# New Piper PA-34-220T

- Type: Aircraft model (FAA registry)
- Registry code: 7103202
- Manufacturer (registry): NEW PIPER AIRCRAFT INC
- Model: PA-34-220T
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 7
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A7SO](https://openairdocs.org/tcds/A7SO) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 8
- Page: https://openairdocs.org/model/new-piper-pa-34-220t

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2024-10-04](https://openairdocs.org/ad/2024-10-04): Wing, Attach Fittings · Piper PA-28-181, PA-28R-201, PA-44-180 and 1 more. Effective Jun 6, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2020-24-09](https://openairdocs.org/ad/2020-24-09): Flight Controls · Piper PA-34-220T. Effective Jan 5, 2021
- [AD 2013-02-13](https://openairdocs.org/ad/2013-02-13): Stabilizer Control System · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Mar 11, 2013
- [AD 2010-15-10](https://openairdocs.org/ad/2010-15-10): Control wheel shafts · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Aug 31, 2010
- [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2005-15-10](https://openairdocs.org/ad/2005-15-10): Combustion heater fuel pumps · Piper PA-34-200T, PA-34-220T, PA-44-180 and 1 more. Effective Aug 26, 2005
- [AD 2005-13-16](https://openairdocs.org/ad/2005-13-16): Nose landing gear (NLG) · Piper PA-34-200, PA-34-200T and PA-34-220T. Effective Aug 8, 2005
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004
- [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 2001
- [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [AD 99-14-01](https://openairdocs.org/ad/99-14-01): AFM - Limitations Section - Icing · Piper PA-23, PA-23-160, PA-23-235 and 21 more. Effective Aug 17, 1999
- [AD 99-05-09](https://openairdocs.org/ad/99-05-09): Induction Air Filter · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 20 more. Effective Mar 19, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 96-10-03](https://openairdocs.org/ad/96-10-03): Flap Handle Attach Bolt · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jun 14, 1996
- [AD 94-13-11](https://openairdocs.org/ad/94-13-11): Main Landing Gear Trunnion · Piper PA-34-200, PA-34-200T, PA-34-220T and 2 more. Effective Aug 12, 1994
- [AD 92-08-04](https://openairdocs.org/ad/92-08-04): Rudder System · Piper PA-34-200, PA-34-200T and PA-34-220T. Effective May 15, 1992
- [AD 88-04-05](https://openairdocs.org/ad/88-04-05): Baggage Compartment Door · Piper PA-34-200, PA-34-200T and PA-34-220T. Effective Feb 16, 1988
- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986
- [AD 82-04-08](https://openairdocs.org/ad/82-04-08): Landing Gear Retraction · Piper PA-34-220T. Effective Feb 25, 1982

Historical (superseded or no longer in force):

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2003-11-14](https://openairdocs.org/ad/2003-11-14) (historical): Combustion heater fuel pump · Piper PA-34-200T, PA-34-220T, PA-44-180 and 1 more. Effective Jun 20, 2003

## Information bulletins (advisory) (16)

- [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015
- [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014
- [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011
- [SAIB CE-11-14](https://openairdocs.org/saib/CE-11-14): Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-13](https://openairdocs.org/saib/CE-11-13): Wings - Piper PA-28, PA-32, PA-34 Forward Spar Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-12](https://openairdocs.org/saib/CE-11-12) (historical): PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Jan 5, 2011
- [SAIB CE-11-11](https://openairdocs.org/saib/CE-11-11): Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-10](https://openairdocs.org/saib/CE-11-10): Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and Ribs. Issued Jan 5, 2011
- [SAIB CE-11-01](https://openairdocs.org/saib/CE-11-01): Stabilizers -Horizontal Stabilator   Turnbuckle. Issued Oct 4, 2010
- [SAIB CE-09-23](https://openairdocs.org/saib/CE-09-23): Fuel: Piper PA-28, PA-32, PA-34. Issued Apr 7, 2009
- [SAIB CE-09-15](https://openairdocs.org/saib/CE-09-15): Landing Gear - Nose Gear Centering Attach Bolt. Issued Mar 2, 2009
- [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006
- [SAIB CE-04-89](https://openairdocs.org/saib/CE-04-89): . Issued Sep 17, 2004
- [SAIB CE-01-30](https://openairdocs.org/saib/CE-01-30): . Issued Jul 11, 2001

