# N932AT: 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: 55073
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 2000
- Certificate issued: December 16, 2024
- Expires: December 31, 2031
- Mode S code: ACED29
- 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=932AT
- Page: https://openairdocs.org/aircraft/N932AT

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/N932AT/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 N932AT.

## FAA accident and incident reports

None matched to N932AT.

## Service difficulty reports (265, 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 DALA2026081704697](https://openairdocs.org/sdr/DALA2026081704697), Aug 16, 2026: SPAR CAP. DAMAGED. HOLES 2IB, 6IB, 12 AND 141WERE FOUND DAMAGED AT LT WING, REAR SPAR, LOWER CAP, XRS=164. COMPLIED WITH ER/A 628386-14. (6542957) (AIRCRAFT GROUNDED).
- [SDR DALA2026081204641](https://openairdocs.org/sdr/DALA2026081204641), Aug 11, 2026: SPAR CAP. DAMAGED. RIGHT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW ER/A 628367-14AD (1751283) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080704570](https://openairdocs.org/sdr/DALA2026080704570), Aug 6, 2026: SPAR CAP. DAMAGED. DAMAGED FASTENER HOLES ON LH LOWER SPAR CAP BTW XRS=110 TO 200 APROX AND LOWER SKIN PANEL ON LH WING, CORRECTIVE ACTION: COMPLIED WITH ER/A 628386-14AD. (174196
- [SDR DALA2026080404489](https://openairdocs.org/sdr/DALA2026080404489), Aug 3, 2026: MOUNT. CORRODED. CORROSION ON FASTENERS HOLES HOLDING (8 EA) ALSO MOUNTING FLANGE (UPPER HOLES) AT RIGHT WING FLAP INNER HINGE. REPAIRED PER BOEING OVERHAL MANUAL 27-50. (173678
- [SDR DALA2026080304469](https://openairdocs.org/sdr/DALA2026080304469), Jul 31, 2026: FUEL SYS. LEAKING. LT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW ER/A 00-628386. (1731448) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080304468](https://openairdocs.org/sdr/DALA2026080304468), Jul 31, 2026: FUEL SYS. LEAKING. RIGHT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW 00-628367. (1731231) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026073004419](https://openairdocs.org/sdr/DALA2026073004419), Jul 30, 2026: DOOR FRAME. CRACKED. CRACK ON UPPER DOOR JAMB AT FWD EMERGENCY EXIT DOOR RH SURROUND STRUCTURE. UPPER DOOR JAMB AT FWD EMERGENCY EXIT DOOR RH SURROUND STRUCTURE WAS REPAIRED PER ER/
- [SDR DALA2026072804382](https://openairdocs.org/sdr/DALA2026072804382), Jul 28, 2026: LUG. GOUGED. GOUGES ON INBD LUG (OUTB FACE) AND WEAR ON OUTBD LUG (INNER FACE) ALSO CORROSION AND SCRATCHES ON BUSHINGS AT LEFT FLAP FWD HINGE FITTING NR 3. REPAIRED PER ERA
- [SDR DALA2026072804381](https://openairdocs.org/sdr/DALA2026072804381), Jul 28, 2026: LUG. WORN. WORN OUTBD LUG INBD FACE AT RIGHT FLAP FWD HINGE FITTING NO. 3. CORRECTIVE ACTION: REPAIRED PER ERA 628285-14. (1724181) AIRCRAFT GROUNDED.
- [SDR DALA2026072404316](https://openairdocs.org/sdr/DALA2026072404316), Jul 24, 2026: CONTROL CABLE. WORN. WEAR ON CABLE 185B BTW STA XIS 100 AND XIS 120 OF SLAT SYSTEM AT LT WING, REPAIRED SLAT CONTROL CABLE PER B717 AMM 27-81. (1716656) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004259](https://openairdocs.org/sdr/DALA2026072004259), Jul 17, 2026: SKIN. CRACKED. CRACKED FUSELAGE SKIN. REPAIRED PER ER/A 605226-14. (1705409) AIRCRAFT GROUNDED.
