- Registered owner
- Asb1 Group LLC
- Location
- Miramar, FL
- Owner type
- LLC
- Serial number
- 31-8152162
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 5, 1981
- Certificate issued
- September 27, 2023
- Expires
- September 30, 2030
- Mode S code
- A4D0AD
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 · 106
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 |
| 1974 | 1 |
| 1975 | 4 |
| 1976 | 3 |
| 1977 | 7 |
| 1978 | 4 |
| 1979 | 7 |
| 1980 | 6 |
| 1981 | 2 |
| 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 | 4 |
| 1998 | 5 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 4 |
| 2006 | 6 |
| 2008 | 4 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 5 |
| 2013 | 2 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 1 |
See all 129 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Piper PA-31-350
SAIB CE-14-07WING SPAR Main Spar Lower Cap CracksSAIB CE-08-11Landing GearSAIB CE-04-86SAIB 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 N40919Matched 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-31-350 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BSYA201403Unknown · malfunctionedMOMENTS AFTER DEPARTURE FROM LWM, PILOT NOTICED RT ENG OIL PRESS DROPPING & OIL TEMP RUNNING HIGH. PILOT NOTIFIED ATC, RETURNED BACK & LANDED SAFELY AT LWM WITHOUT INCIDENT. MAINTENANCE IS INSPECTING.SDR BSYA201402Unknown · malfunctionedMOMENTS AFTER DEPARTURE FROM LWM, PILOT NOTICED LT ENG OIL PRESS DROPPING & TEMP RUNNING HIGH. PILOT NOTIFIED ATC, RETURNED BACK & LANDED SAFELY AT LWM WITHOUT INCIDENT. MAINTENANCE IS INSPECTING.SDR BSYA2012010Alternator · inoperativeAFTER TAKE OFF FROM CYOW, PILOT EXPERIANCED RIGHT ALTERNATOR FAILURE.PILOT RETURNED TO CYOW AND LANDED SAFELY WITHOUT INCIDENT.MAINTENANCE REPLACED RIGHT ALTERNATOR, OPERATIONALY CHECK NORMAL, NO OTHER DEFECTS NOTED.SDR BSYA2011038Controller · out of adjustON TAKEOFF THE RIGHT ENGINE ONLY BOOSTED TO 38 INCHES AND BOTH ENGINES WERE SURGING 1.5 INCH MANIFOLD PRESSURE. RETURNED. MAINTENANCE ADJUSTED RIGHT DENSITY CONTROLLER AND CLEANED LEFT ENG FUEL NOZZLES, BOTH ENG'S OPS CHECK GOOD.SDR BSYA2011035Nozzle · dirtyAFTER DEPARTING PILOT HAD LEFT ENGINE RUNNING ROUGH, DIVERTED. MAINTENANCE CLEANED FUEL NOZZLES AND CHANGED ALL SPARK PLUGS, OPS CHECKED GOOD.SDR BSYA2009062Downlock Hook · dirtyAIRCRAFT GOING INTO ADS HAD NO LEFT GEAR DOWN AND LOCK INDICATION, LANDED NO PROBLEMS. MAINTENANCE CLEANED AND LUBED DOWN AND LOCK HOOK, CYCLED GEAR MANY TIMES, OPS CHECKS GOOD.SDR BSYA2009054Fastener · looseAFTER DEPARTING ADS PILOT NOTICED A COUPLE OF FASTENERS POPPED LOOSE. RETURNED TO ADS, MAINTENANCE SECURED ALL FASTENERS, OK FOR CONTINUED FLIGHT.SDR BSYA2009038Rocker · brokenAFTER DEPARTING HOU, THE LEFT ENGINE STARTED SURGING 50 RPM ON CLIMBOUT. RETURNED TO HOU. FOUND LEFT ENGINE NR 1 CYLINDER INTAKE ROCKER ARM BROKEN. REPLACED CYLINDER, ROCKER ARM AND LIFTER.SDR BSYA2009037Fuel Nozzle · dirtyAPPROXIMATELY 10 MINUTES AFTER TAKEOFF OUT OF HOU TO ADS, THE LEFT ENGINE STARTED SURGING BETWEEN 32 TO 35 INCHES MANIFOLD PRESSURE. RETURNED TO HOU. MAINTENANCE CLEANED FUEL NOZZLES AND LUBED WASTE GATE, GROUND RUN GOOD.SDR 20010122CW004Engine · malfunctionedMIR SDF LEFT ENGINE NOT DEVELOPING FULL POWER FOR TAKE OFF. HAD MAINTENANCE AT SDF C/W COMP CHECK ALL GOOD, RAN AIRCRAFT , COULD NOT DUPLICATE PROBLEM, RETURNED AIRCRAFT TO SERVICE.SDR 97ZZZX3407Connecting Rod · failedLEFT ENGINE FAILED DUE TO CONNECTING ROD FAILURE AT THE NR 4 POSITION. AREA OF WHICH ROD MAY HAVE INITIALLY FAILED, COULD BE RELATED TO LYCOMING SB 439A (INSPECTION OF CONNECTING RODS FOR FRETTING AND/OR GALLING). THE ABOVE STATMENT WAS WRITTEN AFTER DISASSESDR BSYA610CConnect Rod · failedDURING APPROACH INTO CMH, LEFT ENGINE MADE A LOUD POP NOISE. PILOT FEATHERED ENGINE. NR 3 CYLINDER CONNECTING ROD PUT HOLE THROUGH ENGINE CASE. CAUSE AT THIS TIME UNKNOWN. (X)
STCs that may be installed · 300
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-31-350
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
Earlier aircraft with this N-number · 1
This aircraft carried N40919 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.