# N971AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55032
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 13, 2001
- Certificate issued: February 2, 2024
- Expires: February 28, 2031
- Mode S code: AD876E
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, 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=971AT
- Page: https://openairdocs.org/aircraft/N971AT

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 Rolls-Royce BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (Rolls-Royce BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N971AT/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations

None matched to N971AT.

## FAA accident and incident reports

None matched to N971AT.

## Service difficulty reports (229, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2026092405329](https://openairdocs.org/sdr/DALA2026092405329), Sep 24, 2026: BRACKET. LOOSE. R1 GIRT BAR DISARM BRACKET LOOSE, REMOVED & REINSTALLED SLIDE IAW W/C 2561-9005 AND R & R EVACUATION SLIDE COMPARTMENT DOOR IAW AMM 52-42. (9504750) (AIRCRAFT G
- [SDR DALA2026012700605](https://openairdocs.org/sdr/DALA2026012700605), Dec 7, 2025: HINGE FITTING. CORRODED. CORROSION ON HARWARE AND AROUND OF BORE IN OTBD HINGE. LT WING FLAP. THE OTBD FLAP HINGE WAS REPLACED IAW AMM 57-55-25. (1340373)
- [SDR DALA2025121009009](https://openairdocs.org/sdr/DALA2025121009009), Dec 5, 2025: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN ON BS 1037 & 1022, L12R & L14R AT RH FUSELAGE. DAMAGED AREA REPAIRED PER ER/A 630558-14 REV.ORIG. (1337089)
- [SDR DALA2025120808960](https://openairdocs.org/sdr/DALA2025120808960), Dec 1, 2025: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BS 1037, BTW L-14L AND L-13L. FUSELAGE SKIN BS 1037 BTW L-14L AND L-13L WAS REPAIRED IAW PRI 630562-14 REV 5 AND ER/ A 630562-14 REV. (13
- [SDR DALA2025112408546](https://openairdocs.org/sdr/DALA2025112408546), Nov 24, 2025: SKIN. CRACKED. AIRCRAFT 9533, CRACK ON PANEL UPPER SKIN AREA STA Y= 1142 OF LH AND RH PYLON. CORRECTIVE ACTION: PANEL UPPER SKIN AREA STA Y= 1142 OF LH AND RH PYLON WERE REPAI
- [SDR DALA2025061604511](https://openairdocs.org/sdr/DALA2025061604511), Jun 16, 2025: WIRE. BROKEN. AIRCRAFT 9533, EMER EXIT SIGN FWD OF PAX DOOR LOWER INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT CONNECTOR OF EMER EXIT LIGHT. REPAIRED CONNECTOR IAW 717 SWPM 
- [SDR DALA2025062504755](https://openairdocs.org/sdr/DALA2025062504755), May 25, 2025: DRAIN VALVE. LEAKING. AFT BAG BIN HAS FUEL SMELL. FOUND FUEL DRAIN FROM FUEL SHROUD DRAIN VALVE BEHIND RT WHEEL WELL. CLEANING BELOW FLOOR. CHECK GOOD (6811338)
- [SDR DALA2025020500883](https://openairdocs.org/sdr/DALA2025020500883), Feb 5, 2025: LAMP. FAILED. THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS DIM WITH THE SWITCH OFF. THE SYSTEM WAS DEFERRED PER MEL 33-51-02A AND PLACARDS WERE INSTALLED. MAINTENANCE VERIFIE
- [SDR DALA2023120409902](https://openairdocs.org/sdr/DALA2023120409902), Dec 2, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00095: PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1) WAS 
- [SDR DALA2023112909803](https://openairdocs.org/sdr/DALA2023112909803), Nov 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMPARTMENT (C1). SUMMARY OF NRC 00730: CORROSION LEVEL 2. LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMP
- [SDR DALA2023112909800](https://openairdocs.org/sdr/DALA2023112909800), Nov 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON WING BOX UPPER SURFACE STA Y=684 X=-59. SUMMARY OF NRC 00398: CORROSION LEVEL 2. WING BOX UPPER SKIN SURFACE STA Y=684 X=-59 WAS REPAIRED PER ER/A 
