# N960AT: 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: 55022
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 30, 2001
- Certificate issued: December 19, 2023
- Expires: December 31, 2030
- Mode S code: AD5C38
- 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=960AT
- Page: https://openairdocs.org/aircraft/N960AT

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/N960AT/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 N960AT.

## FAA accident and incident reports

None matched to N960AT.

## Service difficulty reports (181, 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 DALA2026090304977](https://openairdocs.org/sdr/DALA2026090304977), Sep 2, 2026: SKIN. DEMODIFICATION. ACFT CONFIGURATION HAD A PREVIOUS REPAIR THAT CONSISTS OF A SERIES OF DOUBLERS, TRIPLERS, QUADRUPLERS INSTALLED COMMON TO THE LOCATION OF THE ORIGINAL AFT ATG4 
- [SDR DALA2026072804383](https://openairdocs.org/sdr/DALA2026072804383), Jul 26, 2026: COMPRESSOR. STALLED. ATB- RETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: RIGHT ENGINE FAILED HPC BORESCOPE. REPLACED NR 2 ENGINE. (9087110) AIRCRAFT GROUND
- [SDR DALA2026030201425](https://openairdocs.org/sdr/DALA2026030201425), Feb 26, 2026: FUEL LINE. LEAKING. FAINT SMELL OF JETT FUEL IN CABIN UPON ARRIVAL TO JET. JET WAS SHUTDOWN WITH EXTERNAL AIR HOOKED UP. FOUND RETURN TO TANK LINE & SHROUD LEAKING IN FWD RT AFT BA
- [SDR DALA2025092907060](https://openairdocs.org/sdr/DALA2025092907060), Sep 27, 2025: RELEASE CABLE. TORN. INITIAL INSPECTION: TORN CABLE OF RELEASE MECHANISM OF TAIL CONE AT AFT ACCESORIES COMPARTMENT. CORRECTIVE ACTION: CABLE ASSY RELEASE HANLDE P/N: 3913359-545 OF
- [SDR DALA2025030501715](https://openairdocs.org/sdr/DALA2025030501715), Mar 4, 2025: VALVE. STIFF. SHIP 9519 -ATB/FUME/DE- DURING CLIMB OUT AT ABOUT 10K FEET, THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO MEM DUE TO UNKNOWN ODOR THROUGHOUT TH
- [SDR DALA2025030401653](https://openairdocs.org/sdr/DALA2025030401653), Feb 11, 2025: ACCESS PANEL. MISSING. LH WING LANDING LIGHT TOOLING ACCESS COVER MISSING. MAINTENANCE DEFERRED IT TO MONITOR PER ERA 607941-14TR REV ORIGINAL. C/W TEMP REPAIR PER SECTION I. ENGINEER
- [SDR DALA2024091909181](https://openairdocs.org/sdr/DALA2024091909181), Sep 18, 2024: CONTROL UNIT. FAILED. SHIP 9519 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE WHEN TRANSITIONING FLAPS FROM 18 TO 40 WITH THE GEAR EXTENDED. THE CREW PERFORMED A GO-
- [SDR DALA2024041004261](https://openairdocs.org/sdr/DALA2024041004261), Mar 7, 2024: NONE. NONE. ERA 612138-14 REV A. ACCOMPLISH SECTION III AT 50,000 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 00-612138 ADDED FOR AC 9519. ERA 612138-14 OK TO CLOSE, OPENED IN ERR
- [SDR DALA2023101008309](https://openairdocs.org/sdr/DALA2023101008309), Oct 10, 2023: UNKNOWN. UNKNOWN. CORROSION TYPE EXFOLIATION ON PREVIOUS REPAIR BTW STA Y=960 TO Y=980, LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. CORROSI
- [SDR DALA2023101008307](https://openairdocs.org/sdr/DALA2023101008307), Oct 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER DOOR JAMB OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. LOWER DOOR JAMB OF AFT CARGO WAS REPAIRED PER B717-200 SRM 53-20
- [SDR DALA2024031103212](https://openairdocs.org/sdr/DALA2024031103212), Oct 6, 2023: SKIN. DAMAGED. DTE, ERA 612138-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN REPAIR AT #2 CARGO DOOR OPENING / Y=954 - 994, L-28R IS PENDING DTE STAGE II & III APPROVAL P
