# N938AT: 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 BR700-715A130](https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130) (registry code 54006)
- 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: 55098
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 18, 2006
- Certificate issued: August 28, 2024
- Expires: August 31, 2031
- Mode S code: AD0373
- 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=938AT
- Page: https://openairdocs.org/aircraft/N938AT

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 BR700-715A130)

- [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/N938AT/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 N938AT.

## 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 20060701017499I](https://openairdocs.org/incident/20060701017499I), Jul 1, 2006: Boeing 717200 (N938AT), Atlanta, GA. (-23) Airtran (trs) flight 263 from tpa-fnt diverted into Atlanta (atl) due to an incapacitated first officer. While in cruise first officer complained she had…

## Service difficulty reports (150, 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 DALA2026100705545](https://openairdocs.org/sdr/DALA2026100705545), Oct 6, 2026: FLAP. DAMAGED. FOUND DAMAGE ON LEFT TRAILING EDGE FLAP, INSTALLED PERMANENT REPAIR PER B717 SRM 57-00-01-02A. (9483579) (AIRCRAFT GROUNDED).
- [SDR DALA2026071404143](https://openairdocs.org/sdr/DALA2026071404143), Jul 13, 2026: DISPLAY. FAULTED. DIVERTED TO BWI DUE TO SYSTEM DISPLAY CONTROL PANEL FAULTS. REPLACED EFIS DISPLAY SELECT PANEL IAW AMM 31-62-01. OPS CHKD GOOD. (8290442) (AIRCRAFT GROUNDED)
- [SDR DALA2026070803992](https://openairdocs.org/sdr/DALA2026070803992), Jul 7, 2026: LAMP. INOPERATIVE. COCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-11. (8290423) (AIRCRAFT GROUNDED).
- [SDR DALA2026012200495](https://openairdocs.org/sdr/DALA2026012200495), Jan 20, 2026: UNKNOWN. VIBRATION. DIVERTED TO SYR DUE TO AIRFRAME VIBRATIONS IN FLIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION PER AMM. PERFORMED IDLE ENGINE RUN WITH BOTH VIBRATION INDICATIONS
- [SDR DALA2026012200494](https://openairdocs.org/sdr/DALA2026012200494), Jan 16, 2026: BATTERY PACK. INOPERATIVE. NUMEROUSE EMERGENCY CEILING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK B5-231 AND OPS CHECKED GOOD IAW BN717 AMM 33-21. (8406044)
- [SDR DALA2025111808426](https://openairdocs.org/sdr/DALA2025111808426), Nov 13, 2025: MODULE. INOPERATIVE. DIVERTED TO MSN DUE TO FUEL QUANTITY INOPERATIVE. REPLACED ELECTRONIC MODULE. OPS CHECK NORMAL.(1301584)
- [SDR DALA2025070805069](https://openairdocs.org/sdr/DALA2025070805069), Jul 7, 2025: VALVE. BINDING. SHIP 9561 -ATB- DUE TO CLT DUE TO SMOKE IN THE CABIN COMING FROM FWD GALLEY AREA. SMOKE DISSIPATED AND EMERGENCY WAS DECLARED. CORRECTIVE ACTION: FOUND BUFFER A
- [SDR DALA2025043003320](https://openairdocs.org/sdr/DALA2025043003320), Apr 29, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS (3 EA) LOCATED AT CEILING PANEL IN FRONT OF FWD LAVATORY, EXIT SIGN AT TOP OF COW 1 AND ABOVE THE SERVICE DOOR DOES NOT OPERATE. THE POWER ASSE
- [SDR DALA2025042403189](https://openairdocs.org/sdr/DALA2025042403189), Apr 22, 2025: SKIN. WORN. WEAR ON SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR. WORN SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR WAS REPA
- [SDR DALA2025041602959](https://openairdocs.org/sdr/DALA2025041602959), Apr 15, 2025: DOUBLER. CRACKED. CRACK FOUND ON INTERNAL DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00686: INTERNAL CAP DOUBLER AT STA Y=1178 CANT L
