# N944AT: 1999 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: 55007
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD1C16
- 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=944AT
- Page: https://openairdocs.org/aircraft/N944AT

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/N944AT/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 N944AT.

## FAA accident and incident reports

None matched to N944AT.

## Service difficulty reports (237, 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 DALA2025110708147](https://openairdocs.org/sdr/DALA2025110708147), Oct 29, 2025: GIRT BAR. DETACHED. SHIP 9504 DOOR 1R GIRT BAR DETACHED FROM SLIDE MECHANISM. CORRECTIVE ACTION: RESECURED PER B717 AMM 25-61. A/C OK FOR SERVICE. (7954750)
- [SDR DALA2025092306960](https://openairdocs.org/sdr/DALA2025092306960), Sep 20, 2025: DOUBLER. DAMAGED. FUEL LEAK FOUND DURING INSPECTION OF THE L/H WING AFT LOWER SKIN DOUBLER IN THE BRACE FITTING AREA AT XRS = 164, REF: EM 5720- 01103-01A. COMPLIED WITH ER/A 628
- [SDR DALA2025091606812](https://openairdocs.org/sdr/DALA2025091606812), Sep 10, 2025: HINGE FITTING. GOUGED. GOUGE DAMAGE NOTED ON THE LT HORIZONTAL STAB INBD HINGE FITTING WHILE IN ATL FOR C CHECK. ER/A 628919-14 CREATED TO PROVIDE TEMPORARY DISPOSITION FOR NOTED DAMA
- [SDR DALA2025090406567](https://openairdocs.org/sdr/DALA2025090406567), Aug 29, 2025: TRACK. CORRODED. G2 OTBD GALLEY TRACK CORRODED. REPAIRED IAW SRM 53-20-52-2R PROC. 5. (1171207)
- [SDR DALA2025082606327](https://openairdocs.org/sdr/DALA2025082606327), Aug 19, 2025: DOOR FRAME. CRACKED. DOOR JAMB AFT CARGO DOOR DAMAGE REPAIRED REF : B717-200 SRM 53-20-15 (1152187)
- [SDR DALA2025082206258](https://openairdocs.org/sdr/DALA2025082206258), Aug 18, 2025: SEAT TRACK. CORRODED. G2 INBD GALLEY TRACK CORRODED. REPAIRED SEAT TRACK PER B717 SRM 53-20-52 (1150808).
- [SDR DALA2025082206257](https://openairdocs.org/sdr/DALA2025082206257), Aug 18, 2025: DOOR LATCH. DAMAGED. AFT CARGO DOOR OPENING,- FORWARD EDGE AT DOOR LATCH. REPAIRED IAW SRM 53-20-15-2R (1150939)
- [SDR DALA2025082206259](https://openairdocs.org/sdr/DALA2025082206259), Aug 17, 2025: SEAT TRACK. CORRODED. G7 INBD GALLEY TRACK CORRODED. REPAIRED THE SEAT TRACK IAW SRM 53-20-52-2R. (1149132)
- [SDR DALA2025082206256](https://openairdocs.org/sdr/DALA2025082206256), Aug 17, 2025: CUSP WEB. CORRODED. CORROSION ON UPPER SURFACE OF CUSP WEB ADJACENT TO STA 237 FRAME ATTACH FITTING AT X60. REPAIRED CUSP WEB PER SRM 53-00-55-2R (1149078).
