# N933AT: 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: 55071
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 2, 2000
- Certificate issued: August 1, 2024
- Expires: August 31, 2031
- Mode S code: ACF0E0
- 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=933AT
- Page: https://openairdocs.org/aircraft/N933AT

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/N933AT/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 N933AT.

## FAA accident and incident reports

None matched to N933AT.

## Service difficulty reports (176, 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 DALA2026102305843](https://openairdocs.org/sdr/DALA2026102305843), Oct 22, 2026: SKIN. CRACKED. FOUND A CRACK INDICATION COMMON TO ONE (1) HOLE ON THE LEADING EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER, COMPLIED WITH ER/A 613198-14. (1879346) (AIRCRAF
- [SDR DALA2026102305842](https://openairdocs.org/sdr/DALA2026102305842), Oct 22, 2026: SKIN. CRACKED. FOUND CRACK ON VERTICAL STABILIZER RHS LEADING EDGE SKIN, COMPLIED WITH ER/A 613198-14. (1879339) (AIRCRAFT GROUNDED).
- [SDR DALA2026050502823](https://openairdocs.org/sdr/DALA2026050502823), Apr 29, 2026: SPAR CAP. NOT REPORTED. AMOC REQUIRED FOR ERA 583922-14AD REV B. AD 2018-10-08, VERTICAL STAB RH SPAR CAP. REPAIRED PER ER/A 00-583922. (1571590) (AIRCRAFT GROUNDED)
- [SDR DALA2026033002080](https://openairdocs.org/sdr/DALA2026033002080), Mar 27, 2026: CAP. CRACKED. CRACKED CAP BS 1178, & LONG 17L, AFT ACCESORY COMPARTMENT. REPAIRED IAW PRI 632618-14. (1514424)
- [SDR DALA2026020900911](https://openairdocs.org/sdr/DALA2026020900911), Feb 8, 2026: CLAMP. LEAKING. SMOKE AND ODOR IN CABIN, NO PASSENGERS ABOARD, ONLY CREW AND MTC. FOUND EXTERNAL LEAK AT TEE CLAMP BETWEEN GEARBOX AND INLET COMPRESSOR. OPENED PLENUM FOUND INL
- [SDR DALA2025101407522](https://openairdocs.org/sdr/DALA2025101407522), Oct 3, 2025: SENSOR. FAULTED. ON THE GROUND ON APU POWER WHEN RT PACK TURNED ON, DID NOT COME ON. SMELLED SMOKE & THEN GOT PACK R FLO DISAG. TURNED SWITCH OFF AND SMELL WENT AWAY. R & R RT A
- [SDR DALA2025082206252](https://openairdocs.org/sdr/DALA2025082206252), Aug 16, 2025: NOT REPORTED. NO DISCREPANCY. WORKING REP CK RH MLG DOOR KEEL BEAM . C/W REP CK PER ER/A 621720-14 (9858048)
- [SDR DALA2025081806155](https://openairdocs.org/sdr/DALA2025081806155), Aug 13, 2025: STRUT. DISCHARGED. ATB/GEAR- RETURNED ATL DUE TO PSEU FAIL MESSAGE WITH LANDING GEAR INDICATION INCORRECT. GEAR HANDLE UP AND INDICATION SHOWS DOWN. FAULT CLEARED WITH CORRECT IND
- [SDR DALA2025040802706](https://openairdocs.org/sdr/DALA2025040802706), Mar 29, 2025: DEFOG SYSTEM. FAULTED. WHEN COCKPIT CREW TURNED ON THE WINSHIELD ANTI-FOG SWITCH, WHILE AT CRUISE, A SHOWER OF SPARKS SHOT OUT OF THE UPPER EDGE OF FIRST OFFICER'S FORWARD FACING WIND
- [SDR DALA2025021001047](https://openairdocs.org/sdr/DALA2025021001047), Feb 9, 2025: LENS. MISSING. THE FIRST EMERGENCY LIGHT ON CATWALK IN EMPENNAGE IS MISSING THE LENS COVER. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (LP 
- [SDR DALA2024041504429](https://openairdocs.org/sdr/DALA2024041504429), Apr 13, 2024: LENS. MISSING. EMERGENCY LENS COVER AT 17CDE MISSING. MAINTENANCE INSTALLED NEW EMERGENCY LENS COVER AT 17CDE PER B717 AMM 33-51. (LP #5874313)
