# N61SW: 2011 Socata TBM 700

- Status: Valid registration
- Airframe: [Socata TBM 700](https://openairdocs.org/model/socata-tbm-700) (registry code 8682000, 7 seats)
- Engine: [Pratt & Whitney Canada PT6A-66 series](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66-series) (registry code 52118)
- Data sheets: [TCDS A60EU](https://openairdocs.org/tcds/A60EU) (Daher Aircraft SAS), [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 560
- Year built: 2011
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: March 9, 2011
- Certificate issued: September 14, 2026
- Expires: September 30, 2033
- Mode S code: A7EE0A
- Registered owner: [Flight Contract Services Inc](https://openairdocs.org/faa-owner/FLIGHT%20CONTRACT%20SERVICES%20INC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.1968° N, 115.2644° W: Placed by OpenAirDocs at the center of ZIP code 89128, 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=61SW
- Page: https://openairdocs.org/aircraft/N61SW

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. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-66 model are included.

## ADs that may apply (OpenAirDocs): 57 in force

### Matched by airframe (Socata TBM 700)

- [AD 2025-26-02](https://openairdocs.org/ad/2025-26-02): Vertical Stabilizer Structure · Daher Aerospace TBM 700. Effective Feb 12, 2026
- [AD 2025-02-08](https://openairdocs.org/ad/2025-02-08): Fire Protection System · DAHER AEROSPACE TBM 700. Effective Mar 19, 2025
- [AD 2025-01-04](https://openairdocs.org/ad/2025-01-04): TE Flap Control System; TE Flap Actuator · DAHER AEROSPACE TBM 700. Effective Mar 11, 2025
- [AD 2023-11-12](https://openairdocs.org/ad/2023-11-12): Emergency Exits · DAHER AEROSPACE TBM 700. Effective Jul 21, 2023
- [AD 2021-25-10](https://openairdocs.org/ad/2021-25-10): Engine Oil System (Airframe) · Daher Aerospace TBM 700. Effective Jan 24, 2022
- [AD 2021-24-13](https://openairdocs.org/ad/2021-24-13): Cabin Pressure Control System · Daher Aerospace TBM700. Effective Jan 12, 2022
- [AD 2017-15-15](https://openairdocs.org/ad/2017-15-15): Flight Controls · SOCATA TBM 700. Effective Sep 6, 2017
- [AD 2015-17-10](https://openairdocs.org/ad/2015-17-10): Landing gear · SOCATA TBM 700. Effective Sep 29, 2015
- [AD 2014-09-03](https://openairdocs.org/ad/2014-09-03): Stabilizers · SOCATA TBM 700. Effective Jun 5, 2014
- [AD 2014-06-06](https://openairdocs.org/ad/2014-06-06): Landing Gear · SOCATA TBM 700. Effective May 2, 2014
- [AD 2012-10-14](https://openairdocs.org/ad/2012-10-14): Landing gear · SOCATA TBM 700. Effective Jul 23, 2012
- [AD 2011-27-09](https://openairdocs.org/ad/2011-27-09): Flight Controls · SOCATA TBM 700. Effective Feb 15, 2012
- [AD 2011-23-03](https://openairdocs.org/ad/2011-23-03): Navigation · SOCATA TBM 700. Effective Dec 6, 2011
- [AD 2011-17-06](https://openairdocs.org/ad/2011-17-06): Flight Controls · SOCATA TBM 700. Effective Sep 19, 2011
- [AD 2011-02-02](https://openairdocs.org/ad/2011-02-02): Air Conditioning. · SOCATA TBM 700. Effective Mar 1, 2011
- [AD 2010-23-28](https://openairdocs.org/ad/2010-23-28): Oxygen · SOCATA TBM 700. Effective Dec 29, 2010
- [AD 2010-11-15](https://openairdocs.org/ad/2010-11-15): Fire Protection · SOCATA TBM 700. Effective Jul 6, 2010
- [AD 2010-07-07](https://openairdocs.org/ad/2010-07-07): Towing and Taxiing · SOCATA TBM 700. Effective May 7, 2010
- [AD 2009-24-15](https://openairdocs.org/ad/2009-24-15): Electric power · SOCATA TBM 700. Effective Jan 4, 2010
- [AD 2007-03-17 R1](https://openairdocs.org/ad/2007-03-17-R1): Fuselage · SOCATA TBM 700. Effective Sep 9, 2009
