# N274WA: 2019 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: 4698103
- Year built: 2019
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 23, 2019
- Certificate issued: March 13, 2025
- Expires: March 31, 2032
- Mode S code: A2B74D
- Registered owner: [Gosch Development LLC](https://openairdocs.org/faa-owner/GOSCH%20DEVELOPMENT%20LLC)
- Location: [Heber City, UT](https://openairdocs.org/faa-place/UT/Heber%20City)
- Owner type: LLC
- Owner's area on the map: 40.3693° N, 111.1870° W: Placed by OpenAirDocs at the center of ZIP code 84032, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=274WA
- Page: https://openairdocs.org/aircraft/N274WA

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 N274WA.

## FAA accident and incident reports

None matched to N274WA.

## 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 N274WA not matched to an aircraft (129, newest 50)

They name N274WA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR WRLA20110608491](https://openairdocs.org/sdr/WRLA20110608491), Jun 8, 2011: STRUCTURE. CRACKED. APU DOOR INNER STRUCTURE CRACKED NEAR SNUBBER FITTING.
- [SDR WRLA20110603489](https://openairdocs.org/sdr/WRLA20110603489), Jun 3, 2011: SUPPORT FITTING. CRACKED. RT NLG SUPPORT FITTINGS 15MM CRACKED.
- [SDR WRLA20110601490](https://openairdocs.org/sdr/WRLA20110601490), Jun 1, 2011: NOSE COWL. CRACKED. ENGINE NR 2 FRONT SPAR OF NOSE COWL INSIDE CRACKED 0400 POS. LIP SKIN ON POSITION 12/3/6/9 CLOCK POS. FOUND SEVERAL NEW CRACKS NEXT TO EXISTING DOUBLER.
- [SDR WRLA20110601488](https://openairdocs.org/sdr/WRLA20110601488), Jun 1, 2011: LONGERON. CORRODED. LT SIDE LONGERON 28 BELOW OVERWING DOOR CORRODED.
- [SDR WRLA20110601487](https://openairdocs.org/sdr/WRLA20110601487), Jun 1, 2011: LONGERON. CORRODED. RT SIDE LONGERON 28 BELOW OVERWING DOOR ON TWICE POSITIONS CORRODED.
- [SDR WRLA20091119326](https://openairdocs.org/sdr/WRLA20091119326), Nov 19, 2009: FITTING. CORRODED. FOUND LT WING OUTBOARD FLAP INBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 5 EA. REPAIRED THE 5EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEET
- [SDR WRLA20091119325](https://openairdocs.org/sdr/WRLA20091119325), Nov 19, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 675, X=107.5 IN M/D CARGO FLOOR. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV
- [SDR WRLA20091116323](https://openairdocs.org/sdr/WRLA20091116323), Nov 16, 2009: DOUBLER. BROKEN. BROKEN - LWR DOUBLER OF LT WING FIXED L/E NOSE SECTION XOS 487. FABRICATED PART IAW EGAT EI W2009P57B-1344 REV 00. INSTALLED PART IAW MD11 SRM 51-33-01 REV 41.
- [SDR WRLA20091116322](https://openairdocs.org/sdr/WRLA20091116322), Nov 16, 2009: SKIN. CORRODED. EXFOLIATION CORROSION - SKIN CTR WING Y=1226~1239 X=-42~-97 WING TANK UPPER SURFACE TOTAL:39 AREA. REPAIRED THE CORROSION AREA IAW EGAT EI W2009A57B-1378 REV 00
- [SDR WRLA20091116321](https://openairdocs.org/sdr/WRLA20091116321), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 1887 X=47.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53.00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-
- [SDR WRLA20091116320](https://openairdocs.org/sdr/WRLA20091116320), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 735 X=107.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-
- [SDR WRLA20091116319](https://openairdocs.org/sdr/WRLA20091116319), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 716 X=-46, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01
- [SDR WRLA20091116318](https://openairdocs.org/sdr/WRLA20091116318), Nov 16, 2009: HINGE FITTING. CORRODED. FOUND RT WING OUTBOARD FLAP OUTBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-01-000-801 REV 65 RMV THE RT WING OU
- [SDR WRLA20091116317](https://openairdocs.org/sdr/WRLA20091116317), Nov 16, 2009: SUPPORT FITTING. CORRODED. FOUND RT WING OUTBOARD FLAP OUTBOARD INTERNAL SUPPORT FITTING MOUNT HOLE CORROSION TOTAL 3 EA. REPAIRED THE 3EA HOLES CORROSION AREA IAW DRAWING SR11570051 SHEE
- [SDR WRLA20091116316](https://openairdocs.org/sdr/WRLA20091116316), Nov 16, 2009: MOUNT. CORRODED. FOUND RT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL 7 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE RT WING OUTBOARD FLAP INBOARD AFT HIN
- [SDR WRLA20091116315](https://openairdocs.org/sdr/WRLA20091116315), Nov 16, 2009: SKIN. CORRODED. CORROSION - SKIN Y=1226~1228 X=57~61 EXFOLIATION AROUND FASTENERS HEAD CTR WING TANK UPPER SURFACE TOTAL: 3 AREAS. REPAIRED THE CORROSION AREA IAW EGAT EI W2009
- [SDR WRLA20091116314](https://openairdocs.org/sdr/WRLA20091116314), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 1887 X=27.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-
- [SDR WRLA20091116313](https://openairdocs.org/sdr/WRLA20091116313), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 638 TO STA 650, X=42, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 S
- [SDR WRLA20091116312](https://openairdocs.org/sdr/WRLA20091116312), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 645 X=24, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 
- [SDR WRLA20091116311](https://openairdocs.org/sdr/WRLA20091116311), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 1163, X=-8.5, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21
- [SDR WRLA20091116310](https://openairdocs.org/sdr/WRLA20091116310), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, STA 1289, X= -47, IN M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD1 SRM 51-21-
- [SDR WRLA20091116309](https://openairdocs.org/sdr/WRLA20091116309), Nov 16, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN BETWEEN STA 630 AND 635 X= 8.5 INCHES IN MID CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING
- [SDR WRLA20091114308](https://openairdocs.org/sdr/WRLA20091114308), Nov 14, 2009: MOUNT. CORRODED. FOUND LT WING OUTBOARD FLAP INBOARD AFT HINGE MOUNT HOLE CORROSION TOTAL: 3 EA. IAW AMM 20-50-02-900-801 REV 65 REMOVED THE LT WING OUTBOARD FLAP INBOARD AFT HI
- [SDR WRLA20091114307](https://openairdocs.org/sdr/WRLA20091114307), Nov 14, 2009: MOUNT FITTING. CORRODED. FOUND LT WING OUTBOARD FLAP INBOARD FWD HINGE LWR MOUNT FITTING AND SIDE BOLT FITTING SURFACE HAS CORROSION. IAW AMM 57-53-04-000-801 REV 65, REMOVED THE LT WIN
