# N936AT: 1999 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: 55058
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 3, 2000
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ACFC05
- 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=936AT
- Page: https://openairdocs.org/aircraft/N936AT

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/N936AT/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 N936AT.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110311004849I](https://openairdocs.org/incident/20110311004849I), Mar 11, 2011: Boeing 717-200 (N936AT), West Palm Beach, FL, No damage. During taxi out captain stopped aircraft suddenly flight attendant fell with injury to arm. Flight attendant removed from flight treated by paramedics…

## Service difficulty reports (206, 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 DALA2026082404796](https://openairdocs.org/sdr/DALA2026082404796), Aug 21, 2026: OXYGEN MASK. UNSECURE. FWD FA JS OXYGEN MASK FELL, SECURED MASKS & STOWAGE BOX IAW AMM 35-13. (6787282) (AIRCRAFT GROUNDED).
- [SDR DALA2026080404491](https://openairdocs.org/sdr/DALA2026080404491), Aug 1, 2026: AOA. FAILED. ATO- APPROX 30KTS DUE TO STICK PUSHER FAIL AND DISARM SPOILERS ANNUNCIATION WITH ASSOCIATED MASTER CAUTION. REPLACED NR 2 AOA SENSOR. ALL OPS CHECK GOOD. (67872
- [SDR DALA2026071304125](https://openairdocs.org/sdr/DALA2026071304125), Jul 10, 2026: STRUCTURE. CORRODED. CORROSION ON INTERNAL STRUCTURE OF BOLT HOLES AND BARREL NUT HOLES 30. INTERNAL STRUCTURE OF BOLT HOLES AND BARREL NUT HOLES 30, 32, AND 34 OF RH SIDE AT HORIZO
- [SDR DALA2026071004048](https://openairdocs.org/sdr/DALA2026071004048), Jul 10, 2026: WEB. CRACKED. CRACK ON AFT CABIN BULKHEAD DOOR WEB AND X= 12 L/H AT CPAX, R & R CABIN BULKHEAD DOOR PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51- 41-01-0G, B717-200 SRM 51-4
- [SDR DALA2026070904034](https://openairdocs.org/sdr/DALA2026070904034), Jul 9, 2026: SKIN. CRACKED. CRACKS ON INTERNAL SKIN BTW STA Y= 760/770 AND BTW STA X= -45/-60 APPROX AT RT MLG DOOR, COMPLIED WITH ER/A 634942-14. (1689728) (AIRCRAFT GROUNDED).
- [SDR DALA2026070603939](https://openairdocs.org/sdr/DALA2026070603939), Jul 5, 2026: SUPPORT BRACKET. WORN. WORN SPRING SUPPORT BRACKET & PULLEY BRACKET OF RELEASE MECHANISM AT TAIL CONE. SPRING SUPPORT BRACKET, SPRING RELEASE MECHANISM & PULLEY BRACKET OF RELEASE MEC
- [SDR DALA2026070703971](https://openairdocs.org/sdr/DALA2026070703971), Jul 3, 2026: SPAR CAP. CORRODED. CORROSION, LT HORIZONTAL STAB UPPER & LOWER AFT PANEL, UPPER CENTER PANEL, REAR SPAR LWR CAP BARREL NUT HOLES 10, 14, 29, 31, 32, 33. REPAIRED IAW ER/A 635147-1
- [SDR DALA2026070603941](https://openairdocs.org/sdr/DALA2026070603941), Jul 1, 2026: SPAR CAP. CORRODED. CORROSION RT HORIZONTAL STAB LOWER AFT PANEL, LOWER REAR SPAR CAP BARREL NUT HOLES 30, 32, 34. REPAIRED IAW ER/A 635300-14AD. (1679290)(AIRCRAFT GROUNDED)