- [AD 2009-08-09](https://openairdocs.org/ad/2009-08-09): Wiring harness · SOCATA TBM 700. Effective May 20, 2009
- [AD 2008-19-10](https://openairdocs.org/ad/2008-19-10): Movement of the emergency landing gear by-pass selector. · SOCATA TBM 700. Effective Oct 23, 2008
- [AD 2008-17-09](https://openairdocs.org/ad/2008-17-09): Alternator · SOCATA TBM 700. Effective Sep 23, 2008
- [AD 2008-03-15](https://openairdocs.org/ad/2008-03-15): Pilot door · SOCATA TBM 700. Effective Mar 11, 2008
- [AD 2007-23-07](https://openairdocs.org/ad/2007-23-07): Main landing gear wheel · SOCATA TBM 700. Effective Nov 28, 2007
- [AD 2007-21-10](https://openairdocs.org/ad/2007-21-10): Upper access door · SOCATA TBM 700. Effective Nov 21, 2007
- [AD 2007-09-07](https://openairdocs.org/ad/2007-09-07): Nose landing gear (NLG) · SOCATA TBM 700. Effective Jun 4, 2007
- [AD 2007-06-14](https://openairdocs.org/ad/2007-06-14): Propeller control cables · SOCATA TBM 700. Effective Apr 20, 2007
- [AD 2007-06-04](https://openairdocs.org/ad/2007-06-04): Flap carriage rollpins · SOCATA TBM 700. Effective Apr 19, 2007
- [AD 2007-05-18](https://openairdocs.org/ad/2007-05-18): Pulley brackets · SOCATA TBM 700. Effective Apr 12, 2007
- [AD 2007-03-16](https://openairdocs.org/ad/2007-03-16): Excessive lateral play caused by a nonconforming washer · SOCATA TBM 700. Effective Mar 15, 2007
- [AD 2007-02-08](https://openairdocs.org/ad/2007-02-08): Master cylinder yoke failure · SOCATA TBM 700. Effective Feb 26, 2007
- [AD 2006-22-11](https://openairdocs.org/ad/2006-22-11): Initial elevator trim actuator greasing · SOCATA TBM 700. Effective Dec 1, 2006
- [AD 2005-20-24](https://openairdocs.org/ad/2005-20-24): VHF1 antenna mounting area · SOCATA TBM 700. Effective Nov 9, 2005
- [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 2003-26-06](https://openairdocs.org/ad/2003-26-06): Safety Belts and Restraint Systems · Anjou Aeronautique Safety Belts and Restraint Systems, AS332C, AS332L and 14 more. Effective Feb 17, 2004
- [AD 2002-09-11](https://openairdocs.org/ad/2002-09-11): Attaching Bolt/Screw Threads of Inboard, Central, and Outboard Carriages · SOCATA TBM 700. Effective Jun 20, 2002
- [AD 2002-03-03](https://openairdocs.org/ad/2002-03-03): Strainer Draining System in the Cabin Fuselage · SOCATA TBM 700. Effective Mar 29, 2002
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 2001-23-06](https://openairdocs.org/ad/2001-23-06): Fuel Tank Air Vent Valves · SOCATA TBM 700. Effective Dec 27, 2001
- [AD 2001-06-05](https://openairdocs.org/ad/2001-06-05): Oil Breather Vent · SOCATA TBM 700. Effective May 11, 2001
- [AD 2001-04-07](https://openairdocs.org/ad/2001-04-07): Control Cable · SOCATA TBM 700. Effective Apr 13, 2001
- [AD 2000-26-19](https://openairdocs.org/ad/2000-26-19): Fuel Tank Air Vent Valve Hose · SOCATA TBM 700. Effective Feb 2, 2001
- [AD 2000-02-29](https://openairdocs.org/ad/2000-02-29): Airframe Pneumatic Deicing Boots · SOCATA TBM 700. Effective Mar 27, 2000
- [AD 98-24-04](https://openairdocs.org/ad/98-24-04): Flap Carriage · SOCATA TBM 700. Effective Dec 28, 1998
- [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 98-21-15](https://openairdocs.org/ad/98-21-15): Oxygen Generators · SOCATA TBM 700. Effective Nov 20, 1998
- [AD 98-12-02](https://openairdocs.org/ad/98-12-02): Elevator Trim Tab Fittings · SOCATA TBM 700. Effective Jul 17, 1998
- [AD 98-08-27](https://openairdocs.org/ad/98-08-27): Left-Hand Wheel Assembly · SOCATA TBM 700 with STC SA2786CE. Effective May 31, 1998
- [AD 98-04-04](https://openairdocs.org/ad/98-04-04): Starter Generator Mounting Adapter · SOCATA TBM 700. Effective Mar 24, 1998

