# N922AT: 2005 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55050
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 25, 2005
- Certificate issued: August 28, 2024
- Expires: August 31, 2031
- Mode S code: ACC5AA
- 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=922AT
- Page: https://openairdocs.org/aircraft/N922AT

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 Rolls-Royce 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 (Rolls-Royce 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/N922AT/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 N922AT.

## FAA accident and incident reports

None matched to N922AT.

## Service difficulty reports (137, 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 DALA2026080404490](https://openairdocs.org/sdr/DALA2026080404490), Jul 31, 2026: UNKNOWN. ODOR. BURNING ODOR SOMEWHERE IN FIRST CLASS AND COMFORT PLUS SECTION. APU COMPARTMENT VENT HAS ODOR AS WELL. INSPECCTED IDG AND CLEAN AND BURNOUT OF BOTH PACKS A/C GO
- [SDR DALA2026071704220](https://openairdocs.org/sdr/DALA2026071704220), Jul 14, 2026: GLOWSTRIP. MISSING. ESCAPE PATH PHOTOLUMINESCENT STRIP MISSING 2" AT 17L, R & R STRIP IAW IPC 33-51-12-01. (8815309) (AIRCRAFT GROUNDED).
- [SDR DALA2025071405285](https://openairdocs.org/sdr/DALA2025071405285), Jul 12, 2025: ENGINE. FAULTED. SHIP 9558 - RTO - CREW REPORTED WITH AUTO-THROTTLE ENGAGED AT 60KNTS RIGHT THROTTLE RETARDED. P30 FAULT, INSPECTED FOR LEAKS/BLOCKAGE WITH NO FINDINGS. REPLACED
- [SDR DALA2025062504753](https://openairdocs.org/sdr/DALA2025062504753), Jun 23, 2025: PUSHROD. NOT REPORTED. ATB, RETURNED TO ATL DUE TO A FLAP INDICATION ISSUE. REPLACED DAMAGED FLAP CONTROL PUSHROD.
- [SDR DALA2025050503411](https://openairdocs.org/sdr/DALA2025050503411), May 1, 2025: HANDLE. DAMAGED. THE CABIN CREW REPORTS THAT THE 1L DOOR INTERIOR HANDLE ROTATES FREELY WITHOUT OPENING THE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND 
- [SDR DALA2024120911543](https://openairdocs.org/sdr/DALA2024120911543), Dec 4, 2024: BATTERY. INOPERATIVE. BOTH OVER-WING EMERGENCY EXIT LIGHTS ARE OUT. ALL OTHER EMERGENCY LIGHTS ARE GOOD. MAINTENANCE REPLACED THE OVER-WING EMERGENCY LIGHT BATTERY PER B717 AMM 31-51
- [SDR DALA2024080507765](https://openairdocs.org/sdr/DALA2024080507765), Aug 3, 2024: BATTERY PACK. NO TEST. FORWARD SMALLER EMERGENCY LIGHTS ARE INOPERATIVE AT DOORS 1LT & 1RT. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT LOCATION B5-118 IAW B717 AMM 33-51. OPERATION
- [SDR DALA2024072507459](https://openairdocs.org/sdr/DALA2024072507459), Jul 24, 2024: PANEL. DAMAGED. DURING PILOT PRE-FLT WALKAROUND, NOTICED DAMAGE TO THE #2 ENGINGE UPPER THRUST REVERSER PANEL. 6-8 FOOT SECTION OF PANEL WAS MISSING. MAINTENANCE REPLACED THE #
- [SDR DALA2024050304923](https://openairdocs.org/sdr/DALA2024050304923), May 3, 2024: BATTERY PACK. FAULTED. EXIT LIGHT OVER 1R DOOR AND EXIT LIGHT IN FRIST CLASS CABIN INTERMITIELY FLASHING. REPLACE THE EMERGENCY BATTERY & POWER SUPPLY UNIT LOCTION AT 247L PER B717 AM
- [SDR DALA2024052005348](https://openairdocs.org/sdr/DALA2024052005348), May 1, 2024: FLAP SYSTEM. MALFUNCTIONED. SHIP 9558 -MISC/DE- FLIGHT TEST. EXPERIMENTAL TEST FLIGHT FOR FLAP 25 LANDINGS. FLIGHT PLANNED FOR ATL-HSV-ATL. BOEING TEST ENGR/PILOT IN LEFT SEAT AND DELTA LL
- [SDR DALA2023082907003](https://openairdocs.org/sdr/DALA2023082907003), Aug 28, 2023: UNKNOWN. UNKNOWN. DURING THE INSPECTION OF EXTERIOR LIGHTS, DISCOVERED THAT THE EXTERIOR EMERGENCY LIGHTS DO NOT TURN ON. SUMMARY OF NRC 00593: EMERGENCY LIGHTING PROBLEM FAULT I