- [SDR DALA2026062503777](https://openairdocs.org/sdr/DALA2026062503777), Jun 25, 2026: SKIN. CORRODED. CORROSION ON UPPER WING SKIN BTW XRS=449 TO XRS=455 AND 12 FROM TRAILING EDGE AT RT WING. REPAIRED PER ER/A 634809-14. (1664981) (AIRCRAFT GROUNDED)
- [SDR DALA2026062303738](https://openairdocs.org/sdr/DALA2026062303738), Jun 23, 2026: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS ON CUSP WEB UPPER SIDE BTW X=-56 AND BS 304-310, BS 456-463, BS 570-577, STA 797-811 AND STA 944. CORROSION LEVEL 2, CUSP WEB UPPER SIDE
- [SDR DALA2026062303737](https://openairdocs.org/sdr/DALA2026062303737), Jun 22, 2026: DIAPHRAGM. CORRODED. CORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA Y=190, AND X46.5 TO X56 STA Y=196.5, AT CPAX (LH SIDE). CORROSION LEVEL 2 DIAPHRAGM BTW STA Y=160 TO STA Y=200 AND 
- [SDR DALA2026061903680](https://openairdocs.org/sdr/DALA2026061903680), Jun 19, 2026: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW X=-44 AND STA 674, STA 717 ALSO IN X=-56 AND STA 1014 AT CPAX. CUSP WEB BTW X=-44 AND STA 674, CUSP WEB BTW X=-56 AND STA 1014 WERE REPAIR
- [SDR DALA2026061903676](https://openairdocs.org/sdr/DALA2026061903676), Jun 17, 2026: SKIN. OUT OF LIMITS. HOLES OUT OF LIMITS ON LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE. LEADING EDGE STRUCTURE SPLI
- [SDR DALA2026061603615](https://openairdocs.org/sdr/DALA2026061603615), Jun 15, 2026: CUSP WEB. CRACKED. AIRCRAFT 9563, INITIAL INSPECTION: CRACK ON LH CUSP WEB BTW X54 STA Y=499, X56.5 STA Y= 631, X46 AND STA Y=675 AT CPAX. LT CUSP WEB BTW X54 STA Y=499, X56.5 STA
- [SDR DALA2026061103543](https://openairdocs.org/sdr/DALA2026061103543), Jun 6, 2026: LONGERON. CRACKED. CRACK ON LONGERONS L7R, L8R, AND L17R STA Y=1022 AND -X=56 AT CPAX. LONGERON L8R WAS CUT OUT ON STA Y=1012 TO STA Y= 1053 AND -X=56 AT CPAX WAS REPAIRED PER B71
- [SDR DALA2025111908460](https://openairdocs.org/sdr/DALA2025111908460), Nov 18, 2025: LANDING GEAR. MALFUNCTIONED. LANDING GEAR DID NOT DEPLOY ALL RED INDICATIONS NO FAULT MESSAGES DISPLAYED. AFTER GO AROUND GEAR DEPLOYED NORMAL ON 2ND ATTEMPT. GEAR HANDLE FULL DOWN HYD PRES
- [SDR DALA2025090906666](https://openairdocs.org/sdr/DALA2025090906666), Sep 5, 2025: ACCESS PANEL. DAMAGED. IN REF NRC 124 AFTER CLEAN ELONGATED HOLE FOUND ON FUEL ACCESS PLATE 520 JB. FUEL ACCESS PLATE 520JB WAS REPAIRED PER ER/A 628967-14AD (1183419)
- [SDR DALA2025081806156](https://openairdocs.org/sdr/DALA2025081806156), Aug 12, 2025: BATTERY. NO TEST. SHIP 9563 AFT BULKHEAD EMERGENCY EXIT LIGHT FLICKERING. CORRECTIVE ACTION: REMOVED AND REPLACED EMERG BATT ASSY B5-260.PER B717 AMM 33-51 AND BATT PER B717B AMM
- [SDR DALA2025081105990](https://openairdocs.org/sdr/DALA2025081105990), Jun 21, 2025: NONE. NONE. SHIP 9563 LOGPAGE CREATED TRACKING SECTION II INSPECTIONS TO ER/A 610356- 14AD. CORECTIVE ACTION: C/W ER/A 571712-14AD. (1037974)
- [SDR DALA2025052704029](https://openairdocs.org/sdr/DALA2025052704029), May 19, 2025: GENERATOR. FAILED. ABORTED TAKE-OFF DUE TO A LEFT ENGINE GENERATOR FAILURE MESSAGE: REPLACED GROND RELAY AND AUX POWER RELAY. TEST GOOD.
