# N131AA: 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: 4698118
- Year built: 2019
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: May 30, 2022
- Certificate issued: May 24, 2022
- Expires: May 31, 2029
- Mode S code: A07EE9
- Registered owner: [Aery Aviation LLC](https://openairdocs.org/faa-owner/AERY%20AVIATION%20LLC)
- Location: [Newport News, VA](https://openairdocs.org/faa-place/VA/Newport%20News)
- Owner type: LLC
- Owner's area on the map: 37.1134° N, 76.5179° W: Placed by OpenAirDocs at the center of ZIP code 23602, 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=131AA
- Page: https://openairdocs.org/aircraft/N131AA

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 N131AA.

## NTSB investigations on N131AA 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 CHI95IA204](https://openairdocs.org/ntsb/CHI95IA204), Jun 27, 1995: McDonnell Douglas DC-10-10 (N131AA), Green Bay, WI, incident, no damage. Probable cause: the weather condition (turbulence in clouds). A factor was the flight crew's abrupt control of the airplane.

## FAA accident and incident reports

None matched to N131AA.

## Reports on N131AA not matched to an aircraft (4)

They name N131AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19950626021809I](https://openairdocs.org/incident/19950626021809I), Jun 26, 1995: Doug DC1010 (N131AA), Chicago, IL. At FL370 encountered cat. Seat belt sight off. Passengers and flight attendents minor injuries.
- [Incident 19881029057969I](https://openairdocs.org/incident/19881029057969I), Oct 29, 1988: Doug DC1010 (N131AA), Phoenix, AZ, Minor damage. Struck a parked airconditioning truck with engine inlet cowl prior to stopping at the gate. Truck in the clear zone
- [Incident 19870327047749I](https://openairdocs.org/incident/19870327047749I), Mar 27, 1987: Doug DC1010 (N131AA), Honolulu, HI. The aircraft encountered clear air turbulence. One passenger burned by coffee, another failed to fasten seat belt.
- [Incident 19800415050879I](https://openairdocs.org/incident/19800415050879I), Apr 15, 1980: Doug DC1010 (N131AA), Chicago, IL. Engine would not accelerate, takeoff aborted.

