N783CA

Part: ENGINE — FAILED (RIGHT) · airframe 37,317 hrs · 33,704 cycles

DURING APP BASE LEG RIGHT ENGINE N1 FLUCTUATED AND NOTABLE A/C ENGINE VIBRATION @ 58 N1. VIBRATION STOPPED. DECLARED EMERGENCY WITH ATC. ON TAXI IN ENG TEMP WENT TO MAX TEMP OIL PRESSURE ZERO SHUT ENG DOWN. R&R THE RT ENGINE IAW AMM. OPS CHECK AND LEAK CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

AFT CARGO FLOOR SUPPORT BEAM AT OTBD LBL 9.00 BETWEEN FS 589.00 AND FS 605.00 HAS CORROSION. R & R PART IAW SRM.

Part: SKIN — GOUGED (RT WING) · airframe 37,317 hrs · 33,704 cycles

RIGHT WING APRON SKIN GOUGE. ALL STEPS COMPLETED OF PERMANENT REPAIR. COMPLIED WITH IAW REO.

Part: SKIN — DENTED (ESCAPE HATCH) · airframe 37,317 hrs · 33,704 cycles

CREW ESCAPE HATCH UPPER LT CORNER HAS A DENT ON OUTER SKIN. COMPLIED WITH STS EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

FLOOR SUPPORT AT FS 349.00 HAS CORROSION OTBD SIDE OF LBL 27.00. C/W PERMANENT REPAIR OF FLOOR SUPPORT BEAM AT FS 349.00 OTBD SIDE OF LBL 27.00 IAW SRM AND STS-EA.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

REPLACE RT INBD FLAP VANE CENTER L/E PN 601R14303-52 FOUND CHAFED. REMOVED AND INSTALLED SERVICEABLE RT INBD FLAP, CENTER L/E IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

AFT CARGO COMPARTMENT AT FS 621.00 HAS CORROSION AT ANGLE STR 17 LT SIDE. INSTALLED NEW ANGLE IN CARGO COMPARTMENT AT FS 621, STR 17L IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

LEFT INBD FLAP VANE L/E CHAFED AT INBD L/E. REMOVED AND INSTALLED NEW SERVICEABLE INBD VANE CAP ON LT INBD FLAP IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT OTBD L/E. REPLACED RT INBD FLAP OTBD L/E IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

LEFT INBD FLAP VANE L/E CHAFED AT OTBD L/E. REMOVED AND INSTALLED NEW LT INBD FLAP, FLAP VANE OTBD L/E SKIN IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

LT INBD FLAP VANE L/E CHAFED AT CENTER L/E. REPLACED LT INBD FLAP VANE CENTER L/E IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

AFT CARGO COMPARTMENT LBL 27.00 INBD AND OTBD FLANGE HAS CORROSION BETWEEN FS 621.00 AND FS 574.00. R & R LBL 27 FLOORBEAM CAP FROM FS 574 TO FS 621 WITH NEW CAP IAW SRM AND REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 37,317 hrs · 33,704 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT INBD L/E. REPLACED L/E PN 601R14303-54 IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

AFT CARGO COMPARTMENT LT SILL HAS CORROSION BETWEEN FS 621.00 AND FS 574.00. C/W PERMANENT REPAIR IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

AFT CARGO COMPARTMENT LBL 9.00 OTBD FLANGE HAS CORROSION BETWEEN FS 621.00 AND FS 589.00. THE FLOORBEAM WAS REMOVED AND A NEW PN: 601R35031-3 WAS INSTALLED IAW REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

MINOR DENT BETWEEN FS 409.00+48 & FS 409.00+64 AND STR 21L & 22L. WORKED OUT DENT AND REMOVED ALL SIGNS OF DENT IAW STS EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,317 hrs · 33,704 cycles

SMALL DENT 6" FWD OF EXTERNAL POWER RECEPTABLE DOOR 1.25" X 1" DIA APPROXIMATELY .005" DEEP LOCATED RT SIDE OF ACFT 6" FWD OF EXTERNAL POWER RECEPTACLE DOOR. REPAIRED DENT IAW STS EA. OPS, RIG CHECKS GOOD.