- [SDR DALA2023100408154](https://openairdocs.org/sdr/DALA2023100408154), Oct 3, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON FRAME CLIP FROM STA 655 LOGERON 30, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00514: CORROSION LEVEL 2. FRAME CLIP FROM STA 655 LOGERON 30
- [SDR DALA2023092807973](https://openairdocs.org/sdr/DALA2023092807973), Sep 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=1022 BTW LONGERON 26 RH TO LONGERON 26 LH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00499: CORROSION LEVEL 2. FRAME CLIP STA Y
- [SDR DALA2023092707958](https://openairdocs.org/sdr/DALA2023092707958), Sep 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAMES STA 1022 BTW LONG 27R-29R AND AT STA 1037 BTW LONG 29R-29L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00622: CORROSION LEVEL 2. FRAMES ST
- [SDR DALA2023092107772](https://openairdocs.org/sdr/DALA2023092107772), Sep 21, 2023: UNKNOWN. UNKNOWN. BROKEN FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-300 AND LONG L 11R. SUMMARY OF NRC 00578: FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-3
- [SDR DALA2023092107771](https://openairdocs.org/sdr/DALA2023092107771), Sep 20, 2023: UNKNOWN. UNKNOWN. CRACK ON PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB (RH EDGE) ON STA Y=1053 BTW LONG PROJECTION 14R AND 16R AT AFT CPAX. SUMMARY OF NRC 00285: PRESSURE BULKHEAD
- [SDR DALA2023091807623](https://openairdocs.org/sdr/DALA2023091807623), Sep 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON MEMBRANES BTW STA 1053 AND L-28L TO L-23R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00573: CORROSION LEVEL 2. MEMBRANES BTW STA 1053 AND L-28L TO L-
- [SDR DALA2023091407541](https://openairdocs.org/sdr/DALA2023091407541), Sep 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON INNER DOUBLER UNDER FITTING OF CENTER BULKHEAD POST STA Y=1053 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INNER DOUBLE
- [SDR DALA2023091407532](https://openairdocs.org/sdr/DALA2023091407532), Sep 12, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON AN INTERCOASTAL AT STA 1037 LONG 30 RH CARGO COMPARTMENT (C2). SUMMARY OF NRC 00643: CORROSION LEVEL 2. INTERCOASTAL AT STA 1037 LONG
- [SDR DALA2023090607280](https://openairdocs.org/sdr/DALA2023090607280), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEB STA Y=273-275, Y=370-389, Y=636-655, Y=832-851, Y=889-908, Y=908-927, Y=927-946, AND X=-56 IS OUT OF LIMIT AT PASSENGER CABIN IN REF NR
- [SDR DALA2023090607278](https://openairdocs.org/sdr/DALA2023090607278), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND. THE LH OUTBD SEAT TRACK BTW STA 318-320 WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.100 IN. THE REMAINING THICKNESS IS 0.032 IN. THEREFORE THE
- [SDR DALA2023090607277](https://openairdocs.org/sdr/DALA2023090607277), Sep 6, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONG L 22R/23RH BTW STA Y=1002/1053 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00192: CORROSION LEVEL 2. LONG L 22R/23RH BTW STA Y=1002/1053 AT 
- [SDR DALA2023090507197](https://openairdocs.org/sdr/DALA2023090507197), Sep 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA X=-56 BTW STA Y=200/216 AT PAX CABIN (W1). SUMMARY OF NRC 00317: CORROSION LEVEL 2. FLOOR SUPPORTS STA X=-56 BTW STA Y=200/216 A
- [SDR DALA2023090507196](https://openairdocs.org/sdr/DALA2023090507196), Sep 4, 2023: UNKNOWN. UNKNOWN. CRACKS ON WEB BTW STA X=44/60 AND BTW STA Y=218/237 AT PAX CABIN (W1). SUMMARY OF NRC 00327: CRACKS ON WEB BTW STA X=44/60 AND BTW STA Y=218/237 AT PAX CABIN WE