## Registered aircraft (8)

- [N301SE](https://openairdocs.org/aircraft/N301SE): [American Air Academy Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIR%20ACADEMY%20INC), [Merritt Island, FL](https://openairdocs.org/faa-place/FL/Merritt%20Island), built 2004, S/N 3449304
- [N343HP](https://openairdocs.org/aircraft/N343HP): [Monada Air Inc Trustee](https://openairdocs.org/faa-owner/MONADA%20AIR%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2003, S/N 3449281
- [N480ND](https://openairdocs.org/aircraft/N480ND): [Island Jet Co](https://openairdocs.org/faa-owner/ISLAND%20JET%20CO), [Merritt Island, FL](https://openairdocs.org/faa-place/FL/Merritt%20Island), S/N 3449306
- [N514BC](https://openairdocs.org/aircraft/N514BC): [Carlton Bradford Robert](https://openairdocs.org/faa-owner/CARLTON%20BRADFORD%20ROBERT), [Cape Coral, FL](https://openairdocs.org/faa-place/FL/Cape%20Coral), S/N 3449308
- [N561JT](https://openairdocs.org/aircraft/N561JT): [Squires Seneca LLC](https://openairdocs.org/faa-owner/SQUIRES%20SENECA%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1999, S/N 3449136
- [N621LG](https://openairdocs.org/aircraft/N621LG): [Adams Aviation Services Inc Trustee](https://openairdocs.org/faa-owner/ADAMS%20AVIATION%20SERVICES%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2002, S/N 3449296
- [N827DB](https://openairdocs.org/aircraft/N827DB): [High Sky Aviation Inc](https://openairdocs.org/faa-owner/HIGH%20SKY%20AVIATION%20INC), [Wauchula, FL](https://openairdocs.org/faa-place/FL/Wauchula), built 2003, S/N 3449276
- [N994BD](https://openairdocs.org/aircraft/N994BD): [Impatient & Paranoid LLC](https://openairdocs.org/faa-owner/IMPATIENT%20%26%20PARANOID%20LLC), [Birmingham, AL](https://openairdocs.org/faa-place/AL/Birmingham), built 2004, S/N 3449310

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20231126022059I](https://openairdocs.org/incident/20231126022059I), Nov 26, 2023: New Piper Aircraft Inc PA-34-220T (N514BC), Punta Gorda, FL, Minor damage. Pilot failed to lower the gear handle prior to landing. Gear warning horn failed to alert the pilot.
- [Accident 19950529039049A](https://openairdocs.org/incident/19950529039049A), May 29, 1995: Piper J3C65 (N31328), Greenville, SC, Destroyed, 1 fatal. CFI took over on second touch and go. Began go around. Made steep turn on climbout. Stalled crashed and burned.

