# N995AT: 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: 55139
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 2002
- Certificate issued: April 12, 2024
- Expires: April 30, 2031
- Mode S code: ADE548
- 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=995AT
- Page: https://openairdocs.org/aircraft/N995AT

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/N995AT/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 N995AT.

## FAA accident and incident reports

None matched to N995AT.

## Service difficulty reports (158, 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 DALA2026092405328](https://openairdocs.org/sdr/DALA2026092405328), Sep 24, 2026: SKIN. DAMAGED. FOUND DAMAGE TO AFT CARGO DOOR CUTOUT AFT SKIN EDGE, COMPLIED WITH ER/A 637149-14. (9115046) (AIRCRAFT GROUNDED).
- [SDR DALA2025111808418](https://openairdocs.org/sdr/DALA2025111808418), Nov 12, 2025: COVER. DETACHED. DURING SERVICE CHECK WALK AROUND, TAIL CONE SLIDE COVER WAS COMPLETELY UNLATCHED AND COVER WAS FULLY TO THE REAR. RESECURED CONTAINER ASSY LATCH IAW CMM 25-66-2
- [SDR DALA2025100807328](https://openairdocs.org/sdr/DALA2025100807328), Sep 26, 2025: SKIN. DAMAGED. SHIP 9540 DUE ER/A 628896-14 REV. ORIG. SECTION II PERMANENT REPAIR INSTRUCTION FOR RIGHT SIDE FUSELAGE SKIN DAMAGED AT STA. 237"- STA. 294". COMPLIED WITH PERM
- [SDR DALA2025091606811](https://openairdocs.org/sdr/DALA2025091606811), Sep 9, 2025: STRINGER. DAMAGED. STRINGER 27R DAMAGED BS 237 - 282. REPAIR SPLICE IAW SRM 53-00-05 (1190061).
- [SDR DALA2025091606810](https://openairdocs.org/sdr/DALA2025091606810), Sep 9, 2025: STRINGER. DAMAGED. STRINGER 26R DAMAGED BETWEEN BS 226 - 282. REPAIRED PER B717 SRM 53-00- 05-2R. (1190030)
- [SDR DALA2025091606809](https://openairdocs.org/sdr/DALA2025091606809), Sep 9, 2025: FRAME. DAMAGED. FS 256 FRAME DAMAGED BETWEEN STR 25 RT-28 RT. REMOVED DAMAGED FRAME SECTION PER B717 SRM 53-20-07-2R (1189997)
- [SDR DALA2025100807325](https://openairdocs.org/sdr/DALA2025100807325), Jan 22, 2025: ACCESS PANEL. OUT OF LIMITS. ELONGATED HOLES (11 EA) WERE FOUND ON ACCESS PANEL OF LIGHT ASSY MB LOWER ARE OUT OF LIMITS PER DWG 5925039 REV. F. HOLES OUT OF LIMITS WERE REPAIRED PER ER/A 6
- [SDR DALA2025012400583](https://openairdocs.org/sdr/DALA2025012400583), Jan 22, 2025: LIGHT. INOPERATIVE. THE EXTERIOR EMERGENCY LIGHT DOESN'T TURN ON. THE OVERWING EMERGENCY LIGHT WAS REPLACED PER B717-200 AMM 33-51-05. ALL TEST OK. (LP #6552182)
- [SDR DALA2025012100470](https://openairdocs.org/sdr/DALA2025012100470), Jan 20, 2025: DOUBLER. WORN. WEAR ON REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00011: PREVIOUS REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUS
- [SDR DALA2025012100469](https://openairdocs.org/sdr/DALA2025012100469), Jan 20, 2025: FRAME. BENT. BENT FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00279: FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMEN
- [SDR DALA2025012000465](https://openairdocs.org/sdr/DALA2025012000465), Jan 17, 2025: DOOR FRAME. CORRODED. CORROSION ON CARGO DOOR JAMB BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: CORROSION LEVEL 2. CARGO DOOR 
- [SDR DALA2025012000463](https://openairdocs.org/sdr/DALA2025012000463), Jan 15, 2025: PAN. CRACKED. CRACKS ON PAN OF INTERNAL STRUCTURE AT AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 2/3 AND BTW BEAM 4/5. ALSO ON FWD EDGE BTW BEAM 3/4. SUMMARY OF NRC 00135:
