# Service difficulty reports: Jaars Inc

A list on [Jaars Inc](https://openairdocs.org/faa-repair-station/EVGR735D/jaars-inc.md).

Reports filed under designator EVGR by a repair station, newest first.

Page 1 of 2 · 81 reports

- [SDR EVGR202610220001](https://openairdocs.org/sdr/EVGR202610220001.md): Rudder Bar · cracked · Sep 30, 2026 · N365BT · Pilats PC6 · Rudder Control System
  > A MECHANIC WAS COMPLETING OUR COMPANY REQUIRED FINAL INSPECTION PRIOR TO RELEASING THE AIRCRAFT BACK TO SERVICE. ONE OF THOSE INSPECTION ITEMS, WAS TO CHECK THE FLIGHT CONTROLS. WHEN HE APPLIED PRESSURE TO THE RUDDER PEDALS HE HEARD A LOUD POP AND THE RUDDER
- [SDR EVGR20260720001](https://openairdocs.org/sdr/EVGR20260720001.md): Pump · leaking · Jul 1, 2026 · N6153Z · Cessna U206G · Fuel Boost Pump
  > DURING A POST FLIGHT INSPECTION THE PILOT OBSERVED BLUE STAINS ON THE BACK OF THE ENGINE DRIVEN FUEL PUMP. FUEL WAS FOUND TO BE SEEPING FROM THE SMALL WEEP HOLE ON THE PUMP NEAR THE UNMETERED FUEL PRESSURE ADJUSTER SCREW. THIS PUMP WAS REMOVED FROM SERVICE A
- [SDR EVGR20260325001](https://openairdocs.org/sdr/EVGR20260325001.md): Actuator · jammed · Mar 25, 2026 · N28NR · Quest KODIAK100 · Elevator Tab Control System
  > PITCH TRIM WHEEL COULD ONLY BE MOVED WITHIN A VERY SMALL RANGE. MAINTENANCE INVESTIGATED AND FOUND THAT THE LH PITCH TRIM ACTUATOR WAS BOUND UP AND WOULD NOT ROTATE. THE ACTUATOR WAS REMOVED AND DISASSEMBLED IAW THE KODIAK 100 AMM CH. 2731.5.10 AND DAHER FIEL
- [SDR EVGR2024040900002](https://openairdocs.org/sdr/EVGR2024040900002.md): Shackle · seized · Apr 9, 2024 · N66BP · Robsin R66 · Main Landing Gear
  > DURING PREFLIGHT INSPECTION, A PILOT NOTICED THAT THE LOWER LEFT LANDING GEAR ASSEMBLY MOUNTING BOLT (NAS6607-20) HAD BEEN TURNING. THIS BOLT MOUNTS THE LANDING GEAR CROSS TUBE TO THE LEFT FORWARD LANDING GEAR SHACKLE AND IS SPECIFIED TO BE TORQUED TO 66 FT-LB
- [SDR EVGR2024012300001](https://openairdocs.org/sdr/EVGR2024012300001.md): Jettison Handle · backed out · Jan 17, 2024 · N365BT · Pilats PC6 · Emergency Equipment
  > THE AIRCRAFT HAD LANDED AND AS THE PILOTS BROUGHT THE POWER LEVER INTO BETA/REVERSE, THE LEFT SIDE PILOT DOOR FELL OFF. IT FELL FORWARD OVER THE MLG STRUT. THE DOOR HIT THE GROUND AND WAS THEN RUN OVER BY THE LEFT WHEEL. THE DOOR WAS THEN THROWN BACK UNDER THE
- [SDR EVGR2024040900001](https://openairdocs.org/sdr/EVGR2024040900001.md): Piston Ring · stuck · Jan 8, 2024 · N67JA · Cessna U206G · Reciprocating Engine Cylinder Section
