# Jaars Inc: FAA repair station EVGR735D

- Type: FAA-certificated repair station (14 CFR Part 145)
- Certificate number: EVGR735D
- Designator: EVGR
- Name on the FAA list: JAARS INC
- Address: 7700 JAARS ROAD, WAXHAW, NC 28173
- Accountable manager: MULL, PHILIP, (704) 843-6426, philip.mill@jaars.org
- Liaison: ROBERTS, ANDREW, (704) 843-6426, andrew.roberts@jaars.org
- On the FAA list: On the list of October 26, 2026; listed since October 26, 2026 or earlier (OpenAirDocs’ first copy)
- Service difficulty reports filed: 81
- Source: FAA Find a Facility dashboard, https://www.faa.gov/av-info/facility-dashboard
- Page: https://openairdocs.org/faa-repair-station/EVGR735D/jaars-inc

The FAA writes names in capitals; the mixed case here is OpenAirDocs'. The dashboard has no certificate dates, and nothing on it shows whether a certificate is in good standing.

## Ratings

- Airframe: Class 3 (All-metal construction of small aircraft)
- Powerplant: Class 1 (Reciprocating engines of 400 horsepower or less); Limited
- Radio: Class 1 (Communication equipment); Class 2 (Navigational equipment); Class 3 (Radar equipment)
- Instrument: Limited
- Accessory: Limited

A Limited class covers only the makes and models in the station's operations specifications (14 CFR 145.61), which the FAA doesn't publish.

## Service difficulty reports (81, newest 50)

Filed under designator EVGR by a repair station (submitter type B).

