# Service difficulty reports: Safran ARRIEL-2B1

A list on [Safran ARRIEL-2B1](https://openairdocs.org/engine/safran-arriel-2b1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 16 · 757 reports

- [SDR QMLA2026081320055](https://openairdocs.org/sdr/QMLA2026081320055.md): Blower Motor · burned out · Aug 13, 2026 · N910U · Urocop EC130B4 · Air Distribution Fan
  > ODOR OF BURNT ELECTRICAL WIRING. FOUND SMELL COMING FROM AFT AC VENTS. FOUND CONDENSATION/WATER IN ELECTRICAL MOTOR. REPLACED AFT BLOWER MOTOR
- [SDR 2A6D20260728001](https://openairdocs.org/sdr/2A6D20260728001.md): Support Angle · cracked · Jun 16, 2026 · N350MV · Snias AS350B3 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON SUPPORT ANGLE OF UPPER LEFT FUSELAGE TO TAILBOOM ATTACHMENT
- [SDR 2026FA0000304](https://openairdocs.org/sdr/2026FA0000304.md): Chip Detector · false indication · Apr 28, 2026 · N11QZ · Urocop EC130B4 · Turbine Engine Accessory Drive
  > ENGINE CHIP EVENT - INTERMITTENT ILLUMINATION OF ENGINE CHIP INDICATION DURING CRUISE FLIGHT AFTER MAKING A TURN. DURING DESCENT AND LANDING AT A LOCAL BALL FIELD, THE CHIP LIGHT FLICKERED MULTIPLE TIMES. MAINTENANCE DISPATCHED FROM HONOLULU AND INSPECTED TH
- [SDR 2A6D20251125001](https://openairdocs.org/sdr/2A6D20251125001.md): Crossbeam · chafed · Nov 25, 2025 · N92OU · Urocop EC130B4 · Fuselage Main, Structure
  > VARIOUS DAMAGES AT THE AFT LANDING GEAR LOCATION, THE FIRST DAMAGE (#1) IS AT THE AFT LANDING GEAR CROSS BEAM SHIM (P/N: 350A214344.20) IN THE FORM OF CHAFING. THE CHAFE DAMAGE IS POSSIBLE DUE TO WEAR IN THE SHIM (P/N: 350A410064.20) BETWEEN THE AFT LANDING GE
- [SDR 2A6R1124202574604](https://openairdocs.org/sdr/2A6R1124202574604.md): Skin · damaged · Nov 24, 2025 · N133HN · Urocop EC130B4 · Fuselage Main, Plate/Skin
  > OVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LOWER FRAME (P/N: 350A211245.22), AND MAINTENANCE STEP (P/N: 350A21137.20) DURING REMOVAL AND REPLACEM
- [SDR 2A6D20251106001](https://openairdocs.org/sdr/2A6D20251106001.md): Bulkhead · chafed · Nov 6, 2025 · N629AM · Snias AS350B3 · Fuselage Main, Bulkhead
  > CHAFING DAMAGE ON THE LT LONGITUDINAL BULKHEAD (X-FRAME) ON THE UPPER INBD FACE MEASURING APPROXIMATELY 0.017" IN DEPTH, 0.10" IN WIDTH, AND 0.210" IN LENGTH. THE DAMAGE WAS REPAIRED WITH A DOUBLER IAW AIR METHODS ENGINEERING AUTHORIZATION 33-5300-EA-5308.
- [SDR 2A6D20251105001](https://openairdocs.org/sdr/2A6D20251105001.md): Beam · chafed · Nov 5, 2025 · N629AM · Snias AS350B3 · Fuselage Main, Structure
  > DAMAGE TO THE RH Y398.5 BEAM (P/N: 350A211351.22) AND STOP DOUBLER (P/N: 350A211363.25) IN THE FORM OF A CHAFE. THE CHAFE DAMAGE IS NEAR THE FWD UPPER SIDE OF THE CUTOUT AND WAS MEASURED TO BE APPROXIMATELY 0.4" IN LENGTH AND 0.040" IN DEPTH.
- [SDR 2A6R1024202574601](https://openairdocs.org/sdr/2A6R1024202574601.md): Rail · chafed · Oct 24, 2025 · N133HN · Urocop EC130B4 · Rotorcraft Tail Boom
  > CHAFING DAMAGE WAS FOUND ON THE TAIL BOOM L/H TRDS SUPPORT RAIL/STIFFENER SHEET (P/N: 350A231028.66) JUST FORWARD OF THE #3 TRDS BEARING SUPPORT. THIS DAMAGE IS A 0.25” IN LENGTH AND 0.1” IN HEIGHT SECTION THAT IS CHAFED THROUGH THE FULL THICKNESS OF THE RAIL.
- [SDR 2A6D20251006001](https://openairdocs.org/sdr/2A6D20251006001.md): Keelbeam · damaged · Oct 6, 2025 · N814SM · Snias AS350B3 · Fuselage Main, Keel
  > A MIS-DRILLED HOLE WAS FOUND ON THE FORWARD LH KEEL BEAM (PN: 350A21-1350-20), AFT LH KEEL BEAM (PN: 350A21-1056- 20) AND FWD KNOT ASSEMBLY LH SPLICE (PN: 350A21-1071-20) LOCATED AT Y400 X 1296. TOOL MARK DAMAGE WAS ALSO DISCOVERED ON THE FWD KNOT ASSEMBLY L
- [SDR QMLA2025100420098](https://openairdocs.org/sdr/QMLA2025100420098.md): Display · faulted · Sep 30, 2025 · N336AM · Urocop EC130B4 · Engine Indicating System
  > JUST LIFTED OFF FROM A PR EVENT & HEADING BACK TO BASE, NOTICED UPPER SCREEN OF VEMD HAD REVERTED TO 3-PARAMETERS ENGINE PAGE & NG INDICATION MISSING & YELLOW. A CAUTION MESSAGE OF OVERLIMIT DETECTED SHOWING ON BOTTOM OF VEMD. LOWERED POWER & DIVERTED TO KRV
- [SDR QMLA2025091520094](https://openairdocs.org/sdr/QMLA2025091520094.md): Engine · power loss · Sep 15, 2025 · N507AM · Snias AS350B3 · Engine Controls
  > WE WERE TAKING OFF FROM THE PAD AT PRESCOTT WITH A PATIENT ONBOARD. HAD GOOD POWER IN HOVER AND ON TAKEOFF ABOUT 200-300 FT AND GOT JUST PAST THE STREETLIGHTS IN FRONT OF THE PAD. POWER SETTING BELOW THE YELLOW RANGE, FOR A BRIEF SECOND THE NOSE ROTATING TO LE
- [SDR 2A6D20250818001](https://openairdocs.org/sdr/2A6D20250818001.md): Mount Flange · gouged · Aug 18, 2025 · N109LN · Snias AS350B3 · Fuselage, Landing Gear Attach Fittings
  > DAMAGE TO THE LANDING GEAR LH OTBD AFT BEARING IN THE FORM OF GOUGE. THE GOUGE DAMAGE IS AT LOWER FLANGE OF THE BEARING AND WAS MEASURED TO BE APPROXIMATELY 0.3895” X 0.1105” X DEPTH MORE THAN HALF THE THICKNESS OF THE BEARING.