- [SDR DALA2025011600359](https://openairdocs.org/sdr/DALA2025011600359), Jan 15, 2025: BEAM. CRACKED. CRACK ON BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00256: BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER E
- [SDR DALA2025011300273](https://openairdocs.org/sdr/DALA2025011300273), Jan 11, 2025: LONGERON. CORRODED. CORROSION ON LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00651: CORROSION LEVEL 2. LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT 
- [SDR DALA2025011300271](https://openairdocs.org/sdr/DALA2025011300271), Jan 10, 2025: FRAME. CRACKED. -AD- CRACK ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=715 LH WAS FOUND IN REF TASK CARD 5310-01436-04B JOB #079-0002, STEP 13. SUMMARY OF N
- [SDR DALA2025011300269](https://openairdocs.org/sdr/DALA2025011300269), Jan 9, 2025: DOUBLER. DAMAGED. WEAR AND GOUGES ON PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDGE PANEL ON XIS=120 AT RH WING. SUMMARY OF NRC 00057: PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDG
- [SDR DALA2025011300266](https://openairdocs.org/sdr/DALA2025011300266), Jan 9, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS OF STA 157-210 -X=45, STA 256 -X=44-24L, STA 174-176 BTW -X=10- 49, STA 200-157 X=10, STA 200-157 -X=10, STA 157-200 BTW X=44, STA 2
- [SDR DALA2025011300274](https://openairdocs.org/sdr/DALA2025011300274), Jan 9, 2025: SKIN. DENTED. DENT #4, XF=89.250" DAE=13.500"; DENT #5, XF=86.500" DAE=11.500"; DENT#6. XF=88.375" DAE=14"; AND DENT#26, XF=81.250" DAE=4.500" WERE FOUND OUT OF LIMITS ON LOW
- [SDR DALA2025010900178](https://openairdocs.org/sdr/DALA2025010900178), Jan 8, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB STA Y:715 X:60 IN PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y:715 X:60 IN PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, 
- [SDR DALA2024123112104](https://openairdocs.org/sdr/DALA2024123112104), Dec 30, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR. SUMMARY OF NRC 00459: CORROSION LEVEL 2. FLOO
- [SDR DALA2024123112103](https://openairdocs.org/sdr/DALA2024123112103), Dec 30, 2024: CUSP WEB. CRACKED. CRACK ON CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX. SUMMARY OF NRC 00467: CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX WAS REPAIRED PER B717-200 
- [SDR DALA2024123012067](https://openairdocs.org/sdr/DALA2024123012067), Dec 29, 2024: PAN. CRACKED. CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 WAS FOUND AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00405: CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 AT FWD CARGO 
- [SDR DALA2024123012066](https://openairdocs.org/sdr/DALA2024123012066), Dec 27, 2024: VANE. DENTED. SEVERAL DENTS ON LOWER SKIN LH AFT MOVEABLE FLAP VANE. SUMMARY OF NRC 00250: DENTS (8 EA) ON LOWER SKIN LH AFT MOVABLE FLAP VANE WERE EVALUATED AND DENTS #1 TO 
- [SDR DALA2024122712034](https://openairdocs.org/sdr/DALA2024122712034), Dec 27, 2024: PAN. CRACKED. CRACK ON PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5. SUMMARY OF NRC-00143: PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5 WAS REPAIRED PER B
- [SDR DALA2024123012065](https://openairdocs.org/sdr/DALA2024123012065), Dec 24, 2024: SEAT TRACK. CORRODED. CORROSION ON LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX. SUMMARY OF NRC 00482: CORROSION LEVEL 2. CORROSION AT LH INB SEAT TRACK (X=22) ON STA Y=200-205 
- [SDR DALA2024122712031](https://openairdocs.org/sdr/DALA2024122712031), Dec 24, 2024: BEAM. CRACKED. CRACK ON BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00255: BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER
- [SDR DALA2024122311961](https://openairdocs.org/sdr/DALA2024122311961), Dec 19, 2024: PAN. CRACKED. CRACK ON INNER PAN AT FWD EDGE BTW BEAM 1 AND 2 WAS FOUND ON AFT CARGO DOOR. SUMMARY OF NRC 00442: OUTER PAN FWD EDGE BTW BEAM 1 AND 2 WAS BLENDED OUT AND MEASU
- [SDR DALA2024121911828](https://openairdocs.org/sdr/DALA2024121911828), Dec 19, 2024: COVER. BROKEN. BROKEN PLASTIC COVER OF TAIL CONE EXTENSION PULL LEVER AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN C
- [SDR DALA2024060605812](https://openairdocs.org/sdr/DALA2024060605812), Jun 6, 2024: STRINGER. CORRODED. CORROSION AT APPROX STATION 1053 ON STRINGER 26. RIVETS POPPED WITH SKIN PROTRUDING. REMOVED STR END FITTING AT STR 26 STA 1053 FOUND TO BE 100% LOSS. OUT OF LI
- [SDR DALA2024042304670](https://openairdocs.org/sdr/DALA2024042304670), Apr 20, 2024: BEARING. FAULTED. THE GATE AGENT REPORTS THAT THE 1L DOOR WAS HARD TO OPEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PAR
- [SDR DALA2024021502204](https://openairdocs.org/sdr/DALA2024021502204), Feb 15, 2024: BATTERY. INOPERATIVE. THE TAIL CONE AREA EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY ASSEMBLY B5-260 BAD. BATTERY ASSEMBLY B5-260 WAS REPLACED P
- [SDR DALA2023082206831](https://openairdocs.org/sdr/DALA2023082206831), Aug 18, 2023: UNKNOWN. UNKNOWN. EXIT SIGN (RIGHT) AT ROW 19 KNOCKED DOWN. MAINTENANCE FOUND THE EMERGENCY SIGN COVERS KNOCKED OFF, RESECURED THEM AS REQUIRED. THE AIRCRAFT IS OK FOR SERVICE. (
- [SDR DALA2022032101833](https://openairdocs.org/sdr/DALA2022032101833), Mar 18, 2022: NOT REPORTED. NOT REPORTED. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING ABOVE SEAT 01B IN THE CABIN. MAINTENANCE RE-SECURED THE EMERGENCY "EXIT" LENS AT 01B AS REQUIRED. THE AIRCRAFT
- [SDR DALA2021102706652](https://openairdocs.org/sdr/DALA2021102706652), Oct 24, 2021: NONE. NONE. VAULT DOOR TAILCONE RELEASE PUSH-PULL CABLE TEFLON SHEATHING TORN AT RELEASE BLOCK STA 1212 AND AT THE 8 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION O
- [SDR DALA2021102606614](https://openairdocs.org/sdr/DALA2021102606614), Oct 24, 2021: NONE. NONE. FWD CARGO DOOR JAMB AREA HAS AREAS OF CHIPPED PAINT, LIGHT CORROSION, AND NO GRAY PAINT AS PER SRM 53-00-15 REPAIR 1 FROM HALFWAY UP JAMB FWD AND AFT SIDES AND 
- [SDR DALA2021102606613](https://openairdocs.org/sdr/DALA2021102606613), Oct 24, 2021: NONE. NONE. RIGHT SIDE AFT COCKPIT WINDOW HAS HEAVY SCRATCHES ON EXTERIOR. SUMMARY SEE NRC 001-0305:5610-2001/002 00062: REPLACED RT SIDE AFT COCKPIT WINDOW PER B717 AMM 56
- [SDR DALA2021102606612](https://openairdocs.org/sdr/DALA2021102606612), Oct 24, 2021: NONE. NONE. RIGHT HAND SIDE PASSENGER WINDOW #30 IS FADED. SUMMARY SEE NRC 001-0308:5620-2001/004 00008: REPLACED WINDOW PER B717 AMM 56-20-01. (LP #1994391)
- [SDR DALA2021050302490](https://openairdocs.org/sdr/DALA2021050302490), May 2, 2021: BATTERY PACK. INOPERATIVE. THE MAIN CABIN MAIN DOOR TOP EMR LIGHT OUT. R & R THE BATTERY PACK B5-123 PER AMM 33-51. OPS CHECK GOOD.
- [SDR DALA2020112303834](https://openairdocs.org/sdr/DALA2020112303834), Nov 22, 2020: LAMP. WRONG PART. BOTH AFT OVERWING EXIT SIGNS ARE INOPERATIVE. MAINTENANCE FOUND THE WRONG LAMPS INSTALLED. COMPLETED RE-LAMP AND OPERATIONAL CHECK WAS GOOD, PER B717 AMM 33-51.
- [SDR DALA2019070804080](https://openairdocs.org/sdr/DALA2019070804080), Jul 6, 2019: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGNS INOPERATIVE. EXIT LIGHTS FLASHING. T/S AS PER FIM 33-50; ALLOW SUFFICIENT TIME FOR BATTERY PACKS TO RE-CHARGE OPS CHECK NORMAL OK FOR SERVI
- [SDR DALA2018051503374](https://openairdocs.org/sdr/DALA2018051503374), May 8, 2018: COMPUTER. MALFUNCTIONED. THE CREW ABORTED THE TAKE-OFF AT 120 KNOTS AFTER THE "STAB TRIM" AURAL WARNING SOUNDED. THE STAB TRIM WAS SET WITHIN THE GREEN BOX AT 4.4 PRIOR TO THE TAKE-OFF 
- [SDR DALA2017112808353](https://openairdocs.org/sdr/DALA2017112808353), Nov 27, 2017: SKIN. CRACKED. CRACK ON INBOARD RT WING BUTE DOOR. INNER SKIN WAS REPLACED PER DWG 5919571 REV BG AND SRM 51-41-02.
- [SDR DALA2017112608328](https://openairdocs.org/sdr/DALA2017112608328), Nov 26, 2017: SKIN. DAMAGED. ELONGATED SCREW HOLES AT LOWER SKIN. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-41-01, AND DWG 5919571, REV BG.
- [SDR DALA2017112608327](https://openairdocs.org/sdr/DALA2017112608327), Nov 25, 2017: CUSP WEB. CRACKED. CRACK ON THE RT CUSP WEB BETWEEN BS 650 - 655, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW ER/A 562407-14, REV ORIGINAL AND ETI 17-17-243, REV 2.
- [SDR DALA2017112508326](https://openairdocs.org/sdr/DALA2017112508326), Nov 24, 2017: DOUBLER. CORRODED. CORROSION ON THE AFT CARGO BAY PRODUCTION DOUBLER IN THE JAMB AREA BETWEEN BS 965 - 979, LONGERONS 27 - 28R.
- [SDR DALA2017112408325](https://openairdocs.org/sdr/DALA2017112408325), Nov 23, 2017: SKIN. CRACKED. CRACK ON VERTICAL STABILIZER SKIN. THE SKIN WAS REPLACED IAW SRM 51-41-02 0G, 51-40-05 0G, AND DWG 5936143, REV AS.
- [SDR DALA2017112408324](https://openairdocs.org/sdr/DALA2017112408324), Nov 23, 2017: CARGO TRACK. CORRODED. CORROSION ON THE CARGO TRACK BS 892 TO 954 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 , 51-41-05, AND 51-41-02.
- [SDR DALA2017112408323](https://openairdocs.org/sdr/DALA2017112408323), Nov 23, 2017: CARGO TRACK. CORRODED. CORROSION ON THE CARGO TRACK BS 994 TO 1022, IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.
- [SDR DALA2017112408322](https://openairdocs.org/sdr/DALA2017112408322), Nov 23, 2017: CARGO TRACK. CORRODED. CORROSION ON CARGO TRACK BS 813 TO 1022 LT SIDE IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.
- [SDR DALA2017112408321](https://openairdocs.org/sdr/DALA2017112408321), Nov 23, 2017: STIFFENER. CRACKED. CRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.

All 158: https://openairdocs.org/aircraft/N995AT/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/N995AT/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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