# N939AT: 2006 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce Deutschland BR700-715B130](https://openairdocs.org/engine/rolls-royce-deutschland-br700-715b130) (registry code 54007)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E00061EN](https://openairdocs.org/tcds/E00061EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 55099
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 19, 2006
- Certificate issued: August 27, 2024
- Expires: August 31, 2031
- Mode S code: AD072A
- 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=939AT
- Page: https://openairdocs.org/aircraft/N939AT

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.

## ADs that may apply (OpenAirDocs): 64 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (Rolls-Royce Deutschland BR700-715B130)

- [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 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 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 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 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 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 2005-16-12](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

### 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 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

All 74: https://openairdocs.org/aircraft/N939AT/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 N939AT.

## FAA accident and incident reports

None matched to N939AT.

## Service difficulty reports (175, 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 DALA2026100505509](https://openairdocs.org/sdr/DALA2026100505509), Oct 1, 2026: STRAP. MISSING. AFT TAILCONE EXIT DOOR STRAP MISSING. INSTALLED PER AIPC 25-29. (1842937) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026082404787](https://openairdocs.org/sdr/DALA2026082404787), Aug 23, 2026: TRANSMITTER. FAULTED. ATO- APPROX 60KTS DUE TO FLAPS AURAL WARNING. REPLACED RT FLAP POSITION TRANSMITTER PER AMM 27-54-01. OPS CHECK GOOD. (8316370) (AIRCRAFT GROUNDED).
- [SDR DALA2026050502826](https://openairdocs.org/sdr/DALA2026050502826), Apr 29, 2026: UNKNOWN. ODOR. DE DIV- CREW REPORTED AN ELECTRICAL ODOR INBOUND TO DTW AND ELECTED TO DIVERT TO CLE. C/W WORKCARD # 0550-9001-B717 NO ODORS FOUND. (6546129) (AIRCRAFT GROUNDED
- [SDR DALA2026042102510](https://openairdocs.org/sdr/DALA2026042102510), Apr 17, 2026: SKIN. CRACKED. CRACK ON SKIN ON STA Y=1133 BTW LONG 3L AND LONG AND LONG 4L AT AFT UPPER FUSELAGE. REPAIRED PER PRI 633822-14 (1548951) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102504](https://openairdocs.org/sdr/DALA2026042102504), Apr 15, 2026: ANGLE. CRACKED. CRACK ON ANGLE STA Y=1178 CANT BTW LONG 16RH -17RH. REPAIRED PER PRI 633437-14 (1545871) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402364](https://openairdocs.org/sdr/DALA2026041402364), Apr 12, 2026: SKIN. CRACKED. CRACKS ON SKIN ON STA Y=1087 BTW LONG13L AND LONG14L ALSO BTW LONG 13R AND LONG14R AT AFT UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ERA 633469-14 (1540973
- [SDR DALA2026041402369](https://openairdocs.org/sdr/DALA2026041402369), Apr 8, 2026: SKIN. CRACKED. FUSELAGE SKIN, BS 1087, L13R - 14R CRACKED. ASSOCIATED ER/A 00-633468 (1536411) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402370](https://openairdocs.org/sdr/DALA2026041402370), Apr 6, 2026: SKIN. CRACKED. FUSELAGE, SKIN, BS 1087, L13 - 14L CRACKED. ACCOMPLISH ER/A 633469-14 (1534688) (AIRCRAFT GROUNDED)