- [SDR QMLA2025071820075](https://openairdocs.org/sdr/QMLA2025071820075.md): Unknown · odor · Jul 18, 2025 · N508AM · Snias AS350B3 · Air Distribution System
  > NURSES REPORTED AFTER TAKING OFF FROM GOODYEAR AIRPORT AFTER GETTING FUEL AFTER A PR EVENT THAT THEY NOTICED A STRONG FUEL SMELL. THEY CONTINUED ON TO THE HELIPAD AT ABRAZO WEST AND LANDED SAFELY. I ARRIVED AT THE HELIPAD AND PERFORMED A INSPECTION OF THE HELI
- [SDR QMLA2025061620067](https://openairdocs.org/sdr/QMLA2025061620067.md): Vent Line · leaking · Jun 14, 2025 · N910U · Urocop EC130B4 · Turbine Engine Oil System
  > MAJOR OIL LEAK. DISCOVERED BY NURSE STOWING EQUIPMENT IN REAR COMPARTMENT. HE ADVISED ME OF OIL ALL OVER THE SIDE OF AIRCRAFT. I SHUT DOWN THE AIRCRAFT AND EXITED TO INSPECT. REMOVED AND RE-INSTALLED OIL VENT LINE FROM TANK, GROUND RUN, LEAK CHECK WAS GOOD, R
- [SDR 2A6D20250602001](https://openairdocs.org/sdr/2A6D20250602001.md): Doubler · chafed · Jun 2, 2025 · N267AM · Snias AS350B3 · Fuselage Main, Plate/Skin
  > CHAFING DAMAGE WAS DISCOVERED ON T/R SERVO GUIDE DOUBLER P/N: 355A23-2000-20
- [SDR 2A6D20250602002](https://openairdocs.org/sdr/2A6D20250602002.md): Floor Support · chafed · Jun 2, 2025 · N267AM · Snias AS350B3 · Fuselage Miscellaneous Structure
  > CHAFE DAMAGE WAS DISCOVERED ON THE R/H CABIN FLOOR EDGE P/N: 350A21-1359-21
- [SDR QMLA2025052820060](https://openairdocs.org/sdr/QMLA2025052820060.md): Hmu · faulted · May 27, 2025 · N390AM · Urocop EC130B4 · Engine (Turbine/Turboprop)
  > MULTIPLE ENGINE CHIP CAUTIONS OVER A HANDFUL OF FLIGHTS SINCE MID-APRIL. MOST RECENT EVENT (THIS INCIDENT) OCCURRED LESS THAN ONE DAY AND 0+45 FLIGHT HOURS AFTER PREVIOUS INCIDENT. MULTIPLE CHIPS (IN EXCESS OF 20) FOUND ON CHIP DETECTOR (M01) AND SEVERAL CH
- [SDR QMLA2025051520056](https://openairdocs.org/sdr/QMLA2025051520056.md): Gearbox · warning light · May 16, 2025 · N328CH · Urocop EC130B4 · Main Rotor Gearbox
  > MAIN ROTOR GEAR BOX CHIP INDICATOR LIGHT ILLUMINATED IN FLIGHT. FIRST SET OF FLIGHTS FROM CHANGING OF MBG OIL FILTER YESTERDAY.
- [SDR QMLA2025032420040](https://openairdocs.org/sdr/QMLA2025032420040.md): Motor · shorted · Mar 23, 2025 · N382AM · Urocop EC130B4 · Humidity Control System
  > ELECTRICAL SMOKE ODOR IN CABIN. AFT EVAPORATOR MOTOR HAD INTERNAL SHORT CAUSING SMOKE SMELL AND CAUSING AFT PORTION OF A/C TO BE INOP.
- [SDR 2A6D20250130001](https://openairdocs.org/sdr/2A6D20250130001.md): Beam · damaged · Jan 30, 2025 · N354CF · Snias AS350B3 · Fuselage Main, Structure
  > FASTENER HOLE DAMAGE (ELONGATION) WAS DISCOVERED ON THE LH MAINTENANCE FOOTSTEP BEAM (P/N 350A21124520) IN THE FUSELAGE REAR STRUCTURE.
- [SDR 2A6D20241209001](https://openairdocs.org/sdr/2A6D20241209001.md): Crossbeam · chafed · Dec 9, 2024 · N317AM · Urocop EC130B4 · Fuselage Main, Structure
  > THE FIRST DAMAGE IS ON THE AFT LANDING GEAR CROSS BEAM (P/N: 350A214311.20). THE AFT CROSS BEAM IS DAMAGED DUE TO MISSING SHIM BETWEEN THE AFT LANDING GEAR LOWER ARM AND LOWER HALF BEARING WHICH CREATED LATERAL MOVEMENT OF LANDING GEAR CROSS TUBE AND CAUSED CH
- [SDR QMLA2024092420125](https://openairdocs.org/sdr/QMLA2024092420125.md): Motor · failed · Sep 23, 2024 · N728AM · Urocop EC130B4 · Air Distribution System
  > CREW NOTED SMELL OF SOMETHING BURNING IN COCKPIT. A/C WAS TURNED OFF AND THE SMELL BECAME LESS SEVERE.
