# N607AT: 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 BR700-715C130](https://openairdocs.org/engine/rolls-royce-deutschland-br700-715c130) (registry code 54008)
- 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: 55074
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 20, 2009
- Certificate issued: May 6, 2025
- Expires: May 31, 2032
- Mode S code: A7E152
- 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=607AT
- Page: https://openairdocs.org/aircraft/N607AT

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 BR700-715C130)

- [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/N607AT/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 N607AT.

## FAA accident and incident reports

None matched to N607AT.

## Service difficulty reports (168, 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 DALA2026012700610](https://openairdocs.org/sdr/DALA2026012700610), Jan 24, 2026: LANDING. DAMAGED. LEFT PYLON, PANEL LANDING IS WORN AND FASTENER HOLE ELONGATED. REPAIRED IAW SRM 54-00-00. (1417977)
- [SDR DALA2026012200501](https://openairdocs.org/sdr/DALA2026012200501), Jan 19, 2026: WARNING MESSAGE. NO INDICATION. DURING FUNCTIONAL CHECK, RT AFT OVR WING EXIT DOOR FAILED TO DISPLAY ALERT MESSAGE. REPAIRED PER B717 WDM 52-71-00. (1408940)
- [SDR DALA2026012200500](https://openairdocs.org/sdr/DALA2026012200500), Jan 18, 2026: CABLE. CORRODED. FOUND CABLE 129F CORRODED. REF AMDS CARD 2000-9000-04 REMOVED AND REPLACED CABLE (1408307)
- [SDR DALA2026012200499](https://openairdocs.org/sdr/DALA2026012200499), Jan 17, 2026: SKIN. GOUGED. FUSELAGE SKIN STA 148.55 LONGERON 19L TO 20L GOUGE DAMAGE. C/W ERA 626451-14 (1406347)
- [SDR DALA2026010509564](https://openairdocs.org/sdr/DALA2026010509564), Dec 29, 2025: FUEL SYS. LEAKING. FUEL LEAK FOUND DURING INSPECTION OF THE LT WING AFT LOWER SKIN AT XRS=164. REPAIRED PER ERA 629418-14AD (1375656)
- [SDR DALA2026010509567](https://openairdocs.org/sdr/DALA2026010509567), Dec 27, 2025: STRINGER. CORRODED. CORROSION ON S-30, BS 936-984. CORRODED LONGERON REPLACED ON NR 450 IAW SRM 53-20-05 (1371383)
- [SDR DALA2025122909458](https://openairdocs.org/sdr/DALA2025122909458), Dec 26, 2025: FRAME. CORRODED. CORROSION AT AFT CARGO KEEL SPLICE STA 974 L28L TO L28R. REPAIRED FRAME SECTION PER B717 SRM 53-20-07-2R-3 AND REPAIRED SKIN FORMER SECTION PER B717 SRM 53-00-0
- [SDR DALA2025122909457](https://openairdocs.org/sdr/DALA2025122909457), Dec 24, 2025: SUPPORT CHANNEL. CORRODED. FOUND CORROSION AROUND HOLE FOR VHF ANTENNA AT BS 916, LONGERON 3. REPLACED ANTENNA SUPPORT CHANNEL REF BAC DWG 5936434. (1367333)
- [SDR DALA2025122909456](https://openairdocs.org/sdr/DALA2025122909456), Dec 22, 2025: DOUBLER. DAMAGED. AFT CARGO DOOR AND FRAME: DOOR CUTOUT DOUBLER AT AFT FRAME DAMAGED. REPLACED REPAIR AT AFT CARGO DOOR JAMB EDGE IAW SRM 53 -20-15-2R (1363827)
- [SDR DALA2026082104776](https://openairdocs.org/sdr/DALA2026082104776), Dec 21, 2025: FRAME. CORRODED. CORROSION ON FORMER AT FRAME 946 BETWEEN STRINGER 30 AND 29L, REPAIRED FORMER PER B717-200SRM 53-00-06-2R. (1362231) (AIRCRAFT GROUNDED).
- [SDR DALA2026082104775](https://openairdocs.org/sdr/DALA2026082104775), Dec 21, 2025: FRAME. CORRODED. CORROSION ON FORMER AT STATION 954, ON BOTH SIDES OF LONGERON 29L, CORRECTIVE ACTION: REPAIRED FORMER PER B717-200SRM 53-00-06-2R. (1362237) (AIRCRAFT GROUNDED)
