLARED EMERGENCY. AILERONS FEEL UNRESPONSIVE WITH A NOTICEABLE DEAD BAND. REMOVED AND REPLACED AILERON TRIM ACTUATOR PER MM.

Part: ECU — FAULTY (NR 1 ENGINE) · airframe 22,981 hrs · 13,507 cycles

AIR TURNBACK, DECLARED EMERGENCY. DURING TAKEOFF ROLL, NR 1 ENGINE POWER, ALL PARAMETERS BECAME ERRATIC. THROUGH CLIMBOUT, ALL PARAMETERS FLUCTUATING, AROUND 10,000 FT, 2 LOUD COMPRESSOR STALLS. REMOVED AND REPLACED NR 1 EEC AND NR 1 VBV PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,936 hrs · 13,482 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,030 hrs · 12,949 cycles

DURING SCHEDULED MV1 CHECK, AFT INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHTS BATTERY PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 21,929 hrs · 12,886 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,890 hrs · 12,289 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,875 hrs · 11,710 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN AT BS 500 + 8, FWD AIRPHONE ANTENNA, CRACKED. REPAIRED FUSELAGE SKIN PER SRM.

Part: LINE — LOOSE (A-HYD SYS) · airframe 19,628 hrs · 11,571 cycles

AIR TURNBACK, A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. RETORQUED A-SYSTEM HYDRAULIC RESERVOIR RETURN LINE PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 18,618 hrs · 11,032 cycles

DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, FROM LT TO RT TRANS ANGLES. REPAIRED FLOORBEAM PER EA.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 17,477 hrs · 10,414 cycles

EEPLS WIRES EXPOSED AT ROW NR 8. SECURED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,178 hrs · 9,727 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN CABIN. REMOVED AND REPLACED EEPLS RECEPTICAL PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 15,624 hrs · 9,416 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,624 hrs · 9,416 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (9 EA) IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 15,624 hrs · 9,416 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TAB — VIBRATION (BOTH ELEVATORS) · airframe 13,101 hrs · 7,976 cycles

LOW FREQUENCY AIRFRAME VIBRATION OCCURRED FOR ABOUT 2 MINUTES IN-FLIGHT. ACCOMPLISHED POST LCO (LIMIT CYCLE OSCILLATION) INSPECTION, REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 12,740 hrs · 7,758 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 9,960 hrs · 6,127 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 9,557 hrs · 5,866 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 7,766 hrs · 4,825 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROWS 1, 11, 14 & 19. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: LINE — DISCONNECTED (NR 2 ENGINE) · airframe 7,625 hrs · 4,743 cycles

IN FLIGHT ENGINE SHUTDOWN, NR 2 ENG ROLLED BACK AT FL390. DESCENDED TO FL240 & ENG RESTARTED WITH APU ASSIST. ON LANDING NR 2 ENG ENGINE CONTROL LIGHT ILLUMINATED. EEC BITE FAULTS PS3 LINE. FOUND PS3 LINE DISCONNECTED AT B- NUT, FAN CASE 6 O''''CLOCK POSITION. SECURED LINE PER MM. RAN ENG, OPS CHECK NORMAL PER MM.

Part: GIRT — OUT OF POSITION (EMER EXIT)

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

Part: SLIDE — DEPLOYED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE DEPLOYED ACCIDENTALLY. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — CRACKED (PAX DOORWAY)

DURING LINE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.