- Registered owner
- Hillman Maritime Services LLC
- Location
- Lafayette, LA
- Owner type
- LLC
- Serial number
- 28-20085
- Year built
- 1964
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- May 4, 1964
- Certificate issued
- March 17, 2023
- Expires
- March 31, 2030
- Mode S code
- A7E3F3
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-320 model are included below.
On this page
Airworthiness directives that may apply · 77
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1965 | 1 |
| 1966 | 1 |
| 1967 | 3 |
| 1968 | 3 |
| 1969 | 2 |
| 1970 | 1 |
| 1971 | 3 |
| 1972 | 4 |
| 1974 | 3 |
| 1975 | 2 |
| 1977 | 4 |
| 1978 | 2 |
| 1979 | 4 |
| 1980 | 4 |
| 1981 | 1 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2010 | 3 |
| 2012 | 1 |
| 2013 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2020 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-28-140
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-24-05Wing SparInformation bulletins that may apply · 30
Advisory, not mandatory.
See all 40 bulletins
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N6072WMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piper PA-28-140 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX2956Support · misinstalledDURING 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.SDR 97ZZZX2342Seat Rail · corrodedRIGHT 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, INSSDR 96ZZZX2569Control Cable · stretchedINSPECTION 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 PR
STCs that may be installed · 469
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-28-140
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller