Cessna 172N

Service difficulty reports · 627

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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 = '172N'
  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 CA080908008Cylinder · separated(CAN) ACFT WAS CLIMBING OUT ON A TRAINING FLIGHT. SHORTLY AFTER HEARD A LOUD BANG AND RPM DROPPED TO APPROX 1200. TURNED BACK AND LANDED SAFELY FOUND THE NR1 CYL HEAD SEPARATED FROM THE BARREL WITH APPROX 1 INCH OF BARREL EXPOSED PAST THE CYLINDER FINS. NR1 INSep 6, 2008 · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA081008001Fork · cracked(CAN) DURING A ROUTINE OPERATION, NR 2 INSP, A SUSPECTED CRACK WAS FOUND ON NLG FORK. EDDY CURRENT REVEALED A LARGE DEFLECTION IN THE SUSPECTED AREA. SUBSEQUENTLY THE INSP WAS CONDUCTED ON THE OPPOSITE SIDE OF THE NLG FORK WITH THE SAME RESULTS. ADDITIONALLY Aug 18, 2008 · Cessna 172N · Nose/Tail Landing GearSDR CA080819001Cable Assy · broken(CAN) ON AUGUST 14, 2008, PILOT REPORTED "PILOT SEAT DOESN`T MOVE BACK, COULD NOT GET OUT". INVESTIGATION BY MAINT FOUND THAT THE CABLE ASSEMBLY FOR THE PILOT SEAT SECONDARY SEAT STOP HAD FAILED PREVENTING THE INERTIAL REEL FROM RELEASING TO ALLOW THE SEAT TO Aug 14, 2008 · Cessna 172N · Flight Compartment EquipmentSDR CA080812001Switch · faulty(CAN) ON JULY 16, 2008 AT APPROX. 13:00, PILOT REPORTED SMOKE IN COCKPIT AND PLASTIC BURNING SMELL. ACFT ELECTRONICS WERE SHUTDOWN AND SMOKE DISSIPATED. DURING POST FLIGHT INSP, MAINT DISCOVERED A FAULTY STROBE LIGHT SWITCH, AND REPLACED THE DEFECTIVE SWITCH.Jul 16, 2008 · Cessna 172N · Exterior LightingSDR CA080613004Bolt · misinstalled(CAN) LEFT RUDDER PEDAL SYSTEM INSPECTED TO VERIFY CLEARANCE BETWEEN THE BOLT AND NUT HOLDING THE BRAKE BELLCRANK LOCATED BESIDE THE RIGHT RUDDER PEDAL ARM BAR ON THE PILOT SIDE AND THE NOSE GEAR STEERING ARM TUBE ATTACHMENT. BOLT WASHER AND NUT REPOSITIONED TJun 5, 2008 · Cessna 172N · Landing Gear Steering SystemSDR 2008FA0000366Arm · brokenBOLT CONNECTING CARBURETOR THROTTLE ARM TO THROTTLE CABLE FAILED RESULTING IN THROTTLE STICKING OPEN. PILOT PLACED MIXTURE CONTROL IN IDLE CUTOFF POSITION AND ATTEMPTED TO GLIDE TO RUNWAY AT AIRPORT. AIRCRAFT IMPACTED POWER LINES SHORT OF RUNWAY. BOLT WAS NOT May 24, 2008 · N75528 · Cessna 172N · Power LeverSDR CA080404009Cable · out of adjustFLIGHT CREW DISCREPANCY, PILOTS SEAT DOES NOT SLIDE BACK INTERMITTENTLY. SEAT REMOVED AND VISUALLY INSPECTED. REEL ASSEMBLY CABLE ADJUSTED AND SEAT FUNCTION TESTED WITH NO DEFECTS FOUND. SEVERAL AIRCRAFT IN OUR FLEET OF CESSNA 100 SERIES AIRCRAFT HAVE EXPERApr 4, 2008 · Cessna 