N496AE

BELL 407 · 1999 · Valid Registration

Registered owner: AIR EVAC EMS INC, MO (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
AIR EVAC EMS, INC. (EVCA)Certificate holderMatched by certificate designator
AIR EVAC EMS, INC. (EVCA)Operator2015-11-02 – 2015-11-02Operator named in NTSB report

Accident & incident history

Acc · 2015-11-02 Operator named in NTSB report
BELL 407 None injury Part 135AIR EVAC EMS, INC.
Source: NTSB case CEN16LA027

Maintenance disclosures

O · 2020-09-24 Matched by certificate designator
ATA 5330

DURING 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.

Source: SDR EVCA2020093001 · FAA SDRS
O · 2019-04-30 Matched by certificate designator
ATA 5320

DURING 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 ACCOMPLISHED WITH REFERENCE TO BHT ALL SRM CH 3

Source: SDR EVCA201904300001 · FAA SDRS
O · 2019-04-30 Matched by certificate designator
ATA 5330

SKIN 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.

Source: SDR EVCA20190430002 · FAA SDRS
O · 2019-04-30 Matched by certificate designator
ATA 5321

DURING INSPECTION AT OUR SWRMO. CORROSION METAL DEBONDING FOUND ON CO-PILOT FLOOR, UNDER INVERTOR.

Source: SDR EVCA20190430003 · FAA SDRS
O · 2017-04-05 Matched by certificate designator
ATA 5312

SEVERE 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 CONTAINED INSULATION. THE DAMAGE WAS CONTAINED TO THE SHELF AND THE FORWARD FACE OF TEH FS155 BULKHEAD.

Source: SDR EVCA20170405 · FAA SDRS
F · 2015-11-02 Matched by certificate designator
ATA 6510

UPON 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 A LOSS OF POWER TO THE TAIL ROTOR & SUBSEQUENT UNCOMMANDED YAW OF THE ACFT.

Source: SDR EVCA20151109001 · FAA SDRS
O · 2014-08-24 Matched by certificate designator
ATA 2150

AFT AIR CONDITIONER BLOWER INOPERATIVE.

Source: SDR EVCA2014082500068 · FAA SDRS
O · 2012-07-16 Matched by certificate designator
ATA 6410

ON DAILY INSPECTION, MECHANIC FOUND RIVET MISSING FROM THE TAIL ROTOR BLADE TIP.

Source: SDR EVCA2012071600032 · FAA SDRS