Part: SKIN — CORRODED (PAX DOOR) · airframe 37,317 hrs · 33,704 cycles

PANEL 832AL ON PASSENGER DOOR HAS CORROSION ON SKIN AROUND NUTPLATE HOLES. UNDER PANEL 832AL ON PASSENGER DOOR SKIN REPAIRED IAW STS EA.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 37,317 hrs · 33,704 cycles

SERVICE DOOR PROTECTOR PLATE HAS CORROSION ON BOTTOM SIDE OF UPPER FLANGE AROUND SCREW HOLES. INSTALLED NEW SERVICE DOOR PROTECTOR PLATE IAW SRM.

Part: OIL SYSTEM — LOW (APU) · airframe 34,198 hrs · 30,619 cycles

APU OIL PRESSURE CAUTION MESSAGE DURING FLIGHT. SERVICED APU WITH OIL. OPERATED APU FOR EXTENDED PERIOD. OPS CHECKED GOOD IAW AMM.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,558 hrs · 29,995 cycles

CORROSION FOUND ON PAX DOOR KICK ANGLE. C-CHECK, RECEIVED AND INSTALLED NEW PAX DOOR SILL KICK ANGLE IAW SRM.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 33,558 hrs · 29,995 cycles

PAX DOOR SILL, AFT HINGE ARM CUT OUT CORRODED. C-CHECK, INSTALLED PAX DOOR SILL AFT HINGE ARM CUT OUT BRACKET IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,558 hrs · 29,995 cycles

LEFT AFT LATCH CUT OUT IN THE TRU SKIN WAS FOUND CRACKED. C-CHECK, R & R LT FWD TRU BAY SKIN, DOOR LAND IAW SRM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 33,558 hrs · 29,995 cycles

FLOORBEAM ANGLE CRACKED AT BS 484 AND RBL 9, WL 73.5. C-CHECK, REPLACED FLOORBEAM ANGLE IAW REO.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 33,558 hrs · 29,995 cycles

FLOORBEAM ANGLE CRACKED AT BS 484 AND RBL 36, WL 73.5. C-CHECK, R & R FLOORBEAM ANGLE IAW REO.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 33,558 hrs · 29,995 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 364. C-CHECK, R & R DAMAGED SEAT TRACK FROM BS 362-396 IAW REO.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 33,558 hrs · 29,995 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 364 RBL 9. C-CHECK, R & R DAMAGED SEAT TRACK FROM BS 362-396, IAW SRM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,558 hrs · 29,995 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 409+8. C-CHECK, R & R DAMAGED SEAT TRACK FROM BS 396-409+128 IAW REO.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,558 hrs · 29,995 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 409+72 AND BS 409+112. C-CHECK, R & R DAMAGED SEAT TRACK FROM FS 396 - 409+128 RBL 9 IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,558 hrs · 29,995 cycles

PAX DOOR PIANO HINGE HALF, DOOR SIDE, LUGS NR 1 AND NR 8, AFT TO FWD, HAVE LIGHT GOUGES. C-CHECK, BLENDED CHAFED AREAS ON PAX DOOR PIANO HINGE, DOOR SIDE, LUGS NR 1 AND NR 8 IAW REO AND SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 33,558 hrs · 29,995 cycles

CRACK NOTED AND MARKED IN UPPER RADIUS OF LT WINDSHIELD CENTER POST. C-CHECK, R & R LT WINDSHIELD CENTER POST IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

RIGHT INBD FLAP VANE CENTER L/E CAP CHAFED. C-CHECK, R & R RT INBD FLAP VANE IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

LEFT INBD FLAP VANE CENTER L/E CAP CHAFED. C-CHECK, R & R LT INBD FLAP VANE IAW SRM.

