# N891AT: 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: 55043
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2004
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: AC491D
- 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=891AT
- Page: https://openairdocs.org/aircraft/N891AT

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/N891AT/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 N891AT.

## FAA accident and incident reports

None matched to N891AT.

## Service difficulty reports (140, 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 DALA2026101305629](https://openairdocs.org/sdr/DALA2026101305629), Oct 10, 2026: SPAR. CRACKED. CRACK INDICATION ON LH WING REAR SPAR INBD. STA 150.45 XRS-177 BEHIND "T" ANGLE. REPAIRED PER ERA 636800-14AD. (1858405) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101305624](https://openairdocs.org/sdr/DALA2026101305624), Oct 10, 2026: SPAR. CRACKED. CRACK INDICATION ON LH WING REAR SPAR INBD STA XRS=150.45-177 BEHIND T ANGLE. REPAIRED PER ERA 636800-14AD. (8818554) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101205598](https://openairdocs.org/sdr/DALA2026101205598), Oct 9, 2026: SPAR CAP. CRACKED. LEFT WING REAR SPAR LOWER CAP AFT FLANGE CRACKED. REPAIRED PER ER/A 636800-14AD. (1857017) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100205475](https://openairdocs.org/sdr/DALA2026100205475), Oct 1, 2026: DOUBLER. CRACKED. FOUND TWO CRACK INDICATION IN THE LT UPPER MLG DOUBLER, COMPLIED WITH ER/A 637001-14. (1842759) (AIRCRAFT GROUNDED).
- [SDR DALA2026093005425](https://openairdocs.org/sdr/DALA2026093005425), Sep 29, 2026: SPAR. CRACKED. LT WING CENTER BUTE DOOR AFT SPAR FLANGE, CRACK INDICATION IN THE 13TH HOLE OTBD OF THE SPAR SPLICE, INSTALLED OVER SIZE HILOK REF B717 SRM 51-41-05. (1839494) 
- [SDR DALA2026092905410](https://openairdocs.org/sdr/DALA2026092905410), Sep 26, 2026: FITTING. CORRODED. LEFT WING INBOARD FLAP FWD FITTING CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 00-637122. (1833480) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090404998](https://openairdocs.org/sdr/DALA2026090404998), Sep 3, 2026: DOUBLER. DEMODIFICATION. FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 6
- [SDR DALA2026090404997](https://openairdocs.org/sdr/DALA2026090404997), Sep 3, 2026: DOUBLER. MISREPAIRED. FOUND PCS DOUBLER LOCATED IN INCORRECT FRAME STATIONS, COMPLIED WITH ER/A 636674-14AD. (1793776) (AIRCRAFT GROUNDED).
- [SDR DALA2026081904727](https://openairdocs.org/sdr/DALA2026081904727), Aug 19, 2026: PANEL. CRACKED. SHIP 9551 FOUND PANEL 530MB (ON LEFT WING BUTE DOOR) SCREW HOLE CRACKED TO EDGE OF PANEL AND STARTING INBOARD, CORRECTIVE ACTION: COMPLIED WITH ER/A 14-636156. 
- [SDR DALA2026080604542](https://openairdocs.org/sdr/DALA2026080604542), Aug 5, 2026: PANEL. CRACKED. FOUND PANEL 530MB ON LEFT WING BUTTE DOOR SCREW HOLE CRACKED, COMPLIED WITH ER/A 636156-14. (9087770) (AIRCRAFT GROUNDED).
- [SDR DALA2026052803225](https://openairdocs.org/sdr/DALA2026052803225), May 22, 2026: NOT REPORTED. CRACKED. REF STEP #8 RC AA5530-01048-02 AND AD 2018-10-08 4 CRACK INDICATIONS BELOW ZFS = 52.267. REPAIRED ON ERA 564482-14AD (8342877) (AIRCRAFT GROUNDED)
- [SDR DALA2026010500068](https://openairdocs.org/sdr/DALA2026010500068), Jan 1, 2026: UNKNOWN. ODOR. ATB, PERFORMED AN AIR TURN BACK DUE TO A FUME OR ODOR CONSISTENT WITH A WET DIRTY SOCK SMELL. MAINTENANCE COMPLIED WITH ALL NO-GO MSI STEPS AND REPLACED THE LEF
- [SDR DALA2025111808421](https://openairdocs.org/sdr/DALA2025111808421), Nov 15, 2025: BATTERY PACK. NO TEST. DURING SERVICE CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION B5-259 IAW AMM 33-51. ALL LIGHTS WOR
- [SDR DALA2025071205248](https://openairdocs.org/sdr/DALA2025071205248), Jul 11, 2025: SLIDE. NO TEST. AIRCRAFT 9551, SLIDE FAILED DEPLOYMENT TEST PER AMDS WORK CARD 2561-9003 FORCAST# 95-0525-8-0131. CORRECTIVE ACTION: SLIDE FAILED TO DEPLOY DUE TO A BROKEN CABL
- [SDR DALA2025032102131](https://openairdocs.org/sdr/DALA2025032102131), Mar 20, 2025: LAMP. INOPERATIVE. THE EMERGENCY LIGHTS FOR THE RH AFT EMERGENCY EXIT AND THE LH AFT LAVATORY WERE FOUND INOPERATIVE. SUMMARY OF NRC 00168: THE LAMPS FOR THE EMERGENCY LIGHTS AT T
- [SDR DALA2025031702027](https://openairdocs.org/sdr/DALA2025031702027), Mar 15, 2025: VANE. CRACKED. CRACK ON UPPER SURFACE OF FLAP MOVABLE VANE AT LH WING. SUMMARY OF NRC 00063: FLAP MOVABLE VANE AT LH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE G
