- Registered owners
- Borreson AnthonyBorreson Michele R
- Location
- Reno, NV
- Owner type
- Co-owned
- Serial number
- 385
- Year built
- 1977
- Type
- Rotorcraft
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 31, 2001
- Certificate issued
- March 17, 2021
- Expires
- March 31, 2028
- Mode S code
- A6AFA5
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming HIO-360 model are included below.
On this page
Airworthiness directives that may apply · 63
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 |
|---|---|
| 1967 | 1 |
| 1969 | 1 |
| 1972 | 1 |
| 1973 | 2 |
| 1975 | 1 |
| 1977 | 6 |
| 1978 | 1 |
| 1979 | 3 |
| 1981 | 1 |
| 1982 | 4 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 4 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 2 |
| 1998 | 2 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 1 |
| 2006 | 3 |
| 2007 | 3 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 4 |
| 2015 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 2 |
| 2024 | 1 |
| 2026 | 1 |
See all 79 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Enstrom F-28C
SAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-12-10R1Fuel Level IndicationEngine · Lycoming HIO-360 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-08-26R3Magneto/DistributorSAIB NE-09-04Fuel Control/Reciprocating EnginesSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-05-40SAIB NE-01-22Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N53SAMatched 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 Enstrom F-28C aircraft
Investigations on N53SA not matched to an aircraft · 2
They name N53SA, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
NTSB LAX86LA090Accident · No injuriesLimited investigationFinal reportCessna 402B · Kalaupapa, HIThe plt said that when he departed rwy 5, the acft 'became airborne prematurely due to a hump and rough nature of the runway.' He further said that 'after wallowing monentarily behind the power curve,' the acft began a normal climb and acceleration profile.…NTSB OAK79FA035Accident · Serious injuriesClosedCessna 402B · Las Vegas, NV
FAA incident reports
No FAA accident or incident reports matched to N53SAMatched 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 Enstrom F-28C aircraft
Reports on N53SA not matched to an aircraft · 2
They name N53SA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Accident 19860113076839ACessna 402B · Kalaupapa, HIAfter an early liftoff and slow climb, the pilot reported the aircraft was struck by a 70 foot wave on departure.Accident 19790720029539ACessna 402B · Las Vegas, NVEngine failed. Pilot made emergency lndg. Performance charts show acft capable of single engine flight.
Service difficulty reports
No reports matched to N53SAGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Enstrom F-28C aircraft
Reports on N53SA not matched to an aircraft · 3
They name N53SA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 96ZZZX490Torque Tube · crackedDURING A PRE-FLIGHT INSPECTION, THE PILOT NOTED WHEN THE LT RUDDER PEDAL WAS PUSHED, NO CONTROL SURFACE MOVEMENT WAS NOTED. INVESTIGATION REVEALED CONTROL CABLE HAD PULLED ITS ATTACH EAR OFF OF THE TORQUE TUBE. THE INTERIOR GUST LOCK WAS INSTALLED FREEZING TSDR 95ZZZX4392Crankcase · crackedDURING A ROUTINE INSPECTION, THE LEFT ENGINE CRANKCASE WAS FOUND CRACKED AT THE NR 4 CYLINDER MOUNTING PAD. AD 77-13-22 DOES NOT APPLY TO THIS CRANKCASE DUE TO MARKINGS. SUSPECT FATIGUE, WEAK DESIGN. SUBMITTER SUGGESTS INSPECTING AREA CLOSELY AT 100-HOUR INSDR 95ZZZX2884Bearing · failedCREW SQUAWKED, 'RIGHT BRAKE DRAGS AND NOISY'. FOUND INBOARD WHEEL BEARING DISINTEGRATED, NOTHING REMAINING EXCEPT INNER RACE OUTBOARD BEARING FAILED, ALL ROLLERS GONE. BOTH WHEEL HALVES 'WALLOWED OUT'. ONLY THING HOLDING WHEEL TO AXLE WAS CLEVELAND BRAKE CA
STCs that may be installed · 76
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 76 STCs