# N934AT: 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: 55070
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 1, 2000
- Certificate issued: July 31, 2024
- Expires: July 31, 2031
- Mode S code: ACF497
- 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=934AT
- Page: https://openairdocs.org/aircraft/N934AT

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/N934AT/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 N934AT.

## FAA accident and incident reports (1)

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

- [Incident 20060922028919I](https://openairdocs.org/incident/20060922028919I), Sep 22, 2006: Boeing 717200 (N934AT), Champaign-Urban, IL. (-23) Air tran flight 895, a Boeing 717 aircraft on a flight from boston, ma to chicago, IL diverted to to Champaign, Illinois due to weather. The flight crew…

## Service difficulty reports (204, 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 DALA2026071304091](https://openairdocs.org/sdr/DALA2026071304091), Jul 10, 2026: TRANSCEIVER. FAULTY. ATB- RETURNED TO DTW DUE TO MULTIPLE FAULTS AFTER GEAR RETRACTION. REPLACED ALL RADIO ALTIMETER ANTENNAS AND BOTH TRANSCEIVERS. GEAR SWING AND RADIO ALTIMETER O
- [SDR DALA2026070103877](https://openairdocs.org/sdr/DALA2026070103877), Jul 1, 2026: COALESCER BAG. ODOR. BURNING SMELL WITH APU ON AND PACKS, R & R COALESCER BAGS PER B717 AMM 21-54-08. (6688572) (AIRCRAFT GROUNDED).
- [SDR DALA2026042902730](https://openairdocs.org/sdr/DALA2026042902730), Apr 24, 2026: HINGE FITTING. DAMAGED. SHIP 9565 LH WING T.E. FLAP ON FWD IDLER HINGE FITTING OUTBD LUG BORE DAMAGED. CORRECTIVE ACTION: REPAIRED PER ER/A 633228-14. (1559850) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402347](https://openairdocs.org/sdr/DALA2026041402347), Apr 7, 2026: NOT REPORTED. NOT REPORTED. REFERENCE ER/A626909-14AD. COMPLIED WITH ER/A626909-14AD (1533159) (AIRCRAFT GROUNDED)
- [SDR DALA2025092306961](https://openairdocs.org/sdr/DALA2025092306961), Sep 22, 2025: STRAP. DAMAGED. COMPLY WITH ER/A 626909-14AD SECTION IV LT WING REAR SPAR LOWER STRAP REPAIR. COMPLIED WITH ER/A 626909-14AD REV. E SECTION IV AND PRI 626909- 14AD REV. E REV 0
- [SDR DALA2025090406564](https://openairdocs.org/sdr/DALA2025090406564), Aug 21, 2025: SPAR CAP. CRACKED. LEFT WING REAR SPAR, LOWER CAP, AFT FLANGE CRACKED NEAR XRS = 164. REPAIRED PER ER/A 00-626909. (1156447)
- [SDR DALA2025062604793](https://openairdocs.org/sdr/DALA2025062604793), Jun 25, 2025: GIRT BAR. DETACHED. SHIP 9565 GIRT BAR DETACHED FROM 1R DOOR. CORRECTIVE ACTION: RE ATTACHED LANYARD ASSY. IAW 717 AMM 25-61 (6588676)
- [SDR DALA2025061504506](https://openairdocs.org/sdr/DALA2025061504506), Jun 13, 2025: SPAR CAP. CRACKED. AIRCRAFT 9565, WHILE MAINTENANCE IN DTW WAS ACCOMPLISHING AA WORKCARD 5720-01103-01A, MTC DISCOVERED A CRACK COMMON TO THE LH WING LOWER SPAR CAP (P/N 5911301-5
- [SDR DALA2025060604344](https://openairdocs.org/sdr/DALA2025060604344), May 29, 2025: SPAR CAP. CRACKED. SHIP 9565 CRACK FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP AFT LEG. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REF FC
- [SDR DALA2025012800656](https://openairdocs.org/sdr/DALA2025012800656), Jan 23, 2025: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS ARE INOPERATIVE AT THE FWD LIGHT ATTENDANT STATION. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IN THE AFT CARGO COMPART