## 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 N131AA not matched to an aircraft (49)

They name N131AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA991023](https://openairdocs.org/sdr/AALA991023), Jul 11, 1999: DUCT. WORN. HNL - FLT 28 - EN ROUTE HNL/SFO DURING CRUISE, CAUSTIC ODOR WAS NOTED IN THE PASSENGER COMPARTMENT IN THE AREA BETWEEN ROWS 16 AND 19. THE AIRCRAFT RETURNED TO 
- [SDR AALA980340](https://openairdocs.org/sdr/AALA980340), Mar 4, 1998: POST. CORRODED. TUL - CORROSION ON ANGLE PANEL AND CASTING AROUND WALL POST AT FLOORING FOR AIRCRAFT C-LIFT DOOR ATTACH POINT STA 875. INSTALLED NEW ANGLE WEB. SPLICED TOGETHER
- [SDR AALA980384](https://openairdocs.org/sdr/AALA980384), Feb 19, 1998: ANGLE. CORRODED. TUL - T-ANGLE FROM SLANT PANEL TO TRAY LBL 65 STA 879 TO STA 749 IS CORRODED. REPLACED CORRODED SECTION OF T-ANGLE PER SRM 51-01-00-05. TST: 60,422.53 HOURS. CY
- [SDR AALA980383](https://openairdocs.org/sdr/AALA980383), Feb 19, 1998: CHANNEL. CORRODED. FORMED SECTION (DOOR POCKET) U-CHANNEL IS CORRODED AT STA 875 LONGERON 38L TO LONGERON 43L (SLANT PANEL WALL). REPLACED CORRODED U-CHANNEL AT STA 875 LONGERON 3
- [SDR AALA980375](https://openairdocs.org/sdr/AALA980375), Feb 19, 1998: LONGERON. CORRODED. TUL - CORROSION ON LONGERON 52 STA 816 TO STA 822 ON RT SIDE OF LONGERON. REMOVED AND REPLACED CORRODED LONGERON SECTION PER SRM 53-10-00. TST: 60,422 HOURS. CY
- [SDR AALA980376](https://openairdocs.org/sdr/AALA980376), Feb 18, 1998: ROLLER TRAY. CORRODED. CORROSION IN OMNI-ROLLER TRAY AFT END OF TRAY IN CORNER STA 1781 - STA 1779 AFT. FABRICATED NEW OMNI-ROLLER TRAY TRACK, ALODINED AND PRIMED, AND PAINTED NEW TRA
- [SDR AALA980362](https://openairdocs.org/sdr/AALA980362), Feb 17, 1998: ROLLER TRAY. CORRODED. ROLLER TRAY NR 5 HAS CORROSION ON LOWER SURFACE AFT OF STA 859 (X +166). CORRODED SECTION OF TRAY REPLACED PER AARD 51-01-00-5 AND ALODINED, TREATED, PRIMED AND
- [SDR AALA980361](https://openairdocs.org/sdr/AALA980361), Feb 17, 1998: ROLLER TRAY. CORRODED. CORROSION ON ROLLER TRAY NR 5 JUST FORWARD OF STA 879 (X +66). CORRODED SECTION OF TRAY REPLACED PER AARD 51-10-00-05 AND ALODINED, TREATED, PRIMED, AND PAINTED
- [SDR AALA980360](https://openairdocs.org/sdr/AALA980360), Feb 17, 1998: ROLLER TRAY. CORRODED. TUL - NR 2 ROLLER TRAY HAS CORROSION FROM STA 595 - STA 745. SPLICED IN NEW TRAY SECTION PER SRM 53-70-00. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980333](https://openairdocs.org/sdr/AALA980333), Feb 16, 1998: ANGLE. CORRODED. TUL - CORROSION ON AFT LOWER FLOORBOARD TO BULKHEAD ATTACH ANGLE IN AFT CARGO. REMOVED AND REPLACED PART PER 51-10-01. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980332](https://openairdocs.org/sdr/AALA980332), Feb 16, 1998: ANGLE. CORRODED. TUL - CORROSION ALONG SLANT PANEL TO FLOOR ATTACH ANGLE. REMOVED AND REPLACED PER 51-21-01. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980331](https://openairdocs.org/sdr/AALA980331), Feb 16, 1998: SUPPORT. CORRODED. TUL - CORROSION AT STA 1781 AFT LOWER WALL SUPPORT. REMOVED AND REPLACED MANUFACTURED SUPPORT PER AARD 51-01-00-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980339](https://openairdocs.org/sdr/AALA980339), Feb 15, 1998: TRACK. CORRODED. TUL - REMOVED CORRODED GALLEY TRACK SECTION, FABRICATED NEW PIECE, AND INSTALLED IAW 51-10-00-01 AND 51-01-00-05 OF AARD CHAPT 51 OF SRM. TST: 60,422.53 HOURS. 
