# Consolidated 108-2 - Type: Aircraft model (FAA registry) - Registry code: 05606IQ - Manufacturer (registry): CONSOLIDATED AIRCRAFT CORP - Model: 108-2 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 ยท Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/consolidated-108-2 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. ## Information bulletins (advisory) (1) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 ## 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 (16) As reported by operators and repair stations, by the model named in the report. - [SDR 2011FA0000372](https://openairdocs.org/sdr/2011FA0000372), May 24, 2011: TERMINAL. MELTED. THE POSITIVE STUD MELTED OUT FROM THE ARMMETER AND THE ACFT LOST POWER TO THE BUSS BAR. - [SDR 2010FA0001054](https://openairdocs.org/sdr/2010FA0001054), Aug 28, 2010: WHEEL. FAILED. CAST SHOULDER THAT HOLDS THE WHEEL BRG RACE FROM MOVING INWARD ON THE AXLE, BROKE OUT, CAUSING THE RACE AND BRG TO TRAVEL INWARD. THE WHEEL WAS NO LONGER HELD C - [SDR CA091113001](https://openairdocs.org/sdr/CA091113001), Oct 25, 2009: TUBE. CORRODED. (CAN) TUBING RUSTED OUT AFT FITTING. - [SDR 2009FA0000850](https://openairdocs.org/sdr/2009FA0000850), Aug 3, 2009: GEAR. FRACTURED. ON A FLIGHT THE ENGINE STOPPED SUDDENLY WITH NO WARNING. THE AIRCRAFT LANDED. THE ENGINE ACCESSORY CASE HAD MAJOR DAMAGE. THE MAGNETOS WERE BROKEN AWAY FROM THE - [SDR 20000717SH010](https://openairdocs.org/sdr/20000717SH010), Jun 10, 2000: CRANKSHAFT. FAILED. ENGINE BEGAN RUNNING ROUGH AND THEN THE PROPELLER LOCKED IN THE VERTICAL POSITION. POST-INCIDENT INSPECTION OF THE ENGINE REVEALED THE CRANKSHAFT HAD FAILED. (X - [SDR 99ZZZX23](https://openairdocs.org/sdr/99ZZZX23), Dec 8, 1998: SEAT. BROKEN. SEAT BROKE AT BOTH HORIZONTAL LEGS. MATERIAL .50 INCH OUTSIDE DIAMETER, .035 INCH WALL 4130 STEEL TUBES. FRACTURES SHOW EVIDENCE OF CRYSTALLIZATION FROM BENDING - [SDR CA980430023](https://openairdocs.org/sdr/CA980430023), Apr 23, 1998: HUB. WORN. (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CYLINDER SUPPORT WAS FOUND BENT AND THE CYLINDER WAS WORN. - [SDR CA980406003](https://openairdocs.org/sdr/CA980406003), Mar 30, 1998: CONTROL COLUMN. CORRODED. (CAN) WHILE PAINT STRIPPING THE CONTROL COLUMN A PIN HOLE APPEARED. REMOVING THE ALUMINUM PLUG, A LINE OF CORROSION WAS FOUND HALF WAY AROUND THE INSIDE OF THE - [SDR 98ZZZX313](https://openairdocs.org/sdr/98ZZZX313), Dec 2, 1997: CRANKSHAFT. CRACKED. INSPECTION FOUND CRANKSHAFT PROPELLER FLANGE CRACKED BETWEEN HOLES IN TWO PLACES. - [SDR CA970305006](https://openairdocs.org/sdr/CA970305006), Feb 4, 1997: WELD. FAILED. (CAN) THE WELD THAT HOLDS THE AXLE ATTACHMENT BUSHING TO THE LANDING GEAR LEG FAILED. REPLACED. - [SDR 96ZZZX3353](https://openairdocs.org/sdr/96ZZZX3353), Jun 5, 1996: VALVE. STUCK. PILOT REPORTED FUEL SELECTOR VALVE STUCK BETWEEN DETENTS WHILE ATTEMPTING TO CHANGE FROM RT TO LT FUEL TANK. AFTER PUTTING BOTH HANDS ON VALVE HANDLE, THE PASSE - [SDR EY2R9600203](https://openairdocs.org/sdr/EY2R9600203), Jan 1, 1996: HUB. CORRODED. PROP ASSY HUB IS CORRODED - [SDR EY2R9600202](https://openairdocs.org/sdr/EY2R9600202), Jan 1, 1996: BLADE. CORRODED. BLADE ASSY SN C45338YS IS CORRODED - [SDR EY2R9600201](https://openairdocs.org/sdr/EY2R9600201), Jan 1, 1996: BLADE. CORRODED. BLADE ASSY SN K31785YS IS CORRODED - [SDR 95ZZZX4488](https://openairdocs.org/sdr/95ZZZX4488), Aug 1, 1995: CRANKSHAFT. BROKE. CRANKSHAFT - REGROUND 18 HOURS EARLIER. AT OVERHAUL, BROKE AT REAR THROW WITH LOSS OF POWER. GRINDING MAY HAVE BEEN THE WORK OF AN AUTOSHOP WITH NO INTEREST IN - [SDR 95ZZZX4201](https://openairdocs.org/sdr/95ZZZX4201), Jun 9, 1995: HORN. NOTCHED. INSPECTION OF CONTROL HORN FOUND IT 'NOTCHED'. HARD RT RUDDER APPLICATION REPEATEDLY HIT VERTICAL ASSEMBLY CAUSING IMPACT DAMAGE. SOME ONE FAILED TO 'FIX' DAMAG ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Stinson 108-2](https://openairdocs.org/model/stinson-108-2): 285 registered aircraft, registry code 9230406 - [Universal Stinson 108-2](https://openairdocs.org/model/universal-stinson-108-2): 38 registered aircraft, registry code 9230416 - [Consolidated Vultee 108-2](https://openairdocs.org/model/consolidated-vultee-108-2): 0 registered aircraft, registry code 0562200 --- 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.