# N603AT: 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: 55127
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 20, 2001
- Certificate issued: December 20, 2024
- Expires: December 31, 2031
- Mode S code: A7D276
- 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=603AT
- Page: https://openairdocs.org/aircraft/N603AT

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/N603AT/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 N603AT.

## FAA accident and incident reports

None matched to N603AT.

## Service difficulty reports (223, 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 DALA2026093005423](https://openairdocs.org/sdr/DALA2026093005423), Sep 26, 2026: SKIN. DAMAGED. FOUND DAMAGE AFT OF AFT CARGO DOOR OPENING, COMPLIED WITH ER/A 637189-14. (9197562) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304128](https://openairdocs.org/sdr/DALA2026071304128), Jul 10, 2026: TAIL CONE. DAMAGED. TAIL CONE HAS MULTIPLE LIGHTNING STRIKES BEYOND ALLOWABLE LIMITS. REPLACED TAIL CONE IAW AMDS W/C 5352-4013. (9204003) (AIRCRAFT GROUNDED)
- [SDR DALA2026052103104](https://openairdocs.org/sdr/DALA2026052103104), May 18, 2026: CONTROL VALVE. FAULTED. UFC/DE- TRAILING EDGE FLAPS LOCKED OUT ON APPROACH. LEADING EDGE SLATS EXTENDED NORMALLY. FOUND FLAP CONTROL VALVE CONTROL ROD BOLT BROKEN/MISSING. REPLACED SAM
- [SDR DALA2026041402371](https://openairdocs.org/sdr/DALA2026041402371), Apr 9, 2026: NONE. NONE. DURING ACCOMPLISHMENT OF ERA 633150-14AD PRI REV 0 STEP 15 FOUND 7 EA UNINSPECTABLE HOLES IN UPPER MLG SUPPORT DOUBLER AND TE PANEL LE. HOLES ARE NUMBERED UNK 1
- [SDR DALA2025092907058](https://openairdocs.org/sdr/DALA2025092907058), Sep 24, 2025: SPAR. CRACKED. WHILE PERFORMING AMDS 5720-01103-01B. INSPECTION FOUND A CRACK AT APPROX STA XRS= 170REAR SPAR. COMPLIED WITH ER/A- 628659-14AD REV. ORIGINAL (1215975)
- [SDR DALA2025110708140](https://openairdocs.org/sdr/DALA2025110708140), Sep 23, 2025: NONE. NONE. SHIP 9594 ER/A 628659-14AD REV ORIGINAL REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: COMPLIED WITH ERA 628
- [SDR DALA2025081806161](https://openairdocs.org/sdr/DALA2025081806161), Aug 14, 2025: REPAIR. OUT OF POSITION. EXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. FOUND AT RT WING REAR SPAR INSPECTION AREA 
- [SDR DALA2025081806160](https://openairdocs.org/sdr/DALA2025081806160), Aug 14, 2025: STRUCTURE. CHAFED. NUMBER 2 LT SLAT ATTACH POINT INSPECTION, SLAT DRIVE TRACK NR 5 CHAFED WING STRUCTURE ON INBD AT EDGE. REPAIRED ERA 628327-14 REV. (1143308)
- [SDR DALA2025031301960](https://openairdocs.org/sdr/DALA2025031301960), Mar 12, 2025: SKIN. CORRODED. -AD- CORROSION FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER INSPECTION FC572
- [SDR DALA2025100807322](https://openairdocs.org/sdr/DALA2025100807322), Mar 10, 2025: SKIN. CORRODED. EXFOLIATING CORROSION FOUND ON RIGHT WING REAR SPAR LOWER CAP AT APPROXIMATELY STATION XRS=164. (6925752)
- [SDR DALA2025031101893](https://openairdocs.org/sdr/DALA2025031101893), Mar 9, 2025: HINGE FITTING. CORRODED. RIGHT WING INBOARD FLAP HINGE FITTING LOWER OUTBOARD STUD ON AFT SPAR HAS HEAVY RUST/PITTING. SUMMARY SEE NRC 004-0001:5720-01103-01B/006 00006: CORROSION LEVEL
- [SDR DALA2025010700131](https://openairdocs.org/sdr/DALA2025010700131), Jan 5, 2025: POWER SUPPLY. NO TEST. THE AFT EMERGENCY EXIT DOORS OVERWING LIGHTS, LT AND RT, ARE NOT COMING ON WHEN TESTED AT ROW 20. MAINTENANCE REPLACED THE B5-119 EMERGENCY POWER SUPPLY PER B71
- [SDR DALA2024071807234](https://openairdocs.org/sdr/DALA2024071807234), Jul 17, 2024: LIGHT. MALFUNCTIONED. EXTERIOR EMERGENCY ILLUMINATION SYSTEM LEFT AFT WING EXTERIOR EMERGENCY LIGHT STAYING ON. LEFT WING EMERGENCY ILLUMINATION WAS FOUND ON DURING PRE-FLIGHT. RELAM
- [SDR DALA2024032103580](https://openairdocs.org/sdr/DALA2024032103580), Mar 17, 2024: BATTERY PACK. INOPERATIVE. FOUND LEFT AND RIGHT AFT EMERGENCY EXIT DOOR LOCATOR SIGNS INOPERATIVE AT THE AFT OVERWING DOORS. MAINTENANCE REPLACED THE EMERGENCY BATTERY (B5-115) POWER SUPP
- [SDR DALA2024010300074](https://openairdocs.org/sdr/DALA2024010300074), Jan 3, 2024: RELAY. UNKNOWN. THE OVERWING ESCAPE PATH LIGHTING IS ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTS REMAINED ILLUMINATED WITH SWITCH I
- [SDR DALA2023112009532](https://openairdocs.org/sdr/DALA2023112009532), Nov 19, 2023: UNKNOWN. UNKNOWN. THE EXTERIOR EMERGENCY LIGHTS STAY ON WHEN SWITCH IS PLACED IN "ARM" POSITION. MAINTENANCE RESET THE EMERGENCY LIGHTS SYSTEM. PERFORMED AN OPERATIONAL CHECK IAW
- [SDR DALA2023090507198](https://openairdocs.org/sdr/DALA2023090507198), Sep 3, 2023: UNKNOWN. UNKNOWN. THE OVERWING EXIT EXTERIOR LIGHTS ARE ON WITH THE SWITCH IN ARM POSITION. MAINTENANCE REPLACED THE OVERWING EMERGENCY POWER SUPPLY PER B717 AMM 33-51. ALL OPERA
- [SDR DALA2023080406301](https://openairdocs.org/sdr/DALA2023080406301), Aug 4, 2023: UNKNOWN. UNKNOWN. CRACK ON AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN. SUMMARY OF NRC 00286: AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=
- [SDR DALA2023080406300](https://openairdocs.org/sdr/DALA2023080406300), Aug 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CORROSION ON I
- [SDR DALA2023080306284](https://openairdocs.org/sdr/DALA2023080306284), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFT CARGO. IN REF NRC0337. C2. SUMMARY OF NRC 00664: CORROSION LEVE
- [SDR DALA2023080306282](https://openairdocs.org/sdr/DALA2023080306282), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER JAMB PAN INTERNAL AND EXTERNAL STRUCTURE STA 946 TO STA 1002 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00337: DOOR JAMB WAS REPLACED PER 
- [SDR DALA2023080306277](https://openairdocs.org/sdr/DALA2023080306277), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND 28LH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00317: L
- [SDR DALA2023072806114](https://openairdocs.org/sdr/DALA2023072806114), Jul 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00306: CORROSION LEVEL 2. TIE TRACK LH SIDE STA 813 TO STA 1022
- [SDR DALA2023072706098](https://openairdocs.org/sdr/DALA2023072706098), Jul 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00645: CORROSION LEVEL 2. FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPA
- [SDR DALA2023072606038](https://openairdocs.org/sdr/DALA2023072606038), Jul 25, 2023: UNKNOWN. UNKNOWN. CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR. SUMMARY OF NRC 00264: CRACKS (3 EA) ON INTERNAL STRUCTURE BE