- [SDR DALA2023090507195](https://openairdocs.org/sdr/DALA2023090507195), Sep 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON PRODUCTION DOUBLER LONGERON 18 RH BTW STA Y 889 AND 908 AT PAX CABIN. SUMMARY OF NRC 00653: CORROSION LEVEL 2. PRODUCTION DOUBLER LONGERON 18 RH BT
- [SDR DALA2023090507193](https://openairdocs.org/sdr/DALA2023090507193), Sep 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEB IS OUT OF LIMITS STA Y=957-946, Y=908-889, AND X=-47 AT PASSENGER CABIN CPAX. SUMMARY OF NRC 00627: CORROSION LEVEL 2. WEB STA Y=957-94
- [SDR DALA2023090507192](https://openairdocs.org/sdr/DALA2023090507192), Sep 3, 2023: UNKNOWN. UNKNOWN. CRACK LH CUSP WEB STA Y 889 AND STA 946 AT PASSENGER CABIN. SUMMARY OF NRC 00599: LH CUSP WEB STA Y 889 AND STA 946 AT PASSENGER CABIN WAS REPAIRED PER B717-200
- [SDR DALA2023090507190](https://openairdocs.org/sdr/DALA2023090507190), Sep 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS (2 EA) STA X=56 BTW STA Y=196/200 AND STA Y=200/215 AT PAX CABIN (W1). SUMMARY OF NRC 00321: CORROSION LEVEL 2. FLOOR SUPPORTS STA X
- [SDR DALA2023090507188](https://openairdocs.org/sdr/DALA2023090507188), Sep 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA Y=218 (1 EA) BTW STA X=-10/13, STA Y=200 (3 EA) BTW STA X=-9/-46, X=-5/5, X= 9/13, STA Y=196 (1 EA) BTW STA X=16/43, STA Y=180 (
- [SDR DALA2023090507187](https://openairdocs.org/sdr/DALA2023090507187), Sep 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA Y=200 (1 EA) BTW STA X=-46-56 AND STA X=55 (1 EA) BTW STA Y=160/196 AT PAX CABIN (W1). SUMMARY OF NRC 00316: CORROSION LEVEL 2. 
- [SDR DALA2023090507186](https://openairdocs.org/sdr/DALA2023090507186), Sep 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK BTW Y=200 TO 246 AND X=-44 AT PAX CABIN STRUCTURE. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO 246 AND X= -44 AT PA
- [SDR DALA2023090507185](https://openairdocs.org/sdr/DALA2023090507185), Sep 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR FITTING STA X=-11 BTW STA Y=200/218 AT PAX CABIN (W1). SUMMARY OF NRC 00319: CORROSION LEVEL 2. FLOOR FITTING STA X=-11 BTW STA Y=200/218 AT 
- [SDR DALA2023090507182](https://openairdocs.org/sdr/DALA2023090507182), Sep 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEBS BTW STA X=55/-55 AND BTW STA Y=160/218 AT PAX CABIN (W1). SUMMARY OF NRC 00323: CORROSION LEVEL 2. WEBS BTW STA X=55/-55 AND BTW STA Y=160/218
- [SDR DALA2023083007069](https://openairdocs.org/sdr/DALA2023083007069), Aug 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR CHANNELS (2 EA) STA X=-7 AND STA X=7 BTW STA Y=160/200 AT PAX CABIN (W1). SUMMARY OF NRC 00320: CORROSION LEVEL 2. FLOOR CHANNELS (2 EA) STA 
- [SDR DALA2023082806940](https://openairdocs.org/sdr/DALA2023082806940), Aug 27, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL SKIN AT FWD CARGO DOOR BTW STA 402 TO STA 415 APROX AND Y=0. SUMMARY OF NRC 00103: INTERNAL SKIN (LOWER OUTER PAN) AT FWD CARGO DOOR BTW STA 4
- [SDR DALA2023082806938](https://openairdocs.org/sdr/DALA2023082806938), Aug 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOUBLER OF AFT PRESSURE BULKHEAD FWD FACE BTW STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00306: CORROSION LEVEL 2. DOUBLER OF 
- [SDR DALA2023082406883](https://openairdocs.org/sdr/DALA2023082406883), Aug 22, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON THE LEFTHAND CUSP WEB. MEASUREMENT THICKNESS WAS ACCOMPLISHED. ORIGINAL WIDTH THICKNESS IS 0.032 IN ON LH CUSP WEB (REPAIR PART) BTW STA 