### Matched by engine (Pratt & Whitney Canada PT6A-66 series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [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
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997

### Historical (superseded or no longer in force)

- [AD 2009-23-12](https://openairdocs.org/ad/2009-23-12) (historical): Oxygen · SOCATA TBM 700. Effective Dec 18, 2009
- [AD 2009-13-05](https://openairdocs.org/ad/2009-13-05) (historical): Oxygen · SOCATA TBM 700. Effective Jul 9, 2009
- [AD 2008-19-06](https://openairdocs.org/ad/2008-19-06) (historical): Replacement of the pulley drive assembly by a new one of an improved design. · SOCATA TBM 700. Effective Oct 8, 2008
- [AD 2008-10-13](https://openairdocs.org/ad/2008-10-13) (historical): Alternator and vapour cycle cooling system · SOCATA TBM 700. Effective May 29, 2008
- [AD 2007-06-11](https://openairdocs.org/ad/2007-06-11) (historical): Vertical stabilizer attachment fitting · SOCATA TBM 700. Effective Apr 20, 2007
- [AD 2007-04-13](https://openairdocs.org/ad/2007-04-13) (historical): Main landing gear cylinders · SOCATA TBM 700. Effective Mar 23, 2007
- [AD 2007-04-08](https://openairdocs.org/ad/2007-04-08) (historical): Pilot door locking stop-fittings · SOCATA TBM 700. Effective Mar 23, 2007
- [AD 2007-03-17](https://openairdocs.org/ad/2007-03-17) (historical): Loose rivets on frames C18 BIS and C19 · SOCATA TBM 700. Effective Mar 15, 2007
- [AD 2002-19-01](https://openairdocs.org/ad/2002-19-01) (historical): Flight  Control System · SOCATA TBM 700. Effective Oct 29, 2002
- [AD 2001-05-03](https://openairdocs.org/ad/2001-05-03) (historical): Flap Attaching Bolts/Screws · EADS SOCATA TBM 700. Effective Apr 27, 2001
- [AD 99-07-11](https://openairdocs.org/ad/99-07-11) (historical): Outboard Hinge Fittings of Horizontal Stabilizer · SOCATA TBM 700. Effective Apr 16, 1999