- [SDR DALA2025072405583](https://openairdocs.org/sdr/DALA2025072405583), Jul 23, 2025: COVER. DAMAGED. SHIP 9504 AFT DOOR ARMING LEVER COVER DAMAGED / POOR CONDITION (B717 ONLY) / LOCATIONS:606. CORRECTIVE ACTION: ADJUSTED LATCH ON AFT BULKHEAD DOOR COVER ASSY (1
- [SDR DALA2024061005956](https://openairdocs.org/sdr/DALA2024061005956), Jun 7, 2024: ACTUATOR. FAULTED. SHIP 9504 -GEAR/DE- ON APPROACH FOR LANDING THE FLIGHT CREW RECEIVED AN "NLG UNSAFE" INDICATION AFTER SELECTING THE GEAR TO EXTEND. THE QRH WAS COMPLIED WITH, A
- [SDR DALA2024061005954](https://openairdocs.org/sdr/DALA2024061005954), Jun 7, 2024: BOLT. MISSING. NLG LOCK LINK ASSY FOUND UPPER PIN RT I/B BOLT MISSING, LT I//B DAMAGED, AND PROTRUDING WITH EMANATING CORROSION ON UPPER LOCK LINK PIN REF B717 IPC 32-22-01-01
- [SDR DALA2024011600593](https://openairdocs.org/sdr/DALA2024011600593), Jan 16, 2024: UNKNOWN. UNKNOWN. ON SERVICE CHECK FOUND A FEW CEILING EMERGENCY LIGHTS OUT. MAINTENACE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT LOCATION B5-227 PER B717 AMM 33-51-04. OPERA
- [SDR DALA2023102308704](https://openairdocs.org/sdr/DALA2023102308704), Oct 23, 2023: UNKNOWN. UNKNOWN. DURING THE SERVICE CHECK, MAINTENANCE FOUND THE L-1 DOOR FWD EXIT LIGHT AND THE R-1 DOOR AFT EXIT LIGHT EACH INOPERATIVE. THE POWER SUPPLY WAS REPLACED PER B717
- [SDR DALA2023080406296](https://openairdocs.org/sdr/DALA2023080406296), Jul 27, 2023: UNKNOWN. UNKNOWN. WEB-CORRODED FS 1053 AFT SIDE AT STR 28 LH (P DOME AREA). SUMMARY NRC 096-0022:5310-2014/003 00258: CLEANED AREA CHECKED LIMITS REF B717-200 SRM 53-00-00-1A. RE
- [SDR DALA2023071205670](https://openairdocs.org/sdr/DALA2023071205670), Jul 10, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. MAINTENANCE REPLACED THE EMERGENCY EXIT COVER AT R1 DOOR. (LP #2858553)
- [SDR DALA2022123008502](https://openairdocs.org/sdr/DALA2022123008502), Dec 29, 2022: BATTERY PACK. INOPERATIVE. THE OVERWING EMERGENCY EXIT LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT SEAT ROW 20 IAW AMM 33-51. OPERATIONAL CHECK WA
- [SDR DALA2022101606675](https://openairdocs.org/sdr/DALA2022101606675), Oct 15, 2022: BATTERY PACK. INOPERATIVE. AIRCRAFT 9504, DURING SVC CHECK FOUND ROW 17 EMERGENCY LIGHTS NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMER LIGHT POWER SUPPLY BATTERY AT STA 645. LP 9420941
- [SDR DALA2022041202524](https://openairdocs.org/sdr/DALA2022041202524), Apr 9, 2022: NONE. NONE. CORROSION ON LOWER DOOR JAMB REPAIR AT AFT CARGO DOOR JAMB BTW STA 954 TO 990 (CCT). SUMMARY OF NRC 00013: LEVEL CORROSION 2, LOWER DOOR JAMB AFT CARGO DOOR WAS
- [SDR DALA2022041202523](https://openairdocs.org/sdr/DALA2022041202523), Apr 9, 2022: NONE. NONE. HIDDEN CORROSION IN REF NRC 013: CORROSION ON INTERNAL PRODUCTION DOUBLER BELOW PAN ON AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 00091: LEVEL CORROS
- [SDR DALA2022041202522](https://openairdocs.org/sdr/DALA2022041202522), Apr 9, 2022: NONE. NONE. AN OUT OF LIMIT CRACK ON FLOOR BEAM STA Y=737 AND BTW X=52 RH TO X=56 RH. SUMMARY OF NRC 00095: FLOOR BEAM STA Y=737 AND BTW X=52 RH TO X=56 RH WAS REPAIRED PER
- [SDR DALA2022041302580](https://openairdocs.org/sdr/DALA2022041302580), Apr 8, 2022: VANE. DENTED. DENTS 2EA ON UPPER SURFACE OF UPPER VANE STA XRS 91.000 LH WING (LW). SUMMARY OF NRC 00027: FWD MOVABLE FLAP VANE LH WAS REMOVED AND INSTALLED PER B717 AMM 27-5
- [SDR DALA2022041302582](https://openairdocs.org/sdr/DALA2022041302582), Apr 7, 2022: VANE. DEBONDED. DISBOND OF 1.10 IN X 1.00 IN LENGHT/WIDTH ON OUTBOARD FIXED GUIDE VANE AT RH WING. SUMMARY OF NRC 00239: OUTBOARD FIXED GUIDE VANE AT RH WING WAS REPAIRED PER B
