# N701DH: 2026 Airbus S A S A321-271NX - Status: Valid registration - Airframe: [Airbus S A S A321-271NX](https://openairdocs.org/model/airbus-s-a-s-a321-271nx) (registry code 3930916, 246 seats) - Engine: [IAE PW1133GA-JM](https://openairdocs.org/engine/iae-pw1133ga-jm) (registry code 34598) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (Airbus SAS), [TCDS E00087EN](https://openairdocs.org/tcds/E00087EN) (International Aero Engines LLC) (OpenAirDocs) - Serial number: 13110 - Year built: 2026 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Experimental, operating kit built - Airworthiness date: June 25, 2026 - Certificate issued: March 18, 2026 - Expires: March 31, 2033 - Mode S code: A95898 - Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=701DH - Page: https://openairdocs.org/aircraft/N701DH 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): 83 in force ### Matched by airframe (Airbus S A S A321-271NX) - [AD 2026-17-04](https://openairdocs.org/ad/2026-17-04): Landing Gear · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Oct 1, 2026 - [AD 2026-18-03](https://openairdocs.org/ad/2026-18-03): Wings · Airbus A318-112, A319-115, A319-132 and 14 more. Effective Sep 18, 2026 - [AD 2026-15-13](https://openairdocs.org/ad/2026-15-13): Pneumatic · Airbus A319-151N, A319-153N, A319-171N and 19 more. Effective Sep 2, 2026 - [AD 2026-14-05](https://openairdocs.org/ad/2026-14-05): Communications · Airbus A319-151N, A319-153N, A319-171N and 19 more. Effective Aug 14, 2026 - [AD 2026-14-04](https://openairdocs.org/ad/2026-14-04): Fuselage · Airbus A319-111, A319-112, A319-113 and 56 more. Effective Aug 14, 2026 - [AD 2026-12-11](https://openairdocs.org/ad/2026-12-11): Fuselage · Airbus A321-251NX, A321-252NX, A321-253NX and 2 more. Effective Aug 3, 2026 - [AD 2026-12-02](https://openairdocs.org/ad/2026-12-02): Fuselage · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Jul 14, 2026 - [AD 2026-10-15](https://openairdocs.org/ad/2026-10-15): Fuselage · Airbus A318-111, A318-112, A318-122 and 35 more. Effective Jul 6, 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 2026-09-17](https://openairdocs.org/ad/2026-09-17): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Jun 18, 2026 - [AD 2026-09-16](https://openairdocs.org/ad/2026-09-16): Fuselage · Airbus A319-111, A319-112, A319-113 and 33 more. Effective Jun 18, 2026 - [AD 2026-11-04](https://openairdocs.org/ad/2026-11-04): Stabilizers · Airbus A319-111, A319-112, A319-113 and 40 more. Effective Jun 15, 2026 - [AD 2026-09-03](https://openairdocs.org/ad/2026-09-03): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Jun 12, 2026 - [AD 2026-09-06](https://openairdocs.org/ad/2026-09-06): Fuselage · Airbus A319-153N, A320-251N, A320-252N and 5 more. Effective May 26, 2026 - [AD 2026-03-10](https://openairdocs.org/ad/2026-03-10): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Apr 8, 2026 - [AD 2026-05-14](https://openairdocs.org/ad/2026-05-14): Turbine/turboprop engine · Airbus A319-171N, A319-173N, A320-271N and 7 more. Effective Mar 25, 2026 - [AD 2025-24-51](https://openairdocs.org/ad/2025-24-51): Flight controls · Airbus A319-111, A319-112, A319-113 and 37 more. Effective Jan 6, 2026 - [AD 2025-20-15](https://openairdocs.org/ad/2025-20-15): Fuselage · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 2, 2026 - [AD 2025-18-03](https://openairdocs.org/ad/2025-18-03): Oxygen · Airbus A318-111, A318-112, A318-121 and 70 more. Effective Oct 20, 2025 - [AD 2025-16-10](https://openairdocs.org/ad/2025-16-10): Flight controls · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Sep 22, 2025 - [AD 2025-16-04](https://openairdocs.org/ad/2025-16-04): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Sep 18, 2025 - [AD 2025-17-17](https://openairdocs.org/ad/2025-17-17): Landing Gear · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Sep 17, 2025 - [AD 2025-13-10](https://openairdocs.org/ad/2025-13-10): Wings · Airbus A319-111, A319-112, A319-113 and 36 more. Effective Aug 14, 2025 - [AD 2025-08-01](https://openairdocs.org/ad/2025-08-01): Doors · Airbus A321-251NX, A321-252NX, A321-253NX and 2 more. Effective Jul 2, 2025 - [AD 2025-10-07](https://openairdocs.org/ad/2025-10-07): Fuselage · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jun 26, 2025 - [AD 2025-10-05](https://openairdocs.org/ad/2025-10-05): Landing gear · Airbus A321-111, A321-112, A321-131 and 15 more. Effective Jun 26, 2025 - [AD 2025-02-04](https://openairdocs.org/ad/2025-02-04): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 17, 2025 - [AD 