# N928AT: 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: 55076
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 13, 2000
- Certificate issued: August 1, 2024
- Expires: August 31, 2031
- Mode S code: ACDBF4
- 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=928AT
- Page: https://openairdocs.org/aircraft/N928AT

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/N928AT/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 N928AT.

## FAA accident and incident reports

None matched to N928AT.

## Service difficulty reports (159, 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 DALA2026083104911](https://openairdocs.org/sdr/DALA2026083104911), Aug 30, 2026: SWITCH. LOOSE. TAIL CONE EXIT TOGGLE SWITCH/LATCH LOOSE. CORRECTIVE ACTION: RESECURED AND ADJUSTED HARDWARE PER B717 AMM 52-22, NO OHTER FAULTS NOTED A/C OK TO CONT IN SVC. (9
- [SDR DALA2026082504809](https://openairdocs.org/sdr/DALA2026082504809), Aug 24, 2026: SKIN. CRACKED. CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT STA Y=1037 BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 624765-14. (1774752) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803991](https://openairdocs.org/sdr/DALA2026070803991), Jul 7, 2026: COALESCER BAG. ODOR. BURNING ELECTRICAL ODOR FROM FWD CARGO COMPARTMENT, R & R COELESCER BAGS PER B717 AMM 21-54. (1687018) (AIRCRAFT GROUNDED).
- [SDR DALA2026052803227](https://openairdocs.org/sdr/DALA2026052803227), May 23, 2026: SLIDE. DETACHED. UPON ARRIVAL & OPENING 1L DOOR, EMERGENCY SLIDE SEPARATED FROM DOOR & FELL INTO JET BRIDGE. SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE IAW B717 AMM 25-61. 
- [SDR DALA2026050502822](https://openairdocs.org/sdr/DALA2026050502822), May 3, 2026: DOOR FRAME. CRACKED. AFTER REMOVAL STOP FITTING CRACK WAS FOUND ON OUTER PAN AFT EDGE BEAM 4 AT AFT CARGO COMPARMENT DOOR. REPAIRED PER ERA 633375-14 (1576138) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502821](https://openairdocs.org/sdr/DALA2026050502821), May 2, 2026: FRAME. CRACKED. CRACK ON CANTED FRAME AT Y=1200 AND PROJECTION. REPAIRED PER SRM 51-70-11-2R (1574671) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502814](https://openairdocs.org/sdr/DALA2026050502814), Apr 29, 2026: SUPPORT ANGLE. CRACKED. CRACK ON ANGLE SUPPORT (FWD BULKHEAD) BTW STA Y= 816 AND LONGERON 30 AT AFT CARGO COMPARTMENT. CRACK ON ANGLE SUPPORT (FWD BULKHEAD) BTW STA Y= 816 AND LONGERON
- [SDR DALA2026050502812](https://openairdocs.org/sdr/DALA2026050502812), Apr 29, 2026: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BTW STA Y=1022.091 TO Y=1037 AND L30 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 51-41-02-0G AND B717-200 SRM 51-41-05. (1568910) (AIRCR
- [SDR DALA2026042902729](https://openairdocs.org/sdr/DALA2026042902729), Apr 27, 2026: SEAT TRACK. CRACKED. SHIP 9571 AFTER REMOVE OF THE CUSP WEB, SEAT TRACK WAS FOUND WHIT CRACK. CORRECTIVE ACTION: SEAT TRACK WHIT CRACK WAS REPAIRED PER B717-200 SRM 53-20-52 (156603
- [SDR DALA2026042902728](https://openairdocs.org/sdr/DALA2026042902728), Apr 27, 2026: CUSP WEB. CRACKED. SHIP 9571 CRACK ON RH CUSP WEB BTW STA Y= 617 TO Y=636 , Y=636 TO Y=655 AND Y=656 TO Y=674. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1565636) (AIR
- [SDR DALA2026042902727](https://openairdocs.org/sdr/DALA2026042902727), Apr 26, 2026: CUSP WEB. CRACKED. SHIP 9571 CRACK ON CUSP WEB BTW STA Y=655 AND X= 56 AT PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 AND SRM 51-41-02-0G