- [SDR DALA2025033102355](https://openairdocs.org/sdr/DALA2025033102355), Mar 30, 2025: POWER SUPPLY. INOPERATIVE. THE EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE B5-235 EMERGENCY BATTERY POWER SUPPLY/CHARGER REF B717 AMM 33-51. OPERATIONA
- [SDR DALA2024110510647](https://openairdocs.org/sdr/DALA2024110510647), Nov 5, 2024: BATTERY PACK. INOPERATIVE. MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN TAIL COMPARTMENT TO BE INOPERATIVE. DETERMINED THAT THE BATTERY PACK B5-116 WAS BAD. BATTERY PACK WAS REPLACED REF
- [SDR DALA2023082406885](https://openairdocs.org/sdr/DALA2023082406885), Aug 23, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE. SUMMARY OF NRC 00066; UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED
- [SDR DALA2023072105930](https://openairdocs.org/sdr/DALA2023072105930), Jul 20, 2023: UNKNOWN. UNKNOWN. THE CABIN OVERWING EMERGENCY EXIT LIGHTS B5-121/P9 AND B5-121/P11 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 PER
- [SDR DALA2023071305677](https://openairdocs.org/sdr/DALA2023071305677), Jul 12, 2023: UNKNOWN. UNKNOWN. WHILE PERFORMING AA 5530-01048 AND AD 2018-10-08, FOUND 3 CRACK INDICATIONS ON LT. LOWER FIXED LEADING EDGE SKIN (MARKED). COMPLIED WITH ER/A 610352-14AD REV OR
- [SDR DALA2023071205667](https://openairdocs.org/sdr/DALA2023071205667), Jul 12, 2023: UNKNOWN. UNKNOWN. FOUND ONE CRACK INDICATION ON RH VERTICAL STAB WHILE PERFORMING AA5530-01048 AND AD 2018-10-08 (MARKED). ONE CRACK INDICATION RH VERTICAL STAB IN SPAR AND WHILE
- [SDR DALA2023071205666](https://openairdocs.org/sdr/DALA2023071205666), Jul 12, 2023: UNKNOWN. UNKNOWN. R/H VERTICAL STAB, WHILE ACCOMPLISHING INSPECTION PER WORK CARD 5530-0148-02 FAA AD 2018, FOUND A CRACK INDICATION TO ONE HOLE OF THE FRONT SPAR CAP. COMPLIED W
- [SDR DALA2023071305676](https://openairdocs.org/sdr/DALA2023071305676), Jul 11, 2023: UNKNOWN. UNKNOWN. FOUR CRACK INDICATIONS ON LH VERTICAL STAB WHILE PERFORMING AA5530- 01048 AND AD 2018-10-08 (MARKED). REINSPECTED AREA FOUND 3 CRACK INDICATIONS IN LOWER SPAR C
- [SDR DALA2022092106229](https://openairdocs.org/sdr/DALA2022092106229), Sep 20, 2022: NONE. NONE. THE J HOOK FOR THE GIRT BAR TO SLIDE WAS DISCONNCTED AT DOOR 1R. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR 
- [SDR DALA2022020800814](https://openairdocs.org/sdr/DALA2022020800814), Feb 5, 2022: NONE. NONE. CORROSION ON AFT CARGO DOOR JAMB LOWER AREA (CCT). SUMMARY OF NRC #00013: AFT CARGO DOOR JAMB LOWER AREA WAS REPAIRED PER B717 SRM 53-20-15-2R, REPAIR 7. (LP #2
- [SDR DALA2022020800813](https://openairdocs.org/sdr/DALA2022020800813), Feb 5, 2022: NONE. NONE. NICK ON FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 (CCD). SUMMARY OF NRC 00017: FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 WAS REPAIRED PER B717 SRM 5
- [SDR DALA2022020800811](https://openairdocs.org/sdr/DALA2022020800811), Feb 4, 2022: NONE. NONE. THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN OUT OF LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIA
- [SDR DALA2021122308001](https://openairdocs.org/sdr/DALA2021122308001), Dec 22, 2021: NONE. NONE. SHIP 9563 -DIV/INFLT SHUTDN- TO MSY DUE TO RIGHT ENGINE FIRE WARNING. CREW PULLED FIRE HANDLE AND DISCHARGED BOTH BOTTLES. CORRECTIVE ACTION: MAINTENANCE REPLAC
- [SDR DALA2021080904512](https://openairdocs.org/sdr/DALA2021080904512), Aug 7, 2021: BATTERY PACK. DISCHARGED. MAINTENANCE FOUND THAT THE B5235 EMERGENCY BATTERY PACK WAS DEAD. THE B5235 EMERGENCY BATTERY PACK WAS REPLACED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. 
- [SDR DALA2021062503447](https://openairdocs.org/sdr/DALA2021062503447), Jun 25, 2021: BATTERY PACK. NO TEST. THE OVERWING EMERGENCY EVACUATION LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK B5-125 PER B717 AMM 33-51. 
