# N967AT: 2001 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: 55028
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, operating kit built
- Airworthiness date: February 24, 2026
- Certificate issued: February 2, 2024
- Expires: February 28, 2031
- Mode S code: AD7639
- 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=967AT
- Page: https://openairdocs.org/aircraft/N967AT

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/N967AT/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 N967AT.

## 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 20050322010329I](https://openairdocs.org/incident/20050322010329I), Mar 22, 2005: Boeing 717200 (N967AT), Rochester, NY. (-23) On 3/22/05, [privacy data omitted] was smoking during flight on air tran flight 390 from fll to roc. The aircraft landed at roc without incident. There…

## Service difficulty reports (197, 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 DALA2026102305841](https://openairdocs.org/sdr/DALA2026102305841), Oct 22, 2026: SKIN. DEBONDED. DISBOND ON LOWER SKIN TRIM TAB RH WING AILERON, CORRECTIVE ACTION: R/R TRIM TAB RH AILERON PER B717 AMM 27-10-05-000-801. (1879775) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305837](https://openairdocs.org/sdr/DALA2026102305837), Oct 22, 2026: BEAM. CRACKED. FOUND CRACK ON LL BEAM N 2 ON STA=161.375 AND STA 197.750 AT L1 PASSENGER ENTRANCE DOOR, REPAIRED BEAM PER B717-200 SRM 52-10-02-2R. (1880039) (AIRCRAFT GROUNDE
- [SDR DALA2026102205828](https://openairdocs.org/sdr/DALA2026102205828), Oct 21, 2026: DUCT. CRACKED. CRACK ON LEADING EDGE OF RAM AIR ILNET DUCT LH SIDE AT VERTICAL STABILIZER, COMPLIED WITH ER/A 382101- 14MA. (1878155) (AIRCRAFT GROUNDED).
- [SDR DALA2026093005424](https://openairdocs.org/sdr/DALA2026093005424), Sep 29, 2026: SIGN. DETACHED. FORWARD CABIN EXIT SIGN FELL OFF, RESECURED THE EXIT SIGN OK FOR SVC. (9488778) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004757](https://openairdocs.org/sdr/DALA2026082004757), Aug 17, 2026: LOCALIZER. FAULTED. FOUND A NON-COMPLIANCE ISSUE RELATED TO SATELLITE-BASED AUGMENTATION SYSTEM (SBAS) MESSAGE TYPE 6, COMPLIED WITH ER/A 636183-14. (6771160) (AIRCRAFT GROUNDED).
- [SDR DALA2026030201422](https://openairdocs.org/sdr/DALA2026030201422), Feb 15, 2026: ILS SYSTEM. UNRELIABLE. ILS IS SOMEWHAT NOT RELIABLE, THEREFORE, AN STC FOR "ILS LOOK-ALIKE" LPV IS BEING DEVELOPED AS A BACK UP FOR ILS. ACCOMPLISHED ER/A 632398-14 (1452682)
- [SDR DALA2026020200757](https://openairdocs.org/sdr/DALA2026020200757), Jan 31, 2026: MMR. NOT REPORTED. REMOVED MMR 2 IAW ER/A 625937-14. INSTALLED MMR 2 PER ER/A 625937-14 REV. B (1428881)
- [SDR DALA2025110708144](https://openairdocs.org/sdr/DALA2025110708144), Nov 1, 2025: SIGN. DAMAGED. SHIP 9526 FORWARD CENTER OVERHEAD EXIT SIGN DAMAGED. CORRECTIVE ACTION: R/R FWD ISLE EMERGENCY LIGHT SIGN IAW B717 AMM 33-51. OPS CHECK GOOD. (7608370)
- [SDR DALA2025080205799](https://openairdocs.org/sdr/DALA2025080205799), Jul 28, 2025: FAN. ODOR. SMOKE & FUMES, THE CREW REPORTED ELECTRICAL SMELL IN THE CABIN DURING PUSHBACK AND START OF NR 2 ENGINE. MAINTENANCE REPLACED GASPER BOOSTER FAN.