- [SDR AALA980338](https://openairdocs.org/sdr/AALA980338), Feb 15, 1998: TRACK. CORRODED. TUL - CORROSION ON LT SLIDING DOOR FORWARD TRACK AT STA 879. REMOVED CORRODED PIECE, FABRICATED NEW AND INSTALLED IAW SRM 51-10-00-01 AND 51-01-00-05 OF AARD 53
- [SDR AALA980337](https://openairdocs.org/sdr/AALA980337), Feb 15, 1998: ROLLER TRAY. CORRODED. TUL - CORROSION UNDER LT SLIDING DOOR AFT SIDE ANGLE STA 876 FORWARD AND INBOARD OF ROLLER TRAY NR 2 IN CARGO. REMOVED CORRODED PIECE, FABRICATED NEW AND INSTAL
- [SDR AALA980336](https://openairdocs.org/sdr/AALA980336), Feb 15, 1998: ROLLER TRAY. CORRODED. TUL - NR 4 ROLLER TRAY HAS NUMEROUS SPOTS OF CORROSION FROM STA 760 TO STA 595. REMOVED CORRODED TRACK, FABRICATED NEW TRACK AND REINSTALLED PER SRM 51-01-05. T
- [SDR AALA980335](https://openairdocs.org/sdr/AALA980335), Feb 15, 1998: ROLLER TRAY. CORRODED. TUL - NUMEROUS SPOTS OF CORROSION IN ROLLER TRAY NR 4 BETWEEN STA 879 AND STA 769. REMOVED CORRODED SECTION OF TRACK, FABRICATED NEW AND INSTALLED PER SRM 51-01
- [SDR AALA980334](https://openairdocs.org/sdr/AALA980334), Feb 15, 1998: ROLLER TRAY. CORRODED. TUL - CORROSION IN ROLLER TRAY NR 4 STA 859 TO STA 865. REMOVED CORRODED SECTION OF TRACK, FABRICATED NEW AND INSTALLED PER SRM 51-01-05. TST: 60,422.53 HOURS. 
- [SDR AALA980341](https://openairdocs.org/sdr/AALA980341), Feb 14, 1998: ROLLER TRAY. CORRODED. TUL - NR 2 ROLLER TRAY HAS NUMEROUS AREAS OF CORROSION STA 745 - STA 875. SPLICED IN NEW TRAY FROM STA 840 - STA 875 PER SRM 53-70-00 VOL I. TST: 60,422.53 HOUR
- [SDR AALA980330](https://openairdocs.org/sdr/AALA980330), Feb 13, 1998: ROLLER TRAY. CORRODED. TUL - AREAS OF CORROSION ON ROLLER TRAY NR 1 FROM STA 770 - STA 879. SPLICED IN NEW TRACK PER SRM 53-70-00. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980320](https://openairdocs.org/sdr/AALA980320), Feb 13, 1998: SILL. CORRODED. CORROSION AROUND RIV-NUT ON AFT SIDE DOOR SILL FACET. TREATED, PAINTED, AND PRIMED AREA PER SRM 51-21 VOL II. DAMAGED AREA OK FOR SERVICE PER ESO 7349 DATED 2-1
- [SDR AALA980319](https://openairdocs.org/sdr/AALA980319), Feb 13, 1998: FLOORBEAM. CORRODED. BLENDED CORROSION FROM FLOOR BEAM - OUT OF LIMITS. MADE AND INSTALLED FLOORBEAM END AND SPLICE, ALODINED AND PRIMED. SRM VOL II 51-21-01, SRM VOL I 53-60-01-3. 
- [SDR AALA980344](https://openairdocs.org/sdr/AALA980344), Feb 12, 1998: INTERCOSTAL. CORRODED. TUL - CORROSION ON INTERCOSTAL ABOVE STR 43L FROM STA 859 - STA 879. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW PER IAW CHAP 51 OF SRM AND AARRD 51-01-00-05
- [SDR AALA980343](https://openairdocs.org/sdr/AALA980343), Feb 12, 1998: ANGLE. CORRODED. TUL - CORROSION ON ANGLE AT STA 1781 TRACKS 1 AND 2, TERMINATING END OF CARGO COMPARTMENT FLOOR AT BULKHEAD. REMOVED AND REPLACED ANGLE FITTING PER SRM 51-21-00
- [SDR AALA980342](https://openairdocs.org/sdr/AALA980342), Feb 12, 1998: DOOR FRAME. CORRODED. TUL - CORROSION AT LEFT CARGO/GALLEY DOOR FRAME BOTTOM INSIDE, STA 869 AND STR 48L. REMOVED CORRODED ANGLE FRAME AND INSTALLED NEW FRAME PER IAW CHAPTER 51 OF S
