- Registered owner
- Hoppe Gregory M
- Location
- Big Lake, AK
- Owner type
- Individual
- Serial number
- 165
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 4, 1992
- Certificate issued
- January 24, 2018
- Expires
- January 31, 2028
- Mode S code
- AC9E59
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 12
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1967 | 1 |
| 1977 | 1 |
| 1979 | 1 |
| 1980 | 1 |
| 2001 | 1 |
| 2006 | 3 |
| 2022 | 1 |
Airframe · Champion 7GCB
AD 2022-03-15Fuel Quantity IndicatorAD 2006-12-07ECi cylinder assembliesAD 2006-03-08Vacuum pumpsAD 2005-24-10Pilot's Operating Handbook (POH) limitationAD 2000-25-02 R1Wood SparsAD 80-21-06Muffler Core and Body AssemblyAD 79-07-02BatteriesAD 77-22-05Operating LimitationsAD 67-03-02Fuel Shutoff Valve BracketAD 64-04-03Air Door HingeAD 48-39-01Control Stick ReworkAD 48-08-02Cleveland WheelsInformation bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX3236Control Rod · brokenTHE AIRCRAFT WAS BEING OPERATED FROM THE FRONT SEAT WITH 2 PEOPLE ON BOARD WHEN THE AIRCRAFT VEERED TO THE LEFT DURING LANDING ROLL OUT AND GROUND LOOPED. POST-ACCIDENT INVESTIGATION REVEALED THE RT FORWARD BRAKE SYSTEM HAD FAILED. THIS OCCURRED WHEN THE CONSDR 98ZZZX3080Locknut · failedTHE PILOT REPORTED HE FELT THE AIRCRAFT SHUDDER DURING LANDING. POST-ACCIDENT INVESTIGATION REVEALED: THE NUT SECURING THE TAIL WHEEL STEERING ASSY TOGETHER LOST ITS TORQUE. THIS ALLOWED PARTS TO SHIFT AND AN INTERNAL LOCK RING TO BE SHEARED OFF. THE TAIL
STCs that may be installed · 148
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Champion 7GCB
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.