# Service difficulty reports: Eurocopter EC 130 T2

A list on [Eurocopter EC 130 T2](https://openairdocs.org/model/eurocopter-ec-130-t2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 130 reports

- [SDR QMLA2026102720082](https://openairdocs.org/sdr/QMLA2026102720082.md): Generator · faulted · Oct 25, 2026 · N216SH · Urocop EC130T2 · AC Generator-Alternator
  > GENERATOR LIGHT CAME ON IN FLIGHT, AMPS DROPPED TO 0, VOLTAGE DROPPED TO 24.8V. GENERATOR WAS TURNED OFF FOR A MINUTE, THEN RESET AND TURNED BACK ON. GENERATOR LIGHT CAME ON AGAIN ABOUT 5 SECONDS AFTER THE RESET. GENERATOR WAS TURNED OFF, AIRCRAFT LANDED AT
- [SDR QMLA 202608272006](https://openairdocs.org/sdr/QMLA%20202608272006.md): Main Rotor · fod · Aug 27, 2026 · N213SH · Urocop EC130T2 · Main Rotor Head
  > JUST PRIOR TO LANDING, A SMALL PLASTIC BAG FLOATED UP AND INTO THE MAIN ROTOR SYSTEM. IT BLEW OUT ALMOST IMMEDIATELY AFTER THE FACT. A NORMAL LANDING AND SHUTDOWN WERE PERFORMED.
- [SDR 2A6D20260814](https://openairdocs.org/sdr/2A6D20260814.md): Frame · corroded · Aug 14, 2026 · N741AC · Urocop EC130T2 · Fuselage Main, Frame
  > CORROSION ON THE COLLECTIVE SPLIT FRAME ON FWD AND AFT SIDE OF OPENING.
- [SDR 2A6D20260813002](https://openairdocs.org/sdr/2A6D20260813002.md): Rib · chafed · Aug 13, 2026 · N741AC · Urocop EC130T2 · Horizontal Stabilizer, Spar/Rib
  > CHAFE DAMAGE ON BL 1263 RIB ON RH SIDE OF HORIZONTAL STABILIZER.
- [SDR 2A6D20260813001](https://openairdocs.org/sdr/2A6D20260813001.md): Crossbeam · chafed · Aug 13, 2026 · N741AC · Urocop EC130T2 · Fuselage Main, Structure
  > GOUGE/CHAFE DAMAGE TO THE AFT LANDING GEAR ATTACHMENT FWD CROSSBEAM AND SUPPORT ANGLE.
- [SDR QMLA2026071820047](https://openairdocs.org/sdr/QMLA2026071820047.md): Bearing · faulted · Jul 15, 2026 · N106VU · Urocop EC130T2 · Hydraulic Pump (Electric/Engine), Main
  > PILOTS REPORT "AFTER ILLUMINATION OF THE HYD2 AND SERVO LIGHTS, NURSE AND MEDIC SAW WHITISH GRAY SMOKE FROM VICINITY IN FRONT OF THE CABIN TDFM RADIO CONTROL HEAD, NEAR THE O2 SHUT-OFF LEVER. I SMELLED A BURNT RUBBER SMELL BUT NEVER SAW ANY SMOKE WHEN I LOOKE
- [SDR PG9A2026070600568](https://openairdocs.org/sdr/PG9A2026070600568.md): Hydraulic System · faulted · Jul 4, 2026 · N699GC · Urocop EC130T2 · Hydraulic System, Main
  > AIRCRAFT WAS DOING LEFT 180 AT QUARTERMASTER CANYON FOR BURNT SPRINGS PILOT STARTED TO NOTICE A STRANGE ODOR IN THE AIRCRAFT. ABOUT 5 SECONDS LATER, A TON OF WHITE SMOKE STARTED TO POUR INTO THE CABIN THROUGH THE A/C VENTS. PILOT IMMEDIATELY TURNED OFF THE A/
- [SDR 2A6R2026031675205](https://openairdocs.org/sdr/2A6R2026031675205.md): Landing Gear · cracked · Mar 16, 2026 · N813AM · Urocop EC130T2 · Main Landing Gear
  > DURING INSPECTION SEVERAL COMPONENTS OF THE LANDING GEAR WERE FOUND DAMAGED BEYOND LIMITS. THE LEFT SKID (350A41-6002-0201) HAD A CRACK MEASURING 1.14''. THE RIGHT SKID (350A41-6002-0301) WAS CORRODED MEASURING TO.032'' DEEP AT ITS DEEPEST. THE FORWARD CRO
- [SDR 2A6R2026040675204](https://openairdocs.org/sdr/2A6R2026040675204.md): Skin · cracked · Mar 16, 2026 · N813AM · Urocop EC130T2 · Rotorcraft Tail Boom
  > DURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.
