# N983AT: Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55052
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: August 29, 2024
- Expires: August 31, 2031
- Mode S code: ADB65B
- 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=983AT
- Page: https://openairdocs.org/aircraft/N983AT

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): 53 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

### 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

All 61: https://openairdocs.org/aircraft/N983AT/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 N983AT.

## FAA accident and incident reports

None matched to N983AT.

## Service difficulty reports (132, 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 DALA2026072004262](https://openairdocs.org/sdr/DALA2026072004262), Jul 17, 2026: BUSTLE. UNSECURE. SLIDE BUSTLE CAME LOOSE. RESECURED BUSTLE DUE TO SLIDE BEING LEFT IN THE ARM POSITION PER AMM 25-61. A/C OK FOR SVC. (8683063) AIRCRAFT GROUNDED.
- [SDR DALA2026060903440](https://openairdocs.org/sdr/DALA2026060903440), Jun 3, 2026: GIRT BAR. OUT OF ADJUST. L1 GIRT BAR DIFFICULT TO OPERATE. READJUSTED GIRT BAR RETAINER IAW AMM 25-61. OPS CHK OK. (8656666) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803226](https://openairdocs.org/sdr/DALA2026052803226), May 23, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 BTW. PERMANENT REPAIR AND PER PRI 634510-14 (1609411) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803219](https://openairdocs.org/sdr/DALA2026052803219), May 21, 2026: LONGERON. CRACKED. CRACKED LONGERON END 2LH , STA Y=1133 AT AFT ACCESSORIES COMPARMENT. REPAIRED PER B717-200 SRM 53-00- 05 (1605407) (AIRCRAFT GROUNDED)
- [SDR DALA2025112408547](https://openairdocs.org/sdr/DALA2025112408547), Nov 24, 2025: ANTI-SKID SYS. FAULTED. PERFORMED GO AROUND AND DECLARED AN EMERGENCY DUE TO LEFT ANTISKID CAUTION MESSAGE ON FINAL APPROACH. RECORDED BCU INTERNAL FAULT CODE 32417A. REPLACED BCU. OPS
- [SDR DALA2025090206468](https://openairdocs.org/sdr/DALA2025090206468), Aug 24, 2025: DOOR. NOT SEATED. AIRCRAFT RETURNED TO ATL DUE TO A CABIN INFLOW MSG. FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION AND REPLACED
- [SDR DALA2025081105986](https://openairdocs.org/sdr/DALA2025081105986), Aug 8, 2025: LATCH. NOT SEATED. SHIP 9560-ATB- AIRCRAFT RETURNED TO CLT DUE TO A CABIN INFLOW MSG. CORRECTIVE ACTION: FOUND AFT CARGO DOOR LATCHED BUT NOT SEATED, RESECURED DOOR AND PERFORMED 
- [SDR DALA2025080205795](https://openairdocs.org/sdr/DALA2025080205795), Jul 28, 2025: SKIN. GROUND DAMAGE. GSE TOW TRUCK CAME IN CONTACT OF LH, OUTBOARD UNDER WING. C/W ER/A 628016-14.
- [SDR DALA2024102910497](https://openairdocs.org/sdr/DALA2024102910497), Oct 26, 2024: DUCT. DISCONNECTED. SHIP 9560 -FUME/DE- DURING THE DECENT WHEN THE POWER WAS REDUCED TO IDLE, THE F/A REPORTED A "BURNT CARPET/CRAYON" SMELL IN THE CABIN. F/O NOTIFIED THE CAPT THA
- [SDR DALA2024103010525](https://openairdocs.org/sdr/DALA2024103010525), Oct 1, 2024: ACCESS DOOR. DETACHED. HORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS WERE DISCOVERED MISSING DURING POSTFLIGHT INSPECTION. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG R
- [SDR DALA2024052305457](https://openairdocs.org/sdr/DALA2024052305457), May 22, 2024: CONNECTOR. DAMAGED. DURING EMERGENCY LIGHTS CHECK, THE EXTERIOR EMERGENCY LIGHTS TURN ON WITH FLIGHT CABIN SWITCH IN ARM POSITION. SUMMARY OF NRC00627: CONTINUITY WAS PERFORMED PER
