# N717JL: 2002 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: 55042
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 29, 2003
- Certificate issued: May 14, 2024
- Expires: May 31, 2031
- Mode S code: A996E1
- 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=717JL
- Page: https://openairdocs.org/aircraft/N717JL

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/N717JL/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 N717JL.

## FAA accident and incident reports

None matched to N717JL.

## Service difficulty reports (207, 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 DALA2026091805208](https://openairdocs.org/sdr/DALA2026091805208), Sep 18, 2026: SKIN. CRACKED. CRACK ON SKIN AT STA Y=1076 AND LONG 14R OF AFT EXTERNAL FUSELAGE, COMPLIED WITH ER/A 635946-14TR. (1819140) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805206](https://openairdocs.org/sdr/DALA2026091805206), Sep 18, 2026: SKIN. CRACKED. CRACK ON SKIN AT STA Y=1076 AND LONG 14R OF AFT EXTERNAL FUSELAGE, COMPLIED WITH ER/A 635946-14TR. (1818917) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805207](https://openairdocs.org/sdr/DALA2026091805207), Sep 17, 2026: SCUFF PLATE. CRACKED. CRACKS ON AFT CARGO COMP DOOR JAMB SCUFF PLATE, COMPLIED WITH ER/A 542149-14TR. (1818676) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805205](https://openairdocs.org/sdr/DALA2026091805205), Sep 17, 2026: SKIN. CRACKED. CRACK WAS FOUND AFFECTING A BUSHING INSTALLED IN THE VERTICAL STABILIZER LEADING EDGE SKIN REPAIR DOUBLER INSTALLATION LOCATED BETWEEN ZFS= 44 AND ZFS=52, HOLE 
- [SDR DALA2026091805204](https://openairdocs.org/sdr/DALA2026091805204), Sep 16, 2026: FRAME. CRACKED. CRACK ON FRAME STA Y=1200, REPAIRED FRAME PER B717-200 SRM 53-30-08-2R. (1816798) (AIRCRAFT GROUNDED).
- [SDR DALA2026092305314](https://openairdocs.org/sdr/DALA2026092305314), Sep 15, 2026: SKIN. CRACKED. FOUND CRACK AT FUSELAGE RIGHT SKIN Y=1076, BETWEEN LONGERON 13R AND 14R, COMPLIED WITH ER/A 636937-14. (1816724) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805203](https://openairdocs.org/sdr/DALA2026091805203), Sep 15, 2026: LANYARD. DAMAGED. BROKEN STRANDS ON LANYARD ASSEMBLIES OF RT AND LT, R & R STRANDS IAW AMDS 5211-4002. (1814626) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805202](https://openairdocs.org/sdr/DALA2026091805202), Sep 15, 2026: PIN. DAMAGED. PASSENGER DOOR EVACUATION SLIDE ARRIVED WITH VALVE RELEASE CABLE PINS NOT INSTALLED ON PARACHUTE CONE, EVACUATION SLIDE WITH TORN NYLON PARACHUTE PIN, R & R NYL
- [SDR DALA2026070703949](https://openairdocs.org/sdr/DALA2026070703949), Jun 19, 2026: RELAY. FAULTED. ATB- DUE TO THE AIRCRAFT NOT PRESSURIZING WITH AN ASSOCIATED -ALL PACKS OFF- MESSAGE. REPLACED R2-5104 PACK SHUTDOWN/AUTO OFF RELAY AND PERFORMED VERIFICATION F
- [SDR DALA2026030201423](https://openairdocs.org/sdr/DALA2026030201423), Feb 25, 2026: SKIN. DAMAGED. FUSELAGE / SKIN / STA 229.00 AND STA 256.00, BETWEEN L-15R & L-16R / LIGHTNING STRIKES. REPAIRED PER ER/A 619580-14AD. (1467470)
- [SDR DALA2026012700604](https://openairdocs.org/sdr/DALA2026012700604), Jan 22, 2026: SKIN. CRACKED. REFERENCE ER/A 619241-14. FUSELAGE SKIN, BS 1037, L13 - 14L CRACKED. REPAIRED IAW ER/A 14-619241. (1414757)
- [SDR DALA2025110708146](https://openairdocs.org/sdr/DALA2025110708146), Nov 3, 2025: SIGN. DETACHED. SHIP 9550 FA REPORTS EXIT SIGN AT FWD FIRST CLASS CABIN DETACHED. CORRECTIVE ACTION: RESECURED HARDWARE ON EXIT SIGN. (7585210)