- [SDR AALA980306](https://openairdocs.org/sdr/AALA980306), Feb 11, 1998: SUPPORT. CORRODED. TUL - FLOORBOARD SUPPORT HAS CORROSION AT STA 825 BETWEEN ROLLER TRAYS AND 1 AND 2. REMOVED CORROSION, FABRICATED NEW SUPPORT AND INSTALLED IAW AARD 51-10-00-21
- [SDR AALA980307](https://openairdocs.org/sdr/AALA980307), Feb 10, 1998: FRAME. CORRODED. TUL - CORROSION ON BELL FRAME FROM STR 50R TO STR 49L AT STA 879. REMOVED CORROSION, INSTALLED DOUBLER. REPAIRED IAW SRM 53-30-00. TST: 60,422.53 HOURS. CYCLES:
- [SDR AALA980292](https://openairdocs.org/sdr/AALA980292), Feb 7, 1998: SIDE RAIL. CORRODED. TUL - RIGHT PALLET SIDE RAIL HAS CORROSION FROM STA 1063 TO STA 1102. INSTALLED/SPLICED IN FABRICATED PIECE PER SRM 51-00-00. TST: 60,422.53 HOURS. CYCLES: 20,1
- [SDR AALA980266](https://openairdocs.org/sdr/AALA980266), Feb 5, 1998: SUPPORT. CORRODED. TUL - CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED SUPPORT SRM AND AARD 51-01-00. ALODINED, PRIMED AND PAINTED PER SRM 51-21-01. TST: 60,422.53 HOURS. CYCLE
- [SDR AALA980265](https://openairdocs.org/sdr/AALA980265), Feb 5, 1998: ROLLER TRAY. CORRODED. TUL - NR 4 ROLLER TRAY HAS CORROSION FROM STA 1601 - STA 1701. REMOVED CORROSION AND SPLICED TRAY STA 1641 PER SRM 53-70-00 VOL I. TST: 60,422.53 HOURS. CYCLES:
- [SDR AALA980264](https://openairdocs.org/sdr/AALA980264), Feb 5, 1998: LONGERON. CORRODED. TUL - LONGERON 52 CORRODED AT STA 1139. REPLACED STR 52 FROM 1156 TO 1139, REINSTALLED BELL FRAMES AND SHEAR TIES PER SRM AARD 51-01-00-05. TREATED, PRIMED AND 
- [SDR AALA980263](https://openairdocs.org/sdr/AALA980263), Feb 5, 1998: ANGLE. CORRODED. TUL - NR 1 ROLLER TRAY HAS CORROSION ON FWD ATTACH ANGLE CLIP STA 623. FABRICATED NEW CLIP ANGLE AND INSTALLED IAW AARD 51-10-00-1. TST: 60,422.53 HOURS. CYCLES
- [SDR AALA980262](https://openairdocs.org/sdr/AALA980262), Feb 5, 1998: SPROCKET BOX. CORRODED. TUL - RIGHT LOAD SYSTEM SPROCKET BOX HAS CORROSION AROUND NUT PLATES AND FITTING LOCATED ABOVE STR 47R. DRILLED OUT HOLES, INSTALLED NEW SPROCKET BOX PER 51-21-
- [SDR AALA980261](https://openairdocs.org/sdr/AALA980261), Feb 4, 1998: ROLLER TRAY. CORRODED. TUL - ROLLER TRAY NR 1 HAS CORROSION AT STA 1621 - STA 1561. REMOVED AND REPLACED TRAY TRACK PER SRM 53-70-00 FIG 7. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA980260](https://openairdocs.org/sdr/AALA980260), Feb 4, 1998: ROLLER TRAY. CORRODED. TUL - NR 1 ROLLER TRAY HAS CORROSION STA 1661. REMOVED AND REPLACED TRAY PER AARD 51-01-00-05. SPLICED PER SRM 53-70-00 FIG 7. TST: 60,422.53 HOURS. CYCLES: 20,
- [SDR AALA980259](https://openairdocs.org/sdr/AALA980259), Feb 4, 1998: GUIDE RAIL. CORRODED. TUL - CENTER CARGO LT SIDE GUIDE RAIL HAS CORROSION FROM STA 1561 - STA 1621. REMOVED AND REPLACED GUIDE RAIL PER AARD 51-00-00-05. TST: 60,422.53 HOURS. CYCLES
- [SDR AALA980251](https://openairdocs.org/sdr/AALA980251), Feb 4, 1998: LONGERON. CORRODED. BELL FRAME HAS CORROSION BETWEEN 50L AND 50R STA 775. INSTALLED REPAIR ANGLE PER SRM 53-30-00 PAGE 31. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)
- [SDR AALA970663](https://openairdocs.org/sdr/AALA970663), Apr 3, 1997: HYD MOTOR. DEFECTIVE. SFO - FLT 39 - AFTER TAKEOFF SFO DURING CLIMB-OUT, NR 3 HYDRAULIC SYSTEM QTY BEGAN TO DECREASE FOLLOWED BY ELEVATOR OFF LIGHT ILLUMINATING. ACCOMPLISHED ABNORMA
