- Registered owner
- Edb Air Inc
- Location
- Wilsonville, OR
- Owner type
- Corporation
- Serial number
- 17280010
- Year built
- 1997
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 18, 1997
- Certificate issued
- April 13, 2001
- Expires
- January 31, 2030
- Mode S code
- A40CC1
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.
On this page
Airworthiness directives that may apply · 85
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 2 |
| 1968 | 1 |
| 1969 | 2 |
| 1971 | 2 |
| 1972 | 1 |
| 1973 | 4 |
| 1974 | 2 |
| 1975 | 1 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 2 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 2 |
| 1992 | 1 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 2 |
| 1998 | 10 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 4 |
| 2006 | 6 |
| 2007 | 3 |
| 2008 | 7 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 5 |
| 2013 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 1 |
See all 102 ADs
Information bulletins that may apply · 27
Advisory, not mandatory.
See all 34 bulletins
NTSB investigations
No NTSB investigations matched to N360ESMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX3202Fuel Servo · malfunctionedPILOT REPORTED ENGINE QUIT IN-FLIGHT AND REQUIRED A DEAD STICK LANDING. ENGINE RESTARTED ON THE GROUND AFTER A SAFE LANDING. MAINTENANCE MADE ADJUSTMENTS TO FUEL SERVO AFTER NOTICING HIGHLY ERRATIC FUEL FLOW INDICATIONS. ALL GROUND CHECKS WERE NORMAL. ACFTSDR 98ZZZX3201Fuel Servo · malfunctionedPILOT REPORTED LOSS OF ENGINE POWER AT 500 FEET AGL ON TAKEOFF AND AGAIN ON FINAL. PILOT MADE A SAFE LANDING. DURING TAXI BACK, MAINTENANCE PERSONNEL NOTICED ENGINE RUNNING EXTREMELY ROUGH. DURING TROUBLESHOOTING ON SUBSEQUENT MAINT RUNS, THE FUEL FLOW GAUGSDR 98ZZZX3200Fuel Servo · malfunctionedPILOT REPORTS ERRATIC ENGINE OPERATION AT LOW POWER SETTINGS AND APPEARED TO BE 'MISFIRING' ON FINAL. MAINTENANCE PERSONNEL RAN ENGINE AND NOTICED AT ANY RPM BELOW 1,500, ENGINE WOULD 'LOPE' AND WAS ACCOMPANIED BY ERRATIC FUEL FLOW INDICATIONS. FUEL SERVO WASDR 98ZZZX3199Fuel Servo · scoredDURING MAINTENANCE FLIGHT WHILE CHECKING THE OPERATION OF THIS FUEL SERVO, ON THE THIRD APPROACH, ENGINE STARTED TO MISS AT REDUCED POWER SETTINGS. GO-AROUND, WHEN ACFT TURNED FINAL AND UPON POWER REDUCTION, THE ENGINE LOST POWER AND UPON ADVANCEMENT OF THE TSDR 97ZZZX4043Stabilizer · rivets looseDURING INSPECTION, FOUND WORKING RIVETS ON TOP OF STABILIZER SKIN JUST UNDERNEATH FAIRING FOR HORIZONTAL STABILIZER TO FUSELAGE.SDR 97ZZZX4252J Box · failedIN-FLIGHT ELECTRIAL FAILURE OF ALL ELECTRICAL EQUIPMENT BEING SERVICED BY BUS NR 1. PILOT COMMENTED SPARKS COMING FROM UNDERNEATH INSTRUMENT PANEL. NO BREAKERS TRIPPED. FOUND WIRE BUNDLE RESTING ON CIRCUIT BREAKER. WIRE BURNED OUT LAYING ACROSS WARNING BRE
STCs that may be installed · 391
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.