- [SDR DALA2025041202832](https://openairdocs.org/sdr/DALA2025041202832), Apr 12, 2025: LONGERON. CRACKED. CRACK WAS FOUND BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE. SUMMARY OF NRC 00660: CRACK BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE WAS REPAIRED PE
- [SDR DALA2025041202830](https://openairdocs.org/sdr/DALA2025041202830), Apr 11, 2025: ACCESS PANEL. CORRODED. CORROSION OUT OF LIMITS ON COUNTERSINKS OF ACCESS PANELS: 520CB (3 HOLES), 520DB (4 HOLES), 520FT (6 HOLES), 620GB (3 HOLES), 620FT (2 HOLES), AND 620DT (3 HOLE
- [SDR DALA2025040802704](https://openairdocs.org/sdr/DALA2025040802704), Apr 8, 2025: CARGO TRACK. CORRODED. DUE TO CORRISION REWORK, (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SIDE TIE TRACK BTW L27L TO L28L AND STA=900 LH TO STA=1022 LH AFT CARGO COMPARTMENT. WIT
- [SDR DALA2025040802702](https://openairdocs.org/sdr/DALA2025040802702), Apr 5, 2025: FRAME. CORRODED. CORROSION ON FRAME STA Y=870 L29L TO L29R. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.029IN THEREFORE AREA IS OUT OF LIMITS PER B717-200
- [SDR DALA2025040802700](https://openairdocs.org/sdr/DALA2025040802700), Apr 5, 2025: SKIN. CORRODED. CORROSION ON BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE (CENTER SECTION). (EHV). SUMMARY OF NRC 00383: CORROSION LEVEL 2. BARREL NUT HOL
- [SDR DALA2025040802698](https://openairdocs.org/sdr/DALA2025040802698), Apr 4, 2025: PAN. CORRODED. CORROSION AROUND DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R. SUMMARY OF NRC 00305: CORROSION LEVEL 2. DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/2
- [SDR DALA2025040402565](https://openairdocs.org/sdr/DALA2025040402565), Apr 3, 2025: FRAME. CRACKED. CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00149: CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO CO
- [SDR DALA2025040402564](https://openairdocs.org/sdr/DALA2025040402564), Apr 3, 2025: LONGERON. CORRODED. CORROSION OUT LIMITS, IN REFERENCE TO NRC 00163: CORROSION ON LONGERON BTW STA Y=956 TO STA Y=964 L30 AT AFT CARGO COMPARTMENT WITH ORIGINAL THICKNESS IS 0.125I
- [SDR DALA2025040302495](https://openairdocs.org/sdr/DALA2025040302495), Apr 2, 2025: ANGLE. CORRODED. CORROSION ON ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00300: CORROSION LEVEL 2. ANGLE OF AFT CA
- [SDR DALA2025040302493](https://openairdocs.org/sdr/DALA2025040302493), Apr 2, 2025: STRAP. CRACKED. CRACKED STRAP STA Y 1178 CANT UPPER CHORD, PROJECTION LONG 2 RH AT AFT ACCESORY COMPARTMENT. INITIAL INSPECTION: PERFORM DECAL CONDITION INSPECTION EVERY C-CHEC
- [SDR DALA2025033102352](https://openairdocs.org/sdr/DALA2025033102352), Mar 28, 2025: SKIN. CRACKED. CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00035: CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 62
- [SDR DALA2025033102350](https://openairdocs.org/sdr/DALA2025033102350), Mar 28, 2025: SKIN. CRACKED. CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L. SUMMARY OF NRC 00444: CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L WAS REPAIRED PER 
- [SDR DALA2025032402191](https://openairdocs.org/sdr/DALA2025032402191), Mar 23, 2025: SKIN. DENTED. DENT ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE. SUMMARY OF NRC 00554: AREA DAMAGE WAS REPAIRED ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VA
- [SDR DALA2025032402189](https://openairdocs.org/sdr/DALA2025032402189), Mar 22, 2025: PAN. CRACKED. CRACKED PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2. SUMMARY OF NRC 00096: PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2 WAS REPAIRED 
- [SDR DALA2025032402188](https://openairdocs.org/sdr/DALA2025032402188), Mar 22, 2025: BEAM. CRACKED. CRACK ON BEAM #8 AFT SIDE AT PASSENGER DOOR. SUMMARY OF NRC 00083: BEAM #8 AFT SIDE AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 14 PAR 6.
