# N951AT: 2000 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: 55013
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2000
- Certificate issued: November 21, 2023
- Expires: November 30, 2030
- Mode S code: AD3870
- 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=951AT
- Page: https://openairdocs.org/aircraft/N951AT

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/N951AT/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 N951AT.

## FAA accident and incident reports

None matched to N951AT.

## Service difficulty reports (209, 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 DALA2026080604545](https://openairdocs.org/sdr/DALA2026080604545), Aug 6, 2026: DOUBLER. WORN. WEAR ON REPAIR DOUBLER ON FIXED LEADING EDGE STA XIS= 134, CUTOUT OF SLAT TRACK 2 AT RIGHT WING, COMPLIED WITH ER/A 635913-14. (1741054) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604544](https://openairdocs.org/sdr/DALA2026080604544), Aug 6, 2026: DOUBLER. WORN. WEAR ON REPAIR DOUBLER ON FIXED LEADING EDGE STA XIS= 134, CUTOUT OF SLAT TRACK 2 AT RIGHT WING, COMPLIED WITH ER/A 635913-14. (1741051) (AIRCRAFT GROUNDED).
- [SDR DALA2026072804380](https://openairdocs.org/sdr/DALA2026072804380), Jul 27, 2026: CUSP WEB. CRACKED. CRACKS ON CUSP WEB WRE FOUND ON STA X= -58 AND STA Y= 674, Y= 696, AND Y= 715 AT CPAX, ALSO CORROSION ON CUSP WEB ON STA X= -58 AND STA Y= 713 AT CPAX. CUSP WEB
- [SDR DALA2026071704222](https://openairdocs.org/sdr/DALA2026071704222), Jul 16, 2026: SKIN. GOUGED. LOWER LT WING SKIN UPPER SURFACE GOUGED AT WS 137 STRINGER 11 APPROX 2.4 LONG AND APPROX 0.017 DEEP, COMPLIED WITH ER/A 63340-14AD. (1702226) (AIRCRAFT GROUNDED
- [SDR DALA2026071704221](https://openairdocs.org/sdr/DALA2026071704221), Jul 16, 2026: SKIN. CRACKED. FOUND STR 11 LT CRACKED APPROX BS 160 AND 3 SKIN CRACKS , 2 AT HOLE S4 AND 1 EMANATING FROM HOLE S3, COMPLIED WITH ER/A 633840-14. (1702209) (AIRCRAFT GROUNDED)
- [SDR DALA2026071304129](https://openairdocs.org/sdr/DALA2026071304129), Jul 12, 2026: PANEL. NO DISCREPANCY. REMOVE AND INSTALL LH I/B SPOILER PANEL TO FOM. REPAIRED LH I/B SPOILER PANEL REF B717 AMM 27-60-01. (1695364) (AIRCRAFT GROUNDED)
- [SDR DALA2026070904036](https://openairdocs.org/sdr/DALA2026070904036), Jul 8, 2026: DOUBLER. CRACKED. CRACK INDICATIONS IN THE LT MLG DOUBLER AREA AT UPPER AUX SPAR #1, #2 AND LOWER AUX SPAR #3, UNK #1,#2,#3, COMLIED WITH ER/A 634210-14. (1688524) (AIRCRAFT GROU
- [SDR DALA2026070803994](https://openairdocs.org/sdr/DALA2026070803994), Jul 7, 2026: SKIN. CRACKED. FOUND CRACK AT INBOARD OF XSR 164 AND THE LOWER WING SKIN BETWEEN STRINGER S-11 AND THE REAR SPAR, COMPLIED WITH ER/A 634526-14AD. (1686898) (AIRCRAFT GROUNDED)
- [SDR DALA2026070603942](https://openairdocs.org/sdr/DALA2026070603942), Jul 3, 2026: SKIN. DAMAGED. SKIN DAMAGE LT VERT CAP FROM AIR GATE FAIRING. REPAIRED PER ER/A 635425-14. (1679920)(AIRCRAFT GROUNDED)
- [SDR DALA2026070303897](https://openairdocs.org/sdr/DALA2026070303897), Jun 23, 2026: SPAR. CRACKED. CRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).
