# N231DN: 2022 Piper PA-46-600TP

- Status: Valid registration
- Airframe: [Piper PA-46-600TP](https://openairdocs.org/model/piper-pa-46-600tp) (registry code 7104650, 6 seats)
- Engine: [Pratt & Whitney Canada PT6A-42A](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-42a) (registry code 52268)
- 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: 4698211
- Year built: 2022
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: June 24, 2022
- Certificate issued: January 13, 2024
- Expires: January 31, 2031
- Mode S code: A20C8F
- Registered owner: [Henrys Investments LLC](https://openairdocs.org/faa-owner/HENRYS%20INVESTMENTS%20LLC)
- Location: [Encinitas, CA](https://openairdocs.org/faa-place/CA/Encinitas)
- Owner type: LLC
- Owner's area on the map: 33.0569° N, 117.2576° W: Placed by OpenAirDocs at the center of ZIP code 92024, 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=231DN
- Page: https://openairdocs.org/aircraft/N231DN

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): 6 in force

### Matched by airframe (Piper PA-46-600TP)

- [AD 2023-25-02](https://openairdocs.org/ad/2023-25-02): Control Column Section · Piper PA-46-350P, PA-46-500TP and PA-46-600TP. Effective Dec 19, 2023
- [AD 2022-11-10](https://openairdocs.org/ad/2022-11-10): Wing Spar · Piper PA-46-600TP. Effective Jun 27, 2022
- [AD 2019-12-12](https://openairdocs.org/ad/2019-12-12): Bulkhead · Piper PA-46-600TP. Effective Jul 12, 2019
- [AD 2018-14-01](https://openairdocs.org/ad/2018-14-01): Fuselage Skin · Piper PA-46-600TP. Effective Jul 25, 2018
- [AD 2017-16-03](https://openairdocs.org/ad/2017-16-03): Wing Spar · Piper PA-46-600TP. Effective Aug 9, 2017

### Matched by engine (Pratt & Whitney Canada PT6A-42A)

- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012

## Information bulletins (advisory) (2 in force)

- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006

## NTSB investigations

None matched to N231DN.

## FAA accident and incident reports

None matched to N231DN.

