Registered owner
Med-Trans Corp
Location
Denton, TX
Owner type
Corporation
Serial number
53254
Year built
1998
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
April 3, 1998
Certificate issued
July 2, 2007
Expires
October 31, 2027
Mode S code
A4C6E4

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 N407CRMatched 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 · 2

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 · 7

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

SDR M3XA20181128706Tube · leakingPILOT MADE A PL WITHOUT INCIDENT NEAR SIX MILE, SC, NO PATIENT ON BOARD WHILE REPOSITIONING THE ACFT. THE ENGINE OIL PRESSURE WAS INDICATING LOW AND FLUCTUATING. UPON MECHANICS INSPECTION, IT WAS DETERMINED THAT THE COMPRESSOR #1 BEARING OIL SUPPLY TUBE HAD Nov 27, 2018 · N407CR · Bell 407 · Turbine Engine Oil SystemSDR 20000622SH026Gauge · leakingOXYGEN GAUGE LEAKING AT CONNECTION PIPE THREADS. SUBMITTER SUGGESTED INSTALLING FLARED OR BRASS FITTINGS TO SEAL BETTER. (X)Mar 17, 2000 · N407CR · Bell 407 · Portable Oxygen SystemSDR 20000622SH025Fuel Control · failedSTART PROBLEMS, I.E., (NON-STARTS, ERRATIC STARTS). CHANGED HMU. OPS NORMAL PER MM (ALLISON). (X)Feb 24, 2000 · N407CR · Bell 407 · Fuel Controlling SystemSDR 20000622SH023Fuel Control · leakingFUEL CONTROL (HMU) FOUND LEAKING AT AMBIENT AIR PASSAGE. LEAK AMOUNT (MOIST TO 1 OR 2 DROPS) AFTER LEAK CHECK, INTERNAL LEAKAGE. (X)Nov 5, 1999 · N407CR · Bell 407 · Fuel Controlling SystemSDR 99ZZZX4409Fcu · leakingFUEL CONTROL LEAKING AT AMBIENT AIR PASSAGE. 1-2 DROPS AFTER START. INTERNAL LEAKAGE.Nov 5, 1999 · N407CR · Bell 407 · Fuel Control/Turbine EnginesSDR 20000622SH024Starter Gen · failedSTARTER/GENERATOR FAILED WITH 405.6 TT. BRUSH LENGTH FAIR TO GOOD. NOT OIL OR FUEL SOAKED. BEARINGS OK. POSSIBLE INTERNAL SHORTING. (X)Nov 4, 1999 · N407CR · Bell 407 · Starter-GeneratorSDR 99ZZZX4410Starter/Gen · failedSTARTER/GENERATOR FAILED WITH 405.6 HOURS TT. BRUSH LENGTH FAIR TO GOOD. NOT OIL OR FUEL SOAKED. BEARINGS OK. SUBMITTER SUGGESTED POSSIBLE INTERNAL SHORTING.Nov 4, 1999 · N407CR · Bell 407 · Starter-Generator

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