# Flexjet, LLC: FAA repair station DJFR206D - Type: FAA-certificated repair station (14 CFR Part 145) - Certificate number: DJFR206D - Designator: DJFR - Name on the FAA list: FLEXJET, LLC - Address: 26180 CURTISS WRIGHT PARKWAY, CLEVELAND, OH 44143 - Phone: (216) 797-8164 - Email: jonathon.rudy@flexjet.com - Accountable manager: RUDY, JONATHON, (205) 503-0120 - Liaison: RUDY, JONATHON, (205) 503-0120, jonathon.rudy@flexjet.com - 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: 34 - Source: FAA Find a Facility dashboard, https://www.faa.gov/av-info/facility-dashboard - Page: https://openairdocs.org/faa-repair-station/DJFR206D/flexjet-llc 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 - Powerplant: Limited - Radio: Limited - Instrument: Limited - Accessory: Limited - Limited: Nondestructive testing (Nondestructive inspection, testing and processing); Specialized services (A process its operations specifications name, such as plating or heat treating) 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 (34) Filed under designator DJFR by a repair station (submitter type B). - [SDR 99ZZZX2388](https://openairdocs.org/sdr/99ZZZX2388), Jun 2, 1999: HUB. LEAKING. PILOT REPORTED RED DYE OIL LEAK. DISASSEMBLED PROPELLER AND FOUND HUB CRACKED, NR 2 BLADE SOCKET. - [SDR 99ZZZX2632](https://openairdocs.org/sdr/99ZZZX2632), Apr 14, 1999: Cessna 414A. FILTER. LEAKING. AFTER AN OIL CHANGE ON THIS AIRCRAFT WHICH IS MODIFIED WITH RAM , STC'D, REMOTE OIL FILTERS, THE ICE LIGHT WIRE CAME IN (N555DG) - [SDR 98ZZZX4692](https://openairdocs.org/sdr/98ZZZX4692), Nov 16, 1998: Lear 25D. BOLT. WORN. REMOVED ELEVATOR DOWN SPRING TO FACILITATE OTHER MAINTENANCE. DISCOVERED THE ELEVATOR DOWN SPRING DRAW BOLT EXCESSIVELY (N531CW) - [SDR 98ZZZX3178](https://openairdocs.org/sdr/98ZZZX3178), Aug 3, 1998: ACTUATING PIN. FAILED. NR 2 BLADE FOUND ROTATING LOOSE IN HUB. DISASSEMBLED AND INSPECTED. FOUND BLADE ACTUATING PIN BROKEN OFF IN FERRULE. SUS - [SDR 98ZZZX2292](https://openairdocs.org/sdr/98ZZZX2292), May 28, 1998: Cessna 441. ELT TRAY. CRACKED. DURING COURSE OF ROUTINE ELT BATTERY CHANGE NOTED 1 EACH MOUNTING SCREW HAD PULLED OUT OF MOUNTING TRAY AND A SECOND HOL (N88GW) - [SDR 98ZZZX2124](https://openairdocs.org/sdr/98ZZZX2124), May 19, 1998: Cessna 340A. BELLCRANK. FAILED. ARM ON CRANK ASSEMBLY SPUN ON SHAFT ALLOWING LANDING GEAR AND DOOR TO COME OUT OF SYNC. LANDING GEAR DOOR CLOSED PRIOR T (N6826Y) - [SDR 98ZZZX877](https://openairdocs.org/sdr/98ZZZX877), Jan 12, 1998: Cessna 340A. WEB. CORRODED. DURING ANNUAL INSPECTION, FOUND LOWER AREA OF NACELLE WEB IN EXHAUST TUNNEL EXFOLIATED. ONLY ONE OF THE TUNNELS ON THIS (N2699D) - [SDR 98ZZZX155](https://openairdocs.org/sdr/98ZZZX155), Dec 2, 1997: Mtsbsi MU2B60. OIL JET. BROKE. OIL JET BROKE AND LODGED ITSELF IN PLANETARIES AND RING GEAR. RING GEAR BROKE AND COUPLER SHAFT SHEARED RESULTING IN ENG (N46AK) - [SDR 98ZZZX134](https://openairdocs.org/sdr/98ZZZX134), Dec 1, 1997: GOVERNOR. MISREPAIRED. AT DISASSEMBLY FOR OVERHAUL, FOUND UNAPPROVED REPAIRS TO THE MAIN HOUSING IDLER GEAR PUMP SOCKET. THE IDLER GEAR STUD FE - [SDR 97ZZZX4660](https://openairdocs.org/sdr/97ZZZX4660), Oct 