- [SDR DALA2022040602319](https://openairdocs.org/sdr/DALA2022040602319), Apr 4, 2022: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH. SUMMARY OF NRC 00114: CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND LONGERON 14 LH WAS REPAIRED 
- [SDR DALA2021091105378](https://openairdocs.org/sdr/DALA2021091105378), Sep 11, 2021: ACCESS PANEL. MISSING. THE ACCESS PLATE IS MISSING FROM THE UPPER VERTICAL RIGHT SIDE STABILIZER BEARING DOOR 370PR. FOUND ON WALK AROUND AT GATE. MAINTENANCE INSTALLED THE ACCESS COV
- [SDR DALA2020121404061](https://openairdocs.org/sdr/DALA2020121404061), Dec 12, 2020: BATTERY PACK. INOPERATIVE. THE AFT TAIL COMP EMERGENCY WALKWAY LIGHTS ARE NOT WORKING. MAINTENANCE REPLACED THE BATTERY PACK AT B5-260 AT STA 1037L, IAW B717 AMM 33-51-03. OPERATIONAL CHE
- [SDR DALA2020042702298](https://openairdocs.org/sdr/DALA2020042702298), Apr 27, 2020: CONNECTOR. LOOSE. THREE (3) ROWS JUST FORWARD OF OVERWING EXIT ROWS, EACH HAVE THE EMERGENCY EXIT PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT THE EMERGENCY LIGHT BATTERY PACK
- [SDR DALA2020022501415](https://openairdocs.org/sdr/DALA2020022501415), Feb 24, 2020: LENS. MISSING. THE CABIN SIDEWALL EMERGENCY LIGHT IS MISSING IT'S COVER. MAINTENANCE INSTALLED A NEW COVER. OPERATIONAL CHECK WAS GOOD. (LP #1503125)
- [SDR DALA2019080904672](https://openairdocs.org/sdr/DALA2019080904672), Aug 8, 2019: POWER SUPPLY. INOPERATIVE. DURING CHECK OF CONDITION OF THE LIGHTED EXIT SIGN LOCATED ABOVE VENTRAL DOOR THE LIGHT DID NOT WORK.. REF CARD 1130-2002 STEP 28. EMERGENCY LIGHTS POWER SUPPLY
- [SDR DALA2019073004483](https://openairdocs.org/sdr/DALA2019073004483), Jul 29, 2019: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATES #520FT, 620AT, AND 620FT WERE FOUND OUT OF LIMITS REF SRM 57-10-01-2R REPAIR 2 CORROSION LEVEL II. NRC 0080
- [SDR DALA2019072904459](https://openairdocs.org/sdr/DALA2019072904459), Jul 28, 2019: ACCESS PANEL. DAMAGED. ELONGATED HOLES IN ACCESS PLATE #520MB AND 520FT AT FUEL TANK LEFT WING (AI). NRC 00611: ELONGATED HOLES IN FUEL ACCESS PLATE #520MB WAS REPAIRED PER SRM 57-10-
- [SDR DALA2019072904482](https://openairdocs.org/sdr/DALA2019072904482), Jul 27, 2019: CHANNEL. CRACKED. CRACKS (2 EA.) IN CHANNEL FLOOR PANEL #222ZF. NRC 00797: CHANNEL FLOOR PANEL #222ZF WAS REPAIRED PER SRM 53-20-50-2R-5 REPAIR 5. (LP #1193258)
- [SDR DALA2019072804456](https://openairdocs.org/sdr/DALA2019072804456), Jul 27, 2019: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL FROM STA Y=946 TO Y=954 ABOVE LONG PROJECTION 29R AT AFT CARGO COMPARTMENT. NRC 00348: CORROSION LEVEL 2, INTERCOSTAL FROM STA Y=946 TO
- [SDR DALA2019072704455](https://openairdocs.org/sdr/DALA2019072704455), Jul 27, 2019: FRAME. CORRODED. EXFOLATION ON FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT. NRC 00362: CORROSION LEVEL 2, FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COM
- [SDR DALA2019072704454](https://openairdocs.org/sdr/DALA2019072704454), Jul 26, 2019: FRAME. CORRODED. CORROSION ON FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CARGO COMPARTMENT. NRC 00338: CORROSION LEVEL 2, FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CA
- [SDR DALA2019072704453](https://openairdocs.org/sdr/DALA2019072704453), Jul 26, 2019: SKIN. PUNCTURED. PUNCTURE ON FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 30 LT SIDE (SM). NRC 00126: FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 
- [SDR DALA2019072604452](https://openairdocs.org/sdr/DALA2019072604452), Jul 25, 2019: FITTING. CORRODED. CORROSION ON FRAME CLIP STA Y=954 BTW LONG 30 TO 29L AT AFT CARGO COMPARTMENT. NRC 00352: CORROSION LEVEL 2, FRAME CLIP STA Y=954 BTW LONG 30 TO 29L AT AFT CARG
