N933CA

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 35,531 hrs · 32,373 cycles

EN ROUTE FROM CVG TO CID RECEIVED HYD 1 LOW MSG, 0 QTY AND PSI. EMERGENCY DECLARED, A/C DIVERTED TO MLI LANDED SAFELY. REMOVED AND REPLACED HYDRAULIC SYSTEM 1 RETURN LINE IN PYLON.

Part: ANTI-ICE VALVE — FAILED (LT COWLING) · airframe 35,397 hrs · 32,273 cycles

EN ROUTE FROM CVG TO EWR RECEIVED LEFT COWL ANTI-ICE CAUTION MSG, WITH COWL ANTI-ICE SWITCHED OFF. EMERGENCY DECLARED, A/C DIVERTED TO PIT LANDED SAFELY. REMOVED AND REPLACED LEFT NOSE COWL ANTI-ICE VALVE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,538 hrs · 31,589 cycles

DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 RT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,538 hrs · 31,589 cycles

DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 LT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557.

Part: CONTROLLER — MALFUNCTIONED (NR 2 ADS) · airframe 33,408 hrs · 30,660 cycles

FLIGHT 5501 - RECEIVED TAT PROBE HEAT, RIGHT AOA HEAT, RIGHT STATIC HEAT AND RIGHT PITOT HEAT CAUTION MESSAGES. RESET NR 2 ADS CONTROLLER. NO FURTHER DEFECTS.

Part: SEALANT — MISSING (FAIRING) · airframe 33,307 hrs · 30,563 cycles

FLIGHT 5451 - UPON FLAP SELECTION TO 8 DEGREES A THUMPING WAS FELT. ABORTED APPROACH, DECLARED EMERGENCY, TOWER VERIFIED GEAR DOWN UPON SELECTION. LANDED WITHOUT INCIDENT. REPLACED MISSING SEALANT TO BELLY AND WING ROOT FAIRINGS. NO FURTHER DEFECTS.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 33,292 hrs · 3,055 cycles

FLIGHT 5236 - RECEIVED GEAR DISAGREE WARNING. RAN QRH, LOWERED GEAR MANUALLY, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. NO FURTHER DEFECTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 32,870 hrs · 30,220 cycles

FLIGHT 5560 - FLAPS FAIL CAUTION MESSAGE DURING APPROACH TO BTV. AIRCRAFT DIVERTED BACK TO JFK AND LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION.

Part: FLAP — MALFUNCTIONED (WING) · airframe 32,616 hrs · 30,034 cycles

FLIGHT 5239 - DURING TAXI OUT FLAPS FAIL CAUTION MESSAGE ILLUMINATED. AIRCRAFT RETURNED BACK TO GATE. 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: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,406 hrs · 29,870 cycles

FLIGHT 4989 - EMERGENCY LIGHT INOP AT PAX DOOR. RELAMPED INOP EMERGENCY LIGHT. NO FURTHER DEFECTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 32,103 hrs · 29,639 cycles

FLIGHT 5459 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. 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: FLAP — MALFUNCTIONED (WING) · airframe 31,906 hrs · 29,483 cycles

FLIGHT 5419 - RECEIVED FLAP FAIL MESSAGE AT GATE. 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 MESSAGES.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 30,941 hrs · 28,733 cycles

FLIGHT 5559 - FLAPS FAIL AT GATE. 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: SENSOR — FAULTY · airframe 30,803 hrs · 28,625 cycles

FLIGHT 5542 - DISPLAY COOK CAUTION MESSAGE RECEIVED. INSPECTED DUCTING, CLEANED FLOW SENSOR CONNECTOR, REPLACED FLOW SENSOR. NO FURTHER DEFECTS.

Part: STRUT — UNDERSERVICED (NLG) · airframe 30,406 hrs · 28,303 cycles

AFTER TAKE-OFF AT APPROXIMATELY 145 KTS, GEAR DISAGREE MESSAGE ILLUMINATED, NOSE GEAR HAD RED HASH MARKS AND AFTER 10 SECONDS NOSE GEAR RETRACTED. AIRCRAFT RETURNED AND LANDED SAFELY. INSPECTED AIRCRAFT AND FOUND NOSE STRUT DID NOT FULLY EXTEND DURING JACKING OF AIRCRAFT. FOUND NOSE STRUT IMPROPERLY SERVICED. RESERVICED NOSE STRUT.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 30,265 hrs · 28,196 cycles

