# N948AT: 1999 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: 55011
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 21, 1999
- Certificate issued: January 2, 2020
- Expires: January 31, 2030
- Mode S code: AD2AF2
- 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=948AT
- Page: https://openairdocs.org/aircraft/N948AT

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/N948AT/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 N948AT.

## FAA accident and incident reports

None matched to N948AT.

## Service difficulty reports (269, 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 DALA2026063003868](https://openairdocs.org/sdr/DALA2026063003868), Jun 27, 2026: LIGHT. DETACHED. LIGHTING OVER EXIT ROW 18-21 LEFT SIDE OF ACFT HANGING LOW. SECURED CABIN LIGHT COVER AS REQUIRED IAW AMM 33-51. (8906374) (AIRCRAFT GROUNDED).
- [SDR DALA2026061003518](https://openairdocs.org/sdr/DALA2026061003518), Jun 9, 2026: LAMP. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT 24C INOP. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 24C PER B717 AMM 33-51. OPS CHK NML. OK FOR SVC. (LP 868086 - AIRCRAFT WAS GROUND
- [SDR DALA2026060903439](https://openairdocs.org/sdr/DALA2026060903439), Jun 3, 2026: SLIDING WINDOW. OUT OF RIG. ATB- PERFORMED AN AIR TURN BACK DUE TO THE CAPTAIN'S SLIDING WINDOW PARTIALLY OPENED DURING TAKEOFF. MAINTENANCE ADJUSTED AND RIGGED THE CAPTAINS CLEARVIEW WIND
- [SDR DALA2026040802227](https://openairdocs.org/sdr/DALA2026040802227), Apr 4, 2026: APU. ODOR. CREW REPORTS ON TAXI IN APU START HAD FUEL FUMES THROUGHOUT CABIN. REPLACED APU. (1528181) (AIRCRAFT GROUNDED)
- [SDR DALA2026031701820](https://openairdocs.org/sdr/DALA2026031701820), Mar 13, 2026: PCDU. FAULTED. ABORTED TAKEOFF DUE TO A RIGHT GENERATOR OFF MESSAGE. MAINTENANCE REPLACED THE RIGHT PCDU AND RIGHT GENERATOR RELAY. ALL ENGINE RUNS AND RETURN TO SERVICE TESTS
- [SDR DALA2026021801129](https://openairdocs.org/sdr/DALA2026021801129), Feb 11, 2026: PSEU. FAILED. RECEIVED A PSEU FAIL MESSAGE WITH AN ABNORMAL SLAT EXTENSION INDICATION. MAINTENANCE REPLACED THE PSEU DUE TO AN INTERNAL FAILURE FAULT CODE AND PERFORMED ALL A
- [SDR DALA2025110708138](https://openairdocs.org/sdr/DALA2025110708138), Nov 3, 2025: PANEL. NOT REPORTED. FABRICATED PANEL STILL NEEDS LIGHT ASSY INSTALLED. INSTALLED AFT COMPARTMENT LT PER B717 AMM 33-51. OP CHECK NORMAL . OK FOR SVC. (7724261)
- [SDR DALA2025103107966](https://openairdocs.org/sdr/DALA2025103107966), Oct 27, 2025: NONE. NONE. MONITOR LOG FOR ER/A 619015-14AD REV A SECTION II. COMPLY WITH SECTION II OF ER/A 619015-14AD (1275112)
- [SDR DALA2025091606817](https://openairdocs.org/sdr/DALA2025091606817), Sep 10, 2025: FAIRING. DAMAGED. DAMAGE NOTED RUDDER FAIRING PANEL 370CR. ER/A 629084-14 CREATED TRACKING TEMPORARY REPAIR ACCOMPLISHMENT. (1191759)
