# N919AT: 2001 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: 55084
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 19, 2001
- Certificate issued: April 1, 2025
- Expires: April 30, 2032
- Mode S code: ACB82C
- 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=919AT
- Page: https://openairdocs.org/aircraft/N919AT

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/N919AT/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 N919AT.

## FAA accident and incident reports

None matched to N919AT.

## Service difficulty reports (204, 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 DALA2026080304470](https://openairdocs.org/sdr/DALA2026080304470), Aug 1, 2026: SKIN. DENTED. CREW REPORTS DENT AFT OF L1 DOOR. REPAIRED PER SRM 53-01. (9085472) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026052903256](https://openairdocs.org/sdr/DALA2026052903256), May 24, 2026: LIGHT SYS. INOPERATIVE. ROW 19 L/R FOWARD LOWER EMERGENCY LIGHTS INOPERATIVE. DEFER PER MEL 33-51-01 A. (8663813) (AIRCRAFT GROUNDED)
- [SDR DALA2026012200493](https://openairdocs.org/sdr/DALA2026012200493), Jan 20, 2026: BATTERY PACK. FAULTED. EMERGENCY LIIGHTS ROW 20 INOP. R & R BATTERY PACK B5-230 LOCATION 726R. OPS TEST OK. (8393910)
- [SDR DALA2026011600375](https://openairdocs.org/sdr/DALA2026011600375), Jan 13, 2026: BATTERY PACK. INOPERATIVE. MULTIPULE EMERGANCY LIGHT OUT IN CABIN. R & R BATTERY PACK AT LOCATION B5-120 PER B717 AMM 33-51 OPS CHECK GOOD. (7804385)
- [SDR DALA2025092907059](https://openairdocs.org/sdr/DALA2025092907059), Sep 26, 2025: COALESCER BAG. ODOR. SMOKE AND ODOR IN CABIN AT GATE WITH PASSENGERS ON BOARD AT DEPARTURE TIME. F/A SAYS SHE SMELLS OIL IN THE CABIN. DECONTAMINATED AFT BULKHEAD AND INSTALLED NEW 
- [SDR DALA2025051403730](https://openairdocs.org/sdr/DALA2025051403730), May 13, 2025: SKIN. CRACKED. CRACK ON FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE. SUMMARY OF NRC 00056: FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT F
- [SDR DALA2025051303688](https://openairdocs.org/sdr/DALA2025051303688), May 13, 2025: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE WAS REPAIRED 
- [SDR DALA2025051203681](https://openairdocs.org/sdr/DALA2025051203681), May 12, 2025: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00048: FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED 
- [SDR DALA2025042103076](https://openairdocs.org/sdr/DALA2025042103076), Apr 19, 2025: CABLE. OUT OF TRACK. GOT A TAILCONE UNLOCK MSG DURING TAXI IN TO GATE. WHILE VERIFYING M PROCEDURES FOR MEL 53-52-018, FOUND LOCKING CABLE LEADS LOOSE, MEL STATES LEADS SHOULD BE TI
- [SDR DALA2025041102824](https://openairdocs.org/sdr/DALA2025041102824), Apr 2, 2025: SKIN. DENTED. GATE AGENT REPORTS L1 DOOR NOT CLOSING AUTO LEVER NOT INSTALLED. MTC INSPECTED DOOR FOUND DENT IN BOTTOM LEFT CORNER WITH DOOR CLOSED FROM JET BRIDGE PUSHING UP
- [SDR DALA2025030101570](https://openairdocs.org/sdr/DALA2025030101570), Feb 23, 2025: HINGE FITTING. GOUGED. -AD- WHILE ACCOMPLISHING NDT INSPECTION PER AMDS 5720-01103-01B FOUND GOUGE IN THE RH AFT SPAR ROUGHLY 8" OUTBOARD OF FLAP HINGE. AREA MARKED. COMPLIED WITH ALL
- [SDR DALA2025021801199](https://openairdocs.org/sdr/DALA2025021801199), Feb 15, 2025: TRANSMITTER. OUT OF TOLERANCE. SHIP 9579 -ATB/DE- THE CREW ACCOMPLISHED AN AIR TURN BACK TO ATL DUE TO A "FLAPS DISAGREE" MESSAGE AFTER FLAP AND SLAT RETRACTION. AN EMERGENCY WAS DECLARED WIT
