STC ST01249NY
FAA DRS lists ST01249NY as Current · Amended, held by Aero Consulting Services Ltd, for Bombardier DHC-8-100 Series, Bombardier DHC-8-200 Series, and Bombardier DHC-8-300 Series. Recorded change: Installation of Take-off Configuration Test Switch and Nose Landing Gear Pin Position Switch. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Take-off Configuration Test Switch and Nose Landing Gear Pin Position Switch.
ST01249NY identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Bombardier DHC-8-100 Series, Bombardier DHC-8-200 Series, and Bombardier DHC-8-300 Series. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Bombardier DHC-8-100 Series and Bombardier DHC-8-200 Series, and 1 more aircraft configuration model, serial range, and configuration?
- 02Which gear, wheel, brake, tire, and hydraulic configurations apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related landing gear and brakes STCs
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Installation of external cargo rack and work platform between the skid gears. Limited to installation on serial number 911079D.
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Installation of an auxiliary electric Hydraulic Pump System in accordance with Simuflight, Seattle Modification and Installation Procedure Instruction Report SS-900. NOTE: This system augments the existing manually operated hydraulic system for the landing gear and flap operation.
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Installation of a machined wrought 2024-T351 tail wheel collar (Republic P/N 1126) in place of a die-forged 2014-T6 original part in accordance with Simuflight, Seattle Drawing Number SP-2000.
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