- [SDR DALA2024052105380](https://openairdocs.org/sdr/DALA2024052105380), May 20, 2024: SKIN. SCRATCHED. SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0. SUMMARY OF NRC 00610: SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0 WAS REPAIRED PER ER/A 618009-14 REV ORI
- [SDR DALA2024052105377](https://openairdocs.org/sdr/DALA2024052105377), May 20, 2024: BEAM. CRACKED. CRACK ON BEAM #1 AT AFT CARGO DOOR. SUMMARY OF NRC 00575: BEAM #1 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 617654-14 REV ORIGINAL. ASSOCIATED ER/A 14-617654 ADDE
- [SDR DALA2024052005346](https://openairdocs.org/sdr/DALA2024052005346), May 18, 2024: STRUCTURE. CORRODED. CORROSION ON HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00589: CORROSION LEVEL 2. HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER W
- [SDR DALA2024052005339](https://openairdocs.org/sdr/DALA2024052005339), May 17, 2024: STRUCTURE. CORRODED. CORROSION ON HOLES 27 AND 28, CENTER BOX RH, AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00581: HOLES 27 AND 28 CENTER BOX RH AT HORIZONTAL STABILIZER. WERE REPAIR
- [SDR DALA2024051705298](https://openairdocs.org/sdr/DALA2024051705298), May 17, 2024: DOUBLER. DAMAGED. MISSING MATERIAL IN ONE HOLE WAS FOUND AT INNER DOUBLER. SUMMARY OF NRC 00583: AREA WAS REPAIRED PER ER/A 617844-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. AS
- [SDR DALA2024051505222](https://openairdocs.org/sdr/DALA2024051505222), May 14, 2024: SKIN. CRACKED. DENT WITH CRACK (1 EA) 19" FROM OTBD EDGE AND 5.500" FROM LEADING EDGE AND DENT WITH DISBOND (1 EA) 34" FROM OUTBD EDGE AND 4" FROM TRALING EDGE ON LOWER SURFAC
- [SDR DALA2024051405176](https://openairdocs.org/sdr/DALA2024051405176), May 13, 2024: BOTTLE. LOW PRESSURE. PRESSURE WAS FOUND TO BE OUT OF RANGE ON THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR
- [SDR DALA2024051305134](https://openairdocs.org/sdr/DALA2024051305134), May 11, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00238: FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT 
- [SDR DALA2024051305133](https://openairdocs.org/sdr/DALA2024051305133), May 11, 2024: DOUBLER. CORRODED. CORROSION ON DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E. SUMMARY OF NRC 00186: CORROSION LEVEL 2. DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E WAS REPLACED PER B7
- [SDR DALA2024051305132](https://openairdocs.org/sdr/DALA2024051305132), May 10, 2024: DOOR FRAME. DAMAGED. BENT AND MISSING MATERIAL ON AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00008: AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAG
- [SDR DALA2024050905042](https://openairdocs.org/sdr/DALA2024050905042), May 8, 2024: SUPPORT FITTING. CORRODED. CORROSION ON R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS. ALSO CORROSION ON PANEL LOCATED BELOW FITTINGS. SUMMARY OF NRC 00426: CORROSION LEVEL 2. R1 DOOR SLIDE GIR
- [SDR DALA2024050805023](https://openairdocs.org/sdr/DALA2024050805023), May 8, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL STA Y=636, X=0 AT C1. SUMMARY OF NRC 00183: INTERCOSTAL STA Y=636, X=0 AT C1 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #03