- [SDR DALA2024022702692](https://openairdocs.org/sdr/DALA2024022702692), Feb 24, 2024: CONTROL VALVE. MALFUNCTIONED. SHIP 9565 -ATB/DE- THE CREW PERFORMED AN AIR TURNBACK AND DECLARED AN EMERGENCY WITH ATC DUE TO A SLAT DISAGREE. THE AIRCRAFT REQUIRED SIGNIFICANT AILERON CORRE
- [SDR DALA2023120609979](https://openairdocs.org/sdr/DALA2023120609979), Dec 5, 2023: UNKNOWN. UNKNOWN. ELONGATED HOLES ON FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE. (IN REF TO NRC: 00238). SUMMARY OF NRC 00298: FUSELAGE BTW CANTED STA Y=1
- [SDR DALA2023120409900](https://openairdocs.org/sdr/DALA2023120409900), Dec 2, 2023: UNKNOWN. UNKNOWN. WEAR ON LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING. SUMMARY OF NRC00114: LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING WAS REPAIRED PER ER/A 613673
- [SDR DALA2024022002333](https://openairdocs.org/sdr/DALA2024022002333), Dec 1, 2023: SKIN. CORRODED. CORROSION ON UPPER SKIN OF CENTER WING AREA BTW STA 710 TO STA 756 AND X=-40 TO X=-56 AT CPAX. SUMMARY OF NRC 00354: CORROSION LEVEL 2. UPPER SKIN OF CENTER WIN
- [SDR DALA2023113009839](https://openairdocs.org/sdr/DALA2023113009839), Nov 29, 2023: UNKNOWN. UNKNOWN. INAPPROPRIATE HOLES ON VERTICAL BEAMS STA Y=817 AND STA X=0, X=13, 25, X=-13, -25 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00184: VERTICAL BEAMS ON STA Y=8
- [SDR DALA2023113009838](https://openairdocs.org/sdr/DALA2023113009838), Nov 29, 2023: UNKNOWN. UNKNOWN. CRACK FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R. SUMMARY OF NRC 00259: PERMANENT REPAIR ON FRAME ON AFT FACE OF 
- [SDR DALA2023113009837](https://openairdocs.org/sdr/DALA2023113009837), Nov 29, 2023: UNKNOWN. UNKNOWN. CRACK AT FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT IN COCKPIT. SUMMARY OF NRC 00583: FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT WAS R
- [SDR DALA2023113009836](https://openairdocs.org/sdr/DALA2023113009836), Nov 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH TIE TRACK BTW STA Y=813/954 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00215: CORROSION LEVEL 2. RH TIE TRACK BTW STA Y=813/954 WAS REPLACED 
- [SDR DALA2023112909802](https://openairdocs.org/sdr/DALA2023112909802), Nov 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 AT AFT PAX CABIN. SUMMARY OF NRC 00250: CORROSION LEVEL 2. LOWER EDGE OF BU
- [SDR DALA2023112909801](https://openairdocs.org/sdr/DALA2023112909801), Nov 29, 2023: UNKNOWN. UNKNOWN. WEAR ON AFT HINGE. ALSO WEAR ON INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR. SUMMARY OF NRC 00075: INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR WAS
- [SDR DALA2023112809762](https://openairdocs.org/sdr/DALA2023112809762), Nov 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH TIE TRACK BTW STA Y=813/1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC S/N 00217: CORROSION LEVEL 2. LH TIE TRACK BTW STA Y=813/1022 AT AFT 
- [SDR DALA2023112809756](https://openairdocs.org/sdr/DALA2023112809756), Nov 27, 2023: UNKNOWN. UNKNOWN. DENT FOUND ON RUDDER CONTROL TAB, RH SURFACE BTW STA ZR=43 TO ZR=52 9.5" FROM T/E. SUMMARY OF NRC 00614: RUDDER CONTROL TAB RH SURFACE BTW STA ZR=43 TO ZR=52 9.
