Registered owner
Air Evac Ems Inc
Location
O Fallon, MO
Owner type
Corporation
Serial number
53428
Year built
2000
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
June 22, 2000
Certificate issued
March 19, 2013
Expires
March 31, 2029
Mode S code
A60656

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

No NTSB investigations matched to N488AEMatched 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 407 aircraft

FAA incident reports

No FAA accident or incident reports matched to N488AEMatched 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 407 aircraft

Service difficulty reports · 6

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

SDR EVCA201901211Frame · crackedDURING INSPECTION AT RMO. STATION 192 FRAME CRACKED ON THE AFT FACE UPPER LEFT SIDE. REPLACED FRAME AT STATION 192 P/N 206-032-305-127. REPAIRS WILL BE DONE IN ACCORDANCE WITH BHT-ALL-SRM.Jan 16, 2019 · N488AE · Bell 407 · Fuselage Main, FrameSDR EVCA201901141Longeron · corrodedDURING INSPECTION, AIRCRAFT WAS FOUND TO HAVE CORROSION, ON AFT FUSELAGE, THAT REQUIRED REPAIR. CONTACTED TO OBTAIN REPAIR DRAWING AND INSTRUCTIONS. SENDING TWO TECHNICIANS TO ASSIST IN REPAIRS. AFT FUSELAGE IS REPAIRED IN ACCORDANCE WITH BHT-ALL-SRM AND BHT-Jan 7, 2019 · N488AE · Bell 407 · Fuselage Main, Longeron/StringerSDR 2019FA0000007Longeron · corrodedDURING INSPECTION, AIRCRAFT WAS FOUND TO HAVE CORROSION, ON AFT FUSELAGE THAT REQUIRED REPAIR. MANUFACTURER WAS CONTACTED TO OBTAIN REPAIR DRAWING AND INSTRUCTIONS. TWO TECHNICIANS WERE SENT TO ASSIST IN REPAIRS. AFT FUSELAGE IS REPAIRED IN ACCORDANCE WITH SRMJan 7, 2019 · N488AE · Bell 407 · Fuselage Main, Longeron/StringerSDR EVCA20160921161Pump · failedDURING CRUISE FLIGHT THE PASSENGERS IN THE AFT CABIN REPORTED TO THE PILOT SMELLING SOMETHING BURNING AND THEN REPORTED SMOKE IN THE AFT CABIN AREA. PILOT PERFORMED A PRECAUTIONARY LANDING IN AN UNIMPROVED AREA DUE TO REMOTE LOCATION OF AIRCRAFT AT THAT TIME. Sep 21, 2016 · N488AE · Bell 407 · Flight Environment DataSDR EVCA201601124Adapter · looseNUMBER 3 TAIL ROTOR DRIVESHAFT FOUND TO HAVE ADAPTER NUT BELOW MINIMUM TORQUE.Nov 23, 2015 · N488AE · Bell 407 · Tail Rotor Drive ShaftSDR EVCA201601200023Drive Shaft · wornNUMBER 2 TAIL ROTOR DRIVE SHAFT FOUND TO HAVE PITTING & A WEAR STEP ON COUPLING SPLINES.Nov 23, 2015 · N488AE · Bell 407 · Tail Rotor Drive Shaft

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