2024-26-05](https://openairdocs.org/ad/2024-26-05): Oxygen · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 87 more. Effective Mar 11, 2025 - [AD 2024-25-12](https://openairdocs.org/ad/2024-25-12): Landing gear · Airbus A319-111, A319-112, A319-113 and 35 more. Effective Mar 7, 2025 - [AD 2025-03-08](https://openairdocs.org/ad/2025-03-08): Flight Controls · Airbus A318-111, A318-112, A318-121 and 70 more. Effective Feb 26, 2025 - [AD 2024-26-04](https://openairdocs.org/ad/2024-26-04): Pneumatic · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Feb 18, 2025 - [AD 2024-24-10](https://openairdocs.org/ad/2024-24-10): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 13, 2025 - [AD 2024-24-09](https://openairdocs.org/ad/2024-24-09): Equipment/Furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 13, 2025 - [AD 2024-23-09](https://openairdocs.org/ad/2024-23-09): Equipment/Furnishings · Airbus A321-251NX, A321-252NX, A321-253NX and 2 more. Effective Jan 13, 2025 - [AD 2024-19-15](https://openairdocs.org/ad/2024-19-15): Oxygen · Safran Aerosystems Oxygen Cylinder, Valve Assembly, Oxygen Valve and 103 more. Effective Nov 26, 2024 - [AD 2024-11-01](https://openairdocs.org/ad/2024-11-01): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jul 3, 2024 - [AD 2024-08-08](https://openairdocs.org/ad/2024-08-08): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jun 6, 2024 - [AD 2024-06-07](https://openairdocs.org/ad/2024-06-07): Wings · Airbus A319-115, A320-214, A320-216 and 14 more. Effective May 22, 2024 - [AD 2023-25-05](https://openairdocs.org/ad/2023-25-05): Landing Gear, Electrical System Installation · Airbus A319-151N, A319-153N, A319-171N and 16 more. Effective Feb 7, 2024 - [AD 2023-10-07](https://openairdocs.org/ad/2023-10-07): Fuel · Airbus A319-151N, A319-153N, A319-171N and 16 more. Effective Nov 9, 2023 - [AD 2023-13-03](https://openairdocs.org/ad/2023-13-03): Doors · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Sep 5, 2023 - [AD 2023-13-01](https://openairdocs.org/ad/2023-13-01): Fuel · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jul 12, 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 2023-02-11](https://openairdocs.org/ad/2023-02-11): Doors · Airbus A321-251NX, A321-252NX, A321-253NX and 2 more. Effective Apr 17, 2023 - [AD 2022-24-14](https://openairdocs.org/ad/2022-24-14): Auto Flight · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Jan 18, 2023 - [AD 2020-25-03 R1](https://openairdocs.org/ad/2020-25-03-R1): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Jan 12, 2023 - [AD 2022-22-11](https://openairdocs.org/ad/2022-22-11): Flight Control System, Navigation · Airbus A319-151N, A319-153N, A319-171N and 16 more. Effective Dec 30, 2022 - [AD 2022-21-04](https://openairdocs.org/ad/2022-21-04): Equipment/Furnishings · Airbus A321-251NX, A321-252NX, A321-253NX and 2 more. Effective Oct 28, 2022 - [AD 2022-19-10](https://openairdocs.org/ad/2022-19-10): Equipment/furnishings · Airbus A321-251N, A321-251NX, A321-252NX and 3 more. Effective Oct 19, 2022 - [AD 2022-18-05](https://openairdocs.org/ad/2022-18-05): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Oct 13, 2022 ### Matched by engine (IAE PW1133GA-JM) - [AD 2025-26-04](https://openairdocs.org/ad/2025-26-04): Miscellaneous Hardware · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 15 more. Effective Feb 17, 2026 - [AD 2024-14-04](https://openairdocs.org/ad/2024-14-04): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 9 more. Effective Aug 20, 2024 - [AD 2024-06-14](https://openairdocs.org/ad/2024-06-14): Turbine Engine Compressor Section · International Aero Engines PW1124G1-JM, PW1127G-JM, PW1127GA-JM and 4 more. Effective Jun 3, 2024 - [AD 2024-05-11](https://openairdocs.org/ad/2024-05-11): Turbine Engine Compressor Section; Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 15 more. Effective Apr 11, 2024 - [AD 2023-20-11](https://openairdocs.org/ad/2023-20-11): Turbine Engine Compressor Section · International Aero Engines PW1124G1-JM, PW1127G-JM, PW1127GA-JM and 4 more. Effective Nov 1, 2023 - [AD 2023-16-07](https://openairdocs.org/ad/2023-16-07): Turbine Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 13 more. Effective Aug 28, 2023 - [AD 2021-19-10](https://openairdocs.org/ad/2021-19-10): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Sep 27, 2021 - [AD 2020-08-04](https://openairdocs.org/ad/2020-08-04): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective May 21, 2020 - [AD 2020-05-28](https://openairdocs.org/ad/2020-05-28): Turbine Engine Accessory Drive · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Apr 21, 2020 - [AD 2020-06-02](https://openairdocs.org/ad/2020-06-02): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Apr 6, 2020 - [AD 2019-25-01](https://openairdocs.org/ad/2019-25-01): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Dec 16, 2019 - [AD 2019-06-01](https://openairdocs.org/ad/2019-06-01): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Apr 10, 2019 - [AD 2018-22-02](https://openairdocs.org/ad/2018-22-02): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Dec 12, 2018 - [AD 2018-21-10](https://openairdocs.org/ad/2018-21-10): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Dec 12, 2018 - [AD 2018-13-03](https://openairdocs.org/ad/2018-13-03): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Jul 11, 2018 ### Historical (superseded or no longer in force) - [AD 2025-17-07](https://openairdocs.org/ad/2025-17-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Oct 1, 2025 - [AD 2025-16-12](https://openairdocs.org/ad/2025-16-12) (historical): Pneumatic · Airbus A319-151N, A319-153N, A319-171N and 19 more. Effective Aug 29, 2025 - [AD 2025-10-12](https://openairdocs.org/ad/2025-10-12) (historical): Fuselage · Airbus A319-111, A319-112, A319-113 and 55 more. Effective Jul 2, 2025 - [AD 2025-11-02](https://openairdocs.org/ad/2025-11-02) (historical): Communications · Airbus A319-151N, A319-153N, A319-171N and 18 more. Effective Jun 11, 2025 - [AD 2025-03-07](https://openairdocs.org/ad/2025-03-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 21, 2025 - [AD 2025-03-06](https://openairdocs.org/ad/2025-03-06) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 21, 2025 - [AD 2024-25-06](https://openairdocs.org/ad/2024-25-06) (historical): Landing Gear · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Dec 30, 2024 - [AD 2024-19-13](https://openairdocs.org/ad/2024-19-13) (historical): Time Limits/Maintenance Checks · Airbus A320-211, A320-212, A320-214 and 43 more. Effective Nov 26, 2024 - [AD 2024-04-07](https://openairdocs.org/ad/2024-04-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 22, 2024 - [AD 2024-04-03](https://openairdocs.org/ad/2024-04-03) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 19, 2024 - [AD 2023-25-09](https://openairdocs.org/ad/2023-25-09) (historical): Oxygen · Airbus A318-111, A318-112, A318-121 and 69 more. Effective Feb 7, 2024 - [AD 2023-13-11](https://openairdocs.org/ad/2023-13-11) (historical): Oxygen · AVOX Systems Oxygen valve assemblies (body and gage assemblies), Oxygen cylinder and valve assemblies, A300 B2-1A and 102 more. Effective Sep 5, 2023 - [AD 2023-13-10](https://openairdocs.org/ad/2023-13-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Sep 5, 2023 - [AD 2023-09-01](https://openairdocs.org/ad/2023-09-01) (historical): Pneumatic · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jun 26, 2023 - [AD 2023-05-02](https://openairdocs.org/ad/2023-05-02) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 18, 2023 - [AD 2023-04-06](https://openairdocs.org/ad/2023-04-06) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 10, 2023 - [AD 2022-24-05](https://openairdocs.org/ad/2022-24-05) (historical): Equipment/Furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 9, 2023 - [AD 2022-22-10](https://openairdocs.org/ad/2022-22-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Dec 30, 2022 - [AD 2022-09-16](https://openairdocs.org/ad/2022-09-16) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Jun 30, 2022 - [AD 2022-07-08](https://openairdocs.org/ad/2022-07-08) (historical): Time Limits/Maintenance Checks, Flight Controls · Airbus A318-111, A318-112, A318-121 and 43 more. Effective May 19, 2022 - [AD 2022-07-15](https://openairdocs.org/ad/2022-07-15) (historical): Landing gear · Airbus A318-111, A318-112, A318-121 and 43 more. Effective May 2, 2022 - [AD 2022-04-09](https://openairdocs.org/ad/2022-04-09) (historical): Oxygen System · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 94 more. Effective Apr 4, 2022 - [AD 2022-04-03](https://openairdocs.org/ad/2022-04-03) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Mar 30, 2022 - [AD 2021-20-08](https://openairdocs.org/ad/2021-20-08) (historical): Electrical Power · Airbus A318-111, A318-112, A318-121 and 72 more. Effective Nov 18, 2021 - [AD 2021-16-01](https://openairdocs.org/ad/2021-16-01) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Sep 28, 2021 - [AD 2021-18-08](https://openairdocs.org/ad/2021-18-08) (historical): Hydraulic Power · Airbus A319-171N, A320-271N, A320-272N and 5 