- Registered owner
- Lakewood Investments LLC
- Location
- Victorville, CA
- Owner type
- LLC
- Serial number
- 17280023
- Year built
- 1997
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 2, 1997
- Certificate issued
- January 6, 2023
- Expires
- January 31, 2030
- Mode S code
- A41F54
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 43
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 |
| 1988 | 1 |
| 1991 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 7 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 4 |
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2013 | 2 |
| 2018 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 47 ADs
Information bulletins that may apply · 16
Advisory, not mandatory.
See all 20 bulletins
NTSB investigations
No NTSB investigations matched to N365ESMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 172R aircraft
FAA incident reports
No FAA accident or incident reports matched to N365ESMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 172R aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR T22R R/O9856Crankshaft · brokenCRANKSHAFT BROKE AT THE NR 4 CONNECTING ROD JOURNAL, SEPARATION OCCURRED AT THE NR 5 CHEEK COUNTING FROM THE FRONT OF CRANKSHAFT.SDR 98ZZZX974Rivets · failedDURING 100-HOUR INSPECTION, FOUND 4 OF THE AN426 RIVETS SECURING THE UPPER HORIZONTAL STABILIZER SKIN PULLED COMPLETELY THROUGH ON THE LEFT SIDE. ALL OF THE REMAINING RIVETS BOTH LEFT AND RIGHT SIDE SHOWED SIGNS OF WORKING THESE RIVETS ARE INBOARD UNDER THE SSDR 98ZZZX973Firewall · crackedDURING 100-HOUR INSPECTION, FOUND FIREWALL CRACKED AT THE LOWER LEFT COWL SHOCK MOUNT BELOW THE BATTERY BOX. VISIBLE PORTION OF CRACK WAS APPROXIMATELY .50 INCH LONG. AFTER CLOSER EXAMINATION FROM INSIDE THE CABIN, THE CRACK APPEARED TO BE ABOUT 3 INCHES LONSDR 98ZZZX164Transmitter · failedRIGHT FUEL QUANTITY GAUGE INOPERABLE. TRACED PROBLEM TO TRANSMITTER IN RT WING. PLASTIC FLOAT HAD SEPARATED FROM THE ARM AND WAS ALLOWING THE ARM TO SINK. FLOAT FAILED BECAUSE OF INADEQUATE CRIMP ON ARM WHICH ALLOWED THE RETAINING WASHER AND FLOAT TO COME SDR 98ZZZX165Transmitter · failedPILOT COMPLAINED OF FLUCTUATING FUEL QUANTITY INDICATING GAUGE. TRACED PROBLEM TO BOTH LEFT AND RIGHT QUANTITY TRANSMITTERS GIVING ERRONEOUS OHM READINGS. REPLACED TRANSMITTERS AND SYSTEM OPERATES NORMALLY.SDR 98ZZZX163Control Cable · misroutedDURING ROUTINE INSPECTION, FOUND AUTOPILOT SERVO CONTROL CABLE WRAPPED AROUND RT AILERON CONTROL CABLE. MM DOES NOT SHOW THESE CABLES CROSSED. INSPECTED CABLES FOR DAMAGE AND POSITIONED PROPERLY. AIRCRAFT WAS DELIVERED FROM THE MANUFACTURER WITH THIS CONDIT
STCs that may be installed · 336
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 172R
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.