Cessna 182S

Service difficulty reports · 120

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 aircraft_model_key = '182S'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 001AFuel Tank · leakingFUEL LEAKING FROM RIGHT WING ROOT, FUEL STAIN ON FUSELAGE. DRAINED FUEL, OPENED ACCESS PANELS OF FUEL TANK, FOUND SEALANT USED AROUND FUEL CELL (WET WING) INTERIOR AT THE OUTLET HAD A VOID AREA UNDER THE OUTLET TUBE ASSEMBLY. APPARENT LACK OF ATTENTION TO DETANov 20, 2002 · N182AM · Cessna 182S · Fuel StorageSDR 2002FA0001205Bolt · defectiveFINAL TORQUE OF CRANKSHAFT BOLT COULD NOT BE REACHED, AFTER REMOVAL OF BOLT, IT WAS FOUND TO BE DEFFECTIVE, AND TAPPERED TOWARDS THE CENTER OF THE SHANK.Oct 17, 2002 · N9562D · Cessna 182S · Reciprocating Engine Power SectionSDR 2002FA0001046Valve Guide · seizedNR 2 CYLINDER EXHAUST VALVE SIEZED IN VALVE GUIDE POSSIBLY DUE TO CARBON BUILD UP. NR 2 PUSHROD AND PUSHROD SHROUD WERE BENT. NR 2 EXHAUST PLUNGER ALSO REPLACED AT MFG RECOMMENDATION.Aug 23, 2002 · N926WB · Cessna 182S · Reciprocating Engine Cylinder SectionSDR 2002FA0000912Retainer · missingNR 3 CYLINDER PUSH ROD BENT, REMOVED THE NR 5 CYLINDER VALVE COVER FOR FURTHER INSPECTION AND FOUND PUSH ROD RETAINING CLIP MISSING AND ASSOCIATED HARDWARE. NO DAMAGE OR PARTS FOUNDJul 19, 2002 · N300WF · Cessna 182S · Reciprocating Engine Cylinder SectionSDR CA020617003Connecting Rod · broken(CAN) CONNECTING ROD APPEARS TO HAVE BROKEN 1 INCH OUT FROM CRANKSHAFT JOURNAL. THIS WRAPPED ITSELF AROUND UNTIL THE CONNECTING ROD CAP DEPARTED AND THE PIECES BROKE THE CASE 60 PERCENT OF THE WAY AROUND THE ENTIRE CASE AND DESTROYED THE CAMSHAFT AND JAMMED UPMay 14, 2002 · Cessna 182S · Reciprocating Engine Power SectionSDR 2002FA0000621Computer · failedTHE AC WAS IN LEVEL FLIGHT WITH AUTOPILOT TURNED OFF. WHEN THE AUTOPILOT COMPUTER, WITHOUT INPUT FROM THE PILOT GAVE AN INDICATION THAT (PITCH WARNING) LIGHT CAME ON WITH A (UP) ARROW. THE PILOT PULLED THE AUTOPILOT CIRCUIT BREAKER TO TURN OFF SYSTEM. ANOTHFeb 22, 2002 · N97TD · Cessna 182S · Autopilot ComputerSDR WXH2002F00000Strainer · damagedUPON REINSTALLATION OF FUEL STRAINER AFTER INSPECTION, STANDPIPE THREADS FATIGUED. FAILED WHEN STANDPIPE WAS TIGHTENED. INSPECTION REVEALED ONLY 1.5 TO 2 TURNS ENGAGEMENT THREADS, DO NOT GO UP TO THE TOP OF STANDPIPE AS IN 182 T MODELS WE THINK THIS IS A SAJan 9, 2002 · N1252E · Cessna 182S · Aircraft Fuel Filter/StrainerSDR 2001FA0000577Fuel Line · chafedDURING 100 HOUR INSPECTION, DISCOVERED NR2 CYLINDER FUEL INJECTION LINE LEAKING WHILE ACCOMPLISHING MFG SB. FUEL LINE SUPPORT CLAMP HAD BECOME LOOSE AND CAUSED LINE TO CONTACT NR2 CYLINDER FINS, WHICH WORE 6 GROOVES IN LINE.Nov 