- [SDR DALA2024041004264](https://openairdocs.org/sdr/DALA2024041004264), Apr 10, 2024: UNION. LEAKING. AN EMERGENCY WAS DECLARED WITH ATC DUE TO THE RIGHT HYDRAULIC FLUID QUANTITY DECREASING. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN TEE ASSEMBLY. OPE
- [SDR DALA2024030703129](https://openairdocs.org/sdr/DALA2024030703129), Mar 2, 2024: SKIN. DAMAGED. BOTTOM FWD CORNER OF AFT CARGO DOOR SKIN DAMAGED. REMOVED CARGO (AFT CARGO) PER B717 AMM 52-31. CUT OUT DAMAGE PER B717 SRM 52-00-01-2R. PERFORMED HFEC INSP OF 
- [SDR DALA2024022002324](https://openairdocs.org/sdr/DALA2024022002324), Feb 20, 2024: SKIN. CORRODED. A.D. RUST IN BARREL NUT AND CORROSION IN BARREL NUT HOLE (HSTAB SKIN) WAS FOUND IN NUT #11 AT RH HSTAB UPPER SIDE, IN REFERENCE NRC 438. SUMMARY OF NRC 00727: H
- [SDR DALA2024021502203](https://openairdocs.org/sdr/DALA2024021502203), Feb 14, 2024: ANGLE. CRACKED. CRACK ANGLE STA 710-715 X=-43 AT CENTER TANK WING UPPER SURFACE AT PAX CABIN (WINGBOX AREA). SUMMARY OF NRC 00320: ANGLE STA 710-715 X=-43 AT CENTER TANK WING U
- [SDR DALA2024021502202](https://openairdocs.org/sdr/DALA2024021502202), Feb 14, 2024: BEAM. CRACKED. CRACKS ON BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER DOOR (L1). SUMMARY OF NRC 00083: BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER
- [SDR DALA2024021402123](https://openairdocs.org/sdr/DALA2024021402123), Feb 14, 2024: UNKNOWN. DAMAGED. ELONGATED HOLES ON AREA TO ATTACH ANCHOR NUT ON SETTLEMENT AREAS OF ACCESS 370CR AT RUDDER LOWER AREA. SUMMARY OF NRC 00455: AREA TO ATTACH ANCHOR NUT ON SETTLE
- [SDR DALA2024021402122](https://openairdocs.org/sdr/DALA2024021402122), Feb 14, 2024: PAN. WORN. WEAR ON EXTERNAL PAN UPPER FWD/AFT CORNERS AT AFT CARGO DOOR. SUMMARY OF NRC 00116: EXTERNAL PAN UPPER FWD CORNER AT AFT CARGO DOOR WAS BLENDED OUT AND MEASURED
- [SDR DALA2024021201855](https://openairdocs.org/sdr/DALA2024021201855), Feb 9, 2024: SKIN. DENTED. DENTS ON RH FWD MOVABLE FLAP. SUMMARY OF NRC 00381: DENTS (10 LOCATIONS) ON RH FWD MOVABLE FLAP, #2, #3, #5, #6, #8, #9, & # 10 WERE EVALUATED AND FOUND TO BE W
- [SDR DALA2024020901764](https://openairdocs.org/sdr/DALA2024020901764), Feb 9, 2024: FRAME. CRACKED. CRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN. SUMMARY OF NRC 00296: CRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN WAS REPAIRED PER PRI 614871-14 REV 2 
- [SDR DALA2024020901763](https://openairdocs.org/sdr/DALA2024020901763), Feb 8, 2024: CAP. CRACKED. CRACK ON CAP STA 1022 AND LONG 1. SUMMARY OF NRC 00351: CAP STA 1022 AND LONG 1 WAS REPAIRED PER PRI 615124-14 REV 0 AND ERA 615124-14 REV ORIGINAL SECTION I: P
- [SDR DALA2024020801687](https://openairdocs.org/sdr/DALA2024020801687), Feb 8, 2024: SKIN. CRACKED. CRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 0514: CRACKS (2 EA) ON FUSELAGE SKIN BTW 
- [SDR DALA2024020801686](https://openairdocs.org/sdr/DALA2024020801686), Feb 7, 2024: SKIN. CRACKED. CRACK ON FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00513: FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT A
- [SDR DALA2024020801684](https://openairdocs.org/sdr/DALA2024020801684), Feb 6, 2024: FRAME. CRACKED. CRACK ON CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX. SUMMARY OF NRC 00257: CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX WAS REPAIRED P
- [SDR DALA2024020601579](https://openairdocs.org/sdr/DALA2024020601579), Feb 6, 2024: FRAME. CRACKED. CRACK ON FRAMES 2 EA, STA Y=660 AND 675 OUTBOARD EDGE LH SIDE OF KEEL BEAM AREA. SUMMARY OF NRC 0807: FRAME STA=660 AND FRAME STA=675 OUTBOARD EDGE LH SIDE OF K
- [SDR DALA2024020601577](https://openairdocs.org/sdr/DALA2024020601577), Feb 4, 2024: PAN. CRACKED. CRACK ON INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR. SUMMARY OF NRC 00103: INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 
- [SDR DALA2024020601576](https://openairdocs.org/sdr/DALA2024020601576), Feb 4, 2024: DOUBLER. CRACKED. CRACK ON INTERNAL DOUBLER AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR. SUMMARY OF NRC 00104: INTERNAL DOUBLER (WEB) AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO D
- [SDR DALA2024022102376](https://openairdocs.org/sdr/DALA2024022102376), Feb 3, 2024: DRAG BRACE. CORRODED. CORROSION ON DRAG BRACE BORE (LH TAPER PIN HOLE) AND CORROSION ON LH / RH (2 EA) TAPER PIN AT NLG. DRAG BRACE WAS REMOVED PER B717-200 AMM 32-22-05 000-802. SUM
- [SDR DALA2024020601575](https://openairdocs.org/sdr/DALA2024020601575), Feb 3, 2024: PAN. CRACKED. CRACK ON LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS FOUND IN REF NRC 00098. SUMMARY OF NRC 00788P: LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS REPAIR
- [SDR DALA2024020601574](https://openairdocs.org/sdr/DALA2024020601574), Feb 3, 2024: FRAME. CRACKED. CRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME STA 696 RH AT PAX CABIN. SUMMARY OF NRC 00462: CRACKED FRAME TAB OF THE OVERWING FRAME STA 696 RH A
- [SDR DALA2024020601572](https://openairdocs.org/sdr/DALA2024020601572), Feb 3, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00087: INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1) WA
- [SDR DALA2024020301507](https://openairdocs.org/sdr/DALA2024020301507), Feb 1, 2024: BEAM. CRACKED. CRACK BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1). SUMMARY OF NRC 00174: BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 51-70
- [SDR DALA2024012901219](https://openairdocs.org/sdr/DALA2024012901219), Jan 25, 2024: FITTING. CRACKED. CRACK ON VERTICAL FITTING ON AFT PRESSURE BULKHEAD STA 1053 LONGERON #1 (ABOVE DOOR CUT OUT) AT PAX CABIN. SUMMARY OF NRC 00522: SPRING OF THE ARM ASSEMBLY WAS 
- [SDR DALA2024012601171](https://openairdocs.org/sdr/DALA2024012601171), Jan 25, 2024: CUSP WEB. CORRODED. CORROSION ON DOUBLER OF LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB. SUMMARY OF NRC 00477: CORROSION LEVEL 2. DOUBLER OF REPAIR ON LH CUSP WEB UPPER BTW
- [SDR DALA2024012501107](https://openairdocs.org/sdr/DALA2024012501107), Jan 25, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN. SUMMARY OF NRC 00510: CORROSION LEVEL 2. AREA ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=
- [SDR DALA2024012501106](https://openairdocs.org/sdr/DALA2024012501106), Jan 25, 2024: FRAME. CRACKED. CRACK ON LH FRAME STA 1037 LONG 17LH AT PAX CABIN. SUMMARY OF NRC 00294: LH FRAME STA 1037 LONG 17LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R. (LP
- [SDR DALA2024011900806](https://openairdocs.org/sdr/DALA2024011900806), Jan 18, 2024: CUSP WEB. CRACKED. CRACKS ON CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN. SUMMARY OF NRC 00376: CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN W
- [SDR DALA2024010900328](https://openairdocs.org/sdr/DALA2024010900328), Jan 8, 2024: UNKNOWN. UNKNOWN. CORROSION ON REPAIR PLUG ON OUTB SEAT TRACK X=56 LH IN STA Y= 547 AND 610 (2 EA). SUMMARY OF NRC 00604: CORROSION LEVEL 2. PLUG ON OUTB SEAT TRACK X=56 LH IN ST
