# N920AT: 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: 55083
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 29, 2001
- Certificate issued: May 8, 2025
- Expires: May 31, 2032
- Mode S code: ACBE3C
- 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=920AT
- Page: https://openairdocs.org/aircraft/N920AT

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/N920AT/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 N920AT.

## FAA accident and incident reports

None matched to N920AT.

## Service difficulty reports (144, 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 DALA2026101205599](https://openairdocs.org/sdr/DALA2026101205599), Oct 9, 2026: SKIN. MECHANIC ERROR. DRILL START INDENTATIONS AT CABIN CEILING BS 927, BTWN STRINGER 3R & 4R. REPAIRED PER ER/A 637414-14. (1856706) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100905576](https://openairdocs.org/sdr/DALA2026100905576), Oct 9, 2026: FRAME. DAMAGED. FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y908, STR 2R-3R, COMPLIED WITH ER/A 637401-14. (1855981) (AICRAFT GROUNDED).
- [SDR DALA2026100905575](https://openairdocs.org/sdr/DALA2026100905575), Oct 9, 2026: FRAME. DAMAGED. FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y927 BETWEEN STRG L3R TO L4R, ADDITIONAL ENGINEERING AUTHORIZATION ER/A REVISION IS REQUIRED. (1855903) (AICRAFT GROUNDED
- [SDR DALA2026082404797](https://openairdocs.org/sdr/DALA2026082404797), Aug 23, 2026: PCDU. FAULTED. MISC/DE- DECLARED AN EMERGENCY DUE TO RIGHT DC BUSS OFF MESSAGE WITH NUMEROUS FAULTS. REPLACED RT PCDU IAW AMM 24-21. OPS CHECK NORMAL. (9197048) (AIRCRAFT GROU
- [SDR DALA2026020200758](https://openairdocs.org/sdr/DALA2026020200758), Jan 28, 2026: RADIO. ODOR. OOD SMELL IN FWD LAV AND EMERG EQUIP DOOR TO RIGHT OF LAV. ODOR LIKE A HOT ELECTRIC MOTOR OR ARMATURE. VERY FAINT ODOR BUT SEVERAL CREW MEMBERS SMELLED IT. FWD 
- [SDR DALA2025122909459](https://openairdocs.org/sdr/DALA2025122909459), Dec 21, 2025: RELEASE MECH. OUT OF ADJUST. FOUND TAIL CONE RELEASE MECHANISM CAM CLOCKED WRONG. TAILCONE RELEASE MECHANISM CAM REF B717 AMM 53-52-03 (1362721)
- [SDR DALA2025122909452](https://openairdocs.org/sdr/DALA2025122909452), Dec 19, 2025: NONE. NONE. ERA 631006-14. : DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA ADVISORY CIRCULAR 120-93. ASSOCIATED ER/A 00-631006 (1
- [SDR DALA2025121509136](https://openairdocs.org/sdr/DALA2025121509136), Dec 11, 2025: SKIN. DAMAGED. FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN STA 164. REPAIRED PER ERA 629782-14AD (1346873)
- [SDR DALA2025121509134](https://openairdocs.org/sdr/DALA2025121509134), Dec 10, 2025: SPAR. DAMAGED. ER/A 629782-14. REPAIR AT RH REAR SPAR AT XRS 164. C/W WITH ER/A 629782-14. (1345202)
- [SDR DALA2025121509133](https://openairdocs.org/sdr/DALA2025121509133), Dec 10, 2025: SPAR. DAMAGED. ER/A 629782-14AD REV ORIGINAL. REPAIR TO RH WING REAR SPAR AT XRS 164. REPAIRED PER ER/A 14-629782. (1345195)
- [SDR DALA2025121009018](https://openairdocs.org/sdr/DALA2025121009018), Dec 4, 2025: DOUBLER. CORRODED. AFT CARGO CORROSION - INTERNAL DOUBLER STR 23R STA 1022 CORRODED. REPAIRED COMPLIED WITH ER/A 630153-14 REV. ORIG. (1335432)
- [SDR DALA2025120808964](https://openairdocs.org/sdr/DALA2025120808964), Nov 29, 2025: SCUFF PLATE. CRACKED. AFT CARGO SCUFF PLATE CRACKED. REPLACED JAMB PAN ON NR 408 IAW LOG 1325090. (1327367)
