- Registered owner
- Copper River Airmotive LLC
- Location
- Copper Center, AK
- Owner type
- LLC
- Serial number
- 17255247
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- October 7, 1966
- Certificate issued
- October 24, 2018
- Expires
- October 31, 2028
- Mode S code
- A44902
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental 0-300 model are included below.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1968 | 1 |
| 1969 | 1 |
| 1971 | 2 |
| 1972 | 1 |
| 1973 | 2 |
| 1974 | 2 |
| 1977 | 1 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1987 | 2 |
| 1988 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 4 |
| 2000 | 3 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 1 |
See all 54 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Cessna 172H
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-18-23Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump SeatsSAIB CE-17-25ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubesSAIB 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-09-42Lights - Landing Light, Beacon Light and Taxi Light Switch ApplicationsSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsSAIB CE-09-01Equipment - EmergencySAIB CE-01-41R2Flight ControlsNTSB investigations · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC02LA105Accident · No injuriesLimited investigationFinal reportFairbanks, AKThe pilot's failure to maintain directional control during the takeoff roll, which resulted in the airplane exiting the runway and colliding with objects. Factors contributing to the accident were the rough and uneven runway, and the premature lift-off of the…NTSB ANC89FA028Accident · No injuriesField investigationFinal reportAnchorage, AKThe 103 hour private pilot was in the process of demonstrating his Cessna 172 conventional gear airplane (tail-dragger) to a prospective purchaser, when he lost directional control during landing and nosed-over. The pilot reported that he had just touched…NTSB ANC73DAG10Accident · No injuriesClosedPalmer, AK
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20020827022169AFairbanks, AK(-23) Pilot failed to maintain directional control during takeoff roll. Aircraft exited the left side of the gravel runway, skidding, struck a parked vehicle and continued into trees along the runway.Accident 19881230057109ATouch And Go Landing · Anchorage, AKLost directional control of the tailwheel modified 172. Zigzagged, left the runway, hit a snowbank and nosed over.
Service difficulty reports
No reports matched to N3752FGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Cessna 172H aircraft
STCs that may be installed · 522
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 172H
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC SA00709CHInstallation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).