FLIGHT 5585 - DURING POWER UP RECEIVED A 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: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 30,177 hrs · 28,129 cycles

FLIGHT 5363- RECEIVED A FLAP FAIL CAUTION MESSAGE WHILE AT THE GATE WITH FLAP SETTING AT 20 DEGREES. 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: RESERVOIR — UNKNOWN (OIL SYSTEM) · airframe 29,593 hrs · 31,786 cycles

FLIGHT 5699 - EN ROUTE CVG-CHA EXPERIENCED HIGH OIL TEMPERATURE, FLIGHT RETURNED TO CVG. DEFERRED THE ENGINE OIL REPLENISHMENT SYSTEM PER MEL 79-12-01.

Part: IDG — FAULTY (RT ENGINE) · airframe 31,033 hrs · 27,233 cycles

FLIGHT 5103 - DURING TAKEOFF ROLL RECEIVED A NR 2 IDG CAUTION MESSAGE, TAKEOFF WAS ABORTED AND FLIGHT RETURNED TO THE GATE. REPLACED THE RIGHT IDG.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 26,778 hrs · 25,294 cycles

DURING COMPLIANCE OF AN H-6 CHECK, ONE CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461 BETWEEN BL 0.0 AND RBL 9.0. THE CRACK WAS 1.5 INCHES LONG. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WTIH REO 601R-53-41-102 REV D DATED 9/29/03 AND REO 601R-53-41-162 DATED 6/9/03. OK FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 26,641 hrs · 25,153 cycles

FLIGHT 5175 - DURING TAKEOFF ROLL, RECEIVED A RIGHT WING ANTI ICE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. C/W RTO INSPECTION AND PERFORMED AN OPERATIONAL CHECK OF THE WING ANTI ICE SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED.

Part: DRAG BRACE — LACK OF LUBE (MLG) · airframe 26,178 hrs · 24,702 cycles

FLIGHT 5466 GEAR DISAGREE WARNING. NLG DID NOT RETRACT. CLEANED AND LUBED NLG DRAG BRACE. RETRACTION CHECKS WERE SATISFACTORY.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 25,271 hrs · 23,850 cycles

FLIGHT 5742 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 24,778 hrs · 23,438 cycles

FLIGHT 5768 FLAPS FAIL CAUTION DURING LANDING ROLL. REPLACED THE FLAP SELECTOR LEVER.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 24,268 hrs · 23,013 cycles

FLIGHT 5463 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01.

Part: PSEU — MALFUNCTIONED (NLG) · airframe 23,930 hrs · 22,730 cycles

FLIGHT 5479 NWS INOP, WOW INPUT CAUTION AND CIRCUIT BREAKER TRIPPED. RESET PSEU AND OPERATIONAL CHECK OF NWS WAS SATISFACTORY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,941 hrs · 21,923 cycles

FLIGHT 5073 FLAPS DID NOT MOVE WHEN SELECTED TO 20 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 21,534 hrs · 20,747 cycles

FLIGHT 5797 SPOILER AND FLIGHT SPOILER CAUTION MESSAGE. REPLACED THE NR 2 SECU.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 21,037 hrs · 20,316 cycles

FLIGHT 5276 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: ANTI-ICE SYSTEM · airframe 19,749 hrs · 19,156 cycles

FLIGHT 5883 LEFT WING ANTI-ICE DUCT WARNING MESSAGE.COULD NOT DUPLICATE. INSPECTED ANTI-ICE SYSTEM - NO FAULTS FOUND.

Part: DOOR · airframe 18,006 hrs · 17,419 cycles

FLIGHT 5409 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.LUBRICATED DOOR LOCKING MECH. OPS CHECK SATISFACTORY.

Part: SKIN — DAMAGED · airframe 17,759 hrs · 17,168 cycles

THE LEFT SIDE OF THE FUSELAGE WAS DAMAGED AT STA 379-394 AND STR 23L-24L. REMOVED THE DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED.

Part: DOOR · airframe 17,653 hrs · 17,064 cycles

FLIGHT 5839 CABIN DOOR OUTER HANDLE MESSAGE.COULD NOT DUPLICATE OPERATED DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS.

