# N990AT: 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: 55134
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 24, 2002
- Certificate issued: July 31, 2024
- Expires: July 31, 2031
- Mode S code: ADD2B5
- 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=990AT
- Page: https://openairdocs.org/aircraft/N990AT

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/N990AT/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 N990AT.

## FAA accident and incident reports

None matched to N990AT.

## Service difficulty reports (246, 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 DALA2026091805213](https://openairdocs.org/sdr/DALA2026091805213), Sep 13, 2026: SKIN. CRACKED. CRACKS FOUND AFFECTING THE SKIN BETWEEN L-L2 AND L-L3 AT APPROXIMATELY STA Y=1133, COMPLIED WITH ER/A 636735-14. (1810811) (AIRCRAFT GROUNDED).
- [SDR DALA2026091405130](https://openairdocs.org/sdr/DALA2026091405130), Sep 13, 2026: SKIN. CRACKED. LEFT FUSELAGE SKIN CRACKS. REPAIRED PER ERA 636735-14AD. (1810803) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091405129](https://openairdocs.org/sdr/DALA2026091405129), Sep 13, 2026: SKIN. CRACKED. CRACK ON EXTERNAL SKIN STA Y=1133 BTW LONG 2LH. CORRECTIVE ACTION: REPAIRED PER ER/A 636735-14AD. (1811500) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091405128](https://openairdocs.org/sdr/DALA2026091405128), Sep 11, 2026: VANE. DENTED. DENTS ON LOWER SURFACE OF FIXED FLAP VANE AT RIGHT WING. REPAIRED PER SRM 57-53-01-2R. (1807386) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091405127](https://openairdocs.org/sdr/DALA2026091405127), Sep 11, 2026: SKIN. DENTED. DENTS ON LOWER SURFACE OF FIXED FLAP VANE AT RIGHT WING. REPAIRED PER SRM 57-53-01-2R. (1807380) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091105080](https://openairdocs.org/sdr/DALA2026091105080), Sep 10, 2026: SCUFF PLATE. CRACKED. SHIP 9528 CRACK AND BENT IN SCUFF PLATE FWD SIDE AT AFT CARGO, CORRECTIVE ACTION: COMPLIED WITH ER/A 542149-14TR. (1805472) (AIRCRAFT GROUNDED).
- [SDR DALA2026081304645](https://openairdocs.org/sdr/DALA2026081304645), Aug 13, 2026: OXYGEN MASK. LEAKING. FO'S O2 MASK LEAKING AIR, R & R FO O2 MASK PER B717 AMM 35-13. (9579428) (AIRCRAFT GROUNDED).
- [SDR DALA2026052803228](https://openairdocs.org/sdr/DALA2026052803228), May 24, 2026: ELEC CONNECTOR. DAMAGED. ATO- DISCONTINUED TAKEOFF ROLL AFTER RECEIVING A RIGHT ENGINE GENERATOR OFF MESSAGE. MAINTENANCE FOUND A PCDU CONNECTOR PIN PUSHED BACK, REINSERTED AND LOCKED P
- [SDR DALA2026051703030](https://openairdocs.org/sdr/DALA2026051703030), Apr 29, 2026: SPAR CAP. NOT REPORTED. AD 2018-10-18 AMOC APPROVAL REQUIRES SPAR CAPS ETHF OPEN HOLE. ACCOMPLISH ERA 633126-14AD (1568579) (AIRCRAFT GROUNDED)
- [SDR DALA2025101707593](https://openairdocs.org/sdr/DALA2025101707593), Oct 10, 2025: SKIN. WORN. SHIP 9528 LEADING EDGE UPPER SKIN PANEL / FASTENERS WORN ALONG OUTER PERIMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 620349-14 (1245364).
