# N894AT: 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: 55046
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 18, 2004
- Certificate issued: August 28, 2024
- Expires: August 31, 2031
- Mode S code: AC5442
- 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=894AT
- Page: https://openairdocs.org/aircraft/N894AT

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/N894AT/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 CEN13LA004](https://openairdocs.org/ntsb/CEN13LA004), Oct 5, 2012: Boeing 717-200 (N894AT), Milwaukee, WI, substantial damage. Probable cause: An obstruction (a sleeve of cups) that lodged under the catering truck brake pedal, which prevented the driver from stopping the truck before it struck the parked airplane.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20121004022789A](https://openairdocs.org/incident/20121004022789A), Oct 4, 2012: Boeing 717-200 (N894AT), Milwaukee, WI, Substantial damage. On oct. 04, 2012 at approximately 2010 CDT, a catering truck owned by airtran airways and operated by an aerotek aviation employee came into contact with…

## Service difficulty reports (119, 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 DALA2024071807236](https://openairdocs.org/sdr/DALA2024071807236), Jul 13, 2024: COAX. LOOSE. SHIP 9554 -ATO- THE FLIGHT CREW ABORTED THE TAKEOFF AT 130 KTS DUE TO THE #1 PRIMARY FLIGHT DISPLAY AND MULTI-FUNCTIONAL DISPLAY BLANKING OUT. CORRECTIVE ACTION
- [SDR DALA2023092207784](https://openairdocs.org/sdr/DALA2023092207784), Sep 21, 2023: UNKNOWN. UNKNOWN. DOOR R1 EXIT SIGN IS MISSING. MAINTENANCE REPLACED AND INSTALLED THE MISSING LENS COVER IAW B717 AMM 33-51. LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK
- [SDR DALA2023071805821](https://openairdocs.org/sdr/DALA2023071805821), Jul 18, 2023: UNKNOWN. UNKNOWN. CRACKS ON LH CUSP WEB AROUND RING BTW STA 652 AND 655. SUMMARY OF NRC 00668: LH CUSP WEB AROUND RING BTW STA 652 AND 655 WAS REPAIRED PER B717 SRM 53-00-55-2R-4
- [SDR DALA2025013000727](https://openairdocs.org/sdr/DALA2025013000727), Mar 15, 2023: SKIN. CORRODED. -AD- CENTER WING BOX LOWER SKIN XCW=20 TO XCW=42 REAR SPAR TO STRINGER #12 HAS CORROSION AND ELONGATED HOLES. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 14MAR
- [SDR DALA2023031401845](https://openairdocs.org/sdr/DALA2023031401845), Mar 9, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON FWD PASSENGER DOOR STAIRWELL INTERNAL STRUCTURE IN REF NRC 2060-1001. SUMMARY OF NRC 00572: CORROSION LEVEL 2. FWD PASSENGER DOOR STAIRWE
- [SDR DALA2023030201555](https://openairdocs.org/sdr/DALA2023030201555), Mar 1, 2023: NONE. NONE. SKIN PANELS BTW STA 954 TO STA 974 LONG 30 TO R29 ARE CORRODED OUT OF LIMITS. WITH ORIGINAL THICKNESS OF 0.071 IN. AND THE MAXIMUM REMOVED MATERIAL FOUND IS 0.0
- [SDR DALA2023030101525](https://openairdocs.org/sdr/DALA2023030101525), Feb 27, 2023: NONE. NONE. SEVERAL DENTS ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING (AI). SUMMARY OF NRC 00160: DENTS (26 EAS) ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING
- [SDR DALA2023022401415](https://openairdocs.org/sdr/DALA2023022401415), Feb 22, 2023: NONE. NONE. CORROSION ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 (CPAX)( W1). SUMMARY OF NRC 00425: CORROSION LEVEL 2. CORROSION WAS REMOV