- [SDR DALA2025091606816](https://openairdocs.org/sdr/DALA2025091606816), Sep 10, 2025: ACCESS PANEL. DAMAGED. ENGINEERING CREATES LOGPAGE TRACKING DAMAGE TO RUDDER ACCESS PANEL PER ER/A 628805-14. ER/A 628805-14 LOGPAGE CREATED TRACKING TEMPORARY REPAIR TO RUDDER ACCESS
- [SDR DALA2025090406563](https://openairdocs.org/sdr/DALA2025090406563), Aug 27, 2025: NONE. NONE. ER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL. ER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL ON OR BEFORE 24 MONTHS FROM 26-AUG-2025
- [SDR DALA2025090906669](https://openairdocs.org/sdr/DALA2025090906669), Aug 26, 2025: PULLEY BRACKET. DAMAGED. L/E CAVITY AFT OF LT #2 SLAT. REPLACED PULLEY BRACKET PER BOEING DWG 5920286 (1164395)
- [SDR DALA2025063004853](https://openairdocs.org/sdr/DALA2025063004853), Jun 19, 2025: NONE. NONE. SHIP 9508 TRACKING FOR DTE FOR 24 MONTHS FROM DATE OF REPAIR APPROVAL. CORRECTIVE ACTION: C/W ERA ERA 626897-14 REV ORIGINAL. (1033207)
- [SDR DALA2025050803560](https://openairdocs.org/sdr/DALA2025050803560), Apr 22, 2025: DOOR SILL. CORRODED. AFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. REPAIRED PER REF B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN CORROS
- [SDR DALA2025042303171](https://openairdocs.org/sdr/DALA2025042303171), Apr 22, 2025: DOOR SILL. CORRODED. AFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. MARKED. SUMMARY SEE NRC 001-0319:5231-2002/001 00174: REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDUR
- [SDR DALA2024062706578](https://openairdocs.org/sdr/DALA2024062706578), Jun 26, 2024: SKIN. CRACKED. AIRCRAFT 9508, WHILE ACCOMPLISHING HFEC INSPECTION PER WORK CARD 5530-01048-02 IN COMPLIANCE WITH FAA AD 2018-10-08, MTC FOUND THREE (3) FASTENER HOLES IN THE V
- [SDR DALA2024062606518](https://openairdocs.org/sdr/DALA2024062606518), Jun 26, 2024: SKIN. CRACKED. CRACK INDICATION NOTED WORKING STEP 12 OF CARD 5530-01048-02 (AD 2018-10-08) WHILE PERFORMING OPEN HOLE HFEC. RH STAB L/E CRACK INDICATION IN SKIN LAYER ONLY. C
- [SDR DALA2023111309310](https://openairdocs.org/sdr/DALA2023111309310), Nov 11, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT COVER IS MISSING AT 1R DOOR. MAINTENANCE INSTALLED A NEW EMERGENCY EXIT LIGHT COVER AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS NOW OK FOR SER
- [SDR DALA2023070405368](https://openairdocs.org/sdr/DALA2023070405368), Jul 3, 2023: UNKNOWN. UNKNOWN. PUNCTURES (2 EA) ON CTR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00172: CTR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 5
- [SDR DALA2023070305312](https://openairdocs.org/sdr/DALA2023070305312), Jul 3, 2023: UNKNOWN. UNKNOWN. PUNCTURES (4 EA) ON INBR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00033: INBR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM
- [SDR DALA2023070305311](https://openairdocs.org/sdr/DALA2023070305311), Jul 3, 2023: UNKNOWN. UNKNOWN. DENTS (2 EA) ON INBR FIXED GUIDE VANE LOWER SKIN AT RH WING. SUMMARY OF NRC 00178: DENTS (2 EA) WITH THE MEASUREMENTS OF: DENT1 "D DIAMETER=2.000 IN, X DEPTH=0.