All 68: https://openairdocs.org/aircraft/N61SW/ads.md

## Information bulletins (advisory) (17 in force)

- [SAIB CE-16-12](https://openairdocs.org/saib/CE-16-12): AUTO FLIGHT - Autopilot. Issued Jan 25, 2016
- [SAIB CE-07-07](https://openairdocs.org/saib/CE-07-07): Anchor Nuts. Issued Oct 27, 2006
- [SAIB CE-06-61](https://openairdocs.org/saib/CE-06-61): . Issued Aug 11, 2006
- [SAIB CE-06-60](https://openairdocs.org/saib/CE-06-60): . Issued Aug 11, 2006
- [SAIB CE-05-62](https://openairdocs.org/saib/CE-05-62): . Issued Jun 27, 2005
- [SAIB CE-04-61](https://openairdocs.org/saib/CE-04-61): . Issued Apr 12, 2004
- [SAIB CE-04-27](https://openairdocs.org/saib/CE-04-27): . Issued Dec 4, 2003
- [SAIB CE-04-26](https://openairdocs.org/saib/CE-04-26): . Issued Dec 4, 2003
- [SAIB CE-04-25](https://openairdocs.org/saib/CE-04-25): . Issued Dec 4, 2003
- [SAIB CE-04-20](https://openairdocs.org/saib/CE-04-20): . Issued Nov 20, 2003
- [SAIB CE-04-19](https://openairdocs.org/saib/CE-04-19): . Issued Nov 14, 2003
- [SAIB CE-04-16](https://openairdocs.org/saib/CE-04-16): . Issued Nov 12, 2003
- [SAIB CE-03-01](https://openairdocs.org/saib/CE-03-01): . Issued Oct 8, 2002
- [SAIB CE-02-44](https://openairdocs.org/saib/CE-02-44): . Issued Sep 4, 2002
- [SAIB CE-02-27](https://openairdocs.org/saib/CE-02-27): . Issued Apr 16, 2002
- [SAIB CE-01-02](https://openairdocs.org/saib/CE-01-02): . Issued Nov 3, 2000
- [SAIB ACE-98-37](https://openairdocs.org/saib/ACE-98-37): . Issued Jun 18, 1998

## NTSB investigations

None matched to N61SW.

## FAA accident and incident reports

None matched to N61SW.

## Reports on N61SW not matched to an aircraft (4)

They name N61SW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19960812030519I](https://openairdocs.org/incident/19960812030519I), Aug 12, 1996: Boeing 7372H4 (N61SW), Detroit, MI. Narrative: southwest airlines (swaa) N61SW 737-2H4 flight no. 1506, cleveland (cle) to chicago (mdw) 1124 ctc on 8/12/96. Fifty miles south of Detroit metro…
- [Incident 19860108003219I](https://openairdocs.org/incident/19860108003219I), Jan 8, 1986: Boeing 7372H4 (N61SW), Kansas City, MO. Returned after gear selector handle would not go beyond off position. Gear would not retract.
- [Incident 19830220011509I](https://openairdocs.org/incident/19830220011509I), Feb 20, 1983: Boeing 7372H4 (N61SW), Tulsa, OK, Minor damage. Nose and left main landing gear missed the paved taxiway. #1 engine received damage to the compressor.
- [Incident 19820713040439I](https://openairdocs.org/incident/19820713040439I), Jul 13, 1982: Boeing 737* (N61SW), Austin, TX. Engine shutdown when engine oil filter clog light came on. Found metal particles in oil filter.