- [SDR DALA2025110708143](https://openairdocs.org/sdr/DALA2025110708143), Nov 2, 2025: SIGN. DETACHED. SHIP 9550 SIGN IN FIRST CLASS CABIN DETACHED FROM CEILING. CORRECTIVE ACTION: RE-ATTACHED EXIT SIGN AS REQUIRED. A/C OK FOR SVC (7585208)
- [SDR DALA2025010700132](https://openairdocs.org/sdr/DALA2025010700132), Jan 3, 2025: LIGHT. ARCED. LIGHT PRODUCES AN ELECTRICAL ARC WHEN THE ATTACHMENT BOLT TOUCHES THE SCREW NEXT TO THE LIGHT ATTACHMENT SOCKET. MAINTENANCE REPLACED THE F/O LIGHT ASSEMBLY PER
- [SDR DALA2024120311397](https://openairdocs.org/sdr/DALA2024120311397), Nov 28, 2024: TRANSDUCER. SHORTED. SHIP 9550 -ATB/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO CAE AND DECLARED AN EMERGENCY DUE TO "STICK PUSHER FAIL" MESSAGE WITH AN ASSOCIATED STALL WARNING LI
- [SDR DALA2024112611224](https://openairdocs.org/sdr/DALA2024112611224), Nov 6, 2024: BULKHEAD. CRACKED. -AD- ACCOMPLISH ER/A 619268-14AD REV A SECTION II - FUSELAGE MAIN FRAME BULKHEADS AT FS 1178, X=10 X=0.0. AFT WEB CRACKED & ELONGATED HOLE. ACCOMPLISH ER/A 6192
- [SDR DALA2024101810189](https://openairdocs.org/sdr/DALA2024101810189), Oct 17, 2024: BUSHING. CRACKED. CRACK ON BUSHING WAS FOUND, PREVIOUSLY TO INSTALL NEW LOWER BRACKET ON LEADING EDGE AT VERTICAL STABILIZER. SUMMARY OF NRC 00927: CRACK ON BUSHING OF VERTICAL S
- [SDR DALA2024100209619](https://openairdocs.org/sdr/DALA2024100209619), Sep 29, 2024: VANE. DENTED. DENTS ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, XV1=211-26. SUMMARY OF NRC 00172: DENTS (16 EA) ON LH WING INBOARD
- [SDR DALA2024091108922](https://openairdocs.org/sdr/DALA2024091108922), Sep 11, 2024: PAN. CRACKED. CRACK ON INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00422: INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPA
- [SDR DALA2024090608755](https://openairdocs.org/sdr/DALA2024090608755), Sep 5, 2024: CABLE. BROKEN. MAINTENANCE FOUND A BROKEN KEVLAR CABLE AT THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 C
- [SDR DALA2024090408734](https://openairdocs.org/sdr/DALA2024090408734), Sep 3, 2024: HINGE FITTING. CORRODED. WEAR AND CORROSION ON HOLES OF LH FLAP HINGE FITTING #3. SUMMARY OF NRC 0885: CORROSION LEVEL 2. LH FLAP HINGE FITTING #3 WAS REPLACED BY A SERVICEABLE PER B717
- [SDR DALA2024090408732](https://openairdocs.org/sdr/DALA2024090408732), Aug 31, 2024: CONTROL SYSTEM. OUT OF ADJUST. -AD- AMDS 2740-01114-07 STEP 6: DUE RESULT OF THE STEP 6A "ADJUST THE HORIZONTAL STABILIZER TRIM SYSTEM AND SHUTOFF CONTROL SYSTEM AMM 27-40-00 820-801. SUMMARY
- [SDR DALA2024083008599](https://openairdocs.org/sdr/DALA2024083008599), Aug 29, 2024: HINGE FITTING. CORRODED. CORROSION WAS FOUND ON THE LH FLAP INBOARD HINGE FITTING FASTENER HOLES (8 ATTACH POINT) IN REF NRC 258. SUMMARY OF NRC 00861: LEVEL CORROSION 2. LH FLAP INBOAR
- [SDR DALA2024083008596](https://openairdocs.org/sdr/DALA2024083008596), Aug 28, 2024: CAP. CRACKED. CRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX. SUMMARY OF NRC 000367: UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX WAS REPAIRED PER PRI 
- [SDR DALA2024083008594](https://openairdocs.org/sdr/DALA2024083008594), Aug 28, 2024: BARREL NUT. CORRODED. CORROSION ON THE BARREL NUT HOLES #26, #27, #28, AND #30, STA HX 6.625 RIGHT, STABILIZER CENTER BOX. SUMMARY OF NRC 00407: BARREL NUT HOLES #26, #27, #28, AND #