Part: BUSHING — WORN (VERT STABILIZER) · airframe 17,158 hrs · 16,559 cycles

L/H VERTICAL STABILIZER BUSHING P/N 600-21061-7 IS WORN.REMOVED THE WORN BUSHING I/A/W CRJ AMM CH 20-26-00-910-802, FABRICATED NEW BUSHING P/N 601R55-31-033-1 I/A/W REO 601R-55-31-033 AND INSTALLED THE BUSHING I/A/W REO 601R-55-31-002.

Part: DOUBLER — CRACKED (FS718.00) · airframe 17,158 hrs · 16,559 cycles

FS 718.00 L/H AND R/H AFT DOUBLERS CRACKED, FRAME SECTIONS L/H UPPER AND R/H UPPER AND LOWER ARE CRACKED.F.S.718.00 L/H AND R/H AFT DOUBLERS REMOVED AND REPLACED IAW CANADAIR REO 601R-53-61-193 REV A. FRAME SECTIONS L/H UPPER AND R/H UPPER AND LOWER REMOVED AND REPLACED IAW CANADAIR REO 601R-53-61-193 REV A.

Part: PCU — FAULTY (LEFT WING) · airframe 16,955 hrs · 16,358 cycles

FLIGHT #5395. DURING TAXI OUT WHILE PERFORMING FLIGHT CONTROL CHECK RECEIVED A FLIGHT SPOILER FAULT STATUS MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE LEFT OUTBOARD POWER CONTROL UNIT.

Part: PSEU — FAULTY (ELECTRICAL BAY) · airframe 16,442 hrs · 16,340 cycles

FLIGHT #5776. DURING TAXI OUT OF HSV RECEIVED A PROXIMITY SYSTEM FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY #2, AIRCRAFT RETURNED TO THE GATE.REPLACED THE PROXIMITY SENSING ELECTRONIC UNIT.

Part: WIRE — LOOSE (NR 2 DISPLAY) · airframe 16,943 hrs · 16,341 cycles

FLIGHT 5931. DURING TAXI OUT OF CVG RECEIVED A PROXIMITY FAULT STATUS MESSAGE ON ELECTRONIC DISPLAY NR 2, AIRCRAFT RETURNED TO THE GATE.REPAIRED WIRING AND SECURED GROUNDING STUD.

Part: WEB — CRACKED · airframe 16,892 hrs · 16,286 cycles

CRACK ON ENGINE SUPPORT BEAM UPPER SKIN.REPAIRED I/A/W REO 601R-53-61-345.

Part: WEB — CRACKED · airframe 16,892 hrs · 16,286 cycles

WHILE PERFORMING REPAIR TO THE ENGINE SUPPORT BEAM PER REO 53-61-345 A CRACK WAS NOTED ON THE UNDER LAYING EXTRUDED ANGLE P/N 601-35006-7 CRACK APPROX 5/16".THE CRACK WAS REPAIRED I/A/W CANADAIR REO 601R-53-61-394.

Part: RIB — CRACKED (PYLON) · airframe 16,868 hrs · 16,252 cycles

THE LT PYLON AT FS 605 IS CRACKED AT THE OUTBOARD LOWER FLANGE. REPAIRED DAMAGED AREA TO THE LT PYLON RIB AT FS 605 AT THE OUTBOARD LOWER FLANGE IAW WVAC EO 601R-54-2401A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,868 hrs · 16,252 cycles

THE ANGLES AT BL27 (LT & RT) AND INTERCOSTALS AT BL 36 (LT & RT) AT FS 484 ARE CRACKED. INSTALLED NEW SERVICEABLE LT & RT INBOARD AND OUTBOARD 484 ANGLES IAW WVAC EO 601R-53-2413A.

Part: NOZZLE — DEPARTED (LT ENGINE) · airframe 16,404 hrs · 15,753 cycles

VIBRATION FELT DURING FLIGHT, VIBRATION STOPPED DURING DECENT. POST FLIGHT INSP FOUND LEFT ENGINE TAILPIPE AND EXHAUST FAIRING HAD DEPARTED ACFT.REPLACED LEFT ENGINE.

Part: BPSU — MALFUNCTIONED (LEFT) · airframe 15,971 hrs · 15,334 cycles

FLAPS FAILED AT 20 DEGREES. REPLACED THE LEFT HAND BPSU.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 15,860 hrs · 15,230 cycles

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

Part: BULB — FAILED (CABIN) · airframe 14,954 hrs · 14,272 cycles

AFT CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.

