# N895AT: 2004 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: 55047
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 20, 2005
- Certificate issued: August 28, 2024
- Expires: August 31, 2031
- Mode S code: AC57F9
- 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=895AT
- Page: https://openairdocs.org/aircraft/N895AT

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/N895AT/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 N895AT.

## FAA accident and incident reports

None matched to N895AT.

## Service difficulty reports (104, 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 DALA2026100205473](https://openairdocs.org/sdr/DALA2026100205473), Oct 1, 2026: ANTI-SKID SYS. WARNING MESSAGE. ATO- DISCONTINUED TAKEOFF ROLL AT 25KTS AFTER RECEIVING AN ANTI-SKID FAIL MESSAGE. MAINTENANCE TROUBLESHOOT PER B717 FIM 32-45, NO MESSAGES AND ALL RETURN TO SE
- [SDR DALA2025120508916](https://openairdocs.org/sdr/DALA2025120508916), Dec 3, 2025: PITOT TUBE. FAULTED. ATB/DE- RETURNED ATL DUE TO RUDDER PITOT HEAT FAIL MESSAGE. REPLACED RUDDER LIMITER PITOT PROBE. MESSAGE CLEARED. OPS CHECK GOOD.(7974434)
- [SDR DALA2025052203940](https://openairdocs.org/sdr/DALA2025052203940), May 16, 2025: WIRE. BROKEN. SHIP 9555-SMKE/FUME- CREW REPORTED ON FINAL THE FWD F/A SMELLED SMOKE FROM FWD LAV AND REPORTED SPARKS. CORRECTIVE ACTION: MAINTENANCE REPAIRED A BROKEN WIRE AT
- [SDR DALA2025042103071](https://openairdocs.org/sdr/DALA2025042103071), Apr 16, 2025: SKIN. CRACKED. DAMAGE T: CRACK ON FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30. SUMMARY OF NRC 00136: FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30 WAS REPAIRED P
- [SDR DALA2025040902759](https://openairdocs.org/sdr/DALA2025040902759), Apr 8, 2025: SKIN. CRACKED. CRACKS ON SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00013: SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 625399-14 
- [SDR DALA2025050603513](https://openairdocs.org/sdr/DALA2025050603513), Apr 6, 2025: PIN. MISINSTALLED. INSPECTION FOUND THAT THE RELEASE CAM PIN WAS INSTALLED INCORRECTLY AND THAT AN ADJUSTMENT WAS NEEDED ON THE TAIL CONE DEPLOYMENT SYSTEM. THIS COULD PREVENT THE
- [SDR DALA2024112611228](https://openairdocs.org/sdr/DALA2024112611228), Nov 25, 2024: SLIDE. OUT OF POSITION. ON WAKE-UP CHECK FOUND THE AFT TAIL CONE SLIDE PACK HAD ROTATED OUT OF SECURED POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NO
- [SDR DALA2024092509408](https://openairdocs.org/sdr/DALA2024092509408), Sep 24, 2024: BATTERY PACK. INOPERATIVE. FOUND THE LEFT FORWARD ENTRY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51. OPERA
- [SDR DALA2023122810696](https://openairdocs.org/sdr/DALA2023122810696), Dec 26, 2023: UNKNOWN. UNKNOWN. DURING SERVICE CHECK FOUND R1 EMERGENCY SLIDE BOTTLE PRESSURE UNSERVICEABLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIA
- [SDR DALA2023052304103](https://openairdocs.org/sdr/DALA2023052304103), May 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON SKIN STA Y=214 BTW STR 28R AND STR 29R AT (E/E). SUMMARY OF NRC 00458: CORROSION LEVEL 2. SKIN STA Y=214 BTW STR 28R AND STR 29R WAS REPAIRED PER E
- [SDR DALA2023052504149](https://openairdocs.org/sdr/DALA2023052504149), May 22, 2023: UNKNOWN. UNKNOWN. BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. FWD PASSENGER ENTRANCE SERVICEABLE DOOR REMOVED. SUMMARY OF NRC 00682: PASSENGER FORWARD ENTRANCE 
