# N998AT: 2002 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 TAY-651-54](https://openairdocs.org/engine/rolls-royce-tay-651-54) (registry code 54564)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 55142
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 27, 2002
- Certificate issued: May 15, 2024
- Expires: May 31, 2031
- Mode S code: ADF06D
- 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=998AT
- Page: https://openairdocs.org/aircraft/N998AT

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): 66 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 TAY-651-54)

- [AD 2019-14-01](https://openairdocs.org/ad/2019-14-01): Turbine Engine Compressor Section · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Aug 26, 2019
- [AD 2016-17-01](https://openairdocs.org/ad/2016-17-01): Stage 1 HPT disks · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Sep 27, 2016
- [AD 2014-06-05](https://openairdocs.org/ad/2014-06-05): Low-pressure (LP) compressor module · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective May 8, 2014
- [AD 2014-03-16](https://openairdocs.org/ad/2014-03-16): Low-pressure compressor (LPC) fan blades · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Mar 18, 2014
- [AD 2013-23-01](https://openairdocs.org/ad/2013-23-01): High-pressure (HP) air bleed valve · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Dec 30, 2013
- [AD 2010-17-12 R1](https://openairdocs.org/ad/2010-17-12-R1): Engine · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Nov 18, 2010
- [AD 2010-20-22](https://openairdocs.org/ad/2010-20-22): Disc · Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Nov 9, 2010
- [AD 2007-26-19](https://openairdocs.org/ad/2007-26-19): Low pressure (LP) compressor case · Rolls-Royce Deutschland TAY 611-8, TAY 611-8C, TAY 620-15 and 2 more. Effective Feb 11, 2008
- [AD 2005-26-18](https://openairdocs.org/ad/2005-26-18): High pressure compressor (HPC) stage 12 disc assembly · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Feb 3, 2006
- [AD 2005-03-06](https://openairdocs.org/ad/2005-03-06): LP fuel tubes · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 17, 2005
- [AD 2003-22-14](https://openairdocs.org/ad/2003-22-14): Fan blades · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Dec 18, 2003
- [AD 2002-09-02](https://openairdocs.org/ad/2002-09-02): Airworthiness Limitations Section (ALS) - Critical Life-Limited Rotating Engine Part · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Jun 6, 2002
- [AD 99-24-01](https://openairdocs.org/ad/99-24-01): Rolls-Royce Deutschland TAY 620-15, TAY 650-15 and TAY 651-54. Effective Jan 18, 2000

### 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 2010-17-12](https://openairdocs.org/ad/2010-17-12) (historical): Low- pressure turbine disks · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Sep 27, 2010
- [AD 2007-03-02](https://openairdocs.org/ad/2007-03-02) (historical): LP compressor fan blades · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 5, 2007
- [AD 2006-18-14](https://openairdocs.org/ad/2006-18-14) (historical): Cyclic life of stage 1 HPT discs, and stage 1 LPT discs · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Oct 13, 2006
- [AD 2004-26-10](https://openairdocs.org/ad/2004-26-10) (historical): Ice-impact Panels Installed in the Low Pressure (LP) Compressor Case · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Jan 21, 2005
- [AD 2004-05-22](https://openairdocs.org/ad/2004-05-22) (historical): Low pressure (LP) compressor case · Rolls-Royce Deutschland TAY 611-8, TAY 611-8C, TAY 620-15 and 2 more. Effective Mar 25, 2004
- [AD 2003-05-04](https://openairdocs.org/ad/2003-05-04) (historical): Low pressure (LP) fuel tubes · Rolls-Royce Deutschland TAY 611-8, TAY 620-15, TAY 650-15 and 1 more. Effective Mar 26, 2003
- [AD 2002-01-29](https://openairdocs.org/ad/2002-01-29) (historical): High Pressure Compressor (HPC) Stage 11/12 Disc Spacer · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Feb 15, 2002
- [AD 2001-22-18](https://openairdocs.org/ad/2001-22-18) (historical): Fan Blades · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54. Effective Dec 18, 2001

All 82: https://openairdocs.org/aircraft/N998AT/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 N998AT.

