N164CA
Registered owner: CIRRUS DESIGN CORP, MN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
2 reports on file, 2012-05-10 – 2018-10-04.
Part: ATTACH BOLT — SEIZED (NLG) · airframe 11,722 hrs
AIRCRAFT HAD NOSE GEAR UP LANDING. THROUGH INVESTIGATION THE AIRCRAFT MAINTENANCE DEPARTMENT HAS DETERMINED THAT THE INCIDENT WAS CAUSED BY THE DRAG LINK BOLT P/N 400-191 (ITEM 69 IN THE IPC) BECOMING SEIZED IN THE NOSE GEAR SPRING ARM ASSEMBLY P/N 67109-000 (ITEM 56 IN THE IPC). THIS ASSEMBLY REQUIRES MOVEMENT OF THE NOSE GEAR SPRING ARM ASSEMBLY, AROUND THE BOLT (ITEM 69 IN THE IPC), DURING GEAR RETRACTION AND EXTENSION. THE FAULT WAS CAUSED BY THE NOSE GEAR SPRING ARM ASSEMBLY TURNING THE SEIZED BOLT (ITEM 69 IN THE IPC). THE ATTACHING NUT (ITEM 69C IN THE IPC), WHEN INSTALLED CORRECTLY, HAS ENOUGH FRICTION TO REMAIN IN PLACE AND WHEN THE SEIZED BOLT (ITEM 69 IN THE IPC) TURNED IT SHEARED THE COTTER PIN P/N 424-052 (ITEM 69D IN THE IPC). THE NOSE GEAR SPRING ARM ASSEMBLY CAN THEN WORK ITSELF OUTBOARD AND AFTER GEAR RETRACTION, THE NOW OUT OF POSITION, NOSE GEAR SPRING ARM ASSEMBLY PREVENTS THE NOSE GEAR FROM EXTENDING PROPERLY.
Part: HOOK AND LOOP — WORN (EXIT PANEL) · airframe 17,570 hrs · 11,920 cycles
RT EMERGENCY EXIT PANEL COVER WON'T STAY ON. R & R HOOK AND LOOP ON RT EXIT PLANEL COVER IAW AMM 25-26-04.