- [SDR DALA2026040802226](https://openairdocs.org/sdr/DALA2026040802226), Apr 3, 2026: VANE. CRACKED. 7.0IN FROM T.E AND 20IN FROM O.B OF 1.5IN LENGTH X2.0IN WIDTH OF THE AFT MOVABLE FLAP VANE. AFT MOVABLE FLAP VANE IT IS OUT OF BOUNDS BECAUSE IT DOES NOT COMPLY
- [SDR DALA2026031301751](https://openairdocs.org/sdr/DALA2026031301751), Mar 2, 2026: SPAR CAP. DAMAGED. SHIP 9562 ERA 614420-14AD REV A ISSUED FOR REPAIRS TO RH WING REAR LOWER SPAR CAP AND WING SKIN, ACCOMPLISH ERA 614420-14AD (1476521).
- [SDR DALA2025122909450](https://openairdocs.org/sdr/DALA2025122909450), Dec 22, 2025: BATTERY PACK. INOPERATIVE. DURING SVC CHECK FOUND LT AFT OVERWING EXIT IDENTIFIER INOP, RT AFT OVERWING EXIT IDENTIFIER INOP, AND AFT CABIN EXIT IDENTIFIER INOP. AFT CABIN EXIT IDENTIFIER
- [SDR DALA2025051203683](https://openairdocs.org/sdr/DALA2025051203683), May 5, 2025: WINDOW. CRACKED. DURING CRUISE, THE CA NOTED AN ARC AND THE WINDSHIELD DEVELOPED A CRACK. MAINTENANCE REPLACED THE CAPT FWD WINDSHIELD REF B717 AMM 56-11. ALL CHECKS WERE GOOD. 
- [SDR DALA2025041502920](https://openairdocs.org/sdr/DALA2025041502920), Apr 10, 2025: DIMMER. FAILED. SHIP 9562 -ATB/FUME/DE- THE CREW PERFORMED AN AIR TURN BACK TO PNS DUE TO STRONG ELECTRICAL FUMES IN THE COCKPIT WITH LIGHTING CONTROL ISSUES. AN EMERGENCY WAS 
- [SDR DALA2024120311392](https://openairdocs.org/sdr/DALA2024120311392), Nov 21, 2024: BULKHEAD. ABNORMAL. -AD- ACCOMPLISH ER/A 558098-14AD REV A SEC II. ACCOMPLISH ER/A 558098-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATE
- [SDR DALA2024050504925](https://openairdocs.org/sdr/DALA2024050504925), Apr 23, 2024: ACCESS PANEL. MISSING. SHIP 9562 -PDA- DURING PREFLIGHT INSPECTION FOUND MISSING ACCESS PANEL ON LEFT HAND OUTER PORTION OF WING NEAR NAVIGATION LIGHT. PERFORMED TEMP REPAIR IAW SECTI
- [SDR DALA2024032503739](https://openairdocs.org/sdr/DALA2024032503739), Mar 23, 2024: POWER SUPPLY. INOPERATIVE. DURING CHECK OF THE EXTERIOR LIGHTS, THE LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPL
- [SDR DALA2024032103576](https://openairdocs.org/sdr/DALA2024032103576), Mar 16, 2024: SPAR. CRACKED. CRACK ON REAR SPAR APPROX XW151 AT RH WING. SUMMARY OF NRC 00175: REAR SPAR, LOWER CAP APPROX XW151 AT RH WING WAS REPAIRED PER ERA 614420-14AD REV ORIGINAL AND
- [SDR DALA2024030603060](https://openairdocs.org/sdr/DALA2024030603060), Mar 5, 2024: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL ON INNER STRUCTURE STA Y=184 BTW BEAMS #4 & 5 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00107: INTERCOSTAL ON INNER STRUCTURE STA Y=184 BTW BEAMS
- [SDR DALA2024020301510](https://openairdocs.org/sdr/DALA2024020301510), Feb 2, 2024: FRAME. CRACKED. CRACK ON MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX. SUMMARY OF NRC 00355: MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX WAS REPAIRED PER ERA 614511-14 REV ORI
- [SDR DALA2024020101445](https://openairdocs.org/sdr/DALA2024020101445), Jan 31, 2024: CUSP WEB. CRACKED. CRACK ON CUSP MEMBRANE ON STA 655 WAS FOUND IN REFERENCE TO CARD 5310-01436-03B STEP 3. SUMMARY OF NRC 00568: CUSP MEMBRANE ON STA 655 WAS REPAIRED PER B717-200
- [SDR DALA2024020101444](https://openairdocs.org/sdr/DALA2024020101444), Jan 31, 2024: FRAME. CRACKED. A.D. CRACK OF 0.500 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF. CARD 5310-01436-04B). SUMMARY OF NRC 00253: FRAME TAB OVERWING 
- [SDR DALA2024012901230](https://openairdocs.org/sdr/DALA2024012901230), Jan 28, 2024: FRAME. CRACKED. CRACK ON UNDER THE FASTENER OF THE FRAME TAB OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-04C). A.D. A.A. SUMMARY OF NRC 00306: OVERWING FRAME AT STA