13, 1997: HUB. CRACKED. FOUND HUB CRACKED DURING OVERHAUL, NR 2 BLADE SOCKET. - [SDR 97ZZZX4774](https://openairdocs.org/sdr/97ZZZX4774), Sep 23, 1997: PISTON. LEAK. WHEN PARTS ARE MANUFACTURED, THEY ARE PAINTED WITH ZINC CHROMATE. SUBMITTER HAS FOUND ON NEARLY EVERY GOVERNOR DISASSEMB - [SDR 97ZZZX5033](https://openairdocs.org/sdr/97ZZZX5033), Sep 4, 1997: Braero HS125700A. VACUUM LINE. CHAFED. A PRESSURIZATION BUMP WAS FELT WHEN MAIN AIR VALVES WERE TURNED ON OR THROTTLES WERE MOVED. FOUND RT AILERON CABLE HAD C (N701NW) - [SDR 97ZZZX2638](https://openairdocs.org/sdr/97ZZZX2638), Apr 21, 1997: Lear 35A. SWITCH. INTERMITTENT. DURING LANDING GEAR RETRACTION FOR MAINTENANCE, NOSE GEAR DOWNLOCK LIGHT BECAME INTERMITTENT. TROUBLESHOT TO NOSE GEAR A (N425AS) - [SDR 97ZZZX2078](https://openairdocs.org/sdr/97ZZZX2078), Apr 21, 1997: Cessna 340A. SKIN. CORRODED. LUMPS OBSERVED UNDER WING DE-ICE BOOT AND BOOT COMING UNGLUED. DE-ICE BOOT WAS REMOVED AND SEVERE CORROSION FOUND. CORRO (N6826Y) - [SDR 97ZZZX1100](https://openairdocs.org/sdr/97ZZZX1100), Feb 5, 1997: Cessna 441. SKIN. CORRODED. RIGHT WING DEICE BOOT WAS REMOVED FOR REPLACEMENT. WING SKIN WAS FOUND TO HAVE EXCESSIVE CORROSION PITS ON MUCH OF THE S (N410MA) - [SDR 96ZZZX5943](https://openairdocs.org/sdr/96ZZZX5943), Nov 19, 1996: Cessna 425. SWITCH. MALFUNCTION. LEFT HAND GENERATOR APPEARED TO CARRY ONLY 60 AMP LOAD. TROUBLESHOT TO AN INDICATION ERROR. FOUND BAT/GEN SWITCH TO CAUS (N35TK) - [SDR 96ZZZX5820](https://openairdocs.org/sdr/96ZZZX5820), Nov 5, 1996: Lear 35A. LINE ASSY. WORN. UPON INSPECTION DISCOVERED LINE CHAFED UNDER ADEL CLAMP. REMOVAL DISCLOSED RUBBER FROM CLAMP PARTIALLY MISSING AND LINE (N425AS) - [SDR 96ZZZX6101](https://openairdocs.org/sdr/96ZZZX6101), Oct 23, 1996: Cessna 441. TEE STRUCTURE. CRACKED. NOSE GEAR TUNNEL FORWARD SUPPORT 'TEE' WAS FOUND CRACKED IN THE RADIUS OF THE 'TEE' STRUCTURE. THIS IS THE THIRD CRACKED (N489CE) - [SDR 96ZZZX5468](https://openairdocs.org/sdr/96ZZZX5468), Oct 17, 1996: HUB. CRACKED. DURING C/W AD 95-24-05, SL 93-11A OIL FILL. HUB FOUND CRACKED IN NR 3 BLADE SOCKET. - [SDR 96ZZZX5594](https://openairdocs.org/sdr/96ZZZX5594), Oct 15, 1996: BLADE. CRACKED. FOUND RED DYED OIL LEAK NR 2 BLADE. DISASSEMBLED PROP, REMOVED FERRULE, FOUND CRACK IN BLADE THREADS. - [SDR 96ZZZX3336](https://openairdocs.org/sdr/96ZZZX3336), Jun 20, 1996: GOVERNOR. EXCESS WEAR. DISASSEMBLED GOVERNOR FOR INSPECTION AND FLUSH DUE TO USE OF MOBIL AV 1 OIL. FOUND SEVERE WEAR ON FLYWEIGHTS AND PINS NE - [SDR 96ZZZX1548](https://openairdocs.org/sdr/96ZZZX1548), Mar 4, 1996: HUB. CRACKED. DURING C/W AD 95-24-05, FOUND HUB CRACKED IN THREADS, NR 2 BLADE SOCKET. TOTAL TIME SINCE OVERHAUL, 1,226.8 HOURS. - [SDR 96ZZZX1097](https://openairdocs.org/sdr/96ZZZX1097), Feb 18, 1996: Cessna 172RG. CONTROL UNIT. FAILED. PILOT REPORTED LOSS OF ELECTRICAL POWER. AFTER LANDING, UNCOWLED ENGINE AND FOUND THE ACU WAS SMOKED. TROUBLESHOT AND FO (N9343D) - [SDR 96ZZZX848](https://openairdocs.org/sdr/96ZZZX848), Jan 17, 1996: Gulstm 690A. STATOR. DEFECTIVE. DURING C/W WITH AD 95-16-08, FOUND HOT SECTION 3RD STATOR WAS IMPROPER DUE TO NOT BEING STAMPED