## Service difficulty reports (297, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2024FA0000239](https://openairdocs.org/sdr/2024FA0000239), Mar 15, 2024: TIRE. FAILED. PILOT REPORTED ON LANDING THAT HE FELT THE AIRCRAFT YAWING TO THE RIGHT AND REALIZED HE HAD A FLAT TIRE. AIRPORT USED A SET OF DOLLIES TO MOVE THE AIRCRAFT BACK
- [SDR 2023FA0000617](https://openairdocs.org/sdr/2023FA0000617), Apr 25, 2023: FORK. CRACKED. DURING ANNUAL INSPECTION, CRACKES WERE FOUND IN THE UPPER 2 BOLT HOLES OF THE FORK ON THE MLG STRUT ASSEMBLIES. LT AND RT MLG. CRACKS MAY BE STRESS PLACED ON TH
- [SDR 8HBR20230415051](https://openairdocs.org/sdr/8HBR20230415051), Apr 15, 2023: BOLT. MISMANUFACTURED. BOLT, PIPER P/N 402-921 QUANTITY OF 8 WERE ORDERED FROM BOEING, 4 OF THE 8 DID NOT HAVE THE HOLE DRILLED THROUGH THE THREADS FOR THE COTTER PIN. PIPER TAGS ON B
- [SDR 2022FA0000739](https://openairdocs.org/sdr/2022FA0000739), Dec 5, 2022: MAGNETO. FAILED. MISFIRE FROM ENGINE IN FLIGHT, AND 200+ RPM DROP ON MAGNETO CHECK AFTER LANDING APPROXIMATELY 120 HOURS SMOH ON ENGINE, TSIO-360-RB2 CONTINENTAL. NORMAL MAGNETO
- [SDR 2021FA0000101](https://openairdocs.org/sdr/2021FA0000101), Apr 12, 2021: ROD END. SHEARED. FAILURE OF THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY, CAUSING A NOSE LANDING GEAR COLLAPSE, AND A DUAL ENGINE PROPELLER STRIKE. THE NOSE GEAR DOWN-LOCK LINK ASSEMBL
- [SDR IKBR2020410101](https://openairdocs.org/sdr/IKBR2020410101), Apr 9, 2020: PITOT LINE. BROKEN. AIRCRAFT WAS DEPARTING AFTER ANNUAL AND AIRSPEED WAS NOT SEEN AND TAKEOFF WAS ABORTED AFTER VERY HEAVY BRAKING AND RUNNING OFF THE END OF THE RUNWAY THE LEFT TI
- [SDR YBBA201908280001](https://openairdocs.org/sdr/YBBA201908280001), Aug 27, 2019: WARNING LIGHT. INOPERATIVE. PIC REPORTS NOSE GEAR INDICATION INOP DURING GEAR DOWN CYCLE, CYCLED GEAR 3 TIMES AND CONFIRMED GEAR DOWN WITH ATC ACKNOWLEDGEMENT DURING FLY BY, AFTER CYCLING 
- [SDR CA190530009](https://openairdocs.org/sdr/CA190530009), May 23, 2019: PROBE. MALFUNCTIONED. (CAN) ON JANUARY 24, 2019 THE LEFT HAND ENGINE CHT SHOWED AN OVER TEMP INDICATION AND ACTIVATED THE MASTER CAUTION. THE CHT WAS REPLACED WITH A NEW UNIT AT 2738
- [SDR 2018FA0000257](https://openairdocs.org/sdr/2018FA0000257), Apr 19, 2018: PUMP. INOPERATIVE. REMOVED HEATER FUEL PUMP, P1-91E92-1, SN A97070063. PUMP INOPERATIVE.
- [SDR XKBA201708180002](https://openairdocs.org/sdr/XKBA201708180002), Aug 16, 2017: STARTER. INOPERATIVE. STARTER MOTOR FAILED AFTER LONG PERIOD OF CRANKING. REPLACED STARTER WITH OVERHAULED.
- [SDR XKBA20170818001](https://openairdocs.org/sdr/XKBA20170818001), Aug 16, 2017: PUMP. INOPERATIVE. ELECTRIC FUEL PUMP INOPERATIVE WHEN TRYING TO START THE AIRCRAFT. INSTALLED A NEW OVERHAULED PUMP.
- [SDR XKBA201706280001](https://openairdocs.org/sdr/XKBA201706280001), Jun 28, 2017: CONTROL CABLE. OUT OF ADJUST. LEFT PROPELLER WOULDN'T FEATHER DURING TRAINING. ADJUSTED THE TRAVEL ON THE GOVERNOR CONTROL AND PROP OPERATED NORMALLY AFTER ADJUSTMENT.
- [SDR 2017FA0000143](https://openairdocs.org/sdr/2017FA0000143), Mar 24, 2017: TORQUE TUBE. OUT OF POSITION. DURING INSPECTION OF THE AIRPLANE, AFTER REPAIR, DISCOVER THAT THE BOLT WAS DAMAGED RIGHT CHANNEL TUNNEL AGAIN. AFTER ISSUE ANALYSIS AT THE AIRPLANE, DISCOVER T
- [SDR XKBA201703290001](https://openairdocs.org/sdr/XKBA201703290001), Mar 3, 2017: SKIN. CRACKED. FOUND SMALL CRACK IN LEFT FLAP SKIN LOWER INBOARD END. INSTALLED NEW FLAP SKIN.
- [SDR 2016FA0000554](https://openairdocs.org/sdr/2016FA0000554), Nov 4, 2016: BOLT. NOT REPORTED.  DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, IND
