# N896AT: 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: 55048
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 2005
- Certificate issued: August 29, 2024
- Expires: August 31, 2031
- Mode S code: AC5BB0
- 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=896AT
- Page: https://openairdocs.org/aircraft/N896AT

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/N896AT/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 N896AT.

## FAA accident and incident reports

None matched to N896AT.

## Service difficulty reports (93, 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 DALA2026081404656](https://openairdocs.org/sdr/DALA2026081404656), Aug 13, 2026: SKIN. GROUND DAMAGE. RAMP STRUCK BOTTOM OF AIRCRAFT WITH HOSE REEL, CREATING DENT, COMPLIED WITH ER/A 636316-16. (9606506) (AIRCRAFT GROUNDED).
- [SDR DALA2026072704341](https://openairdocs.org/sdr/DALA2026072704341), Jul 25, 2026: LIGHT. INOPERATIVE. LT & RT EXT EMERGENCY LIGHT INOP. R & R R2-273 PER B717 33-51-11. BOTH EMERGENCY LIGHTS OPS CK NORMAL AT THIS TIME OK FOR SVC. (9124825) AIRCRAFT GROUNDED.
- [SDR DALA2026040102117](https://openairdocs.org/sdr/DALA2026040102117), Mar 30, 2026: COMPRESSOR. STALLED. CREW REJECTED TAKEOFF AT 70 KNOTS DUE TO RIGHT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF RIGHT ENGINE AND FOUND MULTIPLE HPC BLADES DAMAGED. RE
- [SDR DALA2025020300804](https://openairdocs.org/sdr/DALA2025020300804), Jan 31, 2025: COMPUTER. FAULTED. SHIP 9556 -MISC/DE- THE FLIGHT CREW NOTICED THAT THE AIRCRAFT WAS FLYING UNCOORDINATED DURING THE DESCENT AND THEN THEY RECEIVED "RUDDER RESTRICTED" MESSAGE ON 
- [SDR DALA2025012000464](https://openairdocs.org/sdr/DALA2025012000464), Jan 17, 2025: SKIN. CORRODED. -AD- CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING. SUMMARY OF NRC 0015: CORROSION LEVEL 2. CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WIN
- [SDR DALA2025011400312](https://openairdocs.org/sdr/DALA2025011400312), Jan 13, 2025: SKIN. NICKED. NICK BETWEEN STA 994 AND STGR 24-26 RH AT EXTERNAL FUSELAGE SKIN. SUMMARY OF NRC 00007: EXTERNAL SKIN BETWEEN STA 994 AND STGR 24-26 RH WAS REPAIRED PER B717-20
- [SDR DALA2023102408719](https://openairdocs.org/sdr/DALA2023102408719), Oct 23, 2023: UNKNOWN. UNKNOWN. ROW 21 BOTH L/H AND R/H OVERWING EXIT SIGNS (LOWER) ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-51 AT LOCATION B5-1119. OPERATIONAL C
- [SDR DALA2023052204054](https://openairdocs.org/sdr/DALA2023052204054), May 20, 2023: UNKNOWN. UNKNOWN. THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS DAMAGED AT LOCATION 603. MAINTENANCE RESECURED THE EMERGENCY EXIT COVER LIGHT LENS OV
- [SDR DALA2023021401120](https://openairdocs.org/sdr/DALA2023021401120), Feb 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH TIE TRACK UPPER SURFACES FROM STA Y=900 TO Y=954. SUMMARY OF NRC 0556: CORROSION LEVEL 2. TIE TRACK RH ON STA Y=900 TO Y=954 WAS REPLACED PER B7
- [SDR DALA2023021401117](https://openairdocs.org/sdr/DALA2023021401117), Feb 8, 2023: UNKNOWN. UNKNOWN. SECONDARY IN REFERENCE NRC 496: CORROSION ON LH TIE TRACK UPPER SURFACES FRON STA Y=900 TO Y=1028. SUMMARY OF NRC 00555: CORROSION LEVEL 2. TIE TRACK SECTION FR
- [SDR DALA2023013100773](https://openairdocs.org/sdr/DALA2023013100773), Jan 28, 2023: TAB. DEBONDED. IN REF TO NRC 00041, DISBONDED AREA WAS FOUND ON DENT #1 WITH A MEASURE OF 0.500 IN LENGTH X 0.500 IN WIDTH AT AILERON CONTROL TAB OUTBOARD UPPER FACE AT LH WIN
- [SDR DALA2023012400524](https://openairdocs.org/sdr/DALA2023012400524), Jan 20, 2023: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK HOLE OF LH WING ACCESS PLATE NBR 520CB REF NRC 417. SUMMARY NRC 00506: CORROSION LEVEL 2. FUEL ACCESS PLATE NBR 520CB AT LH WING WAS RE
- [SDR DALA2023012000436](https://openairdocs.org/sdr/DALA2023012000436), Jan 19, 2023: BEAM. CRACKED. CRACK ON BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR. SUMMARY OF NRC 00106: CRACKED BEAM NBR 7 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2023011900387](https://openairdocs.org/sdr/DALA2023011900387), Jan 18, 2023: BEAM. CRACKED. CRACK ON BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR. BEAM NR 1 AFT SECTION AT MAIN ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-02-2R-7.
