# N889MA: 2016 Piper PA46-500TP - Status: Valid registration - Airframe: [Piper PA46-500TP](https://openairdocs.org/model/piper-pa46-500tp) (registry code 7104622, 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: 4697616 - Year built: 2016 - Type: Fixed wing single engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: August 25, 2016 - Certificate issued: July 27, 2026 - Expires: July 31, 2033 - Mode S code: AC4058 - Registered owner: [Freedom Fund US LLC](https://openairdocs.org/faa-owner/FREEDOM%20FUND%20US%20LLC) - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: LLC - Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, 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=889MA - Page: https://openairdocs.org/aircraft/N889MA 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): 15 in force ### Matched by airframe (Piper PA46-500TP) - [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 2021-09-02](https://openairdocs.org/ad/2021-09-02): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Apr 16, 2021 - [AD 2016-01-01](https://openairdocs.org/ad/2016-01-01): Wings · Piper PA-46-500TP. Effective Feb 17, 2016 - [AD 2015-13-09](https://openairdocs.org/ad/2015-13-09): Cabin Pressure Control System · Piper PA-46-350P and PA-46-500TP. Effective Jul 13, 2015 - [AD 2013-13-01](https://openairdocs.org/ad/2013-13-01): Fuel Storage · Piper PA-46-310P, PA-46-350P, PA-46-500TP and 1 more. Effective Jul 10, 2013 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [AD 2008-26-11](https://openairdocs.org/ad/2008-26-11): Stall vane heater · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Jan 28, 2009 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-15-19](https://openairdocs.org/ad/2004-15-19): Protective Cover Over Percussion Caps or Silicon Tube Installed Over the End of the Trigger Mechanism Pin of the Oxygen Generators · Piper PA-46-500TP. Effective Sep 13, 2004 - [AD 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004 - [AD 2004-03-32](https://openairdocs.org/ad/2004-03-32): Electronic control modules · Piper PA-46-500TP. Effective Mar 29, 2004 - [AD 2001-12-01](https://openairdocs.org/ad/2001-12-01): Inboard Flap Drive Bellcrank Assemblies · Piper PA-46-310P, PA-46-350P and PA-46-500TP. Effective Jun 29, 2001 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 ### 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 ### Historical (superseded or no longer in force) - [AD 2021-04-07](https://openairdocs.org/ad/2021-04-07) (historical): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Mar 30, 2021 - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 ## Information bulletins (advisory) (8 in force) - [SAIB CE-17-02](https://openairdocs.org/saib/CE-17-02): Cabin Altitude Encoder Alternative Method of Compliance (AMOC) to Airworthiness Directive (AD) 2015-13-09; Terminating Action. Issued Dec 13, 2016 - [SAIB CE-15-18](https://openairdocs.org/saib/CE-15-18): WING SPAR Main Spar Lower Cap Cracks. Issued Jun 15, 2015 - [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014 - [SAIB CE-09-13R1](https://openairdocs.org/saib/CE-09-13R1): POWERPLANT - ENGINE MOUNT Cracking at nose landing gear attachment and trunnion attachment. Issued Jul 14, 2014 - [SAIB CE-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [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 - [SAIB CE-09-13](https://openairdocs.org/saib/CE-09-13) (historical): Landing Gear: Engine Mount-Nose Landing Gear Attach Section. Issued Feb 23, 2009 ## NTSB investigations None matched to N889MA. ## FAA accident and incident reports None matched to N889MA. ## Reports on N889MA not matched to an aircraft (2) They name N889MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19990302013539I](https://openairdocs.org/incident/19990302013539I), Mar 2, 1999: Boeing 727225 (N889MA), Salt Lake City, UT, Minor damage. On 3-2-99 at approximately 0833 MST le bus #4101 driven by Mr. Gulbransen collided with the left wing tip of aircraft N889MA. The aircraft was parked on the… - [Incident 19960831034309I](https://openairdocs.org/incident/19960831034309I), Aug 31, 1996: Boeing 727200 (N889MA), Lubbock, TX, Minor damage. Narrative: captain stone stated he was making a visual approach to runway 17R at Lubbock International Airport. It was a clear night and he had the runway in… ## 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 N889MA not matched to an aircraft (48) They name N889MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2003F00136](https://openairdocs.org/sdr/2003F00136), Nov 17, 2002: BATTERY PACK. DISCHARGED. DURING P/T FOUND DOOR 2 AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, LIGHTS OPS CHECKS GOOD IAW AMM 33-50-00. (M) - [SDR 2003F00105](https://openairdocs.org/sdr/2003F00105), Nov 17, 2002: LIGHT. INOPERATIVE. DURING P/T FOUND FORWARD MOST E-PATH LIGHT STRIP OUT. REMOVED AND REPLACED E-PATH LIGHT STRIP, OPS CHECK NORMAL. (M) - [SDR 2002F01021](https://openairdocs.org/sdr/2002F01021), Oct 17, 2002: BATTERY. DISCHARGED. DURING PREFLIGHT, FOUND CENTER EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY FOR EXTERIOR OVERWING EXIT LIGHT. OPERATIONAL CH - [SDR 2002F00226](https://openairdocs.org/sdr/2002F00226), Jan 22, 2002: VALVE. DEFECTIVE. FOUND AIRCRAFT COULD NOT PRESSURIZE ON ASCENT, RIGHT PACK VALVE INTERMITTENT. A/C DESCENDED TO 10,000 FT. PERFORMED AOM PROCEDURES A/C LANDED. REPLACED PACK VAL - [SDR 2001F00455](https://openairdocs.org/sdr/2001F00455), Aug 22, 2001: LIGHT. INOPERATIVE. DURING PREFLIGHT, TRANSIT EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 28 CEILING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 28. OPS CHECK OK IAW - [SDR 2001F00096](https://openairdocs.org/sdr/2001F00096), Jun 12, 2001: SHUTOFF VALVE. LEAKING. WHILE ON SINGLE PACK OPERATION AND AT FL250 CABIN PRESS KEPT CLIMBING. FOLLOWED AOM PROCEDURE AND DESCENDED. WHILE DESCENDING CABIN CONTINUED TO CLIMB TO FL160 - [SDR 20010125SG017](https://openairdocs.org/sdr/20010125SG017), Dec 23, 2000: FUEL CONTROL. MALFUNCTIONED. ON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT - [SDR 20010124SG004](https://openairdocs.org/sdr/20010124SG004), Dec 23, 2000: FUEL CONTROL. MALFUNCTIONED. ON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT - [SDR 20010406SG005](https://openairdocs.org/sdr/20010406SG005), Dec 22, 2000: CONTROL CABLE. OUT OF ADJ. IN CRUISE FLIGHT, NOSE GEAR DOOR LIGHTS COMES ''ON'' AT 310 KNOTS COMES BACK ''OFF'' AT 293 KNOTS. INSPECTED NOSE GEAR WW DOORS AND FOUND CABLES TO BE OUT OF TO - [SDR 20000511AP029](https://openairdocs.org/sdr/20000511AP029), Dec 8, 1999: BEAM. CRACKED. FOUND J BEAM HAS TWO .375 INCH CRACKS AT LEFT WING TRAILING EDGE AREA ABOVE NR 7 SPOILER ACTUATOR AREAS. REMOVED WALKING BEAM PANEL AND SMALL SKIN PANEL IAW 51- - [SDR 20000511AP028](https://openairdocs.org/sdr/20000511AP028), Dec 8, 1999: BEAM. CRACKED. FOUND J BEAM HAS .375 INCH CRACK AT RIGHT WING ABOVE NR 8 SPOILER ACTUATOR AREA. REMOVED RIGHT WING TOP SKIN AND WALKING BEAM PANEL IAW 51-30-2 PAGE 2. REMOVED - [SDR 20000511AP027](https://openairdocs.org/sdr/20000511AP027), Dec 8, 1999: RETAINER. CRACKED. SEAL RETAINER CRACKED ABOVE RIGHT ELEPHANT EAR FAIRING ON AFT SEGMENT. REMOVED SEAL RETAINER, DRILLED HOLES IN NEW RETAINER IAW 51-30-2 PAGE 5. INSTALLED RETAIN - [SDR 20000511AP026](https://openairdocs.org/sdr/20000511AP026), Dec 8, 1999: WEB. CRACKED. VERTICAL FIN LEADING EDGE PANEL 9602 INNER CURVED WEB HAS 1 INCH CRACK AT CORNER. STOP DRILLED CRACK IAW 51-10-1 PAGE 613. FABRICATED DOUBLER IAW 51-40-2 PAGE 2 - [SDR 20000511AP025](https://openairdocs.org/sdr/20000511AP025), Dec 8, 1999: WEB. TORN. VERTICAL LEADING EDGE CENTER SECTION INTERIOR WEB IS DAMGED AT THREE CORNERS. CUT OUT DAMAGED AREAS IAWS 51-40-2 PAGES 2/3. HFEC SHOWS NO CRACKS IAW 51-00-00 PA - [SDR 20000511AP024](https://openairdocs.org/sdr/20000511AP024), Dec 8, 1999: BRACKET. CRACKED. FOUND NR 7 SPOILER OUTBOARD HINGE SUPPORT CRACKED. REMOVED CRACKED HINGE SUPPORT BRACKET. DRILLED NEW SUPPORT BRACKET IAW 51-10-1 PAGE 14. INSTALLED NEW HINGE S - [SDR 20000511AP023](https://openairdocs.org/sdr/20000511AP023), Dec 8, 1999: FLOORBEAM. CORRODED. TOP OF FLOORBEAM BS 1110 BL 0 - LBL 12 AND BL 0 - RBL 12. REMOVED CORROSION IAW 51-10-6 PAGE 2. AREA OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 FIG 8. FABR - [SDR 20000511AP022](https://openairdocs.org/sdr/20000511AP022), Dec 8, 1999: FLAP TRACK. CORRODED. RIGHT OUTBOARD MID FLAP INBOARD TRAILING EDGE FLAP TRACK CORRODED. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED RETAINER IAW 51-10-1 PAGE 1. TREATED - [SDR 20000511AP021](https://openairdocs.org/sdr/20000511AP021), Dec 8, 1999: FLOOR SUPPORT. CORRODED. FOUND FLOOR SUPPORT BS 1110 TO 1130 LBL 12 CORRODED. REMOVED FLOOR SUPPORT IAW 51-30-2 PAGE 1. FABRICATED SUPPORT IAW 51-10-1 PAGE 2. TREATED AND PRIMED IAW 51- - [SDR 20000511AP020](https://openairdocs.org/sdr/20000511AP020), Dec 8, 1999: FLOORBEAM. GROOVED. FOUND FLOORBEAM BS 1110 LBL 45 HAS 2.5 INCH GROOVE CENTER OF TOP FLANGE. REMOVED WEB, SIDE WALLS AND SEAT TRACK. CUT OUT DAMAGED AREA IAW 53-10-2 FIG 3. ACCOMPL - [SDR 20000511AP019](https://openairdocs.org/sdr/20000511AP019), Dec 8, 1999: SUPPORT BRACKET. BENT. SUPPORT FOR CONDUIT CRACKED AND BENT BS 1110 TO 1130 LBL 33. REMOVED DAMAGED U CHANNEL SUPPORT AND ANGLE BRACKET IAW 51-30-2 PAGE 1/2. FABRICATED NEW U CHANNEL - [SDR 20000511AP018](https://openairdocs.org/sdr/20000511AP018), Dec 8, 1999: ANGLE. CRACKED. CABIN FLOOR SUPPORT INTERCOSTAL TOP ANGLE CRACKED AT SCREWHEAD BL 0 BETWEEN BS 950A AND 950B. REMOVED ANGLE IAW 51-30-2 PAGE 2. FABRICATED NEW ANGLE IAW 51-40-2 - [SDR 20000511AP017](https://openairdocs.org/sdr/20000511AP017), Dec 8, 1999: RETAINER. CORRODED. FOUND SEAL RETAINER CHANNEL CORRODED, LOCATED AT TRAILING EDGE OF RIGHT OUTBOARD MID FLAP. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED NEW RETAINER - [SDR 20000511AP016](https://openairdocs.org/sdr/20000511AP016), Dec 8, 1999: SKIN. CRACKED. VERTICAL STABILIZER LOWER LEADING EDGE FAIRING NR 9501 HAS .5 INCH CRACK IN SKIN AND CHAFED AROUND END. CUT OUT DAMAGED AREA IAW 51-40-2 FIG 1. FABRICATED DOUBL - [SDR 20000511AP015](https://openairdocs.org/sdr/20000511AP015), Dec 8, 1999: ANGLE. DAMAGED. CABIN FLOOR PANEL SUPPORT RIB BETWEEN STATION 720F AND 740 BL 0 TORN. REMOVED ANGLE SUPPORT BETWEEN STATION 720F TO 740 AT BL 0 IAW 51-30-2 PAGE 1. FABRICATED A - [SDR 20000511AP014](https://openairdocs.org/sdr/20000511AP014), Dec 8, 1999: FAIRING. CRACKED. FOUND .75 INCH CRACK AT TOP OF RIGHT INBOARD FLAP AFT TEARDROP FAIRING. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT TEARDROP FAIRING. (M) - [SDR 20000511AP013](https://openairdocs.org/sdr/20000511AP013), Dec 8, 1999: FAIRING. CRACKED. FOUND 1.5 INCH CRACK AT AFT MOUNT HOLE OF LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. (M) - [SDR 20000511AP011](https://openairdocs.org/sdr/20000511AP011), Dec 8, 1999: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK STATION 360 TO 440 RBL 48 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 12 FOUND OUT OF LIMITS IAW 51-10-1 PAGE 15. FABRICATED NEW SE - [SDR 20000511AP010](https://openairdocs.org/sdr/20000511AP010), Dec 8, 1999: SEAT TRACK. CORRODED. FOUND CABIN TRACK STATION 360 TO 420 RBL 24 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 2 FOUND OUT OF LIMITS. FABRICATES SEAT TRACK IAW 51-10-1. TREATED - [SDR 20000511AP009](https://openairdocs.org/sdr/20000511AP009), Dec 8, 1999: SEAT TRACK. CORRODED. CABIN FLOORBEAM STATION 320 LBL 46 HAS CORROSION AT ANCHOR NOT. REMOVED CORROSION IAW 51-10-6 PAGE 12. ACCOMPLISHED UT THICKNESS CHECK FOUND OUT OF LIMITS. CUT - [SDR 20000511AP008](https://openairdocs.org/sdr/20000511AP008), Dec 8, 1999: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK LBL 44 STATION 1110 TO 1070 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-10-6 PAGE 6. REMVOED SEAT TRACK IAW 51-30-2 PAGE - [SDR 20000511AP007](https://openairdocs.org/sdr/20000511AP007), Dec 8, 1999: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK STATION 1070 LBL 50 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-30-2 PAGE 2. REMOVED HAT CHANNEL STATION 1070 LBL 50 IAW - [SDR 20000511AP006](https://openairdocs.org/sdr/20000511AP006), Dec 8, 1999: STRAP. CRACKED. FOUND .03125 INCH CRACK AT RIGHT WING FIXED LEADING EDGE AT AFT INBOARD END OF CUTOUT WHERE NR 5 SLAT INBOARD HOOK GOES INTO. REMOVED FASTENERS IAW 51-30-2 PAGE - [SDR 20000511AP005](https://openairdocs.org/sdr/20000511AP005), Dec 8, 1999: HINGE. CRACKED. FOUND .3125 INCH CRACK AT CUT OUT ON TOP OF LEFT WING FOR NR 4 SPOILER 2ND FROM OUTBOARD HINGE. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC INSPECTION CONFIRME - [SDR 20000511AP004](https://openairdocs.org/sdr/20000511AP004), Dec 8, 1999: SEAT TRACK. CORRODED. CABIN SEAT TRACK STATION 344 TO 400 LBL 44 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 53-10-1 FIG 3. FABRICATED SEAT TRACK IAW 51-30-5 PAGE 1. TRE - [SDR 20000511AP003](https://openairdocs.org/sdr/20000511AP003), Dec 8, 1999: SEAT TRACK. CRACKED. CABIN SEAT TRACK STATION 344-400 LBL 24 HAS CORROSION. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS IAW 51-10-6 PAGE 12. FABRICATED NEW SEAT TRACK STATI - [SDR 20000511AP002](https://openairdocs.org/sdr/20000511AP002), Dec 8, 1999: ANGLE. CRACKED. FLAP FAIRING SUPPORT ANGLE HAS 1.125 INCH CRACK AT INBOARD SIDE OF LEFT WING NR 3 FLAP TRACK BELOW AFT FALSE SPAR AREA. REMOVED FAIRING, ACCOMPLISHED HFEC INSPE - [SDR 20000511AP001](https://openairdocs.org/sdr/20000511AP001), Dec 8, 1999: ANGLE. CRACKED. ANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATE - [SDR 20000510AP007](https://openairdocs.org/sdr/20000510AP007), Dec 8, 1999: SKIN. CRACKED. FOUND .4374 INCH CRACK THROUGH FASTENER HOLE AT RIGHT OUTBOARD FOREFLAP LEADING EDGE ABOVE NR 7 FLAP TRACK AREA. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 1. FABR - [SDR 20000510AP006](https://openairdocs.org/sdr/20000510AP006), Dec 8, 1999: RIB. CRACKED. FOUND .75 INCH CRACK AT RIGHT WING OUTBOARD MIDFLAP INBOARD MOST RIB AT LOWER AFT END. REMOVED JACKSCREW FAIRING. FABRICATED SINGLE REPAIR IAW 57-50-2 PAGE 5. H - [SDR 20000510AP005](https://openairdocs.org/sdr/20000510AP005), Dec 8, 1999: SKIN. CRACKED. FOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION A - [SDR 20000510AP004](https://openairdocs.org/sdr/20000510AP004), Dec 8, 1999: WEB. CRACKED. FOUND 1.75 INCH CRACK AT LEFT WING OUTBOARD MID FLAP INBOARD MOST RIB AT LOWER AFT END. STOP DRILLED CRACK IAW SRM 51-10-1. FABRICATED WEB REPAIR IAW 51-40-2 PA - [SDR 99ZZZX2824](https://openairdocs.org/sdr/99ZZZX2824), Jul 16, 1999: TRACK. CORRODED. LOG PAGE 25775. DURING INSPECTION OF AREA DUE TO REMOVAL OF FLAP FOR GROUND DAMAGE, FOUND SHIMS MIGRATED ON PAD A. REMOVED TRACK TO REPLACE. REMOVED AND REPLACE - [SDR 99ZZZM381](https://openairdocs.org/sdr/99ZZZM381), Jun 7, 1999: LAMP. DISCONNECTED. ON PREFLIGHT TRANSIT, FOUND EPL TRACK LIGHTS BETWEEN ROW 17-18C INOPERATIVE. RECONNECTED EPL LIGHTS IAW 33-50-0. OPS CHECKED OK. (M) - [SDR 98ZZZM878](https://openairdocs.org/sdr/98ZZZM878), Oct 27, 1998: BATTERY PACK. DISCHARGED. DURING PREFLIGHT, FOUND EXTERIOR EMERGENCY LIGHT, MOST AFT ON LEFT FAIRING INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-50-22. OPS CHECK OK. (M) - [SDR 98ZZZX3400](https://openairdocs.org/sdr/98ZZZX3400), Aug 26, 1998: LIGHT. INOPERATIVE. ON PRE-FLIGHT TRANSIT, FOUND EPL LIGHT INOPERATIVE FROM ROWS 1-4; ALSO, L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. TROUBLESHOT SYSTEM. FOUND POWER CABLE ASSEMBLY - [SDR MYWA970032](https://openairdocs.org/sdr/MYWA970032), Jul 17, 1997: BULB. FAILED. RIGHT AFT EMERGENCY EXIT SIGN - AFT BULB OUT. RELAMPED. OPS CHECK GOOD PER B727 MM 33-50-1. (X) - [SDR MYWA970008](https://openairdocs.org/sdr/MYWA970008), May 21, 1997: TURBINE. FAILED. ON DESCENT WITH POWER APPROX 50 PERCENT, A MODERATE VIBRATION WAS FELT. WITH THRUST LEVER AT IDLE NO VIBRATION NOTE, HOWEVER, ON ACCELERATION VIBRATION INCREASE - [SDR 96ZZZX3977](https://openairdocs.org/sdr/96ZZZX3977), Jun 24, 1996: ACTUATOR. FAILED. LOG REPORT: GL521 AT MIA - RETURN FROM FLIGHT. AFTER TAKEOFF WHILE RETRACTING THE FLAPS FROM THE 5-DEGREE TO THE 