- [SDR DALA2023052304102](https://openairdocs.org/sdr/DALA2023052304102), May 20, 2023: UNKNOWN. UNKNOWN. BENT AND CRACK TWO SECTIONS ON L1 DOOR SKIN LOWER EDGE. PTAS. SUMMARY OF NRC 00090: PASSENGER ENTRANCE DOOR WAS REPLACED FOR SERVICIABLE PASSENGER ENTRANCE DOOR
- [SDR DALA2023052204052](https://openairdocs.org/sdr/DALA2023052204052), May 20, 2023: UNKNOWN. UNKNOWN. SHEARED OUT AND ELONGATED HOLE ON SKIN, CLOSE TO HINGE #1 OH CONTROL TAB AT RH ELEVATOR STA XE=17 HVS. SUMMARY OF NRC 00339: SKIN, CLOSE TO HINGE #1 OH CONTROL 
- [SDR DALA2023052004042](https://openairdocs.org/sdr/DALA2023052004042), May 19, 2023: UNKNOWN. UNKNOWN. CRACK ON FWD STOP FITTING AT AFT CARGO COMPARTMENT DOOR, (PTAS). SUMMARY OF NRC 00205: AFT CARGO DOOR WAS REPLACED FOR SERVICEABLE AFT CARGO DOOR. (LP #2773786)
- [SDR DALA2024112511161](https://openairdocs.org/sdr/DALA2024112511161), May 16, 2023: SKIN. NO DISCREPANCY. REPAIR TO FUSELAGE SKIN & DOUBLER AT STA Y=1037 B/W L-13L & L-14L IS PENDING DTE STAGE II & III APPROVAL WITHIN 24 MONTHS OF 12MAY23. DISCONTINUE REVENUE SERVIC
- [SDR DALA2023051703947](https://openairdocs.org/sdr/DALA2023051703947), May 16, 2023: UNKNOWN. UNKNOWN. CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH (FUS). SUMMARY OF NRC 00512: EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13LH & 14LH WAS REPAIRED
- [SDR DALA2023051603855](https://openairdocs.org/sdr/DALA2023051603855), May 14, 2023: UNKNOWN. UNKNOWN. WEAR ON FWD SEAL RETAINER AREA AFT CARGO DOOR (PTAS). SUMMARY OF NRC 00081: REPAIR ANGLE AT SEAL RETAINER AREA WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDU
- [SDR DALA2023051203748](https://openairdocs.org/sdr/DALA2023051203748), May 11, 2023: UNKNOWN. UNKNOWN. DURING ATENTION OF NRC 00192, AFTER REMOVE CORROSION, LONGERON 30 FROM STA Y=908 TO Y=927 WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00550: CORROSION LEVEL 2. LONG
- [SDR DALA2023051003664](https://openairdocs.org/sdr/DALA2023051003664), May 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SURFACE BTW STA Y=370-427 AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00202: CORROSION LEVEL 2. DOOR LOWER JAMB PAN WAS REPAIRED PER B
- [SDR DALA2023050803569](https://openairdocs.org/sdr/DALA2023050803569), May 7, 2023: UNKNOWN. UNKNOWN. WEAR ON ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT STOWAGE AREA AT AFT CABIN BULKHEAD DOOR (PTAS). SUMMARY OF NRC 00184: ANGLES (2 EA) OF FLIGHT ATTENDANT SEAT AT A
- [SDR DALA2023050803567](https://openairdocs.org/sdr/DALA2023050803567), May 6, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR PANEL STRAP AND FITTINGS AT R1 ENTRY CPAX. SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR PANEL STRAP AND FITTINGS WERE REPLACED PER DGW 9957
- [SDR DALA2023050803566](https://openairdocs.org/sdr/DALA2023050803566), May 6, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1021 LONG 7 LH PAX CABIN (CPAX). SUMMARY OF NRC 00312: FRAME STA 1021 LONG 7 LH WAS REPAIRED PER ER/A 607808-14 REV. ORIGINAL SECTION I: PERM
- [SDR DALA2023050803565](https://openairdocs.org/sdr/DALA2023050803565), May 5, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA (SM). SUMMARY OF NRC 00295: FRAMES STA Y=674 & Y=696 AT LH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 
- [SDR DALA2023050803564](https://openairdocs.org/sdr/DALA2023050803564), May 5, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA (SM). SUMMARY OF NRC 00296: FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 