- [SDR DALA2023112709719](https://openairdocs.org/sdr/DALA2023112709719), Nov 22, 2023: UNKNOWN. UNKNOWN. AFTER PADS WERE REMOVED, PUNCTURE AND CRACKS WERE FOUND ON LOWER MOVABLE FLAP VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00407: MOVABLE FLAP VANE OF RH WING WAS
- [SDR DALA2023112709716](https://openairdocs.org/sdr/DALA2023112709716), Nov 22, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND OUT OF LIMITS ON RH SEAT TRACK (X=-54) STA Y=395-397, Y=748-755, AND Y=765-773 AT PAX CABIN. SUMMARY OF NRC 00555: CORROSION LEVEL 2. RH SEAT TR
- [SDR DALA2023112109570](https://openairdocs.org/sdr/DALA2023112109570), Nov 19, 2023: UNKNOWN. UNKNOWN. CUSP WEB BTW STA Y=715 TO STA Y=756 AND X=-40 TO X=-56 AT PAX CABIN WAS NOTED TO HAVE CRACKS IN THE WEB. SUMMARY OF NRC 00613: CUSP WEB BTW STA Y=715 TO STA Y=7
- [SDR DALA2023112209653](https://openairdocs.org/sdr/DALA2023112209653), Nov 18, 2023: UNKNOWN. UNKNOWN. CRACK ON RH CUSP MEMBRANE WEB BTW STA 484 TO STA 503, ALSO BTW STA 655 TO STA 725 AT PAX CABIN. SUMMARY OF NRC 00331: RH CUSP MEMBRANE WEB ON STA 655 TO STA 715
- [SDR DALA2023112009526](https://openairdocs.org/sdr/DALA2023112009526), Nov 18, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND AT CUSP WEB ON FUSELAGE STA 218, X= 56. SUMMARY OF NRC 00609: LH CUSP WEB ON FUSELAGE STA 218, X=56 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCED
- [SDR DALA2023112009523](https://openairdocs.org/sdr/DALA2023112009523), Nov 18, 2023: UNKNOWN. UNKNOWN. CRACK CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X=56 AT CABIN PAX. SUMMARY OF NRC 00598: CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X =56 WAS REPAIRED PER B717 SRM 53-00
- [SDR DALA2023112009522](https://openairdocs.org/sdr/DALA2023112009522), Nov 17, 2023: UNKNOWN. UNKNOWN. WEAR ON AFT EDGE NEAR OF AFT LATH ON AFT CARGO DOOR. SUMMARY OF NRC 00083: AFT EDGE (INNER PAN) NEAR OF AFT LATH ON AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER 
- [SDR DALA2023112009521](https://openairdocs.org/sdr/DALA2023112009521), Nov 17, 2023: UNKNOWN. UNKNOWN. CRACK ON LH CUSP MEMBRANE WEB STA 597. SUMMARY OF NRC 00603: LH CUSP MEMBRANE WEB STA 597 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 PAR. 5, FIGURE 211. (LP #0
- [SDR DALA2023112009519](https://openairdocs.org/sdr/DALA2023112009519), Nov 17, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP WEBS STA Y=292 TO 294 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. LH CUSP WEB STA Y=292 TO 294 WAS REPAIRED PER B717 SRM 53-00-5
- [SDR DALA2023112009516](https://openairdocs.org/sdr/DALA2023112009516), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP MEMBRANE WEB BTW STA Y=891 TO Y=908 AT PAX CABIN WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 PAR 4 FIG 101. (ORIGINAL THIC
- [SDR DALA2023112009515](https://openairdocs.org/sdr/DALA2023112009515), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS IS OUT LIMITS AT STA Y=148 BTW X=-44 AND X=-51, STA Y=200 BTW X=-9 AND X=-44, STA Y=173 TO STA Y=191 AND X=55, AND STA Y=210 AND X=-
- [SDR DALA2023111609441](https://openairdocs.org/sdr/DALA2023111609441), Nov 16, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND AT JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 LH. SUMMARY NRC 00604: CORROSION LEVEL 2. JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 WAS REP
- [SDR DALA2023111509408](https://openairdocs.org/sdr/DALA2023111509408), Nov 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEBS RH STA Y=953 TO Y=955 AND Y=958 TO Y=963. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CORROSION ON CUSP WEBS RH STA Y=953 TO Y=970 WAS REPAI
- [SDR DALA2023111509406](https://openairdocs.org/sdr/DALA2023111509406), Nov 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEBS STA Y=580 TO 590 AND STA Y=597 IN REF NRC 00551. SUMMARY OF NRC 00573: CORROSION LEVEL 2. CORROSION ON RH CUSP WEBS STA Y=580 TO 590 A
