# N925AT: 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: 55079
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 7, 2000
- Certificate issued: April 2, 2025
- Expires: April 30, 2032
- Mode S code: ACD0CF
- 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=925AT
- Page: https://openairdocs.org/aircraft/N925AT

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/N925AT/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 N925AT.

## FAA accident and incident reports

None matched to N925AT.

## Service difficulty reports (182, 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 DALA2025121709200](https://openairdocs.org/sdr/DALA2025121709200), Dec 15, 2025: ACTUATOR. FAULTED. MISC/DE-DECLARED AN EMERGENCY INTO ATL DUE TO LEFT AND RIGHT MAIN GEAR UNSAFE LIGHTS. REPLACED LANDING GEAR DOOR ACTUATOR. OPS TESTED NORMAL.(5447268)
- [SDR DALA2025121009015](https://openairdocs.org/sdr/DALA2025121009015), Dec 7, 2025: SENSOR. OUT OF ADJUST. ATB, PERFORMED AN AIR TURN BACK DUE TO LEFT AND RIGHT MAIN GEAR UNSAFE LIGHTS. COMPLIED WITH NO GO MSI LOG, ADJUSTED LEFT DOOR ACTUATOR TO WITHIN LIMITS, ADJUST
- [SDR DALA2025120508918](https://openairdocs.org/sdr/DALA2025120508918), Dec 2, 2025: PROXIMITY SWITCH. FAULTED. DIVERTED TO CVG DUE TO A GEAR UNSAFE MESSAGE. REPLACED PSEU, ALL TEST PASS. ADJUSTED RIGHT LANDING DOOR LATCH PROX SWITCH. OPS CHECK NORMAL.(5447210)
- [SDR DALA2025111808428](https://openairdocs.org/sdr/DALA2025111808428), Nov 17, 2025: SPAR CAP. CRACKED. DISCOVERED A CRACK COMMON TO THE RT WING LOWER REAR SPAR CAP. COMPLIED WITH ERA 620694-14AD (1308670).
- [SDR DALA2025111908462](https://openairdocs.org/sdr/DALA2025111908462), Nov 16, 2025: SPAR CAP. CRACKED. WHILE TROUBLESHOOTING A FUEL LEAK, MAINTENANCE DISCOVERED A CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATE
- [SDR DALA2025110708136](https://openairdocs.org/sdr/DALA2025110708136), Nov 2, 2025: PANEL. NOT REPORTED. L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852". REMOVED L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852" (1284968)
- [SDR DALA2025102407795](https://openairdocs.org/sdr/DALA2025102407795), Oct 22, 2025: ACCESS PANEL. DAMAGED. FOUND FASTENER HOLE OUT OF ROUND AT TANK PLATE 520HB. REPAIRED REF ERA 629530-14 REV O (1265545)
- [SDR DALA2025063004854](https://openairdocs.org/sdr/DALA2025063004854), Jun 25, 2025: STRINGER SPLICE. NO DISCREPANCY. SHIP 9574 SPLICE STRINGERS 13L AND 14L AT STA 1022 FOR ACCESS REF NR 1585. CORRECTIVE ACTION: COMPLETED AND MATCH FINAL - E/RA 624873-14 (1045986)
- [SDR DALA2025062604795](https://openairdocs.org/sdr/DALA2025062604795), Jun 25, 2025: SKIN. CRACKED. SHIP 9574 FUSELAGE SKIN. VISUAL INDICATION OF CRACK. LOCATED ABOVE #1 PYLON AT STA 1022. CORRECTIVE ACTION: REPAIRED PER E/RA 624873-14 REV. ORIG. (1045993)
- [SDR DALA2025052203936](https://openairdocs.org/sdr/DALA2025052203936), May 15, 2025: SKIN. CRACKED. SHIP 9574 CRACK INDICATION ABOVE THE L/H PYLON IN THE FUSELAGE SKIN. CORRECTIVE ACTION: DOUBLER REPAIR ON A CRACK DAMAGE ON FUSELAGE SKIN P/N 5936436- 101, STA 
- [SDR DALA2025050503406](https://openairdocs.org/sdr/DALA2025050503406), May 2, 2025: FRAME. DAMAGED. STA 1053.00 PRESSURE BULKHEAD LOWER Y CHORD DAMAGED BETWEEN LONGERON 26L-LONGERON 28L. SUMMARY SEE NRC 001-0575:5300-2013/024 01395: COMPLIED WITH E/RA 625071-1
