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Type Record · As of May 3, 2026

NEW PIPER AIRCRAFT INC PA-34-220T

Fixed Wing Multi Engine · CONT MOTOR TSIO-360 SER

Registered

8

Year Range

1999–2004

NTSB Events

0

Airworthiness Directives

50

01 /  Distribution

Where the fleet lives and was built

Counts of currently-registered NEW PIPER AIRCRAFT INC PA-34-220T aircraft by US state and decade of manufacture, sourced from the FAA Aircraft Registry.

By State (top 10)

  • FL 50.0% 4
  • DE 37.5% 3
  • AL 12.5% 1

By Decade of Manufacture

  • 1990s 12.5% 1
  • 2000s 62.5% 5
  • Unknown 25.0% 2

02 /  NTSB Records

Events involving NEW PIPER AIRCRAFT INC PA-34-220T aircraft

No NTSB-recorded events match NEW PIPER AIRCRAFT INC PA-34-220T in the indexed corpus.

02b /  NASA ASRS Reports

Near-miss reports involving NEW PIPER AIRCRAFT INC PA-34-220T

NASA's voluntary, confidential reporting system surfaces what almost went wrong. 1 de-identified ASRS report references this airframe. Pilot-written narrative. ASRS reports are voluntary and not investigated — they represent the reporter's perspective and cannot infer prevalence.

03 /  Airworthiness Directives

FAA directives applicable to NEW PIPER AIRCRAFT INC PA-34-220T

50 directive(s) on file. Showing the most recent 25 · 25 more in the Federal Register.

  • May 22, 2024

    Airworthiness Directives; Piper Aircraft, Inc. Airplanes

    The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Model PA-28-181, PA-28R-201, PA- 34-220T, and PA-44-180 airplanes. This AD was prompted by a report of a double-drilled bolt hole of the rear wing spar attachment fitting found during an unscheduled inspection of an airplan…

  • Jun 12, 2023

    Airworthiness Directives; Various Airplanes, Helicopters, and Engines

    The FAA is adopting a new airworthiness directive (AD) for turbocharged, reciprocating engine-powered airplanes and helicopters and turbocharged, reciprocating engines with a certain v-band coupling installed. This AD was prompted by multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to t…

  • Dec 1, 2020

    Airworthiness Directives; Piper Aircraft, Inc. Airplanes

    The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc., Model PA-34-220T airplanes. This AD was prompted by a report of damage to the rudder flight control cables and the emergency power supply (EPS) system wiring due to inadequate clearance from the EPS wiring harness. This AD require…

  • Aug 17, 2020

    Airworthiness Directives; Aspen Avionics, Inc.

    The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. The AD applies to certain Aspen Avionics, Inc., Evolution Flight Display (EFD) EFD1000 Emergency Backup Display, EFD1000 Multi-Function Display, and EFD1000 Primary Flight Display systems installed on various airplanes. As pu…

  • Jul 31, 2020

    Airworthiness Directives; Aspen Avionics, Inc.

    The FAA is adopting a new airworthiness directive (AD) for certain Aspen Avionics, Inc., Evolution Flight Display (EFD) EFD1000 Emergency Backup Display, EFD1000 Multi-Function Display, and EFD1000 Primary Flight Display systems installed on various airplanes. This AD imposes operating restrictions on these display sy…

  • Jul 28, 2020

    Airworthiness Directives; Piper Aircraft, Inc. Airplanes

    The FAA proposes to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Model PA-34-220T airplanes. This proposed AD was prompted by a report of damage to the rudder flight control cables and the emergency power supply (EPS) system wiring due to inadequate clearance from the EPS wiring harness. T…

  • Jan 23, 2019

    Airworthiness Directives; Aspen Avionics, Inc., Evolution Flight Display Units

    We are adopting a new airworthiness directive (AD) for certain Aspen Avionics, Inc. (Aspen), Evolution Flight Display (EFD) EFD1000 Primary Flight Display (PFD), EFD1000 Multi-Function Display (MFD), EFD1000 Emergency Backup Display (EBD), and EFD500 MFD units installed on various aircraft. This AD requires disabling…

  • Feb 4, 2013

    Airworthiness Directives; Piper Aircraft, Inc.

