# N996AT: 2002 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55140
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 5, 2002
- Certificate issued: February 5, 2024
- Expires: February 28, 2031
- Mode S code: ADE8FF
- 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=996AT
- Page: https://openairdocs.org/aircraft/N996AT

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 BMW Rolls 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 (BMW Rolls 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/N996AT/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 N996AT.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20060209010299I](https://openairdocs.org/incident/20060209010299I), Feb 9, 2006: Boeing 717200 (N996AT), Minneapolis, MN. (-23) Airtran airways flt 851 departed from msp at 1330Z hours enroute to atl and experienced a left gear door unsafe alert and a red gear unsafe light. The…

## Service difficulty reports (203, 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 DALA2026061603618](https://openairdocs.org/sdr/DALA2026061603618), Jun 16, 2026: BATTERY PACK. INOPERATIVE. AIRCRAFT 9542, AFT EMERGENCY EXIT SIGN AND TAIL COMP EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK B5-260 IAW AMM 33-51. TEST OK. (LP 86307
- [SDR DALA2026052903251](https://openairdocs.org/sdr/DALA2026052903251), May 25, 2026: DOUBLER. GOUGED. GOUGES (2 EAS) ON FIXED LEADING EDGE PREVIOS REPAIR DOUBLER BTW XOS 384.0 TO XOS 386.0 APPROX AT RT WING. REPAIRED PER PRI 634250-14 (1611243) (AIRCRAFT GROUNDE
- [SDR DALA2026050502827](https://openairdocs.org/sdr/DALA2026050502827), May 2, 2026: SLIDE. WRONG PART. TARP WRONG INSTALLED ON TAIL CONE SLIDE DEPLOYMENT AT AFT ACCESSORIES COMPARTMENT. REPLACED AT TAIL CONE SLIDE (1573474) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502816](https://openairdocs.org/sdr/DALA2026050502816), May 1, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN BS Y= 1076 BTW LONG 13RH & 14RH. CORRECTIVE ACTION: REPAIR AND PRI 633992-14 (1571512) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102513](https://openairdocs.org/sdr/DALA2026042102513), Apr 13, 2026: SPAR CAP. MECHANIC ERROR. RIGHT WING, TRAILING EDGE LOWER SPAR CAP MISDRILLED HOLES. REPAIRED PER ERA 608531-14. (1542895) (AIRCRAFT GROUNDED)
- [SDR DALA2026031701819](https://openairdocs.org/sdr/DALA2026031701819), Mar 14, 2026: ENGINE. BIRD INGESTION. IFSD - APPROXIMATELY 13 MINUTES FROM LANDING IN STL, BIRD STRIKE RIGHT ENGINE WITH VIBES. CREW PERFORMED IFSD. REPLACED #2 ENGINE.
- [SDR DALA2026021901204](https://openairdocs.org/sdr/DALA2026021901204), Feb 15, 2026: POWER SUPPLY. INOPERATIVE. AIRCRAFT 9542, AFT WALKWAY EMERG. LIGHTS INOP. FOUND BATTERY POWER SUPPLY FAULTY AT B5-260 REMOVED AND REPLACED POWER SUPPLY PER B717 AMM 33-51. OPS CHECKS GOOD
- [SDR DALA2024102110285](https://openairdocs.org/sdr/DALA2024102110285), Oct 19, 2024: BATTERY. MALFUNCTIONED. EMERGENCY EXIT LIGHT ON TOP OF TAILCONE IS INTERMITTENTLY FLASHING. MAINTENANCE REPLACED THE BATTERY AND BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CH
- [SDR DALA2024072507458](https://openairdocs.org/sdr/DALA2024072507458), Jul 24, 2024: POWER SUPPLY. INOPERATIVE. INTERIOR OVERWING EMERGENCY LIGHT LEFT & RIGHT LOWER LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY PER B717 AMM 33-51 AT LOCATION B5-119. OPERATIONAL CHECK OK. 