Part: SKIN — DENTED (BS 589) · airframe 33,558 hrs · 29,995 cycles

DENT FOUND LT SIDE OF ACFT SKIN, AFT AND BELOW BAGGAGE DOOR, BS 589, S22-23L. C-CHECK, REPAIRED IAW SRM.

Part: SKIN — DENTED (BS 682) · airframe 33,558 hrs · 29,995 cycles

DENT FOUND LT SIDE OF ACFT SKIN BS 682, S19-20L, C-CHECK, REPAIRED IAW EA.

Part: STRUCTURE — GOUGED (LT MLG DOOR) · airframe 33,558 hrs · 29,995 cycles

LEFT MLG DOOR, FWD SIDE OF DOOR IS GOUGED. C-CHECK, REPAIRED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

RIGHT INBD FLAP VANE, INBD CAP IS CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

LEFT INBD FLAP VANE, CENTER CAP CHAFED. C-CHECK, R & R LT INBD FLAP VANE IAW REO AND SRM.

Part: VANE — CHAFED (LEFT WING TE FLA) · airframe 33,558 hrs · 29,995 cycles

LEFT INBD FLAP VANE, INBD CAP CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

RIGHT INBD FLAP VANE, OTBD CAP IS CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,558 hrs · 29,995 cycles

LEFT INBD FLAP VANE, OTBD CAP CHAFED. C-CHECK, BLENDED CHAFE IAW REO AND SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,558 hrs · 29,995 cycles

CRACK NOTED ON BS 621 BULKHEAD WEB. C-CHECK, REPAIRED IAW REO.

Part: CAM — CHAFED (PAX DOOR LEVER) · airframe 33,558 hrs · 29,995 cycles

PASSENGER DOOR FWD PULL-IN LEVER LOWER LOBE CHAFED. C-CHECK, REPAIRED FORWARD PULL IN LEVER IAW REO.

Part: SKIN — DELAMINATED (RT WING) · airframe 33,558 hrs · 29,995 cycles

RT WING L/E 630KL IS DELAMINATED. C-CHECK, BONDED SHROUD TO L/E SKIN ON WING L/E PANEL 630KL IAW REO.

Part: SKIN — DELAMINATED (RT WING) · airframe 33,558 hrs · 29,995 cycles

RIGHT WING L/E 620JL SKIN DELAMINATED. C-CHECK, BONDED SHROUD TO L/E SKIN ON WING L/E PANEL 620JL IAW REO.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,547 hrs · 29,987 cycles

AFT MOST EMERGENCY CEILING LIGHT INOPERATIVE. REPLACED AFT MOST EMERGENCY CEILING LIGHT BULB IAW AMM.

Part: GLOWSTRIP — MISSING (PAX DOOR) · airframe 33,519 hrs · 29,963 cycles

GLOW STRIP ON THE MAIN CABIN DOOR ARE MISSING. INSTALLED NEW GLOW STRIPS.

Part: SKIN — CRACKED (LT WING) · airframe 32,661 hrs · 29,113 cycles

LT WING AFT LOWER WING PLANK HAS A CRACK 0.960 INCHES LONG FROM THE TE AT WS 148.019. C-CHECK REPAIRED LT WING AFT LOWER WING PLANK AT WS 148.019 IAW REO.

Part: YAW DAMPER — FAILED (NR 2) · airframe 32,624 hrs · 29,075 cycles

YD NR 2 KICKS OFF & THERE IS A NOTICEABLE KICK IN THE RT RUDDER. IF RUDDER TRIM MOVES ABOUT A HALF BAR DEFLECTION TO THE LEFT THEN YD 2 DISENGAGES. FLT#4764 REPLACED NR 2 YAW DAMPER IAW AMM. PN DL2233M1-1 SN 3507 SN OFF 3169 PN S24665-134.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 32,212 hrs · 28,680 cycles

LT ENGINE FORWARD MOUNT YOKE LINK HAS GALLED HAT BUSHINGS. C-CHECK REPLACED.