- [SDR DALA2023011900386](https://openairdocs.org/sdr/DALA2023011900386), Jan 18, 2023: PAN. CRACKED. CRACK ON UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR. UPPER PAN AT STA 197.750 & BEAM #1 OF FWD PASSENGER ENTRANCEN DOOR WAS REPAIRED IAW
- [SDR DALA2023011800365](https://openairdocs.org/sdr/DALA2023011800365), Jan 17, 2023: CUSP WEB. CRACKED. DURING REMOVAL OF RH CUSP WEB, DVI WAS PERFORMED AND 3 CRACKS WERE FOUND (EAS). A CRACK AT HOLE OF FASTENER AT CUSP WEB STA 656, A CRACK ON EDGE OF CUSP WEB STA
- [SDR DALA2023011600311](https://openairdocs.org/sdr/DALA2023011600311), Jan 14, 2023: CUSP WEB. CRACKED. CRACK ON CUSP WEB ON STA 229 AT BL 46R AT PAX CABIN. SUMMARY OF NRC 00258: CUSP WEB ON STA 229 AT BL 46R WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP
- [SDR DALA2023011600308](https://openairdocs.org/sdr/DALA2023011600308), Jan 12, 2023: DIAPHRAGM. CORRODED. CORROSION ON DIAPHRAGM STA=192 AND STA=187 RBL=44 ARE OUT OF LIMITS IN REF NRC 00325. SUMMARY OF NRC 00451: LEVEL CORROSION 2. DIAPHRAGM STA=192 AND STA =187 RB
- [SDR DALA2022092806344](https://openairdocs.org/sdr/DALA2022092806344), Sep 28, 2022: NONE. NONE. DURING A SERVICE CHECK, THE AFT GROUP OF EMERGENCY LIGHTS WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY B5-260 REF B717 AM
- [SDR DALA2022092806342](https://openairdocs.org/sdr/DALA2022092806342), Sep 25, 2022: NONE. NONE. THE EMERGENCY LIGHTS BATTERY WAS DISCOVERED TO BE DISCHARGED. MAINTENANCE REPLACED THE POWER SUPPLY AT THE EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. AIRCRAFT 
- [SDR DALA2022033102152](https://openairdocs.org/sdr/DALA2022033102152), Mar 30, 2022: NONE. NONE. MAINTENANCE FOUND THAT THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE DURING THE SERVICE CHECK. TROUBLE SHOOTING PER WD 33-51-12 FOUND THE EMERGENCY LIGHT B
- [SDR DALA2022012500495](https://openairdocs.org/sdr/DALA2022012500495), Jan 22, 2022: NONE. NONE. CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-2
- [SDR DALA2022011700299](https://openairdocs.org/sdr/DALA2022011700299), Jan 17, 2022: NONE. NONE. CORROSION ON PAN BTW STA Y=954 TO Y=994 AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 00008: CORROSION LEVEL 2, PAN BTW STA Y=954 TO Y= 994 AT AFT CARGO DOOR JAMB WAS 
- [SDR DALA2022011700298](https://openairdocs.org/sdr/DALA2022011700298), Jan 15, 2022: NONE. NONE. CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L. SUMMARY OF NRC 00056: CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L WAS REPAIRED PER B717-2
- [SDR DALA2021060403067](https://openairdocs.org/sdr/DALA2021060403067), Jun 2, 2021: BATTERY PACK. INOPERATIVE. FOUND EMERGENCY LIGHT BATTERY INOPERATIVE IN FIRST CLASS. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHTS BATTERIES (2) REF B717 AMM 33-51. OPERATIONAL CHECK 
- [SDR DALA2021042902460](https://openairdocs.org/sdr/DALA2021042902460), Apr 27, 2021: SLIDING WINDOW. FAILED. WHILE ATTEMPTING TO CLEAN THE WINDOWS, MAINTENANCE DETERMINED THAT THE COPILOTS SLIDING WINDOW WILL NOT UNLOCK AND OPEN. THIS COULD PREVENT PROPER OPERATION OF 