  > BETWEEN 24 & 49 HRS OIL CONSUMPTION WAS 8.7 HRS/QT. OIL CONSUMPTION WAS LOWEST AT 10 HRS PER QUART AT 240 HRS AND THEN INCREASED. AT 370 HRS IT WAS 6 HRS/QT. AT 513 HOURS WAS 4.4 HRS/QT. AT 567 HRS (100HR INSP) IT WAS 2.1 HRS/QT OVER 50 HOURS BUT WAS INCREASIN
- [SDR EVGR202100624](https://openairdocs.org/sdr/EVGR202100624.md): Pump · leaking · Dec 6, 2021 · N87763 · Helio H395 · Engine Fuel Pump
  > THE ENGINE DRIVEN PUMP WAS FOUND LEAKING FUEL OUT OF THE PUMP DRAIN AT A SLOW RATE. THE PUMP WAS REPLACED AND THE REPLACEMENT STARTED LEAKING IMMEDIATELY AT A FASTER RATE FROM THE PUMP DRAIN. IT WAS NOTICED THAT THERE IS NO LEAKAGE WHEN THE PUMP WAS CONNECTED
- [SDR EVGR20200624](https://openairdocs.org/sdr/EVGR20200624.md): Tube · split · Jan 28, 2021 · N6153Z · Cessna U206G · Tire Tube
  > PILOT WAS TAXIING AIRCRAFT WHEN ANOTHER PERSON ON THE RAMP GRABBED HIS ATTENTION REGARDING THE LH MAIN TIRE BEING FLAT. HE STOPPED AND SHUT DOWN. WHEEL WAS REMOVED AND DISASSEMBLED. TIRE INNER TUBE WAS REPLACED AND WHEEL REINSTALLED. EXAMINATION OF THE INN
- [SDR EVGR202006240001](https://openairdocs.org/sdr/EVGR202006240001.md): Bearing · leaking · Jun 15, 2020 · N44KV · Robsin R44RAVENII · Tail Rotor Drive Shaft
  > P/N C647-8 TAIL ROTOR DRIVE SHAFT DAMPER BEARING WAS FOUND TO BE LEAKING GREASE AT A SCHEDULED INSPECTION. PART TOTAL TIME IS 231.2 HRS AND WAS INSTALLED NEW IN MARCH 2019 AT THE OVERHAUL OF THE HELICOPTER. THIS BEARING IS THE SUBJECT OF R44 SB-92A WHICH REQ
- [SDR EVGR201908060001](https://openairdocs.org/sdr/EVGR201908060001.md): Points · open · Aug 6, 2019 · Robsin R44RAVENII · Magneto/Distributor
  > BENDIX MAGNETO P/N 10-600646-201 WAS REMOVED FOR REPAIR DUE TO POOR TACHOMETER OPERATION. THE TACHOMETER POINTS WERE REPLACED WITH A NEW SET, TELEDYNE CONTINENTAL MOTORS P/N 10-382584. DURING INSTALLATION, CONTINUITY OF THE POINTS WAS CHECKED AND FOUND TO BE
- [SDR EVGR201908070001](https://openairdocs.org/sdr/EVGR201908070001.md): Pump · leaking · May 6, 2019 · N67JA · Cessna U206G · Engine Fuel Pump
  > DURING A FUEL INJECTION SYSTEM CHECK WITH PRESSURE GAUGES IT WAS NOTED THAT FUEL WAS LEAKING FROM A VENT ON THE BACK SIDE OF THE ENGINE DRIVEN FUEL PUMP JUST BELOW THE LOW PRESSURE RELIEF VALVE ADJUSTMENT SCREW (THIS ADJUSTS THE LOW UNMETERED FUEL PRESSURE). T
- [SDR EVGR20181119001](https://openairdocs.org/sdr/EVGR20181119001.md): Flap Track · broken · Nov 7, 2018 · N62JA · Helio H295 · Trailing Edge Flaps
  > THE LEFT INBOARD FLAP TRACK WAS FOUND TO BE CRACKED (BROKEN) AT THE AFT END DURING THE POST FLIGHT INSPECTION. THIS WAS THE FIRST FLIGHT AFTER A 50 HOUR INSPECTION AND ROUTINE SERVICING. THE CRACK WAS NOT EVIDENT DURING THE PREFLIGHT INSPECTION. THE PILOTS (