- [SDR DALA2024050805021](https://openairdocs.org/sdr/DALA2024050805021), May 7, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215. SUMMARY OF NRC 00343: SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215 WERE REPAIRED PER B717-2
- [SDR DALA2024050604957](https://openairdocs.org/sdr/DALA2024050604957), May 4, 2024: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS IN REF NRC 298, CUSP WEB BTW X=-56 TO -60 AND Y=294-313 AND STA 420 TO 437, STA 674, STA 889 ALSO ON RH CUSP WEB BTW STA X=-44 TO -56 WI
- [SDR DALA2024050204888](https://openairdocs.org/sdr/DALA2024050204888), May 1, 2024: PAN. CRACKED. CRACK ON AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR. SUMMARY OF NRC 00247: AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDUR
- [SDR DALA2024050805018](https://openairdocs.org/sdr/DALA2024050805018), Apr 28, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00086: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABR
- [SDR DALA2024043004794](https://openairdocs.org/sdr/DALA2024043004794), Apr 27, 2024: FLOOR PANEL. CORRODED. CORROSION ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00411: CORROSION LEVEL 2. CORROSION WAS FOUND ON FLOOR PANEL 121TF, 121CF, AT FW
- [SDR DALA2024043004791](https://openairdocs.org/sdr/DALA2024043004791), Apr 26, 2024: CUSP WEB. CORRODED. CORROSION ON LOWER SURFACE OF LH CUSP WEB BTW STA 359-382. ALSO UPPER SURFACE BTW 660-664 PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00315: CORROSION LEVEL 2. CU
- [SDR DALA2024043004789](https://openairdocs.org/sdr/DALA2024043004789), Apr 25, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP WEB BTW STA Y 188\X=58, Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX. SUMMARY OF NRC 00650: CORROSION LEVEL 2. CUSP WEB BTW STA Y257/X=59, 
- [SDR DALA2024042604727](https://openairdocs.org/sdr/DALA2024042604727), Apr 25, 2024: PAN. CRACKED. CRACK ON FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR. SUMMARY OF NRC 00246: FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDUR
- [SDR DALA2023112109574](https://openairdocs.org/sdr/DALA2023112109574), Nov 16, 2023: UNKNOWN. UNKNOWN. UPON ARRIVAL IN BDL, GATE AGENT REPORTED DENT IN L1 DOOR, FORWARD LOWER CORNER NEAR THE EDGE. APPRX 5 TO 6 INCH LONG BY 1 INCH DEEP. *** CONTRACT MAINTENANCE EV
- [SDR DALA2022030101273](https://openairdocs.org/sdr/DALA2022030101273), Feb 26, 2022: NONE. NONE. AFTER CORROSION REMOVAL IN RH SIDE PLATE BTW STA Y=946-Y=956 AT AFT CARGO COMPARTMENT, CARGO SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS IS: 0.
- [SDR DALA2022030201325](https://openairdocs.org/sdr/DALA2022030201325), Feb 24, 2022: NONE. NONE. CORROSION ON INTERCOSTAL BTW Y=994 AND Y=1002, BTW L30 AND L29 RH (SM). SUMMARY OF NRC 00081: CORROSION LEVEL 2, INTERCOSTAL CORRECTIVE ACTION LOCATION PENDING.
- [SDR DALA2022022201131](https://openairdocs.org/sdr/DALA2022022201131), Feb 21, 2022: NONE. NONE. DUE TO THAT THE SAFETY PIN DOES NOT ALIGN WITH THE ESCAPE SLIDE L1, MCC REQUESTED TO REPLACE THE ESCAPE SLIDE. SUMMARY OF NRC 00154: FORWARD ENTRY EVACUATION SL
- [SDR DALA2022022201130](https://openairdocs.org/sdr/DALA2022022201130), Feb 21, 2022: NONE. NONE. CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00029: CORROSION LEVEL 2. BOTH LOWER SPLICE RETAINE