- [SDR DALA2024082708491](https://openairdocs.org/sdr/DALA2024082708491), Aug 27, 2024: DOOR FRAME. CORRODED. AIRCRAFT 9550, CORROSION ON DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 FOUND PREVIUOS HOLE PLUGGED LIKE REPAIR AND NO DECAL FOUND. CORREC
- [SDR DALA2024082308412](https://openairdocs.org/sdr/DALA2024082308412), Aug 22, 2024: SKIN. DAMAGED. AIRCRAFT 9550, LIGHTNING STRIKES ON SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE. CORRECTIVE ACTION: SKIN STA Y=256, 229 AND BTW RH LONGE
- [SDR DALA2024082208362](https://openairdocs.org/sdr/DALA2024082208362), Aug 21, 2024: PAN. CRACKED. AIRCRAFT 9550, INITIAL INSPECTION: CRACK ON INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER PAN AFT SI
- [SDR DALA2024082208358](https://openairdocs.org/sdr/DALA2024082208358), Aug 21, 2024: PAN. CRACKED. AIRCRAFT 9550, CRACK INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. CORRECTIVE ACTION: INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. WAS REPAIRED PER
- [SDR DALA2024082008300](https://openairdocs.org/sdr/DALA2024082008300), Aug 20, 2024: ANGLE. CRACKED. AIRCRAFT 9550, INITIAL INSPECTION: CRACKS ON ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE. CORRECTIVE ACTION: ANGLE OF
- [SDR DALA2024081908242](https://openairdocs.org/sdr/DALA2024081908242), Aug 17, 2024: NUT. CORRODED. CORROSION ON NUTS INSIDE HOLES #26, #27, #28, AND #30 STA HX 6.625 RIGHT STABILIZER CENTER BOX. SUMMARY OF NRC 00494: NUTS INSIDE HOLES #26, #27, #28, AND #30 S
- [SDR DALA2024081608212](https://openairdocs.org/sdr/DALA2024081608212), Aug 16, 2024: FRAME. CRACKED. CRACK ON WEB AND CRACK ON FRAME OF AFT ACCESSORY COMPARTMENT FROM STA 1178 CANT BTW LONG 1 TO LONG 3RH TO 3LH, APPROXIMATELY. SUMMARY OF NRC 00219: WEB AND FRAM
- [SDR DALA2024081508166](https://openairdocs.org/sdr/DALA2024081508166), Aug 14, 2024: FRAME. CORRODED. CORROSION ON FRAME STA Y=1022 BTW LONGERON 28R/L30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00833; CORROSION LEVEL 2. CORROSION ON FRAME STA Y=1022 BTW LONGERON 
- [SDR DALA2024081408112](https://openairdocs.org/sdr/DALA2024081408112), Aug 13, 2024: WINDOW FRAME. CRACKED. CRACK ON LH WINDOW FRAME (RETAINER POLISHED). SUMMARY OF NRC 00623: LH WINDOW FRAME WAS REPAIRED PER PRI 619398-14 REV 2 AND PER ER/A 619398-14 REV ORIGINAL SEC
- [SDR DALA2024081308067](https://openairdocs.org/sdr/DALA2024081308067), Aug 13, 2024: SKIN. CORRODED. CORROSION ON SKIN UPPER EDGE OF LH AND RH WING REAR SPAR BTW XCW=0 TO XW=60 (THROUGH LH AND RH MLG (SPECIFICALLY XCW=30)). SUMMARY OF NRC 00169: CORROSION LEVEL
- [SDR DALA2024081308066](https://openairdocs.org/sdr/DALA2024081308066), Aug 12, 2024: BEAM. CRACKED. CRACKS ON BEAM #6 BTW STA 180-196 AT FWD PASSENGER DOOR. SUMMARY OF NRC 00117: BEAM #6 ON STA 196 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2
- [SDR DALA2024080907920](https://openairdocs.org/sdr/DALA2024080907920), Aug 8, 2024: CAP. CRACKED. CRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX. SUMMARY OF NRC 00816: UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX WAS REPAIRED PER PRI 6
- [SDR DALA2024080907919](https://openairdocs.org/sdr/DALA2024080907919), Aug 8, 2024: STABILIZER. DISTORTED. THE COUNTERSINK OF THE FASTENERS HOLES OF THE VERTICAL STABILIZER LEADING EDGE WERE NOTED WORN ALL AROUND EDGES BETWEEN ZFS 52.267 TO 153.938. SUMMARY OF NRC 00