- [SDR 2015FA0000168](https://openairdocs.org/sdr/2015FA0000168), Apr 29, 2015: BEARING. LOOSE. DURING ANNUAL INSPECTION IT WAS NOTED THAT PRESSED IN BEARING WAS LOOSE IN LOWER DRAG LINK AND ONLY THING HOLDING BEARING IN WAS THE WASHER UNDER THE BOLT HEAD
- [SDR 2013FA0000094](https://openairdocs.org/sdr/2013FA0000094), Feb 2, 2013: CAP. DEPARTED. FUEL CAP ON THE WING INCORRECTLY INSTALLED AFTER REFUELING, FUEL CAP EVENTUALLY DEPARTED THE ACFT INFLIGHT. CAP WAS CHECKED DURING THE PREFLIGHT, AFTER REFUELIN
- [SDR 2012FA0000717](https://openairdocs.org/sdr/2012FA0000717), Oct 12, 2012: CONTACTOR. CORRODED. AFTER ACFT WAS EXPOSED TO HEAVY RAIN. BATTERY WENT DEAD. GPU START NORMAL AND FLIGHT NORMAL. AT SHUTDOWN TURNING MASTER SWITCH OFF, DID NOT TURN POWER OFF. FOUN
- [SDR 2012FA0000310](https://openairdocs.org/sdr/2012FA0000310), May 11, 2012: CONTROL CABLE. FRAYED. FOUND LOWER ELEVATOR CABLE FRAYED WHERE IT RIDES ON A PHENOLIC BLOCK AT FS222.43.
- [SDR CA120221012](https://openairdocs.org/sdr/CA120221012), Nov 25, 2011: LANDING GEAR. COLLAPSED. (CAN) RT LANDING GEAR SELECTED DOWN, NO INDICATION OF RT GEAR LOCKED. AIRCRAFT LANDED AND RT GEAR COLLAPSED AT SLOW SPEED.
- [SDR CA110916004](https://openairdocs.org/sdr/CA110916004), Sep 15, 2011: POTENTIOMETER. BURNED. (CAN) ON CLIMB OUT CREW DETECTED A SMOKE/BURNING - SHORTLY AFTER CABIN FILLED WITH SMOKE. ACFT SHUT ELECTRIAL POWER OFF, SQUAWKED EMERGENCY ON TRANSPONDER AND L
- [SDR CA110805004](https://openairdocs.org/sdr/CA110805004), Aug 4, 2011: CABLE. FRAYED. ON INSP, FOUND A FRAYED ELEVATOR TRIM CABLE.
- [SDR CA100804020](https://openairdocs.org/sdr/CA100804020), Jun 10, 2010: SELECTOR SWITCH. BROKEN. WHEN MOVING THE GEAR SELECTOR SWITCH TO THE GEAR UP POSITION FOLLOWING TAKEOFF, THE GEAR SELECTOR SWITCH PHYSICALLY BROKE OFF AT THE STEM, BETWEEN THE SWITCHES 
- [SDR 2010FA0000705](https://openairdocs.org/sdr/2010FA0000705), Jun 9, 2010: CONTROL CABLE. BROKEN. STABILATOR CONTROL CABLE, PN62701-129, FAILED IN FLIGHT. THE CABLE SEPARATED ON LANDING. THE PILOT WAS UNABLE TO FLARE RESULTING IN A HARD LANDING IN A NOSE LOW
- [SDR 2009FA0000463](https://openairdocs.org/sdr/2009FA0000463), May 1, 2009: CRANKSHAFT. CRACKED. DURING ANNUAL INSP, OIL WAS FOUND AT FRONT OF ENGINE. FURTHER INVESTIGATION REVEALED A CRACK OF THE CRANKSHAFT AT THE PROP MOUNTING FLANGE. CAUSE HAS NOT BEEN D
- [SDR 2009F00027](https://openairdocs.org/sdr/2009F00027), Apr 14, 2009: CABLE. DAMAGED. FAILURE OCCURRED WITH THE AUTOPILOT ROLL SERVO BRIDLE CABLE. THE BRIDLE CABLE APPARENTLY JUMPED AND OVERLAPPED ITSELF ON THE SERVO SPOOL, EFFECTIVELY JAMMING TH
- [SDR 2009FA0000257](https://openairdocs.org/sdr/2009FA0000257), Mar 25, 2009: ENGINE. DAMAGED. PILOT REPORTED THAT THE RT ENGINE LOST OIL PRESSURE AND RPMS. NO N1 INDICATION. ENGINE WAS SHUT DOWN AND ACFT RETURNED TO DEPARTURE.
- [SDR 2009FA0000253](https://openairdocs.org/sdr/2009FA0000253), Mar 19, 2009: LINE. CHAFED. WHILE COMING IN FOR A LANDING, CUSTOMER WENT TO EXTEND LANDING GEAR AND GEAR WOULD NOT EXTEND. USED EMERGENCY GEAR EXTENSION AND LANDED ACFT WITH NO INCIDENT. U
- [SDR 2009FA0000053](https://openairdocs.org/sdr/2009FA0000053), Jan 26, 2009: POINTS. LOOSE. POINTS WERE FOUND NOT MAKING CONTACT, UPON FURTHER EXAMINATION, FOUND THE STATIONARY CONTACT LOOSE IN MAG. IT SEEMED TO HAVE COME OFF THE END, THE CONTACT DISK 
- [SDR 2008FA0000004](https://openairdocs.org/sdr/2008FA0000004), Jan 2, 2008: STRUT. CRACKED. DURING ANNUAL INSPECTION, IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSEMBLY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION O
- [SDR 2008FA0000003](https://openairdocs.org/sdr/2008FA0000003), Jan 2, 2008: STRUT. CRACKED. DURING ANNUAL INSPECTION IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION OF THE
