# Service difficulty reports: Helibras AS 350 B3

A list on [Helibras AS 350 B3](https://openairdocs.org/model/helibras-as-350-b3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 21 · 1,007 reports

- [SDR QMLA2026090620062](https://openairdocs.org/sdr/QMLA2026090620062.md): Gearbox · making metal · Sep 4, 2026 · N507AM · Snias AS350B3 · Tail Rotor Gearbox
  > TRGB CHIP LIGHT. INSPECTED AND CLEANED TGB CHIP DETECTOR. ALL MAINTENANCE COMPLETED.
- [SDR 2026F00191](https://openairdocs.org/sdr/2026F00191.md): Sliding Door · damaged · Aug 28, 2026 · N31BH · Snias AS350B3 · Service Doors
  > LEFT HAND CARGO DOOR DEPARTED DURING FLIGHT. DOOR WAS IN THE OPEN POSITION, LOCKED TO THE REAR.
- [SDR QMLA2026070520043](https://openairdocs.org/sdr/QMLA2026070520043.md): Outlet · odor · Jul 3, 2026 · N810LF · Snias AS350B3 · Equipment/Furnishings Wiring
  > FLIGHT CREW REPORTED SMOKE ODOR IN CABIN DURING FLIGHT.
- [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 4DSR20260604001](https://openairdocs.org/sdr/4DSR20260604001.md): Cradle · damaged · Jun 4, 2026 · N614TC · Snias AS350B3 · Fuel Storage
  > DURING INSTALLATION OF SB AS350-28.91.98R0 REPLACEMENT OF THE STANDARD FUEL TANK BY A CRASH-RESISTANT FUEL SYSTEM(CRFS), IT WAS FOUND THAT THE FWD CRADLE P/N: 350A08-1122-03 RECEIVED IN THE KIT P/N: 350R08-1009-0072 WAS MISSING THE REQUIRED NUT PLATE FOR BONDI
- [SDR QMLA202605120030](https://openairdocs.org/sdr/QMLA202605120030.md): Battery · unserviceable · May 11, 2026 · N4497Y · Snias AS350B3 · Battery/Charger System
  > BATTERY LIGHT ON. COMPLETED BY PLACING REMOVED BATTERY ON BATTERY MINDER. INSTALLED SERVICEABLE BATTERY IAW ICA. RECORDED BATTERY VDC AT INSTALL / CHARGE COMPLETION. OP& RSQUO;S CHECK GOOD. CURRENT BATTERY VDC: 26.64 VISUALLY INSPECTED AIRCRAFT EXTERIOR FOR LI
- [SDR 9SZA202609100148](https://openairdocs.org/sdr/9SZA202609100148.md): Terminal · loose · Mar 24, 2026 · N362AC · Snias AS350B3 · Fire Protection System Wiring
  > ENGINE FIRE CAUTION LIGHT INTERMITTENT. FIRE DETECTORS PASSED BENCH TEST PROCEDURES IAW MM. WITH EXCESSIVE VIBRATION AND MOVEMENT, ENG FIRE CAUTION LIGHT INTERMITENT ILLUMINATION.
- [SDR 9SZA202607100147](https://openairdocs.org/sdr/9SZA202607100147.md): Terminal · loose · Mar 24, 2026 · N362AC · Snias AS350B3 · Fire Protection System Wiring
  > ENGINE FIRE CAUTION LIGHT INTERMITTENT. FIRE DETECTORS PASSED BENCH TEST PROCEDURES IAW MM. WITH EXCESSIVE VIBRATION AND MOVEMENT, ENG FIRE CAUTION LIGHT INTERMITENT ILLUMINATION.
- [SDR QMLA031820019](https://openairdocs.org/sdr/QMLA031820019.md): Oil System · overtemp · Mar 18, 2026 · N4204 · Snias AS350B3 · Turbine Engine Oil System
  > UPON DEPARTING PRESCOTT (KPRC) FOR COTTONWOOD (P52), AIRCRAFT ENGINE OIL TEMPERATURE CLIMBED TO ABOVE LIMITS, (139+) DURING DEPARTURE FROM THE DOWNWIND. PILOT TURNED BACK TO THE AIRPORT, DECLARED AN EMERGENCY, AND LANDED WITHOUT FURTHER INCIDENT AT CUTTER AVIA
- [SDR QMLA2026030720015](https://openairdocs.org/sdr/QMLA2026030720015.md): Unknown · odor · Mar 7, 2026 · N108LN · Snias AS350B3 · Air Distribution System
  > STRANGE BURNING ODOR AND SMELL IN CABIN OF AIRCRAFT.
