# N992AT: 2002 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55136
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 20, 2002
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ADDA23
- 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=992AT
- Page: https://openairdocs.org/aircraft/N992AT

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 BMW Rolls 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 (BMW Rolls 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/N992AT/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 N992AT.

## FAA accident and incident reports

None matched to N992AT.

## Service difficulty reports (170, 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 DALA2026081104626](https://openairdocs.org/sdr/DALA2026081104626), Aug 11, 2026: POWER SUPPLY. INOPERATIVE. FOUND AFT BULKHEAD DOOR EMERGENCY LIGHT INOPERATIVE. R & R AFT CENTER EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51. CHECKS GOOD. OK FOR SVC.
- [SDR DALA2026031101693](https://openairdocs.org/sdr/DALA2026031101693), Mar 10, 2026: PROXIMITY SENSOR. FAULTED. ATB- GEAR UNSAFE INDICATION WITH GEAR HANDLE UP. CORRECTIVE ACTION: REPLACED BOTH GEAR UP AND LATCHED PROX SENSORS. ADJUSTED LEFT DOOR LATCH. REPLACED LEFT DOOR
- [SDR DALA2026030501522](https://openairdocs.org/sdr/DALA2026030501522), Mar 3, 2026: SWITCH. FAULTED. WORKING IB LOG 8283224 RED LINED IN ERROR. R & R THE PSEU IAW AMM 32-61-01 & LG SWITCH IAW AMM 32-62-03 (8283225)
- [SDR DALA2025121509135](https://openairdocs.org/sdr/DALA2025121509135), Dec 11, 2025: COVER. UNSECURE. TAIL EMG EXIT NEEDS RESECURING. REPLACED AFT EIXT ARMING COVER PER B717 AMM 52-12 (7940018)
- [SDR DALA2025111208302](https://openairdocs.org/sdr/DALA2025111208302), Nov 11, 2025: OIL SYSTEM. LEAKING. SMKE - AFTER STARTING APU AND TURNING ON PACKS, CABIN FILLED WITH ACRID, RUBBERY, BURNING VISIBLE SMOKE. TURNED OFF PACKS AND SMOKE DISSIPATED. FOUND APU OIL TA
- [SDR DALA2025102207717](https://openairdocs.org/sdr/DALA2025102207717), Oct 20, 2025: SEAL. FOD. DIVERTED TO BOS DUE TO R1 GALLEY DOOR HIGH PITCH SQUEAL. CLEANED DEBRIS & LUBED DOOR SEAL, PRESSURIZED AIRCRAFT. NO DEFECTS NOTED.(7584826)
- [SDR DALA2025062604792](https://openairdocs.org/sdr/DALA2025062604792), Jun 25, 2025: COALESCER BAG. CONTAMINATED. SHIP 9535 STARTED APU AND DIRTY, MUSTY SMELL OCCURRED ONCE AIR CAME ON. CALLED MX, UNABLE TO FIX IMEDIATLY. CORRECTIVE ACTION: COALESCER BAGS SOAK IN WATER AND 
- [SDR DALA2024122311964](https://openairdocs.org/sdr/DALA2024122311964), Dec 20, 2024: SKIN. DAMAGED. FUSELAGE DAMAGE AFT OF L1 DOOR. REPAIRED A/C PER ER/A 542469-14 REV A. REF 001-0002:0514-2000 NRC 6 FOR DOCUMENTATION OF WORK PERFORMED. (LP #6956730)
- [SDR DALA2024122311962](https://openairdocs.org/sdr/DALA2024122311962), Dec 20, 2024: SKIN. GROUND DAMAGE. AIRCRAFT SUSTAINED DAMAGE FROM JETWAY CONTACT AT LH FRAME STATION BS 237 BETWEEN STR 18L AND STR 17LH. SUMMARY NRC 001-0002:0514-2001/006 00006: COMPLIED WITH E
- [SDR DALA2024122311965](https://openairdocs.org/sdr/DALA2024122311965), Dec 19, 2024: NONE. NONE. DTE TRACKING PER ER/A 542469-14 REV A. REPAIR APPROVAL IS LIMITED TO 12 MONTHS OF SERVICE. ER/A REVISION REQUIRED FOR SERVICE BEYOND THIS LIMIT. DTA REQUIRED IN
- [SDR DALA2024022302565](https://openairdocs.org/sdr/DALA2024022302565), Jan 9, 2024: FAIRING. MISSING. THE #2 ENGINE WAS EXPERIENCING HIGH OIL CONSUMPTION. DURING THE INVESTIGATION, WHEN THE #2 ENGINE COWLS WERE OPENED, MAINTENANCE DISCOVERED THAT THE LOWER LEFT 
- [SDR DALA2024010800321](https://openairdocs.org/sdr/DALA2024010800321), Jan 5, 2024: UNKNOWN. UNKNOWN. THE EXTERIOR EMERGENCY ILLUMINATION SYSTEM IS INOPERATIVE. MAINTENANCE FOUND DAMAGE ON PCB OF POWER SUPPLY. THE PCB OF POWER SUPPLY WAS REPLACED PER B717 AMM 33
- [SDR DALA2023071205665](https://openairdocs.org/sdr/DALA2023071205665), Jul 12, 2023: UNKNOWN. UNKNOWN. CORROSION TYPE EXFOLATION ON FUSELAGE SKIN (LOWER CUTOUT) AT AFT CARGO COMPARTMENT STA 974. SUMMARY OF NRC 00512: CORROSION LEVEL 2. FUSELAGE SKIN LOWER CUTOUT 
- [SDR DALA2023080406299](https://openairdocs.org/sdr/DALA2023080406299), Jul 11, 2023: UNKNOWN. UNKNOWN. ER/A 610235-14; FUSELAGE SKIN AFT CARGO DOOR CUTOUT SKIN AND DOUBLER STA Y=954 TO 994, L-28R IS CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH E
- [SDR DALA2023071205663](https://openairdocs.org/sdr/DALA2023071205663), Jul 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA Y=1021 LONGERON 30+1.5 IN RH/LH. SUMMARY OF NRC 00513: CORROSION LEVEL 2. FRAME STA Y=1021 LONGERON 30 WAS REPAIRED PER B717 SRM 53-20-07
- [SDR DALA2023071205661](https://openairdocs.org/sdr/DALA2023071205661), Jul 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH ANGLE CUSP FROM STA Y=200 TO Y=219 AT PAX CABIN. SUMMARY OF NRC 00253: CORROSION LEVEL 2. RH ANGLE CUSP FROM STA Y=160 TO Y=219 WAS REPAIRED PER
- [SDR DALA2023070405374](https://openairdocs.org/sdr/DALA2023070405374), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00181: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y
- [SDR DALA2023070405373](https://openairdocs.org/sdr/DALA2023070405373), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB SEVERAL POINTS AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00176: CORROSION LEVEL 2. DOOR JAMB AT AFT COMPARTMENT WAS REPLACED PER B717 SRM 5
- [SDR DALA2023070405370](https://openairdocs.org/sdr/DALA2023070405370), Jul 3, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL STA 636 X=0 CEILING AREA, FWD CARGO. SUMMARY OF NRC 00507: INTERCOSTAL STA 636 X=0 CEILING AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCE
- [SDR DALA2023070305309](https://openairdocs.org/sdr/DALA2023070305309), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB SEVERAL POINTS AT AREA DOOR AFT COMPARTMENT (ENTRY AREA) (C2). SUMMARY OF NRC 00175: CORROSION LEVEL 2. WEB AREA DOOR AFT COMPARTMENT WAS REPLA
- [SDR DALA2023070305308](https://openairdocs.org/sdr/DALA2023070305308), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA 1002 LONGERON 29RH TO 29LH AT AFT CARGO. SUMMARY OF NRC 00496: CORROSION LEVEL 2. FRAME CLIP STA 1002 LONGERON 29RH TO 29LH WAS REPL
- [SDR DALA2023070305305](https://openairdocs.org/sdr/DALA2023070305305), Jul 1, 2023: UNKNOWN. UNKNOWN. SEAT TRACK ON STA 545 TO STA 560 WAS FOUND CORRODED OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 1. SUMMARY OF NRC 00473: CORROSION LEVEL 2. SEAT TRACK ON S
- [SDR DALA2023070305301](https://openairdocs.org/sdr/DALA2023070305301), Jul 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH INBD SEAT TRACK STA Y=215 TO Y=220 AT PAX CABIN. SUMMARY OF NRC 00251: CORROSION LEVEL 2. RH INBD SEAT TRACK STA Y=215 TO Y=220 WAS REPAIRED PER
- [SDR DALA2023070305300](https://openairdocs.org/sdr/DALA2023070305300), Jun 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 AT PAX CABIN W1. SUMMARY OF NRC 00309: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 BTW X=-20 AND X=-45 A
- [SDR DALA2023070305298](https://openairdocs.org/sdr/DALA2023070305298), Jun 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON FITTING STA 893.5 BELOW FLOOR LEVEL CUSP WEB AREA WAS FOUND. SUMMARY OF NRC 00503: CORROSION LEVEL 2. FITTING SPLICE ON STA 893.5 RH WAS REPLACED P
- [SDR DALA2023062905211](https://openairdocs.org/sdr/DALA2023062905211), Jun 28, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL ON CUSP WEB (LIGHTNING HOLE) STA 539, STA 648, STA 890 TO 907, AND STA 929 TO 935 AREAS WERE FOUD OUT OF LIMITS PER B717 SRM 53-00-55-1A
- [SDR DALA2023062805189](https://openairdocs.org/sdr/DALA2023062805189), Jun 28, 2023: UNKNOWN. UNKNOWN. EXFOLIATION CORROSION ON DIAPHRAGM STA Y=178 TO Y=198 X=-45 X=-52 AT PAX CABIN W1. SUMMARY OF NRC 00303: CORROSION LEVEL 2. DIAPHRAGM STA Y=178 TO Y=198 X=-45 T
- [SDR DALA2023070305297](https://openairdocs.org/sdr/DALA2023070305297), Jun 27, 2023: UNKNOWN. UNKNOWN. BROKEN FLOOR PANEL 121MF OF FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00470: FLOOR PANEL 121MF WAS MANUFACTURED AND REPLACED PER ERA 544901-14 REV A AND INSTAL
- [SDR DALA2023062805188](https://openairdocs.org/sdr/DALA2023062805188), Jun 27, 2023: UNKNOWN. UNKNOWN. CRACKS ON CUSP WEB STA Y=715 AND Y=897 BELOW SEAT TRACK LBL=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00265: CUSP WEB STA Y=715 AND Y=897 LBL=44 AT PASSENGER
- [SDR DALA2023062805186](https://openairdocs.org/sdr/DALA2023062805186), Jun 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON WIRING CLIPS STA Y=272, Y=291, Y=305, Y=310, Y=539, Y=648, Y=849, Y=875, & Y=885 LBL=57 ALSO Y= 885, Y=886, Y=835, Y=845, Y=848, Y=648, Y=575, Y=73
- [SDR DALA2023062805182](https://openairdocs.org/sdr/DALA2023062805182), Jun 26, 2023: UNKNOWN. UNKNOWN. CRACKS ON PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00372: PAN FWD INNER SIDE PROJECTION BEAMS 1, 3, & 5 AT FWD CAR
- [SDR DALA2023062805181](https://openairdocs.org/sdr/DALA2023062805181), Jun 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE AT L1 DOOR JAM WEB (AFT) STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00438: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAM WEB AFT STA Y=200 AT PAX CABIN
- [SDR DALA2023070305296](https://openairdocs.org/sdr/DALA2023070305296), Jun 25, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON ANGLE BTW STA Y=149 TO Y=160 AND RBL 56 AT R1 DOOR CUTOUT AREA. (CPAX). SUMMARY OF NRC 00460: CORROSION LEVEL 2. ANGLE BTW STA Y=149 TO Y
- [SDR DALA2023062805179](https://openairdocs.org/sdr/DALA2023062805179), Jun 25, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL AT THE EDGES OF LIGHTENING HOLE ON CUSP; WEBS AT STA Y=469, Y=508, Y=518, Y=527, Y=546, AND X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-0
- [SDR DALA2023062805178](https://openairdocs.org/sdr/DALA2023062805178), Jun 25, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL, THE EDGES OF LIGHTENING HOLES ON CUSP WEBS AT STA Y=461, Y=488, Y=585, Y=799, TO Y=809; LBL X=58 WERE FOUND OUT LIMITS PER B717 SRM 53-
- [SDR DALA2023062805176](https://openairdocs.org/sdr/DALA2023062805176), Jun 24, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL AT LONGERON 30, STA 965.5 TO 967.5 AND STA 972.5 TO 973.5 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GE
- [SDR DALA2023062805175](https://openairdocs.org/sdr/DALA2023062805175), Jun 24, 2023: UNKNOWN. UNKNOWN. CORROSION REMOVAL ON CUSP WEB STA Y=843 TO Y=846 IS OUT OF LIMITS PER B717 53-00-55-1A PROCEDURE 1 PAR. 4. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CUSP WEB STA
- [SDR DALA2023062705157](https://openairdocs.org/sdr/DALA2023062705157), Jun 23, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL ON GALLEY FITTING BTW STA Y=200 AND Y=218 BTW X=-20 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAMAGE FIG. 101 (SHEET 2)
- [SDR DALA2023062705155](https://openairdocs.org/sdr/DALA2023062705155), Jun 23, 2023: UNKNOWN. UNKNOWN. RELATED NRC 261 AFTER CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200 BTW X=6 AND X=-6 FLOOR SUPPORT WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A ALLOWABLE DAM
- [SDR DALA2023062305083](https://openairdocs.org/sdr/DALA2023062305083), Jun 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK RBL 22 BTW STA 411-413 AT PAX COMPARTMENT. (CPAX). SUMMARY OF NRC 00467: CORROSION LEVEL2. SEAT TRACK RBL 22 BTW STA 411-413 WAS REPAIRE
- [SDR DALA2023062105025](https://openairdocs.org/sdr/DALA2023062105025), Jun 20, 2023: UNKNOWN. UNKNOWN. EXFOLIATION CORROSION ON FLOOR SUPPORT RH STA Y=198 X=55 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00271: CORROSION LEVEL 2. FLOOR SUPPORT RH STA Y=198 X=55 WAS REPL
- [SDR DALA2023061904973](https://openairdocs.org/sdr/DALA2023061904973), Jun 19, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND AT JAM WEB STA Y=200 ON STRINGER 18. SUMMARY OF NRC 00458: CORROSION LEVEL 2. JAM WEB STA Y=200 ON STRINGER 18 WAS REPAIRED PER B717 SRM 51-
- [SDR DALA2023061904969](https://openairdocs.org/sdr/DALA2023061904969), Jun 17, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=200 X=10 AT PAX CABIN W1. SUMMARY OF NRC 00275: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 X=10 WAS REPLACED PER B717 SRM 51-41
- [SDR DALA2023061904968](https://openairdocs.org/sdr/DALA2023061904968), Jun 17, 2023: UNKNOWN. UNKNOWN. CORROSION ON DIAPHRAGM STA Y=198 TO Y=200 BTW X=-30 AND X=-50 (RH SIDE) AT PAX CABIN. SUMMARY OF NRC 00254: CORROSION LEVEL 2. DIAPHRAGM STA Y=198 TO Y=218 BTW 
- [SDR DALA2023061904965](https://openairdocs.org/sdr/DALA2023061904965), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 (L1 DOOR) AT PAX CABIN. SUMMARY OF NRC 00274: CORROSION LEVEL 2. DIAPHRAGM FROM STA Y=190 TO Y=
- [SDR DALA2023061904964](https://openairdocs.org/sdr/DALA2023061904964), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=175 TO Y=198 X=- 45 AT PAX CABIN W1. SUMMARY OF NRC 00290: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=175 TO Y=198 X=-45 AT PAX CAB
- [SDR DALA2023061604905](https://openairdocs.org/sdr/DALA2023061604905), Jun 16, 2023: UNKNOWN. UNKNOWN. CRACK ON ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR. SUMMARY OF NRC 00128: ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR WAS REPAIRED PER B717-200 
- [SDR DALA2023061604902](https://openairdocs.org/sdr/DALA2023061604902), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=180 AND Y=195 AT PAX CABIN W1. SUMMARY OF NRC 00268: CORROSION LEVEL 2. FLOOR SUPPORT L1 ENTRANCE DOOR STA Y=1
- [SDR DALA2023061504880](https://openairdocs.org/sdr/DALA2023061504880), Jun 15, 2023: UNKNOWN. UNKNOWN. CRACK CUSP WEB STA Y=218 RBL=54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00272: CUSP WEB STA Y=218 RBL=54 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4. (LP #
- [SDR DALA2023061504877](https://openairdocs.org/sdr/DALA2023061504877), Jun 14, 2023: UNKNOWN. UNKNOWN. CRACK ON AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00092: AFT CARGO DOOR FRAME BTW ANGLE AND LACH AT AFT CARGO COMPARTMEN

All 170: https://openairdocs.org/aircraft/N992AT/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/N992AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The BMW Rolls BR-700 series engine: https://openairdocs.org/engine/bmw-rolls-br-700-series.md

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