N85SC

TEXTRON AVIATION INC 525 · 2015 · Fixed-wing multi-engine · 2 engines · 8 seats · Valid Registration

Registered owner: STRUTHOFF CO INC, TX (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
MILLER, DAVEOperatoron 2007-05-22Operator named in NTSB report

Accident & incident history

Accident · 2007-05-22 Operator named in NTSB report
Cessna 421C No injuries Part 135MILLER, DAVE

Operated by MILLER, DAVE (per NTSB report)

Source: NTSB case CHI07CA152

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, 1997-07-03 – 2006-11-11.

OTHER · 2006-11-11 Matched by certificate designator
ATA 5751

Part: SKIN — DEBONDED (RT AILERON)

RT AILERON WAS REMOVED FROM AIRCRAFT DUE TO DEBONDING. SKIN OF AILERON WAS DEBONDED IN SEVERAL PLACES ALONG THE RIBS AND SPAR. SUSPECTED CAUSE IS AGE. (K)

Source: SDR MLJ2006F00001
VIBRATION/BUFFET; PARTIAL RPM/PWR LOSS · 1997-07-03 Unresolved
ATA 8530

Part: VALVE SPRING — FAILED (NR 2 CYLINDER)

THE PILOT NOTICED A VIBRATION AT CRUISE POWER AFTER AN HOUR OF FLIGHT. AFTER LANDING, INVESTIGATION REVEALED THE RIGHT ENGINE WOULD INCREASE IN VIBRATION WITH AN INCREASE IN RPM AND NOT DEVELOP FULL RPM. TROUBLESHOOTING REVEALED THE NR 2 CYLINDER HAD BOTH INNER VALVE SPRINGS BROKEN WHICH ALLOWED THE VALVES TO FLOAT AS RPM WAS INCREASED. REPLACEMENT OF THE VALVE SPRINGS CORRECTED THE PROBLEM. SUBMITTER STATED THIS IS THE SECOND INSTANCE TO ENCOUNTER A BROKEN INNER VALVE SPRING ON THIS SAME TYPE OF ENGINE.

Source: SDR 97ZZZX3495