# N924AT: 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: 55080
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 2000
- Certificate issued: June 27, 2025
- Expires: June 30, 2032
- Mode S code: ACCD18
- 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=924AT
- Page: https://openairdocs.org/aircraft/N924AT

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/N924AT/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 N924AT.

## FAA accident and incident reports

None matched to N924AT.

## Service difficulty reports (174, 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 DALA2026070303894](https://openairdocs.org/sdr/DALA2026070303894), Jun 24, 2026: WARNING MESSAGE. ACTIVATED. FT BULKHEAD DOOR WARNNING ANNUNCIATION, COMPLIED WITH ER/A 635445-14. (1663962) (AIRCRAFT GROUNDED).
- [SDR DALA2026031901911](https://openairdocs.org/sdr/DALA2026031901911), Mar 14, 2026: TIRE. DAMAGED. DUE TO RT NLG TIRE LOOSING TREAD CAP COUSED DENT ON RT SIDE JUST AFT OF FS 110 BETWEEN FS28R AND FS29R. CUT AND REMOVED DAMAGED AREA PER B717 SRM 53-03-01-2R-1 
- [SDR DALA2026031701821](https://openairdocs.org/sdr/DALA2026031701821), Mar 14, 2026: TIRE. SEPARATED. RETURNED TO ATL DUE TO RIGHT NLG TIRE RECAP SEPARATION ON TAKEOFF. DECLARED EMERGENCY AND LANDED SAFELY. REPLACED NOSE LANDING GEAR WHEEL ASSY.
- [SDR DALA2026031801859](https://openairdocs.org/sdr/DALA2026031801859), Mar 14, 2026: CAP. SEPARATED. DUE TO RT NLG TIRE LOOSING TREAD CAP CAUSED DENT ON RT SIDE JUST AFT OF FS110 BETWEEN FS28R AND FS29R. REPAIR PER B717 SRM 53-03-01-2R-1 (1494824)
- [SDR DALA2026020900918](https://openairdocs.org/sdr/DALA2026020900918), Feb 2, 2026: BLADES. DAMAGED. RTO- APPROXIMATELY 25 KNOTS DUE TO A LT ENGINE COMPRESSOR STALL MESSAGE ALONG WITH AN AUDIBLE STALL. PERFORMED BORESCOPE INSPECTION OF LT ENGINE AND FOUND MULTI
- [SDR DALA2025122909453](https://openairdocs.org/sdr/DALA2025122909453), Dec 22, 2025: ACM. SEIZED. SHIP 9575 FUME EVENT ON DESCENT. ACM WAS FOUND SEIZED, REPLACED RT ACM AND BOTH COALESCER BAG ASSY. (8047459)
- [SDR DALA2025111908461](https://openairdocs.org/sdr/DALA2025111908461), Nov 19, 2025: BATTERY PACK. INOPERATIVE. AFT OVER WING EXIT LIGHTS OUT ON BOTH SIDES OF A/C. T/S PER B717 FIM 33-50-00-201 R/R BATTERY ASSY P/N 803949-1 PER B717 AMM 33-51-03 (6532441)
- [SDR DALA2025110708145](https://openairdocs.org/sdr/DALA2025110708145), Nov 2, 2025: DOOR. OUT OF ADJUST. SHIP 9575 AFT BULKHEAD DOOR CAUTION MESSAGE ON DECENT 26000 AND CLEARED AT 7000, REAPPEARED ON LANDING. CORRECTIVE ACTION: T/S PER B717 FIM 52-70 TASK 809. FOUN
- [SDR DALA2025110708142](https://openairdocs.org/sdr/DALA2025110708142), Nov 2, 2025: PROXIMITY SENSOR. FAULTED. SHIP 9575 AFT BULKHEAD DOOR MESSAGE ILLUMINATED ON DECENT THROUGH FL180- 8000 CAME ON AGAIN DUREING APPROACH. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN 
- [SDR DALA2025110708148](https://openairdocs.org/sdr/DALA2025110708148), Oct 28, 2025: LATCH. DIRTY. SHIP 9575 1L DOOR GRIT BAR VERY DIFFICULT TO ARM SLIDE. CORRECTIVE ACTION: FOUND BOTH 1L DOOR RETENTION LATCHES STICKY AND DIRTY. CLEANED AND VERIFIED NORMAL OP
- [SDR DALA2025103107968](https://openairdocs.org/sdr/DALA2025103107968), Oct 27, 2025: HINGE FITTING. EXCESS PLAY. RT WING FLAP O/B HINGE HAS EXCESSIVE PLAY. REPAIRED PER ERA/PRI 629650-14 REV. A (1274899).
