- Registered owner
- Helicopter Express LLC
- Location
- Chamlee, GA
- Owner type
- LLC
- Serial number
- 64064
- Year built
- 1968
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- March 27, 2026
- Certificate issued
- December 6, 2023
- Expires
- December 31, 2030
- Mode S code
- A1D386
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 9
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 2 |
|---|---|
| 1975 | 1 |
| 1976 | 1 |
| 1985 | 2 |
| 1991 | 1 |
| 1997 | 2 |
| 2013 | 1 |
| 2021 | 1 |
| 2023 | 1 |
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Erickson S64E
SAIB SW-07-21Tail Rotor Head AssemblyNTSB investigations
No NTSB investigations matched to N217ACMatched 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 Erickson S64E aircraft
FAA incident reports
No FAA accident or incident reports matched to N217ACMatched 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 Erickson S64E aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JYDR20210715184Engine · overtempSHORT FINAL FOR WATER DROP. PILOT RECEIVED 65% CHIME THEN 60% WARNING. ENGINE SECURED AND AIRCRAFT RETURNED TO BASE SINGLE ENGINE. THIS IS A PRELIMINARY REPORT TO MEET REPORTING TIME LIMITS.SDR JYDR20170321001Gearbox · failedDURING A NORMAL START PROCEDURE, WITH THE NR 1 ENGINE AT GROUND IDLE AND JUST PRIOR TO THE ROTOR BRAKE BEING RELEASED, A FAILURE OCCURRED IN THE MAIN GEARBOX THAT ALLOWED MOMENTARY ROTATION AND SUBSEQUENT LOCKING OF THE MGB. THE ROTOR SYSTEM BARELY MOVED BEFORSDR 20010613CW017Blade · crackedBLADE REMOVED FOR BIM INDICATION. THE SPAR IS CRACKED ON BOTTOM SIDE UNDER NR 9 POCKET, APPROXIMATELY 1 INCH STARTING AT BACK WALL RADIUS, RUNNING CHORDWISE TOWARDS LEADING EDGE. PROBABLE CAUSE: CORROSION.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.