# N892AT: 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: 55044
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 2, 2004
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: AC4CD4
- 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=892AT
- Page: https://openairdocs.org/aircraft/N892AT

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/N892AT/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 N892AT.

## FAA accident and incident reports

None matched to N892AT.

## Service difficulty reports (110, 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 DALA2026051903064](https://openairdocs.org/sdr/DALA2026051903064), May 13, 2026: O-RING. FAILED. DRIVER DO NOT DISPATCH THE AIRCRAFT" - W/O MCC APPROVAL" - CREW REPORTS STRONG FUEL ODOR AFTER APU SHUT DOWN. REMOVED AND REPLACED LT ENG FUEL RETURN LINE O-RIN
- [SDR DALA2025121509132](https://openairdocs.org/sdr/DALA2025121509132), Dec 6, 2025: BOLT. MISSING. MISSING AND SUNKEN BOLTS ALONG DOUBLER SPLICE APPROX BTW STA ZFS=49 AND ZFS=76 AT VERTICAL STABILIZER LEADING EDGE. REPAIRED PER ER/A 630634-14. (1338826)
- [SDR DALA2025121009008](https://openairdocs.org/sdr/DALA2025121009008), Dec 4, 2025: SKIN. CRACKED. TWO CRACKS ON FUSELAGE SKIN PANEL APPROX ON BS 1076 & 1095, L14R. DAMAGED AREA WERE REPAIRED IAW ER/A 630576-14. (1335394)
- [SDR DALA2025111208300](https://openairdocs.org/sdr/DALA2025111208300), Nov 3, 2025: OIL CAP. UNSECURE. NOTICED UNPLEASANT ODOR ON TAXI IN AFTER APU START AND OBSERVED LEAKING DARK FLUID UNDERNEATH APU COMPARTMENT ON SUBSEQUENT WALK AROUND. APU OIL CAP NOT PROPERL
- [SDR DALA2025071105225](https://openairdocs.org/sdr/DALA2025071105225), Jul 10, 2025: RELAY. FAULTED. SHIP 9552-DIV- FLIGHT DIVERSION TO CLE DUE TO LOSS OF LEFT GEN AND LEFT AC BUS CROSS TIE LOCKOUT. / CORRECTIVE ACTION: RESET LEFT PCDU & RESET LEFT BUS TIE SWIT
- [SDR DALA2025051903831](https://openairdocs.org/sdr/DALA2025051903831), May 15, 2025: TAB. DAMAGED. SHIP 9552 RT AILERON CONTROL TAB HAS DAMAGE. CORRECTIVE ACTION: RMEOVED RT AILERON CONTROL TAB PER B717 AMM 27-10 WIP 374716. (0967220)
- [SDR DALA2024072607481](https://openairdocs.org/sdr/DALA2024072607481), Jul 25, 2024: OXYGEN MASK. INOPERATIVE. SHIP 9552 -MISC- REFERENCE LOG PAGE #5879904 ABOUT A RAPID DECOMPRESSION EVENT. MASKS AT SEAT ROWS 11C, 18A, 19C, 21C, 24C, 25A, 29A, & AFT F/A SEAT DID NOT DRO
- [SDR DALA2024072607480](https://openairdocs.org/sdr/DALA2024072607480), Jul 25, 2024: DUCT. DISCONNECTED. SHIP 9552 -DIV/PRESS/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO MEM FOLLOWING THE RAPID LOSS OF CABIN PRESSURIZATION. CREW DONNED O2 MASKS, DECLARED AN EMERGE
- [SDR DALA2024060305738](https://openairdocs.org/sdr/DALA2024060305738), Jun 1, 2024: BATTERY PACK. INOPERATIVE. THE FORWARD DOOR LEVER EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-61. OPERATIONAL TEST WAS GOOD. (LP #
- [SDR DALA2024040404053](https://openairdocs.org/sdr/DALA2024040404053), Mar 25, 2024: NONE. NONE. THE EMERGENCY EXIT SIGNS WERE DISCOVERED TO BE INOPERATIVE AT LOCATIONS: 600, 601, 604, AND 605. THE EXIT SIGNS WERE NOT ILLUMINATED WHEN THE CABIN LIGHTING WAS
- [SDR DALA2024011500579](https://openairdocs.org/sdr/DALA2024011500579), Jan 15, 2024: UNKNOWN. UNKNOWN. ON WALK AROUND FOUND RIGHT REAR EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY REF B717 AMM 33-51. (LP 