- [SDR 2007FA0001074](https://openairdocs.org/sdr/2007FA0001074), Nov 30, 2007: CONTROL SYSTEM. SEIZED. WITH FULL RT RUDDER TRIM, RT RUDDER FOR HARD CLIMBING RT TURN, RUDDER FROZE WITH FULL RT DEFLECTION. RUDDER CABLE TURNBUCKLE IN TAIL SECTION WAS (CAUGHT) UNDER 
- [SDR 2007FA0000942](https://openairdocs.org/sdr/2007FA0000942), Sep 21, 2007: LANDING GEAR. COLLAPSED. AIRCRAFT TAXIED TO RUNWAY AFTER LOADING CARGO. AFTER NORMAL RUNUP, THE PILOT TAXIED ONTO THE RUNWAY AND STOPPED. THE PILOT ADVANCED THROTTLES AND RELEASED BRAKE
- [SDR 2007FA0000729](https://openairdocs.org/sdr/2007FA0000729), Aug 3, 2007: BUSHING. MISINSTALLED. DURING THE PROCESS OF INSPECTING (6 EA) CONNECTING RODS IAW SB 07-1 AND SB 00-3, IT WAS FOUND THAT ALL WRIST PIN BUSHINGS WERE INSTALLED NOT IAW THEIR POSITIONS
- [SDR 2007FA0000292](https://openairdocs.org/sdr/2007FA0000292), Apr 2, 2007: FLOOR PANEL. DEBONDED. FLOORPANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.
- [SDR 2007FA0000291](https://openairdocs.org/sdr/2007FA0000291), Apr 2, 2007: FLOOR PANEL. DEBONDED. FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (
- [SDR 2007FA0000290](https://openairdocs.org/sdr/2007FA0000290), Apr 2, 2007: FLOOR PANEL. DEBONDED. FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (
- [SDR 2007FA0000289](https://openairdocs.org/sdr/2007FA0000289), Apr 2, 2007: FLOOR PANEL. DEBONDED. FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (
- [SDR 2007FA0000288](https://openairdocs.org/sdr/2007FA0000288), Apr 2, 2007: FLOOR PANEL. DEBONDED. FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (
- [SDR 2007FA0000085](https://openairdocs.org/sdr/2007FA0000085), Jan 17, 2007: COUPLING. FAILED. ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATOR, IN IMC SIMULTANEOUSLY. COUPLING FAILURE RESULTED IN TOTAL ELECTRICAL FAILURE, RT ENGINE.
- [SDR 2007FA0000077](https://openairdocs.org/sdr/2007FA0000077), Jan 17, 2007: COUPLING. FAILED. ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, C
- [SDR 2007FA0000076](https://openairdocs.org/sdr/2007FA0000076), Jan 17, 2007: COUPLING. FAILED. ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, C
- [SDR 2006FA0000571](https://openairdocs.org/sdr/2006FA0000571), May 31, 2006: POINTS. FAILED. THE POINTS WHICH ONLY HAD A TOTAL OF 9.3 HR, HAD THE PLASTIC PORTION WHICH RIDES THE CAM, MELT ON THE METAL OF THE POINTS WHICH REDUCED THE GAP TO CAUSE MISFIRE
- [SDR 2006FA0000717](https://openairdocs.org/sdr/2006FA0000717), Mar 11, 2006: RIB. CRACKED. DURING COMPLIANCE WITH SB, LT AND RT RIBS FOUND CRACKED AS SUSPECTED. INSTALLED REPAIR KITS. LT DRAG BRACE PIVOT, PN 39479002, ALSO FOUND CORRODED AND CRACKED. 
- [SDR 2006FA0000372](https://openairdocs.org/sdr/2006FA0000372), Mar 9, 2006: AXLE. CRACKED. CRACKS IN BOTH UPPER BOLT HOLES THAT SECURE AXLE TO STRUT ASSEMBLY ON BOTH LT AND RT MLG. PROBABLE CAUSE MAYBE HARD LANDING OR FATIGUE CRACKS DO TO NORMAL USE. 
- [SDR CA070207006](https://openairdocs.org/sdr/CA070207006), Jan 20, 2006: TRUNNION. FAILED. (CAN) NOSE GEAR TRUNNION DAMAGED AND REPAIRED. (TC NR 20070207006)
- [SDR 43881](https://openairdocs.org/sdr/43881), Dec 13, 2005: FUEL LINE. CHAFED. THE FUEL INJECTOR LINE FROM THE FLOW DIVIDER TO THE NR3 CYLINDER ON THE RT ENGINE WAS ROUTED UNDER A COWL LATCH FOR THE COWLING NOSE BOWL WHICH CAUSED SEVER CHA
- [SDR AU510002142](https://openairdocs.org/sdr/AU510002142), Dec 12, 2005: PUMP. CONTAMINATED. LT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.
- [SDR AU510002141](https://openairdocs.org/sdr/AU510002141), Dec 12, 2005: PUMP. CONTAMINATED. RT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.
- [SDR AU510002140](https://openairdocs.org/sdr/AU510002140), Dec 12, 2005: PUMP. CONTAMINATED. LT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.