more. Effective Sep 14, 2021 - [AD 2021-14-08](https://openairdocs.org/ad/2021-14-08) (historical): Navigation · Airbus A319-151N, A319-153N, A319-171N and 16 more. Effective Jul 1, 2021 - [AD 2020-25-03](https://openairdocs.org/ad/2020-25-03) (historical): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Dec 28, 2020 - [AD 2020-22-16](https://openairdocs.org/ad/2020-22-16) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Dec 10, 2020 - [AD 2020-21-11](https://openairdocs.org/ad/2020-21-11) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 20, 2020 - [AD 2020-21-10](https://openairdocs.org/ad/2020-21-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 19, 2020 - [AD 2020-20-05](https://openairdocs.org/ad/2020-20-05) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 19, 2020 - [AD 2020-16-01](https://openairdocs.org/ad/2020-16-01) (historical): Fire protection · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Aug 19, 2020 - [AD 2020-12-11](https://openairdocs.org/ad/2020-12-11) (historical): Auto Flight · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Jul 24, 2020 - [AD 2020-05-16](https://openairdocs.org/ad/2020-05-16) (historical): Wings · Airbus A319-115, A320-214, A320-216 and 11 more. Effective Apr 24, 2020 - [AD 2020-06-18](https://openairdocs.org/ad/2020-06-18) (historical): Flight controls · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 2, 2020 - [AD 2020-01-17](https://openairdocs.org/ad/2020-01-17) (historical): Equipment/ furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Feb 14, 2020 - [AD 2019-23-01](https://openairdocs.org/ad/2019-23-01) (historical): Time Limits/ Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 37 more. Effective Jan 9, 2020 - [AD 2019-19-15](https://openairdocs.org/ad/2019-19-15) (historical): Time Limits/ Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 36 more. Effective Nov 14, 2019 - [AD 2019-14-04](https://openairdocs.org/ad/2019-14-04) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 37 more. Effective Aug 29, 2019 - [AD 2019-03-17](https://openairdocs.org/ad/2019-03-17) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 36 more. Effective Apr 3, 2019 - [AD 2022-19-15](https://openairdocs.org/ad/2022-19-15) (historical): Turbine Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 7 more. Effective Nov 7, 2022 - [AD 2019-11-08](https://openairdocs.org/ad/2019-11-08) (historical): Turbine Engine Accessory Drive · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Jun 28, 2019 - [AD 2018-24-01](https://openairdocs.org/ad/2018-24-01) (historical): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Mar 15, 2019 All 127: https://openairdocs.org/aircraft/N701DH/ads.md ## Information bulletins (advisory) (2 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 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026 ## NTSB investigations None matched to N701DH. ## FAA accident and incident reports None matched to N701DH. ## Reports on N701DH not matched to an aircraft (1) They name N701DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20010508014059I](https://openairdocs.org/incident/20010508014059I), May 8, 2001: Boeing 72730C (N701DH), Syracuse, NY. (-23) On Tuesday, may 8, 2001, a Boeing 727, N701DH, flight 490, operated by dhl airways, experienced problems with the right main gear during landing. The… ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N701DH not matched to an aircraft (185, newest 50) They name N701DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DHL2001701010](https://openairdocs.org/sdr/DHL2001701010), May 19, 2001: HEAD. MALFUNCTIONED. AUTOPILOT MAKES GRADUAL UNCOMMAND RIGHT TURNS IN MANUAL MODE. DEFERRED IAW DHL MEL 22-1 CAT B MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED, DMI 5661. - [SDR DHL2001701011](https://openairdocs.org/sdr/DHL2001701011), May 18, 2001: COMPUTER. FAULTY. HDG MODE AIRCRAFT BANKS GREATER THAN 30 DEG ANGLE OF BANK, TRACKS 5 DEG LEFT OF SELECTED HDG, AND OVERSHOOTS IN TURNS TO THE SELECTED HDG BY 25 DEG. REPLACED RO - [SDR DHL2001701009](https://openairdocs.org/sdr/DHL2001701009), May 8, 2001: ACTUATOR. FAILED. RT MLG DID NOT GO DOWN. RT MLG EXTENDED WITH GOOD INDICATIONS AFTER COMPLETION OF ABNORMAL MANUAL GEAR EXTENSION. REPLACED RT MLG LOCK ACTUATOR PER B727 M/M 32- - [SDR DHL2001701006](https://openairdocs.org/sdr/DHL2001701006), Apr 28, 2001: COMPUTER. DEFECTIVE. AT FL330 AT M-805 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECT ON SERVO A. DEFERRED A MODE ON A/P PER DHL MEL 22-1-11A. PLACARD INSTALLED. REPLACED ROL - [SDR