- [SDR DALA2023022401414](https://openairdocs.org/sdr/DALA2023022401414), Feb 22, 2023: NONE. NONE. CRACK ON PAN, FWD/UPPER INNER SIDE NEAR TO BEAM 5 OF FWD CARGO COMPARTMENT DOOR. (C1) SUMMARY OF NRC 00541: PAN FWD/UPPER OF FWD CARGO DOOR WAS REPAIRED PER B71
- [SDR DALA2023022201326](https://openairdocs.org/sdr/DALA2023022201326), Feb 22, 2023: NONE. NONE. CORROSION ON FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 (CPAX)(W1). SUMMARY OF NRC 00433: CORROSION LEVEL 2
- [SDR DALA2023022001254](https://openairdocs.org/sdr/DALA2023022001254), Feb 17, 2023: NONE. NONE. CRACK ON LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00414- LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS RE
- [SDR DALA2023021701231](https://openairdocs.org/sdr/DALA2023021701231), Feb 16, 2023: NONE. NONE. A.A. A.D. CRACK WAS FOUND OF 0.250" LENGTH ON FRAME STA Y=737 RH SIDE IN REF CARD 5310-01439-01D JOB# 094-0004 STEP: 4. SUMMARY NRC 00154: OVER WING FRAME STA Y
- [SDR DALA2023021701229](https://openairdocs.org/sdr/DALA2023021701229), Feb 16, 2023: NONE. NONE. CRACK ON INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22, PASSENGER CABIN. SUMMARY OF NRC 00442: INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22 WAS REP
- [SDR DALA2023021701228](https://openairdocs.org/sdr/DALA2023021701228), Feb 15, 2023: NONE. NONE. SEVERAL HIDDEN CRACKS ON RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 IN REF NRC 00154. SUMMARY OF NRC 00514: RH CUSP WEB UNDER RH SEAT TRACK 
- [SDR DALA2023021501180](https://openairdocs.org/sdr/DALA2023021501180), Feb 13, 2023: NONE. NONE. CORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=200 X=-9 TO X=-44. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.045 IN, THEREFORE THE 
- [SDR DALA2023021501179](https://openairdocs.org/sdr/DALA2023021501179), Feb 13, 2023: NONE. NONE. IN REFERENCE TO NRC 00066, AFTER REMOTION OF RETAINER SEALS, CRACK WAS FOUND ON PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2. SUMMARY OF
- [SDR DALA2023021401136](https://openairdocs.org/sdr/DALA2023021401136), Feb 11, 2023: UNKNOWN. UNKNOWN. CORRODED DIAPHRAGM ON STA Y=200 X=-22. ORIGINAL THICKNESS WAS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.012 IN, THEREFORE IT IS OUT LIMITS IN REF NRC 00424 
- [SDR DALA2023021401134](https://openairdocs.org/sdr/DALA2023021401134), Feb 11, 2023: UNKNOWN. UNKNOWN. CORRODED FLOOR SUPPORT STA Y=157-200 AND X=44.5, STA Y=180 AND X=12 TO X=38. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.035 IN, THEREF
- [SDR DALA2023021401129](https://openairdocs.org/sdr/DALA2023021401129), Feb 10, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER LONGERON 11 LH AND LONGERON 15 LH. (CPAX). SUMMARY OF NRC 00394: WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER 
- [SDR DALA2023021401127](https://openairdocs.org/sdr/DALA2023021401127), Feb 10, 2023: UNKNOWN. UNKNOWN. CRACKS (2EAS, FWD AND AFT SIDES) WERE FOUND ON BEAM 1 DURING THE WORK PROCESS ON NRC 00081 AT L1 PASSENGER DOOR. (PTAS). SUMMARY OF NRC 00487: FWD AND AFT SIDES
- [SDR DALA2023021401126](https://openairdocs.org/sdr/DALA2023021401126), Feb 10, 2023: UNKNOWN. UNKNOWN. CORROSION IS OUT OF LIMITS AT THE LH CUSP WEB MEMBRANE AT STA 395 X=54 TO X=59. ORIGINAL THICKNESS WAS 0.020 INCHES AND REMAINING THICKNESS AT STA 395 IS 0.008 
- [SDR DALA2023021401125](https://openairdocs.org/sdr/DALA2023021401125), Feb 9, 2023: UNKNOWN. UNKNOWN. PUNCTURES (2EA) WERE FOUND ON FLOOR WEB STA Y=128 AND X=17 AT FLIGHT DECK IN REF CARD 2060-1007. SUMMARY OF NRC 00503: WEB STA Y=128 AND X=17 AT FLIGHT DECK WAS