14, 2001 · N931SJ · Cessna 182S · Engine Fuel DistributionSDR 2001FA0000489Main Bearing · delaminatedFRONT MAIN BEARING DELAMINATION. DEFECT AREA WAS ABOUT THE SIZE OF A DIME. THERE WAS EVIDENCE OF SUBSURFACE FLAWS IN THE SURROUNDING AREA. THE CAUSE WOULD BE IMPROPER MANUFACTURING.Nov 1, 2001 · N61US · Cessna 182S · Reciprocating Engine Power SectionSDR 2001FA0000580Pitot Line · burnedPITOT HEAT INSULATION, BURN MARKS WERE FOUND ON PITOT PRESSURE LINE. CONDITION RESULTS FROM HAVING PLASTIC LINE CONNECTED TO HEATED PITOT MAST. THE SB CORRECTS THIS BY ADDING PLASTIC SPIRAL WRAP TO LINE AND POWER WIRES AT THE PITOT MAST. THIS PREVENTS PITOTOct 31, 2001 · N9472F · Cessna 182S · Pitot/Static SystemSDR 2001FA0000411Switch · failedPUSH TO TALK SWITCH FAILED AFTER 1 HOUR OF OPERATION. HAS HAPPENED FOUR TIMES IN A ROW.Oct 4, 2001 · N3261M · Cessna 182S · Communications SystemSDR 2001FA0000386Switch · inoperativeTHE PILOTS SIDE PUSH TO TALK SWITCH WENT BAD WITH ONLY 548.0 TACH TIME. REPLACE THE BAD SWITCH WITH A NEW ONE. THE NEW SWITCH WAS BAD ALSO, THEN REPLACED THE NEW SWITCH THE SECOND NEW SWITCH TESTED OK. WHEN INSTALLING SWITCHES, WAS CAREFUL NOT TO OVERHEAT SSep 18, 2001 · N3261M · Cessna 182S · Communications SystemSDR 2001FA0000136Fitting · brokenTHE PILOT REPORTED THAT THERE WAS ZERO VACUUM INDICATED ON THE GAUGE AND THAT THE HSI GYRO WOULD NOT ERECT. A VISUAL INSPECTION BY A MAINTENANCE TECHNICIAN REVEALED THAT THE VACUUM SUPPLY LINE REDUCER FITTING WAS BROKEN IN TWO.Jul 5, 2001 · N7260Q · Cessna 182S · Vacuum Distribution SystemSDR 2001FA0000182Gasket · missingWHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, AND OIL LEAK WAS NOTICED COMING FROM THE LOWER VACUUM PUMP DRIVE PAD. FURTHER INSPECTION REVEALED THAT THE GASKET FOR THE PUMP WAS MISSING. A NEW GASKET WAS INSTALLED AND A LEAK CHECK WAS PERFORMED.Jun 14, 2001 · N132ME · Cessna 182S · Vacuum Distribution SystemSDR 2001FA0000069Elevator · weakWHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, SEVERAL WRINKLES AND LOOSE RIVETS WERE DISCOVERED ON BOTH ELEVATORS ALONG WHERE THE BALANCE TAB ATTACHES TO THE ELEVATOR SPAR. THE STRUCTURE AROUND THIS AREA APPEARED VERY WEAK AND FLEXIBLE. CESSNA WAS Jun 14, 2001 · N132ME · Cessna 182S · Elevator Control SystemSDR 2001FA0000064Elevator · weakWHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, SEVERAL WRINKLES AND LOOSE RIVETS WERE DISCOVERED ON BOTH ELEVATORS ALONG WHERE THE BALANCE TAB ATTACHES TO THE ELEVATOR SPAR. THE STRUCTURE AROUND THIS AREA APPEARED VERY WEAK AND FLEXIBLE. CESSNA WAS Jun 14, 2001 · N132ME · Cessna 182S · Elevator Control SystemSDR 20010612CW003Spar · crackedREAR STABILIZER/ REAR SPAR LEFT SIDE/ CRACKED.May 