# N977AT: 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: 55036
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 11, 2002
- Certificate issued: April 23, 2024
- Expires: April 30, 2031
- Mode S code: AD9DB8
- 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=977AT
- Page: https://openairdocs.org/aircraft/N977AT

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/N977AT/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 N977AT.

## FAA accident and incident reports

None matched to N977AT.

## Service difficulty reports (159, 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 DALA2026052803223](https://openairdocs.org/sdr/DALA2026052803223), May 23, 2026: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BTW STA. Y=1037 & LONG 14R AT RH PYLON. REPAIRED PER ER/A 634213-14 (1607725) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803222](https://openairdocs.org/sdr/DALA2026052803222), May 22, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA 1087 LONG 14 RH. REPAIRED PER PRI 634296-14 (1606252) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803218](https://openairdocs.org/sdr/DALA2026052803218), May 20, 2026: VANE. DEBONDED. ONE DISBONDED AREA OF 1.000IN ( LENGTH) X 1.000IN (WIDTH) WAS FOUND ON FLAP VANE, ON UPPER SURFACE AT RIGHT WING. REPAIRED PER PRI 634257-14 REV 2 AND ER/A NO.6
- [SDR DALA2026051903066](https://openairdocs.org/sdr/DALA2026051903066), May 13, 2026: SKIN. NOT REPORTED. ERA 634294-14 ISSUED FOR FUSELAGE SKIN REPAIR AT STA 1076, L14L, FOLLOW ON INSPECTIONS ARE REQUIRED. ACCOMPLISH ERA 634294-14 SECTION II INSPECTIONS (1600062) (
- [SDR DALA2026051703029](https://openairdocs.org/sdr/DALA2026051703029), May 12, 2026: DOOR FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR ON DOOR JAMB STA Y= 994 BTW LONG 26R AND LONG 27R AT AFT CARGO COMPARTMENT. PREVIOUS REPAIR ON DOOR JAMB STA Y= 994 BTW LONG 26R AN
- [SDR DALA2025082206253](https://openairdocs.org/sdr/DALA2025082206253), Aug 15, 2025: NOT REPORTED. NOT REPORTED. ER/A 628422-14AD REVISION ORIGINAL. REPAIR AT LT SIDE OF VERTICAL STAB SPAR AT ZFS=52.267. (1144341)
- [SDR DALA2025081806154](https://openairdocs.org/sdr/DALA2025081806154), Aug 15, 2025: SKIN. CRACKED. SHIP 9541 C/W ERA 628422-14AD REV ORIG VERTICAL STABILIZER LHS & RHS LEADING EDGE SKIN ZFS52.267 FASTENER HOLES CRACKED. CORRECTIVE ACTION: C/W PRI 628422-14AD.
- [SDR DALA2025060704355](https://openairdocs.org/sdr/DALA2025060704355), Jun 5, 2025: FITTING. DAMAGED. AIRCRAFT 9541, LEFT WING LOWER SURFACE BRACE FITTING AT STA XRS 164 HOLE HAS DAMAGE (1EA) LABLED C1. CORRECTIVE ACTION: LEFT WING LOWER SERFACE BRACE FITTING ST
- [SDR DALA2025060604342](https://openairdocs.org/sdr/DALA2025060604342), May 30, 2025: SPAR. DAMAGED. SHIP 9451 LH WING AFT SPAR FLAP TRACK MOUNT REQUIRES REMOVAL OF 8 BUSHINGS TO FOM SPAR REPAIR. CORRECTIVE ACTION: REPAIRED PER 623679-14AD REV 0 (0996171)
- [SDR DALA2025052704025](https://openairdocs.org/sdr/DALA2025052704025), May 23, 2025: SKIN. DAMAGED. SHIP 9541 LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137. CORRECTIVE ACTION: DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD (0982
- [SDR DALA2025052704026](https://openairdocs.org/sdr/DALA2025052704026), May 22, 2025: SPAR CAP. CRACKED. SHIP 9541 B717-200 / RH WING / REAR SPAR / LOWER CAP / XRS=164 / CRACK. CORRECTIVE ACTION: ASSOCIATED ER/A 00-623681 C/W. (0980036)
- [SDR DALA2025050103359](https://openairdocs.org/sdr/DALA2025050103359), Apr 30, 2025: SPAR WEB. DAMAGED. LEFT WING AFT SPAR WEB O/B LOWER HOLE HAS DAMAGE (1 EA), LABELED AS B1. NO DAMAGE FOUND IAW DELTA ER/A 623679-14AD REV 0, PRI REV 7 SECTION 4 STEP #1 AND TABLE 
- [SDR DALA2025050103358](https://openairdocs.org/sdr/DALA2025050103358), Apr 30, 2025: SKIN. DAMAGED. LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137 (7 EA) MARKED AS A1 THRU A7. DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD REV 0 
- [SDR DALA2025011300272](https://openairdocs.org/sdr/DALA2025011300272), Jan 10, 2025: SPAR CAP. CRACKED. -AD- CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT REF FC5720-0
- [SDR DALA2024112711257](https://openairdocs.org/sdr/DALA2024112711257), Nov 26, 2024: SPAR. CRACKED. -AD- WORKING PRI 615810-14AD REV 0. LH WING SPAR CRACK FUEL LEAK. ACCOMPLISHED PRI 615810-14AD REVISION D, REV 3. VERIFIED ERA 615810-14AD REV D SECTION VI TIME
- [SDR DALA2024103010502](https://openairdocs.org/sdr/DALA2024103010502), Oct 29, 2024: NONE. NONE. -AD- WORKING PRI 615810AD REV 3. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS ARE C/W AND MATCH PRI 621847-14AD REV 0, 