- [SDR DALA2024121911830](https://openairdocs.org/sdr/DALA2024121911830), Dec 19, 2024: IDG. FAILED. SHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE "LEFT GENERATOR FAIL" MESSAGE DURING APPROACH INTO PHL. THE APU WAS ALREADY ON 
- [SDR DALA2024080607843](https://openairdocs.org/sdr/DALA2024080607843), Aug 6, 2024: LIGHT. INOPERATIVE. CABIN OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACKS AT B5-118 & B5-130 BAD. REPLACED THE EMERGENCY BATTERY PACKS PER B717 AM
- [SDR DALA2024010800322](https://openairdocs.org/sdr/DALA2024010800322), Jan 7, 2024: UNKNOWN. UNKNOWN. TWO FWD WINDOW SIGN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED FWD WINDOW EMERGENCY EXIT SIGN BATTERY PACK IAW B717 AMM 33-51. THE
- [SDR DALA2023121310204](https://openairdocs.org/sdr/DALA2023121310204), Dec 13, 2023: UNKNOWN. UNKNOWN. SHIP 9579 -FCNT/DE- THE CREW NOTED A "PSEU" MESSAGE DISPLAYED ON THE EAD DURING CRUISE. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED WITH ATC, AND THE C
- [SDR DALA2023070605440](https://openairdocs.org/sdr/DALA2023070605440), Jul 4, 2023: UNKNOWN. UNKNOWN. SHIP 9579 -DIV- THE AIRCRAFT WAS DIVERTED TO IAD DUE TO A SUSPECTED HIGHER THAN NORMAL FUEL CONSUMPTION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE CENT
- [SDR DALA2023062705158](https://openairdocs.org/sdr/DALA2023062705158), Jun 24, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA 1037 AND S-14L AT PAX CABIN. SUMMARY OF NRC 00398: CRACK ON FRAME STA 1037 AND S-14L AT PAX CABIN WAS REPAIRED PER ER/A 609263-14 REV. ORIGIN
- [SDR DALA2023062705151](https://openairdocs.org/sdr/DALA2023062705151), Jun 23, 2023: UNKNOWN. UNKNOWN. EXISTING REPAIR LOCATED BETWEEN FS 427-446 AT STR 28R HAS DAMAGE EXTENDING FORWARD OF THE REPAIR DOUBLER. SUMMARY OF NRC 0489: THIS ACTIVITY MUST BE FOLLOW-UP W
- [SDR DALA2023062305080](https://openairdocs.org/sdr/DALA2023062305080), Jun 22, 2023: UNKNOWN. UNKNOWN. REPAIR DOUBLER LOCATED AT THE AFT CARGO DOOR-AFT FRAME (FS 994 AND STR 26R) IS DAMAGED ON THE EXTERIOR SURFACE. SUMMARY OF NRC 00477: REPAIR DOUBLER LOCATED AT 
- [SDR DALA2023062205056](https://openairdocs.org/sdr/DALA2023062205056), Jun 21, 2023: UNKNOWN. UNKNOWN. CRACKS ON FRAME STA 1022 AND S-7L AT PAX CABIN. SUMMARY OF NRC 00397: CRACKS ON FRAME STA 1022 AND S-7L AT PAX CABIN WAS REPAIRED PER ER/A 609314-14 REV. ORIGIN
- [SDR DALA2023062105026](https://openairdocs.org/sdr/DALA2023062105026), Jun 21, 2023: UNKNOWN. UNKNOWN. CORROSION AROUND SETTLEMENT AREA OF VOR/LOC ANTENNA PANELS UPPER LH (2L), LOWER LH (1L), UPPER RH (2R), AND LOWER RH (1R). SUMMARY IN REF NRC 00403: LEVEL CORRO
- [SDR DALA2023061904962](https://openairdocs.org/sdr/DALA2023061904962), Jun 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH OUTBRD SEAT TRACK FROM STA Y=865 TO 1002 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 503: LEVEL CORROSION 2. SEAT TRACK FROM STA Y=865 TO 1002 
- [SDR DALA2023061304788](https://openairdocs.org/sdr/DALA2023061304788), Jun 9, 2023: UNKNOWN. UNKNOWN. AFTER CORROSION REMOVAL ON OTBD SEAT TRACK LH ON STA Y:577 TO 578 AT PAX CABIN, THE TRACK WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00500: CORROSION LEVEL 2. SEAT
- [SDR DALA2023060604560](https://openairdocs.org/sdr/DALA2023060604560), Jun 4, 2023: UNKNOWN. UNKNOWN. CRACK ON DOOR BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT. SUMMARY OF NRC 00163: BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT WAS REPAIRED PER B717-200 SRM 52-10-0