- [SDR DALA2025010500069](https://openairdocs.org/sdr/DALA2025010500069), Dec 9, 2024: FUEL CELL. LEAKING. -AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING THROUGH FLAP FITTING BOLTS (4 EA WET LEAK) AT XRS=164 LOWER SURFACE (OUTB BOLTS). CONTACT LIAISON ENGINEER
- [SDR DALA2024121611733](https://openairdocs.org/sdr/DALA2024121611733), Jan 30, 2024: REPAIR. UNKNOWN. ERA 615468-14 SECTION I REPAIR REQUIRES DTE WITHIN 12 MONTHS OF AIRCRAFT RETURN TO SERVICE. ADDED FOR AC 9526. REDEFERRED LOG TO QC, ESTAB MON INSP. ER/A 615468
- [SDR DALA2024020101442](https://openairdocs.org/sdr/DALA2024020101442), Jan 28, 2024: SKIN. CRACKED. CRACK AT FWD UPPER CORNER OF R1 DOOR ON FUSELAGE SKIN. REMOVED PAINT AND FASTENER FOR FURTHER EVALUATION PER B717 SRM 51-22-01 AND SRM 51-40-02-06. VERIFIED CRA
- [SDR DALA2024112711264](https://openairdocs.org/sdr/DALA2024112711264), Jun 29, 2023: FRAME. CORRODED. CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R S
- [SDR DALA2023031501885](https://openairdocs.org/sdr/DALA2023031501885), Mar 11, 2023: UNKNOWN. UNKNOWN. NLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUTOUT DAMAGED 2 PLACES. (MARKED) SUMMARY SEE NRC 005-0003:3221-4001/002 00005: REPLACED NLG WHEEL WELL AFT FRAME FOR GEA
- [SDR DALA2023031001761](https://openairdocs.org/sdr/DALA2023031001761), Mar 10, 2023: NONE. NONE. LMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 008-0003:3211-4001/001 00006: REPAIRED PER CMM 57-40-1. (LP #2663943)
- [SDR DALA2023031001760](https://openairdocs.org/sdr/DALA2023031001760), Mar 10, 2023: NONE. NONE. RMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 006-0003:3211-4004/001 00007: REPAIRED PER CMM 57-40-1. (LP #2663936)
- [SDR DALA2023020300858](https://openairdocs.org/sdr/DALA2023020300858), Feb 2, 2023: NOT ENTERED. NOT ENTERED. MAINTENANCE FOUND THE R1 DOOR SLIDE PARTIALLY DEPLOYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.
- [SDR DALA2023010600090](https://openairdocs.org/sdr/DALA2023010600090), Jan 5, 2023: SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN LEFT SIDE AT FS 325, STR 10L, BETWEEN 2 FASTNERS. REMOVED DAMAGED SKIN PER B717 SRM 53-03-01-2R-1 FIG 205 SHEET 5. FABRICATED 
- [SDR DALA2022112107448](https://openairdocs.org/sdr/DALA2022112107448), Nov 17, 2022: ANGLE. CORRODED. EXFOLATION CORROSION ON RH ANGLE CUSP STA 200 TO 206 AT CPAX (CFS). SUMMARY OF NRC 00441: CORROSION LEVEL 2. RH ANGLE CUSP STA 168 TO 218 WAS REPAIRED PER PRI 6
- [SDR DALA2022111707401](https://openairdocs.org/sdr/DALA2022111707401), Nov 16, 2022: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL OVER LONG 30 BTW STA Y=1022 AND Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: CORROSION LEVEL 2. INTERCOSTAL OVER LONG 30 BTW 
- [SDR DALA2022110907242](https://openairdocs.org/sdr/DALA2022110907242), Nov 8, 2022: NONE. NONE. FREEPLAY ON LH WING FLAP OUTBD HINGES PIVOT AREA (STA 331.1). SUMMARY OF NRC 00186: LH WING FLAP OUTBD HINGES PIVOT AREA WAS REPAIRED PER PRI 603178-14 REV 2 & 
- [SDR DALA2022110907241](https://openairdocs.org/sdr/DALA2022110907241), Nov 8, 2022: NONE. NONE. FREEPLAY ON RH WING FLAP OUTBD HINGES PIVOT AREA (STA 331.1). SUMMARY OF NRC 00188: RH WING FLAP OUTBD HINGES PIVOT AREA WAS REPAIRED PER PRI 603122-14 REV 3 & 
- [SDR DALA2022110807205](https://openairdocs.org/sdr/DALA2022110807205), Nov 7, 2022: NONE. NONE. CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R S
- [SDR DALA2022110807204](https://openairdocs.org/sdr/DALA2022110807204), Nov 7, 2022: NONE. NONE. CRACK ON BRACKET UPPER CORNER AFT SIDE OF CUT OUT AT RH SLIDING CLEARVIEW WINDOW COCKTPIT (CPIL) IN REF NRC 00019. SUMMARY OF NRC 00073: CORNER AFT SIDE OF CUT 
- [SDR DALA2022110807203](https://openairdocs.org/sdr/DALA2022110807203), Nov 7, 2022: NONE. NONE. CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R S
- [SDR DALA2022110807202](https://openairdocs.org/sdr/DALA2022110807202), Nov 4, 2022: NONE. NONE. FOUND CORROSION ON FLOOR SUPPORTS STA Y=160-200 AND X=-53 AT CPAX (CFS)(W1)(IN REF NRC NBR 00468). SUMMARY OF NRC 00613: CORROSION LEVEL 2 IS OUT OF LIMITS. SUP
- [SDR DALA2022110207099](https://openairdocs.org/sdr/DALA2022110207099), Oct 31, 2022: WEB. CRACKED. CRACKS (2 PLACES) ON UPPER WEB OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00063: UPPER WEB OF AFT CABIN BULKHEAD DOOR WAS REPLACED PER B717 SRM 51-41-05-0G PAR.