- [SDR DALA2023121810335](https://openairdocs.org/sdr/DALA2023121810335), Dec 15, 2023: UNKNOWN. UNKNOWN. CRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00273: CRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT A
- [SDR DALA2023121810334](https://openairdocs.org/sdr/DALA2023121810334), Dec 15, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR. SUMMARY OF THE NRC 00081: BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02
- [SDR DALA2023121510288](https://openairdocs.org/sdr/DALA2023121510288), Dec 13, 2023: UNKNOWN. UNKNOWN. SKIN DELAMINATION ON LOWER SURFACE OF VANE. SUMMARY OF NRC 00495: SKIN ON LOWER SURFACE OF VANE WAS REPAIRED PER ERA 613937-14 REV ORIG. SECCTION I: PERMANENT R
- [SDR DALA2023120810060](https://openairdocs.org/sdr/DALA2023120810060), Dec 7, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT IN REF NRC 00408. SUMMARY OF NRC 00487: UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT WAS R
- [SDR DALA2023120810059](https://openairdocs.org/sdr/DALA2023120810059), Dec 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS REPAIR ON FRAME STA 927 BTW LONGERONS 29L-28L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. PREVIOUS REPAIR ANGLE ON 
- [SDR DALA2023120109871](https://openairdocs.org/sdr/DALA2023120109871), Nov 30, 2023: UNKNOWN. UNKNOWN. CRACK ON OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR. SUMMARY OF NRC 00059: OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 
- [SDR DALA2023113009840](https://openairdocs.org/sdr/DALA2023113009840), Nov 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB LOWER AT AFT CARGO DOOR. SUMMARY OF NRC 00067: CORROSION LEVEL 2. DOOR JAMB LOWER AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 53-20-1
- [SDR DALA2023112709726](https://openairdocs.org/sdr/DALA2023112709726), Nov 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN SEAT TRACK X=-44.5, BTW Y =200/256. SUMMARY OF NRC 00226: CORROSION LEVEL 2. SEAT TRACK X=-44.5, BTW Y=200/256 WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2023112209648](https://openairdocs.org/sdr/DALA2023112209648), Nov 21, 2023: UNKNOWN. UNKNOWN. A CRACK ON FLOOR WEB, STA Y=196 TO 200 X-30 TO X-35 APROX WAS FOUND AT PASSENGER CABIN IN REF NRC #00226. SUMMARY OF NRC 00490: REPAIR WAS PERFORMED PER B717 SR
- [SDR DALA2023112109571](https://openairdocs.org/sdr/DALA2023112109571), Nov 20, 2023: UNKNOWN. UNKNOWN. CRACK ON REAR SPAR RUDDER ACCESS PANEL 1. SUMMARY OF NRC 00312: REAR SPAR RUDDER ACCESS PANEL 1 WAS REPAIRED PER B717-200 SRM 55-00-00-2R PROCEDURE 2, REPAIR 2,
- [SDR DALA2023112009528](https://openairdocs.org/sdr/DALA2023112009528), Nov 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT, STA X=7, BTW Y=148/200. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=7, BTW Y=148/200 WAS FABRICATED PER DWG 
- [SDR DALA2023112009527](https://openairdocs.org/sdr/DALA2023112009527), Nov 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT, STA X=-7, BTW Y=148/200. SUMMARY OF NRC 00211: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=-7, BTW Y=148/200 WAS FABRICATED PER DW
- [SDR DALA2023112009525](https://openairdocs.org/sdr/DALA2023112009525), Nov 18, 2023: UNKNOWN. UNKNOWN. CRACK INTERCOSTAL BTW BEAM NO 4 TO BEAM NO 5 AND STA Y=185.5 AT FWD PASSENGER DOOR INTERNAL EXTRUCTURE. SUMMARY OF NRC 00368: INTERCOSTAL BTW BEAM NO 4 TO BEAM 
