N929CA
Registered owner: HYANNIS AIR SERIVE INC, MA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HYANNIS AIR SERVICE INC. (HYIA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ON CLIMBOUT FROM JFK RECEIVED NOSE DOOR WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE.
PERMANENT REPAIR NEEDS PERFORMED TO REPLACE TEMP REPAIR THAT WAS DONE AT FS 559.00 WEB BETWEEN RBL 9-18. REMOVED TEMP REPAIR AND INSTALLED A PERMANENT REPAIR ON FS 559 BULKHEAD WEB BETWEEN RBL 9 AND RBL 18 PER CRJ TASKCARD: SMA-2-53R0002 SECTION 2.
LEFT FS 640.00 FRAME, REINFORCING DOUBLER AND BONDED SKIN DOUBLER ARE CRACKED BETWEEN STR 9 AND 13. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER REO 601R-53-61-3184 REV A. S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C, 601R53-61-569 REV A AND EA10-5361-02621.
EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHT BATTERY PACK NR 2.
FLIGHT 5300 - RECEIVED INTERMITTENT BATTERY BUSS CAUTION MESSAGE. DIVERTED TO MCO, LANDED WITHOUT INCIDENT. REPLACED MAIN BATTERY. NO FURTHER DEFECTS.
FLIGHT 5300 - ABORTED TAKEOFF APPROX 105 - 110 KTS DUE TO ANTI-SKID CAUTION MESSAGE. REPLACED LEFT OUTBOARD LOWER MLG HARNESS ASSEMBLY. NO FURTHER DEFECTS.
DURING HMV7 INSPECTION FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REMOVE DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-61-2168 AND REO 301R-53-61-1230.
DURING HMV7 INSPECTION FOUND FLOOR SUPPORT CHANNEL CRACKED AT LEFT CORNER FS 295, LBL 10. INSTALLED NEW P/N 600-34017-351 CHANNEL IAW SRM 51-42-06.
DURING HMV7 INSPECTION FOUND BULKHEAD POST LOWER END CRACKED, FS 559, RBL 9. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-057.
FLIGHT 5320 - CRACK ON RBL 9.0 O/B RADIUS OF VERTICAL STIFFENER AT FS 559.00. REPAIRED CRACK ON RBL 9.0 O/B RADIUS OF VERTICAL STIFFENER IAW REO 601R-53-41-057.
CRACK AT RIGHT SIDE FS 574.00 BETWEEN STRINGERS 6 AND 7. REPLACED SPLICE ANGLE IAW SRM 51-42-06.
TWO CRACKS VERIFIED WITH EDDY CURRENT ON SEMI-PRESSURE BULKHEAD AT FS 559 BETWEEN RBL 9 AND RBL 18. REPAIRED SEMI-PRESSURE BULKHEAD AT FS 559 AS PER REO 601R-53-41-353.
FLIGHT 9461- GEAR DISAGREE WARNING AND NOSE DOOR OPEN MESSAGE WHEN GEAR SELECTED DOWN. REMOVED AND REPLACED NLG SELECTOR VALVE.
FLIGHT 4973 - DURING PREFLIGHT INSPECTION RECEIVED A FLAP FAIL CAUTION 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.
FLIGHT 5102 - THE EMERGENCY FLOOR LIGHTS FROM ROW 9 TO THE LAVATORY FAILED TO ILLUMINATE DURING TEST. REPAIRED CONNECTOR P40LY.
FLIGHT 5519 - SECTION OF THE EMERGENCY FLOOR LIGHTING IS INOPERATIVE. DISCONNECTED, CLEANED AND INSPECTED AFFECTED CONNECTOR FOR INOPERATIVE SECTION OF FLOOR LIGHTING.
FLIGHT 5684 - THE EMERGENCY FLOOR PATH EXIT LIGHTING FAILED TEST BETWEEN ROWS 9-12. DEFERRED INOPERATIVE SECTION OF EMERGENCY FLOOR PATH EXIT LIGHTING PER MEL 33-51-01-5.
