- Registered owner
- Sherman Aviation LLC
- Location
- Fairfield, NJ
- Owner type
- LLC
- Serial number
- 17275991
- Year built
- 1983
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- May 18, 1983
- Certificate issued
- October 22, 2024
- Expires
- October 31, 2031
- Mode S code
- A8D0D5
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 CHI91LA139Accident · No injuriesLimited investigationFinal reportDetroit, MIThe proper touchdown point was not attained and the pilot failed to perform a go around. A factor related to the accident was the tailwind condition in which the pilot was attempting to land.NTSB CHI88LA078Accident · No injuriesLimited investigationFinal reportSebewaing, MIThe plt rprtd that when he landed, the acft bounced twice & went straight forward for about 200 ft. when he applied brakes, the acft veered to the left. Subsequently, the acft went off the runway & into a ditch where the nose gear collapsed. The plt believed…
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20070911829869ALow Level Operations · Culpeper, VA(-23) At night during landing the instructor noted there was a herd of deer on the runway at Culpeper Regional Airport. Instructor informed student to do a balk landing. During this procedure the aircraft was just above the runway, and a deer jumped up and…Accident 19910425012529ARoll-Out (Fixed Wing) · Detroit-Grosse, MILanded long and fast. Overran runway and nosed over. Had quartering tail wind on landing.Accident 19880320005999ARoll-Out (Fixed Wing) · Sebewaing, MILost directional control on landing. Went off the runway into a ditch.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 99ZZZX1946Line · misinstalledTHE MAIN FUEL SUPPLY LINE WAS IMPROPERLY INSTALLED. THE RUDDER CONTROL CABLE WAS ROUTED BENEATH THE FUEL LINE IN SUCH A WAY TO BE RUBBING DIRECTLY ON THE LINE. WHEN DISCOVERED, THE LINE WAS CUT MORE THAN HALFWAY THROUGH, BUT ONLY SLIGHTLY LEAKING.SDR 98ZZZX1284Fuel Line · cutIMPROPERLY INSTALLED FUEL LINE RUBBING ON RUDDER CABLE CAUSING MAIN FUEL SUPPLY TO BE CUT COMPLETELY OFF. SUBMITTER STATED INSTALLATION APPEARS TO BE FACTORY.
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).