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Aircraft record

N214962009 Schweizer 269C-1

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:1 NTSB accident (substantial damage, Nov 2015)3 ADs may apply

Registration
Valid
expires May 31, 2030
Based in
Hobbs, NM
owner city / state
Engine
HIO-360-G1A · 180 hp
Lycoming
Owners
1
since 2023
NTSB events
1
substantial, 2015
ADs may apply
3
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Danos Oilfield Service LLC
Owner type
LLC
City, state
Hobbs, NM
Certificate issued
May 14, 2023
Expires
May 31, 2030
Airworthiness
Standard · Normal
Airworthiness date
May 14, 2009

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Schweizer
Model
269C-1
Year
2009
Serial number
0358
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
4H12
Mode S code
A1CC10

Engine

Make and model
Lycoming Hio-360-G1a
Type
Reciprocating
Power
180 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2023 – nowDanos Oilfield Service LLCHobbs, NM · current
  2. 2003Pilot International INCValley Center, KS · different airframe: 2003 Cessna T206h S/N T20608422
  3. 1953 – 1955Individual ownerPryor, OK · different airframe: Piper J-3 S/N 2205
Show all 4 registrations
  1. until 1977Individual ownerByers, TX · different airframe: Cessna 172m S/N 17263958

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Nov 4, 2015 · Mount Pocono, PA

The student pilot's failure to remove the tension applied to the cyclic before takeoff, which resulted in a loss of directional control and the tail rotor striking the ground.

Damage
Substantial
Injuries
None
Report
GAA16CA045

From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA16CA045)

Accident history for this model

ADs published since 1998 that may apply (3)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2017-14-06Sikorsky Aircraft Corporation Helicopters (Type Certificate Previously Held by Schweizer…Aug 25, 2017Airframe (269C-1)Only with: Lower coupling driveshaft P/N 269-5412, 269A5504, 269A5504-003, 269A5504-005, 269A5559, or 269A5559-003 installed.
2015-23-01Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft…Dec 15, 2015Airframe (269C-1)
99-17-10Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D…Sep 2, 1999Airframe (269C-1)Only with: Tail rotor swashplate shaft P/N 269A6049-3 installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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