N766SW

Part: LIGHT — DAMAGED (CABIN) · airframe 61,814 hrs · 36,147 cycles

FORWARD LAVATORY EMERGENCY LIGHT ASSEMBLY ON THE AFT WALL FOUND DAMAGED. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: SEAT TRACK — CORRODED (BS 520) · airframe 61,814 hrs · 36,147 cycles

CABIN SEAT TRACK CORRODED BETWEEN BS 520 TO 520 -10, LBL 45. R & R THE SEAT TRACK IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

STRINGER CRACKED AT BS 927, STR 8L. R&R STRINGER IAW DWG.

Part: ANGLE — CORRODED (BS 747) · airframe 61,814 hrs · 36,147 cycles

AFT CARGO BAY ANGLE CORRODED BETWEEN BS 807 TO 747+6, LBL 22. R & R THE ANGLE IAW SRM AND DWG.

Part: GIRT BAR — CORRODED (DOOR) · airframe 61,814 hrs · 36,147 cycles

FORWARD WET AREA GIRT BAR ATTACH Z CORRODED AT BS 344, LBL 61. REPAIRED GIRT BAR IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

AFT WET AREA FLOOR SUPPORT CORRODED AT BS 947+6, RBL 8. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (BS 1016) · airframe 61,814 hrs · 36,147 cycles

AFT WET AREA WEB STRAP CORRODED BETWEEN BS 1016, LBL 3. R & R THE WEB STRAP IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

FORWARD WET AREA INTERCOSTAL CORRODED AT BS 312-5, LBL 12. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

FORWARD CARGO BAY FLOOR Z ANGLE CORRODED BETWEEN BS 500 TO BS 500D, RBL 23. R&R Z ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 951-986) · airframe 61,814 hrs · 36,147 cycles

AFT WET AREA CREASE BEAM FLANGES CORRODED BETWEEN BS 951 TO 986+10, RBL 54. R & R THE CREASE BEAM IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

AFT WET AREA WEB CORRODED AT BS 1016, LBL 34. R&R WEB IAW DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 61,814 hrs · 36,147 cycles

RT WING TRAILING EDGE PANEL CENTER SUPPORT BRACKET CRACKED BETWEEN WSTA 253 AND WSTA 278.50. R&R ANGLE IAW SRM.

Part: WEB — CRACKED (BS 670) · airframe 61,814 hrs · 36,147 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS 670, LBL 35. REPAIRED THE WEB IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

FORWARD CARGO CUTOUT INNER FRAME STRAP CORRODED AT BS 440, RBL 25. R&R STRAP IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 61,814 hrs · 36,147 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 675, RBL 40. REPAIRED WEB IAW EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 61,814 hrs · 36,147 cycles

FORWARD CARGO DOOR CUTOUT FORWAR LOWER THRESHOLD SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW EA.

Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 61,814 hrs · 36,147 cycles

CEILING PANEL OVERWING EMERGENCY EXIT LIGHT MOUNT BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: FITTING — DAMAGED (R2 GIRT BAR) · airframe 61,814 hrs · 36,147 cycles

R2 DOOR SLIDE AFT GIRT BAR FLOOR MOUNT FITTING DAMAGED. R & R THE FITTING IAW AMM.

Part: STRAP — LOOSE (R2 DOOR) · airframe 61,672 hrs · 36,058 cycles

R2 DOOR SAFETY STRAP VELCRO LOOSE. R&R STRAP IAW SIP.

Part: PLATE — LOOSE (R2 DOOR) · airframe 61,651 hrs · 36,046 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR LOOSE. R&R PLATE ASSEMBLY PER SIP.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,878 hrs · 35,570 cycles

L2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,878 hrs · 35,570 cycles

R2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,878 hrs · 35,570 cycles

R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 60,878 hrs · 35,570 cycles

L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,685 hrs · 34,852 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL PER SRM.

Part: BUMPER — MISSING (R1 DOOR) · airframe 58,638 hrs · 34,244 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER AFT BUMPER END CAP MISSING. INSTALLED AFT BUMPER AMM.

Part: HANGER ASSY — LOOSE (R1 DOOR) · airframe 58,638 hrs · 34,244 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER FORWARD GIRT BAR HANGER LOOSE. SECURED HANGER PER AMM.

Part: STRINGER — DAMAGED (BS 500D) · airframe 58,344 hrs · 34,074 cycles

STRINGER 14L DAMAGED AT BS 500D+5. REPAIRED THE STRINGER IAW SRM.