- [SDR EVGR202610220001](https://openairdocs.org/sdr/EVGR202610220001), Sep 30, 2026: Pilats PC6. RUDDER BAR. CRACKED. A MECHANIC WAS COMPLETING OUR COMPANY REQUIRED FINAL INSPECTION PRIOR TO RELEASING THE AIRCRAFT BACK TO SERVICE. ONE OF  (N365BT)
- [SDR EVGR20260720001](https://openairdocs.org/sdr/EVGR20260720001), Jul 1, 2026: Cessna U206G. PUMP. LEAKING. DURING A POST FLIGHT INSPECTION THE PILOT OBSERVED BLUE STAINS ON THE BACK OF THE ENGINE DRIVEN FUEL PUMP. FUEL WAS FOUN (N6153Z)
- [SDR EVGR20260325001](https://openairdocs.org/sdr/EVGR20260325001), Mar 25, 2026: Quest KODIAK100. ACTUATOR. JAMMED. PITCH TRIM WHEEL COULD ONLY BE MOVED WITHIN A VERY SMALL RANGE. MAINTENANCE INVESTIGATED AND FOUND THAT THE LH PITCH TRI (N28NR)
- [SDR EVGR2024040900002](https://openairdocs.org/sdr/EVGR2024040900002), Apr 9, 2024: Robsin R66. SHACKLE. SEIZED. DURING PREFLIGHT INSPECTION, A PILOT NOTICED THAT THE LOWER LEFT LANDING GEAR ASSEMBLY MOUNTING BOLT (NAS6607-20) HAD BE (N66BP)
- [SDR EVGR2024012300001](https://openairdocs.org/sdr/EVGR2024012300001), Jan 17, 2024: Pilats PC6. JETTISON HANDLE. BACKED OUT. THE AIRCRAFT HAD LANDED AND AS THE PILOTS BROUGHT THE POWER LEVER INTO BETA/REVERSE, THE LEFT SIDE PILOT DOOR FELL OFF.  (N365BT)
- [SDR EVGR2024040900001](https://openairdocs.org/sdr/EVGR2024040900001), Jan 8, 2024: Cessna U206G. PISTON RING. STUCK. 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 I (N67JA)
- [SDR EVGR202100624](https://openairdocs.org/sdr/EVGR202100624), Dec 6, 2021: Helio H395. PUMP. LEAKING. THE ENGINE DRIVEN PUMP WAS FOUND LEAKING FUEL OUT OF THE PUMP DRAIN AT A SLOW RATE. THE PUMP WAS REPLACED AND THE REPLAC (N87763)
- [SDR EVGR20200624](https://openairdocs.org/sdr/EVGR20200624), Jan 28, 2021: Cessna U206G. TUBE. SPLIT. PILOT WAS TAXIING AIRCRAFT WHEN ANOTHER PERSON ON THE RAMP GRABBED HIS ATTENTION REGARDING THE LH MAIN TIRE BEING FLAT.  (N6153Z)
- [SDR EVGR202006240001](https://openairdocs.org/sdr/EVGR202006240001), Jun 15, 2020: Robsin R44RAVENII. BEARING. LEAKING. P/N C647-8 TAIL ROTOR DRIVE SHAFT DAMPER BEARING WAS FOUND TO BE LEAKING GREASE AT A SCHEDULED INSPECTION. PART TOTAL TI (N44KV)
- [SDR EVGR201908060001](https://openairdocs.org/sdr/EVGR201908060001), Aug 6, 2019: Robsin R44RAVENII. POINTS. OPEN. BENDIX MAGNETO P/N 10-600646-201 WAS REMOVED FOR REPAIR DUE TO POOR TACHOMETER OPERATION. THE TACHOMETER POINTS WERE REP
- [SDR EVGR201908070001](https://openairdocs.org/sdr/EVGR201908070001), May 6, 2019: Cessna U206G. PUMP. LEAKING. DURING A FUEL INJECTION SYSTEM CHECK WITH PRESSURE GAUGES IT WAS NOTED THAT FUEL WAS LEAKING FROM A VENT ON THE BACK SID (N67JA)
- [SDR EVGR20181119001](https://openairdocs.org/sdr/EVGR20181119001), Nov 7, 2018: Helio H295. FLAP TRACK. BROKEN. THE LEFT INBOARD FLAP TRACK WAS FOUND TO BE CRACKED (BROKEN) AT THE AFT END DURING THE POST FLIGHT INSPECTION. THIS WAS  (N62JA)
- [SDR EVGR201810232](https://openairdocs.org/sdr/EVGR201810232), Oct 8, 2018: Robsin R44. INTAKE VALVE. BURNED. SUPPLEMENTAL INFORMATION (PLEASE REPLACE THE TEXT FROM THE PREVIOUSLY SUBMITTED REPORT WITH THE FOLLOWING CORRECTED TEXT (N41LY)
