N979CA

Part: SPRING — MISSING (DOOR HANDLE) · airframe 24,043 hrs · 21,354 cycles

FLIGHT 5819 - CABIN DOOR WARNING. REPLACED MISSING SPRING ON OUTER HANDLE LATCH BUTTON.

Part: SELECTOR VALVE — UNRELIABLE (NLG) · airframe 20,304 hrs · 19,426 cycles

FLIGHT 5839 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 20,244 hrs · 19,374 cycles

FLT 5035 RECEIVED A GEAR DISAGREE CAUTION DURING CLIMBOUT OF CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED THE NLG PRIORITY VALVE.

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 20,244 hrs · 19,374 cycles

FLIGHT 5035 RECEIVED A GEAR DISAGREE CAUTION DURING CLIMBOUT OF CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED THE MLG PRIORITY VALVE.

Part: WARNING LIGHT — ILLUMINATED (APU BAY) · airframe 20,142 hrs · 19,288 cycles

FLIGHT 5106 DURING CRUISE FLIGHT RECEIVED AN APU OIL TEMPERATURE CAUTION MESSAGE, EXECUTED QRH PROCEDURE AND DIVERTED TO CMH. INTERROGATED APU ECU, INSPECTED OIL LEVEL AND CHECKED FOR LEAKS, OPERATED APU WITH NO FAULTS.

Part: COMPENSATOR — FAILED (COCKPIT) · airframe 19,759 hrs · 18,946 cycles

FLIGHT 5713 DURING CLIMBOUT OF CVG RECEIVED MULTIPLE EFIS COMP MON MESSAGES AND ALL COMPASSES WERE UNREADABLE. AIRCRAFT RETURNED TO CVG. PERFORMED FULL RECOMPENSATION OF NR 1 AND NR 2 REMOTE COMPENSATING UNITS.

Part: PRIORITY VALVE — UNRELIABLE (NLG) · airframe 19,593 hrs · 18,802 cycles

FLIGHT 5452 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.

Part: PUMP — MALFUNCTIONED (NR 2 HYD SYSTEM) · airframe 18,780 hrs · 18,075 cycles

FLIGHT 5361 NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION. REPLACED THE RT EDP.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 18,365 hrs · 17,740 cycles

FLIGHT 5391 AHRS FAILURE DURING TAKEOFF. REPLACED THE NR 1 AHRS.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 16,979 hrs · 16,583 cycles

FLIGHT 5745 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: CAP — CHAFED (T/E FLAP) · airframe 16,389 hrs · 16,090 cycles

RIGHT INBOARD FLAP LEADING EDGE VANE MIDDLE CAP P/N 601R14303-52 IS CHAFED .017 INCH AT FLAP STATION 60. REMOVED AND REPLACED CAP P/N 601R14303-52 IAW CRJ 200 SRM 51-42-10.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 16,389 hrs · 16,090 cycles

RIGHT FORWARD SIDE OF FS 621 BULKHEAD IS CHAFED AT FOUR LOCATIONS. REMOVED FASTENERS, BLENDED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION, ALODINED AND INSTALLED FASTENERS IAW WVAC EO 601R-53-4466.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 16,390 hrs · 16,090 cycles

THE RT FORWARD SIDE OF THE AFT PRESSURE BULKHEAD AT FS 621 IS CHAFED .012 INCH DEEP X .150 INCH WIDE AT RBL 36, WL 103. THE DAMAGE WAS CAUSED FROM BAGGAGE BAY LINER HARDWARE BEING TOO LONG. THE DAMAGED AREA WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW WVAC EO 601R-53-4465.

Part: DOUBLER — CRACKED (FUSELAGE FRAME) · airframe 16,390 hrs · 16,090 cycles

RIGHT SIDE FS 718.0 AFT FRAME DOUBLER IS CRACKED. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER P/N 600-36030-32 IAW BOMBARDIER, INC REO 601R-53-61-193 REV A.

Part: COMPUTER — MALFUNCTIONED (TE FLAPS) · airframe 15,365 hrs · 15,235 cycles

FLIGHT 5158 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.

Part: FLAP · airframe 12,739 hrs · 12,873 cycles

FLIGHT 5270 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: LAMP — INOPERATIVE (CABIN) · airframe 12,523 hrs · 12,666 cycles

FLIGHT 5089 1ST SECTION OF EMERGENCY FLOOR LIGHTING IS INOP.REPLACED 1ST SECTION OF FLEXIBLE LAMP.

