Registered owner
Air Evac Ems Inc
Location
O Fallon, MO
Owner type
Corporation
Serial number
45300
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
August 31, 1979
Certificate issued
October 26, 2005
Expires
August 31, 2028
Mode S code
A6AE19

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 64

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
ADs by the year they took effect: 71 ADs
19803
19813
19821
19831
19852
19861
19871
19882
19892
19914
19922
19943
19953
19962
19992
20011
20022
20032
20042
20051
20072
20082
20092
20101
20111
20123
20133
20142
20151
20171
20192
20214
20224
20232
20241
See all 73 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N53AEMatched 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 · 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 · 6

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

SDR EVCA202310110001Unknown · unknownCREW AND PILOT NOTICED ACRID SMELL IN AIRCRAFT. CREW INITIALLY UNSURE WHETHER IS WAS ENVIRONMENTAL OR INSIDE AIRCRAFT. PILOT SAID SMELL WAS INDICITAVE OF A ELECTRICAL ISSUE OR BURNING WIRES. SMELL SUBSIDED AFTER OPENING WINDOWS. ON THE SUBSEQUENT FLIGHT, THE SOct 10, 2023 · N53AE · Bell 206L1 · Air Distribution SystemSDR EVCA2019070800002Blower Motor · malfunctionedSMOKE COMING FRONT AC VENTS. THE PROBLEM WAS FOUND TO BE THE FORWARD BLOWER EVAPORATOR MOTOR, REMOVED AND REPLACED WITH SERVICEABLE.Jul 8, 2019 · N53AE · Bell 206L1 · Humidity Control SystemSDR EVCA2017091400001Bulkhead · crackedDURING INSPECTION OF TAILBOOM ATTACHMENT FITTINGS IAW AD 2013-25-10 IT WAS NOTED THAT TAILBOOM RING WAS CRACKED. CRACK MEASURED APPROXIMATELY 3.2 INCHES LONG AND EXTENDS THROUGH BOTH FLANGES OF TAILBOOM RING.Sep 12, 2017 · N53AE · Bell 206L1 · Rotorcraft Tail BoomSDR EVCA201606291Pump · leakingDURING FLIGHT, PILOT REPORTED HEARING A GRINDING NOISE AT VARIOUS PITCHES COMING FROM THE TRANSMISSION AREA. WHEN MAINTENANCE ARRIVED TO INSPECT ACFT THEY FOUND HYDRAULIC FLUID COVERING THE DECK FROM THE HYDRAULIC PUMP AFT AND THE HYDRAULIC FLUID RESERVOIR WAJun 29, 2016 · N53AE · Bell 206L1 · Hydraulic Pump (Electric/Engine), MainSDR EVCA2015071315Fitting · crackedFOUND AN APPROX 1 INCH LONG CRACK ALONG WITH SEVERAL SMALLER, APPROX .25 INCH LONG CRACKS IN A CLIP LOCATED ON THE FS 145 BULKHEAD, CLIP PN 206-033-107-055.Jul 9, 2015 · N53AE · Bell 206L1 · Fuselage Main, BulkheadSDR EVCA2013090900049Skin · crackedDURING A ROUTINE INSPECTION, FOUND SKIN CRACKING ISSUES ALONG WITH LOOSE RIVETS.Sep 9, 2013 · N53AE · Bell 206L1 · Fuselage Main, Plate/Skin

STCs that may be installed · 459

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

See all 459 STCs