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N617MM

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2000 Raytheon C90A · Pratt & Whitney Canada PT6A-6 series

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Registered owner
Cal-Ore Life Flight LLC
Location
Brookings, OR
Owner type
LLC
Serial number
LJ-1587
Year built
2000
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 25, 2000
Certificate issued
November 10, 2023
Expires
November 30, 2030
Mode S code
A809DE
Raytheon C90AAirframe model · 9 seats · 2 engines · 155 registeredTCDS 3A20Airframe · Raytheon C90AEngine modelPratt & Whitney Canada PT6A-6 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.

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Airworthiness directives that may apply · 47

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
See all 51 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical bulletins · 2
SAIB CE-10-34R1Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08Issued Aug 20, 2013SAIB CE-10-34Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08Issued May 18, 2010

NTSB investigations · 1

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

NTSB WPR18LA197Accident · No injuriesClass 3 · LimitedFinal reportTolani Lake, AZAn autopilot deviation during climb for undetermined reasons, which resulted in an in-flight upset and loss of airplane control. Contributing to the accident was the pilot’s failure to adequately monitor flight systems due to a distraction.Jul 12, 2018 · Substantial damage

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.

Accident 20180712010929AClimb · Winslow, AZIn flight event. Under investigation. Aircraft not airworthy pending further insp. Substantial damage. Aircraft made uncontrolled input that put aircraft in uncommanded loss of control. PIC states: Leg to kflg to kgup we were climbing out of 17000 feet to our…Jul 12, 2018 · Substantial damage

Service difficulty reports · 4

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

SDR G1IA20220814030Controller · malfunctionedDURING CLIMB TO FL200 THE CABIN HI ALT MASTER WARNING LIGHT ILLUMINATED. THE CABIN RATE OF CLIMB INDICATED GREATER THAN 1000 FPM DONNED O2 MASKS AND DESCENDED TO 14,000. CYCLED LH & RH BLEED VALVES WITH NO CHANGE. ENSURED CAAug 14, 2022 · N617MM · Beech C90A · Cabin Pressure ControllerSDR G1IA201702160001Blower Motor · malfunctionedTHE PILOT REPORTED DURING A FLIGHT FROM KE91 TO KINW, DURING CRUISE PORTION OF FLIGHT, AN ELECTRICAL BURNING SMELL AND FUMES WERE NOTED IN THE COCKPIT AND CABIN, WITH THE CREW OBSERVING LIGHT SMOKE. THE AIRCRAFT RETURNED TO THE AIRPORT OF ORIGIN AND MADE AN UNFeb 15, 2017 · N617MM · Beech C90A · Air Distribution FanSDR CG02002F00001Wheel · crackedDURING TIRE CHANGE, FOUND SEVERAL BOLT HOLES CRACKED DURING ROUTINE EDDY-CURRENT INSPECTION OF BOLT HOLE AND TIRE BEAD SEAT AREAS.Sep 11, 2002 · N617MM · Beech C90A · Wheel/Ski/FloatSDR CG02002F00000Wheel · crackedDURING TIRE CHANGE FOUND SEVERAL BOLT HOLES CRACKED DURING ROUTINE EDDY-CURRENT INSPECTION OF BOLT HOLE AND TIRE BEAD SEAT AREAS. SUSPECT PROBABLY CAUSED BY OVERTORQUING OF TIE BOLTS DURING PAST TIRE CHANGES.Sep 11, 2002 · N617MM · Beech C90A · Wheel/Ski/Float

STCs that may be installed · 277

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

See all 277 STCs