- [SDR DALA2023082806937](https://openairdocs.org/sdr/DALA2023082806937), Aug 26, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00063: PAN OF FWD UPPER CORNER AT PASSENGER DOOR L1 WAS REPLACED PER B717-200 SRM 51-41-01-
- [SDR DALA2023082406884](https://openairdocs.org/sdr/DALA2023082406884), Aug 22, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL STRUCTURE AT AFT CARGO DOOR. SUMMARY OF NRC 00072: INTERNAL STRUCTURE AT AFT CARGO DOOR WAS REPAIRED PER ERA 610790-14 REV ORIGINAL. SECTION I
- [SDR DALA2023082106760](https://openairdocs.org/sdr/DALA2023082106760), Aug 19, 2023: UNKNOWN. UNKNOWN. DENT #9 OUT OF LIMITS ON LOWER SURFACE OF AFT MOVABLE FLAP VANE AT RH WING. SEPARATE ITEMS ON NRC 00101. SUMMARY OF NRC 563: DENT #9 ON LOWER SURFACE OF AFT MOV
- [SDR DALA2023080906492](https://openairdocs.org/sdr/DALA2023080906492), Aug 8, 2023: UNKNOWN. UNKNOWN. CRACK ON DOUBLER AND FILLER DOOR JAMB AT FWD CARGO DOOR. SUMMARY OF NRC 00084: REPAIR DOUBLER ON AFT INNER PAN SECTION DOOR JAMB AT FWD CARGO DOOR WAS REPLACED 
- [SDR DALA2023080906491](https://openairdocs.org/sdr/DALA2023080906491), Aug 8, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB BTW STA 715 AND STA 737 LH SIDE (CPAX). SUMMARY OF NRC 00271: CUSP WEB BTW STA 715 AND STA 737 LH SIDE (CPAX) WAS REPAIRED PER B717-200 SRM 53
- [SDR DALA2023080806437](https://openairdocs.org/sdr/DALA2023080806437), Aug 5, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL AT FLOOR SUPPORTS RH SIDE: #1 FROM STA Y=148 TO STA Y=200 AND - X7, #4 FROM STA Y=180 AND -X26, AND #6 FROM STA Y=160 TO STA Y=200 AND -
- [SDR DALA2023080706370](https://openairdocs.org/sdr/DALA2023080706370), Aug 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON CHANNEL AT GENERATION FLOOR 221SF OF PAX CABIN. SUMMARY OF NRC 00350: CHANNEL (PANEL) OF GENERATION FLOOR 221SF AT PAX CABIN WAS FABRICATED AND REP
- [SDR DALA2023080706369](https://openairdocs.org/sdr/DALA2023080706369), Aug 5, 2023: UNKNOWN. UNKNOWN. CRACK ON ATTACH ANGLE APPROX STA 1178 CANT BTW LONGERON 1LH AND LONGERON 3LH AT EMPENNAGE AREA. SUMMARY OF NRC 00035: REPAIR ON ATTACH ANGLE APPROX STA 1178 CAN
- [SDR DALA2023080706368](https://openairdocs.org/sdr/DALA2023080706368), Aug 5, 2023: UNKNOWN. UNKNOWN. CRACKS ON UPPER FWD CORNER STA Y=756, LOWER FWD CORNERS STA Y=794, Y=851, Y=908, AND UPPER AFT CORNERS STA Y=832, Y=870, Y=889 OF LH RING PANS AT INNER STRUCTUR
- [SDR DALA2023080706367](https://openairdocs.org/sdr/DALA2023080706367), Aug 5, 2023: UNKNOWN. UNKNOWN. CRACKS ON UPPER AFT CORNERS STA Y=636, Y=696 , Y=832 AND LOWER AFT CORNER STA Y=870 OF RH RING PANS AT INNER STRUCTURE OF PAX CABIN. SUMMARY OF NRC 00309: REPAI
- [SDR DALA2023080706366](https://openairdocs.org/sdr/DALA2023080706366), Aug 5, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB BTW STA 696 AND STA 715 LH SIDE (CPAX). SUMMARY OF NRC 00272: CUSP WEB BTW STA 696 AND STA 715 LH SIDE (CPAX) WAS REPAIRED PER B717-200 SRM 53
- [SDR DALA2023080706363](https://openairdocs.org/sdr/DALA2023080706363), Aug 4, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON STA=994 TO STA=1053. ORIGINAL THICKNESS OF 0.052 IN. AND MINIMUM REMAINING THICKNESS IS 0.009 IN ON SIDE PARTS, THEREFORE AREAS ARE O