Part: BEARING — DAMAGED (ENGINE MOUNT) · airframe 32,212 hrs · 28,680 cycles

LT ENGINE FORWARD YOKE MOUNT LOWER BALL BEARING IS PITTED. C-CHECK REPLACED.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 31,953 hrs · 28,432 cycles

PAX DOOR HANDLE OUT CAUTION MESSAGE. FLT#7377 LUBED PAX DOOR OUTER HANDLE LATCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,380 hrs · 26,987 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,948 hrs · 26,589 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4545) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,821 hrs · 26,475 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4673) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,709 hrs · 26,372 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4696) RELAMPED EMERGENCY LIGHT.

Part: PROBE — ERODED (PITOT/STATIC SYS) · airframe 29,124 hrs · 25,817 cycles

RIGHT PITOT PROBE HAS SOME BURNT MATERIAL ON IT. (SERVICE) FOUND MATERIAL ON THE RIGHT PITOT STATIC PROBE TO BE EROSION. REPLACED THE RIGHT PITOT STATIC PROBE WITH A SERVICEABLE UNIT.

Part: ADG — DEPLOYED · airframe 29,009 hrs · 25,715 cycles

ADG DEPLOYED. (FLT 4636) RESTOWED ADG.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 28,924 hrs · 25,636 cycles

FORWARD BULKHEAD ON FORWARD SIDE, LEFT LOWER OUTBOARD CORNER AREA HAS A STRINGER TO BULKHEAD CLEAT THAT IS CRACKED. (SERVICE) REPLACED AFFECTED SKIN CLEAT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,996 hrs · 25,702 cycles

CORROSION ON THE PASSENGER DOOR ENTRY FLOOR SUPPORT. (SERVICE) REPLACED ENTRY FLOOR SUPPORT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,926 hrs · 23,779 cycles

BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-3381 AND COMAIR TASK CARD REO 601R-53-1230.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,926 hrs · 23,779 cycles

FRAME AT FS 333.00 CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED AND REPLACED CORRODED FRAME SECTION FROM FACTORY SPLICE AT STRINGER 23L TO FACTORY SPLICE AT STRINGER 23R, IAW SRM 51-42-06 AND 51-42-21.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 24,570 hrs · 21,781 cycles

ON APPROACH INTO JFK RECEIVED CARGO BOTTLE LOW MSG. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. REMOVED AND REPLACED NR 1 CARGO FIRE EXTINGUISHER BOTTLES.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 24,570 hrs · 21,781 cycles

ON APPROACH INTO JFK RECEIVED CARGO BOTTLE LOW MSG. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. REMOVED AND REPLACED NR 2 CARGO FIRE EXTINGUISHER BOTTLES.

Part: WIRE HARNESS — FAILED (RT MLG WOW) · airframe 23,665 hrs · 21,075 cycles

ENROUTE, RECEIVED WOW INPUT MSG. EMERGENCY DECLARED, ACFT DIVERTED AND LANDED SAFELY. REMOVED AND REPLACED RT MLG WOW WIRE HARNESS NR 1.

Part: FRAME — CRACKED (FS 640) · airframe 23,393 hrs · 20,865 cycles

LT FS 640 FRAME DOUBLER IS CRACKED BETWEEN STR 9 AND 12. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640 FRAME AND DOUBLER PER SB601R-53-061 KIT DRWG. K601R36009 REV B AND 601R5361569 REV A.

Part: FRAME — CRACKED (PAX DOOR) · airframe 23,393 hrs · 20,865 cycles

PAX DOOR AFT INNER FRAME AT FS 338.9 IS CRACKED. REMOVED DAMAGED PORTION OF FRAME AT FS 338.9, FABRICATED AND INSTALLED SERVICEABLE REPAIR PARTS PER CRJ REO 601R-52-11-402 REV H.

