N784CA
Registered owner: EAGLE CAPITAL HOLDINGS LLC, PA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Comair Limited | Operator | on 2001-01-08 | Operator named in NTSB report |
Accident & incident history
Operated by COMAIR INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
45 reports on file, 1999-10-03 – 2011-11-11.
Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 28,292 hrs · 25,318 cycles
ON CLIMBOUT FROM RDU LANDING GEAR WOULD NOT RETRACT. EMERGENCY DECLARED, A/C RETURNED TO RDU LANDED SAFELY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. NO FURTHER DEFECTS NOTED.
Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 27,491 hrs · 24,516 cycles
ON CLIMBOUT FROM JAX, CLIMBING THROUGH 15000FT RECEIVED STAB TRIM/MACH TRIM CAUTION MSG, UNABLE TO REENGAGE. EMERGENCY DECLARED, A/C RETURNED TO JAX LANDED SAFELY. REMOVED AND REPLACED HORIZONTAL STAB TRIM MCU. OPS CHECK GOOD.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,800 hrs · 23,869 cycles
CRACK IN RT SIDE CAP ANGLE OF FS 559 AT RBL 18.00. REMOVED DAMAGE AND INSTALLED REPAIR IAW REO 601R-53-41-260.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,800 hrs · 23,869 cycles
FS 559 CAP ANGLE CRACKED AT LBL 9. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW REO 601R-53-41-260 AND TASK CARD REO 601R-53-41-260 LT REP.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,800 hrs · 23,869 cycles
FS 559 CAP ANGLE CRACKED AT LBL 18. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW REO 601R-53-41-260 AND TASK CARD REO 601R-53-41-260 LT REP.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,800 hrs · 23,869 cycles
CRACK IN CAP ANGLE OF FS 559 AT LBL 18.00 AND LBL 9.00. REMOVED DAMAGE AND INSTALLED REPAIR IAW REO 601R-53-41-260.
Earlier reports · 1999–2010 · 39 reports
2010
Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 25,057 hrs · 22,346 cycles
ON CLIMBOUT FROM JFK RECEIVED FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 8 DEG ON RETRACTION. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.
2008
Part: FLAP — MALFUNCTIONED (WING) · airframe 23,150 hrs · 20,763 cycles
ON APPROACH INTO FSD RECEIVED FLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS TO 8 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.
Part: SKIN — DAMAGED (LT WING) · airframe 23,006 hrs · 20,650 cycles
FUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON AFT SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEABLE FREEZE PLUG BUSHING FOR FUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT AFT SCREW ATTACH HOLE IAW COMAIR EA # 10-5721-02413.
Part: REPAIR — CRACKED (LT ENGINE BEAM) · airframe 23,006 hrs · 20,650 cycles
LT SIDE OF ENGINE BEAM PREVIOUS REPAIR ON LOWER OTBD WEB IS CRACKED. REMOVED AND INSTALLED SERVICEABLE REPAIR PARTS PER REO 601R53-61-366.
Part: SKIN — CORRODED (RT WING) · airframe 23,006 hrs · 20,650 cycles
RT WING FUEL ACCESS PANEL CUTOUT AT 640BB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE NON CRITICAL AREA AT FUEL ACCESS PANEL 640BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
Part: SKIN — DAMAGED (LT WING) · airframe 23,006 hrs · 20,650 cycles
FUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON FWD SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEABLE FREEZE PLUG BUSHING FOR FUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT FWD SCREW ATTACH HOLE IAW COMAIR EA # 10-5721-02413.
Part: SKIN — CRACKED (PAX DOOR) · airframe 23,006 hrs · 20,650 cycles
PAX DOOR INNER SKIN IS CRACKED AT DOOR DATUM 1 BETWEEN FS340 AND DOOR DATUM 1. CUT OUT DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER WITH SHIMS PER EA 10-5210-02412 DATED 10/06/08.
Part: SKIN — CORRODED (LT WING) · airframe 23,066 hrs · 20,650 cycles
LT WING FUEL ACCESS PANEL CUTOUT AT 510AB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 510AB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
Part: FITTING — CRACKED (LT MLG ACTUATOR) · airframe 23,006 hrs · 20,650 cycles
LT MLG SIDE STAY ACTUATOR UPPER FITTING CRACKED. R&R SERVICEABLE LT SIDE STAY ACTUATOR UPPER FITTINGS.