- [SDR DALA2021012200455](https://openairdocs.org/sdr/DALA2021012200455), Oct 3, 2020: COVER. MISSING. THE INBOARD COWL HOIST COVER IS MISSING ON LEFT ENGINE. CONTRACT MAINTENANCE FORWARDED THE DISCREPANCY TO NEF 71- 10-02. COWL HOIST SCREW COULD NOT BE INSTALLED
- [SDR DALA2020030201516](https://openairdocs.org/sdr/DALA2020030201516), Mar 1, 2020: POWER SUPPLY. INOPERATIVE. THE EXTERIOR EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT IS SHUTDOWN. MAINTENANCE REPLACED THE POWER SUPPLY AND RELAY PER B717 AMM 33-51. THE OPERATIONAL CHGEC
- [SDR DALA2020021801207](https://openairdocs.org/sdr/DALA2020021801207), Feb 13, 2020: WINDSHIELD WIPER. BROKEN. THE CAPTAIN SIDE WIPER ARM BROKE OFF ON TOUCH DOWN (22L) AT JFK. MAINTENANCE REPLACED THE CAPTAIN SIDE WINDSHIELD WIPER IN REF B717 AMM 30-43. OPERATIONAL CHECK
- [SDR DALA2019110506386](https://openairdocs.org/sdr/DALA2019110506386), Nov 2, 2019: RELEASE CABLE. WORN. KEVLAR RELEASE CABLE IS WORN IN THE TAILCONE. REMOVED WORN KEVLAR RELEASE CABLE, INSTALLED NEW KEVLAR RELEASE CABLE, WITH COMPLETION OF KEVLAR CABLE ON AMDS CAR
- [SDR DALA2019110506385](https://openairdocs.org/sdr/DALA2019110506385), Nov 2, 2019: BRACKET. WORN. THE TAILCONE KEVLAR CABLE SPRING BRACKET ON THE RIGHT SIDE IS WORN. MAINTENANCE REPLACED THE TAIL CONE KEVLAR CABLE SPRING BRACKET WITH A NEW BRACKET. (LP #1343
- [SDR DALA2019090905217](https://openairdocs.org/sdr/DALA2019090905217), Sep 6, 2019: LIGHT. INOPERATIVE. WHILE PERFORMING SERVICE CHECK FOUND 2ND FROM FORWARD EMERGENCY ESCAPE PATH LIGHT ABOVE TAIL CATWALK INOPERATIVE. MAINTENANCE REPAIRED THE WIRE PER SWPM 20 AND 
- [SDR DALA2019073104498](https://openairdocs.org/sdr/DALA2019073104498), Jul 21, 2019: DOOR. MISSING. POTABLE WATER DOOR MISSING. REF LP 5476442. (LP #5476460)
- [SDR 2019F00176](https://openairdocs.org/sdr/2019F00176), Mar 29, 2019: SPOILER. DELAMINATED. DELAMINATED LT INBOARD SPOILER.
- [SDR DALA2018031301682](https://openairdocs.org/sdr/DALA2018031301682), Mar 9, 2018: SLIDE. DAMAGED. THE OUT OF PLACE INFLATION CABLE PIN WAS ALSO MISSING VALVE LOCK PIN ON L1 DOOR SLIDE. THE DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-61-01.
- [SDR DALA2018031001597](https://openairdocs.org/sdr/DALA2018031001597), Mar 9, 2018: VANE. DEBONDED. DISBONDED AREA OF 2"X2" ON RT AFT MOVEABLE VANE LOWER SURFACE. THE VANE LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4, FIGU
- [SDR DALA2018031001596](https://openairdocs.org/sdr/DALA2018031001596), Mar 9, 2018: SKIN. DEBONDED. DISBONDED AREA OF 1.5"X 1.5" ON RH INBD SPOILER LWR SURFACE. THE SPOILER LOWER SURFACE WAS REPAIRED IAW SRM 51-70-02-2R-3.
- [SDR DALA2018030701456](https://openairdocs.org/sdr/DALA2018030701456), Mar 7, 2018: FRAME. CRACKED. CRACKED FRAME, BS 1225, BETWEEN 6 AND 7 HRS. THE FRAME WAS REPLACED IAW SRM 51-41-02 AND 51-40-08.