    We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft Inc.) PA-28, PA-32, PA-34, and PA-44 airplanes. This AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stabilator contro…

  • Aug 2, 2012

    Airworthiness Directives; Piper Aircraft, Inc. Airplanes

    We propose to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft Inc.) PA-28, PA-32, PA-34, and PA-44 airplanes. This proposed AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stab…

  • Jul 27, 2010

    Airworthiness Directives; Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes

    We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-28, PA-32, PA-34, and PA-44 series airplanes. This AD requires you to inspect the control wheel shaft on both the pilot and copilot sides and, if necessary, replace the control wheel shaft. This AD results from two field rep…

  • Oct 30, 2009

    Airworthiness Directives; Piper Aircraft, Inc. PA-28, PA-32, PA-34 and PA-44 Series Airplanes

    We propose to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-28, PA-32, PA-34 and PA-44 series airplanes. This proposed AD would require an inspection of the control wheel shaft for both the pilot and copilot sides and, if necessary, replacement of the control wheel shaft. This pr…

  • Feb 27, 2009

    Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)

    We are adopting a new airworthiness directive (AD) to supersede AD 2008-06-28 R1, which applies to certain Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (part numbers (P/Ns) 700-00006-000, -001, -002, -003, and -100) that are installed on airplanes. AD 2008-06-28 R1 currently requires you to do a check…

  • Nov 14, 2008

    Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)

    We propose to supersede Airworthiness Directive (AD) 2008-06- 28 R1, which applies to certain Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (part numbers (P/Ns) 700-00006-000, -001, -002, -003, and -100) that are installed on airplanes. AD 2008-06-28 R1 currently requires you to do a check of the mainte…

  • Apr 14, 2008

    Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)

    The FAA is adopting a new airworthiness directive (AD) to revise AD 2008-06-28, which applies to certain Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (Part Numbers (P/Ns) 700- 00006-000, -001, -002, -003, and -100) that are installed on airplanes. AD 2008-06-28 currently requires you to do a check of t…

  • Mar 26, 2008

    Airworthiness Directives; Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)

    The FAA is adopting a new airworthiness directive (AD) for certain Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (Part Numbers (P/Ns) 700-00006-000, -001, -002, -003, and -100) that are installed on airplanes. This AD requires a check of the maintenance records and inspection of the PFD (if necessary) t…

  • Jul 26, 2005

    Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T Airplanes

    The FAA adopts an airworthiness directive (AD) to supersede AD 2003-11-14, which applies to certain The New Piper Aircraft, Inc. (Piper) Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T airplanes that have a model 91E92-1 or model 91E93-1 combustion heater fuel pump installed. AD 2003-11-14 currently requires…

  • Jun 22, 2005

    Airworthiness Directives; The New Piper Aircraft, Inc. PA-34 Series Airplanes

    The FAA adopts an airworthiness directive to supersede AD 93- 24-14 applicable to all The New Piper Aircraft, Inc. (Piper) PA-34 series airplanes. This AD results from many service difficulty reports related to the collapse of the nose landing gear (NLG). Consequently, this AD retains the actions required in AD 93-24-…

  • Feb 9, 2005

    Airworthiness Directives; The New Piper Aircraft, Inc. PA-34 Series Airplanes

    The FAA proposes to supersede Airworthiness Directive (AD) 93- 24-14, which applies to all The New Piper Aircraft, Inc. (Piper) PA-34 series airplanes. AD 93-24-14 currently requires you to repetitively replace the bolt and stack up that connect the upper drag link to the nose gear trunnion. This proposed AD is the re…

  • Jan 19, 2005

    Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

    The FAA is adopting a new airworthiness directive (AD) to supersede Airworthiness Directive 2004-10-15, which applies to certain GTX 330 and GTX 330D Mode S transponders that are installed on airplanes. AD 2004-10-15 currently requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This AD a…

  • Oct 7, 2004

    Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

    The FAA proposes to supersede Airworthiness Directive (AD) 2004-10-15, which applies to certain GTX 330 and GTX 330D Mode S transponders that are installed on airplanes. AD 2004-10-15 currently requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This proposed AD applies to certain GTX 33…

  • Aug 20, 2004

    Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32- 301FT, PA-32-301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP Airplanes

