# N947AT: 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: 55010
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 4, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD273B
- 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=947AT
- Page: https://openairdocs.org/aircraft/N947AT

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/N947AT/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 N947AT.

## FAA accident and incident reports

None matched to N947AT.

## Service difficulty reports (231, 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 DALA2026062903844](https://openairdocs.org/sdr/DALA2026062903844), Jun 28, 2026: ACCUMULATOR. LEAKING. ATB- RETURNED TO DTW DUE TO A LEFT HYDRAULIC QUANTITY LOW MESSAGE. MAINTENANCE FOUND THE LEFT SYSTEM ACCUMULATOR LEAKING AND REPLACED SAME. ALL OPERATIONAL AND 
- [SDR DALA2026020900904](https://openairdocs.org/sdr/DALA2026020900904), Feb 1, 2026: SIGN. DAMAGED. EMERGENCY EXIT SIGN ON CEILING BETWEEN 1B AND 1C IS DAMAGED. REPLACED DAMAGED EXIT SIGN IAW AMM 33-51. (8182268)
- [SDR DALA2025111808424](https://openairdocs.org/sdr/DALA2025111808424), Nov 16, 2025: LATCH. DIRTY. GIRT BAR BRACKETS HARD TO OPERATE / LOCATIONS:601. CLEANED AND LUBED DOOR 1L GIRT BAR LATCH CHECKS GOOD REF B717 MM 25-61 OK FOR SVC (1306981).
- [SDR DALA2025111108258](https://openairdocs.org/sdr/DALA2025111108258), Nov 6, 2025: SKIN. CRACKED. CRACK ON EXTERNAL SKIN, BS 1087, BTW L-13R AND L-14R AT AFT FUSELAGE. PERMANENT REPAIR AND PRI 630164-14 REV. 3. (1291355)
- [SDR DALA2025110708141](https://openairdocs.org/sdr/DALA2025110708141), Nov 4, 2025: SKIN. CRACKED. SHIP 9507 FUSELAGE / SKIN / STA Y=1087, L=13R & L=14R / CRACK. CORRECTIVE ACTION: ACCOMPLISH ER/A 630164-14 (1290083)
- [SDR DALA2025110708135](https://openairdocs.org/sdr/DALA2025110708135), Oct 31, 2025: SLIDE. UNPACKED. IN REF. TO AMDS 5211-4001: EMERGENCY SLIDE PACK WAS FOUND UNFOLDED, DOOR L1 WAS REPLACED UNDER AMDS 97-2561-9-0003 AND AMDS 2561- 9004 (1281137)
- [SDR DALA2025110708139](https://openairdocs.org/sdr/DALA2025110708139), Oct 29, 2025: SKIN. CRACKED. CRACK SKIN INSIDE OF ACCESS PANEL 370BL FWD /UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN. CORRECTIVE ACTION: UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN W
- [SDR DALA2025103107965](https://openairdocs.org/sdr/DALA2025103107965), Oct 29, 2025: VANE. PUNCTURED. INSPECTION: PUNCTURE ON FWD MOVABLE VANE LOWER SURFACE AT LT WING. FWD MOVABLE VANE LOWER SURFACE AT LH WING WAS REPAIRED IAW SRM 57-53-01 (1277612).
