# N929AT: 2000 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55075
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 2000
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ACDFAB
- 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=929AT
- Page: https://openairdocs.org/aircraft/N929AT

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 BMW Rolls 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 (BMW Rolls 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/N929AT/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 N929AT.

## FAA accident and incident reports

None matched to N929AT.

## Service difficulty reports (187, 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 DALA2026102105785](https://openairdocs.org/sdr/DALA2026102105785), Oct 21, 2026: SPAR CAP. CRACKED. CRACK FOUND DURING INSPECTION OF LT WING REAR SPAR LOWER CAP AFT LEG, COMPLIED WITH ER/A 637410-14AD. (9540404) (AIRCRAFT GROUNDED).
- [SDR DALA2026102105787](https://openairdocs.org/sdr/DALA2026102105787), Oct 20, 2026: SPAR. CRACKED. FOUND CRACK EXTENDING AFT FROM ONE OF THE IB BUTE DOOR ATTACH LOCATIONS IN THE AFT FLANGE OF THE LOWER REAR SPAR CHORD, COMPLIED WITH ER/A 637410-14AD. (1876126
- [SDR DALA2026102105786](https://openairdocs.org/sdr/DALA2026102105786), Oct 20, 2026: SPAR. CRACKED. FOUND CRACK AT LT WING REAR SPAR NEAR XRS = 164, COMPLIED WITH ER/A 637410-14AD. (1876109) (AIRCRAFT GROUNDED).
- [SDR DALA2026041402368](https://openairdocs.org/sdr/DALA2026041402368), Apr 12, 2026: UNKNOWN. SMOKE. SMOKE/FUMES IN CABIN. R & R D1- 80 CABIN HIGH LIMIT TEMP ANTICIPATOR IAW AMM 21-62 (1541379) (AIRCRAFT GROUNDED)
- [SDR DALA2026011600374](https://openairdocs.org/sdr/DALA2026011600374), Jan 13, 2026: SKIN. CRACKED. CRACK ON SKIN FUSELAGE BTW L15R, BS 037 AT AFT FUSELAGE AREA. DAMAGED FUSELAGE AREA WAS REPAIRED PER PRI 631355-14 REV. (1399353)
- [SDR DALA2026011600376](https://openairdocs.org/sdr/DALA2026011600376), Jan 11, 2026: SKIN. NOT REPORTED. DTA ER/A 631355-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 11-JAN-26. CONTACT LIAISON ENGINEERING. REPAIRED PER ER/A 
- [SDR DALA2026010500066](https://openairdocs.org/sdr/DALA2026010500066), Dec 31, 2025: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (13
- [SDR DALA2026010500065](https://openairdocs.org/sdr/DALA2026010500065), Dec 31, 2025: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN( AREA UNDER FILLET PANELS) Y=590 BTW LONG 24RH, Y=615 BTW LONG 23RH-25RH, Y=901 BTW LONG 25LH-26LH , Y=586-590 LONG 24 RH , Y=588 TO 
- [SDR DALA2025062504747](https://openairdocs.org/sdr/DALA2025062504747), Jun 21, 2025: WIRE SPLICE. DAMAGED. EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP AT 12C AND 27C CEILING. INSP AND FOUND DAMAGED SPLICES R5-6720 @ LIGHT L2-746 & R5-6722 @ LIGHT L2-771. REPLACE
- [SDR DALA2025041502919](https://openairdocs.org/sdr/DALA2025041502919), Apr 15, 2025: DOOR. UNSECURE. SHIP 9570 -ATB/DE- AIRCRAFT HAD AN UNCOMMANDED HEAVY ROLL IN FLIGHT DURING CLIMB AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED THE AIRCRAF
- [SDR DALA2024120211376](https://openairdocs.org/sdr/DALA2024120211376), Nov 30, 2024: LIGHT. INOPERATIVE. EMERGENCY LIGHTS ABOVE ROWS 24-27 ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY (B5-231) AND OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51. (LP #6585094)
- [SDR DALA2024102910498](https://openairdocs.org/sdr/DALA2024102910498), Oct 29, 2024: BATTERY PACK. FAILED. THE EMERGENCY LIGHTS AT LOCATION SEAT ROW 20 ARE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK AT LOCATION B5-230 WAS BAD. THE BATTERY AT LOCATION B5-230
- [SDR DALA2024092609433](https://openairdocs.org/sdr/DALA2024092609433), Sep 25, 2024: CONNECTOR. NOT SEATED. THE AFT EMERGENCY CEILING LIGHT REMAINED ON IN THE ARM POSITION. MAINTENANCE RESEATED THE CANNON PLUG ON THE AFT CABIN EMERGENCY LIGHT BATTERY IAW B717 AMM 33-5
- [SDR DALA2024061005955](https://openairdocs.org/sdr/DALA2024061005955), Jun 9, 2024: BATTERY PACK. INOPERATIVE. DURING SVC CHK FOUND R FWD AND L FWD OVERWING EXIT IDENTIFIER INOPERATIVE. T/S PER B717 WD 33-51-14, FOUND BATTERY PACK B5-118 INOPERATIVE. REPLACED BATTERY PAC
- [SDR DALA2024050604958](https://openairdocs.org/sdr/DALA2024050604958), May 3, 2024: HEATER. INOPERATIVE. LT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)
