# N915AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55085
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 14, 2001
- Certificate issued: May 13, 2025
- Expires: May 31, 2032
- Mode S code: ACA950
- 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=915AT
- Page: https://openairdocs.org/aircraft/N915AT

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/N915AT/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 N915AT.

## 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 20100915046669I](https://openairdocs.org/incident/20100915046669I), Sep 15, 2010: Boeing 717-200 (N915AT), Pittsburgh, PA, No damage. On September 15, 2010, at approximately 16:52 eastern time, aircraft N915AT, a Boeing 717-200, conducted under 14 CFR part 121, operated by airtran airways…

## Service difficulty reports (197, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2026091805212](https://openairdocs.org/sdr/DALA2026091805212), Sep 17, 2026: BATTERY PACK. INOPERATIVE. LT & RT OVERWING FWD EMERGENCY EXIT DOOR LIGHTS ARE INOP, R/R EMERGENCY POWER SUPPLY BATTERY PACK FOR FWD OVERWING EXIT PER B717 AMM 53-51-03. (9484062) (AIRCRA
- [SDR DALA2026072004261](https://openairdocs.org/sdr/DALA2026072004261), Jul 17, 2026: GIRT BAR. DIRTY. GIRT BARS DIRTY AND HARD TO ARM. INSPECTED BARS & OPS CHECK OF LATCHES GOOD IAW AMM 25-61. (8826616) AIRCRAFT GROUNDED.
- [SDR DALA2026021801128](https://openairdocs.org/sdr/DALA2026021801128), Feb 10, 2026: BATTERY. DISCHARGED. AFT OVERWING EXIT ROW LIGHTS INOPERATIVE. RESET BATTERY AND LET RECHARGE FOR FEW HOURS, OPS CHECKED GOOD IAW AMM 33-51 (8111544).
- [SDR DALA2026010509565](https://openairdocs.org/sdr/DALA2026010509565), Dec 27, 2025: WARNING MESSAGE. FALSE ACTIVATION. ATO, ABORTED TAKE-OFF AT 60KTS DUE TO A STABILIZER CONFIGURATION MESSAGE. MAINTENANCE PERFORMED A HORIZONTAL STABILIZER CHECK, THE SYS OPS PROPERLY, AND AIRCRAF
- [SDR DALA2025121009020](https://openairdocs.org/sdr/DALA2025121009020), Dec 6, 2025: DOOR FRAME. DAMAGED. AFT CARGO DOOR FRAME STATION 944 - FOUND PLUG RIVET UNDER SPLICE PLATE REMOVED FOR REPAIR. REPAIRED PER ER/A 630377-14 REV. ORIG. (1338586)
- [SDR DALA2025121009019](https://openairdocs.org/sdr/DALA2025121009019), Dec 5, 2025: THRESHOLD. CORRODED. CORROSION IN THRESHOLD PAN SEVERAL LOCATIONS. CORROSION DAMAGE SPLICE REPAIR - CHECKED AND REPLACED HI-SHEAR FASTENERS REF: B717-200 SRM 51-41-04 (1336682)
- [SDR DALA2025101407520](https://openairdocs.org/sdr/DALA2025101407520), Oct 3, 2025: SPAR. CORRODED. WORKING PRI 629584-14 REV 0, REV1, REV 2, REV 3, AND ERA 629584- 14AD REV ORIG. LT REAR SPAR XRS 179 CORROSION. ACCOMPLISHED PRI 629584-14AD REV 3 LT WING REAR 
- [SDR DALA2025043003322](https://openairdocs.org/sdr/DALA2025043003322), Apr 29, 2025: HOLDER. SPARKS. WHILE MOVING CAPT NOTE PAD HOLDER HAD SPARKS BEHIND THE HOLDER & ALL MAP LIGHTS WENT OUT. ALSO, CIRCUIT BREAKER W29 TRIPPED. MAINTENANCE REPAIRED BARE WIRES PER
- [SDR DALA2024110410592](https://openairdocs.org/sdr/DALA2024110410592), Nov 3, 2024: BATTERY PACK. INOPERATIVE. BOTH AFT OVERWING LOWER SIDE WALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. 