172N · Flight Compartment EquipmentSDR CA080331002Cable Assy · cracked(CAN) DURING INSTALLATION OF SERVICE KIT SK210-175 - SECONDARY SEAT STOP, IT WAS FOUND THAT THE THREADS ON THE HOUSING FOR THE ADJUSTMENT CABLE WERE CRACKED. (TC NR 20080331002)Mar 12, 2008 · Cessna 172N · Flight Compartment EquipmentSDR 2007FA0000823Rotor · failedPILOT DEPARTED ON A VFR, DAY FLIGHT. DURING THE CLIMB FROM DEPARTURE, THE PILOT NOTICED A SLIGHT ENGINE ROUGHNESS THAT LASTED ONLY A SECOND. THE ENGINE SMOOTHED OUT UNTIL THE AC WAS LEVELED OUT AT CRUISE ALTITUDE AND CRUISE POWER SETTINGS THE ENGINE BEGAN RUAug 24, 2007 · N733XN · Cessna 172N · Magneto/DistributorSDR CA070802005Bulkhead · cracked(CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. CRACKS WERE FOUND FORMING PARALLEL FROM THE PROP BOLT HEAD CONTACT SURFACE ON (3) OF THE (6) HOLES. HAVE TO LOOK VERY CAREFULLY AS THEJul 26, 2007 · Cessna 172N · Propeller Spinner SectionSDR CA070802006Cylinder · cracked(CAN) (2) CRACKS FOUND DURING ENGINE ON-CONDITION INSPECTION. CRACKS START FROM BOTTOM SPARK PLUG HOLE AND EACH CRACK GOES TO A VALVE SEAT. THESE CRACKS WERE NOT DETECTED DURING DIFFERENTIAL PRESSURE INSPECTION OR LEAK TEST. INTERNAL BORESCOPE INSP WAS DETECTIJul 24, 2007 · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA070807007Control Cable · worn(CAN) ONCE AIRCRAFT REACHED 5000 FT THE PILOT COMMENCED CRUISE CHECKLIST, LEANED THE MIXTURE OF THE ENGINE WHEN THE POWER REDUCED TO IDLE. PILOT COULD NOT REGAIN ENGINE POWER AND MADE THE DECISION TO LAND IN A FIELD APPROX 3 MILES NE OF AIRPORT. UPON LANDING Jul 15, 2007 · Cessna 172N · Fuel Control/Reciprocating EnginesSDR CA070717016Elt · intermittent(CAN) EARLY ACTIVATION. SELF-ACTIVATION REPORTED TWICE. (TC NR 20070717016)Jul 5, 2007 · Cessna 172N · Emergency Locator BeaconSDR CA070717011Arm · bent(CAN) ON ROLL OUT AFTER LANDING THE RT MAIN LANDING GEAR COLLAPSED. INVESTIGATION FOUND THAT THE ACTUATING CYLINDER BENT (P/N D68194-A-4). FURTHER INVESTIGATION FOUND THE RETRACT ARM P/N 21A05000-016 HAD WORN ELONGATED BOLT HOLES NOT ALLOWING A DOWN LOCK OVER Jun 21, 2007 · Cessna 172N · Main Landing Gear Strut/Axle/TruckSDR CA070622002Engine · leaking(CAN) OIL LEAKING FROM FRONT LT AREA OF ENGINE. (TC NR 20070622002)Jun 20, 2007 · Cessna 172N · Reciprocating Engine Oil SystemSDR CA070608005Elt · inoperative(CAN) WHEN TESTING ELT FOR THE REQUIREMENT OF CAR 571 APPENDIX G FOUND G SWITCH INOPERATIVE. UNIT BEING RETURNED TO MFG FOR REPAIR. (TC NR 20070608005)Jun 8, 2007 · Cessna 172N · Emergency Locator BeaconSDR CA070625001Cylinder · cracked(CAN) INSTRUCTOR