N341CA
Registered owner: COVENANT AIR LLC, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Comair Limited | Operator | on 1987-03-09 | 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.
20 reports on file, 1995-01-14 – 1996-04-16.
Part: GCU — OUT OF ADJUST (LT DC GEN)
LEFT DC GENERATOR FAILED AND WOULD NOT RESET. ADJUSTED THE LT GENERATOR CONTROL UNIT.
Part: EROSION GUARD — SEPARATED (RT PROP)
ONE BLADE ON RT PROPELLER, LEADING EDGE EROSION GUARD IS SEPARATING. REBONDED EROSION GUARD.
Part: WIRE — CHAFED (LT AC GENERATOR)
LEFT AC GENERATOR FAILED IN FLIGHT. REPAIRED WIRE NR XA510, XA509, XA508 AT WING FLAP INTERCONNECT AREA. WIRING WAS CHAFED AND BURNED.
Part: GCU — DEFECTIVE (LT DC GEN)
LEFT ENGINE WILL NOT START (NO ROTATION) USING CROSS GENERATOR PROCEDURE. REPLACED THE LT GENERATOR CONTROL UNIT. PART TOTAL CYCLES, 6,629.
Part: INLET — BURNED (RT ENGINE)
RT ENGINE INLET HEAT FAILED. REPLACED THE LOWER INLET ASSY. PART TOTAL CYCLES, 12,972.
Part: ANTI ICE VALVE — DEFECTIVE (RT ENGINE)
RT ENGINE INDICATED NO TORQUE DROP WHEN ANTI-ICE SELECTED ON. REPLACED THE ANTI-ICE VALVE. PART TOTAL CYCLES, 7,921.
Earlier reports · 1995 · 14 reports
1995
Part: DUCT ASSY — FAILED (RT ENGINE)
RT ENGINE INTAKE HEAT FAIL INDICATION AND A WHITE FLASHING GLOW VISIBLE INSIDE INTAKE. REPLACED UPPER INLET ASSY.
Part: CONTROLS — LACK OF LUBE (AILERONS)
AILERONS ARE BINDING. INSPECTED AILERON SYSTEM AND NO FAULTS FOUND. LUBRICATED AILERON CENTERING CAMS AND ACFT RETURNED TO SERVICE.
Part: SWITCH — DEFECTIVE (RT PITCH TRIM)
PITCH TRIM FUNCTION FROM COPILOTS POSITION IS INTERMITTENT. REPLACED THE COPILOTS PITCH TRIM SWITCH.
Part: PROPELLER HUB — CRACKED (BOLT HOLE)
DURING ULTRASONIC INSP OF HUB REAR FACE, A FLAW WAS INDICATED AT THE BOLT HOLE ADJACENT TO BLADE PORT NR 3. PROPELLER WAS DISSEMBLED, HUB (S/N CW1044) AND REMOVED FROM SERVICE.
Part: CONNECTOR — DEFECTIVE (RT NACELLE)
RIGHT TAIL PIPE HOT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. ENGINE WAS SHUT DOWN AND LIGHT EVENTUALLY WENT OUT. FLIGHT RETURNED TO CVG. REPLACED WIRING CONNECTOR 162VP.
Part: HUB — CRACKED (PROPELLER)
DURING OVERHAUL INSPECTION MULTIPLE CRACK INDICATIONS WERE FOUND DURING ULTRASONIC INSPECTION (IAW SB 61-58 APPENDIX C, SCAN B) HUB S/N 110502 WAS DISASSEMBLED AND REMOVED FROM SERVICE.
Part: DETECTOR — FALSE WARN (CARGO)
CARGO SMOKE WARNING ACTIVATED DURING TAKEOFF. REPLACED THE CARGO SMOKE DETECTOR.
Part: HOT WARNING — ILLUMINATED (RT TAIL PIPE)
RT TAIL PIPE HOT WARNING LIGHT CAME ON AFTER TAKEOFF. COULD NOT DUPLICATE PROBLEM. INSPECTED SYSTEM AND FOUND NO DEFECTS.
Part: PROP BLADE — DAMAGED (RT ENGINE)
RT PROPELLER, BLADE LEADING EDGE ERROSION GUARD IS LOOSE. REPLACED PROPELLER ASSY.
Part: BOLT — BROKEN (LT ELEVATOR)
DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR MOST INBD COUNTER WEIGHT BOLT BROKEN. REPLACED BROKEN COUNTER WEIGHT BOLT.
Part: LAMP — FAILED (INST PANEL)
RT MLG DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. FOUND INDICATOR LAMPS IN CONTROL HANDLE TO BE AT FAULT. REPLACED LAMPS.
Part: INNER RACE — SPUN (RT MLG WHEEL)
MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO THE WORN LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR.
Part: QUADRANT — MALFUNCTIONED (COCKPIT)
FRICTION LOCK ON CONTROLS QUADRANT IS NOT WORKING. REPLACED QUADRANT.
Part: CONNECTOR — DIRTY (RT NACELLE)
RT TAIL PIPE HOT WARNING ACTIVATED DURING CLIMB. CLEANED WIRING CONNECTION FOR TAIL PIPE HEAT SENSORS AND AIRCRAFT RETURNED TO SERVICE.