- [SDR EVGR2019030600001](https://openairdocs.org/sdr/EVGR2019030600001), Jun 29, 2018: Robsin R44. CONTACT BREAKER. OPEN. THE OVERHAULED MAGNETO WAS PURCHASED. UPON INSTALLATION OF THE MAGNETO, THE TACHOMETER DID NOT WORK. FURTHER TROUBLESHOO (N69KA)
- [SDR EVGR201806080001](https://openairdocs.org/sdr/EVGR201806080001), Jun 6, 2018: Pilats PC6B2H4. WIRE. DISCONNECTED. EXPERIENCED A STABILIZER TRIM RUNAWAY AFTER LANDING AND SHUTDOWN. COULD HEAR THE STABILIZER TRIM MOTOR RUNNING CONTINUOU (N365BT)
- [SDR EVGR2018060500044](https://openairdocs.org/sdr/EVGR2018060500044), Jun 4, 2018: Helio HT295. CYLINDER. WORN. DURING A ROUTINE OIL AND FILTER CHANGE. NOTHING ABNORMAL WAS NOTED DURING THE ENGINE RUN UP, NOR WAS THE ANY ABNORMALITY (N5387G)
- [SDR EVGR20180125](https://openairdocs.org/sdr/EVGR20180125), Jan 5, 2018: Pilats PC6B2H4. ROLLER. LOOSE. THE LEFT SLIDING DOOR CAME OPEN IN FLIGHT ABOUT 6 INCHES. IT DID NOT SLIDE OPEN, BUT RATHER PULLED AWAY FROM THE AIRCRAF (N365BT)
- [SDR EVGR201710130001](https://openairdocs.org/sdr/EVGR201710130001), Aug 23, 2017: Cessna U206G. ROD BEARING. BROKEN. DUE TO SLOWLY PROGRESSING OIL CONSUMPTION RATE, PULLED THE NR 1 CYLINDER AND DISCOVERED THE NR 2 CONNECTING ROD CAP WAS  (N5302X)
- [SDR EVGR2017101600001](https://openairdocs.org/sdr/EVGR2017101600001), Jun 26, 2017: Robsin R44RAVENII. POINTS. FAULTY. ON INSTALLATION OF THE OVERHAULED MAGNETO IN THE AIRCRAFT, THE TACHOMETER DID NOT WORK. FURTHER INVESTIGATION REVEALED T (N788G)
- [SDR EVGR201701170001](https://openairdocs.org/sdr/EVGR201701170001), Jan 17, 2017: Helio H295. TORQUE TUBE. BROKEN. ACFT HAS A HISTORY OF TAIL WHEEL SHIMMY. TROUBLESHOOTING INSPECTION FOUNR THE PILOT'S PEDALS WERE STAGGERED AND THE PILO (N62JA)
- [SDR EVGR201611080001](https://openairdocs.org/sdr/EVGR201611080001), Oct 13, 2016: Robsin R44RAVENII. SPRAG ASSY. MAKING METAL. DURING THE 100 HOUR INSPECTION, THE CLUTCH LUBRICATION INSPECTION WAS PERFORMED PER ROBINSON MM 7.210. WHEN THE OIL WAS  (N622)
- [SDR EVGR201602180001](https://openairdocs.org/sdr/EVGR201602180001), Feb 15, 2016: Cessna U206G. CRANKCASE. CRACKED. CRACKED CRANKCASE, LT SIDE BETWEEN CYLINDERS NR 2 AND NR 4 INTO THE NR 2 CYLINDER APERTURE. CRACKS WERE DISCOVERED AT A  (N342EA)
- [SDR EVGR20160215](https://openairdocs.org/sdr/EVGR20160215), Feb 5, 2016: Robsin R44RAVENII. BULKHEAD. CRACKED. DURING THE ANNUAL INSPECTION, AFT CABIN WALL, FOUND THAT THERE WAS A SMALL CRACK AROUND A RIVET ON BOTH THE LT AND RT SI (N8YL)
- [SDR EVGR201601280001](https://openairdocs.org/sdr/EVGR201601280001), Jan 25, 2016: Robsin R44RAVENII. FUEL TANK. LEAKING. DURING A 100 HR. INSPECTION THE LT FUEL TANK WAS REMOVED TO ACCESS A SEEPING HYDRAULIC FITTING. WHEN THE TANK ASSY WAS R (N325SM)
- [SDR EVGR20150904](https://openairdocs.org/sdr/EVGR20150904), Sep 4, 2015: Robsin R44RAVENII. MOUNT. CRACKED. DURING 100 HOUR INSPECTION, THE TAIL ROTOR GUARD MOUNTING BLOCK ASSY WAS FOUND TO BE CRACKED ON 3 SIDES OF THE SMALL BOL (N622)
- [SDR EVGR20150820](https://openairdocs.org/sdr/EVGR20150820), Aug 14, 2015: Robsin R44RAVENII. CONTACT. DEBONDED. THERE WAS A ROUGH MAGNETO DROP DURING RUN-UP. TROUBLESHOOTING REVEALED A LARGE MAXIMUM POINT GAP AND CORRESPONDING ERRON (N8YL)
