- Registered owner
- Helio Alaska Inc
- Location
- Chugiak, AK
- Owner type
- Corporation
- Serial number
- 1443
- Year built
- 1972
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 4, 2002
- Certificate issued
- November 10, 2021
- Expires
- November 30, 2028
- Mode S code
- A814AD
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming GO-480 model are included below.
On this page
Airworthiness directives that may apply · 20
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1962 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1977 | 1 |
| 1979 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2012 | 1 |
| 2022 | 2 |
| 2023 | 1 |
See all 21 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N62JAMatched 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 Helio H-295 aircraft
FAA incident reports
No FAA accident or incident reports matched to N62JAMatched 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 Helio H-295 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVGR20181119001Flap Track · brokenTHE LEFT INBOARD FLAP TRACK WAS FOUND TO BE CRACKED (BROKEN) AT THE AFT END DURING THE POST FLIGHT INSPECTION. THIS WAS THE FIRST FLIGHT AFTER A 50 HOUR INSPECTION AND ROUTINE SERVICING. THE CRACK WAS NOT EVIDENT DURING THE PREFLIGHT INSPECTION. THE PILOTS (SDR EVGR201701170001Torque Tube · brokenACFT HAS A HISTORY OF TAIL WHEEL SHIMMY. TROUBLESHOOTING INSPECTION FOUNR THE PILOT'S PEDALS WERE STAGGERED AND THE PILOT’S LT PEDAL HAD SLIGHT FORE AND AFT MOVEMENT WITH THE RT PEDAL HELD STATIONARY. THE TWO BOLTS THAT CONNECT THE PILOT’S RUDDER TORQUE TUBE TSDR 20050415Frame · crackedCARRY-THRU CRACKS, REWORKED TO B-401-5 TO MEET REQUIREMENTS OF AD 82-16-08. TOTAL TIME ON THE CARRY THRU IS UNKNOWN. WHILE PERFORMING A 100HR INSPECTION, CRACKS WERE FOUND RADIATING FROM CUT-OUT FOR UPPER WING ATTACH BOLTS ON BOTH SIDES OF CARRY-THRU. 2 LOSDR 040505Rocker Cover · wornROCKER BOX, PN 68795 WAS WORN BY THE VALVE ROCKER SHAFT UNTIL THE SHAFT CUT THROUGH THE SHAFT RETAINER WHICH IS SPOT WELDED TO THE VALVE COVER. THREE OF SIX COVERS WERE SEVERELY WORN. A FOURTH COVER'S BRACKET WAS WORN THROUGH AND THE RESULTING SLUG OF METAL
STCs that may be installed · 212
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-295
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
Earlier aircraft with this N-number · 1
This aircraft carried N62JA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.