- [SDR WRLA20091105306](https://openairdocs.org/sdr/WRLA20091105306), Nov 5, 2009: PANEL. CRACKED. CRACK PANEL RUDDER REAR CENTER SPAR TO REAR SPAR LWR PANEL RT SIDE. REPAIRED THE CRACK AREA IAW MD11 SRM 55-30-02 FIG 201 REV 41. APPLY PROTECTION COATING IAW M
- [SDR WRLA20091105305](https://openairdocs.org/sdr/WRLA20091105305), Nov 5, 2009: DOUBLER. CRACKED. CRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 546. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. COND CHECK NORMAL AND JOB COMPLET
- [SDR WRLA20091105304](https://openairdocs.org/sdr/WRLA20091105304), Nov 5, 2009: DOUBLER. CRACKED. CRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 560 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. CO
- [SDR WRLA20091105303](https://openairdocs.org/sdr/WRLA20091105303), Nov 5, 2009: DOUBLER. CRACKED. CRACK - BEADED DOUBLER FIXED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 9 INCHES. REPAIR BEADED DOUBLE IAW MD-11 SRM 57-40-02 REV 41. CON
- [SDR WRLA20091105302](https://openairdocs.org/sdr/WRLA20091105302), Nov 5, 2009: DOUBLER. CRACKED. CRACK - BEADED DOUBLER FINED L/E UPPER STRUCTURE RIGHT WING STA XORS 540 LENGTH THE FRONT SPAR 11 INCH. REPAIR BEADED DOUBLER IAW MD-11 SRM 57-40-02 REV 41. CON
- [SDR WRLA20091105327](https://openairdocs.org/sdr/WRLA20091105327), Nov 5, 2009: SEAT TRACK. WORN. WORN - SEAT TRACK CROWN, BETWEEN STA 1661. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41. JOB COMP
- [SDR WRLA20091101287](https://openairdocs.org/sdr/WRLA20091101287), Nov 1, 2009: FITTING. CRACKED. CRACK - FITTING RT WING LOWER WINGLET STRUCTURE, DIMENSION =2.6 INCH QTY 1 EA. IAW AMM 57-31-00-000-801 REV 65 REMOVED THE RT LOWER WINGLET. REFERENCE THE EI W2
- [SDR WRLA20091101301](https://openairdocs.org/sdr/WRLA20091101301), Nov 1, 2009: FITTING. CRACKED. CRACK - ONE CLIP CRACKED ABOUT 1 INCH Y=1341, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY=1. FABRICATED PART IAW EGAT EI W2009P53B-1375 REV 00. INSTAL
- [SDR WRLA20091101300](https://openairdocs.org/sdr/WRLA20091101300), Nov 1, 2009: FITTING. CRACKED. CRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND 
- [SDR WRLA20091101299](https://openairdocs.org/sdr/WRLA20091101299), Nov 1, 2009: INTERCOSTAL. CRACKED. CRACK - INTERCOSTAL, STA Y=6-50, L-42R, FWD CARGO COMPARTMENT L=0.1 INCH. REPAIRED INTERCOSTAL CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.
- [SDR WRLA20091101298](https://openairdocs.org/sdr/WRLA20091101298), Nov 1, 2009: BRACKET. DAMAGED. CRACK - BRACKET TAIL CONE WORK PLATFORM DOOR LOCK/UNLOCK SENSOR SUPPORT ATTACHED AFT FUSELAGE BULKHEAD AFT FACE, Y=2164, Z=73, LENGTH =.5 INCH. REPLACED DAMAGE 
- [SDR WRLA20091101297](https://openairdocs.org/sdr/WRLA20091101297), Nov 1, 2009: SKIN. DEFORMED. DEFORMED - EDGE OF SKIN FWD LOWER CORNER OF CENTER CARGO DOOR. MEASURE DEFORMED AREA DIMENSION (LXWXD = 1.5"X1.5"X0.03") AND NDT CHECK NORMAL AND IAW MD11 SRM 5
- [SDR WRLA20091101296](https://openairdocs.org/sdr/WRLA20091101296), Nov 1, 2009: BRACKET. CRACKED. CRACK - BRACKET OF TAIL CONE WORK PLATFORM LIGHT BOTH OF AFT FUSELAGE BULKHEAD ABOUT 1 INCH QTY = 2EA. REPLACED NEW BRACKET IAW MD11 SRM 51-35-01 REV 41.
