# Service difficulty reports: Bell 222U

A list on [Bell 222U](https://openairdocs.org/model/bell-222u.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 212 reports

- [SDR CA190426021](https://openairdocs.org/sdr/CA190426021.md): Engine · power loss · Apr 26, 2019 · Bell 222U · Engine (Turbine/Turboprop)
  > (CAN) REPORTED TO HAVE A POWER LOSS SHORTLY AFTER TAKEOFF AND CRASHED INTO RESIDENTIAL BUILDINGS AIRCRAFT CAME TO REST ON THE LEFT SIDE. EXTENT OF INJURIES NOT REPORTED BUT NO FATALITIES INVOLVED. (TC# 20190426021)
- [SDR QMLA2015031315016](https://openairdocs.org/sdr/QMLA2015031315016.md): Bolt · sheared · Mar 13, 2015 · N427MA · Bell 222U · Main Rotor Head
  > DURING AN AIRFRAME ZONE 1 INSPECTION, FOUND ONE SIDE OF THE MR HUB, PN 222-012-101-107 SN A98, CORD WEIGHT MOUNT LOOSE. UPON REMOVAL OF THE NUT FROM THE LONG, ALL THREAD, PORTION OF THE MOUNT & THE WEIGHT ITSELF, FOUND ONE BOLT HEAD LAYING LOOSE UNDER THE WEI
- [SDR QMLA2014090514107](https://openairdocs.org/sdr/QMLA2014090514107.md): Engine · leaking · Sep 5, 2014 · N222MN · Bell 222U · Engine (Turbine/Turboprop)
  > RETURNING TO BASE AT THE COMPLETION OF A SCENE FLIGHT, THE ECS UNIT WAS TURNED ON. AFTER A FEW MINUTES THE MEDIC, IN THE CABIN, STATED THAT THERE WAS A FOG IN THE CABIN & A STRONG SMELL OF JET FUEL. THE PILOT BACKED UP BY THE NURSE HOLDING THE RFM RAN THE SM
- [SDR QMLA2014050614050](https://openairdocs.org/sdr/QMLA2014050614050.md): Fuel Line · broken · May 6, 2014 · N222AM · Bell 222U · Fuel Controlling System
  > WHILE IN CRUISE FLIGHT, THE NR 1 ENG BEGAN RUNNING ERRATICALLY & THE NP WAS ATTEMPTING TO OVER SPEED. THE PILOT WAS ABLE TO ARREST THE ENG POWER BY MANUALLY RETARDING THE NG CONTROL TWIST GRIP. MADE AN UNEVENTFUL LANDING AT KBVU. MADE AN INITIAL VISUAL INSP
- [SDR QMLA2013073013108](https://openairdocs.org/sdr/QMLA2013073013108.md): Wire · frayed · Jul 30, 2013 · N222MN · Bell 222U · Engine Indicating System Wiring
  > PILOT REPORTED HIGH OIL TEMP WITH CONTINOUS RISING ON NR 1 ENGINE. MADE A PRECAUTIONARY LANDING. ON APPROACH NOTICED THE OIL PRESSURE WAS ALSO HIGH ON NR 1 ENGINE. TROUBLESHOT & FOUND MOISTURE (OIL AND WATER) IN THE MAIN ENGINE ELECTRICAL DISCONNECT CONNEC
- [SDR QMLA2013063013087](https://openairdocs.org/sdr/QMLA2013063013087.md): Cable · broken · Jun 30, 2013 · N220LN · Bell 222U · Fire Protection System Wiring
  > PILOT WAS IN FLIGHT TO REFUEL AFTER A CALL. DURING FLIGHT HE OBSERVED THE NR 1 ENG FIRE WARNING LIGHT FLICKERING INTERMITTENTLY AND PROCEEDED TO LAND AT THE BASE. AFTER RECEIVING THE CALL-OUT, RESPONDED TO THE BASE AND STARTED TROUBLESHOOTING FOR A FAULTY FI
- [SDR QMLA2013031313039](https://openairdocs.org/sdr/QMLA2013031313039.md): Skin · cracked · Mar 13, 2013 · N222AM · Bell 222U · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE, FOUND CRACK IN BELLY SKIN APPROX,.7".
