# N927AT: 2000 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: 55077
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 2000
- Certificate issued: August 6, 2025
- Expires: August 31, 2032
- Mode S code: ACD83D
- 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=927AT
- Page: https://openairdocs.org/aircraft/N927AT

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/N927AT/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 N927AT.

## 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 20041031031999I](https://openairdocs.org/incident/20041031031999I), Oct 31, 2004: Boeing 717200 (N927AT), Rochester, NY. (-23) On October 31, 2004, an airtran B-717, N927AT, registered to wells fargo bank nw na, trustee, and operated by airtran airlines, ingested a bird upon…

## Service difficulty reports (218, 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 DALA2026091105082](https://openairdocs.org/sdr/DALA2026091105082), Sep 10, 2026: APU. ODOR. BOARDING THE ACFT W/APU ON THERE IS A VERY STRONG DIRTY SOCK SMELL IN ALL AREAS OF THE COCKPIT AND CABIN, CORRECTIVE ACTION: R/R APU IAW W/C 4900-9901. (9518000
- [SDR DALA2026090905049](https://openairdocs.org/sdr/DALA2026090905049), Sep 9, 2026: VANE. DAMAGED. EVIDENCE OF RUBBING ON AFT SIDE OF RIGHT MAIN LANDING GEAR AND LEADING EDGE OF FLAP, R&R RT FWD MOVEABLE VANE REF AMDS WC 2750-4010. (9488696) (AIRCRAFT GROUNDE
- [SDR DALA2026082404795](https://openairdocs.org/sdr/DALA2026082404795), Aug 23, 2026: COALESCER BAG. ODOR. SLIGHT DIRTY SOCK SMELL AFTER LONG IDLE DESCENT. R & R COALESCER BAGS IAW AMM 21-54-08. (9488641) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903842](https://openairdocs.org/sdr/DALA2026062903842), Jun 28, 2026: ELEC CONNECTOR. DAMAGED. R1 EMERGENCY LIGHT INOP. REPINNED CONNECTOR PERB717 AMM 20-30. (9221037) (AIRCRAFT GROUNDED).
- [SDR DALA2026042202564](https://openairdocs.org/sdr/DALA2026042202564), Apr 19, 2026: ENGINE. FAILED. SMKE/FUME - PRIOR TO PUSH, CREW REPORTED WHITE HAZY SMOKE AND AN OIL SMELL IN THE CABIN FOLLOWED BY A HARD CLUNK AND AN APU AUTO SHUTDOWN. RAMP REPORTED FLAMES 
- [SDR DALA2026012200496](https://openairdocs.org/sdr/DALA2026012200496), Jan 17, 2026: FADEC. FAULTED. FLIGHT CREW DIVERTED TO ATL DUE TO RIGHT ENGINE FADEC ALTERNATE MODE CAUSING FLIGHT TO BE REMOVED FROM CAT 1/2/3 AND RVSM. REMOVED AND REPLACED RIGHT ENGINE P20
- [SDR DALA2025111808427](https://openairdocs.org/sdr/DALA2025111808427), Nov 14, 2025: ENGINE. SURGES. ATB- RETURNED TO MSP DUE TO LEFT ENGINE SURGING. REDUCED THRUST AND SURGING STOPPED. REPLACED LEFT ENGINE. OPS CHECK NORMAL. (8225854).
- [SDR DALA2025091606815](https://openairdocs.org/sdr/DALA2025091606815), Sep 11, 2025: COMPRESSOR. DAMAGED. ATB TO ATL DUE TO NR 1 ENGINE COMPRESSOR STALL ON CLIMB OUT. BORESCOPED LT ENGINE AND FOUND MULTIPLE BLADES IN HPC DAMAGED. REPLACED ENGINE.(7723471)
- [SDR DALA2025081105984](https://openairdocs.org/sdr/DALA2025081105984), Aug 3, 2025: POWER SUPPLY. FAULTED. SHIP 9572 EMERGENCY LIGHT EXTERIOR DON'T TURN ON. CORECTIVE ACTION: OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. TEST 
- [SDR DALA2025080205796](https://openairdocs.org/sdr/DALA2025080205796), Jul 28, 2025: FUEL CELL. CORRODED. CORROSION ON CENTER FUEL TANK UPPER SKIN AFT FLANGE STA 747 X=-55 TO X=-59. REPAIRED PER PRI 626998-14.
