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Aircraft record

N6711Y1968 Piper PA-23-250

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply2 service difficulty reports

Registration
Valid
expires Oct 31, 2028
Based in
Woods Cross, UT
owner city / state
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
8
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Aero Services Lc
Owner type
LLC
City, state
Woods Cross, UT
Certificate issued
Oct 26, 2018
Expires
Oct 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Oct 17, 1968

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Piper
Model
PA-23-250
Year
1968
Serial number
27-4039
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A8E201

Engine

Make and model
Lycoming Ti0-540 Ser
Type
Reciprocating
Power
310 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2018 – nowAero Services LcWoods Cross, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (8)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2021-25-11Horizontal Stabilizer StructureJan 25, 2022Airframe (PA-23-250)Certain serial numbers: PA-23-250 27-7654001–27-7954121
2017-15-05Air ConditioningAug 28, 2017Airframe (PA-23-250)
2009-13-06 R1Piper Aircraft, Inc. AirplanesNov 3, 2011Airframe (PA-23-250)Only with: Equipped with a baggage door in the fuselage nose section (nose baggage door).
2005-01-10The New Piper Aircraft, Inc. Models PA-23-235, PA-23-250, and PA-E23-250 AirplanesFeb 22, 2005Airframe (PA-23-250)Only with: Equipped with Garrett (formerly AiResearch) turbosuperchargers installed under STC SA852WE, SA909WE, or SA978WE, or under Piper Aircraft Drawing Number 32016.
2003-09-13the New Piper Aircraft, Inc. Models PA-23, PA-23-160, PA-23-235, PA-23-250, and…Jun 23, 2003Airframe (PA-23-250)Certain serial numbers: PA-23 23-1–23-2046; PA-23-160 23-1–23-2046; PA-23-235 27-505–27-622; PA-23-250 27-1–27-504; PA-23-250 27-2000–27-8154030; PA-E23-250 27-2505–27-4916; …. Only with: Applies only to airplanes that do not incorporate P/N 17634-002 flap control torque tube or P/N 104622-002 or 104622-004 flap control torque tube assembly.
Show all 8 ADs
ADSubjectEffectiveApplies to
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-23-250)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-01–27-2504; PA-24-180 24-103–24-3687; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5028; …. Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2).
83-22-01 R1The New Piper Aircraft, Inc.; Models PA-23-235, PA-23-250, and PA-E23-250 AirplanesOct 22, 1998Airframe (PA-23-250)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-1–on; PA-E23-250 27-2505–27-7554168; PA-E23-250 27-7654001–on
98-04-27The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250…Mar 13, 1998Airframe (PA-23-250)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (2)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Flight controls · bolt · corrodedApr 7, 2016

    WHILE COMPLYING WITH AD74-13-03, SB 1160, AND SAIB CE-04-88, SEVERE CORROSION WAS DISCOVERED ON THE STABILATOR HORN AND BALANCE WEIGHT TUBE FITTING ATTACHMENT BOLTS, NO PART NUMBER CALLOUT. THE STABILATOR TO TORQUE TUBE ATTACHMENT BOLT HOLES WERE FOUND ELONGATED, AND LIGHT CORROSION WAS DISCOVERED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · bearing · seizedApr 7, 2016

    WHILE COMPLYING WITH AD74-13-03, SB 1160, AND SAIB CE-04-88, BOTH STABILATOR BEARINGS, PN 452-363 WERE FOUND SEVERELY CORRODED AND SEIZED. THESE ARE SEALED BEARINGS AND ROUTINE LUBRICATION IS NOT FEASIBLE. IT IS BELIEVED THESE WERE ORIGINAL BEARINGS WITH OVER 7000 HRS IN SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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