# N964AT: 2001 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: 55025
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2001
- Certificate issued: February 27, 2024
- Expires: February 28, 2031
- Mode S code: AD6B14
- 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=964AT
- Page: https://openairdocs.org/aircraft/N964AT

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/N964AT/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 N964AT.

## 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 20060725016289I](https://openairdocs.org/incident/20060725016289I), Jul 25, 2006: Boeing 717200 (N964AT), Boston, MA, Minor damage. (-23) Airtran airways inc., N964AT, nose #723, s/n 55025, B-717-200, struck a baggage cart during pushback from terminal c, gate 1E at Boston, MA, at…

## Service difficulty reports (264, 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 DALA2026031001645](https://openairdocs.org/sdr/DALA2026031001645), Mar 8, 2026: NOT REPORTED. NOT REPORTED. SHIP 9523 ERA 632996-14 ISSUED FOR REPAIR TO STA 207-218,L L17-18RH. CORRECTIVE ACTION: REPAIRED PER ERA 632996-14. (1485115)
- [SDR DALA2026031001641](https://openairdocs.org/sdr/DALA2026031001641), Mar 6, 2026: SKIN. CRACKED. SHIP 9523 CRACKS (2EAS) ON UPPER EXTERNAL FUSELAGE SKIN APPROX Y=1087 BTW LONG 13R-14R. CORRECTIVE ACTION: REPAIRED PER ER/A 632448-14 (1482120)
- [SDR DALA2026031001640](https://openairdocs.org/sdr/DALA2026031001640), Mar 6, 2026: FRAME. CRACKED. SHIP 9523 CRACKED FRAME AND FRAME CLIP BTW STA 1152 BTW L=1/2R AT AFT ACCESORY COMPARMENT. CORRECTIVE ACTION: PERMANENT REPAIR AND PER PRI 632524-14 REV 1. (148
- [SDR DALA2026031001646](https://openairdocs.org/sdr/DALA2026031001646), Mar 5, 2026: SKIN. DAMAGED. SHIP 9523 ERA 632448-14 ISSUED FOR REPAIRS TO STA 1087 AND 1076 L13R TO L1 4R FUSELAGE SKIN. CORRECTIVE ACTION: ASSOCIATED ER/A 00-632448 (1480632)
- [SDR DALA2026030501526](https://openairdocs.org/sdr/DALA2026030501526), Mar 3, 2026: HINGE FITTING. CORRODED. CORROSION ON LOWER OTBD ATTACH POINT STUD AND MIDDLE FLAP HINGE FITTING STA Y XRS 267 APPROX AT RT WING. REPLACED PER SERVICEABLE CENTER WING FLAP HINGE FITTING
- [SDR DALA2026030201424](https://openairdocs.org/sdr/DALA2026030201424), Feb 28, 2026: SKIN. CRACKED. CRACKS (2 EA) ON INTERNAL SKIN OF INBRD BUTE DOOR (OUTBOARD EDGE) AT RH WING. CORRECTIVE ACTION: REPAIR ASSOCIATED ER/A 14-618696 (1472759)
- [SDR DALA2026022501337](https://openairdocs.org/sdr/DALA2026022501337), Feb 21, 2026: BULKHEAD. NICKED. NICK ON FWD BULKHEAD BTW STA Y=37 AND X=10 AT NOSE GEAR WHEEL WELL. DAMAGED AREA REPAIRED PER B717-200 SRM 51-00-00 (1460835)
- [SDR DALA2025072005441](https://openairdocs.org/sdr/DALA2025072005441), Jul 19, 2025: TRANSCEIVER. FAULTED. SHIP 9523-ATO- ABORTED TAKE-OFF DUE TO RECEIVING A STICK PUSHER FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH RADIO ALTIMETER TRANSCEIVERS AND PERF
- [SDR DALA2024123112106](https://openairdocs.org/sdr/DALA2024123112106), Dec 10, 2024: NONE. NONE. -AD- OVERWEIGHT LANDING. LW - 110.1. MAX 110.0. VERTICAL SPEED AT TOUCHDOWN ~ 50 FT/MN. WT EXITING RUNWAY INDICATED 109.8. PERFORMED B717 AMM 05-51-04 210-801 A
- [SDR DALA2024032803863](https://openairdocs.org/sdr/DALA2024032803863), Mar 27, 2024: WARNING MESSAGE. FALSE INDICATION. SHIP 9523 -MISC/DE- ON CLIMB OUT, AT APPROXIMATELY 5,000 FEET, THE "PSEU FAIL" MESSAGE ILLUMINATED. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED WIT
