N945CA

Part: CYLINDER — FAILED (UNKNOWN) · airframe 1,660 hrs · 1,326 cycles

PILOT REPORTED BLACK AND GREY SMOKE FROM RIGHT ENGINE EXHAUST. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE #5 CYLINDER OIL SOAKED. CYLINDER WAS REPLACED.

Part: SKIN — DENTED (CABIN DOOR) · airframe 15,092 hrs · 14,734 cycles

FUSELAGE SKIN AT FS310.0 NEAR PAX DOOR HAS TEMPORARY REPAIR THAT REQUIRES PERMANENT REPAIR.PERFORMED A PERMANENT MAJOR REPAIR TO FUSELAGE SKIN AT FS 310.0 I/A/W CRJ REO 601R-53-21-180 AND WVAC EO 601R-53-2832.

Part: WEB — CRACKED (AFT EQUIPMENT BA) · airframe 15,092 hrs · 14,734 cycles

ENGINE SUPPORT BEAM UPPER PLATE AT RBL3 HAS A CRACK GOING FROM THE AFT EDGE INTO A RIVET HOLE.PERFORMED A TEMPORARY MAJOR REPAIR TO CENTER ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-345 REV B.

Part: LIGHT · airframe 14,566 hrs · 14,182 cycles

EMERG LIGHTS ILLUMINATED WITH SWITCH IN AUTO POSITION.FOUND CANNON PLUG JB-6 DISCONNECTED. SECURED CONNECTOR AND SYSTEM TEST NORMAL.

Part: BUSHING — SCORED · airframe 14,501 hrs · 14,103 cycles

FOUND 3 EACH VERTICAL TO HORIZONTAL PIVOT POINT BUSHINGS TO BE SCORED.REMOVED HORIZONTAL STAB ASSY. REMOVED THE DAMAGED BUSHINGS. INSTALLED 3 EACH NEW BUSHINGS AND FINAL REAMED. REINSTALLED SAME HORIZONTAL STAB ASSEMBLY. ALL WORK WAS PERFORMED I/A/W CRJ AMM AND WVAC E.O. #601R-55-2509A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,501 hrs · 1,410 cycles

LEFT AND RIGHT FS 484 ANGLES ARE CRACKED. REPAIRED LEFT AND RIGHT FS 484 ANGLES IAW WVAC EO 601R-53-2507.

Part: VANE — CHAFED (T/E FLAP) · airframe 14,501 hrs · 14,103 cycles

RT INBOARD FLAP VANE CHAFED BEYOND LIMITS. REPAIRED RIGHT INBOARD FLAP VANE IAW AERODESIGN REPORT 1286.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,912 hrs · 13,510 cycles

FLOOR PATH EMERGENCY LIGHTS ROW 5 FORWARD ARE INOPERABLE.REPLACED THE LAMP.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 13,609 hrs · 13,213 cycles

LEFT ENGINE T/R UNLOCKED CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM, NO DEFECTS FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (STALL WARNING) · airframe 13,293 hrs · 12,910 cycles

STALL FAIL AND CONFIG SPOILERS WARNING DURING TAKEOFF. CYCLED CIRCUIT BREAKER, COULD NOT DUPLCIATE. SYSTEM TEST NORMAL.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 13,071 hrs · 12,682 cycles

PASSENGER DOOR SUPPORT ANGLE (P/N 601R-31527-221) CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR BY REPLACING PASSENGER DOOR SUPPORT ANGLE IAW WVAC EO 601R-53-1597.