- [SDR DALA2025072905675](https://openairdocs.org/sdr/DALA2025072905675), Jul 25, 2025: SKIN. CRACKED. SHIP 9572 INITIAL INSPECTION: CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 BTW. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN STA 1076 BTW LONG 13-14 LH WAS REPAIRED PE
- [SDR DALA2025072405582](https://openairdocs.org/sdr/DALA2025072405582), Jul 23, 2025: HINGE. CORRODED. SHIP 9572 AFTER MIDLE FLAP HINGE , CORROSION ON HINGE FITTING HOLES AT LH FLAP. ALSO SCRATCHES HINGE BOLTS (3EA). CORRECTIVE ACTION: HINGE FITTING HOLES AT LH F
- [SDR DALA2025072405581](https://openairdocs.org/sdr/DALA2025072405581), Jul 22, 2025: SKIN. CORRODED. SHIP 9572 IN REF NRC 00308, CORROSION ON CENTER WING UPPER SKIN BTW STA Y= 715/720 X = -60 AT WING BOX. CORRECTIVE ACTION: CORROSION ON CENTER WING UPPER SKIN B
- [SDR DALA2025071805420](https://openairdocs.org/sdr/DALA2025071805420), Jul 18, 2025: PAN. CRACKED. AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, SEVEN (7 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO 
- [SDR DALA2025071705384](https://openairdocs.org/sdr/DALA2025071705384), Jul 17, 2025: PAN. CRACKED. AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC 5231-2005, FIVE (5 QTY) CRACKS WERE FOUND AFFECTING THE FWD CARG
- [SDR DALA2025071705383](https://openairdocs.org/sdr/DALA2025071705383), Jul 17, 2025: PAN. CRACKED. AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO 
- [SDR DALA2025071105224](https://openairdocs.org/sdr/DALA2025071105224), Jul 11, 2025: PAN. CRACKED. AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC. 5231-2005, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE FWD CA
- [SDR DALA2025070805068](https://openairdocs.org/sdr/DALA2025070805068), Jun 30, 2025: NOT REPORTED. NOT REPORTED. SHIP 9572 DTA ER/A 626436-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 30-JUN-25. CONTACT LIAISON ENGINEERING, DEPT 555
- [SDR DALA2025070104875](https://openairdocs.org/sdr/DALA2025070104875), Jun 30, 2025: HINGE FITTING. CORRODED. SHIP 9572 DURING HCK AT QRO, CORROSION WAS NOTED ON THE LH INBD T/R FWD FLAP HINGE FITTING, XW 251. CORRECTIVE ACTION: ER/A REVISION REQUIRED TO INCORPORATE DTE
- [SDR DALA2025063004851](https://openairdocs.org/sdr/DALA2025063004851), Jun 26, 2025: SKIN. CORRODED. SHIP 9572 CORROSION ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING. CORRECTIVE ACTION: CORROSION LEVEL 2. AREA ON WING UPPER TRAILING 
- [SDR DALA2025062604789](https://openairdocs.org/sdr/DALA2025062604789), Jun 25, 2025: CARGO TRACK. CORRODED. SHIP 9572 CORROSION OUT LIMITS,IN REF TO NRC 00250 :CORROSION ON TIE TRACKS THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LH STA Y=896- 1022. CORRECTIVE ACTION: DAM
- [SDR DALA2025062604788](https://openairdocs.org/sdr/DALA2025062604788), Jun 25, 2025: TAB. DELAMINATED. SHIP 9572 DELAMINATED CONTROL TAB OF RH ELEVATOR. CORRECTIVE ACTION: CONTROL TAB OF RH ELEVATOR WAS REPAIRED PER PRI 626667-14 REV. 2. AND ER/A 626667-14 REV OR
- [SDR DALA2025062504752](https://openairdocs.org/sdr/DALA2025062504752), Jun 17, 2025: NONE. NONE. DTA ER/A 626583-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. CORRECTIVE ACTION: C.W ERA 626583.