- [SDR DALA2022022201129](https://openairdocs.org/sdr/DALA2022022201129), Feb 21, 2022: NONE. NONE. CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). SUMMARY OF NRC 00028: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPA
- [SDR DALA2022021601012](https://openairdocs.org/sdr/DALA2022021601012), Feb 15, 2022: NONE. NONE. CORROSION ON BOTH LOWER SPLICE RETAINERS AT LOWER DOOR JAMB, FWD CARGO COMPARTMENT DOOR (C1). SUMMARY OF NRC 00030, CORROSION LEVEL 2: FWD LOWER SPLICE RETAINER
- [SDR DALA2019091105261](https://openairdocs.org/sdr/DALA2019091105261), Sep 10, 2019: COVER. DEPARTED. PART DEPARTED AIRCRAFT. ROUND ACCESS PANEL MISSING FROM LEFT WING INBOARD FLAP FAIRING COVER. INSTALLED ACCESS PANEL PER PS 900-7-3 NR 03. (LP #5156790)
- [SDR DALA2018080604879](https://openairdocs.org/sdr/DALA2018080604879), Jul 29, 2018: LENS. DAMAGED. EMERGENCY EXIT LENS WAS DAMAGED.
- [SDR DALA2018070204301](https://openairdocs.org/sdr/DALA2018070204301), Jun 23, 2018: DOOR. UNSECURE. GROUND AIR CONDITIONER DOOR FELL OFF. DEFERRED. WILL NEED A SUPPLEMENTAL SDR.
- [SDR DALA2017101107422](https://openairdocs.org/sdr/DALA2017101107422), Oct 11, 2017: BATTERY PACK. INOPERATIVE. BOTH AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPS CHECKED NORMAL IAW AMM 33-51.
- [SDR DALA2017041202997](https://openairdocs.org/sdr/DALA2017041202997), Apr 11, 2017: SKIN. CRACKED. CRACK ON SKIN BS 1022 BETWEEN LONGERONS 12 - 14R. REPAIRED IAW ETI-17-17-037 REV. 3, AND ER/A 556344-14 REV ORIGINAL.
- [SDR DALA2017041102992](https://openairdocs.org/sdr/DALA2017041102992), Apr 10, 2017: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BS 1022 BETWEEN LONGERONS 13 - 14L. THE DAMAGE WAS REPAIRED IAW ETI-17-17-038 REV 1, AND ER/A 556345-14 REV. ORIG.
- [SDR DALA2017041102991](https://openairdocs.org/sdr/DALA2017041102991), Apr 10, 2017: SKIN. CRACKED. CRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 14L. DAMAGED WAS REPAIRED IAW ETI-17-17-040 REV 1 AND ER/A 556347-14 REV. ORIG.
- [SDR DALA2017041102990](https://openairdocs.org/sdr/DALA2017041102990), Apr 10, 2017: SKIN. CRACKED. CRACK ON SKIN BS 1076 BETWEEN LONGERONS 12 - 14R. DAMAGED WAS REPAIRED IAW ETI-17-17-042 REV. 1 AND ER/A 556350-14 REV. ORIG.
- [SDR DALA2017041102989](https://openairdocs.org/sdr/DALA2017041102989), Apr 10, 2017: ATTACH ANGLE. CRACKED. CRACKED LONGERON ATTACH ANGLE ON AFT LAVATORY SUPPORT BULKHEAD BS 1022, LONGERON 7L. DAMAGE WAS REPAIRED IAW ETI-17-17-045 REV. 1, AND ER/A 556351-14 REV. ORIG.
- [SDR DALA2017040702810](https://openairdocs.org/sdr/DALA2017040702810), Apr 6, 2017: SKIN. DAMAGED. SEVERAL ELONGATED HOLES ON VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. REPAIRED IAW SRM 55-30-01-2R-7, 51-41-01, AND 51-41-05.
- [SDR DALA2017040602763](https://openairdocs.org/sdr/DALA2017040602763), Apr 5, 2017: CARGO TRACK. CORRODED. CORROSION ON THE RIGHT CARGO TRACK BETWEEN BS 994 - 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACEDIAW SRM 51-41-01, AND 51-40-08.
- [SDR DALA2017040602762](https://openairdocs.org/sdr/DALA2017040602762), Apr 5, 2017: BEAM. CRACKED. CRACKED BEAM NR 3, BS 160 BETWEEN UPPER & LOWER HINGE YOKE, FORWARD RIGHT GALLEY SERVICE DOOR STRUCTURE. THE BEAM WAS REPAIRED IAW SRM 52-00-00 2R.

All 132: https://openairdocs.org/aircraft/N983AT/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/N983AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md

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