- [SDR EVGR201810232](https://openairdocs.org/sdr/EVGR201810232.md): Intake Valve · burned · Oct 8, 2018 · N41LY · Robsin R44 · Reciprocating Engine Cylinder Section
  > SUPPLEMENTAL INFORMATION (PLEASE REPLACE THE TEXT FROM THE PREVIOUSLY SUBMITTED REPORT WITH THE FOLLOWING CORRECTED TEXT): THE AIRCRAFT OPERATOR COMPLAINED OF AN INTERMITTENT POWER LOSS. TROUBLESHOOTING LED TO THE POSSIBILITY OF A STUCK INTAKE OR EXHAUST VALVE
- [SDR EVGR2019030600001](https://openairdocs.org/sdr/EVGR2019030600001.md): Contact Breaker · open · Jun 29, 2018 · N69KA · Robsin R44 · Magneto/Distributor
  > THE OVERHAULED MAGNETO WAS PURCHASED. UPON INSTALLATION OF THE MAGNETO, THE TACHOMETER DID NOT WORK. FURTHER TROUBLESHOOTING REVEALED THAT THE TACHOMETER CONTACT ASSEMBLY HAD NO CONTINUITY ACROSS THE POINTS. THE CONTACT ASSEMBLY WAS REPLACED WITH A NEW CONT
- [SDR EVGR201806080001](https://openairdocs.org/sdr/EVGR201806080001.md): Wire · disconnected · Jun 6, 2018 · N365BT · Pilats PC6B2H4 · Flight Control System Wiring
  > EXPERIENCED A STABILIZER TRIM RUNAWAY AFTER LANDING AND SHUTDOWN. COULD HEAR THE STABILIZER TRIM MOTOR RUNNING CONTINUOUSLY AND THAT THE INDICATOR IN THE COCKPIT SHOWED NOSE DOWN. AFTER TROUBLESHOOTING, DISCONNECTED THE TRIM CONTROL SWITCHES ON EACH OF THE
- [SDR EVGR2018060500044](https://openairdocs.org/sdr/EVGR2018060500044.md): Cylinder · worn · Jun 4, 2018 · N5387G · Helio HT295 · Reciprocating Engine Cylinder Section
  > DURING A ROUTINE OIL AND FILTER CHANGE. NOTHING ABNORMAL WAS NOTED DURING THE ENGINE RUN UP, NOR WAS THE ANY ABNORMALITY REPORTED FROM THE PILOT. WHEN THE EXTERNAL REMOTE MOUNTED OIL FILTER WAS CUT OPEN, A LOT OF METAL WAS DISCOVERED IN THE PAPER PLEATS. IT
- [SDR EVGR20180125](https://openairdocs.org/sdr/EVGR20180125.md): Roller · loose · Jan 5, 2018 · N365BT · Pilats PC6B2H4 · Doors
  > THE LEFT SLIDING DOOR CAME OPEN IN FLIGHT ABOUT 6 INCHES. IT DID NOT SLIDE OPEN, BUT RATHER PULLED AWAY FROM THE AIRCRAFT. LANDED AT HOME BASE WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND THAT THE LEFT DOOR WAS STILL LATCHED AT THE REAR BUT THAT THE LOWER
- [SDR EVGR201710130001](https://openairdocs.org/sdr/EVGR201710130001.md): Rod Bearing · broken · Aug 23, 2017 · N5302X · Cessna U206G · Reciprocating Engine Power Section
  > DUE TO SLOWLY PROGRESSING OIL CONSUMPTION RATE, PULLED THE NR 1 CYLINDER AND DISCOVERED THE NR 2 CONNECTING ROD CAP WAS LIGHTLY SCRAPING THE BOTTOM PISTON PIN BOSS AREA OF THE NR 1 PISTON. INVESTIGATION REVEALED THE NR 1 CONNECTING ROD BEARING HAD BROKEN.