## 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 N61SW not matched to an aircraft (53, newest 50)

They name N61SW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SWAA000680](https://openairdocs.org/sdr/SWAA000680), Apr 10, 2000: INDICATOR. DISLODGED. AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT VIEW. REPOSITIONED SLIDE ASSY PER MM.
- [SDR SWAA000465](https://openairdocs.org/sdr/SWAA000465), Mar 11, 2000: INTERCOSTAL. CRACKED. DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FWD SIDE NR 1 THROUGH NR 5 STOP FITTING INTERCOSTALS CRACKED. REMOVED AND REPLACED INTERCOSTALS PER SRM.
- [SDR SWAA000425](https://openairdocs.org/sdr/SWAA000425), Mar 6, 2000: SKIN. CRACKED. DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED UNDER SIDEWALL PANEL FWD OF AFT CARGO DOOR, BS 727A, STRINGER 25R. REPAIRED SKIN PER RA NR 1-253-2231.
- [SDR SWAA991779](https://openairdocs.org/sdr/SWAA991779), Oct 24, 1999: LIGHT. INOP. DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
- [SDR SWAA990689](https://openairdocs.org/sdr/SWAA990689), Apr 12, 1999: POWER SUPPLY. INOPERATIVE. DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT CONTROL CURCUIT BREAKER POPPED DURING ENGINE RUN. REMOVED AND REPLACED BATTERY POWER SUPPLY PER MM.
- [SDR SWAA990688](https://openairdocs.org/sdr/SWAA990688), Apr 12, 1999: SKIN. CRACKED. DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK AT FASTENER HOLE , LOWER ROW OF SKIN LAP AT BS 884, STRINGER 20R. REPAIRED SKIN PER SRM.
- [SDR SWAA990680](https://openairdocs.org/sdr/SWAA990680), Apr 10, 1999: FRAME. CORRODED. DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BS 1016 FRAME, BETWEEN STRINGERS 26L-26R. REPAIRED PER SRM.
- [SDR SWAA990531](https://openairdocs.org/sdr/SWAA990531), Mar 17, 1999: BATTERY PACK. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT OVERWING DOORS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
- [SDR SWAA990530](https://openairdocs.org/sdr/SWAA990530), Mar 17, 1999: FIRE LOOP. SHORTED. AIR TURNBACK DUE TO LEFT FIRE LIGHT ILLUMINATED ON CLIMB-OUT. AFTER LEFT OVERHEAT DETECTOR SWITCH WAS MOVED TO FIRE, THE LIGHT WENT OUT. ON ENGINES SHUT DOWN TH
- [SDR SWAA990254](https://openairdocs.org/sdr/SWAA990254), Feb 13, 1999: BATTERY BASE. INOP. DURING SCHEDULED SC CHECK, FOUND LT OVERWING EMERG LIGHTS ILLUMINATED WHEN POWER WAS SELECTED OFF. REMOVED AND REPLACED BATTERY BASE PER BOEING M/M.
- [SDR 98ZZZX4180](https://openairdocs.org/sdr/98ZZZX4180), Sep 23, 1998: SKIN. CRACKED. TEN CRACKED FASTENER HOLES FOUND ALONG STR 14R AT STA 908 - STA 951. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-222 DATED 9-8-98, AND BOEING 737 SRM 53-30-3
- [SDR 98ZZZX4178](https://openairdocs.org/sdr/98ZZZX4178), Sep 23, 1998: SKIN. CRACKED. SKIN CRACKED AT HINGE CUTOUTS ALONG STR 10L AND STR 10R, STA 908 - STA 951. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-220 DATED 9-8-98, AND BOEING 737 SRM 
- [SDR 98ZZZX4179](https://openairdocs.org/sdr/98ZZZX4179), Sep 22, 1998: SKIN. CRACKED. SIXTEEN CRACKED FASTENER HOLES FOUND ALONG STR 14L AT STA 908 - 951. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-221 DATED 9-8-98, AND BOEING 737 SRM 53-30-3
- [SDR SWAA970728](https://openairdocs.org/sdr/SWAA970728), Aug 15, 1997: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND A 4 INCH FUSELAGE SKIN CRACK AT BS 951, AT S24R. REPAIRED PER BOEING SRM.
- [SDR SWAA970503](https://openairdocs.org/sdr/SWAA970503), May 23, 1997: SKIN. CRACKED. DURING SCHEDULED TERMINAL CHECK, FOUND A 4 CRACK IN FUSELAGE SKIN AT BS 380. REPAIRED PER BOEING SRM.