- [SDR DALA2023050803563](https://openairdocs.org/sdr/DALA2023050803563), May 5, 2023: UNKNOWN. UNKNOWN. CRACKED LONGERON 2 RH/LH ON STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00417: LONGERON 2 RH/LH ON STA Y=1133 WERE REPAIRED PER B717-200 SRM 53-00-0
- [SDR DALA2023050803562](https://openairdocs.org/sdr/DALA2023050803562), May 4, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH SIDE AT PASSENGER CABIN. SUMMARY OF NRC 00415: CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) R
- [SDR DALA2023050403460](https://openairdocs.org/sdr/DALA2023050403460), May 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 AT PAX CABIN. SUMMARY OF NRC 00623: CORROSION LEVEL 2. RH CUSP WEB STA Y=474, Y=
- [SDR DALA2023050303432](https://openairdocs.org/sdr/DALA2023050303432), May 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND Y=952-953 AND CUSP WEB STA Y=952-953 AND 975-976 RH SIDE AT PAX CABIN IN REF NRC S/N 403. SUMM
- [SDR DALA2023050303431](https://openairdocs.org/sdr/DALA2023050303431), May 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP WEB ON LIGHTENING HOLE UPPER SIDE ALSO LOWER SIDE STA Y=633, STA Y=670, AND STA Y=810 AT CABIN PAX FLOOR SRTUCTURE. FUS. IN REF NRC 0402. S
- [SDR DALA2023050203396](https://openairdocs.org/sdr/DALA2023050203396), May 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEB SPLICE LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59. SUMMARY OF NRC 00408: CORROSION LEVEL 2. RH CUSP WEB SPLICE UPPER AND 
- [SDR DALA2023050203392](https://openairdocs.org/sdr/DALA2023050203392), Apr 29, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX (CPAX). SUMMARY OF NRC 00592: INTERCOSTAL BTW STA Y=1002 TO Y=1022 AND X=0 AT CABIN PAX WAS R
- [SDR DALA2023042803323](https://openairdocs.org/sdr/DALA2023042803323), Apr 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON FORWARD STAIRWELL DOOR INTERNAL SKIN AND RUSTED HARDWARE WERE FOUND IN REFERENCE TO NRC 00256. SUMMARY OF NRC 00577: CORROSION LEVEL 2. FORWARD STA
- [SDR DALA2023042803321](https://openairdocs.org/sdr/DALA2023042803321), Apr 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP WEB UPPER SIDE STA Y=421 ALSO STA Y=468 TO Y=471 IN REF NRC 00401. SUMMARY OF NRC 00614: CORROSION LEVEL 2. LH CUSP WEB STA Y=421 ALSO STA 
- [SDR DALA2023042803320](https://openairdocs.org/sdr/DALA2023042803320), Apr 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON SETLEMENT ON INBD SEAT TRACK STA 196 TO 200 RBL 20 AT PAX CABIN. W1. SUMMARY OF NRC 00503: CORROSION LEVEL 2. SECTION SEAT TRACK STA 196 TO 265 RBL
- [SDR DALA2023042603249](https://openairdocs.org/sdr/DALA2023042603249), Apr 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200 LBL 44 & 54 AT PAX CABIN. (W1). SUMMARY OF NRC 00526: CORROSION LEVEL 2. FLOOR SUPPORTS FROM STA Y=157 TO Y=
- [SDR DALA2023042603247](https://openairdocs.org/sdr/DALA2023042603247), Apr 25, 2023: UNKNOWN. UNKNOWN. CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 R
- [SDR DALA2023042603246](https://openairdocs.org/sdr/DALA2023042603246), Apr 25, 2023: UNKNOWN. UNKNOWN. CRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 R
- [SDR DALA2023042703289](https://openairdocs.org/sdr/DALA2023042703289), Apr 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN FLOOR STRUCTURE. W1. SUMMARY OF NRC 597: CORROSION LEVEL 2. GALLEY SUPPORT STA 218 RBL 11 AT PAX CABIN F