- [SDR DALA2025122909455](https://openairdocs.org/sdr/DALA2025122909455), Dec 21, 2025: SHEAR TIE. CORRODED. FOUND CORROSION ON SKIN CLIP AT FRAME 927 BETWEEN STRINGER 29L AND 30. REMOVED AND REPLACED DAMAGED FORMER PN 9915524-33 PER BOEING DWG 9915524 (1362226)
- [SDR DALA2026082104774](https://openairdocs.org/sdr/DALA2026082104774), Dec 19, 2025: SHEAR TIE. CORRODED. CORROSION ON 2 SKIN CLIPS AT FRAME 908, LEFT AND RIGHT OF LONGERON 30, CORRECTIVE ACTION: REPAIRED SKIN CLIPS PER B717-200SRM 53-00-06-2R. (1358889) (AIRCRAFT G
- [SDR DALA2025122909454](https://openairdocs.org/sdr/DALA2025122909454), Dec 19, 2025: DOOR FRAME. GOUGED. AFT CARGO DOOR AND FRAME: UNIDENTIFIED BLEND OUT AT DOOR FWD FRAME CUTOUT HAS GOUGE AND DAMAGE. REPAIRED PER B717-200 SRM 53-20-15-2R. (1359038).
- [SDR DALA2025122309345](https://openairdocs.org/sdr/DALA2025122309345), Dec 17, 2025: PAN. CORRODED. SHIP 9569 AFT CARGO DOOR AND FRAME: CORROSION AT DOOR PAN AREA AROUND FASTENERS. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-20- 15-2R (1355626)
- [SDR DALA2026082104773](https://openairdocs.org/sdr/DALA2026082104773), Dec 16, 2025: STRINGER. CORRODED. CORROSION ON STRINGER 30, STA 984-101, CORRECTIVE ACTION: REPAIRED STRINGER 30 PER NR 450. (1354308) (AIRCRAFT GROUNDED).
- [SDR DALA2025121709204](https://openairdocs.org/sdr/DALA2025121709204), Dec 16, 2025: LONGERON. CORRODED. CORROSION ON STRINGER 30 STA 997. REMOVED AND REPLACED DISCREPENT LONGERON 30 IAW SRM 53-20-05 (1354315)
- [SDR DALA2025121709203](https://openairdocs.org/sdr/DALA2025121709203), Dec 16, 2025: LONGERON. CORRODED. FOUND CORROSION ON LONGERON 30, BS 900 TO 936. REMOVED AND REPLACED DISCREPENT LONGERON 30 FROM IAW SRM 53-20-05 (1354312)
- [SDR DALA2025121709202](https://openairdocs.org/sdr/DALA2025121709202), Dec 16, 2025: LONGERON. CORRODED. AFT CARGO LONGERON 30 AT APROX STATION 1005 AND FWD CORRODED. REPAIRED ON NR 450 IAW SRM 53-20-05-2R PRO. 1, & BAC DWG 5919707. (1354309)
- [SDR DALA2025120808962](https://openairdocs.org/sdr/DALA2025120808962), Dec 3, 2025: PAN. CORRODED. AFT CARGO BS 1022 - 1053, CORROSION AT LAV TANK DUMP CHUTE AT LAV PAN. REMOVED CORROSION FROM PAN IAW SRM 51-40-02 (1333475)
- [SDR DALA2025111108259](https://openairdocs.org/sdr/DALA2025111108259), Nov 7, 2025: BATTERY PACK. INOPERATIVE. CEILING EMERGENCY LIGHTS INOP BETWEEN ROWS 24 TO 29. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY AT B5-231 PER B717 AMM 33-51. CHECKS GOOD. (7957044)
- [SDR DALA2025103107961](https://openairdocs.org/sdr/DALA2025103107961), Oct 24, 2025: FUEL CELL. LEAKING. FUEL LEAK FOUND DURING INSPECTION OF THE LT WING AFT LOWER SKIN DOUBLER XRS=164. : COMPLIED WITH PRI 629418-14AD (1268439).
- [SDR DALA2025103107969](https://openairdocs.org/sdr/DALA2025103107969), Oct 24, 2025: FUEL CELL. LEAKING. FUEL LEAK FOUND DURING INSPECTION OF RT WING AFT LOWER SKIN XRS=164. RT WING AFT LOWER SKIN DOUBLER XRS=164, & RT WING REAR SPAR LOWER CAP. COMPLIED WITH PRI 62
- [SDR DALA2025102407794](https://openairdocs.org/sdr/DALA2025102407794), Oct 23, 2025: RIB. DAMAGED. HOUR GLASS PANEL LOWER WING RIB, UPPER ROW, FWD FASTENER HOLE DAMAGED. REPAIRED PER PRI 630032-14 REV. 0, 1 AND 2 AND ER/A 630032-14 REV ORIGINAL. (1267567)
- [SDR DALA2025090206467](https://openairdocs.org/sdr/DALA2025090206467), Aug 27, 2025: COMPRESSOR. STALLED. ATB TO ORD DUE TO LT ENGINE COMPRESSOR STALL. REPLACED LEFT ENGINE. (7851686)