Part: SKIN — CRACKED (FS 559 RBL 9-18) · airframe 23,393 hrs · 20,865 cycles

PERMANENT REPAIR REQUIRED DUE TO TEMP REPAIR THAT WAS DONE AT FS 559 WEB BETWEEN RBL 9-18. REMOVED TEMP REPAIR AND INSTALLED A PERMANENT REPAIR DOUBLER ON FS 559 BULKHEAD WEB.

Part: SKIN — CRACKED (BS 235) · airframe 23,393 hrs · 20,865 cycles

RT FUEL SKIN IS CRACKED AT FS 235 IN THE RT AFT RADIUS OF THE NLG CUTOUT. REMOVED DAMAGED SKIN AND INSTALLED PERMANENT REPAIR PER BOMBARDIER AEROSPACE REO 601R-53-11-048.

Part: SKIN — CORRODED (LT WING) · airframe 23,393 hrs · 20,865 cycles

LT WING 540BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED LT WING FUEL ACCESS PANEL CUTOUT 540BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III.

Part: FRAME — CRACKED (FS 640) · airframe 23,393 hrs · 20,865 cycles

RT FS 640 FRAME DOUBLER IS CRACKED BETWEEN STR 9 AND 12. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R36009-4 ON RT FS 640 FRAME AND DOUBLER PER SB601R-53-061 KIT DRWG. K601R36009 REV B AND 601R5361569 REV A.

Part: SKIN — CORRODED (RT WING) · airframe 23,393 hrs · 20,865 cycles

RT WING 640BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED RT WING FUEL ACCESS PANEL CUTOUT 640BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,353 hrs · 19,222 cycles

FLIGHT 5129 - EN ROUTE CVG - TUL PILOT'S WINDSHIELD CRACKED. LANDED TUL WITHOUT INCIDENT. REPLACED PILOT'S WINDSHIELD. NO FURTHER DEFECTS.

Part: BPSU — FAULTY (T/E FLAP) · airframe 21,030 hrs · 18,973 cycles

FLIGHT 5199 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED EO 27-046AD AND REPLACED LEFT BPSU. NO FURTHER DEFECTS.

Part: BPSU — FAULTY (T/E FLAP) · airframe 21,023 hrs · 18,968 cycles

FLIGHT 5366 - FLAP FAIL MESSAGE RECEIVED AFTER LANDING. REPLACED LEFT BPSU. NO FURTHER DEFECTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 20,056 hrs · 18,195 cycles

FLAPS FAIL MSG AT 30 DEGREES AT FINAL, GO AROUND INITIATED, FLT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: DETECTOR — DIRTY (A/C PACK) · airframe 19,942 hrs · 18,104 cycles

FLIGHT 9451 - EN ROUTE BNA - CVG RECEIVED A DISPLAY COOL AND EXHAUST FAIL MESSAGE, FLIGHT DIVERTED TO EVV. CLEANED THE DISPLAY AIR FLOW DETECTOR.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 19,841 hrs · 18,019 cycles

FLIGHT 5443 - HYD PUMP 3A HIGH TEMP, FOLLOWED QRH HYD PUMP 3A OFF 3B ON THEN RECEIVED GEAR DISAGREE WARNING DURING GEAR EXTENSION WITH 3B HYD PUMP ONLY. REMOVED AND REPLACED HYD PUMP 3B FOR GEAR DISAGREE. OPS CHECKS GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,486 hrs · 17,752 cycles

FLIGHT 4940 - ON FINAL APPROACH WHEN FLAPS SELECTED FROM 30 TO 45 DEGREES FLAPS STAYED AT 30 DEGREES WITH FLAP FAIL MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: PUSHROD — BROKEN (PAX DOOR) · airframe 19,469 hrs · 17,736 cycles

FLIGHT 4979 - CABIN WOULD NOT PRESSURIZE DURING CLIMB. STOPPED CLIMB AT 10,000 FT RECEIVED EXHAUST STATUS MESSAGE AND DISPLAY COOL CAUTION MESSAGE. FOLLOWED QRH, DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. FERRIED TO JFK, REPLACED PAX DOOR FLAPPER DOOR ROD. NO FURTHER DEFECTS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,969 hrs · 17,331 cycles