- [SDR DALA2023082206830](https://openairdocs.org/sdr/DALA2023082206830), Aug 21, 2023: UNKNOWN. UNKNOWN. CORROSION ON SPLICE STA Y=694 AND X=-49 AT PASSENGER CABIN (CPAX). SUMMRY OF NRC 00375: SPLICE WAS REPLACED PER B717 SRM 53-00-55- 2R. (LP #2929400)
- [SDR DALA2023082206829](https://openairdocs.org/sdr/DALA2023082206829), Aug 21, 2023: UNKNOWN. UNKNOWN. CRACKS ON CUSP WEB LOWER SIDE (2 EA) STA Y=718 LH/RH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00374: CRACKS ON CUSP WEB LOWER SIDE STA Y=718 LH/RH PASSENGER CABIN
- [SDR DALA2023082106763](https://openairdocs.org/sdr/DALA2023082106763), Aug 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR TRACK STA X=-44 AND BTW STA Y=1022/1059 AT PAX CABIN (W2). SUMMARY OF NRC 00379: CORROSION LEVEL 2. NEW FLOOR TRACK WAS REPLACED PER B717 SRM
- [SDR DALA2023082106762](https://openairdocs.org/sdr/DALA2023082106762), Aug 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA X=-54 AND BTW STA Y=1022/1055 AT PAX CABIN (W2). SUMMARY OF NRC 00380: CORROSION LEVEL 2. FLOOR SUPPORT STA X=-54 AND BTW STA Y=1
- [SDR DALA2023082106761](https://openairdocs.org/sdr/DALA2023082106761), Aug 19, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1037 ABOVE LONG 17L AT PAX CABIN. SUMMARY OF NRC 00236: FRAME STA Y=1037 ABOVE LONG 17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07
- [SDR DALA2020031001743](https://openairdocs.org/sdr/DALA2020031001743), Mar 8, 2020: HINGE. LOOSE. THE TAIL CONE SLIDE COVER HAS LOOSE HINGES. MAINTENANCE REPLACED THE TAIL CONE SLIDE CONTAINER IAW B717 AMM 25-61-02. INSTALLED SLIDE ON NEW SLIDE CONTAINER AND
- [SDR DALA2019110606424](https://openairdocs.org/sdr/DALA2019110606424), Nov 6, 2019: POWER SUPPLY. INOPERATIVE. THE AFT BULKHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY, MPN 803925-1, AND THE OPERATIONAL CHECK WAS GOOD. (LP #6
- [SDR DALA2019070304007](https://openairdocs.org/sdr/DALA2019070304007), Jul 2, 2019: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BETWEEN STA 1002 AND STA 1022, FWD END. NRC 005-0001:21-0553-8-0817/022 00026: REPLACED INTERCOSTAL REF DWG #9958233. (LP #1151894)
- [SDR DALA2019070304006](https://openairdocs.org/sdr/DALA2019070304006), Jul 2, 2019: STRINGER. CORRODED. DUE TO CORROSION DAMAGE, SPLICE IN NEW SECTION OF STRINGER 30 FROM STA 900-1012. NRC 005-0001 21-0553-8-0817/025 00029: NEW SECTION OF STRINGER WAS SPLICED IN, 
- [SDR DALA2019070304005](https://openairdocs.org/sdr/DALA2019070304005), Jul 2, 2019: STRINGER. CORRODED. STA 927-908 STRINGER 29L CORRODED. NRC 005-0001:21-0553-8-0817/014 00016: SPLICED IN NEW SECTION OF STRINGER REF DWG #5919707. (LP #1151743)
- [SDR DALA2019070203975](https://openairdocs.org/sdr/DALA2019070203975), Jul 1, 2019: SHEAR TIE. CORRODED. CLIP CORRODED ON AFT SIDE OF STA 944 BETWEEN S30 AND S29R. NRC 005-0001:21-0553-8-0817/005 00007: SPLICED IN NEW SECTION OF SHEAR CLIP REF SRM 53-00-06-2R-2 FIG
- [SDR DALA2019070203972](https://openairdocs.org/sdr/DALA2019070203972), Jul 1, 2019: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED BETWEEN STA 944 AND 954 JUST O/B OF S30 (M). NRC 005-0001:21-0553-8-0817/011 00013: REPLACED INTERCOSTAL REF DWG #9915578. (LP #1149950)
- [SDR DALA2023052504150](https://openairdocs.org/sdr/DALA2023052504150), Jun 18, 2019: UNKNOWN. UNKNOWN. THIS ER/A 527176-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV A. AT OR PRIOR TO 35,500 TOTAL A

All 181: https://openairdocs.org/aircraft/N960AT/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/N960AT/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.