Cessna 206 Stationair — U.S. Fleet History & Risk Data
Piston · 2,552 aircraft on the U.S. registry · built 1918–2026
NTSB records whose airframe serial does not match the aircraft currently holding the registration are excluded, as are service difficulty reports filed while a registration belonged to a different aircraft. U.S. registrations get reused; these counts are reconciled to the airframes actually in this fleet.
Where this fleet reports maintenance difficulties
FAA Service Difficulty Reports filed against Cessna 206 Stationair airframes, grouped by JASC system chapter — a factual picture of what mechanics actually report on this type.
- 85 — Reciprocating Engine : 71 reports
- 74 — Ignition : 37 reports
- 24 — Electrical Power : 27 reports
- 32 — Landing Gear : 24 reports
- 27 — Flight Controls : 21 reports
Recent airworthiness directives matched to this type
- AD 2025-11-09 (recurring) · effective 2025-07-11 — reports of mis-wired fire extinguishing bottles
- AD 2024-15-09 · effective 2024-10-22 — report of the potential for a failure of the ATLAS system in which a loss of load alleviation would be un-annunciated
- AD 2020-18-01 (recurring) · effective 2020-11-12 — The FAA is adopting a new airworthiness directive (AD) for certain Textron Aviation Inc. (Textron) Model 172N, 172P, 172Q, 172RG, F172N, F172P, FR172K, R172K, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, T182, F182P, F182Q, FR182, R182, TR182, 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 207, 207A, T207, T207A, 210-5 (205), 210-5A (205A), 210B, 210C, 210D, 210E, 210F, and T210F airplanes. This AD was prompted by crack
- AD 2011-10-09 (recurring) · effective 2011-06-17 — We are superseding an existing airworthiness directive (AD) for Cessna Aircraft Company (Cessna) 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 series airplanes. That AD currently requires repetitive inspections and replacement of parts, if necessary, of the seat rail and seat rail holes; seat pin engagement; seat rollers, washers, and axle bolts or bushings; wall thickness of roller housing and the tang; and lock pin springs. This new AD requires retaining all of the actions from the previous AD and adding steps to the inspection procedures in th
- AD 2008-26-10 · effective 2010-11-16 — The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to the products listed above. In the Information Heading and in the SUMMARY section of the published AD, we incorrectly included Cessna 188 series airplanes. In the Unsafe Condition section, we incorrectly designated that paragraph as (e) instead of (d). Also in the Compliance section, paragraph (f)(2), and in Figure 1, we incorrectly stated the mailing address for the report. We are issuing this document to help eliminate any confusion that this AD may have created in the Informat
ADs published since 1994 in our Federal Register database — the full list of directives applicable to an older airframe is longer; build it at drs.faa.gov. Open/superseded status reflects our last sync. Compliance for a specific airframe can only be verified in its logbooks — that's exactly what our per-aircraft report flags.