- [SDR DALA2023042703288](https://openairdocs.org/sdr/DALA2023042703288), Apr 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA Y=198 LBL 57 AT PAX CABIN FLOOR SUPPORT. CPAX. SUMMARY OF NRC 00596: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=198 LBL 57 AT PAX CA
- [SDR DALA2023042503241](https://openairdocs.org/sdr/DALA2023042503241), Apr 24, 2023: UNKNOWN. UNKNOWN. CRACKED FRAME STA Y=1037 LONG 17 LH AT PAX CABIN (W2). SUMMARY OF NRC 00553: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM. 53-20-07-2R PROCEDURE 4 
- [SDR DALA2023042503239](https://openairdocs.org/sdr/DALA2023042503239), Apr 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS FROM STA Y=157 TO Y=200, LBL 7, RBL 7, RBL 44, & RBL 53 AT PAX CABIN (W1). SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORTS (
- [SDR DALA2023042103142](https://openairdocs.org/sdr/DALA2023042103142), Apr 20, 2023: UNKNOWN. UNKNOWN. DURING REMOVED FLOOR SUPPORT FROM STA Y=157 TO STA Y=200 & LBL 54 AT PAX CABIN (2EAS) CORROSION ON WEB WAS FOUND IN REFERENCE TO NRC 00526. SUMMARY OF NRC 00580
- [SDR DALA2023042103140](https://openairdocs.org/sdr/DALA2023042103140), Apr 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON SPLICES 29L AND 29RH, INTERNAL STRUCTURE AFT FUSELAGE STA 1110 TO 1120 APROX. SUMMARY OF NRC 00327: CORROSION LEVEL 2. LONGERON SPLICES 29
- [SDR DALA2023042003111](https://openairdocs.org/sdr/DALA2023042003111), Apr 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS AT STA Y=177 FROM RBL 10 TO RBL 43 AND STA Y=200 FROM RBL 10 TO RBL 43 IN REF NRC 0522. SUMMARY OF NRC 00595: CORROSION LEVEL 2. FLO
- [SDR DALA2023041803051](https://openairdocs.org/sdr/DALA2023041803051), Apr 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 AT PAX CABIN. SUMMARY OF NRC 00507: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=1026 AND Y=1056 LBL 46 WAS RE
- [SDR DALA2020062202492](https://openairdocs.org/sdr/DALA2020062202492), Jun 20, 2020: POWER SUPPLY. INOPERATIVE. THE EMERGENCY LIGHTS AT WING EXIT DOORS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IN REFERENCE TO B717 AMM 33-51. OPERATIONAL 
- [SDR DALA2019111866741](https://openairdocs.org/sdr/DALA2019111866741), Nov 15, 2019: PRESSURE BLKHD. DAMAGED. HOLE IN PRESSURE DOME BELOW THE NOSE LANDING GEAR ACTUATOR. NRC 001-0270:5300-2001/001 00014: COMPLIED WITH ER/A 582891-14 REV O. (LP #1361132)
- [SDR DALA2023050903612](https://openairdocs.org/sdr/DALA2023050903612), Nov 14, 2019: UNKNOWN. UNKNOWN. FUSELAGE BULKHEAD STA 110 LBL 14 WEB DAMAGE. REPAIR APPROVAL IS LIMITED TO THE NEXT C-CHECK (NOT TO EXCEED 24 MONTHS) SERVICE FROM DATE OF APPROVAL ONLY. ADDITI
- [SDR DALA2019111106536](https://openairdocs.org/sdr/DALA2019111106536), Nov 8, 2019: THRESHOLD. CORRODED. FOUND CORROSION IN C-2 THRESHOLD AREA. NRC 001-0262:5300-2016/001 00011: CORROSION LEVEL 1, MAINTENANCE REPLACED THE DOOR JAMB PAN REF B717 SRM 53-20-15-2R PROC
- [SDR DALA2019092305440](https://openairdocs.org/sdr/DALA2019092305440), Sep 22, 2019: BATTERY PACK. DISCHARGED. THE OVERWING EMERGENCY ESCAPE LIGHTS WILL TURN ON WHEN THE SWITCH IS TURNED OFF. MAINTENANCE REPLACED THE OVERWING EMERGENCY ESCAPE LIGHTING BATTERY PACK IAW AM

All 104: https://openairdocs.org/aircraft/N895AT/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/N895AT/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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