- [SDR 2A6R2026031675203](https://openairdocs.org/sdr/2A6R2026031675203.md): Stator · corroded · Mar 16, 2026 · N813AM · Urocop EC130T2 · Rotorcraft Tail Boom
  > DURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM.020 TO.030 DEEP. PER AIRBUS TE-2026-EC130-00406, THE STATOR ASSEMBLY WAS REMOVED AND REPLACED. FOR MORE INFORMATION
- [SDR 2A6R2026031675202](https://openairdocs.org/sdr/2A6R2026031675202.md): Xmsn Deck · chafed · Mar 16, 2026 · N813AM · Urocop EC130T2 · Fuselage Main, Structure
  > DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK FWD DOUBLER AND THE AFT DOUBLER IN THE FORM OF SEVERAL CHAFE DAMAGE AREAS. THE CHAFE DAMAGE AREAS ARE ALL LOCATED UNDER THE MGB BAR FITTING INSTALLATION AREAS. THE DAMAGE AREAS ON THE FWD DOUBLER WERE WITHIN AN AR
- [SDR 2A6R2026031675201](https://openairdocs.org/sdr/2A6R2026031675201.md): Support Frame · damaged · Mar 16, 2026 · N813AM · Urocop EC130T2 · Fuselage Main, Structure
  > DAMAGE TO THE LEFT EDGE FRAME AND RT EDGE FRAME, IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. A DETAILED DESCRIPTION OF THE APPROVED REPAIR/INSTALLATION PROCEDURES IS PROVIDED IN AIRBUS REPA
- [SDR 2A6D20260305001](https://openairdocs.org/sdr/2A6D20260305001.md): Fuel Line · bent · Mar 3, 2026 · N11KQ · Urocop EC130T2 · Aircraft Fuel Distribution System
  > WHILE HOVER TAXIING THE AIRCRAFT DURING CHECK FLIGHTS, THE PILOT REPORTED A FUEL P LIGHT AND TURNED THE AIRCRAFT AROUND TO RETURN TO THE RAMP. DURING THE FLIGHT BACK, THE PILOT WAS ALERTED TO AN AMBER GOV LIGHT AND NOTICED THAT THE AIRCRAFT WAS LOSING POWER. T
- [SDR QMLA2025101420105](https://openairdocs.org/sdr/QMLA2025101420105.md): Unknown · odor · Oct 14, 2025 · N240SH · Urocop EC130T2 · Air Distribution System
  > STRONG BURNING SMELL IN COCKPIT.
- [SDR QMLA2025100620099](https://openairdocs.org/sdr/QMLA2025100620099.md): Ics Box · faulted · Oct 5, 2025 · N410W · Urocop EC130T2 · Communications System
  > HEAVY STATIC IN ICS SYSTEM. PROBLEM OCCURRED APPROXIMATELY 10-12 MINUTES IN FLIGHT AND THEN DISAPPEARED. INSPECTED AUDIO CONTROLLER/INTERCOM HARNESS AND PINS, COULD NOT DUPLICATE. THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE, REF # MEC-016217
- [SDR 2A6R 09222025743](https://openairdocs.org/sdr/2A6R%2009222025743.md): Skin · cracked · Sep 22, 2025 · N223SH · Urocop EC130T2 · Rotorcraft Tail Boom
  > DURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF THE BATTERY COMPARTMENT DOOR DOUBLER MEASURING 1.35" IN LENGTH AND STOPPING AT A RIVET HOLE. THIS C
- [SDR QMLA2025092220097](https://openairdocs.org/sdr/QMLA2025092220097.md): Skin · cracked · Sep 22, 2025 · N223SH · Urocop EC130T2 · Rotorcraft Tail Boom
  > DURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF THE BATTERY COMPARTMENT DOOR DOUBLER MEASURING 1.35" IN LENGTH AND STOPPING AT A RIVET HOLE. THIS C
- [SDR QMLA2025081320087](https://openairdocs.org/sdr/QMLA2025081320087.md): Motor · failed · Aug 13, 2025 · N930U · Urocop EC130T2 · Air Distribution Fan
  > ENROUTE BACK TO BASE AFTER A TRANSPORT, THE CREW SMELLED A BURNING ELECTRICAL SMELL. SMOKE IN THE COCKPIT EP WAS FOLLOWED AND IT WAS DETERMINED THAT THE SMELL WENT AWAY WHEN THE ECS WAS TURNED OFF. IAW THE EP, WE LEFT THE ECS OFF AND CONTINUED TO BASE WITHOUT
- [SDR QMLA2025072520078](https://openairdocs.org/sdr/QMLA2025072520078.md): Wire · broken · Jul 25, 2025 · N930U · Urocop EC130T2 · Electrical Power System Wiring
  > GENERATOR LIGHT ILLUMINATED IN FLIGHT AND WOULD NOT RESET. LANDED AT A NEARBY AIRPORT. FOUND WIRE BROKEN AT TERMINAL ON THE GENERATOR.