- [SDR DALA2022110107061](https://openairdocs.org/sdr/DALA2022110107061), Oct 31, 2022: ANGLE. CRACKED. CRACK ON CLIP ANGLE NEAR TO UPPER BELLCRANK OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00065: CLIP ANGLE (FITTING ASSY) NEAR TO UPPER BELLCRANK OF AFT CABIN BUL
- [SDR DALA2022110107060](https://openairdocs.org/sdr/DALA2022110107060), Oct 31, 2022: SEAT TRACK. CORRODED. EXFOLATION RH SEAT TRACK X=-22 STA 200 TO 206 AT CPAX (CFS). SUMMARY OF NRC 00446: CORROSION LEVEL 2. RH SEAT TRACK SECTION X=-22 BTW STA 200 TO STA 265 WAS REP
- [SDR DALA2022110107059](https://openairdocs.org/sdr/DALA2022110107059), Oct 29, 2022: SEAT TRACK. CORRODED. AFTER RH SEAT TRACK REMOTION, CORROSION WAS FOUND ON DIAPHRAGM BTW Y=200 AND Y=206 X-22 IN REF NRC 00446. SUMMARY OF 00573: CORROSION LEVEL 2. DIAPHRAGM (WEB) B
- [SDR DALA2022110107058](https://openairdocs.org/sdr/DALA2022110107058), Oct 28, 2022: LONGERON. CORRODED. CORROSION ON LONG 29LH STA Y=908 TO 927 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00260: CORROSION LEVEL 2. LONG 29LH BTW STA Y=908 TO 927 AT AFT CARGO COMP
- [SDR DALA2022102706965](https://openairdocs.org/sdr/DALA2022102706965), Oct 26, 2022: NONE. NONE. CORROSION ON L1 DOOR JAMB SUPPORT STA Y=160-200 AT PAX CABIN (W1). SUMMARY OF NRC 00470: CORROSION LEVEL 2. L1 DOOR JAMB SUPPORTS, 2 EA, STA Y=160-200 AT PAX CA
- [SDR DALA2022102606953](https://openairdocs.org/sdr/DALA2022102606953), Oct 23, 2022: MEMBRANE. CORRODED. CORROSION ON CUSP MEMBRANES BTW X=-54-X=-60 AND BTW STA Y=408-427, 506, 525, 598. ORIGINAL THICKNESS IS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, TH
- [SDR DALA2022102606952](https://openairdocs.org/sdr/DALA2022102606952), Oct 22, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1054 RBL 56 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORT BTW S
- [SDR DALA2022102606951](https://openairdocs.org/sdr/DALA2022102606951), Oct 21, 2022: FLOOR SUPPORT. CORRODED. EXFOLATION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CAPX)(W1). SUMMARY OF NRC 00482: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160- 200 X=-44 WAS REPLACED PER B717-20
- [SDR DALA2022102606950](https://openairdocs.org/sdr/DALA2022102606950), Oct 21, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CAPX)(W1). SUMMARY OF NRC 00472: CORROSION LEVEL 2. FLOOR SUPPORT AT STA Y= 200 BTW X=-9 AND X=-46 WAS 
- [SDR DALA2022102606949](https://openairdocs.org/sdr/DALA2022102606949), Oct 21, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1055 RBL 48 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00492: CORROSION LEVEL 2. FLOOR SUPPORT BTW S
- [SDR DALA2022102606948](https://openairdocs.org/sdr/DALA2022102606948), Oct 21, 2022: FLOOR SUPPORT. CORRODED. EXFOLATION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-43 (CAPX)(W1). SUMMARY OF NRC 00481: CORROSION LEVEL 2. SUPPORT STA Y=180 BTW X =-9 - X=-43 WAS REPLACED PER
- [SDR DALA2022101806740](https://openairdocs.org/sdr/DALA2022101806740), Oct 18, 2022: FLOORBEAM. CORRODED. AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=9 AND X=13 (CAPX)(W1). CORRECTIVE ACTION: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=20
