- Registered owner
- Pacific Integrated Handling Inc
- Location
- Tacoma, WA
- Owner type
- Corporation
- Serial number
- 31T-8166018
- Year built
- 1981
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 25, 2016
- Certificate issued
- June 14, 2016
- Expires
- June 30, 2029
- Mode S code
- A07FA5
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every U/A Canada PT6A model are included below.
On this page
Airworthiness directives that may apply · 23
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1982 | 1 |
|---|---|
| 1985 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 3 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 1 |
| 2017 | 1 |
See all 24 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Piper PA-31T2
SAIB CE-17-05Electrical Power/Electrical Power System WiringSAIB CE-08-11Landing GearNTSB investigations
No NTSB investigations matched to N131HPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-31T2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N131HPMatched 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-31T2 aircraft
Service difficulty reports
No reports matched to N131HPGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-31T2 aircraft
Reports on N131HP not matched to an aircraft · 2
They name N131HP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 200600073Skin · cracked2EA CRACKS WERE DETECTED WHILE PERFORMING AD 2002-19-14, 1 CRACK EMANATING FROM A FASTENER HOLE LOCATED AT FS 543 RT CW STA 70 LOWER WING AND 1 CRACK EMANATING FROM A FASTENER HOLE AT FS 569, LT CW STA 57, LOWER WING. BOTH CRACKS ARE .1250 INCH LONG.SDR 1001Spar · crackedFORWARD WING SPAR WEB WAS CRACKED IN THE SAME LOCATION BOTH SIDES STA. 85 CENTER WING. 3 DIFFERENT LOWER WING STRINGER ATTACH ANGLES CRACKED IN THE SAME FASHION CWS 216 LT SIDE. LOWER WING STRINGER CRACKED CWS 216 LEFT. LEFT WING LOWER SKIN CRACKED CWS 218.
STCs that may be installed · 181
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-31T2
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