- Registered owner
- Valiair Lc Trustee
- Location
- Casper, WY
- Owner type
- LLC
- Serial number
- 31-7512012
- Year built
- 1975
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 29, 1975
- Certificate issued
- November 28, 2023
- Expires
- November 30, 2030
- Mode S code
- A52AD3
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.
On this page
Airworthiness directives that may apply · 100
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1971 | 1 |
| 1973 | 1 |
| 1975 | 2 |
| 1976 | 2 |
| 1977 | 7 |
| 1978 | 5 |
| 1979 | 6 |
| 1980 | 6 |
| 1981 | 1 |
| 1983 | 2 |
| 1984 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 2 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 8 |
| 1997 | 5 |
| 1998 | 5 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 4 |
| 2006 | 5 |
| 2008 | 4 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 5 |
| 2013 | 2 |
| 2015 | 2 |
| 2016 | 1 |
| 2017 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 1 |
Airframe · Piper PA-31-325
AD 2023-09-09Exhaust Turbine System (Recip)AD 2017-10-20Fuselage--Main BulkheadAD 2016-05-01FuselageInformation bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Piper PA-31-325
SAIB CE-14-07WING SPAR Main Spar Lower Cap CracksSAIB CE-08-11Landing GearSAIB ACE-98-44Engine · Lycoming TI0-540 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-08-26R3Magneto/DistributorSAIB NE-09-04Fuel Control/Reciprocating EnginesSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-03-18SAIB NE-03-12SAIB NE-01-37Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N432CWMatched 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-31-325 aircraft
FAA incident reports
No FAA accident or incident reports matched to N432CWMatched 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-31-325 aircraft
Service difficulty reports
No reports matched to N432CWGeneral 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-31-325 aircraft
Reports on N432CW not matched to an aircraft · 2
They name N432CW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2006F00005Rib · crackedHORIZONTAL STABILIZER INBOARD RIB P/N 45A21104-012 FOUND WITH 3 INCH CRACK ALONG LOWER EDGE OF STAB CENTERING ROLLER BRACKET. BEEF UP ANGLES P/N 45A21085-004, AND 45A21086-004 ALSO FOUND WITH MULTIPLE STRESS CRACKS. EXCESSIVE LOADS ON ROLLER APPEAR TO HAVE CSDR 2005FA0001138Pressure Switch · failedRT WING OVERPRESSURE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. FOUND S128 PRESSURE SWITCH TO HAVE CONTINUITY WITH NO PRESSURE SWITCH TO HAVE CONTINUITY WITH NO PRESSURE APPLIED. REPLACED SWITCH ASSY WITH NEW UNIT IAW MM, OPERATIONS NORMAL. (K)
STCs that may be installed · 290
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-31-325
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