# N966AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55027
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 7, 2001
- Certificate issued: February 5, 2024
- Expires: February 28, 2031
- Mode S code: AD7282
- Registered owners: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Dept 595 Aircraft Registrations](https://openairdocs.org/faa-owner/DEPT%20595%20AIRCRAFT%20REGISTRATIONS)
- 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=966AT
- Page: https://openairdocs.org/aircraft/N966AT

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (Rolls-Royce BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N966AT/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 N966AT.

## FAA accident and incident reports

None matched to N966AT.

## Service difficulty reports (197, 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 DALA2026092905408](https://openairdocs.org/sdr/DALA2026092905408), Sep 26, 2026: DOUBLER. INSTALLED. FUSELAGE CROWN Y503 - Y522, L-1 - L-3R EXISTING DOUBLER NEAR STC INSTALL AREA. REPAIRED PER ER/A 637037-14. (1833976) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026081904728](https://openairdocs.org/sdr/DALA2026081904728), Aug 13, 2026: TRANSMITTER. FAULTED. CORROSION UNDER THE NR 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30, CORRECTIVE ACTION: COMPLIED WITH ER/A 631535-14. (1753411) (AIRCRAFT GRO
- [SDR DALA2026012200497](https://openairdocs.org/sdr/DALA2026012200497), Jan 17, 2026: UPLOCK SENSOR. FAULTED. PERFORMED GO AROUND DUE TO RIGHT MLG UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. INDICATION RETURNED TO NORMAL AIRCRAFT LANDED SAFELY. CORRECTIVE ACTION: 
- [SDR DALA2026011600381](https://openairdocs.org/sdr/DALA2026011600381), Jan 11, 2026: SKIN. NOT REPORTED. AIRCRAFT IS NOT TO BE RELEASE TO SERVICE UNTIL ERA 631535-14 HAS BEEN REVISED TO REFLECT FAA APPROVAL. REPAIRED PER ERA 631535-14. (1397287)
- [SDR DALA2026011600380](https://openairdocs.org/sdr/DALA2026011600380), Jan 11, 2026: SKIN. CORRODED. CORROSION UNDER NR 2 RECEIVE RADIO ALTIMETER ANTENNA. COMPLIED WITH ERA 631535-14 REV ORIG FUSELAGE SKIN REPAIR. (1397282)
- [SDR DALA2026011600373](https://openairdocs.org/sdr/DALA2026011600373), Jan 11, 2026: SKIN. CORRODED. ENGINEERING 12-MONTH DTE LOG PAGE FOR CORROSION UNDER# 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30 PER ER/A 631535-14 REV A. REPAIRED PER ER
- [SDR DALA2026010900240](https://openairdocs.org/sdr/DALA2026010900240), Jan 3, 2026: SEAT TRACK. CORRODED. FOUND CORROSION ON RT INB SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52 (1383323)
- [SDR DALA2026010500071](https://openairdocs.org/sdr/DALA2026010500071), Jan 1, 2026: SEAT TRACK. CORRODED. FOUND CORROSION ON RH OTBD SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52. (1380043)
- [SDR DALA2026010509566](https://openairdocs.org/sdr/DALA2026010509566), Dec 29, 2025: WEB. CORRODED. AFTER REMOVAL OF INBOARD RT SEAT TRACK, SUB FLOOR SKIN IS CORRODED. REPAIRED SUB FLOOR MEMBRANE IAW SRM 53-00-55 (1375171)
- [SDR DALA2024121611740](https://openairdocs.org/sdr/DALA2024121611740), Dec 15, 2024: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS POWERED BY BATTERIES B5-235 AND B5-118 ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS B5-235 AND B5-118 PER B717 AMM 33-51. 
- [SDR DALA2024012901232](https://openairdocs.org/sdr/DALA2024012901232), Jan 27, 2024: BATTERY PACK. INOPERATIVE. FOUND THE FORWARD ENTRANCE EXIT PATHWAY SIGN GOING INTO COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. LIGHT OPERATION NOW CHECKS GOOD IAW B7
- [SDR DALA2023101608456](https://openairdocs.org/sdr/DALA2023101608456), Oct 14, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS DON'T OPERATE CORRECTLY DURING SERVICE CHECKS. SUMMARY OF NRC 00700: DURING CONTINUITY AND VOLTAGE CHECK TERMINAL 10, 11, AND 12 ON S3-559 
- [SDR DALA2023101608482](https://openairdocs.org/sdr/DALA2023101608482), Oct 13, 2023: UNKNOWN. UNKNOWN. IMPROPERLY INSTALLED TAIL-CONE KEVLAR LANYARD (CAT). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703
- [SDR DALA2023101408442](https://openairdocs.org/sdr/DALA2023101408442), Oct 12, 2023: UNKNOWN. UNKNOWN. ELONGATED HOLES (2 EA) ON FAIRING PANEL 360AT. SUMMARY OF NRC 00511: ANGLE WAS FABRICATED AND REPLACED PER DWG 5912175 REV BR AND B717-200 SRM 51-41-02-0G AND F
