# N854MA: 2017 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: 4698027
- Year built: 2017
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: February 10, 2017
- Certificate issued: September 21, 2020
- Expires: September 30, 2027
- Mode S code: ABB748
- Registered owner: [Isi-M600 Inc Trustee](https://openairdocs.org/faa-owner/ISI-M600%20INC%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7452° N, 75.5937° W: Placed by OpenAirDocs at the center of ZIP code 19805, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=854MA
- Page: https://openairdocs.org/aircraft/N854MA

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 N854MA.

## NTSB investigations on N854MA not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI81IA065](https://openairdocs.org/ntsb/CHI81IA065), Jun 13, 1981: Mitsubishi MU-2B (N854MA), Middletown, OH, incident, minor damage

## FAA accident and incident reports

None matched to N854MA.

## Reports on N854MA not matched to an aircraft (1)

They name N854MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19810613035999I](https://openairdocs.org/incident/19810613035999I), Jun 13, 1981: Mtsbsi MU2B36A (N854MA), Middletown, OH, Minor damage. Pilot forgot to extend landing gear due to improper use of checklist.

## 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 N854MA not matched to an aircraft (20)

They name N854MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2012FA0000489](https://openairdocs.org/sdr/2012FA0000489), Jul 19, 2012: BRIDAL CABLE. DISENGAGED. ON CLIMBOUT, PILOT ENGAGED AUTOPILOT AND ACFT BEGAN TO PITCH UP AND CLIMB. AUTOPILOT WAS DISENGAGED AND CONTROL WAS MAINTAINED. PILOT AGAIN ENGAGED AUTOPILOT AN
- [SDR MALA975699](https://openairdocs.org/sdr/MALA975699), Oct 11, 1997: LIGHT RECEPTACLE. FAILED. DURING PREFLIGHT, NOTICED ELECTRICAL SMELL EMANATING FROM ROW 3-4 AREA. TROUBLESHOT PER MX CONTROL, FOUND THIRD OVERHEAD LIGHT ON RIGHT SIDE TO BE ARCING AT FOR
- [SDR MALA975668](https://openairdocs.org/sdr/MALA975668), Sep 19, 1997: BULB. FAILED. DURING INSPECTION, CENTER AISLE OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. (M)
- [SDR DHC8102](https://openairdocs.org/sdr/DHC8102), Sep 8, 1997: LAMP. FAILED. DURING INSPECTION, TWO RED FLOOR TRACK LIGHTS INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)
- [SDR MALA975500](https://openairdocs.org/sdr/MALA975500), Jul 4, 1997: LIGHT. INOPERATIVE. DURING INSPECTION, TWO FLOOR TRACK EMERGENCY LIGHTS AND ONE FORWARD EMERGENCY OVERHEAD EXIT LIGHT HAS BULBS BURNED OUT. MAINTENANCE RELAMPED. ALL CHECKS GOOD. (
- [SDR MALA975463](https://openairdocs.org/sdr/MALA975463), Jun 12, 1997: BULB. FAILED. DURING INSPECTION, EMERGENCY EXIT LIGHT WAS FOUND INOPERABLE. MAINTENANCE RELAMPED. OPS CHECK GOOD. (X)
- [SDR MALA965094](https://openairdocs.org/sdr/MALA965094), Aug 14, 1996: SKIN. DENTED. DURING SCHEDULED C-CHECK INSPECTION IN INT, MAINTENANCE FOUND SURFACE DENTS IN THE PASSENGER DOOR. REPAIRS WERE COMPLETED IAW RD8-52-040 BY INSTALLATION OF 2024
- [SDR MALA965093](https://openairdocs.org/sdr/MALA965093), Aug 13, 1996: SILL CAP. WORN. DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WRE COMPLETED THROUGH COMPLIANCE WITH RD 8-53-213
- [SDR 96ZZZM1293](https://openairdocs.org/sdr/96ZZZM1293), Aug 13, 1996: FITTING. WORN. DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WRE COMPLETED THROUGH COMPLIANCE WITH RD 8-53-213
- [SDR 96ZZZM1292](https://openairdocs.org/sdr/96ZZZM1292), Aug 13, 1996: SILL CAP. WORN. DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WERE COMPLETED THROUGH COMPLIANCE WITH RD 8-53-21
- [SDR MALA965072](https://openairdocs.org/sdr/MALA965072), Jul 14, 1996: CONNECTOR. DIRTY. DURING THE PREFLIGHT INSPECTION IN DTW, THE FLIGHT ATTENDANT WAS UNABLE TO TURN ON THE EMERGENCY LIGHTS. MAINTENANCE CLEANED A DIRTY CONNECTION AT THE EMERGENCY
- [SDR MALA965046](https://openairdocs.org/sdr/MALA965046), Jun 18, 1996: LAMP. INOPERATIVE. FLT NR 3370 - DURING THE PREFLIGHT INSPECTION IN MSP, THE CREW FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY EXIT LAMP ASS
- [SDR MALA964931](https://openairdocs.org/sdr/MALA964931), Mar 28, 1996: LIGHT. INOPERATIVE. DTW - FLT 3407 - DURING PRE-FLIGHT, CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LAMP ASSEMBLY WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPE
- [SDR MALA964817](https://openairdocs.org/sdr/MALA964817), Jan 10, 1996: ITT INDICATOR. INTERNAL FAULT. DTW - FLT 3106 - AFTER DEPARTURE FROM DTW, THE NR 1 ITT GAUGE BEGAN FLUCTUATING AND READ 300 DEGREES LESS THAN NR 2. THE AIRCRAFT RETURNED TO DTW AND LANDED WIT
- [SDR MALA954716](https://openairdocs.org/sdr/MALA954716), Nov 21, 1995: RIB. CRACKED. DURING A WALKAROUND INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER END RIB OF THE FORE RUDDER. THEY REPLACED RIB IAW SRM 51-40-00. (M)
- [SDR MALA954680](https://openairdocs.org/sdr/MALA954680), Oct 27, 1995: HSI/HDG WARNING. ACTIVATED. FLT NR 3396 - EN ROUTE TO YXU, THE CREW RECEIVED A HSI HDG MISMATCH ADVISORY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE CYCLED THE POWER AND WAS UNABLE TO DUPLI
- [SDR MALA954428](https://openairdocs.org/sdr/MALA954428), Apr 21, 1995: EEL. INOP. FLT 3205 - DURING THE PREFLIGHT IN MSP, THE COCKPIT HAND HELD EMERGENCY LIGHT WAS INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATED SATIS
- [SDR MALA954386](https://openairdocs.org/sdr/MALA954386), Mar 26, 1995: EEL BATTERY PACK. DISCHARGED. DURING THE PREFLIGHT IN DTW, ONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD BATTERY PACK. SYSTEM OPERATED SATISFACTORILY
- [SDR MALA954332](https://openairdocs.org/sdr/MALA954332), Feb 21, 1995: EEL. FAILED. DURING A MAINTENANCE GATE WALK-AROUND, THE COCKPIT OVERHEAD EMERGENCY LIGHT ABOVE THE JUMP SEAT WAS FOUND INOPERATIVE. MECHANICS REPLACED THE HAND HELD EMERGENC
- [SDR MALA954241](https://openairdocs.org/sdr/MALA954241), Jan 13, 1995: EXHAUST SHROUD. CRACKED. CKB - DURING SCHEDULED INSPECTION, MAINTENANCE NOTED THAT THE RT EXHAUST SHROUD, LT AND RT SIDE SKIN WAS CRACKED AND BUCKLED. REPAIRS WERE COMPLETED IAW WVAC EU

## 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

## 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

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