- [SDR EVGR2017101600001](https://openairdocs.org/sdr/EVGR2017101600001.md): Points · faulty · Jun 26, 2017 · N788G · Robsin R44RAVENII · Magneto/Distributor
  > ON INSTALLATION OF THE OVERHAULED MAGNETO IN THE AIRCRAFT, THE TACHOMETER DID NOT WORK. FURTHER INVESTIGATION REVEALED THAT THE TACHOMETER POINTS HAD ZERO CONTINUITY BETWEEN THE TERMINALS AND THE POINTS. REPLACED THE TACHOMETER POINTS AND THE TACHOMETER WORK
- [SDR EVGR201701170001](https://openairdocs.org/sdr/EVGR201701170001.md): Torque Tube · broken · Jan 17, 2017 · N62JA · Helio H295 · Rudder Control System
  > ACFT HAS A HISTORY OF TAIL WHEEL SHIMMY. TROUBLESHOOTING INSPECTION FOUNR THE PILOT'S PEDALS WERE STAGGERED AND THE PILOT’S LT PEDAL HAD SLIGHT FORE AND AFT MOVEMENT WITH THE RT PEDAL HELD STATIONARY. THE TWO BOLTS THAT CONNECT THE PILOT’S RUDDER TORQUE TUBE T
- [SDR EVGR201611080001](https://openairdocs.org/sdr/EVGR201611080001.md): Sprag Assy · making metal · Oct 13, 2016 · N622 · Robsin R44RAVENII · Engine/Transmission Coupling
  > DURING THE 100 HOUR INSPECTION, THE CLUTCH LUBRICATION INSPECTION WAS PERFORMED PER ROBINSON MM 7.210. WHEN THE OIL WAS INSPECTED SEVERAL PIECES OF METAL WERE FOUND. ROBINSON WAS CONTACTED AND THE CLUTCH ASSEMBLY WAS REMOVED FROM THE AIRCRAFT AND AN OVERHA
- [SDR EVGR201602180001](https://openairdocs.org/sdr/EVGR201602180001.md): Crankcase · cracked · Feb 15, 2016 · N342EA · Cessna U206G · Reciprocating Engine Power Section
  > CRACKED CRANKCASE, LT SIDE BETWEEN CYLINDERS NR 2 AND NR 4 INTO THE NR 2 CYLINDER APERTURE. CRACKS WERE DISCOVERED AT A ROUTINE 50 HOUR INSPECTION AND SERVICING WHILE TRYING TO ADDRESS AN OIL LEAK.
- [SDR EVGR20160215](https://openairdocs.org/sdr/EVGR20160215.md): Bulkhead · cracked · Feb 5, 2016 · N8YL · Robsin R44RAVENII · Fuselage Main, Bulkhead
  > DURING THE ANNUAL INSPECTION, AFT CABIN WALL, FOUND THAT THERE WAS A SMALL CRACK AROUND A RIVET ON BOTH THE LT AND RT SIDE LOCATED JUST INBD OF THE MOUNTING BOLT FOR THE INBD SEAT STRAP. THESE RIVETS HOLD ONE CORNER OF A STEEL REINFORCEMENT ON THE ENGINE SIDE
- [SDR EVGR201601280001](https://openairdocs.org/sdr/EVGR201601280001.md): Fuel Tank · leaking · Jan 25, 2016 · N325SM · Robsin R44RAVENII · Fuel Storage
  > DURING A 100 HR. INSPECTION THE LT FUEL TANK WAS REMOVED TO ACCESS A SEEPING HYDRAULIC FITTING. WHEN THE TANK ASSY WAS REMOVED, FUEL STAINS WERE SEEN ON THE LOWER FRONT EDGE OF THE TANK ASSY. THE END SECTION OF THE FUEL TANK WAS REMOVED, MORE FUEL STAIN WAS
- [SDR EVGR20150904](https://openairdocs.org/sdr/EVGR20150904.md): Mount · cracked · Sep 4, 2015 · N622 · Robsin R44RAVENII · Rotorcraft Tail Boom
  > DURING 100 HOUR INSPECTION, THE TAIL ROTOR GUARD MOUNTING BLOCK ASSY WAS FOUND TO BE CRACKED ON 3 SIDES OF THE SMALL BOLT HOLE CONTAINING A HELICOIL INSERT.