Part: PLATE — MISMANUFACTURED (FS 449) · airframe 13,071 hrs · 12,682 cycles

WHILE PERFORMING S/B 601R-53-037 TITANIUM FLOORBEAM MOD, FOUND STRAPS 2 EA P/N 601R-31030-7715 ARE MANUFACTURED INCORRECTLY. FABRICATED NEW DOUBLER PLATES FROM 7075 T6 IAW WVAC EO 601R-53-1603.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

THE RIGHT HAND SIDE FUSELAGE SKIN WAS SCRATCHED AND WAS SLIGHTLY DENTED AT FS 409+16 STR 20. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 409+16 STR 20 BY RE-CONTOURING TO NEAR ORIGINAL CONTOUR IAW WVAC EO 601R-53-1600.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

THE RIGHT HAND FUSELAGE SKIN WAS SCRATCHED AND WAS SLIGHTLY DENTED AT FS 409+16 STR 25. PERFORMED A MAJOR REPAIR BY RE-CONTOURING TO NEAR ORIGINAL CONTOUR FUSELAGE SKIN AT FS 409+16 STR 25 IAW WVAC EO 601R-53-1601.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

PAX DOOR SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED ANGLE AND FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R0-53-1597.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

FS 280 FORWARD J ANGLE CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW SERVICEABLE J ANGLE IAW WVAC EO 601R-53-1596.

Part: O-RING — LEAKING (SCAVANGE PUMP) · airframe 13,107 hrs · 12,719 cycles

RIGHT HAND ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED THE O-RING ON A SUMP LUB SCAVANGE PUMP.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 13,071 hrs · 12,682 cycles

THE FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 HAS A 2 INCH CRACK, APPROXIMATELY 1 - 2 INCHES TO THE RIGHT OF FLOOR SUPPORT AT RBL 9.0. PERFORMED A MAJOR REPAIR TO CRACKED FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 IAW WVAC EO 601R-53-1589.

Part: BEAM — CUT (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

THE TRANSVERSE BEAM WAS CUT AT THE LOWER FLANGE AT FS 379 LBL 9 DURING INCORPORATION OF SB 601R-53-037 REV A. PERFORMED A MAJOR REPAIR TO TRANSVERSE BEAM AT FS 379 LBL 9 IAW WVAC EO 601R-53-1599.

Part: BEAM — CUT (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

TRANSVERSE BEAM AT FS 295 AT RBL 9 WAS GROUND INTO WHEN REMOVING FLOORBEAM RBL 9 DURING ACCOMPLISHMENT OF SB 601R-53-027. REPAIRED BEAM IAW WVAC EO 601R-53-1591.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

THE FWD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-1596.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

THE AFT J-CHANNEL AT FS 280.0 IS CORRODED AT BL 0. PERFORMED A MAJOR REPAIR TO CORRODED AFT J-CHANNEL AT FS 280.0 BL 0.0 IAW WVAC EO 601R-53-1588.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,071 hrs · 12,682 cycles

FUSELAGE DAMAGED AT FS 310 AT PAX DOOR. REPAIRED DAMAGED FUSELAGE SKIN AT LOWER LEFT PAX DOOR IAW REO 601R-53-21-180 REV NC.

Part: SIGN — BROKEN (CABIN) · airframe 12,904 hrs · 12,490 cycles

EXIT SIGN AT SERVICE DOOR IS BROKEN. REPLACED EXIT SIGN.

Part: CONTROL UNIT — INOPERATIVE (STAB TRIM) · airframe 12,449 hrs · 12,027 cycles

STABILIZER AND MACH TRIM INOP. CYCLED AIRCRAFT POWER, SYSTEM TEST SATISFACTORY. COULD NOT DUPLICATE.

Part: FLANGE — BENT (PAX DOOR) · airframe 12,290 hrs · 11,860 cycles

PASSENGER DOOR SEAL STRIKER AT FS 310.0 LT, STR 15 - 16 DAMAGED BY IMPACT WITH PASSENGER DOOR LOCK PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR SEAL STRIKER AT FS 310.0 LT BETWEEN STR 15 - 16 IAW CRJ REO 601R-52-11-008 REV B.

Part: BRACKET — DAMAGED (NLG)

NLG DID NOT RETRACT. REPLACED THE NLG WOW AND CENTERED PROXIMITY BRACKET.

Part: ACTUATOR — FAILED (TE FLAP)

FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTBOARD OUTER FLAP ACTUATOR.