- [SDR DALA2023021401121](https://openairdocs.org/sdr/DALA2023021401121), Feb 9, 2023: UNKNOWN. UNKNOWN. SCRATCH (2 EA) ON DIAPHRAGM STA Y=189 AND X=45 (CPAX) (W1). SUMMARY OF NRC 00423: DIAPHRAGM STA Y=189 AND X=45 WAS PERMANENTLY REPAIRED PER B717-200 SRM 51-70-1
- [SDR DALA2023021401119](https://openairdocs.org/sdr/DALA2023021401119), Feb 8, 2023: UNKNOWN. UNKNOWN. ELONGATED AND BENT HOLE ON RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 IN REF NRC 00154. SUMMARY OF NRC 00446: RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 WAS REPAI
- [SDR DALA2023021401118](https://openairdocs.org/sdr/DALA2023021401118), Feb 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE (PAX CAB) (W2). SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR SUPPORT BT
- [SDR DALA2023020800983](https://openairdocs.org/sdr/DALA2023020800983), Feb 7, 2023: NOT REPORTED. NOT REPORTED. SECONDARY NRC 00428: FLOOR SUPPORT STA Y=180 AND X=-9 TO X=-43 HAS CORROSION. ORIGINAL THICKNESS IS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.020 IN, THEREF
- [SDR DALA2023020800982](https://openairdocs.org/sdr/DALA2023020800982), Feb 7, 2023: NOT REPORTED. NOT REPORTED. CORROSION ON FLOOR SUPPORTS (3 EA) STA Y=196 TO 200 FROM X=16 TO X=55.5 AT PAX CABIN FLOOR STRUCTURE. CPAX. SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPO
- [SDR DALA2023020700925](https://openairdocs.org/sdr/DALA2023020700925), Feb 7, 2023: NOT REPORTED. NOT REPORTED. CRACK ON RH CUSP WEB MEMBRANE AT STA 655 TO 674 & X=-54 TO X=-59 PASSENGER CABIN FLOOR (CPAX). SUMMARY OF NRC 00292: RH CUSP WEB MEMBRANE AT STA 655 TO 674 & X=
- [SDR DALA2020112303837](https://openairdocs.org/sdr/DALA2020112303837), Nov 23, 2020: BATTERY PACK. INOPERATIVE. BOTH THE L1 AND R1 LOWER EXIT SIGNS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK ABOVE SEAT 2CD, IAW B717 AMM 33 -51. OPERATIONAL CHECK WAS GOOD.
- [SDR 2020F00248](https://openairdocs.org/sdr/2020F00248), Feb 26, 2020: SPOILER. DELAMINATED. DISBONDED
- [SDR DALA2020011600323](https://openairdocs.org/sdr/DALA2020011600323), Jan 15, 2020: STRINGER. CORRODED. AFT CARGO COMPARTMENT STRINGER 30, BETWEEN STA 948- 954 IS CORRODED. NRC 040-0008:5331-2001/004 00196: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM S
- [SDR DALA2020011600322](https://openairdocs.org/sdr/DALA2020011600322), Jan 15, 2020: STRINGER. CORRODED. AFT CARGO COMPARTMENT STRINGER 30, STA 986 IS CORRODED. NRC 040-0008:5331-2001/001 00193: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 965-1012 R
- [SDR DALA2020010700089](https://openairdocs.org/sdr/DALA2020010700089), Jan 6, 2020: DOUBLER. DAMAGED. RAMP REPORTS DAMAGE AT AFT LOWER EDGE OF C1 CARGO DOOR. DAMAGE IS TO EXISTING DOUBLER EDGE. REMOVED, FABRICATED, AND DRILLED UP NEW DOUBLER AND TRIMED DAMAGE IA
- [SDR 2019F00174](https://openairdocs.org/sdr/2019F00174), Mar 29, 2019: SKIN. DELAMINATED. INB SPOILER HAS DELAMINATION BOTTON SURFACE. LARGE DELMINATION AREA.
- [SDR DALA2018120306972](https://openairdocs.org/sdr/DALA2018120306972), Dec 2, 2018: COVER. MISSING. HORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS - MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. ON WALK AROUND FOUND HORIZONTAL 
- [SDR DALA2018070404359](https://openairdocs.org/sdr/DALA2018070404359), Jul 3, 2018: LIGHT. BROKEN. FOUND EMERGENCY LIGHT L2-938 BROKEN AFT COMPARTMENT. REPLACED TERMINALS NEEDS LIGHT ASSY MOUNTED. MOUNTED LIGHT ASSY CKS GOOD.