- [SDR QMLA2024091920118](https://openairdocs.org/sdr/QMLA2024091920118.md): Starter Gen · failed · Sep 18, 2024 · N336AM · Urocop EC130B4 · Starter-Generator
  > STAR GEN FAILED ON APPROACH. WOULD NOT RESET.
- [SDR QMLA2024091620116](https://openairdocs.org/sdr/QMLA2024091620116.md): Engine · surges · Sep 15, 2024 · N130HN · Urocop EC130B4 · Engine (Turbine/Turboprop)
  > DURING FLIGHT ON AN AIR AMBULANCE OPERATION. AS THE INCREASE OF COLLECTIVE TO APPROXIMATLEY 9.0 FLI, HEARD THE ENG SURGE WITH A LEFT YAW TO THE ACFT. IMMEDIATELY LOWERED COLLECTIVE & VERIFIED ALL SYS NORMAL. SMOOTHLY AND SLOWLY INCREASED THE COLLECTIVE & AT A
- [SDR QMLA2024091520116](https://openairdocs.org/sdr/QMLA2024091520116.md): Anticipator · faulted · Sep 15, 2024 · N130HN · Urocop EC130B4 · Engine (Turbine/Turboprop)
  > REMOVED AND REPLACED ANTICIPATOR. THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE. REF# 7481.091524.2054.TT
- [SDR 2A6D20240828001](https://openairdocs.org/sdr/2A6D20240828001.md): Floor Panel · corroded · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Floor Panel
  > THERE IS CORROSION DAMAGE TO THE CABIN FLOOR EDGING (PN: 350A21-1359-20/21).
- [SDR 2A6D20240828002](https://openairdocs.org/sdr/2A6D20240828002.md): Structure · gouged · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE LH UPPER CARGO EDGING (P/N: 350A211041.22) IN THE FORM OF A GOUGE CAUSED WHILE INSTALLING BLIND FASTENER. THE GOUGE DAMAGE NEAR AFT SIDE OF THE LH EDGING AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.15” X 0.02”.
- [SDR 2A6D20240828003](https://openairdocs.org/sdr/2A6D20240828003.md): Bulkhead Web · chafed · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Structure (General)
  > DAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.86) IN THE FORM OF SEVERAL CHAFES. THE CHAFES WERE REPORTED TO BE 0.20” X 0.10” AND 0.004” DEEP, AS WELL AS 0.20” X 0.30” AND 0.010” DEEP
- [SDR 2A6D20240828004](https://openairdocs.org/sdr/2A6D20240828004.md): Stiffener · worn · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE LH STA2700 STIFFENER (LH PN: 350A21-1071.22; RH PN: 350A211071.23) IN THE FORM OF WEAR CAUSED BY A NEARBY BOLT HEAD.
- [SDR 2A6D20240828005](https://openairdocs.org/sdr/2A6D20240828005.md): Support · damaged · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE RH BI-DIRECTIONAL SUPPORT FITTING (P/N: 350A211232.23) AND SUPPORT BEAM (P/N: 350A211293.20) IN THE FORM OF CHAFING CAUSED DUE TO CABLE. THE CHAFE DAMAGE AT SUPPORT BEAM MEASURED TO BE APPROXIMATELY 0.30” X 0.20” X 0.015”. THE CHAFE DAMAGE AT BI-
- [SDR 2A6D20240828006](https://openairdocs.org/sdr/2A6D20240828006.md): Structure · gouged · Aug 28, 2024 · N108LN · Snias AS350B3 · Fuselage Structure (General)
  > GOUGE AT THE OUTBOARD FLANGE RIVNUT LOCATION IN THE FORM OF SHEAR OUT. THE GOUGE WAS MEASURED TO BE APPROXIMATELY 0.1” X 0.1285”X 0.060”.