## 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 20040829020869I](https://openairdocs.org/incident/20040829020869I), Aug 29, 2004: Boeing 717200 (N998AT), Flint, MI, Minor damage. (-23) Around 07:am on August 29, 2004 an air tran aircraft N998AT was taking off from Flint Bishop international airport (fnt). About 20 miles east of fnt the…

## Service difficulty reports (212, 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 DALA2026100505510](https://openairdocs.org/sdr/DALA2026100505510), Oct 2, 2026: SKIN. DAMAGED. FUSELAGE SKIN FS 294-351 S-28R TO S-27L DAMAGED. REPAIRED PER ER/A 590835-14. (1845326) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092505347](https://openairdocs.org/sdr/DALA2026092505347), Sep 24, 2026: SKIN. DENTED. FOUND DENT AFFECTING THE FUSELAGE SKIN BETWEEN STA 237 TO 256 AND L-15 -16R, COMPLIED WITH ER/A 624583-14. (1829579) (AIRCRAFT GROUNDED).
- [SDR DALA2026090404999](https://openairdocs.org/sdr/DALA2026090404999), Sep 4, 2026: UNKNOWN. ODOR. CREW REPORTED A BURNING ELECTRICAL ODOR, INSPECTED ALL COFFEE MAKERS AND OVENS FOR RESIDUAL DEBRIS. NO DEBRIS NOTED; ALSO RAN COFFEE MAKERS AND OVENS, NO ODOR T
- [SDR DALA2026080604551](https://openairdocs.org/sdr/DALA2026080604551), Aug 5, 2026: ELECTRICAL SYS. FAULTED. ATO- APPROX 60KTS DUE TO ELECTRICAL FAULT AND STICK PUSHER FAIL ANNUNCIATION. PERFORMED ENGINE RUN WITH BOTH ENGINES AT ALL POWER SETTINGS NO FAULTS NOTED. RT G
- [SDR DALA2026060903442](https://openairdocs.org/sdr/DALA2026060903442), May 30, 2026: UNKNOWN. NOISE. DIV- CREW REPORTED A BEEPING NOISE FROM FIRST CLASS TO EMERGENCY EXIT UNDER FLOOR AREA. (FOSR) EMERGENCY DECLARED WITH ATC. INSPECT AIRCRAFT COULD NOT DUPLICATE
- [SDR DALA2026042902734](https://openairdocs.org/sdr/DALA2026042902734), Apr 26, 2026: ECU. FAILED. APU AUTO SHUTDOWN PROCESS BEGAN. RAN THE QRH WITH NO FIRE VISIBLE. APU WAS SHUT DOWN. THERE WAS AN ELECTRICAL SMELL IN THE AFT CABIN. R/R APU ECU REF B717 AMM 4
- [SDR DALA2026021801126](https://openairdocs.org/sdr/DALA2026021801126), Feb 10, 2026: VALVE. ODOR. DIRTY SOCK ODOR. REPLACED 35 DEGREE VALVE & MUFFLER IAW AMM 21-54. (8499820).