- [SDR DALA2025103107963](https://openairdocs.org/sdr/DALA2025103107963), Oct 27, 2025: WIRE. BROKEN. BROKEN WIRES ON ESCAPE SLIDE LANYARD ASSEMBLY (2 EA) AT R1 & L1 DOOR. LANYARDS ASSEMBLIES AT L1 DOOR AND R1 DOOR WERE REPLACED & VERIFIED IAW AIPC 25-61-01-01 T
- [SDR DALA2025102407793](https://openairdocs.org/sdr/DALA2025102407793), Oct 20, 2025: ROLLER. FAULTED. RETURNED TO ATLANTA DUE TO A LEFT GEAR UNSAFE INDICATION. PERFORMED TROUBLE SHOOT PER B717 FIM 32-60. REPLACED EMERGENCY RELEASE ROLLER FOR LEFT GEAR. TEST GOOD
- [SDR DALA2025102207719](https://openairdocs.org/sdr/DALA2025102207719), Oct 19, 2025: SENSOR. FAULTED. RETURNED TO AGS DUE TO A LEFT GEAR UNSAFE INDICATION. MAINTENANCE REPLACED THE LEFT DOOR UP AND LATCHED SENSOR. CYCLED GEAR OPS CHECK NORMAL.(7707452)
- [SDR DALA2025050603514](https://openairdocs.org/sdr/DALA2025050603514), Apr 23, 2025: BATTERY PACK. INOPERATIVE. AFT OVERWING (L&R) EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-119 & B5-230. OPERATIONAL CHECK IS NOW NORMAL REF B717 A
- [SDR DALA2025041502917](https://openairdocs.org/sdr/DALA2025041502917), Apr 14, 2025: NOT REPORTED. CRACKED. -AD- DUE TO CRACK INDICATION FOUND DURING INSP, COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 624259-14. COMPLIED WITH PRI 624259-14AD REV 
- [SDR DALA2025041502916](https://openairdocs.org/sdr/DALA2025041502916), Apr 14, 2025: SPAR CAP. CRACKED. -AD- CRACK WAS FOUND IN LOWER SPAR CAP NEAR XRS=164 DURING INSP OF LT WING REAR SPAR INSP AMDS 5720-01103-01A. "CONTACT LIAISON ENGINEERING FOR REPAIR PRIOR TO 
- [SDR DALA2025020400814](https://openairdocs.org/sdr/DALA2025020400814), Feb 3, 2025: NONE. NONE. -AD- COMPLY WITH ERA 623716-14AD REV ORIGINAL. SUMMARY NRC 002-0001:0514-2001/008 00009: COMPLIED WITH ER/A 623716-14AD REV 0, PRI REV 0, 1, AND 2. ENSURED PRI 
- [SDR DALA2025010800157](https://openairdocs.org/sdr/DALA2025010800157), Jan 2, 2025: STAB SYSTEM. OUT OF ADJUST. WHILE PERFORMING W/C 2740-01114-07, THE JACKSCREW DID NOT STOP AUTOMATICALLY AND CONTACTED THE UPPER STOP. HORIZ STAB ADJ REQUIRED PER B717 AMM 27-40-00 820-801
- [SDR DALA2024112711256](https://openairdocs.org/sdr/DALA2024112711256), Nov 25, 2024: LIGHT. SPARKS. F/O BRIEFCASE LIGHT IS SPARKING INTERNALLY. MAINTENANCE REPLACED THE F/O BRIEFCASE LIGHT IAW B717 AMM 33-16. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERV
- [SDR DALA2024042304671](https://openairdocs.org/sdr/DALA2024042304671), Apr 22, 2024: LIMIT SWITCH. OUT OF ADJUST. WHILE WORKING A.A. WORKCARD 2740-01114-07 HORIZONTAL JACK SCREW INSPECTION FAILED ONLY DURING ALTERNATE NOSE UP. HITS THE UPPER STOP. WITH PRIMARY SWITCH WORKS 
- [SDR DALA2024041804531](https://openairdocs.org/sdr/DALA2024041804531), Apr 16, 2024: SKIN. DAMAGED. REF LOG #0286119: C/W ER/A 617263-14 REV ORIG. C/W ER/A 617263-14 REV ORIG SECTION II STEPS 1 AND 2. NO FURTHER DEFECTS NOTED. CUT OUT DAMAGED SKIN AND DRILLED 
- [SDR DALA2024011700681](https://openairdocs.org/sdr/DALA2024011700681), Jan 16, 2024: DOOR FRAME. CRACKED. RT MAIN GEAR WHEEL WELL DOOR JAMB FWD CHANNEL WAS FOUND CRACKED / DAMAGED. MAINTENANCE CLEANED UP DAMAGE AND INSPECTED PER B717 SRM 53-20-02-2R PROC 3. CRACK IN
- [SDR DALA2023091107389](https://openairdocs.org/sdr/DALA2023091107389), Sep 9, 2023: UNKNOWN. UNKNOWN. LIGHTS OF WALKWAY PATH DO NOT TURN ON AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00214: CONNECTOR R5-1211 WAS CONNECTED CORRECTLY PER B717 WDM 33-51-14. THEN
- [SDR DALA2025090206466](https://openairdocs.org/sdr/DALA2025090206466), Sep 8, 2023: SKIN. DENTED. ER/A 611604-14; WINGS / OUTER WING / L.E. RHS / SKIN XOS 250-260 / DENT. ER/A 611604-14 HAS BEEN REVISED CURRENT STATUS IS REV. A. (2960169)
