N810SK

Part: PRESSURE DECK — CORRODED (FUSELAGE) · airframe 32,803 hrs · 20,711 cycles

RT PRESSURE SILL DECK, CORROSION. ORIGINAL THICKNESS .080 REMAINING THICKNESS AFTER BLEND, .027. ACCOMPLISHED ULTRA SOUND THICKNESS AND HFEC OF CORRODED AREA. REPAIRED IAW REO 690-53-41-195. NEXT INSPECTION DUE 1600 FLIGHT HOURS FROM CURRENT T.T. AND T.C.

Part: PRESSURE DECK — CORRODED (BS 708-813) · airframe 32,803 hrs · 20,711 cycles

CORROSION DAMAGE AND OVERSIZE FASTENER HOLES TO THE PRESSURE FLOOR SILL AND ANGLES. REFERENCE ( DWG: SH^()-36110, REF BETWEEN FS 708.00 AND FS 813.70. ACCOMPLISHED ULTRA SOUND FOR THICKNESS AND HFEC FOR FURTHER CORROSION OR CRACKS. NO DEFECTS NOTED AT THIS TIME. REPAIR COMPLETED PER REO 690-53-41-192 REV (B).

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 32,803 hrs · 20,711 cycles

CORROSION TO LHS AFT PRESSURE SILL DECK. ORIGINAL THICKNESS .080. BLENDED AREA 1.80L X W.080 X .040 MINIMUM REMAINING THICKNESS. ACCOMPLISHED HFEC AND ULTRA SOUND INSPECTION OF DEFECTED AREA. REPAIRED AREA PER BOMBARDIER REO 690-53-41-189 REV (A). REPETITIVE INSPECTION, DUE NEXT 1600 FLIGHT HOURS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,803 hrs · 20,711 cycles

CORROSION ON LATERAL FLOORBEAM @ RT SIDE NEAR SILL. AREA OF BLENDED CORROSION DAMAGE TO THE UPPER FLANGE & AND WEB OF CROSS BEAM @ FS1051.300 BETWEEN RBL27.0 & OUTER EDGE. IAW REO 690-53-61-867.

Part: SKIN — CHAFED (BS 897-942) · airframe 32,806 hrs · 20,711 cycles

LIGHT CHAFE INTO FUSELAGE SKIN JUST AFT OF FS 913 AT STRINGER 27 REPAIRED IAW REO 60-53-51-195

Part: SKIN — CRACKED (PYLON) · airframe 32,803 hrs · 20,711 cycles

WHILE PERFORMING SERVICE BULLETIN 670BA-54-007. #1 PYLON FS1088.20 - 1098. DURING HFEC OPEN HOLE INSPECTION OF LOWER CHORD. #5 FASTENER HOLE WAS FOUND TO BE CRACKED. CRACK INDICATION WAS EMITTING FROM 4:30 POSITION AND .010 IN LENGTH. ORIGINAL FASTENER SIZE WAS .247 AFTER REAMING .277. BOMBARDIER ISSUED ENGINEERING REPAIR ORDER 690-54-51-031. REO STATES AIRCRAFT NOT TO BE OPERATED BEYOND 12, CALENDAR MONTHS DUE TO INSPECTION.

Part: BUSHING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 32,803 hrs · 20,711 cycles

BUSHING ON UPPER ATTACH LUG FOR OUTBOARD FLAP CENTER HINGE ARM WS 220.0 CORRODED RH WING. REPAIRED PER REO 690-57-53-088 NOTE 1 AIRCRAFT NOT TO BE OPERATED BEYOND 12 MONTHS. (ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS)

Part: SKIN — CORRODED (BS 364-394) · airframe 32,803 hrs · 20,711 cycles

AVIONICS BAY DOOR SEAL INTERFACE/DOOR CUTOUT HAS LIGHT CORROSION WITH SMALL NICKS AROUND ENTIRE CIRCUMFERENCE ON INNER SKIN REPAIRED REO 690-53-21-032 (RECOMMENDED MOD IS69053210009 TO BE INCORPORATED) REPEAT INSPECTION 13,100 FLIGHT CYCLES

Part: COMPUTER — FAILED (FUEL SYSTEM) · airframe 32,306 hrs · 20,396 cycles

BOTH XFLOW PUMPS FAIL. XFLOW PUMP CAUTION. RAN QRH MESSAGE PERSISTED. REACHED 1000LB IMBALANCE AND RETURNED TO FIELD. (FLT 3562) CLOSED REMOVED AND REPLACED FQGC IAW AMM AND SYS OPS CHECKS NORMAL IAW FIM.