All 297: https://openairdocs.org/model/new-piper-pa-34-220t/reports.md

## STCs that may be installed (OpenAirDocs) (246, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists PA-34 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA02798SE](https://openairdocs.org/stc/SA02798SE): Installation of Absolute Solutions LLC Gear Warning System Upgrade. Absolute Solutions LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/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
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00073AT](https://openairdocs.org/stc/SA00073AT): Installation of main landing gear fairings. Whelen Aerospace Technologies
- [STC SA00162AT](https://openairdocs.org/stc/SA00162AT): Installation of flap gap seals. Whelen Aerospace Technologies
- [STC SA00163AT](https://openairdocs.org/stc/SA00163AT): Installation of "Speed Splitter" flap bracket fairings. Whelen Aerospace Technologies
- [STC SA01038AT](https://openairdocs.org/stc/SA01038AT): Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28, -28R, -32, -32R, -34 series MODELS WITH CONSTANT-CHORD WINGS). Whelen Aerospace Technologies. Lists PA-34 Series
- [STC SA01206AT](https://openairdocs.org/stc/SA01206AT): Installation of a cowling nose bowl. Whelen Aerospace Technologies
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA01875WI](https://openairdocs.org/stc/SA01875WI): BasicMed 6-Place Occupancy Restriction. Aeronautix LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA04195NY](https://openairdocs.org/stc/SA04195NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System (FCS) upgraded from KFC 200 FCS. Honeywell International Inc. (Bendix King)
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA02384CH](https://openairdocs.org/stc/SA02384CH): Installation of Flight Boss LTD SPA-32/34 Series Organizers. Flight Boss Ltd
- [STC SA04181NY](https://openairdocs.org/stc/SA04181NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System. Honeywell International Inc
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA4234WE](https://openairdocs.org/stc/SA4234WE): Installation of inflatable door seal. TALCO Aviation Corp
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA1310SW](https://openairdocs.org/stc/SA1310SW): Installation of stretcher in lieu of rear seats. Aviation Fabricators Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA00666WI-D](https://openairdocs.org/stc/SA00666WI-D): Installation of Bendix/King KFC 225 automatic flight control system. Honeywell International Inc
- [STC SA1147CE](https://openairdocs.org/stc/SA1147CE): Installation of King Model KFC 200 2 axis (3 optional) flight control system, autopilot only or autopilot with flight director. Honeywell International Inc