- [SDR DALA2024010800318](https://openairdocs.org/sdr/DALA2024010800318), Dec 2, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00095: WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APP
- [SDR DALA2024022002334](https://openairdocs.org/sdr/DALA2024022002334), Dec 1, 2023: HINGE FITTING. CORRODED. CORROSION WAS FOUND ON BOLTS HOUSING AT FLAP HINGE FITTING #3 AND #2. (AI). SUMMARY OF NRC 00366: LH CENTER WING FLAP HINGE FITTING WAS REPLACED PER B717-200 AM
- [SDR DALA2023120409898](https://openairdocs.org/sdr/DALA2023120409898), Nov 30, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON OUTER AND INNER PAN IN LOWER AREA STA Y=974 AT AFT CARGO DOOR. SUMMARY OF NRC 00469 AFT CARGO DOOR WAS REMOVED PER B717-200 AMM 52-31-01 AND 
- [SDR DALA2023112909799](https://openairdocs.org/sdr/DALA2023112909799), Nov 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00053: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-2
- [SDR DALA2023112809761](https://openairdocs.org/sdr/DALA2023112809761), Nov 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX. SUMMARY OF NRC 00308: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX WAS REPAIRED PE
- [SDR DALA2023112809752](https://openairdocs.org/sdr/DALA2023112809752), Nov 26, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1). SUMMARY OF NRC 00507: WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2
- [SDR DALA2023112709725](https://openairdocs.org/sdr/DALA2023112709725), Nov 25, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX. SUMMARY OF NRC 00483: CORROSION LEVEL 2. SEAT TRACK BTW STA 208 TO STA 218, X=-54 
- [SDR DALA2023112709720](https://openairdocs.org/sdr/DALA2023112709720), Nov 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PREVIOUS REPAIR OF RH CUSP MEMBRANE BT
- [SDR DALA2023112709718](https://openairdocs.org/sdr/DALA2023112709718), Nov 22, 2023: UNKNOWN. UNKNOWN. CRACK ON L2L STA 1144 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00192: LONGERON ON L2 STA 1144 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-
- [SDR DALA2023112209651](https://openairdocs.org/sdr/DALA2023112209651), Nov 21, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00188: FRAME TAB OF THE 
- [SDR DALA2023112209650](https://openairdocs.org/sdr/DALA2023112209650), Nov 21, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00189: FRAME TAB OF THE 
- [SDR DALA2023112109573](https://openairdocs.org/sdr/DALA2023112109573), Nov 20, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE. SUMMARY OF NRC 00252: FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE WAS REPAIRED PER ERA 6
- [SDR DALA2023112009530](https://openairdocs.org/sdr/DALA2023112009530), Nov 20, 2023: UNKNOWN. UNKNOWN. CRACK ON FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT. SUMMARY OF NRC 00290: FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT WAS REPAIRED PER B717 SRM 53-00-00
- [SDR DALA2023112009529](https://openairdocs.org/sdr/DALA2023112009529), Nov 20, 2023: UNKNOWN. UNKNOWN. CRACKS (2 EA) ON EXTERNAL FUSELAGE SKIN ON PREVIOUS REPAIR AREA, BTW STA 503-522 AND BTW LONG 27RH AND 29RH. SUMMARY OF NRC 00505: EXTERNAL FUSELAGE SKIN BTW ST
- [SDR DALA2023112009518](https://openairdocs.org/sdr/DALA2023112009518), Nov 16, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON THE CONTRAFRAME STRUCTURE OF THE AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00362: COUNTERFRAME STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11
- [SDR DALA2023111509404](https://openairdocs.org/sdr/DALA2023111509404), Nov 14, 2023: UNKNOWN. UNKNOWN. CRACKS ON PAN AFT UPPER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00130: PAN AFT UPPER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDU
- [SDR DALA2023110809201](https://openairdocs.org/sdr/DALA2023110809201), Nov 7, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1037 L17L AT PAX CABIN. SUMMARY OF NRC 00201: FRAME STA 1037 L17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-41-05-0G PAR 8 AND 53-20-07-2
- [SDR DALA2023110709160](https://openairdocs.org/sdr/DALA2023110709160), Nov 6, 2023: UNKNOWN. UNKNOWN. CRACKS WERE GENERATED AROUND FASTENER HOLES OF REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APPROX, DURING REMOVAL OF FASTENERS. 