- [SDR DALA2025120808963](https://openairdocs.org/sdr/DALA2025120808963), Nov 27, 2025: PAN. CORRODED. AFT CARGO: C-2 DOOR THRESHOLD PAN CORRODED. REPLACED REPAIR AFT CARGO DOOR LOWER JAMB PAN IAW SRM 53-20-15-2R, PROCEDURE 7, REPAIR 7. AFT CARGO DOOR LOWER JAMB 
- [SDR DALA2025120108776](https://openairdocs.org/sdr/DALA2025120108776), Nov 27, 2025: NONE. NONE. REPETITIVE INSP PER SECT II. OF ERA 630153-14 REV ORIGINAL. C/W ER/A630153-14 REV ORIGINAL. (1324948)
- [SDR DALA2025111908464](https://openairdocs.org/sdr/DALA2025111908464), Nov 18, 2025: STRINGER FITTING. CORRODED. AFT CARGO P/R: STRINGER END FITTING MARKED FS1053 28R IS CORRODED. REPLACED AFT END FITTING LONGERON 28R PER B717 DWG 5910228 (1310506)
- [SDR DALA2025111908463](https://openairdocs.org/sdr/DALA2025111908463), Nov 18, 2025: LONGERON SPLICE. CORRODED. AFT CARGO BAY BS 1002 L25R END SPLICE CORRODED. REPLACED LONGERON 25R AND FWD END FITTING REF: DACDWG 5919707-521 (1310504)
- [SDR DALA2025111808440](https://openairdocs.org/sdr/DALA2025111808440), Nov 12, 2025: THRESHOLD. CORRODED. C1 DOOR THRESHOLD: LIGHT SURFACE CORROSION IN DOOR SILL AREA. REPLACED REPAIRED FORWARD CARGO DOOR LOWER JAMB PAN REF: B717-200 SRM 53-20-15-2R (1300666).
- [SDR DALA2025090906665](https://openairdocs.org/sdr/DALA2025090906665), Sep 2, 2025: ACCESS PANEL. MECHANIC ERROR. LEFT WING OUTER, LOWER SURFACE, ACCESS COVER SETTLEMENT AREA, XRS=383-414, MISDRILLED HOLE. ACCOMPLISH ER/A 611899-14 (1178468)
- [SDR DALA2025040802705](https://openairdocs.org/sdr/DALA2025040802705), Apr 7, 2025: LENS. MISSING. THE OVERHEAD EMERGENCY LIGHT LENS AT 24L IS MISSING. MAINTENANCE REPLACED LENS IAW B717 AMM 33-51-08. (LP #6963274)
- [SDR DALA2025021801198](https://openairdocs.org/sdr/DALA2025021801198), Feb 16, 2025: AUTOPILOT SYS. FAILED. SHIP 9578 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO JAX (VFR) DUE TO LOSS OF AUTOPILOT AND LATERAL ROLL MODE GUIDANCE ON APP
- [SDR DALA2023110709163](https://openairdocs.org/sdr/DALA2023110709163), Nov 7, 2023: UNKNOWN. UNKNOWN. ON WALK AROUND DURING THE SERVICE CHECK, MAINTENANCE FOUND THAT THE AFT RIGHT HAND EXTERIOR EMERGENCY LIGHT STAYS ON AT ALL TIMES. MAINTENANCE REPLACED RELAY R2
- [SDR DALA2023101808565](https://openairdocs.org/sdr/DALA2023101808565), Oct 17, 2023: UNKNOWN. UNKNOWN. DENTS ON INB SURFACE AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00098: INBOARD SURFACE OF AFT MOVABLE FLAP VANE (LH WING) WAS REPAIRED PER ER/A 612278-14 
- [SDR DALA2023101408447](https://openairdocs.org/sdr/DALA2023101408447), Oct 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL BTW STA 1022-1037 AND LONGERON 30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00708: CORROSION LEVEL 2. INTERCOSTAL BTW STA 1022-1037 AND LO
- [SDR DALA2023101408439](https://openairdocs.org/sdr/DALA2023101408439), Oct 11, 2023: UNKNOWN. UNKNOWN. IN REF AMDS: 2040-0009: OPEN LEFT WING, FUEL TANK ZONE 520, DURING REMOVED ACCESS PLATE NBR 520 MB; CUT OUT SKIN OF FUEL ACCESS PLATE 520MB WAS DRILLED AT LH WI
- [SDR DALA2023101408436](https://openairdocs.org/sdr/DALA2023101408436), Oct 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON PAN OF PASSENGER DOOR JAMB (EXTERNAL/INTERNAL SURFACE) BTW STA Y=200 AND PROJECT LONG 18L AT PAX CABIN. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PA