- [SDR DALA2024103010501](https://openairdocs.org/sdr/DALA2024103010501), Oct 29, 2024: FUEL CELL. LEAKING. -AD- L/H WING REAR SPAR LOWER CAP LEAKING FUEL. C/W PRI 621847-14AD REV 2. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS
- [SDR DALA2024103010500](https://openairdocs.org/sdr/DALA2024103010500), Oct 29, 2024: FUEL CELL. LEAKING. -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING REAR SPAR LOWER CAP. CONTACT LIAISON ENG. REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT, AA#FC5720-01103. LEAK
- [SDR DALA2024112111101](https://openairdocs.org/sdr/DALA2024112111101), Oct 28, 2024: SPAR. CRACKED. -AD- LH WING REAR SPAR XRS 164 CRACKED. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 06NOV2024 (AD EFFECTIVE DATE)
- [SDR DALA2024092309315](https://openairdocs.org/sdr/DALA2024092309315), Sep 22, 2024: LENS. MISSING. THE 1AB EMERGENCY LIGHT LENSE IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT COVER AT 1AB AS REQUIRED. OK FOR SERVICE. (LP #0569847)
- [SDR DALA2024071207052](https://openairdocs.org/sdr/DALA2024071207052), Jul 11, 2024: BATTERY PACK. NO TEST. DURING THE SERVICE CHECK, THE TAIL SIDE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK (B5-260) DEFECTIVE. THE BATTERY PACK WAS REP
- [SDR DALA2024042204628](https://openairdocs.org/sdr/DALA2024042204628), Apr 16, 2024: LANYARD. MISSING. SLIDE DISARMING PIN ATTACHING LANYARD MISSING. LATCH MECHANISM MISSING TO SECURELY ARM TAILCONE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND 
- [SDR DALA2024040804183](https://openairdocs.org/sdr/DALA2024040804183), Apr 6, 2024: DOOR FRAME. DAMAGED. CRACK DOOR ON FRAME DOOR ANGLE BTW STA 195 (AFT UPPER CORNER) AT FWD SERVICE DOOR R1. SUMMARY OF NRC 00075: ANGLE WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DR
- [SDR DALA2024040804182](https://openairdocs.org/sdr/DALA2024040804182), Apr 5, 2024: BEAM. DAMAGED. CRACK BEYOND STOPDRILL, (PREVIOUS REPAIR) ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00071: DOOR BEAM 1 BTW STA 
- [SDR DALA2024040504134](https://openairdocs.org/sdr/DALA2024040504134), Apr 4, 2024: SPAR. CRACKED. CRACK ON REAR SPAR XRS 150 AT LH WING. SUMMARY OF NRC 0054: REAR SPAR XRS 150 AT LH WING WAS REPAIRED PER ERA 615810-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR
- [SDR DALA2024032703840](https://openairdocs.org/sdr/DALA2024032703840), Mar 26, 2024: PAN. CRACKED. CRACK PAN ON AFT EDGE AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00154: FWD CARGO COMPARMENT DOOR WAS REPAIRED PER ERA 559551-14 REV A. SECTION II. ASSOCIATED
- [SDR DALA2024032503737](https://openairdocs.org/sdr/DALA2024032503737), Mar 24, 2024: SKIN. DEBONDED. TWO DISBONDS FOUND ON LH AFT MOVABLE FLAP VANE LOWER SKIN: 1) LENGTH=1.700IN, WIDTH=1.500IN AND 2) LENGTH=2.100IN, WIDTH= 1.000IN (IN REF MON/9541/0138992 JOB #
- [SDR DALA2024032303704](https://openairdocs.org/sdr/DALA2024032303704), Mar 23, 2024: PAN. CRACKED. CRACK ON PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00155: PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR WAS REPAIRED PER B717-200 SR
- [SDR DALA2024032103592](https://openairdocs.org/sdr/DALA2024032103592), Mar 21, 2024: WINDOW FRAME. CRACKED. CRACK ON UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW, AT COCKPIT. SUMMARY OF NRC 00439: UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW AT COCKPIT WAS REPAIRED PE
- [SDR DALA2024032103579](https://openairdocs.org/sdr/DALA2024032103579), Mar 18, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP ANGLE BTW STA Y=148 TO Y=218. SUMMARY OF NRC 00438: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA Y=148 TO Y=218 WAS REPAIRED PER ERA 616020-14 
- [SDR DALA2024032103574](https://openairdocs.org/sdr/DALA2024032103574), Mar 15, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=160-200 X=6, X=0 AND X=-6. SUMMARY OF NRC 00620: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=160-200 X=6, X=0 AND X=-6 WERE
- [SDR DALA2024031503377](https://openairdocs.org/sdr/DALA2024031503377), Mar 15, 2024: ANGLE. CORRODED. CORROSION ON FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00101: CORROSION LEVEL 2. FRAME CLIP STA Y=1087 AND LONGERON 18R
- [SDR DALA2024031403327](https://openairdocs.org/sdr/DALA2024031403327), Mar 13, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BTW Y=200 TO STA Y=256, COORDINATE X=-44 (RH SIDE). SUMMARY OF NRC 00696: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO STA Y=341, COORDINA
- [SDR DALA2024031303280](https://openairdocs.org/sdr/DALA2024031303280), Mar 13, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB LOWER SURFACES BTW STA 446 TO STA 465 AND STA 494 TO STA 500. SUMMARY OF NRC 00669: CORROSION LEVEL 2. RH CUSP WEBS BTW STA 446 TO STA 
- [SDR DALA2024030803181](https://openairdocs.org/sdr/DALA2024030803181), Mar 7, 2024: PAN. CRACKED. CRACK ON DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR. SUMMARY OF NRC 00119: DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52
- [SDR DALA2024030703128](https://openairdocs.org/sdr/DALA2024030703128), Mar 7, 2024: WEB. CORRODED. CORROSION ON WEB BTW STA Y=200/205 AND STA X=54 AT C PAX (W1) WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00719: CORROSION LEVEL 2. WEB BTW STA Y=200/205 AND STA X=
- [SDR DALA2024030703127](https://openairdocs.org/sdr/DALA2024030703127), Mar 7, 2024: CUSP WEB. CORRODED. AWR, AA, AD IN REF TO AMDS 5310-01436-03B STEP 3: AFTER RH CUSP WEB REMOVAL, SEVERAL CRACKS AND CORROSION WERE FOUND ON RIGHT CUSP WEB FROM STA Y 655 TO 715. SU
- [SDR DALA2024030703125](https://openairdocs.org/sdr/DALA2024030703125), Mar 6, 2024: LONGERON. CORRODED. CORROSION WAS FOUND OUT OF LIMITS AT LONGERON ENDS 28LH AND 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00713: CORROSION LEVEL 2. LONGERON ENDS 28LH AND 28RH 
- [SDR DALA2024030603061](https://openairdocs.org/sdr/DALA2024030603061), Mar 5, 2024: FRAME. CRACKED. CRACK ON FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN. SUMMARY OF NRC 00411: FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07
- [SDR DALA2024030503006](https://openairdocs.org/sdr/DALA2024030503006), Mar 4, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPOORT BTW STA Y=200 TO 218 X-54 AT PAX CABIN. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 TO 218 X-54 WAS FABRICAT
- [SDR DALA2024030402937](https://openairdocs.org/sdr/DALA2024030402937), Mar 2, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB REPAIR DOUBLER BTW STA 484 TO 494 PAX CABIN. SUMMARY OF NRC 00484: CORROSION LEVEL 2. RH CUSP WEB REPAIR DOUBLER AND RING DOUBLER BTW S
- [SDR DALA2024030402935](https://openairdocs.org/sdr/DALA2024030402935), Mar 1, 2024: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 BTW LONGERON 29L AND 29R AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT. SUMMARY O
- [SDR DALA2024030402932](https://openairdocs.org/sdr/DALA2024030402932), Mar 1, 2024: WEB. CORRODED. CORROSION ON MEMBRANE STA Y=196 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00618: CORROSION LEVEL 2. MEMBRANE STA Y=196 X=54.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 5
- [SDR DALA2024030402930](https://openairdocs.org/sdr/DALA2024030402930), Mar 1, 2024: BULKHEAD WEB. CORRODED. CORROSION ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00462: CORROSION LEVEL 1. CORROSION O
- [SDR DALA2024022802768](https://openairdocs.org/sdr/DALA2024022802768), Feb 28, 2024: FRAME. CRACKED. AD. CRACK OF 0.734 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, S
- [SDR DALA2024022802767](https://openairdocs.org/sdr/DALA2024022802767), Feb 28, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=164, Y=190, AND Y=200 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00616: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=164, Y=190, AND Y=200 
- [SDR DALA2024022802766](https://openairdocs.org/sdr/DALA2024022802766), Feb 28, 2024: FRAME. CRACKED. AD. CRACK OF 0.359 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, S
- [SDR DALA2024022602638](https://openairdocs.org/sdr/DALA2024022602638), Feb 24, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CABIN. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CAB
- [SDR DALA2024022602637](https://openairdocs.org/sdr/DALA2024022602637), Feb 24, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN. SUMMARY OF NRC 00609: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN
- [SDR DALA2024022602636](https://openairdocs.org/sdr/DALA2024022602636), Feb 24, 2024: CUSP WEB. MECHANIC ERROR. MISDRILLED ON CUSP WEB BTW STA Y=674 AT LH CABIN PAX. SUMMARY OF NRC 00426: CUSP WEB BTW STA Y=674 AT LH CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PRO

All 159: https://openairdocs.org/aircraft/N977AT/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/N977AT/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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