- [SDR JBZA20250710001](https://openairdocs.org/sdr/JBZA20250710001.md): Elec Connector · arced · Jul 2, 2025 · N415RX · Urocop EC130T2 · Communications System Wiring
  > DURING FINAL APPROACH TO BASE AN ELECTRICAL SMELL WAS DETECTED COMING FROM THE CENTER CONSOLE TDFM / SKY TRAC PANELS. DURING EVALUATION OF THE SYSTEMS IT WAS DISCOVERED THE CONNECTOR TO THE TDFM WAS THE SOURCE OF THE SMELL. FOUND CONNECTER WITH BROKEN MALE PIN
- [SDR 2A6D20250502001](https://openairdocs.org/sdr/2A6D20250502001.md): Xmsn Deck · chafed · Jun 2, 2025 · N11UQ · Urocop EC130T2 · Fuselage Main, Structure
  > GOUGING- TOOL DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE DEPTH IS APPROXIMATELY 0.026". THE MAXIMUM APPROXIMATE LENGTH IS.6 AND WIDTH IS 0.85".
- [SDR EVCA20250502001](https://openairdocs.org/sdr/EVCA20250502001.md): Structure · cracked · May 1, 2025 · N863LH · Urocop EC130T2 · Rotorcraft Tail Boom
  > CRACK EXCEEDING THE MANUFACTURES LIMITS IN THE HORIZONTAL STABILIZER
- [SDR QMLA2025040920046](https://openairdocs.org/sdr/QMLA2025040920046.md): Wire · shorted · Apr 7, 2025 · N7940K · Urocop EC130T2 · Electrical Power System Wiring
  > ARCING OM ENGINE DECK, FOUND STARTER WIRE ELECTRICAL SHORT TO ENGINE COWLING AND FUSELAGE.
- [SDR QMLA2025022520026](https://openairdocs.org/sdr/QMLA2025022520026.md): Fan · damaged · Feb 25, 2025 · N741AC · Urocop EC130T2 · Air Distribution Fan
  > AFTER LIFTING GENESIS EAST MED CENTER AND HEADING TO IOWA CITY. THE AV FAN CAME ON FOLLOWED BY A STRONG BURNING SMELL. FOUND INOP AVIONICS FAN RIGHT SIDE UNDER INSTRUMENT PANEL.
- [SDR QMLA2024110420142](https://openairdocs.org/sdr/QMLA2024110420142.md): Connector · contaminated · Oct 31, 2024 · N237SH · Urocop EC130T2 · Electrical Power System Wiring
  > FAULT PRESENTED IN FLIGHT FL1 FAIL OVERLIMIT DETECTED, FAILURE DETECTED MSG, THIS OCCURRED ON THE WAY TO PICK UP PATIENT FROM NEARBY HOSPITAL AND PILOT RETURNED TO BASE AND MADE WRITEUP IN LOGBOOK. THIS MALFUNCTION WAS IDENIFIED ON THE LEG WITH NO PATIENT ON B
- [SDR QMLA2024090620108](https://openairdocs.org/sdr/QMLA2024090620108.md): Engine · power loss · Sep 5, 2024 · N930U · Urocop EC130T2 · Engine (Turbine/Turboprop)
  > ON PICKUP I NOTICED THE FLI WAS HIGHER THAN NORMAL, I CAN USUALLY LIFTOFF AT 7/7.5 ON THE FLI AT MGW BUT THIS TIME I WAS 100LBS UNDER MGW AND IT DIDNT LIFT OFF UNTIL OVER 8 ON THE FLI. ON CLIMB-OUT IT FELT SLUGGISH SO I CHECKED MY NUMBERS. I WAS AROUND 98 N1/N
- [SDR 2A6D20240614001](https://openairdocs.org/sdr/2A6D20240614001.md): Attach Angle · cracked · Jun 14, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Attach Fittings
  > DAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” IN DIAMETER.
