# N945AT: 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: 55008
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 19, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD1FCD
- 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=945AT
- Page: https://openairdocs.org/aircraft/N945AT

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/N945AT/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 N945AT.

## FAA accident and incident reports

None matched to N945AT.

## Service difficulty reports (228, 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 DALA2026071704217](https://openairdocs.org/sdr/DALA2026071704217), Jul 16, 2026: COALESCER BAG. ODOR. PUNGENT ODOR THROUGHOUT THE ENTIRE AIRPLANE, R & R COALESCER BAGS IAW AMM 21-54. (1703467) (AIRCRAFT GROUNDED).
- [SDR DALA2026061603616](https://openairdocs.org/sdr/DALA2026061603616), Jun 15, 2026: IDG. MALFUNCTIONED. SHIP 9505-ATO- RIGHT GENERATOR OFF MESSAGE AT THROTTLE UP. REPLACED THE RIGHT IDG. ALL RTS NORMAL. (LP 8906976 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026042102514](https://openairdocs.org/sdr/DALA2026042102514), Apr 15, 2026: GIRT BAR. UNSECURE. R1 DOOR GIRT BAR CONNECTOR IS DETACHED FROM SLIDE. RESECURED RELEASE LATCH FOR SLIDE AMM 25-61 (8554330) (AIRCRAFT GROUNDED).
- [SDR DALA2026040102118](https://openairdocs.org/sdr/DALA2026040102118), Mar 24, 2026: TIRE. FAILED. RETURNED TO ATL DUE TO NR 1 MLG TIRE FAILURE, RT SYS HYDRAULIC LOSS AND SUBSEQUENT LT ENGINE DAMAGE ON TAKEOFF. REPLACED #1 ENGINE AND REPAIRED DAMAGE.(8616524)
- [SDR DALA2026032401969](https://openairdocs.org/sdr/DALA2026032401969), Mar 18, 2026: TIRE. FAILED. ATB/TIRE- RETURNED TO ATL DUE TO #1 MLG TIRE FAILURE, RT SYS HYDRAULIC LOSS AND SUBSEQUENT LT ENGINE DAMAGE ON TAKEOFF. CORRECTIVE ACTION: REPLACED #1 ENGINE.
- [SDR DALA2026012200498](https://openairdocs.org/sdr/DALA2026012200498), Jan 20, 2026: TEE FITTING. DETACHED. DOOR ARMING MECHANISIM ON FOWARD SERVICE DOOR INOP. FOUND TEE CLIP ON THE SLIDE LANYARD OFF. REATTACHED SAME PER B717 AMM 25-61. A/C OK FOR SVC. (7904618)
- [SDR DALA2026010500067](https://openairdocs.org/sdr/DALA2026010500067), Dec 31, 2025: CABLE. MISINSTALLED. GALLEY SERVICE DOOR R1 DOOR GIRT BAR CABLE MAY BE IMPROPERLY INSTALLED. REPOSITIONED CABLE REF AMM 25-61, OK TO CONTINUE (8385642)
- [SDR DALA2025111108260](https://openairdocs.org/sdr/DALA2025111108260), Nov 8, 2025: SKIN. PUNCTURED. PUNCTURE ON LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136. LT ELEVATOR LOWER SURFACE BTW STA XHS 108 TO XHS 136 WAS REPAIRED PER SRM 51-70-13 (1293791)
- [SDR DALA2025103107964](https://openairdocs.org/sdr/DALA2025103107964), Oct 29, 2025: LONGERON. CRACKED. CRACKED LONGERON 2R AT BS 1133. LONGERON 2R REPAIRED IAW SRM 53-00-05. (1277454)
- [SDR DALA2025081105985](https://openairdocs.org/sdr/DALA2025081105985), Aug 8, 2025: COMPRESSOR. STALLED. SHIP 9505 GOING THRU 10,000 ON CLIMBOUT WE GOT COMPRESSOR STALL TGT HAD AN X OFF AND ON. CORECTIVE ACTION: EPLACED HARNESS PER B717 AMM 77-21. REPLACED ALL 6 TG
- [SDR DALA2025070104877](https://openairdocs.org/sdr/DALA2025070104877), Jun 29, 2025: BULKHEAD. NO DISCREPANCY. SHIP 9505 DUE TO HARD LANDING ON FL1405, PERFORM DETAILED INSP IAW ER/A 565522-14AD. CORRECTIVE ACTION: INSPECTED A/C 9505 CANTED BULKHEAD IAW ER/A 565522-14AD.
