# N981AT: 2002 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: 55040
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 22, 2002
- Certificate issued: April 8, 2024
- Expires: April 30, 2031
- Mode S code: ADAEED
- 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=981AT
- Page: https://openairdocs.org/aircraft/N981AT

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/N981AT/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 N981AT.

## FAA accident and incident reports

None matched to N981AT.

## Service difficulty reports (199, 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 DALA2026101905721](https://openairdocs.org/sdr/DALA2026101905721), Oct 18, 2026: SKIN. DENTED. FOUND DENT AT VERTICAL STABILIZER RUDDER TAP SKIN, BETWEEN ZRT=5.70 - 30.30, CORRECTIVE ACTION: COMPLIED WITH ER/A 637462-14. (1872819) (AICRAFT GROUNDED).
- [SDR DALA2026101605698](https://openairdocs.org/sdr/DALA2026101605698), Oct 15, 2026: SEALANT. MISSING. FOUND CRACKS ON SCUFF PLATE FWD/INBD EDGE AND CENTER SECTION OF AFT CARGO COMPARTMENT ALSO MISSING SEALANT ON SCUFF PLATE FWD CARGO COMPARTMENT, COMPLIED WITH E
- [SDR DALA2026101605697](https://openairdocs.org/sdr/DALA2026101605697), Oct 15, 2026: DOOR FRAME. DAMAGED. FOUND BENTS AND CRACKS ON AFT EDGE OF AFT CARGO DOOR CUTOUT AT Y=984 APPROX. BTW L-24R AND L-26R, REPAIRED AFT EDGE OF AFT CARGO DOOR CUTOUT PER SRM 53-20-15-2R
- [SDR DALA2026101505659](https://openairdocs.org/sdr/DALA2026101505659), Oct 14, 2026: LONGERON. CRACKED. FOUND A CRACK AT LONGERON 2L BS 1133 AT AFT ACCESORY COMPARTMENT, R/R LONGERON PER B717-200 SRM 53-00-05-2R. (1866121) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405653](https://openairdocs.org/sdr/DALA2026101405653), Oct 14, 2026: STRUCTURE. CRACKED. CRACK FOUND ON FIXED LEADING EDGE XFS:537 & TORN SEAL, SLAT NR 5 AT RT WING. COMPLIED WITH ER/A 545680-14TR. (1864537) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405652](https://openairdocs.org/sdr/DALA2026101405652), Oct 14, 2026: RETAINER. CHAFED. FOUND WEAR DAMAGE ON FIXED LEADING EDGE, XW= 536, CHAFING ON THE OTBD SEAL RETAINER ON SLAT NR 5 AT LT WING. COMPLIED WITH ER/A 545680-14TR. (1864542) (AIRCRAFT
- [SDR DALA2026091805211](https://openairdocs.org/sdr/DALA2026091805211), Sep 18, 2026: SKIN. DAMAGED. FOUND EXISTING LIGHTNING STRIKE (PLUG) TEMPORARY REPAIR BETWEEN Y522 AND Y541, 2.750 OTBD STC DOUBLER, COMPLIED WITH ER/A 636812-14. (1818758) (AIRCRAFT GROUNDE
- [SDR DALA2026091805210](https://openairdocs.org/sdr/DALA2026091805210), Sep 18, 2026: REPAIR. INTERFERENCE. FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER AT Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14AD. (1818755) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805209](https://openairdocs.org/sdr/DALA2026091805209), Sep 18, 2026: DOUBLER. DEMODIFICATION. FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 6
- [SDR DALA2026091805217](https://openairdocs.org/sdr/DALA2026091805217), Sep 17, 2026: PLUG. TEMP REPAIR. FOUND EXISTING LIGHTNING STRIKE (PLUG) TEMPORARY REPAIR BETWEEN Y522 AND Y541, 2.750 OTBD STC DOUBLER, COMPLIED WITH ER/A 636812-14. (1818080) (AIRCRAFT GROUND
- [SDR DALA2026091805216](https://openairdocs.org/sdr/DALA2026091805216), Sep 17, 2026: DOUBLER. INTERFERENCE. FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER (P/N 8485-5310-404-3) AT Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14AD. (1817946
- [SDR DALA2026091805215](https://openairdocs.org/sdr/DALA2026091805215), Sep 17, 2026: DOUBLER. INTERFERENCE. FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14. (1817938) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805214](https://openairdocs.org/sdr/DALA2026091805214), Sep 17, 2026: ANTENNA. DEMODIFICATION. FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER (P/N 8485-5310-404-1) BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R
- [SDR DALA2026072204286](https://openairdocs.org/sdr/DALA2026072204286), Jul 22, 2026: SLIDE. UNSECURE. L1 DOOR SLIDE CAME LOOSE DURING DOOR OPENING, SECURED 1L DOOR SLIDE IAW AMM 25-61. (8543436) (AIRCRAFT GROUNDED).