Part: ACTUATOR — FAILED (TE FLAP)

FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTER FLAP INBOARD ACTUATOR.

Part: FRAME — CRACKED (BS 718)

FRAME AT FS 718.00 HAD A TEMPORARY REPAIR PER WVAC EO 601R-53-0056B ON THE FRAME PREVIOUSLY INSTALLED. PERFORMED A PERMANENT MAJOR REPAIR TO CRACKED FRAME FLANGE AT FS 718.00 STR 11 LHS IAW WVAC EO 601-53-0347.

Part: ENGINE — FAILED (RIGHT)

ON CLIMBOUT, RIGHT ENGINE OIL PSI MESSAGE ON ED-1 SHUT DOWN NR 2 ENGINE. DROPPED TO 22 PSI. FOUND SKYDROL IN ACCESSORY GEARBOX. REMOVED AND REPLACED RIGHT ENGINE.

Part: ENGINE — FAILED (RIGHT)

IDG NR 2 CAUTION MESSAGE, FOLLOWED BY GEN NR 2 CAUTION MESSAGE ON TAKEOFF. IDG NR 2 CAUTION MESSAGE WENT OUT DURING ABORT. NR 2 GEN WAS RESET. FOUND SKYDROL IN ACCESSORY GEARBOX OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE.

Part: STRINGER — CRACKED (BS 718)

DOUBLER AFT OF FS 718 HAS APPROX 4 INCH CRACK IN RADIUS AT STRINGER 11. REPAIRED PER WVAC EO NR 601R-53-0058.

Part: SHIELD — CRACKED (APU COMPT)

APU EXHAUST SHIELD HAS A CRACK AT THE 7 O'CLOCK POSITION. REPAIRED PER CANADAIR REO 601R-49-81-003.

Part: FRAME — CRACKED (BS 718)

FRAME FLANGE AT FS 718 LT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES JUST BELOW STRINGER 11. TEMPORARILY REPAIRED IAW WVAC EO 601R-53-00560. MUST BE PERMANENTLY REPAIRED NO LATER THAN NEXT C-CHECK.

Part: FRAME — CRACKED (BS 718)

FRAME FLANGE AT FS 718 RT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES. REPAIRED PER WVAC EO 601R-53-0057.

Part: PCU — LEAKING (RT AILERON)

RIGHT AILERON OUTBOARD PCU LEAKING BEYOND LIMITS. REPLACED PCU.

Part: DUCT — BROKEN (APU EXHAUST)

APU EXHAUST DUCT HAS SEVERAL BROKEN FINGER CLAMP STOPS. REPLACED EXHAUST DUCT.

Part: STRIKER — CRACKED (PASSENGER DOOR)

PAX DOOR SEAL STRIKER AT FS 349 IS DAMAGED. REPAIRED PER REO 601R-52-11-00 REPAIR A.

Part: BRACKET — MISSING (CARGO DOOR)

CARGO DOOR STOP BRACKET IS MISSING. INSTALLED CARGO DOOR STOP BRACKET.

Part: STRIKER — CRACKED (PASSENGER DOOR)

PAX DOOR SEAL STRIKER AT FS 3100 PREVIOUS REPAIR IS DAMAGED. REPAIRED PER REO 601R-52-11-008, REPAIR C.

Part: CAP — CHAFED (RT TE FLAP)

RIGHT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS.

Part: CAP — CHAFED (LT TE FLAP)

LEFT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS.

Part: FUEL — LEAKING (LEFT, RIGHT WING)

FLUID LEAKING FROM LEFT AND RIGHT WINGS AT THE FUEL VENT AREA. INSPECTED AIRCRAFT FOR FUEL LEAKS AND NONE FOUND.

