- Registered owner
- Lr Properties LLC
- Location
- Goodyear, AZ
- Owner type
- LLC
- Serial number
- 17273317
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- September 29, 1979
- Certificate issued
- July 29, 2025
- Expires
- July 31, 2032
- Mode S code
- A5BD8C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 41
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 |
| 1976 | 1 |
| 1977 | 2 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 3 |
| 1982 | 1 |
| 1983 | 3 |
| 1987 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 2 |
| 2001 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 2 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 43 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Cessna 172N
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 CHI87LA143Accident · No injuriesLimited investigationFinal reportPrairie Duchien, WIWhile in cruise flight, tape which was holding a piece of plexiglass over the cracked windshield came loose. The windshield lifted up and the pilot was not able to maintain altitude. During the forced landing in a soft field. The nose gear sheared off.NTSB BFO86LA001Accident · No injuriesLimited investigationFinal reportAnnapolis, MDThe plt crossed mid-field, and entered a left down wind for rwy 30. He then checked wind direction, completed a base leg, and entered final apch. After reducing his airspeed, the acft 'floated' prior to touching down aprx 600 ft short of mid-fld. The plt…
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.
Incident 19950619022979ITo Aborted (Fixed Wing) · Maple Lake, MNCheckout in type and crosswind demo. Began go around full flaps. CFI dumped flaps. Unable climb. Aborted,overshot.Accident 19870612020229AFcd/Prec Ldg From Cruise · Prairie Du Chie, WIA plexiglass patch on a cracked windshield came loose. The aircraft was unable to remain airborne.
Service difficulty reports
No reports matched to N4691GGeneral 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 172N aircraft
STCs that may be installed · 516
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 172N
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).