## 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 N231DN not matched to an aircraft (11)

They name N231DN, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR PIDR2006007](https://openairdocs.org/sdr/PIDR2006007), Jun 19, 2006: SKIN. DENTED. DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, INSPECTION NOTED DENTS BEYOND ALLOWABLE LIMITS IN FUSELAGE SKIN FROM BS887 TO BS907 BETWEEN ST
- [SDR PIDR2006008](https://openairdocs.org/sdr/PIDR2006008), Jun 13, 2006: SKIN. DENTED. DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, INSPECTION NOTED A DENT IN THE FUSELAGE SKIN BEYOND ALLOWABLE LIMITS AT BS 887 STR 22 LT. REPA
- [SDR PIDR2006009](https://openairdocs.org/sdr/PIDR2006009), Jun 6, 2006: SKIN. DAMAGED. DURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, DAMAGE NOTED ON THE RIGHT HORIZONTAL STABILIZER APPROXIMATELY 8 FEET FROM THE INBOARD END. REP
- [SDR DL73G050546](https://openairdocs.org/sdr/DL73G050546), Sep 14, 2005: PROBE. OVERHEATED. ATB DUE TO FO PITOT TUBE OVERHEATING AND CAUSING INSULATION IN COCKPIT SIDEWALL TO SMOLDER. REPLACED PROBE.
- [SDR DL73G050406](https://openairdocs.org/sdr/DL73G050406), Jul 26, 2005: BRAKE. DAMAGED. ON TRANSIT CHECK, FOUND METAL SHARDS UNDERNEATH NR 4 BRAKE ASSY, SHARDS ARE FROM OUTER DISK. REPLACED NBR 4 MAIN BRAKE ASSY PER MM.
- [SDR DL73G030775](https://openairdocs.org/sdr/DL73G030775), Aug 20, 2003: SKIN. DEBONDED. LT WING OUTBOARD FORE FLAP DISBONDED. TE WEDGE REBUILT IAW ER/A 423088-14.
- [SDR DL73G030774](https://openairdocs.org/sdr/DL73G030774), Aug 20, 2003: SKIN. DAMAGED. RT FUSELAGE SKIN / STA 312-360 / S14-S19. DAMAGED REPLACEMENT SKIN SECTION FABRICATED IAW ER/A 423343-14.
- [SDR DL733001929](https://openairdocs.org/sdr/DL733001929), Oct 2, 2000: LIGHT. DAMAGED. PASSENGER SEAT 02B EMERGENCY LIGHTING FLOOR LIGHT DAMAGED. REPLACED LIGHT ASSY, OPS NORMAL.
- [SDR DL733001401](https://openairdocs.org/sdr/DL733001401), Jul 25, 2000: MODULE. FAULTY. UPON STARTING NR 2 ENG, GOT MASTER FIRE WARNING LIGHT AND HORN. NO TEE HANDLES ILLUMINATED. SHUT DOWN NR 2 ENG APU EGT WAS NORMAL. ALL TEST OK. RAN ENG, UNABLE 
- [SDR DL733991511](https://openairdocs.org/sdr/DL733991511), Jul 4, 1999: LIGHT. INOPERATIVE. EMERGENCY EXIT BULLNOSE LIGHT AT 21D INOP. RELAMPED, OPS CKS NORMAL.
- [SDR DL733980819](https://openairdocs.org/sdr/DL733980819), Apr 16, 1998: SKIN. DENTED. TWO DENTS EXIST IN THE FUSE SKIN AT APPROX BS227 BETWEEN S17R AND S19R. PRIOR TO ENTERING REVENUE SERVICE; REPAIR PER ERA 331623-14.

## STCs that may be installed (OpenAirDocs) (23)

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-46-600TP)

- [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 SA12438IB](https://openairdocs.org/stc/SA12438IB): MT-Propeller Entwicklung MTV-37-1-E-C-F-R(P)/CFR205-353( ). MT-Propeller Entwicklung GmbH
- [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [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 SA04734NY](https://openairdocs.org/stc/SA04734NY): Installation of LAI LH Heated Windshield. Lee Aerospace 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 SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA01050DE](https://openairdocs.org/stc/SA01050DE): Installation of aircraft main battery replacement. Concorde Battery Corporation
- [STC SA02654SE](https://openairdocs.org/stc/SA02654SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approvaL. AeroMech Incorporated
- [STC SA02135SE](https://openairdocs.org/stc/SA02135SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data). Electronics International Inc
- [STC SA02276AK](https://openairdocs.org/stc/SA02276AK): Installation of AMSAFE Aviation Inflatable Restraints. AMSAFE Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [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

### Approved for the engine (Pratt & Whitney Canada PT6A-42A)

- [STC SE00001EN](https://openairdocs.org/stc/SE00001EN): Engines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 2, 8/16/95. MORE Company Inc
- [STC SE01805NY](https://openairdocs.org/stc/SE01805NY): Installation of Fuel Nozzle Adapters using studs and nuts. Atlantic Turbines International Inc

## Earlier aircraft with N231DN

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N231DN before.

- [Cancelled 1993-08-18](https://openairdocs.org/deregistered/N231DN-1993-08-18): Mooney M20K, S/N 250170. Exported to Germany. Owner: [Jarschke Reinhard](https://openairdocs.org/faa-owner/JARSCHKE%20REINHARD), [Angwin, CA](https://openairdocs.org/faa-place/CA/Angwin)

## Related

- Other Piper PA-46-600TP aircraft: https://openairdocs.org/model/piper-pa-46-600tp/aircraft.md
- The Pratt & Whitney Canada PT6A-42A engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-42a.md

---
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.