Part: ACTUATOR — WORN (TE FLAP) · airframe 14,841 hrs · 14,146 cycles

FOUND LEFT OUTBOARD FLAP, INBOARD ACTUATOR HAD PLAY AT FORWARD BUSHING MOUNT. REMOVED AND REPLACED ACTUATOR WITH A SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — WORN (TE FLAP) · airframe 14,841 hrs · 14,146 cycles

FOUND RIGHT OUTBOARD FLAP, INBOARD ACTUATOR HAS EXCESSIVE PLAY AT AFT END. REMOVED AND REPLACED ACTUATOR WITH A SERVICEABLE ONE. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,516 hrs · 13,821 cycles

OIL SMELL IN COCKPIT WHEN APU STARTED. COULD NOT DUPLICATE. NO OIL SMELL NOTED IN AIRCRAFT DURING GROUND RUNS.

Part: TRIM ACTUATOR — MALFUNCTIONED (RUDDER)

RUDDER TRIM INDICATOR SHOWED FULL SCALE LEFT DEFLECTION. REPLACED THE RUDDER TRIM ACTUATOR.

Part: WARNING SYSTEM — ILLUMINATED (TE FLAP)

FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM PER AD98 20 01.

Part: ANGLE — CRACKED (BS 280)

THE AFT J-ANGLE AT FS 380 AND RBL 9.0 WAS CRACKED. REMOVED CRACKED SECTION AND SPLICED NEW SECTION OF ANGLE (P/N 600-34017-595) IAW WVAC EO 601R-53-0535.

Part: FLOORBEAM — CORRODED (BS 280)

THE FLOORBEAM AT FS 280 WAS CORRODED ON THE UPPER EDGE BETWEEN RBL 9 AND LBL 9. PERFORMED A MAJOR REPAIR TO CORRODED FLOORBEAM WEB AT FS 280 BETWEEN RBL 9 AND LBL 9 IAW WVAC EO 601R-53-0505.

Part: FLOORBEAM — MISDRILLED (BS 349)

FLOORBEAM CAP LBL 9 HAS A OVERSIZED HOLE AT FS 349. REAMED OVERSIZED HOLE AT FS 349 FLOORBEAM CAP LBL 9 TO ACCOMODATE FASTENER H18P38-3 HI-LOK AND INSTALLED FASTENER IAW CRJ WVAC EO 601R-53-0516A.

Part: SUPPORT — CORRODED (BS 349)

FLOOR SUPPORT PLATES AT FS 349.0 (P/N'S 601R38673-17,-19,-21 AND -25) BETWEEN LBL 42 TO RBL 42 WERE CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING FLOOR SUPPORT PLATES (P/N 601R38673-17,--19,-21 AND -25) AT FS 349 BETWEEN LBL 42 TO RBL 42 IAW EVAC EO 601R-53-0515.

Part: FLOORBEAM — CORRODED (BS 280-370)

FLOOR SUPPORT BEAM CAP (P/N 601R31113-67) AT RBL 9 WAS CORRODED BETWEEN FS 280 TO FS 370. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED SECTION OF FLOORBEAM CAP (P/N 601R31113-67) AT RBL 9 BETWEEN FS 280 TO FS 409 IAW CRJ REO 601R-53-00-027 NC.

Part: ANGLE — CRACKED (BS 280)

CRACK IN J CHANNEL ON FS 280 ON O/B SIDE OF RBL 9, CRACK IS 1.7 INCH LONG. REPAIRED AFT J ANGLE ON FS 280.0 O/B SIDE OF RBL 9 IAW WVAC EO 601R-53-0535.

Part: FLOORBEAM — CORRODED (BS 280-356)

FLOOR SUPPORT BEAM CAP (P/N 601R31113-67) AT RBL 27 WAS CORRODED BETWEEN FS 310 TO FS 349. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED SECTION OF FLOORBEAM CAP (P/N 601R31113-67) AT LBL 27 BETWEEN FS 280 TO FS 356 IAW CRJ 601R-53-00-027 NC AND WVAC EO 601R-53-0482A.

Part: DOUBLER — CORRODED (SERVICE DOORWAY)

SERVICE DOOR DOUBLER FORWARD OF DOOR HAD CORRODED AREA. REMOVED AND REPLACED DOUBLER FORWARD OF DOOR IAW WVAC EO 601R-53-0530.