- [SDR DALA2026062303739](https://openairdocs.org/sdr/DALA2026062303739), Jun 23, 2026: LAMP. INOPERATIVE. FLIGHT DECK O/H EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-11. (LP 7959221 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2025100807327](https://openairdocs.org/sdr/DALA2025100807327), Oct 2, 2025: SEALANT. NOT REPORTED. WORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717
- [SDR DALA2025100807326](https://openairdocs.org/sdr/DALA2025100807326), Oct 2, 2025: SKIN. LEAKING. WORKING PRI 629612-14, RH WING LOWER SKIN XRS 164 FUEL SEEP. C/W SECTION I LEAK EVALUATION OF ERA 629612-14AD (1231435)
- [SDR DALA2025092907061](https://openairdocs.org/sdr/DALA2025092907061), Sep 26, 2025: COVER. MISSING. LEFT WING HAS ONE LOWER SLAT TRACK COVER MISSING. FWD TO CDL 57-47-03. PLAC. INSTALLED. (7709014)
- [SDR DALA2025010900177](https://openairdocs.org/sdr/DALA2025010900177), Jan 8, 2025: PIN. OUT OF POSITION. TAIL CONE EXIT RELEASE CAM PIN IS NOT 34.5 TO 38.5 DEGREES FROM THE CENTERLINE OF THE BASE AT AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATIO
- [SDR DALA2025010800158](https://openairdocs.org/sdr/DALA2025010800158), Jan 7, 2025: ROD END. DAMAGED. DAMAGED DURING ADJUSTMENT OF RH INBD SPOILER PANEL. THE HOLDDOWN ACTUATOR ROD-END INADVERTENTLY EXTENDED CAUSING A PUNCTURE ON RH INBD GUIDE VANE. SUMMARY OF NR
- [SDR DALA2025010700130](https://openairdocs.org/sdr/DALA2025010700130), Jan 7, 2025: ANGLE. CRACKED. UPPER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED WAS REMOVED. LOWER ANGLE COMMON TO REMOVED ANGLE WAS FOUND CRACKED. SUMMARY
- [SDR DALA2024122712033](https://openairdocs.org/sdr/DALA2024122712033), Dec 24, 2024: ANGLE. CORRODED. CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE DOOR JAMB AT CPAX. SUMMARY OF NRC 00506: CORROSION LEVEL 2. 
