# N979AT: 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: 55038
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 23, 2002
- Certificate issued: April 12, 2024
- Expires: April 30, 2031
- Mode S code: ADA526
- 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=979AT
- Page: https://openairdocs.org/aircraft/N979AT

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/N979AT/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 N979AT.

## FAA accident and incident reports

None matched to N979AT.

## Service difficulty reports (219, 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 DALA2026090204948](https://openairdocs.org/sdr/DALA2026090204948), Sep 1, 2026: SPAR CAP. CORRODED. FOUND CORROSION IN BARREL NUT HOLE AFFECTING THE FRONT SPAR UPPER CAP BARREL NUT HOLE NR 27 OF THE RT HORIZONTAL STAB, COMPLIED WITH ER/A 622779-14. (1789394) (
- [SDR DALA2026082704864](https://openairdocs.org/sdr/DALA2026082704864), Aug 27, 2026: LAMP. INOPERATIVE. OVERHEAD EMERGENCY LIGHT INOP AT 27AB SEAT, RE-LAMP EMERGENCY LIGHT AT SEAT 27AB IAW AMM 33-51. (9222934) (AIRCRAFT GROUNDED).
- [SDR DALA2026060203343](https://openairdocs.org/sdr/DALA2026060203343), May 31, 2026: LANYARD. OUT OF POSITION. R1 DOOR GIRT BAR IRREGULARITY. FOUND LANYARD OUT OF PLACE. RE-POSITIONED LANYARD. OK FOR SVC. (8236554) (AIRCRAFT GROUNDED)
- [SDR DALA2026020900916](https://openairdocs.org/sdr/DALA2026020900916), Feb 1, 2026: LIGHT. DAMAGED. FLOOR EMERGENCY PHOTO LUMINESCENT STRIP DAMAGED AT ROW 21 ABC EXIT ROW. REPLACED IAW AMM 33-52. OPS CHECKED FINE. OK FOR SERVICE. (7421382)
- [SDR DALA2025101707597](https://openairdocs.org/sdr/DALA2025101707597), Oct 16, 2025: NONE. NONE. SHIP 9544 REPETITIVE INSPECTIONS WITHIN FORTY-SIX HUNDRED (4,600) FLIGHT CYCLES UPON ER/A 617313-14. CORRECTIVE ACTION: C/W REPAIRED PER ERA 617313 (1255743).
- [SDR DALA2025101707596](https://openairdocs.org/sdr/DALA2025101707596), Oct 16, 2025: NOT REPORTED. NOT REPORTED. SHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)
- [SDR DALA2025022501470](https://openairdocs.org/sdr/DALA2025022501470), Feb 22, 2025: FUEL CELL. LEAKING. -AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN BTW STA XRS 154 TO STA XRS 164, AFT EDGE BTW LOWER PRODUCTION DOUBLER AND LOWER WING SKIN. 
- [SDR DALA2025032602224](https://openairdocs.org/sdr/DALA2025032602224), Feb 20, 2025: NOT REPORTED. NOT REPORTED. -AD- DAMAGE TOLERANCE EVALUATION, ER/A 622334-14 SECT II WITH AMOC TO AD 2024-21-01. DTA MONITOR INSPECTION REQUIRES DTA / AMOC APPROVAL BEFORE THE 1ST OF 30 DA
- [SDR DALA2025021801194](https://openairdocs.org/sdr/DALA2025021801194), Feb 13, 2025: CABLE. OUT OF POSITION. TAILCONE DEPLOYMENT SYSTEM CABLE OUT POSITION OF PULLEY STA 1225 IN 2 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF 
- [SDR DALA2025100807321](https://openairdocs.org/sdr/DALA2025100807321), Feb 5, 2025: HINGE FITTING. CORRODED. IN REFERENCE TO NRC 00309: AFTER REMOVAL SEALANT WAS FOUND CORROSION ON CENTER FLAP HINGE AT LH WING. CENTER WING FLAP HINGE FITTING WAS REMOVED PER B717 AMM 57
- [SDR DALA2025020300803](https://openairdocs.org/sdr/DALA2025020300803), Feb 1, 2025: RETAINER. CRACKED. CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00468: CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER 