- [SDR DALA2025032402187](https://openairdocs.org/sdr/DALA2025032402187), Mar 22, 2025: PAN. CRACKED. A CRACK WAS FOUND ON THE #2 INNER PAN AT AFT EDGE OF THE FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00598: INNER PAN ON AFT EDGE BEAM #2 AT FWD CARGO COMPARTMENT
- [SDR DALA2025032402186](https://openairdocs.org/sdr/DALA2025032402186), Mar 22, 2025: DOOR FRAME. CRACKED. CRACK ON BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00290: BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10
- [SDR DALA2025032102134](https://openairdocs.org/sdr/DALA2025032102134), Mar 21, 2025: FRAME. CRACKED. CRACK OF 0.093 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #090-0004, STEP 
- [SDR DALA2025032102132](https://openairdocs.org/sdr/DALA2025032102132), Mar 20, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER. SUMMARY OF NRC 00338: CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PAS
- [SDR DALA2025032002096](https://openairdocs.org/sdr/DALA2025032002096), Mar 19, 2025: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN. SUMMARY OF NRC 00360: CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN WAS REPAIRED PER B717-200 53-
- [SDR DALA2025032002094](https://openairdocs.org/sdr/DALA2025032002094), Mar 19, 2025: CUSP WEB. DAMAGED. ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER. SUMMARY OF NRC 00339: ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER W
- [SDR DALA2025031902063](https://openairdocs.org/sdr/DALA2025031902063), Mar 18, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER. SUMMARY OF NRC 00330: CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER WAS REPAI
- [SDR DALA2025031702029](https://openairdocs.org/sdr/DALA2025031702029), Mar 16, 2025: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN. SUMMARY OF NRC 00361: FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07
- [SDR DALA2025031702025](https://openairdocs.org/sdr/DALA2025031702025), Mar 14, 2025: LONGERON. CRACKED. CRACK ON INTERNAL AREA OF LONGERON 7R, 8R, 5R, STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00363: LONGERON 8R, 5R, STA Y=1022 AT PASSENGER CABIN WERE REPAIRED
- [SDR DALA2025031702022](https://openairdocs.org/sdr/DALA2025031702022), Mar 14, 2025: SEAT TRACK. CORRODED. CORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00398: CORROSION LEVEL 2. CORROSION ON RH SEAT TRACK STA Y=236-238 -
- [SDR DALA2025031401969](https://openairdocs.org/sdr/DALA2025031401969), Mar 13, 2025: LONGERON. CRACKED. CRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00432: CRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN W
- [SDR DALA2024042604730](https://openairdocs.org/sdr/DALA2024042604730), Apr 24, 2024: COVER. MISSING. THE CABIN CEILING EMERGENCY STANDBY LIGHT LENS COVER IS MISSING AT SEAT ROW 3. MAINTENANCE FORWARDED IT TO NEF 33-21-02. CABIN LIGHT LENS MISSING SEAT ROW 3. (L
- [SDR DALA2024010500149](https://openairdocs.org/sdr/DALA2024010500149), Jan 5, 2024: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS FROM ROW 1 TO ROW 13 CEILING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT B5-227 PER B717 AMM 33-51. OPERATIO