- [SDR DALA2018030601405](https://openairdocs.org/sdr/DALA2018030601405), Mar 6, 2018: CHANNEL. CRACKED. CRACKED CHANNELS OF FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187. PERMANENT REPAIR. FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187 WERE REPAIRED PER S
- [SDR DALA2018021400883](https://openairdocs.org/sdr/DALA2018021400883), Feb 14, 2018: WIRE. SHORTED. DURING SLAT RETRACTION, AFTER TAKEOFF RECEIVED A PSEU FAIL CAUTION INDICATION. DURING APPROACH, EXTENSION OF SLATS, DOWN ARROW STAYED ON, THOUGH INTERMITTENT. P
- [SDR DALA2017112908380](https://openairdocs.org/sdr/DALA2017112908380), Nov 16, 2017: FMS. MALFUNCTIONED. THE CREW DECLARED AN EMERGENCY ON APPROACH AFTER THE LOSS OF FMS GUIDED FLIGHT PLAN. MAINTENANCE FOUND BOTH VIA NR 1 & 2 DATA BUSS FAULT CODES 344343 AND 344344
- [SDR DALA2016121509877](https://openairdocs.org/sdr/DALA2016121509877), Dec 9, 2016: ENGINE. OVERHEATED. THE CREW DIVERTED, FOLLOWING AN OVERHEAT OF THE LEFT ENGINE BEARING AND ASSOCIATED ROLLBACK. THE ENGINE WAS REPLACED.
- [SDR DALA2016031501940](https://openairdocs.org/sdr/DALA2016031501940), Mar 14, 2016: FUEL TANK. CORRODED. LEFT CTR WING TANK UPPER SURFACE, BS 706 SKIN EXFOLIATED. REPAIRED IAW PRI 543588-14, REV 3 AND ER/A 543588, REV A.
- [SDR DALA2016031301880](https://openairdocs.org/sdr/DALA2016031301880), Mar 8, 2016: CUSP WEB. DAMAGED. LT CUSP WEB HAS MULTIPLE DEFECTS FROM BS 157 TO BS 1022. REPAIRED MULTIPLE DEFECTS IN LT CUSP WEB FROM BS 157 TO BS 1022 IAW SRM 53-00-55, REPAIR 4, DEPTH GAUGE
- [SDR DALA2015081204916](https://openairdocs.org/sdr/DALA2015081204916), Aug 12, 2015: BATTERY PACK. INOPERATIVE. LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED OVERWING EMERGENCY EXIT LIGHT BATTERY.
- [SDR DALA2015060803628](https://openairdocs.org/sdr/DALA2015060803628), Jun 7, 2015: SPRING. OUT OF ADJUST. DECLARED AN EMERGENCY BECAUSE THE NOSE GEAR DID NOT EXTEND USING NORMAL PROCEDURES. THE ALTERNATE GEAR EXTENSION WAS SUCCESSFUL AND THE FLIGHT CREW HAD A 3 GREE
- [SDR DALA2015051803313](https://openairdocs.org/sdr/DALA2015051803313), May 18, 2015: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, EMERGENCY LIGHTS ABOVE FWD F/A SEAT AND CEILING WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AMM 33-51 AND CHECKS WERE GOOD.
- [SDR DALA2015031602168](https://openairdocs.org/sdr/DALA2015031602168), Mar 15, 2015: WARNING LIGHT. FALSE ACTIVATION. DURING LANDING GEAR EXTENSION, RT HYD QUANTITY LOW MESSAGE DISPLAYED. QUANTITY OF RIGHT HYD SYSTEM WAS INDICATING 3.5 AND HELD THERE WITH 3,000 PSI PRESSURE. DE
- [SDR DALA2015030901994](https://openairdocs.org/sdr/DALA2015030901994), Mar 8, 2015: FRAME. CRACKED. FOUND LT OVERWING FRAME STA 715 HAS CRACK INDICATION THE LENGTH IS GREATER THAN .125. VERIFIED CRACK IAW NDT SPM 06-10-01.001 WIP QC1965. REPLACED LT STA 715 OV
- [SDR DALA2014102005637](https://openairdocs.org/sdr/DALA2014102005637), Oct 17, 2014: BATTERY PACK. INOPERATIVE. DURING CABIN CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE IN FWD GALLEY AND FWD AISLE CEILING PANEL. FOUND BATTERY PACK AT B5-259 POWER SUPPLY AT FAULT. R

All 93: https://openairdocs.org/aircraft/N896AT/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/N896AT/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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