- [SDR QMLA2013F00086](https://openairdocs.org/sdr/QMLA2013F00086.md): Skin · cracked · Mar 13, 2013 · N222AM · Bell 222U · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE FOUND.7 INCH CRACK IN BELLY SKIN AT FS 245.3, BL -16, WL 25.
- [SDR 2013F00083](https://openairdocs.org/sdr/2013F00083.md): Skin · cracked · Mar 13, 2013 · N222AM · Bell 222U · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE FOUND CRACK.7 IN LONG IN LOWER LEFT BELLY SKIN TRAILING EDGE AT FS 245.3-246 BL -16 WL 25.
- [SDR QMLA2012121912193](https://openairdocs.org/sdr/QMLA2012121912193.md): Bulkhead · cracked · Dec 19, 2012 · N431MA · Bell 222U · Fuselage Main, Bulkhead
  > DURING 300HR AF INSPECTION, DISCOVERED A CRACK RUNNING FORE AND AFT ALMOST CENTERLINE BETWEEN THE HYD FILTER BRACKETS. AFTER A THOROUGH CLEANING, ADDITIONALLY FOUND THE CRACK EXTENDING TO STA 233 TO THE DRIP PAN AND ALSO INTERNAL BEHIND THE RADIO RACK.
- [SDR QMLA2012103012172](https://openairdocs.org/sdr/QMLA2012103012172.md): Transmission · contaminated · Oct 30, 2012 · N222LN · Bell 222U · Main Rotor Gearbox
  > DURING CRUISE FLIGHT, LOWER TRANSMISSION CHIP LIGHT ILLUMINATED. PRESSURE AND TEMPERTURE WERE NORMAL RANGE. CHIP WOULD NOT BURN OFF.
- [SDR QMLA2012101712168](https://openairdocs.org/sdr/QMLA2012101712168.md): Longeron · cracked · Oct 17, 2012 · N222MN · Bell 222U · Fuselage Main, Longeron/Stringer
  > DURING AIRFRAME ZONE 9, INSPECTION, FOUND MULTIPLE SMALL CRACKS IN AIRFRAME AND DOUBLERS ON THE TAIL ROTOR DIRECTIONAL SUPPORT LONGERONS FROM BS 340 TO 356 AND THE AFT SUPPORT FOR LONGERONS AT BS 356. CRACKS ARE ON A PREVIOUSLY REPAIRED LOCATIONS ON THE LONGE
- [SDR QMLA2012090612146](https://openairdocs.org/sdr/QMLA2012090612146.md): Skin · cracked · Sep 6, 2012 · N222LN · Bell 222U · Fuselage Main, Plate/Skin
  > DURING AIRWORTHINESS CHECK, A CRACK IN A PRE-EXISTING SKIN REPAIR LOCATED ON THE TOP DECK OF THE HELICOPTER BETWEEN THE SYS 1 AND 2 HYD FILTER MANIFOLDS AT APPROX BS 233. ON REMOVAL OF CRACKED PATCH, A TWO PART CRACK APPROX 5 INCHES RUNNING FORE & AFT WAS UNCO
- [SDR QMLA2012032912038](https://openairdocs.org/sdr/QMLA2012032912038.md): Actuator · inoperative · Mar 29, 2012 · N222AM · Bell 222U · Power Lever
  > ON A ROUTINE ENGINE OVERSPEED SYS CHECK, WANTED TO INCREASE THE ENGINE RPM SLIGHTLY WITH THE TRIM SWITCH. FOUND UNABLE TO GET THE SWITCH TO DO ANYTHING. ON INSPECTION, MECHANIC FOUND THAT THE LINEAR ACTUATOR WAS INOPERATIVE AND SUBSEQUENTLY REPLACED THAT PAR
- [SDR QMLA2012031512029](https://openairdocs.org/sdr/QMLA2012031512029.md): Shaft · sheared · Mar 15, 2012 · N222LN · Bell 222U · Turbine Engine Accessory Drive