- [SDR DALA2023072505982](https://openairdocs.org/sdr/DALA2023072505982), Jul 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON PRODUCTION DOUBLER OF INNER FUSELAGE SKIN DRAIN STA 1007 BTW L30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00300: CORROSION LEVEL 2. DOUBLER OF
- [SDR DALA2023072505980](https://openairdocs.org/sdr/DALA2023072505980), Jul 23, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN. SUMMARY OF NRC 00630: RH CUSP MEMBRANE WEB BTW STA 579 TO 598 AT PAX CABIN WAS REPAIRED
- [SDR DALA2023072505979](https://openairdocs.org/sdr/DALA2023072505979), Jul 23, 2023: UNKNOWN. UNKNOWN. CRACK ON FLOOR MEMBRANE WAS FOUND BTW STA Y 813-832 AND X=-44 TO X=-54 AT PAX CABIN. SUMMARY OF NRC 00648: FLOOR MEMBRANE BTW STA Y 813-832 AND X=-44 TO X=-54 W
- [SDR DALA2023072505977](https://openairdocs.org/sdr/DALA2023072505977), Jul 21, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1). SUMMARY OF NRC 00643: CORROSION LEVEL 2. FLOOR SUPPORT BTW -X 45 FROM STA 157 TO 200 (W1) WAS REP
- [SDR DALA2023072505976](https://openairdocs.org/sdr/DALA2023072505976), Jul 21, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT (1 EA) BTW X 55 AND STA 200-204.5 WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.063 IN. MAXIMUM MATERIAL REMOVED IS 0.030 IN AND THERE
- [SDR DALA2023072105929](https://openairdocs.org/sdr/DALA2023072105929), Jul 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR FITTING ON AFT BULKHEAD BTW STA Y=1060 AND X=-22 AT AFT PAX CABIN. SUMMARY OF NRC 00374: CORROSION LEVEL 2. FLOOR FITTING ON AFT BULKHEAD BTW
- [SDR DALA2023072105928](https://openairdocs.org/sdr/DALA2023072105928), Jul 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK, X-44 BTW STA 200-205 AT PAX CABIN. SUMMARY OF NRC 00369: CORROSION LEVEL 2. SEAT TRACK, X-44 BTW STA 200 TO 264 WAS REPLACED PER B717 S
- [SDR DALA2023072105925](https://openairdocs.org/sdr/DALA2023072105925), Jul 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON GUSSET WITH NP: 3925389-1 UNDER VENTRAL DOOR STA Y=1065 AND X=18 AT CABIN PAX. SUMMARY OF NRC 00442: CORROSION LEVEL 2. GUSSET WITH NP: 3925389-1 U
- [SDR DALA2023072105924](https://openairdocs.org/sdr/DALA2023072105924), Jul 20, 2023: UNKNOWN. UNKNOWN. FLOOR SUPPORT BTW X=13 TO 38.5 BTW STA Y=180 AT W1 AREA, IS CORRODED OUT OF LIMITS IN CABIN PAX. SUMMARY OF NRC 00638: CORROSION LEVEL 2. FLOOR SUPPORT BTW X=13
- [SDR DALA2023071705783](https://openairdocs.org/sdr/DALA2023071705783), Jul 17, 2023: UNKNOWN. UNKNOWN. CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX. SUMMARY OF NRC 00356: CRACK ON LH CUSP MEMBRANE WEB (2 EA) BTW STA 655 TO 695 AT CABIN PAX
- [SDR DALA2023071705779](https://openairdocs.org/sdr/DALA2023071705779), Jul 16, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON LH MEMBRANE WEB UPPER, LOWER SURFACE BTW STA 463 TO STA 466 AT PAX CABIN IN REF NRC 0353. SUMMARY OF NRC 00657: CORROSION LEVEL 2. CO
- [SDR DALA2023071705776](https://openairdocs.org/sdr/DALA2023071705776), Jul 15, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN. SUMMARY OF NRC 00438: INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN WA
- [SDR DALA2023071705775](https://openairdocs.org/sdr/DALA2023071705775), Jul 14, 2023: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMIT ON FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 AND X=44, AND FROM STA Y=1022 TO STA Y=1053 AND X=53.5 AT CABIN PAX. (W2) 