Part: FADEC — FAILED (RT ENGINE) · airframe 32,224 hrs · 20,341 cycles

€ŒR FADEC FAULT€? CAUTION MESSAGE AFTER TAKEOFF. COMPLIED WITH QRH, RETURNED TO FIELD. (FLT#4654) CLOSED REMOVED AND REPLACED THE R FADEC IAW AMM. RAN ENGINE MULTIPLE TIMES WITH NO FADEC FAULTS. OPS CHECK GOOD AT THIS TIME.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 30,885 hrs · 19,428 cycles

FOUND CORROSION ON THE SERVICE DOOR LOWER SILL ANGLE. REMOVED AND REPLACED THE SERVICE DOOR LOWER SILL ANGLE IAW SRM.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 30,885 hrs · 19,428 cycles

FOUND CORROSION ON SERVICE DOOR LOWER SEAL STRIKER. REMOVED & REPLACED SERVICE DOOR LOWER STRIKER SEAL IAW SRM. LEAK CHECK GOOD.

Part: ATTACH ANGLE — CORRODED · airframe 30,885 hrs · 19,428 cycles

FOUND CORROSION ON SERVICE DOOR LOWER SILL AFT AND MID-AFT FLOOR PROTECTOR WEBS AND ATTACH ANGLES. REPLACED SERVICE DOOR LOWER SILL AFT AND MID-AFT FLOOR PROTECTOR MOUNT ANGLES IAW SRM.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 30,885 hrs · 19,428 cycles

FOUND CORROSION ON SERVICE DOOR LOWER SILL FWD AND MID-FWD FLOOR PROTECTOR WEBS AND ATTACH ANGLES. REPLACED SERVICE DOOR LOWER SILL FWD AND MID-FWD FLOOR PROTECTOR ANGLES IAW SRM.

Part: DOOR SILL — CORRODED · airframe 30,885 hrs · 19,428 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 30,885 hrs · 19,428 cycles

AFT CARGO DOOR LOWER COAMING DAMAGED. REMOVED & REPLACED CARGO DOOR LOWER COAMING IAW SRM. LEAK CHECKED GOOD.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 30,885 hrs · 19,428 cycles

PASSENGER DOOR LOWER SILL HAS CORROSION. REMOVED AND REPLACED THE DOOR SILL IAW SRM.

Part: DOOR SILL — CORRODED (BS 349) · airframe 30,885 hrs · 19,428 cycles

BS 349 AT FWD GALLEY SERVICE DOOR LOWER SILL CORRODED. REPAIRED THE DOOR SILL IAW REO. ALL CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 29,926 hrs · 18,862 cycles

RETURNED TO THE FIELD. FORWARD LAV SMOKE DETECTOR WENT OFF. (FLT 4632) CLOSED REMOVED AND REPLACED THE FORWARD LAV SMOKE DETECTOR IAW AMM.

Part: STRINGER — CORRODED (BS 280-300) · airframe 25,057 hrs · 15,698 cycles

CORROSION FOUND ON STR 27 BETWEEN FS 280.00 AND FS 300.00. R & R STR 27, PN: SH670-31642-1 IAW SRM. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (BS 333-350) · airframe 25,057 hrs · 15,698 cycles

CORROSION FOUND ON STR 27 BETWEEN FS 333 AND FS 350. R & R STR 27 BETWEEN FS 333.00 TO FS 350.00 IAW SRM. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (BS 305-333) · airframe 25,057 hrs · 15,698 cycles

CORROSION FOUND ON STR 27 BETWEEN FS 305 AND FS 333. R & R NEW STR 27 BETWEEN FS 305.00 AND FS 333.00 IAW SRM. PRESSURIZED THE ACFT AND CHECKED FOR LEAKS IN THE REPAIR AREA IAW AMM. NO LEAKS NOTED.