RETURNED FROM A FLIGHT WHERE HE EXPERIENCED A ROUGH ENGINE AND LOSS OF POWER FOR A FEW MOMENTS, AFTER WHICH THE ENGINE RAN NORMALLY AGAIN. WHEN MAINTENANCE REMOVED THE COWLING TO CHECK OVER THE ENGINE, A LOT OF OIL WAS NOTICED IN THE COWL, FUJun 6, 2007 · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA070517001Adapter · cracked(CAN) DURING GROUND RUN AFTER OVERHAUL, AN OIL LEAK WAS NOTICED ORIGINATING FROM THE LOWER RT ATTACH POINT OF THE OIL FILTER ADAPTER. UPON CLOSE VISUAL INSPECTION A CRACK WAS FOUND IN THE RADIUS OF THE LOWER RT FLANGE. UNIT WAS REPLACED AND LEAK CHECKED. (TCMay 15, 2007 · Cessna 172N · Engine Oil Distribution (Airframe Furnished)SDR M2L2007F00002Drive Gear · brokenDURING AN ENGINE START, THE STARTER BENDIX DRIVE GEAR BROKE. THIS IN TURN LOCKED THE RING GEAR WHICH LOCKS PROP AND ENGINE. (K)May 6, 2007 · N737MY · Cessna 172N · Engine StarterSDR CA070514009Gear · improper part(CAN) THE GEARS ON THE STARTER DID NOT MESH WITH THE RING GEAR FROM THE ENGINE CAUSING THE TEETH TO RIDE UP AND HIT THE TOP OF THE OPPOSITE GEAR. THIS CAUSED THE ENGINE AND STARTER TO LOCK UP. (TC NR 20070514009)Apr 26, 2007 · Cessna 172N · Engine StarterSDR CA070803001Flap Track · separated(CAN) DURING HARD MANEUVERING WITH FLAPS DOWN, A LOUD BANG WAS HEARD BY THE PILOTS WHO NOTICED THE LT FLAP BEING PUSHED BACK AT A STRANGE ANGLE. THE FLAPS WERE LEFT IN THE DOWN POSITION AND THE AIRCRAFT WAS RETURNED WITHOUT INCIDENT. UPON INVESTIGATION THE LApr 20, 2007 · Cessna 172N · Trailing Edge FlapsSDR 2007FA0000389Cylinder · crackedCRACK FROM EXH STUD AROUND CYLINDER TO UPPER SPARK PLUG. (K)Apr 20, 2007 · N4801D · Cessna 172N · Reciprocating Engine Cylinder SectionSDR 2007FA0000333Rocker · brokenTHE STAMPED EXHAUST STEEL ROCKER ARM WAS FOUND BROKEN THROUGH AT PUSH ROD, AND THE INTAKE ROCKER ARM WAS CRACKED, AND THE PUSH ROD WAS BENT BADLY. THE ENGINE HAD 120 HR TSO AND NEW FACTORY CYLIDERS WERE INSTALLED. (K)Apr 6, 2007 · N2994E · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA070313001Lifter · unlocked(CAN) DURING THE REAMING OF A STICKY EXHAUST VALVE GUIDE IN CYLINDER NR 4, IT WAS FOUND THAT THE NR 4 CYLINDER INTAKE HYDRAULIC LIFTER HAD LOST ITS SNAP RING. THE WEAR PATTERN SHOWED THAT THE SNAP RING HAD MIGRATED ALONG BETWEEN THE PUSHROD AND THE SHROUD TUBMar 12, 2007 · Cessna 172N · Reciprocating Engine Cylinder SectionSDR 2007FA0000189Control Cable · frayedPILOT REPORTED EXCESSIVE MOVEMENT IN LT FLAP DURING PRE-FLIGHT WALK AROUND OF AIRCRAFT. INITIAL INVESTIGATION BY MAINTENANCE PERSONNEL CONFIRMED FINDINGS. MAINTENANCE PERSONNEL DISCOVERED THAT CABLE