- [SDR DALA2024121911829](https://openairdocs.org/sdr/DALA2024121911829), Dec 19, 2024: FRAME. CORRODED. CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00609: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=908 FROM LO
- [SDR DALA2024121711766](https://openairdocs.org/sdr/DALA2024121711766), Dec 16, 2024: RETAINER. CRACKED. CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00782: CRACK INNER RETAINER OF COCKPIT WIND
- [SDR DALA2024121611736](https://openairdocs.org/sdr/DALA2024121611736), Dec 13, 2024: PAN. GOUGED. GOUGE ON INNER PAN AFT EDGE, 2 INCHES BELLOW BEAM #1 AFT EDGE, ON AFT CARGO DOOR (C2). SUMMARY OF NRC 00321: INNER PAN ON AFT LOWER CORNER CLOSE TO BEAM #1 AT A
- [SDR DALA2024121611735](https://openairdocs.org/sdr/DALA2024121611735), Dec 13, 2024: LONGERON. CORRODED. CORROSION ON LONGERON 29L UPPER/LOWER SURFACE BTW STA Y=900-946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LONGERON 29L BTW STA Y= 898 T
- [SDR DALA2024121311703](https://openairdocs.org/sdr/DALA2024121311703), Dec 12, 2024: SKIN. DENTED. DAMAGE T: ELONGATE HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R. SUMMARY OF NRC 00627: ELONGATED HOLES, PROTRUDING DENTS, AND
- [SDR DALA2024121211665](https://openairdocs.org/sdr/DALA2024121211665), Dec 12, 2024: FLOOR SUPPORT. CORRODED. CORROSION OUT OF LIMITS ON FLOOR SUPPORTS ON STA Y=157-200 AND X=45 (1 EA) PER B717-200 SRM 53-00-00-1A PROCEDURE, ALLOWABLE DAMAGE GENERAL, PAR 4.C, FIG 103. S
- [SDR DALA2024121611738](https://openairdocs.org/sdr/DALA2024121611738), Dec 11, 2024: HINGE FITTING. CORRODED. CORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING
- [SDR DALA2024121111616](https://openairdocs.org/sdr/DALA2024121111616), Dec 11, 2024: LUG. WORN. WEAR ON HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING. SUMMARY OF NRC 00803: HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING WERE REPAIRED PER P
- [SDR DALA2024120211371](https://openairdocs.org/sdr/DALA2024120211371), Nov 28, 2024: CUSP WEB. CRACKED. CRACKS ON LH CUSP WEB (3 EA) STA Y=657 & X=56 AND STA Y=716 & X=44.5 AND Y=888 & X=56 AT PASSENGER CABIN. SUMMARY OF NRC 00426: FABRICATED WEB STA Y-655 TO Y-71
- [SDR DALA2024120211370](https://openairdocs.org/sdr/DALA2024120211370), Nov 27, 2024: RIB. ELONGATED. ELONGATED HOLE ON RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217. SUMMARY OF NRC 00410: RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FI
- [SDR DALA2025011500350](https://openairdocs.org/sdr/DALA2025011500350), Nov 26, 2024: SKIN. DAMAGED. LIGHTNING STRIKE ON THE FUSELAGE AT THE RH WINDOW PANEL, STA 484 TO 503. ACCOMPLISH ER/A 622755-14 SECTION II INSPECTION WITHIN EVERY 24 MONTHS UNTIL ACCOMPLISH
- [SDR DALA2024112711259](https://openairdocs.org/sdr/DALA2024112711259), Nov 26, 2024: SKIN. MECHANIC ERROR. EXTERNAL SURFACE OF FUSELAGE SKIN COMMON TO VHF ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L IN REF NRC 12. SUMMARY OF NRC 00169: FUSELA
- [SDR DALA2024112511164](https://openairdocs.org/sdr/DALA2024112511164), Nov 23, 2024: DOOR FRAME. CORRODED. CORROSION ON DOOR JAMB FWD/AFT AT REPAIR SPLICES AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00806: CORROSION LEVEL 2. AFT CARGO DOOR JAMB FWD/AFT REPAIR SPLICES W
- [SDR DALA2024112511163](https://openairdocs.org/sdr/DALA2024112511163), Nov 23, 2024: CUSP WEB. CRACKED. CRACKS ON LH CUSP WEB (2 EA) STA Y=595 & X=56 AND STA Y=907 & X=56 BELOW SEAT TRACK SPLICE IN PASSENGER CABIN. SUMMARY OF NRC 00425: CUSP WEBS BTW STA Y 579-598
