# N608AT: 2000 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR700-715C130](https://openairdocs.org/engine/bmw-rolls-br700-715c130) (registry code 09497)
- 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: 55081
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 19, 2010
- Certificate issued: May 7, 2025
- Expires: May 31, 2032
- Mode S code: A7E509
- Registered owners: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Dept 595 Aircraft Registrations](https://openairdocs.org/faa-owner/DEPT%20595%20AIRCRAFT%20REGISTRATIONS)
- 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=608AT
- Page: https://openairdocs.org/aircraft/N608AT

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 (BMW Rolls 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/N608AT/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 N608AT.

## 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 20110829020559I](https://openairdocs.org/incident/20110829020559I), Aug 29, 2011: Boeing 717-200 (N608AT), Orlando, FL, Substantial damage. On aug 29, 2011 at 10:55AM flight trs 491 (717-200, N975AT) was struck by a bird during a 5 mile final approach to runway 17L at Orlando International Airport…

## Service difficulty reports (165, 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 DALA2026080704572](https://openairdocs.org/sdr/DALA2026080704572), Aug 7, 2026: COALESCER BAG. ODOR. FLIGHT ATTENDANTS REPORTED A CHEMICAL ODOR IN THE GALLEY DURING DESCENT, R/R LT AND RT COELESER BAGS - PACKS OP NML REF B717 AMM 21-50. (8904098) (AIRCRAFT GROU
- [SDR DALA2026072704340](https://openairdocs.org/sdr/DALA2026072704340), Jul 24, 2026: SKIN. WORN. WORN LOWER WING SKIN AT RT WING. REPAIRED PER ER/A 635223-14AD. (1718237) AIRCRAFT GROUNDED.
- [SDR DALA2026072404315](https://openairdocs.org/sdr/DALA2026072404315), Jul 24, 2026: DOOR. CRACKED. WEAR AND CRACK ON SLAT TRACK DOOR NR 3 AND NR 10 AT LT WING, COMPLIED WITH ER/A 540095-14MA. (1716756) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204284](https://openairdocs.org/sdr/DALA2026072204284), Jul 21, 2026: SKIN. DAMAGED. LIGHT STRIKE ON UPPER SURFACE XE=225.83 AT RT ELEVATOR STABILIZER, REPAIRED ELEVATOR IAW SRM 51-70-13-2R. (1712401) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204282](https://openairdocs.org/sdr/DALA2026072204282), Jul 21, 2026: DOOR FRAME. CRACKED. CRACK ON UPPER DOOR JAMB AREA BTW STA 725- 735 (JAMB OF LH AFT EMERGENCY EXIT DOOR) AT PAX CABIN, COMPLIED WITH ER/A 635314-14. (1711229) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204281](https://openairdocs.org/sdr/DALA2026072204281), Jul 20, 2026: SKIN. WORN. WEAR ON L/E INBD SIDE LOWER SKIN OF AFT MOVEABLE FLAP VANE AT LT WING, COMPLIED WITH ER/A 635472-14. (1710269) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004260](https://openairdocs.org/sdr/DALA2026072004260), Jul 19, 2026: CARGO TRACK. CORRODED. CORROSION ON LT & RT CARGO TRACKS. REPLACED IAW SRM 51-41. (1708534) AIRCRAFT GROUNDED.
- [SDR DALA2026071704219](https://openairdocs.org/sdr/DALA2026071704219), Jul 16, 2026: PANEL. DELAMINATED. DELAMINATED OUTBOARD SPOILER XRS=324.00 APROX AT RT WING, REPLACED SPOILER PANEL IAW AMM 27-60-01. (1703682) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704216](https://openairdocs.org/sdr/DALA2026071704216), Jul 16, 2026: PAN. CRACKED. CRACK ON INNER PAN FWD EDGE AND 14 INCHES FROM BOTTOM EDGE TO TOP EDGE AT FWD CARGO DOOR, COMPLIED WITH ER/A 635216-14. (1703867) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704212](https://openairdocs.org/sdr/DALA2026071704212), Jul 15, 