# N946AT: 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: 55009
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 5, 1999
- Certificate issued: January 2, 2020
- Expires: January 31, 2030
- Mode S code: AD2384
- 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=946AT
- Page: https://openairdocs.org/aircraft/N946AT

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/N946AT/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA22LA191](https://openairdocs.org/ntsb/DCA22LA191), Aug 29, 2022: Boeing 717-200 (N946AT), Detroit, MI, no damage. Probable cause: An encounter with moderate turbulence during descent.

## 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 20020127001479I](https://openairdocs.org/incident/20020127001479I), Jan 27, 2002: Boeing 717200 (N946AT), Atlanta, GA. (-23) Flight TRS778 enroute from orlando to philadelphia into Atlanta. During cruise and after the service was underway, the lead flight attendant notified the…

## Service difficulty reports (270, 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 DALA2026072704342](https://openairdocs.org/sdr/DALA2026072704342), Jul 24, 2026: STOP. OUT OF ADJUST. MAIN CABIN DOOR WOULD NOT CORRECTLY LATCH INTO GUST LOCK. READJUST DOOR LATCH MECH/RUBBER STOP IAW AMM 52-12 GUST LOCK ENGAGES/ DISENGAGES AS NORMAL. DOOR OPS C
- [SDR DALA2026041402345](https://openairdocs.org/sdr/DALA2026041402345), Apr 10, 2026: SKIN. CRACKED. REF ERA 606161-14AD REV B STEP 4 OHEC INSP OF LEFT SIDE OF VERT STAB-5TH HOLE FROM BOTTOM HAS CRACK INDICATION. REPAIRED DAMAGE PER ER/A 606161-14AD (8672001) (
- [SDR DALA2025101707595](https://openairdocs.org/sdr/DALA2025101707595), Oct 15, 2025: SPAR CAP. CRACKED. SHIP 9506 CRACK WAS FOUND ON HOLE 6 HRS AT STA ZFS=51.267 APROX. FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE. CORRECTIVE ACTION: REPAIR ON FRONT S
- [SDR DALA2025101707594](https://openairdocs.org/sdr/DALA2025101707594), Oct 13, 2025: SKIN. DAMAGED. FASTENERS (45 EA) ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR STA ZFS =52. CORRECTIVE ACTION: VERTICAL STAB LEADING EDGE REPAIR STA ZFS =52 WERE REMOVE AND IN
- [SDR DALA2025101707591](https://openairdocs.org/sdr/DALA2025101707591), Oct 10, 2025: SERVICE PANEL. CORRODED. SHIP 9506 CORROSION ON LOWER AREA OF LAVATORY SERVICE PANEL BTW TRAY-PANEL AND PREVIOUS REAPAIR INTERNAL FILLER. CORRECTIVE ACTION: REPAIRED PER ER/A 542102- 14
- [SDR DALA2025101407521](https://openairdocs.org/sdr/DALA2025101407521), Oct 7, 2025: VANE. DENTED. DISBOND OF 2.300IN X 3.100IN. ON DENT LOCATED AT LH AFT MOVABLE FLAP VANE, LOWER SURFACE. REPAIRED PER B717-200 SRM 57-53-01-2R (1239681)
- [SDR DALA2025101407519](https://openairdocs.org/sdr/DALA2025101407519), Oct 4, 2025: NONE. NONE. DTA ER/A 542233-14 REV D REPAIR MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-OCT-25. C/W ER/A 542233-14. (1245089)
- [SDR DALA2025030101574](https://openairdocs.org/sdr/DALA2025030101574), Feb 27, 2025: TRANSFER VALVE. FAILED. SHIP 9506-ATB- THE FLIGHT CREW PERFORMED AN AIR TURN BACK DUE TO A RIGHT HYDRAULIC SYSTEM FAILURE. AN EMERGENCY WAS DECLARED WITH ATC. THE LANDING WAS UNEVENTFU
- [SDR DALA2024121111611](https://openairdocs.org/sdr/DALA2024121111611), Dec 4, 2024: UNKNOWN. NOT REPORTED. -AD- MONITOR LOG REQUIRES PERMANENT REPAIR INSTRUCTIONS FOR ER/A 542233-14AD SECTION IV PRIOR TO 30-NOV-2025. CONTACT LIAISON ENGINEERING, DEP 555, FOR INSTRUCT