FLIGHT 5532 - MOST REAR CABIN EMERGENCY FLOOR STRIP INOPERATIVE. REPLACED INOPERATIVE CABLE ASSEMBLY.
FLIGHT 5023 - PERFORMED A HIGH SPEED ABORT DUE TO ANTI-SKID CAUTION. PERFORMED A SYSTEM RESET FOR SECU NR 1 AND NR 2.
FLIGHT 5181 - AFTER LANDING RECEIVED A FLAP FAIL CAUTION AT 45 DEGREES. REPLACED BPSU.
FLIGHT 5568 - DURING LGA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 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.
FLIGHT 5455 - FLAP FAIL CAUTION MESSAGE ON GROUND. 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.
FLIGHT 5137 - DURING LANDING AT YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE BRAKE POSITION SENSING UNIT.
FLIGHT 5137 - DURING LANDING AT YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR.
DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE LEFT INBOARD FLAP OUTBOARD FLAP ACTUATOR.
FLIGHT 5137 - DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE RIGHT INBOARD FLAP INBOARD ACTUATOR.
FLIGHT 5137 - DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE RIGHT INBOARD FLAP OUTBOARD FLAP ACTUATOR.
FLIGHT 5266- FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED RT BPSU.
FLIGHT 5202 - FLAPS FAILED CAUTION MESSAGE OCCURRED ON FINAL APPROACH AT 45 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.
FLIGHT 5616 - DURING TAXI OUT RECEIVED A FLAP FAIL MESSAGE, FLIGHT RETURNED TO THE GATE. 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.
FLIGHT 5078 - DURING BUF APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 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.
FLIGHT 5227 - NLG DOOR OPEN WARNING. LUBRICATED AND FREED UP FROZEN ROLLER IN NLG DOORS OPERATING MECHANISM.
FLIGHT 5306 - THE AFT CABIN EMERGENCY FLOOR LEVEL LIGHTING FAILED TEST. REPAIRED WIRING ON AFT EMERGENCY FLOOR LEVEL FLEX STRIP CONNECTOR.
FLIGHT 5499- OVERBOARD COOL CAUTION. AIRCRAFT DID NOT PRESSURIZE. FOUND OVERBOARD AND INBOARD EXHAUST VALVES IN WRONG POSITION. PREVIOUS DEFERRAL ITEM.
FLIGHT 5851 - DURING CLIMBOUT OF DSM RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT.
DURING HEAVY MAINTENANCE CHECK, THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED WITH FACTORY NEW PARTS USING THE CL 6002B-19 STRUCTURAL REPAIR MANUAL
DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN AT FS 460.0, BETWEEN BL 0.0 AND RBL 9.0 THE CRACK WAS 2.0 INCH IN LENGTH. REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9-29-2003.
FLIGHT 4962, LOUD CLUNKING NOISE FROM NLG. REPLACED THE NLG DOORS SELECTOR VALVE.
FLIGHT 5822 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL CHECKS AND INSPECTION OF LANDING GEAR FOUND NO DEFECTS.
FLIGHT 4988 EMERGENCY FLOOR PATH LIGHTS ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY.
FLIGHT 5659 GEAR DISAGREE WARNING ON APPROACH. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE NORMAL. ADJUSTED NLG UPLOCK HOOK TO M/M SPECS.
FLIGHT 5870 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG UPLOCK.
FLIGHT 5596 GEAR DISAGREE WARNING, NLG INDICATED INTRANSIT. REPLACED THE NLG PRIORITY VALVE.
FLIGHT 5689 AFTER TAKEOFF AND GEAR RETRACTION THE NLG INDICATED DOWN AND LOCKED WITH THE HANDLE IN THE UP POSITION. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). CLEANED AND LUBRICATED THE NLG PIVOT POINTS.
FLIGHT 5745 AFTER TAKEOFF AND GEAR RETRACTION RECEIVED A NLG DISAGREE CAUTION WITH A NOSE GEAR DOOR OPEN MESSAGE. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). REPLACED THE NLG DOOR ACTUATOR.