Part: SILL — CORRODED (SERVIC DOORWAY)

THE FLOOR SILL FWD OF THE SERVICE DOOR P/N 601R31148-79 IS CORRODED.\NPERFORMED A MAJOR REPAIR BY REPLACING FLOOR SILL P/N 601R31148-79 FWD OF THE SERVICE DOOR IAW WVAC EO 601R-53-0531.

Part: ANGLE — CORRODED (SERVICE DOORWAY)

SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE WAS CORRODED (P/N 601R38303-105). REMOVED UNSERVICEABLE THRESHOLD ANGLE (P/N 601R38303-105) AND INSTALLED NEW SERVICEABLE ANGLE (P/N 3992T 7075 T6511) EXTRUSION IAW WVAC EO 601R-53-0478A.

Part: ANGLE — CRACKED (BS 280)

VERTICAL L ANGLE FWD FS 280.0 AT LBL 9 IS CRACKED (P/N 600-34017-723). PERFORMED A MAJOR REPAIR. REMOVED CRACKED L ANGLE FWD OF FS 280 JUST O/B OF LBL 9 AND REPLACED WITH NEW ANGLE IAW WVAC EO 601R-53-0517.

Part: ANGLE — CORRODED (PAX DOORWAY)

PAX DOOR ENTRANCE FLOOR SUPPORT ANGLE HAD CORROSION (P/N 601R31527-46R). REMOVED AND INSTALLED PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0479A.

Part: BPSU — FAILED (LT TE FLAP)

FLAP FAIL CAUTION MESSAGE DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AT CVG. REPLACED THE LEFT BRAKE POSITIONING SENSING UNIT.

Part: ENGINE — FAILED (LEFT)

OILY SMELL FROM LEFT HAND ENGINE BLEED AIR. REPLACED ENGINE.

Part: ENGINE — FAILED (LEFT)

OIL SMELL IN COCKPIT DURING FLIGHT. REPLACED LEFT ENGINE.

Part: BULB — FAILED (PAX DOOR)

EMERGENCY LIGHT INOPERABLE, MAIN CABIN DOOR. REPLACED LIGHT BULB.

Part: PSEU — MALFUNCTION (AVIONICS)

LANDING GEAR WILL NOT EXTEND. USED FREE FALL SYSTEM TO LOWER GEAR. REPLACED THE PSEU.

Part: CONTROL UNIT — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE DOES NOT RESPOND TO POWER LEVER MOVEMENT, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE ELECTRONIC SPEED CONTROL SYSTEM. AIRCRAFT RETURNED TO SERVICE.

Part: CLAMP — CORRODED (BLEED AIR SYSTEM)

A 24, 48 MONTH INSPECTION, BLEED AIR DUCT CLAMP CORRODED. REPLACED CLAMP.

Part: CONNECTOR — BROKEN (CABIN)

A 24, 28 MONTH INSPECTION, EMERGENCY FLOOR STRIP LIGHT HAS BROKEN CONNECTORS. REPLACED CONNECTORS.

Part: ANGLE — CRACKED (BS 621)

ANGLE (P/N 601-35012-51) IN AFT EQUIPMENT BAY, LEFT HAND SIDE OF FS 621 BULKHEAD CRACKED. REPLACED ANGLE AS PER REO 601R-53-61.

Part: STRUT — LEAKING (NLG)

NOSE LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. RESEALED AND RESERVICED NLG SHOCK STRUT.

Part: SWITCH — MALFUNCTION (LT ENG COWL)

LEFT COWL ANTI-ICE CAUTION MESSAGE. REPLACED THE COWL ANTI-ICE PRESSURE SWITCH.

Part: FLAP WARNING — ACTIVATED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE WHEN FLAPS SELECTED UP AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF FLAP SYSTEM SATISFACTORY.

Part: FLEX SHAFT — BROKEN (RT TE FLAP)

FLAPS FAILED AT 0 DEGREES DURING LANDING. REPLACED THE RIGHT HAND NR 4 FLEX DRIVE CABLE.

Part: SECU — TRIPPED (GROUND SPOILER)

GROUND SPOILER CAUTION MESSAGE. RESET SECU'S, OPERATIONAL CHECK NORMAL.

Part: PCU — FAILED (RT SPOILERON)

INBOARD GROUND SPOILER FAULT LIGHT COMES ON INTERMITTENTLY IN-FLIGHT. REPLACED RIGHT INBOARD SPOILERON PCU, OPERATION CHECK GOOD.