- [SDR DALA2024120311391](https://openairdocs.org/sdr/DALA2024120311391), Nov 13, 2024: BULKHEAD. ABNORMAL. -AD- ACCOMPLISH ER/A 542233-14AD REV B SEC II. ACCOMPLISH ER/A 542233-14AD REV B SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATE
- [SDR DALA2024081908281](https://openairdocs.org/sdr/DALA2024081908281), Aug 18, 2024: SPLICE. CRACKED. -AD- FOUND 2 CRACK INDICATIONS ON LEFT SIDE OF VERTICAL STAB BELOW SPLICE AT STA 2F552.267 WHILE PERFORMING BHEC PER AA 5530-01048 STEP 8 REF AD2018-10-08. HOLE
- [SDR DALA2023102008639](https://openairdocs.org/sdr/DALA2023102008639), Oct 19, 2023: UNKNOWN. UNKNOWN. INSPECTOR FOUND THE HALF HINGE INSTALLED WRONG ON THE TAIL EMERGENCY SLIDE COVER. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN CO
- [SDR DALA2023101808564](https://openairdocs.org/sdr/DALA2023101808564), Oct 16, 2023: UNKNOWN. UNKNOWN. SEVERAL DENTS ON LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING. SUMMARY OF NRC 00033: LOWER SURFACE AT INB FWD MOVABLE FLAP VANE RH WING WAS REPAIRED PER B
- [SDR DALA2023101608457](https://openairdocs.org/sdr/DALA2023101608457), Oct 15, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN IN BEAM 2 AND ON PAN BTW BEAM 7 TO 8 ON AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00095: PAN IN BEAM 2 AND PAN BTW BEAM 7 TO 8 AT AFT SIDE OF P
- [SDR DALA2023101608455](https://openairdocs.org/sdr/DALA2023101608455), Oct 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL BTW STA Y=927-946 ON LONGERON 29R. ALSO CORROSION ON INTERCOSTAL BTW STA 1022 TO 1037 AND LONGERON 30 AT AFT CARGO. SUMMARY OF NRC 0011
- [SDR DALA2023101408448](https://openairdocs.org/sdr/DALA2023101408448), Oct 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON AFT PRESSURE BULKHEAD FWD FACE LOWER AREA BTW LONG PROJECTION 28L TO 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. AFT PRE
- [SDR DALA2023101408446](https://openairdocs.org/sdr/DALA2023101408446), Oct 14, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM 6 AFT SIDE OF PASSENGER DOOR L1. SUMMARY OF NRC 00094: BEAM 6 AFT SIDE OF PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 12. (
- [SDR DALA2023101408445](https://openairdocs.org/sdr/DALA2023101408445), Oct 13, 2023: UNKNOWN. UNKNOWN. HIDDEN CRACK ON FRAME WEB RH, AND ENLOGATED HOLES BTW LONGERON 27 RH TO LONGERON 28 RH, FROM STA 1053 (AFT CARGO). SUMMARY OF NRC 00184: CRACK AND ELOGATED HOLE
- [SDR DALA2023101408444](https://openairdocs.org/sdr/DALA2023101408444), Oct 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON 30 BTW FRAME STA 908 AND 1022.901 INCLUDING SPLICE (1 EA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00109: CORROSION LEVEL 2. LONGERON 30 B
- [SDR DALA2023101408440](https://openairdocs.org/sdr/DALA2023101408440), Oct 12, 2023: UNKNOWN. UNKNOWN. CORROSION ON FWD REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: FWD PREVIOUS REPAIR SPLICE AT LOWER DOOR JAMB AFT CARGO COMPARTME
- [SDR DALA2023052504151](https://openairdocs.org/sdr/DALA2023052504151), May 25, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT SIGN AT THE AFT CABIN BULKHEAD DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE BF-260 BATTERY PACK PER B717 AMM 33-51. THE OPERATIONAL CHECK WA
- [SDR DALA2023030201551](https://openairdocs.org/sdr/DALA2023030201551), Feb 28, 2023: NONE. NONE. FOUND DAMAGE AFT CARGO DOOR OPENING. AFT SIDE SEAL RETAINER SPLICE ANGLE CRACKED NEAR TEFLON GUIDE. REMOVED AFT DEPRESSOR SPLICE PER B717 SRM 53-20-15-2R-10. RE
- [SDR DALA2023022701429](https://openairdocs.org/sdr/DALA2023022701429), Feb 27, 2023: NONE. NONE. THE R1 DOOR EMERGENCY INDENTIFIER SIGN LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS
- [SDR DALA2023022701431](https://openairdocs.org/sdr/DALA2023022701431), Feb 25, 2023: NONE. NONE. FOUND 2 HOLES WITH CRACK INDICATIONS ON LH VERT STAB FRONT SPAR CAP FWD FLANGE, REF AA 5530-01048 AND AD 2018-10-08. REMOVED LH FASTENERS FROM VERT LEADING EDGE
- [SDR DALA2024121311699](https://openairdocs.org/sdr/DALA2024121311699), Feb 24, 2023: SKIN. DAMAGED. -AD- AMOC 606161-14AD - B717-200 VERTICAL STABILIZER LEADING EDGE SKIN ZFS 52.267 OVERSIZE HOLES. REPAIR APPROVAL IS LIMITED TO TWENTY-FOUR (24) MONTHS SERVICE 
- [SDR DALA2022092806343](https://openairdocs.org/sdr/DALA2022092806343), Sep 27, 2022: NONE. NONE. DURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS FOR ROWS 1-10, TO BE INOPERATIVE. THE BATTERY PACK B5-227 WAS REPLACED AND THE EMERGENCY LIGHTS R
- [SDR DALA2022070504623](https://openairdocs.org/sdr/DALA2022070504623), Jul 2, 2022: NONE. NONE. ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY BATTERY PACK 135-119 WERE INOPERATIVE. REPLACED 135-119 AND APPLICABLE POWER SUPPY PER 
- [SDR DALA2022070504627](https://openairdocs.org/sdr/DALA2022070504627), Jul 2, 2022: NONE. NONE. ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS POWERED BY B5-231 WERE INOPERATIVE. REPLACED B5-231 AND APPLICABLE POWER SUPPY PER B717 AMM 33-51.
- [SDR DALA2022053103724](https://openairdocs.org/sdr/DALA2022053103724), May 28, 2022: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT SIGN FOR THE OVER WING EXIT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME RE
- [SDR DALA2022053103723](https://openairdocs.org/sdr/DALA2022053103723), May 28, 2022: BATTERY PACK. INOPERATIVE. THE FIRST CLASS EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK IS NORMAL AT THIS TIME REF B717 AMM 33-51. (LP #8804888)
- [SDR DALA2022040702384](https://openairdocs.org/sdr/DALA2022040702384), Apr 6, 2022: SIGN. MISSING. SERVICE CHECK FOUND THAT THE EXIT SIGN IS MISSING AT 1R DOOR. MAINTENANCE REPLACED THE EXIT SIGN AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP 
- [SDR DALA2021122908129](https://openairdocs.org/sdr/DALA2021122908129), Dec 21, 2021: NONE. NONE. **THIS LOG REPLACES LOG 2010626.** DENTS LEFT UPPER FLAP MOVEABLE VANE. SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70
- [SDR DALA2024040804187](https://openairdocs.org/sdr/DALA2024040804187), Nov 8, 2021: VANE. DENTED. DENTS LEFT UPPER FLAP MOVEABLE VANE (AI). SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON RE
- [SDR DALA2021110606828](https://openairdocs.org/sdr/DALA2021110606828), Nov 6, 2021: NONE. NONE. CORROSION ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW L-28L TO L-28R. SUMMARY OF NRC 00199: CORROSION LEVEL 2: AFTER BLENDING FOUND DAMGE TO BE OUT
- [SDR DALA2021110606827](https://openairdocs.org/sdr/DALA2021110606827), Oct 29, 2021: NONE. NONE. ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ACCOMPLISH VA 84027 MA AD IN CONJUNCTION WITH EM WORKCARD 5530-01048-02. ASSOCIATED AA 
- [SDR DALA2021102606618](https://openairdocs.org/sdr/DALA2021102606618), Oct 26, 2021: NONE. NONE. ELONGATED HOLE WAS FOUND ON RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND WING AILERON STRUCTURE. SUMMARY OF NRC 00027: RIB STA XA 390 (INBOARD SIDE) OF LEFT HAND 
- [SDR DALA2021051702719](https://openairdocs.org/sdr/DALA2021051702719), May 15, 2021: BATTERY PACK. INOPERATIVE. THE AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE ON ARRIVAL. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK PER B717 AMM 3-51. (LP #7298548)
