# N997AT: 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: 55141
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 7, 2002
- Certificate issued: April 8, 2024
- Expires: April 30, 2031
- Mode S code: ADECB6
- 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=997AT
- Page: https://openairdocs.org/aircraft/N997AT

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/N997AT/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 N997AT.

## FAA accident and incident reports

None matched to N997AT.

## Service difficulty reports (206, 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 DALA2026090705016](https://openairdocs.org/sdr/DALA2026090705016), Sep 4, 2026: LATCH. DETACHED. GIRT BAR CAME OFF AND CAME UNLATCHED. REATTACHED L1 DOOR GIRT BAR LATCH PER AMM 25-61. (7631672) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026021901200](https://openairdocs.org/sdr/DALA2026021901200), Feb 15, 2026: SKIN. CRACKED. AIRCRAFT 9545, CRACK ON UPPER FUSELAGE SKIN STA Y=1152 BTW LONG 2L & 3L AFT FUSELAGE. CORRECTIVE ACTION: CRACK ON UPPER FUSELAGE SKIN STA Y=1152 BTW LONG 2L & 3
- [SDR DALA2026021901197](https://openairdocs.org/sdr/DALA2026021901197), Feb 15, 2026: HINGE FITTING. EXCESS PLAY. AFTER REMOVING SEALANT, FOUND FREE PLAY ON FLAP HINGE NR 3 AT RT WING. FLAP HINGE NR 3 AT RT WING WAS REPAIRED IAW PRI 632047-14, REV 3, & ER/A 632047-14, REV O
- [SDR DALA2026021801118](https://openairdocs.org/sdr/DALA2026021801118), Feb 12, 2026: DOUBLER. CRACKED. CRACKED DOUBLER, BS 1178, BTW LONGERONS 15 -16L, AFT ACCESSORY COMPARMENT. REPAIRED IAW PRI 632147-14 (1448393).
- [SDR DALA2026021801113](https://openairdocs.org/sdr/DALA2026021801113), Feb 9, 2026: SKIN. CRACKED. CRACKED EXTERNAL FUSELAGE SKIN BS 1087 BTW LONGERONS 12 - 13R. REPAIRED IAW PRI 631947-14 (1442449).
- [SDR DALA2026020900906](https://openairdocs.org/sdr/DALA2026020900906), Feb 3, 2026: LANYARD. DAMAGED. BROKEN THREADS LANYARD ON RT & LT DOOR SLIDE DEPLOYMENT AT CPAX. REPAIRED PER AMDS 5211-4002 (1434470)
- [SDR DALA2026020900913](https://openairdocs.org/sdr/DALA2026020900913), Feb 2, 2026: SKIN. CRACKED. FUSELAGE SKIN, BS 1087, L13L TO L14L, CRACKED. REPAIRED IAW ERA 631962-14. (1439311)
- [SDR DALA2026020900912](https://openairdocs.org/sdr/DALA2026020900912), Feb 2, 2026: SKIN. CRACKED. FUSELAGE SKIN, Y=1087, L13R TO L14R CRACKED. REPAIRED IAW ER/A 631947-14. (1435871)
- [SDR DALA2025120108774](https://openairdocs.org/sdr/DALA2025120108774), Nov 27, 2025: OIL SYSTEM. LEAKING. SHIP 9545 MUSTY SOCK SMELL FROM FORWARD GALLEY VENT. FOUND APU OIL LEAKING. R/R APU PER B717 AMM 49-10 OPS CHK GOOD (7952228)
- [SDR DALA2025112308529](https://openairdocs.org/sdr/DALA2025112308529), Nov 21, 2025: SIGN. DISLODGED. FWD EXIT SIGN DAMAGED. (F/A REPORTED PASSENGER HIT IT WITH HIS BAG). RESECURED, OPS NORMAL. (LP 7952210)
- [SDR DALA2025102407797](https://openairdocs.org/sdr/DALA2025102407797), Oct 21, 2025: WARNING MESSAGE. FALSE ACTIVATION. ATO- DURING TAKEOFF ROLL THE CREW REPORTED A STAB OUT OF TRIM AURAL WARNING AND ABORTED TAKEOFF. MAINTENANCE PERFORMED STABILIZER SYSTEM TESTS AND RETURNED TO S
- [SDR DALA2024112711260](https://openairdocs.org/sdr/DALA2024112711260), Nov 24, 2024: FASTENER. LOOSE. -AD- FOUND LOOSE FASTENERS ON RH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY NRC 018-0001:5530-01048-02 / 002 00005: CHECK IF T