- [SDR DALA2025061704574](https://openairdocs.org/sdr/DALA2025061704574), Jun 17, 2025: BEAM. CRACKED. CRACK BEYONDS STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR. STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR WAS PERFORMED AND NOT A
- [SDR DALA2025061604510](https://openairdocs.org/sdr/DALA2025061604510), Jun 15, 2025: SKIN. CRACKED. AIRCRAFT 9572, CRACK ON EXTERNAL FUSELAGE SKIN STA 1037 AND 1152 BTW LONG 13-RH-14RH. CORRECTIVE ACTION: TRIMMED SKIN, DOUBLER TO REMOVE CRACKS, AND PREFORMED H
- [SDR DALA2025061104459](https://openairdocs.org/sdr/DALA2025061104459), Jun 11, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9572, CORROSION WAS FOUND OUT LIMITS ON SEAT TRACKS STA Y=906-1015 X=-56 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACKS S
- [SDR DALA2025061104456](https://openairdocs.org/sdr/DALA2025061104456), Jun 9, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9572, CORROSION ON RH OUTB SEAT TRACK (X-56) ON STA Y465 TO STA 484 AT PAX CABIN. WITH AN ORIGINAL THICKNES; ON CROWN= 0.115"; BOTTOM= 0.100"; AND MINI
- [SDR DALA2025061104463](https://openairdocs.org/sdr/DALA2025061104463), Jun 5, 2025: SKIN. CRACKED. AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A LOWER FUSELAGE INCLUDING RADOME AND LOWER WING FILLETS INSPECTION PER WC 0593-2009, ONE DENT WITH TWO CRACK
- [SDR DALA2025060704352](https://openairdocs.org/sdr/DALA2025060704352), Jun 2, 2025: FLOOR SUPPORT. CORRODED. AIRCRAFT 9572, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT (2EA) FROM STA Y=160 TO 200 X=7 AND X= - 7. ALSO, CORROSION ON FLOOR SUPPORT STA Y=145 TO 147 X= -
- [SDR DALA2025060704350](https://openairdocs.org/sdr/DALA2025060704350), Jun 2, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9572, CORROSION ON RH MID SEAT TRACK (X=-44) ON STA Y= 200-218 AT PAX CABIN WITH AN ORIGINAL THICKNESS ON CROWN=0.115IN BOTTOM= 0.100IN AND MINIMUM REM
- [SDR DALA2025060604339](https://openairdocs.org/sdr/DALA2025060604339), May 30, 2025: MEMBRANE. CORRODED. SHIP 9572 CORROSION OUT OF LIMIT ON MEMBRANE, STA Y 160 TO 197 BTW X=44 TO X= 54; STA Y 200 BTW X= 52 & X=54 AT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER
- [SDR DALA2025060604338](https://openairdocs.org/sdr/DALA2025060604338), May 30, 2025: CUSP WEB. CRACKED. SHIP 9572 INITIAL INSPECTION: CRACK ON CUSP WEB STA Y=657 X=57 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4 (0995798)
- [SDR DALA2025060604334](https://openairdocs.org/sdr/DALA2025060604334), May 29, 2025: WEB. CORRODED. SHIP 9572 IN REF NRC 00391 AFTER REMOVAL SEAT TRACK, CORROSION WAS FOUND ON DIAPHRAGM STA Y=200 TO 220 APROX X:-44 AT CABIN PAX. CORRECTIVE ACTION: REPAIRED PER
- [SDR DALA2025060604333](https://openairdocs.org/sdr/DALA2025060604333), May 28, 2025: WEB. CRACKED. SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y=258 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (099075
- [SDR DALA2025060604332](https://openairdocs.org/sdr/DALA2025060604332), May 28, 2025: FLOOR SUPPORT. CORRODED. SHIP 9572 CORROSION OUT LIMITS, IN REF TO NRC 00467: CORROSION ON FLOOR SUPPORT FROM STA 1022 TO Y=1059 X=44, AT AFT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRE
- [SDR DALA2025060604330](https://openairdocs.org/sdr/DALA2025060604330), May 27, 2025: WEB. CRACKED. SHIP 9572 CRACK ON MEMBRANE STA Y=813 X=45 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990285)
- [SDR DALA2025060604325](https://openairdocs.org/sdr/DALA2025060604325), May 26, 2025: CUSP WEB. CRACKED. SHIP 9572 CRACK ON MEMBRANE STA Y=715 X=44 AT LH PASSENGER CABIN (CPAX). REPAIRED PER B717-200 SRM 53-00-55-2R-4 (09881240988124)