Part: STRINGER — DAMAGED (BS 500D) · airframe 58,344 hrs · 34,074 cycles

STRINGER 15L DAMAGED AT BS 500D+14. REPAIRED THE STRINGER IAW SRM.

Part: RIB — CRACKED (LEFT WING) · airframe 58,370 hrs · 34,089 cycles

LEFT WING RIB CRACKED INBOARD LEADING EDGE FRAME. R & R THE RIB IAW EA.

Part: SKIN — DAMAGED (BS 500D-520) · airframe 58,349 hrs · 34,077 cycles

SKIN DAMAGED BETWEEN BS 500D TO 520, BETWEEN STRINGERS 13 TO 18L. REPAIRED SKIN IAW EA.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 58,349 hrs · 34,077 cycles

L/H HORIZONTAL STABILIZER LEADING EDGE DAMAGED FROM IMPACT. / R&R STABILIZER IAW AMM.

Part: ENGINE — FAILED (NR 1) · airframe 58,349 hrs · 34,077 cycles

NR 1 ENGINE FAILED AT CRUISE FL 390. DIVERTED. R & R NR 1 ENGINE IAW MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,086 hrs · 33,915 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. R & R THE LENS IAW MM.

Part: SHUTOFF VALVE — FAULTY (NR 2 ENGINE) · airframe 57,977 hrs · 33,847 cycles

DECLARED EMERGENCY LOSS OF PRESSURIZATION AT FL300 DESCENDING TO FL270 MADE EMERGENCY DESCENT TO 10,000 FT. CABIN ALTERNATE NEVER EXCEEDED 10,000 FT, ONLY LIGHT WARNING WAS CABIN ALTERNATE. WARNING HORN ALONG WITH CABIN ALTERNATE LIGHT. R & R NR 2 ENGINE PRESSURE REGULATOR SHUTOFF VALVE IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,925 hrs · 33,822 cycles

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 13. REPLACED THE LAMP IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,925 hrs · 33,822 cycles

LEFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 17. REPLACED THE LAMP IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 57,925 hrs · 33,822 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT M1669. R & R THE BATTERY PACK IAW DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,925 hrs · 33,822 cycles

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

Part: FITTING — CRACKED (LE SLAT) · airframe 55,964 hrs · 32,686 cycles

LEFT WING NR 4 SLAT FITTING CRACKED AT STATION 85.74. R & R NR 4 SLAT IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

SUPPORT ANGLE CRACKED AT BS 663.7, LBL 19. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FORWARD FACE SUPPORT ANGLE CRACKED AT BS 663.75, BETWEEN LBL 8 - 31. R & R ANGLE IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 55,964 hrs · 32,686 cycles

LEFT WING NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW EA & SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

MAIN WW COMPARTMENT, STIFFENER CRACKED AT BS 663.75, LBL 16. R & R STIFFENER IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,964 hrs · 32,686 cycles

LEFT WING NR 4 LE SLAT SKIN CRACKED AT STATION 85.74. R & R SLAT IAW MM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

SUPPORT BRACKET CRACKED AT BS 559, RBL 5. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FRAME WEB CRACKED AT BS 907, BETWEEN STRINGER 7R - 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FRAME WEB CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FRAME WEB CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

FRAME WEB CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM OTBD FLANGE, CRACKED AT BS 727B, RBL 45.50, 6 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.50, INBD FLANGE AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.50, OTBD FLANGE 12 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.50, INBD FLANGE 12 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM FITTING CRACKED AT BS 727B, LBL 24.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.75 INBD FLANGE AT 5 & 7 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM FITTING CRACKED AT BS 727B, RBL 45.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM FITTING, CRACKED AT BS 727B, RBL 24.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.50, AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 55,964 hrs · 32,686 cycles

LONGITUDINAL FLOORBEAM AFT SEAT TRACK, INBD FLANGE CRACKED AT BS 727B, LBL 24.50 AT CTR WING BOX. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,964 hrs · 32,686 cycles

LEFT WING LE NR 3 SLAT NOSE SKIN, CRACKED AT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: COVER — UNSECURE (CABIN) · airframe 55,706 hrs · 32,530 cycles

FORWARD ENTRY DOOR EGRESS LIGHT COVER FELL OFF. SECURED COVER IAW SIP.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,498 hrs · 32,395 cycles

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

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,042 hrs · 32,128 cycles

L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,942 hrs · 32,069 cycles

RIGHT AFT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: CONTROL PANEL — FAULTY (FIRE WARNING) · airframe 54,313 hrs · 31,714 cycles