- [SDR SWAA970393](https://openairdocs.org/sdr/SWAA970393), Apr 17, 1997: CONNECTOR. CORRODED. AT CRUISE, A BRIEF APU FIRE WARNING BELL SOUNDED WITH LIGHT, TWO DIFFERENT TIMES. INSPECTED AND FOUND FIRE LOOP CANNON PLUG IN APU TAIL CONE CORRODED. REPLACED 
- [SDR SWAA970136](https://openairdocs.org/sdr/SWAA970136), Jan 27, 1997: BATTERY. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.
- [SDR SWAA970137](https://openairdocs.org/sdr/SWAA970137), Jan 23, 1997: FIRE WARNING. ACTIVATED. AT GATE, APU FIRE WARNING ILLUMINATED AND BELL SOUNDED. ACTIVATED FIRE HANDLE AND DISCHARGED BOTTLE. INSPECTED WITH NO EVIDENCE OF FIRE OVERHEAT CONDITION, CONT
- [SDR SWAA970074](https://openairdocs.org/sdr/SWAA970074), Jan 16, 1997: BELTFRAME. CRACKED. DURING SCHEDULED C3 CHECK, FOUND BELTFRAME WEB CRACKED .5 INCH LONG AT BS 639, S18L. REPAIRED PER BOEING SRM.
- [SDR SWAA961179](https://openairdocs.org/sdr/SWAA961179), Oct 28, 1996: SKIN. CRACKED. DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED .25 AT AFT SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM.
- [SDR SWAA961118](https://openairdocs.org/sdr/SWAA961118), Oct 16, 1996: FLOORBEAM. CORRODED. DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, WL 208, RBL 3 TO 8. REPAIRED PER BOEING SRM.
- [SDR SWAA961117](https://openairdocs.org/sdr/SWAA961117), Oct 16, 1996: BATTERY. DISCHARGED. DURING SCHEDULED D-CHECK, FOUND FWD CENTER AISLE EMERGENCY LIGHT BATTERY PACK NOT CHARGING. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.
- [SDR SWAA961121](https://openairdocs.org/sdr/SWAA961121), Oct 15, 1996: FLOORBEAM. CORRODED. DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 1208, RBL 14, 26, 27 AND 32. REPAIRED PER BOEING SRM.
- [SDR SWAA961105](https://openairdocs.org/sdr/SWAA961105), Oct 12, 1996: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT S16L, BS 357, WL 217. REPAIRED PER BOEING SRM.
- [SDR SWAA961104](https://openairdocs.org/sdr/SWAA961104), Oct 12, 1996: SKIN. HOLE. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN HOLE AT BS 507, BETWEEN S2 AND 3L. REPAIRED PER BOEING SRM.
- [SDR SWAA961102](https://openairdocs.org/sdr/SWAA961102), Oct 12, 1996: CLIP. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, S14R. REPAIRED PER BOEING SRM.
- [SDR SWAA961101](https://openairdocs.org/sdr/SWAA961101), Oct 12, 1996: FLOORBEAM. CORRODED. DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 987, LBL 53, WL 208 AND AT BS 1006, WL 208, LBL 30. REPAIRED PER BOEING SRM.
- [SDR SWAA961100](https://openairdocs.org/sdr/SWAA961100), Oct 12, 1996: FLOORBEAM. CRACKED. DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED PER BOEING SRM.
- [SDR SWAA961099](https://openairdocs.org/sdr/SWAA961099), Oct 12, 1996: SUPPORT. CRACKED. DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 313 TO 329, LBL 46, WL 208. REPAIRED PER BOEING SRM.
- [SDR SWAA961098](https://openairdocs.org/sdr/SWAA961098), Oct 12, 1996: FRAME. DAMAGED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DAMAGED AT BS 312, 18 INCHES BELOW FWD AIRSTAIR DOOR OPENING. REPAIRED PER BOEING SRM.
- [SDR SWAA961097](https://openairdocs.org/sdr/SWAA961097), Oct 12, 1996: BULKHEAD. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 191 AND 201, LBL 5. REPAIRED PER BOEING SRM.
- [SDR SWAA961096](https://openairdocs.org/sdr/SWAA961096), Oct 12, 1996: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 400 S22 TO 23L, BS 420 S24 TO 25L, BS 500 S24 TO 25L, BS 500A S23 TO 24L, BS 500B 23 TO 24L, BS 50
- [SDR SWAA961095](https://openairdocs.org/sdr/SWAA961095), Oct 12, 1996: STIFFENER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STIFFENER CRACKED AT BS 540 PRESSURE BULKHEAD AT BS 540, LBL 25, WL 194. REPAIRED PER BOEING SRM.