- [SDR DALA2025042103075](https://openairdocs.org/sdr/DALA2025042103075), Apr 19, 2025: SPAR. CORRODED. LH AUX SPAR WEB 9919401-3 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/207 01575: REPLACED PER B717 DWG 9919401. (LP #0921231)
- [SDR DALA2025042103074](https://openairdocs.org/sdr/DALA2025042103074), Apr 19, 2025: STIFFENER. CORRODED. LH AUX SPAR WEB STIFFENER 9919401-5 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/209 01577: REPLACED PER B717 DWG 9919401. (LP #09212
- [SDR DALA2026012700608](https://openairdocs.org/sdr/DALA2026012700608), Apr 9, 2025: SUPPORT ANGLE. CORRODED. AFT SIDE OF FRAME WEB & LOWER SUPPORT ANGLE ARE CORRODED, JUST FWD OF PRESSURE DOME FWD FACE, LBL14 -RBL 14. REPLACED DOUBLER SUPPORT ANGLE BETWEEN JACK SUPPORT
- [SDR DALA2026012700607](https://openairdocs.org/sdr/DALA2026012700607), Apr 9, 2025: SEAT TRACK. CORRODED. RIGHT OTBD SEAT TRACK, FWD TIE FITTING AT FWD END OF TRACK, BS 212 CORRODED. REPLACED THE SEAT TRACK END FITTING IAW DWG 5930566. (0903766)
- [SDR DALA2025102407791](https://openairdocs.org/sdr/DALA2025102407791), Apr 9, 2025: HINGE FITTING. CORRODED. LT FLAP I/B FWD HINGE FITTING MOUNT PINS ON REAR SPAR CORRODED 4EA. REPAIRED PER ERA 620694-14AD. (0904194)
- [SDR DALA2025040902761](https://openairdocs.org/sdr/DALA2025040902761), Apr 9, 2025: WEB. CORRODED. WEB FOUND CORRODED LHS OF Y CHORD AT STA 1053. SUMMARY SEE NRC 001-0575:5300-2013/027 01414: REPAIRED WEB REF B717 SRM 51-70-10-2R REPAIR 1. (LP #0903790)
- [SDR DALA2025040902757](https://openairdocs.org/sdr/DALA2025040902757), Apr 8, 2025: NONE. NONE. CUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-35 AT APPROX LBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/018 01367: CUT, REMOVED, AND REINSTALLED A
- [SDR DALA2025040902756](https://openairdocs.org/sdr/DALA2025040902756), Apr 8, 2025: NONE. NONE. CUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-36 AT APPROX RBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/019 01368: CUT, REMOVED, AND REINSTALLED A
- [SDR DALA2025040102468](https://openairdocs.org/sdr/DALA2025040102468), Mar 26, 2025: FRAME. CORRODED. FS 1022, LOWER PRIOR FRAME REPAIR AT STR 29LT-30 IS CORRODED. SUMMARY SEE NRC 001-0545:5331-2001/010 01244: CORROSION LEVEL 2. REPAIRED 3 ROLLED Z-FRAME REPAIR 
- [SDR DALA2025031902065](https://openairdocs.org/sdr/DALA2025031902065), Mar 19, 2025: FRAME. CORRODED. CORROSION FOUND ON FRAME AT F.S. 889 BETWEEN STRINGER 29L. SUMMARY SEE NRC 001-0508:2550-2001/008 01228: CLEANED UP FRAME REF B717-200 SRM 53-00-00-1A ALLOWABLE
- [SDR DALA2025031702026](https://openairdocs.org/sdr/DALA2025031702026), Mar 15, 2025: SEAT TRACK. CORRODED. RIGHT MID SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/013 00986: REPAIRED PER B717 SRM 53-20-52 REPAIR 5 (CP LEVEL 2) CLOSING
- [SDR DALA2025031702024](https://openairdocs.org/sdr/DALA2025031702024), Mar 14, 2025: SEAT TRACK. CORRODED. RIGHT I/B SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/012 00985: REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 (CPCP LEVEL 1)