OR SIGNED AND SERIAL NUM (N690HF) - [SDR 96ZZZX842](https://openairdocs.org/sdr/96ZZZX842), Jan 16, 1996: Cessna 550. ANTIROTATE RING. FAILED. AFTER ENGINE START, ENGINE SOUNDED STRANGE (LIKE VACUUM CLEANER). TROUBLESHOT AND SUSPECTED INTERNAL DAMAGE. ENGINE REMO (N511AB) - [SDR 96ZZZX829](https://openairdocs.org/sdr/96ZZZX829), Jan 16, 1996: Cessna 550. BLADE. FAILURE. ENGINE SOUNDED STRANGE AFTER START. TROUBLESHOT TO ENGINE INTERNAL. SENT OUT FOR OVERHAUL. FOUND 3 HT BLADES FAILED. (N120JP) - [SDR 96ZZZX483](https://openairdocs.org/sdr/96ZZZX483), Jan 8, 1996: Cessna 414A. PLUG SEAL. FAILED. HYDRAULIC FILLER PLUG SEAL LEAKED WATER WHILE ACFT PARKED OUTSIDE. WATER WAS CIRCULATED THROUGH HYD SYSTEM DURING NORMAL (N25SC) - [SDR 97ZZZX399](https://openairdocs.org/sdr/97ZZZX399), Jan 2, 1996: CLAMP. CRACKED. BLADE CLAMP FOUND CRACKED 2 INCHES STARTING AT COUNTERWEIGHT DOWEL PIN HOLE. - [SDR 95ZZZX6411](https://openairdocs.org/sdr/95ZZZX6411), Nov 2, 1995: Cessna 182. HUB. CRACKED. DURING OVERHAUL, A CRACK WAS FOUND IN THREADS OF NR 1 BLADE SOCKET. - [SDR 95ZZZX6459](https://openairdocs.org/sdr/95ZZZX6459), Oct 10, 1995: Gulstm 690A. LINE. DEFECTIVE. DURING C/W SL 327, NOTED AFT FLARE ON BLEED LINE HAD ALMOST COMPLETELY WORN AWAY. PART WAS VERY CLOSE TO FAILURE WHICH W (N690HF) - [SDR 95ZZZX5839](https://openairdocs.org/sdr/95ZZZX5839), Sep 7, 1995: Cessna 441. AUTOPILOT SYSTEM. PINS OPEN. AIRCRAFT PORPOISES VIOLENTLY UPON AUTOPILOT COUPLED APPROACH TO AIRPORT WITH HILLY TERRAIN. TROUBLESHOT SYSTEM AND FOUND (N1210Z) - [SDR 95ZZZX5597](https://openairdocs.org/sdr/95ZZZX5597), Jul 12, 1995: Gulstm 690A. TUBE. FAILED. PILOT REPORTED LOSS OF ALL PRIMARY ELECTRICAL FLIGHT INSTRUMENTS AS WELL AS ALL AVIONICS. TROUBLESHOT AND FOUND TUBE FAI (N333CA) - [SDR 95ZZZX1227](https://openairdocs.org/sdr/95ZZZX1227), Feb 28, 1995: Cessna 421. BEARING. CRACKED. C/W AD 90-02-13 STRUCTURAL INTEGRITY OF THE MAIN GEAR BARREL INNER BEARING, PER CESSNA SB MEB88-7A. FOUND RT AND LT INNE (N4564L) - [SDR 95ZZZX1226](https://openairdocs.org/sdr/95ZZZX1226), Feb 28, 1995: Cessna 421. BEARING. CRACKED. C/W AD 90-02-13 STRUCTURAL INTEGRITY OF THE MAIN GEAR BARREL INNER BEARING, PER CESSNA SB MEB88-7A. FOUND RT AND LT INNE (N4564L) ## Other certificates of this company (3) - [DJF2206D](https://openairdocs.org/faa-repair-station/DJF2206D/flexjet-llc): Flexjet, LLC, Teterboro, NJ - [DJF4206D](https://openairdocs.org/faa-repair-station/DJF4206D/flexjet-llc): Flexjet, LLC, Westchester County Air, NY - [DJF5206D](https://openairdocs.org/faa-repair-station/DJF5206D/flexjet-llc): Flexjet, LLC, Dallas, TX ## STCs held under this name STC holders whose name matches the station's, matched by OpenAirDocs; a shared name can be another company. - FlexJet, LLC (OpenAirDocs): 3 STCs, https://openairdocs.org/search?q=FlexJet%2C%20LLC&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. - [FLEXJET LLC](https://openairdocs.org/faa-owner/FLEXJET%20LLC.md) (OpenAirDocs): 243 registered aircraft - [FLEXJET LLC](https://openairdocs.org/faa-owner/FLEXJET%20%20LLC.md) (OpenAirDocs): 1 registered aircraft --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.