- [SDR SWAA961094](https://openairdocs.org/sdr/SWAA961094), Oct 12, 1996: BULKHEAD ANGLE. CORRODED. DURING SCHEDULED D-CHECK, FOUND LOWER BULKHEAD ANGLE CORRODED AT BS 520, AT S26 LT AND RT. REPAIRED PER BOEING SRM.
- [SDR SWAA961093](https://openairdocs.org/sdr/SWAA961093), Oct 12, 1996: FLOORBEAM. CRACKED. DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR BEAM CRACKED AT BS 440 AND 500, ABOVE S27R. REPAIRED PER BOEING SRM.
- [SDR SWAA961092](https://openairdocs.org/sdr/SWAA961092), Oct 12, 1996: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1001, LBL 15, WL 170. REPAIRED PER BOEING SRM.
- [SDR SWAA961091](https://openairdocs.org/sdr/SWAA961091), Oct 12, 1996: SKIN. GOUGED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957, LBL 61, WL 182, AT BS 390 TO 410, RBL 33, WL 156, AND AT BS 251, RBL 27, WL 168. REPAIRED PER BO
- [SDR SWAA961090](https://openairdocs.org/sdr/SWAA961090), Oct 12, 1996: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR CUTOUT FRAME CRACKED AT AFT UPPER STOP FITTING. REPAIRED PER BOEING SRM.
- [SDR SWAA961086](https://openairdocs.org/sdr/SWAA961086), Oct 12, 1996: CLIPS. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER T-CLIPS CRACKED AT BS 400 S4R, BS 360 S5R AND AT BS 559 S17L. REPAIRED PER BOEING SRM.
- [SDR SWAA961031](https://openairdocs.org/sdr/SWAA961031), Sep 30, 1996: SEAL. OUT OF POSITION. RETURNED DUE TO FWD ENTRY DOOR SQUEALING VERY LOUD ON CLIMBOUT. REPOSITIONED FWD ENTRY DOOR SEAL AND PRESSURE TESTED PER BOEING M/M.
- [SDR SWAA960860](https://openairdocs.org/sdr/SWAA960860), Aug 22, 1996: BATTERY. DISCHARGED. DURING SCHEDULED SERVICE CHECK, FOUND CABIN AFT CEILING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M.
- [SDR SWAA960813](https://openairdocs.org/sdr/SWAA960813), Aug 12, 1996: FIRE DET MODULE. MALFUNCTIONED. DIVERTED TO DTW DUE TO NUMBER 2 ENGINE FIRE WARNING SOUNDING IN FLIGHT AND FIRE BOTTLES ACTIVATED. CREW PERFORMED ENGINE SHUTDOWN PROCEDURES. AIRCRAFT LANDED AT
- [SDR SWAA960605](https://openairdocs.org/sdr/SWAA960605), Jul 1, 1996: TR UNIT. INOPERATIVE. AFTER TAKEOFF, CREW EXPERIENCED T/R ISOLATION VALVE LIGHT ILLUMINATING. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED ENGINE ACCESSORY UNIT 
- [SDR SWAA960597](https://openairdocs.org/sdr/SWAA960597), Jun 27, 1996: FRAME. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND AIRSTAIR DOOR FRAME CRACKED UNDER FWD UPPER STOP. REPAIRED PER BOEING SRM.
- [SDR SWAA960596](https://openairdocs.org/sdr/SWAA960596), Jun 27, 1996: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE HAD 2 SKIN CRACKS AT BS 757 STRINGER 17L. REPAIRED PER BOEING SRM.
- [SDR SWAA950792](https://openairdocs.org/sdr/SWAA950792), Dec 20, 1995: PANEL. CRACKED. DURING SCHEDULED B-CHECK, FOUND NOSE GEAR WHEELWELL ACCESS PANEL OPENING CRACKED. REPAIRED PER BOEING SRM.
- [SDR SWAA0658](https://openairdocs.org/sdr/SWAA0658), Oct 10, 1995: ACTUATOR. MALFUNCTIONED. IN FLIGHT, EXPERIENCED NUMBER 4 L/E SLAT UNCOMMANDED DEPLOYMENT. AIRCRAFT DIVERTED TO LAS AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 4 L/E SLAT ACTUATOR.
- [SDR SWAA950566](https://openairdocs.org/sdr/SWAA950566), Jul 31, 1995: EEL BATTERY. DISCHARGED. DURING SCHEDULED A1 CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.
- [SDR SWAA950473](https://openairdocs.org/sdr/SWAA950473), Jun 19, 1995: FLOOR BEAM. CRACKED. DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0. REPAIRED PER BOEING STR.
- [SDR SWAA950088](https://openairdocs.org/sdr/SWAA950088), Jan 25, 1995: SKIN. CRACKED. DURING WALKAROUND INSPECTION, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L. A 2.25 INCH CRACK AT BS 814 S16L, AND A 2.75 INCH CRACK AT BS 831