  > DURING CRUISE FLIGHT, NR 2 ENGINE OIL TEMPERATURE JUMPED FROM 80 DEGREES C TO OVER 120 DEGREES C. THE FLIGHT WAS ABORTED AND RETURNED TO BASE USING MINIMUM POWER FROM THE ENGINE UNTIL LANDING, APPROXIMATLY 10 MINUTES LATER. OIL PRESSURE REMAINED IN THE GRE
- [SDR QMLA2012012612010](https://openairdocs.org/sdr/QMLA2012012612010.md): Connector · dirty · Jan 26, 2012 · N427MA · Bell 222U · Hydraulic Power System Wiring
  > DURING FLIGHT PILOT REPORTED NR 1 HYD PRESSURE DROPPED TO ZERO. MECHANIC INSPECTED, CLEANED ELECRICAL CONNECTORS, FUNCTION CHECKED SYS. OPS CHECK FLIGHT PERFORMED WITH NO FURTHER FAULTS.
- [SDR CA111130011](https://openairdocs.org/sdr/CA111130011.md): Arm · damaged · Nov 30, 2011 · Bell 222U · Main Rotor Head
  > (CAN) UPON INSPECTION OF THE ARM ASSY, IT WAS FOUND THAT THE INNER SURFACE AT THE AREA SURROUNDING THE FLOATING BUSHING HAD SEVERE MECHANICAL DAMAGE. DAMAGE WAS FOUND TO 50 PERCENT OF THE CIRCUMFERENCE OF THE AFFECTED AREA.
- [SDR QMLA2011101811101](https://openairdocs.org/sdr/QMLA2011101811101.md): Bracket · cracked · Oct 18, 2011 · N222AM · Bell 222U · Auxiliary Gear (Tail Skid)
  > TAIL SKID BRACKET ON BOTTOM OF VERTICAL FIN CRACKED AT TAIL STINGER AND TAIL ROTOR GUARD ATTACHMENT POINT. REMOVED VERTICAL FIN TO FACILITATE REMOVAL OF CRACKED BRACKET. REPLACED BRACKET WITH NEW TAIL SKID BRACKET AND REINSTALLED VERTICAL FIN.
- [SDR QMLA2011101411099](https://openairdocs.org/sdr/QMLA2011101411099.md): Bulkhead · cracked · Oct 14, 2011 · N427MA · Bell 222U · Fuselage Main, Bulkhead
  > CRACK IN BULKHEAD ASSY, 222-031-506-103 (BHT-222U-MM-5 FIG 53-1029, NR 32) AT FASTENER THAT ATTACHES SUPPORT LT, 222-031-522-101 (BHT-222U-MM-5 FIG, 53-1028, NR 11). CRACK ON INSIDE FACE OF BULKHEAD NR STA 270, BL 8.0L TO 10.0L, WL 79.0 TO 80.5. BULKHEAD ASSY
- [SDR QMLA2011082311088](https://openairdocs.org/sdr/QMLA2011082311088.md): Fitting · unserviceable · Aug 23, 2011 · N222MN · Bell 222U · Engine Bleed Air System
  > LIFTING, AT ABOUT 70 FT, ACFT SLIGHTLY YAWED & LOST POWER IN NR 1 ENGINE. TORQUE IN NR 2 ENGINE WAS AT MAX & NR 1 NG SURGING. LANDED AT NEARBY AIRFIELD. MX PERFORMED OPS GROUND RUN. NOTICED EXCESSIVE HOT AIR FROM ENGINE AT 0800 POSITION FUTHER INVESTIGATION
- [SDR QMLA2011080911083](https://openairdocs.org/sdr/QMLA2011080911083.md): Switch · faulty · Aug 9, 2011 · N222MN · Bell 222U · Fire Detection
  > FIRE DETECTION LIGHT CAME ON IN FLIGHT. PROBLEM FIXED BY REPLACING FIRE DETECTION SWITCH AND FIX WIRES ON LIGHT.
