# N926AT: 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: 55078
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 2003
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ACD486
- 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=926AT
- Page: https://openairdocs.org/aircraft/N926AT

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/N926AT/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 N926AT.

## FAA accident and incident reports

None matched to N926AT.

## Service difficulty reports (179, 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 DALA2026100805562](https://openairdocs.org/sdr/DALA2026100805562), Oct 8, 2026: LIGHT. MISSING. EXIT LIGHTING STRIP AND TRIM MISSING IN FRONT FWD SIDE, INSTALLED EMERGENCY LIGHTING STRIP IAW AMM 23-50. (8981540) (AIRCRAFT GROUNDED).
- [SDR DALA2026092105263](https://openairdocs.org/sdr/DALA2026092105263), Sep 19, 2026: BATTERY PACK. NO TEST. ON SVC CHK FOUND EMER LIGHTS AT ROW 25 TO 28 OUT. R/R EMERGENCY LIGHT BATTERY PACK AT ROW 25 IAW B717 AMM 33-51 OPS CHK GOOD. (9115266) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026041402361](https://openairdocs.org/sdr/DALA2026041402361), Apr 10, 2026: FUEL CAP. LEAKING. FUEL SMELL IN THE CABIN. FOUND ALL FUEL TANKS AT MAX CAP. AND FUEL LEAK FROM RT OVERWING AUX FUEL FILL PORT. SUSPECT SEAL BAD. R/R AUX FUEL FILL CAP SEAL REF. B
- [SDR DALA2025091606814](https://openairdocs.org/sdr/DALA2025091606814), Sep 14, 2025: DOOR. OUT OF ALIGNMENT. DIVERTED TO STL DUE TO INTERMITTENT AIRFRAME VIBRATION ABOVE 270KTS, SLOWED TO 250KTS AND VIBRATION STOPPED. FOUND RIGHT NOSE GEAR DOOR GAP MUCH LARGER THAN LEF
- [SDR DALA2025043003317](https://openairdocs.org/sdr/DALA2025043003317), Apr 30, 2025: DOUBLER. CRACKED. DOUBLER CRACKED. AFT LOWER CORNER OF AFT CARGO DOOR. MARKED NRC 455. REMOVED EXISTING REPAIR & REPLACED DOUBLER REF B717 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12.
- [SDR DALA2025042303170](https://openairdocs.org/sdr/DALA2025042303170), Apr 22, 2025: WIRE. DAMAGED. SEAT EMERGENCY PATH LIGHTS ARE INOPERATIVE. SUMMARY SEE NRC 087-0001:3351-2001/001 00359: REPAIRED WIRE E9405-7-16N REF B717 SWPM 20-10-03. REPLACED POWER SUPPL
- [SDR DALA2025032402192](https://openairdocs.org/sdr/DALA2025032402192), Mar 23, 2025: PUMP. LEAKING. SHIP 9573 -ATB- ON ROTATION, THE CREW RECEIVED A "HYD R LO PRESS" MESSAGE AND THE INABILITY TO RETRACT THE GEAR. THEY MOVED THE GEAR SELECTION LEVER DOWN AND RE
- [SDR DALA2024122712036](https://openairdocs.org/sdr/DALA2024122712036), Dec 27, 2024: RESERVOIR. LEAKING. SHIP 9573 -MISC- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LOSS AFTER GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE FOUND TH
- [SDR DALA2023112809769](https://openairdocs.org/sdr/DALA2023112809769), Nov 28, 2023: UNKNOWN. UNKNOWN. DOOR 1L WILL NOT OPEN FROM INSIDE OR OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. S
- [SDR DALA2023112809767](https://openairdocs.org/sdr/DALA2023112809767), Nov 27, 2023: UNKNOWN. UNKNOWN. THE 1L DOOR WOULD NOT OPEN FROM THE OUTSIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MA
- [SDR DALA2023061304794](https://openairdocs.org/sdr/DALA2023061304794), Jun 12, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL REPAIR DOUBLERS BTW STA 966/1000 AND BTW STR 28L/25L APROX AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00158: CORROSION LEVEL 2. REPAIR 