- [SDR DALA2025063004852](https://openairdocs.org/sdr/DALA2025063004852), Jun 26, 2025: BRACE. NOT REPORTED. SHIP 9575 LH WING BRACE FITTING BEING REPLACED. CORRECTIVE ACTION: BRACE FITTING INSTALLED ON ERA622844-14AD (1047886)
- [SDR DALA2025063004855](https://openairdocs.org/sdr/DALA2025063004855), Jun 19, 2025: NONE. NONE. SHIP 9575 DTE, 624256-14AD. CORRECTIVE ACTION: ACCOMPLISH DTE FOR ERA 622844-14AD (1033944)
- [SDR DALA2025062604791](https://openairdocs.org/sdr/DALA2025062604791), Jun 19, 2025: INSPECTION. NONE. SHIP 9575 AMOC, ERA 624259-14AD. CORRECTIVE ACTION: CURRENT AMOC APPROVAL IS LIMITED TO 24 MONTHS. ADDITIONAL ERA REVISION IS REQUIRED FOR AMOC APPROVAL BEYOND 
- [SDR DALA2024110510646](https://openairdocs.org/sdr/DALA2024110510646), Oct 31, 2024: FRAME. DAMAGED. R/H FRAME ON STATION Y1133 DAMAGED NEAR LONGERON R8. REMOVED DAMAGED FRAME REF B717 SRM 53-20-07-2R PROCEDURE 1. FABRICATED, ALODINE, PRIMED, AND PAINTED REPAIR
- [SDR DALA2024102410343](https://openairdocs.org/sdr/DALA2024102410343), Oct 23, 2024: LONGERON. DAMAGED. LONGERON R8 AT STATION Y1133 DAMAGED. REMOVED DAMAGED R8 LONGERON 16.5 INCHES OF MATERAL SURROUNDING Y1133 REF 53-00-05-2R PROCEDURE 2. PERFORMED DAMAGE CONTAME
- [SDR DALA2024061606116](https://openairdocs.org/sdr/DALA2024061606116), Jun 15, 2024: FIRE DETECTOR. FALSE INDICATION. SHIP 9575 -ATB/DE- AS THE AIRCRAFT CLIMBED OUT ON DEPARTURE, THE APU FIRE WARNING (LEVEL 2) ACCOMPANIED BY THE MASTER CAUTION, ALL ILLUMINATED. THE CREW DECLARE
- [SDR DALA2024040504133](https://openairdocs.org/sdr/DALA2024040504133), Mar 29, 2024: SKIN. CRACKED. AD -- OPEN HOLE HFEC (BHEC) INDICATED CRACK 2 FASTENER HOLES BELOW EXISTING DOUBLER ON RT VERT L/E. MARKED. FOUND ON STEP 12 OF AA 5530-01048 AD 2018-10-08. SEP
- [SDR DALA2024011800752](https://openairdocs.org/sdr/DALA2024011800752), Jan 18, 2024: BATTERY PACK. NO TEST. DURING SERVICE CHECK FOUND AFT OVER WING (RT/LT) EMERGENCY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726 
- [SDR DALA2023121910405](https://openairdocs.org/sdr/DALA2023121910405), Dec 19, 2023: UNKNOWN. UNKNOWN. DURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY BATTERY PACK B5-230 WAS REPLACED 
- [SDR DALA2023112009514](https://openairdocs.org/sdr/DALA2023112009514), Nov 15, 2023: UNKNOWN. UNKNOWN. WHILE WORKING AD TASK CARD 2540-01288-01, NOTED FWD LAV & AFT RT LAV WASTE RECEPTACLE FLAPPER DOORS WILL NOT FULLY CLOSE. ADJUSTED SPRING TENSION ON BOTH SPRING
- [SDR DALA2023110108979](https://openairdocs.org/sdr/DALA2023110108979), Oct 31, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT LIGHT COVER OVER ROW 29 FELL OFF. MAINTENANCE REPLACED THE EXIT LIGHT LENS. (LP #4997060)
- [SDR DALA2023071205659](https://openairdocs.org/sdr/DALA2023071205659), Jul 8, 2023: UNKNOWN. UNKNOWN. AFTER REMOVAL OF THE RECHARGEABLE BATTERY ASSEMBLY, THE RECEPTACLE PINS WERE FOUND DAMAGED. THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REMOVED P
- [SDR DALA2023070605439](https://openairdocs.org/sdr/DALA2023070605439), Jul 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053. SUMMARY OF NRC 00367: CORROSION LEVEL 2. FLOOR SUPPORT BELOW ACCESORY CO
- [SDR DALA2023070505394](https://openairdocs.org/sdr/DALA2023070505394), Jul 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00633: CORROSION LEVEL 2. CUSP ANGL