DIVERSION & DECLARED EMER. FWD CARGO FIRE LIGHT CAME ON IN FLIGHT, FLASHED SEVERAL TIMES THEN STEADY. PERFORMED QRH PROCEDURE, INCLUDING BOTTLE DISCHARGE. NO FIRE INDICATION IN CARGO BIN UPON INSPECTION. R & R CARGO FIRE CONTROL PANEL IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 53,501 hrs · 31,241 cycles

L2 DOOR EMER EXIT SIGN LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 51,206 hrs · 29,895 cycles

AFT ENTRY DOOR EMER EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

LT NR 1 WINDOW FRAME ASSEMBLY CRACKED. R & R FRAME ASSEMBLY IAW ACO.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,852 hrs · 29,092 cycles

RT HORIZONTAL STABILIZER RIB INBD 92.70 FWD VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 49,852 hrs · 29,092 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM & EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 49,852 hrs · 29,092 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,852 hrs · 29,092 cycles

RT HORIZONTAL STABILIZER STATION 92.7 VERTICAL STIFFENER CRACKED THIRD FROM FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,852 hrs · 29,092 cycles

RT HORIZONTAL STABILIZER STAB STATION 92.70 SECOND VERTICAL STIFFENER FROM FWD CRACKED. REPAIRED STABILIZER IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,852 hrs · 29,092 cycles

RT HAND HORIZONTAL STABILIZER INBD VERTICAL STIFFENER CRACKED AT 92.70. REPAIRED STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,852 hrs · 29,092 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

LT NR 3 FLIGHT DECK FIXED WINDOW FRAME, FWD SIDE WINDOW PANE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

RT NR 3 FLIGHT DECK FIXED WINDOW FRAME FWD SIDE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,852 hrs · 29,092 cycles

RT NR 3 FLIGHT DECK FIXED WINDOW FRAME, FWD SIDE WINDOW PANE CRACKED. REPAIRED FRAME IAW ACO.

Part: ANGLE — CRACKED (LT WING) · airframe 49,852 hrs · 29,092 cycles

LT WING INBD FIXED TE INTERCOSTAL ANGLE CRACKED ABOVE NR 1 ENG AFT PYLON FAIRING. R & R ANGLE IAW SRM & DRAWING.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,422 hrs · 28,832 cycles

RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,422 hrs · 28,832 cycles

LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 49,088 hrs · 28,639 cycles

DECLARED EMERGENCY DUAL BLEED TRIP FAILURE @ FL 410 RT BLEED TRIP LIGHT ILLUMINATED FOLLOWED BY LT BLEED TRIP LIGHT INITIATED EMERGENCY DESCENT. FOUND BAD PRECOOLER CONTROL VALVE. R & R NR 1 ENGINE PRECOOLER CONTROL VALVE IAW MM.

Part: LENS — MISSING (CABIN) · airframe 47,537 hrs · 27,746 cycles

AFT RIGHT EMERGENCY LIGHT COVER (PLASTIC LENS) MISSING. R & R LIGHT ASSY IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,210 hrs · 27,537 cycles

CAPTAIN'S L1 WINDOW FRAME OTBD POST CRACKED NEAR TOP OF POST. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 47,210 hrs · 27,537 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STABILIZER STA 101.9. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 45,742 hrs · 26,606 cycles

MID-CABIN EMERGENCY EXIT SIGN BROKEN. REPLACED MID CABIN EMERGENCY EXIT SIGN PER MM, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,610 hrs · 26,536 cycles

LEFT FWD EXTERIOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED IAW AMM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,024 hrs · 24,940 cycles

BELT FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,024 hrs · 24,940 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,024 hrs · 24,940 cycles

BELT FRAME CRACKED AT BS STR 8R, BS 360. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,588 hrs · 24,103 cycles

FRAME CRACKED AT STR 8L BS 520. REPAIRED FRAME PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 43,024 hrs · 24,940 cycles

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

Part: WINDOW — CRACKED (COCKPIT) · airframe 42,345 hrs · 24,528 cycles

RT COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED WINDOW IAW MM.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 41,773 hrs · 24,204 cycles

MAIN FUEL TANKS DO NOT FEED PROPERLY; NR 2 (RIGHT) FEEDS SLOWER THAN NR 1 AT A RATE OF ABOUT 300LBS PER 15 MINUTES AT CRUISE, FL 380. REMOVED AND REPLACED CENTER TANK CROSSFEED VALVE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,724 hrs · 23,600 cycles

DURING SCHEDULED HC2 CHECK RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,724 hrs · 23,600 cycles

DURING SCHEDULED HC2 CHECK LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,002 hrs · 22,621 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 37,606 hrs · 21,829 cycles

OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT MID CABIN. SECURED LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,718 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 729B, LBL 2. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,718 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B LEADING EDGE NR 2 SLAT EXTERNAL SKIN CRACKED. REPAIRED NR 2 SLAT PER AAR EA.