- [SDR DALA2024091909180](https://openairdocs.org/sdr/DALA2024091909180), Sep 19, 2024: PSEU. FAILED. SHIP 9580 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO A "PSEU FAIL" MESSAGE. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR POSITION INDICATIONS WERE
- [SDR DALA2023120710011](https://openairdocs.org/sdr/DALA2023120710011), Dec 5, 2023: UNKNOWN. UNKNOWN. SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. SECOND ATTEMPT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR MALFUNCTIONED. NORMAL GEAR RETRACTIO
- [SDR DALA2023120710010](https://openairdocs.org/sdr/DALA2023120710010), Dec 4, 2023: UNKNOWN. UNKNOWN. SHIP 9580 -ATB/DE- FUNCTIONAL CHECK FLIGHT. THE CREW RETURNED TO THE DEPARTURE FIELD AFTER THE LANDING GEAR FAILED TO RETRACT PROPERLY. GEAR RETRACTION SHORTLY 
- [SDR DALA2023120409901](https://openairdocs.org/sdr/DALA2023120409901), Dec 2, 2023: UNKNOWN. UNKNOWN. CRACKS ON OUTER PAN (3 EA) ON STOP FITTING AREA (AFT EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 0072: CRACKS OUTER PAN ON STOP FITTINGS AREA (AFT EDGE) AT AFT CARG
- [SDR DALA2023120109873](https://openairdocs.org/sdr/DALA2023120109873), Nov 30, 2023: UNKNOWN. UNKNOWN. CORROSION FRAMES CLIP STA=927 STGR 29RH TO STGR 28LH AT AFT CARGO COMPARTMENT C2 (ON REFERENCE NRC 0139). SUMMARY OF NRC 00493: CORROSION LEVEL 2. FRAME CLIP ST
- [SDR DALA2023112809755](https://openairdocs.org/sdr/DALA2023112809755), Nov 27, 2023: UNKNOWN. UNKNOWN. CRACK ON LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00496: LONGERON L2L AND STA Y 1133 AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER
- [SDR DALA2023112709722](https://openairdocs.org/sdr/DALA2023112709722), Nov 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00058: CORROSION LEVEL 2. DOOR JAMB STA Y 954 TO STA Y 994 AT AFT CA
- [SDR DALA2024022102373](https://openairdocs.org/sdr/DALA2024022102373), Nov 23, 2023: TRUNNION. CORRODED. WEAR AND CORROSION ON FIXED STRUT MLG ATTACH FITTING AND BUSHING ALSO (TRAPEZOIDAL PANEL) AND BUSHING AT RH MLG IN REF AMDS 3211-4004 STEP 4. SUMMARY OF NRC 004
- [SDR DALA2023111609439](https://openairdocs.org/sdr/DALA2023111609439), Nov 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB STA Y 370 TO STA Y 424 AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00057: CORROSION LEVEL 2. DOOR JAMB AT FWD CARGO COMPARTMENT (C1) WA
- [SDR DALA2023111409348](https://openairdocs.org/sdr/DALA2023111409348), Nov 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT FROM STA Y=160 TO STA Y=200 AND X=56 AT LOWER SIDE OF FWD PASSENGER DOOR JAMB. SUMMARY OF NRC 00254: CORROSION LEVEL 2. FLOOR SUPPORT
- [SDR DALA2023110809202](https://openairdocs.org/sdr/DALA2023110809202), Nov 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB (LOWER SURFACE) BTW STA Y=1022-1037 -X=57 TO -X=60 AT RH WEB PAX CABIN. SUMMARY OF NRC 00291: CORROSION LEVEL 2. WEB (LOWER SURFACE) BTW STA Y=
- [SDR DALA2023101408450](https://openairdocs.org/sdr/DALA2023101408450), Oct 13, 2023: UNKNOWN. UNKNOWN. EMERGENCY EXIT LIGHT ASSEMBLY ABOVE R1 DOOR HANDLE, BR9051-001, IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE R1 DOOR. OPERATIONAL CH
- [SDR DALA2023101408449](https://openairdocs.org/sdr/DALA2023101408449), Oct 13, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 332 - 351 PANEL P1-118 EIN B5-118 IS DEFECTIVE REF B717 33-51-14. MAINTENANCE REPLACED THE EMERGENCY LIGHT CHARGER AT