- [SDR DALA2026070303896](https://openairdocs.org/sdr/DALA2026070303896), Jun 23, 2026: SPAR. CRACKED. CRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).
- [SDR DALA2026070303895](https://openairdocs.org/sdr/DALA2026070303895), Jun 23, 2026: SKIN. CRACKED. CRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).
- [SDR DALA2026042102508](https://openairdocs.org/sdr/DALA2026042102508), Apr 15, 2026: SKIN. CRACKED. CRACK INDICATION ON LOWER SKIN, INBD SIDE OF STA=164 BRACE DOUBLE 1.375" FROM INBD AFT EDGE. REF ERA 633599-14AD FOR ALL MAINT REPAIR. (1546137) (AIRCRAFT GROUN
- [SDR DALA2026042102515](https://openairdocs.org/sdr/DALA2026042102515), Apr 15, 2026: SKIN. CRACKED. LEFT WING INTERNAL LOWER SKIN HAS ONE CRACK 6 INCHES INBOARD OF XRS=164. RUNNING FWD AND AFT 1.0" FWD OF REAR SPAR CAP. VERIFIED WITH HFEC. IAW ERA 633599-14AD 
- [SDR DALA2026031301750](https://openairdocs.org/sdr/DALA2026031301750), Mar 9, 2026: UNKNOWN. ODOR. FA'S REPORTED DIRTY SOCK SMELL IN CABIN ON APPROACH INTO BWI. NO SMOKE OR FUMES WERE NOTED, ODOR ONLY. COMPLETED W/C 0550-9001-B717 (8476228)
- [SDR DALA2025042103070](https://openairdocs.org/sdr/DALA2025042103070), Apr 16, 2025: WARNING MESSAGE. ILLUMINATED. SHIP 9510 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 110 KTS DUE TO RECEIVING AN AURAL "SLAT CONFIGURATION" MESSAGE. CORRECTIVE ACTION: MAINTENANCE (LP #75077
- [SDR DALA2024100409700](https://openairdocs.org/sdr/DALA2024100409700), Oct 3, 2024: BARREL NUT. CORRODED. CORROSION ON BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH), AND 29 (LOWER RH) AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00544: CORROSION LEVE
- [SDR DALA2024100209618](https://openairdocs.org/sdr/DALA2024100209618), Sep 28, 2024: SKIN. CORRODED. -AD- CORROSION ON UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL. SUMMARY OF NRC 00216: CORROSION LEVEL 2. UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT L
- [SDR DALA2024100209616](https://openairdocs.org/sdr/DALA2024100209616), Sep 27, 2024: SKIN. CRACKED. -AD- CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH (FUS). SUMMARY OF NRC 00348: CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH WAS REPAIRED PER ER/A 6199
- [SDR DALA2024091809138](https://openairdocs.org/sdr/DALA2024091809138), Sep 17, 2024: SKIN. CRACKED. CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R. SUMMARY OF NRC 00047: CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R WAS REPAIRE
- [SDR DALA2024090508739](https://openairdocs.org/sdr/DALA2024090508739), Sep 4, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00135: CORROSION LEVEL 2. FLOORBEAM STA Y=653 BTW LONG 28L A
- [SDR DALA2024090408733](https://openairdocs.org/sdr/DALA2024090408733), Sep 3, 2024: PAN. CORRODED. CORROSION ON JAMB PAN (BTW LONG 25RH-29RH) LOWER EDGE AND AFT EDGE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2. JAMB PAN (BTW LONG 25
- [SDR DALA2024090308638](https://openairdocs.org/sdr/DALA2024090308638), Sep 2, 2024: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00804: CORROSION LEVEL 2. INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E C
- [SDR DALA2024090308634](https://openairdocs.org/sdr/DALA2024090308634), Aug 31, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN. SUMMARY OF NRC 00753: CORROSION LEVEL 2. LH CUSP WEB UPPER/LOWER SUR
- [SDR DALA2024090308633](https://openairdocs.org/sdr/DALA2024090308633), Aug 30, 2024: DOUBLER. CORRODED. CORROSION ON DOUBLER PRODUCTION OF MASTER DRAIN BTW STA Y=199 AND Y=218, L28R, AND L29R. ALSO STA Y=163, Y= 183 BTW L29L AND L30 AT E/E COMPARTMENT. SUMMARY OF 
- [SDR DALA2024083008597](https://openairdocs.org/sdr/DALA2024083008597), Aug 29, 2024: BEAM. CRACKED. CRACK BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00225: BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT WAS R