- [SDR DALA2025040802696](https://openairdocs.org/sdr/DALA2025040802696), Mar 27, 2025: LANYARD. SEVERED. FOUND R1 DOOR SLIDE RELEASE LANYARD CABLE SEVERED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.7
- [SDR DALA2024111410954](https://openairdocs.org/sdr/DALA2024111410954), Nov 5, 2024: DOUBLER. CRACKED. -AD- STA 1178.225 LONGERON 3L BULKHEAD DOUBLER CRACKED. ACCOMPLISH ER/A 565522-14AD REV A SECTION IV FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS
- [SDR DALA2024042404675](https://openairdocs.org/sdr/DALA2024042404675), Apr 24, 2024: POWER SUPPLY. INOPERATIVE. THE EMERGENCY EXIT SIGN ON ROW 19CDE IS INOPERATIVE. MAINTENANCE THE FOUND POWER SUPPLY INOPERATIVE. THE POWER SUPPLY (B5-121) WAS REPLACED PER B717 AMM 33-51. 
- [SDR DALA2023101408451](https://openairdocs.org/sdr/DALA2023101408451), Oct 13, 2023: UNKNOWN. UNKNOWN. MULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE TAIL COMPARTMENT CEILING. MAINTENANCE REPLACED THE BATTERY AND THE PSU AT THE RIGHT AFT LAVATORY CEILING. TAIL 
- [SDR DALA2023092908007](https://openairdocs.org/sdr/DALA2023092908007), Sep 28, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY CEILING LIGHTS ROW 24-27 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTER PACK AT SEAT 25 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD
- [SDR DALA2023090507189](https://openairdocs.org/sdr/DALA2023090507189), Sep 2, 2023: UNKNOWN. UNKNOWN. CRACK INDICATION AT LEFT OVERWING FRAME STA 696 WHILE PERFORMING AMDS 5310-01436-01B STEP 10. COMPLIED WITH AMDS CARD 5310-01436-03A FOR L/H OVER-WING FRAME REP
- [SDR DALA2023090507181](https://openairdocs.org/sdr/DALA2023090507181), Aug 31, 2023: UNKNOWN. UNKNOWN. L1 DOOR SLIDE FOUND LACED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REPLACED SLIDE PER B 717
- [SDR DALA2024022102372](https://openairdocs.org/sdr/DALA2024022102372), Aug 20, 2023: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED JUST I/B OF R-1 DOOR UNDER FLOOR PANEL 221EF- MARKED. SUMMARY SEE NRC 087-0025:5310-2005/009 00399: REPLACED FLOOR SUPPORT REF BOEING DWG
- [SDR DALA2023070405375](https://openairdocs.org/sdr/DALA2023070405375), Jul 3, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT LIGHT LENS COVER AT ROW 19 NEEDS TO BE REATTACHED. MAINTENANCE ATTACHED THE EMERGENCY LIGHT LENS COVER AT ROW 19CDE. THE AIRCRAFT IS OK FOR S
- [SDR DALA2023062705160](https://openairdocs.org/sdr/DALA2023062705160), Jun 26, 2023: UNKNOWN. UNKNOWN. SHIP 9505 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE RIGHT HYDRAULIC QUANTITY READING LOW. THE CREW WAS ABLE TO PRESSURIZE THE R HYD SYS
- [SDR DALA2022081005448](https://openairdocs.org/sdr/DALA2022081005448), Aug 10, 2022: SKIN. DAMAGED. B717-200-FUSELAGE SKIN DAMAGE BETWEEN STA 994 1002 AND STR 24R 26R. NRC 002-0001:0514-2001/001 00001: REPAIRED PER ER/A 601169-14 REV. ORIGINAL (PRI 601169-14 R
- [SDR DALA2022081005447](https://openairdocs.org/sdr/DALA2022081005447), Aug 10, 2022: FRAME. DAMAGED. FRAME AT STA 994 SHOWS EVIDENCE OF DAMAGE CAUSED BY BELT LOADER IMPACT. NRC 002-0001:0514-2001/013 00013: REPAIRED FRAME PER B717 SRM 51-70-11-2R-1. (LP #235878
- [SDR DALA2022081005446](https://openairdocs.org/sdr/DALA2022081005446), Aug 10, 2022: THRESHOLD. DAMAGED. THE AFT CARGO DOOR JAMB WEB JUST AFT OF STA 994 WAS DAMAGED FROM BELT LOADER IMPACT. NRC 002-0001:0514-2001/006 00006: REPAIRED WEB PER ERA 601169-14 REV ORIG. 