Part: STRINGER — CORRODED (BS 333) · airframe 25,057 hrs · 15,698 cycles

CORROSION ON STR JOINT PIECE AT FS 333 COMMON TO STR 26L. R & R STR JOINT PIECE AT FS 333.00 STR 26L IAW SRM. PRESSURIZED THE ACFT AND CHECKED FOR LEAKS IN THE REPAIR AREA IAW AMM. NO LEAKS NOTED.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,057 hrs · 15,698 cycles

RIGHT FS 280 LOWER WEB CORRODED IN MULTIPLE LOCATIONS. REMOVED RT LOWER WEB SECTION FROM FS 280.00 BULKHEAD AND INSTALLED RT LOWER WEB SECTION AT FS 280.00 BULKHEAD IAW SRM.

Part: STRINGER — CORRODED (BS 333-364) · airframe 25,057 hrs · 15,698 cycles

STRINGER 26R HAS CORROSION AROUND FASTENERS BETWEEN FS 333 AND FS 364. R & R NEW STR 26R BETWEEN FS 333.00 AND FS 364.00 IAW SRM. PRESSURIZED THE ACFT AND CHECKED FOR LEAKS IN THE REPAIR AREA IAW AMM. NO LEAKS NOTED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,057 hrs · 15,698 cycles

BS 280.00 CROSSBEAM AT LBL 9.0 CORRODED. R & R IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 25,057 hrs · 15,698 cycles

UPON MOVING 232BRF FLOORBOARD DISCOVERED CORROSION ON FLOOR SUPPORT JUST FWD OF RT SIDE SERVICE DOOR. REMOVED AND INSTALLED NEW SERVICABLE RT FLOOR SUPPPORT FROM BS 280.00-319.70 IAW SRM.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 25,057 hrs · 15,698 cycles

AFT CARGO COMPARTMENT, CARGO DOOR SILL, THRESHOLD, HAS CORROSION. R & R AFT BAGGAGE BAY DOOR SILL IAW SRM.

Part: LONGERON — CORRODED (BS 333-364) · airframe 25,057 hrs · 15,698 cycles

LEFT LONGERON BETWEEN FS 333 AND FS 364 HAS CORROSION AROUND FASTENERS. R & R NEW SERVICEABLE LT LONGERON 25L IAW SRM.

Part: STRINGER — CORRODED (BS 333-364) · airframe 25,057 hrs · 15,698 cycles

STRINGER 26L HAS CORROSION AROUND FASTENER BETWEEN FS 333 AND FS 364. R & R STR 26L BETWEEN FS 333.00 AND FS 364.00 IAW SRM. NO PRESSURE LEAKS NOTED.

Part: STRINGER — CORRODED (BS 333) · airframe 25,057 hrs · 15,698 cycles

CORROSION ON STRINGER 25L JOINT PIECE AT FS 333. R & R S IAW SRM. PRESSURE CHECKED GOOD.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 25,057 hrs · 15,698 cycles

CORROSION ON STRINER SPLICE 25R AT BS 333. R & R IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 25,057 hrs · 15,698 cycles

CORROSION ON STRINGER SPLICE 25R AT BS 333 COMMON TO STR 26R. INSTALLED STRINGER SPLICE IAW SRM.

Part: FRAME — CORRODED (BS 310) · airframe 25,057 hrs · 15,698 cycles

FS 310 FRAME HAS CORROSION BETWEEN STR 26L TO 26R. REMOVED AND INSTALLED REPAIR IAW REO. LEAK CHECKED GOOD.

Part: WEB — CORRODED (PAX DOOR) · airframe 25,057 hrs · 15,698 cycles

PASSENGER DOOR FWD WEB HAS CORROSION NEXT TO LOWER CORNER. COMPLIED WITH EA.

Part: LONGERON — CORRODED (BS 333-364) · airframe 25,057 hrs · 15,698 cycles

RIGHT LONGERON 25R BETWEEN FS 333 TO FS 364 HAS CORROSION AROUND FASTENERS. R & R WITH NEW SERVICEABLE LONGERON IAW SRM.

Part: FRAME — CORRODED (BS 295) · airframe 25,057 hrs · 15,698 cycles

FS 295 FRAME HAS CORROSION BETWEEN STR 26L TO 26R. PERFORMED PERMANANT REPAIR FS 295.00, FRAME SECTOR SPLICE FROM STR 26L TO 26R IAW REO.

Part: STRINGER — CORRODED (BS 280-333) · airframe 25,057 hrs · 15,698 cycles

STRINGER 26R HAS CORROSION AROUND FASTENERS FROM BS 280 TO 333. R & R THE STRINGER IAW SRM.