- [SDR PN1R202602200002](https://openairdocs.org/sdr/PN1R202602200002.md): Servo Control · leaking · Feb 20, 2026 · N568AE · Snias AS350B3 · Rotorcraft Servo System
  > DURING INSPECTION FOUND RIGHT HAND MAIN ROTOR SERVO HAS STATIC LEAK. REPLACED SERVO.
- [SDR QMLA2025121320124](https://openairdocs.org/sdr/QMLA2025121320124.md): Line · failed · Dec 10, 2025 · N350MV · Snias AS350B3 · Airspeed/Mach Indicator
  > AIRSPEED INDICATOR FAILED IN FLIGHT, REMOVED DASH AND FOUND 1 DISCONNECTED PITOT LINE FROM THE AIRSPEED INDICATOR, R & R PRESSURE PITOT LINE P DHS212-720.20. PREFORMED CHECK OF THE PITOT LINE & AIRSPEED WITH NO DEFECTS NOTED IAW AMM 34-14-00,5-1. AIRSPEED I
- [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 2025F00249](https://openairdocs.org/sdr/2025F00249.md): Deck Plate · dented · Oct 23, 2025 · N350LF · Snias AS350B3 · Fuselage Miscellaneous Structure
  > A DENT WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROX. 0.6" LONG, 0.6" WIDE WITH A MAXIMUM DEPTH OF 0.0120".
- [SDR 4DSR20251023002](https://openairdocs.org/sdr/4DSR20251023002.md): Brake · out of tolerance · Oct 23, 2025 · N613TC · Snias AS350B3 · Main Rotor Brake
  > DURING A SCHEDULED 12YR INSPECTION, THE MGB ROTOR BRAKE WAS FOUND TO BE OUT OF TOLERANCE/LOOSE AND REQUIRED REPLACEMENT. RECEIVED ROTOR BRAKE P/N: 350A32-0500-02 FROM NAMPA VALLEY HELICOPTERS IN "REPAIRED" STATUS/WORK. AFTER VISUAL RECEIVING INSPECTION, THE AT
- [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 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 QMLA2025081920089](https://openairdocs.org/sdr/QMLA2025081920089.md): Motor · failed · Aug 19, 2025 · N418TY · Snias AS350B3 · Air Distribution Fan
  > BURNING ODOR PRODUCED WHILE RUNNING AIR CONDITIONING SYSTEM.
- [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 QMLA20250820083](https://openairdocs.org/sdr/QMLA20250820083.md): Fuel Cap · leaking · Aug 4, 2025 · N108L · Snias AS350B3 · Fuel Storage
  > PILOT REPORTED AT 0410 THAT THE CREW SMELT FUEL IN THE CABIN. AIRCRAFT TAKEN OUT OF SERVICE. ARRIVED AT BASE AND HEARD FROM THE PILOT THAT THE CREW HAD SMELT A PROPANE LIKE SMELL. ASKED IF THEY HAD GOTTEN FUELED BEFORE RETURNING TO BASE, THEY DID GET FUEL BEF
- [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 2025FA0000511](https://openairdocs.org/sdr/2025FA0000511.md): Pump · damaged · Jul 12, 2025 · N544AS · Snias AS350B3 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT WAS FLYING AN EXTERNAL LOAD OPERATION WHEN THE PILOT NOTICED THE RED LOW HYDRAULIC WARNING IND LIGHT WAS ILLUMINATED. THE PILOT WAS ABLE TO SAFELY SET LOAD ON THE GROUND AND LAND BACK AT THE HELI-PAD. UPON VISUAL INSPECTION OF THE HYDRAULIC PUMP, THE
- [SDR QMLA2025062120068](https://openairdocs.org/sdr/QMLA2025062120068.md): Sensor · failed · Jun 20, 2025 · N109LN · Snias AS350B3 · Main Rotor System
  > LOSS OF NR INDICATION ONE CLIMB OUT. REMOVED NR SPEED SENSOR AND REPLACED WITH NEW AS PER AIRBUS AS350B3 AMM 62-31-00, 4-3.CLEANED AND APPLIED STABILANT 22 TO MGB HARNESS CANON PLUG. GROUND RAN AIRCRAFT. OPS CHECK GOOD.