- [SDR DALA2026071704215](https://openairdocs.org/sdr/DALA2026071704215), Jul 16, 2026: SKIN. CORRODED. CORROSION ON WING BOX UPPER SKIN AREA BTW STA 716 TO 737 X=-44.5 TO X=-56.0, COMLIED WITH ER/A 634543-14AD. (1702309) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704214](https://openairdocs.org/sdr/DALA2026071704214), Jul 16, 2026: DOUBLER. CORRODED. CORROSION ON DOUBLER STA Y=1053 BTW LONG'S 29RH TO 29LH APROX LWR AREA AT AFT CARGO COMPARTMENT, REPLACED DOUBLER IAW SRM 51-41-05-0G AND SRM 51-41-02-0G. (1702
- [SDR DALA2026071704213](https://openairdocs.org/sdr/DALA2026071704213), Jul 15, 2026: DOUBLER. CRACKED. CRACK AT PREVIOUS REPAIR DOUBLER ON INTERNAL PAN BTW BEAM 1 AND 2 AT AFT EDGE OF FWD CARGO DOOR (C1), COMPLIED WITH ER/A 634307-14. (1702038) (AIRCRAFT GROUNDED
- [SDR DALA2026071304127](https://openairdocs.org/sdr/DALA2026071304127), Jul 13, 2026: STIFFENER. CRACKED. CRACK ON INNER SKIN BELOW FWD LOWER STIFFENER AT FWD CARGO DOOR. REPAIRED PER PRI 634332-14. (1696617) (AIRCRAFT GROUNDED)
- [SDR DALA2026070603940](https://openairdocs.org/sdr/DALA2026070603940), Jul 3, 2026: RETAINER. CRACKED. CRACKED RETAINER BELOW RT ELEVATOR BOOST CYLINDER AT RT HORIZONTAL STAB. RETAINER BELOW RH ELEVATOR BOOST CYLINDER AT RT HORIZONTAL STAB WAS REPLACED IAW AMM 27
- [SDR DALA2026070603938](https://openairdocs.org/sdr/DALA2026070603938), Jul 3, 2026: SKIN. DENTED. DENTS ON SKIN PANEL RT SIDE BTW ZRS=75.762 TO ZRS=93.821 RUDDER. REPAIRED IAW SRM 51-70-13-2R. (1680626)(AIRCRAFT GROUNDED)
- [SDR DALA2026070603937](https://openairdocs.org/sdr/DALA2026070603937), Jul 3, 2026: SKIN. DENTED. DENTED SKIN PANEL RH SIDE BTW ZRS=75.762 TO ZRS=93.821 RUDDER. MEASURED AND FOUND WITHIN LIMITS IAW SRM 55-40-01-1A. (1680620)(AIRCRAFT GROUNDED)
- [SDR DALA2026070603936](https://openairdocs.org/sdr/DALA2026070603936), Jul 3, 2026: SKIN. DENTED. DENTED ON SKIN PANEL RT SIDE AT RUDDER. REPAIRED IAW SRM 51-70-13-2R. (1680621)(AIRCRAFT GROUNDED).
- [SDR DALA2026070303899](https://openairdocs.org/sdr/DALA2026070303899), Jul 3, 2026: SKIN. CRACKED. CRACK WAS FOUND ON EXTERNAL SKIN NEXT TO HOLE TO ATTACH SLIN AT RUDDER, REPAIRED EXTERNAL SKIN PER SRM 51 -70-13-2R. (1679238) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903838](https://openairdocs.org/sdr/DALA2026062903838), Jun 27, 2026: DOOR FRAME. CORRODED. CORROSION LEVEL 2. DOOR JAMB BTW STA Y=370 TO Y=427. REPLACED DAMAGED COMPONENT IAW SRM 51-41-02-0G AND SRM 51-41-08-0G. (1669491) (AIRCRAFT GROUNDED).
- [SDR DALA2026061903679](https://openairdocs.org/sdr/DALA2026061903679), Jun 19, 2026: HINGE FITTING. CORRODED. CORROSION LEVEL 2 IN FASTENERS HOLES HOLDING 8 EAS LT WING FLAP INNER HINGE. LT WING FLAP INNER HINGE WAS REPLACED PER SERVICEABLE INNER HINGE IAW AMM 57-55-25.