Part: ACTUATOR — FAULTY (AILERON TRIM) · airframe 21,928 hrs · 19,774 cycles
FLIGHT 9657 - HESITATION FELT IN CONTROLS WHEN TURNING RIGHT, AUTO-PILOT OFF, ALL HYDRAULICS ON, PILOT AND CO-PILOT SIDES. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED AILERON TRIM ACTUATOR. NO FURTHER DEFECTS.
2007
Part: COMPUTER — FAILED (E&E BAY) · airframe 21,067 hrs · 19,110 cycles
FLIGHT 5452 - AHC NR 1 FAILED EN ROUTE, CVG TO ABE. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NR 1 AHC.
Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 26,985 hrs · 19,033 cycles
FLIGHT 5218 - BOTH CARGO FIRE LIGHTS ILLUMINATED UPON LANDING. COMPLIED WITH QRH PROCEDURE, BOTH BOTTLES DISCHARGED. REMOVED AND REPLACED CARGO FIRE CONTROL PANEL.
Part: SMOKE WARNING — ACTIVATED (CARGO BAY) · airframe 20,981 hrs · 19,031 cycles
FLIGHT 5539 - CARGO SMOKE MESSAGE ILLUMINATED. DISCHARGED NORMAL AND STANDBY BOTTLES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT CARGO FIRE EXTINGUISHER BOTTLE. NO FURTHER DEFECTS.
Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY) · airframe 20,981 hrs · 19,031 cycles
FLIGHT 5539 - CARGO SMOKE MESSAGE ILLUMINATED. DISCHARGED NORMAL AND STANDBY BOTTLES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT CARGO FIRE EXTINGUISHER BOTTLE. NO FURTHER DEFECTS.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,317 hrs · 17,683 cycles
FLIGHT 5620 - RECEIVED FLAPS FAIL MESSAGE ON APPROACH, DECLARED EMERGENCY, 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 MESSAGES.
Part: ENGINE — POWER LOSS (NR 2) · airframe 19,210 hrs · 17,602 cycles
FLIGHT 5103 - DURING ADDITION OF POWER FOR TAKEOFF NR 2 ENGINE WILL NOT SPOOL ABOVE 30 PERCENT. ABORTED TAKEOFF AT 15 KTS. INSPECTED ENGINE, NO DEFECTS NOTED. PERFORMED LOW AND HIGH POWER RUNS, NO DEFECTS NOTED (CND).
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 19,171 hrs · 17,573 cycles
FLIGHT 5317 - DURING CLIMBOUT OF CVG RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. ADJUSTED THE NLG PROXIMITY SENSOR S03 AND RETRACTED LANDING GEAR MULTIPLE TIMES WITH NO DISCREPANCIES NOTED.
2006
Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 18,925 hrs · 17,380 cycles
FLIGHT 5431 - EN ROUTE MSN-ATL RECEIVED A RIGHT ENGINE COWL ANTI-ICE MESSAGE, FLIGHT DIVERTED TO CVG. REPLACED THE COWL ANTI-ICE VALVE.
Part: PUMP — FAULTY (HYD SYSTEM) · airframe 18,872 hrs · 17,351 cycles
FLIGHT 5347 - ON APPROACH RECEIVED GEAR DISAGREE, NOSE DOOR WARNING. INDICATION WENT AWAY IN ABOUT 10 SECONDS. RECEIVED 3 GREEN, LANDED WITHOUT INCIDENT. FOUND 3B ACMP TO BE PRODUCING LOW PRESSURE ON GEAR RETRACTION AND EXTENSION. REPLACED 3B PUMP. NO FURTHER DEFECTS.
Part: FLOORBEAM — CRACKED (FS 484) · airframe 18,444 hrs · 17,007 cycles
ANGLE BRACKET AT FS 484.00 RBL36 MARKED IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET CLIP IAW REO 601R-53-41-059.
Part: CONTROLLER — SURGES (ENGINE SPEED) · airframe 18,263 hrs · 16,856 cycles
FLIGHT 5320 - EN ROUTE CVG-GSO ENCOUNTERED SURGING OF THE LEFT ENGINE N1 AND N2, FLIGHT RETURNED TO CVG. DEFERRED THE ENGINE SPEED CONTROLLERS PER MEL 76-11-01.
Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 16,692 hrs · 15,820 cycles
FLIGHT 5153 - SMOKE IN COCKPIT. CLEANED THE COALESCER BAGS, RAN BOTH PACKS, NO SMELL OR SMOKE.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 16,878 hrs · 15,739 cycles
FLIGHT 5233 - EMERGENCY LIGHT AT EXIT DOOR IS INOPERABLE. REPAIRED BROKEN WIRE AT LIGHT.
2004
Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 18,259 hrs · 17,642 cycles
CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. REPAIRED IAW REO 601R-53-61-870.
Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 12,353 hrs · 11,820 cycles
FLIGHT 5229 EMERGENCY FLOOD LIGHT AT CABIN DOOR IS INOP. REPLACED THE NR 2 EMERGENCY BATTERY.
2002
Part: UPLOCK · airframe 7,378 hrs · 7,589 cycles
FLIGHT 5646 GEAR DISAGREE MESSAGE WHEN GEAR SELECTED DOWN.ADJUSTED THE NLG UPLOCK ASSY.
Part: LANDING GEAR · airframe 7,306 hrs · 7,518 cycles
FLIGHT 5429 GEAR DISAGREE WARNING WHEN GEAR SELECTED DOWN.COULD NOT DUPLICATE EXTENSION AND RETRACT CHECKS WERE NORMAL.
Part: ALTERNATOR · airframe 6,836 hrs · 7,052 cycles
FLIGHT 9478 - LOUD VIBRATION DURING GEAR RETRACTION.FOUND ADG DEPLOYED - STOWED ADG AND SYSTEM TEST NORMAL.
Part: VALVE — MALFUNCTIONED (NLG) · airframe 6,836 hrs · 7,052 cycles
FLIGHT 5004 - NLG DID NOT RETRACT.REPLACED THE NLG SELECTOR VALVE.
2001
Part: WINDOW — INOPERATIVE (L/H) · airframe 5,503 hrs · 5,666 cycles
FLIGHT - LEFT WINDOW HEAT FAIL MESSAGE.REPLACED THE PILOTS LEFT SIDE WINDOW.
Part: SKIN · airframe 4,979 hrs · 5,119 cycles
FLIGHT 5774. BIRDSTRIKE DURING T/O. T/O ABORTED.C/W BIRDSTRIKE INSPECTION. NO DAMAGE FOUND. C/W REJECTED T/O INSPECTION NO DAMAGE FOUND.
Part: BPSU — FAULTY (LEFT WING) · airframe 4,764 hrs · 4,880 cycles
FLIGHT #5494. DURING CHA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITION, AIRCRAFT LANDED SAFELY.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT.
Part: DRIVE GEAR — FAULTY (CENTER WING) · airframe 4,764 hrs · 4,880 cycles
FLIGHT #5494. DURING CHA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITON, AIRCRAFT LANDED SAFELY.REPLACED THE FLAP POWER DRIVE UNIT.
Part: HOSE — DAMAGED (COCKPIT) · airframe 4,004 hrs · 4,087 cycles
DAMAGE TO HOSE UNDER PILOTS SIDE PITOT TUBE. REPAIRED PER REO 601R-53-2108.
2000
Part: VALVE — MALFUNCTIONED (LT ANTI ICE SYS) · airframe 3,947 hrs · 4,026 cycles
LEFT ENGINE COWL ANTI-ICE IS INOPERABLE. REPLACED COW ANTI-ICE VALVE.
Part: PRESSURE SWITCH — MALFUNCTIONED (APU) · airframe 2,737 hrs · 2,779 cycles
APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE OIL PRESSURE SWITCH.
Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 2,215 hrs · 2,274 cycles
FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
Part: WIRE — DAMAGED (ROW 1) · airframe 2,168 hrs · 2,220 cycles
FLOOR TRACK LIGHTING AT ROW 1 IS INOPERABLE. REPLACED THE CABLE ASSY.
1999
Part: RADONE — BIRD STRIKE (NOSE)
AFTER DEPARTURE FROM CVG, THE AIRCRAFT ENCOUNTERED A BIRD STRIKE ON NOSE SECTION. AIRCRAFT RETURNED TO THE FIELD. COMPLIED WITH BIRD STRIKE INSPECTION, NO DEFECTS NOTED.