- Registered owner
- Flight School Of Gwinnett Inc
- Location
- Lawrenceville, GA
- Owner type
- Corporation
- Serial number
- 17275244
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- August 19, 1981
- Certificate issued
- October 15, 2020
- Expires
- October 31, 2027
- Mode S code
- A82137
From the FAA registry file of October 24, 2026.
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.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1971 | 2 |
| 1973 | 2 |
| 1974 | 2 |
| 1977 | 1 |
| 1979 | 1 |
| 1981 | 3 |
| 1982 | 1 |
| 1983 | 3 |
| 1986 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 2 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 38 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Cessna 172P
SAIB AIR-21-16FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt InspectionSAIB 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ERA22LA167Accident · Serious injuriesClass 3 · LimitedFinal reportWinder, GAMaintenance personnel’s failure to detect the damaged aileron cable during the most recent inspections, which resulted in the separation of the aileron control cable and subsequent loss of airplane control.NTSB NYC08CA103Accident · No injuriesData collectionFinal reportGainesville, FLThe pilot's improper flare.
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 20220325004359ALanding: Approach · Winder, GADuring the post-crash aircraft wreckage inspection, LH control yoke direct cable to the right aileron was found separated 18 inches from the turnbuckle. The break occurred near the pulley at the bottom of the control column. This separation of the cable…Accident 20080214011089ALevel Off Touchdown · Gainesville, FL(-23) On February 14, 2008, the pilot [privacy data omitted] was administering his first solo cross country flight on a Cessna 172 N62283. His flight originated from sanford airport, FL (ksfb) to Gainesville airport, FL (kgnv) where the pilot [privacy data…
Service difficulty reports
No reports matched to N62283General 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 172P aircraft
STCs that may be installed · 460
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 172P
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).