- [SDR DALA2025013000725](https://openairdocs.org/sdr/DALA2025013000725), Jan 29, 2025: DRAIN. CRACKED. CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00027: CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER 
- [SDR DALA2025012000466](https://openairdocs.org/sdr/DALA2025012000466), Jan 18, 2025: FRAME. CRACKED. CRACK ON FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 264: FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT 
- [SDR DALA2025011600360](https://openairdocs.org/sdr/DALA2025011600360), Jan 15, 2025: FRAME. CORRODED. CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00839: CORROSION LEVEL 2. CORROSION ON
- [SDR DALA2025011400313](https://openairdocs.org/sdr/DALA2025011400313), Jan 13, 2025: PAN. WORN. WEAR ON INNER PAN FWD LOWER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00083: INNER AND OUTER PAN FWD EDGE LOWER CORNER OF FWD CARGO DOOR WAS REPAIRED PER PRI 622
- [SDR DALA2025011300270](https://openairdocs.org/sdr/DALA2025011300270), Jan 9, 2025: SKIN. DAMAGED. -AD- ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50, ALSO ON SAME ANGLE BTW X=44 AND X=50 (4 EA) AT WINGBOX AREA. (CPAX). SUMMA
- [SDR DALA2025011300268](https://openairdocs.org/sdr/DALA2025011300268), Jan 9, 2025: SKIN. DAMAGED. CORROSION AND TOOL MARKS WERE FOUND ON INNER HOLE #27 AND WEAR ON UPPER SKIN AROUND FROM #27 AT RH HORIZONTAL STAB. SUMMARY OF NRC 00735: CORROSION LEVEL 2. COR
- [SDR DALA2025011300267](https://openairdocs.org/sdr/DALA2025011300267), Jan 9, 2025: STRUCTURE. DAMAGED. CORROSION AND SCRATCHES ON INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB. SUMMARY OF NRC 00742: LEVEL CORROSION 2. CORROSION IN INNER BOL
- [SDR DALA2025011300265](https://openairdocs.org/sdr/DALA2025011300265), Jan 9, 2025: BULKHEAD. CORRODED. -AD- CORROSION ON FWD BULKHEAD OF LH WHEEL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS). SUMMARY OF NRC 00140: CORROSION LEVEL 2. CORROSION ON FWD BU
- [SDR DALA2025011300264](https://openairdocs.org/sdr/DALA2025011300264), Jan 9, 2025: STRUCTURE. DAMAGED. SCRATCHES AND MISSING MATERIAL WERE FOUND ON INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER. SUMMARY OF NRC 00729: INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDE
- [SDR DALA2025010700129](https://openairdocs.org/sdr/DALA2025010700129), Jan 6, 2025: FRAME. CRACKED. -AD- CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-01D). SUMMARY OF NRC 0470: OVERWING FRAME 
- [SDR DALA2025010500067](https://openairdocs.org/sdr/DALA2025010500067), Jan 4, 2025: CARGO TRACK. CORRODED. CORROSION ALONG CARGO TRACK RH AT AFT CARGO COMPARTMENT. SUMMARY: CORROSION LEVEL 2. CORROSION ALONG TRACK RH BTW STA Y=813 TO STA Y=954, AT AFT CARGO COMPARTME
- [SDR DALA2025010300045](https://openairdocs.org/sdr/DALA2025010300045), Jan 2, 2025: DOOR FRAME. CORRODED. CORROSION ON DOOR JAMB PAN. ALSO ON PREVIOUS REPAIR DOUBLER AT AFT CARGO COMPARMENT BTW STA Y=954 TO STA Y=994 APROX C2. SUMMARY OF NRC 00133: CORROSION LEVEL 2
- [SDR DALA2024123012068](https://openairdocs.org/sdr/DALA2024123012068), Dec 29, 2024: SKIN. CRACKED. CRACK ON AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT. SUMMARY OF NRC 00707: AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT WAS REPA
- [SDR DALA2024122411973](https://openairdocs.org/sdr/DALA2024122411973), Dec 24, 2024: CARGO TRACK. CORRODED. CORROSION ON TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA). SUMMARY OF NRC 00722: CORROSION LEVEL 2. TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR 