FLIGHT 5221 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. FOUND OUTER HANDLE OPEN - OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS NOTED.
FLIGHT 5219 RUDDER TRIM STUCK AT 1/4 RIGHT. REPLACED THE RUDDER TRIM PANEL.
FLIGHT 5443 LEFT ANGLE OF ATTACK HEAT CAUTION MESSAGE.RESET SYSTEM - COULD NOT DUPLICATE.
FLIGHT 5063 LOUD WHISTLING COMING FROM R/H FORWARD SIDE OF AIRCRAFT.FOUND GROUND INTERPHONE DOOR OPEN - INSPECTED FOR DAMAGE AND CLOSED DOOR.
FLIGHT 5984 GEAR DISAGREE MESSAGE.REPLACED THE PSEU.
FLIGHT 5433 TRIM CAUTION MESSAGE - TRIM STUCK AT 2.8REPLACED THE HORZ STAB TRIM ACTUATOR.
FLIGHT 5553 - PILOT TO COPILOT INTERCOM INTERMITTENT.REPLACED THE #1 ACP.
FLIGHT #5902. GER DISAGREE WARNING - NLG INDICATED UNSAFE. NLG THEN INDICATED DOWN AND LOCK DURING GO AROUND.ADJUSTED THE NLG DOORS ACTUATOR AND MECHANISM. SYSTEM OPERATED NORMALLY.
STAB CHANNEL 1 INOP MESSAGE DURING APPROACH.REPLACED THE HSTCU.
FLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A FLAP CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITH FLAPS OSCILLATING BETWEEN 2 AND 5 ABOVE SELECTED POSITION.REPLACED THE FLAP POSITION TRANSMITTER.
FLIGHT 6082. FLIGHT SPOILER AND OUTBOARD GROUND SPOILER FAULT MESSAGE DURING T/O. T/O ABORTEDRESET SYSTEM AND C/W OPERATIONAL CHECKS. NO FAULTS FOUND.
FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB. CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.
FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE HORIZONTAL STABILIZER TRIM MOTOR CONTROL UNIT.
FLIGHT #5322. WHILE PARKED AT THE GATE AT EVV STABILIZER TRIM CHANNEL #2 WOULD NOT ENGAGE.REPLACED STAB/MACH TRIM PANEL ASSEMBLY.
EMERGENCY LIGHT ROW 11 IS INOPERABLE.DEFERRED MAINTENANCE PER M.E.L.
LEFT AND RIGHT VERTICAL STABILIZER BUSHINGS ARE MIGRATED. REMOVED AND REPLACED LT AND RT VERTICAL STABILIZER BUSHINGS IAW WVAC EO 601R-55-2429.
THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE P/N 601-36001-30 AND INSTALLED A NEW ANGLE P/N 601-36001-30 IAW WVAC EO 601R-53-2390.
THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE (P/N 601-36001-30) AND INSTALLED A NEW ANGLE (P/N 601-36001-30) IAW WVAC EO 601R-53-2390.
FLAPS FAIL MESSAGE. REPLACED THE FECU.
EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.
FLAPS FAIL MESSAGE. REPLACED THE RDU.
FLAPS FAIL MESSAGE. REPLACED THE RT BPSU.
OVERBOARD COOL CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF PASSENGER DOOR AND WARNING SYSTEM WAS NORMAL.
CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED OUTER HANDLE LATCH SPRING.
PAX DOOR OUTER HANDLE WARNING IN FLIGHT, COULD NOT OPEN DOOR UPON LANDING. INSPECTED AND LUBED DOOR, NO FAULT MESSAGE.
PAX DOOR HANDLE CAUTION LIGHTS CAME ON AFTER DEPARTURE. REMOVED EXCESS GREASE FROM HANDLE.
WING OVERHEAT WARNING. REPLACED THE RIGHT HAND WING CONTROL SENSOR.
