Twin piston

N7626Y

Piper PA-30 TWIN Comanche / Twin Comanche PA-30 / Turbo TWIN Comanche

Registered 2 NTSB/FAA records
Built
—
Serial
30-700
Class
Twin piston
Engines
2 × Lycoming IO-320 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Sherwood, AR
Registration record

N7626Y on the FAA register

Type
Piper PA-30 TWIN Comanche / Twin Comanche PA-30 / Turbo TWIN Comanche
Serial
30-700
Engines
2 × Lycoming IO-320 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Sherwood, AR
Certificate issued
2017-03-13
Airworthiness date
1965-01-18
Registration expires
2027-03-31
Airworthiness class
Standard · normal
Mode S (hex)
AA4C37
Mode S (octal)
52446067
Seats (type)
6
Weight class
up to 12,499 lb
Range (type)
1,188 nm
Cruise (type)
192 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2027-03-31
    Registration expires (renewal due).
  • 2017-03-13
    Certificate of registration issued as N7626Y.
  • 1968-01-24
    Accident at Bloomington,Ill, 13; damage: substantial.
  • 1966-07-25
    Accident at Philadelphia Pa, 38; damage: substantial.
  • 1965-01-18
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N7626Y

N7626Y is a Piper PA-30 TWIN Comanche / Twin Comanche PA-30 / Turbo TWIN Comanche, serial number 30-700. It is registered to an individual in Sherwood, Arkansas. The current certificate of registration was issued on March 13, 2017 and expires on March 31, 2027.

The FAA aircraft reference file describes the type as a twin piston, two Lycoming IO-320 series engines and 6 seats. Published figures for the type give a cruise speed of about 192 knots and a range of about 1,188 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated January 18, 1965.

N7626Y has 2 accident/incident records on file (most serious damage: substantial); details are below.

Cruise
192 kt
Range
1,188 nm
Power / thrust (each)
160
Takeoff over 50 ft
1,570 ft
Landing over 50 ft
1,875 ft
Fuel burn
17 gph

Published figures for the Piper PA-30 TWIN Comanche / Twin Comanche PA-30 / Turbo TWIN Comanche type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

1968-01-24 Accident · Bloomington,Ill, 13 Damage: Substantial NTSB · 3 0159
Reported aircraft: Piper PA-30
Probable cause: T OF DOWN GR LIMIT SWITCH.PLT FAILED TO USE EMGCY.
1966-07-25 Accident · Philadelphia Pa, 38 Damage: Substantial NTSB · 3 2097
Reported aircraft: Piper PA-30

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.