- [SDR DALA2018030901588](https://openairdocs.org/sdr/DALA2018030901588), Mar 9, 2018: LATCH. DAMAGED. TAIL CONE SLIDE COVER WAS FOUND NOT SECURE. REPLACED A DAMAGED LATCH ON THE SLIDE COVER IAW AMM 25-61-02 AND RIG SLIDE IAW TASK CARD 2561-9006.
- [SDR DALA2018030601404](https://openairdocs.org/sdr/DALA2018030601404), Mar 6, 2018: FRAME. GOUGED. GOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 RT SIDE APPROX RBL 4-6. NRC 001-0253:5300-2004/005 00214: 566363-14 REV 1 AND ER/A
- [SDR DALA2018030601403](https://openairdocs.org/sdr/DALA2018030601403), Mar 6, 2018: FRAME. GOUGED. GOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 LT SIDE APPROX LBL 4-7. NRC 001-0253:5300-2004/004 00213: PRI 566363-14 REV 1 AND 
- [SDR DALA2018030401383](https://openairdocs.org/sdr/DALA2018030401383), Mar 3, 2018: BEARING. LOOSE. RIGHT INBD SPOILER PANEL CENTER HINGE BEARING LOOSE IN BORE. THE SPOILER PANEL WAS REPLACED.
- [SDR DALA2018021901529](https://openairdocs.org/sdr/DALA2018021901529), Feb 18, 2018: LENS. DAMAGED. EMERGENCY LIGHT LENS DAMAGED. REPLACED THE DAMAGED LENS.
- [SDR DALA2018030801530](https://openairdocs.org/sdr/DALA2018030801530), Jul 28, 2017: BRACKET. DAMAGED. FOUND EMERGENCY LIGHT AT ESCAPE RAMP PANEL IN POOR CONDITION. REPLACED THE BRACKETS IAW SRM 51-40-02.
- [SDR DALA2017032802517](https://openairdocs.org/sdr/DALA2017032802517), Mar 28, 2017: CHARGER. INOPERATIVE. ON SVC FOUND EMERG BATT PACK INOPERATIVE. R&R BATT CHARGER / BATT B5-235 REF AMM 33-51, WDM 33-51. CHECKS GOOD. OK FOR SVC.
- [SDR DALA2016040502626](https://openairdocs.org/sdr/DALA2016040502626), Apr 5, 2016: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY SIDEWALL WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND TH
- [SDR DALA2016040502568](https://openairdocs.org/sdr/DALA2016040502568), Apr 4, 2016: CUSP WEB. CORRODED. RIGHT CUSP WEB BS 389-503 UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW CUSP WEB IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05.
- [SDR DALA2016040502567](https://openairdocs.org/sdr/DALA2016040502567), Apr 4, 2016: CUSP WEB. CORRODED. LEFT OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, 
- [SDR DALA2016032902390](https://openairdocs.org/sdr/DALA2016032902390), Mar 28, 2016: SPAR. CORRODED. LEFT CENTER TANK UPPER REAR SPAR CORRODED AT XCW 13, 18, 52, & 59L. CORROSION ON UPPER CENTER TANK WAS REPAIRED IAW ER/A 543586-14, FASTENER HOLES DAMAGED COMMO
- [SDR DALA2016032702329](https://openairdocs.org/sdr/DALA2016032702329), Mar 26, 2016: SKIN. CRACKED. BS 1087 ABOVE STRINGER 14R, SKIN HAS A 2 DIRECTIONAL CRACK, VERTICAL LEG .5" & HORIZONAL LEG .1250". HFEC VERIFIED IAW NDT SPM 06-10-01.001 REQUEST ENGINEERING 
- [SDR DALA2016032202228](https://openairdocs.org/sdr/DALA2016032202228), Mar 21, 2016: SKIN. CRACKED. BS 1022, STRINGER 14R, SKIN HAS A TWO INCH HORIZONTAL CRACK HFEC VERIFIED IAW NDT SPM 06-10-01.001 PROCEDURE 1. INSTALLED REPAIR IAW PRI 543585-14, REVISION 2, 
- [SDR DALA2016030901764](https://openairdocs.org/sdr/DALA2016030901764), Mar 7, 2016: SKIN. CRACKED. BS 1133, 1.5" OTBD OF STR 2L HAS .1250 INCH SKIN CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDTSPM 06-10-01, 001 PROCEDURE, 1 REF ORNRC 0300-0005. 

All 119: https://openairdocs.org/aircraft/N894AT/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/N894AT/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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