- Registered owner
- Helicopter Express LLC
- Location
- Chamblee, GA
- Owner type
- LLC
- Serial number
- 64033
- Year built
- 1967
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Multiple
- Airworthiness date
- November 28, 2011
- Certificate issued
- May 2, 2024
- Expires
- May 31, 2031
- Mode S code
- A1D73D
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney JFTD12A model are included below.
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 N218ACMatched 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 N218ACMatched 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
Reports on N218AC not matched to an aircraft · 1
They name N218AC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another 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 2013FA0000416Lock · brokenENGINE REMOVED, DURING DISASSEMBLY MINOR DAMAGE WAS NOTED ON THE BLADES AND VANES AFT IF 5TH STAGE. THE DAMAGE WAS CAUSED BY A 5TH STAGE DISK TAB LOCK THAT HAD BROKEN AND ALLOWED THE BLADE TO MOVE AFT IN THE DISK MAKING CONTACT WITH THE 6TH STAGE STATOR.SDR 20001219SH021Housing · crackedMAIN LANDING GEAR, PN 6425-50100-013, -014, WAS REMOVED FOR OVERHAUL. DURING THE FLUORESCENT MAGNETIC PARTICLE INSPECTION PROCESS, 15 LINEAR INDICATIONS, NOT VISIBLE TO THE NAKED EYE, WERE REVEALED ON THE UPPER COLLAR HOUSING WITH MEASUREMENTS OF .093 INCH TOSDR 20001218SH003Housing · crackedMAIN LANDING GEAR PN 6425-50100-013, -014 WAS REMOVED FOR OVERHAUL. DURING THE FLUORESCENT MAGNETIC PARTICLE INSPECTION PROCESS, 15 LINEAR INDICATIONS, NOT VISIBLE TO THE NAKED EYE, WERE REVEALED ON THE UPPER COLLAR HOUSING WITH MEASUREMENTS OF .093 INCH TO SDR 20001218SH002Housing · crackedMAIN LANDING GEAR PN 6425-50100-013, -014 WAS REMOVED FOR OVERHAUL. DURING THE FLUORESCENT MAGNETIC PARTICLE INSPECTION PROCESS, 15 LINEAR INDICATIONS, NOT VISIBLE TO THE NAKED EYE, WERE REVEALED ON THE UPPER COLLAR HOUSING WITH MEASUREMENTS OF .093 INCH TO
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.