N785CA
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
Maintenance disclosures
ON APPROACH INTO CVG RECEIVED LEFT I/B ANTI-SKID CAUTION MSG, FOLLOWED QRH. EMERGENCY DECLARED, A/C LANDED SAFELY IN CVG. REPINNED LEFT I/B ANTI-SKID TRANSDUCER CONNECTOR. NO FURTHER DEFECTS NOTED.
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF DRAG ANGLE IAW SRM 51-42-13 AND 51-42-22.
CORROSION ON FLOOR SUPPORT, FS 280, LBL 9 - RBL 9. REPAIRED FS 280 FLOOR SUPPORT ANGLE BY CUTTING OUT CORRODED SECTION AND SPLICING A REPAIR SECTION IAW REO 601R-53-11-136, REV A.
CRACK INDICATION IN RADIUS OF LEFT FS 559 CAP ANGLE AT LBL 9 AND LBL 18. REPAIRED LEFT FS 559 CAP ANGLE AT LBL 9 AND LBL 18 IAW REO 601R-53-41-260 LT REP.
FS 559.00 RBL 18, WL 59.10, WEB CRACKED ADJACENT TO DOME NUT. REPAIRED FS 559 WEB AT RBL 18 BY CUTTING OUT DAMAGE AND INSTALLING A DOUBLER IAW REO 601R-53-41-260 RT REP.
FS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE CUTOUT. REPAIRED FS 202 BULKHEAD IAW REO601R53-11-563 REPAIR 2, REV-A, DATED 2011/04/04 AND DEVIATION REO601R-53-11-1968 REV A, DATED 2011/04/06.
FS 559 LOWER CAP ANGLE IS CRACKED AT RBL 9 AND RBL 18. REMOVED AND REPLACED DAMAGED SECTION OF 559 CAP ANGLE IAW REO 601R-53-41-260 RT REP.
FOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.
FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACK ON REAR PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 AND REO 601R-53-61-3460.
ON APPROACH, NR2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENGINE FUEL CONTROL.
ON APPROACH, NR 2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENG FUEL PUMP.
LT WING LOWER DRAIN ATTACHMENT HOLE JUST AFT OF PANEL 510 AB, BETWEEN WS 0.00 AND WS 22.50, AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.
LT WING LOWER DRAIN ATTACHMENT HOLES JUST FWD OF PANEL 540AB AT WS.0.00, FWD AND AFT SCREW HOLES ARE DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.
ENGINE CENTER SUPPORT BEAM IS CRACKED AT RBL 8.5 AT SENSING LOOP SUPPORT BRACKET. REPAIRED ENGINE SUPPORT BEAM PER CRJ REO 601R-53-61345 REV F.
LT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 540 AB, AT WS 67.75 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.
RT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 640 DB AT WS 85.50 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.
DURING CLIMBOUT FROM CVG RT ENG HIGH OIL TEMP. EMERGENCY DECLARED, ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND RT ENG AGB OVER SERVICED WITH OIL. REMOVED AND REPLACED RT ENG BYPASS CHECK VALVE. (S)
FLIGHT 5151 - ON TAKEOFF ROLL RECEIVED CONFIG SPOILERS MESSAGE WITH FLIGHT SPOILER MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. REMOVED AND REPLACED NR 2 SECU.
FLIGHT 5350 - RECEIVED STEERING INOP CAUTION. RAN QRH, DIVERTED TO PHL, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. A/C WAS TUGGED FROM RUNWAY. REPLACED RIGHT NOSE STEERING RVDT.
FLIGHT 5699 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS.
FLIGHT 5042 - AFTER TAKEOFF ENGAGED AUTO PILOT AT 12000 FT, AT 20000 FT FELT SLIGHT VIBRATION AND YAW MOTION. EICAS SHOWED AILERON FLUTTERING. REPLACED AILERON SERVO, INSPECTED AILERON AND RUDDER CONTROL SYSTEMS AND PERFORMED AUTO PILOT OPERATIONAL CHECKS. NO FURTHER DEFECTS.
FLIGHT 5284 - F/O WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD.
FLIGHT 5206 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED PDU.
FLIGHT 5011 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. 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 9495 - AFTER TAKEOFF AND DURING CLIMBOUT OF CVG ENCOUNTERED SURGING OF LEFT ENGINE N1 AND N2, FLIGHT RETURNED TO CVG. REPLACED THE LEFT SPEED CONTROL AMPLIFIER.
FLIGHT 5852 - RT THRUST REVERSER WARNING. SECURED CANNON PLUGS ON THE STOW, DEPLOY AND PDU SWITCHES. OPERATIONAL CHECKS NORMAL.
FLIGHT 5811- CABIN ALTITUDE CAUTION. F/A REPORTS LOUD SQUEAL FROM CABIN DOOR. FOUND DOOR TRIM OBSTRUCTING THE DOOR VENT VALVE, SECURED TRIM. PRESSURE CHECKS SATISFACTORY.
WHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX.
FLT 5372 RECEIVED A LT ENGINE COWL CAUTION DURING CRUISE FLIGHT (IND-JFK), AIRCRAFT DIVERTED TO CVG. REPLACED THE LT ENGINE ANTI-ICE COWL VALVE.
FLIGHT 4961 FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL HANDLE.
FLIGHT 5834 APU SMELLED LIKE FUEL, SMOKE COMING FROM INTAKE. COULD NOT DUPLICATE. INSPECTED APU FOR FUEL LEAKS. NO DEFECTS FOUND.
LOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539.
LOWER NOSE SKIN DAMAGED FORWARD OF FS 280 BETWEEN STRINGERS 25R AND 26R. REPAIRED IAW EA 10-5310-00515.
RIGHT HAND 718 FRAME CRACKED. REPAIRED IAW EO 53-027.
LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 10 AND 12. REPAIRED IAW EO 53-027.
LEFT HAND FS FRAME 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117.
FS 280 IS CORRODED ON FORWARD AFT ANGLES AFT OF CREW ENTRY WAY. REPAIRED IAW REO 601R-53-11-584.
FLIGHT 5731, CARGO SMOKE WARNING. COULD NOT DUPLICATE. FOUND NO DEFECTS, REPLACED DISCHARGED FIRE BOTTLES
FLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN AFT EQUIP BAY.
FLIGHT 5808 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED BLEED LEAK SENSING ELEMENT IN PYLON.
FLIGHT 5129 WING OVERHEAT WARNING DURING T/O. REPLACED THE ANTI-ICE CONTROLLER.
FLIGHT 5298 WING OVERHEAT MESSAGE DURING T/O. DEFERRED MAINT PER MEL.
FLIGHT 5295 NWS CAUTION MESSAGE AFTER T/O.COULD NOT DUPLICATE. SYSTEM TEST NORMAL.
FLIGHT 5708 WHEN FLIGHT SPOILERS DEPLOYED, AIRCRAFT ROLLED TO LEFT.REPLACED THE #2 SECU.
FLIGHT 5648 L/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #1 ADSHC.
FLIGHT 5420. FLAPS FAILED AT 23 DEGREES DURING LANDING APPROACH. POST FLIGHT INSP. FOUND R/H OUTBD FLAP TWISTED.REPLACED THE R/H OUTBD FLAP, BOTH FLAP ACTUATORS AND THE FLEX DRIVE SHAFT.
FLIGHT #5725. DURING CRUISE FLIGHT RECEIVED A FLAP SYSTEM FAIL CAUTION WITH FLAP AT ZERO DEGREE POSITION, CREW DECLARED AN EMERGENCY AND LANDED AT DESTINATION CITY ATW SAFELY.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT.
FLIGHT #N/A. EMERGENCY CEILING LIGHT AT ROW 13 IS INOPERATIVE.REPLACED THE EMERGENCY FLOOD LIGHT BULB AT ROW 13.
LEFT HAND EMERGENCY LIGHT IS INOPERABLE. REPLACED THE LIGHT BULB.
FLAPS FAIL CAUTION MESSAGE. REPLACED THE PDU.
LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED THE LT WINDOW HEAT CONTROLLER.
WHEN FLAP SELECTED TO 45 DEGGREES, THE AIRCRAFT ROLLED RIGHT. POST FLIGHT INSP FOUND RT FLIGHT SPOILER BROKEN. REPLACED FLIGHT SPOILER.
CONFIG STAB AND CONFIG TRIM WARNING. REPLACED THE HSTA.
APU OIL PRESSURE MESSAGE. REPLACED APU LOW OIL PRESSURE SWITCH.
EMERGENCY LIGHTS AFT OF ROW 9 ARE INOPERABLE. AFTER AIRCRAFT WARMED, COULD NOT DUPLICATE, EMERGENCY LIGHTS OPERATE NORMAL.
LEFT AOA HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKERS, SYSTEM FUNCITONS NORMAL.
FLAPS FAILED MESSAGE. REPLACED THE FLAP SELECTOR LEVER.
FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
DURING CLIMBOUT FROM CVG, THE RIGHT AOA CAUTION MESSAGE ACTIVAGED. AIRCRAFT RETURNED TO THE FIELD. CYCLED THE CIRCUIT BREAKER FOR THE RIGHT AIR DATA SENSING HEATER CONTROLLER.
DURING CLIMB-OUT FROM CVG, THE ANIT-ICE WARNING ACTIVATED, CREW FOLLOWED QRH PROCEDURE, MESSAGE CLEARED AFTER CLOSING 14TH STAGE BLEED AIR. PERFORMED AN ELECTRICAL CHECK OF LEFT AND RIGHT 14TH STAGE LOOPS AND PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED.
ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.
CARGO OVERHEAT WARNING. DEFERRED CARGO FAN.
FLAPS FAIL MESSAGE. REPLACED FECU.