- [SDR DALA2023102008641](https://openairdocs.org/sdr/DALA2023102008641), Oct 19, 2023: UNKNOWN. UNKNOWN. THE LOWER EMERGENCY LIGHTS ARE INOPERATIVE AT THE AFT EMERGENCY EXIT. MAINTENANCE REPLACED THE BATTERY (B5-119) PER B717 AMM 33-51-04. ALL EMERGENCY LIGHT OPERA
- [SDR DALA2023062305084](https://openairdocs.org/sdr/DALA2023062305084), Jun 22, 2023: UNKNOWN. UNKNOWN. ON A SERVICE CHECK, THE SIDE PAX DOOR EMERGENCY EXIT LIGHT AND SERVICE DOOR SIDE EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EME
- [SDR DALA2023052004046](https://openairdocs.org/sdr/DALA2023052004046), May 19, 2023: UNKNOWN. UNKNOWN. MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE CABIN AT STA 715-737R TO BE INOPERATIVE. THE EMERGENCY LIGHTS BATTERY SUPPLY (B5-230) WAS REPLACED. OPERATIONA
- [SDR DALA2022090405925](https://openairdocs.org/sdr/DALA2022090405925), Sep 4, 2022: NONE. NONE. AIRCRAFT 9561, EXIT LOCATOR SIGN FWD/AFT FACING DOES NOT ILLUMINATE. LIGHTED SIGN IS LOCATED ON CEILING OF CABIN BETWEEN OVER-WING EMERGENCY EXITS. CORECTIVE AC
- [SDR DALA2022041202525](https://openairdocs.org/sdr/DALA2022041202525), Apr 10, 2022: NONE. NONE. EMERGENCY LIGHTS AT LOWER AFT OVERWING DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOO
- [SDR DALA2022010300010](https://openairdocs.org/sdr/DALA2022010300010), Dec 31, 2021: NONE. NONE. HIDDEN DAMAGE DURING THE DOUBLER REMOVE PROCESS. WEB DAMAGE WAS FOUND ON LEFT HAND SIDE, LOCATED ON INTECECTION STA 674 AND STGR 18LH. SUMMARY OF NRC 00175: WEB
- [SDR DALA2021112407218](https://openairdocs.org/sdr/DALA2021112407218), Nov 24, 2021: NONE. NONE. THERE ARE MULTIPLE CABIN EMERGENCY ESCAPE LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 IAW B717 AMM 33-51. OPERATIONAL CHECK
- [SDR DALA2020111303714](https://openairdocs.org/sdr/DALA2020111303714), Nov 13, 2020: BATTERY PACK. INOPERATIVE. DURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT CEILING PANELS 11, 12, AND 13 WERE INOPERATIVE. THE BATTERY PACK, B5-231, WAS REPLACED, P
- [SDR DALA2020031301823](https://openairdocs.org/sdr/DALA2020031301823), Mar 13, 2020: PUMP. MALFUNCTIONED. ACCORDING TO THE AOS REPORT, EMERGENCY DECLARED - HYD R TEMP HI MESSAGE AFTER T/O. R&R RT ENG EDP PER B717 AMM 29-11. OPS AND LEAK CHK OK. ODI PAPERWORK C/W. PU
- [SDR 2020F00283](https://openairdocs.org/sdr/2020F00283), Jan 31, 2020: SKIN. DELAMINATED. NON ROUTINE CHECK, UPPER AND LOWER SKINS OF THE RT WING SPOILER WAS DELAMINATED.
- [SDR DALA2024012401104](https://openairdocs.org/sdr/DALA2024012401104), Jan 8, 2020: SKIN. DENTED. DENT INSPECTION RHS AFT MOVABLE VANE, UPPER SKIN - QTY 6. #5) APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. 5) DENT DIMENSIONS WIDTH 1.3" X DEPTH 0.024" APPROX 25" 
- [SDR DALA2019121807399](https://openairdocs.org/sdr/DALA2019121807399), Dec 17, 2019: SKIN. CORRODED. FUSELAGE SKIN CORRODED INTERNALLY AT CUTOUT FOR DRAIN MAST IN FLOOR OF E/E COMPARTMENT. EXTERNAL FILLET SEALER AROUND MAST SHOWS CORROSION PROTRUSION ALSO. NRC 

All 150: https://openairdocs.org/aircraft/N938AT/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/N938AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce Deutschland BR700-715A130 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130.md

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