# N354MC: 2026 Piper PA-46-701TP

- Status: Valid registration (dealer)
- Airframe: [Piper PA-46-701TP](https://openairdocs.org/model/piper-pa-46-701tp) (registry code 7107573, 6 seats)
- Engine: [Pratt & Whitney Canada PT6A-52](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-52) (registry code 52200)
- Data sheets: [TCDS A25SO](https://openairdocs.org/tcds/A25SO) (Piper Aircraft Inc.), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 46020124
- Year built: 2026
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 7, 2026
- Mode S code: A3F4BF
- Registered owner: [Piper Aircraft Inc](https://openairdocs.org/faa-owner/PIPER%20AIRCRAFT%20INC)
- Location: [Vero Beach, FL](https://openairdocs.org/faa-place/FL/Vero%20Beach)
- Owner type: Non-citizen corporation
- Owner's area on the map: 27.6407° N, 80.4036° W: Placed by OpenAirDocs at the center of ZIP code 32960, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=354MC
- Page: https://openairdocs.org/aircraft/N354MC

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Piper PA-46-701TP)

None in force.

### Matched by engine (Pratt & Whitney Canada PT6A-52)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N354MC.

## FAA accident and incident reports

None matched to N354MC.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N354MC not matched to an aircraft (17)

They name N354MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 0913200602](https://openairdocs.org/sdr/0913200602), Sep 13, 2006: FAN. FAILED. ENCOUNTER SMOKE IN THE COCKPIT AT CRUISE FLIGHT LEVEL 330. PERFORMED PROCEDURES IAW AOM VOL 1. UNSCHEDULE LANDNG. FINDINGS AFTER LANDING. MAINTENANCE FOUND UNSE
- [SDR 0726200601](https://openairdocs.org/sdr/0726200601), Jul 26, 2006: HYDRAULIC LINE. LEAKING. ON LANDING (ELLX) SUFFERED COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM. PERFORMED AFTER LANDING, LOSS OF HYD AND SHUTDOWN CHECKLIST. AT SAFE TAXI SPEED CLEARED RUNWA
- [SDR 0609200601](https://openairdocs.org/sdr/0609200601), Jun 8, 2006: CONTROL UNIT. FAILED. APPROXIMATELY ONE HOUR AFTER DEPARTURE FROM ELIX, NR 3 HYD SYSTEM LOSS. AS PER CHECK SHEET NR 3 EDP TO -SUPPLY OFF-, NR 3 ENGINE RUNNING. RETURN TO ELIX, NO FUR
- [SDR 0820200501](https://openairdocs.org/sdr/0820200501), Aug 28, 2005: ENGINE. LEAKING. ABOUT (1) HR AFTER DEPARTURE FROM (ORD), AT CRUISE FLT, NR 3 ENGINE LOSS OIL QTY AND OIL PRESSURE (TO ZERO) ACCOMPANIED BY ENGINE OIL PRESSURE NR 3 LIGHT. ACCOM
- [SDR P5CA0401060](https://openairdocs.org/sdr/P5CA0401060), Mar 17, 2004: INDICATOR. FAILED. STANDBY ATTITUDE INDICATOR ROLLS 10 DEG RIGHT AND LEFT IN LEVEL FLIGHT. REMOVED AND REPLACED STBY AI, PERFORMED CHECK PER 34-24-00. SYSTEM OPS CHECKS NORMAL.
- [SDR P5CA0301003](https://openairdocs.org/sdr/P5CA0301003), Dec 7, 2003: CSD. LEAKING. NR 4 ENGINE CSD LIGHT ON. CSD DISCONNECTED. TRANSFERRED TO DMI 31912 PER MEL 24-1 1A CSD AND GENERAL REMOVED PER MM 24-11-00.
- [SDR P5CA0300996](https://openairdocs.org/sdr/P5CA0300996), Nov 28, 2003: SLIDE. DEPLOYED. WHILE ATTEMPTING TO INSERT SAFETY PIN IN SLIDE, FOR SLIDE TIME CHANGE, SLIDE INADVERTENTLY DEPLOYED INSIDE A/C. SLIDE MANUALLY DEFLATED/REPLACED WITH SERVICEABL
- [SDR P5CA0300984](https://openairdocs.org/sdr/P5CA0300984), Nov 9, 2003: STRIP. WORN. NR 1 ENG FAN STATOR ASSY ABRADALE STRIP DAMAGE AT 4 TO 5 O'CLOCK POS. ENG CHANGE REPLACEMENT REQ'D PER ATLAS AIR FORM 01-AA-45. ACCOMPLISH PYLON INSP PER CF6-50
- [SDR P5CA0300954](https://openairdocs.org/sdr/P5CA0300954), Sep 24, 2003: ENGINE. MALFUNCTIONED. ON START UP NO (N1) INDICATION ON NR 1 ENG RESET C/13 NO HELP. DEFERRED NR 1 ENG (N1) IAW MEL 77-1-2.
- [SDR P5CA0300913](https://openairdocs.org/sdr/P5CA0300913), Aug 17, 2003: DRIVE SYSTEM. INOPERATIVE. NR 1 AND NR 2 RADAR ANT FAULT WX RADAR INOPERATIVE. REMOVED AND REPLACED WX RADAR ANTENNA DRIVE IAW MM 34-43-03. OPS CK AND FUCTION TEST SAT IS IAW MM 34-43-00.
- [SDR P5CA0300890](https://openairdocs.org/sdr/P5CA0300890), Jun 18, 2003: ANTENNA. FAULTY. RADAR SYS 1 & 2 ANT FAULT ON BOTH SCREENS INTERMITENT IN BOTH TEST & WX MODE, RETURNED TO GATE. WEATHER RADAR FAIL. REPLACED WEATHER RADAR ANTENNA. UNKNOWN WEAT
- [SDR P5CA0300716](https://openairdocs.org/sdr/P5CA0300716), Dec 31, 2002: SEAL. LEAKING. AFTER FUELING WAS COMPLETED, A STEADY DRIPPING OF FUEL ONTO #2 ENGINE FROM #2 PYLON WAS NOTICED. FOUND LEAK COMING FROM SEALANT ON FWD SPAR ON #2 ENGINE PYLON. 
- [SDR P5CA0200709](https://openairdocs.org/sdr/P5CA0200709), Nov 21, 2002: DUCT. SEPARATED. NR 4 ENG - FIRE INDICATION AFTER TAKEOFF IN CLIMB. PRECAUTIONARY ENGINE SHUTDOWN & FUEL DUMP PERFORMED. FIRE BOTTLE NOT REQUIRED. FOUND 8TH STAGE BLEED CROSSOVE
- [SDR P5CA0200699](https://openairdocs.org/sdr/P5CA0200699), Sep 12, 2002: COMPRESSOR. STALLED. CLIMBING THROUGH 15,000 FT NR 3 ENGINE COMPRESSOR STALLED. EGT WAS 100 DEGREES CELCIUS. LOWER THAN OTHER MOTOR & N2 WAS LOWER WITH NACELLE ANTI-ICE ON. TROUBLES
- [SDR P5CA0200695](https://openairdocs.org/sdr/P5CA0200695), Aug 7, 2002: SKIN. DAMAGED. UPON WALKAROUND IN ANC, FOUND THAT AIRCRAFT TAIL HAD APPARENTLY MADE GROUND CONTACT DURING TAKEOFF FROM ICN, CAUSING DAMAGE TO APU ACCESS DOORS TO BULKHEAD 2764
- [SDR P5CA0200694](https://openairdocs.org/sdr/P5CA0200694), Aug 5, 2002: ADC. FAILED. DUAL CADC FAILURE CAUSING FAILURE IN TRANSPONDER ALTITUDE REPORTING & INACCURATE ALTIMETER & AIRSPEED INDICATIONS. NR 1 & NR 3 INS WOULD NOT UPDATE. REMOVED AND
- [SDR UIEA01105](https://openairdocs.org/sdr/UIEA01105), Nov 10, 2001: CONNECTOR. SHORTED. NR 1 ENGINE START VALVE OPEN LIGHT CAME ON AT TOP OF DESCENT (INTO XXW) ALTITUDE 27,000 FEET. SHUT DOWN ENGINE IAW FHB. NO ENGINE PARAMETERS EXCEEDED. FIRE SWIT