- [SDR EVGR20150820](https://openairdocs.org/sdr/EVGR20150820.md): Contact · debonded · Aug 14, 2015 · N8YL · Robsin R44RAVENII · Magneto/Distributor
  > THERE WAS A ROUGH MAGNETO DROP DURING RUN-UP. TROUBLESHOOTING REVEALED A LARGE MAXIMUM POINT GAP AND CORRESPONDING ERRONEOUS E-GAP. CLOSER EXAMINATION REVEALED THE TUNGSTEN CONTACT BECAME UNATTACHED FROM THE RIVET ON THE FRAME SIDE OF THE CONTACT ASSEMBLY.
- [SDR EVGR20150427001](https://openairdocs.org/sdr/EVGR20150427001.md): Switch · broken · Apr 24, 2015 · N61JA · Helio H295 · AC Generation System
  > THE BATON OR TOGGLE OF THE ELEC FUEL PUMP SWITCH BROKE OFF IN FLIGHT WHEN THE PILOT ATTEMPTED TO SWITCH IT ON. THE SWITCH FAILED IN THE OFF POSITION. THANKFULLY, THE ENG DRIVEN FUEL PUMP CONTINUED TO RUN & THE ACFT RETURNED TO HOME BASE SAFELY.
- [SDR EVGR201502200001](https://openairdocs.org/sdr/EVGR201502200001.md): Coil · worn · Feb 20, 2015 · N6335Q · Mooney M20C · Magneto/Distributor
  > THE MAGNETO WAS INSTALLED NEW. DURING THE FIRST 500 HOUR INSPECTION, WE DISCOVERED THE COIL WAS INSTALLED WITH THE TAB NOT CORRECTLY ADJUSTED AND CAUSING ABNORMAL WEAR.
- [SDR EVGR201409250001](https://openairdocs.org/sdr/EVGR201409250001.md): Spring · cracked · Sep 25, 2014 · N61JA · Helio H295 · Nose/Tail Landing Gear
  > BOTH HOOKS OF ONE OF THE TWO SPRING HOOKS, TAIL WHEEL STEERING SPRING, CRACKED AND FAILED. THE ASSEMBLY ONLY HAD 7.6 HOURS TIME IN SERVICE AND 18 LANDINGS WHEN IT FAILED. VISUAL EXAMINATION WITH A MAGNIFYING LENS REVEALED RUST IN THE CRACK INITIATION AREA O
- [SDR EVGR201408080001](https://openairdocs.org/sdr/EVGR201408080001.md): Axle · cracked · Aug 6, 2014 · N61JA · Helio H295 · Main Landing Gear Strut/Axle/Truck
  > THE LT AND RT MLG AXLE FLANGES WERE FOUND TO BE CRACKED DURING THE 1500 HOURS, ICA MAGNAFLUX INSPECTION OF THE MLG. THESE AXLE FLANGES ARE PART OF STC LANDING GEAR MODIFICATION SA 00781TA. THE CRACKS WERE IN OR AT THE EDGE OF THE WELD CONNECTING THE AXLE HOU
- [SDR EVGR201402280001](https://openairdocs.org/sdr/EVGR201402280001.md): Elt · corroded · Feb 26, 2014 · N6335Q · Mooney M20C · Emergency Locator Beacon