FLIGHT 5614 - FLAPS FAILED AT 30 DEGREES ON APPROACH TO SDF. COMPLIED WITH AD 2006-12-21, FLAP FAIL CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM RESET WITH NO FURTHER MESSAGES.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,875 hrs · 17,255 cycles

FLIGHT 4943 - FLAP FAIL AT 26 DEGREES ON TAXI IN. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: OVERHEAT LOOP — FAULTY (AFT E/E BAY) · airframe 18,444 hrs · 16,929 cycles

DURING CLIMBOUT, RECEIVED A LT 14TH STAGE DUCT WARNING MESSAGE, FLIGHT RETURNED TO DEPARTURE. REPLACED SEGMENTS OF THE LT 14TH STAGE DUCT HEAT SENSING ELEMENTS.

Part: DUCT — UNSERVICEABLE (LT PYLON) · airframe 18,444 hrs · 16,929 cycles

DURING CLIMBOUT OF ORF RECEIVED A LEFT 14TH STAGE DUCT WARNING MESSAGE, FLIGHT RETURNED TO ORF. REPLACED THE 14TH STAGE DUCT BLEED AIR DUCT ASSEMBLY.

Part: OVERHEAT LOOP — FAULTY (AFT E/E BAY) · airframe 18,444 hrs · 16,929 cycles

DURING CLIMB-OUT , RECEIVED A LT 14TH STAGE DUCT WARNING MESSAGE, FLIGHT RETURNED TO DEPARTURE. REPLACED SEGMENTS OF THE LT 14TH STAGE DUCT HEAT SENSING ELEMENTS.

Part: OVERHEAT SENSOR — FAULTY (AFT E/E BAY) · airframe 18,444 hrs · 16,929 cycles

DURING CLIMBOUT OF ORF RECEIVED A LT 14TH STAGE DUCT WARNING MESSAGE, FLIGHT RETURNED TO DEPARTURE. REPLACED SEGMENTS OF THE LT 14TH STAGE DUCT HEAT SENSING ELEMENTS.

Part: SWITCH — FAULTY (STAB TRIM) · airframe 18,354 hrs · 16,854 cycles

FLIGHT 5575 - AFTER DEPARTURE FROM CVG RECEIVED A STAB-MACH TRIM CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE TRIM DISCONNECT SWITCH.

Part: LIGHT — NO TEST (CABIN) · airframe 17,705 hrs · 16,353 cycles

FLIGHT 5231 - EMERGENCY LIGHTING SYSTEM FAILED TEST. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. SYSTEM IS FUNCTIONING PROPERLY.

Part: FLAP SYSTEM — OUT OF SEQUENCE (TE FLAPS) · airframe 17,131 hrs · 15,857 cycles

EN ROUTE, DURING CLIMB, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY AND DIVERTED. FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: BPSU — FAULTY (LEFT WING) · airframe 16,268 hrs · 15,124 cycles

FLIGHT 5402 - DURING APPROACH INTO MCO WHEN FLAPS SELECTED TO 20 DEGREES RECEIVED A FLAP FAIL CAUTION. REPLACED THE LEFT BRAKE POSITION SENSING UNIT.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 16,298 hrs · 15,150 cycles

FLIGHT 5212 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,803 hrs · 13,841 cycles

FLIGHT 5013 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,501 hrs · 13,576 cycles

FLIGHT 4936 FLOOR EMERGENCY LIGHT AT ROW 1 IS INOP. REPLACED BROKEN POWER CABLE ASSY.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 14,234 hrs · 13,331 cycles

FLIGHT 5794 FLAPS FAIL CAUTION. REPLACED THE FECU.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 14,209 hrs · 13,305 cycles

FLIGHT 5108 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,195 hrs · 13,296 cycles

FLIGHT 5028 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 14,071 hrs · 13,192 cycles