CABIN DOOR WARING. REPLACED OUTER HANDLE LATCH SPRING.
SMOKE IN CABIN DURING TAXI OPS. REPLACED DEFECTIVE LIGHT BALLAST AT ROW 5.
DISPLAY COOL CAUTION MESSAGE. CLEANED DUST FROM THE CRT DISPLAY SCREENS.
FS 280.00 AFT J ANGLE (P/N 600-34017-595) WAS CORRODED. TRIMMED OUT DAMAGED AREA OF J ANGLE AND FABED NEW SECTION, INSTALLED IAW WVAC EO 601R-53-0774.
FS 280.00 WEB (P/N 600-34017-587) CORRODED. REMOVED FORWARD J ANGLE TO ACCESS WEB, TRIMMED OUT DAMAGED AREA FAB FILLER AND REPAIR DOUBLER, INSTALLED, REINSTALLED FWD J ANGLE IAW WVAC EO 601R-53-0773.
FS 280.00 FWD J ANGLE (P/N 600-34017-351) IS CORRODED. REMOVED DAMAGED J ANGLE AND REPLACED IAW WVAC EO 601R-53-0758.
FS 280.00 LBL 9 HAD CRACKED FLOOR SUPPORT ANGLE. REMOVED DAMAGED ANGLE AND FABED NEW ANGLE, INSTALLED IAW WVAC EO 601R-53-0760.
VERTICAL STIFFENESS CRACKED AT FS 28 DEGREES BELOW CBP-1 AND CBP-2 AT LBL 12 AND RBL 12. INSTALLED NEW STIFFENERS IAW WVAC EO 601R-53-0759.
PAX DOOR THRESHOLD TOP ANGLE (P/N 601R31527-46) WAS CORRODED. INSTALLED NEW PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0757.
OUTBOARD WEB AT LBL 27 FS 307 HAD ELONGATED HOLE .27 DEGREES DIAMETER (P/N 601R31113-17). INSTALLED NEW WEB IAW WVAC EO 6501R-53-0772.
SERVICE DOOR THRESHOLD TOP ANGLE (P/N 601R38303 105) WAS CORRODED FS 317 - FS 342. INSTALLED NEW THRESHOLD TOP ANGLE IAW WVAC EO 601R-53-0757.
DOUBLER PLATE AT RBL 42 FS 310 - FS 319 (P/N 601R38669-49) WAS CORRODED. INSTALLED NEW DOUBLER PLATE AT RBL 42 FS 310 - 319 IAW WVAC EO 601R-53-0778.
THE ATTACH ANGLES AT FS 484 AT RBL 27 AND LBL 36 WERE CRACKED. INSTALLED NEW BRACKETS IAW WVAC EO 601R-53-07628.
CENTER TANK GRAVITY FILL SCUPPER ASSY HAS SEVERAL DAMAGED HI-LOC PIN HOLES. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-077.
DOOR OUTER HANDLE WARNING AFTER TAKEOFF. ADJUSTED DOOR HANDLE SPRING TENSION.
DOOR UNLOCKED WARNING AFTER TAKEOFF. FOUND DOOR HANDLE UNLATCHED. INSPECTED LATCH MECHANISM AND FOUND NO DEFECTS.
CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. NO DEFECTS FOUND WITH CABIN DOOR.
AFTER TAKEOFF, PASSENGER OUTER DOOR HANDLE STOW AND OVERBOARD COOL CAUTION MESSAGE CAME ON. ADJUSTED PROX SENSOR.
OUTER DOOR HANDLE MESSAGE AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND.
FLAPS FAIL CAUTION MESSAGE. INSPECTED FLAPS PER EO 27-045 AND AD 98-20-01. NO DEFECTS FOUND.
CABIN DOOR OUTER HANDLE CAUTION MESSAGE. INSPECTED AND FOUND NO DEFECTS WITH DOOR HANDLE.
WING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED THE RIGHT WING BLEED AIR PICCOLO TUBE.