DHL2001701005](https://openairdocs.org/sdr/DHL2001701005), Apr 28, 2001: BUSHING. OUT OF ADJ. A/C REQUIRES 5 DEG RT BANK TO MAINTAIN STRAIGHT FLIGHT. ADJUSTED ECCENTRIC BUSHINGS OF RIGHT WING INBOARD AFT FLAP PER MM 27-51-2. - [SDR DHL2001701007](https://openairdocs.org/sdr/DHL2001701007), Apr 27, 2001: SENSOR. LOOSE. AT FL330 AT M.78 YOKE OSCILLATES BACK AND FORTH WITH AUTO-PILOT SELECTED ON SERVO-A. TIGHTENED CRANK ON A-SYS ELEVATOR POSITION SENSOR IAW B727 22-11-77 OP CK G - [SDR DHL2001701004](https://openairdocs.org/sdr/DHL2001701004), Mar 29, 2001: INDICATOR. MALFUNCTIONED. NR 3 LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAXI. QUANITY AND PRESS NORMAL. TRANSFERRED TO DMI PER MEL 79-4. VISUALLY VERIFIED OIL QUANITY FULL, CONTROL 4933 - [SDR DHL2001701003](https://openairdocs.org/sdr/DHL2001701003), Feb 28, 2001: INDICATOR. DEFECTIVE. NR 2 OIL PRESURE GAUGE BEGAN READING 20 PSI AT POSITION AND HOLD. PULLED-OFF RUNWAY AND SHUTDOWN ENGINE NR 2. TROUBLESHOT SYSTEM AND FOUND NR 2 ENGINE OIL PRESS - [SDR DHL2001701002](https://openairdocs.org/sdr/DHL2001701002), Feb 23, 2001: SUPPORT FITTING. CRACKED. DURING A POST-MOD INSPECTION OF PYLON, CRACKS WERE FOUND IN FWD ENGINE SUPPORT FITTING UPPER FLANGE BOLT HOLES E AND F. REPAIRED NR 3 ENGINE PYLON AT BOLT HOLES - [SDR DHL2001701001](https://openairdocs.org/sdr/DHL2001701001), Feb 12, 2001: SKIN. DELAMINATED. REFERENCE DMI 4025 RT O/B MID FLAP INSP OF REPAIR NEXT 30 DAYS AT 5 DAY INTERVALS TILL REPAIR COMPLETED. REMOVED TEMP REPAIR, INSTALLED PERM REPAIR RT O/B MID F - [SDR DHL2000701008](https://openairdocs.org/sdr/DHL2000701008), Nov 22, 2000: WINDOW. LEAKING. PRESSURIZATION LEAK OUT OF R-1 WINDOW. RETORQUED SCREWS ON R-1 WINDOW PER M/M 56-11-11. GROUND RAN A/C AND PRESSURIZED TO 4 PSI, NO LEAKS NOTED. - [SDR DHL2000701007](https://openairdocs.org/sdr/DHL2000701007), Nov 8, 2000: INDICATOR. MALFUNCTIONED. NR 2 EGT HIGH AFTER T/O. CLIMB THRUST SET, HAD TO PULL BACK THRUST LEVER ENGINE NR 2 TO KEEP EGT FROM EXCEEDING LIMITS. ENG NR 2 THRUST REDUCED TO EPR 1.58, N1 - [SDR DHL2000701006](https://openairdocs.org/sdr/DHL2000701006), Oct 2, 2000: FAIRING. MISSING. RT FWD WING TO BODY FAIRING MISSING FROM A/C ON ARRIVAL AT CVG. - [SDR DHL2000701005](https://openairdocs.org/sdr/DHL2000701005), Sep 24, 2000: STRUCTURE. CORRODED. FWD E&E COMPT-NOSE W/W RBL 146 WL 169 EXTRUSION OR CHORD HAS SPOTS OF CORROSION BETWEEN BS 328 AND BS 360.0 (RT WEB OF WALKWAY). REMOVED WALKWAY WL STA 294.5 TO - [SDR DHL2000701004](https://openairdocs.org/sdr/DHL2000701004), Sep 23, 2000: SCREW. LOOSE. IN FLIGHT A/C MOMENTARILY PULLS TO THE LEFT. WHEN CORRECTION APPLIED A/C RETURNS TO LEVEL. THIS IS INTERMITTENT AND AT ALL SPEEDS AND FLAP CONFIGURATIONS. ABOVE - [SDR DHL2000701003](https://openairdocs.org/sdr/DHL2000701003), Aug 2, 2000: STRUCTURE. VIBRATION. TAKEOFF REJECTED BECAUSE OF AIRCRAFT SHAKING AND VIBRATING AT 40-50 KTS. INSPECTED NOSE GEAR AND TIRES, NO DEFECTS. INSPECTED MLG AND TIRES, NO DEFECTS. CREW PE - [SDR DHL2000701002](https://openairdocs.org/sdr/DHL2000701002), Jul 27, 2000: CONNECTOR. LOOSE. ON INITAL GEAR EXTENSION NOSE GEAR AGREE LIGHT DID NOT ILLUMINATE. WARNING HORN SOUNDED AT FLAPS 30. NORMAL INDICATION UPON COMPLETION OF ABNORMAL PROCEDURES. M - [SDR DHL9970101A](https://openairdocs.org/sdr/DHL9970101A), Aug 29, 1999: WEB. CRACKED. AT A CHECK, 3.5 INCH CRACK NOSE WHEEL WELL 15 AFT OF FWD BULKHEAD LEFT SIDE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER PER SRM 41-40-2. - [SDR DHL99701001](https://openairdocs.org/sdr/DHL99701001), Jul 7, 1999: MOTOR. LEAKING. HAD A SYSTEM HYDRAULIC FAILURE. FOUND OUTBD FLAP POWER UNIT HYDRAULIC MOTOR LEAKING. REMOVED AND REPLACED PER MM 27-51-62 LEAK CHECK GOOD SERVICED SYSTEM. - [SDR DHL9970153D](https://openairdocs.org/sdr/DHL9970153D), Apr 16, 1999: FITTING. CRACKED. AT D-CHECK, LEFT WING O/B AILERON O/B HINGE FITTING CRACKED AT AFT UPPER END AT SKIN ATTACH FLANGE. REMOVED O/B HINGE FITTING AT LEFT WING PER SRM 51-30-2. REPL - [SDR DHL9970165D](https://openairdocs.org/sdr/DHL9970165D), Apr 12, 1999: STRINGER. CRACKED. AT D-CHECK, EAR CRACKED ON AFT SIDE OF FWD VENT STRINGER WS 601. INSTALLED REPAIR PER S/B 57A159, 11 INCHES LONG. - [SDR DHL9970162D](https://openairdocs.org/sdr/DHL9970162D), Apr 12, 1999: BRACKET. CRACKED. AT D-CHECK, BRACKET SUPPORT FOR AFT CARGO COMPT UP LATCH CRACKED. REMOVED BRACKET SUPPORT, REPLACED SUPPORT PER SRM 51-10-1, 17 X 7. - [SDR DHL9970112D](https://openairdocs.org/sdr/DHL9970112D), Apr 8, 1999: SKIN. DENTED. AT D-CHECK, FUSELAGE SKIN DENTED AT APPROX STA 1343 FROM STR 21R TO