- [SDR DALA2023100608221](https://openairdocs.org/sdr/DALA2023100608221), Oct 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA. SUMMARY OF NRC 00163: CORROSION LEVEL 2. CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W
- [SDR DALA2023100408160](https://openairdocs.org/sdr/DALA2023100408160), Oct 4, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00649: FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B7
- [SDR DALA2023100408156](https://openairdocs.org/sdr/DALA2023100408156), Oct 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO. SUMMARY OF NRC 00366: CORROSION LEVEL 2. SPLICE BTW STA 617 TO 636 FROM L-30
- [SDR DALA2023100408159](https://openairdocs.org/sdr/DALA2023100408159), Oct 3, 2023: UNKNOWN. UNKNOWN. CRACK ON BRACKET AND SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR. SUMMARY OF NRC 00099: SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPAIRED PER B717-20
- [SDR DALA2023100408155](https://openairdocs.org/sdr/DALA2023100408155), Oct 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT. (CCT) SUMMARY OF NRC 00622: CORROSION LEVEL 2. STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT
- [SDR DALA2023100408152](https://openairdocs.org/sdr/DALA2023100408152), Oct 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00336: CORROSION LEVEL 2. SPLICE OF LONGERON B
- [SDR DALA2023100308096](https://openairdocs.org/sdr/DALA2023100308096), Oct 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00230: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AF
- [SDR DALA2023100308095](https://openairdocs.org/sdr/DALA2023100308095), Oct 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00203: CORROSION LEVEL 2. INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CA
- [SDR DALA2023100308093](https://openairdocs.org/sdr/DALA2023100308093), Oct 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00197: CORROSION LEVEL 2. FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT 
- [SDR DALA2023100308089](https://openairdocs.org/sdr/DALA2023100308089), Sep 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00349: CORROSION LEVEL 2. FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AF
- [SDR DALA2023100308088](https://openairdocs.org/sdr/DALA2023100308088), Sep 30, 2023: UNKNOWN. UNKNOWN. CORROSION EXCESSIVE ON STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00643: CORROSION LEVEL 2. STRAP L-
- [SDR DALA2023100308085](https://openairdocs.org/sdr/DALA2023100308085), Sep 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR FITTING STA 200 TO 218 RBL=11 WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C, ORIGINAL THICKNESS IS 0.975IN AND MINIMUM REMAINING THICKNESS IS
- [SDR DALA2023100308083](https://openairdocs.org/sdr/DALA2023100308083), Sep 29, 2023: UNKNOWN. UNKNOWN. FITING AT STA 620 TO STA 636 L-30 HAD CORROSION FOUND ON SAME FITTING. CORROSION LEVEL 2. FITTING AT STA 620 TO STA 636 L-30 WAS FABRICATED PER DWG 5971577 REV 
- [SDR DALA2023092908006](https://openairdocs.org/sdr/DALA2023092908006), Sep 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 0345: CORROSION LEVEL 2. FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT
- [SDR DALA2023092908005](https://openairdocs.org/sdr/DALA2023092908005), Sep 29, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1
- [SDR DALA2023092908004](https://openairdocs.org/sdr/DALA2023092908004), Sep 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL STA Y=916 OVER STRG 28R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00328: CORROSION LEVEL 2. INTERCOSTAL ON STA Y=908 TO Y=927 STGR 28 RH 
- [SDR DALA2023092807971](https://openairdocs.org/sdr/DALA2023092807971), Sep 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00139: CORROSION LEVEL 2. WEB BTW STA 940 TO 950 AND L25R TO L26
- [SDR DALA2023092707953](https://openairdocs.org/sdr/DALA2023092707953), Sep 26, 2023: UNKNOWN. UNKNOWN. CRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00603: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2988
- [SDR DALA2023092707952](https://openairdocs.org/sdr/DALA2023092707952), Sep 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR WEB DOUBLER BTW STA=641 TO 646 X=-58. CORROSION ON WEB DOUBLER BTW STA=476 TO STA=498 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00542: CORRO