- [SDR DALA2023070305304](https://openairdocs.org/sdr/DALA2023070305304), Jul 1, 2023: UNKNOWN. UNKNOWN. DISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE UPPER SKIN. SUMMARY OF NRC 00102: RH WING AFT MOVABLE VANE UPPER SKIN WAS REPAIRED PER B717-200 SRM 57-53
- [SDR DALA2023063005261](https://openairdocs.org/sdr/DALA2023063005261), Jun 29, 2023: UNKNOWN. UNKNOWN. DISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE LOWER SKIN. SUMMARY OF NRC 00103: REPAIR WAS PERFORMED ON RH WING AFT MOVABLE VANE LOWER SKIN PER B717-20
- [SDR DALA2023063005260](https://openairdocs.org/sdr/DALA2023063005260), Jun 29, 2023: UNKNOWN. UNKNOWN. DISBONDS (2 EA) WERE FOUND ON LH WING INBD FIXED VANE LOWER SKIN. SUMMARY OF NRC 00104: REPAIR WAS PERFORMED ON LH WING INBD FIXED VANE LOWER SKIN PER B717-200 
- [SDR DALA2023062805187](https://openairdocs.org/sdr/DALA2023062805187), Jun 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SIDE PLATE AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00122: CORROSION LEVEL 2. LOWER SECTION OF JAMB PAN WAS REPLACED PER B717-200 S
- [SDR DALA2023063005264](https://openairdocs.org/sdr/DALA2023063005264), Jun 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT WAS FOUND. SUMMARY OF NRC 00156: CORROSION LEVEL 2. FLOOR SUPPORT WAS FABRICATED PER DWG 993634-7 REV BW AND WAS REPLACED PER B717- 2
- [SDR DALA2023062805180](https://openairdocs.org/sdr/DALA2023062805180), Jun 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE ON AFT LOWER SEAL DEPRESSOR AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00124: CORROSION LEVEL 2. ANGLE ON AFT LOWER SEAL DEPRESSOR AT
- [SDR DALA2023051703948](https://openairdocs.org/sdr/DALA2023051703948), May 16, 2023: UNKNOWN. UNKNOWN. THE LEFT FIXED FOWARD POSITION LIGHT LENSE COVER AND ATTACHING HARDWARE WAS DISCOVERED MISSING. THE LEFT FWD POSITION LIGHT LENS WAS FORWRDED TO CDL 33-42-03. A
- [SDR DALA2022080205280](https://openairdocs.org/sdr/DALA2022080205280), Jul 28, 2022: LENS. MISSING. THE THRESHOLD LIGHT LENS WAS MISSING ABOVE 29C. MAINTENANCE INSTALLED THE STANDBY LIGHT LENS COVER IN THE AFT CABIN REF B717 AMM 33-52. (LP #9299354)
- [SDR DALA2022050603164](https://openairdocs.org/sdr/DALA2022050603164), May 5, 2022: BATTERY. INOPERATIVE. AFT UPPER OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-230 PER B717 AMM 33-51. (LP #8616540)
- [SDR DALA2021041902264](https://openairdocs.org/sdr/DALA2021041902264), Apr 19, 2021: BATTERY PACK. INOPERATIVE. THE COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT STA 175 ABOVE R1 DOOR PER B717 AMM 33-51. (LP #7
- [SDR DALA2021022501094](https://openairdocs.org/sdr/DALA2021022501094), Feb 22, 2021: LENS. MISSING. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 1C. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT COVER FOR THE FORWARD CABIN. OPERATIONAL CHECK WAS GOOD. (L
- [SDR DALA2020102003406](https://openairdocs.org/sdr/DALA2020102003406), Oct 20, 2020: STRUCTURE. DAMAGED. ON WALKAROUND FOUND DAMAGE ON FWD CARGO DOOR BOTTOM FWD CORNER. MAINTENANCE REMOVED FWD CARGO DOOR FROM A/C TO FACILITATE REPAIR, PER B717 AMM 52-31-01 020-001.
- [SDR DALA2020030501635](https://openairdocs.org/sdr/DALA2020030501635), Mar 1, 2020: PLATE. MISSING. #2 ENG, UPPER COWL, INBOARD SIDE, HAS PLATE MISSING . MAINTENANCE ACCOMPLISHED SECTION I TIME LIMITED REPAIR PER ER/A 585840-14 REV ORIGINAL. COMPLIED WITH THE 
- [SDR DALA2020022311344](https://openairdocs.org/sdr/DALA2020022311344), Feb 20, 2020: PLATE. MISSING. THE #2 ENG UPPER COWL HAS A PLATE MISSING ON THE INBOARD SIDE. MAINTENANCE ACCOMPLISHED A TIME LIMITED REPAIR, PER ER/A 547093-14MA AND DEFERRED THE PERMANENT R
- [SDR DALA2020013000697](https://openairdocs.org/sdr/DALA2020013000697), Jan 27, 2020: COVER. MISSING. THE EMERGENCY EXIT LIGHT IS MISSING THE COVER. MAINTENANCE REPLACED THE EXIT COVER PER B717 AMM 52-22. OK FOR SERVICE.
- [SDR DALA2020011300236](https://openairdocs.org/sdr/DALA2020011300236), Jan 11, 2020: BATTERY. DISCHARGED. THE LT AND RT OVERWING EXIT IDENTIFIER SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY/ POWER PACK IAW AMM 33-51. OPERATIONAL CHECKS ARE NORMAL.