- [SDR DALA2025072905677](https://openairdocs.org/sdr/DALA2025072905677), Jul 26, 2025: FUEL LINE. LEAKING. SHIP 9528 -DIV- TO ORD DUE TO LEFT FUEL QUANTITY LOSS. CORRECTIVE ACTION: MAINTENANCE FOUND A LEFT SHROUDED FUEL RETURN TO TANK LINE AND COUPLING LOOSE AND LEAK
- [SDR DALA2024112611229](https://openairdocs.org/sdr/DALA2024112611229), Nov 26, 2024: CABLE. DISCONNECTED. THE GIRT BAR RETAINER WITH THE CABLE WAS DISCONNECTED FROM THE SLIDE BUSSLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIA
- [SDR DALA2024102110284](https://openairdocs.org/sdr/DALA2024102110284), Oct 19, 2024: PAN. CRACKED. CRACKS ON INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00726: INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DO
- [SDR DALA2024101810191](https://openairdocs.org/sdr/DALA2024101810191), Oct 17, 2024: PAN. CRACKED. CRACK PAN INTERNAL SIDE FWD EDGE ON BEAM #4 AND #5 (2 EA) AT AFT CARGO DOOR. SUMMARY OF NRC 00129: INNER PAN ON FWD EDGE BETWEEN BEAM #4 AND #5 AT AFT CARGO COM
- [SDR DALA2024101410045](https://openairdocs.org/sdr/DALA2024101410045), Oct 12, 2024: PAN. CRACKED. CRACK PAN INTERNAL SIDE OF AFT EDGE ON BEAM #3, #4, AND #5 AT AFT CARGO DOOR. SUMMARY OF NRC 00127: INNER PAN OF AFT EDGE ON BEAM #3 AT AFT CARGO DOOR WAS REPAI
- [SDR DALA2024101410044](https://openairdocs.org/sdr/DALA2024101410044), Oct 11, 2024: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN EDGE, AROUND HANDLE ON PASSENGER DOOR (L1). SUMMARY OF NRC 00302: EXTERNAL FUSELAGE SKIN EDGE AROUND HANDLE ON PASSENGER DOOR (L
- [SDR DALA2024101109965](https://openairdocs.org/sdr/DALA2024101109965), Oct 8, 2024: DOOR. BROKEN. -AD- BROKEN INBD BUTE DOOR OUTBD EDGE AT RH WING. (AD) SUMMARY OF NRC 00171: INBD BUTE DOOR OUTBD EDGE AT RH WING WAS REPAIRED PER ERA 618696-14TR REV ORIGINAL 
- [SDR DALA2024100809790](https://openairdocs.org/sdr/DALA2024100809790), Oct 7, 2024: SKIN. DAMAGED. CREASE IN FUSELAGE SKIN WAS FOUND ON REPAIR AREA. SUMMARY 00593: CREASE WAS REPAIRED PER ER/A 620891-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620891-
- [SDR DALA2024100409701](https://openairdocs.org/sdr/DALA2024100409701), Oct 3, 2024: ANGLE. CORRODED. CORROSION ON DOOR JAMB ANGLE AND DOOR JAMB WEB BTW STA Y=200-210 AND X=56 AT FWD PASSENGER DOOR JAMB (L1). SUMMARY OF NRC 00450: CORROSION LEVEL 2. DOOR JAMB AN
- [SDR DALA2024092609432](https://openairdocs.org/sdr/DALA2024092609432), Sep 26, 2024: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSELAGE. SUMMARY OF NRC 00020: FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSE
- [SDR DALA2024092609431](https://openairdocs.org/sdr/DALA2024092609431), Sep 25, 2024: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSELAGE. SUMMARY OF NRC 00049: FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSEL
- [SDR DALA2024092509407](https://openairdocs.org/sdr/DALA2024092509407), Sep 24, 2024: LONGERON. CRACKED. CRACK ON LONGERON 5LH, 8LH, 16LH, 5RH, 7RH, AND 9RH STA 1022 AT PAX CABIN. SUMMARY OF NRC 00404: LONGERONS 5LH, 8LH, 16LH, 5RH, AND 7RH STA 1022 AT PAX CABIN WE
- [SDR DALA2024092509406](https://openairdocs.org/sdr/DALA2024092509406), Sep 23, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS (2 EA) BTW STA=1022 TO STA=1053 ON X=56, AND -X=20 AT PAX CABIN. SUMMARY OF NRC 00835: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) BTW 