- [SDR DALA2023070405372](https://openairdocs.org/sdr/DALA2023070405372), Jul 3, 2023: UNKNOWN. UNKNOWN. CRACK ON MEMBRANE (LWR SEAT TRACK AREA) IN STA Y=220 AND X=55 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00648: MEMBARANE WAS REPLACED PER B717-200 SRM 
- [SDR DALA2023070405371](https://openairdocs.org/sdr/DALA2023070405371), Jul 3, 2023: UNKNOWN. UNKNOWN. DURING REMOVAL OF FLOOR SUPPORT, CRACK AND CORROSION ON CUSP WEB Y=199 TO Y=160 X54 (CPAX) WAS FOUND. SUMMARY OF NRC 00598: CORROSION LEVEL 2. CUSP WEB WAS REPA
- [SDR DALA2023070405369](https://openairdocs.org/sdr/DALA2023070405369), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT OF MAIN ENTRANCE DOOR FROM STA Y=162 TO STA Y=194 & LBL 54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00381: CORROSION LEVEL 2. SUPPOR
- [SDR DALA2024022002335](https://openairdocs.org/sdr/DALA2024022002335), Jul 2, 2023: HINGE FITTING. CORRODED. CORROSION ON INBD/OUTBD ATTACHMENT POINTS OF CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR. SUMMARY OF NRC 00167: CENTER WING FLAP HINGE FITTING
- [SDR DALA2023070305302](https://openairdocs.org/sdr/DALA2023070305302), Jul 1, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1037 BTW LONGERON 17 LH AT CABIN. SUMMARY OF NRC 00239: FRAME STA 1037 BTW LONGERON 17 LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07
- [SDR DALA2023063005262](https://openairdocs.org/sdr/DALA2023063005262), Jun 29, 2023: UNKNOWN. UNKNOWN. FLOOR PAN BTW RBL 43 AND LBL 0 BTW STA Y=160 AND STA Y=193 AT CPAX CABIN WAS FOUND WITH CORROSION DAMAGE OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DA
- [SDR DALA2023063005259](https://openairdocs.org/sdr/DALA2023063005259), Jun 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR FITTING BTW STA Y=218 AND RBL 9 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00614: CORROSION LEVEL 2. FLOOR FITTING BTW STA Y=218 AND RBL 9 
- [SDR DALA2023062805190](https://openairdocs.org/sdr/DALA2023062805190), Jun 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP ANGLE FROM STA Y=168 TO STA Y=218 AND -X=54 TO -X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00452: CUSP ANGLE FROM STA Y=168 TO ST
- [SDR DALA2023062705156](https://openairdocs.org/sdr/DALA2023062705156), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND ON MENBRANE STA Y=200 TO STA Y=218 AND X=60 TO X=22 AT PASSENGER CABIN. SUMMARY OF NRC 00645: CORROSION LEVEL 2. MEMBRANE STA Y=200 TO STA Y=218
- [SDR DALA2023062705154](https://openairdocs.org/sdr/DALA2023062705154), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK X=-44 BTW STA 197- 217, OUT OF LIMIT. SUMMARY OF NRC 00606: CORROSION LEVEL 2. SECTION OF SEAT TRACK X=- 44 BTW STA 197-217 WAS REPLACED
- [SDR DALA2023062705153](https://openairdocs.org/sdr/DALA2023062705153), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH SEAT TRACK X-22 BTW STA Y=197 TO STA Y=266 AT PAX CABIN WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.100 IN. REMAINING THICKNESS IS 0.050 IN. TH
- [SDR DALA2023062705152](https://openairdocs.org/sdr/DALA2023062705152), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS (2EA) STA Y:148 APPROX BTW -X:22 TO -X:56 AT CABIN PAX. SUMMARY OF NRC 00473: CORROSION LEVEL 2. FLOOR SUPPORT (1EA) STA Y:148 APPRO