- [SDR DALA2026042902726](https://openairdocs.org/sdr/DALA2026042902726), Apr 25, 2026: CUSP WEB. CRACKED. SHIP 9571 CRACK AND MISSING MATERIAL ON RH CUSP WEB AT STA 460 X=56 AT CPAX. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1561674) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902725](https://openairdocs.org/sdr/DALA2026042902725), Apr 25, 2026: CUSP WEB. CRACKED. SHIP 9571 CORROSION ON RH CUSP WEB LOWER AREA BTW STA 218 AND 228, X=54 AT CPAX. CORRECTIVE ACTION: REPAIRED PER 717-200 SRM 51-41-05-0G AND SRM 51-40-02. (1561
- [SDR DALA2026042902724](https://openairdocs.org/sdr/DALA2026042902724), Apr 25, 2026: CUSP WEB. CRACKED. CRACK ON CUSB WEB BTW STA Y= 715 TO STA Y= 737 AND X=44. REPAIRED PER B717-200 SRM 53-00-55 (1561470) (AIRCRAFT GROUNDED)
- [SDR DALA2026042302604](https://openairdocs.org/sdr/DALA2026042302604), Apr 22, 2026: FRAME. CRACKED. INITIAL INSPECTION: CRACK ON CAP IN FRAME Y=1022 AND L 7R AT CPAX. REPAIR AND PRI 633416-14 (1557376) (AIRCRAFT GROUNDED)
- [SDR DALA2026042302603](https://openairdocs.org/sdr/DALA2026042302603), Apr 22, 2026: WEB. CORRODED. CORROSION ON WEB BTW STA Y=180, STA Y=200, X =54 AND X=44.5 AT CPAX. REPAIRED PER B717-200 SRM 51-70-10 (1557318) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202563](https://openairdocs.org/sdr/DALA2026042202563), Apr 20, 2026: WEB. CRACKED. CRACK ON CORNER AT LOWER WEB STA Y= 219 X= 55. REPAIRED PER B717-200 SRM 51-70-10 (1554629) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202561](https://openairdocs.org/sdr/DALA2026042202561), Apr 19, 2026: FLOOR SUPPORT. CORRODED. CORROSION FLOOR SUPPORT ON X=44.5 BTW STA Y= 148 AND STA Y=200 AT CPAX. REPAIRED PER SRM 51-41-02-0G AND B717-200 SRM 51-41- 05. (1551876) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202560](https://openairdocs.org/sdr/DALA2026042202560), Apr 18, 2026: INTERCOSTAL. CRACKED. SHIP 9571 CRACK ON INTERCOSTAL ON UPPER AFT CORNER ALSO CRACK NEAR FASTENERS ON CLIP IN THE SAME INTERCOSTAL X=0 ON STA Y=1022 AT CPAX. REPAIRED PER B717-200 SR
- [SDR DALA2026041702447](https://openairdocs.org/sdr/DALA2026041702447), Apr 13, 2026: CUSP WEB. CRACKED. AFTER CRACK REMOVAL ON CUSP WEB STA Y=655-684 RH SIDE, AT PASSENGER COMPARTMENT. REPAIRED PER B717-200 SRM 53-00-55 (1542990) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402367](https://openairdocs.org/sdr/DALA2026041402367), Apr 12, 2026: FRAME. CRACKED. CRACK ON FRAME BS 1037 AND L17R. REPAIRED PER SRM 53-20-07 (1541418) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402346](https://openairdocs.org/sdr/DALA2026041402346), Apr 10, 2026: LONGERON. CRACKED. CRACK ON LONGERON RH #17, RH #8 AND RH #6 STA Y=1022 AT CPAX. REPAIRED PER SRM 53-00-05 (1538208) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402344](https://openairdocs.org/sdr/DALA2026041402344), Apr 10, 2026: SKIN. DENTED. DENTS 2E/A ON LH EXTERNAL SKIN OF RUDDER ZR 42. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-70-13-2R-1. (1536804) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402343](https://openairdocs.org/sdr/DALA2026041402343), Apr 9, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BTW LONG 13 RT & 14 RT. REPAIRED PER PRI 633254-14 REV. 2 AND ER/A 633254-14 (1536512) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402348](https://openairdocs.org/sdr/DALA2026041402348), Apr 7, 2026: HINGE FITTING. CORRODED. CORROSION ON CENTER FLAP HINGE FITTING (OUTB/ LOWER HOLE AND STUD) STA XRS 260.000 APROX AT LH WING. CORRECTIVE ACTION: FITTING WAS REMOVED PER B717-200 AMM 57-