15, 2001 · N63CE · Cessna 182S · Horizontal Stabilizer, Spar/RibSDR AUS20010665Cylinder · leaking(AUS) RH BRAKE MASTER CYLINDER LEAKING AT ELBOW FITTING. INVESTIGATIONFOUND THAT THE ELBOW HAD NOT BEEN FULLY SCREWED IN AND THESEALING O' RING WAS DISPLACED ONTO THE THREADS OF THE ELBOW INSTEAD OF FITTING INTO THE SEAL RECESS DUE TO THE B' NUTCOVERING THE RApr 26, 2001 · Cessna 182S · Master Cylinder/Brake ValveSDR 20010323CW011Cylinder · brokenSEAT LOCK CYLINDER PN C1650310101 ON PILOTS SEAT. THE SHAFT ON CYLINDER BROKE WHERE IT GOES INTO THE FORK THAT ATTACHES TO SEAT BACK.Feb 28, 2001 · N63CE · Cessna 182S · Flight Compartment EquipmentSDR 20010227CW010Light · inoperativePILOT/OWNER REPORTED THAT RADIO INDICATOR BACKLIGHTING AND RADIO CONTROL BACKLIGHTING HAD NOT WORKED SINCE AIRCRAFT DELIVERY. TROUBLESHOT SYSTEM, FOUND THAT PIN 1 OF JC005 WAS AT GROUND POTENTIAL, PREVENTING DIMMER POTENTIOMETER FROM FUNCTIONING AS IT IS SUPPFeb 12, 2001 · N72689 · Cessna 182S · Instrument PanelSDR 20010124CW009Rudder · interferenceWHEN CHECKING RUDDER TRAVEL, ELEVATOR WAS IN NEUTRAL POSITION. WHILE THE RUDDER WAS DEFLECTED FULL IN EITHER DIRECTION, THE ELEVATOR WOULD HIT THE RUDDER WHEN THE ELEVATOR WAS RAISED. THE RUDDER TRAVEL WAS RIGGED CORRECTLY PER MAINTENANCE MANUAL. THIS COULJan 24, 2001 · N162TC · Cessna 182S · Rudder Control SystemSDR AU010029Flow Divider · corroded(AUS) ENGINE FUEL FLOW DIVIDED CORRODED. PARTICLES OF CORROSION BLOCKING FUEL INJECTORS. AIRCRAFT HAD BEEN CONTAMINATED WITH EDAAND DECONTAMINATED IAW AD/GEN/80 AND MANUFACTURERS INSTRUCTIONS.Jan 16, 2001 · Cessna 182S · Engine Fuel DistributionSDR 20001121SH005Connector · corrodedAT 100-HOUR INSPECTION, REMOVED TAILCONE AND FOUND IT FILLED WITH APPROXIMATELY 1.50 INCHES OF WATER. WATER HAD CORRODED CONNECTOR FOR TAIL NAVIGATION LIGHT. CONNECTOR WAS REPLACED AND LOWER ATTACH SCREW FOR TAILCONE WAS NOT RE-INSTALLED TO ALLOW FOR FUTURE Oct 17, 2000 · N23735 · Cessna 182S · Exterior LightingSDR 20000927SH003Pulley · burredWHILE PERFORMING SB 00-27-02, DATED AUGUST 14, 2000, TO INSPECT FOR PROPER RADIUS WHERE INTERCONNECT CABLE IS ATTACHED TO QUADRANT, AILERON CABLE 0510105-328 WAS FOUND SEVERELY WORN. CABLE WEAR WAS WHERE CABLE CONTACTED PULLEY GROOVE (OUTER SECTION OF 1260112Sep 26, 2000 · N543MC · Cessna 182S · Aileron Control SystemSDR 20000914SH018Seal · leakingPROPELLER OIL LEAKING FROM SERVICE PLUG, AND BLADE SEALS. NO INSTRUCTIONS PROVIDED FOR APPROVAL FOR RETURN TO SERVICE. (X)Sep 3, 2000 · N913CT · Cessna 182S · Propeller Blade SectionSDR 20000814SH016Propeller · leakingPILOT/OWNER REPORTED OIL ON PROPELLER BLADES, WINDSHIELD. INSPECTION OF PROPELLER HUB FOUND RED DYE LEAKING