  > EMERGENCY LOCATOR BEACON, CORROSION WAS FOUND ON 1 OF 4 OUTSIDE CASE SCREWS. INSIDE CORROSION WAS FOUND ON THE POWER CONNECTOR NEGATIVE LEAD ON THE ELECTRONICS SIDE. THERE WAS ACID FILLING THE INSIDE OF THE NEGATIVE CONNECTOR. NO CORROSION WAS FOUND AT ALL
- [SDR EVGR201304120001](https://openairdocs.org/sdr/EVGR201304120001.md): Plug · worn · Nov 4, 2013 · N5387G · Helio HT295 · Reciprocating Engine Power Section
  > OIL ANALYSIS CAME BACK WITH VERY HIGH ALUMINUM METAL CONTENT IN THE OIL. METAL WAS ALSO VISIBLE IN THE DRAINED OIL WITH AN APPEARANCE LIKE METAL-FLAKE PAINT. THE FLAKES WERE SMALL ENOUGH THAT SOME WERE NOT BEING TRAPPED IN THE OIL FILTER EXCEPT SOME AS SLUDG
- [SDR EVGR201310310001](https://openairdocs.org/sdr/EVGR201310310001.md): Tire · cracked · Oct 24, 2013 · Helio H295 · Tire
  > CRACKS HAVE DEVELOPED IN SEVERAL 10.00 SC 8 PLY TIRES. THE CRACKS TYPICALLY APPEAR IN THE SIDEWALL ADJACENT TO THE MOLD VENTS IN THE SIDE WALL. CRACKS RANGE IN LENGTH FROM.1250" TO OVER.5". THE CRACKS EXPOSED THE CORDS.
- [SDR EVGR20140110](https://openairdocs.org/sdr/EVGR20140110.md): Transmitter · leaking · Oct 22, 2013 · N622 · Robsin R44RAVENII · Fuel Quantity Sensor
  > A BLUE FUEL STAIN ON HORIZONTAL FIREWALL WAS FOUND DURING PREFLIGHT. FURTHER EXAMINATION WITH A LIGHT AND INSPECTION MIRROR, AND OBSERVING AN ONGOING DRIP EVERY 35 SECONDS, EASILY CONFIRMED THAT FUEL WAS COMING FROM CENTER STUD, WHERE WIRE TERMINAL RING ATTAC
- [SDR EVGR2013120400002](https://openairdocs.org/sdr/EVGR2013120400002.md): Coil · cracked · Sep 25, 2013 · N788G · Robsin R44RAVENII · Magneto/Distributor
  > THE MAGNETOS ON THIS HELICOPTER WERE BEING O/H DUE TO CALENDAR TIME. IT SHOULD ALSO BE NOTED THAT BOTH MAGNETOS WERE RUNNING FLAWLESSLY PRIOR TO REMOVAL. THE COILS IN BOTH MAGNETOS WERE CRACKED IN THE SAME PLACE, WITH THE SAME LENGTH OF CRACK (ABOUT 1" LONG)
- [SDR EVGR2013120400001](https://openairdocs.org/sdr/EVGR2013120400001.md): Coil · cracked · Sep 25, 2013 · N788G · Robsin R44RAVENII · Magneto/Distributor
  > THE MAGNETOS ON THIS HELICOPTER WERE BEING O/H DUE TO CALENDAR TIME. IT SHOULD ALSO BE NOTED THAT BOTH MAGNETOS WERE RUNNING FLAWLESSLY PRIOR TO REMOVAL. THE COILS IN BOTH MAGNETOS WERE CRACKED IN THE SAME PLACE, WITH THE SAME LENGTH OF CRACK, ABOUT 1" LONG.