FLIGHT 4958 - FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: RUDDER — FLUCTUATES (EMPENNAGE) · airframe 13,951 hrs · 13,079 cycles

FLIGHT 5853 RUDDER FLUCTUATES LT AND RT DURING CRUISE. C/W YAW OSCILLATION TROUBLESHOOTING, NO DEFECTS FOUND.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,845 hrs · 12,986 cycles

LEFT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,845 hrs · 12,986 cycles

RIGHT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 13,844 hrs · 12,896 cycles

INTERCOSTAL AT FS 484.00 CRACKED AT RBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,845 hrs · 12,986 cycles

FS 574 FRAME SUPPORT ANGLE HAS MISDRILLED HOLD. REPAIRED IAW REO 601R-53-61-1187.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 13,844 hrs · 12,896 cycles

INTERCOSTAL AT FS 484.00 CRACKED AT LBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 13,845 hrs · 12,986 cycles

LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,844 hrs · 12,986 cycles

CARGO DOOR LANDING PLATE IS CRACKED AT FS 574. REPAIRED IAW REO 601R-53-61-690.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 12,528 hrs · 11,944 cycles

FLIGHT 5364 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER, NO DEFECTS FOUND.

Part: WARNING LIGHT — INTERMITTENT (FLT SPOILERS) · airframe 11,205 hrs · 10,880 cycles

FLIGHT 5416 FLIGHT SPOILER FAULT MESSAGE. RESET SPOILERS - COULD NOT DUPLICATE FAULT.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 10,315 hrs · 10,151 cycles

CRACK ON ENGINE SUPPORT BEAM LOWER WEB AT FWD I/B CORNER OF LT ACCESS PANEL. REPAIRED IAW REO 601R-53-61-366.

Part: FLAP · airframe 8,748 hrs · 8,812 cycles

FLIGHT 5718 FLAPS FAILED AFTER LANDING.COULD NOT DUPLICATE. INSPECTED FLAPS PER AD 98-20-01 - NO FAULTS FOUND.

Part: CONTROL HANDLE — MALFUNCTIONED (INST PANEL) · airframe 8,093 hrs · 8,240 cycles

FLIGHT 5706 FLAPS FAILED WHEN SELECTED UP AFTER LANDING.REPLACED THE FLAP CONTROL LEVER.

Part: VALVE — FAILED (CTR FUSELAGE SEC) · airframe 7,584 hrs · 7,765 cycles

FLIGHT 6688. AFTER T/O DURING GEAR RETRACTION RECEIVED AN ANTI-SKID O/B AND PARKING BRAKE CAUTION MESSAGE, AIRCRAFT RETUREND TO THE FIELD.REPLACED THE MLG SELECTOR VALVE.

Part: BATTERY — DISCHARGED (AVIONICS) · airframe 6,888 hrs · 7,080 cycles

FLIGHT 5676 SEVERAL EMERGENCY LIGHTS ARE INOP.REPLACED THE #3 EMERGENCY BATTERY

Part: LIGHT · airframe 6,742 hrs · 6,930 cycles

FLIGHT 5812 DUIRNG PRE-FLIGHT CHECK FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.PLACED EMERGENCY LIGHTING ON DEFERRED DISCREPANCY LIST PER MEL 66-51-02.

Part: LIGHT · airframe 6,742 hrs · 6,930 cycles

FLIGHT 5812 DUIRNG PRE-FLIGHT CHECK FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.PLACED EMERGENCY LIGHTING ON DEFERRED DISCREPANCY LIST PER MEL 66-51-02.

Part: SUPPORT — CRACKED (LT WING) · airframe 6,473 hrs · 6,660 cycles

CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540CB. REPAIRED IAW 601R-57-21-030.

Part: SUPPORT — CRACKED (LT WING) · airframe 6,473 hrs · 6,660 cycles

CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540AB. REPAIRED IAW 601R-57-21-030 AND REO 601R-57-21-183.