  • Jul 9, 2004

    Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP Airplanes

    The FAA is adopting a new airworthiness directive (AD) for certain The New Piper Aircraft, Inc. (Piper), Models PA-28-161, PA-28- 181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32- 301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP airplanes. This AD requires you to inspect the control wheel at…

  • May 21, 2004

    Airworthiness Directives; GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

    The FAA adopts a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders that are installed on aircraft. This AD requires you to install GTX 330/330D Software Upgrade Version 3.03, 3.04, or 3.05. This AD is the result of observations that the GTX 330 and GTX 330D may…

  • Dec 30, 2003

    Airworthiness Directives; GARMIN International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

    The FAA proposes to adopt a new airworthiness directive (AD) for certain GARMIN International Inc. GTX 330/GTX 330D Mode S transponders. This proposed AD would require you to install GTX 330/ 330D Software Upgrade Version 3.03. This proposed AD is the result of observations that the GTX 330 and GTX 330D may detect, fr…

  • Jul 21, 2003

    Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T Airplanes

04 /  Type Certificate Data Sheets

FAA TCDS for NEW PIPER AIRCRAFT INC PA-34-220T

The TCDS is the legal certification document — weight limits, performance, equipment, AD compliance times, operating limitations. 1 match in the FAA catalog.

  • A7SO Current Rev 13 · 12/18/1996

    The New Piper Aircraft Inc.

    Models: PA-34-200 (Seneca), PA-34-200T (Seneca II), PA-34-220T (Seneca III), PA-34-220T (Seneca IV) + 4 more

05 /  Special Airworthiness Information Bulletins

Advisories applicable to NEW PIPER AIRCRAFT INC PA-34-220T

4 SAIBs on file. SAIBs are FAA advisory notices — not mandatory like ADs, but worth reviewing for service bulletins and emerging issues.

06 /  Supplemental Type Certificates

Modifications approved for NEW PIPER AIRCRAFT INC PA-34-220T

451 STCs on file — every FAA-approved modification, alteration, or installation for this aircraft. STOL kits, avionics, fuel systems, floats, engine swaps, you name it.

  • 03/03/2026

    STC SA02511SE

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 07/24/2025

    STC SA02511SE

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 07/21/2025

    STC SA02511SE

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 04/01/2025

    STC SA04046CH PAGE 2

    Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500)

    Acron Aviation Inc.

  • 04/01/2025

    STC SA02738CH (PAGE 2)

    Installation of L-3 Communications Avionics Systems

    Acron Aviation Inc.

  • 11/22/2024

    STC SA04378CH

    Installation of an engine modified per STC SE04349CH

    SureFly Partners Ltd.

  • 11/20/2024

    STC SA01120SE

    Installation of Door Steward.

    Mountain View Aviation LLC

  • 09/26/2024

    STC SA02594SE

    SkyView HDX Instrumentation and Autopilot System manufactured

    Dynon Avionics

  • 08/27/2024

    STC SA04837NY

    Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights

    AeroLED's Holdings, LLC

  • 08/27/2024

    STC SA02386AK

    Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems

    AeroLED's Holding LLC

  • 07/29/2024

    STC SA01866WI

    Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection

    Garmin International Inc.

  • 06/14/2024

    STC SA02798SE

    Installation of Absolute Solutions LLC Gear Warning System Upgrade

    Absolute Solutions LLC

  • 06/13/2024

    STC SA02511SE

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 06/13/2024

    STC SA02511SE (2 OF 2)

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 06/13/2024

    STC SA02511SE (2 OF 3)

    Installation of replacement fuel quantity indicator sending unit(s)

    CiES Inc.

  • 02/02/2024

    STC SA02658SE (1 OF 2)

    Installation of Garmin GI 275 Multi-Function Display System

    Garmin International Inc.

  • 01/31/2024

    STC SA01866WI

    Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection

    Garmin International Inc.

  • 11/16/2023

    STC SA02532AT

    Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.

    Michelin North America Inc.

  • 09/08/2023

    STC SA01866WI

    Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection

    Garmin International Inc

  • 08/10/2023

    STC SA02019WI

    Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.

    Peregrine

  • 07/19/2023

    STC SA04378CH

    Installation of an engine modified per STC SE04349CH on an aircraft listed on FAA approved model list #SA04378CH dated 1/13/19 or later FAA approved revision, IAW SureFly installat…

    SureFly Partners Ltd.