- [SDR DALA2023101408435](https://openairdocs.org/sdr/DALA2023101408435), Oct 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON CHORD ANGLE AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 27LH-27RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00230: CORROSI
- [SDR DALA2023101008308](https://openairdocs.org/sdr/DALA2023101008308), Oct 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON L30 BTW STA 908 TO STA 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00578: CORROSION LEVEL 2. LONGERON SECTION OF L30 BTW STA 908 TO STA 950 AT AFT
- [SDR DALA2023101008305](https://openairdocs.org/sdr/DALA2023101008305), Oct 8, 2023: UNKNOWN. UNKNOWN. CORROSION ALONG OF TIE TRACK STA 954 TO 1022 LONGERON 28LH AT AFT CARGO IN REF NRC 213. SUMMARY OF NRC 00625: CORROSION LEVEL 2. TIE TRACK STA 954 TO 1022 LONGE
- [SDR DALA2023101008306](https://openairdocs.org/sdr/DALA2023101008306), Oct 7, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL STA 1223 CANT 12 O'CLOCK POSITION AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00251: RUDDER STOP SPRING RH (1 EA) WAS REMOVED AND INSTALLED 
- [SDR DALA2023100608224](https://openairdocs.org/sdr/DALA2023100608224), Oct 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK X 56 ON STA: Y=332 TO Y=333 ORIGINAL T. SUMMARY OF NRC 00428: CORROSION LEVEL 2. SEAT TRACK X=56R BTW STA Y=218 AND STA Y=334 WAS REPLAC
- [SDR DALA2023100608223](https://openairdocs.org/sdr/DALA2023100608223), Oct 5, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR (L1). SUMMARY OF NRC 00296: BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR WAS REPAIRED PER B717-2
- [SDR DALA2023100608220](https://openairdocs.org/sdr/DALA2023100608220), Oct 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON FWD REPAIR DOUBLER SPLICE ON AFT CARGO DOOR JAMB. CORROSION LEVEL 2. REPAIR DOUBLER SPLICES (2 EA) WERE REPLACED PER SRM 53-20-15-2R PROCEDURE 7 RE
- [SDR DALA2023100408157](https://openairdocs.org/sdr/DALA2023100408157), Oct 3, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN. SUMMARY OF NRC 00441: FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN WAS REPAIRED PER B717-
- [SDR DALA2023100308099](https://openairdocs.org/sdr/DALA2023100308099), Oct 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON END 24RH AND STA 1011 AT AFT CARGO. SUMMARY OF NRC 00650: CORROSION LEVEL 2. LONGERON END 24RH AND STA 1011 AT AFT CARGO WAS REPLACED PER 
- [SDR DALA2023100308097](https://openairdocs.org/sdr/DALA2023100308097), Oct 2, 2023: UNKNOWN. UNKNOWN. CRACK ANGLE INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00156: ANGLE (INTERCOSTAL) INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT P
- [SDR DALA2023100308094](https://openairdocs.org/sdr/DALA2023100308094), Oct 1, 2023: UNKNOWN. UNKNOWN. CRACKS (2 EA) ON FWD AND AFT PANS UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00151: FWD PAN UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-2
- [SDR DALA2023100308091](https://openairdocs.org/sdr/DALA2023100308091), Oct 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON END (1 EA) STA Y:1053 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00652: CORROSION LEVEL 2. LONGERON END AT STA Y:1053 LONGERON