- [SDR QMLA2024060520058](https://openairdocs.org/sdr/QMLA2024060520058.md): Electrical Sys · burned · Jun 5, 2024 · N11YQ · Urocop EC130T2 · Electrical Power System
  > DURING NORMAL STARTUP AFTER N1 REACHED 67% AND THE GENERATOR SWITCH WAS TURNED ON. THERE WAS A BURNING SMELL OF BURNED RUBBER, AND THEN SMOKE STARTED COMING OUT FROM THE COCKPIT AREA. I IMMEDIATELY HAD THE CREW EVACUATE AND SHUTDOWN THE ENGINE.
- [SDR 2A6D20240528001](https://openairdocs.org/sdr/2A6D20240528001.md): Frame · corroded · May 28, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Frame
  > DAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANGE OF FRAME AT LH AND RH BOTTOM SIDE NEAR THE AFT LOWER FRAME. THE LH SIDE CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 0.71: X 2.05” AND TH
- [SDR QMLA2024051720053](https://openairdocs.org/sdr/QMLA2024051720053.md): Indicator · failed · May 14, 2024 · N237SH · Urocop EC130T2 · Airspeed/Mach Indicator
  > AIRSPEED INDICATOR FAILED IN FLIGHT (BOTH G500 AND BACKUP INDICATOR). UPON LANDING AT BASE MECHANIC FOUND MUD DOBBER IN PITOT TUBE, BUG/DEBRIS WAS REMOVED AND SYSTEM FUNCTIONED PROPERLY. THIS MALFUNCTION WAS IDENIFIED ON THE RETURN LEG WITH NO PATIENT ON BOARD
- [SDR 2A6D20240509003](https://openairdocs.org/sdr/2A6D20240509003.md): Floorbeam · corroded · May 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Floor Beam
  > DAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRACK DAMAGES AT TWO FASTENER HOLES TO EOP WHICH RESULTS IN REPLACEMENT OF LH FITTING.
- [SDR 2A6D20240509002](https://openairdocs.org/sdr/2A6D20240509002.md): Bonding Plate · corroded · May 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Structure
  > DAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCESSIVELY CORRODED AND DEPTH OF THE DAMAGE IS ALL THE WAY THROUGH THICKNESS WHICH RESULTS IN REPLACEMENT OF ANTENNA BASE PLATE.
- [SDR 2A6D20240509001](https://openairdocs.org/sdr/2A6D20240509001.md): Bulkhead · corroded · May 9, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Bulkhead
  > THE UPPER 7° BULKHEAD DOUBLER (PN: 350A21-0849.20) IS CORRODED AT THE LOCATION OF A PASS-THRU HOLE. THE DAMAGE AREA WAS REPORTED TO BE 0.80” X 0.50” AND 0.030” DEEP AT THE DEEPEST POINT
- [SDR 2A6D20240508003](https://openairdocs.org/sdr/2A6D20240508003.md): Crosstube · corroded · May 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Structure
  > THE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEPEST DAMAGE AREA WAS REPORTED TO BE 0.022” DEEP AND THE LARGEST AREA IS APPROXIMATELY 0.40” WIDE WITH VARIOUS LENGTHS
- [SDR 2A6D20240508002](https://openairdocs.org/sdr/2A6D20240508002.md): Crossbeam · corroded · May 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Structure (General)
  > THE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DAMAGE WAS REPORTED TO BE 0.572” X 0.179” AND 0.028” DEEP
- [SDR 2A6D20240508001](https://openairdocs.org/sdr/2A6D20240508001.md): Crossbeam · corroded · May 8, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Structure
  > THE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.20)
- [SDR QMLA2024043020045](https://openairdocs.org/sdr/QMLA2024043020045.md): Skin · cracked · Apr 25, 2024 · N230TJ · Urocop EC130T2 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON TOP OF THE HORIZONTAL STABILIZER, CURRENTLY WORKING WITH SERVICE ENGINEERING DEPT. TO DETERMINE THE REPAIRABLE LIMITS.
- [SDR 2A6D20240425009](https://openairdocs.org/sdr/2A6D20240425009.md): Skin Panel · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE ON THE FWD UPPER SKIN MEASURED TO BE APPROXIMATELY 0.80” X 0.60” X 0.003”
- [SDR 2A6D20240425008](https://openairdocs.org/sdr/2A6D20240425008.md): Stiffener · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Rotorcraft Tail Boom
  > DAMAGE TO THE TAIL BOOM LH FWD STIFFENER MEASURED TO BE APPROXIMATELY 0.85” X 0.85” X 0.0125” IN THE FORM OF CORROSION.
