- Registered owner
- Arnold Mark W
- Location
- Columbus, OH
- Owner type
- Individual
- Serial number
- 34-7970096
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Certificate issued
- July 12, 2016
- Expires
- July 31, 2029
- Mode S code
- A1DD53
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-360 model are included below.
On this page
Airworthiness directives that may apply · 56
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1971 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 3 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 2 |
| 1986 | 2 |
| 1988 | 2 |
| 1991 | 1 |
| 1992 | 2 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 2 |
| 2022 | 2 |
| 2023 | 4 |
See all 69 ADs
Information bulletins that may apply · 18
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations
No NTSB investigations matched to N2190KMatched 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-34-200T aircraft
FAA incident reports
No FAA accident or incident reports matched to N2190KMatched 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-34-200T aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0001236Elt · malfunctioned(BIER) ELT REMOVED FOR INSP AND TESTING IAW CFR PART 91.207D. DURING BENCH TESTING OF ME-406 ELT, THE ELT WOULD NOT TURN OFF OR RESET. INTERNAL BATTERY HAD TO BE UNPLUGGED TO PREVENT ELT FROM REPEATED TRANSMITTION. ELT PN 453-6603, SN 14668 WAS SENT FOR NEEDSDR 2008FA0000678Elt · no testELT EMERGENCY LOCATOR TRANSMITTER WILL NOT TEST PROPERLY ON A CONSISTENT BASIS BY DISPLAYING CORRECT 3-DIGIT COUNTRY CODE OR 15 DIGIT HEX ID CODE. THIS ELT HAS BEEN TESTED WITH (2) DIFFERENT 406 MHZ TESTERS. DISTRIBUTED, PN 453-1000 AND 453-0131 AND THE PERFSDR 2008FA0000677Elt · failedELT EMERGENCY LOCATOR TRANSMITTER WILL NOT TEST PROPERLY ON A CONSISTENT BASIS BY DISPLAYING CORRECT 3-DIGIT COUNTRY CODE OR 15 DIGIT HEX ID CODE. THIS ELT HAS BEEN TESTED WITH (2) DIFFERENT 406 MHZ TESTERS DISTRIBUTED BY PN 453-1000 AND PN 453-0131 (MEASURE SDR 2008FA0000509Arm · wornNLG MOUNT ASSY ATTACHMENT POINT FOR STEERING ARM ASSY HAS EXCESSIVE WEAR AT LWR MOUNT HOLE, SRM DOES NOT SPECIFY AT FIX OR ALLOWABLE LIMIT FOR PN 95551-23. DISCREPANCY FOUND DURING INSP IAW SB 1123A & B AND ANNUAL INSPECTION IAW SRM INSPECTION GUIDE. SB 1123SDR 2004FA0000774Housing · brokenDURING SEARCH FOR OIL LEAK ONTO ALTERNATOR FOUND. OIL SCAVENGE PUMP HOUSING HAD BROKEN MOUNT LUG. REPLACED WITH NEW PART. CAUSE OF FAILURE BELIEVED TO BE WEAK CONSTRUCTION. AIRCRAFT FREON COMPRESSOR MOUNTS HERE. AIRCRAFT HAS HAD DYNAMIC PROP BALANCES. SESDR 2001FA0000659Torque Tube · damagedWHILE INSPECTING RUDDER ON ANNUAL INSPECTION THE INSPECTOR FOUND LOOSENESS AT THE RUDDER TORQUE TUBE ATTACH BOLTS. TEARDOWN INSPECTION SHOWED BOLT HOLES OVERSIZE AND ELONGATED. NEW PARTS INSTALLED BECAUSE (AN 174) BOLTS WERE LARGEST SIZE BOLTS PERMITTED. MFSDR 98ZZZX3938Angle · corrodedWHILE C/W SB 977, CORROSION WAS FOUND ON TOP OF LEFT, AFT WING ATTACH AND LOWER CABIN DOOR POST ATTACH. SUSPECT WATER LEAKING IN AFT CABIN DOOR AT SOME PREVIOUS TIME. LEFT CABIN INTERIOR WAS REMOVED FOR AVIONICS INSTALL AND PROVIDED ACCESS FOR BETTER INSPECTSDR 98ZZZX3937Valve · failedDURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTERSDR 98ZZZX3936Valve · failedDURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTERSDR 98ZZZX3934Stop · damagedDURING AIRCRAFT INSPECTION, NOSE LANDING GEAR WAS FOUND BADLY DAMAGED DUE TO OVERSTEERING WHEN TOWING. PARTS HAD TO BE REPLACED. SUBMITTER SUGGESTED MFG INSTALL TOW LIMIT MARKING TO AID IN PREVENTING EXCEEDING TOW LIMITS. ALSO, FOUND P/ N 7853500 TILLER ARM
STCs that may be installed · 320
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 320 STCs