- [SDR M3XA202506165003](https://openairdocs.org/sdr/M3XA202506165003.md): Bearing · failed · Jun 16, 2025 · N855MB · Snias AS350B3 · Hydraulic Pump (Electric/Engine), Main
  > PILOT PERFORMED A PRECAUTIONARY LANDING FOR #2 HYDRAULICS FAILED IN FLIGHT. MECHANIC DISCOVERED THE HYDRAULIC PUMP BELT HAD SHEARED. DURING REMOVAL IT WAS DISCOVERED THE HYDRAULIC PUMP BEARING FAILED AND CAUSED THE BELT TO SHEAR. MECHANIC REMOVED AND REPLAC
- [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 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 2025FA0000364](https://openairdocs.org/sdr/2025FA0000364.md): Starflex · excess play · May 20, 2025 · N191NR · Snias AS350B3 · Main Rotor Head
  > NOTE: MODEL IS AS350B3. DURING INSPECTION, FOUND 3EA M/R STARFLEX BALL JOINT BEARINGS HAD EXCESSIVE PLAY. INSTALLED 3EA NEW P/N 704A33633124 BALL JOINT BEARINGS.
- [SDR QMLA2025042920054](https://openairdocs.org/sdr/QMLA2025042920054.md): Bonding Wire · broken · Apr 29, 2025 · N807LF · Snias AS350B3 · Main Rotor Head
  > BONDING BRAIDS (P/N SA350A31185100) ARE PRONE TO BREAKING PREMATURELY AND ARE NOT LASTING AS EXPECTED. DESPITE PROPER INSTALLATION, THE COMPONENTS SHOW SIGNS OF FAILURE AFTER MINIMAL FLIGHT HOURS, INDICATING A POTENTIAL DURABILITY ISSUE.
- [SDR 4DSR202504170637](https://openairdocs.org/sdr/4DSR202504170637.md): Ball Joint · scored · Apr 17, 2025 · N6968A · Snias AS350B3 · Main Rotor Mast/Swashplate
  > DURING A SCHEDULED 300HR INSPECTION OF THE M/R SWASHPLATE BALL-JOINT, THE SWASHPLATE GUIDE WAS FOUND TO HAVE SCORING AROUND THE ENTIRE SURFACE. PER AIRBUS AS350B3 AMM 62-32-00, 6-3 PROCEDURE FIGURE 1. DAMAGE IN ZONE A IS NONE REQUIRING REPLACEMENT OF THE GUIDE
- [SDR QMLA2025041420049](https://openairdocs.org/sdr/QMLA2025041420049.md): Windshield · defective · Apr 13, 2025 · N493LG · Snias AS350B3 · Flight Compartment Windows
  > UPON COMPLETION OF INSTALLATION OF A NEW AIRBUS LEFT HAND WINDSHIELD ASSEMBLY, PART NUMBER 350A25137403, SERIAL NUMBER 1745 THE PROTECTIVE PLASTIC COVERING WAS REMOVED FROM THE EXTERIOR OF THE WINDSHIELD. AFTER REMOVAL OF PROTECTIVE PLASTIC COVERING IT WAS DIS
- [SDR QMLA2025030420032](https://openairdocs.org/sdr/QMLA2025030420032.md): Unknown · odor · Mar 4, 2025 · N508AM · Snias AS350B3 · Air Distribution System
  > BURNING SMELL IN FLIGHT. RTB. NO OTHER ISSUES.
- [SDR QMLA2025022620028](https://openairdocs.org/sdr/QMLA2025022620028.md): Unknown · vibration · Feb 26, 2025 · N355CF · Snias AS350B3 · Standard Practices/Structures
  > VIBRATION IN SEAT AND PEDALS
- [SDR 2025FA0000123](https://openairdocs.org/sdr/2025FA0000123.md): Bearing · deteriorated · Feb 20, 2025 · N804CP · Snias AS350B3 · Tail Rotor Blades
  > DURING INSPECTION, FOUND T/R LAMINATED HALF SHELL BEARINGS DETERIORATED BEYOND ACCEPTABLE LIMITATIONS.
