- Registered owner
- Moore Aviation Inc
- Location
- Beaver Falls, PA
- Owner type
- Corporation
- Serial number
- 4495003
- Year built
- 1989
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- August 9, 1989
- Certificate issued
- July 28, 2007
- Expires
- January 31, 2028
- Mode S code
- A16D12
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 2 |
| 1979 | 5 |
| 1980 | 6 |
| 1981 | 4 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 2000 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-44-180
AD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorAD 2015-26-08Rudder Control SystemInformation bulletins that may apply · 21
Advisory, not mandatory.
See all 30 bulletins
NTSB investigations
No NTSB investigations matched to N191NDMatched 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-44-180 aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20210414006029ILanding: Touchdown · Beaver Falls, PANose landing gear collapsed upon landing on runway 28 at Beaver County Airport (bvi). Upon inspection, the nose landing gear drag link pivot bolt was found sheared and the head of the bolt was missing. The bolt had backed out of the pivot point (connection of…Incident 19981030043129ILevel Off Touchdown · Devils Lake, ND(-5)The flight, conducted under 14 CFR part 91, for the purpose of student instruction, landed with the landing gear in the retracted position resulting in minor damage to the aircraft. The flight instructor who was also the pilot in command stated that he…
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2005FA0001253Starter · brokenPILOT ATTEMPTED START BUT STARTER WOULD NOT CRANK. UPON VISUAL INSP OF STARTER FOUND BENDIX HAD STUCK IN THE EXTENDED POSITION ON THE PREVIOS START CAUSINING THE GEAR TO BREAK AND BREAKING 2 MOUNTING PADS OF THE BENDIX HOUSING. DAMAGE WAS ALSO NOTED ON THE ENGSDR 98ZZZX1855Gear Lockplate · brokenDURING SCHEDULED ENGINE INSPECTION, CRANKSHAFT LOCK TAB WAS FOUND IN THE OIL SUMP SCREEN. REMOVED SUMP AND ACCESSORY HOUSING TO VERIFY. TAB ON BOLT WAS CONFIRMED BROKEN. CRANKSHAFT GEAR BOLT WAS FOUND TO HAVE MINIMAL TORQUE REMAINING. (LESS THAN 100 INCH/P
STCs that may be installed · 249
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-44-180
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