- [SDR DALA2023091107388](https://openairdocs.org/sdr/DALA2023091107388), Sep 8, 2023: UNKNOWN. UNKNOWN. OUT SERVICE CEILING EMERGENCY LIGHT AT ROWS 29, 26, 22, 20, 19, 15, AND 12. ALSO OUT SERVICE LOWER EMERGENCY SIGN OF AFT RH OVERWING EXIT DOOR. SUMMARY OF NRC 0
- [SDR DALA2023091107385](https://openairdocs.org/sdr/DALA2023091107385), Sep 7, 2023: UNKNOWN. UNKNOWN. DURING PC POWER SYSTEM OPERATIONAL TEST AT EMERGENCY EXITS; SEAT RH AND LH WAS FOUND TURNED OFF. STATUS LEDS (GREEN LIGHT) OF MOUNTED OUTLED UNID (OU) AT PASSEN
- [SDR DALA2023090607279](https://openairdocs.org/sdr/DALA2023090607279), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPAR
- [SDR DALA2023090607276](https://openairdocs.org/sdr/DALA2023090607276), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON FRAME STA Y=1022 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0183: CORROSION LEVEL 2. FRAME STA Y=1022 BTW LONG 29LH-29RH
- [SDR DALA2023090607275](https://openairdocs.org/sdr/DALA2023090607275), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPAR
- [SDR DALA2023090607272](https://openairdocs.org/sdr/DALA2023090607272), Sep 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP AT STA Y=1022 BTW LONG 30 AND LONG 29L. AREA EXCEEDS MORE THAN 50 PERCENT OF THE ALLOWED DAMAGE PER B717-200 SRM 53-00-00-1A PAR 4. SUMM
- [SDR DALA2023090507191](https://openairdocs.org/sdr/DALA2023090507191), Sep 3, 2023: UNKNOWN. UNKNOWN. TORN KEVLAR CABLE OF SLIDE RELEASE MECHANISM INSIDE TAILCONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PAR
- [SDR DALA2023090507184](https://openairdocs.org/sdr/DALA2023090507184), Sep 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON GUSSET OF DOOR JAMB PAN BTW STA Y=994 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00122: CORROSION LEVEL 2. GUSSET OF DOOR JAMB PAN BTW S
- [SDR DALA2023062705159](https://openairdocs.org/sdr/DALA2023062705159), Jun 26, 2023: UNKNOWN. UNKNOWN. UPPER EMERGENCY LIGHTS OVER WING EXITS ARE INOPERATIVE. MAINTENANCE RPLACED THE EMERGENCY LIGHT BATTERY PACK STA 726 PER B717 33-51. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2023060904691](https://openairdocs.org/sdr/DALA2023060904691), May 24, 2023: UNKNOWN. UNKNOWN. ON WALK-AROUND FOUND AFT CARGO DOOR FRAME DAMAGE JAMB AREA. INSPECTED DAMAGE AREA. BLENDED IAW SRM 52-30-02-R PROCEDURE 8. PERFORMED TEMP REPAIR IAW ERA 609141-
- [SDR DALA2023030201557](https://openairdocs.org/sdr/DALA2023030201557), Mar 1, 2023: NONE. NONE. CABIN STANDBY EMERGENCY LIGHTING IS MISSING TWO LENS COVERS (LOC ROW 22 AND 26). FORWARD MISSING CABIN STANDBY EMERGENCY LIGHTING TO MEL 33-52-01. PLACARDS INST
- [SDR DALA2022053103725](https://openairdocs.org/sdr/DALA2022053103725), May 27, 2022: LENS. MISSING. THE OVERHEAD EMERGENCY LIGHT LENS COVER IS MISSING AT SEAT ROWS 24 AND 27. MAINTENANCE INSTALLED NEW OVERHEAD EMERGENCY LIGHT LENS COVERS FOR SEAT ROWS 24 AND 2
- [SDR DALA2021110906895](https://openairdocs.org/sdr/DALA2021110906895), Nov 8, 2021: NONE. NONE. THE R1 DOOR SLIDE PRESSURE GAUGE INDICATION IS IN THE RED ZONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE SLIDE AND IT IS NOT IN COMPLIANCE WITH 14 CFR 
- [SDR DALA2021090705225](https://openairdocs.org/sdr/DALA2021090705225), Sep 3, 2021: TAIL CONE. OUT OF ADJUST. MULTIPLE WIRTEUPS FOR TAIL CONE CAM RIGGING. RAM 1. PLEASE REMOVE TAIL CONE AND INSPECT ALL ATTACH FITTINGS CABLES BRACKETS AND CAMS PER AMDS WORK CARD 5352-401
- [SDR DALA2021090305223](https://openairdocs.org/sdr/DALA2021090305223), Sep 2, 2021: CAM. COCKED. THE TAILCONE RELEASE CAM IS CLOCKED WRONG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY 