S-20R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 12 X 8' PER SRM 53-30-3. - [SDR DHL9970105D](https://openairdocs.org/sdr/DHL9970105D), Apr 6, 1999: FLOORBEAM. CORRODED. AT D-CHECK, FUSE FLOORBEAM CORRODED AT STA 380 BL 49L. CUT OUT FLOORBEAM TO LBL 49. CUT FLOORBEAM CAP OUT FROM LBL 12 TO O/B END. FABRICATED NEW FLOORBEAM TOP C - [SDR DHL9970114D](https://openairdocs.org/sdr/DHL9970114D), Apr 1, 1999: BULKHEAD WEB. CRACKED. AT D-CHECK, FWD BULKHEAD STA 178 CRACKED. CUT OUT DAMAGED AREA, INSTALLED WEB REPAIR PER SRM 53-10-9, 9.5 X 5. - [SDR DHL9970113D](https://openairdocs.org/sdr/DHL9970113D), Apr 1, 1999: BULKHEAD ANGLE. CORRODED. AT D-CHECK, FWD BULKHEAD STA 178 LOWER CHORD ANGLE CORRODED. REMOVED AND REPLACED LOWER CHORD ANGLE PER SRM 53-10-2. - [SDR DHL9970158D](https://openairdocs.org/sdr/DHL9970158D), Mar 31, 1999: RIB. CRACKED. AT D-CHECK, NR 6 L/E SLAT NR 3 RIB CRACKED AT BOTTOM RADIUS. REMOVED AND REPLACED NR 3 RIB PER SRM 51-30-2. - [SDR DHL9970101D](https://openairdocs.org/sdr/DHL9970101D), Mar 31, 1999: SKIN. DENTED. AT D-CHECK, LT WING LEADING EDGE HAS LARGE DENT JUST AFT OF NR 1 SLAT O/B SIDE. CUT OUT DAMAGED AREA , INSTALLED REPAIR PER SRM 57-30-4, 7 X 12. - [SDR DHL9970139D](https://openairdocs.org/sdr/DHL9970139D), Mar 30, 1999: SKIN. DELAMINATED. AT D-CHECK, LEADING EDGE FLAP LOWER SURFACE DELAMINATED. INSTALLED FILLER REPAIRS PER SRM 51-40-1, 30 X 2. - [SDR DHL9970138D](https://openairdocs.org/sdr/DHL9970138D), Mar 30, 1999: FAIRING. CRACKED. AT D-CHECK, NR 2 FLAP TRACK MOVEABLE FAIRING HAS SKIN CRACKED AT FWD BOTTOM END. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 4 X 2.75. - [SDR DHL9970137D](https://openairdocs.org/sdr/DHL9970137D), Mar 30, 1999: SKIN. GOUGED. AT D-CHECK, LEFT WING L/E SKIN GOUGED AT NR 1 SLAT STA 433 I/B OF TIP. CUT OUT DAMAGED AREA, INSTALLED REPAIR PARTS PER SRM 57-30-4, 6 X 3. - [SDR DHL9970115D](https://openairdocs.org/sdr/DHL9970115D), Mar 30, 1999: FAIRING. CRACKED. AT D-CHECK, LEFT WING FUSE FAIRING HAS CRACK. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 51-30-2, 6 X 4. - [SDR DHL9970169D](https://openairdocs.org/sdr/DHL9970169D), Mar 29, 1999: BRACKET. CRACKED. AT D-CHECK, RT WING O/B BRACKET CRACKED AT MLG BEAM PANEL AND NR 8 SPOILER ACTUATOR BRACKET. FABRICATED NEW BRACKET SUPPORT PER SRM 57-20-1, 9 X 5. - [SDR DHL9970157D](https://openairdocs.org/sdr/DHL9970157D), Mar 29, 1999: SUPPORT. CRACKED. AT D-CHECK, RT WING NR 6 L/E SLAT O/B TRACK O/B VERTICAL SUPPORT FLANGE CRACKED. REMOVED O/B TRACK, REMOVED AND REPLACED VERTICAL SUPPORT RIB PER SRM 51-30-2. - [SDR DHL9970156D](https://openairdocs.org/sdr/DHL9970156D), Mar 29, 1999: RIB. CRACKED. AT D-CHECK, RT WING NR 6 L/E SLAT I/B TRACK I/B VERTICAL SUPPORT FLANGE CRACKED. REMOVED AND REPLACED VERTICAL RIB PER SRM 51-10-1. - [SDR DHL9970151D](https://openairdocs.org/sdr/DHL9970151D), Mar 29, 1999: CHORD. CRACKED. AT D-CHECK, LT HORIZ STAB REAR LOWER CHORD HAVE HOLES AND TRIM OUTS. REPAIRED LOWER CHORD PER AVITAS EO 99AVHM012R0-1. - [SDR DHL9970148D](https://openairdocs.org/sdr/DHL9970148D), Mar 29, 1999: SEAT TRACK. CORRODED. AT D-CHECK, NR 7 CABIN FLOOR TRACK HAS CORROSION SPOTS AT STA 580, 680, 700 AND 720. REMOVED TRACK FROM 670 TO 740 AND REINSTALLED. REMOVED SEAT TRACK FROM 530 - [SDR DHL9970147D](https://openairdocs.org/sdr/DHL9970147D), Mar 29, 1999: SEAT TRACK. CORRODED. AT D-CHECK, FWD END OF NR 3 SEAT TRACK HAS INNER GRANULAR CORROSION. REMOVED AND INSTALLED SEAT TRACK PER SRM 53-10-5 20 LONG. - [SDR DHL9970131D](https://openairdocs.org/sdr/DHL9970131D), Mar 29, 1999: SUPPORT. GOUGED. AT D-CHECK, LT HORIZONTAL STAB NR 2 SUPPORT ELEVATOR HAS A GOUGE IN IT. REPLACED SUPPORT PER S/B 55-72. - [SDR DHL9970130D](https://openairdocs.org/sdr/DHL9970130D), Mar 29, 1999: ANGLE. CRACKED. AT D-CHECK, RIGHT I/B LEADING EDGE WEB AT LEADING EDGE STA 130 I/B SIDE UPPER OLD ANGLE REPAIR CRACKED. REMOVED ANGLE REPAIR, INSTALLED ANGLE REPAIR PER SRM 51- - [SDR DHL9970129D](https://openairdocs.org/sdr/DHL9970129D), Mar 29, 1999: ANGLE. CRACKED. AT D-CHECK, RIGHT WING I/B LEADING EDGE STA 130 I/B LOWER ATTACH ANGLE CRACKED AT ATTACH FASTENER. REMOVED CRACKED ANGLE SUPPORT, REPLACED ANGLE SUPPORT AND INS - [SDR DHL9970104D](https://openairdocs.org/sdr/DHL9970104D), Mar 29, 1999: FITTING. CORRODED. AT D-CHECK, RT WING NR 5 FLAP CENTER HINGE SUPPORT FITTING O/B FLANGE ATTACH HOLE CORRODED. REMOVED AND REPLACED SUPPORT FITTING PER SRM 57-50-2. - [SDR DHL9970103D](https://openairdocs.org/sdr/DHL9970103D), Mar 29, 1999: CASTING. CORRODED. AT D-CHECK, LEFT WING I/B AILERON LOWER INPUT