Part: DAMPENER — MALFUNCTIONED (EMPENNAGE) · airframe 5,391 hrs · 5,593 cycles

FLIGHT #5437 - AIRCRAFT HAS SIDE TO SIDE YAWING MOTION.REPLACED THE #1 YAW DAMPENER.

Part: LAMP · airframe 5,184 hrs · 5,389 cycles

FLIGHT #5480. FLOOR PATH EMERGENCY LIGHTING, ROWS 9 THRU 13, ARE INOPERABLE.RECONECTED LOOSE LIGHT STRIP - SYSTEM TEST NORMAL.

Part: CONNECTOR · airframe 4,927 hrs · 5,115 cycles

FLIGHT #5741. DURING APPROACH INTO TRI RECEIVED A FLAP FAIL CAUTION MESSAGE AT 22 DEGREES FLAP POSITION.REMOVED CONNECTOR B2CE ON FLAP POWER DDRIVE UNTI, CLEANED AND REINSTALLED.

Part: HEATER — MALFUNCTIONED (COCKPIT WINDOW) · airframe 4,310 hrs · 4,456 cycles

LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED THE LEFT SIDE WINDOW.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 4,193 hrs · 4,324 cycles

STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 4,073 hrs · 4,204 cycles

OVERHEAD CABIN EMERGENCY LIGHT INOP. REPLACED EMERGENCY BATTERY.

Part: CONTROL UNIT — MALFUNCTIONED (NLG STEERING) · airframe 4,011 hrs · 4,134 cycles

NWS INOP CAUTION MESSAGE. C/W RIGGING OF NWS SYSTEM TO M/M SPECS.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 3,935 hrs · 4,064 cycles

F.S. 718.00 AFT DOUBLER IS CRACKED LEFT HAND SIDE P/N 600-36030-31.REMOVED AND REPLACED AFT DOUBLER AT F.S. 718 LEFT SIDE IAW CANADAIR REO 601R-53-61-193 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 3,935 hrs · 4,064 cycles

THE FUSELAGE SKIN IS DENTED AFT OF PILOTS SIDE WINDOW. REPAIRED DENT IN FUSELAGE SKIN BY TRIMMING OUT DAMAGED AREA, FABING EXTERNAL DOUBLER, FILLER AND INSTALLING I/A/W W.V.A.C. E.O. 601R-53-1985.

Part: PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 3,656 hrs · 3,791 cycles

TAKEOFF CONFIG WARNING. REPLACED THE RUDDER TRIM SWITCH PANEL.

Part: HANDLE — FAILED (FLAP CONTROL) · airframe 3,375 hrs · 3,520 cycles

FLAP FAIL CAUTION MESSAGE DURING FLIGHT WHEN SELECTED TO 27 DEGREES. REPLACED THE FLAP CONTROL HANDLE ASSEMBLY.

Part: POWER UNIT — MALFUNCTIONED (TE FLAP) · airframe 2,632 hrs · 2,716 cycles

FLAPS FAIL MESSAGE. REPLACED THE FLAP POWER DRIVE UNIT.

Part: FCU — MALFUNCTIONED (E/E BAY) · airframe 2,499 hrs · 2,585 cycles

FLAPS FAIL MESSAGE. REPLACED THE FECU.

Part: BPSU — MALFUNCTIONED (RIGHT) · airframe 2,324 hrs · 2,406 cycles

FLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU.

Part: APU — SMOKE (APU BAY)

FIRE DEPARTMENT NOTIFIED CREW OF WHITE SMOKE COMING FROM THE RIGHT HAND ENGINE AREA. CREW REPORTED ALL INDICATIONS IN COCKPIT WERE NORMAL. CREW HAD JUST STARTED THE APU. INSPECTION OF APU AND ENGINE FOUND NO PROBLEM. AIRCRAFT RETURNED TO SERVICE.

Part: FECU — MALFUNCTIONED (TE FLAPS)

NWS CAUTION MESSAGE DURING FLIGHT. REPLACED THE FECU.