- [SDR DALA2024051305135](https://openairdocs.org/sdr/DALA2024051305135), May 12, 2024: PUMP. LEAKING. SHIP 9542 -HYD/DE- LOSS OF RIGHT HYDRAULIC SYSTEM ON APPROACH REQUIRING A MANUAL GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE HYDRAULIC RE
- [SDR DALA2024042304666](https://openairdocs.org/sdr/DALA2024042304666), Apr 22, 2024: NOT REPORTED. CORRODED. -AD- CORRORION WAS FOUND ON LH HORIZ STAB BARREL NUT HOLE #26. SUMMARY OF NRC 00719: CORROSION LEVEL 2. LH HORIZ STAB BARREL NUT HOLE #26 WAS REPAIRED PER ER/A 
- [SDR DALA2024042204626](https://openairdocs.org/sdr/DALA2024042204626), Apr 21, 2024: SKIN. DAMAGED. -AD- CRACK ON SKIN DRILL FOUND. SUMMARY OF NRC 00852: FUSELAGE SKIN STA 1133 BTW L1-L3LH WAS REPAIRED PER ER/A 617266-14AD REV ORIGINAL SECTION I: PERMANENT REP
- [SDR DALA2024042204623](https://openairdocs.org/sdr/DALA2024042204623), Apr 21, 2024: UNKNOWN. CRACKED. CRACK ON LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 AT RH ELEVATOR. SUMMARY OF NRC 00385: LOWER MATING SURFACE BTW ACCESS 330XB 
- [SDR DALA2024042204621](https://openairdocs.org/sdr/DALA2024042204621), Apr 19, 2024: SPAR CAP. DAMAGED. PERFORM PERMANENT REPAIR ON RH WING TRAILING EDGE LOWER SPAR CAP DUE TO MISDRILLED HOLES WITH TIME LIMITED REPAIR. SUMMARY OF NRC 00856: RH WING TRAILING EDGE L
- [SDR DALA2024041804527](https://openairdocs.org/sdr/DALA2024041804527), Apr 16, 2024: VANE. DEBONDED. SEVEN DISBONDS WERE FOUND ON LH AFT MOVABLE VANE LOWER SKIN, 1) LENGTH 1.550IN AND WIDTH 1.125IN, 2) LENGTH 1.000IN AND WIDTH 0.850IN, 3) LENGTH 1.250IN AND WID
- [SDR DALA2024041804526](https://openairdocs.org/sdr/DALA2024041804526), Apr 15, 2024: GUIDE VANE. DAMAGED. DAMAGE T DURING TEST OF FLIGHT SPOILER ACTUATOR. FLAPS WAS RETRACTED AND RH FLAP GUIDE VANE WAS DENTED WITH INDB FLAP INGE SUPPORT BRACKET (HINGE FAIRING REMOVA
- [SDR DALA2024041504426](https://openairdocs.org/sdr/DALA2024041504426), Apr 13, 2024: BEAM. CRACKED. CRACK ON BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00221: BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1 WAS REPAIR
- [SDR DALA2024041504421](https://openairdocs.org/sdr/DALA2024041504421), Apr 13, 2024: ANGLE. CORRODED. CORROSION WAS FOUND IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0. SUMMARY OF NRC 00803: CORROSION LEVEL 2. CORROSION IN ANGLE OVER CENTER WING UPPER SKIN 
- [SDR DALA2024041504423](https://openairdocs.org/sdr/DALA2024041504423), Apr 12, 2024: FRAME. DAMAGED. ELONGATE HOLES AND WRONG DRILLED ON FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00674: FRAME STA Y=994 BTW LONGERONS 26RH/2
- [SDR DALA2024041204361](https://openairdocs.org/sdr/DALA2024041204361), Apr 11, 2024: PAN. CORRODED. CORROSION ON LOWER PAN AREA AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 0070: CORROSION LEVEL 2. LOWER PAN AREA AT AFT CARGO DOOR JAMB WAS REPLACED PER B717-200 SRM 
- [SDR DALA2024041204360](https://openairdocs.org/sdr/DALA2024041204360), Apr 11, 2024: DOUBLER. CORRODED. CORROSION ON INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0273: CORROSION LEVEL 2. INTERNAL PR
- [SDR DALA2024041004262](https://openairdocs.org/sdr/DALA2024041004262), Apr 9, 2024: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L
- [SDR DALA2024041004263](https://openairdocs.org/sdr/DALA2024041004263), Apr 8, 2024: SCREW. DAMAGED. AD - BURRS WERE FOUND ON THE THREADS OF THE ACME SCREW AT THE HORIZONTAL STABILIZER. SUMMARY NRC 00437: HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS REPLACED UN
