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N239AE

Open the Markdown

1980 Bell Helicopter Textron 206L-1 · Rolls-Royce 250-C30P

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Registered owner
Air Evac Ems Inc
Location
O Fallon, MO
Owner type
Corporation
Serial number
45367
Year built
1980
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
June 29, 2007
Certificate issued
April 20, 2006
Expires
January 31, 2030
Mode S code
A229F4
Bell Helicopter Textron 206L-1Airframe model · 7 seats · 1 engine · 149 registeredTCDS H2SWAirframe · Bell Helicopter Textron 206L-1TCDS E1GLEngine · Rolls-Royce 250-C30P

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 79

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1980In forceSuperseded2026
See all 89 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 1
SAIB SW-10-42Emergency Float KitsIssued Aug 5, 2010

NTSB investigations

No NTSB investigations matched to N239AEMatched 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 Bell Helicopter Textron 206L-1 aircraft

FAA incident reports

No FAA accident or incident reports matched to N239AEMatched 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 Bell Helicopter Textron 206L-1 aircraft

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR EVCA20220825001Unknown · odorFUEL SMELL IN HOVER AND WHEN BANKING RIGHT. PILOT COULD NOT SMELL FUEL. ONE CREW CAN SMELL FUEL IN AFT CABIN. NO FUEL LEAKS PRESENT. CANNOT SEAL HOSE ON END TO LEAK CHECKAug 24, 2022 · N239AE · Bell 206L1 · Air Distribution SystemSDR EVCA20210623002Support Fitting · seizedON THE P/N 206-033-426-001 SUPPORT FITTING ASSY., THE MOUNTING EARS WHICH PROVIDES THE PIVOT POINT FOR T/R CONTROL BELLCRANK P/N 206-001-763-001, WE DISCOVERED THAT THE PIVOT BOLT WAS SEIZED INSIDE THE MOUNT BUSHINGS AND ITS BUSHINGS MOVING WITHIN THE MOUNTINJun 21, 2021 · N239AE · Bell 206L1 · Tail Rotor HeadSDR EVCA03232021Tub Assy · corrodedFORWARD TUB ASSEMBLY CORRODED.Mar 23, 2021 · N239AE · Bell 206L1 · Standard Practices/StructuresSDR EVCA20191229002Blade · corrodedRED M/R BLADE S/N: BH468848 HAS ONE SPOT OF CORROSION ON BOTTOM SIDE TRAILING EDGE NEAR OUTBOARD TRIM TAB. REMOVED AND REPLACED MAIN ROTOR BLADE WITH SERVICEABLE.Dec 29, 2019 · N239AE · Bell 206L1 · Main Rotor BladesSDR EVCA20191229001Blade · corrodedWHITE M/R BLADE S/N: BH468847 HAS MULTIPLE SPOTS OF CORROSION ON TRAILING EDGE. REMOVED AND REPLACED MAIN ROTOR BLADE WITH SERVICEABLE.Dec 29, 2019 · N239AE · Bell 206L1 · Main Rotor BladesSDR EVCA2013050900043Drive Shaft · shearedDURING A ROUTINE TAILROTOR GEARBOX CHANGE, WHILE COMPLETING THE TAILROTOR BALANCING PROCEDURES. AFTER MX OBTAINED THE VIBRATION READING AT 100 PERCENT, THE PILOT DECELERATED THE ACFT TO FLIGHT IDLE AND APPROX 10 SECONDS INTO THE COOL DOWN PROCEDURES (AT FLIGHMay 7, 2013 · N239AE · Bell 206L1 · Tail Rotor Drive ShaftSDR EVCA00021Frame · corrodedFOUND PITTING AND CORROSION, SOME THAT GOES THROUGH OUTER LAYER OF HONEY COMB TUB, IN THE AREA JUST BELOW AND AFT OF THE LEFT HAND REAR DOOR JAM AT THE BOTTOM AFT CORNER.May 10, 2011 · N239AE · Bell 206L1 · Fuselage Main, Frame

STCs that may be installed · 464

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 464 STCs