- [SDR DALA2024122712029](https://openairdocs.org/sdr/DALA2024122712029), Dec 23, 2024: PIN. OUT OF POSITION. THE INFLATION CABLE PIN WAS OUT OF PLACE. ALSO MISSING THE VALVE LOCK PIN ON THE FWD PASSENGER ENTRANCE DOOR SLIDE (L1). THIS COULD PREVENT THE PROPER OPERATION
- [SDR DALA2024122311966](https://openairdocs.org/sdr/DALA2024122311966), Dec 21, 2024: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y=636-655 X=- 44 TO X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 826: CUSP WEB BTW STA Y=636-655 X=-44 TO X=-60 AT PASSENGER CABIN 
- [SDR DALA2024121911826](https://openairdocs.org/sdr/DALA2024121911826), Dec 18, 2024: STOP FITTING. CRACKED. DOOR STOP FITTING #4 WAS FOUND CRACK ON INNER PAN FWD SIDE OF AFT CARGO DOOR. SUMMARY OF NRC 00716: INNER PAN ON FWD SIDE STOP #4 AT AFT CARGO COMPARTMENT DOOR 
- [SDR DALA2024121711767](https://openairdocs.org/sdr/DALA2024121711767), Dec 16, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927. SUMMARY OF NRC 00725: CORROSION LEVEL 2. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927 WAS REPAIRED P
- [SDR DALA2024121611737](https://openairdocs.org/sdr/DALA2024121611737), Dec 14, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00579: FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTME
- [SDR DALA2024121311701](https://openairdocs.org/sdr/DALA2024121311701), Dec 12, 2024: LONGERON. CRACKED. CRACKED LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX). SUMMARY OF NRC 00580: LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y
- [SDR DALA2024121111615](https://openairdocs.org/sdr/DALA2024121111615), Dec 10, 2024: CUSP WEB. CRACKED. CRACK ON CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00606: CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SR
- [SDR DALA2024121111614](https://openairdocs.org/sdr/DALA2024121111614), Dec 10, 2024: BEAM. CRACKED. CRACK ON INTERNAL STRUCTURE LL BEAM #1 STA 195 AT PASSENGER DOOR. SUMMARY OF NRC 00293: BEAM #1 ON INTERNAL STRUCTURE STA 195 AT PASSENGER DOOR (L1) WAS REPAIRE
- [SDR DALA2024121111613](https://openairdocs.org/sdr/DALA2024121111613), Dec 10, 2024: LONGERON. CRACKED. CRACKED LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX) SUMMARY OF NRC 00581: LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTM
- [SDR DALA2024121111612](https://openairdocs.org/sdr/DALA2024121111612), Dec 10, 2024: FRAME ANGLE. CRACKED. CRACK ON FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH. SUMMARY OF NRC 00536: FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7
- [SDR DALA2024120911539](https://openairdocs.org/sdr/DALA2024120911539), Dec 8, 2024: CUSP WEB. DAMAGED. TOOL MARK ON CUSP WEB AND SPLICE BTW STA Y=794, X44 TO X54 AT CABIN PASENGER. SUMMARY OF NRC 00547: CUSP WEB ON STA 796 X44 TO X54 WAS REPAIRED PER B717 SRM 53-
- [SDR DALA2024120911538](https://openairdocs.org/sdr/DALA2024120911538), Dec 6, 2024: DOUBLER. CRACKED. CRACK ON EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1). SUMMARY OF NRC 00088: EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DO
- [SDR DALA2024120911537](https://openairdocs.org/sdr/DALA2024120911537), Dec 6, 2024: LONGERON. CRACKED. CRACK ON LONGERON 17 LH, LONGERON 8 LH, AND LONGERON 13 LH BTW STA Y=1020 AND STA Y=1023 LH SIDE. SUMMARY OF NRC 537: LONGERON 17 LH AND LONGERON 8 LH BTW STA Y