- [SDR DALA2019061103495](https://openairdocs.org/sdr/DALA2019061103495), Jun 10, 2019: SKIN. DENTED. DENTS ON FUSELAGE SKIN AT STA 427 BETWEEN LONGERON 27L AND 29L. ACCOMPLISHED PERMANENT REPAIR REF PRI #578768-14, REV. 1 AND ER/A #578768 -14 REV. ORIGINAL. REQ
- [SDR DALA201906113489](https://openairdocs.org/sdr/DALA201906113489), Jun 9, 2019: SKIN. DENTED. DENT ON FUSELAGE SKIN AT STA 524 TO 527 1" BELOW LONG 26L LAP SEAM. PER B717 SRM 53-01-01-1A-3 CONDITION 5 DENT IS OUT OF LIMITS. REMOVED DAMAGE 1" X 3" PER B71
- [SDR DALA2019010200009](https://openairdocs.org/sdr/DALA2019010200009), Dec 31, 2018: TERMINAL. BROKEN. THE AFT WALKWAY EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TERMINAL BROKEN. THE WIRE TERMINAL WAS REPAIRED PER SWPM CHAPTER 20. THE 
- [SDR DALA2018120547036](https://openairdocs.org/sdr/DALA2018120547036), Dec 3, 2018: SEAL. MISSING. LEFT WING INBOARD SLAT MISSING ABOUT 9.5" OF SEAL. MISSING SEAL STARTS AT 30 IN. FROM MOST INBD EDGE OF SEAL ON LT WING #1 SLAT. FWD TO CDL 57-48-01. SDR REPORT
- [SDR DALA2018092005668](https://openairdocs.org/sdr/DALA2018092005668), Sep 19, 2018: WARNING SYSTEM. FALSE ACTIVATION. THE CREW ABORTED THE TAKEOFF AFTER 110 KNOTS FOLLOWING AN AURAL STABILIZER MOTION WARNING AND AN ILLUMINATED RED "STAB TRIM" MESSAGE. MAINTENANCE VERIFIED THAT 
- [SDR DALA2018091805645](https://openairdocs.org/sdr/DALA2018091805645), Sep 15, 2018: LIGHT. UNKNOWN. EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. MAINTENANCE REINSTALLED THE EMERGENCY LIGHT AT 28B.
- [SDR DALA2017022101389](https://openairdocs.org/sdr/DALA2017022101389), Feb 21, 2017: LIGHT. INOPERATIVE. DURING A LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT WING EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED
- [SDR DALA2016061904762](https://openairdocs.org/sdr/DALA2016061904762), Jun 18, 2016: WEB. DAMAGED. TOOL MARK ON WEB STA Y=674 BETWEEN LONGERON 11RT TO 10RT AND LONGERON 14RT TO 15RT AT CPAX, SM, CARD 6, ZONE 201. WEB WAS REPAIR IAW ER/A 547802-14, REV ORIGINA
- [SDR DALA2016061604672](https://openairdocs.org/sdr/DALA2016061604672), Jun 15, 2016: STRAP. CRACKED. CRACK ON FWD STRAP AT BEAM NR 6 L1 PASSEGER DOOR. STRAP WAS REPLACED IAW SRM 51-41-02, 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND DWG 9955750, REV. U. CRAC
- [SDR DALA2016061604671](https://openairdocs.org/sdr/DALA2016061604671), Jun 15, 2016: ANGLE. CORRODED. CORROSION ON CUSP ANGLE AT LBL 60 BETWEEN BS 157 AND 218. DUE TO EXCESSIVE DAMAGE BY CORROSION. CUSP ANGLE WAS REPAIRED IAW ETI 17-16-054, REV 1 AND ER/A 547810
- [SDR DALA2016061504667](https://openairdocs.org/sdr/DALA2016061504667), Jun 14, 2016: STRUCTURE. BENT. BEND ON FWD/AFT LOWER CORNER AT EXTERNAL SURFACE PASSENGER L1 DOOR. LOWER CORNER AT EXTENAL SURFACE PASSENGER ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-01, FIG 2
- [SDR DALA2016061504666](https://openairdocs.org/sdr/DALA2016061504666), Jun 14, 2016: DOUBLER. CRACKED. CRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG .656 AND .468".
- [SDR DALA2016061504665](https://openairdocs.org/sdr/DALA2016061504665), Jun 14, 2016: DOUBLER. CRACKED. CRACK ON DOUBLER AFT END AT BEAM NR 7 L1 DOOR. AFT END AT BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 13. CRACK LONG 0.812".