- [SDR DALA2023112009524](https://openairdocs.org/sdr/DALA2023112009524), Nov 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORTS (2 EA) STA Y=200, BTW X=7/-7, AND BTW X=-45.5/-56.5 (OUT OF LIMITS). SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORTS (
- [SDR DALA2023111609436](https://openairdocs.org/sdr/DALA2023111609436), Nov 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT, STA X=44.5, BTW Y=160/196. SUMMARY OF NRC 00215: CORROSION LEVEL 2. FLOOR SUPPORT, STA X= 44.5, BTW Y=160/196 WAS FABRICATED P
- [SDR DALA2023111409352](https://openairdocs.org/sdr/DALA2023111409352), Nov 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT, STA X=-44.5, BTW Y=160/200. SUMMARY OF NRC 00212: CORROSION LEVEL 2. CABIN FLOOR SUPPORT STA X=-44.5 BTW Y=160/200 WAS REPLACE
- [SDR DALA2023111309296](https://openairdocs.org/sdr/DALA2023111309296), Nov 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORTS (2 EA), STA Y=180, BTW X=13/38 AND BTW X=-7/-44.5. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR SUPPORT (2 EA), STA Y=180, B
- [SDR DALA2023111309295](https://openairdocs.org/sdr/DALA2023111309295), Nov 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR WEB, STA Y=196 TO 200 X-50 TO X-55 AND Y=201 AT X- 44 TO X-48 AT PASSENGER CABIN (OUT OF LIMIT). PER NRC 0411: CORROSION LEVEL 2. FLOOR WEB S
- [SDR DALA2023110909225](https://openairdocs.org/sdr/DALA2023110909225), Nov 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON CABIN FLOOR SUPPORT, STA Y=196, BTW X=22/44.5. SUMMARY OF NRC 00221: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=196, BTW X=22/44.5 WAS REPLACED PER DWG
- [SDR DALA2018102206192](https://openairdocs.org/sdr/DALA2018102206192), Oct 19, 2018: LENS. MISSING. EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING AT LOCATIONS: 600. EMERGENCY EXIT COVER IS MISSING AND BARE WIRES ARE EXPOSED. MAINTENANCE REPLACED THE EM
- [SDR DALA201808064878](https://openairdocs.org/sdr/DALA201808064878), Aug 2, 2018: LENS. DAMAGED. EMERGENCY EXIT LIGHT LENS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.
- [SDR DALA201808064877](https://openairdocs.org/sdr/DALA201808064877), Aug 2, 2018: LENS. DAMAGED. EMERGENCY EXIT LENS WAS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.
- [SDR DALA2018072504673](https://openairdocs.org/sdr/DALA2018072504673), Jul 23, 2018: COVER. LOOSE. THE FWD CENTER AISLE CEILING EMERGENCY EXIT SIGN COVER IS LOOSE. MAINTENANCE REATTACHED THE EXIT SIGN. OPERATIONAL CHECK IS GOOD.
- [SDR DALA2018071604490](https://openairdocs.org/sdr/DALA2018071604490), Jul 14, 2018: LIGHT. UNSECURE. THE FORWARD MOST EMERGENCY EXIT LIGHT IS NOT SECURELY FASTENED TO THE CEILING AS DESIGNED. MAINTENANCE SECURED THE LIGHT ASSEMBLY AS REQUIRED. OK FOR SERVICE.
- [SDR DALA2018040902285](https://openairdocs.org/sdr/DALA2018040902285), Apr 8, 2018: BRACKET. BROKEN. LOUD BUZZING NOISE AND VIBERATION UNDER THE FLOOR AT ROW 19A. FOUND EIGHT RUBBER NUTS AT THE LT OVERWING FILLET PANEL. RAN HYD PUMPS AND FUEL PUMPS, ALL SOUND O
- [SDR DALA2018030301831](https://openairdocs.org/sdr/DALA2018030301831), Mar 2, 2018: SKIN. CRACKED. CRACKED LOWER SKIN AT RT UPPER MOVABLE VANE. RT UPPER MOVABLE VANE WAS REPAIRED PER SRM 57-53-01-2R-1 PARAGRAPH 4 FIG 201.
- [SDR DALA2018022801266](https://openairdocs.org/sdr/DALA2018022801266), Feb 27, 2018: DOOR FRAME. CRACKED. A CRACK WAS FOUND ON THE AFT CARGO DOOR FRAME AFT EDGE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-20-15-2R, PROCEDURE 12, PARAGRAPH 6 A.
