N205FC
Registered owner: GM LEASING CO LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Survival Flight Services LLC (7ALA) | Certificate holder | — | Matched by certificate designator |
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.
32 reports on file, 1995-11-08 – 2012-04-18.
Part: WEB — CORRODED (CARGO DOOR) · airframe 20,156 hrs
CARGO DOOR WEB WAS FOUND TO BE CORRODED.
Part: WIRE — BROKEN (INTERCOM) · airframe 20,104 hrs
INTERCOM SWITCH SPARKED AND SMOKED WHEN DEPRESSED. INSPECTED AND FOUND ICS SWITCH WIRING BROKEN AT SWITCH AND ARCING ACROSS CYCLIC STICK. RESOLDERED WIRING AT SWITCH AND TESTED GOOD.
Earlier reports · 1995–2003 · 30 reports
2003
Part: TUBE — CORRODED (FUEL DIST) · airframe 13,804 hrs
FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.
Part: TUBE — CORRODED (FUEL DIST) · airframe 13,804 hrs
FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.
Part: FUEL CELL — DAMAGED (FUSELAGE) · airframe 13,804 hrs
FUEL CELL HAS A LARGE BLISTER INSIDE ON THE LOWER BACK EDGE.
Part: TUBE — CORRODED (FUEL DIST) · airframe 13,804 hrs
FUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.
Part: BEARING — WORN (HORN ASSY)
HORIZONTAL STAB HORN HAS A WORN BEARING. REPAIRED.
Part: BATTERY — WEAK (MAIN) · airframe 13,657 hrs
MAIN BATTERY WEAK. REPLACED BATTERY.
Part: ELT — WILL NOT TEST (CABIN) · airframe 13,701 hrs
ELT WOULD NOT TEST ON MONTHLY INSPECTION.
2002
Part: RECEIVER — INTERMITTENT (LORAN SYS) · airframe 13,668 hrs
LORAN SYSTEM LOSES POWER INTERMITTENTLY. REPLACED WITH SERVICEABLE PART.
Part: BEARING — WORN (T/R CONTROL TUBE)
TAIL ROTOR CONTROL TUBE HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART.
2001
Part: TRANSCEIVER — FAILED (VHF COMMS) · airframe 13,353 hrs
FIRST AND LAST DIGITS DISAPPEAR INTERMITTENTLY. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY NOT DIMMING PROPERLY. REPLACED V901 PHOTOCELL. REPAIRED. FOUND FREQUENCY SELECTORS INTERMITTENT AND MHZ CHANGED BY ITSELF A COUPLE OF TIMES. FOUND FREQUENCY SELECTOR CONTACTS VERY DIRTY. CLEANED. REPAIRED. REGLUED DISPLAY LENS WHICH WAS LOOSE. ADJUSTED FREQUENCY. BENCH CHECK GOOD.
1999
Part: STACK — CRACKED (EXHAUST SYSTEM)
CRACK NEXT TO VOID ON AFT LOWER RIGHT SIDE OF EXHAUST ASSEMBLY.
Part: RECEIVER — ERRATIC (LORAN)
RECEIVER HAD ERRATIC OPERATION.
Part: REGULATOR — FAILED (DC SYSTEM)
VOLTAGE REGULATOR WILL NOT COME ON-LINE.
Part: INDICATOR — STICKS (FUEL QUANTITY)
FUEL QUANTITY INDICATOR'S NEEDLE STICKS THROUGHOUT RANGE.
1998
Part: INDICATOR — FAILED (DUAL TACH)
DUAL TACHOMETER TURBINE NEEDLE INTERMITTENTLY FALLS OFF.
Part: TACH GENERATOR — FAILED (ROTOR)
TACH GENERATOR FAILED. NO ROTOR INDICATION.
Part: INDICATOR — MIS MARKED (DUAL TACH)
DUAL TACH HAS WRONG RANGE MARKINGS. NEEDS YELLOW BAND FROM 100% TO 103%.
Part: ALTIMETER — LEAKING (COCKPIT)
ALTIMETER LEAKING AT KNOB.
Part: CYLINDER — LEAKING (M/R SERVO)
SERVO LEAKING AT BOTH ENDS OF CYLINDER. TIME SINCE REPAIR 0:00.
Part: STABILIZER ASSY — DEFECTIVE (GUIDE PINS)
STAB ASSY GUIDE PINS STUCK. SEPARATED ON FRONT EDGE.
1997
Part: INDICATOR — FAILED (ENG TOT)
ENG TOT INDICATOR READS 4 UNITS HIGH
Part: FUEL CELL — LEAKAGE (CELL SEAMS)
FUEL CELL EXCESSIVE CRACKS ON SEAMS. EXCESSIVE LEAKAGE.
Part: SKID TUBE — CRACKED (RT SKID)
RT SKID TUBE CRACKED BELOW AFT CROSSTUBE SUPPORT. SCRAPPED AND REPLACED WITH SERVICEABLE SKID TUBE.
Part: SKID TUBE — CORRODED (LT SKID)
SKID TUBE CORRODED DEPTH BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE SKID TUBE.
Part: STOP ASSY — DELAMINATED (M/R MOUNT)
STOP ASSY DELAMINATED.
Part: RESTRAINT — DETERIORATED (XMSN)
TRANSMISSION RESTRAINT RUBBER DETERIORATION.
Part: TACH GEN — DEFECTIVE (ROTOR)
TACH GEN RPM INDICATOR NEEDLE BOUNCES ON START.
1996
Part: INDICATOR — FAILED (DUAL TACH)
ROTOR NEEDLE HAS NO INDICATION.
1995
Part: FRAME — CRACKED (TAILBOOM)
PART IS CRACKED. (FRAME CRACKED AT BOTH UPPER CASTING AREAS) REPLACED WITH SERVICEABLE FRAME ASSEMBLY.
Part: CHANNEL — CRACKED (FUSELAGE)
PART IS CRACKED. (CRACKED IN FITTING AREA STARTING AT RIVET HOLES) REPLACED CHANNEL WITH NEW CHANNEL.