Part: PYLON — CORRODED (EMPENNAGE) · corrosion level 2 · airframe 12,377 hrs · 12,506 cycles

DURING REMOVAL OF THE LEFT ENIGNE ASSEMBLY, DISCOVERS FRETTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB 6 TO 2 O'CLOCK POSITION ON FWD SIDE.REPAIRED IN ACCORDANCE WITH 601R-54-50-044.

Part: CONNECTOR — FAULTY (CARGO) · airframe 11,515 hrs · 11,655 cycles

FLIGHT 5838 CARGO FIRE BOTTLE LOW MESSAGE.REPAIRED WIRING CONNECTOR AT FIRE BOTTLE.

Part: BATTERY — WEAK (CABIN) · airframe 10,407 hrs · 10,562 cycles

FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.

Part: BATTERY — WEAK (CABIN) · airframe 10,407 hrs · 10,562 cycles

FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.

Part: BATTERY — WEAK (CABIN) · airframe 10,407 hrs · 10,562 cycles

FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.

Part: BATTERY — WEAK (CABIN) · airframe 10,407 hrs · 10,562 cycles

FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.

Part: SKIN — CORRODED (WS95.950) · corrosion level 2 · airframe 10,406 hrs · 10,553 cycles

R/H LOWER WING FUEL TANK ACCESS HOLE (640DB) HAS CORROSION ON FORWARD AND AFT CUT-OUT AREAS.REPAIRED R/H LOWER WING FUEL TANK ACCESS HOLE (640DB) I/A/W CANADAIR R.E.O. 601R-57-21-148 AND 601R-57-21-030 REV A.

Part: DOUBLER — CORRODED (310.00) · corrosion level 2 · airframe 10,406 hrs · 10,553 cycles

THE DOUBLER PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED DOUBLER AND REPLACED I/A/W WVAC E.O. 601R-53-2732.

Part: ANGLE — CORRODED (FLOOR) · corrosion level 2 · airframe 10,406 hrs · 10,553 cycles

FWD/AFT J-ANGLE AT FS280 HAS CORROSION, FLOOR BEAM WEB AT FS280 HAS CORROSION.REPAIRED FWD/AFT J-ANGLES AND FLOOR BEAM WEB I/A/W WVAC EO 601R-53-2731, 601R-53-2733, 601R-53-2734.

Part: PCU — FAULTY (ELECTRICAL BAY) · airframe 10,175 hrs · 10,321 cycles

AFTER PUSH BACK AT CVG, SPOILERS FAULT STATUS MESSAGE WOULD NOT EXTINQUISH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE FLIGHT SPOILER POWER CONTROL UNIT.

Part: WEB — CRACKED · airframe 10,110 hrs · 10,256 cycles

LEFT SIDE LOWER WEB OF ENG SUPPORT HAS 1.5 INCH CRACK AT FS 635, LBL 42, WL 111.09COMPLIED WITH REO 601R-53-61-366 REV B BY CUTTING AWAY DAMAGED SECTION NDT INSP AND INSTALLING FABRICATED REPAIR PARTS I/A/W REO 601R-53-61-366 REV B.

Part: ECU — FAILED (EE BAY) · airframe 9,875 hrs · 10,033 cycles

STEERING INOP CAUTION MESSAGE. REPLACED THE STEERING ECU.

Part: CONNECTOR — DIRTY (CABIN) · airframe 9,857 hrs · 10,015 cycles

FORWARD FLOOR EMERGENCY LIGHT IS INOP. CLEANED CONNECTION, LIGHT OPERATION IS NORMAL.

Part: COMPUTER — MALFUNCTIONED (SPOILERS) · airframe 9,553 hrs · 9,711 cycles

CONFIG SPOILERONS WARNING DURING T/O. COULD NOT DUPLICATE. FOUND NO FAULT CODES IN COMPUTER.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 9,011 hrs · 9,139 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,539 hrs · 8,637 cycles

EMERGENCY LIGHTS AT ROW 8 ARE INOPERABLE. REPLACED FLOOR LIGHTING CABLE ASSY.

Part: STRUCTURE — BIRD STRIKE (FUSELAGE) · airframe 8,454 hrs · 8,546 cycles

BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION, NO DAMGE FOUND.