2-DEGREE POSITIONS, THE LE FLAP AMBER INTRANSIT ## STCs that may be installed (OpenAirDocs) (116, first 50) 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 PA46-500TP) - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA12506NY](https://openairdocs.org/stc/SA12506NY): Installation of de-ice heaters (also known as horizontal tail heaters) and associated parts on the left hand and right hand of the horizontal stabilizer. Sterling Helicopter - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA04188NY](https://openairdocs.org/stc/SA04188NY): Installation of LAI CoolView Windshields and Windows. Lee Aerospace Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA11893IB](https://openairdocs.org/stc/SA11893IB): Installation of the Pratt & Whitney PT6A-135A engine. MT-Propeller Entwicklung GmbH - [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International 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 - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [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 SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA01705WI](https://openairdocs.org/stc/SA01705WI): Installation of the Garmin G950 Integrated Flight Deck Installation. Aeronautix LLC - [STC SA01834WI](https://openairdocs.org/stc/SA01834WI): Installation of a modified Climate Control System. Cutter Aviation Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA01050DE](https://openairdocs.org/stc/SA01050DE): Installation of aircraft main battery replacement. Concorde Battery Corporation - [STC SA01006WI-D](https://openairdocs.org/stc/SA01006WI-D): Installation of Bendix/King KMD 850 Multi-Function Display System and the optional Bendix/King KMH 980/KMH 880 Multi-Hazard Awareness Systems/KTA 870 Traffic Awareness System/KTA 970 Traffic Alert and Collision Avoidance System and KDR 510 VHF Datalink System. Honeywell International Inc - [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc - [STC SA02654SE](https://openairdocs.org/stc/SA02654SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approvaL. AeroMech Incorporated - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA01750SE](https://openairdocs.org/stc/SA01750SE): Fabrication and Installation of Dahlia Doubler. Fliegen Works Inc - [STC SA01751SE](https://openairdocs.org/stc/SA01751SE): Fabrication and Installation of Panida Doubler. Fliegen Works Inc - [STC SA01752SE](https://openairdocs.org/stc/SA01752SE): Fabrication and Installation of Panida Doubler. Fliegen Works Inc - [STC SA04364NY](https://openairdocs.org/stc/SA04364NY): Installation of Wheels & Brake System. Beringer Aero S.A.S - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02135SE](https://openairdocs.org/stc/SA02135SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data). Electronics International Inc - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA02276AK](https://openairdocs.org/stc/SA02276AK): Installation of AMSAFE Aviation Inflatable Restraints. AMSAFE Inc - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC All 116: https://openairdocs.org/aircraft/N889MA/stcs.md ## Related - Other Piper PA46-500TP aircraft: https://openairdocs.org/model/piper-pa46-500tp/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.