- Registered owner
- Rempe Richard Henry
- Location
- Bumpass, VA
- Owner type
- Individual
- Serial number
- 18258844
- Year built
- 1968
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 20, 1968
- Certificate issued
- July 22, 1994
- Expires
- October 31, 2027
- Mode S code
- A4FF07
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental O-470 model are included below.
On this page
Airworthiness directives that may apply · 68
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1967 | 1 |
| 1969 | 2 |
| 1971 | 1 |
| 1973 | 3 |
| 1974 | 1 |
| 1975 | 2 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 3 |
| 1980 | 1 |
| 1981 | 3 |
| 1983 | 2 |
| 1984 | 1 |
| 1985 | 1 |
| 1987 | 2 |
| 1988 | 3 |
| 1989 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 2 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 3 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 5 |
| 2024 | 1 |
See all 78 ADs
Information bulletins that may apply · 17
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N42072Matched 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 182L 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HK0Y2025071600503Blade · damagedESN42072 FAN BLADES (P/N: FW23741, SN: RGF22695) WAS REJECTED IN THE WATER COUPLED PHASED ARRAY INSPECTION IN-SERVICE. RR ENGINEERING ASSESSMENT HAS CONCLUDED THAT THE REPORTED DEVIATION IS EXTENSIVE AND CANNOT BE ACCEPTED OR REPAIRED. HENCE, THE PARTS ARE REJSDR 95ZZZX4473Reinforcement · corrodedANNUAL INSPECTION FOUND SEVERE CORROSION AT STA 65.33 BELOW FLOORBOARDS. STEEL REINFORCEMENT HAD CORRODED BADLY. SURROUNDING STRUCTURE STARTED TO CORRODE. REINFORCEMENT IS MAJOR STRUCTURE FOR LANDING GEAR BULKHEAD, PN 0710600, AND IS FASTENED WITH HI-SHEAR SDR 95ZZZX4431Cylinder · crackedCYLINDER SHOWED LOW COMPRESSION. DETAILED INSPECTION REVEALED CRACK IN EXHAUST VALVE AREA ON HEAD NEAR VALVE EXHAUST PORT. CYLINDER WAS PREVIOUSLY WELDED IN THIS AREA. CYLINDER SCRAPPED. EXCHANGE UNIT INSTALLED. NO WAY OF KNOWING TIME SINCE NEW ON THIS CYSDR 95ZZZX4429Bulkhead · crackedDURING ANNUAL INSPECTION OF AIRCRAFT, NOTED WHAT APPEARED TO BE VERY SMALL CRACKS RADIATING FROM PROP SPINNER BULKHEAD FASTENER HOLES. CRACKS VERY SMALL. CONFIRMED USING EDDY CURRENT INSPECTION AND ZYGLO. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA. N
STCs that may be installed · 631
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 182L
STC 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).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.