Part: SENSOR — OUT OF ADJ (LT MLG) · airframe 8,408 hrs · 8,491 cycles

GEAR DISAGREE WARNING, LEFT HAND MLG INTRANSIT. ADJUSTED THE LEFT HAND MLG UPLOCK PROXIMITY SENSOR.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 8,296 hrs · 8,386 cycles

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

Part: DOOR — NOISY (MAIN CABIN) · airframe 7,817 hrs · 7,907 cycles

CREW HEARD LOUD SQUEALING NOISE THAT INCREASED WITH SPEED AND ALTITUDE. CHECKED CABIN DOOR FOR PROPER FIT AND OPERATION. COULD NOT DUPLICATE. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,798 hrs · 7,886 cycles

EMERGENCY LIGHT IS INOPERABLE IN THE AFT CABIN AREA. REPLACED THE LIGHT BULB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,704 hrs · 7,771 cycles

FRAME AT FS 718.00 HAS CRACK IN RADIUS AND CRACKED AFT DOUBLER BETWEEN STR 11 AND 12 BOTH LHS & RHS OF AIRCRAFT. FS 718.00 RIGHT AND LEFT SIDES, BETWEEN STRINGERS 11 AND 12, REPAIRED CRACK IN FRAME FLANGE AND REPLACED CRACK DOUBLERS WITH NEW SERVICEABLE DOUBLERS IAW CANADAIR REO 601R-53-61-193-REV A.

Part: APU — MALFUNCTIONED (TAIL)

TOILET SMOKE CAUTION MESSAGE. FOUND SMOKE SOURCE TO BE THE APU. DEFERRED APU PER MEL.

Part: SKIN — DAMAGED (BS 310 STR 16-17)

FWD FUSELAGE SKIN DAMAGED FS 310 STR 16-17 LHS. REPAIRED SKIN IAW WVAC EO 601R-53-1015.

Part: SERVICE DOOR — OPEN (FUSELAGE)

LOUD HIGH PITCH NOISE ON RIGHT HAND SIDE OF COCKPIT. SECURED O2 SERVICE DOOR CLOSED.

Part: SKIN — CRACKED (RT WING)

SEVEN SMALL CRACKS IN THE FORWARD AND AFT HORIZONTAL SURFACES OF RIGHT HAND WING ACCESS HOLE AT PANEL 640DB. REPAIRED CRACKS IAW BOMBARDIER REO NR 601R-57-21-030.

Part: SKIN — CRACKED (WS 95.95)

SEVEN SMALL CRACKS IN THE FWD AND AFT HORIZONTAL SURFACES OF RIGHT HAND WING ACCESS HOLE AT PANEL 640 DB. REPAIRED CRACKS IAW BOMBARDIER REO NR 601R-57-21-030.

Part: AIR DIST — ODOR (COCKPIT)

STRONG BURNING SMELL IN COCKPIT. CLEANED RESIDUAL, COMPRESSOR WAS HOT FROM AIRCRAFT SYSTEM.

Part: SIGN — INOP (EMER EXIT)

LEFT OVERWING EMERGENCY EXIT SIGN IS INOPERABLE. REPLACED EXIT SIGN.

Part: WHEEL — CRACKED (MLG)

MECHANIC REMOVED BOTH MAIN WHEELS FROM A/C 7159 BECAUSE RIGHT O/B TIRE WAS FOUND FLAT. DURING A VISUAL LEAK CHECK IN WHEEL SHOP FOUND SUBASSEMBLY CRACKED AT BOTTOM OF KEY BOSS APPROXIMATELY 1 INCH LONG. WHEEL SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS.

Part: BULB — FAILED (CABIN)

AFT CABIN OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.

Part: VANE — CHAFED (LT TE FLAP)

C-CHECK TASK 27-580-100, LT I/B FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE.

Part: START VALVE — MALFUNCTION (RT ENGINE)

RIGHT ENGINE START MESSAGE CAME ON AFTER TAKEOFF. REPLACED THE ENGINE AIR START VALVE.

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: LAMP — FAILED (CABIN)

ONE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP AND ONE EMERGENCY EXIT SIGN INOP. DRIED WET FLOOR LIGHTING AND REPLACED EXIT SIGN LIGHT BULB.

Part: BPSU — MALFUNCTIONED (LT/RT TE FLAP)

FLAP FAIL CAUTION MESSAGE DURING FLIGHT. REPLACED THE LEFT AND RIGHT BPSU.

Part: STOP ASSY — OUT OF ADJUST (CABIN DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE AFTER TAKEOFF. ADJUSTED THE DOOR STOP ASSY.

Part: DOOR LIGHT — ILLUMINATED (PAX DOOR)

PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY, DOOR OPERATION NORMAL.

Part: WARNING — MALFUNCTIONED (CABIN DOOR)

OUTER DOOR HANDLE UNSAFE MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY. DOOR AND WARNING SYTEM OPERATE NORMAL.