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N133LN

Open the Markdown

2005 Eurocopter EC 130 B4 · Turbomeca ARRIEL-2B1

Open in FAA registry

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Registered owner
Air Methods LLC
Location
Greenwood Village, CO
Owner type
LLC
Serial number
3983
Year built
2005
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
May 24, 2006
Certificate issued
April 30, 2011
Expires
April 30, 2027
Mode S code
A0875D
Eurocopter EC 130 B4Airframe model · 6 seats · 1 engine · 154 registeredTCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 64

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2002In forceSuperseded2026
See all 90 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 1
SAIB SW-17-23R1Fuel SystemIssued Mar 2, 2018

NTSB investigations

No NTSB investigations matched to N133LNMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter EC 130 B4 aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20080421831499ITo Running(Helicopter/Vtol Ac) · London, KY(-23) Dual controls were installed in the aircraft and the check airman was giving a 6 month check ride. Both pilots performed the walkaround preflight of the aircraft. They stated "all cowling was closed at that time." The pilot receiving instruction got in…Apr 21, 2008 · Minor damage

Service difficulty reports · 8

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR QMLA2024071120085Motor · overtempAIR CONDITIONER FUNCTIONAL UNTIL A TEMPORARY DECREASE IN FAN SPEED BUT RETURNED TO NORMAL OPERATING SPEED. AFTER CHANGE, THERE WAS AN ODOR OF BURNING (ELECTRICAL). TURNED A/C OFF & BURNING SMELL DISSIPATED. SWITCHED FRESH AIR FAN ON & NO BURNING SMELL PRESENTJul 2, 2024 · N133LN · Urocop EC130B4 · Cabin Cooling SystemSDR QMLA2018101518112Floor Panel · crackedTHE MECHANIC REMOVED THE AUXILIARY SEATING FLOOR OVERLAY PANEL AS PER AMC AAIP C1040 AND DISCOVERED TWO CRACKS ON THE AFT CABIN FLOOR PANEL. THE CRACKS STARTED AT THE LEADING EDGE OF THE FLOOR PANEL AND RADIATED AFT. THE DAMAGE IS AT STA 70" AND RIGHT BL 4.5".Oct 15, 2018 · N133LN · Urocop EC130B4 · Fuselage Floor PanelSDR QMLA2015093015089Compressor · seizedAFTER DEPARTURE, THE WHOLE CREW SMELLED A RUBBER & ELEC BURN TYPE SMELL. THE PILOT ISOLATED THE SMELL TO THE AIR CONDITIONER & TURNED OFF THE AIR CONDITIONER SYS & THE SMELL WENT AWAY. WE CONTINUED THE FLIGHT BACK TO THE BASE WITH NO OTHER INCIDENTS & COMPLESep 30, 2015 · N133LN · Urocop EC130B4 · Cabin Cooling SystemSDR QMLA2014072614090Unknown · odorFOLLOWING DEPARTURE CREW NOTED STRONG ELEC SMELL IN CABIN. AIR CONDITIONER SWITCHED OFF WHILE SIMULTANEOUSLY ABORTING TAKEOFF & RETURNING TO BASE. ELEC SMELL DISSIPATED. ACFT SHUTDOWN & CHECKED EXTENSIVELY FOR SOURCE BY PILOT & MECHANIC. NO SOURCE IDENTIFIJul 26, 2014 · N133LN · Urocop EC130B4 · Air Distribution SystemSDR QMLA2014061114073Skin · crackedCRACK FOUND IN THE TAIL BOOM SKIN WHILE PERFORMING A DYE PENETRANT INSPECTION OF THE AREA DESCRIBED IN SDR QMLA2014061114072. THE CRACK IN THE TAIL BOOM SKIN IS CURRENTLY BEING EVALUATED FOR AN APPROVED REPAIR. THE REPAIR TEAM THEY WILL BE SENDING TO ACCOMPLJun 11, 2014 · N133LN · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2014061114072Attach Fitting · crackedWHILE COMPLYING WITH EAD 2014-12-51, THE RT SIDE HORIZONTAL ATTACHMENT FITTING CRACKED UPON REMOVAL. THIS STABILIZER HAD BEEN DETERMINED TO BE FAIRLY DIFFICULT TO REMOVE & REINSTALL ON PREVIOUS MX EVENTS INVOLVING THIS TASK. MOBILE SUPPORT REPAIR TEAM TO BE Jun 11, 2014 · N133LN · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2012062312105Skin · crackedCRACK IN HORIZONTAL STABILIZER WITH OVERALL LENTH OF 1.49". THIS CRACK IS ON THE UPPER LT SIDE OF THE STABILIZER. IT BEGINS AT A MEASUREMENT OF 10.3125" AFT OF THE LT STABILIZER ATTACHMENT PIN AND CONTINUES AT AN APPROX 45 DEGREE ANGLE OF THE GENERAL ORIENTAJun 23, 2012 · N133LN · Urocop EC130B4 · Horizontal Stabilizer, Plate/SkinSDR QMLA2012030112048Bolt · failedDURING AIRWORTHINESS CHECK, A BOLT WAS DISCOVER UNSECURED ON THE TRANSMISSION DECK JUST FWD OF THE MAIN GEAR BOX DIRECTLY BELOW THE PART THAT WAS REPLACED. VISUAL EXAMINATION DISCOVERED THAT THE BOLT HAD ORIGINATED FROM THE FORWARD GEAR DRIVEN HYD PUMP. WAS Mar 1, 2012 · N133LN · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), Main

STCs that may be installed · 134

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 134 STCs