- [SDR DALA2024112611225](https://openairdocs.org/sdr/DALA2024112611225), Nov 24, 2024: FASTENER. LOOSE. -AD- FOUND LOOSE FASTENERS ON LH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY OF NRC 018-0001:5530-01048-02 /001 00004: CHECKED 
- [SDR DALA2024020601580](https://openairdocs.org/sdr/DALA2024020601580), Feb 6, 2024: SKIN. BENT. BENT ON EDGE EXTERNAL SKIN AFT UPPER, AFT LOWER, AND BEAM #4 AT SERVICE DOOR L1. SUMMARY OF NRC 00069: EXTERNAL SKIN ON AFT UPPER EDGE AND EDGE OF EXTERNAL SKIN
- [SDR DALA2024020301512](https://openairdocs.org/sdr/DALA2024020301512), Feb 2, 2024: WEB. CRACKED. CRACK MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA. SUMMARY OF NRC 00357: MEMBRANE ON UPPER SURFACE 
- [SDR DALA2024020301508](https://openairdocs.org/sdr/DALA2024020301508), Feb 1, 2024: SKIN. CORRODED. CORROSION ON INNER SKIN BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INTERNAL SKIN DOUBLE
- [SDR DALA2024020301506](https://openairdocs.org/sdr/DALA2024020301506), Feb 1, 2024: DOOR FRAME. CORRODED. CORROSION ON DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT. C2. SUMMARY OF NRC 00071: CORROSION LEVEL 2. PREVIOUS REPAIR SECTION OF DOOR JAMB STA 951 TO
- [SDR DALA2024020101448](https://openairdocs.org/sdr/DALA2024020101448), Feb 1, 2024: LONGERON. CORRODED. CORROSION ON LOWER SURFACE LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00172: CORROSION LEVEL 2. CLIP LONGERON END STA 360 L26R AT FWD COM
- [SDR DALA2024012601170](https://openairdocs.org/sdr/DALA2024012601170), Jan 25, 2024: FLOOR SUPPORT. CRACKED. CRACK ON FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00170: FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1) 
- [SDR DALA2024012501108](https://openairdocs.org/sdr/DALA2024012501108), Jan 25, 2024: CUSP WEB. CORRODED. CORROSION ON ANGLE CUSP BTW STA Y=168 AND STA Y=200, AND STA X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY). SUMMARY OF NRC 00245: CORROSION LEVEL 2. CUSP ANGLE BTW 
- [SDR DALA2024012200906](https://openairdocs.org/sdr/DALA2024012200906), Jan 20, 2024: ANGLE. CRACKED. CRACK ON ANGLE STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1. SUMMARY OF NRC 00073: ANGLE (INTERCOSTAL) STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1 WAS MA
- [SDR DALA2024011900807](https://openairdocs.org/sdr/DALA2024011900807), Jan 18, 2024: WEB. CRACKED. CARCK ON WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX. SUMMARY OF NRC 00342: WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #01
- [SDR DALA2024011800751](https://openairdocs.org/sdr/DALA2024011800751), Jan 17, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB LOWER SURFACE BTW STA Y=435 TO Y=465 PAX CABIN. SUMMARY OF NRC 00558: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=435 TO Y=465 PAX CABIN W
- [SDR DALA2024011600591](https://openairdocs.org/sdr/DALA2024011600591), Jan 16, 2024: WEB. CRACKED. CRACKS ON WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX. SUMMARY OF NRC 00346: WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX WAS REPAIRED PER 
- [SDR DALA2024011500575](https://openairdocs.org/sdr/DALA2024011500575), Jan 13, 2024: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR AT CPAX. SUMMARY OF NRC 00485: CORROSION LEVEL 2. CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR WERE R
- [SDR DALA2024011200539](https://openairdocs.org/sdr/DALA2024011200539), Jan 11, 2024: UNKNOWN. UNKNOWN. CORROSION OF MEMBRANE WEP ON STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEP ON STA Y=198 AND STA X
- [SDR DALA2024011200538](https://openairdocs.org/sdr/DALA2024011200538), Jan 11, 2024: UNKNOWN. UNKNOWN. CORROSION ON MEMBRANE WEB AT STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEB AT STA Y=198 AND STA X
- [SDR DALA2024011000451](https://openairdocs.org/sdr/DALA2024011000451), Jan 10, 2024: UNKNOWN. UNKNOWN. CRACKED WEB AT STA Y=674 -X=44 CABIN FLOOR IN CPAX. SUMMARY OF NRC 00336: CRACK ON WEB STA Y=674 -X=44 CABIN FLOOR IN CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R
- [SDR DALA2023120710009](https://openairdocs.org/sdr/DALA2023120710009), Dec 6, 2023: UNKNOWN. UNKNOWN. DENT ON 1L DOOR SKIN. LEFT LOWER CORNER. DENT MEASURES 3" X .5". FOUND DAMAGE TO PRESSURE SEAL MEASURES APPROX 1.5'. ACCOMPLISHED SECTION 1 FERRY FLIGHT PREPERA
- [SDR DALA2022053103722](https://openairdocs.org/sdr/DALA2022053103722), May 27, 2022: BATTERY PACK. INOPERATIVE. FOUND THE CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERWING EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33 -51. OPERATIONAL CH
- [SDR DALA2022051003228](https://openairdocs.org/sdr/DALA2022051003228), May 9, 2022: GASPER FAN. SEIZED. SHIP 9545 - THE FLIGHT CREW DIVERTED THE AIRCRAFT TO JAX DUE TO A STRONG ODOR IN THE COCKPIT AND SMOKE IN THE CABIN AS REPORTED BY THE CABIN CREW. AN EMERGENCY 
- [SDR DALA2021121607775](https://openairdocs.org/sdr/DALA2021121607775), Dec 10, 2021: NONE. NONE. AFT CARGO LOWER DOOR JAMB FROM MID DOOR TO FWD END OF JAMB HAS LARGE AREAS OF SURFACE CORROSION.(M) SUMMARY SEE NRC 054-0009 5300-2007/002 00319: CORROSION LEVE
- [SDR DALA2021110406789](https://openairdocs.org/sdr/DALA2021110406789), Nov 2, 2021: NONE. NONE. THE EMERGENCY FLOOR PATH LIGHTING AT 19D IS MISSSING. MAINTENANCE REPLACED 19D EMERGENCY FLOOR LIGHT STRIP PER B717 AMM 33-50. OPERATIONAL CHECK WAS GOOD. (LP #
- [SDR DALA2021092805822](https://openairdocs.org/sdr/DALA2021092805822), Sep 25, 2021: NONE. NONE. THE FORWARD ATTENDANT EMERGENCY EXIT SIGN AND THE CEILING PANELS #11 AND #12 EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY PACKS A
- [SDR DALA2021082404983](https://openairdocs.org/sdr/DALA2021082404983), Aug 21, 2021: BATTERY PACK. INOPERATIVE. THE RIGHT AND LEFT AFT OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS ARE INOPERATIVE. IN REFERENCE TO THE B717 AMM 33-51, MAINTENANCE REPLACED THE EXIT LIGHT POWER 
- [SDR DALA2021120907586](https://openairdocs.org/sdr/DALA2021120907586), Apr 27, 2021: NONE. NONE. LEADING EDGE SLAT TRACK CUTOUT MISSING ON #3 SLAT. FORWARD CUTOUT DOOR TO CDL 57-47-01. PLACARD INSTALLED. MISSING PART NUMBER IN IPC IS NOT EFFECTIVE FOR THIS 
- [SDR DALA2021041902263](https://openairdocs.org/sdr/DALA2021041902263), Apr 18, 2021: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT IDENTIFIER LIGHT AT THE FIRST ROW OF SEATS AND THE OVERHEAD EMERGENCY FLOODLIGHT AT THE SERVICE DOOR ARE BOTH INOPERATIVE. MAINTENANCE REPLAC
- [SDR DALA2020121104051](https://openairdocs.org/sdr/DALA2020121104051), Dec 10, 2020: SKIN. CRACKED. VERTICAL STAB ZFS 52.267 LT SKIN CRACK INDICATION. MAINTENANCE COMPLIED WITH ALL STEPS OF PRI 588955-14AD REV ORIG, 1, 2, 3, AND 4. COMPLIED WITH TIME LIMITED R
- [SDR DALA2020121104050](https://openairdocs.org/sdr/DALA2020121104050), Dec 10, 2020: SPAR CAP. CRACKED. THE THIRD BOLT HOLE BELOW STA ZFS=52.267 ON LT VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA 5530-01048 AND AD 2018-10-08. MAINTENANCE COMPLIED WITH
- [SDR DALA2020121004034](https://openairdocs.org/sdr/DALA2020121004034), Dec 10, 2020: SPAR CAP. CRACKED. 4TH BOLT HOLE BELOW STA ZFS=52.267 ON LT SIDE OF VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA5530-01048 & AD 2018 -10-08. C/W CRACK VERIFICATION, P
- [SDR DALA2022092906387](https://openairdocs.org/sdr/DALA2022092906387), Dec 9, 2020: NONE. NONE. DAMAGE TOLERANCE EVALUATION ERA 5882955-14AD ISSUED FOR VERTICAL STABILIZER SKIN CRACK REPAIR. FOLLOW ON ACTION REQUIRED. ACCOMPLISH DAMAGE TOLERANCE EVALUATION
- [SDR DALA2020112303836](https://openairdocs.org/sdr/DALA2020112303836), Nov 21, 2020: FRAME. CRACKED. A CRACK WAS FOUND ON THE REAR FRAME (48 SECTION UPPER). THE AFT TAIL CONE WAS DROPPED. MAINTENANCE REMOVED THE DAMAGED 48 SECTION OF THE UPPER FRAME AND INSTALL
- [SDR DALA2020111203697](https://openairdocs.org/sdr/DALA2020111203697), Nov 10, 2020: ACCESS DOOR. MISSING. DURING THE POST-FLIGHT INSPECTION, THE PILOT DISCOVERED THAT THE RIGHT ELEVATOR OUTBOARD MOST HINGE NUT LOWER ACCESS DOOR WAS MISSING. MAINTENANCE FORWARDED IT 
- [SDR DALA2020102603460](https://openairdocs.org/sdr/DALA2020102603460), Oct 25, 2020: SKIN. CRACKED. LT SIDE OF VERTICAL STAB LEADING EDGE HAS 3 CRACK INDICATIONS IN HOLES NR 2, 3, & 4 BELOW STA 2FS=52.267, REF AMDS CARD 5530-01048-02 STP 8, AA5530-01048 AD 201
- [SDR DALA2020102603459](https://openairdocs.org/sdr/DALA2020102603459), Oct 25, 2020: SKIN. CRACKED. THE RT SIDE OF VERTICAL STAB LEADING EDGE HAS A CRACK INDICATION IN HOLE NR 3 BELOW STA 2FS=52.267, REF AMDS CARD 5230-01048-02 STEP 8, AA 5530-01048 AD 2018-10
- [SDR DALA2022092906386](https://openairdocs.org/sdr/DALA2022092906386), Oct 24, 2020: NONE. NONE. DAMAGE TOLERANCE EVALUATION IN REFERENCE TO ERA 588282-14AD. ASSOCIATED ER/A 14-588282 ADDED FOR AC 9545. UPDATED MONITOR TITLE. REFER TO ERA 588955-14AD AND MO
- [SDR DALA201904222553](https://openairdocs.org/sdr/DALA201904222553), Apr 19, 2019: FRAME. CRACKED. FUSELAGE FRAME AT STA Y 696 RT SIDE HAS A CRACK. REF AA 5310-01436 CRACK IS CONDITION 3. NRC 026-0004:5310-01436-01D/001 00060: REPLACED FRAME AT STA 696 RH PER
- [SDR DALA201811206696](https://openairdocs.org/sdr/DALA201811206696), Nov 17, 2018: SLIDE. UNSERVICEABLE. DURING TAIL CONE ESCAPE SLIDE PIN CHECK, MAINTENANCE FOUND THE SLIDE TO BE UNSERVICEABLE (FAULT NOT SPECIFIED). MAINTENANCE REPLACED THE TAIL CONE SLIDE PER B71
- [SDR DALA2018021400884](https://openairdocs.org/sdr/DALA2018021400884), Feb 14, 2018: LIGHT. INOPERATIVE. RIGHT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT IAW AMM 33-50, OPS CHECKED GOOD.
- [SDR DALA2017061504722](https://openairdocs.org/sdr/DALA2017061504722), Jun 14, 2017: DOUBLER. CRACKED. CRACK ON PRODUCTION DOUBLER BS 1178 BETWEEN LONGERONS 19R TO 20R. REPAIRED IAW DWG 9911859, REV BU AND SRM 51-20-09.

All 206: https://openairdocs.org/aircraft/N997AT/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/N997AT/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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