N27766
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.
28 reports on file, 1995-06-13 – 2003-06-09.
Part: RESTRAINT — STUCK (M/R HEAD)
FLAP RESTRAINT STICKING. REPAIRED.
Part: BEARING — WORN (BELLCRANK ASSY)
CYCLIC CONTROL BELLCRANK HAS PLAY IN THE PIVOT BEARING. REPLACED BEARING DUE TO BEING WORN. REPAIRED.
Part: STARTER GEN — FAILED (ENGINE) · airframe 13,767 hrs
STARTER GENERATOR WILL NOT STAY ON LINE.
Part: MIXER BOX — MALFUNCTIONED (COMM SYS) · airframe 13,455 hrs
FM RADIO RECEIVES WEAK ON PILOT SIDE. REPAIRED.
Earlier reports · 1995–2002 · 24 reports
2002
Part: FITTING — CRACKED (ENGINE OIL) · airframe 13,236 hrs
OIL LEAKING FROM ELBOW JAMB NUT. FOUND FITTING CRACKED AT JAMB NUT FLANGE. CRACK RUNS AROUND RADIUS AND MEASURES APPROXIMATELY 1/4 IN LENGTH. REPLACED FITTING.
Part: RADIO — WEAK (FM SYSTEM) · airframe 13,455 hrs
FM RADIO RECEIVE WEAK ON PILOT SIDE. REPLACED WITH SERVICEABLE PART.
2001
Part: INTERPHONE — MALFUNCTIONED (CABIN)
SENSITIVITY TOO LOW.
1999
Part: INDICATOR — INACCURATE (DUAL TACHOMETER)
DUAL TACHOMETER INDICATORS HAVE 3 PERCENT SPLIT.
Part: EXHAUST STACK — CRACKED (ENGINE)
EXHAUST ASSEMBLY CRACKED.
Part: RECEIVER — MALFUNCTIONED (LORAN)
RIGHT OUTER KNOB PULLS OUT BUT DOES NOT SCROLL NUMBERS ON LORAN.
1997
Part: INDICATOR — CRACKED (VERT SPEED)
VERT SPEED INDICATOR STATIC PORT IS CRACKED.
Part: INDICATOR — CRACKED (VERT SPEED)
VERT SPEED INDICATOR STATIC PORT IS CRACKED.
Part: COMPASS — DEFECTIVE (COCKPIT)
COMPASS WITH NOT SWING.
Part: ALTIMETER — DEFECTIVE (COCKPIT)
KOLLSMAN KNOB WILL NOT ADJUST AND DIAL INVERTED.
Part: PANEL ASSY — SEPARATED (FUSELAGE)
PANEL ASSY SEPARATED; NOT REPAIRABLE AT THIS STATION.
Part: TRANSCEIVER — MALFUNCTION (COCKPIT VHF)
POWER OUT HESITATING AT 138.000MHZ AND 138.1000MHZ.
Part: TRANSMITTER — DEFECTIVE (FUEL QTY)
DOES NOT TRANSMIT SIGNAL TO INDICATOR FROM ZERO TO 120 LBS.
Part: FUEL CELL — UNBONDING (FLANGE)
FUEL CELL HAS EXCESSIVE BLISTERING AND UNBONDING FLANGE AND CRACKING.
Part: CYLINDER — LEAKING (M/R)
M/R SERVO LEAKING AT FORWARD END.
Part: OIL COOLER — DAMAGED (ENG OIL)
OIL COOLER HAS DAMAGED FINS. NEEDS RECORING.
Part: LONGERON — MIS MFG (FUSELAGE)
UPPER FLANGE AT AFT END OF LONGERON IS ABOUT 1/8" SHORTER THAN EXISTING LONGERON. ALSO, THE AFT END OF LONGERON IS ABOUT 1/8" WIDER THAN EXISTING LONGERON.
Part: EXHAUST ASSY — CRACKED (ENGINE)
STACK CRACK ON BACKSIDE AT CENTER WELD AT BOTTOM.
1996
Part: RESTRAINT — WORN EXCESS (XMSN)
RESTRAINT IS WORN EXCESSIVELY. (UNSTAKED BEARING)
Part: TRANSDUCER — DEFECTIVE (FUEL PRESSURE)
INDICATES "0" PRESSURE.
1995
Part: BLADE — CORRODED (M/R)
EXCESSIVE AMOUNT OF EXFOLIATION OF THE LEADING EDGE.
Part: SUPPORT — DEFECTIVE (SWASHPLATE)
PER ASB 206L-93-89N REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)
Part: CONTROL UNIT — DEFECTIVE (COCKPIT VHF)
100MHZ THUMBWHEEL INTERMITTENT. REPLACED S1 THUMBWHEEL. REPAIRED.
Part: BLADE — CORRODED (M/R)
SEVERAL AREAS OF INNER GRANULAR CORROSION ON THE LEADING EDGE SPAR. BLADE HELD IN BLADE SHOP