Part: RETRACT SYST — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AT 8 DEGREES. RESET FLAPS PER AD 98-20-01. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (BS 599)

DAMAGE FOUND BY CREW ON POST FLIGHT INSPECTION. DENT BELOW CARGO DOOR AREA AT FS 599.00 AND STRINGER 22L AND 23 DENT WAS .098 DEEP, WITH A GOUGE OF .015. DAMAGED AREA WAS REMOVED AND REPAIRED IN ACCORDANCE WITH CRJ SRM 53-00-31.

Part: LIGHT — DIM (CABIN)

EMERGENCY FLOOR LIGHTING IS DIM, AFT CABIN AREA. REPLACED AFT TRACK LIGHT ASSY.

Part: PCU — MALFUNCTIONED (LT SPOILERS)

CONFIG SPOILERS WARNING DURING TAKEOFF. REPLACED LEFT HAND OUTBOARD SPOILERON PCU.

Part: ACTUATOR — MALFUNCTIONED (AILERON TRIM)

CONFIG TRIM WARNING DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE AILERON TRIM ACTUATOR FOR TROUBLESHOOTING.

Part: LIGHT — OVERHEATED (GALLEY)

STRONG ELECTRICAL ODOR DETECTED BY CREW DURING TAXI. REPLACED THE GALLEY WORK LIGHT ASSY.

Part: ELECTRICAL — ODOR (COCKPIT)

BURNING ELECTRICAL SMELL IN COCKPIT. COULD NOT DUPLICATE DISCREPANCY. POWERED ALL SYSTEMS ON AIRCRAFT AND COULD DETECT BURNING ODOR.

Part: VALVE SEAL — MISSING (PRESS MANIFOLD)

LANDING GEAR RETRACTION TIME WAS 3 TIMES LONGER THAN NORMAL. REPLACED MISSING SEAL ON THE PRESSURE MANIFOLD RELIEF VALVE.

Part: TR UNIT — MALFUNCTIONED (RT ENGINE)

ON CLIMBOUT, RT THRUST REVERSER UNLOCKED MSG CAME ON. REV DID NOT DEPLOY. DEFERRED RT T/R I/A/W MEL 78-30-1 CAT B.

Part: TR UNIT — MALFUNCTIONED (RT ENGINE)

RT ENGINE THRUST REVERSER UNLOCKED MESSAGE ON EICAS DURING TAKEOFF. SECURED THRUST REVERSER CLOSED AND TRANSFERRED DISCREPANCY TO DEFERRED MAINTENANCE LIST.

Part: TR UNIT — MALFUNCTIONED (RT ENGNE)

RT ENGINE THRUST REVERSER UNLOCKED MESSAGE ON EICAS. SECURED THRUST REVERSER CLOSED AND TRANSFERRED TO DEFERRED MAINTENANCE LIST.

Part: SKIN — BIRD STRIKE (FWD FUSELAGE)

BIRD STRIKE JUST FORWARD OF COPILOTS WINDSHIELD. C/W BIRD STRIKE INSPECTION, NO DAMAGE FOUND AND AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (RT TE FLAP)

FLAPS FAILED AFTER TAKEOFF. REPLACED THE RT WING FLAP SYSTEM WIRING HARNESS.

Part: SENSOR — MALFUNCTION (TE FLAPS)

FLAPS FAILED DURING CRUISE. REPLACED THE FLAP BRAKE AND POSITION SENSOR.

Part: COMPUTER — FAILED (STALL WARNING)

STALL FAIL MESSAGE ON EICAS. REPLACED THE STALL PROTECTION COMPUTER.

Part: CONTROL CABLE — LACK OF LUBE (AILERON CONTL)

PILOTS AILERON CONTROLS SEEM TO BE EITHER LOOSE OR BINDING. INSPECTED AILERON CONTROL PATH AND FOUND NO DEFECTS. CLEANED AND LUBED AILERON CABLE PATH.

Part: WIRE — CHAFED (FUEL PRESSURE)

LEFT ENGINE LOW FUEL PRESSURE MESSAGE ON EICAS. REPAIRED CHAFED WIRING IN AFT EQUIPMENT BAY AND ACFT RETURNED TO SERVICE.