- [SDR QMLA2024061720064](https://openairdocs.org/sdr/QMLA2024061720064.md): Unknown · odor · Jun 15, 2024 · N358AM · Urocop EC130B4 · Air Distribution System
  > DURING FLIGHT AND RETURN TO BASE FROM FLIGHT, CREW NOTIFIED PILOT THAT THEY SMELLED A ELECTRICAL BURNING AROUND THE BACK CABIN WALL. IT WAS DARK INSIDE THE CABIN SO VISUAL IDENTIFICATION WAS DIFFICULT. PILOT AND CREW INSPECTED THE AREA BUT COULD NOT IDENTIFY T
- [SDR QMLA2024042520043](https://openairdocs.org/sdr/QMLA2024042520043.md): Potentiometer · worn · Apr 25, 2024 · N137HN · Urocop EC130B4 · Engine Controls
  > TOOK OFF FROM BASE GOT TO LEVEL FLIGHT STARTED POWER CHECK GOT THE SOLID AMBER GOV LIGHT. RETURNED TO BASE.
- [SDR 2A6D20240321001](https://openairdocs.org/sdr/2A6D20240321001.md): Floor Support · corroded · Mar 21, 2024 · N4497Y · Snias AS350B3 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE DISCOVERED TO THE L/H CABIN FLOOR EDGING P/N: 350A21-1359-20.
- [SDR 2A6D20240321002](https://openairdocs.org/sdr/2A6D20240321002.md): Floor Support · corroded · Mar 21, 2024 · N4497Y · Snias AS350B3 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE DISCOVERED TO THE R/H CABIN FLOOR EDGING P/N: 350A21-1359-21.
- [SDR QMLA202420025](https://openairdocs.org/sdr/QMLA202420025.md): Duct · cracked · Mar 1, 2024 · N533AM · Snias AS350B3 · Air Distribution System
  > PILOT REPORTED DURING CLIMB OUT FROM BASE AT KDMN EN ROUTE TO SENDING FACILITY HE TURNED ON THE CABIN VENTILATION AND WATER STARTED POURING OUT OF UPPER A/C VENTS. HE THEN TURNED OFF THE A/C VENT SYSTEM AND RETURNED TO BASE AND SHUT THE AIRCRAFT DOWN WITHOUT
- [SDR 2A6D20240229001](https://openairdocs.org/sdr/2A6D20240229001.md): Bulkhead · cracked · Feb 29, 2024 · N344AM · Urocop EC130B4 · Fuselage Main, Bulkhead
  > A CRACK WAS DISCOVERED ON THE AFT BULKHEAD CENTER STRUCTURE. THE CRACK MEASURES APPROXIMATELY 1.0 INCH LONG
- [SDR 2A6D20240201001](https://openairdocs.org/sdr/2A6D20240201001.md): Angle · corroded · Feb 1, 2024 · N11FQ · Urocop EC130B4 · 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 2A6D20240201002](https://openairdocs.org/sdr/2A6D20240201002.md): Web · corroded · Feb 1, 2024 · N11FQ · Urocop EC130B4 · Fuselage Miscellaneous Structure
  > DAMAGE TO THE LOWER CENTER WEB (P/N: 350A21-4300.20) 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 QMLA2024012920009](https://openairdocs.org/sdr/QMLA2024012920009.md): Unknown · odor · Jan 29, 2024 · N728AM · Urocop EC130B4 · Air Distribution System
  > SMELL OF FUEL IN CABIN. FLIGHT LEG ABORTED AND RETURNED TO AIRPORT. MECHANIC NOTIFIED AND RESPONDED. CHECKED ALL COMPONENTS AND AREAS OF HELICOPTER FOR SOURCE. NO FUEL LOCATED IN OR AROUND AIRCRAFT OR STRUCTURES, CABINS, COMPARTMENTS. PERFORMED ENGINE RUN-UP W
- [SDR QMLA2023112820110](https://openairdocs.org/sdr/QMLA2023112820110.md): Bulkhead · damaged · Nov 28, 2023 · N335AM · Urocop EC130B4 · Fuselage Main, Bulkhead
  > CRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEB P/N 350A21-4002 UNDER THE RH FLOOR AT STA 845, RBL 673.3 WL 2806.2.
- [SDR QMLA2023112720108](https://openairdocs.org/sdr/QMLA2023112720108.md): Outlet · odor · Nov 26, 2023 · N279AM · Snias AS350B3 · Air Distribution System
  > CREW REPORTED UNUSUAL ODOR IN CABIN AFTER LIFTOFF.