- [SDR DALA2018022801265](https://openairdocs.org/sdr/DALA2018022801265), Feb 27, 2018: DOOR FRAME. CRACKED. CRACK FOUND ON THE LT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.
- [SDR DALA2018022801264](https://openairdocs.org/sdr/DALA2018022801264), Feb 27, 2018: DOOR FRAME. CRACKED. CRACK ON THE RT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.
- [SDR DALA2018021500906](https://openairdocs.org/sdr/DALA2018021500906), Feb 15, 2018: LAMP. INOPERATIVE. DURING A SERVICE CHECK, FOUND THE TAIL CONE EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW AMM 33-51. CLEANED AND REPLACED THE LAMPS. OPS CHEC
- [SDR DALA2016102407460](https://openairdocs.org/sdr/DALA2016102407460), Oct 23, 2016: PYLON. CRACKED. NUMBER 1 PYLON UPPER AND LOWER AFT COWL ATTACH POINTS HAVE CRACKS IN CUTOUTS ON SKIRT FAIRING. REMOVED BRACKETS, FITTINGS, GUSSETS, AND SHIMS. BLENDED OUT CRACK
- [SDR DALA2016102307459](https://openairdocs.org/sdr/DALA2016102307459), Oct 22, 2016: PYLON. CRACKED. LEFT ENGINE PYLON APRON FOUND TO BE CRACKED IN FOUR LOCATIONS. REPAIRED IAW ER/A 552108-14.
- [SDR DALA2016100306961](https://openairdocs.org/sdr/DALA2016100306961), Oct 2, 2016: SKIN. DAMAGED. REV ORIG, PERFORMED CUT OUT OF DAMAGE AS SHOWN FIG 1. C/W HFEC AND BHEC PER PRI 551316-14 REV ORIG NR ITEMS 2034. FABRICATED REPAIR PARTS AS SHOWN FIG 1 REF PRI
- [SDR DALA2016050203478](https://openairdocs.org/sdr/DALA2016050203478), Apr 29, 2016: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING BETWEEN ROWS 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR TH
- [SDR DALA2016102807813](https://openairdocs.org/sdr/DALA2016102807813), Feb 22, 2016: CUSP WEB. CORRODED. LEFT OUTER CUSP WEB CORRODED AT BS 488. CORRISION BLENDED AND FOUND BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00
- [SDR DALA2016022201276](https://openairdocs.org/sdr/DALA2016022201276), Feb 21, 2016: FUEL TANK. CORRODED. LEFT WHEEL WELL TO RT WHEEL WELL FUEL TANK SKIN PLANK PANEL T/E CORRODED AT SEVERAL LOCATIONS. CLEAN/ EVAL, TREAT & PAINT REF OR NRC 62937-0100-0065. BLENDED OU
- [SDR DALA2016102707773](https://openairdocs.org/sdr/DALA2016102707773), Feb 16, 2016: SEAT TRACK. CORRODED. CENTER SEAT TRACK HAS MULTIPLE DEFECTS FROM BS 148 TO 1022. CLEANED RH CENTER SEAT TRACK AS MARKED, STA 148-STA 1032 AND FOUND ALL DEFECTS TO BE NEGLIGIBLE IAW 
- [SDR DALA2016022001268](https://openairdocs.org/sdr/DALA2016022001268), Feb 16, 2016: CUSP WEB. CORRODED. RIGHT CUSP WEB HAS CORROSION AROUND FWD LIGHTING HOLE AFT OF BS 522. BLENDED AREA IAW 53-00-00, PG 105, FIG 103. REMOVING .006", FOUND TO BE OUT OF LIMITS, DRIL
- [SDR DALA2016021801160](https://openairdocs.org/sdr/DALA2016021801160), Feb 16, 2016: CUSP WEB. CRACKED. RT CUSP WEB IS CRACKED AT APPROXIMATELY RBL 47 UNDER SEAT TRACK BS 674. REMOVED OLD CUSP WEB FROM BS 656 TO 715 INSTALLED NEW CUSP WEB IAW SRM 51-41-05 & 51-41-

All 110: https://openairdocs.org/aircraft/N892AT/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/N892AT/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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