N991CA

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 21,111 hrs · 19,774 cycles

FLIGHT 5163 - EMERGENCY FLOOR LIGHTING FROM ROW 6 TO 8 IS INOPERATIVE. REPLACED BROKEN CABLE SECTIONS IN CABIN AT ROW 12 AND ROW 8 WITH SERVICEABLE CABLES.

Part: CAUTION MESSAGE — ILLUMINATED (TE FLAP SYSTEM) · airframe 20,531 hrs · 19,310 cycles

FLIGHT 5469 - FLAPS FAIL CAUTION MESSAGE AT 18 DEGREES. 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: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,205 hrs · 19,028 cycles

FLIGHT 5108 - FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM IAW EO 27-045 AND DEFERRED PER MEL GMM 5-2 CAT I.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,138 hrs · 18,973 cycles

FLIGHT 5000 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES. 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: FLAP — MALFUNCTIONED (WING) · airframe 20,111 hrs · 18,955 cycles

FLIGHT 5224 - DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES, CREW DECLARED AN EMERGENCY AND 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 — UNRELIABLE (TE FLAPS) · airframe 19,837 hrs · 18,728 cycles

FLIGHT 5667 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU.

Part: PRIORITY VALVE — UNRELIABLE (NLG) · airframe 18,790 hrs · 17,817 cycles

FLIGHT 5454 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.

Part: PSEU — MALFUNCTIONED (LG) · airframe 18,465 hrs · 17,524 cycles

GEAR DISAGREE WARNING DURING TAXI. REPLACED PSEU FOR TROUBLESHOOTING.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,537 hrs · 14,140 cycles

FLIGHT 5530 FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE NR 2 INVERTER.

Part: RESERVOIR — MALFUNCTIONED (NR 3 HYS SYS) · airframe 14,499 hrs · 14,107 cycles

FLIGHT 5898 GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR.

Part: IDG — LACK OF LUBE (NR 1 GENERATOR) · airframe 14,365 hrs · 13,985 cycles

FLIGHT 5251 IDG NR 1 FAULT MESSAGE DURING T/O. SERVICED THE IDG OIL SYSTEM.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 14,204 hrs · 13,858 cycles

FLIGHT 5230 NLG FAILED TO EXTEND, USED EMERGENCY RELEASE SYSTEM. COULD NOT DUPLICATE. REPLACED NLG PRIORITY VALVE FOR TROUBLESHOOTING.

Part: ELEMENT — FALSE INDICATION (LEFT ENGINE) · airframe 13,473 hrs · 13,272 cycles

FLT 5051 LT ENGINE FIRE WARNING DURING TAXI. REPLACED THE LT ENGINE FIRE LOOP-B.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 13,261 hrs · 13,098 cycles

FLIGHT 5188 GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A.

Part: OIL SYSTEM · airframe 10,368 hrs · 10,555 cycles

FLIGHT 5736 R/H ENGINE OIL PRESSURE WARNING DURING T/O.COULD NOT DUPLICATE. OIL PRESSURE INDICATIONS NORMAL DURING MAINT. RUNS.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 9,911 hrs · 10,101 cycles

FLIGHT 5294 GEAR DISAGREE WARNING DURING RETRACION.REPLACED THE MLG SELECTOR VALVE.

Part: SPOILER · airframe 9,880 hrs · 10,075 cycles

FLIGHT 5535 CONFIG SPOILERS CAUTION DURING T/O.FOUND SPOILER LEVER AJAR - RESET LEVER AND SYSTEM TEST NORMAL.

Part: BUSHING — CRACKED (STABILIZER) · airframe 9,124 hrs · 9,318 cycles

HORIZONTAL STABILIZER ATTACH FITTING R.H. PIVOT PIN BUSHING LOOSE.REPLACED BUSHING I/A/W S.B. 601R-55-007 STEP 4 PAGE 51 THROUGH STEP 15 PAGE 64 AND REO 601R-55-31-036.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 9,124 hrs · 9,318 cycles

RH HORIZ STAB VISOR FITTING CRACKED.INSTALLED NEW SERVICEABLE FITTING.I/A/W REO 601R-55-11-016 AND SRM 51-42-06.

Part: ENGINE — FAILED (RIGHT) · airframe 9,121 hrs · 9,317 cycles

FLIGHT 5266 - DURING CLIMBOUT OF ATW RECEIVED ABNORMAL VIBRATION FROM THE RIGHT ENGINE. CREW DECLARED AN EMERGENCY AND PERFORMED AN IFSD. REPLACED THE RIGHT ENGINE ASSY.

Part: LAMP — BURNED OUT (ROW 5) · airframe 8,459 hrs · 8,622 cycles

EMERGENCY CEILING LIGHT AT ROW 5 IS INOP.REPLACED THE LIGHT BULB.

Part: ANGLE — CRACKED · airframe 7,758 hrs · 7,903 cycles

VERTICAL "J" ANGLE CLIP INSIDE CBPI @BL 9.0 L/H IS CRACKED.INSTALLED NEW "J" ANGLE CLIP P/N #600-34017-723 I/A/W WVAC E.O. #601R-53-2543A.

Part: ANGLE — CRACKED · airframe 7,758 hrs · 7,903 cycles

VERTICAL "J" ANGLE CLIP INSIDE CBPI @BL 9.0 LEFT HAND IS CRACKED.INSTALLED NEW "J" ANGLE CLIP P/N #600-34017-723 I/A/W WVAC E.O.#601R-53-2543A.