- [SDR QMLA2011072511082](https://openairdocs.org/sdr/QMLA2011072511082.md): Door Frame · cracked · Jul 25, 2011 · N222LN · Bell 222U · Fuselage Main, Structure
  > INTERMITTENT FLICKERING OF DOOR LIGHT ON CAUTION/ADVISORY PANEL MADE ME INITIATE A VISUAL INSPECTION OF CABIN DOOR FRAMES DUE TO PAST EXPERIENCE WITH CRACKS IN THESE AREAS CAUSING THIS LIGHT TO FLICKER. FOUND RIGHT CABIN DOOR FRAME, EXTRUSION, AND SKIN CRACKED
- [SDR QMLA2011061511065](https://openairdocs.org/sdr/QMLA2011061511065.md): Gearbox · making metal · Jun 15, 2011 · N220LN · Bell 222U · Turbine Engine Reduction Gear
  > AFTER ZONE INSPECTION ON NR1 ENGINE, ACFT WAS BEING GROUND RUN FOR LEAK CHECKS. ON START UP, THE ENGINE G/B CHIP LIGHT IMMEDIATELY CAME ON, PILOT SHUTDOWN STRAIGHT AWAY. MECHANIC PULLED THE CHIP PLUG AND FOUND NUMEROUS CHIPS ON THE PLUG. THIS WAS THE SECOND
- [SDR QMLA2011050211055](https://openairdocs.org/sdr/QMLA2011050211055.md): Bulkhead · cracked · May 2, 2011 · N222LN · Bell 222U · Fuselage Main, Bulkhead
  > DURING SCHEDULED MX, FOUND A CRACK ALONG STA 270 BULKHEAD, BUTTLINE 8.5 LT, WATERLINE 81.6. CRACK ORIGINATED FROM LOCK FASTENER JOINING LT AFT NODAL BEAM SUPPORT, PN 222-031-592-103 AND STA 270 BULKHEAD. NO PREVIOUS REPAIRS IN THIS AREA. ACFT OUT OF SERVICE.
- [SDR QMLA2011042511051](https://openairdocs.org/sdr/QMLA2011042511051.md): B-Nut · loose · Apr 25, 2011 · N431MA · Bell 222U · Hydraulic System, Main
  > PILOT NOTICED HYD FLUID LEAKING ON GROUND AND LT SIDE OF ACFT. MECHANIC ARRIVED AND SERVICED NR2 HYD SYS. PERFORMED GROUND RUN AND FOUND FLUID SQUIRTING FROM B-NUT/ T-FITTING ON THE RETURN LINE, COMING FROM THE FILTER MANIFOLD. DISCOVERED B-NUT WAS NOT EVEN
- [SDR QMLA2010092210062](https://openairdocs.org/sdr/QMLA2010092210062.md): Bulkhead · cracked · Sep 22, 2010 · N431MA · Bell 222U · Fuselage Main, Structure
  > DURING SCHEDULED MX, FOUND 2 STRUCTURAL CRACKS ALONG STA 270 BULKHEAD, BUTTLINE 8.5 LT, WATERLINE 81.6. CRACKS ORIGINATE FROM FASTENERS JOINING LT AFT NODAL BEAM SUPPORT PN 222-031-592-103 AND STA 270 BULKHEAD. NO PREVIOUS REPAIRS, ACFT OUT OF SERVICE.