- [SDR DALA2025031702023](https://openairdocs.org/sdr/DALA2025031702023), Mar 14, 2025: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00146: INTERCOSTAL ON STA Y=636 APPROX BL=0 AT FOWARD CARGO COMP
- [SDR DALA2024060305739](https://openairdocs.org/sdr/DALA2024060305739), Jun 2, 2024: BATTERY PACK. INOPERATIVE. ON SERVICE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FWD OVERWING UPPER EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE #6 &#7 EMERGENCY LIGHT BATTERY PACKS WERE RE
- [SDR DALA2024052005347](https://openairdocs.org/sdr/DALA2024052005347), May 18, 2024: BATTERY. FAILED. THE FWD L1 DOOR EMERGENCY LIGHT IS INOPERATIVE. CONDITION WAS FOUND ON SERVICE CHECK. MAINTENANCE FOUND THE BATTERY ASSEMBLY BAD AND REPLACED IT IN REF TO B717 
- [SDR DALA2023082406886](https://openairdocs.org/sdr/DALA2023082406886), Aug 21, 2023: UNKNOWN. UNKNOWN. SHIP 9551 -ATB- THE CREW NOTED STRONG AIRFRAME VIBRATION AS THE AIRCRAFT ACCELERATED THROUGH 300 KTS AT 15,000 FT. THE VIBRATION WAS FELT THROUGH THE YOKE, SEAT
- [SDR DALA2023071205669](https://openairdocs.org/sdr/DALA2023071205669), Jul 7, 2023: UNKNOWN. UNKNOWN. THE AFT EXIT DOOR EMERGENCY LIGHT ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY (B5-260) 
- [SDR DALA2023071205668](https://openairdocs.org/sdr/DALA2023071205668), Jul 7, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHT IS FLICKERING ON THE L SIDE OF GRATE. IS NOT RELATED TO AIR SWITCH/CONTROLS. *** CONTRACT MAINTENANCE EVENT - OCM: 265651 *** RESET EMERGENC
- [SDR DALA2023042503240](https://openairdocs.org/sdr/DALA2023042503240), Apr 23, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00214: PAN ON FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER ER
- [SDR DALA2023042503236](https://openairdocs.org/sdr/DALA2023042503236), Apr 21, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL STA Y1110 AND STRINGERS R24 AND R25 AFT ACCESSORIES. SUMMARY OF NRC 00318: STRINGERS R25 STA Y=1110 WAS REPAIRED PER B717-200 SRM 51-70-11-
- [SDR DALA2023042103141](https://openairdocs.org/sdr/DALA2023042103141), Apr 20, 2023: UNKNOWN. UNKNOWN. DURING STEP 3 AMDS 2060-1001 CORROSION WAS FOUND ON FWD PASSENGER STAIRWELL DOOR (CPAX). SUMMARY OF NRC 540: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLA
- [SDR DALA2023042103139](https://openairdocs.org/sdr/DALA2023042103139), Apr 20, 2023: UNKNOWN. UNKNOWN. FOUND CORROSION ON FITTING FOR FIXED STRUT AT AFT FACE RH MLG. SUMMARY OF NRC 00489: CORROSION LEVEL 2. FITTING FOR FIXED STRUT AT AFT FACE RH MLG WAS REPAIRED 
- [SDR DALA2025013000726](https://openairdocs.org/sdr/DALA2025013000726), Apr 19, 2023: NONE. NONE. DTA MONITOR INSPECTION LOG REF ERA 606978-14 PENDING DTE APPROVAL DUE PRIOR TO 11APR25. DISCONTINUE REVENUE SERVICE ON OR BEFORE 11APR25 PENDING DTE APPROVAL FR
- [SDR DALA2023042003109](https://openairdocs.org/sdr/DALA2023042003109), Apr 19, 2023: UNKNOWN. UNKNOWN. CRACK ON FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH. SUMMARY OF NRC 00043: FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH WAS REPAIRED PER PRI 606978-14 REV.2 AND ER/A 
- [SDR DALA2023041803046](https://openairdocs.org/sdr/DALA2023041803046), Apr 14, 2023: UNKNOWN. UNKNOWN. CRACKS ON FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE). SUMMARY OF NRC 00373: FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE) WERE REPAIRED PER PRI
- [SDR DALA2023041402965](https://openairdocs.org/sdr/DALA2023041402965), Apr 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS (2EA) BTW STA 148-200, X=7 AND X=-7 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1 ). SUMMARY OF NRC 00356: CORROSION LEVEL 2. FLOOR SUP
- [SDR DALA2023041402964](https://openairdocs.org/sdr/DALA2023041402964), Apr 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW STA 157-200 FROM X=44. SUMMARY OF NRC 00523: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 157-200 FROM X=44 WAS REPLACED PER B717-200
- [SDR DALA2023041402963](https://openairdocs.org/sdr/DALA2023041402963), Apr 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=179 BTW X=-8 TO X=-40, ALSO ON FLOOR SUPPORT BTW STA Y=157-195 AND X=-44 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY O