- [SDR DALA2026041302317](https://openairdocs.org/sdr/DALA2026041302317), Apr 6, 2026: FLOOR SUPPORT. CORRODED. SHIP 9571 CORROSION ON FLOOR SUPPORT APPROX STA Y=180 BTW X=44.5 AND X=15 AT CPAX. DAMAGED AREA REPAIRED PER DWG 9936534-43 AND B717-200 SRM 51-41-02 (1531523) 
- [SDR DALA2026033002083](https://openairdocs.org/sdr/DALA2026033002083), Mar 29, 2026: BEAM. CRACKED. CRACKED OUTER PAN, FWD EDGE, BEAM NR 5 AT THE FWD CARGO DOOR. THE BEAM WAS REPAIRED IAW SRM 52-30-02. (1518647)
- [SDR DALA2026033002082](https://openairdocs.org/sdr/DALA2026033002082), Mar 29, 2026: PAN. CRACKED. CRACKED OUTER PAN, FWD EDGE, BEAM NR 3 IN THE FWD CARGO DOOR. THE CARGO DOOR WAS REPAIRED IAW SRM 52-30-02. (1518642)
- [SDR DALA2026033002081](https://openairdocs.org/sdr/DALA2026033002081), Mar 29, 2026: LONGERON. CRACKED. CRACKED LONGERON 8L, BS 1022. CRACKED LONGERON 8L WAS REPAIRED IAW SRM 53-00-05, (1518640)
- [SDR DALA2026031001647](https://openairdocs.org/sdr/DALA2026031001647), Mar 6, 2026: CONTROLLER. FAULTED. SHIP 9571-ATB- RETURNED TO ATL DUE TO A FLAP/SLAT DISAGREE MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #2 FCC DUE TO ERRATIC SENSOR READOUTS. COMPLIED 
- [SDR DALA2025031001823](https://openairdocs.org/sdr/DALA2025031001823), Mar 10, 2025: SKIN. CRACKED. CRACK EVIDENCE ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L. SUMMARY OF NRC 0180: AREA WAS REPAIRED ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L PER PRI
- [SDR DALA2025031001822](https://openairdocs.org/sdr/DALA2025031001822), Mar 8, 2025: ELEC CONNECTOR. DAMAGED. THE EMERGENCY LIGHT DOES NOT TURN ON IN THE AFT ACCESSORY VENTRAL WALKWAY. SUMMARY OF NRC 00219: CONNECTOR P1-260 OF BATTERY PACK B5-250 AND CONNECTOR P1-116 OF
- [SDR DALA2025031001819](https://openairdocs.org/sdr/DALA2025031001819), Mar 7, 2025: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 LONG 17 LH. SUMMARY OF NRC 00189: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #084
- [SDR DALA2025030401649](https://openairdocs.org/sdr/DALA2025030401649), Mar 3, 2025: SKIN. WORN. WEAR ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1. SUMMARY OF NRC 00036: DAMAGE ON EXTERNAL SKIN, NEAR CUT OUT OF HOOK, AT PASSENGER DOOR L1 WAS
- [SDR DALA2025030301648](https://openairdocs.org/sdr/DALA2025030301648), Mar 1, 2025: PAN. CORRODED. CORROSION ON AFT CARGO DOOR JAMB PAN BTW LONG 24RH TO LONG 27RH (NEW SECTION AND PRODUCTION SECTION OF PAN). SUMMARY OF NRC 00118: CORROSION LEVEL 2. CARGO DOOR
- [SDR DALA2025022101361](https://openairdocs.org/sdr/DALA2025022101361), Feb 19, 2025: FASTENER. LOOSE. -AD- LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE FOUND IN REFERENCE TO AMDS 5530-01048-02 STEP 3 "AA 5530-0104
- [SDR DALA2024071006986](https://openairdocs.org/sdr/DALA2024071006986), Jul 8, 2024: BATTERY. INOPERATIVE. ON SERVICE CHECK FOUND OVERWING EMERGENCY EVACUATION LIGHTS NOT ILLUMINATING. REPLACED OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATION
- [SDR DALA2024042404676](https://openairdocs.org/sdr/DALA2024042404676), Apr 24, 2024: LENS. MISSING. THE CABIN CREW NOTED THAT THE AFT TAIL COMPT EMERGENCY EXIT LIGHT LENS IS MISSING. MAINTENANCE INSTALLED THE MISSING LIGHT COVER AT AFT TAIL OF AIRCRAFT. THE AI
