N979CA
Registered owner: HYANNIS AIR SERVICE 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
THE PILOT REPORTED A FUEL SMELL IN THE CABIN DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE HEATER FUEL PUMP LEAKING. THIS WAS REMOVED AND REPLACED WITH NO FURTHER DEFECTS NOTED.
FLIGHT 5819 - CABIN DOOR WARNING. REPLACED MISSING SPRING ON OUTER HANDLE LATCH BUTTON.
FLIGHT 5839 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.
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.
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.
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.
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.
FLIGHT 5452 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
FLIGHT 5361 NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION. REPLACED THE RT EDP.
FLIGHT 5391 AHRS FAILURE DURING TAKEOFF. REPLACED THE NR 1 AHRS.
FLIGHT 5745 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
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.
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.
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.
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.
FLIGHT 5158 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
FLIGHT 5270 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
FLIGHT 5089 1ST SECTION OF EMERGENCY FLOOR LIGHTING IS INOP.REPLACED 1ST SECTION OF FLEXIBLE LAMP.
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.
FLIGHT 5838 CARGO FIRE BOTTLE LOW MESSAGE.REPAIRED WIRING CONNECTOR AT FIRE BOTTLE.
FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.
FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.
FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.
FLIGHT #5423. PRIOR TO DEPARTURE FROM CVG DISCOVERED THE EMERGENCY LIGHTING INOPERATIVE.REPLACED DRAINED BATTERY FOR THE EMERGENCY LIGHTING.
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.
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.
THE DOUBLER PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED DOUBLER AND REPLACED I/A/W WVAC E.O. 601R-53-2732.
AFTER PUSH BACK AT CVG, SPOILERS FAULT STATUS MESSAGE WOULD NOT EXTINQUISH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE FLIGHT SPOILER POWER CONTROL UNIT.
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.
STEERING INOP CAUTION MESSAGE. REPLACED THE STEERING ECU.
FORWARD FLOOR EMERGENCY LIGHT IS INOP. CLEANED CONNECTION, LIGHT OPERATION IS NORMAL.
CONFIG SPOILERONS WARNING DURING T/O. COULD NOT DUPLICATE. FOUND NO FAULT CODES IN COMPUTER.
FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
EMERGENCY LIGHTS AT ROW 8 ARE INOPERABLE. REPLACED FLOOR LIGHTING CABLE ASSY.
BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION, NO DAMGE FOUND.
GEAR DISAGREE WARNING, LEFT HAND MLG INTRANSIT. ADJUSTED THE LEFT HAND MLG UPLOCK PROXIMITY SENSOR.
FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
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.
EMERGENCY LIGHT IS INOPERABLE IN THE AFT CABIN AREA. REPLACED THE LIGHT BULB.
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.
TOILET SMOKE CAUTION MESSAGE. FOUND SMOKE SOURCE TO BE THE APU. DEFERRED APU PER MEL.
FWD FUSELAGE SKIN DAMAGED FS 310 STR 16-17 LHS. REPAIRED SKIN IAW WVAC EO 601R-53-1015.
LOUD HIGH PITCH NOISE ON RIGHT HAND SIDE OF COCKPIT. SECURED O2 SERVICE DOOR CLOSED.
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.
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.
STRONG BURNING SMELL IN COCKPIT. CLEANED RESIDUAL, COMPRESSOR WAS HOT FROM AIRCRAFT SYSTEM.
LEFT OVERWING EMERGENCY EXIT SIGN IS INOPERABLE. REPLACED EXIT SIGN.
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.
AFT CABIN OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.
C-CHECK TASK 27-580-100, LT I/B FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE.
RIGHT ENGINE START MESSAGE CAME ON AFTER TAKEOFF. REPLACED THE ENGINE AIR START VALVE.
CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
ONE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP AND ONE EMERGENCY EXIT SIGN INOP. DRIED WET FLOOR LIGHTING AND REPLACED EXIT SIGN LIGHT BULB.
FLAP FAIL CAUTION MESSAGE DURING FLIGHT. REPLACED THE LEFT AND RIGHT BPSU.
CABIN DOOR OUTER HANDLE CAUTION MESSAGE AFTER TAKEOFF. ADJUSTED THE DOOR STOP ASSY.
PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY, DOOR OPERATION NORMAL.
OUTER DOOR HANDLE UNSAFE MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY. DOOR AND WARNING SYTEM OPERATE NORMAL.