- [SDR DALA2022081005445](https://openairdocs.org/sdr/DALA2022081005445), Aug 7, 2022: SKIN. DAMAGED. COMPLY WITH PRI/ERA 601064-14 REPAIR OF FUSELAGE SKIN DAMAGE AFT OF AFT CARGO DOOR. COMPLIED WITH STEPS 1,2,3, AND 4 OF PRI 601064-14 REV ORIGINAL PRI REV 0. PE
- [SDR DALA2022041902666](https://openairdocs.org/sdr/DALA2022041902666), Apr 15, 2022: NONE. NONE. A CRACKED AFT BULKHEAD IN THE NOSE LANDING GEAR WHEEL WELL STA 110 WAS FOUND (IN REF NRC 00167). SUMMARY OF NRC 00169: BULKHEAD WAS REPAIRED PER ERA 598690-14 R
- [SDR DALA2022040802421](https://openairdocs.org/sdr/DALA2022040802421), Apr 7, 2022: DOOR FRAME. CORRODED. CORROSION ON AFT DOOR JAMB OF AFT CARGO DOOR (SM). SUMMARY OF NRC 00007: CORROSION LEVEL 2, PREVIOUS REPAIR AT DOOR JAM OF AFT CARGO WAS REPLACED PER B717 SRM 5
- [SDR DALA2022030301343](https://openairdocs.org/sdr/DALA2022030301343), Jan 17, 2022: NONE. NONE. THE FUSELAGE INTERCOSTAL WAS FOUND CRACKED AT BEND STA 1212 STA 1225, WHICH AFFECTED THE TAILCONE DEPLOYMENT CABLE ATTACH POINT. THIS COULD PREVENT PROPER OPERA
- [SDR DALA2020110403576](https://openairdocs.org/sdr/DALA2020110403576), Oct 29, 2020: CAM. MISINSTALLED. THE TAIL CONE RELEASE CAM MECHANISM IS NOT INSTALLED CORRECTLY. THE ROLLERS DO NOT ENGAGE CAM WHEN TURNED. MAINTENANCE ADJUSTED THE TAILCONE RELEASE MECHANISM C
- [SDR DALA2019082654961](https://openairdocs.org/sdr/DALA2019082654961), Aug 23, 2019: CABLE. MISROUTED. TAIL CONE LOCK IS CABLE ROUTED INCORRECTLY TO THE EXTERIOR RELEASE HANDLE. MAINTENANCE REROUTED THE LOCKING CABLE CORRECTLY TO EXTERIOR HANDLE ASSEMBLY IAW B717
- [SDR DALA2019081504764](https://openairdocs.org/sdr/DALA2019081504764), Aug 14, 2019: DOUBLER. CORRODED. CORROSION ON INTERNAL PRODUCTION DOUBLER BTW STA 1022 AND LONG 29RH AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED PER ER/A 580391-14 REV ORIG AND ETI -17-1
- [SDR DALA2019081504763](https://openairdocs.org/sdr/DALA2019081504763), Aug 14, 2019: TRAY. CORRODED. SPOTS OF CORROSION ON WASTE SRVC TRAY PANEL. CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G AND REMAINING THICKNESS IS 0.030"; OUT OF LIMITS IAW SRM 53- 00-
- [SDR DALA2019081404755](https://openairdocs.org/sdr/DALA2019081404755), Aug 13, 2019: SLIDING WINDOW. CRACKED. CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE (CPIL). NRC 00575: CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-
- [SDR DALA2019081434753](https://openairdocs.org/sdr/DALA2019081434753), Aug 12, 2019: FRAME ANGLE. CRACKED. CRACKED FRAME CLIP ON STA 1152 AND X=9 CROWN AREA, AFT ACCESORY COMPARTMENT (CAT). NRC 00422: AREA WAS REPAIRED PER ER/A 580410-14 REV ORIG AND ETI-17-19-141 RE
- [SDR DALA2019081204733](https://openairdocs.org/sdr/DALA2019081204733), Aug 11, 2019: FRAME. CORRODED. CORROSION ON FRAME ON BS 890, STRINGER 25L IS OUT OF LIMITS AT AFT CARGO COMPARTMENT, MINIMUM REMAINING THICKNNES IS 0.032" AND OUT OF LIMITS IAW SRM 53-00-00-1
- [SDR DALA2019081204732](https://openairdocs.org/sdr/DALA2019081204732), Aug 10, 2019: DOOR. DAMAGED. ELONGATED SCREW HOLES ON LH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER INNER SKIN AND PAN AT LH FWD OVERWING EMERGENCY EXIT DOOR REPAIRED IAW ETI-17-19-134
- [SDR DALA2019081204730](https://openairdocs.org/sdr/DALA2019081204730), Aug 10, 2019: SKIN. DELAMINATED. DELAMINATED AREA WAS FOUND ON LOWER SKIN DENTED. DELAMINATED AREA (0.875 IN X 0.625) ON LOWER SKIN AT RT UPPER MOVABLE VANE WAS REPAIRED IAW ETI-17-19-143 REV. 