- [SDR CA100603003](https://openairdocs.org/sdr/CA100603003.md): Blade · delaminated · May 26, 2010 · Bell 222U · Main Rotor Blades
  > THE PILOT AND CO-PILOT WERE THE ONLY 2 PERSONS ONBOARD THE ACFT DURING A TRAINING FLIGHT. AT APPROX 11,000`, PA AND 110 KIAS THE PILOTS NOTICED AN UNUSUAL VIBRATION AND ELECTED TO MAKE A PRECAUTIONARY LANDING. POST FLIGHT INSP BY A MX REVEALED DELAMINATION B
- [SDR QMLR3253U](https://openairdocs.org/sdr/QMLR3253U.md): Bulkhead · cracked · Mar 26, 2010 · N416MA · Bell 222U · Fuselage Main, Bulkhead
  > DURING OTHER MX, 2 CRACKS WERE FOUND IN BULKHEAD, PN 222-031-505-001 AT ATTACHMENT POINT OF NODAL BEAM SUPPORT, PN 222-031-519-103.
- [SDR QMLA2010031510006](https://openairdocs.org/sdr/QMLA2010031510006.md): Engine · out of rig · Mar 15, 2010 · N415MA · Bell 222U · Engine (Turbine/Turboprop)
  > UPON DEPARTURE FROM ROOFTOP PAD, NR 1 ENGINE TORQUE EXCEEDED 86.4 PERCENT AND NR 2 ENGINE TORQUE WAS NEAR ZERO WITH DECREASING RPM. ENDED UP THE ENG RIGGING NEEDED TO BE ADJUSTED.
- [SDR QMLA2010021710004](https://openairdocs.org/sdr/QMLA2010021710004.md): Receptacle · burned · Feb 17, 2010 · N911NM · Bell 222U · Equipment/Furnishings Wiring
  > CREWMEMBER DETECTED ELECTRICAL SMELL, SAW FLUID DRIPPING ON NEBULIZER PLUG IN THE AC OUTLET. UNPLUGGED NEBULIZER AND REMOVED FLUID BAG, SOLVED THE PROBLEM. ON POST-FLIGHT, FOUND THE OUTLET BREAKER WOULD NOT TEST. CALLED MX.
- [SDR QMLA2009052309019](https://openairdocs.org/sdr/QMLA2009052309019.md): Wire · broken · May 23, 2009 · N220LN · Bell 222U · Light System Wiring
  > THE ACFT HAD BEEN STARTED IN RESPONSE TO A REQUEST FOR A SCENE CALL AND JUST BEEN BROUGHT TO A HOVER, DETECTED SMOKE IN THE COCKPIT. THE ACFT WAS SET BACK DOWN ON THE PAD, WHILE SCANNING THE INSTRUMENTS AND COCKPIT FOR A SOURCE OF THE SMOKE. IT WAS OBSERVED CO
- [SDR QMLA20090213](https://openairdocs.org/sdr/QMLA20090213.md): Vent Line · worn · Feb 13, 2009 · N227AM · Bell 222U · Fuel Storage
  > MED CREWS SMELLED ODOR INSIDE ACFT. FLIGHT WAS ABORTED AND RETURNED TO BASE. MX IDENTIFIED AND CHANGED VENT TUBE.