CASTING IS CORRODED. REMOVED AND REPLACED CASTING PER SRM 59-50-1. REBALANCE NOT REQD PER SRM 51-80-1. RERIGGED PE - [SDR DHL9970154D](https://openairdocs.org/sdr/DHL9970154D), Mar 28, 1999: CASTING. CORRODED. AT D-CHECK, LEFT AILERON LOCKOUT SUPPORT CASTING IS PITTED AT ALL THRU BOLT ATTACH POINTS. REMOVED AND REPLACED SUPPORT CASTING PER SRM 51-30-2. - [SDR DHL9970102D](https://openairdocs.org/sdr/DHL9970102D), Mar 28, 1999: FLAP. GOUGED. AT D-CHECK, LEFT HANED O/B FOREFLAP LEADING EDGE I/B OF NR 1 FLAP TRACK IS GOUGED AT PREV REPAIR. REMOVED AND REPLACED REPAIR PER SRM 57-50-4, 6 X 3. - [SDR DHL9970136D](https://openairdocs.org/sdr/DHL9970136D), Mar 27, 1999: PANEL. DISBONDED. AT C-CHECK, PANEL NR 8342 L/E SEPARATED AND O/B CORNER CRACKED. INSTALLED BONDED REPAIR PER SRM 51-40-6, 20 X 10. - [SDR DHL9970118D](https://openairdocs.org/sdr/DHL9970118D), Mar 27, 1999: FRAME. CORRODED. AT D-CHECK, CORROSION ON ANCHOR NUTS AND ATTACH MOUNTS OF DOOR FRAME BS 580 STR 25R TO 26R. CORROSION OUT OF LIMITS, INSTALLED REPAIR PER SRM 51-40-2, 5.5 X 10. - [SDR DHL9970117D](https://openairdocs.org/sdr/DHL9970117D), Mar 27, 1999: ANGLE. CORRODED. AT D-CHECK, FWD LAV FLOOR SUPPORT CORRODED ON UPPER SURFACE STA 330 TO 340 RBL 15. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2. - [SDR DHL9970116D](https://openairdocs.org/sdr/DHL9970116D), Mar 27, 1999: ANGLE. CORRODED. AT D-CHECK, FWD LAV FLOOR SUPPORT ANGLE AT DOOR FWD LOWER CORNER IS CORRODED ON LOWER SIDE APPROX STA 325 RBL 14. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51- - [SDR DHL9970168D](https://openairdocs.org/sdr/DHL9970168D), Mar 26, 1999: FITTING. CORRODED. AT D-CHECK, VERTICAL FIN RT HORIZ STAB STAINLESS RUB BLOCK STRIP OVER VERTICAL FIN BULGED. REMOVED AND REPLACED VERTICAL FITTING PER SRM 55-30-2. All 185: https://openairdocs.org/aircraft/N701DH/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (91, 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 (Airbus S A S A321-271NX) - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [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 ST02528LA](https://openairdocs.org/stc/ST02528LA): Installation of the Thales Avionics, Inc. Data Transfer Device (DTD) or Solid State Drive (SSD) into the existing Cabin Media Loader (CML). Thales Avionics Inc - [STC ST04498AT](https://openairdocs.org/stc/ST04498AT): Interior Reconfiguration of an Airbus A321-271NX. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC ST04474NY](https://openairdocs.org/stc/ST04474NY): Activation of Wireless Local Area Network (WLAN) system. Jet Aviation AG - [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects - [STC ST09850DS](https://openairdocs.org/stc/ST09850DS): Series Starlink to IFE & AID Interface Installation. United Airlines - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [STC ST03416NY](https://openairdocs.org/stc/ST03416NY): Installation of Intelsat Connectivity Antenna (with demod option). Delta Engineering Corporation - [STC ST02913NY](https://openairdocs.org/stc/ST02913NY): Installation of a Panasonic Avionics Corporation Global Communications Suite (GCS) and/or In-Flight Entertainment System. Delta Engineering Corporation - [STC ST01700AT-D](https://openairdocs.org/stc/ST01700AT-D): Installation of Airshow 420 System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists A321 Series - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03741NY](https://openairdocs.org/stc/ST03741NY): Viasat KA SATCOM Antenna System Installation, approve configurations. ALOFT AeroArchitects - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc - [STC ST12325SE](https://openairdocs.org/stc/ST12325SE): Installation of the SpaceX Starlink Aero Terminal. Space Exploration Technologies Corp./Starlink Aviation - [STC ST12326SE](https://openairdocs.org/stc/ST12326SE): SpaceX Starlink Aviation System Installation and Activation. Space Exploration Technologies Corp./Starlink Aviation - [STC ST03742NY](https://openairdocs.org/stc/ST03742NY): Viasat KA Cabin Distribution System Installation. ALOFT AeroArchitects - [STC ST02890NY](https://openairdocs.org/stc/ST02890NY): Installation of a Panasonic Avionics Corporation Global Communications Suite Antenna. Delta Engineering Corporation - [STC ST04759NY](https://openairdocs.org/stc/ST04759NY): Installation of a single cockpit USB charger. Eirtech Aviation Services Inc - [STC ST02356LA](https://openairdocs.org/stc/ST02356LA): Installation of Inflight Warning Systems Fan Vibration Monitor Unit. Astronics Advanced Electronic Systems (AES) - [STC