- [SDR DALA2023060604561](https://openairdocs.org/sdr/DALA2023060604561), Jun 5, 2023: UNKNOWN. UNKNOWN. AFTER P DOME STIFFENER REMOVAL, 4 HOLE LOCATIONS WERE NOTED TO BE MISSDRILED. IN REF TO NRC 00209. SUMMARY OF NRC 00566: HOLES (4 LOCATIONS) WERE REPAIRED PER P
- [SDR DALA2023060604555](https://openairdocs.org/sdr/DALA2023060604555), Jun 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON CHORD ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00208: CORRO
- [SDR DALA2023060104389](https://openairdocs.org/sdr/DALA2023060104389), Jun 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG 1
- [SDR DALA2023060104388](https://openairdocs.org/sdr/DALA2023060104388), Jun 1, 2023: UNKNOWN. UNKNOWN. SEVERE CORROSION ON GALLEY SERVICE DOOR CUSP ANGLE STA 168 TO 201 X=-44 TO X=-60. SUMMARY OF NRC 374: CORROSION LEVEL 2. CUSP ANGLE OF GALLEY SERVICE DOOR STA 1
- [SDR DALA2023060104387](https://openairdocs.org/sdr/DALA2023060104387), Jun 1, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH AT CPAX (CPAX). SUMMARY OF NRC 00215: FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH WAS REPAIRED PER PRI 6084
- [SDR DALA2023060104386](https://openairdocs.org/sdr/DALA2023060104386), Jun 1, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH AT CPAX (CPAX). SUMMARY OF NRC 00210: FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH WAS REPAIRED PER PRI 60
- [SDR DALA2023053104338](https://openairdocs.org/sdr/DALA2023053104338), May 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00207: CORROSION LEVEL 2. R
- [SDR DALA2023053004252](https://openairdocs.org/sdr/DALA2023053004252), May 27, 2023: SKIN. CRACKED. CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH. (FUS). SUMMARY OF NRC 00300: FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14 RH WAS REPAIRED PER PRI 608247-14 
- [SDR DALA2023052604191](https://openairdocs.org/sdr/DALA2023052604191), May 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60. SUMMARY OF NRC 00454: CORROSION LEVEL 2. MEMBRANE STA 148 TO 201, X=- 44 TO X=- 60 WAS REPAIRED PER B717
- [SDR DALA2023052204053](https://openairdocs.org/sdr/DALA2023052204053), May 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG.1
- [SDR DALA2023052004044](https://openairdocs.org/sdr/DALA2023052004044), May 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORTS RH X=- 30 TO X=- 60 STA 148 WERE REPLACED PER B
- [SDR DALA2023052004043](https://openairdocs.org/sdr/DALA2023052004043), May 19, 2023: UNKNOWN. UNKNOWN. REMOVAL CABIN FLOOR SUPORT AT STA Y=148 BTW X=- 44 TO X=- 60, REVEALED CORROSION ON IT, IN REF TO NRC 00454. SUMMARY OF NRC 00565: CORROSION LEVEL 2. FLOOR SUPP
- [SDR DALA2023052304104](https://openairdocs.org/sdr/DALA2023052304104), May 18, 2023: UNKNOWN. UNKNOWN. AFTER REMOVAL OF SUPPORT, CORROSION WAS FOUND ON FLOOR SUPORT STA Y=160 BTW RBL 44 TO RBL 54 CABIN PAX (CPAX). SUMMARY OF NRC 00548: CORROSION LEVEL 2. FLOOR SU
- [SDR DALA2023052004041](https://openairdocs.org/sdr/DALA2023052004041), May 17, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON FLOOR SUPORT STA Y=180 BTW RBL 44 TO RBL 10 CABIN PAX (CPAX) AFTER REMOVAL OF SUPPORT. SUMMARY OF NRC 00547: CORROSION LEVEL 2. FLOOR SUP
- [SDR DALA2023051803949](https://openairdocs.org/sdr/DALA2023051803949), May 17, 2023: UNKNOWN. UNKNOWN. SEVERE CORROSION ON MAIN ENTRANCE DOOR JAMB WEB STA 200. SUMMARY OF NRC 00372: CORROSION LEVEL 2. DOOR JAMB WEB WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4.