- [SDR DALA2026061903678](https://openairdocs.org/sdr/DALA2026061903678), Jun 19, 2026: WINDOW FRAME. CRACKED. LT AND RT SLIDE WINDOW FRAME UPPER AFT CORNER AT COCKPIT WERE FOUND: CRACKS ON INNER SURFACE AT UPPER/LOWER RETAINERS LT/RT COCKPIT. CRACKS ON INNER SURFACE AT 
- [SDR DALA2026060903436](https://openairdocs.org/sdr/DALA2026060903436), Jun 3, 2026: NOT REPORTED. CORRODED. IN REFERENCE TO NRC 706 WIP NR 9, CORROSION OUT OF LIMITS AT RT SIDE. REPAIRED IAW SRM 53-00-55 (1628543) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203340](https://openairdocs.org/sdr/DALA2026060203340), May 30, 2026: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS, IN REFERENCE TO NRC 00700: CORROSION ON LH SIDE FLOOR CUSP WEB. REPAIRED PER B717-200 SRM 53-00-55 (1621710) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903259](https://openairdocs.org/sdr/DALA2026052903259), May 28, 2026: STRUCTURE. CORRODED. AFTER BOLT AND BARREL NUT REMOVAL. CORROSION ON INNER HOLE, BOLT, WASHER AND NUT BARREL WERE FOUND. REPAIRED PER ER/A 634191-14AD. (1618112) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903254](https://openairdocs.org/sdr/DALA2026052903254), May 26, 2026: CUSP WEB. CORRODED. OUT OF LIMITS CORROSION ON RT SIDE FLOOR CUSP WEB. REPAIRED PER SRM 53-00-55 (1613746) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803224](https://openairdocs.org/sdr/DALA2026052803224), May 23, 2026: LONGERON. CRACKED. CRACKED LONGERONS 5R, 6R, 7R AND 8R AT BS 1022. REPAIRED PER SRM 53-00-05 (1607816) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803220](https://openairdocs.org/sdr/DALA2026052803220), May 21, 2026: CUSP WEB. CRACKED. CRACK ON LH SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60. CRACK ON LT SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60 WAS REPAIRE
- [SDR DALA2026051903061](https://openairdocs.org/sdr/DALA2026051903061), May 6, 2026: NOT REPORTED. NOT REPORTED. DTA ER/A 634191-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. C/W ER/A 00-634191. (1592353) (AIRCRAFT GROUNDED)
- [SDR DALA2026051102944](https://openairdocs.org/sdr/DALA2026051102944), May 6, 2026: BEAM. CRACKED. CRACK ON BEAM 1 FWD UPPER EDGE BEYOND STOP DRILL ON PREVIOUS REPAIR AT PASSENGER ENTRANCE DOOR L1. REPAIRED PER B717-200 S.R.M. 52-10-02 (1579574) (AIRCRAFT GRO
- [SDR DALA2026051102942](https://openairdocs.org/sdr/DALA2026051102942), May 5, 2026: WIRE. BROKEN. BROKEN WIRES ON LANDYARD ASSEMBLY (2EAS) OF FORWARD SERVICE/PASSENGER DOOR SLIDE. REPAIRED PER AMDS 5211-4002 AND AMDS 5211-4004 (1579444) (AIRCRAFT GROUNDED)
- [SDR DALA2026031301748](https://openairdocs.org/sdr/DALA2026031301748), Mar 12, 2026: DOOR FRAME. CORRODED. SHIP 9568 SEVERAL AREAS WITH CORROSION ON DOOR JAMB AT AFT CARGO. CORRECTIVE ACTION: DOOR JAMB AT AFT CARGO WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 
- [SDR DALA2025090906667](https://openairdocs.org/sdr/DALA2025090906667), Sep 4, 2025: NONE. NONE. DTA ER/A 628389-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-SEP-25. CORRECTIVE ACTION: REPAIRED ASSOCIATED ER/A 00-
- [SDR DALA2025090206465](https://openairdocs.org/sdr/DALA2025090206465), Aug 24, 2025: NONE. NONE. DTA ER/A 628285-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 24-AUG-25. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NE
- [SDR DALA2025060604331](https://openairdocs.org/sdr/DALA2025060604331), May 27, 2025: SHEAR TIE. CRACKED. SHIP 9568 INITIAL INSPECTION: CRACKED FRAME CLIP ON STA Y=1144 BTW LONG 1 AND LONG 2L ALSO ON STA Y=1152 BTW LONG 1 AND LONG 2L AT AFT ACC . COMPARTMENT. CORREC
- [SDR DALA2025051903829](https://openairdocs.org/sdr/DALA2025051903829), May 15, 2025: LONGERON. CRACKED. SHIP 9568 INITIAL INSPECTION: CRACK ON LONG 2 LH STA Y=1133 AT AFT ACC COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 (0967936)
- [SDR DALA2025051903830](https://openairdocs.org/sdr/DALA2025051903830), May 6, 2025: TAB. DELAMINATED. SHIP 9568 INITIAL INSPECTION: DELAMINATED CONTROL TAB OF AILERON AT LH WING. CORRECTIVE ACTION: AILERON CONTROL TAB WAS REMOVED (PN: UNK, SN: 5106) AND SERVICEA
- [SDR DALA2025041102822](https://openairdocs.org/sdr/DALA2025041102822), Apr 9, 2025: SKIN. LEAKING. -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN AT XRS=164 AA #FE5720-01103. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC 5223]. 