- [SDR DALA2024083008595](https://openairdocs.org/sdr/DALA2024083008595), Aug 28, 2024: WINDOW FRAME. CRACKED. CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW. SUMMARY OF NRC 00693: FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW WAS RE
- [SDR DALA2024082808523](https://openairdocs.org/sdr/DALA2024082808523), Aug 27, 2024: WEB. CRACKED. AIRCRAFT 9510, CRACK UNDER, INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX. CORRECTIVE ACTION: INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT
- [SDR DALA2024082808522](https://openairdocs.org/sdr/DALA2024082808522), Aug 27, 2024: CUSP WEB. CORRODED. AIRCRAFT 9510, CORROSION OUT OF LIMITS WAS FOUND ON PASSENGER CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN. CORRECTIVE ACTION: CORRO
- [SDR DALA2024082708490](https://openairdocs.org/sdr/DALA2024082708490), Aug 27, 2024: LONGERON. CRACKED. AIRCRAFT 9510, CRACK ON LONGERON END (2EAS) FROM STA 1133 BTW LONG 2 LH TO LONG 2RH OF AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: LONGERON END FROM STA 1133 
- [SDR DALA2024082708489](https://openairdocs.org/sdr/DALA2024082708489), Aug 26, 2024: CUSP WEB. CORRODED. AIRCRAFT 9510, CORROSIONS ON CUSP MEMBRANE (WEB) RH ON SEVERAL LOCATIONS FROM STA Y=560 TO STA Y=579 AND STA Y=503 TO STA Y=522 AND STA Y=484 TO STA Y=503 AND S
- [SDR DALA2024082708488](https://openairdocs.org/sdr/DALA2024082708488), Aug 26, 2024: CUSP WEB. CRACKED. AIRCRAFT 9510, INITIAL INSPECTION: CRACK ON CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH BTW STA Y=389 T
- [SDR DALA2024082708487](https://openairdocs.org/sdr/DALA2024082708487), Aug 26, 2024: CUSP WEB. CRACKED. AIRCRAFT 9510, AFTER BLEND OUT CRACKS WERE FOUND AT LH CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB ON STATIONS 
- [SDR DALA2024082708486](https://openairdocs.org/sdr/DALA2024082708486), Aug 26, 2024: WINDOW FRAME. CRACKED. AIRCRAFT 9510, HIDDEN DISCPRECANCY; AFTER BRACKET WAS REMOVED, CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW. CORRECTIVE ACTION: FR
- [SDR DALA2024082408420](https://openairdocs.org/sdr/DALA2024082408420), Aug 24, 2024: CUSP WEB. CORRODED. AIRCRAFT 9510, CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 A
- [SDR DALA2024082308415](https://openairdocs.org/sdr/DALA2024082308415), Aug 23, 2024: CUSP WEB. CRACKED. AIRCRAFT 9510, CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX. CORRECTIVE ACTION: CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX WER
- [SDR DALA2024082208361](https://openairdocs.org/sdr/DALA2024082208361), Aug 21, 2024: FLOORBEAM. CORRODED. AIRCRAFT 9510, CORROSION ON FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 AT PAX CABIN STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 
- [SDR DALA2024082108331](https://openairdocs.org/sdr/DALA2024082108331), Aug 20, 2024: CUSP WEB. CORRODED. AIRCRAFT 9510, INITIAL INSPECTION: CORROSION ON LH REPAIR DOUBLER OF CUSP WEB STA Y=841, Y=866 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2-LH CUSP WEB ST
- [SDR DALA2024081908280](https://openairdocs.org/sdr/DALA2024081908280), Aug 16, 2024: BEAM. CRACKED. CRACK ON BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR. SUMMARY OF NRC 00357: BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV OR
- [SDR DALA2024081908241](https://openairdocs.org/sdr/DALA2024081908241), Aug 16, 2024: SKIN. GOUGED. GOUGE ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00704: EXTERNAL SKIN ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 5
- [SDR DALA2024081608208](https://openairdocs.org/sdr/DALA2024081608208), Aug 15, 2024: CUSP WEB. CRACKED. CRACK ON INBD CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX. SUMMARY OF NRC 00389: CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX WAS R
- [SDR DALA2024081408113](https://openairdocs.org/sdr/DALA2024081408113), Aug 14, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2). SUMMARY OF NRC 00670: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.