- [SDR DALA2026020900917](https://openairdocs.org/sdr/DALA2026020900917), Feb 1, 2026: UNKNOWN. ODOR. DIRTY SOCK ODOR DURING DESCENT AT 14,000 FT, ANTI-ICE WAS ON CABIN DID NOT NOTICE THE ODOR, STRONG ODOR IN COCKPIT. FOUND AN OIL/FUEL LIKE MIX TO COME OUT. INSP
- [SDR DALA2026010500070](https://openairdocs.org/sdr/DALA2026010500070), Jan 2, 2026: ENGINE. FIRE. REJECTED TAKEOFF AT 140 KNOTS DUE TO A LEFT ENGINE FIRE INDICATION. FOUND LEFT ENGINE INNER CORE PANELS DAMAGED AND BLOWN OUT. ALSO NOTED DAMAGED FIRE DETECTOR 
- [SDR DALA2025101707598](https://openairdocs.org/sdr/DALA2025101707598), Oct 14, 2025: IDG. FAULTED. SHIP 9547-MISC/DE- ON DESCENT THE CREW RECEIVED A "RT GEN OFF" MESSAGE WITH THE APU ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED 
- [SDR DALA2025101707599](https://openairdocs.org/sdr/DALA2025101707599), Oct 12, 2025: OIL SYSTEM. LEAKING. SHIP 9547 OIL FUMES PRESAENT IN COCKPIT AND FORWARS GALLEY WITH APU RUNNING AND LEFT PACK IN AUTO. COCKPIT SMELLED OF FRESH OIL & GALLEY SMELLED OF BURNED POPCO
- [SDR DALA2025051503782](https://openairdocs.org/sdr/DALA2025051503782), May 15, 2025: POWER SUPPLY. INOPERATIVE. FOUND EMERGENCY LIGHTS TO BE INOPERATIVE FOR THE TAILCONE HANDLE RELEASE AND WALKWAY. MAINTENANCE REPLACED B5-260 EMERGENCY LIGHTS BATTERY POWER SUPPLY AND BATT
- [SDR DALA2025042103073](https://openairdocs.org/sdr/DALA2025042103073), Apr 18, 2025: PAN. CRACKED. CRACK ON UPPER PAN. ALSO FWD EDGE PAN ON BEAM #2 CRACKED AT LH FWD EMERGENCY EXIT. SUMMARY OF NRC-00781: UPPER PAN AND ALSO FWD EDGE PAN CRACKS ON BEAM #2 AT LH
- [SDR DALA2025042103072](https://openairdocs.org/sdr/DALA2025042103072), Apr 18, 2025: SKIN. DAMAGED. WORN AND BENT ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1. ALSO LOOSE RIVETS ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA). 
- [SDR DALA2025041602960](https://openairdocs.org/sdr/DALA2025041602960), Apr 16, 2025: PAN. CRACKED. CRACK ON INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00139: INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO C
- [SDR DALA2025041202833](https://openairdocs.org/sdr/DALA2025041202833), Apr 12, 2025: CARGO TRACK. CORRODED. CORROSION ALONG OF LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0255: CORROSION LEVEL 2. LH TRACK BTW STA=1022-890, STA=898-8
- [SDR DALA2025040902760](https://openairdocs.org/sdr/DALA2025040902760), Apr 9, 2025: REPAIR. MISINSTALLED. FASTENER DISCREPANT INSTALLATION ON PREVIOUS FUSELAGE SKIN REPAIR, ALSO THERE ARE LIGHTNING STRIKES AT TWO LOCATIONS ADJACENT TO REPAIR FASTENERS AT AFT LH ALTE
- [SDR DALA2025040902758](https://openairdocs.org/sdr/DALA2025040902758), Apr 8, 2025: LONGERON. CORRODED. CORROSION ON LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT. SUMMARY OF NRC 0256: CORROSION LEVEL 2. LONGERON 30 STA=994-946, STA=927-908 AFT CARGO 
- [SDR DALA2025040802699](https://openairdocs.org/sdr/DALA2025040802699), Apr 4, 2025: VANE. DENTED. DENTS ON AFT MOVABLE VANE (LOWER SURFACE) AT LH WING. SUMMARY OF NRC 00468: AFT MOVABLE VANE (LOWER SURFACE) AT LH WING WAS REPAIRED PER ER/A 624886-14 REV ORIG
- [SDR DALA2025040802697](https://openairdocs.org/sdr/DALA2025040802697), Apr 4, 2025: SUPPORT. CRACKED. CRACKED ON SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00740: SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CA
- [SDR DALA2025040302494](https://openairdocs.org/sdr/DALA2025040302494), Apr 2, 2025: RETAINER. CRACKED. CRACK WAS FOUND ON RETAINER OF LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00878: CRACK ON RETAINER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ER/A 624944-14 REV