- [SDR DALA2016061504664](https://openairdocs.org/sdr/DALA2016061504664), Jun 14, 2016: DOUBLER. WORN. WEAR ON DOUBLER PRODUCTION AT INNER RT PAN A SIDE LOWER HINGE AFT EMERGENCY EXIT. DOUBLER PRODUCTION WAS REPAIRED IAW SRM 52-10-02, FIG 201, REP 16. MEASURE: OT
- [SDR DALA2016061504662](https://openairdocs.org/sdr/DALA2016061504662), Jun 14, 2016: SKIN. CRACKED. CRACKED FUSELAGE SKIN ON CUTOUT OF RT/LT NLG AFT DOOR AFT HINGE. SKIN WAS REPLACED IAW SRM 53-10-01, 51-41-02, 51-41-05, 51-10-3 P. 21, 15.
- [SDR DALA2016061404601](https://openairdocs.org/sdr/DALA2016061404601), Jun 13, 2016: CARGO TRACK. CORRODED. CORROSION ON RT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 900-954. DUE TO EXCESSIVE DAMAGE, CARGO TRACK SECTION WAS REPLACED IAW SRM 51-41-05 AND 51-41-02.
- [SDR DALA2016061404600](https://openairdocs.org/sdr/DALA2016061404600), Jun 13, 2016: ANGLE. CRACKED. CRACK ON ANGLE OF WING BOX FLOOR STRUCTURE BS 712 TO 714 X -20 AND Z -8. ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05 AND DWG 5910464, REV "DE" ITEM 24.
- [SDR DALA2016061404599](https://openairdocs.org/sdr/DALA2016061404599), Jun 13, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520EB AT LT WING. CORROSION ON COUNTERSINK OF ACCESS DOOR 520EB WAS REMOVED IAW SRM 51-10-04 AN
- [SDR DALA2016061304548](https://openairdocs.org/sdr/DALA2016061304548), Jun 12, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 29 LT BELOW OF SPLICE BS 960 IN AFT CARGO COMPARTMENT. DAMAGE ON SECTION LONGERON WAS REMOVED AND WAS REPAIRED IAW SRM 51-10-04 AND 53-20-
- [SDR DALA2016061304547](https://openairdocs.org/sdr/DALA2016061304547), Jun 12, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620EB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 620EB WERE REMOV
- [SDR DALA2016061304546](https://openairdocs.org/sdr/DALA2016061304546), Jun 12, 2016: FRAME. CORRODED. CORROSION ON FRAME ANGLE BS 908 BETWEEN LONGERON 29 AND 30L IN AFT CARGO COMPARTMENT. FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06, FIG 201.
- [SDR DALA2016061104537](https://openairdocs.org/sdr/DALA2016061104537), Jun 10, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DB AT RT WING. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01 A
- [SDR DALA2016061104536](https://openairdocs.org/sdr/DALA2016061104536), Jun 10, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620CB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01. F
- [SDR DALA2016061104533](https://openairdocs.org/sdr/DALA2016061104533), Jun 10, 2016: FLOOR PANEL. CRACKED. CRACKED STIFFENERS ON PASSENGER CABIN FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.
- [SDR DALA2016061104532](https://openairdocs.org/sdr/DALA2016061104532), Jun 10, 2016: FLOOR PANEL. CRACKED. CRACKED FLOOR PANEL 211ACF. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV.
- [SDR DALA2016061004502](https://openairdocs.org/sdr/DALA2016061004502), Jun 9, 2016: FLOOR PANEL. DAMAGED. CRACK ON PASSENGER CABIN FLOOR PANEL NR 222ZF. SM, CARD 52, ZONE 000. FLOOR PANEL 222ZF WAS REPAIRED IAW SRM 53-00-00, REPAIR 2, FIG 201. HFEC INSPECTION WAS AC
- [SDR DALA2016061004501](https://openairdocs.org/sdr/DALA2016061004501), Jun 9, 2016: FLOOR PANEL. DAMAGED. DAMAGE AND MISSING FERRULES ON FLOOR PANELS, NR 222ABF, 222AAF, 222AEF, AND 222AKF AT PAX CABIN. SM, CARD 79, ZONE 000. DAMAGE FERRULES WERE REPLACED ON FLOOR P
- [SDR DALA2016061004500](https://openairdocs.org/sdr/DALA2016061004500), Jun 9, 2016: FLOOR PANEL. DAMAGED. DAMAGE AND MISSING FERRULES ON FLOOR PANELS 221FF, 221CF, 22BF, 22LF, 222JF, 222RF, AND 222UF. SM, CARD 77, ZONE 000. DAMAGE FERRULES ON FLOOR PANEL NR 222BF, 2

All 197: https://openairdocs.org/aircraft/N915AT/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/N915AT/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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