- [SDR DALA2023112809757](https://openairdocs.org/sdr/DALA2023112809757), Nov 27, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN (2 EA) AFT UPPER SIDE BEAM 5, STA Y 425 APROX FWD UPPER SIDE STA Y 389 APROX (HINGE DOOR) AT FWD CARGO DOOR. SUMMARY OF NRC 00137: PAN AFT UPPER SI
- [SDR DALA2023112809754](https://openairdocs.org/sdr/DALA2023112809754), Nov 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON HOLE UPPER SURFACE NBR 28 AT RH HORIZONTAL STABILIZER CENTER BOX PLATE. SUMMARY OF NRC 00492: CORROSION LEVEL 2. HOLE UPPER SURFACE NBR 28 AT RH HO
- [SDR DALA2023112709721](https://openairdocs.org/sdr/DALA2023112709721), Nov 23, 2023: UNKNOWN. UNKNOWN. CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00706: CRACK ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT INNER
- [SDR DALA2023112009517](https://openairdocs.org/sdr/DALA2023112009517), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION (SEVERAL PLACES) ON TIE TRACK UPPER AND LOWER FACE BTW LONGERONS 27 TO 28 LH/RH BTW STA 817 TO STA=946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00357:
- [SDR DALA2023111609442](https://openairdocs.org/sdr/DALA2023111609442), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT CARGO (C2). SUMMARY OF NRC 00160: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT 
- [SDR DALA2023111609440](https://openairdocs.org/sdr/DALA2023111609440), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT IN REF TO NRC 00254. SUMMARY OF NRC S/N 00654: CORROSION LEVEL 2. FRAME AT STA 889.0
- [SDR DALA2023111609438](https://openairdocs.org/sdr/DALA2023111609438), Nov 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON UPPER SKIN STA XOS 395 AT RH WING. SUMMARY OF NRC 00080: CORROSION LEVEL 2. UPPER SKIN STA XOS 395 AT RH WING WAS REPAIRED PER ER/A 612778-14 REV O
- [SDR DALA2023111409354](https://openairdocs.org/sdr/DALA2023111409354), Nov 14, 2023: UNKNOWN. UNKNOWN. CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00707: CRACK ON INNER SKIN ON UPPER AFT CORNER AT LH SLIDING WINDO
- [SDR DALA2023111309306](https://openairdocs.org/sdr/DALA2023111309306), Nov 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO (C1). SUMMARY OF NRC 00222: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO 
- [SDR DALA2023111309305](https://openairdocs.org/sdr/DALA2023111309305), Nov 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON UNION SKIN BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00702: CORROSION LEVEL 2. UNION SKIN (FINGER DOUBLER) BTW
- [SDR DALA2023111309300](https://openairdocs.org/sdr/DALA2023111309300), Nov 10, 2023: UNKNOWN. UNKNOWN. EXFOLIATION UPPER SKIN OF CENTRAL TANK ON REAR SPAR AREA STA Y=748 AND STA XCW 1 TO 3, XCW 24 TO 26, ALSO XCW 42 TO 52 APROX AT LH MLG WHELLWELL. SUMMARY OF NRC
- [SDR DALA2023111309299](https://openairdocs.org/sdr/DALA2023111309299), Nov 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL) BTW STA 851-870 LONG 28L IN REF TO NRC 00671. SUMMARY OF NRC 00705
- [SDR DALA2023111309297](https://openairdocs.org/sdr/DALA2023111309297), Nov 9, 2023: UNKNOWN. UNKNOWN. CORROSION SKIN WEB STA=201 BTW LONG 18LH TO 17LH ALSO CORROSION ON HORIZONTAL STRAP BTW STA Y=201-208 AT PAX CABIN. SUMMARY OF NRC 00674: CORROSION LEVEL 2. SKI
- [SDR DALA2023110609115](https://openairdocs.org/sdr/DALA2023110609115), Nov 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK X=-44 BTW STA 218 TO STA 237 AT PAX CABIN. SUMMARY OF NRC 00553: CORROSION LEVEL 2. SEAT TRACK AT X=-44 BTW Y=200 TO 341 WAS DRILLED, AD
- [SDR DALA2023110108978](https://openairdocs.org/sdr/DALA2023110108978), Nov 1, 2023: UNKNOWN. UNKNOWN. WEAR AND CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=674 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00678: CORROSION LEVEL2. FLOOR SUPPORT STA Y=674 AND X=56 AT PAX C
