Turbine helicopter

N912LH

2001 Md Helicopters MD 900

Registered 1 NTSB/FAA record
Built
2001
Serial
900-00095
Class
Turbine helicopter
Engines
2 × Pratt & Whitney Canada PW207E
Status
Current as of October 2026
Registered owner
Brim Equipment Leasing LLC (LLC)
Based
Ashland, OR
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Registration record

N912LH on the FAA register

Type
2001 Md Helicopters MD 900
Serial
900-00095
Engines
2 × Pratt & Whitney Canada PW207E
Registered owner
Brim Equipment Leasing LLC
Ashland, OR
Certificate issued
2025-05-29
Airworthiness date
2007-08-13
Registration expires
2032-05-31
Airworthiness class
Standard · normal
Mode S (hex)
AC9F1B
Mode S (octal)
53117433
Seats (type)
8
Weight class
12,500–19,999 lb
Range (type)
2,050 nm
Cruise (type)
438 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2032-05-31
    Registration expires (renewal due).
  • 2025-05-29
    Certificate of registration issued as N912LH.
  • 2007-08-13
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2006-03-22
    Accident at Mesa, AZ; damage: substantial.
  • 2001
    Manufactured (2001).
Overview

About N912LH

N912LH is a 2001 Md Helicopters MD 900, serial number 900-00095. The FAA register lists Brim Equipment Leasing LLC as the registrant in Ashland, Oregon. The current certificate of registration was issued on May 29, 2025 and expires on May 31, 2032.

The FAA aircraft reference file describes the type as a turbine helicopter, two Pratt & Whitney Canada PW207E engines and 8 seats. Published figures for the type give a cruise speed of about 438 knots and a range of about 2,050 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated August 13, 2007.

N912LH has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
438 kt
Range
2,050 nm
Takeoff over 50 ft
7,300 ft
Fuel burn
41 gph

Published figures for the Md Helicopters MD 900 type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2006-03-22 Accident · Mesa, AZ Damage: Substantial NTSB · ANC06LA038
Reported aircraft: MD Helicopters, MD 900
Probable cause: The manufacturer's inadequate design clearance of the main rotor blade grip pitch cases, which resulted in damage to the pitch cases when they contacted main rotor perimeter bolts during maneuvering flight.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.