N5204J1998 Eurocopter AS 350 B2
This N-number isn't registered right now. Below is its last known registration, canceled Jul 2, 2024.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply12 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- U S Dept Of Homeland Security
- Owner type
- Government
- City, state
- Washington, DC
- Certificate issued
- Jun 17, 1999
- Canceled
- Jul 2, 2024
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 4, 1998
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 dataAirframe
- Manufacturer
- Eurocopter
- Model
- AS 350 B2
- Year
- 1998
- Serial number
- 3118
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H9EU
- Mode S code
- A68BDB
Engine
- Make and model
- Turbomeca Arriel 1ser
- Type
- Turbo-shaft
- Power
- 681 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1999 – 2024U S Dept Of Homeland SecurityWashington, DC
- 1975Floair INCWichita, KS · different airframe: Cessna 402b S/N 402b0891
- until 1988Individual ownerdifferent airframe: Cessna 172n S/N 17273730
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (4)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-23-09 | Eurocopter France Helicopters | Dec 27, 2013 | Airframe (AS 350 B2)Only with: Helicopters with sliding doors installed, except those with modification AL.4262. |
| 2013-21-01 | Eurocopter France (Eurocopter) Helicopters | Oct 25, 2013 | Airframe (AS 350 B2)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed. |
| 2013-08-19 | Eurocopter France Helicopters | Jun 5, 2013 | Airframe (AS 350 B2)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed. |
| 2010-11-51 | Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and… | Sep 2, 2010 | Airframe (AS 350 B2)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N 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 (12)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Hydraulic power · servo control · leakingFeb 13, 2008
ON A ROUTINE PREFLIGHT INSPECTION, THE LT HYDRAULIC ROLL CONTROL SERVO WAS DISCOVERED TO BE LEAKING HYDRAULIC FLUID AT THE PISTON SHAFT SEAL. THE LEAK COULD NOT BE DUPLICATED DURING GROUND TESTING WITH A HYDRAULIC POWER CART IAW THE MM INSTRUCTIONS. SUBSEQUENT FLIGHT TESTING REVEALED THE LEAK…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · fcu · leakingJan 25, 2008
FUEL CONTROL UNIT IS LEAKING FUEL FROM A DIAPHRAM BREATHER HOLE IN THE CASING. THE LEAKING HOLE IS LOCATED BELOW AND SLIGHTLY IB OF THE PRESSURE REDUCING VALVE ATTACHED TO THE FCU. FUEL LEAK WAS INITIALLY OBSERVED AS A SEEP, PROGRESSING TO A LOW PRESSURE STEADY TRICKLE THROUGHOUT MULTIPLE ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor drive · drive shaft · misoverhauledJan 26, 2006
DURING ROUTINE TBO REPLACEMENT OF TAIL ROTOR DRIVESHAFT; IT WAS DISCOVERED THAT THE FORWARD END OF THE RECENTLY OVERHAULED REPLACEMENT WAS UNPAINTED CAUSING THE NR 5 BEARING FIT TOLERANCES TO BE TOO LOOSE. MFG TECHNICAL REPRESENTATIVES VERIFIED THAT THE DRIVESHAFT IS SUPPOSED TO BE PAINTED UP TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Tail rotor drive · drive assy · misoverhauledJan 26, 2006
DURING ROUTINE TBO REPLACEMENT, DISCOVERED THE NEWLY OVERHAULED TAIL ROTOR DRIVESHAFT FORWARD END WAS UNPAINTED CAUSING AN UNSERVICEABLY LOOSE FIT OF THE NR 5 BEARING. MANUFACTURER TECHNICAL REPRESENTATIVES VERIFIED THAT THE AREA IN QUESTION IS SUPPOSED TO BE PAINTED UP TO THE SPLINES. PART WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor · bearing · crackedJul 10, 2002
THE TAIL ROTOR WAS REMOVED FOR THE 500 HOUR INSPECTION AND DURING INSPECTION, THE LAMINATED HALF BEARINGS WERE FOUND TO BE CRACKED. THE RUBBER IN THE BEARINGS WAS SPLIT BEYOND LIMITS. IT IS TO BE NOTED THAT THIS AIRCRAFT SPENDS MOST OF IT'S TIME OUTSIDE ON THE RAMP AND THE DETERIORATION IS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · coupling · deformedJul 11, 2001
COUPLING FOUND EXCESSIVELY DEFORMED AT 100 HR INSPECTION. NO OTHER PROBLEMS FOUND AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor drive · drive shaft · damagedNov 7, 2000
DURING 500-HOUR INSPECTION, FOUND INNER SLEEVE OF AFT MOST BEARING SLIPPING ON T/R DRIVESHAFT. IT APPEARED TO HAVE BEEN SPINNING FOR SOME TIME AND RUBBER HAD ACTUALLY TRANSFERRED FROM SLEEVE TO SHAFT. SHAFT ITSELF WAS NOT DAMAGED. REPLACED ENTIRE SHAFT ASSEMBLY DUE TO WARRANTY AND REPAIR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · bolt · corrodedNov 7, 2000
DURING 500-HOUR INSPECTION, FOUND CORROSION ON SLEEVE ATTACHING BOLTS. NOTED MASTINOX WAS NOT USED AT THE TIME OF ASSEMBLY. REF: S/NS 6327, 6329, 6339, 6343, 6370, AND 6380. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · flange · corrodedNov 7, 2000
DURING 500-HOUR INSPECTION, FOUND CORROSION ON UPPER SLEEVE FLANGE HOLES. NOTED MASTINOX WAS NOT USED AT THE TIME OF ASSEMBLY. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · flange · corrodedNov 7, 2000
DURING 500-HOUR INSPECTION, FOUND CORROSION ON LOWER SLEEVE FLANGE. NOTED MASTINOX WAS NOT USED AT THE TIME OF ASSEMBLY. REF: S/N M4413, M4415, M4417. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 12 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026