- [SDR DALA2023060604558](https://openairdocs.org/sdr/DALA2023060604558), Jun 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FWD AND AFT REPAIRS SPLACE DOUBLERS DOOR JAMB AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00100: CORROSION LEVEL 2. FWD AND AFT REPAIR SPLICE DOU
- [SDR DALA2023060604557](https://openairdocs.org/sdr/DALA2023060604557), Jun 3, 2023: UNKNOWN. UNKNOWN. GOUGE WAS FOUND ON PERMANENT REPAIR BTW STA Y=243 AND 3" ABOVE OF LONGERON 17L AT FUSELAGE. SUMMARY OF NRC 00283: DOUBLER ON PERMANENT REPAIR BTW STA Y=243 AND 
- [SDR DALA2023060204426](https://openairdocs.org/sdr/DALA2023060204426), Jun 2, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP MEMBRANE (WEB) X=56 AND STA 611 AT CPAX. CRACK WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 204. (LP #2795916)
- [SDR DALA2023060104385](https://openairdocs.org/sdr/DALA2023060104385), May 31, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX. SUMMARY OF NRC 00431: CRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX WAS REPAIRED PER B717-200 SRM
- [SDR DALA2023053004254](https://openairdocs.org/sdr/DALA2023053004254), May 27, 2023: CUSP WEB. CRACKED. CRACK CUSP MEMBRANE AT STA 715 L-18LH. SUMMARY OF NRC 00296: CUSP MEMBRANE AT STA 715 L-18LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R- PROCEDURE 4. (LP #278753
- [SDR DALA2023041302910](https://openairdocs.org/sdr/DALA2023041302910), Apr 14, 2023: UNKNOWN. UNKNOWN. SHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC INTO ATLANTA DUE TO A SUSPECTED LEFT SIDE BRAKES GRABBING CONDITION. CORRECTIVE ACTION: MAINT
- [SDR DALA2022121908182](https://openairdocs.org/sdr/DALA2022121908182), Dec 17, 2022: BATTERY PACK. NO TEST. DURING PRE-FLIGHT CHECK, FOUND BOTH AFT EMERGENCY OVER WING EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT B5-119 IAW B717 AMM 33-51. O
- [SDR DALA2022111507348](https://openairdocs.org/sdr/DALA2022111507348), Nov 13, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ON CEILING FROM ROW 13 AND FORWARD ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHTS BATTERY REF B717 AMM 33-51. OPERATIONAL CHECK
- [SDR DALA2022110107063](https://openairdocs.org/sdr/DALA2022110107063), Oct 30, 2022: WIRE. BROKEN. LOOSE ANTI-FOG WIRES AT CAPTAIN SIDE WINDOW. ARCHED TWICE WITH ANTI-FOG ON. MAINTENANCE FOUND BROKEN WIRES ON CAPTAIN SIDE WINDOW. REPAIRED WIRES REF ERA 95-521
- [SDR DALA2022100606489](https://openairdocs.org/sdr/DALA2022100606489), Oct 6, 2022: NONE. NONE. THE FORWARD OVERHEAD EXIT SIGN IS MISSING. MAINTENANCE FOUND THE MISSING LENS COVER AND RESECURED IT TO THE LIGHT. OPERATIONAL CHECK WAS NORMAL IAW B717-AMM 33 
- [SDR DALA2021111807113](https://openairdocs.org/sdr/DALA2021111807113), Nov 17, 2021: NONE. NONE. THE EXIT SIGN ON CEILING NEXT TO ROW 1 FELL FROM ITS MOUNT UPON LANDING. MAINTENANCE REPLACED THE EXIT SIGN REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #
- [SDR DALA2021071904072](https://openairdocs.org/sdr/DALA2021071904072), Jul 15, 2021: SKIN. DENTED. AFT CARGO DOOR SKIN BENT ON FWD SIDE JUST UP FROM SCUFF PLATE REF NRC 92. REMOVED AND REPLACED AFT CARGO DOOR PER B717 AMM 53-31-01 ON NRC 92. (LP #1875796)
- [SDR DALA2021071403985](https://openairdocs.org/sdr/DALA2021071403985), Jul 13, 2021: DOOR FRAME. GOUGED. FWD CARGO DOOR CUTOUT, AFT SIDE, HAS DEEP GOUGES AND SCRATCHES APPROX. FROM LONGERON 25R TO 26R. MARKED. REPAIRED PER B717 SRM 53-20-15-2R REPAIR 12. SEE NR 123
