N27545
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.
11 reports on file, 1995-01-26 – 2002-03-21.
Part: SHAFT — WORN (SPUR ADAPTER)
ENGINE MAKING METAL. WORN AFT SPLINES BELOW SPECS.
Part: BLADE — CORRODED (MAIN ROTOR)
INSPECTION OF AIRCRAFT DURING REFURBISHING, FOUND INTERGRANULAR CORROSION OF LEADING EDGE OF MAIN ROTOR BLADES. (X)
Part: BLADE — CORRODED (MAIN ROTOR)
INSPECTION OF AIRCRAFT DURING REFURBISHING FOUND INTERGRANULAR CORROSION OF LEADING EDGE OF MAIN ROTOR BLADES. (X)
Part: BLADE — CRACKED (M/R)
DISCOVERED DURING DAILY INSPECTION, M/R BLADE SPAR CRACKED AT TIP.
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 NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 284.1 HOURS.
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 NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 284.1 HOURS.
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, NAS6605D64, BOLTS, 1 EACH, 206-010-470-101, BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 467.7.
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, NAS6605D64, BOLTS, 1 EACH, 206-010-470-101, BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 467.7.
Part: BEARING — ROUGH (ARMATURE SHAFT)
ON RUN-UP, FOUND ENGINE MAXIMUM ATTAINABLE N2 RPM WAS 95 PERCENT, ALSO, TORQUE WAS FLUCTUATING. VIBRATION OF STARTER/GENERATOR WAS HARMONICAL WITH THE FUEL CONTROL RPM CAUSING FLUCTUATION. ON DISASSEMBLY OF THE STARTER/GENRATOR, THE BEARING WAS FOUND ROUGH AND GREASE WAS DRY. LUBRICANT IN BEARING APPEARS TO BE THE ABSOLUTE MINIMUM QUANTITY.
Part: LINK IDLER — WORN (PYLON)
DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, PN 206-010-338-001 SPACERS, 4 EACH, PN 206-010-337-001 BEARINGS, 2 EACH, NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, AND BOLTS TT 410.5.
Part: LEVER ASSEMBLY — WORN (PYLON)
DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, PN 206-010-338-001 SPACERS, 4 EACH, PN 206-010-337-001 BEARINGS, 2 EACH, NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, AND BOLTS TT 410.5.