- [SDR DALA2024092309314](https://openairdocs.org/sdr/DALA2024092309314), Sep 21, 2024: CUSP WEB. CRACKED. CRACK ON LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN. SUMMARY OF NRC 00509: LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN WAS REPAIRED PER B
- [SDR DALA2024092309313](https://openairdocs.org/sdr/DALA2024092309313), Sep 20, 2024: PAN. CRACKED. CRACK ON PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR. SUMMARY OF NRC 00301: PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-
- [SDR DALA2024092009272](https://openairdocs.org/sdr/DALA2024092009272), Sep 19, 2024: CUSP WEB. CRACKED. CRACK ON BELOW CUSP WEB BTW STA Y=520 LOWER FACE X=-44 AND STA Y=650 X=-46 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00230: CUSP WEB BTW STA Y=520 LOWER FACE X=-
- [SDR DALA2024091809141](https://openairdocs.org/sdr/DALA2024091809141), Sep 18, 2024: FLOORBEAM. CORRODED. CORRODED HORIZONTAL FLOOR SUPPORTS AT W1 ON STA Y=180 X-9 TO X-43 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.044", STA Y=196 X 16 TO X 43 W
- [SDR DALA2024091809139](https://openairdocs.org/sdr/DALA2024091809139), Sep 17, 2024: PAN. CRACKED. CRACK ON PAN INTERNAL EDGE BTW BEAM #1 AND #2 AT AFT CARGO DOOR AFT EDGE. SUMMARY OF NRC 00126: INNER PAN ON INTERNAL AFT EDGE BTW BEAM #1 AND #2 AT AFT CARGO C
- [SDR DALA2024091609052](https://openairdocs.org/sdr/DALA2024091609052), Sep 16, 2024: DOUBLER. WORN. WEAR ON INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00289: INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN 
- [SDR DALA2024091609050](https://openairdocs.org/sdr/DALA2024091609050), Sep 14, 2024: LONGERON. CRACKED. CRACK ON LONGERON 17LH SIDE STA=1022 AFT OF BULKHEAD. CRACK ON LONGERON 12RH SIDE STA=1022 FWD OF BULKHEAD. CRACK ON LONGERON 14 RH STA=1022 FWD OF BULKHEAD AT 
- [SDR DALA2024091609049](https://openairdocs.org/sdr/DALA2024091609049), Sep 13, 2024: FRAME. CRACKED. CRACKED FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX. SUMMARY OF NRC 00386: FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX WAS REPAIRED PER 
- [SDR DALA2024091609048](https://openairdocs.org/sdr/DALA2024091609048), Sep 13, 2024: DOUBLER. CORRODED. CORROSION ON REPAIR DOUBLER OF JAMB WEB STA Y=954 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00264: CORROSION LEVEL 2. JAMB WEB STA Y=954 AND LONG 29
- [SDR DALA2024091308985](https://openairdocs.org/sdr/DALA2024091308985), Sep 13, 2024: SKIN. CRACKED. CRACKS WERE FOUND ON SKIN AT COCKPIT ON AFT UPPER CORNER CUTOUT SLIDING WINDOW. SUMMARY OF NRC 00718: CRACKS ON AFT UPPER CORNER CUTOUT SLIDING WINDOW ON SKIN A
- [SDR DALA2024091809137](https://openairdocs.org/sdr/DALA2024091809137), Sep 12, 2024: WEB. DAMAGED. ELONGATED HOLE ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONGA
- [SDR DALA2024091308984](https://openairdocs.org/sdr/DALA2024091308984), Sep 12, 2024: DOOR FRAME. DAMAGED. ELONGATED HOLES ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONG
- [SDR DALA2024091308983](https://openairdocs.org/sdr/DALA2024091308983), Sep 12, 2024: FLOORBEAM. CRACKED. CORROSION ON FLOOR SUPPORT ON W1 STA Y=198 TO Y=160 X=-5.5 TO X=-9 AT PAX CABIN. SUMMARY OF NRC 00748: CORROSION LEVEL 2. SUPPORT WAS REPLACED ON W1 STA Y=198 T
- [SDR DALA2024091308981](https://openairdocs.org/sdr/DALA2024091308981), Sep 12, 2024: CUSP WEB. CRACKED. CRACKED CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT. SUMMARY OF NRC 00413: CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT WAS REPLACE