Part: STRINGER — CORRODED (BS 280-333) · airframe 25,057 hrs · 15,698 cycles

STRINGER 25L HAS CORROSION AROUND FASTENERS FROM FS 280 TO FS 333. R & R STRINGER IAW SRM. PRESSURE CHECK GOOD.

Part: FRAME — CORRODED (BS 333) · airframe 25,057 hrs · 15,698 cycles

FS 333 FRAME HAS CORROSION BETWEEN STRINGERS 26L TO 26R. REMOVED AND INSTALLED NEW FRAME AND REPAIR IAW REO. LEAK CHECKED GOOD.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 25,057 hrs · 15,698 cycles

ATTACH ANGLE AT STRINGER 26L HAS CORROSION BETWEEN BS 349 AND FS 364. REPLACED ATTACHMENT ANGLE AT STR 26L BETWEEN FS 349.00-364.00 IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,057 hrs · 15,698 cycles

INTERCOSTAL AT STR 27L HAS CORROSION BETWEEN FS 349 AND FS 364. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,917 hrs · 15,601 cycles

ELECTRICAL ODOR MID CABIN ON DESCENT. PERFORMED VISUAL INSPECTION AND SMELLED FOR ELECTRICAL BURN ODOR IN PASSENGER CABIN, NO FAULTS OR ODOR NOTED. INVESTIGATED CIRCUMSTANCES AND ADJUSTMENT TO TEMPERATURE WAS DONE JUST BEFORE ODOR APPEARED. RAN AIR CONDITION SYSTEM USING APU NO ODORS NOTED. SYSTEM OPS CHECKED GOOD.

Part: HANDLE — CHAFED (CARGO BAY) · airframe 20,170 hrs · 12,338 cycles

FWD CARGO RETRIEVAL MODULE AFT HANDLE CHAFED. C CHECK REPLACED FWD CARGO AFT RETRIEVAL MODULE HANDLE IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 20,170 hrs · 12,338 cycles

FWD FORMER PN 601R318031 5 ON PAX DOOR CORRODED. C CHECK REPLACED IAW SRM & AMM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 20,170 hrs · 12,338 cycles

PAX DOOR FWD FORMER HAS SIGNS OF CORROSION NEAR THE TENSION TIE BAR. C CHECK REPLACED PAX DOOR FWD IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,170 hrs · 12,338 cycles

PAX DOOR AFT DRAG ANGLE CRACKED IN RADIUS. C CHECK REPLACED DAMAGED AFT DRAG ANGLE WITH NEW DRAG ANGLE PN 601R31772-5S IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION RBL 9 FLOOR SEAT RAIL FS 693.0. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION ON RBL 9 SEAT RAIL FS 661.0+32. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION ON RBL 9 FLOOR SEAT RAIL FS 360.0. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION RBL 9 FLOOR SEAT RAIL FS 661.0+74. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION LBL 9 FLOOR SEAT RAIL FS 830.40. C-CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION ON SEVERAL AREAS LBL 9 SEAT RAIL FS 581.0 TO FS 661.0 +32. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION SEVERAL AREAS RBL 9 SEAT RAIL FS 485.0 TO FS 581.0. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION LBL 9 FLOOR SEAT RAIL FS 661.0 + 74. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION RBL 9 FLOOR SEAT RAIL FS 847.00 +16 TO FS 926.00. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION RBL 9 FLOOR SEAT RAIL FS 847.0+16. C CHECK BLENDED CORRODED AREA IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CORROSION ON INNER FUSELAGE SKIN AT AVIONICS BAY DOOR SEAL INTERFACE ALONG FWD END OF DOOR CUT OUT. C CHECK REPAIRED IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

SURFACE CORROSION AT FLOOR SILL GALLEY SERVICE DOOR FS 349.00. C CHECK BLENDED OUT SURFACE CORROSION AT FLOOR SILL AFT OF GALLEY SERVICE DOOR FS 349.00 IAW SRM & REO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

CRACK ON THE LT FUSELAGE FRAME AT FS 235, JUST BELOW WL 110. C CHECK REPAIRED CRACK ON THE LT FUSELAGE FRAME AT FS 235.00, JUST BELOW WL 110 IAW STS EA.