- [SDR DALA2025031702021](https://openairdocs.org/sdr/DALA2025031702021), Mar 14, 2025: FITTING. CORRODED. STR 25R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/567 01398: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1
- [SDR DALA2025031702020](https://openairdocs.org/sdr/DALA2025031702020), Mar 14, 2025: STRINGER. CORRODED. STR 26R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/566 01397: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1
- [SDR DALA2026012700609](https://openairdocs.org/sdr/DALA2026012700609), Mar 13, 2025: LONGERON. CORRODED. CORROSION UNDER BATTERY TRAYS, LONGERON. REMOVED AND REPLACED THE LONGERON IAW DWG 5911401. (0855196)
- [SDR DALA2025031201903](https://openairdocs.org/sdr/DALA2025031201903), Mar 11, 2025: STRINGER. CORRODED. CORRODED STR 30 IN MAIN E&E JUST UNDER BATTERY TRAYS. CLEANED CORROSION ON LONGERON REF: B717-200 SRM 53-00-05-2R REPAIR 3. LONGERON (HAT SECTION) REPAIR. LOCAL
- [SDR DALA2025031101886](https://openairdocs.org/sdr/DALA2025031101886), Mar 7, 2025: FRAME. DAMAGED. STA 1225 CANTED FRAME: TAILCONE ALIGNMENT PIN AND CANTED FRAME DAMAGED AT APPROX 7 O'CLOCK POSITION -MARKED-. THIS COULD PREVENT THE PROPER OPERATION OF THE ESC
- [SDR DALA2025030601772](https://openairdocs.org/sdr/DALA2025030601772), Mar 6, 2025: LONGERON. CORRODED. CORROSION ON LONGERON 29R, FWD OF STA. 370. "M" AND PIC ATTACHED. SUMMARY SEE NRC 001-0513:5331-2007/001 00558: CORROSION LEVEL 2. CMOR CLEANED CORROSION ON LON
- [SDR DALA2025022101360](https://openairdocs.org/sdr/DALA2025022101360), Feb 19, 2025: DOOR. DAMAGED. C-1 FWD CARGO DOOR HAS EXCESSIVE DAMAGE. REPLACED FWD CARGO DOOR. LOG CREATED FOR PARTS CHANGE DOCUMENTATION. INSTALLED ON ROUTINE CARD 5231-4003. (LP #0818827)
- [SDR DALA2025021201092](https://openairdocs.org/sdr/DALA2025021201092), Feb 11, 2025: SUPPORT. CORRODED. AFT CARGO DOOR INNER SUPPORT AT LOWER END IS CORRODED. SUMMARY SEE NRC 001-0467:2000-1002/191 00296: CORROSION LEVEL 1. AFT CARGO DOOR WAS REPLACED ON NRC 293. 
- [SDR DALA2025020500884](https://openairdocs.org/sdr/DALA2025020500884), Feb 4, 2025: SPAR. CRACKED. THE #13 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/024 00024: N
- [SDR DALA2025020500880](https://openairdocs.org/sdr/DALA2025020500880), Feb 4, 2025: SPAR CAP. CRACKED. A CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP. AS A PRECAUTION AN ER/A HAS BEEN ISSUED REQUIRING MAINTENANCE TO ACCOMPLISH INSPECTIONS OF THE LH WING LOWER 
- [SDR DALA2025020500879](https://openairdocs.org/sdr/DALA2025020500879), Feb 4, 2025: SPAR. CRACKED. THE #12 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/028 00028: N
- [SDR DALA2025020500878](https://openairdocs.org/sdr/DALA2025020500878), Feb 4, 2025: SPAR. CRACKED. THE #16 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514
- [SDR DALA2025020500877](https://openairdocs.org/sdr/DALA2025020500877), Feb 4, 2025: SPAR. CRACKED. THE #15 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514
- [SDR DALA2025020500876](https://openairdocs.org/sdr/DALA2025020500876), Feb 4, 2025: SKIN. CRACKED. THE #14 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514
- [SDR DALA2025020500875](https://openairdocs.org/sdr/DALA2025020500875), Feb 4, 2025: SPAR. CRACKED. THE #11 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/023 00023: N