- [SDR DALA2023041402962](https://openairdocs.org/sdr/DALA2023041402962), Apr 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44. SUMMARY OF NRC 00524: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44 WAS REPLACED PER B717
- [SDR DALA2023041302909](https://openairdocs.org/sdr/DALA2023041302909), Apr 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=- 8 AND X=-44 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00362: CORROSION LEVEL 2. FLOOR SUPPORT WAS REP
- [SDR DALA2023041302908](https://openairdocs.org/sdr/DALA2023041302908), Apr 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORT STA 200 AND X=-4
- [SDR DALA2023041302907](https://openairdocs.org/sdr/DALA2023041302907), Apr 12, 2023: UNKNOWN. UNKNOWN. CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00041: EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH WAS REPAI
- [SDR DALA2023041302906](https://openairdocs.org/sdr/DALA2023041302906), Apr 12, 2023: UNKNOWN. UNKNOWN. IN REF 429: CORROSION OUT LIMITS ON RH CENTER SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT. SUMMARY OF NRC 00516: SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT
- [SDR DALA2023041302905](https://openairdocs.org/sdr/DALA2023041302905), Apr 12, 2023: UNKNOWN. UNKNOWN. CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00042: EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH WAS REPAI
- [SDR DALA2023041202863](https://openairdocs.org/sdr/DALA2023041202863), Apr 12, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 541-560, ALSO BTW STA 598-617 AND BTW STA 617-636, X=-57 AT PAX COMPARTMENT. (CPAX) SUM
- [SDR DALA2025013000728](https://openairdocs.org/sdr/DALA2025013000728), Apr 11, 2023: SKIN. CRACKED. FUSELAGE SKIN Y=1037, L13R TO L14R HAS CRACK REPAIR & INSPECTIONS. ACCOMPLISH ER/A 606978-14 REV A SECTION II INSPECTION WITHIN EVERY 15,000 CYCLES AFTER ACCOMP
- [SDR DALA2023041002745](https://openairdocs.org/sdr/DALA2023041002745), Apr 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00365: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 
- [SDR DALA2023041002743](https://openairdocs.org/sdr/DALA2023041002743), Apr 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEBS INNER AND UPPER SURFACE (4EA) BTW STA Y=433 AND STA Y=503, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00398: CORROSION LEVEL 2. CUSP
- [SDR DALA2023041002740](https://openairdocs.org/sdr/DALA2023041002740), Apr 7, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX. SUMMARY OF NRC 00443: FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-
- [SDR DALA2023041002739](https://openairdocs.org/sdr/DALA2023041002739), Apr 7, 2023: UNKNOWN. UNKNOWN. SEVERAL CORROSION POINTS ON MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00358: CORROS
- [SDR DALA2023040602680](https://openairdocs.org/sdr/DALA2023040602680), Apr 5, 2023: UNKNOWN. UNKNOWN. CRACKS ON PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Y=427 OF AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 0
- [SDR DALA2023040602679](https://openairdocs.org/sdr/DALA2023040602679), Apr 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB BTW STA 927-946 AND ON STA 807 X-57. SUMMARY OF NRC 00522: CORROSION LEVEL 2. CUSP WEB BTW STA 927-946 AND ON STA 807 X-57 WAS REPAIRED PE
- [SDR DALA2023040602678](https://openairdocs.org/sdr/DALA2023040602678), Apr 4, 2023: UNKNOWN. UNKNOWN. IN REF NRC 00384: CORROSION ON LH CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57. SUMMARY OF NRC 00521: CORROSION LEVEL 2. CUSP WEB BTW STA 746 TO 756, 636 TO 64
- [SDR DALA2023040502675](https://openairdocs.org/sdr/DALA2023040502675), Apr 4, 2023: UNKNOWN. UNDERTORQUED. SECONDARY NRC, HIDDEN DAMAGE: CRACK ON CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00490: CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN
- [SDR DALA2023040402599](https://openairdocs.org/sdr/DALA2023040402599), Apr 1, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN FWD UPPER SECTION AT L1 PASSENGER DOOR. SUMMARY OF NRC 00051: PAN ON FWD UPPER SECTION AT L1 PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-
- [SDR DALA2023040402598](https://openairdocs.org/sdr/DALA2023040402598), Mar 31, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00213: PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT F

All 140: https://openairdocs.org/aircraft/N891AT/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/N891AT/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.