- [SDR DALA2023071305678](https://openairdocs.org/sdr/DALA2023071305678), Jul 12, 2023: UNKNOWN. UNKNOWN. CRACKED CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00399: CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-2
- [SDR DALA2023071205662](https://openairdocs.org/sdr/DALA2023071205662), Jul 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON BULKHEAD STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00314: CORROSION LEVEL 2. BULKHEAD DOUBLER STA 1053 BTW L28R/L28L AT 
- [SDR DALA2020031801918](https://openairdocs.org/sdr/DALA2020031801918), Mar 18, 2020: LIGHT. INOPERATIVE. SEVERAL EMERGENCY LIGHTS IN CABIN CEILING ARE INOPERATIVE. MAINTENANCE RELAMPED THEM IAW B717 AMM 33-51. (LP #6674820)
- [SDR DALA2018123197452](https://openairdocs.org/sdr/DALA2018123197452), Dec 28, 2018: POWER SUPPLY. MALFUNCTIONED. THE AFT BULKHEAD EMERGENCY DOOR EXIT SIGN IS INOPERATIVE AND THE MID CABIN OVERHEAD AISLE EMERGENCY EXIT LIGHT IS ALSO INOPERATIVE. MAINTENANCE REPLACED THE POW
- [SDR DALA2018110606495](https://openairdocs.org/sdr/DALA2018110606495), Nov 3, 2018: BATTERY PACK. SHORTED. ON SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR BOTH LEFT AND RIGHT FORWARD FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THAT BATTERY 
- [SDR DALA2018101506043](https://openairdocs.org/sdr/DALA2018101506043), Oct 14, 2018: LENS. UNSECURE. EMERGENCY EXIT AT DOOR 1L HAS A DAMAGED DIFFUSER LENS ON THE EXIT SIGN AND THE COVER FALLS OFF. MAINTENANCE REPLACED THE LIGHT COVER ABOVE DOOR 1L AND INSTALLED
- [SDR DALA2018101105975](https://openairdocs.org/sdr/DALA2018101105975), Oct 11, 2018: LIGHT. INOPERATIVE. 8 EMERGENCY LIGHTS INOP AISLE OVHD DURING SVC CK. RELAMPED INOP LTS, NO HELP. FOUND 3 BULBS BURNT OUT. RELAMPED. OPS CKD PER AMM 33-52-00. ALL LIGHTS WORK. OK F
- [SDR DALA2018082085142](https://openairdocs.org/sdr/DALA2018082085142), Aug 17, 2018: DOOR FRAME. CORRODED. SEVERAL AREAS ON THE FORWARD LOWER CARGO DOOR FRAME HAD SIGNS OF CORROSION. REPLACED THE FWD CARGO DOOR LOWER FRAME PAN IAW SRM 53-20-15-2R, REPAIR 6.
- [SDR DALA2018081605102](https://openairdocs.org/sdr/DALA2018081605102), Aug 15, 2018: CAM. COCKED. TAILONE RELEASE CAM TAB WAS CLOCKED INCORRECTLY. ADJUSTED THE RELEASE CAM IAW AMM 53-52-03.
- [SDR DALA2018041802584](https://openairdocs.org/sdr/DALA2018041802584), Apr 17, 2018: BRACKET. DAMAGED. FOUND THE EMERGENCY LIGHT BATTERY PACK BRACKET TO BE DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL
- [SDR DALA2018040202116](https://openairdocs.org/sdr/DALA2018040202116), Mar 30, 2018: LENS. MISSING. EMERGENCY EXIT SIGN LENS MISSING IN THE FIRST CLASS CABIN. MAINTENANCE INSTALLED THE LENS. THE AIRCRAFT IS OK FOR SERVICE.
- [SDR DALA2018032601906](https://openairdocs.org/sdr/DALA2018032601906), Mar 24, 2018: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, FOUND BOTH AFT OVERWING EXIT HATCH LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE FOUND BATTERY PACK TO BE BAD. REPLACED THE BATTERY PACK ASSEM

All 223: https://openairdocs.org/aircraft/N603AT/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/N603AT/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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