- [SDR DALA2023051803950](https://openairdocs.org/sdr/DALA2023051803950), May 13, 2023: UNKNOWN. UNKNOWN. SHIP 9570 -ATO- THE PILOT ABORTED THE TAKEOFF AT 100 KTS DUE TO THE AIRCRAFT DRIFTING LEFT OF CENTER LINE. CORRECTIVE ACTION: MAINTENANCE PERFORMED A HIGH ENERG
- [SDR DALA2023050203398](https://openairdocs.org/sdr/DALA2023050203398), May 2, 2023: UNKNOWN. UNKNOWN. FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51. OPERATIO
- [SDR DALA2023030201550](https://openairdocs.org/sdr/DALA2023030201550), Feb 23, 2023: NONE. NONE. FOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PR
- [SDR DALA2023022201320](https://openairdocs.org/sdr/DALA2023022201320), Feb 17, 2023: NONE. NONE. LONGERON TEMPORARY REPAIR INSTALLED AT 25R BETWEEN STA 1022 AND STA 1042. COMPLIED WITH LONGERON SPLICE REPAIR PER B717 SRM 53-00-05-2R REPAIR 2 LONGERON REPAIR
- [SDR DALA2023021501182](https://openairdocs.org/sdr/DALA2023021501182), Feb 13, 2023: NONE. NONE. AIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOC
- [SDR DALA2022110107062](https://openairdocs.org/sdr/DALA2022110107062), Oct 10, 2022: UNKNOWN. FAULTED. UPON LANDING GEAR EXTENSION, ALL OF THE EMERGENCY EXIT LIGHTS EXTINGUISHED (WENT INOPERATIVE). MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS. ALL LIGHT
- [SDR DALA2022080305324](https://openairdocs.org/sdr/DALA2022080305324), Jul 23, 2022: NONE. NONE. ---SUPPLEMENTAL INFORMATION: ATL 10AUG22 INSTALLED LEFT LOGO LIGHT PER B717 AMM 33-41. OPS CHECK GOOD. THIS CLEARS CDL. PLACARDS REMOVED. M PROCEDURES REVERSED.
- [SDR DALA2022022401206](https://openairdocs.org/sdr/DALA2022022401206), Feb 24, 2022: NONE. NONE. THE AFT EMERGENCY OVERWING DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51-04. OPERATIONAL CHECKS IS NOW GOOD. (LP #854
- [SDR DALA2021110406788](https://openairdocs.org/sdr/DALA2021110406788), Oct 25, 2021: NONE. NONE. CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA). SUMMARY NRC #00213: CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA) WAS TREATED. THE AREA REWORKED IS
- [SDR DALA2021102606617](https://openairdocs.org/sdr/DALA2021102606617), Oct 25, 2021: NONE. NONE. CORROSION ON LOWER DOOR JAMB PAN BTW STA 954 -994 AT AFT CARGO COMPARMTENT. SUMMARY OF NRC 00067: CORROSION LEVEL 2, LOWER DOOR JAMB PAN BTW STA 954-994 AT AFT 
- [SDR DALA2021102606616](https://openairdocs.org/sdr/DALA2021102606616), Oct 25, 2021: NONE. NONE. CORROSION ON FRAME AT STA Y=927 AND L-30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00222: CORROSION LEVEL 2, FRAME AT STA Y=927 AND L-30 WAS REPAIRED PER B-717-200
- [SDR DALA2021102606615](https://openairdocs.org/sdr/DALA2021102606615), Oct 25, 2021: NONE. NONE. CORROSION ON FRAME AT STA Y=908 AND L-29L TO L-29R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2 FRAME AT STA Y=908 AND L-29L TO L-29R WAS REP
- [SDR DALA2021102606611](https://openairdocs.org/sdr/DALA2021102606611), Oct 23, 2021: NONE. NONE. LOOSE FASTENER ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00249: PERMANENT REPAIR WAS PERFORMED ON CLIP STA Y=1152 AND LONG 1L 
- [SDR DALA2021102606610](https://openairdocs.org/sdr/DALA2021102606610), Oct 23, 2021: NONE. NONE. CARGO DOOR JAMB WEB WAS FOUND CRACKED ON FRAME AT STA Y=954 AND BETWEEN L-29R TO L-27R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: FRAME AT STA Y=954 AND BETW
- [SDR DALA2021102606609](https://openairdocs.org/sdr/DALA2021102606609), Oct 23, 2021: NONE. NONE. CARGO DOOR JAMB WEB WAS FOUND CRACKED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00221: REPAIR WAS PERFOMED O
- [SDR DALA2023120710005](https://openairdocs.org/sdr/DALA2023120710005), Oct 22, 2021: UNKNOWN. UNKNOWN. FUSELAGE FRAMES STA 954.0 BETWEEN L- 28R & L-29R IS CRACKED. REPAIR PER SECTION I IS TIME LIMITED AND REQUIRES REPLACEMENT WITH SECTION II PERMANENT REPAIR. ACC
- [SDR DALA2021101806407](https://openairdocs.org/sdr/DALA2021101806407), Oct 17, 2021: NONE. NONE. CORROSION ON LONGERON L-29L AT STA Y=946 AND Y=954, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00244: CORROSION LEVEL 2, LONGERON L-29L AT STA Y=946 AND Y=954 AFT CA

All 187: https://openairdocs.org/aircraft/N929AT/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/N929AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The BMW Rolls BR-700 series engine: https://openairdocs.org/engine/bmw-rolls-br-700-series.md

---
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