- [SDR DALA2023042603245](https://openairdocs.org/sdr/DALA2023042603245), Apr 24, 2023: UNKNOWN. UNKNOWN. PARTS DEPARTED AICRAFT. GROUND CREW FOUND AIRCRAFT PANEL ACCESS DOOR MISSING. MAINTENANCE REPLACED THE GROUND AIR PANEL ACCESS DOOR. TOP/3998-23 (LP #4027955)
- [SDR DALA2023042503244](https://openairdocs.org/sdr/DALA2023042503244), Apr 22, 2023: UNKNOWN. UNKNOWN. ARCING LIGHT WITH ASSOCIATED SMELL AND NOISE FROM BEHIND TRIM FORWARD OF F/O CLEARVIEW WINDOW. CBZ24 PULLED R/H WINDSHIELD ANTI-ICE FOR TROUBLESHOOTING NA 23754
- [SDR DALA2023033102475](https://openairdocs.org/sdr/DALA2023033102475), Mar 29, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9571, INITIAL INSPECTION: BROKEN BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING. CORRECTIVE ACTION: BRACKET INSIDE ACCESS PANEL NBR 530AF ON 
- [SDR DALA2023033102474](https://openairdocs.org/sdr/DALA2023033102474), Mar 29, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9571, INITIAL INSPECTION: CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS R
- [SDR DALA2023032602317](https://openairdocs.org/sdr/DALA2023032602317), Mar 25, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9571, CORROSION AT SLIDE SUPPORTS LOCATED AT RBL 53 BETWEEN STA-163 AND STA-186. CORRECTIVE ACTION: NEW SUPPORTS (2EAS) WERE REPLACED PER B717-200 SRM 
- [SDR DALA2023032602315](https://openairdocs.org/sdr/DALA2023032602315), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9571, DURING OK TO TREAT RH WING BOX AREA WITH CIC, CRACKED CUSP MEMBRANE WEB WAS FOUND ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE. COR
- [SDR DALA2023030801721](https://openairdocs.org/sdr/DALA2023030801721), Mar 4, 2023: NONE. NONE. SHIP 9571 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY INTO ATL DUE TO THE "RIGHT HYDRAULIC LOW-PRESSURE" MESSAGE. THE ALTERNATE GEAR EXTENSION PROCEDURES WER
- [SDR DALA2023011000173](https://openairdocs.org/sdr/DALA2023011000173), Jan 9, 2023: LIGHT. MISWIRED. FOUND EMERGENCY LIGHT FLOOD LIGHT AT R1 DOOR INOPERATIVE. FOUND POWER WIRE FOR EMERGENCY LIGHT IN WRONG TERMINAL. RE-CONFIGURED PER WDM 33-51-12. ALSO FOUND POW
- [SDR DALA2022061704243](https://openairdocs.org/sdr/DALA2022061704243), Jun 13, 2022: HUB CAP. MISSING. ON LANDING IN KGRR, GOT "ANTI-SKID L FAIL" MESSAGE. ON SD BRAKES WERE NOT APPLIED UNTIL ABOUT 75 KNOTS ON LANDING ROLL. *** CONTRACT MAINTENANCE EVENT - OCM: 24
- [SDR DALA2020021801205](https://openairdocs.org/sdr/DALA2020021801205), Feb 18, 2020: SIGN. INOPERATIVE. THE EMERGENCY EXIT SIGN IS INOPERATIVE AT 603. EXIT PLACARD MISSING ON CEILING EXIT SIGN AT WINDOW EXITS. MAINTENANCE FOUND THE MISSING EXIT SIGN LENS AND REINS
- [SDR DALA2020021801204](https://openairdocs.org/sdr/DALA2020021801204), Feb 18, 2020: SIGN. INOPERATIVE. THE EMERGENCY EXIT SIGN IS INOPERATIVE AT 602. EXIT PLACARD IS MISSING ON CEILING EXIT SIGN AT WINDOW EXITS. MAINTENANCE FOUND THE MISSING EXIT SIGN AND REINSTA
- [SDR DALA2019111906762](https://openairdocs.org/sdr/DALA2019111906762), Nov 19, 2019: POWER SUPPLY. INOPERATIVE. THE TAIL COMPARTMENT EMERGENCY FLOOD LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, B5-260, IAW B717 AMM 33

All 159: https://openairdocs.org/aircraft/N928AT/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/N928AT/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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