# N923AT: 2005 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55051
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 26, 2005
- Certificate issued: August 27, 2024
- Expires: August 31, 2031
- Mode S code: ACC961
- 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=923AT
- Page: https://openairdocs.org/aircraft/N923AT

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 Rolls-Royce 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 (Rolls-Royce 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/N923AT/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 N923AT.

## FAA accident and incident reports

None matched to N923AT.

## Service difficulty reports (102, 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 DALA2026060903482](https://openairdocs.org/sdr/DALA2026060903482), Jun 8, 2026: LONGERON. CRACKED. CRACK LONGERONS NBR 2 RT/LT SIDES AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. CRACK LONGERONS NR 2 RT/LT SIDES AT STA Y=1133 AT 12HRS POSITION 
- [SDR DALA2026060903481](https://openairdocs.org/sdr/DALA2026060903481), Jun 8, 2026: SKIN. CRACKED. AIRCRAFT 9559, CRACK ON EXTERNAL SKIN STA Y= 1133 BTW PROJECTION LONG 2 RH TO LONG 3 RH AT AFT FUSELAGE SECTION. CORRECTIVE ACTION: CRACK ON EXTERNAL SKIN STA Y
- [SDR DALA2026060903437](https://openairdocs.org/sdr/DALA2026060903437), Jun 4, 2026: CONTROL CABLE. LOW TENSION. IN REF TO AMDS 2780-2003: LOW TENSION ON EXTEND CONTROL CABLE OF SLAT 1 AT RIGHT WING. FINAL ADJUSTMENT OF THE EXTEND CONTROL CABLE (195A-B) AT SLAT 1 AT RIGHT 
- [SDR DALA2026020900915](https://openairdocs.org/sdr/DALA2026020900915), Feb 5, 2026: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R1 GALLEY OVERHEAD. REMOVED & REPLACED THE B5-259 BATTERY IAW AMM 33-51. (8406307)
- [SDR DALA2025121709201](https://openairdocs.org/sdr/DALA2025121709201), Dec 16, 2025: SKIN. CRACKED. LEFT FLAP TRAILING EDGE CRACK AND DELAMINATION. REPAIRED PER ER/A 631162-14. (8401817)
- [SDR DALA2025111808422](https://openairdocs.org/sdr/DALA2025111808422), Nov 13, 2025: NONE. NONE. DTA ER/A 618121-14 REV A SECTION I MONITOR LOG REQUIRES DTA STATE 3 APPROVAL ON OR BEFORE 82,000 TOTAL CYCLES. C/W ER/A 00-618121 (1304050).
- [SDR DALA2025071605343](https://openairdocs.org/sdr/DALA2025071605343), Jul 15, 2025: LONGERON. DAMAGED. AIRCRAFT 9559, LONGERON BETWEEN ST 256 & 275 DAMAGED. REMOVED DAMAGE SECTION OF LONGERON IAW B717 SRM 53-00-05-2R PRO 2. FABRICATED LONGERON AND HATS P717 SRM 5
- [SDR DALA2024122712035](https://openairdocs.org/sdr/DALA2024122712035), Dec 25, 2024: BATTERY PACK. INOPERATIVE. THE FOUR LOWER OVERWING EXIT LIGHTS, LEFT AND RIGHT, ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY R5-119 PER B717 AMM 33-51-03. SYSTEM NOW
- [SDR DALA2024061306057](https://openairdocs.org/sdr/DALA2024061306057), Jun 7, 2024: BEAM. CRACKED. CRACKS ON INTERNAL BEAM #1 AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00356: INTERNAL BEAM #1 (UPPER WEB) AT AFT CABIN BULKHEAD DOOR (CPAX) WAS FABRICATE
- [SDR DALA2024053105689](https://openairdocs.org/sdr/DALA2024053105689), May 30, 2024: FUEL TANK. CORRODED. -AD- CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. SUMMARY OF NRC 00777: LO
- [SDR DALA2024051605255](https://openairdocs.org/sdr/DALA2024051605255), May 14, 2024: ATTACH FITTING. CORRODED. RUSTED ON LUG AT ATTACH FIXED STRUT, ALSO ON FITTING TO RH LANDING GEAR. SUMMARY OF NRC 00731: RUSTED ON FITTING TO RH LANDING GEAR WAS REMOVED PER BOEING OM 57