Part: AXLE — CORRODED (LT MLG) · airframe 20,170 hrs · 12,338 cycles

LT MLG NR 2 PISTON AXLE CORRODED. C CHECK REPAIRED NR 2 PISTON AXLE IAW REO.

Part: AXLE — CORRODED (RT MLG) · airframe 20,170 hrs · 12,338 cycles

RT MLG NR 3 PISTON AXLE CORRODED. C CHECK REPAIRED NR 3 PISTON AXLE IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 20,170 hrs · 12,338 cycles

PAX DOOR PIANO HINGE IS CHAFED AT AFT 2 LUGS. C CHECK BLENDED OUT CHAFE ON AFT 2 LUGS ON PAX DOOR PIANO HINGE DOOR SIDE IAW REO.

Part: AXLE — CORRODED (RT MLG) · airframe 20,170 hrs · 12,338 cycles

RT MLG NR 4 PISTON AXLE CORRODED. C CHECK REPAIRED NR 4 PISTON AXLE IAW REO.

Part: AXLE — CORRODED (LT MLG) · airframe 20,170 hrs · 12,338 cycles

LT MLG NR 1 PISTON AXLE CORRODED. C CHECK REPAIRED NR 1 PISTON AXLE IAW REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

RT FS 193.00 IN TRU BAY CRACKED. C CHECK REPAIRED RT FS 193.00 CRACK IAW REO.

Part: SKIN — GOUGED (FUSELAGE) · airframe 20,170 hrs · 12,338 cycles

GOUGE ON FUSELAGE EXTERNAL SKIN LOCATED UNDER PANEL 195DL AT BL 0. C CHECK REPAIRED THE FUSELAGE SKIN UNDER PANEL 195DL AT BL 0 IAW REO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,778 hrs · 10,815 cycles

EMERGENCY EXIT SIGN ROW 4C/D DOES NOT ILLUMINATE. (FLT 4710) REPLACED THE NR 1 ELBP IAW AMM. P/N: AD-2013-1A S/N ON: 105290 S/N OFF: 72498

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,454 hrs · 10,616 cycles

CEILING EMERGENCY LIGHT AT ROW 8 IS BURNED OUT. (FLT 4707) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,886 hrs · 10,256 cycles

SECOND TO LAST CEILING OVERHEAD LIGHT IS BURNED OUT. (FLT#4645) RELAMPED OVERHEAD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,057 hrs · 9,734 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 15,875 hrs · 9,602 cycles

THE 280 BEAM CRACKED ON BOTH SIDES. (C-CHECK) REPAIR PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,853 hrs · 9,579 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,648 hrs · 9,422 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4836) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,589 hrs · 9,389 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,501 hrs · 9,317 cycles

EMERGENCY AISLE FLOOD LIGHT FORWARD OF LAV DOOR IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,315 hrs · 9,170 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,256 hrs · 9,138 cycles

FLT 4441, OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,992 hrs · 8,949 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4646) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,960 hrs · 8,924 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4535) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,960 hrs · 8,924 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,850 hrs · 8,861 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED JUST ABOVE DOOR ASSIST PULLEY MOUNTING BRACKET. (SERVICE) REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,825 hrs · 8,832 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4785) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,810 hrs · 8,823 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4811) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,721 hrs · 8,758 cycles

NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4467) RELAMPED EMERGENCY LIGHT.

Part: HANDLE — BROKEN (CABIN DOOR) · airframe 14,696 hrs · 8,746 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE AND OPEN. (FLT 4494) REPLACED THE INNER HANDLE DETENT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,451 hrs · 8,580 cycles

FORWARD 2 CEILING EMERGENCY LIGHTS ARE OUT. (FLT 4557) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,425 hrs · 8,558 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,204 hrs · 8,420 cycles

OVERHEAD EMERGENCY LIGHT OUT AT ROW 14. (FLT 4841) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,032 hrs · 8,295 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4679) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — BROKEN (BLEED AIR SYS) · airframe 13,979 hrs · 8,266 cycles

LEFT BLEED WARNING MESSAGE. (FLT 4526) REPLACED BROKEN CONNECTOR ON LEFT BLEED LOOP MT141. REPLACED AILC. P/N ON GG690-80012-3, S/N OFF 00426.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,979 hrs · 8,266 cycles