- [SDR DALA2023110108977](https://openairdocs.org/sdr/DALA2023110108977), Oct 31, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1037 LONGERON 17 LH AT CPAX (W2). SUMMARY OF NRC 00407: FRAME STA 1037 LONGERON 17 LH AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R RE
- [SDR DALA2023110108975](https://openairdocs.org/sdr/DALA2023110108975), Oct 31, 2023: UNKNOWN. UNKNOWN. HFEC INSPECTION WAS PERFORMED ON UPPER RADIUS OF THE FRAME TAB STA Y=715 AND 01 CRACK WAS FOUND OF 0.097IN. PER CARD 5310-01436-04B. STEP 13. SUMMARY OF NRC 001
- [SDR DALA2023103108930](https://openairdocs.org/sdr/DALA2023103108930), Oct 30, 2023: UNKNOWN. UNKNOWN. DENT ON PREVIOUS REPAIR AT LH AFT MOVABLE FLAP VANE. SUMMARY OF NRC 00539: LH AFT MOVABLE FLAP VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1, 51-70-02-2R-3, 
- [SDR DALA2023103108929](https://openairdocs.org/sdr/DALA2023103108929), Oct 30, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON WEB BTW STA Y=715 TO 756 X=44 TO X=60. SUMMARY OF NRC 00601: WEB BTW STA Y=715 TO 756 X=44 TO X=60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R 
- [SDR DALA2023103008883](https://openairdocs.org/sdr/DALA2023103008883), Oct 30, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN. SUMMARY OF NRC 00393: CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN WAS MANUFACTURED AND REPAIRED PER DG
- [SDR DALA2023103008881](https://openairdocs.org/sdr/DALA2023103008881), Oct 29, 2023: UNKNOWN. UNKNOWN. WEAR AND DENT ON RH LOWER ANGLE NEAR TO LOWER HINGE AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00110: RH LOWER ANGLE NEAR TO LOWER HINGE
- [SDR DALA2024022002331](https://openairdocs.org/sdr/DALA2024022002331), Oct 28, 2023: HINGE. CORRODED. CORROSION WAS FOUND AT HINGE HOLES AT LH WING. SUMMARY NRC 00598: FLAP HINGE WAS REPLACED PER B717-200 AMM 57-55-25 AND EFECTIVITY WAS VERIFIED PER B717-200 IPC
- [SDR DALA2023103008880](https://openairdocs.org/sdr/DALA2023103008880), Oct 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH FLOOR SUPPORTS BTW STA 160 TO STA 196 BTW X=43, STA 196 TO STA 200 BTW X=53. SUMMARY OF NRC 00683: CORROSION LEVEL 2. FLOOR SUPPORT STA 160 TO S
- [SDR DALA2023103008879](https://openairdocs.org/sdr/DALA2023103008879), Oct 28, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2). SUMMARY OF NRC 00408: FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2) WAS REPAIRED PER B717-200 SRM-53-20-07
- [SDR DALA2023103008878](https://openairdocs.org/sdr/DALA2023103008878), Oct 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON SUPPORT BTW STA Y=1056-1022 X=-54 AT CPAX. SUMMARY OF NRC 00672: CORROSION LEVEL 2. SUPPORT BTW STA Y=1056-1022 X=-54 WAS FABRICATED AND REPLACED P
- [SDR DALA2023102708864](https://openairdocs.org/sdr/DALA2023102708864), Oct 26, 2023: UNKNOWN. UNKNOWN. WEAR ON PAN STA 954 AND 990 BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2. SUMMARY OF NRC 00134: INNER PAN ON STA 954 AND 990 BET
- [SDR DALA2023102608796](https://openairdocs.org/sdr/DALA2023102608796), Oct 25, 2023: UNKNOWN. UNKNOWN. CRACK ON INNER PAN (2 EA) BEAM 5 UPPER FWD SIDE, BEAM 3 AFT SIDE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00146: INNER PAN (2 EA) ON BEAM 5 UPPER FWD SIDE 
- [SDR DALA2023102508760](https://openairdocs.org/sdr/DALA2023102508760), Oct 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB, BOTH SIDES, BTW STA 178 TO STA 218, BTW X=-44 AND -52 RH SIDE AT CPAX. SUMMARY OF NRC 00366: CORROSION LEVEL 2. CUSP WEB BTW STA 178 TO STA 21
- [SDR DALA2023102308702](https://openairdocs.org/sdr/DALA2023102308702), Oct 19, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB STA 636 AND X=50 AT CPAX. SUMMARY OF NRC 00396: CUSP WEB WAS REPAIRED PER B717 SRM 51-70-10 2R PROCEDURE 2 PAR 4. (LP #0025277)
