N2092U
Registered owner: LAW ROBERT R, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SILVER STAR AVIATION | Operator | on 1988-10-30 | Operator named in NTSB report |
Accident & incident history
Operated by SILVER STAR AVIATION (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.
4 reports on file, 1995-05-31 – 1996-08-28.
Part: BLADE — CORRODED (M/R)
DURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND DELAMINATED AT TIP.
Part: LINK IDLER — WORN (PYLON)
DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 634.3 HOURS,
Part: LEVER ASSY — WORN (PYLON)
DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 634.3 HOURS,
Part: BULKHEAD — CRACKED (FORWARD ON T/B)
AFTER REMOVAL OF SHIMS TO COMPLY WITH TB 206L-94-169, CRACK WAS FOUND UNDER SHIM AT LEFT LOWER ATTACH POINT. APPARENTLY, A STRESS CRACK CAUSED BY WORKING RIVETS IN INTERCOSTAL ASSEMBLY.