- [SDR DALA2023062205058](https://openairdocs.org/sdr/DALA2023062205058), Jun 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00212: CORROSION LEVEL 2. FLOOR SUPPORT BTW LBL 5 AND RBL 5 STA Y=193 AT 
- [SDR DALA2023062205057](https://openairdocs.org/sdr/DALA2023062205057), Jun 22, 2023: UNKNOWN. UNKNOWN. SEVERAL AREAS OF CORROSION ON FLOOR TRACKS (2 EA) BTW LBL 8 AND RBL 8 BTW STA Y=148 AND STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR 
- [SDR DALA2023062205055](https://openairdocs.org/sdr/DALA2023062205055), Jun 21, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR FITTING RBL11 STA Y=157 AT CPAX CABIN WAS REPLACED AND 
- [SDR DALA2023062005002](https://openairdocs.org/sdr/DALA2023062005002), Jun 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMPARTMENT C-1. SUMMARY OF NRC 00447: FLOOR SUPPORT BTW L28R TO L28L STA 332 AT FWD CARGO COMP
- [SDR DALA2023061904972](https://openairdocs.org/sdr/DALA2023061904972), Jun 18, 2023: UNKNOWN. UNKNOWN. CRACK ON INNER SURFACE OF CUSP WEB MEMBRANE LH STA Y=655. SUMMARY OF NRC 00223: CUSP WEB MEMBRANE LH STA Y=655 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDU
- [SDR DALA2023061904971](https://openairdocs.org/sdr/DALA2023061904971), Jun 18, 2023: UNKNOWN. UNKNOWN. SEVERAL AREAS OF CORROSION ON FLOOR SUPPORT BTW RBL 9 AND RBL 39 STA Y=193 AT CPAX CABIN. SUMMARY OF NRC 00213: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 9 AND R
- [SDR DALA2023061904967](https://openairdocs.org/sdr/DALA2023061904967), Jun 17, 2023: UNKNOWN. UNKNOWN. CORROSION ON GUSSET BELOW AFT ACCESSORY COMPARMENT DOOR RBL 15 STA Y=1072 AT CPAX CABIN. SUMMARY OF NRC 00378: CORROSION LEVEL 2. GUSSET BELOW AFT ACCESSORY COM
- [SDR DALA2023061904966](https://openairdocs.org/sdr/DALA2023061904966), Jun 17, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT CPAX CABIN. SUMMARY OF NRC 00218: CORROSION LEVEL 2. FLOOR SUPPORT BTW RBL 0 TO RBL 15 STA Y=237 AT 
- [SDR DALA2023061904963](https://openairdocs.org/sdr/DALA2023061904963), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00567: CORROSION LEVEL 2. LH CUPS WEB IN STA Y=503 AT PASSENGER CABIN STRUCTU
- [SDR DALA2023061904961](https://openairdocs.org/sdr/DALA2023061904961), Jun 16, 2023: UNKNOWN. UNKNOWN. CRACK ON LOWER SKIN AT CUSP WEB MEMBRANE STA 634. SUMMARY OF NRC 00149: LOWER SKIN AT CUSP WEB MEMBRANE STA 634 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCED
- [SDR DALA2023061604904](https://openairdocs.org/sdr/DALA2023061604904), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00566: CORROSION LEVEL 2. LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTU
- [SDR DALA2023061504878](https://openairdocs.org/sdr/DALA2023061504878), Jun 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON UPPER SIDE AND LOWER SIDE OF CUSP WEB BTW STA Y=200 TO STA Y=220 AT PASSENGER CABIN. SUMMARY OF NRC 00203: CORROSION LEVEL 2. CUSP WEB BTW STA Y=20
- [SDR DALA2023061304793](https://openairdocs.org/sdr/DALA2023061304793), Jun 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1. SUMMARY CORROSION LEVEL 2. FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO

All 174: https://openairdocs.org/aircraft/N924AT/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/N924AT/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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