- [SDR DALA2023080706361](https://openairdocs.org/sdr/DALA2023080706361), Aug 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOORS SUPPORTS (9 EA) LH SIDE: #1 FROM STA Y=160 TO STA Y=197 AND +X=55, #2 FROM STA Y=200 AND +X 55, #3 FROM STA Y=186 TO STA Y=195 AND +X=52, #4
- [SDR DALA2023080406302](https://openairdocs.org/sdr/DALA2023080406302), Aug 4, 2023: UNKNOWN. UNKNOWN. HOLE AT UPPER SKIN AND PROTUBERANCE AT LOWER SKIN OF RH ELEVATOR BETWEEN XHS 122.241 AND XHS 104.000 (ER/A RELATED 610064-14). SUMMARY OF NRC 00460: UPPER SKIN 
- [SDR DALA2023080106212](https://openairdocs.org/sdr/DALA2023080106212), Aug 1, 2023: UNKNOWN. UNKNOWN. DENT ON LOWER SURFACE OF AFT MOVABLE VANE AT LH FLAP. SUMMARY OF THE NRC 00359: AFT MOVABLE VANE AT LH FLAP WAS REMOVED PER B717 AMM 27-50-03 AND DENT REPAIRED 
- [SDR DALA2023080106206](https://openairdocs.org/sdr/DALA2023080106206), Jul 30, 2023: UNKNOWN. UNKNOWN. CRACKS ON STRINGERS 6LH, 8LH AND 6RH STA Y=1022 AT INTERNAL FUSELAGE (PAX CABIN). SUMMARY OF NRC 00153: REPAIR ON STRINGERS 6LH, 8LH AND 6RH STA Y = 1022 AT INT
- [SDR DALA2023083107082](https://openairdocs.org/sdr/DALA2023083107082), Jun 30, 2023: UNKNOWN. UNKNOWN. AD RELATED. FERRY FLIGHT ER/A 610173-14 REMOVES ALL PAX SEATS FROM A/C AND TRACKS ACCOMPLISHEMENT OF PERMANENT REPAIR. ASSOCIATED ER/A 14-610173 ADDED FOR AC 95
- [SDR DALA2019090305121](https://openairdocs.org/sdr/DALA2019090305121), Sep 2, 2019: POWER SUPPLY. INOPERATIVE. THE THREE (3) AFT ACCESSORY SIDEWALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY B5-116 PER AMM 33- 51 AND RELAMPED AS NEEDE
- [SDR DALA2019090305120](https://openairdocs.org/sdr/DALA2019090305120), Sep 2, 2019: POWER SUPPLY. INOPERATIVE. THE AFT EMERGENCY LIGHT ABOVE AFT F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY B5-116 PER AMM 33- 51 AND RELAMPED AS NEEDED. OPERATION
- [SDR DALA2019072304372](https://openairdocs.org/sdr/DALA2019072304372), Jul 22, 2019: BATTERY PACK. DISCHARGED. THE EMERGENCY EXIT SIGNS ABOVE 1L DOOR, 1L F/A SEAT, 1R DOOR, AND CENTER AISLE 1 ABCD ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK
- [SDR DALA2019060303373](https://openairdocs.org/sdr/DALA2019060303373), May 30, 2019: LENS. DAMAGED. THRESHOLD LIGHT LENS COVER DAMAGED ABOVE AFTJUMPSEAT. FORWARD TO MEL 33-52-01. PLACARDS INSTALLED. R&R LENS COVER IAW B717 AMM 33-25. OK FOR SERVICE. MCO/PLAC R
- [SDR DALA2019051503027](https://openairdocs.org/sdr/DALA2019051503027), May 14, 2019: CLAMP. DISCONNECTED. THE AFT EMERGENCY EXIT LIGHT SPONTANEOUSLY COMES ON AND OFF. IT WAS ALSO NOTED THAT THERE IS WATER IN THAT AREA OF THE CEILING. MAINTENANCE FOUND A DRAIN LINE H
- [SDR DALA2019012200395](https://openairdocs.org/sdr/DALA2019012200395), Jan 20, 2019: LENS. MISSING. EMERGENCY EXIT COVER DIFFUSER LENS MISSING AT 604 INTERIOR. RE-INSTALLED DIFFUSER LENS AT ROW 20. (LP #0911582)
- [SDR DALA2019010700050](https://openairdocs.org/sdr/DALA2019010700050), Jan 3, 2019: NOT REPORTED. MALFUNCTIONED. ON TAKEOFF WE RECEIVED A "GEAR DOOR OPEN" ALERT WITH GEAR HANDLE IN THE UP POSITION. ALSO A "LEFT GEAR UNSAFE" RED LIGHT WAS ILLUMINATED. NO SOUNDS OR VIBRATION
- [SDR DALA2018123197451](https://openairdocs.org/sdr/DALA2018123197451), Dec 27, 2018: POWER SUPPLY. MALFUNCTIONED. IN FLIGHT AFT EXIT SIGN FLASHING. ON GROUND LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED AFT EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PER B717 AMM 33-51. TEST W
- [SDR DALA2018122607395](https://openairdocs.org/sdr/DALA2018122607395), Dec 24, 2018: BATTERY PACK. INOPERATIVE. THE AFT EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOO
- [SDR DALA2018110606453](https://openairdocs.org/sdr/DALA2018110606453), Nov 5, 2018: SKIN. CRACKED. THE VERTICAL STAB LEADING EDGE SKIN COMMON TO THE RHS FRONT SPAR IS CRACKED COMMON TO THE 2ND FASTENER HOLE AS SEEN IN FIG 1. AN EXISTING EXTERNAL REPAIR IS INS
- [SDR DALA2018110606452](https://openairdocs.org/sdr/DALA2018110606452), Nov 5, 2018: FRAME. CRACKED. OVERWING FRAME AT STA Y=674.0 RH SHOWS CRACK GREATER THAN 0.125 DURING GVI. NRC 040-0003:5310-01436-01C/001 00021 FRAME REPLACEMENT ON AMDS CARD 5310-01436-03B 
- [SDR DALA20181106450](https://openairdocs.org/sdr/DALA20181106450), Nov 2, 2018: LONGERON. NONE. CUT LONGERON 11RT AT APPROX. STA 668 FOR FRAME REMOVAL. NRC 040-0003:5310-01436-01C/002 00153: REPAIRED REF ER/A 530437-14MA REV O. (LP #0810425)
- [SDR DALA2018061804045](https://openairdocs.org/sdr/DALA2018061804045), Jun 17, 2018: BATTERY PACK. INOPERATIVE. THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHTS BATTERY PACK AND CHARGER IAW AMM 33-51-06. OPS
- [SDR DALA2018051503326](https://openairdocs.org/sdr/DALA2018051503326), May 14, 2018: POWER SUPPLY. MALFUNCTIONED. THE OUTSIDE WING EMERGENCY LIGHTS REMAIN ILLUMINATED AFTER TESTING. MAINTENANCE REPLACED THE THE OVERWING LIGHTS POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD
- [SDR DALA2018041602478](https://openairdocs.org/sdr/DALA2018041602478), Apr 15, 2018: SWITCH. INTERMITTENT. THE UPPER EMERGENCY LIGHTS AT 20DC AND 20B WERE FOUND TO BE INOPERATIVE. MAINTENANCE CYCLED THE EMERGENCY SWITCH AND ALL OPERATIONS CHECKED NORMAL.
- [SDR DALA2018032601905](https://openairdocs.org/sdr/DALA2018032601905), Mar 26, 2018: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT SIGN ABOVE L1 F/A SEAT IS INOPERATIVE. MAINTENANCE TROUBLESHOT IAW ASM 33-51-0 AND REPLACED THE B5-235 BATTERY PACK IAW AMM 33-51. SYSTEM CHE
- [SDR DALA2018022601170](https://openairdocs.org/sdr/DALA2018022601170), Feb 26, 2018: POWER SUPPLY. DEFECTIVE. THE TAIL CONE EMERGENCY EXIT LIGHT ILLUMINATED ON THE GROUND UNCOMMANDED. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY EXIT LIGHT POWER SUPPLY PER AMM 33-51. TH
- [SDR DALA2017111308078](https://openairdocs.org/sdr/DALA2017111308078), Nov 12, 2017: POWER SUPPLY. INOPERATIVE. AFT ACCESSORY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-260 IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA2017042703415](https://openairdocs.org/sdr/DALA2017042703415), Apr 26, 2017: LENS. MISSING. EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 19C. FLOOR MOUNTED LIGHTING ALL OK. OVERHEAD EMERGENCY LIGHT AT ROW 19 MISSING LENS, INSTALLED LENS
- [SDR 2017FAA123000019](https://openairdocs.org/sdr/2017FAA123000019), Dec 30, 2016: SKIN. DELAMINATED. DURING UNSCHEDULE MAINTENANCE CHECK L/H O/B SPOILER FOUND DELAMINATED.
- [SDR DALA2016111608846](https://openairdocs.org/sdr/DALA2016111608846), Nov 15, 2016: LENS. BROKEN. THE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS BROKEN. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2016111108709](https://openairdocs.org/sdr/DALA2016111108709), Nov 10, 2016: SKIN. CRACKED. CRACK IN SKIN AT TOP FASTENER AT STA 1152 JUST BELOW DORSAL FIN ON RIGHT SIDE. REPAIRED SKIN CRACK AT STA 1152 RT IAW ER/A 549635-14 REV 0.

All 137: https://openairdocs.org/aircraft/N922AT/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/N922AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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