- [SDR DALA2024020601578](https://openairdocs.org/sdr/DALA2024020601578), Feb 5, 2024: SPAR. CRACKED. CRACK ON REAR SPAR LOWER SECTION LH WING AT XRS=214.000. SUMMARY OF NRC 00651: REAR SPAR LOWER SECTION LH WING AT XRS=214.000 WAS REPAIRED PER ERA 615443-14AD R
- [SDR DALA2024020601573](https://openairdocs.org/sdr/DALA2024020601573), Feb 3, 2024: PAN. CRACKED. CRACKED PAN AND FITTING ON BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00156: FITTING REPLACED PER B717-200 SRM 51-41-03-0G, 51-41-01-0G, AN
- [SDR DALA2024020301511](https://openairdocs.org/sdr/DALA2024020301511), Feb 2, 2024: PAN. CRACKED. CRACKED PAN AND FITTING ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00154: FITTING WAS FABRICATED PER DWG 3914025 REV C AND PAN ON BEAM #
- [SDR DALA2024020101447](https://openairdocs.org/sdr/DALA2024020101447), Feb 1, 2024: FRAME. CRACKED. CRACK ON FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00146: FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMP
- [SDR DALA2024020101446](https://openairdocs.org/sdr/DALA2024020101446), Feb 1, 2024: ANGLE. CORRODED. CORROSION WAS FOUND ON LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN. SUMMARY OF NRC 00571: CORROSION LEVEL 2. LH UPPER
- [SDR DALA2024020301505](https://openairdocs.org/sdr/DALA2024020301505), Jan 31, 2024: WEB. CRACKED. CRACKS ON INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR. SUMMARY OF NRC 00255: INTERNAL STRUCTURE (WEB) BTW STA Y=1053, 
- [SDR DALA2024013101412](https://openairdocs.org/sdr/DALA2024013101412), Jan 31, 2024: ANGLE. CORRODED. CORROSION ON FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTME
- [SDR DALA2024013001358](https://openairdocs.org/sdr/DALA2024013001358), Jan 29, 2024: CARGO TRACK. CORRODED. CORROSION ON FLOOR TRACK LH STA Y=889, AFT CARGO WAS REMOVED AND REMAINDER TRACK IS OUT OF LIMITS. SUMMARY OF NRC 00648: CORROSION LEVEL 2. FLOOR TRACK LH STA Y
- [SDR DALA2024013001356](https://openairdocs.org/sdr/DALA2024013001356), Jan 29, 2024: PAN. CRACKED. CRACK ON INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR. SUMMARY OF NRC 00239: INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD
- [SDR DALA2024012901231](https://openairdocs.org/sdr/DALA2024012901231), Jan 28, 2024: LONGERON SPLICE. CORRODED. CORROSION ON LONGERON SPLICE 24L BTW STA Y=889 AND STA Y=908 IN REFERENCE TO NRC 00644. SUMMARY OF NRC 00650: CORROSION LEVEL 2. SPLICE ON LONGERON 24L BTW STA 
- [SDR DALA2024012901227](https://openairdocs.org/sdr/DALA2024012901227), Jan 27, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB. SUMMARY OF NRC 00361: CORROSION LEVEL 2. LH CUSP WEB UPPER AND LOW
- [SDR DALA2024012901226](https://openairdocs.org/sdr/DALA2024012901226), Jan 27, 2024: WEB. CORRODED. CORROSION ON WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB (UPPER SURFACE) B
- [SDR DALA2024012901225](https://openairdocs.org/sdr/DALA2024012901225), Jan 27, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT (1 EA) (UPPER/ LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00408: CORROSION LEVEL 2. FLOOR 
- [SDR DALA2024012901224](https://openairdocs.org/sdr/DALA2024012901224), Jan 27, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 407: CORROSION L
