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N5388V

Cancelled 2021
Open the Markdown

Deregistered aircraft · 1963 Hiller UH-12E · Lycoming VO-540 series

Open in FAA registry

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Cancelled
May 8, 2021
Status when cancelled
Registration expired, pending cancellation
Serial number
2099
Year built
1963
Type
Rotorcraft
Engine
Reciprocating
Airworthiness
Multiple
Airworthiness date
April 11, 1963
Certificate issued
June 3, 1969
Last registry action
September 16, 2017
Mode S code
A6D1A9
Owner when cancelled
Pope James R DBA
Location
Clarkston, WA
Owner type
Individual
Airframe modelHiller UH-12ETCDS 4H11 · ADs, bulletins and aircraft registered nowEngine modelLycoming VO-540 seriesTCDS E-304 · Reciprocating

From the FAA registry file of November 4, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 2

Matched to this aircraft by N5388V and the event date: up to this one’s cancellation.

NTSB SEA00TA013Accident · Serious injuriesFinal reportStites, IDInadequate inspection of the control rotor cuff by a company mechanic and subsequent fatigue fracture of the cuff, resulting in an inflight separation of the control rotor blade. Factors contributing to the accident were: inadequate quality control during…Nov 2, 1999 · Substantial damageNTSB SEA67A0060Accident · No injuriesClosedOrofino, IDApr 21, 1967 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N5388V and the event date: up to this one’s cancellation.

Accident 19991102043059AStites, ID(-23) Pilot reported loss of control of helicopter when control rotor tube assembly separated from helicopter. Helicopter fell through electrical power lines before impacting terrain causing substantial damage. Pilot and one passenger sustained minor…Nov 2, 1999 · No damage

Service difficulty reports · 1

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

SDR 99ZZZX4550Cuff · failedCONTROL ROTOR CUFF SPLIT IN TWO AT THE INBOARD BOLT HOLE. OUTBOARD SECTION AND CONTROL ROTOR TUBE ASSEMBLY SEPARATED FROM HELICOPTER CAUSING LOSS OF CONTROL. CRACK APPEARS TO HAVE STARTED AT INBOARD BOLT HOLE. BOTH HALVES OF CUFF SENT TO NTSB LAB FOR ANALYSNov 10, 1999 · N5388V · Hiller UH12E · Tail Rotor Blades