- Registered owner
- Run For The Hills LLC
- Location
- Kalispell, MT
- Owner type
- LLC
- Serial number
- P3370217
- Year built
- 1975
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 2, 1975
- Certificate issued
- November 12, 2024
- Expires
- November 30, 2031
- Mode S code
- A2866A
From the FAA registry file of October 21, 2026. The registry lists only the engine series, so ADs for every Continental IO-360 model are included below.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 3 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 2 |
| 1980 | 1 |
| 1981 | 2 |
| 1988 | 2 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1997 | 1 |
| 1998 | 3 |
| 2000 | 2 |
| 2002 | 1 |
| 2005 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2022 | 2 |
| 2023 | 5 |
See all 48 ADs
Information bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Cessna T337G
SAIB AIR-21-16FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt InspectionSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsEngine · Continental IO-360 series
SAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-04Fuel Control/Reciprocating EnginesSAIB CE-02-09NTSB investigations
No NTSB investigations matched to N262Matched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna T337G aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date.
Service difficulty reports · 11
Reports filed since June 23, 1948, when this mark’s previous registration was cancelled.
SDR CHQA000457Wire · exposedPROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4.SDR CHQA000460Wire · exposedPROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4.SDR CHQA000424Engine · malfunctionedDURING CLIMB OUT OF LGA HIGH ITT WAS NOTED ON NR 2 ENGINE. AT MAX CLIMB THRUST ITT WAS AMBER AND RISING ABOVE 290. WE PULLED POWER BACK 7 PERCENT N1 LOWER THAN NR 1 ENGIN FOR REST OF FLIGHT ITT ON NR 2 ENGINE RAN AT 880-890 DEGREES WHEN N1 WAS PULLED BACK 7 SDR CHQA000423Heater · smokeODOR NOTED IN COCKPIT FOLLOWED BY VISIBLE TRAIL OF WHITE SMOKE EMANATING FROM JUNCTION OF F/O WINDSHIELD AND GLARESHIELD. EMERGENCY DECLARED, QRH MEMORY ITEMS ACCOMPLISHED FOR SMOKE/FUMES AND IMMEDIATE DIVERSION TO NEAREST AIRPORT(CLE). SMOKE DISSIPATED AFTESDR 000246Shutoff Valve · failedBRAKE OUTBOARD INOPERATIVE MSG ON APP. FOLLOWED POH. NO FIX. DECLARED EMERGENCY FOR LANDING. TRIED BRAKES THEY SEEMED OK. A/C TAXIED TO TERMINAL WITH NO PROBLEMS. RR'D BRAKE CONTROL SHUTOFF VALVESDR 000166Warning System · activatedE2 ATTCS NO MARGIN EICAS MESSAGE.SDR CHQ000164Warning System · activatedENG 2 ATTCS NO MARGIN ON EICAS. FERRY A/C TO IND.SDR 000162A/C Pack · malfunctionedNR 2 PACK OVERLOAD ON EICAS FOLLOWED BY SMOKE IN CABIN. DEFERRED NR 2 PACK.SDR CHQ000133Flap · malfunctionedAFTER TAKEOFF WHEN FLAPS SELECTED UP EICAS FLAP FAIL MESSAGE APPEARED UNABLE TO RAISE LOWER FLAPS. FLAPS REMAINED AT 0 DEGREES.SDR CHQ000128Anti-Ice System · malfunctionedICE CONDITION A/I INOP, W/A STAB A/I INOP EICAS MESSAGE AFTER T/O. RESET AIRCRAFT POWER, A/I TEST OPS CHECK GOOD.SDR CHQA200262528Warning System · malfunctionedAFTER TAKEOFF- THERE WAS EICAS INDICATION THAT ALL PRESSURIZATION WAS LOST. A/C RETURNED TO FIELD. MAINTENANCE PERFORMED OPERATIONAL CHECK OF PRESSURIZATION CONTROL SYSTEM. RAN GROUND AND TEST FLIGHT, OPS CHECK GOOD.
Earlier aircraft with this N-number · 2
These aircraft carried N262 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.