- [SDR DALA2019112286839](https://openairdocs.org/sdr/DALA2019112286839), Nov 16, 2019: CONNECTOR. DAMAGED. DURING SERVICE CHECK MAINTENANCE FOUND THAT THE CEILING MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 24 LEFT IS INOPERATIVE. RELAMPED WAS NO HELP. NO POWER TO LIG
- [SDR DALA2019111806743](https://openairdocs.org/sdr/DALA2019111806743), Nov 16, 2019: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT IDENTIFIERS WERE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED POWER SUPPLY B5-119. OPERATION
- [SDR DALA2019071304237](https://openairdocs.org/sdr/DALA2019071304237), Jul 12, 2019: WINDOW FRAME. CRACKED. CRACK ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER. (CPIL). NRC 00528: REPAIR SECTION I WAS PERFORMED ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER P
- [SDR DALA2019071304236](https://openairdocs.org/sdr/DALA2019071304236), Jul 12, 2019: SKIN. CORRODED. SEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2
- [SDR DALA2019071304235](https://openairdocs.org/sdr/DALA2019071304235), Jul 12, 2019: SPLICE. CORRODED. CORROSION ON SPLICE BTW LONG 26L TO 26R AT STA Y=815 AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00421: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579
- [SDR DALA2019071304234](https://openairdocs.org/sdr/DALA2019071304234), Jul 12, 2019: WINDOW FRAME. CRACKED. CRACK ON FRAME OF CLEAR VIEW WINDOW LT, UPPER AFT CORNER. (CPIL). NRC 00527: CRACK WAS REPAIRED PER SRM 56-10-02-2R-1 REPAIR 1 FIG.201, PERFORM LEAK CHECK PRESS
- [SDR DALA2019071104149](https://openairdocs.org/sdr/DALA2019071104149), Jul 10, 2019: FRAME. CRACKED. INITIAL INSPECTION: CRACK ON FRAME STA 1225 CANT BTW 3/4 O CLOCK POSITION AT AFT FUSELAGE. SUMMARY: OF NRC 00412 AREA WAS REPAIRED PER ER/A 579525-14 REV. ORIGI
- [SDR DALA2019071004139](https://openairdocs.org/sdr/DALA2019071004139), Jul 9, 2019: HINGE. CRACKED. INITIAL INSPECTION: CRACK ON INBD FLAP FAIRING HINGE AT STA. XRS =137. 750 AT LT WING. (AI). INB FLAP HINGE FAIRING WAS REPLACED SERVICEABLE PN: 5912150-509 PER
- [SDR DALA2019070904113](https://openairdocs.org/sdr/DALA2019070904113), Jul 8, 2019: ACCESS PANEL. CORRODED. PART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATES NR 520DT AND 520GB. CORROSION LEVEL 2. FUEL ACCESS PLATES NR 520DT AND 520GB WERE REPLACED AND V
- [SDR DALA2019070904112](https://openairdocs.org/sdr/DALA2019070904112), Jul 8, 2019: SKIN. CRACKED. AWR IN REFERENCE MON 2071758 : A CRACK WAS FOUND ON DENT # 10 AT RT AFTER MOVABLE VANE LOWER SKIN (AD). SUMMARY OF THIS N.R.C. 00747": IN REFERENCE MON 2071758 
- [SDR DALA2019070804078](https://openairdocs.org/sdr/DALA2019070804078), Jul 7, 2019: RELEASE CABLE. BROKEN. INITIAL INSPECTION: BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM. BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE 
- [SDR DALA2019070804077](https://openairdocs.org/sdr/DALA2019070804077), Jul 7, 2019: ACCESS PANEL. CORRODED. PART RACKS: CORROCION ON COUNTERSINK AREA ON FUEL ACCESS PLATE NBR 620DT AND 620DB. CORROSION LEVEL 2. FUEL ACCESS PLATE NR 620DT AND 620DB WERE REPLACED PER SR
- [SDR DALA2019070804076](https://openairdocs.org/sdr/DALA2019070804076), Jul 7, 2019: ACCESS PANEL. DAMAGED. PART RACKS: ELONGATED HOLES ON FUEL ACCESS PLATES NBR 141AL AND 520CB. ACCESS PLATES NBR 141AL AND 520CB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015

All 269: https://openairdocs.org/aircraft/N948AT/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/N948AT/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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