- [SDR 2A6D20240425007](https://openairdocs.org/sdr/2A6D20240425007.md): Attach Angle · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage, Landing Gear Attach Fittings
  > REAR LANDING GEAR ATTACHMENT LOWER ANGLE HAS DAMAGE IN THE FORM OF CORROSION. THE DAMAGE NEAR THE ANGLE OVERLAPS WITH MACHINED FRAME AND AFT LOWER BELLY FAIRING. THE DAMAGE IS ON THE VERTICAL FACE OF THE ANGLE AT PREVIOUS REPAIR LOCATION AND IS MEASURED TO BE
- [SDR 2A6D20240425006](https://openairdocs.org/sdr/2A6D20240425006.md): Cradle · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuel Storage
  > RH AFT FUEL CRADLE REINFORCEMENTS HAS DAMAGE IN THE FORM OF CORROSION. THE RH AFT CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 2.1” X 0.80” X 0.009”.
- [SDR 2A6D20240425005](https://openairdocs.org/sdr/2A6D20240425005.md): Cradle · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuel Storage
  > THE LH FWD FUEL CRADLE REINFORCEMENTS HAD DAMAGE IN THE FORM OF CORROSION. THE LH FWD CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 1.0” X 0.80” X 0.008”.
- [SDR 2A6D20240425004](https://openairdocs.org/sdr/2A6D20240425004.md): Skin Panel · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/Skin
  > DAMAGE IS ON THE AFT FUSELAGE RH SIDE SKIN PANEL (P/N: 350A210046-21 IN THE FORM OF CORROSION. THE RH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLAPS AND MEASURED TO BE APPROXIMATELY 0.15” X 0.20” X 0.011”.
- [SDR 2A6D20240425003](https://openairdocs.org/sdr/2A6D20240425003.md): Skin Panel · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Main, Plate/Skin
  > FIRST DAMAGE IS ON THE AFT FUSELAGE LH SIDE SKIN PANEL IN THE FORM OF CORROSION. THE LH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLAPS AND MEASURED TO BE APPROXIMATELY 0.15” X 0.35” X 0.009”.
- [SDR 2A6D20240425002](https://openairdocs.org/sdr/2A6D20240425002.md): Brace · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END OF THE ANGLE, AND WAS MEASURED TO BE APPROXIMATELY 0.875” X 0.875” IN SIZE THROUGH THE FULL THICKNE
- [SDR 2A6D20240425001](https://openairdocs.org/sdr/2A6D20240425001.md): Web · corroded · Apr 25, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE LOWER CENTER WEB IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUGH THICKNESS IN DEPTH.
- [SDR 2A6D20240320001](https://openairdocs.org/sdr/2A6D20240320001.md): Support Angle · corroded · Mar 20, 2024 · N11FQ · Urocop EC130T2 · Fuselage Miscellaneous Structure
  > EXFOLIATION CORROSION LOCATED ON FWD. L/H SIDE STIFFENER OF MASTER ELECTRICAL BOX.
- [SDR M3XA2024012219001](https://openairdocs.org/sdr/M3XA2024012219001.md): B-Nut · loose · Jan 19, 2024 · N892GT · Urocop EC130T2 · Turbine Engine Oil System
  > PILOT REPORTED ON POST FLIGHT INSPECTION, DISCOVERED OIL ON OUTSIDE OF ENGINE COWLING, DRAINING FROM ENGINE DECK DRAIN LINES AND SMOKE COMING OFF OUTSIDE OF EXHAUST DUCT AND OIL ON OUTSIDE OF THE ENGINE. MECHANIC FOUND B-NUT VENT LINE LOOSE AND DISCONNECTED.
- [SDR QMLA202312231222](https://openairdocs.org/sdr/QMLA202312231222.md): Unknown · unknown · Dec 23, 2023 · N11YQ · Urocop EC130T2 · Rotorcraft Flight Control
  > DURING CLIMB OUT THE AIRCRAFT HAD SIGNIFICANT INCREASED RIGHT CYCLIC PRESSURE THAT SUDDENLY RELEASED CAUSING THE AIRCRAFT TO SLIGHTLY JOLT TO THE RIGHT. THE FLIGHT WAS ABORTED AND AIRCRAFT SAFELY LANDED BACK AT BASE.
- [SDR QMLA2023111420103](https://openairdocs.org/sdr/QMLA2023111420103.md): Motor · odor · Nov 13, 2023 · N105VU · Urocop EC130T2 · Engine Bleed Air System
  > DURING SHUT DOWN AT JACKSON GENERAL HOSPITAL AFTER DROPPING OFF PATIENT, SMELLED AN ELECTRICAL BURNING SMELL COMING FROM COCKPIT. REPLACED BLOWER MOTOR.

Next page: https://openairdocs.org/model/eurocopter-ec-130-t2/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'EC130T2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/eurocopter-ec-130-t2/reports

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