2026: DOUBLER. WORN. WORN LOWER WING SKIN DOUBLER BTW XCW 58 AND STA Y=703 AT LT WING, COMPLIED WITH ER/A 635209-14AD. (1701724) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704211](https://openairdocs.org/sdr/DALA2026071704211), Jul 14, 2026: DOOR FRAME. CRACKED. CRACK ON FITTING OF STOP PAD (1 EA) IN BEAM 3 ON AFT EDGE AT FWD CARGO DOOR, COMPLIED WITH ER/A 635553-14. (1700114) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304126](https://openairdocs.org/sdr/DALA2026071304126), Jul 12, 2026: SKIN. WORN. WORN LOWER WING SKIN BTW XCW 58 AND STA Y= 703 AT RT WING. LOWER WING SKIN BTW XCW 58 AND STA Y=703 AT RH WING WAS REPAIRED PER ER/A 635223-14AD. (1696084) (AIR
- [SDR DALA2026071004047](https://openairdocs.org/sdr/DALA2026071004047), Jul 9, 2026: RETAINER. WORN. SHIP 9576 WEAR ON INTERNAL/EXTERNAL PAN AND SEAL RETAINERS AT FWD LOWER CORNER OF AFT CARGO DOOR, CORRECTIVE ACTION: COMPLIED WITH ER/A 633377-14. (1690771) (AI
- [SDR DALA2026070904035](https://openairdocs.org/sdr/DALA2026070904035), Jul 8, 2026: PAN. DAMAGED. ELONGATED HOLE IN INNER PAN OF FWD HINGE AT FWD CARGO DOOR, COMPLIED WITH ER/A 635381-14. (1688814) (AIRCRAFT GROUNDED).
- [SDR DALA2026070904033](https://openairdocs.org/sdr/DALA2026070904033), Jul 8, 2026: SKIN. CRACKED. CRACK ON CORNER OF UPPER AT XHS 104.00 APPROX AT HORIZONTAL STABILIZER, COMPLIED WITH ER/A 635420-14. (1688831) (AIRCRAFT GROUNDED).
- [SDR DALA2026070904032](https://openairdocs.org/sdr/DALA2026070904032), Jul 8, 2026: ACCESS PANEL. CRACKED. CRACKS ON ACCESS PANEL NR 370CR OF COUNTERSINK, COMPLIED WITH ER/A 635413-14TR. (1688768) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803990](https://openairdocs.org/sdr/DALA2026070803990), Jul 8, 2026: PAN. CRACKED. CRACK WAS FOUND ON OUTER PAN UPPER EDGE 19 INCHES FROM AFT EDGE AT FWD COMPARMENT DOOR, REPAIRED OUTER PAN PER B717-200 SRM 52-30 -02-2R. (1687917) (AIRCRAFT GR
- [SDR DALA2026070803989](https://openairdocs.org/sdr/DALA2026070803989), Jul 8, 2026: PAN. CRACKED. CRACK ON OUTER PAN ON UPPER EDGE AND 18 INCH TO FWD EDGE AT FWD CARGO DOOR, REPAIRED OUTER PAN PER B717-200 SRM 52-30- 02-2. (1687786) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803988](https://openairdocs.org/sdr/DALA2026070803988), Jul 8, 2026: FRAME. CORRODED. CRACK ON FRAME CAP STA 1022 LONG 4LH AT PAX CABIN, COMPLIED WITH ER/A 635304-14. (1687775) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803987](https://openairdocs.org/sdr/DALA2026070803987), Jul 8, 2026: CUSP WEB. CORRODED. CORROSION LEVEL 2 AT CUSP WEB BTW STA Y=715 TO STA Y=737 RH SIDE, REPAIRED CUSP WEB PER B717-200 SRM 53-00-55-2R. (1687773) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803986](https://openairdocs.org/sdr/DALA2026070803986), Jul 7, 2026: CUSP WEB. CORRODED. FOUND CORROSION LEVEL 2 AT CUSP WEB BTW STA Y=889 TO STA Y=908 LH, R & R CUSP WEB IAW SRM 51-41-02-0G. (1687224) (AIRCRAFT GROUNDED).
- [SDR DALA2026070603935](https://openairdocs.org/sdr/DALA2026070603935), Jul 5, 2026: CUSP WEB. CRACKED. CRACKED CUSP WEB BS Y=674 X=- 44 AT WING BOX. THE CUSP WEB BS Y=674 X=- 44 AT WING BOX WAS REPAIRED IAW SRM 53-00-55-2R. (1683637)(AIRCRAFT GROUNDED)
- [SDR DALA2026070303898](https://openairdocs.org/sdr/DALA2026070303898), Jul 2, 2026: PAN. CRACKED. CRACK WAS FOUND ON OUTER PAN AFT EDGE BTW STOP PAD AND BEAM #4, OUTER PAN AFT EDGE BTW STOP PAD AND BEAM #4 DIRECTION AT FWD CARGO COMPARMENT DOOR WAS REPAIRED 
- [SDR DALA2026070203886](https://openairdocs.org/sdr/DALA2026070203886), Jul 2, 2026: FLOOR SUPPORT. CORRODED. CORROSION LEVEL 2, FLOOR SUPPORT BTW X- 15.5, AT STA Y=1025 TO 1059, X=-16, REPLACED FLOOR SUPPORT IAW SRM 51-41-01-0G. (1677598) (AIRCRAFT GROUNDED).