- [SDR WRLA20091101295](https://openairdocs.org/sdr/WRLA20091101295), Nov 1, 2009: SUPPORT ANGLE. CRACKED. CRACK - NR 3 ENG PRECOOLER COMPARTMENT WIRE SUPPORT ANGLE CRACK ABOUT 2 INCHES. REPAIRED THE CRACK AREA IAW MD11 SRM 54-00-00 FIG 208 REV 41.
- [SDR WRLA20091101294](https://openairdocs.org/sdr/WRLA20091101294), Nov 1, 2009: RETAINER. CRACKED. CRACK - RETAINER STA 1521 LBL 49 PRESSURE BULKHEAD OF CENTER CARGO COMPARTMENT QTY =1EA. REPLACED WITH NEW RETAINER IAW EGAT EI W2009P53B-1374 REV 00.
- [SDR WRLA20091101293](https://openairdocs.org/sdr/WRLA20091101293), Nov 1, 2009: RETAINER. CRACKED. CRACK - RETAINER STA 1521 LBL 11 PRESSURE BULKHEAD CENTER CARGO COMPARTMENT DIMENSION: 1 INCH. REPLACED WITH NEW RETAINER IAW MD11 SRM 53-00-01 REV 41.
- [SDR WRLA20091101292](https://openairdocs.org/sdr/WRLA20091101292), Nov 1, 2009: SEAT TRACK. CRACKED. CRACK - SEAT TRACK STA 635 X=8 M/D CARGO FLOOR L=3". REPAIRED THE SEAT TRACK IAW ME11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41
- [SDR WRLA20091101291](https://openairdocs.org/sdr/WRLA20091101291), Nov 1, 2009: SEAT TRACK. CRACKED. CRACK - SEAT TRACK STA 755 X=47.5 M/D CARGO FLOOR. REPAIRED THE SEAT TRACK IAW MD11 SRM 53-00-52 REV 41. APPLY PROTECTION COATING IAW MD11 SRM 51-21-01 REV 41.
- [SDR WRLA20091101290](https://openairdocs.org/sdr/WRLA20091101290), Nov 1, 2009: INTERCOSTAL. CRACKED. CRACK - INTERCOSTAL 3 AIR CONDITION DOOR L=0.5" QTY =1 AREA. REPLACED INTERCOSTAL IAW MD11 SRM 51-35-01 REV 41.
- [SDR WRLA20091101289](https://openairdocs.org/sdr/WRLA20091101289), Nov 1, 2009: INTERCOSTAL. CRACKED. CRACK - INTERCOSTAL 2 AIR CONDITION DOOR L=5", QTY = 1 AREA. REPLACED WITH NEW INTERCOSTAL ON 2 AIR CONDITION DOOR IAW MD11 SRM 51-35-01 REV 41.
- [SDR WRLA20091101286](https://openairdocs.org/sdr/WRLA20091101286), Nov 1, 2009: SUPPORT BRACKET. CRACKED. CRACK - THE SUPPORT BRACKET OF FUEL PIPE AT Y=1441, L32L, LEFT UPPER FUSELAGE, CRACKED ABOUT .25 INCH. FABRICATED NEW PART IAW EGAT EI W2009P53B-1353 REV 00. IN
- [SDR WRLA20091101285](https://openairdocs.org/sdr/WRLA20091101285), Nov 1, 2009: ANGLE. CRACKED. CRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. 
- [SDR WRLA20091101284](https://openairdocs.org/sdr/WRLA20091101284), Nov 1, 2009: WEB. CRACKED. CRACK - WEB, LT WING TO BODY FAIRING SUPPORT STRUCTURE, L=1.5", Y=1341. REPAIRED WEB CRACK AREA IAW MD11 SRM 53-00-00 FIG 204 REV 41.
- [SDR WRLA20091101283](https://openairdocs.org/sdr/WRLA20091101283), Nov 1, 2009: WEB. CRACKED. CRACK - WEB, LT OF FWD UPPER HORIZONTAL STAB COMPARTMENT ACCESS CUTOUT Y = 2042,, X=14, LENGTH = .375 INCH. REPAIRED THE CRACK AREA IAW MD11 SRM 53-00-00 FIG 21
- [SDR WRLA20091101282](https://openairdocs.org/sdr/WRLA20091101282), Nov 1, 2009: STIFFENER. CRACKED. CRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.
- [SDR WRLA20091101281](https://openairdocs.org/sdr/WRLA20091101281), Nov 1, 2009: STIFFENER. CRACKED. CRACK - STIFFENER, STA 1841, RBL 38 LWR SIDE WEB OF FLOORBEAM, AFT CARGO COMPARTMENT L=0.5 INCH. REPLACED WITH NEW STIFFENER IAW MD11 SRM 51-33-01 FIG 2 REV 41.

All 129: https://openairdocs.org/aircraft/N274WA/unmatched-reports.md

## 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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