OVERHEAD EMERGENCY LIGHT AT 17 IS OUT. (FLT 4818) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,979 hrs · 8,266 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 4818) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,849 hrs · 8,155 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 4515) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,840 hrs · 8,149 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4814) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,799 hrs · 8,125 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,723 hrs · 8,078 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4606) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,632 hrs · 7,998 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4651) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,632 hrs · 7,998 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4578) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,526 hrs · 7,919 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,484 hrs · 7,890 cycles

NR 7 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4563) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,454 hrs · 7,865 cycles

NR 1 AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4611) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,146 hrs · 7,630 cycles

NR 6 AND 7 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,646 hrs · 7,331 cycles

NR 6 EMERGENCY CEILING LIGHT IS OUT. (FLT 4611) RELAMPED EMERGENCY LIGHT.

Part: WIRE HARNESS — CHAFED (RT ENGINE) · airframe 12,104 hrs · 7,025 cycles

RIGHT ENGINE HAD A UNCOMMANDED ROLL BACK DURING CRUISE. (FLT 4486) FOUND CHAFED RIGHT ENGINE YELLOW WIRING HARNESS. REPLACED YELLOW HARNESS WITH A SERVICEABLE UNIT. REPLACED RIGHT ENGINE FADEC AND FUEL CONTROL UNIT AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,366 hrs · 6,555 cycles

EMERGENCY LIGHT AT ROW 14 INOPERATIVE. (FLT 4792) RELAMPED EMERGENCY LIGHT.

Part: PRINTED CKT BOARD — FAULTY (CABIN) · airframe 10,785 hrs · 6,167 cycles

EMERGENCY LIGHTS CYCLE CONTINUOUSLY. (FLT 4617) REMOVED AND REPLACED PCB5 IN JB11.

Part: CONTROL VALVE — SEPARATED (AC BAY) · airframe 10,403 hrs · 5,917 cycles

THE "LEFT BLEED DUCT" WARNING AT FL120. (FLT 4580) FOUND RIGHT FLOW CONTROL VALVE AND PACK INLET DUCT SEPARATED, RE-CONNECTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,221 hrs · 5,804 cycles

EMERGENCY FLOODLIGHT OVER ROW 8 INOP. (FLT 4608) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,180 hrs · 4,648 cycles

SECOND FROM AFT CEILING EMERGENCY LIGHT INOP. (FLT 4820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,082 hrs · 4,595 cycles

EMERGENCY LIGHTS POD 3 OUT OF SERVICE. (FLT 4719) RELAMPED EMERGENCY LIGHT CEILING POD NR 3 IAW AMM 33-51-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,795 hrs · 4,439 cycles

EMERGENCY CEILING LIGHT NR 5 INOP. (FLT 4504) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,608 hrs · 4,338 cycles

LAST CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 4563) RELAMPED EMERGENCY LIGHT.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,545 hrs · 4,301 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. (C CHECK) REPLACED PER REO.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,582 hrs · 4,325 cycles

FS 280 BEAM CORRODED. (C CHECK) REPAIRED PER REO.

Part: WEB — CRACKED (PAX DOOR) · airframe 7,545 hrs · 4,301 cycles

PASSENGER DOOR AFT WEB CRACKED. (C CHECK) REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,793 hrs · 3,871 cycles

FLT 4533 - CEILING LEVEL EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 6,290 hrs · 3,576 cycles

FLT 4663 - CEILING EMERGENCY LIGHT AFT OF EMERGENCY EXIT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 5,910 hrs · 3,352 cycles

FLT 4813 - THE SIXTH EMERGENCY CEILING FLOOD LIGHT AFT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,804 hrs · 3,295 cycles

FLT 4530 - CEILING EMERGENCY LIGHT AFT CABIN INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,453 hrs · 3,084 cycles

FLT 3968 - AFT CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 4,114 hrs · 2,336 cycles

EXTERIOR MAIN CABIN DOOR HANDLE IS BROKEN. REPLACED EXTERIOR HANDLE ON MAIN CABIN DOOR IAW 52-11-03. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,673 hrs · 957 cycles

CREW REPORTS STRONG FUEL ODOR FROM FORWARD AND AFT LAVS. PERFORMED CLEANING AND FLUSHING PROCEDURES IAW MONOGRAM CMM 38-35-04 ON BOTH THE FORWARD AND AFT LAVS. SNIFFER INDICATED AIR CONCENTRATION IS WITHIN LIMITS.