# Schreck Fba 310 - Type: Aircraft model (FAA registry) - Registry code: 05635VZ - Manufacturer (registry): SCHRECK FBA - Model: 310 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 ยท Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/schreck-fba-310 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (91, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000835](https://openairdocs.org/sdr/2026FA0000835), Oct 14, 2026: SWITCH. MALFUNCTIONED. LANDING GEAR SWITCH, DOWN POSITION SAFETY FAILED DUE TO WEAR ALLOWING INADVERTENT UP POSITION ACTUATION WHEN BUMPED. - [SDR 2021FA0000285](https://openairdocs.org/sdr/2021FA0000285), Sep 13, 2021: HEAT EXCHANGER. DAMAGED. RIGHT ENGINE FUEL LEAK OF HEAT EXCHANGER OIL-FUEL DRAIN, DURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK AT RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVI - [SDR 2021FA0000235](https://openairdocs.org/sdr/2021FA0000235), Aug 17, 2021: LANDING GEAR. COLLAPSED. LANDED AND ON ROLL OUT THE PILOT NOTICED A VIBRATION ON RIGHT SIDE OF AIRCRAFT. AFTER NOTICING THE VIBRATION THE RIGHT MAIN GEAR COLLAPSED CAUSING DAMAGE TO RIG - [SDR 2017FA0000471](https://openairdocs.org/sdr/2017FA0000471), Aug 30, 2017: RELAY. SHORTED. AIRCRAFT LOST ALL AVIONICS POWER WHILE IN LEVEL FLIGHT, PILOT DECLARED EMERGENCY LANDING AND LANDED AIRCRAFT WITHOUT INCIDENT. MECHANICS DETERMINED THAT THE STA - [SDR CA150820003](https://openairdocs.org/sdr/CA150820003), Aug 11, 2015: WARNING LIGHT. ILLUMINATED. (CAN) DURING TAKEOFF ROLL, WHEN SET POWER WAS ACHIEVED, THE RIGHT OIL FILTER BYPASS LIGHT ILLUMINATED. POWER WAS REDUCED TO IDLE, LIGHT WENT OUT, AIRCRAFT RETUR - [SDR 2010FA0000003](https://openairdocs.org/sdr/2010FA0000003), Dec 11, 2009: ROD END. BROKEN. ROD END BROKE WHEN ATTEMPTING TO EXTEND THE LANDING GEAR IN FLIGHT. COULD NOT EXTEND THE GEAR, RESULTING IN A GEAR-UP LANDING. UPON INSPECTION OF THE ROD END, F - [SDR 2004FA0000149](https://openairdocs.org/sdr/2004FA0000149), Jan 20, 2004: COUNTERWEIGHT. CRACKED. PART HAD APPROX 700.00 HOURS SINCE OVERHAUL, FATIGUE CRACK APPEARS TO HAVE ORIGINATED AT FORWARD BOLT HOLE. PROPELLER/ENGINE BEGAN VIBRATING IN FLIGHT DUE TO CO - [SDR 2003FA0001063](https://openairdocs.org/sdr/2003FA0001063), Oct 15, 2003: SKIN. CORRODED. AFTER REMOVAL OF NACELLE AUX FUEL TANK, DISCOVERED A LARGE AREA OF CORROSION ON THE TOP WING SKIN. THE TANK HAD TRAPPED MOISTURE BETWEEN IT AND THE WING TOP OVE - [SDR 2003FA0001085](https://openairdocs.org/sdr/2003FA0001085), Oct 15, 2003: RIVET. LOOSE. THE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS P - [SDR 2003FA0001084](https://openairdocs.org/sdr/2003FA0001084), Oct 15, 2003: RIVET. LOOSE. THE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS P - [SDR 20000817SH013](https://openairdocs.org/sdr/20000817SH013), Jul 31, 2000: NUT. CRACKED. PROPELLER IN FOR OVERHAUL. DISASSEMBLED, FOUND BOTH RETENTION NUTS CRACKED. (X) - [SDR 20000407SH012](https://openairdocs.org/sdr/20000407SH012), Jan 31, 