All 246: https://openairdocs.org/model/new-piper-pa-34-220t/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120510874920260723131534.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [LM29749-20629](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111891980420260705233749.0001): Cone. Timken Corporation · PMA PQ4105CE · Replaces 214-01400, LM29749, 753 448, 753-448 · Jun 4, 2026
- [RAP164-21600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132311683620260722154733.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-21600 · Jun 3, 2026
- [RAP164-02300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131469465520260722154717.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-02300 · Jun 3, 2026
- [SSV35-231765-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142043761020260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-334, 452-357, M34-14, M34-14M · May 4, 2026
- [SSV35-231765-1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132699716920260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 131765-1F, 452-335, F34-14, F34-14… · May 4, 2026
- [AS-GHBA-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121296658520260508190540.0001): Gear Horn and Bracket Assembly. Absolute Solutions LLC · PMA PQ05464NM · Modification part · May 4, 2026
- [SSV35-231765-L1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104549240720260713144520.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-336, FL34-14 · May 4, 2026
- [MC9812-0023-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195858733620250929141436.0001): Fuel Level Sender. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces PS10013-5, 550-503, 7740‑00040 · Sep 5, 2025
- [MDL RR1-2-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188380771120250311133057.0001): Alternate Avionic SupportStrut Assemblies. Radiorax Aviation Systems LLC · PMA PQ00040WB · Modification part · Jan 17, 2025
- [AF37189-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172904918720250106200858.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Dec 18, 2024
- [AF37178-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165005724620250106200858.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Dec 18, 2024
- [AF37126-008](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163464623220250106200857.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Dec 18, 2024
- [W-2809-RH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153118358820241230193839.0001): Piper PA-34-220T Late Wingtip Lens Cover (Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 36761-035 · Dec 18, 2024
- [AF37175-034](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151619076320250106200857.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Dec 18, 2024
- [W-2809-LH](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101015161220241230193838.0001): Piper PA-34-220T Late Wingtip Lens Cover (Left). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 36761-034 · Dec 18, 2024
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187312814920250417183925.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [A81842](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123113391920240501210149.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces 48184240007 · Apr 23, 2024
- [AF37120-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144895742620240610151340.0001): LH Rear Baffle Assembly (LH & RH Engine). Airforms LLC · PMA PQ2644CE · Replaces 37120-05 · Apr 18, 2024
- [AF37178-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133341647220240610151341.0001): Rear Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 37178-03 · Apr 18, 2024
- [AF37175-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132269245420240610151341.0001): RH Rear Baffle Assembly (LH & RH Engine). Airforms LLC · PMA PQ2644CE · Replaces 37175-05 · Apr 18, 2024
- [110HS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193059656020240221142908.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110H-4 · Jan 30, 2024
- [110SS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184612663120240221142904.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110 · Jan 30, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185775606020240221143428.0001): SkyView HDX Instrumentation and Autiopilot. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [90D39-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165136830320250729170755.0001): Heater Blower. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 90D39-1,452-955 · Jan 8, 2024
- [90D39-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122765715020250729170755.0001): Heater Blower. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 90D39-2,689-941 · Jan 8, 2024
- [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194359759020240221143039.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023
- [PM-175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184450210620260625151412.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 21, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195191485020231121213733.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183755207820231121213755.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178767051320231121213639.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172207506620231121213726.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160696609120231121213630.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145728637520231121213720.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142853543720231121213741.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140840702720231121213748.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139193991320231121213713.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139166150120231121213656.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129029611820231121213614.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119907555720231121213704.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116084500820231121213647.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114247538020231121213622.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108716278720231121213802.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168735715720231108124804.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [A80564](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172675386920240730171257.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Griggs Aircraft Refinishing, LLC… · Oct 26, 2023
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102488499820231102131426.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Sep 25, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [90D39-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163030537120220916110238.0001): Combustion Air Blower Assy. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Piper 452-955 · Aug 24, 2022
- [90D39-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156827712620220916110238.0001): Combustion Air Blower Assy. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Piper 689-941 · Aug 24, 2022
- [A23D04-7.5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126088705220220916110239.0001): Fuel Regulator and Shutoff Valve. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Piper 461-731 · Aug 24, 2022

All of them: https://openairdocs.org/model/new-piper-pa-34-220t/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Piper PA-34-220T](https://openairdocs.org/model/piper-pa-34-220t): 235 registered aircraft, registry code 7103420
- [Piper PA-34-220T](https://openairdocs.org/model/piper-pa-34-220t): 13 registered aircraft, registry code 7103223

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.