- [SDR DALA2024120911535](https://openairdocs.org/sdr/DALA2024120911535), Dec 5, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK X=56 AND STA 996 IN PAX CABIN. SUMMARY OF NRC 723: CORROSION LEVEL 2. SEAT TRACK X=56 AND STA 996 IN PAX CABIN WAS REPAIRED PER B717 SRM
- [SDR DALA2024120211372](https://openairdocs.org/sdr/DALA2024120211372), Nov 29, 2024: DOUBLER. CORRODED. CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00563: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERO
- [SDR DALA2024111911025](https://openairdocs.org/sdr/DALA2024111911025), Nov 15, 2024: VANE. DENTED. -AD- DENTS ON RH WING FWD MOVABLE VANE INBD SURFACE. SUMMARY OF NRC 00326: DENTS (3 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE RH WING WERE EVALUATED AND FOUN
- [SDR DALA2024041804532](https://openairdocs.org/sdr/DALA2024041804532), Apr 16, 2024: SKIN. CRACKED. -AD- FOUND 4 EA HOLES ON LT VERT BELOW EXISTING DOUBLER AT SPLICE SHOWING CRACK INDICATIONS. C/W ER/A 617313-14AD REV ORIG SECTION I PERMANENT REPAIR. ALL RII C
- [SDR DALA2024041804530](https://openairdocs.org/sdr/DALA2024041804530), Apr 16, 2024: SKIN. CRACKED. -AD- VERTICAL STAB LEFT SIDE 4 EA HOLES HAVE CRACK INDICATIONS, IN SKIN LAYER ONLY, JUST BELOW ZFS 52.267. BHEC INSP CONFIRMS CRACKS IN 4 EA HOLES IN SKIN LAYER
- [SDR DALA2024011900811](https://openairdocs.org/sdr/DALA2024011900811), Jan 18, 2024: LENS. MISSING. CABIN EMERGENCY LIGHT LENS MISSING AT 2B. MAINTENANCE FOUND STAND-BY OVERHEAD EMERGENCY LIGHT COVER MISSING AT ROW 2. INSTALLED THE LIGHT COVER AS REQUIRED REF 
- [SDR DALA2023102308703](https://openairdocs.org/sdr/DALA2023102308703), Oct 20, 2023: UNKNOWN. UNKNOWN. ELONGATED AND CRACKED HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L IN REF NRC 00086. SUMMARY OF NRC 00123: DAMAGE IN HOLES ON FUSELAGE SKIN AT ST
- [SDR DALA2023102008643](https://openairdocs.org/sdr/DALA2023102008643), Oct 19, 2023: UNKNOWN. UNKNOWN. SEVERAL DENTS ON UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00053: UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING WAS REPAIRED PER ER/A 6128
- [SDR DALA2023102008640](https://openairdocs.org/sdr/DALA2023102008640), Oct 19, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2. SUMMARY OF NRC-0087: INNER AND OUTBOARD PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2 WERE REPAIRED PER B717-200
- [SDR DALA2023092507854](https://openairdocs.org/sdr/DALA2023092507854), Sep 21, 2023: UNKNOWN. UNKNOWN. FOUND INTERCOSTAL CRACKED BETWEEN STA 946.5 AND 954. FABBED NEW INTERCOSTAL PER DWG 9915578 AND SRM 53-20-51-0I PROC 7. INSTALLED INTERCOSTAL PER B717 SRM 51-41
- [SDR DALA2023022701432](https://openairdocs.org/sdr/DALA2023022701432), Feb 22, 2023: PANEL. DAMAGED. PANEL DAMAGED AND BENT. REPAIRED AND FABRICATED PANEL.
- [SDR DALA2022080205278](https://openairdocs.org/sdr/DALA2022080205278), Jul 27, 2022: BATTERY. INOPERATIVE. THE OVER WING EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. MAINTENANCE REPLACED THE FWD OVER WING EMERGENCY EXIT LIGHT BATTERY ASSEMBLY PER B717 AMM 33- 11. OPER

All 219: https://openairdocs.org/aircraft/N979AT/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/N979AT/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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