- [SDR DALA2023092507867](https://openairdocs.org/sdr/DALA2023092507867), Sep 24, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON CUSP WEB RBL=57 AND STA 266, 331, 926, 935, AND 944. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND REMAINING THICKNESS OF 0.007 INCH
- [SDR DALA2023092507860](https://openairdocs.org/sdr/DALA2023092507860), Sep 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y=680 X=-50, AT CABIN PAX. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB BTW STA 655 TO STA 684 X=-50 AT CABIN PAX WAS REPAIRED PE
- [SDR DALA2023092507859](https://openairdocs.org/sdr/DALA2023092507859), Sep 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO 
- [SDR DALA2023092507857](https://openairdocs.org/sdr/DALA2023092507857), Sep 22, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00093: WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PE
- [SDR DALA2023092507855](https://openairdocs.org/sdr/DALA2023092507855), Sep 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA FROM Y=860 TO Y=870 X=- 58, AT CABIN PAX. SUMMARY OF NRC 00621: CORROSION LEVEL 2. CUSP WEB STA FROM Y=860 TO Y=870 X=- 58 WAS REPAIRE
- [SDR DALA2023092207783](https://openairdocs.org/sdr/DALA2023092207783), Sep 21, 2023: UNKNOWN. UNKNOWN. AFTER INNER SKIN REMOVAL, A CRACK WAS FOUND ON BEAM #1 AFT SECTION OF L1 DOOR. SUMMARY OF NRC 00647: BEAM #1 AFT SECTION OF L1 DOOR WAS REPAIRED PER B717-200 SR
- [SDR DALA2023092007728](https://openairdocs.org/sdr/DALA2023092007728), Sep 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y=256 X=-58. SUMMARY OF NRC 00618: CORROSION LEVEL 2. CUSP WEB STA 256 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 220
- [SDR DALA2023092107767](https://openairdocs.org/sdr/DALA2023092107767), Sep 19, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON CABIN FLOOR CUSP WEB STA=377, STA=390, STA=417, AND STA=636 BTW -X=46 TO -X=59 RH SIDE AT PAX CABIN. ORIGINAL THICKNESS IS 0.020IN RE
- [SDR DALA2023092007724](https://openairdocs.org/sdr/DALA2023092007724), Sep 19, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON CUSP WEB X=+57 STA 444, 517, 523, 544 TO 557, 608, 646 TO 660, AND 804 AT CPAX. WITH AN ORIGINAL THICKNESS=0.020 INCHES AND REMAINING
- [SDR DALA2023091907686](https://openairdocs.org/sdr/DALA2023091907686), Sep 19, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL. SUMMARY OF NRC 00381: FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL WAS REPAIRED PER B717 SR
- [SDR DALA2023091907683](https://openairdocs.org/sdr/DALA2023091907683), Sep 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX. SUMMARY OF NRC 00301: CORROSION LEVEL 2. FLOOR STRUCTUTRE (2 EA) BTW STA 
- [SDR DALA2023091907682](https://openairdocs.org/sdr/DALA2023091907682), Sep 18, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00388: FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SR
- [SDR DALA2023091907681](https://openairdocs.org/sdr/DALA2023091907681), Sep 18, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND AT FLOOR SUPPORT ON STA 200.0 LBL 12. SUMMARY OF NRC 00634: CORROSION LEVEL 2. FLOOR SUPPORT ON STA 200.0 LBL 12 WAS REPLACED PER B717 SRM 5
- [SDR DALA2023091907680](https://openairdocs.org/sdr/DALA2023091907680), Sep 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB. SUMMARY OF NRC 00628: CORROSION LEVEL 2. CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB WERE 
- [SDR DALA2023091907679](https://openairdocs.org/sdr/DALA2023091907679), Sep 18, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA 200 AND LBL=5-10 AT FWD CPAX. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND MINIMUM REMAINING THICKNESS OF 0.013, 
- [SDR DALA2023091807631](https://openairdocs.org/sdr/DALA2023091807631), Sep 18, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00389: FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SR
- [SDR DALA2023091807630](https://openairdocs.org/sdr/DALA2023091807630), Sep 17, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS WAS FOUND ON THE CUSP WEB STA 696 AND 715 X=-58, AT CABIN PAX. SUMMARY OF NRC 00620: CORROSION LEVEL 2. CUSP WEB STA 696 AND 715 X=-58 W

All 197: https://openairdocs.org/aircraft/N966AT/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/N966AT/stcs.md

## Related

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

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