- [SDR DALA2026070103875](https://openairdocs.org/sdr/DALA2026070103875), Jun 30, 2026: SEAT TRACK. CORRODED. CORROSION OUT OF LIMIT ON RH INBD SEAT TRACK BTW X-22 AND STA Y=211 TO STA Y=265 AT PAX CABIN FLOOR STRUCTURE, REPLACED PAX CABIN FLOOR STRUCTURE PER B717-200 S
- [SDR DALA2026063003867](https://openairdocs.org/sdr/DALA2026063003867), Jun 29, 2026: SUPPORT. OUT OF LIMITS. AREA OUT OF LIMITS IAW SRM 53-00-00-1A. SUPPORT ON STA Y=195 BTW X=16 TO X=43 WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G. (1673252) (AIRCRAFT GROUNDED
- [SDR DALA2026063003866](https://openairdocs.org/sdr/DALA2026063003866), Jun 29, 2026: DOUBLER. CORRODED. CORROSION ON DOUBLER BS 1053 AND L30 AT LOWER AFT CABIN PRESSURE BULKHEAD. DOUBLER WAS REPLACED IAW SRM 51-41-05-0G AND SRM 51-10-02-0G. (1673059) (AIRCRAFT GRO
- [SDR DALA2026062903841](https://openairdocs.org/sdr/DALA2026062903841), Jun 28, 2026: FLOOR SUPPORT. CORRODED. CORROSION FOUND AT FLOOR SUPPORT BTW STA Y=182 TO STA Y=200 AND X=-44, REPLACED SUPPORT PER B717-200 SRM 51-40-05-0G. (1671861) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903839](https://openairdocs.org/sdr/DALA2026062903839), Jun 27, 2026: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 APPROX. L-17R AT CPAX. REPAIRED FRAME PER B717-200 SRM. 53-20-07-2R. (1669584) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903837](https://openairdocs.org/sdr/DALA2026062903837), Jun 26, 2026: CUSP WEB. CRACKED. CRACK ON CUSP WEB, LT SIDE AT PASSENGER CABIN. REPAIRED IAW SRM 53-00-55-2R. (1668316) (AIRCRAFT GROUNDED)
- [SDR DALA2026062503781](https://openairdocs.org/sdr/DALA2026062503781), Jun 24, 2026: CUSP WEB. CRACKED. CRACKED CUSP WEB RT SIDE AT PASSENGER CABIN. CUSP WEB RT SIDE AT PASSENGER CABIN WAS REPAIRED IAW SRM 53-00-55-2R. (1664201) (AIRCRAFT GROUNDED).
- [SDR DALA2026062403762](https://openairdocs.org/sdr/DALA2026062403762), Jun 23, 2026: CUSP WEB. CRACKED. CRACK ON CUSP WEB STA Y=660 X=-58 RH SIDE AT PASSENGER CABIN, DAMAGED AREA REPAIRED PER B717-200 SRM 53-00-55-2R. (1662856) (AIRCRAFT GROUNDED).
- [SDR DALA2026062303736](https://openairdocs.org/sdr/DALA2026062303736), Jun 22, 2026: CUSP WEB. CRACKED. AIRCRAFT 9576, CRACK ON CUSP WEB STA Y=219 X=-44 RH SIDE AT PASSENGER CABIN. CUSP WEB STA Y=219 X=-44 RH SIDE AT PASSENGER CABIN WAS REPAIRED B717-200 SRM 53-00
- [SDR DALA2026062003686](https://openairdocs.org/sdr/DALA2026062003686), Jun 19, 2026: SLIDE. DAMAGED. OUT LIMITS (NO GO) PRESSURE GAUGE FROM TAIL CONE SLIDE AND MISSING RETAINERS CLIP (2EAS) OF RELEASE CABLE AT SLIDE COVER. TAIL CONE SLIDE WAS REPLACED AND VERIF
- [SDR DALA2026061903677](https://openairdocs.org/sdr/DALA2026061903677), Jun 17, 2026: SKIN. SCRATCHED. SCRATCH ON LOWER SKIN OF AFT MOVABLE VANE (3 INCHES FROM T.E. AND 6 INCHES FROM INBRD EDGE APPROX) AT RT WING. LOWER SKIN OF AFT MOVABLE VANE WERE REPAIRED IAW 
- [SDR DALA2026021901203](https://openairdocs.org/sdr/DALA2026021901203), Feb 19, 2026: PSEU. FAILED. SHIP 9576-MISC/DE- PSEU FAIL MESSAGE IN CRUISE, COMPLIED WITH QRH AND SYSTEM RETURNED TO NORMAL. EMERGENCY DECLARED AS PRECAUTIONARY. MAINTENANCE REPLACED THE P
- [SDR DALA2025121009011](https://openairdocs.org/sdr/DALA2025121009011), Dec 8, 2025: SLIDE. DISLODGED. L1 EVACUATION SLIDE COMPARTMENT OPEN, SLIDE DISMOUNTED. INSTALLED L1 DOOR EVACUATION SLIDE IAW AMDS WORKCARD 2561-9004. (7796904)