- [SDR DALA2024012901223](https://openairdocs.org/sdr/DALA2024012901223), Jan 27, 2024: STRINGER SPLICE. CORRODED. CORROSION ON PREVIOUS REPAIR SPLICE AT STA Y=908 BTW LONG 26L AND LONG 27L IN AFT CARGO COMPARTMENT. SUMMARY OF NRC 00647: CORORSION LEVEL 2. SPLICE OF STA Y=90
- [SDR DALA2024012901222](https://openairdocs.org/sdr/DALA2024012901222), Jan 27, 2024: DOUBLER. CORRODED. CORROSION ON PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN. SUMMARY OF NRC 00395: CORROSION LEVEL 2. PREVIOUS REPAIR 
- [SDR DALA2024012901221](https://openairdocs.org/sdr/DALA2024012901221), Jan 27, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00413: CORROSION LEVEL 2. FLOOR S
- [SDR DALA2024012901220](https://openairdocs.org/sdr/DALA2024012901220), Jan 26, 2024: ANGLE. CORRODED. CORROSION WAS FOUND ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH, PAX CABIN. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CUSP ANGLE ON LH/LOWER CUSP ANGLE BTW 
- [SDR DALA2024013101411](https://openairdocs.org/sdr/DALA2024013101411), Jan 25, 2024: SKIN. DAMAGED. FASTENER HOLES AND COUNTERSINKS ARE ELONGATED OUT OF LIMITS ON 1/4 FASTENERS ROW AT VERT STAB FIX LE. ALSO, ON VERT STAB REMOVABLE LE STA ZFS=52.267 REF SERVICE
- [SDR DALA2024012401101](https://openairdocs.org/sdr/DALA2024012401101), Jan 24, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK X=-44.5 BTW STA 200-219 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00403: SEAT TRACK SECTION X=-44.5 BTW STA 200-246 AT PAX CABIN FLOO
- [SDR DALA2024012401100](https://openairdocs.org/sdr/DALA2024012401100), Jan 24, 2024: SKIN. DAMAGED. CREASES WERE FOUND ON REPAIR SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH PER B717 SRM 53-00-01-02 REPAIR 6 PAR. 7. SUMMARY OF NRC 00270: SKIN SECTION
- [SDR DALA2024012301009](https://openairdocs.org/sdr/DALA2024012301009), Jan 23, 2024: SKIN. GOUGED. GOUGE AND DENT ON FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L. SUMMARY OF NRC 00615: FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L WAS PERMANENT REPAIRED PER B717-200
- [SDR DALA2024012301008](https://openairdocs.org/sdr/DALA2024012301008), Jan 20, 2024: WEB. CRACKED. WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION. SUMMARY OF NRC 00599: WEB FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION WAS REPAIRED PER ER
- [SDR DALA2024012301007](https://openairdocs.org/sdr/DALA2024012301007), Jan 20, 2024: WEB. CRACKED. WEB CRACKED FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION. SUMMARY OF NRC 00598: WEB FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION WAS REPAIRED PER 
- [SDR DALA2024012200905](https://openairdocs.org/sdr/DALA2024012200905), Jan 20, 2024: WEB. PUNCTURED. PUNCTURES (2 EA) ON WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00415: WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX
- [SDR DALA2024012200902](https://openairdocs.org/sdr/DALA2024012200902), Jan 19, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUP
- [SDR DALA2024011900810](https://openairdocs.org/sdr/DALA2024011900810), Jan 19, 2024: CUSP WEB. CRACKED. CRACK ON RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00397: RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PA
- [SDR DALA2024011900805](https://openairdocs.org/sdr/DALA2024011900805), Jan 18, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORTS AT W1 AREA STA 200 BTW X=7 AND X=-44 IN REF TO NRC 00401. SUMMARY OF NRC 00539: CORROSION LEVEL 2. FLOOR SUPPORTS WERE REPLACED PER 