- [SDR DALA2023102008642](https://openairdocs.org/sdr/DALA2023102008642), Oct 19, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB STA Y=341 WAS FOUND AFTER SEAT TRACK STA Y=-44 REMOVAL. SUMMARY OF NRC 00606: CUSP WEB STA Y=-44 STA Y=341 WAS REPAIRED PER B717-200 SRM 53-00
- [SDR DALA2023102008638](https://openairdocs.org/sdr/DALA2023102008638), Oct 18, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB (BELOW) BTW STA Y=252 AND X=-46 AT CABIN PAX. SUMMARY OF NRC 00390: CUSP WEB STA Y=252 AND X=-46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-R
- [SDR DALA2023071805820](https://openairdocs.org/sdr/DALA2023071805820), Jul 18, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE DAMAGE LOCATED ON STATION 1166, LH SIDE OF FUSELAGE. (LABELED #7) COMPLIED WITH ER/A 610530-14 REV ORIG. ALL PRI REVISION INSTRUCTIONS ARE COMP
- [SDR DALA2023071705782](https://openairdocs.org/sdr/DALA2023071705782), Jul 17, 2023: UNKNOWN. UNKNOWN. LIGHTNING STRIKE DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L. (LABELED #1) REPAIRED SKIN DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L PER B717 SR
- [SDR DALA2022061604217](https://openairdocs.org/sdr/DALA2022061604217), Jun 14, 2022: POWER SUPPLY. INOPERATIVE. THE LEFT AFT OVERWING EXIT ILLUMINATOR IS INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EXIT POWER SUPPLY. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51-0
- [SDR DALA2022061604218](https://openairdocs.org/sdr/DALA2022061604218), Jun 13, 2022: ANTI-SKID SYS. WARNING MESSAGE. SHIP 9533 - DUE TO THE "ANTI-SKID FAIL" MESSAGE CYCLING ON & OFF AT LEAST THREE TIMES ON APPROACH, A GO-AROUND WAS EXECUTED. THE MESSAGE HAPPENED AGAIN ON THE S
- [SDR DALA2022061604219](https://openairdocs.org/sdr/DALA2022061604219), Jun 12, 2022: ANTI-SKID SYS. WARNING MESSAGE. SHIP 9533 - WHILE ON APPROACH, THE CREW NOTICED THE "ANTI-SKID FAIL" MESSAGE WAS CYCLING ON & OFF. A GO-AROUND WAS EXECUTED, BUT MESSAGE PERSISTED SO AN EMERGEN
- [SDR DALA2022051903435](https://openairdocs.org/sdr/DALA2022051903435), May 17, 2022: NONE. NONE. SHIP 9533 - THE CREW DECLARED AN EMERGENCY FOR AN ANTI-SKID FAIL MESSAGE ON FINAL APPROACH. THE QRH WAS COMPLIED WITH, AND ON THE NEXT APPROACH, THE FAILURE MES
- [SDR DALA2021121607776](https://openairdocs.org/sdr/DALA2021121607776), Dec 14, 2021: NONE. NONE. SHIP 9533 - THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE "RT GEAR UNSAFE" INDICATION ILLUMINATING SHORTLY AFTER TAKEOFF. ON APPROACH, THE GEAR WAS SELECTED 
- [SDR DALA2021111206965](https://openairdocs.org/sdr/DALA2021111206965), Nov 11, 2021: NONE. NONE. THE OVERHEAD CABIN CEILING EMERGENCY LIGHTS ARE OUT AT ROWS 1-4 AND 10-13CDE. MAINTENANCE REPLACED THE BATTERY PACK AT 10CDE PER B717 AMM 33-51. THE EMERGENCY L

All 229: https://openairdocs.org/aircraft/N971AT/reports.md

## STCs that may be installed (OpenAirDocs) (71, 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 (Boeing 717-200)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04122AT](https://openairdocs.org/stc/ST04122AT): Installation of an oven. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST04816NY](https://openairdocs.org/stc/ST04816NY): Installation of Electronically Steerable (ESA) Antenna and Power Supply. ALOFT AeroArchitects
- [STC ST12026AT](https://openairdocs.org/stc/ST12026AT): Installation of Portable Emergency Locator Transmitter. Delta Flight Products LLC