- [SDR DALA2022101806739](https://openairdocs.org/sdr/DALA2022101806739), Oct 18, 2022: FLOORBEAM. CORRODED. AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CAPX)(W1). CORRECTIVE ACTION: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=20
- [SDR DALA2022101806738](https://openairdocs.org/sdr/DALA2022101806738), Oct 16, 2022: CUSP WEB. CORRODED. AIRCRAFT 9526, INITIAL INSPECTION : CORROSION ON PREVIOUSLY REPAIR DOUBLER RH CUSP WEB BTW X=-54 - X=-60 AND STA Y=446-465. CORRECTIVE ACTION: DOUBLER RH CUSP W
- [SDR DALA2022101606676](https://openairdocs.org/sdr/DALA2022101606676), Oct 14, 2022: HINGE. DAMAGED. AIRCRAFT 9526, INITIAL INSPECTION. WEAR ON INTERNAL DOUBLER BTW LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR. CORECTIVE ACTION: PAN OF AFT CABIN BULKHEA
- [SDR DALA2022101406662](https://openairdocs.org/sdr/DALA2022101406662), Oct 13, 2022: LONGERON SPLICE. CORRODED. AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON LONG SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: LONG SPLICE 30 BTW STA Y=889-9
- [SDR DALA2019082644954](https://openairdocs.org/sdr/DALA2019082644954), Aug 24, 2019: SLIDE. NO TEST. THE R1 DOOR SLIDE FAILED THE DEPLOYMENT TEST PER AMDS CARD #2561-9002 FORECAST #95-0525-8-0121. MAINTENANCE REMOVED AND INSTALLED A NEW SERVICEABLE R1 DOOR SLID
- [SDR DALA2019062703887](https://openairdocs.org/sdr/DALA2019062703887), Jun 27, 2019: BATTERY PACK. INOPERATIVE. THE EXIT SIGN ABOVE THE AFT BULKHEAD DOOR IS INOPERATIVE (EMERGENCY LIGHT). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY IAW B717 AMM 33-57-03. OPERATIONAL 
- [SDR DALA2018100205846](https://openairdocs.org/sdr/DALA2018100205846), Sep 30, 2018: BATTERY PACK. DISCHARGED. THE FORWARD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235 REF AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #3914354)
- [SDR DALA2018092005666](https://openairdocs.org/sdr/DALA2018092005666), Sep 18, 2018: DOOR FRAME. CORRODED. CORROSION WAS FOUND ON THE FORWARD CARGO DOOR JAMB. REPLACED DOOR JAMB IN STEPS 1 THRU 5 REF SRM 53-20-15-2R PROC 6.
- [SDR DALA2018091805643](https://openairdocs.org/sdr/DALA2018091805643), Sep 14, 2018: MECHANISM. OUT OF ADJUST. TAILCONE RELEASE CAM MECHANISM IS CLOCKED WRONG. CHECKED CLOCKING AND ADJUSTED, REF BAC DWG 5961568 & AMM 53-52-03.
- [SDR DALA2018082705270](https://openairdocs.org/sdr/DALA2018082705270), Aug 25, 2018: LENS. MISSING. THE FLIGHT ATTENDANT DISCOVERED THE OVERWING EXIT EMERGENCY SIGN COVER WAS MISSING. MAINTENANCE REPLACED THE LENS ASSEMBLY AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR DALA2018052103460](https://openairdocs.org/sdr/DALA2018052103460), May 20, 2018: POWER SUPPLY. CONTAMINATED. THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE FOUND THE POWER SUPPLY ABOVE THE AFT F/A SEAT TO BE SATURATED WITH WATER. MAINTENANCE REPLACED POWER S

All 197: https://openairdocs.org/aircraft/N967AT/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/N967AT/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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