Part: BOLT — BROKEN (LT MLG)

AFTER TAKEOFF, LANDING GEAR RETRACT LEVER COULD NOT BE SELECTED UP. OVERRIDE WAS USED, NLG RETRACTED BUT MLG REMAINED DOWN. THE LT MLG TRAILING ARM HINGE PIN BOLT WAS BROKEN ALLOWING THE HINGE PIN TO ROTATE AND GIVE FALSE SIGNAL TO WOW SWITCHES. REPLACED BOLT.

Part: HANDLE ASSY — CRACKED (CARGO DOOR)

CARGO DOOR LATCH RELEASE DOES NOT SPRING OPEN WHEN LATCH IS OPENED. REPLACED THE CARGO DOOR HANDLE AND HOUSING ASSY.

Part: BRAKE ASSY — OVERHEAT (LT MLG)

DURING TAXI, THE LT MLG OUTBD BRAKE OVER HEATED CAUSING WHEEL FUSE LUGS TO MELT AND DEFLATE TIRE. REPLACED THE LT MLG BRAKE ASSY AND WHEEL ASSY.

Part: SECU — FAILED (NR 2 SPOILER)

GROUND SPOILERS DO NOT AUTO DEPLOY DURING LANDING. REPLACED THE NR 2 SPOILER ELECTRONIC CONTROL UNIT.

Part: BPSU — MALFUNCTION (LT TE FLAP)

FLAPS FAILED AT 8 DEGREES, WHEN SELECTED UP AFTER TAKEOFF. REPLACED THE LT FLAP BRAKE AND POSITION SENSOR.

Part: TAT PROBE HEAT — FAILED (FUSELAGE)

TAT PROBE HEAT CAUTION MESSAGE ON EICAS. REPLACED THE TAT PROBE.

Part: AMPLIFIER — DEFECTIVE (RT ENGINE)

RT ENGINE WILL NOT ACHIEVE TAKEOFF THRUST. REPLACED THE N1 AMPLIFIER AND ENGINE RUNS NORMAL, ACFT RETURNED TO SERVICE.

Part: DETECTOR — MALFUNCTIONED (CARGO)

CARGO SMOKE WARNING DURING TAXI, FIRE BOTTLES WERE DISCHARGED. REPLACED THE CARGO COMPARTMENT SMOKE DETECTOR AND FIRE BOTTLES, FALSE WARNING, NO INDICATION OF SMOKE OR FIRE.

Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY)

CARGO SMOKE WARNING ON TAXI OUT. ARMED AND FIRED BOTTLES. ACTION: FOUND LIVE BIRDS (300 CANARIES IN CAGES) HAD CAUSED DETECTORS TO ACTIVATE; REMOVED AND REPLACED FIRE BOTTLES AND SQUIBS WITH SERVICEABLE UNITS.

Part: HYD PUMP — LEAKING (LT ENGINE)

THE LT ENGINE DRIVEN HYDRAULIC PUMP IS LEAKING FLUID. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP.

Part: RADIO ALTIMETER — DEFECTIVE (NR 1)

GROUND LIFT DUMP IS SLOW TO DEPLOY. REPLACED THE NR 1 RADIO ALTIMETER.

Part: CONNECTOR — DEFECTIVE (RT TE FLAPS)

FLAPS FAIL MESSAGE ON EICAS. FLAPS FAILED AT ZERO DEGREES. RESEATED PIN IN WIRING CONNECTOR AT THE RT BPSU.

Part: BPSU WIRE — BROKEN (RT TE FLAP)

FLAPS FAIL MESSAGE ON EICAS. REPAIRED BROKEN WIRE AT CONNECTOR 2P2CE AT RT BPSU.

Part: STALL UNIT — DEFECTIVE (AVIONICS)

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

Part: PCU — DEFECTIVE (LT SPOILER)

INBD GROUND LIFT DUMPERS WILL NOT DEPLOY. REPLACED LT INBD FLIGHT SPOILER PCU.

Part: BRAKES — CONTAMINATED (MAIN GEAR)

TOWER PERSONNEL REPORTED HEAVY SMOKE COMING FROM MLG. FOUND SMOKE TO BE CAUSED BY DE-ICING GLYCOL ON BRAKES. CLEANED BRAKE ASSY, AND AIRCRAFT CONTINUED SERVICE.