- [SDR DALA2024051405170](https://openairdocs.org/sdr/DALA2024051405170), May 10, 2024: JACKSCREW. NICKED. -AD- A NICK WAS FOUND ON THREAD OF THE ACME SCREW AT THE HORIZONTAL STAB. SUMMARY OF NRC 00485: HORIZONTAL STABILIZER ACTUATOR JACKSCREW ASSY WAS REPLACED FOR S
- [SDR DALA2024050204889](https://openairdocs.org/sdr/DALA2024050204889), May 1, 2024: NOT REPORTED. SCRATCHED. -AD- SCRATCHES WERE FOUND AT FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER. SUMMARY OF NRC 00666: FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER (HOLE #19) WAS REP
- [SDR DALA2024042604728](https://openairdocs.org/sdr/DALA2024042604728), Apr 26, 2024: PAN. CRACKED. CRACKS WERE FOUND ON PAN, BTW BEAMS 3/4 AND AFT SIDE AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00348: AFT INNER PAN ON BEAM #3 AND BEAM #4 AT AFT CARGO COMPARTMENT
- [SDR DALA2024050104837](https://openairdocs.org/sdr/DALA2024050104837), Apr 25, 2024: NONE. NONE. -AD- AMOC ER/A 617393-14AD MONITOR LOG REQUIRES DTA WITH NEW AMOC ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR R
- [SDR DALA2024050104836](https://openairdocs.org/sdr/DALA2024050104836), Apr 25, 2024: NONE. NONE. -AD- DTA ER/A 616393-14AD MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS
- [SDR DALA2024042404673](https://openairdocs.org/sdr/DALA2024042404673), Apr 23, 2024: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R. SUMMARY OF NRC 00041: FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R WAS REPAIRED PER ERA 617080-14 REV ORIGI
- [SDR DALA2024041904566](https://openairdocs.org/sdr/DALA2024041904566), Apr 18, 2024: DIAPHRAGM. CRACKED. CRACK ON DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX (W1). SUMMARY OF NRC 00689: DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT C
- [SDR DALA2024041804533](https://openairdocs.org/sdr/DALA2024041804533), Apr 17, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BTW STA Y=429 AND Y=434, AND BTW STA Y=459 AND Y=462 X-56 (IN REFERENCE TO NRC 00542). S
- [SDR DALA2024041804529](https://openairdocs.org/sdr/DALA2024041804529), Apr 16, 2024: BEAM. CRACKED. CRACKS ON FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00245: FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 S
- [SDR DALA2024041804528](https://openairdocs.org/sdr/DALA2024041804528), Apr 16, 2024: BEAM. CRACKED. CRACKS 2 EA ON FWD PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00243: FWD PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 
- [SDR DALA2024041504428](https://openairdocs.org/sdr/DALA2024041504428), Apr 13, 2024: BEAM. CRACKED. CRACKS ON FWD PANE BEAM 3 AT FWD CARGO DOOR. SUMMARY OF NRC 00244: FWD PANE BEAM 3 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAI
- [SDR DALA2024041204363](https://openairdocs.org/sdr/DALA2024041204363), Apr 12, 2024: BEAM. CRACKED. CRACK ON BEAM #1 STA 161 AND STA 197 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00216: DAMAGED SECTIONS (STA 161 AND STA 197) OF BEAM #1 AT PASSENGER ENTRA
- [SDR DALA2024041204359](https://openairdocs.org/sdr/DALA2024041204359), Apr 11, 2024: WEB. CRACKED. CRACK ON OUT WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR. SUMMARY OF NRC 00252: OUTER WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR 
- [SDR DALA2024041204358](https://openairdocs.org/sdr/DALA2024041204358), Apr 11, 2024: BEAM. CRACKED. CRACK ON AFT PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00242: AFT PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR
- [SDR DALA2023091407542](https://openairdocs.org/sdr/DALA2023091407542), Sep 13, 2023: UNKNOWN. UNKNOWN. AFT CARGO SLANT PANEL DAMAGED LT SIDE FWD OF CARGO DOOR. REMOVED SLANT FLOOR PANEL PER B717 AMM 25-58. FABRICATED AND INSTALLED PANEL PER ER/A 612079-14 REV 0 S
- [SDR DALA2023070305306](https://openairdocs.org/sdr/DALA2023070305306), Jul 2, 2023: UNKNOWN. UNKNOWN. SEVERAL EMERGENCY LIGHTS IN THE CABIN COMPARTMENT ARE INOPERATIVE OR DIE IN LESS THAN 30 SECONDS AT TAXI. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK 
- [SDR DALA2022100406444](https://openairdocs.org/sdr/DALA2022100406444), Oct 2, 2022: NONE. NONE. SHIP 9559 - DE/HYD - THE CREW DECLARED AN EMERGENCY ON DESCENT FOR LANDING DUE TO THE RIGHT HYDRAULIC SYSTEM FLUID LOSS. THE ALTERNATE LANDING GEAR EXTENSION PR
- [SDR DALA2022030901526](https://openairdocs.org/sdr/DALA2022030901526), Mar 4, 2022: NONE. NONE. DURING THE EMERGENCY LIGHT CHECK ON A SERVICE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT OVER WING EVACUATION LIGHTS TO BE INOPERATIVE. SUMMARY SEE NRC 053-000
- [SDR DALA2022030201330](https://openairdocs.org/sdr/DALA2022030201330), Mar 2, 2022: NONE. NONE. THE TAILCONE RELEASE LANYARD IS WORN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE N
- [SDR DALA2022030201326](https://openairdocs.org/sdr/DALA2022030201326), Mar 1, 2022: NONE. NONE. SUPPLEMENTAL INFORMATION: 001-0210:5300-1001/001 00403 INSTALLED FWD CARGO, LOWER DOOR PAN PER B717 SRM 53-20-15-2R PROCEDURE 6. CORROSION LEVEL CLASSIFIED AS L
- [SDR DALA2022021701036](https://openairdocs.org/sdr/DALA2022021701036), Feb 16, 2022: NONE. NONE. SHIP 9559 - THE CREW DIVERTED THE AIRCRAFT TO LAX DUE TO ALL THREE GEAR NOT RETRACTING WHEN SELECTED. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE GEAR HANDLE 
- [SDR DALA2019062003670](https://openairdocs.org/sdr/DALA2019062003670), Jun 20, 2019: LENS. MISSING. THE AFT DOOR EMERGENCY LIGHT LESN MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.
- [SDR 2019F00197](https://openairdocs.org/sdr/2019F00197), Apr 30, 2019: SPOILER. DELAMINATED. RT WING SPOILER DELAMINATED.
- [SDR DALA2024010500204](https://openairdocs.org/sdr/DALA2024010500204), Apr 26, 2019: UNKNOWN. UNKNOWN. FUSELAGE SKIN DAMAGE AFT OF R1 DOOR. CUTOUT DAMAGED SECTION OF SKIN APPROX. 3" X 7.4" PER B717 SRM 53-03-01-2R-1 REPAIR 1. CUTOUT CONTAINMENT ACCOMPLISHED PER N
- [SDR DALA2019042202555](https://openairdocs.org/sdr/DALA2019042202555), Apr 21, 2019: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS AT STA 389 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE BATTERY PACK PER B717 AMM 33-51-03. (LP #5456807)
- [SDR DALA2018091005512](https://openairdocs.org/sdr/DALA2018091005512), Sep 7, 2018: BATTERY PACK. DISCHARGED. LOWER OVERWING EXIT SIGNS ARE INOPERATIVE DURING EEPLS TEST. MAINTENANCE REPLACED THE BATTERY PACK B5-119. CHECK IS OK REF AMM 33-51.
- [SDR DALA2018082205204](https://openairdocs.org/sdr/DALA2018082205204), Aug 21, 2018: BATTERY PACK. INOPERATIVE. DURING A SERVICE CHECK, MAINTENANCE THE FOUND L1 AND R1 DOOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BATTERY IAW 
- [SDR DALA2018073104780](https://openairdocs.org/sdr/DALA2018073104780), Jul 27, 2018: BATTERY PACK. DISCHARGED. MULTIPLE CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-121 AND B5-235 REF AMM 33-51. OPERATIONAL CHECK IS GOOD.