- [SDR DALA2024012200903](https://openairdocs.org/sdr/DALA2024012200903), Jan 19, 2024: FLOOR SUPPORT. CORRODED. CORROSION AT FLOOR SUPPORT ON X=56 BTW STA Y=160/200 PAX CABIN. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORT ON X=56 BTW STA Y=160 TO Y=200 WAS FABRIC
- [SDR DALA2024011500578](https://openairdocs.org/sdr/DALA2024011500578), Jan 15, 2024: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS COORDINATE X=-56, BTW STA Y=200 TO 210, COORDINATE X=-44 BTW STA Y=160 TO 200 AND COORDINATE X=0 TO COORDINATE X=-44, STA Y=200. SUM
- [SDR DALA2024011500574](https://openairdocs.org/sdr/DALA2024011500574), Jan 13, 2024: UNKNOWN. UNKNOWN. PUNCTURES ON DIAPHRAGM UNDER FLOOR SUPPORT STA 180-192 X=54 AT PAX CABIN IN REF NRC 455. SUMMARY OF NRC 00659: DIAPHRAGM UNDER FLOOR SUPPORT STA 180-192 X=54 WA
- [SDR DALA2024010800320](https://openairdocs.org/sdr/DALA2024010800320), Jan 5, 2024: UNKNOWN. UNKNOWN. CRACK ON LONGERON 6L STA Y1020 AT PASSENGER CABIN. SUMMARY OF NRC 00419: LONGERON SECTION 6 LH FROM STA Y=1012 TO STA Y=1053 WAS REPAIRED PER B717-200 SRM 53-00
- [SDR DALA2024010200012](https://openairdocs.org/sdr/DALA2024010200012), Dec 31, 2023: UNKNOWN. UNKNOWN. CORROSION AT FLOOR SUPPORTS ON X=-7 BTW STA.Y=158/200 PAX CABIN. SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR SUPPORT ON X=-7 BTW STA.Y=158/200 WAS FABRICATED
- [SDR DALA2023122410543](https://openairdocs.org/sdr/DALA2023122410543), Dec 23, 2023: UNKNOWN. UNKNOWN. AFT CABIN FLOOR INTERCOSTAL CRACKED 3 PLACES AT UPPER FLANGE NEAR NUT PLATE HOLES, STATION 1002-1037 BL0. SUMMARY OF NRC 00641: FLOOR INTERCOSTAL STA 1002-1037 
- [SDR DALA2023100608226](https://openairdocs.org/sdr/DALA2023100608226), Oct 6, 2023: UNKNOWN. UNKNOWN. DURING THE SERVICE CHECK, MAINTENANCE FOUND THE TAIL COMPARTMENT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY ASSEMBLY, B5-260, IAW B717
- [SDR DALA2023092507868](https://openairdocs.org/sdr/DALA2023092507868), Sep 22, 2023: UNKNOWN. UNKNOWN. THE DOOR R1 EMERGENCY EXIT TOP SIGN IS INOPERATIVE. MAINTENANCE FOUND A BROKEN PIN IN THE IN-LINE JUNCTION. REPINNED AND REPLACED THE IN-LINE JUNCTION REF BOEIN
- [SDR DALA2022090906000](https://openairdocs.org/sdr/DALA2022090906000), Sep 8, 2022: NONE. NONE. FOUND THAT THE AFT OVERWING EXIT MARKER LIGHTS WERE INOPERATIVE ON THE SERVICE CHECK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION B5-119 P
- [SDR DALA2021112207152](https://openairdocs.org/sdr/DALA2021112207152), Nov 20, 2021: NONE. NONE. CORROSION ON PANEL FROM STA Y=168 TO Y=200 BTW X=-53 AND X=-58 AT W1 AREA. (CPCP CARD 2021-2001). SUMMARY OF NRC 00200: CORROSION LEVEL 2, FLOOR PANEL FROM STA 
- [SDR DALA2021112207151](https://openairdocs.org/sdr/DALA2021112207151), Nov 19, 2021: NONE. NONE. CORROSION ON CLIPS FRAME STA=907 AND STA=909 BTW STRINGERS 29LH TO 29RH (SM). SUMMARY OF NRC 00121: CORROSION LEVEL 2, CLIP FRAME STA=907 AND STA=909 BTW STRING
- [SDR DALA2021112207150](https://openairdocs.org/sdr/DALA2021112207150), Nov 19, 2021: NONE. NONE. CORROSION ON MEMBRANE FROM STA Y=184 TO Y=200 BTW X=-50 AND X=-53 AT W1 AREA. (CPCP CARD 2021-2001). SUMMARY OF NRC 00199: CORROSION LEVEL 2, REPAIR WAS PERFORM
- [SDR DALA2021112207149](https://openairdocs.org/sdr/DALA2021112207149), Nov 19, 2021: NONE. NONE. CORROSION ON STRINGER 30 BTW STA=890 AND STA=895 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00119: CORROSION LEVEL 2, STRINGER 30 BTW STA=890 AND STA=895 AFT CA
- [SDR DALA2021111907132](https://openairdocs.org/sdr/DALA2021111907132), Nov 18, 2021: NONE. NONE. CORROSION ON AFT CARGO DOOR JAMB (CCT). SUMMRY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB WAS REPAIRED (PERMANENT REPAIR) PER B717 SRM 53-20-15-2R PROCEDURE 7. 