2000: TORQUE TUBE. BROKEN. PART FAILED AT GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR COLLAPSED AT LANDING. COMPONENT WAS REDESIGNED STARTING WITH A/C SN 35042. SUBMITTER SUGGESTED ADDED EMP - [SDR 99ZZZX4659](https://openairdocs.org/sdr/99ZZZX4659), Dec 11, 1999: CONTROL CABLE. LOOSE. DURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGER WHERE THEY PASSED THROUGH (BELOW THE F - [SDR 20000621SH011](https://openairdocs.org/sdr/20000621SH011), Oct 6, 1999: COOLER. LEAKING. OIL COOLER RUPTURED AT POINT OF PREVIOUS EPOXY REPAIR CAUSING SEVERE LEAK. EPOXY FAILURE IS COMMON AND SHOULD BE ELIMINATED FROM BEING USED IN OIL COOLERS. (X) - [SDR 20000712SH036](https://openairdocs.org/sdr/20000712SH036), Jun 9, 1999: COOLER. LEAKING. PART BEGAN LEAKING DURING NORMAL SERVICE DUE TO EPOXY REPAIR FAILURE. SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY REPAIR ON AND IN OIL COOLERS AS EPOXY REPAI - [SDR 99ZZZX2633](https://openairdocs.org/sdr/99ZZZX2633), Jun 1, 1999: TORQUE TUBE. WORN. UPON INSPECTION, FOUND BOTH FUEL SELECTOR TORQUE TUBE ASSEMBLIES, PN 0820000-5 AND PN 0812000-13, SUFFERED SEVERE WEAR. TUBE, PN 082000-5, WORN AT FUSELAGE GROM - [SDR 99ZZZX2397](https://openairdocs.org/sdr/99ZZZX2397), May 9, 1999: TUBE. FAILED. UPON LANDING TOUCHDOWN AT YIP, THE LEFT MLG COLLAPSED. INVESTIGATION SHOWED A FAILURE OF THE LT MAIN GEAR DRIVE TUBE ASSY WHICH PREVENTED THE LEFT MAIN GEAR FRO - [SDR CA981116006](https://openairdocs.org/sdr/CA981116006), Oct 15, 1998: CONTROL CABLE. FRAYED. (CAN) ELEVATOR CABLE FOUND FRAYED DOWN CENTER JUST FORWARD OF THE THE REAR SPAR AT THE PULLEY AND THE ELEVATOR TRIM CABLE FRAYED DOWN CENTER BEHIND THE REAR SPA - [SDR 98ZZZX229](https://openairdocs.org/sdr/98ZZZX229), Jan 1, 1998: IDLER BELLCRANK. FAILED. PILOT AND 1 PASSENGER DEPARTED ON A LOCAL VFR FLIGHT. UPON RETRACTING LANDING GEAR, PILOT HEAR A LOUD THUMP AND AT THE SAME TIME, FELT A THUD UNDER HIS FEET. TH - [SDR EY2R9601087](https://openairdocs.org/sdr/EY2R9601087), Oct 1, 1996: BLADE. CORRODED. BLADE, SN C41944YS, FOUND CORRODED. - [SDR EY2R9601086](https://openairdocs.org/sdr/EY2R9601086), Oct 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9601085](https://openairdocs.org/sdr/EY2R9601085), Oct 1, 1996: BLADE. CORRODED. BLADE FOUND CORRODED. - [SDR EY2R9601033](https://openairdocs.org/sdr/EY2R9601033), Oct 1, 1996: BLADE. CORRODED. BLADE, SN B29888YS, FOUND CORRODED. - [SDR EY2R9601032](https://openairdocs.org/sdr/EY2R9601032), Oct 1, 1996: BLADE. CORRODED. BLADE, SN C30806YS, FOUND CORRODED. - [SDR EY2R9600136](https://openairdocs.org/sdr/EY2R9600136), Oct 1, 1996: HUB. CRACKED. HUB CRACKED IN BLADE SOCKET - [SDR EY2R9600117](https://openairdocs.org/sdr/EY2R9600117), Oct 1, 1996: BLADE. CRACKED. BLADE NR1 SOCKET CRACKED - [SDR CA961007005](https://openairdocs.org/sdr/CA961007005), Sep 19, 1996: PISTON ROD. BROKEN. (CAN) ROD FAILURE AT CRANKSHAFT, ROD BROKE IN HALF. ROD EXITED THROUGH TOP OF CRANKCASE REAR LEFT SIDE. - [SDR