- [SDR DALA2025040402562](https://openairdocs.org/sdr/DALA2025040402562), Sep 11, 2024: HINGE FITTING. DAMAGED. CORROSION AND SCRATCHES ON HOLES OF OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTBRD WING FLAP HINGE FITTING AT LH WING. SUMMARY OF NRC 00785: CO
- [SDR DALA2024090608754](https://openairdocs.org/sdr/DALA2024090608754), Sep 5, 2024: FLOOR SUPPORT. CRACKED. CRACK ON INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00231: INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO 
- [SDR DALA2024072307418](https://openairdocs.org/sdr/DALA2024072307418), Jul 19, 2024: COVER. DETACHED. EMERGENCY LIGHT COVER AT SEAT 13B CAME OFF. MAINTENANCE RESECURED THE COVER BACK ONTO THE SEAT PER B717 AMM 25-21. (LP #6193590)
- [SDR DALA2024061806171](https://openairdocs.org/sdr/DALA2024061806171), Jun 18, 2024: BATTERY PACK. INOPERATIVE. DURING SERVICE, FOUND THE EMERGENCY LIGHTS IN AFT CABIN AT ROWS 24-29, TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN BATTERY PACK PER B717 AMM 33-55. OP
- [SDR DALA2024061005957](https://openairdocs.org/sdr/DALA2024061005957), Jun 10, 2024: BATTERY. INOPERATIVE. BOTH RT AND LT AFT EMERGENCY DOOR EXIT SIGNS OVER WINGS DO NOT ILLUMINATE.T/S PER B717 FIM 33-50. REPLACED EMERGENCY BATTERY FOR POWER SUPPLY B5-230 PER B717 AM
- [SDR DALA2024020301509](https://openairdocs.org/sdr/DALA2024020301509), Jan 26, 2024: DOOR FRAME. DAMAGED. RAMP REPORTS DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGE PER B717 SRM 53-20-15-2R REPAIR 10 OPTION 2. FABRICATED, TREATED, & PAI
- [SDR DALA2023091507587](https://openairdocs.org/sdr/DALA2023091507587), Sep 14, 2023: UNKNOWN. UNKNOWN. DURING RH OVERWING FRAME REMOVAL, STA 655 TO 715 CUSP WEB WAS FOUND BROKEN. SUMMARY OF NRC 00093: CUSP WEB RH ON STA 655 TO 715 WAS FABRICATED AND REPLACED PER 
- [SDR DALA2023091407538](https://openairdocs.org/sdr/DALA2023091407538), Sep 13, 2023: UNKNOWN. UNKNOWN. DURING LH OVERWING FRAME REMOVAL, STA 655 TO 715 CUSP WEB WAS FOUND BROKEN. SUMMARY OF NRC 00094: CUSP WEB LH ON STA 655 TO 715 WAS FABRICATED AND REPLACED PER 
- [SDR DALA2023091407535](https://openairdocs.org/sdr/DALA2023091407535), Sep 13, 2023: UNKNOWN. UNKNOWN. A.D. CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-04D). SUMMARY OF NRC 00073: OVERWING FRAME AT STA
- [SDR DALA2023091407534](https://openairdocs.org/sdr/DALA2023091407534), Sep 13, 2023: UNKNOWN. UNKNOWN. A.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 RH (REF CARD 5310-01436-04D). SUMMARY OF NRC 00072: OVERWING FRAME AT ST
- [SDR DALA2023091407533](https://openairdocs.org/sdr/DALA2023091407533), Sep 13, 2023: UNKNOWN. UNKNOWN. A.D. CRACK OF 0.200 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=715.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00071: OVERWING FRAME AT ST
- [SDR DALA2023042503235](https://openairdocs.org/sdr/DALA2023042503235), Apr 21, 2023: UNKNOWN. UNKNOWN. THE TAIL CONE SLIDE COVER IS LOOSE AND THE SLIDE UNRAVELING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART
- [SDR DALA2023042503234](https://openairdocs.org/sdr/DALA2023042503234), Apr 21, 2023: UNKNOWN. UNKNOWN. THE AFT TAIL SLIDE RETAINER CABLE CLIP IS BROKEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. M

All 246: https://openairdocs.org/aircraft/N990AT/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/N990AT/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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