- [SDR 2A6D20231102001](https://openairdocs.org/sdr/2A6D20231102001.md): Floor Support · corroded · Nov 2, 2023 · N574AM · Snias AS350B3 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE CABIN FLOOR EDGING ON THE LH AND RH SIDE (P/N: 350A21-1359-20/21)
- [SDR QMLA2023110220099](https://openairdocs.org/sdr/QMLA2023110220099.md): Unknown · unknown · Nov 1, 2023 · N332AM · Urocop EC130B4 · Engine Controls
  > AFTER AMBER AND RED GOV LIGHT ILLUMINATED, MYSELF AND THE CREW COULD SMELL AN ELECTRICAL SMOKE ODOR. AFTER LANDING AND SHUTDOWN. ARRIVED AT AIRCRAFT, CLEANED ELECTRICAL CONNECTORS ON FADEC AND NF SENSOR. GOV LIGHT WENT OUT.
- [SDR QMLA2023100420081](https://openairdocs.org/sdr/QMLA2023100420081.md): Compressor · odor · Oct 2, 2023 · N490H · Snias AS350B3 · Cabin Cooling System
  > PILOT REPORTED SMOKE SMELL IN CABIN, TURNED OFF THE A/C SYSTEM AND SMELL WENT AWAY. LANDED AT BASE WITH NO FURTHER ISSUES. MECHANIC ON SITE FOUND WHERE A/C COMPRESSOR CLUTCH WAS INOP.
- [SDR QMLA2023060420043](https://openairdocs.org/sdr/QMLA2023060420043.md): Unknown · unknown · Jun 2, 2023 · N332AM · Urocop EC130B4 · Engine (Turbine/Turboprop)
  > UPON DEPARTURE FROM KPDK, ENG CHIP LIGHT ILLUMINATED ON THE WARNING PANEL. IT WENT OUT AFTER A FEW SECONDS. LANDED AS SOON AS POSSIBLE BACK TO KPDK AND SHUT DOWN ENGINE, CHECKED THE CHIP PLUGS AND THERE WAS NOTHING ON THEM. GROUND RUN THE AIRCRAFT WITH NO LI
- [SDR 2A6D20230525001](https://openairdocs.org/sdr/2A6D20230525001.md): Floorbeam · damaged · May 25, 2023 · N118LN · Snias AS350B3 · Fuselage Main, Floor Beam
  > DURING INSPECTION, TWO NUTPLATES WERE FOUND TO BE INCORRECTLY INSTALLED CAUSING DAMAGE TO THE FLOOR BEAM AT APPROXIMATELY STA 1510 AND RBL 398.
- [SDR 2A6D20230523001](https://openairdocs.org/sdr/2A6D20230523001.md): Support Beam · elongated · May 23, 2023 · N118LN · Snias AS350B3 · Fuselage Main, Structure
  > DAMAGE WAS DISCOVERED ON THE L/H BEAM UNDER THE ENGINE DECK (P/N: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE, NEAR THE AFT END OF THE PART
- [SDR 2A6D20230523002](https://openairdocs.org/sdr/2A6D20230523002.md): Floorbeam · corroded · May 23, 2023 · N118LN · Snias AS350B3 · Fuselage Main, Floor Beam
  > DURING INSPECTION, CORROSION DAMAGE WAS DISCOVERED TO THE R/H CABIN FLOOR EDGING P/N: 350A21-1359-21.
- [SDR 2A6D20230510001](https://openairdocs.org/sdr/2A6D20230510001.md): Deck Plate · chafed · May 10, 2023 · N3831 · Snias AS350B3 · Fuselage Structure (General)
  > CHAFING WAS DISCOVERED IN 2 PLACES ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE FIRST DAMAGE AREA IS APPROXIMATELY 0.300” LONG, 0.275”WIDE, AND 0.015” DEEP AT THE DEEPEST POINT. THE SECOND DAMAGE AREA IS APPROX

Next page: https://openairdocs.org/engine/safran-arriel-2b1/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 engine_model_key = 'ARRIEL2B1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/safran-arriel-2b1/reports

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