- [SDR DALA2025033102354](https://openairdocs.org/sdr/DALA2025033102354), Mar 29, 2025: REPAIR. CRACKED. CRACKED PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH. SUMMARY OF NRC 00334: PREVIOUS REPAIR DOUBLERS (2 EA)
- [SDR DALA2025033102351](https://openairdocs.org/sdr/DALA2025033102351), Mar 28, 2025: PAN. CRACKED. CRACKED INNER PAN OVER BEAM #4 AFT EDGE, AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00171: INNER PAN OVER BEAM #4 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REP
- [SDR DALA2025033102348](https://openairdocs.org/sdr/DALA2025033102348), Mar 27, 2025: SKIN. DENTED. PERFORM REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP. SUMMARY OF NRC 00637: SKIN BTW STA 237-256 B
- [SDR DALA2025033102346](https://openairdocs.org/sdr/DALA2025033102346), Mar 26, 2025: LONGERON. CRACKED. CRACK LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00456: LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCE
- [SDR DALA2025032502209](https://openairdocs.org/sdr/DALA2025032502209), Mar 24, 2025: LONGERON. CORRODED. CORROSION ON END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF THE NRC 00284: CORROSION LEVEL 2. END-LONGERON BTW STA 1002 LONGERON 2
- [SDR DALA2025032402190](https://openairdocs.org/sdr/DALA2025032402190), Mar 23, 2025: SUPPORT. CORRODED. CORROSION ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING. SUMMARY OF NRC 00770: CORROSION LEVEL 2. AREA ON INNER STRUCTURE OF RUDDER YOKE BEARING SUP
- [SDR DALA2025032402184](https://openairdocs.org/sdr/DALA2025032402184), Mar 21, 2025: ACCESS PANEL. CORRODED. CORROSION ON CONTACT AREA OF FUEL ACCESS PLATE 620QB. ALSO, CORROSION ON FASTENER HOLES OF PLATE 620JB AT RH WING. SUMMARY OF NRC 00604: CORROSION LEVEL 2. ACCE
- [SDR DALA2025032402183](https://openairdocs.org/sdr/DALA2025032402183), Mar 21, 2025: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK ON FUEL ACCESS PLATES 620GB, 620HB, 620CB, 620FT, 620DB, AND ARB0872-535 AT RH WING WAS FOUND. SUMMARY OF NRC 00602: CORROSION LEVEL 2.
- [SDR DALA2025032102133](https://openairdocs.org/sdr/DALA2025032102133), Mar 20, 2025: BARREL NUT. CORRODED. CORROSION ON HORIZONTAL STAB BARREL NUTS RH SIDE #13 AND #27. SUMMARY OF NRC 00800: LEVEL CORROSION 2. BARREL NUTS HORIZONTAL STAB RH SIDE #13 AND 27 WERE REPAI
- [SDR DALA2025031902066](https://openairdocs.org/sdr/DALA2025031902066), Mar 19, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS BTW STA Y=210 TO STA Y=218 X=-11, Y=180 TO STA Y=190 X=-56, STA Y=190 TO STA Y=198 X=54, STA Y=197 X=22 TO X=42 AND STA Y=180 X=-22 
- [SDR DALA2025031902062](https://openairdocs.org/sdr/DALA2025031902062), Mar 18, 2025: PAN. CRACKED. CRACK ON INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00532: INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIR
- [SDR DALA2025031401970](https://openairdocs.org/sdr/DALA2025031401970), Mar 14, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00649: CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID CABIN PASSENGER WAS REPA
- [SDR DALA2025031201904](https://openairdocs.org/sdr/DALA2025031201904), Mar 11, 2025: FRAME. CRACKED. CRACK AT FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00638: FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE WAS REPAIRED
- [SDR DALA2025031201902](https://openairdocs.org/sdr/DALA2025031201902), Mar 11, 2025: SKIN. DENTED. DENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BT
- [SDR DALA2025031201901](https://openairdocs.org/sdr/DALA2025031201901), Mar 11, 2025: SKIN. DENTED. DENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BT