- [SDR DALA2024070106608](https://openairdocs.org/sdr/DALA2024070106608), Jun 15, 2024: APU. FIRE. SHIP 9510 -FIRE- WORKING APU MEL FOR NO START, TECHNICIANS REPLACED FCU AND START FUEL PURGE VALVE. APU WAS RUNNING FOR 15 MINUTES FOR LEAK AND OPS CHECKED WHEN
- [SDR DALA2024022002328](https://openairdocs.org/sdr/DALA2024022002328), Feb 18, 2024: BATTERY PACK. INOPERATIVE. THE OVERWING EMERGENCY LIGHTS STAY ON. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY REF B717 AMM 33-51. BATTERY WAS CHARGED UP. O
- [SDR DALA2023111309309](https://openairdocs.org/sdr/DALA2023111309309), Nov 11, 2023: UNKNOWN. UNKNOWN. BOTH THE LH & RH FWD OVERWING EXIT FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY AT STA 342R PER B717 AMM 33
- [SDR DALA2023061504875](https://openairdocs.org/sdr/DALA2023061504875), Jun 14, 2023: UNKNOWN. UNKNOWN. WORKING AMDS AA CARD 5310-01436-03B. REPLACED RT SIDE FRAME AT STA 674 ON AMDS AA CARD 5310-01436-03B. (LP #4669550)
- [SDR DALA2023060804665](https://openairdocs.org/sdr/DALA2023060804665), Jun 7, 2023: UNKNOWN. UNKNOWN. CRACK INDICATION AT OVERWING FRAME TAB STA 674 RT SIDE, MARKED (FLOOR LEVEL). SUMMARY SEE NRC 073-0004:5310-01436-01D/002 00055: REPLACED DAMAGED FRAME ON WC 53
- [SDR DALA2023060704642](https://openairdocs.org/sdr/DALA2023060704642), Jun 5, 2023: UNKNOWN. UNKNOWN. LONGERON AT 11R FWD OF FRAME STA 674" REQUIRES REMOVAL FOR ACCESS TO MAKE FRAME REPLACEMENT AT STA. 674". SUMMARY SEE NRC 129-0002:5310-01436-03B/003 00293: COM
- [SDR DALA2023030701662](https://openairdocs.org/sdr/DALA2023030701662), Mar 4, 2023: NONE. NONE. THE AISLE OVERHEAD EMERGENCY LIGHT COVER IS MISSING AT ROW 3. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE. (LP #9677521)
- [SDR DALA2022120607805](https://openairdocs.org/sdr/DALA2022120607805), Dec 5, 2022: ACCESS PANEL. MISSING. THE LEFT WING INBOARD FLAP IS MISSING THE INSPECTION COVER. MAINTENANCE INSTALLED AN ACCESS COVER.

All 209: https://openairdocs.org/aircraft/N951AT/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/N951AT/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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