- [SDR DALA2023100308087](https://openairdocs.org/sdr/DALA2023100308087), Sep 30, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN. SUMMARY OF NRC 00442: FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN WAS REPAIRED PER B717-
- [SDR DALA2023092908002](https://openairdocs.org/sdr/DALA2023092908002), Sep 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00231: CORRO
- [SDR DALA2023092908001](https://openairdocs.org/sdr/DALA2023092908001), Sep 28, 2023: UNKNOWN. UNKNOWN. BROKEN INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL=0 AT AFT CARGO. SUMMARY OF NRC 00214: INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL= 0 AT AFT CARGO WAS REPAIRED B7
- [SDR DALA2023092807974](https://openairdocs.org/sdr/DALA2023092807974), Sep 27, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00152: BEAM NBR 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B
- [SDR DALA2023092707956](https://openairdocs.org/sdr/DALA2023092707956), Sep 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN IN REF NRC 00538. SUMMARY OF NRC 00614: CORROSION LEVEL 2. CUSP WEB FROM Y=160 TO Y=200 -X8 T
- [SDR DALA2023092707950](https://openairdocs.org/sdr/DALA2023092707950), Sep 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT Y=180 FROM X=-10 TO X=-43, FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX IN REF NRC 00541. SUMMARY OF NRC 00610: CORROSION LEVEL 2. FLOO
- [SDR DALA2023092507865](https://openairdocs.org/sdr/DALA2023092507865), Sep 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX. SUMMARY OF NRC 00324: CORROSION LEVEL 2. FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT 
- [SDR DALA2023092507864](https://openairdocs.org/sdr/DALA2023092507864), Sep 24, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=275 BTW STRG 15L/14L AT CPAX. SUMMARY OF NRC 00286: FRAME STA Y=275 BTW STRG 15L/14L AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REP
- [SDR DALA2023092107770](https://openairdocs.org/sdr/DALA2023092107770), Sep 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT CPAX. SUMMARY OF NRC 00437: CORROSION LEVEL 2. 
- [SDR DALA2023092107768](https://openairdocs.org/sdr/DALA2023092107768), Sep 20, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB ON STA Y=579 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00389: WEB ON STA Y=579 AND X=-44 AT PAX CABIN WAS REPAIRED PER B 717-200 SRM 53-00-55-2R REPAI
- [SDR DALA2023091907684](https://openairdocs.org/sdr/DALA2023091907684), Sep 18, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB STA Y 190, LBL44 AT CPAX. SUMMARY OF NRC 00436: WEB STA Y 190, LBL44 WAS REPAIRED PER B 717-200 SRM 51-70-10-2R REP 1 FIG 201. (LP #2976349)
- [SDR DALA2023091807628](https://openairdocs.org/sdr/DALA2023091807628), Sep 17, 2023: UNKNOWN. UNKNOWN. REWORKED CORRODED AREA RH CUSP WEB BTW STA Y=465 AND STA=484. ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS OF 0.014 IN. REWORKED AREA IS OUT L
- [SDR DALA2023091807624](https://openairdocs.org/sdr/DALA2023091807624), Sep 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON SHIELD X=56R AND X=44.5R BTW STA Y=1022 TO Y=1053 AND WEB X=56R STA Y=1042 AT PAX CABIN. SUMMARY OF NRC 00233: CORROSION LEVEL 2. SUPPORT X=56R AND

All 144: https://openairdocs.org/aircraft/N920AT/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/N920AT/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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