- [SDR DALA2019082005180](https://openairdocs.org/sdr/DALA2019082005180), Aug 9, 2019: SKIN. CORRODED. FUSELAGE / SKIN / DOUBLER / STA Y=1022.091 AND L29R / ARE CORRODED. ASSOCIATED ER/A 00-580391 ADDED FOR AC 9505. (LP #1214643)
- [SDR DALA2019081204729](https://openairdocs.org/sdr/DALA2019081204729), Aug 9, 2019: DOOR. DAMAGED. ELONGATED SCREW HOLES ON LH AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. LT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-135 REV 1 AND 
- [SDR DALA2019081204728](https://openairdocs.org/sdr/DALA2019081204728), Aug 9, 2019: DOOR. DAMAGED. ELONGATED SCREW HOLES ON RH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-137 REV ORIGIN
- [SDR DALA2019081204727](https://openairdocs.org/sdr/DALA2019081204727), Aug 9, 2019: DOOR. DAMAGED. ELONGATED SCREW HOLES ON THE RT AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-138 REV OR
- [SDR DALA2019081204726](https://openairdocs.org/sdr/DALA2019081204726), Aug 9, 2019: CARGO TRACK. CORRODED. CORROSION ON LH TIE TRACK BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-04-0G PAR 26. MAXIMUM REMAINING THICKNESS IS 0.0
- [SDR DALA2019080904673](https://openairdocs.org/sdr/DALA2019080904673), Aug 8, 2019: FRAME. CRACKED. AWR HIDDEN CRACK: AFTER REMOVAL OF LONGERON IN REFERENCE NRC 00484 CRACK ON FRAME WAS FOUND STA Y 1037 AND LONG 17 LH. AREA WAS REPAIRED PER B717-200 SRM 53-20-
- [SDR DALA2019080804651](https://openairdocs.org/sdr/DALA2019080804651), Aug 8, 2019: DOOR FRAME. CRACKED. CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00402: CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14
- [SDR DALA2019080804650](https://openairdocs.org/sdr/DALA2019080804650), Aug 8, 2019: DOOR FRAME. CRACKED. CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00404: CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14
- [SDR DALA2019080804649](https://openairdocs.org/sdr/DALA2019080804649), Aug 7, 2019: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANELS (620CB & 620GB) ON COUNTERSINK AND SETTLEMENT AREA. (FUS). NRC 00619: LEVEL CORROSION 2, FUEL ACCESS PANELS #620CB & 620GB ARE O
- [SDR DALA2019080804647](https://openairdocs.org/sdr/DALA2019080804647), Aug 7, 2019: GUSSET. CRACKED. CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD (CPAX). NRC 00530: CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD WAS REPAIRED PER ETI-17-19-12
- [SDR DALA2019080544573](https://openairdocs.org/sdr/DALA2019080544573), Aug 3, 2019: LONGERON. CRACKED. CRACKED LONGERON 6R, BS 1022, AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.
- [SDR DALA2019080544572](https://openairdocs.org/sdr/DALA2019080544572), Aug 3, 2019: LONGERON. CRACKED. CRACKED LONGERON 4R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.
- [SDR DALA2019080544571](https://openairdocs.org/sdr/DALA2019080544571), Aug 3, 2019: LONGERON. CRACKED. CRACKED LONGERON 7L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.

All 228: https://openairdocs.org/aircraft/N945AT/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/N945AT/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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