- [SDR DALA2019072604420](https://openairdocs.org/sdr/DALA2019072604420), Jul 25, 2019: FRAME. CRACKED. CRACK (0.250" LENGTH) ON THE UPPER RADIUS OF THE FRAME TAB OF THE RH OVERWING FRAME AT STA Y=715. NRC 0283: RH OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD
- [SDR DALA2019072604419](https://openairdocs.org/sdr/DALA2019072604419), Jul 25, 2019: FRAME. CRACKED. CRACK (0.218" LENGTH) ON THE UPPER RADIUS OF THE FRAME TAB OF THE RT OVERWING FRAME AT STA Y=674. NRC 0282: RT OVERWING FRAME AT STA Y=674 WAS REPLACED PER CARD
- [SDR DALA2019072604418](https://openairdocs.org/sdr/DALA2019072604418), Jul 25, 2019: FLOOR PANEL. BROKEN. BROKEN FLOOR PANEL #1680B AT PAX CABIN. NRC 00613: FLOOR PANEL #1680B WAS FABRICATED, REPLACED, AND IDENTIFIED PER AMM 53-01-01-201. (LP #1189752)
- [SDR DALA2019072604416](https://openairdocs.org/sdr/DALA2019072604416), Jul 25, 2019: ACCESS PANEL. CORRODED. CORROSION ON HOLES COUNTERSUNK AND AREA SETTLEMENT AT ACCESS #620CT AND 520CT. FUEL TANK (AD,AI). NRC 00612: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 62
- [SDR DALA2019072504391](https://openairdocs.org/sdr/DALA2019072504391), Jul 25, 2019: FITTING. CORRODED. CORROSION ON FRAME CLIP STA Y=927 BTW LONG 28L TO LONG 28R AT AFT CARGO COMPARTMENT. NRC 00337: CORROSION LEVEL 2, CORROSION ON FRAME CLIP STA Y=927 BTW LONG 28
- [SDR DALA2019072504387](https://openairdocs.org/sdr/DALA2019072504387), Jul 24, 2019: INTERCOSTAL. CRACKED. INTERCOSTAL WAS FOUND CRACKED ON STA Y=674 LONGERON 17R, IN REF 5310-01436-03B STEP F, AT CABIN PASSENGER (CPAX). NRC 00741: INTERCOSTAL ON STA Y=674 LONGERON 1
- [SDR DALA2019072404371](https://openairdocs.org/sdr/DALA2019072404371), Jul 23, 2019: WINDOW FRAME. CRACKED. CRACK ON WINDOW FRAME BTW STA 715 RT SIDE CABIN PAX (SM). NRC 00677: WEB FRAME STA 715 BTW LONG 12 TO LONG 15 SIDE RT WAS REPLACED PER SRM 51-41-02-0G AND 51-41
- [SDR DALA2019072404370](https://openairdocs.org/sdr/DALA2019072404370), Jul 23, 2019: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BTW STA Y=579 TO 598 UPPER AND LOWER SURFACES (CPAX). NRC 00593: CORROSION LEVEL 2, RT CUSP WEB BTW STA Y=579 TO 598 UPPER AND LOWER SU
- [SDR DALA2019072404369](https://openairdocs.org/sdr/DALA2019072404369), Jul 23, 2019: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BTW STA Y=465 TO 484 UPPER AND LOWER SURFACES (CPAX). NRC 00600: CORROSION LEVEL 2, RT CUSP WEB BTW STA Y=389 TO 503 UPPER AND LOWER SU
- [SDR DALA2019072204386](https://openairdocs.org/sdr/DALA2019072204386), Jul 22, 2019: ACCESS PANEL. CORRODED. CORROSION ON FUEL TANK ACCESS PLATE. NRC 774: CORROSION LEVEL 2, CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE WAS FOUND OUT OF LIMITS REF SRM 57-10-01-2R
- [SDR DALA2019072304359](https://openairdocs.org/sdr/DALA2019072304359), Jul 22, 2019: SUPPORT. CRACKED. CRACK ON SUPPORT OF FLOOR ACCESS PANEL #223AF (SM). NRC 00642: SUPPORT OF FLOOR ACCESS PANEL #223AF WAS REPAIRED PER SRM 53-20-50-2R-5. (LP #1184074)
- [SDR DALA2019072204358](https://openairdocs.org/sdr/DALA2019072204358), Jul 22, 2019: LONGERON. CORRODED. CORROSION ON LONG 30 BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. NRC 00331: CORROSION LEVEL 2, LONG 30 BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT WA
- [SDR DALA2019072204357](https://openairdocs.org/sdr/DALA2019072204357), Jul 21, 2019: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANELS #211AJF AND 211ANF IN THE COCKPIT (COM). NRC 00629: DELAMINATED FLOOR PANEL #211ANF WAS REPLACED PER SRM 53-20-50-2R-3. THE FLOOR PANEL

All 237: https://openairdocs.org/aircraft/N944AT/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/N944AT/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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