- [SDR DALA2024040504135](https://openairdocs.org/sdr/DALA2024040504135), Apr 4, 2024: SKIN. DENTED. DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE. SUMMARY OF NRC 00338: DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SP
- [SDR DALA2024040404051](https://openairdocs.org/sdr/DALA2024040404051), Apr 4, 2024: WEB. CORRODED. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH. SUMMARY OF NRC 00651: CORROSION LEVEL 2. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 
- [SDR DALA2024040103937](https://openairdocs.org/sdr/DALA2024040103937), Mar 30, 2024: LONGERON. CORRODED. CORROSION WAS FOUND ON LONGERON 22LH FROM STA 1017/STA 1049 AND LONGERON ENDS 22LH AND 24 LH STA 1053. ALSO CORROSION ON SHIMS OF LONGERONS 22LH, 23LH, AND 24LH
- [SDR DALA2024040504132](https://openairdocs.org/sdr/DALA2024040504132), Mar 29, 2024: LONGERON. OUT OF LIMITS. THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.080 IN. REMAINING THICKNESS IS 0.043 IN
- [SDR DALA2025103107967](https://openairdocs.org/sdr/DALA2025103107967), Mar 28, 2024: TAB. CORRODED. CORROSION ON SKIN LT & RT SIDE AT RUDDER TAB. REPLACED BY SERVICIABLE RUDDER CONTROL TAB (0266679).
- [SDR DALA2024040103934](https://openairdocs.org/sdr/DALA2024040103934), Mar 28, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON RH FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN (W1). SUMMARY OF NRC 00464: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CAB
- [SDR DALA2024032703842](https://openairdocs.org/sdr/DALA2024032703842), Mar 27, 2024: PAN. CRACKED. CRACKS ON PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00222: DAMAGED SECTIONS OF PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD C
- [SDR DALA2024032703841](https://openairdocs.org/sdr/DALA2024032703841), Mar 27, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1). SUMMARY OF NRC 00468: CORROSION LEVEL 2. L/R FLOOR SUPPORTS BTW STA 160-200 AT X
- [SDR DALA2024032703838](https://openairdocs.org/sdr/DALA2024032703838), Mar 25, 2024: WINDOW FRAME. CRACKED. CRACK WAS FOUND ON FRAME ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00802: UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT WAS REPAIRED PER B7
- [SDR DALA2024032203636](https://openairdocs.org/sdr/DALA2024032203636), Mar 22, 2024: FRAME. CORRODED. CORROSION WAS FOUND ON PREVIOUS REPAIR SPLICES AND FRAME, STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT. SUMMARY OF NRC S/N 00339: CORROSION LEVEL 2. 
- [SDR DALA2024032203634](https://openairdocs.org/sdr/DALA2024032203634), Mar 21, 2024: BEAM. CRACKED. CRACK ON BEAM 1 LH EDGE AT AFT CABIN PRESSURE BULKHEAD. SUMMARY OF NRC 00097: WEB WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND DWG 9915565 REV BD
- [SDR DALA2024032203630](https://openairdocs.org/sdr/DALA2024032203630), Mar 21, 2024: CUSP WEB. CRACKED. CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN. SUMMARY OF NRC 00514: RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN WAS REPAIR
- [SDR DALA2024032103590](https://openairdocs.org/sdr/DALA2024032103590), Mar 20, 2024: LONGERON. CRACKED. CRACKED LONGERON 17LH STA 1022 PAX CABIN. SUMMARY OF NRC 00352: LONGERON 17LH STA 1022 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #0254278)
- [SDR DALA2024032103589](https://openairdocs.org/sdr/DALA2024032103589), Mar 20, 2024: FRAME. CRACKED. CRACKED LH FRAME STA 1037 AT LONG 17LH PAX CABIN. SUMMARY OF NRC 00449: LH FRAME STA 1037 AT LONG 17LH PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE
- [SDR DALA2024032103588](https://openairdocs.org/sdr/DALA2024032103588), Mar 20, 2024: LONGERON. CRACKED. CRACKED LONGERON 17RH STA 1022 PAX CABIN. SUMMARY OF NRC 00353: LONGERON 17RH STA 1022 PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #0254033)
- [SDR DALA2024032103587](https://openairdocs.org/sdr/DALA2024032103587), Mar 20, 2024: DOUBLER. CORRODED. CORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 0069: CORROSION LEVEL 2. FWD AND AFT DOUBLERS OF FWD CARGO C
- [SDR DALA2024032103585](https://openairdocs.org/sdr/DALA2024032103585), Mar 19, 2024: PAN. CRACKED. CRACK ON SPLICE AND PAN NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00219: SPLICE (REPAIR DOUBLER) NEAR TO AFT TORQUE TUBE ARE
- [SDR DALA2024032103578](https://openairdocs.org/sdr/DALA2024032103578), Mar 17, 2024: SKIN. DENTED. DENTS OUT LIMITS WERE FOUND ON REVALUATION DENTS OF LOWER SKIN FWR MOVABLE VANE FLAP AT LH WING. SUMMARY OF NRC 00659: PERMANENT REPAIR WAS PERFORMED ON FWD MOV
- [SDR DALA2024032103572](https://openairdocs.org/sdr/DALA2024032103572), Mar 15, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB BTW STA X=-56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN. SUMMARY OF NRC 00749: CORROSION LEVEL 2. RH CUSP WEB BTW STA X=- 56 TO -60 STA
- [SDR DALA2024032103571](https://openairdocs.org/sdr/DALA2024032103571), Mar 15, 2024: CUSP WEB. CRACKED. CRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN. SUMMARY OF NRC 00513: RH SECTION CUSP WEB WAS FABRICATED AND REPAIRED ON STA X=-56 TO -60 AN
- [SDR DALA2024032103570](https://openairdocs.org/sdr/DALA2024032103570), Mar 15, 2024: CUSP WEB. CRACKED. CRACK ON RH CUSP WEB STA X=-56 AND Y=636-655 ALSO CORROSION AND MISSING FASTENERS AT PASSENGER CABIN. SUMMARY OF NRC 00512: CORROSION LEVEL 2. RH CUSP WEB STA X
- [SDR DALA2024030803186](https://openairdocs.org/sdr/DALA2024030803186), Mar 4, 2024: RELEASE CABLE. OUT OF LIMITS. THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN BEYOND ALLOWABLE LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT 
- [SDR DALA2022110807208](https://openairdocs.org/sdr/DALA2022110807208), Nov 7, 2022: NONE. NONE. ON THE SERVICE CHECK, FOUND AFT F/A JUMPSEAT CEILING EMERGENCY LIGHT OUT AND EXIT SIGN NEAR FLOOR WITH LAMPS OUT. MAINTENANCE RELAMPED THE CEILING EMERGENCY LIG
- [SDR DALA2022110807206](https://openairdocs.org/sdr/DALA2022110807206), Nov 7, 2022: NONE. NONE. ON SERVICE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS WITH MULTIPLE LAMPS OUT. MAINTENANCE RELAMPED BOTH OF THE OVER WING EMERGENCY EXIT LOWER SIGNS PE
- [SDR DALA2022091906175](https://openairdocs.org/sdr/DALA2022091906175), Sep 18, 2022: NONE. NONE. DURING SERVICE CHECK THE RIGHT HAND EMERGENCY LIGHTS IN THE FIRST CLASS ROWS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY
- [SDR DALA2022060103808](https://openairdocs.org/sdr/DALA2022060103808), May 31, 2022: LENS. MISSING. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT ROW 29. MAINTENANCE REPLACED THE MISSING AFT COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2258245)
- [SDR DALA2022060103809](https://openairdocs.org/sdr/DALA2022060103809), May 28, 2022: PSEU. FAULT MESSAGE. SHIP 9542 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING APPROACH DUE TO A PSEU FAILURE MESSAGE. A GO-AROUND WAS PERFORMED, THE QRH WAS COMPLIED WITH, AND THE S

All 203: https://openairdocs.org/aircraft/N996AT/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/N996AT/stcs.md

## Related

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

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