- Registered owner
- Elias 48 LLC
- Location
- Morristown, AZ
- Owner type
- LLC
- Serial number
- R18201785
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- January 24, 2025
- Expires
- January 31, 2032
- Mode S code
- A3E30A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1983 | 3 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 22 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Cessna R182
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-17-25ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubesSAIB CE-17-16Main Landing Gear Actuator InspectionSAIB CE-13-16Hydraulic Power Pack/Landing Gear SystemSAIB CE-12-41Flight Controls Loose Glide ScrewSAIB 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-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsSAIB CE-08-02Flight ControlsSAIB CE-06-46R1SAIB CE-04-11SAIB CE-02-10NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 20050601009879IGo Round (Aborted VFR) · Prescott, AZ(-23) The crew stated that the aircraft was very stable until short final, about 100 feet above the touchdown zone. The aircraft started sinking rapidly and lost 10 knots of airspeed almost instantly. The crew applied full throttle and initiated a go-around.…Incident 19980629026269IFcd/Prec Ldg From Cruise · Little Rock, ARAfter takeoff from pbf at 11:30AM CDT on an avionics varification flight, a leak occurred at the pressure outlet port tee fitting on the hydraulic/electric power pack. The leak was the result of the failure of a flare on a #4 aluminum hydraulic line leading…
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2004FA0000234Plate · crackedDURING AN INSPECTION, THE BULKHEAD MOUNTING PLATES WERE FOUND CRACKED AND BROKEN AROUND THE HOLES THROUGH WHICH THE PROPELLER MOUNTING STUDS PASS. THIS CONDITION IS FOUND VERY OFTEN AND THE PLATES REALLY NEED TO BE REDESIGNED TO NOT CRACK AS EASILY AS THEY DOSDR 2004FA0000195Plug · looseDURING CLIMB OUT ENGINE RPM WOULD START CLIMBING AND THE PROP CONTROL HAD NO EFFECT ON REDUCING RPM. DURING TROUBLESHOOTING FOUND THE REAR CRANKSHAFT PLUG HAD COME LOOSE IN THE CRANKSHAFT ALLOWING OIL TO BYPASS BACK TO THE ENGINE SUMP. UNABLE TO DETERMINE THSDR 2003FA0001231Fitting · crackedDURING ANNUAL INSPECTION FOUND THE AFT ATTACH FITTING FOR THE NOSE GEAR ACTUATOR CRACKED IN TWO PLACES. THE CRACKS START AT THE ACTUATOR PIN BOSS AND PROGRESS UPWARD THROUGH THE FLANGE AREA TO THE EDGE OF THE FITTING. UNABLE TO DETERMINE CAUSE (AGE, FATIGUE SDR 98ZZZX2621Line · failedA HYDRAULIC INDICATOR WAS INSTALLED IN THE AIRCRAFT UTILIZING AN EXISTING 'TEE' ON THE HYDRAULIC POWER PACK. THE FLARE ON THE LINE GOING TO THE HYDRAULIC PRESSURE GAUGE FAILED CAUSING THE LINE TO BLOW OUT OF ITS 'B' NUT. THE HYDRAULIC FLUID SUPPLY WAS SUBSEQ
STCs that may be installed · 419
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna R182
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.