- [SDR DALA2023051603856](https://openairdocs.org/sdr/DALA2023051603856), May 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA=389 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00424: CORROSION LEVEL 2. CUSP WEB STA=389 RH WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCE
- [SDR DALA2023051203747](https://openairdocs.org/sdr/DALA2023051203747), May 12, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB STA=370 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00423: CUSP WEB STA=370 RH SIDE AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-41-02-0G PAR 4 AND 
- [SDR DALA2023051203746](https://openairdocs.org/sdr/DALA2023051203746), May 11, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB RH STA=650 TO STA=660 PROX. SUMMARY OF NRC 00439: CUSP WEB RH STA=650 TO STA=660 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 
- [SDR DALA2023051003668](https://openairdocs.org/sdr/DALA2023051003668), May 10, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM #1, STA Y=195 FWD PASSENGER DOOR (L1). SUMMARY OF NRC-00101: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, F
- [SDR DALA2023051003667](https://openairdocs.org/sdr/DALA2023051003667), May 10, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM #1, STA Y=160 FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00100: CRACK WAS FOUND PREVIOUSLY REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 7, PAR. 6, F
- [SDR DALA2023050803572](https://openairdocs.org/sdr/DALA2023050803572), May 8, 2023: UNKNOWN. UNKNOWN. WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 520MB LH WING. SUMMARY OF NRC 459: FUEL ACCESS PLATE 520MB WAS NOT POSSIBLE REPAIR AS PER B717-200 SRM-57-
- [SDR DALA2023050803571](https://openairdocs.org/sdr/DALA2023050803571), May 8, 2023: UNKNOWN. UNKNOWN. WEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 620PB RH WING. SUMMARY OF NRC 470: FUEL ACCESS PLATE 620PB DUE TO REPAIR OF WAS NOT POSSIBLE AS PER B717-2
- [SDR DALA2023050803570](https://openairdocs.org/sdr/DALA2023050803570), May 7, 2023: UNKNOWN. UNKNOWN. WEAR ON AFT INNER EDGE NEAR OF DOOR LATCH AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00059: INNER PAN AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200
- [SDR DALA2023050403458](https://openairdocs.org/sdr/DALA2023050403458), May 3, 2023: UNKNOWN. UNKNOWN. CRACK EVIDENCE ON FWD LWR CORNER OF LH WINDOW BELT STA S 851 AND 908 AT PAX CAB. SUMMARY OF NRC 00408: REPAIR WAS PERFORMED PER B717-200 SRM 56-20-02-2R PROCEDU
- [SDR DALA2023050303433](https://openairdocs.org/sdr/DALA2023050303433), May 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS X=-8 TO X=8 STA 201. SUMMARY OF NRC 00451: CORROSION LEVEL 2. FLOOR SUPPORT LH STA 201 X=-8 TO X=8 WAS REPLACED PER B717-200 SRM 53-
- [SDR DALA2023031401857](https://openairdocs.org/sdr/DALA2023031401857), Mar 11, 2023: UNKNOWN. UNKNOWN. THE R1 EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENACE REPLACED THE BATTERY B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4072112)
- [SDR DALA2022100406442](https://openairdocs.org/sdr/DALA2022100406442), Oct 3, 2022: NONE. NONE. THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-55. (LP #7679774)