- [SDR DALA2024112011084](https://openairdocs.org/sdr/DALA2024112011084), Nov 20, 2024: SEAT TRACK. MECHANIC ERROR. MISDRILLED SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN. SUMMARY OF NRC 00751: SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X
- [SDR DALA2024112011083](https://openairdocs.org/sdr/DALA2024112011083), Nov 19, 2024: TRIPLER. CORRODED. CORROSION ON PREVIOUS REPAIR TRIPLER ON FUSELAGE UNDER FILLET FAIRINGS AREA STA Y=843-860 LONG 28L-28R. SUMMARY OF NRC 00467: CORROSION LEVEL 2. PREVIOUS REPAIR
- [SDR DALA2024111911027](https://openairdocs.org/sdr/DALA2024111911027), Nov 18, 2024: LONGERON SPLICE. CORRODED. CORROSION ON UPPER AND LOWER SURFACE OF LONGERON AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LONGERON L29 R/H 
- [SDR DALA2024111510968](https://openairdocs.org/sdr/DALA2024111510968), Nov 15, 2024: SKIN. CRACKED. CRACKED FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT. SUMMARY OF NRC 00054: FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN J
- [SDR DALA2024111510966](https://openairdocs.org/sdr/DALA2024111510966), Nov 14, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN. SUMMARY OF NRC 730: CORROSION LEVEL 2. RH CUSP WEB UPPER/LOWER SURFACE
- [SDR DALA2024111410948](https://openairdocs.org/sdr/DALA2024111410948), Nov 13, 2024: DIAPHRAGM. CRACKED. CORROSION ON DIAPHRAGM BTW STA Y=200/218 AND X-54/X-22 AT CABIN PAX. SUMMARY OF NRC 00632: CORROSION LEVEL 2. DIAPHRAGM BTW STA Y=200 /218 AND X-54/X-22 WAS REP
- [SDR DALA2024111410947](https://openairdocs.org/sdr/DALA2024111410947), Nov 13, 2024: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 WAS REPAIR
- [SDR DALA2024111210887](https://openairdocs.org/sdr/DALA2024111210887), Nov 11, 2024: SEAT TRACK. MISINSTALLED. WRONG INSTALLED FASTENERS ON SEAT TRACK AND CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN. SUMMARY OF NRC 00427: CUSP WEB STA Y=914-919 & X =56 AT PASSENGER
- [SDR DALA2024111110806](https://openairdocs.org/sdr/DALA2024111110806), Nov 11, 2024: CHANNEL. CORRODED. CORROSION AT CHANNEL BETWEEN STA 827 AND 832 L22R EXTERNAL FUSELAGE. SUMMARY OF NRC 407: CORROSION LEVEL 2. CHANNEL BTW STA Y=827 AND Y=832 L22R EXTERNAL FUSELA
- [SDR DALA2024111110801](https://openairdocs.org/sdr/DALA2024111110801), Nov 9, 2024: SKIN. CRACKED. CRACKED FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER. SUMMARY OF NRC 00052: FUSELAGE SKIN STA Y 1087 LONG 1
- [SDR DALA2024111110797](https://openairdocs.org/sdr/DALA2024111110797), Nov 8, 2024: LONGERON. CRACKED. CRACK ON LONGERON #8RH STA Y1022 AT PAX CABIN. SUMMARY OF NRC 00501: LONGERON #8RH STA Y1022 AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-05-2R-2. (LP #065
- [SDR DALA2024110810726](https://openairdocs.org/sdr/DALA2024110810726), Nov 7, 2024: VANE. DENTED. DENTS (2 EA) ON UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=91 AT RH WING. SUMMARY OF NRC 00143: UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA 
- [SDR DALA2024110710703](https://openairdocs.org/sdr/DALA2024110710703), Nov 7, 2024: LONGERON. CRACKED. CRACK ON LONGERON 6LH STA Y=1022 AT PAX CABIN. SUMMARY OF NRC 00499: LONGERON 6LH STA Y=1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2,
- [SDR DALA2024110710702](https://openairdocs.org/sdr/DALA2024110710702), Nov 5, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 AT PASSENGER CABIN. SUMMARY OF NRC 00475: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) X

All 199: https://openairdocs.org/aircraft/N981AT/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/N981AT/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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