- [SDR DALA2023111509405](https://openairdocs.org/sdr/DALA2023111509405), Nov 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR MEMBRANES STA Y=198 X=-15, Y=198 X=-20, Y=180 X=-15, Y=184 X=-20, Y=183 X=-6, AND Y=197 X=50. SUMMARY OF NRC 00547: CORROSION LEVEL 2. CORROS
- [SDR DALA2023111409353](https://openairdocs.org/sdr/DALA2023111409353), Nov 14, 2023: UNKNOWN. UNKNOWN. CRACK FLOOR BEAM STA Y=737 AND X=53 APROX AT PAX CABIN. SUMMARY OF NRC 00262: FLOOR BEAM STA Y=737 AND X=53 APROX WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-
- [SDR DALA2023111309308](https://openairdocs.org/sdr/DALA2023111309308), Nov 13, 2023: UNKNOWN. UNKNOWN. OUT OF LIMITS CUSP MEMBRANE WEB STA 944, X=58 AND STA 948, X=50 AT CABIN PAX. SUMMARY OF NRC 00564: CORROSION LEVEL 2. CUSP MEMBRANE WEB STA 944, X=58 AND STA 9
- [SDR DALA2023111309307](https://openairdocs.org/sdr/DALA2023111309307), Nov 13, 2023: UNKNOWN. UNKNOWN. CRACK ON LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 AT PAX CABIN. SUMMARY OF NRC 00327: LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 WAS REPAIRED PER B717 SRM 5
- [SDR DALA2023111309304](https://openairdocs.org/sdr/DALA2023111309304), Nov 10, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN BTW BEAM 1-3 STA 160 AT FWD PASS DOOR. SUMMARY OF NRC 00050: PAN WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0059117)
- [SDR DALA2023111309302](https://openairdocs.org/sdr/DALA2023111309302), Nov 10, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB BTW STA Y=190 TO 180 X=55 APROX AT CABIN PAX. SUMMARY OF NRC 00574: WEB BTW STA Y=190 TO 180 X=55 APROX WAS REPAIRED PER B717 SRM 51-70-10-2R REPAI
- [SDR DALA2023111309301](https://openairdocs.org/sdr/DALA2023111309301), Nov 10, 2023: UNKNOWN. UNKNOWN. CORROSION LH CUSP MEMBRANE WEB BTW STA Y=562 TO Y=579 IS OUT OF LIMITS. SUMMARY OF NRC 00570: CORROSION LEVEL 2. MEMBRANE WEB BTW STA Y=562 TO Y=579 WAS REPAIRE
- [SDR DALA2023110909224](https://openairdocs.org/sdr/DALA2023110909224), Nov 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEBS RH STA Y=1026 TO Y=1030. SUMMARY OF NRC 00490: CORROSION LEVEL 2. CUSP WEB RH STA Y=1026 TO Y=1030 WAS REPLACED PER B717 SRM 51-41-02-0G 
- [SDR DALA2023110809200](https://openairdocs.org/sdr/DALA2023110809200), Nov 7, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN. SUMMARY OF NRC 00269: FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN WAS REPAIRED PER B717 SRM 
- [SDR DALA2023110709162](https://openairdocs.org/sdr/DALA2023110709162), Nov 7, 2023: UNKNOWN. UNKNOWN. BROKEN UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR (L1). SUMMARY OF NRC 00383: UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR W
- [SDR DALA2023040502674](https://openairdocs.org/sdr/DALA2023040502674), Mar 31, 2023: UNKNOWN. UNKNOWN. AFT CARGO DOOR FRAME STRUCK BY BELT LOADER IN MSP. REMOVED DAMAGE DOUBLER, DAMAGE CONTAINED. ACCOMPLISHED HFEC INSPECTION OF CUT-OUT IAW NDT SPM 06-10-01.01. NO
- [SDR DALA2022121308026](https://openairdocs.org/sdr/DALA2022121308026), Dec 12, 2022: LIGHT. INOPERATIVE. THE OVER WING EMERGENCY EXIT LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE (FWD LIGHTS). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND THE EMERGE
- [SDR DALA2021112307180](https://openairdocs.org/sdr/DALA2021112307180), Nov 22, 2021: NONE. NONE. THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN COVER IS MISSING AT DOOR 1R. MAINTENANCE INSTALLED EXIT SIGN COVER. OPERATIONAL CHECK WAS GOOD. (LP #
- [SDR DALA2021102606607](https://openairdocs.org/sdr/DALA2021102606607), Oct 18, 2021: NONE. NONE. FLOOR SUPPORT AT RBL 12 AND STA 160 TO STA 200 HAS AREAS OF LIGHT CORROSION. SUMMARY SEE NRC 061-0023:5310-2005/006 00477: REMOVED CORROSION ON SUPPORT AND FOUN

All 204: https://openairdocs.org/aircraft/N934AT/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/N934AT/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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