All 53: https://openairdocs.org/aircraft/N61SW/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (86, 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 (Socata TBM 700)

- [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 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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA12408LA](https://openairdocs.org/stc/SA12408LA): Description of Type Design Change: Installation of Dedicated Gas Generator Case drain. Blackhawk Modifications, 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 SA12179DE](https://openairdocs.org/stc/SA12179DE): Replacement of the original Pratt and Whitney PT6A-64 engine with a Pratt and Whitney PT6A-66D engine. Blackhawk Modifications LLC
- [STC SA12024SE](https://openairdocs.org/stc/SA12024SE): Installation of Ram Air Cowling. American Aviation 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 SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA01572CH](https://openairdocs.org/stc/SA01572CH): Installation of a Honeywell KMH 880 and KTA 870 Multi-hazard Awareness and Traffic Advisory system. Amphenol Cable and Interconnect Technologies Inc
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA01596SE](https://openairdocs.org/stc/SA01596SE): Installation of Butterfield Industries Oil Residue Collection System, kit P/N BI 3401-1. Raisbeck Engineering Inc
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems 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 SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA00930WI-D](https://openairdocs.org/stc/SA00930WI-D): Installation of Bendix/King KMD 550/850 Multi-Function Display (MFD) system and optional Bendix/King KGP 560 General Aviation Enhanced ground proximity warning system (GA-EGPWS). Honeywell International Inc
- [STC SA2328CE-D](https://openairdocs.org/stc/SA2328CE-D): Installation of the Bendix/King KLN 88 Loran C system. Honeywell International Inc
- [STC SA01522WI-D](https://openairdocs.org/stc/SA01522WI-D): SERIAL NUMBERS up to and including 433 Excluding 269: Installation of the alternate part number EFS 40 SG 465 Symbol Generator. Honeywell International Inc
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [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 SA8107SW](https://openairdocs.org/stc/SA8107SW): Installation of Electrically Powered vapor cycle Air Conditioning System utilizing freon 12 or R134A refrigerant. Air Comm Corporation
- [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 SA02486LA](https://openairdocs.org/stc/SA02486LA): Replacement of Socata Leading Edge Assemblies and Pneumatic Deicer. SMR Technologies Inc
- [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 SA04263NY](https://openairdocs.org/stc/SA04263NY): Installation of Gogo Business Aviation ATG System. Maxcraft Avionics Ltd
- [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 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 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 SA2786CE](https://openairdocs.org/stc/SA2786CE): Installation of fuselage shell upholstery panels, window shade assemblies, cabinets, table, and seat upholstery. Textron Aviation 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 SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 2](https://openairdocs.org/stc/SA01933LA-D%20PAGE%202): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA03931AT-D](https://openairdocs.org/stc/SA03931AT-D): Installation of a Modified Battery Heat Shield. Socata North America 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 SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation
- [STC SA02717NY PAGE 2](https://openairdocs.org/stc/SA02717NY%20PAGE%202): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC

All 86: https://openairdocs.org/aircraft/N61SW/stcs.md

## Related

- Other Socata TBM 700 aircraft: https://openairdocs.org/model/socata-tbm-700/aircraft.md
- The Pratt & Whitney Canada PT6A-66 series engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66-series.md

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