Part: ANGLE — CORRODED · airframe 7,758 hrs · 7,903 cycles

THE FWD "J" ANGLE @ F.S. 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED.REMOVED AND REPLACED "J" ANGLE I/A/W WVAC E.O. #601R-53-2540 REF MAN LOG PAGE 405333. WORK PERFORMED UNDER COMAIR W/O #169657.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 7,739 hrs · 7,885 cycles

RUDDER TRIM WENT FULL NOSE LEFT UNCOMMANDED. REPLACED THE RUDDER TRIM SWITCH PANEL.

Part: BRAKE — LEAKING (LT MLG) · airframe 7,715 hrs · 7,856 cycles

SMOKE COMING FROM LT MLG. REPLACED THE LT OUTBOARD BRAKE ASSY.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,567 hrs · 7,785 cycles

FLOOR SUPPORT ANGLE AT FS 621.0 WL 72 RBL 27 RBL 42 CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED FLOOR SUPPORT ANGLE AT FS 621.0 RBL 27 - RBL 42 IAW CRJ REO 601R-53-61-117 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,567 hrs · 7,780 cycles

FS 718 RT FRAME IS CRACKED. ROUTED OUT DAMAGE. INSTALLED DOUBLER AND RADIUS BLOCKS AND FWD DOUBLER IAW CANADAIR REO 601R-53-61-193 REV A.

Part: CONTROL UNIT — LOOSE (E/E BAY) · airframe 7,169 hrs · 7,326 cycles

MULTIPLE FAILURES, ELEC HYD. PRESSURE, FLIGHT CONTROLS, APU PUMP, FUEL PUMP, AUTO PILOT, AND PROX SYSTEM FAIL.FOUND JB 10 LOOSE, SECURED JB-10. ALL SYSTEM OPS NORMAL.

Part: RADAR — FAILED (E/E BAY) · airframe 5,687 hrs · 5,843 cycles

WEATHER RADAR FAILED. REPLACED THE RTA-844.

Part: FLOORBEAM — CRACKED (BS 621)

FS 621.00 FLOOR SUPPORT STRUCTURE CRACKED BETWEEN LBL42 AND LBL9 W.L. 73 LEFT SIDE. REPAIRED FS 621.00 FLOOR SUPPORT STRUCTURE LEFT SIDE I/A/W CANADAIR REO 601R-53-61-117 REV A.

Part: SKIN — DAMAGED (BS 310)

SKIN FORWARD OF MAIN CABIN DOOR BY LOWER LOCKING PIN DAMAGED FS 310 STR 15 AND 16R. REPAIRED SKIN DAMAGE FS 310 BETWEEN STRINGER 15 AND 16 IAW REO 601R-53-21-160 AND WVAC EO 601R-53-1014.

Part: TILLER — MISRIGGED (COCKPIT)

STEERING INOPERATIVE MESSAGE APPEARED AFTER TAKEOFF FROM MCO, AIRCRAFT RETUREND TO THE FIELD. RE-CENTERED THE STEERING TILLER.

Part: ENGINE — FAILED (LEFT)

LEFT ENGINE ITT 880 DEGREES, VIB 4.0 IFSD. REPLACED LEFT HAND ENGINE.

Part: PDU — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED DURING LANDING. REPLACED THE PDU.

Part: BRACKET — BENT (NLG)

NLG DISAGREE MESSAGE. REPLACED THE NLG CENTERING PROXIMITY SWITCH BRACKET.

Part: BULB — FAILED (EMERGENCY EXIT)

OVERWING EMERGENCY EXIT SIGN IS INOPERABLE. REPLACED LIGHT BULB.

Part: AIR DIST — ODOR (GALLEY)

SMOKE SMELL FROM GALLEY AREA. COULD NOT DUPLICATE. INSPECTED GALLEY AREA AND FOUND NO DEFECTS.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

CARGO SMOKE WARNING, FIRE BOTTLES DISCHARGED. FALSE WARNING. REPLACED FIRE BOTTLES AND SMOKE DETECTORS.

Part: TUBING — FAILED (NR 3 HYD SYST)

AFTER FLT DEPT CAE, NR 3 HYDRAULIC QUANTITY READ ZERO. NOSE GEAR INDICATED DOWN, ONE MAIN INDICATED UP, THE OTHER MAIN INTRANSIT. CREW EXTENDED GEAR MANUALLY. FLT DECLARED AN EMERGENCY AND DIVERTED BACK TO CAE. FLT LANDED IN CAE WITHOUT FURTHER INCIDENT. INSTALLED NEW HYD TUBING (P/N 600-75226-60), (S/N 1307718), PERFORMED LEAK CHECK AFTER SWAGING. NO DISCREPANCIES NOTED.

Part: CONNECTOR — DIRTY (RT ECU)

UNCOMMANDED ACCELERATION RIGHT HAND ENGINE DURING CRUISE FLIGHT. CLEANED WIRING CONNECTOR AT ENGINE ECU.

Part: PIN — INSTALLED (MLG)

LANDING GEAR WOULD NOT RETRACT DURING CLIMB OUT, AIRCRAFT RETURNED TO THE FIELD. REMOVED GEAR DOWN LOCK PINS FROM MLG.