N316CA

CESSNA 172M · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: CHOICE AVIATION LLC, MT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CHOICE AVIATION, LLC (VPEA)Certificate holder—Matched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

4 reports on file, 2006-06-08 – 2014-12-08.

OTHER · 2014-12-08 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (ZONE 100) · airframe 2,689 hrs

DURING ANNUAL INSPECTION, A LONGERON WAS FOUND CRACKED AT THE AFT MLG ATTACHMENT HOLE ON BOTH SIDES.

Source: SDR OG5S2014FA0000691
OTHER · 2010-11-17 Matched by certificate designator
ATA 6111

Part: BLADE — DELAMINATED (PROPELLER) · airframe 1,724 hrs

APPROX 8 INCHES OUT FROM BLADE CUFF IN CTR OF THE BACK OF THE PROP FOUND TO BE AN AREA OF DELAMINATION 1 INCH DIAMETER.

Source: SDR 2010FA0001185
FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2006-06-08 Matched by certificate designator
ATA 2810

Part: VENT LINE — CRACKED (FUEL CELL) · airframe 152 hrs · 152 cycles

CREW REPORTED STRONG SMELL OF FUEL IN CABIN. MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE AND CONNECTOR REPLACED NO LEAKS NOTED.

Source: SDR 2006FA0000590
FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2006-06-08 Matched by certificate designator
ATA 2810

Part: SLEEVE — BROKEN (FUEL LINE) · airframe 152 hrs · 152 cycles

CREW REPORTED STRONG ODOR OF FUEL IN CABIN.MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LEFT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE AND CONNECTOR REPLACED NO LEAKS NOTED.

Source: SDR 2006FA0000591