- [SDR DALA2024010500203](https://openairdocs.org/sdr/DALA2024010500203), Nov 23, 2023: UNKNOWN. UNKNOWN. -AD- A SKIN LAYER CRACK WAS FOUND ON THE LEADING-EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER OF A B717-200. THE CRACK WAS REPAIRED PER ER/A 613198-14. THIS 
- [SDR DALA2023112009531](https://openairdocs.org/sdr/DALA2023112009531), Nov 18, 2023: UNKNOWN. UNKNOWN. ALL TAIL COMPARTMENT EMERGENCY PATHWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-260 & B5-116 PER B717 AMM 33-51. OPERAT
- [SDR DALA2023103008882](https://openairdocs.org/sdr/DALA2023103008882), Oct 30, 2023: UNKNOWN. UNKNOWN. FOUR (4) CRACK INDICATIONS NOTED ON RT VERT STAB (MARKED) REF STEP 12 OF AMDS CARD 5530-01048-02 (AD2018-10-08). AFTER SEPERATION OF LAYERS PER AMDS 5530-01048-
- [SDR DALA2023112809766](https://openairdocs.org/sdr/DALA2023112809766), Oct 29, 2023: UNKNOWN. UNKNOWN. AD RELATED. DTE ERA 613198-14 REV ORIGINAL. ERA ISSUED FOR VERT STAB FRONT SPAR REPAIR AT ZFS=43.000, RHS. DAMAGE TOLERANCE EVALUATION REQUIRED ADDL TIME RLTD M
- [SDR DALA2023021401130](https://openairdocs.org/sdr/DALA2023021401130), Feb 6, 2023: UNKNOWN. UNKNOWN. AFT LOWER CARGO COMPARTMENT LINERS METAL TRANSITION STRIP BENT UP. MCC FCP DEFERRAL TO MEL 25-50-01, FLIGHT CREW PLACARD INSTALLED. LOWER COMPARTMENT LINERS BIN
- [SDR DALA2023011200228](https://openairdocs.org/sdr/DALA2023011200228), Jan 11, 2023: LIGHT. INOPERATIVE. THE EXTERIOR EMERGENCY LIGHTS WERE ON IN THE ARM POSITION AT WAKE UP. MAINTENANCE REPLACED THE EMERGENCY LIGHTS RACK PER B717 AMM 33-51. OPERATIONAL CHECK IS OK
- [SDR DALA2022120607806](https://openairdocs.org/sdr/DALA2022120607806), Dec 4, 2022: SLIDE. FAILED. CATERING ATTEMPTED TO OPEN 1L WITHOUT VISUAL CONFIRMATION FROM LEAD FA, AFTER JET WAY PULLED AND DOORS ARMED. THE RAFT FELL AND DID NOT INFLATE. THIS COULD PREV
- [SDR DALA2022102606954](https://openairdocs.org/sdr/DALA2022102606954), Oct 22, 2022: BATTERY. INOPERATIVE. DURING THE SERVICE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHTS TO NOT BE TESTING PROPERLY. THE OVERWING EMERGENCY EVACUATION BATTERY WAS REPLACED PER
- [SDR DALA2022082205657](https://openairdocs.org/sdr/DALA2022082205657), Aug 19, 2022: NONE. NONE. ON WALKAROUND FOUND MISSING PANEL ON UNDERSIDE OF LEFT HAND ELEVATOR. MAINTENANCE INSTALLED A NEW PANEL PER AMM 06-33 B717. (LP #9236464)
- [SDR DALA2022051003226](https://openairdocs.org/sdr/DALA2022051003226), May 8, 2022: FRAME. CORRODED. CORROSION ON FRAME CHANNEL STA Y=889 BTW LONG 29LH AND 29 RH AT AFT CARGO COMPARTMENT IN REF NRC 00107. SUMMARY OF NRC 00214: CORROSION LEVEL 2, FRAME WAS REPAI
- [SDR DALA2022050603162](https://openairdocs.org/sdr/DALA2022050603162), May 5, 2022: SKIN PANEL. CRACKED. CRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING (LW). SUMMARY OF NRC 00030: CRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING 
- [SDR DALA2022050503142](https://openairdocs.org/sdr/DALA2022050503142), May 4, 2022: CHANNEL. CORRODED. CORROSION ON FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT. SUMMARY OF NRC 00113: CORROSION LEVEL 2, FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT, WAS 

All 176: https://openairdocs.org/aircraft/N933AT/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/N933AT/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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