- [SDR EVGR201304260001](https://openairdocs.org/sdr/EVGR201304260001.md): Tube · ruptured · May 3, 2013 · Quest KODIAK100 · Tire Tube
  > ON ROLL OUT AFTER LANDING THE RT MAIN TIRE WENT FLAT. PILOT WAS ABLE TO KEEP THE AIRCRAFT ON THE AIRSTRIP AND NO DAMAGE RESULTED TO THE AIRCRAFT. FOLLOWING INSPECTION OF THE FLAT TIRE ASSEMBLY, IT WAS FOUND THAT THERE WAS DAMAGE TO THE TUBE WHICH APPEARED TO B
- [SDR EVGR201304250002](https://openairdocs.org/sdr/EVGR201304250002.md): Tube · broken · Apr 23, 2013 · N68884 · Helio HT295 · Landing Gear Steering System
  > ACFT TENDS TO TURN LT DURING TAXI AND TAKEOFF ROLL. MECHANIC FOUND RT STEERING BUNGEE ASSY BROKEN AND SEPARATED AT THREADED AREA AFT OF THE FORWARD HEIM BALL. THE HEIM BALL TURNS FREELY AND WAS NOT BOUND OR FROZEN. ON DISASSEMBLY OF THE STEERING BUNGEE IT WA
- [SDR EVGR20120326001](https://openairdocs.org/sdr/EVGR20120326001.md): Skin · corroded · Mar 26, 2012 · N91222 · Cessna 182P · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND UNDER THE BLACK SOUND DEADENING PATCHES ON THE INSIDE OF THE ACFT SKIN, AND WAS NOT DETECTED UNTIL THE PATCHES WERE REMOVED.
- [SDR EVGR20101006](https://openairdocs.org/sdr/EVGR20101006.md): Fcu · leaking · Oct 5, 2010 · N497KQ · Quest KODIAK100 · Fuel Control/Turbine Engines
  > BRG GREASE WAS WASHED OUT DUE TO FUEL PUMP SEAL FAILURE. BLUE DYE WAS FOUND IN THE DRAIN BETWEEN THE FUEL PUMP AND FUEL CONTROL UNIT.
- [SDR EVGR20101005](https://openairdocs.org/sdr/EVGR20101005.md): Pump · leaking · Oct 5, 2010 · N497KQ · Quest KODIAK100 · Fuel Boost Pump
  > (EGVR) FUEL PUMP SEAL FAILED, WASHING OUT BLUE DYE FROM THE BEARING. DYE WAS FOUND COMING OUT THE FUEL PUMP /FCU DRAIN LINE.
- [SDR EVGR060210](https://openairdocs.org/sdr/EVGR060210.md): Fire Detector · chafed · Jun 2, 2010 · N61JA · Helio H295 · Fire Detection
  > (EVGR) THE FIRE DETECTION LOOP IN THE ENGINE COMPARTMENT CHAFED AGAINST SCAT TUBE CAUSING INTERMITTENT ALARM. THE UNIT IS FIRE DETECTION SYSTEM INSTALLED UNDER STC SA1586SO.