- [SDR DALA2021090305221](https://openairdocs.org/sdr/DALA2021090305221), Sep 2, 2021: CONDUIT. DENTED. THE CONDUIT FOR TAILCONE RELEASE CABLE IS DENTED, RT SIDE LOWER AREA (MARKED). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANC
- [SDR DALA2021083105135](https://openairdocs.org/sdr/DALA2021083105135), Aug 28, 2021: CAM. OUT OF POSITION. THE TAILCONE RELEASE CAM IS CLOCKED WRONG AND OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR 
- [SDR DALA2021052702916](https://openairdocs.org/sdr/DALA2021052702916), May 26, 2021: BATTERY. INOPERATIVE. THE EMERGENCY EXIT SIGN AT ROW 19 WOULD NOT LIGHT UP WHEN THE EMERGENCY LIGHTS WERE TURNED ON. MAINTENANCE REPLACED THE EMERGENCY BATTERY B5-120. OPERATIONAL CH
- [SDR DALA2021083005089](https://openairdocs.org/sdr/DALA2021083005089), Apr 10, 2021: FRAME. DAMAGED. ER/A 581113-14 REV A WAS ISSUED FOR DAMAGE AT STA 1037, L-14L. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 581113-14 REV A, SECTION II WITHIN 3,500FC FOLLOWIN
- [SDR DALA2021042902459](https://openairdocs.org/sdr/DALA2021042902459), Apr 9, 2021: SKIN. DAMAGED. ER/A 560974-14AD REV D ISSUED FOR REPAIRS TO LOWER FIXED LE ON VERTICAL STAB. ACCOMPLISH ER/A 560974-14AD REV D SECTION III REPEAT INSPECTIONS EVERY 3,000FC FOL
- [SDR DALA2025060704356](https://openairdocs.org/sdr/DALA2025060704356), Apr 8, 2021: SPAR CAP. CRACKED. AIRCRAFT 9507, STABILIZERS / VERTICAL / APPROX. ZFS =62 - 44 / RH SPAR CAP, AND FORWARD SPAR WEB / CRACKS / AMOC 21-151. CORRECTIVE ACTION: COMPLIED WITH ER/A 5
- [SDR DALA2021042902458](https://openairdocs.org/sdr/DALA2021042902458), Apr 8, 2021: SKIN. DAMAGED. VERTICAL STABILIZER LH LOWER FIXED LEADING EDGE SKIN FASTENER HOLES / BUSHING REPAIR / AD RELATED. REF PREVIOUS LOG 1263304. ER/A 562080-14 REV C ISSUED AND IS 
- [SDR DALA2020060802451](https://openairdocs.org/sdr/DALA2020060802451), Jun 5, 2020: POWER SUPPLY. INOPERATIVE. THE CEILING EMERGENCY LIGHTS IN THE FIRST CLASS CABIN TO ROW 14 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY B5-227 IAW B717 A
- [SDR DALA2019091105260](https://openairdocs.org/sdr/DALA2019091105260), Sep 10, 2019: RETAINER. CRACKED. CRACK ON RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA (SM). NRC 00720: RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA WAS REPAIRED PER ER/A 5812
- [SDR DALA2019091005239](https://openairdocs.org/sdr/DALA2019091005239), Sep 10, 2019: LONGERON SPLICE. CORRODED. CORROSION ON SPLICE BTW STA 650 AND 660 LONGERON 30 C1 AREA (SM). NRC 00490: SPLICE BTW STA 650 AND 660 LONGERON 30 C1 WAS REPAIRED PER ETI-17-19-168 REV 2 AND 
- [SDR DALA2021041202110](https://openairdocs.org/sdr/DALA2021041202110), Sep 9, 2019: SKIN. DAMAGED. ERA 560974-14AD REV C ISSUED FOR REPAIRS TO LOWER FIXED LE ON VE RTICAL STAB. DTA / DTE IS REQUIRED. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. ASSOCIATED ER/A
- [SDR DALA2019091005238](https://openairdocs.org/sdr/DALA2019091005238), Sep 9, 2019: SUPPORT. CRACKED. CRACK ON AREA AND HOLES OF SETTLEMENT THE SUPPORT AT AFT UPPER CORNER OF COCKPIT RT SLINDING WINDOW CUT OUT (SM). NRC 00654: AFT UPPER CORNER OF COCKPIT RT SLIN
- [SDR DALA2019090905216](https://openairdocs.org/sdr/DALA2019090905216), Sep 8, 2019: RUB STRIP. CORRODED. CORROSION AT SEVERAL FILLET FAIRING RUBSTRIPS BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES (FUS). NRC 00520: CORROSION LEVEL 2, RUBSTRIPS (8

All 231: https://openairdocs.org/aircraft/N947AT/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/N947AT/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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