- [SDR EVGR20150427001](https://openairdocs.org/sdr/EVGR20150427001), Apr 24, 2015: Helio H295. SWITCH. BROKEN. THE BATON OR TOGGLE OF THE ELEC FUEL PUMP SWITCH BROKE OFF IN FLIGHT WHEN THE PILOT ATTEMPTED TO SWITCH IT ON. THE SWITC (N61JA)
- [SDR EVGR201502200001](https://openairdocs.org/sdr/EVGR201502200001), Feb 20, 2015: Mooney M20C. COIL. WORN. THE MAGNETO WAS INSTALLED NEW. DURING THE FIRST 500 HOUR INSPECTION, WE DISCOVERED THE COIL WAS INSTALLED WITH THE TAB N (N6335Q)
- [SDR EVGR201409250001](https://openairdocs.org/sdr/EVGR201409250001), Sep 25, 2014: Helio H295. SPRING. CRACKED. BOTH HOOKS OF ONE OF THE TWO SPRING HOOKS, TAIL WHEEL STEERING SPRING, CRACKED AND FAILED. THE ASSEMBLY ONLY HAD 7.6 HOU (N61JA)
- [SDR EVGR201408080001](https://openairdocs.org/sdr/EVGR201408080001), Aug 6, 2014: Helio H295. AXLE. CRACKED. THE LT AND RT MLG AXLE FLANGES WERE FOUND TO BE CRACKED DURING THE 1500 HOURS, ICA MAGNAFLUX INSPECTION OF THE MLG. THES (N61JA)
- [SDR EVGR201402280001](https://openairdocs.org/sdr/EVGR201402280001), Feb 26, 2014: Mooney M20C. ELT. CORRODED. EMERGENCY LOCATOR BEACON, CORROSION WAS FOUND ON 1 OF 4 OUTSIDE CASE SCREWS. INSIDE CORROSION WAS FOUND ON THE POWER CON (N6335Q)
- [SDR EVGR201304120001](https://openairdocs.org/sdr/EVGR201304120001), Nov 4, 2013: Helio HT295. PLUG. WORN. OIL ANALYSIS CAME BACK WITH VERY HIGH ALUMINUM METAL CONTENT IN THE OIL. METAL WAS ALSO VISIBLE IN THE DRAINED OIL WITH  (N5387G)
- [SDR EVGR201310310001](https://openairdocs.org/sdr/EVGR201310310001), Oct 24, 2013: Helio H295. TIRE. CRACKED. CRACKS HAVE DEVELOPED IN SEVERAL 10.00 SC 8 PLY TIRES. THE CRACKS TYPICALLY APPEAR IN THE SIDEWALL ADJACENT TO THE MOLD 
- [SDR EVGR20140110](https://openairdocs.org/sdr/EVGR20140110), Oct 22, 2013: Robsin R44RAVENII. TRANSMITTER. LEAKING. A BLUE FUEL STAIN ON HORIZONTAL FIREWALL WAS FOUND DURING PREFLIGHT. FURTHER EXAMINATION WITH A LIGHT AND INSPECTION MIR (N622)
- [SDR EVGR2013120400002](https://openairdocs.org/sdr/EVGR2013120400002), Sep 25, 2013: Robsin R44RAVENII. COIL. CRACKED. THE MAGNETOS ON THIS HELICOPTER WERE BEING O/H DUE TO CALENDAR TIME. IT SHOULD ALSO BE NOTED THAT BOTH MAGNETOS WERE RUN (N788G)
- [SDR EVGR2013120400001](https://openairdocs.org/sdr/EVGR2013120400001), Sep 25, 2013: Robsin R44RAVENII. COIL. CRACKED. THE MAGNETOS ON THIS HELICOPTER WERE BEING O/H DUE TO CALENDAR TIME. IT SHOULD ALSO BE NOTED THAT BOTH MAGNETOS WERE RUN (N788G)
- [SDR EVGR201304260001](https://openairdocs.org/sdr/EVGR201304260001), May 3, 2013: Quest KODIAK100. TUBE. RUPTURED. ON ROLL OUT AFTER LANDING THE RT MAIN TIRE WENT FLAT. PILOT WAS ABLE TO KEEP THE AIRCRAFT ON THE AIRSTRIP AND NO DAMAGE 
- [SDR EVGR201304250002](https://openairdocs.org/sdr/EVGR201304250002), Apr 23, 2013: Helio HT295. TUBE. BROKEN. ACFT TENDS TO TURN LT DURING TAXI AND TAKEOFF ROLL. MECHANIC FOUND RT STEERING BUNGEE ASSY BROKEN AND SEPARATED AT THREA (N68884)
- [SDR EVGR20120326001](https://openairdocs.org/sdr/EVGR20120326001), Mar 26, 2012: Cessna 182P. SKIN. CORRODED. CORROSION WAS FOUND UNDER THE BLACK SOUND DEADENING PATCHES ON THE INSIDE OF THE ACFT SKIN, AND WAS NOT DETECTED UNTIL T (N91222)