## STCs that may be installed (OpenAirDocs) (10)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Piper PA-46-701TP)

- [STC SA12438IB](https://openairdocs.org/stc/SA12438IB): MT-Propeller Entwicklung MTV-37-1-E-C-F-R(P)/CFR205-353( ). MT-Propeller Entwicklung GmbH
- [STC SA12017SE](https://openairdocs.org/stc/SA12017SE): Installation of improved Static Ports. Aero Mech Incorporated
- [STC SA04188NY](https://openairdocs.org/stc/SA04188NY): Installation of LAI CoolView Windshields and Windows. Lee Aerospace Inc
- [STC SA01843CH](https://openairdocs.org/stc/SA01843CH): Replacement of certain Goodrich pneumatic deicer boots. SMR Aquisition LLC dba SMR Technologies 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. Lists PA-46 Series
- [STC SA2557NM](https://openairdocs.org/stc/SA2557NM): Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. K S Avionics Inc. Lists PA-46 Series
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies. Lists PA-46 Series
- [STC SA01848AT](https://openairdocs.org/stc/SA01848AT): Installation of Cockpit Display System. Archangel Avionics. Lists PA-46 Series
- [STC SA01224AT](https://openairdocs.org/stc/SA01224AT): Installation of wheel hub cabs with valve stem access door. LoPresti Speed Merchants. Lists PA-46 Series
- [STC SA157NE](https://openairdocs.org/stc/SA157NE): Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Insight Instrument Corp. Lists PA-46 Series

## Related

- Other Piper PA-46-701TP aircraft: https://openairdocs.org/model/piper-pa-46-701tp/aircraft.md
- The Pratt & Whitney Canada PT6A-52 engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-52.md

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