FROM HUB SERVICE PLUG. SUBMITTER STATED THIS IS THE SECOND 182S MCCAULEY PROPELLER WITH A LEAK FROM PLUG. ALSO, A CESSNA 206H MCCAULEY PROPELLER WAS Aug 14, 2000 · N7267Z · Cessna 182S · Propeller SystemSDR 20000816SH035Bushing · deformedDURING A ROUTINE INSPECTION OF THE AIRFRAME, THE LEFT MAIN LANDING GEAR BUSHING WAS FOUND DEFORMED. THE INSIDE BUSHING MATERIAL WAS PROTRUDING FROM THE EDGE OF THE BUSHING. THE BUSHING WAS FURTHER INSPECTED AFTER REMOVAL FROM THE AIRCRAFT AND CONTAINED STRESJul 26, 2000 · N321HW · Cessna 182S · Main Landing Gear Strut/Axle/TruckSDR 20000721SH031Bracket · inadequate****PART LOC: ELEV CABLE PULLEY BRACKET*****WHILE TRYING TO C/W CESSNA MANDATORY SB 00-27-01, REPLACEMENT OF ELEVATOR CONTROL CABLE SUPPORT BRACKET, FOUND NEW BRACKET PN 2213063-203 WAS IMPROPERLY MANUFACTURED AND WILL NOT PERFORM ITS INTENDED FUNCTION. (X)Jun 30, 2000 · N6870L · Cessna 182S · Elevator Control SystemSDR 20000620SH009Pump · leakingSEAL BETWEEN PUMP AND MOTOR LEAKING SEVERELY OUT DRAIN TUBE. THE ONLY WAY TO STOP IT FROM LEAKING IS TO TURN THE FUEL SELECTOR VALVE TO THE OFF POSITION. THE ORIGINAL PUMP WAS REPLACED FOR THE SAME PROBLEM AT 81.9 HOURS. INSTALL OVERHAULED PUMP P/N 5100-00-Jun 1, 2000 · N664PB · Cessna 182S · Fuel Boost PumpSDR 20000516SH011Guide · failedEXHAUST VALVE STUCK, BENDING PUSH ROD AND HOUSING. SEE LYC SI 1425H, 1485. SB388B. FOUND 3 OTHER CYLINDERS WITH STUCK VALVES. SUBMITTER SUGGESTED AD BE ISSUED. (X)Apr 19, 2000 · N7267H · Cessna 182S · Reciprocating Engine Cylinder SectionSDR 20000504SH010Control Cable · out of rigWHILE CHECKING FOR ELEVATOR TRIM OPERATOR AFTER C/W SB 00-22-01A ON KAP-104 AUTOPILOT SERVO, NOTED THE ELEVATOR TRIM WOULD NOT GO FULL TRAVEL. AFTER INVESTIGATING, NOTED THE SERVO TRIM CABLE SWEDGED BALL WAS OUTSIDE THE SERVO DRUM, THE AUTOPILOT CABLE WAS NOTApr 15, 2000 · N789LM · Cessna 182S · Elevator Tab Control SystemSDR 20000413SH062Roll Servo · inoperativeFOUND AUTOPILOT ROLL SERVO IDLER GEAR ATTACH NUT BACKED OFF SCREW AND OUTPUT GEAR BEARINGS DEFECTIVE DURING COMPLIANCE WITH SB KS271C-5 ALERT DATED FEB 1, 2000. SUBMITTER STATED FAILURE COULD CAUSE SERVO TO REMAIN ENGAGED EVEN WHEN AUTOPILOT IS DISENGAGED. Mar 27, 2000 · N23383 · Cessna 182S · Autopilot SystemSDR 20000407SH021Servo · wornWHILE PERFORMING A SERVICE BULLETIN ON PRIMARY SERVO (SB KS271C-5 ALERT NOTED THE SERVO GEAR TEETH TO HAVE EXCESSIVE WEAR. GEAR BEARING APPEARS TO BE MAKING METAL. THERE WAS A BLACKISH METAL POWDER RESIDUE UNDER THE GEAR. WHEN THE GEAR IS TURNED BY HAND IT Mar 1, 2000 · N351BR · Cessna 182S · Leading Edge Slat Control SystemSDR 20000407SH010Servo · wornWHILE PERFORMING A SERVICE BULLETIN ON A PRIMARY SERVO (SB KS271C-5 ALERT) NOTED THE SERVO GEAR TEETH TO HAVE EXCESSIVE WEAR. GEAR BEARING APPEARS TO BE MAKING METAL. MEAL POWDER RESIN VISIBLE UNDER THE GEAR. GEAR ROTATION IS NOT SMOOTH AND MAKES A SLIGHT GFeb 20, 2000 · N116ZX · Cessna 182S · Flight Control SystemSDR 2000ZZZX656Switch · failedOIL PRESSURE SWITCH FAILED IN-FLIGHT. LOST 7-1/2 QUARTS OF OIL IN 20 MINUTE FLIGHT. HAS 9 QUART SUPPLY. SWITCH FAILED AT PLASTIC HOUSING. SINCE OIL GOES UNDER AND ON BELLY, HAVE NO IDEA OF OIL LEAK IN-FLIGHT. CESSNA SAID IT HAS HAD AT LEAST 4 FAILURES. (Feb 9, 2000 · N9539L · Cessna 182S · Engine Oil PressureSDR 2000ZZZX136Fairing · mismanufacturedPART INDICATED CAME FROM FACTORY INSTALLATION ON BRAND NEW AIRCRAFT WITHOUT 2 FORWARD HOLES DRILLED AND FITTED.Dec 16, 1999 · N213CM · Cessna 182S · Horizontal Stabilizer StructureSDR 20000623SH005Rudder Pedal · wrong partTHE PILOT''S LEFT RUDDER PEDAL HAS THE WRONG PART NUMBER FORWARD SHAFT INSTALLED FROM FACTORY AND IN THE PARTS BREAKDOWN. PN 0411778-5 IS TOO SHORT AND WILL SHEAR THE COTTER PIN ALLOWING SHAFT TO COME OUT. THIS WOULD CAUSE POTENTIAL LOSS OF RUDDER CONTROL. Nov 22, 1999 · N95260 · Cessna 182S · Rudder Control SystemSDR 99ZZZX3605Starter · malfunctionedON TAKEOFF ROLL, PILOT NOTICED ALL RADIO LIGHTS FLICKERING AND VOLTMETER AT AROUND 21 VDC. PILOT ABORTED TAKEOFF AND PERFORMED RUN-UP AGAIN, OK. STARTED TAKEOFF AND HAD SAME PROBLEM. AIRCRAFT TURNED OVER TO MAINTENANCE. MAINTENANCE TECH WENT OUT TO START AAug 29, 1999 · N4193Y · Cessna 182S · Engine StarterSDR 99ZZZX3609Pump · leakingOWNER/OPERATOR REPORTED FUEL LEAK FROM UNDER COWL WHEN AIRCRAFT WAS PARKED. INSPECTION REVEALED THAT ELECTRIC BOOST PUMP WAS LEAKING OUT OVERBOARD VENT LINE. REPLACED FUEL PUMP WITH NEW PART, OPS CHKS GOOD.Aug 25, 1999 · N383ES · Cessna 182S · Fuel Boost PumpSDR 99ZZZX3181Bolt · misinstalledFOUND LEFT AND RIGHT UPPER WING STRUT ATTACH BOLTS INSTALLED BACKWARDS FACING AFT TO FORWARD. IPC SHOWS BOLTS INSTALLED FORE TO AFT.Aug 2, 1999 · N9539P · Cessna 182S · Wing, Attach FittingsSDR 99ZZZX1873Exhaust · loosePILOT NOTICED EXHAUST FUMES IN CABIN. INVESTIGATED AND FOUND NR 1 EXHAUST GASKET BLOWN OUT AND ATTACHING HARDWARE MISSING. NUTS WERE LATER LOCATED IN THE BOTTOM OF ENGINE COWLING. RIGHT HEAT SHROUD HAD SLID DOWN EXHAUST MUFFLER WHICH ALLOWED EXHAUST FUMES TApr 23, 1999 · N182EL · Cessna 182S · Engine Exhaust SystemSDR 99ZZZX2024Lock Washer · failedSB 97-78-01 C/W AT 59.2 HOURS AND NUT WAS TORQUE CHECKED. NUT AND 'STAR' TYPE LOCK WASHER FAILED TO HOLD WHEN GASKET BLEW. SUBMITTER RECOMMENDED UPGRADED GASKETS HAVE MANDATORY INSTALLATION (SB 97-78-01) AND SELF-LOCKING NUTS USED INSTEAD OF STAR-TYPE LOCK WApr 20, 1999 · N182EL · Cessna 182S · Engine Collector/Tailpipe/NozzleSDR 99ZZZX2023Nut · failedSB 97-78-01 C/W AT 59.2 HOURS AND NUT WAS TORQUE CHECKED. NUT AND 'STAR' TYPE LOCK WASHER FAILED TO HOLD WHEN GASKET BLEW. SUBMITTER RECOMMENDED UPGRADED GASKETS HAVE MANDATORY INSTALLATION (SB 97-78-01) AND SELF-LOCKING NUTS USED INSTEAD OF STAR-TYPE LOCK WApr 20, 1999 · N182EL · Cessna 182S · Engine Collector/Tailpipe/NozzleSDR 99ZZZX2022Gasket · failedAIRCRAFT TT: 145.7 HOURS. PILOT NOTICED EXHAUST FUMES IN CABIN. FOUND NR 1 EXHAUST GASKET BLOWN-OUT AND ATTACHING HARDWARE LOCATED IN BOTTOM OF COWLING. RIGHT HEAT SHROUD HAD SLID DOWN EXHAUST MUFFLER ALLOWING FUMES TO ENTER CABIN THROUGH HEATER. HARDWAREApr 20, 1999 · N182EL · Cessna 182S · Engine Collector/Tailpipe/NozzleSDR 99ZZZX1875Wire · meltedDURING AN ANNUAL INSPECTION, PITOT HEAT WIRING WAS FOUND MELTED/CHAFED INTO PITOT TUBING APPROXIMATELY .0625 INCH. THE PITOT HEAT WIRING HAS VERY LITTLE CLEARANCE FROM THE TUBING. NEED TO ENSURE WIRING IS SECURED AWAY FROM TUBING.Apr 20, 1999 · N2352B · Cessna 182S · Pitot/Static SystemSDR 99ZZZX1031Pitot · leakingPERFORMED STATIC LEAK CHECK PER SIB 98-22-02R1 AND SB KC 140-2. FOUND PITOT TUBE TO HAVE INTERNAL LEAK INSIDE OF PITOT TUBE ASSY AND HEATER ELEMENT WAS CRACKED. REPLACED PITOT TUBE ASSY. OPS CHECK NORMAL. (IPC 34-11-00, ITEM 30).Jan 27, 1999 · N784AC · Cessna 182S · Pitot/Static SystemSDR 99ZZZX1400Lock · loosePILOT AND COPILOT CONTROL ASSEMBLY SEAT LOCKS PN 1611021-01 ARE MOUNTED WITH 2 SCREWS. THESE 2 SCREWS VIBRATING LOOSE. CONTROL COULD FALL OFF CAUSING PILOT OR COPILOT NOT TO BE ABLE TO MOVE SEAT. SCREWS HAVE NO LOCKING DEVICE. PILOT AND COPILOT SEAT, PN 051Jan 7, 1999 · N820HP · Cessna 182S · Cabin Equipment/FurnishingsSDR 99ZZZX531Rudder Wheel · malfunctionedOWNER SQUAWKED AIRCRAFT WAS NOT PRODUCING ENOUGH RT RUDDER TRIM TO CENTER THE TURN COORDINATOR BALL. THIS CONDITION WAS CORRECTED TWICE TO NO AVAIL BY POPPING THE INDICATOR PIN BACK INTO ITS GROOVE. THE CONDITION WOULD RECUR DURING NEXT FLIGHT. AFTER FURTHEJan 6, 1999 · N182S · Cessna 182S · Rudder Tab Control SystemSDR 99ZZZX88Doubler · crackedAIRCRAFT IN FOR FIRST ANNUAL SINCE NEW. FOUND LOWER FIREWALL REINFORCEMENT DOUBLER CRACKED ON EACH SIDE WHERE LOWER COWL ATTACHES TO IT.Dec 14, 1998 · N9510A · Cessna 182S · Fuselage Main, BulkheadSDR 98ZZZX4124Elbow · crackedELBOW IS MANUFACTURED FROM THIN FIBERGLASS OVERLAY, AND WAS MANUFACTURED WITH A SEAM IN THE FINISHED PRODUCT. THIS ELBOW IS INSTALLED IN THE AIRCRAFT WITH A RUBBER BOOT INSTALLED OVER EACH END. THE BOOTS ARE ATTACHED WITH WORM-STYLE CLAMPS. THE FORWARD CLAMOct 28, 1998 · N72MR · Cessna 182S · Engine Air Intake System
Back to Cessna 182S