N431CA
Registered owner: CHEM-AIR LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CHEM-AIR, LLC (GOXA) | Certificate holder | — | Matched by certificate designator |
| Comair Limited | Operator | on 2006-08-27 | 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.
23 reports on file, 2001-08-05 – 2005-11-01.
Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 12,598 hrs · 10,486 cycles
FLIGHT 5118 - RT REVERSER UNLOCKED MESSAGE. RT REVERSER WAS PREVIOUSLY DEFERRED, FOUND CONNECTOR STILL CONNECTED. REMOVED AND STOWED CONNECTOR PER MEL.
Earlier reports · 2001–2004 · 22 reports
2004
Part: FRAME — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
RIGHT 640 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-487.
Part: SILL — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
CARGO LANDING PLATE CRACKED AROUND LOCK FITTING HOLE ON FORWARD SCUFF PLATE FITTING AT 574.00. REPAIRED IAW REO 601R-53-61-1222.
Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 10,138 hrs · 8,284 cycles
LEFT HAND LOWER ENGINE SUPPORT BEAM HAS CRACK. REPAIRED IAW REO 601R-53-61-366.
Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
RIGHT LOWER ENGINE SUPPORT BEAM CRACK. REPAIRED IAW REO 601R-53-61-366.
Part: FRAME — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
LEFT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117.
Part: FRAME — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
RIGHT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 10,138 hrs · 8,284 cycles
LEFT HAND INTERCOSTALS AT FS 484.00 OUTBOARD CRACKED. REPAIRED IAW REO 601R-53-41-059.
Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 9,930 hrs · 8,080 cycles
FLIGHT 4973 FUEL INBALANCE CAUTION MESSAGE. REPLACED THE CROSS FLOW PUMP.
Part: SENSING ELEMENT — DAMAGED (LT PYLON) · airframe 9,491 hrs · 7,735 cycles
DURING CLIMB OUT OF RDU RECEIVED A LT 14TH STAGE DUCT WARNING, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LT PYLON BLEED LOOP SENSING ELEMENT AW59WK.
2003
Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 5,018 hrs · 4,148 cycles
FLIGHT 5002 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
2002
Part: PDU — FAILED (T/E FLAP) · airframe 2,285 hrs · 1,945 cycles
FLAPS FAILED AT 20 DEGREES. REPLACED THE FLAP PDU.
Part: COMPUTER · airframe 2,250 hrs · 1,922 cycles
FLIGHT 5356 YAW DAMPNER #1 INOP WARNING DURING T/O.RESET IAPS SYSTEM - YAW DAMP SYTEM TEST NORMAL.
Part: FCU · airframe 2,103 hrs · 1,802 cycles
FLIGHT 5471 FLAPS FAIL MESSAGE.ADJUSTED THE FECU POTENTIOMETERS.
Part: FCU — MALFUNCTIONED (AVIONICS) · airframe 1,822 hrs · 1,571 cycles
FLIGHT 5583 FLAPS FAIL MESSAGE DURING PUSH-BACK.REPLACED THE FECU.
2001
Part: FCU — MALFUNCTIONED (AVIONICS) · airframe 814 hrs · 692 cycles
FLIGHT #5453. FLAPS FAILED AT 30 DEGREES DURING DESCENT.REPLACED THE FECU.
Part: CARD — FAULTY (AVIONICS BASY) · airframe 595 hrs · 510 cycles
FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 FCC CARD. (FCC-4000)
Part: DAMPER — FAULTY (AVIONICS BAY) · airframe 595 hrs · 510 cycles
FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #2 YAW DAMPER ACTUATOR. (SVL-4000).
Part: DAMPER — FAULTY (AVIONICS BAY) · airframe 595 hrs · 510 cycles
FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #1 YAW DAMPER ACTUATOR. (SVL-4000).
Part: CARD — FAULTY (AVIONICS BAY) · airframe 595 hrs · 510 cycles
FLIGHT #5247. DURING CRUISE FLIGHT THE AIRCRAFT DEMONSTRATED YAW CHARACTERISTICS, ESPECIALLY DURING CLIMB.REPLACED THE #1 FCC CARD. (FCC-4000)
Part: LIGHT · airframe 501 hrs · 429 cycles
FLIGHT #5570. DURING PRE-FLIGHT INSPECTION AT GRR FOUND SECTION OF RIGHT FLOOR EMERGENCY LIGHTING INOPERATIVE.CLEANED AND RE-SEATED AFFECTED FLOOR EMERGENCY LIGHTING STRIPS, OPERATIONAL CHECK WAS SATISFACTORY.
Part: LIGHT — FAULTY (FLOOR) · airframe 503 hrs · 430 cycles
FLIGHT #5339. DURING PRE-FLIGHT AT CVG FOUND SECTION OF FLOOR EMERGENCY LIGHTING INOPERATIVE.REPLACED EMERGENCY FLOOR LIGHT TRACKS ROWS 2 THROUGH 5 ON RIGHT SIDE OF CABIN.
Part: BATTERY PACK — FAULTY · airframe 413 hrs · 363 cycles
FAINT ELECTRICAL ODOR FROM THE GALLEY AREA DISCOVERED AFTER LANDING.REPLACED THE EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK.