# N906AT: 2001 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: 55087
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 12, 2001
- Certificate issued: May 14, 2025
- Expires: May 31, 2032
- Mode S code: AC8588
- 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=906AT
- Page: https://openairdocs.org/aircraft/N906AT

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/N906AT/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 N906AT.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040808025919I](https://openairdocs.org/incident/20040808025919I), Aug 8, 2004: Boeing 717200 (N906AT), Akron, OH. (-23) Seat on aircraft was stained with blood from previous passenger. Flight attendants blocked seat. Passenger attempted to place luggage in blocked seat.…

## Service difficulty reports (160, 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 DALA2026090304980](https://openairdocs.org/sdr/DALA2026090304980), Sep 3, 2026: FLAP. NO DISCREPANCY. EVIDENCE OF RUBBING ON LEADING EDGE OF LEFT INBOARD FLAP LOCATED JUST ABOVE MAIN LANDING GEAR. PAINT SHOWING BARE METAL IN THAT AREA, INSPECTED LT INBD FLAP AND
- [SDR DALA2026090304979](https://openairdocs.org/sdr/DALA2026090304979), Sep 2, 2026: FLAP. NO DISCREPANCY. POTENTIAL RUB DAMAGE ON UNDERSIDE OF THE LEFT WING FLAP. LOCATED JUST ABOVE MAIN LANDING GEAR, INSPECTED LT INBD FLAP AND FOUND NO EVIDENCE OF RUBBING OR CHAFIN
- [SDR DALA2026082504810](https://openairdocs.org/sdr/DALA2026082504810), Aug 24, 2026: GIRT BAR. UNSECURE. L1 DOOR SLIDE APPEARS TO BE BROKEN, RESECURED GIRT BAR IAW AMM 52-11. (9092292) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304130](https://openairdocs.org/sdr/DALA2026071304130), Jul 10, 2026: O-RING. LEAKING. NR 1 ENGINE FUEL LEAK ON WALK AROUND STRONG FUEL ODOR ON APU AIR. R & R O-RING IAW AIPC 73-12-05-22. (8831910) (AIRCRAFT GROUNDED)
- [SDR DALA2026011600378](https://openairdocs.org/sdr/DALA2026011600378), Jan 10, 2026: WINDSHIELD. CRACKED. DIVERTED TO BNA FOR CAPT. WINDSHIELD OUTER PANE CRACKED. MAINTENANCE CLEANED, INSPECTED, PRESSURIZED AND RETURNED TO SERVICE WITH NO FAULTS DETECTED.(7498293)
- [SDR DALA2026010900242](https://openairdocs.org/sdr/DALA2026010900242), Jan 5, 2026: HANDLE. BROKEN. AFT CARGO DOOR HANDLE IS BROKEN OFF & MISSING. INSTALLED AFT CARGO DOOR HANDLE REF B717 CMM 52-30-2. OPS CHECK GOOD. (7498261)
- [SDR DALA2024111410956](https://openairdocs.org/sdr/DALA2024111410956), Nov 14, 2024: BATTERY PACK. NO TEST. THE EMERGENCY EXIT SIGNS ARE INOPERATIVE AT STATION 180, STATION 247, AND STATION 706. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACKS B5-235, B5-259, AND B5-1
- [SDR DALA2024081608213](https://openairdocs.org/sdr/DALA2024081608213), Aug 16, 2024: BATTERY PACK. INOPERATIVE. OVERWING DOOR EMERGENCY LIGHTS ARE INOPERATIVE. T/S OVERWING DOOR EMERGENCY LIGHTS PER B717 FIM 33-50-00 810-801. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT L
- [SDR DALA2024062106299](https://openairdocs.org/sdr/DALA2024062106299), Jun 19, 2024: LATCH. LOOSE. SHIP 9582 -GEAR/DE- DURING THE FINAL APPROACH FOR LANDING THE AIRCRAFT INDICATED A "GEAR UNSAFE" CONDITION FOR ALL 3 GEAR POSITIONS. AN EMERGENCY WAS DECLARED W
- [SDR DALA2024042304672](https://openairdocs.org/sdr/DALA2024042304672), Apr 22, 2024: RELAY. FAULTED. SHIP 9582 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH INTO MSP. AN EMERGENCY WAS DECLARED BY THE CR
- [SDR DALA2023121110134](https://openairdocs.org/sdr/DALA2023121110134), Dec 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL SKIN AT STAIRWAY DOOR. SUMMARY OF NRC 00568: CORROSION LEVEL 2. STAIRWAY DOOR ASSEMBLY WAS REPLACED PER B717-200 AMM 52-63-01 420-801. (LP
- [SDR DALA2023120609977](https://openairdocs.org/sdr/DALA2023120609977), Dec 5, 2023: UNKNOWN. UNKNOWN. CRACK PAN ON FWD AND AFT UPPER CORNERS AT (L1) PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00176: PAN OF FWD UPPER CORNER AT (L1) PASSENGER ENTRA
- [SDR DALA2023112809760](https://openairdocs.org/sdr/DALA2023112809760), Nov 27, 2023: UNKNOWN. UNKNOWN. CRACK ON PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 160-165 APPROX INTERNAL STRUCTURE (L1). SUMMARY OF NRC 00687: PASSENGER ENTRANCE DOOR NO.1 BEAM BTW STA Y 1
- [SDR DALA2023112809753](https://openairdocs.org/sdr/DALA2023112809753), Nov 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH IN REF NRC 00216. SUMMARY OF NRC 00685: CORROSION LEVEL 2. PREVIOUS SPLICE REPAIR ON 
- [SDR DALA2023112809765](https://openairdocs.org/sdr/DALA2023112809765), Nov 25, 2023: UNKNOWN. UNKNOWN. DIMENSIONAL MEASUREMENTS WERE FOUND OUT OF LIMITS ON SECTION OF WING BOX UPPER SKIN BTW STA Y=750 AND X=19 TO X=59 AT LH MLG/ WHEEL WELL (SM) AFTER CORROSION RE
- [SDR DALA2023112709724](https://openairdocs.org/sdr/DALA2023112709724), Nov 25, 2023: UNKNOWN. UNKNOWN. CORRODED LH TIE TRACK BTW STA Y=902/1022 AT AFT CARGO COMPARTMENT AREA WAS REWORKED AND IS OUT OF LIMITS. SUMMARY OF NRC 00683: CORROSION LEVEL 2. LH TIE TRACK 
- [SDR DALA2023112209652](https://openairdocs.org/sdr/DALA2023112209652), Nov 21, 2023: UNKNOWN. UNKNOWN. CRACKS ON CORNER FWD ON SCUFF PLATE AT AFT CARGO. SUMMARY OF NRC 00002: SCUFF PLATE AT AFT CARGO WAS REPAIRED PER ER/A 542149-14TR REV B. SECTION I, PERMAMENT R
- [SDR DALA2023112109572](https://openairdocs.org/sdr/DALA2023112109572), Nov 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=946 AND BTW LONG 29R/28L AT AFT CARGO COMPARTMENT, WAS FOUND TO BE OUT OF LIMITS. SUMMARY OF NRC 00636: CORROSION LEVEL 2. FRAME C
- [SDR DALA2023112009520](https://openairdocs.org/sdr/DALA2023112009520), Nov 17, 2023: UNKNOWN. UNKNOWN. CRACK ON UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT IN REF TO NRC 00651. SUMMARY OF NRC 00663: UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLID
- [SDR DALA2023111509407](https://openairdocs.org/sdr/DALA2023111509407), Nov 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB BTW STA Y=954/994 AND BTW LONG=28R/29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: CORROSION LEVEL 2. WEB BTW STA Y=954/994 AND BTW LONG=28
- [SDR DALA2023111409351](https://openairdocs.org/sdr/DALA2023111409351), Nov 13, 2023: UNKNOWN. UNKNOWN. CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-0
- [SDR DALA2023111409349](https://openairdocs.org/sdr/DALA2023111409349), Nov 13, 2023: UNKNOWN. UNKNOWN. CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY. SUMMARY OF NRC 00660: CRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY WAS REPAIRED PER B717-200 SRM 53-00-0
- [SDR DALA2023111309303](https://openairdocs.org/sdr/DALA2023111309303), Nov 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO STA Y 986 C2. SUMMARY OF NRC 00040: CORROSION LEVEL 2. DOOR JAMB AFT CARGO COMPARTMENT STA Y 960 TO ST
- [SDR DALA2023110709161](https://openairdocs.org/sdr/DALA2023110709161), Nov 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON (Y CHORD) FRAME OF BULKHEAD STA Y=1053 AND BTW LONG 28L/28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00229: CORROSION LEVEL 2. (Y CHORD) FRAME OF B
- [SDR DALA2023110609114](https://openairdocs.org/sdr/DALA2023110609114), Nov 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON AFT PRESSURE BULKHEAD SKIN LOWER AREA STA Y=1053 AND BTW LONGERON 27R/27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00428: CORROSION LEVEL 2. AFT PR
- [SDR DALA2023110409089](https://openairdocs.org/sdr/DALA2023110409089), Nov 3, 2023: UNKNOWN. UNKNOWN. CRACK ON LOWER SURFACE OF CUSP WEB STA Y 217 TO STA Y237 AND X=56 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA Y 217 TO STA Y237 AND X=56 WAS REPAIRED PER B717-2
- [SDR DALA2023110409088](https://openairdocs.org/sdr/DALA2023110409088), Nov 3, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX. SUMMARY OF NRC 00374: CUSP WEB BTW STA 651 TO STA 661 AND X=56 AT CPAX WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2023110309045](https://openairdocs.org/sdr/DALA2023110309045), Nov 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA Y 148 TO STA Y 200 AND X=7 AND STA Y 162 TO STA Y 195 AND X=56 AT PASSENGER CABIN. IN REF NRC 0395. W1. SUMMARY OF NRC 00559: CO
- [SDR DALA2023110309044](https://openairdocs.org/sdr/DALA2023110309044), Nov 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEBS BTW ON STA Y=470, Y=493, AND Y=526 X=-56 AT PAX CABIN. SUMMARY OF NRC 00566: CORROSION LEVEL 2. RH CUSP WEBS BTW ON STA Y=470, Y=493, 
- [SDR DALA2023110309043](https://openairdocs.org/sdr/DALA2023110309043), Nov 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER CABIN. W1. SUMMARY OF NRC 00521: CORROSION LEVEL 2. FLOOR SUPPORT STA 185 TO 194 X=54 AT PASSENGER C
- [SDR DALA2023110108976](https://openairdocs.org/sdr/DALA2023110108976), Oct 31, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT CPAX (W1). SUMMARY OF NRC 00396: CORROSION LEVEL 2. WEB STA Y 185 TO STA Y 200 BTW X=49 TO X=56 AT C
- [SDR DALA2023103108932](https://openairdocs.org/sdr/DALA2023103108932), Oct 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT BTW STA Y 160 TO STA Y 200 AND -X44 AT PASSENGER CABIN IN REF TO NRC 00392. SUMMARY OF NRC 00477: CORROSION LEVEL 2. NEW FLOOR SUPPOR
- [SDR DALA2023103108931](https://openairdocs.org/sdr/DALA2023103108931), Oct 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH OUTBD SEAT TRACK REPAIR PLUG BTW STA 984 TO 988 PAX CABIN. SUMMARY OF NRC 00638: CORROSION LEVEL 1. SEAT TRACK REPAIR PLUG WAS REPLACED PER B717
- [SDR DALA2023103008877](https://openairdocs.org/sdr/DALA2023103008877), Oct 27, 2023: UNKNOWN. UNKNOWN. PUNCTURE ON DIAPHGRAM STA Y 155 X=7 AT PAX CABIN IN REF NRC 0395. W1. SUMMARY OF NRC 00561: DIAPHGRAM STA Y 155 X=7 AT PAX CABIN WAS REPAIRED PER B717 SRM 51-70
- [SDR DALA2020032001944](https://openairdocs.org/sdr/DALA2020032001944), Mar 20, 2020: POWER SUPPLY. DEFECTIVE. THE AFT EXIT LIGHT IS MALFUNCTIONING BLINKING. MAINTENANCE REPLACED THE AFT POWER SUPPLY PER B717 AMM 33-51. OPERATION IS NOW NORMAL. (LP #7217374
- [SDR DALA2020011700374](https://openairdocs.org/sdr/DALA2020011700374), Jan 16, 2020: BATTERY. DISCHARGED. THE AFT EMERGENCY EXIT SIGN, CAPTAINS SIDE, IS INOPERATIVE. MAINTENANCE FOUND THAT ALL OF THE ASSOCIATED LIGHTS WITH EMERGENCY POWER SUPPLY B5-260 WERE FLASHING
- [SDR DALA2019051302990](https://openairdocs.org/sdr/DALA2019051302990), May 10, 2019: BATTERY. DISCHARGED. THE AFT EXIT AND EMERGENCY LIGHTS IN THE CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGED IT AT B-5260. LIGHTS NOW CHECK NORMAL PER AMM 33-
- [SDR DALA2019020400714](https://openairdocs.org/sdr/DALA2019020400714), Feb 1, 2019: BATTERY PACK. INOPERATIVE. THE TAIL CONE EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE CHARGER PER B717 AMM 33-51. CHECK WAS GOOD. (LP #3790932)
- [SDR DALA2018111986673](https://openairdocs.org/sdr/DALA2018111986673), Nov 17, 2018: BATTERY PACK. INOPERATIVE. THE CAT WALK IN THE TAIL CONE LOWER EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN REAR OF AIRCRAFT AND THE CAT WALK EMERGEN
- [SDR DALA2018081305059](https://openairdocs.org/sdr/DALA2018081305059), Aug 8, 2018: SKIN. CORRODED. SURFACE CORROSION FOUND AT THE LT UPPER WING SKIN, STRINGER 5 LWS 343 TO 348.5. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01, ALLOWABLE DAMAGE 1.
- [SDR DALA2018080704894](https://openairdocs.org/sdr/DALA2018080704894), Aug 6, 2018: FRAME. CRACKED. CRACK INDICATION GREATER THAN 0.125 INCH AT THE BS 696 FRAME TAB UPPER RADIUS. REPLACED THE FRAME IAW AMDS 5310-01436-03B.
- [SDR DALA2018080604893](https://openairdocs.org/sdr/DALA2018080604893), Aug 4, 2018: SLIDE. LOOSE. TAILCONE SLIDE PACK WAS LOOSE AND UNRAVELED. INSTALLED A NEW TAILCONE SLIDE IAW AMM 25-61-02, AND AMDS CARD 5352-4002.
- [SDR DALA2018032601904](https://openairdocs.org/sdr/DALA2018032601904), Mar 25, 2018: BATTERY PACK. INOPERATIVE. EMERGENCY CEILING LIGHTS ARE INOPERATIVE BETWEEN SEAT ROWS 1 AND 13. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-03. EMERGENCY LIGHT OPS NORMAL.
- [SDR DALA2016082506196](https://openairdocs.org/sdr/DALA2016082506196), Aug 24, 2016: DOOR FRAME. CRACKED. RIGHT FORWARD GALLEY SERVICE DOOR, LOWER FORWARD CORNER, LOWER HORIZONTAL FRAME CRACKED. REPLACED GALLEY SERVICE DOOR LOWER HORIZONTAL FRAME IAW SRM 51-41-02, 5
- [SDR DALA2017010500109](https://openairdocs.org/sdr/DALA2017010500109), Aug 23, 2016: SEAL DEPRESSOR. DAMAGED. FOUND AFT LOWER SEAL DEPRESSOR TO BE DAMAGED. COMPLIED WITH PRI 549608-14, AND ER/A 549608-14. BY FABRICATING PROTECTING & INSTALLATION OF AFT SEAL DEPRESSOR ON
- [SDR DALA2016110208149](https://openairdocs.org/sdr/DALA2016110208149), Aug 23, 2016: SKIN. CORRODED. SKIN CORRODED AFT OF BS 1002 ABOVE STRINGER 26. BLENDED AREA IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER/A 54713-14 REV O.
- [SDR DALA2016082406194](https://openairdocs.org/sdr/DALA2016082406194), Aug 23, 2016: DOOR FRAME. CRACKED. AFT CARGO INTERNAL FUSELAGE CUT OUT, LOWER DOOR JAMB PAN HAS NUMEROUS AREAS OF CORROSION THAT IS AROUND THE AFT CAM LATCH FITTING AND LOWER AFT STOP ASSY TO THE
- [SDR DALA2016082306153](https://openairdocs.org/sdr/DALA2016082306153), Aug 22, 2016: SKIN. CRACKED. FUSELAGE SKIN CRACKED BS 1076 STRINGER 14R. REPAIRED THE SKIN IAW ER/A 547505-14.
- [SDR DALA2016082306152](https://openairdocs.org/sdr/DALA2016082306152), Aug 22, 2016: INTERCOSTAL. CORRODED. FOUND INTERCOSTAL ABOVE LONGERON 28R, BS 1002-1022 TO BE CORRODED. REPLACED THE INTERCOSTAL IAW SRM 51-41-02 ORIGINAL, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-0
- [SDR DALA2016082306154](https://openairdocs.org/sdr/DALA2016082306154), Aug 20, 2016: SUPPORT ANGLE. CRACKED. SUPPORT ANGLE IS CRACKED INSIDE L1 DOOR FWD SIDE AT UPPER STOP. REPLACED SUPPORT ANGLE IAW SRM 51-41-02 PG 40 PARA B, 51-41-02 PG 1 PARA 4, AND 51-41-05 PG 17 P

All 160: https://openairdocs.org/aircraft/N906AT/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/N906AT/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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