Part: ANGLE — CORRODED (COCKPIT) · airframe 36,718 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR ANGLE CORRODED AT BS 270, LBL 10 TO RBL 10. REPAIRED ANGLE PER EA.

Part: SOCKET — DAMAGED (CABIN) · airframe 36,718 hrs · 21,315 cycles

DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHTS INOP AT ROW1 TO ROW 6. REPAIRED LIGHT SOCKET PER MM & WD.

Part: FLAP — DELAMINATED (LT WING) · airframe 36,069 hrs · 20,950 cycles

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

Part: SKIN — CRACKED (L1 DOOR) · airframe 35,275 hrs · 20,460 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR SKIN CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,208 hrs · 20,423 cycles

AFT GALLEY EMERGENCY FLASHLIGHT LOW VOLTAGE. REMOVED AND REPLACED BATTERY PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,941 hrs · 20,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,941 hrs · 20,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,630 hrs · 19,481 cycles

AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 33,374 hrs · 19,325 cycles

EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: FLAP — PUNCTURED (RT WING) · airframe 32,290 hrs · 18,655 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD T/E FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 31,711 hrs · 18,321 cycles

FOUND R1 DOOR SLIDE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,419 hrs · 16,914 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 951, RBL 5. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,419 hrs · 16,914 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 32 TO RBL 50. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,419 hrs · 16,914 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 807 AND BS 847, RBL 70. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 29,419 hrs · 16,914 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,008 hrs · 16,057 cycles

DURING SCHEDULED CABIN VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 26,972 hrs · 15,447 cycles

ON CLIMBOUT OF MCO NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: GLOWSTRIP — WORN (CABIN) · airframe 26,760 hrs · 15,315 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 26,760 hrs · 15,315 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 26,760 hrs · 15,315 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,818 hrs · 14,771 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — MISSING (L1 DOOR SLIDE) · airframe 22,007 hrs · 12,570 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR VIEWER WINDOW MISSING. INSTALLED WINDOW PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,151 hrs · 12,071 cycles

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

Part: CASE — LOOSE (R1 DOOR SLIDE) · airframe 20,629 hrs · 11,781 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED SLIDE CONTAINER PER MM.

Part: LIGHT — LOOSE (ROW 9 ABC) · airframe 20,090 hrs · 11,485 cycles

EEPLS TRACK LOOSE AT ROW 9 ABC. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM.

Part: LIGHT — PEELING (FWD CABIN) · airframe 18,319 hrs · 10,448 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EEPLS STRIP PEELING. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 17,149 hrs · 9,781 cycles

DURING SCHEDULED HC2 CHECK, FWD AND MID CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — DISCHARGED (R1 DOOR) · airframe 15,998 hrs · 9,140 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 14,992 hrs · 8,566 cycles

FWD SERVICE DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,960 hrs · 8,546 cycles

DURING SPV, FOUND EMERGENCY EXIT LIGHTS AT R1, R2 AND L1 DOORS, INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM.

Part: BUSHING — WORN (LT ELEV) · airframe 10,268 hrs · 5,942 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55), LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM.

Part: BUSHING — WORN (RT ELEV) · airframe 10,268 hrs · 5,942 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55), RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 6,906 hrs · 4,068 cycles

DECLARED EMERGENCY, INFLIGHT SHUTDOWN, AIR TURNBACK. DURING CLIMB POSSIBLE COMPRESSOR STALL OF NR 1 ENGINE, FOLLOWED BY SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SLIDE — DEPLOYED (AFT SVC DOOR) · airframe 5,662 hrs · 3,337 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED INADVERTENTLY. R&R SLIDE PER MM.

Part: BOTTLE — DISCHARGED (PAX DOOR SLIDE) · airframe 1,575 hrs · 936 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED FWD ENTRY SLIDE PER MM.

Part: WARNING LIGHT — FALSE INDICATION (CARGO DOOR) · airframe 1,327 hrs · 791 cycles

ABORTED TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. VERIFIED DOOR CLOSED AND DEFERRED PER MEL, LATER DURING RON AT MDW, ADJUSTED AFT CARGO DOOR TARGET PER MM.

Part: SWITCH — FALSE INDICATION (CARGO DOOR) · airframe 492 hrs · 271 cycles

ABORTED TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. REMOVED DEBRIS FROM AFT CARGO DOOR LIGHT POSITION SWITCH. OPS CHECK GOOD.