- [SDR DALA2024080807881](https://openairdocs.org/sdr/DALA2024080807881), Aug 7, 2024: ANGLE. CORRODED. CORROSION ON RH CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN (W1.) SUMMARY OF NRC 00467: CORROSION LEVEL 2. CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN WAS REPAIRED PE
- [SDR DALA2024080707852](https://openairdocs.org/sdr/DALA2024080707852), Aug 6, 2024: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL 29R STA Y=1002 TO Y=1005 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00332: CORROSION LEVEL 2. INTERCOSTAL 29R STA Y=1002 TO Y=1005 A
- [SDR DALA2024080607842](https://openairdocs.org/sdr/DALA2024080607842), Aug 6, 2024: AUTOBRAKE SYS. INTERMITTENT. CRACK ON FRAME CAP STA Y=1133 AND BTW LONG 2LH TO 3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00685: FRAME CAP (STIFFENER) STA Y=1133 AND BTW LONG 2LH TO 3
- [SDR DALA2024080607841](https://openairdocs.org/sdr/DALA2024080607841), Aug 6, 2024: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1022, 1037, 1087 AT AFT FUSELAGE. SUMMARY OF NRC 00046: (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FU
- [SDR DALA2024080607840](https://openairdocs.org/sdr/DALA2024080607840), Aug 5, 2024: WING ROOT. CORRODED. CORROSION ON LH CENTER WING UPPER SURFACE (WING BOX) BTW STGR 6-5 AND STGR 5-4 PAX CABIN. SUMMARY OF NRC 00693: CORROSION LEVEL 2. CORROSION ON LH CENTER WING U
- [SDR DALA2024080507763](https://openairdocs.org/sdr/DALA2024080507763), Aug 2, 2024: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN RH SIDE B
- [SDR DALA2024080507762](https://openairdocs.org/sdr/DALA2024080507762), Aug 2, 2024: FRAME. CRACKED. CRACK ON MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN. SUMMARY OF NRC 00354: MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN WAS REPAIRED PER PRI 619352-14 R
- [SDR DALA2024080507761](https://openairdocs.org/sdr/DALA2024080507761), Aug 2, 2024: LONGERON. CRACKED. CRACKS ON LONGERONS 3, 4, 5, 6, AND 17 LH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00371: LONGERON 3 BTW STA Y=1012 TO STA Y=1027 LH, LONGERON 4 BTW STA Y=1011 T
- [SDR DALA2024073007625](https://openairdocs.org/sdr/DALA2024073007625), Jul 30, 2024: FRAME. DAMAGED. NICKS ON FRAME STA Y=351 BTW LONGERON 17R / L18R. SUMMARY OF NRC 00711: FRAME'S STA Y=351 BTW LONGERON 17R / L18R WAS REPAIRED PER B717-200 SRM 53-00-07-2R PROC
- [SDR DALA2024073007624](https://openairdocs.org/sdr/DALA2024073007624), Jul 29, 2024: LONGERON. CRACKED. CRACKS ON LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00370: LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX WERE REPAIRED PER
- [SDR DALA2024072907540](https://openairdocs.org/sdr/DALA2024072907540), Jul 28, 2024: CUSP WEB. CORRODED. CRACK ON CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN. SUMMARY OF NRC 00453: CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN WAS FABRICATED PER B
- [SDR DALA2024072907538](https://openairdocs.org/sdr/DALA2024072907538), Jul 27, 2024: CUSP WEB. CRACKED. CRACK WAS FOUND AFTER REMOVED CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56 TO -X=44 AT CABIN PAX. SUMMARY OF NRC 00820: CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56

All 207: https://openairdocs.org/aircraft/N717JL/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/N717JL/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.