- [SDR DALA2017082306343](https://openairdocs.org/sdr/DALA2017082306343), Aug 23, 2017: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT LIGHTS AT THE FORWARD DROP CEILING, EXIT IDENTIFIER IN FIRST CLASS CABIN AND THE SERVICE DOOR OVERHEAD LIGHT ARE INOPERATIVE. MAINTENANCE REP
- [SDR DALA2017071305389](https://openairdocs.org/sdr/DALA2017071305389), Jul 12, 2017: LENS. MISSING. EMERGENCY LIGHT LENS MISSING. INSTALLED THE LIGHT LENS.
- [SDR DALA2017042603395](https://openairdocs.org/sdr/DALA2017042603395), Apr 26, 2017: LAMP. INOPERATIVE. FOUND LT EMERGENCY LIGHT INOP. REPLACED THE LAMPS IAW AMM 33-51. OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR DALA2017021501229](https://openairdocs.org/sdr/DALA2017021501229), Feb 14, 2017: SKIN. CRACKED. SKIN CRACKED BS 1133 OTDB OF LONGERON2L. REPAIRED THE SKIN IAW ER/A 553669-14AD REV 0.
- [SDR DALA2017021501266](https://openairdocs.org/sdr/DALA2017021501266), Feb 13, 2017: SKIN. CORRODED. FORWARD CARGO HAS CORROSION ON SKIN INBOARD OF LONGERON 28L BETWEEN STA 636 AND STA 655. REMOVED CORRODED INTERNAL DOUBLER AND INSTALLED NEW INTERNAL DOUBLER BE
- [SDR DALA2017021501267](https://openairdocs.org/sdr/DALA2017021501267), Feb 9, 2017: DOOR. CORRODED. L1 PASSENGER DOOR AIRSTAIR DOOR HAS CORROSION IN FORWARD AND AFT LOWER CORNERS AND AROUND AND INCLUDING NUT CLIPS AND GOUGES IN LOWER FLANGE. INSTALLED NEW AIRS
- [SDR DALA2017020801035](https://openairdocs.org/sdr/DALA2017020801035), Feb 7, 2017: SEAT TRACK. CORRODED. SEAT TRACK RBL 44.5 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 900 - 986. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-30-07 FIG 18, 53-00-00-1A. LOCAT
- [SDR DALA2017020801034](https://openairdocs.org/sdr/DALA2017020801034), Feb 7, 2017: FRAME. CRACKED. BS 1022 BULKHEAD REAR FRAME ANGLE IS CRACKED STRINGER 7L, VERIFIED WITH HFEC . REPAIRED IAW SRM 51-70-11 REPAIR 1.
- [SDR DALA2017020901078](https://openairdocs.org/sdr/DALA2017020901078), Feb 3, 2017: CUSP WEB. CRACKED. UPPER CABIN CUSP WEB FOUND CRACKED AT STA 832 LBL 58. UPPER CABIN CUSP WEB CRACK REPAIRED IAW SRM 53-00-55-R2-4. REMOVED AND INSTALLED SEAT TRACK TO ACCESS, IAW
- [SDR DALA2017020601004](https://openairdocs.org/sdr/DALA2017020601004), Feb 3, 2017: SEAT TRACK. CORRODED. RIGHT CENTER SEAT TRACK STA 556-656 RBL 44.5 HAS CORROSION AND NEED PAINT TOUCHED UP. REPAIRED SEAT TRACK SECTION RBL 44.5 BETWEEN STA 581-644 BLENDED OUT OF LI
- [SDR DALA2017020601003](https://openairdocs.org/sdr/DALA2017020601003), Feb 3, 2017: SEAT TRACK. CORRODED. LEFT CENTER SEAT TRACK HAS AREAS OF CORROSION, GOUGING, AND AREAS OF MISSING PRIMER AND TOPCOAT FROM STA 556 TO STA 656. REPAIRED SEAT TRACK SECTION 44.5 BETWEE

All 102: https://openairdocs.org/aircraft/N923AT/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/N923AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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