- [SDR DALA2025060604323](https://openairdocs.org/sdr/DALA2025060604323), May 26, 2025: FLOOR SUPPORT. CORRODED. SHIP 9572 DUE TO CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200, X=10, WAS MEASURE WITH ORIGINAL THICKNESS: 0.070IN MINIMUM REMAINING THICKNESS 0.042 IN THEREFORE
- [SDR DALA2025052704030](https://openairdocs.org/sdr/DALA2025052704030), May 22, 2025: WEB. CRACKED. SHIP 9572 CRACK ON MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASS
- [SDR DALA2025052704023](https://openairdocs.org/sdr/DALA2025052704023), May 20, 2025: WEB. CRACKED. SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y =692 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55. (0976468)
- [SDR DALA2025052203939](https://openairdocs.org/sdr/DALA2025052203939), May 20, 2025: TORQUE TUBE. CORRODED. SHIP 9572 ON REF AMDS 2027-2004 CORROSION ON SPLINE AND BORE OF RUDDER DRIVE TORQUE TUBE P/N 5912802-13, ALSO CORROSION ON WASHER LOWER BRG P/N 2913035-1 OF RUD
- [SDR DALA2025050503410](https://openairdocs.org/sdr/DALA2025050503410), May 2, 2025: SPAR. CRACKED. -AD- LH WING SPAR CRACK. LEFT WING SPAR REPARED PER ERA 621363-14AD REV ORG. FINAL ERA REV ORG HAS BEEN RECEIVED AND MATCHES PRI REV. 21. ASSOCIATED ER/A 14-621
- [SDR DALA2025051403731](https://openairdocs.org/sdr/DALA2025051403731), May 1, 2025: NONE. NONE. -AD- PER ERA 621363-14 AD REV 0 STAGE VIII STEP 9, PRIOR TO ACCESS CLOSE-UP, PERFORM A GENERAL VISUAL INSPECTION OF THE AREA FOR CLEANLINESS, AS DEFINED IN TOPP
- [SDR DALA2025051403725](https://openairdocs.org/sdr/DALA2025051403725), May 1, 2025: NONE. NONE. -AD- PER ERA 621441-14AD REV ORIG STEP 25, PERFORM GVI OF RH WING AREA BEFORE ACCESS CLOSE UP. STEP 25 OF ERA 621441-14AD REV O WAS COMPLIED WITH ON NRC 11 DURI
- [SDR DALA2025051403724](https://openairdocs.org/sdr/DALA2025051403724), May 1, 2025: SPAR. CRACKED. -AD- DUE TO CRACK INDICATION, COMPLY WITH RH WING SPAR REPAIR PER ERA 621441-14AD REV ORIG. SPAR REPAIRED PER PRI 621441-14AD REVS 0 THRU 8. COMPARED PRI 621441
- [SDR DALA2025051403723](https://openairdocs.org/sdr/DALA2025051403723), May 1, 2025: HINGE FITTING. WORN. -AD- LH WING, OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. COMPLIED WITH ERA 623200-14AD REV ORG. REPAIRED LH WING OUBOARD FLAP HINGE POINT AC SIDE PER E
- [SDR DALA2025043003312](https://openairdocs.org/sdr/DALA2025043003312), Apr 25, 2025: HINGE FITTING. WORN. LH WING OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. MACHINED IB AND OB LUGS TO REMOVE DAMAGE. OB LUG BORE FINAL SIZE IS .533. IB LUG FINAL SIZE IS .594.
- [SDR DALA2024100209620](https://openairdocs.org/sdr/DALA2024100209620), Sep 30, 2024: SPAR CAP. CRACKED. CRACK IN LH WING REAR SPAR LOWER CAP RADIUS. REFERENCE AA NUMBER FC 5720-01103. CRACK LOCATION IS XRS 156.950. SUMMARY NRC 010-0001:5720-01103-01A/001 00001 COM
- [SDR DALA2024041204357](https://openairdocs.org/sdr/DALA2024041204357), Apr 10, 2024: DOOR FRAME. CORRODED. CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00091: CORROSION LEVEL 2. AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PE
- [SDR DALA2022123008503](https://openairdocs.org/sdr/DALA2022123008503), Dec 29, 2022: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS ON THE GALLEY OVERHEAD, AT SEATS 1-14, AND AT SEATS 24-29 ARE INOPERATIVE. MAINTENANCE FOUND BAD BATTERY PACKS AND BATTERY RACKS AT B5- 259

All 218: https://openairdocs.org/aircraft/N927AT/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/N927AT/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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