- [SDR DALA2024112711265](https://openairdocs.org/sdr/DALA2024112711265), Nov 27, 2024: DOOR. DAMAGED. CONT OF LOG #693782 L1 DOOR FWD LOWER DOOR DAMAGED. FABRICATED REPAIR DOUBLER AND FILLER PER B717 SRM 52-10-01-2R PROC 1. COMPLETED FWD PASSANGER DOOR LOWER FWD
- [SDR DALA2024112711263](https://openairdocs.org/sdr/DALA2024112711263), Nov 27, 2024: SKIN. DENTED. RAMP REPORTS DENT ON L1 DOOR BOTTOM FWD CORNER. ATEMPTED TO REWORK/STRAIGHTEN DOOR EDGE PER B717 SRM 52-00-00-2R -3. FOUND CRACK APPOX 1/4" LONG 1/4" FROM BOTTO
- [SDR DALA2024082708493](https://openairdocs.org/sdr/DALA2024082708493), Aug 26, 2024: LAMP. INOPERATIVE. AIRCRAFT 9576, EXT OVERHEAD IND NEEDS RELAMPED. CORRECTIVE ACTION: RELAMPED EXT IND OVERHEAD. OPS CK GOOD. (LP 5945559)
- [SDR DALA2023081406585](https://openairdocs.org/sdr/DALA2023081406585), Aug 10, 2023: UNKNOWN. UNKNOWN. SHIP 9576 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "ANTI-SKID FAIL' MESSAGE ILLUMINATING DURING APPROACH. THE LANDING WAS UNEVENTFUL,
- [SDR DALA2023080406297](https://openairdocs.org/sdr/DALA2023080406297), Aug 2, 2023: UNKNOWN. UNKNOWN. CRACK ON ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR. SUMMARY OF NRC 00198: ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR WAS REPLACED PER DWG 4
- [SDR DALA2023080306283](https://openairdocs.org/sdr/DALA2023080306283), Aug 2, 2023: UNKNOWN. UNKNOWN. CRACK ON FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING. (AD) SUMMARY OF NRC 00051: FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING WAS REPAI
- [SDR DALA2023080306281](https://openairdocs.org/sdr/DALA2023080306281), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y 954-994. SUMMARY OF NRC 00180: INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR
- [SDR DALA2023080106209](https://openairdocs.org/sdr/DALA2023080106209), Jul 31, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SILL STRUCTURE BTW STA 954 TO STA 994 OF AFT DOOR AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00089: CORROSION LEVEL 2. LOWER SILL STRUCTURE (DO
- [SDR DALA2023080106205](https://openairdocs.org/sdr/DALA2023080106205), Jul 30, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON LH OVERWING FRAME STA Y=696, GREATER THAN 0.125IN IN REF TASK CARD 5310-01436-01B JOB #078-0002 STEP 10. SUMMARY OF NRC 00181: LH OVERWING FR
- [SDR DALA2023072806111](https://openairdocs.org/sdr/DALA2023072806111), Jul 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER DOOR JAMB AT FWD CARGO COMPARTMENT BTW STA Y370 AND STA Y427 (INNER AND OUTER SIDE). SUMMARY OF NRC 00081: CORROSION LEVEL 2. LOWER DOOR JAMB
- [SDR DALA2023072706099](https://openairdocs.org/sdr/DALA2023072706099), Jul 27, 2023: UNKNOWN. UNKNOWN. CORROSION AT ANGLES (2 EA) WAS FOUND DURING DOOR JAMB DISASSEMBLY. SUMMARY OF NRC 00196: CORROSION LEVEL 2. ANGLES (2 EA) WERE FABRICATED AND INSTALLED PER B717
- [SDR DALA2023072505983](https://openairdocs.org/sdr/DALA2023072505983), Jul 24, 2023: UNKNOWN. UNKNOWN. CRACK WAS FOUND ON EDGE OF CUSP MEMBRANE. SUMMARY OF NRC 00190: CUSP MEMBRANE WAS FABRICATED PER B717 SRM 53-00-55-2R-4 TABLE 2 AND INSTALLED WITH CARD 5310-014
- [SDR DALA2023072105926](https://openairdocs.org/sdr/DALA2023072105926), Jul 20, 2023: UNKNOWN. UNKNOWN. DURING LH CUSP MEMBRANE STA 655-715 REMOVAL, CRACK WAS FOUND ON EDGE. SUMMARY OF NRC 00192: LH CUSP MEMBRANE STA 655-715 WAS REPAIRED PER B717-200 SRM 53-00-55-

All 165: https://openairdocs.org/aircraft/N608AT/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/N608AT/stcs.md

## Related

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

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