- [SDR DALA2025080505854](https://openairdocs.org/sdr/DALA2025080505854), Jul 30, 2025: HYDRAULIC LINE. LEAKING. RETURNED TO ATL DUE TO A RIGHT SYSTEM HYDRAULIC FLUID AND PRESSURE LOSS REQUIRING A MANUAL GEAR EXTENSION. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR BUNGE
- [SDR DALA2025052704027](https://openairdocs.org/sdr/DALA2025052704027), May 15, 2025: SKIN. DAMAGED. SHIP 9569 FUSELAGE SCRAPE AND GOUGE JUST BELOW L1 DOOR AREA. CORRECTIVE ACTION: REPAIRED PER ERA 6264451-14. (0967283)
- [SDR DALA2025031702030](https://openairdocs.org/sdr/DALA2025031702030), Mar 15, 2025: BATTERY PACK. FAULTED. THE AFT EMERGENCY EXIT LIGHT IS FLICKERING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 1050. OPERATIONAL CHECK WAS GOOD AND THE AIRCRA
- [SDR DALA2024061606115](https://openairdocs.org/sdr/DALA2024061606115), Jun 15, 2024: RELAY. FAILED. SHIP 9569 -MISC/DE- THE "ANTI-SKID FAIL" ALERT POSTED WHEN THE LANDING GEAR WAS SELECTED DOWN. A GO-AROUND WAS PERFORMED. DUE TO WET RUNWAYS, THE CREW DECLARED 
- [SDR DALA2024050104839](https://openairdocs.org/sdr/DALA2024050104839), Apr 29, 2024: SEAL. CUT. SHIP 9569 -ATB- CABIN CREW STATED THAT THERE WAS A SLOW DEPRESSURIZATION OCCURRING DURING THE CLIMB OUT AFTER TAKEOFF. THE LEAD F/A PASSED OUT (REGAINED CONSCIO
- [SDR DALA2024031203221](https://openairdocs.org/sdr/DALA2024031203221), Mar 10, 2024: SKIN. DAMAGED. FOUND DAMAGE TO FWD SIDE OF AFT CARGO DOOR CUTOUT SKIN. ACCOMPLISHED REPAIR PER B717 SRM 53-20-15-2R PROCEDURE 10, PARA 4E. .187 MATERIAL REMOVED. NO REPETITIVE
- [SDR DALA2024022602643](https://openairdocs.org/sdr/DALA2024022602643), Feb 24, 2024: BATTERY PACK. INOPERATIVE. THE FWD OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #542476
- [SDR DALA2023100608219](https://openairdocs.org/sdr/DALA2023100608219), Oct 4, 2023: UNKNOWN. UNKNOWN. EXFOLIATION CORROSION ON FRAME CLIP STA Y=655 LONGERON 29R AND 29L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00213: CORROSION LEVEL 2. FRAME CLIP ON STA Y=655 LO
- [SDR DALA2023100408158](https://openairdocs.org/sdr/DALA2023100408158), Oct 3, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON PRODUCCION DOUBLER ON CHANNEL AFT CARGO COMPARTMENT AT STA Y=974 TO STA Y=994. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORROSION ON PROD
- [SDR DALA2023100408153](https://openairdocs.org/sdr/DALA2023100408153), Oct 3, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL STRUCTURE LOWER (PAN) AT FWD CARGO DOOR. SUMMARY OF NRC 00194: INTERNAL STRUCTURE LOWER (PAN) AT FWD CARGO DOOR WAS REPAIRED PER PRI 611939-14
- [SDR DALA2023100308098](https://openairdocs.org/sdr/DALA2023100308098), Oct 2, 2023: UNKNOWN. UNKNOWN. WEAR ON DOOR EXTERNAL SKIN FWD LOWER EDGE AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00145: EXTERNAL SKIN ON FWD LOWER EDGE AT AFT CARGO COMPARTMENT DOOR WAS
- [SDR DALA2023100308092](https://openairdocs.org/sdr/DALA2023100308092), Oct 1, 2023: UNKNOWN. UNKNOWN. CRACK ON LONGER 17LH AND STA 1022 AT PAX CABIN IN REF NRC 00588. SUMMARY OF NRC 00603: LONGER 17LH AND STA 1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00
- [SDR DALA2023100308090](https://openairdocs.org/sdr/DALA2023100308090), Oct 1, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL STRUCTURE (WEB) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: AREA INTERNAL STRUCTURE (WEB) AT FWD CARGO DOOR WAS REPAIRED PER ER/A 611845-14 REV O