- [SDR QMLA1218200808056](https://openairdocs.org/sdr/QMLA1218200808056.md): Unknown · odor · Dec 18, 2008 · N224LN · Bell 222U · Air Distribution System
  > ACFT DEPARTED HOSPITAL FOR RETURN TO BASE ON THIRD LEG OF SECOND MISSION OF THE DAY. APPROX 5 MIN INTO FLIGHT, A CREWMEMBER STATED THAT HE SMELLED AN ELECTRICAL ODOR EMITTING IN THE AFT AREA OF THE CABIN. PILOT CHECKED GAUGES, WHICH ALL WERE IN NORMAL OPERATIN
- [SDR CA081222008](https://openairdocs.org/sdr/CA081222008.md): Servo · unknown · Dec 8, 2008 · Bell 222U · Rotorcraft Servo System
  > (CAN) SOLID RESISTANCE FELT WITH AFT CYCLIC MOVEMENT DURING OPERATIONS WITH FORCE TRIM ON & UTILIZING CYCLIC TRIM RELEASE SWITCH. ON FIRST OCCURRENCE RESISTANCE RELEASED WITH A FIRM BUMP & FAULTY LT CYCLIC TRIM RELEASE SWITCH SUSPECTED HOWEVER WITH SECOND OCC
- [SDR QML2008F00016](https://openairdocs.org/sdr/QML2008F00016.md): Brake · out of adjust · Oct 16, 2008 · N402MA · Bell 222U · Main Rotor Brake
  > ON REPOSITION FLIGHT, APPROX 6 MILES FROM LANDING, ROTOR BREAK AND MASTER CAUTION ILLUMINATED. THIS IS A LAND AS SOON AS POSSIBLE EVENT. CONSULTED THE CHECKLIST. VERIFIED POSITION OF ROTOR BREAK HANDLE. THE HANDLE WAS SECURE. IN ADDITION, VERIFIED TRANSMI
- [SDR 4756705112008](https://openairdocs.org/sdr/4756705112008.md): Selector Switch · worn · May 11, 2008 · N220LN · Bell 222U · Fuel Selector/Shut-Off Valve
  > PILOT, COMING ONTO SHIFT, REFUELED THE AIRCRAFT, DID HIS PREFLIGHT INSPECTION, AND SAW NOTHING UNUSUAL AT 0900. AT 1017, THE AIRCRAFT WAS LAUNCHED ON A SCENE CALL, CLIMBED TO 4,500 FEET MSL AND LEVELED OFF IN CRUISE FLIGHT WHEN THE AC YAWED AND THE NR2 ENGINE
- [SDR 475332837](https://openairdocs.org/sdr/475332837.md): Structure · cracked · Aug 14, 2007 · N222HX · Bell 222U · Rotorcraft Tail Boom
  > TAILBOOM HAS CRACK APPROXIMATELY 1.26 INCHES LONG, 8 INCHES FORWARD OF THE VERTICAL STABILIZER. BOOM STATION 229.2 WL 82.19
- [SDR BAQA200700022](https://openairdocs.org/sdr/BAQA200700022.md): Blade · loose · Jun 27, 2007 · N587MG · Bell 222U · Tail Rotor Blades
  > WHILE COMPLETING A GROUND RUN FOR MAINTENANCE, A VIBRATION WAS FELT, AIRCRAFT WAS SHUTDOWN, AND FOUND THE IB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYLE BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIRED.
- [SDR 2007F00034](https://openairdocs.org/sdr/2007F00034.md): Lever · loose · May 9, 2007 · N222UT · Bell 222U · Main Rotor Mast/Swashplate
  > ON COLLECTIVE LEVER P/N 222-010-497-109FM, PIN P/N 222-010-456-005 SPUN INSIDE BORE OF COLLECTIVE LEVER PRODUCING A BLACK GREASE TRAIL ON SWASHPLATE AND LEVER ASSY. PIN IS THERMAL FIT AND PRESSED INTO COLLECTIVE LEVER. THE PIN BORE OF COLLECTIVE LEVER IS WORN
- [SDR HEEA109824](https://openairdocs.org/sdr/HEEA109824.md): Actuator · malfunctioned · Jun 17, 2006 · N6992 · Bell 222U · Compressor Bleed Control
  > ENROUTE TO PICK UP PATIENT, HEARD POPPING NOISE FROM THE NR 1 ENGINE SIDE. RETURNED TO BASE AND CREW WENT BY FIXED WING. REPLACED ACTUATOR. BENCH CHECK REVEALS AT 60 PSI WITH ACTUATOR HOT EXHIBITS VERY RATCHETY OPERATION.
- [SDR HEEA109823](https://openairdocs.org/sdr/HEEA109823.md): Actuator · malfunctioned · Jun 16, 2006 · N6992 · Bell 222U · Compressor Bleed Control
  > ENROUTE TO PICK UP PATIENT, PILOT AND CREW HEARD 3 SHARP LOUD NOISES FROM TOP OF AIRCRAFT WITHIN 10 MINUTES. DIVERTED TO NEAREST AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. ADJUSTED ACTUATOR RANGE.