- [SDR DALA2025031101891](https://openairdocs.org/sdr/DALA2025031101891), Mar 11, 2025: PAN. CRACKED. CRACKS ON INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FWD EDGE) AT FWD CARGO DOOR WERE FOUND. SUMMARY OF NRC 00501: INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FW
- [SDR DALA2025031101889](https://openairdocs.org/sdr/DALA2025031101889), Mar 11, 2025: FRAME. CRACKED. CRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B
- [SDR DALA2025031101892](https://openairdocs.org/sdr/DALA2025031101892), Mar 10, 2025: SKIN. CORRODED. -AD- CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG W/W AREA. SUMMARY OF NRC 00670: CORROSION LEVEL 1. CORROSION ON AFT EDGE LOWER 
- [SDR DALA2025031101887](https://openairdocs.org/sdr/DALA2025031101887), Mar 10, 2025: LONGERON. CRACKED. CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00652: CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL 
- [SDR DALA2025031001821](https://openairdocs.org/sdr/DALA2025031001821), Mar 8, 2025: LONGERON. CRACKED. CRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00794: CRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717
- [SDR DALA2025031001820](https://openairdocs.org/sdr/DALA2025031001820), Mar 8, 2025: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=660-665, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN,
- [SDR DALA2025030601745](https://openairdocs.org/sdr/DALA2025030601745), Mar 6, 2025: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=777-780, PER B717 SRM 51-10-02-0G PAR 8.F.(1). SUMMARY OF NRC 00832: CORROSION LEVEL
- [SDR DALA2025030501714](https://openairdocs.org/sdr/DALA2025030501714), Mar 5, 2025: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS, IN REF TO NRC 0642. CORROSION ON RH CUSP WEB STA Y=262-270, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN,
- [SDR DALA2025030501713](https://openairdocs.org/sdr/DALA2025030501713), Mar 5, 2025: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=389, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER
- [SDR DALA2025030501712](https://openairdocs.org/sdr/DALA2025030501712), Mar 5, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00650: CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN WAS REPA
- [SDR DALA2025021801195](https://openairdocs.org/sdr/DALA2025021801195), Feb 16, 2025: SKIN. DENTED. PERFORM PERMANENT REPAIR DUE TO DENT ON EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE. SUMMARY OF NRC 00299: EXTERNAL SKIN OF AFT CARGO DOOR L
- [SDR DALA2025030601774](https://openairdocs.org/sdr/DALA2025030601774), Dec 3, 2024: ACCESS DOOR. MISSING. -PDA- THE LEFT ELEVATOR LEFT CENTER HINGE NUT ACCESS LOWER DOOR IS MISSING. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED. FWD TO CDL 55-25-01, PLACARD INSTALLED
- [SDR DALA2024071607170](https://openairdocs.org/sdr/DALA2024071607170), Jul 14, 2024: STRINGER SPLICE. DAMAGED. STR 26L PRODUCTION SPLICE AREA, 1EA FASTENER SHOWS INDICATION WITH VISIBLE DAMAGE TO THE BACKSIDE OF THE STRINGER HOLE-LOCATED FIVE HOLES AFT OF PRODUCTION CUT 
- [SDR DALA2024071607169](https://openairdocs.org/sdr/DALA2024071607169), Jul 14, 2024: SKIN. DENTED. C/W ER/A 610260-14 REV B FUSELAGE SKIN DENTS. SUMMARY SEE NRC 004-0001:10-0653-8-7621/002 00006: COMPLIED WITH ER/A 610260-14 REV B. PRI REV "0", "1", "2", "3",

All 212: https://openairdocs.org/aircraft/N998AT/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/N998AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce TAY-651-54 engine: https://openairdocs.org/engine/rolls-royce-tay-651-54.md

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