N8107D1979 Piper PA-34-200T
This N-number isn't registered right now. Below is its last known registration, canceled Oct 1, 2022.
Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Dodson International Parts INC
- Owner type
- Corporation
- City, state
- Rantoul, KS
- Certificate issued
- Jun 6, 2019
- Canceled
- Oct 1, 2022
- Airworthiness
- Standard · Normal
- Airworthiness date
- Oct 15, 1979
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 dataAirframe
- Manufacturer
- Piper
- Model
- PA-34-200T
- Year
- 1979
- Serial number
- 34-8070010
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 7
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AB0CAD
Engine
- Make and model
- Cont Motor Tsio-360 Ser
- Type
- Reciprocating
- Power
- 225 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019 – 2022Dodson International Parts INCRantoul, KS
- 1958Jonas Aircraft & Arms Co INCNew York City, NY · different airframe: Piper Pa-22-160 S/N 22-6116
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (7)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-34-200T) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-34-200T)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; … |
| 2005-15-10 | The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T… | Aug 26, 2005 | Airframe (PA-34-200T)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump. |
| 2005-13-16 | The New Piper Aircraft, Inc. PA-34 Series Airplanes | Aug 8, 2005 | Airframe (PA-34-200T) |
| 99-05-09 | The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series Airplanes | Mar 19, 1999 | Airframe (PA-34-200T)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). |
Show all 7 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-01-01 R1 | The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series… | Dec 8, 1998 | Airframe (PA-34-200T)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies. |
| 98-04-27 | The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250… | Mar 13, 1998 | Airframe (PA-34-200T) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
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.
- Stabilizers · stabilizer · rivet shearedJul 21, 1997
BOTH LOWER RIVETS (LT AND RT) WERE FOUND SHEARED ON THE AFT SPAR OF THE VERTICAL STABILIZER WHERE THE VERTICAL STABILIZER ATTACHES TO THE EMPENNAGE. SUBMITTER STATED THIS IS AIRCRAFT NR 3 IN FLEET OF PA 34-200T'S THAT HAS BEEN FOUND TO HAVE THIS PROBLEM.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · wire · burnedDec 11, 1996
BRAIDED WIRE TYPE BATTERY CABLES LOOSE AT BATTERY TERMINALS, CAUSES SEVERE VOLTAGE FLUCTUATIONS AND FLIGHT INTERRUPTION. OPERATOR REPORTS NUMEROUS PROBLEMS WITH THIS TYPE CABLE. EXTREMELY DANGEROUS CONDITIONS RESULT WHEN BRAIDING COMES UNDONE AND BATTERY TERMINALS GET LOOSE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · landing gear · malfunctionNov 25, 1996
PILOT DEPARTED FIELD WITH SNOW ON TAXIWAYS AND RUNWAY. LANDING GEAR FAILED TO FULLY RETRACT DUE TO BLOCKAGE BY CHUNKS OF ICE AND SNOW. SUBMITTER SUGGESTS P.O.H. REVISION TO PRECLUDE OPERATION OF THIS MODEL AIRCRAFT FROM FIELDS WITH ANY FORM OF ICE, SNOW, SLUSH.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Doors · lock assy · fails testOct 15, 1996
KEY CAN BE REMOVED FROM DOOR LOCK WHEN LOCK IS IN OPEN POSITION REGARDLESS OF DOOR LATCH POSTION. FAILS TESTS PER AD 88-04-05. SUBMITTER STATED THE AD SHOULD BE A 100-HOUR RECURRING MAINTENANCE REQUIREMENT. MOST PILOTS UNAWARE OF NEED FOR PRE/POST-FLIGHT CHECKS PER PAPER SB 633B.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · latch assy · defectiveOct 15, 1996
LOWER LATCH ASSY IS ELONGATING HOLE IN LOWER SILL OF FWD BAGGAGE DOOR ASSY. FAILS TESTS PER AD 88-04-05 EVEN THOUGH AD PREVIOUSLY C/W. SUBMITTER STATES INSPECTIONS REQUIRED BY AD SHOULD BE 100-HR MAINTENANCE REQUIREMENTS. MOST PILOTS UNAWARE OF NEED FOR PRE/POST-FLIGHT CHECK PER PIPER SB 633B.
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