- [SDR QMLA2025021920020](https://openairdocs.org/sdr/QMLA2025021920020.md): Warning Light · false activation · Feb 18, 2025 · N533AM · Snias AS350B3 · Central Warning
  > PILOT REPORTED THAT DURING APPROACH TO LANDING, HE GOT A AMBER GOV LIGHT. HE ABORTED LANDING AND DIVERTED TO EL PASO FBO. VEMD FAULT CODES WHERE SW ENG CTL (HEX 4204 AND HEX 000C) EMM REFERRED TO START STOP SWITCH, AIRCRAFT JUST CAME OUT OF HEAVY MAINTENANCE
- [SDR QMLA2025020320012](https://openairdocs.org/sdr/QMLA2025020320012.md): Unknown · odor · Feb 2, 2025 · N108LN · Snias AS350B3 · Air Distribution System
  > DURING TAKE-OFF AND CLIMB THERE WAS A STRONG ODOR THROUGHOUT THE CABIN. THE BEST WAY TO DESCRIBE IT, IS THAT IT SMELLS LIKE PROPANE. THIS HAS BEEN AN ONGOING ISSUE WITH THE AIRCRAFT. THE CREW DID NOT FEEL COMFORTABLE FLYING IN THE AIRCRAFT UNTIL FIXED, SO THE
- [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 2024FA0000956](https://openairdocs.org/sdr/2024FA0000956.md): Bulkhead · chafed · Dec 10, 2024 · N490H · Snias AS350B3 · Fuselage Main, Bulkhead
  > AS350 S/N 4539 NOTED CHAFING DAMAGE ON THE LH LATERAL BULKHEAD (X FRAME) ON THE INBOARD FACE AS SHOWN IN FIGURE 1. THE LH X-FRAME HAS ONE CHAFED AREA LOCATED ON ITS INBD BEADED FACE MEASURING APPROXIMATELY 0.90” LONG AND 0.30” WIDE WITH A MAX DEPTH OF 0.024”
- [SDR 2024FA0000955](https://openairdocs.org/sdr/2024FA0000955.md): Mount · chafed · Dec 10, 2024 · N490H · Snias AS350B3 · Rotorcraft Tail Boom
  > TAIL GEARBOX MOUNTING PLATE CHAFE DAMAGE.
- [SDR 2024F00314](https://openairdocs.org/sdr/2024F00314.md): Support · chafed · Dec 10, 2024 · N490H · Snias AS350B3 · Fuselage Main, Structure
  > THE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE.
- [SDR 4DSR202412050001](https://openairdocs.org/sdr/4DSR202412050001.md): Support Bracket · corroded · Dec 5, 2024 · N6974A · Snias AS350B3 · Rotorcraft Tail Boom
  > DURING A SCHEDULED 12YR (144M) INSPECTION OF THE TAIL BOOM SECTION, THE NO. 6 BEARING SUPPORT BRACKET WAS FOUND TO HAVE MAJOR CORROSION TO THE INSIDE BOTTOM LEFT CORNER OF THE BRACKET. AIRBUS TECH REP WAS CONTACTED AND DETERMINED TO BE A MINOR REPAIR. R&R OF T
- [SDR QMLA2024102420138](https://openairdocs.org/sdr/QMLA2024102420138.md): Sending Unit · malfunctioned · Oct 21, 2024 · N267AM · Snias AS350B3 · Fuel Indicating System
  > FUEL SYSTEM IS SUSPECTED OF NOT INDICATING PROPERLY, SEE AIDMOR FOR FULL DESCRIPTION.
- [SDR 4DSR202409110001](https://openairdocs.org/sdr/4DSR202409110001.md): Skin Panel · cracked · Sep 11, 2024 · N6977A · Snias AS350B3 · Rotorcraft Tail Boom
  > AIRBUS AS350B3E: DURING A SCHEDULED 12YR INSPECTION, THE TAIL BOOM WAS INSPECTED FOR CRACKS. A CRACK WAS DISCOVERED ON THE RIGHT-SIDE SKIN PANEL. THE CRACK IS NEAR THE AFT EDGE FEED THROUGH OPENING FOR THE HORIZONTAL STABILIZER. AIRBUS WAS CONTACTED AND A REP
- [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 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 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 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 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 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 QMLA2024070520082](https://openairdocs.org/sdr/QMLA2024070520082.md): Motor · failed · Jul 5, 2024 · N279AM · Snias AS350B3 · Air Distribution Fan
  > INFLIGHT RETURN TO BASE LEG PILOT REPORTED A BURNING SMELL IN CABIN, TURNED OFF A/C SYSTEM AND SMELL WENT AWAY. LANDED AIRCRAFT AT 94E AIRPORT. WHEN MECHANIC WAS INSPECTING THE AIRCRAFT FOUND THAT AIR COMM AFT EVAPORATOR BLOWER MOTOR HAD FAILED AND WAS THE CA

Next page: https://openairdocs.org/model/helibras-as-350-b3/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 = 'AS350B3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/helibras-as-350-b3/reports

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