EY2R9601064](https://openairdocs.org/sdr/EY2R9601064), Sep 1, 1996: NUT. CORRODED. NUT CORRODED. - [SDR EY2R9601063](https://openairdocs.org/sdr/EY2R9601063), Sep 1, 1996: RETAIN BEARING. CORRODED. RETAIN BEARING FOUND CORRODED. - [SDR EY2R9601575](https://openairdocs.org/sdr/EY2R9601575), Jul 1, 1996: HUB. DAMAGED. PROP HUB STAKING PIN HOLE TOO DEEP - [SDR EY2R9601574](https://openairdocs.org/sdr/EY2R9601574), Jul 1, 1996: HUB. MIS DRILLED. NR1 SOCKET, STAKNG PIN DRILLED WRONG - [SDR EY2R9600100](https://openairdocs.org/sdr/EY2R9600100), Jul 1, 1996: HUB. CRACKED. HUB CRACKED IN NR2 SOCKET - [SDR EY2R9600099](https://openairdocs.org/sdr/EY2R9600099), Jul 1, 1996: CRACKED. HUB CRACKED IN THREAD AREA - [SDR EY2R9600748](https://openairdocs.org/sdr/EY2R9600748), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600732](https://openairdocs.org/sdr/EY2R9600732), Jun 1, 1996: BLADE. CORRODED. BLADE, SN F75090YS, FOUND CORRODED. - [SDR EY2R9600731](https://openairdocs.org/sdr/EY2R9600731), Jun 1, 1996: BLADE. CORRODED. BLADE, SN K76877YS, FOUND CORRODED. - [SDR EY2R9600730](https://openairdocs.org/sdr/EY2R9600730), Jun 1, 1996: BLADE. CORRODED. BLADE, SN K76239YS, FOUND CORRODED. - [SDR EY2R9600729](https://openairdocs.org/sdr/EY2R9600729), Jun 1, 1996: BLADE. CORRODED. BLADE, SN K76240YS, FOUND CORRODED. - [SDR EY2R9600728](https://openairdocs.org/sdr/EY2R9600728), Jun 1, 1996: BLADE. CORRODED. BLADE, SN K76165YS, FOUND CORRODED. - [SDR EY2R9600727](https://openairdocs.org/sdr/EY2R9600727), Jun 1, 1996: BLADE. CORRODED. BLADE, SN BG348YS, FOUND CORRODED. - [SDR EY2R9600726](https://openairdocs.org/sdr/EY2R9600726), Jun 1, 1996: BLADE. CORRODED. BLADE, SN BG409YS, FOUND CORRODED. - [SDR EY2R9600725](https://openairdocs.org/sdr/EY2R9600725), Jun 1, 1996: BLADE. CORRODED. BLADE, SN BF119YS, FOUND CORRODED. - [SDR EY2R9600724](https://openairdocs.org/sdr/EY2R9600724), Jun 1, 1996: BLADE. CORRODED. BLADE, SN BD1015YS, FOUND CORRODED. - [SDR EY2R9600723](https://openairdocs.org/sdr/EY2R9600723), Jun 1, 1996: BLADE. CORRODED. BLADE, SN BD1029YS, FOUND CORRODED. - [SDR EY2R9600722](https://openairdocs.org/sdr/EY2R9600722), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600721](https://openairdocs.org/sdr/EY2R9600721), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600720](https://openairdocs.org/sdr/EY2R9600720), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600716](https://openairdocs.org/sdr/EY2R9600716), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600715](https://openairdocs.org/sdr/EY2R9600715), Jun 1, 1996: HUB. CORRODED. HUB FOUND CORRODED. - [SDR EY2R9600714](https://openairdocs.org/sdr/EY2R9600714), Jun 1, 1996: NUT. CORRODED. NUT CORRODED. All 91: https://openairdocs.org/model/schreck-fba-310/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Cessna 310](https://openairdocs.org/model/cessna-310): 103 registered aircraft, registry code 2074202 --- 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.