- [SDR DALA2021111707083](https://openairdocs.org/sdr/DALA2021111707083), Nov 16, 2021: NONE. NONE. CORROSION ON STRINGER 30 BTW STA=992 TO STA=995 AT AFT CARGO COMPARTMENT IN REF NRC 00124. SUMMARY OF NRC 00203: CORROSION LEVEL 2, PERMANENT REPAIR WAS PERFORM
- [SDR DALA2019040502210](https://openairdocs.org/sdr/DALA2019040502210), Apr 4, 2019: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT SIGN IS INOPERATIVE AT 20A. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. LOCATION PASS SEATS: 20A
- [SDR DALA2018082865292](https://openairdocs.org/sdr/DALA2018082865292), Aug 25, 2018: FINGER DOUBLER. DAMAGED. FINGER DOUBLER DAMAGED AT THE LAP SEAM LONGERON 26L, BS 446 - 484. CUT OUT THE DAMAGED FINGER DOUBLER DIM 30". INSTALLED A NEW FINGER DOUBLER IAW ER/A 596015-14
- [SDR DALA2018082855291](https://openairdocs.org/sdr/DALA2018082855291), Aug 24, 2018: FINGER DOUBLER. DAMAGED. FINGER DOUBLER WAS DAMAGED AT BS 475, LONGERON 26L. CUT OUT THE DAMAGED FINGER DOUBLER, DIM 45. INSTALLED NEW FINGER DOUBLER IAW ER/A 596015-14, REV ORIGINAL.
- [SDR DALA2018082855290](https://openairdocs.org/sdr/DALA2018082855290), Aug 24, 2018: LONGERON. BENT. LONGERON 26L WAS BENT BETWEEN BS 446 - 484. REPAIRED THE LONGERON IAW ER/A 596015-14, REV ORIGINAL.
- [SDR DALA2018082755264](https://openairdocs.org/sdr/DALA2018082755264), Aug 24, 2018: SKIN. DAMAGED. FUSELAGE SKIN BETWEEN BS 389 - 484, LONGERON 22L - 26L WAS DAMAGE. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 6.
- [SDR DALA2018082755263](https://openairdocs.org/sdr/DALA2018082755263), Aug 24, 2018: SKIN. DAMAGED. FUSELAGE SKIN WAS CRACKED AND CREASED BETWEEN BS 458 - 475, LONGERON 26L - 28L. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 6.
- [SDR DALA2018082755265](https://openairdocs.org/sdr/DALA2018082755265), Aug 23, 2018: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT SIGNS OVER THE LT & RT AFT OVERWING EXIT HATCHES WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED SATISFA
- [SDR DALA2018082745261](https://openairdocs.org/sdr/DALA2018082745261), Aug 23, 2018: FORMER. DAMAGED. FORMER, BS 465, BETWEEN LONGERONS 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.
- [SDR DALA2018082745260](https://openairdocs.org/sdr/DALA2018082745260), Aug 23, 2018: FORMER. DAMAGED. FORMER STA 465 BETWEEN LONGERONS 25L - 26L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.
- [SDR DALA2018082745259](https://openairdocs.org/sdr/DALA2018082745259), Aug 23, 2018: FRAME. DAMAGED. FRAME BS 427 BETWEEN LONGERONS 24L AND 26L WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-41-02, AND DRAWING 3912348, REV E.
- [SDR DALA2018082745258](https://openairdocs.org/sdr/DALA2018082745258), Aug 23, 2018: FORMER. DAMAGED. FORMER AT BS 427 BETWEEN LONGERONS 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.
- [SDR DALA2018082745257](https://openairdocs.org/sdr/DALA2018082745257), Aug 23, 2018: FORMER. DAMAGED. FORMER, BS 465, LONGERON 27L WAS DAMAGED. ACCOMPLISHED A FORMER REPAIR IAW SRM 53-00-06, REPAIR 2.
- [SDR DALA2018082835289](https://openairdocs.org/sdr/DALA2018082835289), Aug 22, 2018: FORMER. DAMAGED. DAMAGED FORMER AT BS 446, LONGERON 27L. ACCOMPLISHED A PERMANENT REPAIR TO THE FORMER IAW SRM 53-00-06, REPAIR 2, AND DRAWING 9912454, REV K.

All 175: https://openairdocs.org/aircraft/N939AT/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/N939AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce Deutschland BR700-715B130 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-715b130.md

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