  • 06/29/2023

    STC SA04400NY

    Installation of the Integrated Back-up Battery System (IBBS)

    TCW Technologies LLC

  • 05/08/2023

    STC SA04192NY

    KFD 900 Primary Flight Display System Additional Functions

    Honeywell International Inc

  • 04/05/2023

    STC SA00756DE

    Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Se…

    Peregrine

  • 04/04/2023

    STC SA11137SC

    Installation of Plane-Power ALT-FLX alternator

    Hartzell Engine Technologies, LLC

  • 01/24/2023

    STC SA01206AT

    Installation of a cowling nose bowl

    Whelen Aerospace Technologies

  • 01/24/2023

    STC SA00163AT

    Installation of "Speed Splitter" flap bracket fairings

    Whelen Aerospace Technologies

  • 01/24/2023

    STC SA00162AT

    Installation of flap gap seals

    Whelen Aerospace Technologies

  • 01/24/2023

    STC SA00073AT

    Installation of main landing gear fairings.

    Whelen Aerospace Technologies

  • 01/10/2023

    STC SA04378CH

    Installation of an engine modified per STC SE04349CH on an aircraft listed on FAA approved model list #SA04378CH dated 1/13/19 or later FAA approved revision, IAW SureFly installat…

    SureFly Partners Ltd

+ 421 more STCs on file

07 /  PMA replacement parts

FAA-approved replacement parts for NEW PIPER AIRCRAFT INC PA-34-220T

60+ parts on file from the FAA Parts Manufacturer Approval database. Each is a non-OEM part the FAA has authorized for use as a replacement on this aircraft type.

  • Drawing List 24000#https://drs.faa.gov/browse/excelExternalWindow/DC09A36DEE8A06418625818400662F87.0001##

    Nacelle Fuel Tank

    Griggs Aircraft Refinishing LLC replaces Modification Part

    PMA holder →
  • EIS-61000-T1M#https://drs.faa.gov/browse/excelExternalWindow/8FE5767734ABB04686257E2F006DF69B.0001##

    Electroair Electronic Ignition System (Kit)

    Electroair Acquisition Corporation replaces Modification Part

    PMA holder →
  • CD29115#https://drs.faa.gov/browse/excelExternalWindow/C004A0EDB12B35FF86257E1900673BEC.0001##

    Pump Assy, Fuel 12V

    C & D Associates Inc replaces Janitrol P/N 91E93-1 Piper P/Ns 481-842, 84251-02, 37167-17, 37167-23, 751872, 751799, 451872, 83744-157, 37167-23, 37167-51, 755134, 754902

    PMA holder →
  • Parts Listed in Nayak Aircraft Drawing List 24000, Revision D dated 3/19/1986, or later FAA approved revisions#https://drs.faa.gov/browse/excelExternalWindow/F5B76396D7896C53852570490056D61F.0001##

    Nacelle Fuel Tank

    O&N Aircraft Modifications Inc replaces Modification Parts

    PMA holder →
  • AK982 dtd 05-10-88 Dwg. 87A1193 dtd 05-10-88#https://drs.faa.gov/browse/excelExternalWindow/4E026DC34DA76C208625752E00744D53.0001##

    Century 2010/2030/2031 Antopi1ot

    Century Flight Systems Inc replaces Modification Part

    PMA holder →
  • Edo Avionics Model AK895#https://drs.faa.gov/browse/excelExternalWindow/318F6F126EB29E288625752E00688619.0001##

    Century 31 Autopilot

    Century Flight Systems Inc replaces -

    PMA holder →
  • Mitchell Model AK561#https://drs.faa.gov/browse/excelExternalWindow/B7E4AA8E43A61D528625752E006882BC.0001##

    Century III Autopilot

    Century Flight Systems Inc replaces -

    PMA holder →
  • Mitchell Model AK881 or AK881FD#https://drs.faa.gov/browse/excelExternalWindow/650FAA0BEAA2FF9B8625752E0065E946.0001##

    Century 41 Autopilot or Century 41 Flight Director

    Century Flight Systems Inc replaces -

    PMA holder →
  • Mitchell Model AK882#https://drs.faa.gov/browse/excelExternalWindow/0B258942821F23668625752E0065E964.0001##

