# N930AT: 2000 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: 55072
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 3, 2000
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ACE5BB
- 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=930AT
- Page: https://openairdocs.org/aircraft/N930AT

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/N930AT/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 DCA17CA096](https://openairdocs.org/ntsb/DCA17CA096), Nov 21, 2016: Boeing 717 200 (N930AT), Hopewell, VA, no damage. Probable cause: the flight attendant's inadvertent bump into a retractable galley tray.

## FAA accident and incident reports

None matched to N930AT.

## Service difficulty reports (188, 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 DALA2026062903840](https://openairdocs.org/sdr/DALA2026062903840), Jun 28, 2026: DOOR FRAME. CRACKED. CORROSION AND CRACK ON FWD CARGO DOOR JAMB LOWER SECTION AT FWD CARGO COMPARTMENT. FWD CARGO DOOR JAMB LOWER SECTION AND SPLICE ANGLES (4EAS) AT FWD CARGO DOOR 
- [SDR DALA2026062503778](https://openairdocs.org/sdr/DALA2026062503778), Jun 24, 2026: LANYARD. FRAYED. FRAYED LANYARD OF SLIDE DOOR LT. REPLACED IAW AIPC 25-61-01-01. (1663123) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903065](https://openairdocs.org/sdr/DALA2026051903065), May 17, 2026: NOT REPORTED. NOT REPORTED. AD 2024-21-01 ER/A 634524-14AD. ASSOCIATED ER/A 14-634524 (1598852) (AIRCRAFT GROUNDED)
- [SDR DALA2026040102132](https://openairdocs.org/sdr/DALA2026040102132), Mar 31, 2026: WINDSHIELD. ARCED. CENTER WINDSHIELD ANTIICE FAIL DUE TO ARCING HEATER CRACK IN WINDSHIELD. REPLACED CENTER WINDSHIELD PER B717 AMM 56-11-01 LEAK CK OK A/C OK FOR SERVICE (8424138
- [SDR DALA2025122309343](https://openairdocs.org/sdr/DALA2025122309343), Dec 17, 2025: SLIDE. DISLODGED. OPS REPORTS R1 DOOR SLIDE DISLODGED. DOOR SLIDE IAW AMM 25-61. ACFT OK FOR SERVICE. (8406508)
- [SDR DALA2025111208301](https://openairdocs.org/sdr/DALA2025111208301), Nov 11, 2025: CABLE. OUT OF ADJUST. ATB- RETURNED TO ATL DUE TO AIR/GROUND FAULTS. ADJUSTED GROUND SHIFT CABLE. OPS NORMAL.(7834142)
- [SDR DALA2025061104461](https://openairdocs.org/sdr/DALA2025061104461), Jun 10, 2025: POWER SUPPLY. INOPERATIVE. AIRCRAFT 9567, ON SVC CK FOUND AFT L/R OVER WING DOOR EMERGENCY BOTTOM LIGHT INOP. CORRECTIVE ACTION: REPLACED EMERGENGY BATT POWER SUPPLY IAW B717 AMM 33-51-03
- [SDR DALA2025021201091](https://openairdocs.org/sdr/DALA2025021201091), Feb 11, 2025: LIGHT. UNKNOWN. THE F/A REPORTED THAT THE EXIT ROW EMERGENCY LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE PERFORMED A TEST OF THE EMERGENCY LIGHT SYSTEM AND NO FAULTS WERE FOUND. A
- [SDR DALA2025010300046](https://openairdocs.org/sdr/DALA2025010300046), Jan 2, 2025: POWER SUPPLY. FAULTED. FOUND ROW 21 EMERGENCY EXIT LIGHT B5-230/P9 TO BE INOPERATIVE. MAINTENANCE TRIED A NEW EMERGENCY LIGHT BATTERY. NO HELP, REINSTALLED ORIGINAL. REPLACED POWER SU
- [SDR DALA2024090408735](https://openairdocs.org/sdr/DALA2024090408735), Sep 4, 2024: LIGHT. INTERMITTENT. WITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. MAINTENANCE TROUBLESHOT PER B71