- [SDR DALA2024011500577](https://openairdocs.org/sdr/DALA2024011500577), Jan 14, 2024: UNKNOWN. UNKNOWN. CRACK ON LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB. SUMMARY: LH CUSP WEB LOWER BTW STA Y=294 TO Y=313 FROM X=45 AT PAX CAB WAS REPAIRED PER 
- [SDR DALA2024011500576](https://openairdocs.org/sdr/DALA2024011500576), Jan 14, 2024: UNKNOWN. UNKNOWN. CRACK OF 0.125 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00205: OVERWING FRAME AT STA Y=6
- [SDR DALA2024010900327](https://openairdocs.org/sdr/DALA2024010900327), Jan 8, 2024: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT CPAX. SUMMARYOF NRC 00600: CORROSION LEVEL II. FLOOR SUPPORT BTW STA Y=1022 TO Y=1053 X=44 AT 
- [SDR DALA2024010900326](https://openairdocs.org/sdr/DALA2024010900326), Jan 8, 2024: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1037 LONG 17 RH AT PAX CABIN. SUMMARY OF NRC 00289: FRAME STA 1037 LONG 17 RH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDUR
- [SDR DALA2024010900325](https://openairdocs.org/sdr/DALA2024010900325), Jan 7, 2024: UNKNOWN. UNKNOWN. CRACK ON RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00445: RH CUSP MEMBRANE ON STA Y=716 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717-
- [SDR DALA2024010900324](https://openairdocs.org/sdr/DALA2024010900324), Jan 7, 2024: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SKIN LOWER SURFACE BTW STA 389 AND X=-58 AT FWD CARGO DOOR JAMB AREA. SUMMARY OF NRC 00203: CORROSION LEVEL 2. FLOOR SKIN LOWER SURFACE BTW S
- [SDR DALA2024010800319](https://openairdocs.org/sdr/DALA2024010800319), Jan 4, 2024: UNKNOWN. UNKNOWN. CRACK ON RH CUSP MEMBRANE ON STA Y=813 AND X =-44 AT PAX CABIN. SUMMARY OF NRC 00446: RH CUSP MEMBRANE ON STA Y=813 AND X=-44 AT PAX CABIN WAS REPAIRED PER B717
- [SDR DALA2024010210753](https://openairdocs.org/sdr/DALA2024010210753), Dec 30, 2023: UNKNOWN. UNKNOWN. TOOL MARK ON CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PAX CABIN. SUMMARY OF NRC 00448: CUSP MEMBRANE (INTERNAL SIDE) ON STA Y=916 AND X=-56 AT PA
- [SDR DALA2023122410541](https://openairdocs.org/sdr/DALA2023122410541), Dec 22, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOOR. SUMMARY OF NRC 00136: INTERNAL STRUCTURE APROX BTW STA 370 AND L-19R AT FWD CARGO DOO
- [SDR DALA2023092107773](https://openairdocs.org/sdr/DALA2023092107773), Sep 21, 2023: UNKNOWN. UNKNOWN. SHIP 9523 -HYD/DE- THE CREW RECEIVED A "HYD R QTY LOW" MESSAGE AT TOP OF CLIMB. THEY WERE UNABLE TO REPRESSURIZE THE SYSTEM. THE QRH WAS COMPLIED WITH AND PERFO
- [SDR DALA2022121308025](https://openairdocs.org/sdr/DALA2022121308025), Dec 9, 2022: POWER SUPPLY. INOPERATIVE. THE EXTERIOR EMERGENCY LIGHTS IN THE AFT FUSELAGE WILL NOT EXTINGUISH. MAINTENANCE REPLACED THE AFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK WAS
- [SDR DALA2022100406443](https://openairdocs.org/sdr/DALA2022100406443), Oct 1, 2022: NONE. NONE. THE LOWER AFT OVERWING EXIT DOOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW GOOD. (LP #895406

All 264: https://openairdocs.org/aircraft/N964AT/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/N964AT/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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