- Registered owner
- Moore Joshua M
- Location
- North Pole, AK
- Owner type
- Individual
- Serial number
- 18503173
- Year built
- 1977
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Multiple
- Airworthiness date
- April 9, 1999
- Certificate issued
- November 5, 2022
- Expires
- November 30, 2029
- Mode S code
- ACE8CE
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 61
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1977 | 2 |
| 1979 | 2 |
| 1980 | 3 |
| 1981 | 3 |
| 1983 | 2 |
| 1986 | 1 |
| 1987 | 4 |
| 1988 | 4 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 3 |
| 2004 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 6 |
See all 73 ADs
Information bulletins that may apply · 18
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N93055Matched 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 A185F aircraft
FAA incident reports
No FAA accident or incident reports matched to N93055Matched 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 A185F aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0000520Starter · brokenSTARTER HAS A PARTIAL SEPARATION BETWEEN THE HOUSING THAT ATTACHES TO THE STARTER ADAPTER AND THE MAIN STARTER HSG. EXTERIOR BOLTS THAT SECURE THE HSGS TOGETHER ARE INTACT AND TIGHT. PILOT REPORTED STARTING DIFFICULTY. PROBLEM WAS VISIBLY OBVIOUS. STARTER WASSDR 20001218SH036Bushing · crackedON INSPECTION OF TAILWHEEL SUPPORT BUSHINGS, FOUND NEWLY INSTALLED BUSHINGS SEVERELY WORN, EXTRUDED AND CRACKED. THESE BUSHINGS, OBTAINED FROM CESSNA, ARE MADE OF INFERIOR MATERIALS. (X)SDR 20001218SH035Bushing · wornTAILWHEEL TO AFT BULKHEAD SUPPORT BUSHINGS FOUND SEVERELY WORN. SUBMITTER STATED NEW PARTS OBTAINED FROM CESSNA APPEAR TO BE MADE FROM INFERIOR MATERIALS. (X)SDR 98ZZZX3076Regulator · failedOVERVOLTAGE LIGHT CAME ON IN-FLIGHT. REPLACED VOLTAGE REGULATOR.SDR 96ZZZX4793Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4792Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4791Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4790Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS AIRCRAFT IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.SDR 96ZZZX4789Rib · crackedWHILE DOING THE CESSNA CONTINUAL AIRWORTHINESS PROGRAM, FOUND LEADING EDGE RIB BROKEN. THIS IS A PUBLIC AIRCRAFT AND IS SUBJECTED TO MANY HOURS OF LOW LEVEL FLYING.
STCs that may be installed · 575
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna A185F
STC 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.STC SA01861SEFabrication and installation of Landing Light Controller