- Registered owner
- Branham Chris R
- Location
- Anchorage, AK
- Owner type
- Individual
- Serial number
- 2538
- Year built
- 1968
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Certificate issued
- May 13, 2013
- Expires
- May 31, 2029
- Mode S code
- A84822
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-540 model are included below.
On this page
Airworthiness directives that may apply · 44
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 2 |
|---|---|
| 1964 | 1 |
| 1966 | 2 |
| 1969 | 2 |
| 1977 | 2 |
| 1979 | 2 |
| 1982 | 2 |
| 1989 | 2 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2002 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 2 |
| 2017 | 1 |
| 2022 | 2 |
| 2024 | 1 |
| 2026 | 2 |
See all 52 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Helio H-250
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-18-14Main Landing Gear: Improved inspection at Drag Brace LocationSAIB CE-08-47Wings - Attachment FittingsEngine · Lycoming 0-540 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-13-06Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series EnginesSAIB NE-08-26R3Magneto/DistributorSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-05-40SAIB NE-03-18SAIB NE-03-12Historical bulletins · 2
NTSB investigations · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC16LA072Accident · No injuriesLimited investigationFinal reportAnchorage, AKThe fatigue fracture failure of both main landing gear (MLG) legs during the landing roll, which resulted in the collapse and separation of both MLG legs.NTSB ANC06LA072Accident · No injuriesLimited investigationFinal reportAnchorage, AKThe pilot's improper use of the carburetor heat control during takeoff, which resulted in a partial loss of engine power, a hard landing, and an on ground encounter with terrain. A factor contributing to the accident was an inadvertent ground loop.NTSB ANC76AA042Accident · No injuriesClosedTeller, AK
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20160926024819ALanding: Rollout · Anchorage, AKThe PIC landed at the lake hood strip. He stated he made a normal wheel landing, let the tail come down and as soon as the tail wheel touched down it started to shimmy and he applied the brakes normally and both main gear sheared off at the same time and the…Accident 20060519012049ATo Aborted (Fixed Wing) · Anchorage, AK(-23) At approximately 20 ft. altitude, the pilot aborted a takeoff from a 3,000 ft gravel runway because he felt the engine was not developing full power. He stated that after reducing power to abort the takeoff the airplane landed hard and ground looped…Accident 19750928033679ATo Init Climb(1st Pwr Reduct) · Teller, AKAbt 53LBS ovr max gross wt. Short strip with house 100FT frm dep end. Ran into pond.
Service difficulty reports
No reports matched to N6324VGeneral 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 Helio H-250 aircraft
STCs that may be installed · 218
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Helio H-250
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