- [SDR EVGR20100405](https://openairdocs.org/sdr/EVGR20100405.md): Oil Filter · chafed · Apr 2, 2010 · Robsin R44RAVENII · Reciprocating Engine Oil System
  > (EVGR) AS THE MECHANIC WAS PREPARING TO REMOVE THE OIL FILTER FOR AN ANNUAL INSP, HE NOTICED THE RUST LIKE DUST ON THE OIL FILTER TOP SIDE. AS HE LOOKED CLOSER HE THOUGHT, "THIS IS AN INCORRECT OIL FILTER FOR THIS INSTALLATION." AFTER HE GOT THE FILTER OUT H
- [SDR EVGR062910](https://openairdocs.org/sdr/EVGR062910.md): Collar · bent · Mar 22, 2010 · Engine (Reciprocating)
  > (EVGR) PN 626739M010 TRANSFER COLLAR. THE COLLAR SEEMS TO HAVE BEEN DAMAGED AFTER IT WAS GROUND. ON ONE SIDE THE SPLIT LINE DOES NOT LINE UP, YOU CAN CATCH A FINGERNAIL ON IT. WHEN INSTALLED IT IS TIGHT AND RUBS AT THAT POINT AS SHOWN BY THE MAGIC MARKER RUBBE
- [SDR EVGR20091028](https://openairdocs.org/sdr/EVGR20091028.md): Bearing · separated · Oct 26, 2009 · N622 · Robsin R44RAVENII · Power Lever
  > BEARING FAILED, SB-62 PREVIOUSLY COMPLIED WITH, WHICH INSTALLED LARGE AREA WASHERS. THE WASHERS DID THEIR JOB AND PREVENTED THE BEARING FROM FALLING APART AND CAUSING LOSS OF THROTTLE CONTROL.
- [SDR EVGR20090623](https://openairdocs.org/sdr/EVGR20090623.md): Cam · worn · Jun 19, 2009 · N149P · Robsin R44RAVENII · Magneto/Distributor
  > CUSTOMER REPORTED AN EXCESSIVE MAG DROP (UPWARDS OF 10 PERCENT) AND HARD STARTING. BROUGHT IN LT MAG, IT WAS HARD TO TIME. COULDN'T MAKE THE POINTS TIME, AND THEY WERE SOMEWHAT PITTED, CHANGED THEM. STILL COULDN'T TIME THEM, AS THEY WENT FROM -10 TO +22 FOR P
- [SDR 20070125](https://openairdocs.org/sdr/20070125.md): Gear · worn · Jan 24, 2007 · N622 · Robsin R44RAVENII · Reciprocating Engine Power Section
  > DURING INSPECTION OF THE ENGINE WHILE REPLACING THE CRANKSHAFT IAW SB 569A, IT WAS OBSERVED THAT (PN 13519647) CRANKSHAFT GEAR WAS EXCESSIVELY WORN. THE GEAR WAS REPLACED WITH A NEW PART.
- [SDR EVGR1113735](https://openairdocs.org/sdr/EVGR1113735.md): Door Frame · corroded · Nov 9, 2006 · N65JA · Beech 65A901 · Fuselage Main, Structure
  > CORROSION WAS FOUND AT THE AFT DOOR FRAME AT FUSELAGE STATION 255.5 JUST BELOW AND OUT BOARD OF THE DOOR SNUBBER MOUNT. DAMAGE WAS REPAIRED IAW SIRM PN 9839006C, DATED MARCH 2003, ATA 20-10-03 FIGURE 202, PAGES 204 AND 205 AND ATA 20-10-34, FIGURE 201, PAGES
- [SDR EVGR20060915](https://openairdocs.org/sdr/EVGR20060915.md): Coil · worn · Sep 13, 2006 · N628PM · Robsin R44 · Magneto/Distributor
  > DURING THE FIRST 500 HOUR MAGNETO INSPECTION, THE TAB ON THE COIL WAS MISALIGNED AND EXHIBITED EXCESSIVE WEAR.
- [SDR 20051129](https://openairdocs.org/sdr/20051129.md): Tube · cracked · Nov 29, 2005 · N641LW · Helio H295 · Wing Spar
  > WING SPAR CARRY THRU P/N 295-030-401 IS CRACKED ON LT VERTICAL TUBE, TOP, FRONT SIDE.

Next page: https://openairdocs.org/faa-repair-station/EVGR735D/jaars-inc/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 submitter_designator = 'EVGR' AND submitter_type_code = 'B'
ORDER BY difficulty_date DESC, sdr_id DESC
```

This list as a web page: https://openairdocs.org/faa-repair-station/EVGR735D/jaars-inc/reports

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