N6072W1964 Piper PA-28-140
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply3 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Hillman Maritime Services LLC
- Owner type
- LLC
- City, state
- Lafayette, LA
- Certificate issued
- Mar 17, 2023
- Expires
- Mar 31, 2030
- Airworthiness
- Standard · Normal, Utility
- Airworthiness date
- May 4, 1964
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-28-140
- Year
- 1964
- Serial number
- 28-20085
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A7E3F3
Engine
- Make and model
- Lycoming 0-320 Series
- Type
- Reciprocating
- Power
- 180 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – nowHillman Maritime Services LLCLafayette, LA · current
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 (5)
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 |
|---|---|---|---|
| 2018-07-03 | Placard and Markings | Apr 20, 2018 | Airframe (PA-28-140)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28-140) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28-140)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; … |
| 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-28-140)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). |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-28-140)Only with: Equipped with oil cooler hose assemblies that do not meet TSO-C53a, Type D requirements. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
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.
- Lights · support · misinstalledJun 5, 1997
DURING A 100-HOUR INSPECTION, THE LANDING LIGHT SUPPORT WAS FOUND INSTALLED UPSIDE-DOWN PREVENTING THE CASE FROM DRAINING. SUBMITTER SUGGESTS INATTENTION DURING RE-ASSEMBLY. PLACARD THE PART 'THIS SIDE UP'. ALIGN PROPERLY AND RIVET TO AIR FILTER RETAINER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat rail · corrodedApr 30, 1997
RIGHT OUTBOARD SEAT TRACK SEVERELY CORRODED UNDER LIP OF TRACK. SUSPECT CAUSE OF CORROSION WAS TRAPPED WATER IN THE CARPET FROM ENTRY INTO AIRCRAFT. ALSO, CARPET WAS NOT OF AIRCRAFT QUALITY OR TYPE (HOME SHAG CARPET). TO PREVENT RECURRENCE OF CORROSION, INSPECT CARPET AND REPLACE IF NOT AIRCRAFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control cable · stretchedApr 30, 1996
INSPECTION FOUND RT RUDDER CABLE STRETCHED NOT ALLOWING FOR PROPER PEDAL ALIGNMENT OF 8 DEGREES. SUSPECT CAUSE, STRETCHING OF CABLE DURING TOWING AND/OR OVERTURNING STOPS THAT ARE NOT PROPERLY ADJUSTED. THRASHING OF RUDDER IN CROSS WIND. SUBMITTER STATED PREVENTION BY PLACARDED WARNING ON TURN…
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