- [SDR DALA2021071203891](https://openairdocs.org/sdr/DALA2021071203891), Jul 11, 2021: LONGERON. CORRODED. AFT CARGO BILGE AREA HAS CORROSION L29L STA 907 TO STA 966 "MARKED". REPLACED LONGERON PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1871297)
- [SDR DALA2021071403983](https://openairdocs.org/sdr/DALA2021071403983), Jul 10, 2021: FRAME ANGLE. CORRODED. REPLACE FRAME CLIP AT STA 1022 25L TO 25R DUE TO CORROSION. SUMMARY FROM NRC 00401: REPAIRED FRAME CLIP PER B717 SRM 53-00- 06-2R PROCEDURE 3. (LP #1870910)
- [SDR DALA2021071203890](https://openairdocs.org/sdr/DALA2021071203890), Jul 10, 2021: SUPPORT. CORRODED. CORROSION WAS FOUND BETWEEN STA 1022 AND 1037 ON WASTE BLOWER SUPPORT CONNECTED TO L30. MARKED IN RED. SUMMARY SEE NRC 001-0291:2550-2003/001 00187: REPLACED IN
- [SDR DALA2021071203889](https://openairdocs.org/sdr/DALA2021071203889), Jul 10, 2021: INTERCOSTAL. CORRODED. THE AFT CARGO BILGE AREA HAS CORROSION ON INTERCOSTAL AT L30 STA 1022 TO STA 1037 "MARKED". SUMMARY NRC 062-0008:5331-2001/015 00363: REPLACED INTERCOSTAL PER B
- [SDR DALA2021071203888](https://openairdocs.org/sdr/DALA2021071203888), Jul 10, 2021: FRAME. CORRODED. CORROSION WAS FOUND ON FRAME AT STA 1022 IN MULTIPLE LOCATIONS. BETWEEN L29 AND R29. BETWEEN L27 AND L25. BETWEEN R27 AND R28. ALL MARKED IN RED. SUMMARY SEE NR
- [SDR DALA2021071203887](https://openairdocs.org/sdr/DALA2021071203887), Jul 9, 2021: SPLICE. CORRODED. AFT CARGO BILGE AREA HAS CORROSION L30 STA 900 AT FACTORY SPLICE TO STA 966. "MARKED". SUMMARY NRC 062-0008:5331-2001/009 00357: INSTALLED NEW SPLICE PER LONG B
- [SDR DALA2021071203886](https://openairdocs.org/sdr/DALA2021071203886), Jul 9, 2021: PAN. CORRODED. THE FWD CARGO DOOR PAN IS HEAVILY CORRODED IN FOUR LOCATIONS AROUND THE LOWER STOP FITTINGS. MARKED IN RED. REPAIRED PER B717 SMR 53-20-15-2R PROCEDURE 6. (LP #
- [SDR DALA2021070903835](https://openairdocs.org/sdr/DALA2021070903835), Jul 9, 2021: SHEAR TIE. CORRODED. AFT CARGO BILGE AREA HAS CORROSION STA 907 FRAME SHEAR CLIP L29R - L28L "MARKED". REPLACED FRAME CLIP PER B717 SRM 53-00-06-2R PROCEDURE 2, REF NRC 353. (LP #18
- [SDR DALA2021070903834](https://openairdocs.org/sdr/DALA2021070903834), Jul 7, 2021: FLOOR SUPPORT. CORRODED. FLOOR PANEL 211BF AT L-1 DOOR O/B FLOOR SUPPORT IS CORRODED. SUMMARY NRC 001-0024:2040-0024/002 00416: REPLACED SUPPORT REF DWG #9936534. (LP #1866600)
- [SDR DALA2021070503699](https://openairdocs.org/sdr/DALA2021070503699), Jul 3, 2021: PRESSURE BLKHD. CORRODED. CORROSION AFT OF STA 1053 ON LOWER PART OF P-DOME NEAR L30. MARKED IN RED. (FROM N/R 191). REPLACED DOUBLER PER B717 SRM 51-40-02. (LP #1862416)
- [SDR DALA2021070503698](https://openairdocs.org/sdr/DALA2021070503698), Jul 3, 2021: PAN. CORRODED. FWD CARGO DOOR PAN HEAVILY CORRODED IN FOUR (EACH) LOCATIONS AROUND THE LOWER STOP FITTINGS. MARKED IN RED. REPAIRED PER B717 SMR 53-20-15-2R PROCEDURE 6. (LP #
- [SDR DALA2021052102837](https://openairdocs.org/sdr/DALA2021052102837), May 19, 2021: BATTERY PACK. FAILED. FOUND TWO BATTERY PACKS FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE TWO BATTERY PACKS IN THE FORARD CABIN PER B717 AMM 33-51-03. (LP #1814149)

All 204: https://openairdocs.org/aircraft/N919AT/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/N919AT/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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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