- [SDR DALA2020112303835](https://openairdocs.org/sdr/DALA2020112303835), Nov 22, 2020: BATTERY PACK. INOPERATIVE. THE LOWER EXIT SIGNS AT DOORS 1L AND 1R NOT WORKING. MAINTENANCE FOUND THE BATTERY 35-118 TO BE INOPERATIVE. THE BATTERY WAS REPLACED, PER B717 AMM 33-51-03. OP
- [SDR DALA2019062903951](https://openairdocs.org/sdr/DALA2019062903951), Jun 29, 2019: SKIN. NICKED. NICKS AT LT WING LOWER SKIN, LOWER SURFACE AROUND FUEL ACCESS PLATES, #520EB, 520LB, AND 520MB. NRC 00603: NICKS AROUND FUEL ACCESS PLATES #520EB AND 520LB WERE
- [SDR DALA2019070304029](https://openairdocs.org/sdr/DALA2019070304029), Jun 28, 2019: SKIN. DENTED. INITIAL INSPECTION, DENT ON AILERON CONTROL TAB UPPER FACE AT RT WING. AILERON CONTROL TAB RT P/N 5910047-410 S/N 518 WAS REMOVED PER AMM 27-10-02 AILERON CONTR
- [SDR DALA2019062903950](https://openairdocs.org/sdr/DALA2019062903950), Jun 28, 2019: PIN. MISSING. DURING INSTALLATION OF TAILCONE SLIDE, PIN P/N MS20392-2C9 WAS NOT FOUND IN REFERENCE TO 5352-4002 STEP 6 ( CPAX). NRC 0721: NEW PIN FOR THE TAILCONE SLIDE WAS 
- [SDR DALA2019062903939](https://openairdocs.org/sdr/DALA2019062903939), Jun 28, 2019: SKIN. NICKED. NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING (AD). NRC 00236: NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING WERE REPAIRED PER SRM 57-53-01-
- [SDR DALA2019062803912](https://openairdocs.org/sdr/DALA2019062803912), Jun 27, 2019: FRAME. CORRODED. EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AF
- [SDR DALA2019062703886](https://openairdocs.org/sdr/DALA2019062703886), Jun 26, 2019: STIFFENER. CORRODED. CORROSION ON STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00322: CORROSION LEVEL 2, STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT 
- [SDR DALA2019062703884](https://openairdocs.org/sdr/DALA2019062703884), Jun 26, 2019: FRAME. CORRODED. EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT 
- [SDR DALA2019062703883](https://openairdocs.org/sdr/DALA2019062703883), Jun 26, 2019: FRAME. CORRODED. CORROSION ON FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT AFT CARGO COMPARTMENT. NRC 00267: CORROSION LEVEL 2, FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT 
- [SDR DALA2019062703877](https://openairdocs.org/sdr/DALA2019062703877), Jun 26, 2019: INTERCOSTAL. CORRODED. EXFOLATION ON INTERCOSTAL STA Y=1037 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00315: CORROSION LEVEL 2, INTERCOSTAL WAS REPLACED PER B717-200 SRM 53-20-51-0I 7
- [SDR DALA2019062703876](https://openairdocs.org/sdr/DALA2019062703876), Jun 26, 2019: RETAINER. CRACKED. CRACK AT AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS FOUND (CPIL). NRC 00654: AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS REPAIRED PER B717-200 SRM 56-10-
- [SDR DALA2019062603864](https://openairdocs.org/sdr/DALA2019062603864), Jun 25, 2019: LONGERON. CORRODED. LONGERON 30 CORROED BS 1022. THE LONGERON WAS REPLACED IAW SRM 53-20-05 PROCEDURE 3 ITEM 9, 51- 41-02-OG, AND 51-41-05-OG.
- [SDR DALA2019062603860](https://openairdocs.org/sdr/DALA2019062603860), Jun 25, 2019: LONGERON. CORRODED. CORROSION BTW LONGERON 25L, BS 1002 - 1037 AT CARGO COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2 AND SRM 51-40-08-0G.
- [SDR DALA2019062603859](https://openairdocs.org/sdr/DALA2019062603859), Jun 25, 2019: SKIN. CRACKED. CRACK AT FUSELAGE SKIN BS 1076 BETWEEN LONGERON 13 & 14R. THE SKIN WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.
- [SDR DALA2019062603858](https://openairdocs.org/sdr/DALA2019062603858), Jun 25, 2019: SKIN. DAMAGED. DAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPA

All 206: https://openairdocs.org/aircraft/N936AT/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/N936AT/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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