    Century 21 Autopilot

    Century Flight Systems Inc replaces -

    PMA holder →
  • 201B(H)#https://drs.faa.gov/browse/excelExternalWindow/5635EAA89F8B4C6886257425006B20EB.0001##

    Transducer

    Instrument Tech Corp. replaces Modification Part

    PMA holder →
  • 201B(M)#https://drs.faa.gov/browse/excelExternalWindow/C5078A7E668D0F2E86257425006B20D4.0001##

    Transducer

    Instrument Tech Corp. replaces Modification Part

    PMA holder →
  • 201B(L)#https://drs.faa.gov/browse/excelExternalWindow/596371380B07148786257425006B20A2.0001##

    Transducer

    Instrument Tech Corp. replaces Modification Part

    PMA holder →
  • 41832AT-1#https://drs.faa.gov/browse/excelExternalWindow/A993D6C0EF1F626486257329004CC584.0001##

    Fuel Cell Assembly

    Aero-Tech Services Inc replaces 454-373, 2F1-6-41832-1

    PMA holder →
  • 201B(M)#https://drs.faa.gov/browse/excelExternalWindow/2E743B2417E1D93C862571C3006B1598.0001##

    Transducer

    Instrument Tech Corp. replaces 201B

    PMA holder →
  • 201B(L)#https://drs.faa.gov/browse/excelExternalWindow/8C1A3B8548CADCD3862571C3006B0E0B.0001##

    Transducer

    Instrument Tech Corp. replaces 201B

    PMA holder →
  • 201B(H)#https://drs.faa.gov/browse/excelExternalWindow/BB094B7ADAD34C7E862571C3006B06A4.0001##

    Transducer

    Instrument Tech Corp. replaces 201B

    PMA holder →
  • 3-1-2#https://drs.faa.gov/browse/excelExternalWindow/06D10CE7A026454886257104001D54D5.0001##

    Reinforcing Ring

    Bogert Aviation, Inc. replaces Modification Parts

    PMA holder →
  • 3-1-1#https://drs.faa.gov/browse/excelExternalWindow/B69AB50916A61AEE86257104001D4571.0001##

    Plate

    Bogert Aviation, Inc. replaces Modification Parts

    PMA holder →
  • SMR2235-3#https://drs.faa.gov/browse/excelExternalWindow/FF9C7165E2D87BB986257ECE0057B0AA.0001##

    Wire Harness

    B/E Aerospace Inc, DBA, SMR Technologies Inc replaces 4E2235-3

    PMA holder →
  • SMR2092-9#https://drs.faa.gov/browse/excelExternalWindow/720EAEFFCC88B40886257ECE0057B086.0001##

    Wire Harness

    B/E Aerospace Inc, DBA, SMR Technologies Inc replaces 3E2092-9

    PMA holder →
  • 25S-7D5036-07#https://drs.faa.gov/browse/excelExternalWindow/BA94AF7226CD3AD186257C14005BEDDC.0001##

    Wing De-Icer, LH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 553-604

    PMA holder →
  • 4E1967-1#https://drs.faa.gov/browse/excelExternalWindow/C54C194E32642EAB86257C14005BEDC8.0001##

    De-Icer Wire Harness

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 464-097

    PMA holder →
  • 3E3158-1#https://drs.faa.gov/browse/excelExternalWindow/E5FE17C01332C7DF86257C14005BEDB7.0001##

    Wire Harness

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 755-379

    PMA holder →
  • P25S-7D5036-08#https://drs.faa.gov/browse/excelExternalWindow/B360A14B6D57D41E86257C14005BEDDF.0001##

    Wing De-Icer, RH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Goodrich P/N 25S-7D5036-08

    PMA holder →
  • 3E2092-5#https://drs.faa.gov/browse/excelExternalWindow/863FBE336B96602486257C14005BEDB0.0001##

    Wire Harness Assembly

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 755-302

    PMA holder →
  • 25S-7D5036-10#https://drs.faa.gov/browse/excelExternalWindow/EB1E2D9CB2B040ED86257C14005BEDE1.0001##

    Horizontal Stabilizer De- Icer, RH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 690-901

    PMA holder →
  • 4E2235-3#https://drs.faa.gov/browse/excelExternalWindow/ED44A5BC8298135B86257C14005BEDCC.0001##