- [STC ST02478NY](https://openairdocs.org/stc/ST02478NY): Installation of an advertisement container on the bottom of a seat back tray table on Weber Model 5300 passenger seats (Weber Part Numbers 852454, 852455, 852456, 852457, 852458, and 852459). Atin OOH, LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST04813NY](https://openairdocs.org/stc/ST04813NY): Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System. ALOFT AeroArchitects
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST03682AT](https://openairdocs.org/stc/ST03682AT): Installation of an Aircell Broadband Service (ABS) Passenger Cabin Air-To-Ground (ATG) Voice/Data Communication System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST11388DS](https://openairdocs.org/stc/ST11388DS): Expansion of the Delta Comfort+® Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02637AT](https://openairdocs.org/stc/ST02637AT): Installation of SafTGlo Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST04416AT](https://openairdocs.org/stc/ST04416AT): Installation of the Rockwell Collins Multi-Mode Receiver (MMR). Woven Electronics LLC
- [STC ST04418AT](https://openairdocs.org/stc/ST04418AT): Installation of the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST01465LA-D](https://openairdocs.org/stc/ST01465LA-D): Installation of B/E Aerospace, Inc. Air Chiller Part Number 374-8. B/E Aerospace Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01096SE](https://openairdocs.org/stc/ST01096SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST01640SE](https://openairdocs.org/stc/ST01640SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST03418NY](https://openairdocs.org/stc/ST03418NY): Installation of a UTC Electronic Flight Bags. Rockwell Collins Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04029CH](https://openairdocs.org/stc/ST04029CH): Modification of an existing Aircell Broadband Services (ABS) System with ATG4 Enhancements. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST04468NY](https://openairdocs.org/stc/ST04468NY): Installation of Honeywell ADS-B Transponder Upgrade. H4 Aerospace (UK) Ltd
- [STC ST02152LA](https://openairdocs.org/stc/ST02152LA): Installation of AmSafe Aviation Inflatable Restraint (AAIR) System. AMSAFE Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04167NY](https://openairdocs.org/stc/ST04167NY): Installation of TCAS System upgrade to Change 7.1. H4 Aerospace (UK) Ltd
- [STC ST03846NY](https://openairdocs.org/stc/ST03846NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST04242CH](https://openairdocs.org/stc/ST04242CH): Installation of ACSS Automatic Dependent Surveillance-Broadcast (ADS-B) compliant Mode S Transponders. Canard Aerospace Corporation
- [STC ST04186CH](https://openairdocs.org/stc/ST04186CH): Retrofit installation of Rosemount Aerospace Model 0861EW2 Angle of Attack (AOA) Sensors. Rosemount Aerospace Inc
- [STC ST02479SE](https://openairdocs.org/stc/ST02479SE): Installation of class dividers and cross aisle curtain headers. Northwest Aerospace Technologies Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST02991AT](https://openairdocs.org/stc/ST02991AT): Installation of LiveTV XM Satellite Radio System. Thales Avionics Inc
- [STC ST03449CH](https://openairdocs.org/stc/ST03449CH): Installation of LH and RH Passenger Window - STA 218 to STA 237. AAR Aircraft Services
- [STC ST04206AT](https://openairdocs.org/stc/ST04206AT): Interior reconfiguration. Delta Air Lines Inc
- [STC ST03442CH](https://openairdocs.org/stc/ST03442CH): Installation of New Interior Arrangement. AAR Aircraft Services
- [STC ST03817AT](https://openairdocs.org/stc/ST03817AT): Installation of a Thales-KANNAD Emergency Locator Transmitter. Avionics Support Group Inc

All 71: https://openairdocs.org/aircraft/N971AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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