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Atlas / TCDS / A00018AT

FAA · Type Certificate Data Sheet

TCDS A00018AT

Honda Aircraft Company LLC

Current Aircraft Small Airplane Rev 2 12/22/2016 drs.faa.gov ↗

Models covered (1)

Applicable airworthiness directives (18)

ADs joined from the FAA Federal Register by (Honda Aircraft Company LLC × model). Click any AD to see the full Federal Register record. Mandatory; flying out of compliance grounds the airplane.

  • 2026-10606 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2026-05-28
  • 2026-06527 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2026-04-03
  • 2026-01198 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2026-01-22
  • 2026-00454 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2026-01-13
  • 2025-23719 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2025-12-23
  • 2025-12555 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2025-07-07
  • 2025-06070 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2025-04-11
  • 2023-11636 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2023-06-01
  • 2022-19021 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2022-09-02
  • 2022-05222 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2022-03-14
  • 2021-24097 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2021-11-04
  • 2021-21104 Airworthiness Directives; Honda Aircraft Company, LLC Airplanes 2021-09-30
  • 2020-05891 Airworthiness Directives; Honda Aircraft Company LLC 2020-03-20
  • 2018-22750 Airworthiness Directives; Honda Aircraft Company LLC 2018-10-23
  • 2018-15978 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2018-08-07
  • 2018-12127 Airworthiness Directives; Honda Aircraft Company LLC 2018-06-07
  • 2018-11067 Airworthiness Directives; Honda Aircraft Company LLC Airplanes 2018-05-24
  • 2018-06091 Airworthiness Directives; Honda Aircraft Company LLC 2018-03-29

Special Conditions + ELOS findings

Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.

  • SC 23-271-SC Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Cruise Speed Control System
  • SC 23-269-SC Special Conditions: Honda Aircraft Company, Model HA-420 HondaJet, Lithium-ion Batteries
  • SC 23-270-SC Special Conditions: Honda Aircraft Company, Model HA-420, HondaJet; Ventilation Requirements in High Altitude Operations
  • SC 23-265-SC Special Conditions: Honda Aircraft Company, Model HA-420; Fire Extinguishing for Overwing Pylon Mounted Engines
  • ELOS ACE-15-09 Rev 1 Equivalent Level of Safety (ELOS) Finding for Honda Aircraft Company, Model HA-420 (HondaJet), Digital Display Only,
  • ELOS AT16447AT-A-A-1 Material Strength Properties and Design Values Requirements of § 23.613 for the Honda Model HA-420 Aircraft
  • ELOS AT15774AT-A-F-1 Steep Approach to Landing
  • ELOS ACE-15-11 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft Company, Model HA-420 (HondaJet), Airspeed Indicator (ASI) Flap Markings, Project TC9438AT-A
  • ELOS ACE-15-15 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft, Model HA-420 (HondaJet), 14 CFR part 23, Amendment 23-62: Project TC9438AT-A
  • ELOS ACE-15-08 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft Company, Model HA-420, Use of 1-g Stall Speed in lieu of Minimum Speed in Stall as a Basis for Determining Compliance, Project #: TC9438AT-A
  • ELOS ACE-15-09 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft Company, Model HA-420 (HondaJet), Digital Display Only, Project TC9438AT-A
  • ELOS ACE-15-10 INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft, Model HA-420 (HondaJet), Battery System, Project TC9438AT-A

Certification basis — 14 CFR

Specific sections

  • Sec. 1.1
  • Sec. 1.2
  • Sec. 23.2
  • Sec. 23.3
  • Sec. 21.21
  • Sec. 23.13
  • Sec. 23.45
  • Sec. 23.49
  • Sec. 23.51
  • Sec. 23.63
  • Sec. 23.65
  • Sec. 23.67
  • Sec. 23.69
  • Sec. 23.73
  • Sec. 23.77
  • Sec. 23.143
  • Sec. 23.145
  • Sec. 23.147
  • Sec. 23.149
  • Sec. 23.157
  • Sec. 23.161
  • Sec. 23.175
  • Sec. 23.177
  • Sec. 23.181
  • Sec. 23.201
  • Sec. 23.203
  • Sec. 23.207
  • Sec. 23.221
  • Sec. 23.251
  • Sec. 23.253
  • Sec. 23.561
  • Sec. 23.562
  • Sec. 23.571
  • Sec. 23.729
  • Sec. 23.735
  • Sec. 23.785
  • Sec. 23.791
  • Sec. 23.831
  • Sec. 23.1001
  • Sec. 23.1195
  • Sec. 23.1197
  • Sec. 23.1199
  • Sec. 23.1201
  • Sec. 23.1305
  • Sec. 23.1309
  • Sec. 23.1325
  • Sec. 23.1329
  • Sec. 23.1337
  • Sec. 23.1353
  • Sec. 23.1545
  • Sec. 23.1549
  • Sec. 23.1553
  • Sec. 23.1581
  • Sec. 23.1583
  • Sec. 23.1587
  • Sec. 23.75
  • Sec. 21.183

Fleet view · 231 registered tails

Engineering specs aggregated from the FAA Aircraft Registry — what every actually-flying tail under this TCDS reports. Median + 10th–90th-percentile range across the active fleet.

Seats

8

n=231

Year of mfr

2019

2015–2026

Engines on the type, by tail count

  • GE HONDA HF-120 207

NTSB events

38

across all model variants

Applicable ADs

17

FAA airworthiness directives

Per-tail rate

0.16 events / tail · 0.07 ADs / tail

The TCDS PDF on drs.faa.gov is the authoritative document for design-as-certified weight limits, performance, equipment, AD compliance times, and operating limitations. Open on drs.faa.gov ↗ DRS frequently breaks — when it does, the fleet view above and the cross-links below are usually what you actually need.