    De-Icer Wire Harness

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 755-339

    PMA holder →
  • 4E3172#https://drs.faa.gov/browse/excelExternalWindow/19A1F3F91B86EC4F86257C14005BEDCF.0001##

    Split Mounting Plate

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 690-502

    PMA holder →
  • 25S-7D5036-08#https://drs.faa.gov/browse/excelExternalWindow/45BE64E6A5C55B1C86257C14005BEDDE.0001##

    Wing De-Icer, RH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 553-603

    PMA holder →
  • 3E2062-2#https://drs.faa.gov/browse/excelExternalWindow/598E3980FE7ED33786257C14005BEDAE.0001##

    Modulator Brush Block Assembly

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 758-462

    PMA holder →
  • P25S-7D5036-07#https://drs.faa.gov/browse/excelExternalWindow/1CD39FFAF193D22186257C14005BEDDD.0001##

    Wing De-Icer, LH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Goodrich P/N 25S-7D5036-07

    PMA holder →
  • 25S-7D5036-09#https://drs.faa.gov/browse/excelExternalWindow/36DF5156CB64DFF986257C14005BEDE0.0001##

    Horizontal Stabilizer De- Icer, LH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 690-900

    PMA holder →
  • 4E3177#https://drs.faa.gov/browse/excelExternalWindow/46DD64AB215055FD86257C14005BEDD0.0001##

    Slip Ring/ Sleeve Assembly

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 767-237

    PMA holder →
  • 4E2058#https://drs.faa.gov/browse/excelExternalWindow/1C8430E4761E637186257C14005BEDC9.0001##

    Mounting Plate

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 475-177

    PMA holder →
  • 3E2092-5#https://drs.faa.gov/browse/excelExternalWindow/F0D9410C5D12252A86257A990064D7B3.0001##

    Wire Harness Assembly

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 755-302

    PMA holder →
  • 4E3177#https://drs.faa.gov/browse/excelExternalWindow/FB49526BEEC9DAB786257A990064D7DC.0001##

    Slip Ring/ Sleeve Assembly

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 767-237

    PMA holder →
  • 4E2058#https://drs.faa.gov/browse/excelExternalWindow/C9C2610986D8BFCF86257A990064D7D3.0001##

    Mounting Plate

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 475-177

    PMA holder →
  • 3E3158-1#https://drs.faa.gov/browse/excelExternalWindow/C51BDB321317070986257A990064D7BE.0001##

    Wire Harness

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 755-379

    PMA holder →
  • 4E1967-1#https://drs.faa.gov/browse/excelExternalWindow/A952B4CA750A50F386257A990064D7D1.0001##

    De-Icer Wire Harness

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 464-097

    PMA holder →
  • 25S-7D5036-10#https://drs.faa.gov/browse/excelExternalWindow/9375E2D785DC536E86257A990064D7EF.0001##

    Horizontal Stabilator De- Icer, RH

    UTC Aerospace Systems, Goodrich Sensors & Integrated Systems replaces Piper P/N 690-901

    PMA holder →

+ 20 more PMA parts on file

09 /  Equivalent Level of Safety findings

ELOS findings issued for NEW PIPER AIRCRAFT INC PA-34-220T

1 ELOS finding on file. The FAA issues an ELOS when an applicant proposes an alternative means that achieves the same safety outcome as a literal regulation — a standing record of which certification deviations the agency has approved for this model series.

05 /  Aircraft of this type

All 8 registered N-numbers

Every tail currently on the FAA registry for this make/model. Click an N-number to query the FAA Aircraft Inquiry; rows flagged have NTSB events on file. Tails seeded with full TallyAero pages link directly.

8 of 8
N-number St Year NTSB FAA
N301SE FL 2004 · Look up ↗
N343HP DE 2003 · Look up ↗
N480ND FL · Look up ↗
N514BC FL · Look up ↗
N561JT DE 1999 · Look up ↗
N621LG DE 2002 · Look up ↗
N827DB FL 2003 · Look up ↗
N994BD AL 2004 · Look up ↗

Source — FAA Aircraft Registry · click "Look up" to query the live registry record (owner, address, last airworthiness)

05 /  Sources & Methodology

Every count traces back to a primary US-government source

We render counts and lists as the agency publishes them. Read the methodology →