Registered owner
Air Evac Ems Inc
Location
O Fallon, MO
Owner type
Corporation
Serial number
53328
Year built
1999
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
January 6, 1999
Certificate issued
January 28, 2008
Expires
April 30, 2029
Mode S code
A62667

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 250-C47 model are included below.

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Airworthiness directives that may apply · 49

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

1982In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19821
19961
19971
19984
19994
20006
20014
20025
20034
20041
20053
20062
20071
20081
20094
20112
20123
20135
20141
20152
20181
20192
20212
20234
20242
20251
20262
See all 72 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations · 1

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

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 8

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

SDR EVCA2020093001Skin · crackedDURING ROUTINE MAINTENANCE, THE LOWER SKIN OF THE FUSELAGE NEAR TAILBOOM ATTACHMENT WAS FOUND CRACKED APPROXIMATELY FOUR INCHES LONG FORWARD AND AFT AND AN INCH-AND-HALF RUNNING OUTBOARD. FS 75, WL 61.77, RBL 2.0.Sep 24, 2020 · N496AE · Bell 407 · Fuselage Main, Plate/SkinSDR EVCA20190430003Floor Skin · debondedDURING INSPECTION AT OUR SWRMO. CORROSION METAL DEBONDING FOUND ON CO-PILOT FLOOR, UNDER INVERTOR.Apr 30, 2019 · N496AE · Bell 407 · Fuselage Floor PanelSDR EVCA20190430002Skin · crackedSKIN CRACKED LH AIRFRAME JUST BELOW BAGGAGE DOOR. REPAIRED DAMAGE USING SPECIFICATIONS AS OUTLINED IN BHT ALL SRM CH 4 PARA 4-4-9 APPLICATION B.Apr 30, 2019 · N496AE · Bell 407 · Fuselage Main, Plate/SkinSDR EVCA201904300001Stiffener · crackedDURING INSPECTION AT OUR SWRMO, FOUND BAGGAGE COMPARTMENT OVERHEAD STIFFENER CRACKED/MISSING NUT PLATES. REMOVED DAMAGED STIFFENER AND REPLACED WITH NEW STIFFENER PN 206-032-309-095 AND DAMAGED SUPPORT WITH NEW SUPPORT PN 206-032-309-113 . ALL MAINTENANCE ACApr 30, 2019 · N496AE · Bell 407 · Fuselage Miscellaneous StructureSDR EVCA20170405Bulkhead · corrodedSEVERE CORROSION WAS FOUND IN SHELF LOCATED INTERNALLY TO THE 145-155 ROLLOVER BULKHEAD ON THE LT SIDE OF THE AIRCRAFT. THE SHEETMETAL SHELF THAT SITS INSIDE OF THE ACCESS PANEL AND ACTS AS THE BOTTOM OF THE CAVITY WAS FOUND TO BE SEVERELY CORRODED. THIS AREA Apr 5, 2017 · N496AE · Bell 407 · Fuselage Main, BulkheadSDR EVCA20151109001Drive Shaft · shearedUPON TAKING OFF THE ACFT EXPERIENCED AN UNCOMMANDED YAW. THE PILOT IMMEDIATELY LANDED & SHUTDOWN THE ACFT. UPON MX INSPECTION IT WAS FOUND THAT THE TAIL ROTOR SEGMENTED DRIVESHAFT LOCATED ABOVE THE HORIZONTAL STABILIZER ON THE TAIL BOOM HAD SHEARED CAUSING ANov 2, 2015 · N496AE · Bell 407 · Tail Rotor Drive ShaftSDR EVCA2014082500068Blower · inoperativeAFT AIR CONDITIONER BLOWER INOPERATIVE.Aug 24, 2014 · N496AE · Bell 407 · Cabin Cooling SystemSDR EVCA2012071600032Blade · damagedON DAILY INSPECTION, MECHANIC FOUND RIVET MISSING FROM THE TAIL ROTOR BLADE TIP.Jul 16, 2012 · N496AE · Bell 206L4 · Tail Rotor Blades

STCs that may be installed · 327

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

See all 327 STCs