- [SDR AALA970348](https://openairdocs.org/sdr/AALA970348), Feb 15, 1997: WIRE. BROKEN. SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FORWARD OF L1 AND L2 DOORS AND BY AFT LEFT FIRST CLASS COAT CLOSET INOPERATIVE. REPAIRED BROKEN/SHORTED EME
- [SDR AALA960131](https://openairdocs.org/sdr/AALA960131), Jan 24, 1996: FLOOR SUPPORT. CORRODED. TUL - A 15 INCH SECTION OF FLOOR SUPPORT CORRODED. A SECTION APPROXIMATELY 15 INCHES LONG WAS REPLACED PER ESO 7349. TST, 54,115.43 HOURS. CYCLES, 18,537. (X)
- [SDR AALA960124](https://openairdocs.org/sdr/AALA960124), Jan 23, 1996: SUPPORT. CORRODED. TUL - CORROSION HOLES IN TRACK SIDE WALL SUPPORT IN AREA JUST FORWARD OF CARGO DOOR (MKD). REPLACED WITH NEW RAIL SEGMENT PER SRM 51-00-01, PAGE 5. TREATED, PRI
- [SDR AALA960123](https://openairdocs.org/sdr/AALA960123), Jan 23, 1996: SUPPORT. CORRODED. TUL - TWO INCHES OF SUPPORT CORRODED, NO PREVIOUS MODS. REPLACED SECTION OF TRACK PER FS07349. TST: 54,115.43 HOURS. CYCLES, 18,537. (X)
- [SDR AALA960092](https://openairdocs.org/sdr/AALA960092), Jan 18, 1996: FLOORBEAM. CORRODED. TUL - CORROSION ON UPPER FLOORBEAM FLANGE TOP AND BOTTOM AT NUTPLATE HOLES AT STA 1841, LONGERONS 43L TO 43R. MANUFACTURED AND INSTALLED NEW FLOORBEAM PER AARD 
- [SDR AALA960069](https://openairdocs.org/sdr/AALA960069), Jan 16, 1996: BELL FRAME. CORRODED. TUL - CORROSION AT BELL FRAME LOWER FLANGE STA 959 NEAR STRINGER ATTACH POINT. MANUFACTURED AND INSTALLED DOUBLER PER REPAIR SRM 53-30-00, PAGE 31, FIGURE 8, SH
- [SDR AALA960068](https://openairdocs.org/sdr/AALA960068), Jan 16, 1996: FITTING. CRACKED. TUL - CAST FITTING BETWEEN LONGERONS 28 AND 29 AT STA 1156 ARE CRACKED FROM TOP AFT HOLE THROUGH FASTENER TO RADIUS. CUT OUT CRACKED AREA PER 53-30-00, PAGE 27.
- [SDR AALA960065](https://openairdocs.org/sdr/AALA960065), Jan 15, 1996: SEAT TRACK. CORRODED. TUL - SEAT TRACK CORROSION OUT OF LIMITS. REPLACED 35 INCHES OF NR 6 SEAT TRACK BY SPLICING IN NEW MATERIAL. TST, 54,115.43 HOURS. CYCLES, 18,537. (X)
- [SDR AALA960064](https://openairdocs.org/sdr/AALA960064), Jan 10, 1996: ROLLER TRAY. CORRODED. TUL - CORROSION IN ROLLER TRAY BETWEEN STA 1631 TO STA 1661. REPLACED ROLLER TRAY PER SRM 53-70-00. TST: 54,115.43 HOURS. CYCLES, 18,537. (X)
- [SDR AALA960093](https://openairdocs.org/sdr/AALA960093), Jan 9, 1996: SUPPORT. CORRODED. TUL - SUPPORT UNDER MID-GALLEY BETWEEN SEAT TRACKS HAS CORROSION ON LAST INCH OF SUPPORT. BLENDED, ALODINED, PAINTED PER FSO 7349. TST: 54,175. CYCLES, 18,535. 
- [SDR AALA951092](https://openairdocs.org/sdr/AALA951092), Jun 14, 1995: EEL CONNECTOR. BROKEN. MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 27 THROUGH 29 AT RT AISLE INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT ST

## 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 N131AA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N131AA before.

- [Cancelled 2013-03-04](https://openairdocs.org/deregistered/N131AA-2013-03-04): Robinson Helicopter R44 II, S/N 10215, built 2003. Sale reported. Owner: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)

## 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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