- [SDR DALA2022091906176](https://openairdocs.org/sdr/DALA2022091906176), Sep 17, 2022: NONE. NONE. UPON SERVICE CHECK, THE FIRST CLASS EMERENGCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EMERENGCY LIGHTS BATTERY AT B5-259 PER B717 AMM 33-51. OPERAT
- [SDR DALA2022081605531](https://openairdocs.org/sdr/DALA2022081605531), Aug 14, 2022: NONE. NONE. THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT SEAT ROW 20. MAINTENANCE SECURED EXIT ROW SIGN COVER. (LP #2365299)
- [SDR DALA2021050602570](https://openairdocs.org/sdr/DALA2021050602570), May 5, 2021: BATTERY PACK. INOPERATIVE. THE CEILING EMERGENCY LIGHTS IS OUT AT 16,17,18. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT 17CDE, O/H BIN, PER B717 AMM 33-51. THE EMERGENCY LIG
- [SDR DALA2021032301674](https://openairdocs.org/sdr/DALA2021032301674), Mar 21, 2021: SIGN. DISLODGED. THE EXIT SIGN AT RO 19 IS DISLODGED. MAINTENANCE SECURED THE EXIT SIGN. (LP #7446516)
- [SDR DALA2020120703985](https://openairdocs.org/sdr/DALA2020120703985), Dec 7, 2020: BATTERY PACK. INOPERATIVE. THE LEFT AND RIGHT FORWARD OVER WING EXIT IDENTIFIER LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY FOR POWER SUPPLY B5-118 BAD AND REPLACED
- [SDR DALA2020102003405](https://openairdocs.org/sdr/DALA2020102003405), Oct 20, 2020: CHARGER. INOPERATIVE. THE EMERGENCY EXIT SIGN AT ROW 1 IS INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY AT B5-259. OPERATIONAL CHECK IS NORMAL, PER B717 AMM 33-54.
- [SDR DALA2020091703103](https://openairdocs.org/sdr/DALA2020091703103), Sep 17, 2020: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, FOUND 5 EACH EMERGENCY CEILING LIGHTS IN THE AFT SECTION INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-231, PER B717 AMM 33-51. OP
- [SDR DALA2020082402837](https://openairdocs.org/sdr/DALA2020082402837), Aug 24, 2020: BATTERY PACK. INOPERATIVE. BOTH FORWARD OVERWING EXIT SIGN LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS GOOD REF B717 AMM 33-55
- [SDR DALA2020032602045](https://openairdocs.org/sdr/DALA2020032602045), Mar 25, 2020: THRESHOLD. CORRODED. CORROSION FOUND AT AFT CARGO DOOR THRESHOLD - MARKED. RCN 067-0008:5331-2001/009 00165: REPAIRED REF B717 SRM 53-20-15-2R PROCED 7. CLOSING REQUIREMENTS RII: IN
- [SDR DALA2020032602043](https://openairdocs.org/sdr/DALA2020032602043), Mar 24, 2020: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT IS CORRODED AT STA 196 LBL 52. NRC 068-0011:2531-4006/001 00280: REPLACED SUPPORT REF BOEING DWG #9936534. (LP #1538491)
- [SDR DALA2017121108490](https://openairdocs.org/sdr/DALA2017121108490), Dec 9, 2017: ENGINE. SURGES. SHIP 9573 - THE CREW EXPERIENCED AN ENGINE SURGE AND HIGH EXHAUST TEMPERATURES WITH THE #2 ENGINE SO THE FLIGHT DIVERTED TO CAE. THE PILOT DID REDUCE POWER ON T
- [SDR DALA2017081606258](https://openairdocs.org/sdr/DALA2017081606258), Aug 15, 2017: COVER. LOOSE. EMERGENCY EXIT SIGN COVER LOOSE. SECURED THE SIGN, CHECKED OK.

All 179: https://openairdocs.org/aircraft/N926AT/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/N926AT/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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