- [SDR DALA2021021000771](https://openairdocs.org/sdr/DALA2021021000771), Feb 9, 2021: SIGN. DETACHED. THE EXIT ROW SIGN ON THE AIRCRAFT LEFT IS DETACHED. MAINTENANCE REATTACHED THE SIGN. OPERATIONAL CHECK IS GOOD. (LP #7581138)
- [SDR DALA2021011100138](https://openairdocs.org/sdr/DALA2021011100138), Jan 11, 2021: BATTERY PACK. INOPERATIVE. THE INTERIOR OVERWING EXIT DOORS, AFT BOTTOM POSITION ON LEFT AND RIGHT SIDES, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK BS-119, P
- [SDR DALA201910216015](https://openairdocs.org/sdr/DALA201910216015), Oct 20, 2019: SIGN. BROKEN. BROKEN ON OVER WING EMERGENCY EXIT SIGN (2 EA) (CPAX). SUMMARY OF NRC 00544: OVER WING EMERGENCY EXIT SIGNS (2 EA) P/N: BR9051-001 WERE REPLACED PER B717-200 AM
- [SDR DALA2019101805973](https://openairdocs.org/sdr/DALA2019101805973), Oct 17, 2019: FRAME. CRACKED. INITIAL INSPECTION: CRACK ON CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. CANTED FRAME STA Y=1225 7:00 O'CLOCK POSITION AT AFT AC
- [SDR DALA2019101705944](https://openairdocs.org/sdr/DALA2019101705944), Oct 16, 2019: PAN. CRACKED. INITIAL INSPECTION: CRACK ON PAN OF FWD CARGO DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00184 PAN OF FWD CARGO DOOR INTERNAL STRUCTURE WAS REPAIRED PER ETI -17-19
- [SDR DALA2019101705943](https://openairdocs.org/sdr/DALA2019101705943), Oct 16, 2019: DOOR FRAME. CRACKED. HIDDEN DAMAGED: IN REF NRC= 00103: CRACK ON LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00639: LOWER DOOR JAMB BT
- [SDR DALA2019101605930](https://openairdocs.org/sdr/DALA2019101605930), Oct 16, 2019: CUSP WEB. CANNING. INITIAL INSPECTION: OIL CAN ON CUSP WEB BTW STA= 430 AND STA=445 LH SIDE CABIN PAX . SUMMARY OF NRC 00502: CUSP WEB BTW STA= 430 AND STA= 445 LH SIDE CABIN PAX 
- [SDR DALA2019101505901](https://openairdocs.org/sdr/DALA2019101505901), Oct 15, 2019: ACCESS PANEL. CORRODED. CORROSION ON INTERNAL STRUCTURE OF WATER WASTE ACCESS PANEL. WATER WASTE PANEL WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND DWG 5965767 REV. J.
- [SDR DALA2019101505900](https://openairdocs.org/sdr/DALA2019101505900), Oct 15, 2019: FRAME. CORRODED. FRAME CORRODED OUT OF LIMITS, BS 1022, LONGERON 27L TO 27R . THE FRAME 2 WAS REPAIRED PER SRM 53-20-07-2R-3.
- [SDR DALA2019101405887](https://openairdocs.org/sdr/DALA2019101405887), Oct 14, 2019: LONGERON. CORRODED. CORROSION LONGERON AT L=30 BTW Y=908/1037 AFT CARGO COMPARTMENT. (CORROSION LEVEL 2) LONGERON WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-00-05-2R-2 RE
- [SDR DALA2019101405888](https://openairdocs.org/sdr/DALA2019101405888), Oct 13, 2019: WIRE. BROKEN. BROKEN WIRES ON LOCKING CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 CANT. CABLE AT TAIL CONE EMERGENCY RELEASE SYSTEM STA Y=1225 WAS REPLACED PER B71
- [SDR DALA2019101405886](https://openairdocs.org/sdr/DALA2019101405886), Oct 13, 2019: DOOR FRAME. CORRODED. CORROSION ON LOWER DOOR JAMB OF AFT COMPARTMENT CARGO. (CORROSION LEVEL 2) LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 53-20-15-2R-7 PROCEDURE 7 AND B717-200 
- [SDR DALA2019101205869](https://openairdocs.org/sdr/DALA2019101205869), Oct 12, 2019: DOOR FRAME. CRACKED. CRACK ON FWD DOOR JAMB OF RH MLG. FWD DOOR JAMB OF RH MLG WAS REPAIRED PER ETI-17-19-186 REV. 2 AND ER/A 582048-14 REV. ORIGINAL. SECTION I : PERMANENT REPAIR.

All 270: https://openairdocs.org/aircraft/N946AT/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/N946AT/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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