LEFT 14TH STAGE DUCT LEAK MESSAGE. REPLACED THE LEFT HAND ENGINE PYLON BLEED LEAK SENSING ELEMENT.
ANTI-ICE DUCT LEAK WARNING MESSAGE. REPLACED THE LEFT ENGINE PYLON SENSING ELEMENT.
BLEED AIR DUCT LEAK WARNING DURING TAKEOFF. REPLACED THE BLEED LEAK CONTROL UNIT.
ANTI-ICE DUCT LEAK WARNING DURING TAKEOFF. REPLACED THE BLEED AIR LEAK CONTROLLER.
EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES.
A/C UTILITY BUS NR 2 SHED IMMEDIATLEY AFTER FLAPS ARE SELECTED OUT OF 0 DEGREES. REMOVED THE A/C UTILITY BUS CONTACTOR NR 1K4XD IAW CRJ CONCESSION LETTER CO95-651.
LEFT PITOT HEAT CAUTION MESSAGE ON EICAS. REPLACED THE HEAT CONTROLLER.
DURING CLIMBOUT, FLAPS STUCK AT 12 DEGREES. AIRCRAFT RETURNED TO THE FIELD. REPLACED RIGHT OUTBOARD FLAP DRIVE CABLE ASSEMBLY, CABLE WAS FOUND SEIZED.
FLAPS FAIL MESSAGE ON EICAS. REPLACED THE RT OUTBOARD FLAP DRIVE CABLE.
ALL ENGINE AND APU FIRE WARNINGS AND FAIL LIGHTS CAME ON. REPLACED THE FIRE DETECTION CONTROLLER.
STALL FAIL ABNORMAL CAPTION DISPLAYED. REPLACED STICK PUSHER ACTUATOR.
PILOTS ALTIMETER AND VERTICAL SPEED INDICATORS FAILED. REPLACED THE NR 1 AIR DATA COMPUTER.
PASSENGER DOOR OUTER HANDLE NOT STOWED MESSAGE ON EICAS. AIRCRAFT WOULD NOT PRESSURIZE. COULD NOT DUPLICATE DISCREPANCY. DOOR OPERATION AND OUTER HANDLE STOW MECHANISM ALL OPERATE NORMAL.
FLAPS FAILED AT 20 DEGREES DURING RETRACTION. REPLACED THE LT AND RT BRAKE AND POSITON SENSOR UNITS. PART TOTAL CYCLES, 5,181.
NR 1 HYDRAULIC SYSTEM CAUTION MESSAGE RECEIVED AFTER TAKEOFF. NR 1 HYDRAULIC SUPPLY LINE CHAFED AND LEAKING AT SUPPORT CLAMP. REPLACED LEAKING LINE.
LEFT ENGINE FAN SECTION HAS FOD DAMAGE. REPLACED 5 SETS OF FAN BLADES.
OXYGEN SERVICE DOOR OPEN IN FLIGHT. CLOSED AND SECURED DOOR.
NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.
UNABLE TO RETRACT NOSE LANDING GEAR. REPLACED NLG DRAG BRACE ASSY.
HORIZONTAL STABILIZER TRIM CHANNEL NR 2 INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.
LOWER EMERGENCY LIGHT ON MAIN PASSENGER DOOR HAS A BROKEN LENSE AND DOES NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY.
ANTI-SKID SYSTEM FAIL, CIRCUIT BREAKER TRIPPED. REPLACED ANTI-SKID CONTROL BOX.
INBD ANTI-SKID MESSAGE AND PROXIMITY SYSTEM FAULT MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT.
NLG STEERING IS INOP. REPLACED THE NLG SELECTOR VALVE.
GEAR DISAGREE MESSAGE ON EICAS, NLG DID NOT DOWN LOCK. EMERGENCY PROCEDURE USED TO EXTEND LANDING GEAR. REPLACED NLG SELECTOR VALVE.
NOSE WHEEL STEERING IS INOP. REPLACED THE SBW HARNESS ON NLG.