- [SDR DALA2024071507164](https://openairdocs.org/sdr/DALA2024071507164), Jul 15, 2024: ANGLE. CORRODED. CORROSION ON CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 AT PASSENGER CABIN. SUMMARY OF NRC 541: CORROSION LEVEL 2. CUSP ANGLE INSI
- [SDR DALA2024071507161](https://openairdocs.org/sdr/DALA2024071507161), Jul 14, 2024: PAN. CRACKED. CRACKS (3 EA) WERE FOUND ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00573: CRACKS (3 EA) ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR WERE REPAIRED PER 
- [SDR DALA2024071507156](https://openairdocs.org/sdr/DALA2024071507156), Jul 12, 2024: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK ON OPEN POSITION. ALSO FWD PREVIOUSLY REWORK DOES NOT MEET WITH RADII. SUMMARY OF NRC
- [SDR DALA2024070206725](https://openairdocs.org/sdr/DALA2024070206725), Jul 1, 2024: SKIN. CRACKED. AIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT 
- [SDR DALA2024062906603](https://openairdocs.org/sdr/DALA2024062906603), Jun 28, 2024: SEAT TRACK. CORRODED. AIRCRAFT 9567, CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION ON INBOARD SEAT TRACK
- [SDR DALA2024062906599](https://openairdocs.org/sdr/DALA2024062906599), Jun 27, 2024: SEAT TRACK. CORRODED. AIRCRAFT 9567, CORROSION ON CENTER SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2. SECTION CENTE
- [SDR DALA2024062906598](https://openairdocs.org/sdr/DALA2024062906598), Jun 27, 2024: LONGERON. CRACKED. AIRCRAFT 9567, INITIAL INSPECTION: CRACK ON LONGERON END L2R AND STA 1133 ALSO BRACKET SUPPORT LOWER SECTION CANTED BULKHEAD 1103 RH SIDE AFT ACCESORY COMPARTME
- [SDR DALA2024062706576](https://openairdocs.org/sdr/DALA2024062706576), Jun 27, 2024: ANGLE. CRACKED. AIRCRAFT 9567, CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE. W1. CORRECTIVE ACTION: CORROSION LEVEL 2. COR
- [SDR DALA2024062706577](https://openairdocs.org/sdr/DALA2024062706577), Jun 25, 2024: SKIN. DAMAGED. AIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 
- [SDR DALA2024062706572](https://openairdocs.org/sdr/DALA2024062706572), Jun 25, 2024: SKIN. CRACKED. AIRCRAFT 9567, CRACK ON DOOR SKIN ADJACENT TO EXTERNAL DOOR HANDLE HOUSING AT LEFT PASSENGER ENTRANCE DOOR. SUMMARY OF NRC SERIAL 00370: DUE TO SEVERAL DAMAGE O
- [SDR DALA2024062506488](https://openairdocs.org/sdr/DALA2024062506488), Jun 24, 2024: LONGERON. CORRODED. CORROSION OUT OF LIMIT ON LONGERON END STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT. C2. SUMMARYOF NRC 00857: CORROSION LEVEL 2. LONGERON END ON STA Y 1002 LO
- [SDR DALA2024062406343](https://openairdocs.org/sdr/DALA2024062406343), Jun 22, 2024: CUSP WEB. CRACKED. CRACKS WERE FOUND ON MEMBRANE OF PASSENGER CABIN AT CUSP WEB BTW STA 218/237 AND BTW STA X=-56/-22. SUMMARY OF NRC 00678: CUSP WEB BTW STA 218/237 AND BTW STA X
- [SDR DALA2024062406339](https://openairdocs.org/sdr/DALA2024062406339), Jun 21, 2024: FRAME. CRACKED. A.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF
- [SDR DALA2024062106294](https://openairdocs.org/sdr/DALA2024062106294), Jun 20, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL WAS FOUND ON STA Y=636 X=0 AT PAX CABIN. SUMMARY OF NRC 00838: CRACK ON INTERCOSTAL ON STA Y=636 X=0 AT PAX CABIN WAS REPAIRED PER B717-200