- [SDR 47540060306](https://openairdocs.org/sdr/47540060306.md): Tube · cracked · Jun 3, 2006 · N402MA · Bell 222U · Fuel Controlling System
  > ONE OF THE AIR LINES THAT RUNS FROM THE FUEL CONTROL TO THE OVERSPEED SOLENOID CRACKED AT A FLARE, CAUSING ENGINE TO DECEL.
- [SDR HEEA107416](https://openairdocs.org/sdr/HEEA107416.md): Transmitter · failed · Dec 17, 2005 · N6992 · Bell 222U · Engine Oil Pressure
  > NR 1 ENGINE OIL PRESSURE GAUGE PEGGED OUT ON THE HIGH SIDE. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE TRANSMITTER.
- [SDR 47504123104](https://openairdocs.org/sdr/47504123104.md): Servo · failed · Dec 31, 2004 · N431MA · Bell 222U · Hydraulic Power System
  > SCENE FLIGHT FROM BASE 7 LAS VEGAS, NV TO JEAN, NV TO UNIVERSITY MEDICAL CENTER (UMC), LAS VEGAS, NV. APPROXIMATELY 1 MILE SOUTH OF UMC, NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIEN
- [SDR 047504123104](https://openairdocs.org/sdr/047504123104.md): Servo · malfunctioned · Dec 31, 2004 · N431MA · Bell 222U · Hydraulic System, Main
  > NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACED SERVO.
- [SDR 47567122504](https://openairdocs.org/sdr/47567122504.md): Link · failed · Dec 25, 2004 · N220LN · Bell 222U · Main Rotor Transmission Mount
  > WHILE IN CRUISE FLIGHT WITH PATIENT ABOARD. TWO LOAD BANGS WERE HEARD. A PRECAUTIONARY LANDING WAS MADE AT DCU. LANDED AIRCRAFT AND INSPECTED DOORS. NOTHING WAS FOUND. RESUMED THE FLIGHT AND APPROXIMATELY 2 MIN LATER A LOUD BANG BEGAN ACCOMPANIED BY VIBRATION
- [SDR CA041007009](https://openairdocs.org/sdr/CA041007009.md): Skin · cracked · Sep 29, 2004 · Bell 222U · Rotorcraft Tail Boom
  > (CAN) CARRYING OUT A DAILY CHECK IT WAS OBSERVED THAT A VERTICAL LATERAL CRACK HAD DEVELOPED ON THE LOWER SKIN OF TAILBOOM JUST 5 INCHES AFT OF THE HORIZONTAL STABILIZER. THE SKIN IS 2024 T3.032 IN.
- [SDR BAQA094473](https://openairdocs.org/sdr/BAQA094473.md): Indicator · sticks · Apr 30, 2004 · N223HX · Bell 222U · Fuel Quantity Indicator
  > FUEL QYT INDICATOR RT NEEDLE STICKS ON UNIT. REPLACED WITH SERVICABLE UNIT. 05/10/2004
- [SDR BAQA092500](https://openairdocs.org/sdr/BAQA092500.md): Indicator · reads high · Apr 22, 2004 · N587MG · Bell 222U · Hydraulic Indicating System
  > TEP GAUGE READS 50 DEGREES HIGH. ABOVE P.O. NR WAS CUT FOR A/C S/N 47534, BUT WAS USED ON A/C S/N 47566. REPLACED WITH SERVICABLE UNIT. 05/04/2004
- [SDR BAQA094048](https://openairdocs.org/sdr/BAQA094048.md): Transceiver · inoperative · Apr 14, 2004 · N222LF · Bell 222U · DME/TACAN System
  > EXCHANGE - CORE RETURN FOR EXCHANGE PO 202342803, DMF INOPERATIVE ON CORE,IS NOT RECEIVING A SIGNAL. REPLACED WITH SERVICEABLE UNIT FROM AVGROUP, 04/22/2004

Next page: https://openairdocs.org/model/bell-222u/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 = '222U'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bell-222u/reports

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