- [SDR DALA2025041102821](https://openairdocs.org/sdr/DALA2025041102821), Apr 9, 2025: ACCESS PANEL. LEAKING. -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CONTACT LIAISON ENG FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT AA #F
- [SDR DALA2025021101060](https://openairdocs.org/sdr/DALA2025021101060), Feb 9, 2025: ATTACH BRACKET. CRACKED. -AD- PRI 622371-14AD, REV 3 HOLE #9 ON OUTBOARD FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DO
- [SDR DALA2025021101059](https://openairdocs.org/sdr/DALA2025021101059), Feb 9, 2025: ATTACH BRACKET. CRACKED. -AD- PRI 622371-14AD, REV 3 HOLE #8 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SK
- [SDR DALA2025021101058](https://openairdocs.org/sdr/DALA2025021101058), Feb 9, 2025: ATTACH BRACKET. CRACKED. -AD- PRI 622371-14AD, REV 3 HOLE #5 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SK
- [SDR DALA2025021101057](https://openairdocs.org/sdr/DALA2025021101057), Feb 9, 2025: ATTACH BRACKET. CRACKED. -AD- PRI 622371-14AD, REV 3 HOLE #1 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SK
- [SDR DALA2025021101056](https://openairdocs.org/sdr/DALA2025021101056), Feb 9, 2025: ATTACH FITTING. CRACKED. -AD- PRI 622371-14AD, REV 2 HOLE #6 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKI
- [SDR DALA2025021101055](https://openairdocs.org/sdr/DALA2025021101055), Feb 9, 2025: ATTACH FITTING. CRACKED. -AD- PRI 622371-14AD, REV 2 HOLE #5 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLCAED DUEING LEFT WING LOWER SKI
- [SDR DALA2025020600921](https://openairdocs.org/sdr/DALA2025020600921), Feb 1, 2025: ATTACH BRACKET. CRACKED. -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #2 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS A CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LE
- [SDR DALA2025020600920](https://openairdocs.org/sdr/DALA2025020600920), Feb 1, 2025: SUPPORT FITTING. DAMAGED. -AD- ON LEFT WING XRS 164.00 LOWER FLAP HINGE SUPPORT FITTING 2ND NUT FORWARD ON INBOARD SIDE IS LOOSE. FASTENER REPLACED DURING LEFT WING LOWER SKIN REPAIR ON 
- [SDR DALA2025020600919](https://openairdocs.org/sdr/DALA2025020600919), Feb 1, 2025: ATTACH BRACKET. DAMAGED. -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #4 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. HOLE #4 OVERSIZED TO 0.363" ON STEP 41 OF PRI 62
- [SDR DALA2025020600918](https://openairdocs.org/sdr/DALA2025020600918), Feb 1, 2025: ATTACH BRACKET. DAMAGED. -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #3 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS 2 CRACK INDICATIONS. HOLE #3 OVERSIZED TO 0.547" ON STEP 41 OF PRI

All 265: https://openairdocs.org/aircraft/N932AT/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/N932AT/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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