- [SDR DALA2024062006268](https://openairdocs.org/sdr/DALA2024062006268), Jun 19, 2024: BEAM. CRACKED. CRACK ON INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00685: INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR A
- [SDR DALA2024061806170](https://openairdocs.org/sdr/DALA2024061806170), Jun 17, 2024: SKIN. CRACKED. CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS
- [SDR DALA2024061606112](https://openairdocs.org/sdr/DALA2024061606112), Jun 15, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE. IN REFERENCE NRC 00604. SUMMARY OF NRC 00789: CORROSION LEVEL 2. FLOOR SUPPORT S
- [SDR DALA2024061606110](https://openairdocs.org/sdr/DALA2024061606110), Jun 14, 2024: CUSP WEB. CRACKED. CRACKS CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00610: CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=
- [SDR DALA2024061606109](https://openairdocs.org/sdr/DALA2024061606109), Jun 14, 2024: PAN. CRACKED. CRACK ON INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE. SUMMARY OF NRC 00686: INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE WAS 
- [SDR DALA2024061606108](https://openairdocs.org/sdr/DALA2024061606108), Jun 13, 2024: FRAME. DAMAGED. TOOL MARKS ON OVERWING FRAME STA737 L-18R AT WING BOX. SUMMARY OF NRC 00533: OVERWING FRAME STA737 L-18R AT WING BOX WAS REPAIRED PER PRI 618675-14 REV.0 AND ER
- [SDR DALA2024061306056](https://openairdocs.org/sdr/DALA2024061306056), Jun 13, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00791: CORROSION LEVEL 2, LH CUSP WEB STA Y=936-940 AND X=55 AT PASSEN
- [SDR DALA2023081606669](https://openairdocs.org/sdr/DALA2023081606669), Aug 15, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS IN ROWS 15-19 ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-120 TO BE INOPERATIVE AND REPLACED THE BATTERY PER B717 AMM 33-51. OPE
- [SDR DALA2023051803951](https://openairdocs.org/sdr/DALA2023051803951), May 15, 2023: UNKNOWN. UNKNOWN. SHIP 9567 -HYD/DE- THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID INDICATION WITH THE LEFT SYSTEM. THE QRH WAS COMPLIED WITH AND THE LEFT ENGINE DRIVEN HYDRA
- [SDR DALA2022112907614](https://openairdocs.org/sdr/DALA2022112907614), Nov 27, 2022: LENS. DETACHED. THE EXIT LENS COVER AT ROW 19 IS MISSING. MAINTENANCE REPLACED THE MISSING LENS COVER AT ROW 19. (LP #2513959)
- [SDR DALA2022032802027](https://openairdocs.org/sdr/DALA2022032802027), Mar 25, 2022: LONGERON. DAMAGED. SECOND DAMAGE AFTER CORROSION REMOVAL ON L29 LH BTW STA 900 TO STA 968 REMAINING THICKNESS IS OUT OF LIMITS. IN REFERENCE NRC 184. SUMMARY OF NRC 00252: CORROSI
- [SDR DALA2022032502000](https://openairdocs.org/sdr/DALA2022032502000), Mar 25, 2022: FRAME SPLICE. CORRODED. CORROSION ON REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: (CORROSION LEVEL 2) REPAIR SPLICE FRAME STA 1022
- [SDR DALA2022032401937](https://openairdocs.org/sdr/DALA2022032401937), Mar 23, 2022: UNKNOWN. UNKNOWN. CORROSION ON SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00196: CORROSION LEVEL 2, SPLICE OF STRINGER 30 STA=960 TO 975 AFT 
- [SDR DALA2022032201862](https://openairdocs.org/sdr/DALA2022032201862), Mar 21, 2022: NOT REPORTED. NOT REPORTED. SECONDARY DAMAGE AREAS WERE FOUND AT DENTS #8 & #10 ON INNER FACE OF REAR MOVABLE VANE AT LH WING. AREAS WERE FOUND DEBONDED (IN REF NRC 00060). SUMMARY OF NRC 
- [SDR DALA2022032101831](https://openairdocs.org/sdr/DALA2022032101831), Mar 20, 2022: NOT REPORTED. NOT REPORTED. CORROSION ON DOOR JAMB BTW STA 950 TO 1000 OF AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB OF AFT CARGO COMPARTMENT WAS REPAIR
- [SDR DALA2019082004881](https://openairdocs.org/sdr/DALA2019082004881), Aug 19, 2019: LENS. MISSING. THE FORWARD FACING LENS FROM THE CENTER AISLE EMERGENCY EXIT SIGN AT THE OVERWING EXIT IS MISSING. MAINTENANCE INSTALLED THE CENTER AISLE FORWARD FACING LENS AT
- [SDR DALA2019010400049](https://openairdocs.org/sdr/DALA2019010400049), Jan 4, 2019: SKIN. DAMAGED. THE LEFT HAND INBOARD FLAP LEADING EDGE WAS FOUND DAMAGED. NRC 010-0001:0514-2001/001 00011: REMOVED AFT VANE PER AMM 27-50-03. REMOVED NOSE ASSY AND ROUTED TO 
- [SDR DALA2018111206582](https://openairdocs.org/sdr/DALA2018111206582), Nov 11, 2018: LENS. MISSING. THE FIRST EMERGENCY LIGHT IN THE AFT ACCESSORY COMPARTMENT IS MISSING THE LENS COVER. MAINTENANCE HAS RE-INSTALLED THE COVER. LIGHT OPERATIONAL CHECK IS GOOD. (
- [SDR DALA2018091805644](https://openairdocs.org/sdr/DALA2018091805644), Sep 14, 2018: POWER SUPPLY. INOPERATIVE. ON A SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERHEAD CEILING EMERGENCY LIGHTS TURNING ON AND THEN OFF. MAINTENANCE REPLACED THE FORWARD TWO EMERGENCY LIGH
- [SDR DALA2017112008243](https://openairdocs.org/sdr/DALA2017112008243), Nov 19, 2017: LENS. MISSING. AFT EXIT DOOR CEILING LIGHT MISSING THE LENS. MAINTENANCE INSTALLED A NEW LENS.
- [SDR DALA201706301](https://openairdocs.org/sdr/DALA201706301), Jun 30, 2017: SKIN. DELAMINATED. DURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.
- [SDR DALA2017042603394](https://openairdocs.org/sdr/DALA2017042603394), Apr 25, 2017: FLOOR PANEL. CRACKED. CABIN FLOOR PANEL 223AF IS CORRODED IN SEVERAL AREAS AND CRACKED AT CORNER. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-20-50-01. STOP DRILLED TH
- [SDR DALA2017042403350](https://openairdocs.org/sdr/DALA2017042403350), Apr 23, 2017: PAN. CORRODED. CORROSION ON DOOR JAMB PAN AT LOWER CENTER DOOR STOP. BLENDED CORROSION ON ALC DOOR JAMB PAN AT LOWER CENTER DOOR STOP, REMOVED .020" OUT OF .050" ORIGINAL THIC
- [SDR DALA2017042303302](https://openairdocs.org/sdr/DALA2017042303302), Apr 21, 2017: FLOOR SUPPORT. CORRODED. UPPER CABIN FLOOR SUPPORTS BETWEEN STA 178 - 202 AT RBL 30-44 ARE CORRODED IN SEVERAL AREAS. REPLACE FLOOR SUPPORT RBL 30.00-44 PER SRM 51-41-02 & DRAWING 99365
- [SDR DALA2017042203299](https://openairdocs.org/sdr/DALA2017042203299), Apr 21, 2017: CUSP WEB. CORRODED. RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND UPPER AND LOWER SURFACES OF LIGHTENING HOLES. REPAIRED CUSP WEB AT STA 446 TO 465 IAW SRM 53-00-55-2R-4 SHEE
- [SDR DALA2017042203298](https://openairdocs.org/sdr/DALA2017042203298), Apr 21, 2017: CUSP WEB. CORRODED. RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND AROUND LOWER SURFACE OF LIGHTENING HOLES AT STA 484 TO 503. BLENDED CORROSION ON CUSP WEB AT FS 484-503R OT 

All 188: https://openairdocs.org/aircraft/N930AT/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/N930AT/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.