- [SDR EVGR20101006](https://openairdocs.org/sdr/EVGR20101006), Oct 5, 2010: Quest KODIAK100. FCU. LEAKING. BRG GREASE WAS WASHED OUT DUE TO FUEL PUMP SEAL FAILURE. BLUE DYE WAS FOUND IN THE DRAIN BETWEEN THE FUEL PUMP AND FUEL  (N497KQ)
- [SDR EVGR20101005](https://openairdocs.org/sdr/EVGR20101005), Oct 5, 2010: Quest KODIAK100. PUMP. LEAKING. (EGVR) FUEL PUMP SEAL FAILED, WASHING OUT BLUE DYE FROM THE BEARING. DYE WAS FOUND COMING OUT THE FUEL PUMP /FCU DRAIN L (N497KQ)
- [SDR EVGR060210](https://openairdocs.org/sdr/EVGR060210), Jun 2, 2010: Helio H295. FIRE DETECTOR. CHAFED. (EVGR) THE FIRE DETECTION LOOP IN THE ENGINE COMPARTMENT CHAFED AGAINST SCAT TUBE CAUSING INTERMITTENT ALARM. THE UNIT I (N61JA)
- [SDR EVGR20100405](https://openairdocs.org/sdr/EVGR20100405), Apr 2, 2010: Robsin R44RAVENII. OIL FILTER. CHAFED. (EVGR) AS THE MECHANIC WAS PREPARING TO REMOVE THE OIL FILTER FOR AN ANNUAL INSP, HE NOTICED THE RUST LIKE DUST ON THE O
- [SDR EVGR062910](https://openairdocs.org/sdr/EVGR062910), Mar 22, 2010: COLLAR. BENT. (EVGR) PN 626739M010 TRANSFER COLLAR. THE COLLAR SEEMS TO HAVE BEEN DAMAGED AFTER IT WAS GROUND. ON ONE SIDE THE SPLIT L
- [SDR EVGR20091028](https://openairdocs.org/sdr/EVGR20091028), Oct 26, 2009: Robsin R44RAVENII. BEARING. SEPARATED. BEARING FAILED, SB-62 PREVIOUSLY COMPLIED WITH, WHICH INSTALLED LARGE AREA WASHERS. THE WASHERS DID THEIR JOB AND PREVEN (N622)
- [SDR EVGR20090623](https://openairdocs.org/sdr/EVGR20090623), Jun 19, 2009: Robsin R44RAVENII. CAM. WORN. CUSTOMER REPORTED AN EXCESSIVE MAG DROP (UPWARDS OF 10 PERCENT) AND HARD STARTING. BROUGHT IN LT MAG, IT WAS HARD TO TIM (N149P)
- [SDR 20070125](https://openairdocs.org/sdr/20070125), Jan 24, 2007: Robsin R44RAVENII. GEAR. WORN. DURING INSPECTION OF THE ENGINE WHILE REPLACING THE CRANKSHAFT IAW SB 569A, IT WAS OBSERVED THAT (PN 13519647) CRANKSHAF (N622)
- [SDR EVGR1113735](https://openairdocs.org/sdr/EVGR1113735), Nov 9, 2006: Beech 65A901. DOOR FRAME. CORRODED. CORROSION WAS FOUND AT THE AFT DOOR FRAME AT FUSELAGE STATION 255.5 JUST BELOW AND OUT BOARD OF THE DOOR SNUBBER MOUNT.  (N65JA)
- [SDR EVGR20060915](https://openairdocs.org/sdr/EVGR20060915), Sep 13, 2006: Robsin R44. COIL. WORN. DURING THE FIRST 500 HOUR MAGNETO INSPECTION, THE TAB ON THE COIL WAS MISALIGNED AND EXHIBITED EXCESSIVE WEAR. (N628PM)
- [SDR 20051129](https://openairdocs.org/sdr/20051129), Nov 29, 2005: Helio H295. TUBE. CRACKED. WING SPAR CARRY THRU P/N 295-030-401 IS CRACKED ON LT VERTICAL TUBE, TOP, FRONT SIDE. (N641LW)

All 81: https://openairdocs.org/faa-repair-station/EVGR735D/jaars-inc/reports.md

## STCs held under this name

STC holders whose name matches the station's, matched by OpenAirDocs; a shared name can be another company.

- JAARS Inc. (OpenAirDocs): 18 STCs, https://openairdocs.org/search?q=JAARS%20Inc.&type=stc

## Aircraft registered to this name

Registry owners whose name matches the station's, matched by OpenAirDocs; a shared name can be another company.

- [JAARS INC](https://openairdocs.org/faa-owner/JAARS%20INC.md) (OpenAirDocs): 16 registered aircraft

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