ST02699LA](https://openairdocs.org/stc/ST02699LA): Installation of Vogt Aero Nickel Cadmium Battery P/N 2758-LMVA or 2758-RMVA. Vogt Aero LLC - [STC ST12229IB](https://openairdocs.org/stc/ST12229IB): Installation of Thinkom antenna on the top rear fuselage. EAD Aerospace Airworthiness T/A Eclipse Technics - [STC ST04288CH](https://openairdocs.org/stc/ST04288CH): Installation of an Automatic Dependent Surveillance Broadcast Out (ADS-B Out) Transponder System with Honeywell Integrated Multi-Mode Receiver (IMMR), Model Number IMMR 20.1 installed with TSO-C190 compliant GPS antenna. Amphenol Cable and Interconnect Technologies Inc - [STC ST04292CH](https://openairdocs.org/stc/ST04292CH): Installation of JADE SATCOM Antenna System Provisions. Amphenol Cable and Interconnect Technologies Inc - [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF - [STC ST12056IB](https://openairdocs.org/stc/ST12056IB): The Manufacture and Installation of External Printed Aircraft Graphics Film. Libellule Monde Inc - [STC ST03417NY](https://openairdocs.org/stc/ST03417NY): Installation with demod option of Intelsat Cabin Connectivity System. Delta Engineering Corporation - [STC ST02717LA](https://openairdocs.org/stc/ST02717LA): Upgrade of T3CAS and installation of ACSS SafeRoute+TM ADS-B In System. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST04089NY](https://openairdocs.org/stc/ST04089NY): Installation of Cabin Seating. Delta Engineering Corporation - [STC ST04798NY](https://openairdocs.org/stc/ST04798NY): AAR Engineering Services Seat Re-pitch. Delta Engineering Corporation - [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 ST02626CH](https://openairdocs.org/stc/ST02626CH): Installation of ECS EZMount® mechanical mounting assemblies on lower frames of cockpit sliding windows. Amphenol Cable and Interconnect Technologies Inc - [STC ST04328CH](https://openairdocs.org/stc/ST04328CH): Installation and activation of the RAVE Wireless Broadband System. Amphenol Cable and Interconnect Technologies Inc - [STC ST04334CH](https://openairdocs.org/stc/ST04334CH): Installation and activation of an ARINC 791 SATCOM System. Amphenol Cable and Interconnect Technologies Inc - [STC ST04287CH](https://openairdocs.org/stc/ST04287CH): The Certification for Transmitting Portable Electronic Device (TPED). Amphenol Cable and Interconnect Technologies Inc - [STC ST11872IB](https://openairdocs.org/stc/ST11872IB): Installation of Iridium Antenna. Aerotec Concept - [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST02716SE](https://openairdocs.org/stc/ST02716SE): Conversion of an Airbus A321-200 passenger configuration airplane to a freighter configuration. 321 Precision Conversions LLC - [STC ST02744LA](https://openairdocs.org/stc/ST02744LA): Installation of the Thales In-Flight Entertainment System. Thales Avionics Inc - [STC ST04071NY](https://openairdocs.org/stc/ST04071NY): Installation of VisionSafe Emergency Vision Assurance System (EVAS). VisionSafe LLC - [STC ST02814CH](https://openairdocs.org/stc/ST02814CH): Installation of Rosemount Aerospace Electronic Flight Bag (EFB) System and Provisions. Rosemount Aerospace Inc - [STC ST09939AC](https://openairdocs.org/stc/ST09939AC): Installation of the Spacex Starlink Aviation Satcom System. Space Exploration Technologies Corp./Starlink Aviation - [STC ST04577AT](https://openairdocs.org/stc/ST04577AT): Installation of the ARTEX 4000 Emergency Locator Transmitter (ELT) System. Woven Electronics LLC - [STC ST00156IB](https://openairdocs.org/stc/ST00156IB): Removal of the linefit Moveable Class Divider (MCD) and installation of replacement by a customized lateral MCD. Airbus S.A.S - [STC ST00143IB](https://openairdocs.org/stc/ST00143IB): Installation of the ACES Inc. Seat Table Inset (STI) Assembly, Part Number 2521-4002, at the Middle Seat in the First Three (3) Left-Hand and Right-Hand Rows. ACES Inc - [STC ST00126IB](https://openairdocs.org/stc/ST00126IB): Replacement of Halon agent with alternate Halon-free Portable Fire Extinguisher agent. AMAC Aerospace Switzerland AG - [STC ST02267NY](https://openairdocs.org/stc/ST02267NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG - [STC ST02768SE](https://openairdocs.org/stc/ST02768SE): Installation of a Pexco AirShield. Pexco Aerospace Inc All 91: https://openairdocs.org/aircraft/N701DH/stcs.md ## Related - Other Airbus S A S A321-271NX aircraft: https://openairdocs.org/model/airbus-s-a-s-a321-271nx/aircraft.md - The IAE PW1133GA-JM engine: https://openairdocs.org/engine/iae-pw1133ga-jm.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.