- [SDR DALA2023092507863](https://openairdocs.org/sdr/DALA2023092507863), Sep 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON EXTERNAL SKIN BTW STA Y=1037 TO Y=1022, L-29R TO L-28R AT LOWER FUSELAGE. SUMMARY OF NRC 00085: CORROSION LEVEL 2. EXTERNAL SKIN BTW STA Y=1037 TO 
- [SDR DALA2023092507861](https://openairdocs.org/sdr/DALA2023092507861), Sep 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00148: CORROSION LEVEL 2. PAN JAMB LOWER WA
- [SDR DALA2023092507856](https://openairdocs.org/sdr/DALA2023092507856), Sep 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON 30 BTW STA 909 TO STA 912, STA 921 TO STA 922, STA 962 TO STA 968, STA 998 TO STA 1000, LONGERON 29L STA 910 TO STA 912, STA 940 TO STA 95
- [SDR DALA2023091907687](https://openairdocs.org/sdr/DALA2023091907687), Sep 19, 2023: UNKNOWN. UNKNOWN. SCRATCHES ON DOUBLER OF AFT CARGO DOOR CUTOUT (AFT EDGE) BTW LONG PROJECT 24R AND LONG PROJECT 26R AT AFT FUSELAGE. SUMMARY OF NRC 00147: DOUBLER REPAIR OF AFT 
- [SDR DALA2023091907678](https://openairdocs.org/sdr/DALA2023091907678), Sep 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH TIE TRACK BTW STA 813 TO STA 1022 BTW L-28L TO L-27L OF AFT CARGO. SUMMARY OF NRC 00412: CORROSION LEVEL 2. TIE TRACK BTW STA 813 TO STA 1022 BT
- [SDR DALA2023091507586](https://openairdocs.org/sdr/DALA2023091507586), Sep 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON FILLET FAIRING FORMER LH SIDE STA Y=832. SUMMARY OF NRC 00603: CORROSION LEVEL 2. FILLET FAIRING FORMER LH SIDE STA Y=832 WAS REPLACED PER B-717-20
- [SDR DALA2023091407529](https://openairdocs.org/sdr/DALA2023091407529), Sep 12, 2023: UNKNOWN. UNKNOWN. CRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00555: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2965
- [SDR DALA2023091107393](https://openairdocs.org/sdr/DALA2023091107393), Sep 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON SUPPORT SETTLEMENT (ELECTRIC CONECTORS) STA Y=746 BTW L-20 AT LH MLG WHEEL WELL (FYT). SUMMARY OF NRC 00166: CORROSION LEVEL 2. SUPPORT WAS FABRICA
- [SDR DALA2023091107392](https://openairdocs.org/sdr/DALA2023091107392), Sep 10, 2023: UNKNOWN. UNKNOWN. AD. CRACK OF 2.900IN LENGTH APPROX AROUND UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH IN REF CARD 5310-01436-04B JOB #154-0002. STEP
- [SDR DALA2023091107391](https://openairdocs.org/sdr/DALA2023091107391), Sep 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORT STA Y=370, Y=427, Y=465, Y=636 BTW LONGERON 28L AND 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR SUPP
- [SDR DALA2023091107387](https://openairdocs.org/sdr/DALA2023091107387), Sep 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON 27LH BTW STA Y=813-832 AT UNDER OF FILLET FAIRING AREA. SUMMARY OF NRC 00304: CORROSION LEVEL 2. SECTION OF LONGERON 27LH BTW STA Y=813-83
- [SDR DALA2023091107386](https://openairdocs.org/sdr/DALA2023091107386), Sep 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00142: CORROSION LEVEL 2. DOOR JAMB LOWER E

All 168: https://openairdocs.org/aircraft/N607AT/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/N607AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce Deutschland BR700-715C130 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-715c130.md

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