- Registered owners
- Department Of Homeland SecurityUS Customs And Border PatrolAir And Marine Operations
- Location
- Washington, DC
- Owner type
- Government
- Serial number
- 2912
- Year built
- 1996
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 27, 1996
- Certificate issued
- December 29, 2021
- Expires
- December 31, 2028
- Mode S code
- A4BAE2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 86
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1990 | 3 |
| 1995 | 1 |
| 1996 | 1 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 4 |
| 2001 | 3 |
| 2002 | 7 |
| 2003 | 6 |
| 2004 | 3 |
| 2005 | 1 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 1 |
| 2010 | 4 |
| 2011 | 3 |
| 2012 | 2 |
| 2013 | 9 |
| 2014 | 5 |
| 2015 | 2 |
| 2016 | 1 |
| 2017 | 3 |
| 2018 | 3 |
| 2019 | 2 |
| 2020 | 6 |
| 2021 | 12 |
| 2022 | 6 |
| 2023 | 2 |
| 2024 | 2 |
| 2025 | 3 |
| 2026 | 10 |
Airframe · Eurocopter AS 350 B2
AD 2026-20-03Placards and MarkingsAD 2026-16-05Hydraulic power systemAD 2026-16-01Main rotor driveInformation bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Eurocopter AS 350 B2
SAIB AIR-21-13Engine Emergency Shutdown SystemSAIB SW-17-23R2Fuel SystemSAIB SW-15-20Air Conditioning System WiringSAIB SW-15-04Cabin Ventilation Air Scoop DrainingSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-11-07Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 HelicoptersSAIB SW-07-22R1Serrated lock washersHistorical bulletins · 1
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N4035WMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter AS 350 B2 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2015FA0000344Bolt · mismanufacturedLANDING GEAR SKID BOLTS, WERE IMPROPERLY COATED. NEW PARTS REJECTED BY QUALITY CONTROL. BOLTS APPEAR TO HAVE CORROSION BUT UPON FURTHER INSPECTION, IT IS THE PROTECTIVE COATING THAT HAS BEEN IMPROPERLY APPLIED.SDR RCO2002F00000Lever · seizedDURING A SCHEDULED PHASE INSPECTION, WE ARE TO BE LOOKING FOR A HOLE THAT IS WORN OUT OF ROUND ON THE YAW CONTROL COMPENSATOR LEVER. WHEN THE CONTROL WAS REMOVED IT WAS FOUND THAT THE BEARING HAD FROZEN. THE BEARIING STILL HAD MOVEMENT IN THE SMALL RANGE IT SDR 20010523CW003Seal · missingAT A SCHEDULED INSPECTION THE SELF ADHESIVE SEAL PN 350A-1063-20 WAS FOUND NOT TO BE INSTALLED. THIS IS A SEAL THAT IS INSTALLED FOR DISSIMILAR METAL CORROSION ON THE TAIL ROTOR DRIVE SHAFT HANGAR SUPPORT AND THE HANGAR BEARINGS.SDR 20010523CW002Bearing · rotatedAT A SCHEDULED INSPECTION THE BEARING PN 83A851BC3 HAD ROTATED IN THE RUBBER BUSHING PN FA3819 APPROX .3750. WE HAVE BEEN COMPLYING WITH SB REGARDING THE GREASING AND INSPECTION OF THESE BEARINGS AND STILL HAD A BEARING TURN. THIS IS AN AREA THAT CALLS FOR SSDR 20001229SH019Bracket · wornDURING A 100-HOUR INSPECTION, FOUND THE FORWARD BATTERY HOLD-DOWN BRACKET PN G10110 AND THE AFT BATTERY HOLD-DOWN BRACKET PN G10115 WERE BADLY WORN AT THE SLOTS THAT HOLD THE BATTERY IN PLACE. THERE ARE 3 AIRCRAFT WITH THE SAME STC INSTALLING THE BATTERY IN TSDR 20001017SH014Case · crackedDURING 100-HOUR INSPECTION, LEAD ACID BATTERY WAS FOUND WITH A CASE CRACK IN ALL THE LOWER BOX CORNERS. ALL OF THE CRACKS ARE 1 INCH TO 2 INCHES LONG. BATTERY IS INSTALLED IN THE TAIL BOOM UNDER AN AEC STC. AT APPROX 119.48 STA, THE LEAD ACID BATTERY IS 4 SDR 20000828SH034Adapter · detachedAFTER A FLIGHT AND ON THE POST-FLIGHT INSPECTION, THE TAIL STROBE BEACON WAS FOUND HANGING ON THE SIDE OF THE VERTICAL FIN. THE CLAMP WAS STILL IN PLACE BUT LOOSE ALLOWING THE STROBE LENS TO WEAR AWAY THE HOLDING ADAPTER FOR THE STROBE. WHEN ENOUGH MATERIAL SDR 98ZZZX2587Detector · failedDURING 500-HOUR T INSP' INSPECTION OF 3 OF THE 6 ENGINE FIRE DETECTORS WERE FOUND DEFECTED PER TURBOMECA MM CHAP 26-11-00 PARA 1 INSPECTION PROCEDURES. TWO WERE OVERHEATED AND ON ONE THE OHMS WERE TOO LOW. SUBMITTER STATED THE OPERATOR BELIEVES THEY SHOULD HSDR 98ZZZX2586Detector · failedDURING 500-HOUR T INSP' INSPECTION OF 3 OF THE 6 ENGINE FIRE DETECTORS WERE FOUND DEFECTED PER TURBOMECA MM CHAP 26-11-00 PARA 1 INSPECTION PROCEDURES. TWO WERE OVERHEATED AND ON ONE THE OHMS WERE TOO LOW. SUBMITTER STATED THE OPERATOR BELIEVES THEY SHOULD HSDR 97ZZZX3197Screw · defectiveDURING C/W SB 05.08 PARA 1C(2A) WHEN REINSTALLING SCREW INTO BEARING SUPPORT MOUNT BRACKET, MECHANIC STATED THAT TORQUE DID NOT FEEL STABLE. REMOVED AND INSPECTED, FOUND NO OBVIOUS DEFECTS. REINSTALLED TORQUED NUT AND, AGAIN, DID NOT FEEL LIKE TORQUE STABILISDR 97ZZZX1137Freewheel Shaft · extra o ringDURING REPLACEMENT OF MODULE I MAG ASSEMBLY, DISCOVERED AN O-RING ON POWER SHAFT BETWEEN FREEWHEEL UNIT AND MAG SEALING RING HOLDER. THIS PARTICULAR MODEL ENGINE DOES NOT USE AN O-RING IN THIS LOCATION. THE PRESENCE OF THIS O-RING COULD RESTRICT SOME FLOW OFSDR 96ZZZX5613Control Head · miswiredDME WOULD NOT WORK ON SEVERAL CHANNELS. THE AIRCRAFT WAS RECENTLY DELIVERED FROM MANUFACTURING AND WAS MISSING JUMPER IN CONTROL HEAD K1572 BETWEEN PINS 30 AND 47. THIS APPEARS TO BE A REVISION THAT WAS NOT INCORPORATED BY THE INSTALLER. THE OLD INSTALL MAN
STCs that may be installed · 487
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 487 STCs
Earlier aircraft with this N-number · 3
These aircraft carried N4035W before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.