- [SDR DALA2025020500874](https://openairdocs.org/sdr/DALA2025020500874), Feb 4, 2025: SPAR. CRACKED. THE #10 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/022 
- [SDR DALA2025020500873](https://openairdocs.org/sdr/DALA2025020500873), Feb 4, 2025: SPAR CAP. CRACKED. -AD- CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATELY 5.0" INBD OF XRS 164.000. THE MAIN CRACK MEASURES AP
- [SDR DALA2024081608214](https://openairdocs.org/sdr/DALA2024081608214), Aug 16, 2024: CONTACT. SHORTED. SHIP 9574 -SMKE- AFTER LIGHT TEST, WE NOTICED THAT THE RIGHT APU BUS LIGHT WAS INOPERATIVE. WE TRIED RESETTING THE LIGHT BUT THE BULB AND SOCKET BRIEFLY EMITS S
- [SDR DALA2023122810695](https://openairdocs.org/sdr/DALA2023122810695), Dec 24, 2023: UNKNOWN. UNKNOWN. DURING 1L DOOR (LT) SLIDE CHANGE, MAINTENANCE FOUND CONTAINER LANYARD ASSEMBLY CABLE FRAYED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT I
- [SDR DALA2023110709164](https://openairdocs.org/sdr/DALA2023110709164), Nov 6, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT SIGN AT THE TAILCONE, FELL OFF. MAINTENANCE RESECURED THE LIGHT COVER AS REQUIRED. OK FOR SERVICE. (LP #4279682)
- [SDR DALA2023060704647](https://openairdocs.org/sdr/DALA2023060704647), Jun 6, 2023: UNKNOWN. UNKNOWN. EXIT SIGN AT FRONT OF CABIN IS BROKEN OFF FROM THE CEILING AND IS HANGING BY THE WIRES. MAINTENANCE REPLACED THE FWD CABIN SIGN PER B717 AMM 33-51. OPERATIONAL 
- [SDR DALA2023032602319](https://openairdocs.org/sdr/DALA2023032602319), Mar 25, 2023: UNKNOWN. UNKNOWN. SHIP 9574-ATB-DE/ENVIROMENTAL. PERFORMED AN AIR RETURN DUE TO A BIRD STRIKE TO THE RADOME AND LOSS OF WEATHER RADAR. CORRECTIVE ACTION: MAINTENANCE PERFORMED A 
- [SDR DALA2023031501887](https://openairdocs.org/sdr/DALA2023031501887), Mar 14, 2023: UNKNOWN. UNKNOWN. SHIP 9574 -ATB- THE FLIGHT CREW ACCOMPLISHED AN AIR TURN BACK AFTER THE CONTROL TOWER INFORMED THEM OF SOMETHING OBSERVED TRAILING THE AIRCRAFT. THE CREW CONFIR
- [SDR DALA2022030201328](https://openairdocs.org/sdr/DALA2022030201328), Mar 1, 2022: NONE. NONE. CORROSION ON UPPER AND LOWER SURFACE AT SEAT TRACK RH RBL=54 BTW STA=715 TO STA=737 AT CPAX REF NRC 202. SUMMARY OF NRC 00292: CORROSION LEVEL 2, SEAT TRACK RH 
- [SDR DALA2022030201327](https://openairdocs.org/sdr/DALA2022030201327), Mar 1, 2022: NONE. NONE. THE FORWARD RETAINER CLIP, ON THE COVER ASSEMBLY AT THE TAILCONE SLIDE, WAS FOUND BROKEN DURING STEP 13 OF JIC 5352-4002. THIS COULD PREVENT PROPER OPERATION OF
- [SDR DALA2022022401205](https://openairdocs.org/sdr/DALA2022022401205), Feb 23, 2022: NONE. NONE. CORROSION ON JAM BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00075: CORROSION LEVEL 2, JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT 
- [SDR DALA2022022401204](https://openairdocs.org/sdr/DALA2022022401204), Feb 23, 2022: NONE. NONE. CORROSION ON JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00030: CORROSION LEVEL 2, JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2) WAS REPAIRED PER 

All 182: https://openairdocs.org/aircraft/N925AT/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/N925AT/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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