P/N 0510105-93 HAD MULTIPLE BROKEN STRANDS/FRAYING NEAR THEFeb 26, 2007 · N31SZ · Cessna 172N · Trailing Edge Flap Control SystemSDR CA070215004Alternator · malfunctioned(CAN) ON CLIMB OUT A LOW VOLTAGE LIGHT INDICATION. PILOT RECYCLED ALTERNATOR, LOW VOLTAGE INDICATION WAS NOT CORRECTED AND PILOT RETURNED FOR LANDING (TC NR 20070215004)Feb 10, 2007 · Cessna 172N · DC Generator-AlternatorSDR 2007FA0000063Skin · mismanufacturedDURING AN RECEIVING INSPECTION OF NEW RT OB LEADING EDGE SKIN, IT WAS FOUND TO HAVE BEEN DRILLED UP INCORRECTLY SINCE NONE OF THE NOSE RIBS WOULD LINE UP AND THE SET UP WOULD HAVE LT INSUFFICIENT EDGE DISTANCE ON THE LOWER MAIN WING SPAR RIVET LINE. THIS IS ZJan 10, 2007 · Cessna 172N · Wing, Plate/SkinSDR 2007FA0000122Nut · looseTHE NR 3 CYLINDER EXHAUST ROCKER ARM RETAINING NUT BECAME LOOSE, REDUCING LIFT ON THE EXHAUST VALVE, NOT ALLOWING SUFFICIENT AIR TO EXIT THE CYLINDER. PRESSURE IN THE CYLINDER EXCEDED THE STRENGTH OF THE INTAKE VALVE SYSTEM TO OPEN, CAUSING THE INTAKE PUSHRODJan 5, 2007 · N5123E · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA061218019Bulkhead · cracked(CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. THE (FORWARD SPINNER BULKHEAD) IS CRACKED AGAIN WITH LESS THEN 50 HOURS TSN, CRACKS RADIATING .2500 TO 1 INCH FROM 3 OF THE 6 HOLES. Dec 18, 2006 · Cessna 172N · Propeller Spinner SectionSDR CA061123005Flapper Valve · worn(CAN) DURING PROGRESSIVE CARE OPERATION NR 2, INSP OF THE CARBURETOR HEAT BOX (P/N 05521644) REVEALED THAT THE 2 ALUMINUM RIVETS THAT HOLD THE FLAPPER DOOR TO THE ACTUATOR SHAFT WERE VERY CLOSE TO SHEARING OFF. IF THE ALUMINUM RIVETS DID SHEAR, AND THE AC WAS Nov 21, 2006 · Cessna 172N · Fuel Control/Reciprocating EnginesSDR RTE2007F00000Bulkhead · crackedDURING ROUTINE PHASE INSPECTION, FOUND FWD PROP BULKHEAD ASSY TO BE CRACKED IN SEVERAL PLACES, ALL NEAR THE BOLT HOLES AND NEARBY RADIUS. HAVE FOUND SEVERAL IN THE SAME CONDITION ON THIS AND OTHER AC. SUSPECT EITHER IMPROPER HEAT TREATING DURING MFG AND OR INov 15, 2006 · N731QQ · Cessna 172N · Propeller Spinner SectionSDR 2006FA0001099Wire · brokenALTERNATOR FAILED AND MAIN POWER BUS FEED WIRE BROKEN FROM ALTERNATOR. TERMINAL ENDS, PROBABLY DUE TO VERY TIGHT AREA AND VIBRATION. PREVENTION MIGHT BE TO ENLARGE AREA WHERE WIRES PASS THRU BAFFLING TO LIGHTEN VIBRATION AND STRESS ON WIRES BEING BENT TO FITNov 7, 2006 · N2059E · Cessna 172N · Electrical Power System WiringSDR 2006FA0001098Primer Line · leakingNOTED FUEL SPRAYING OUT WHEN TRYING TO PRIME ENGINE FOR START. FOUND LINE CRACKING AT WELDED TIP AREA. ON PRIMER LINE, WHERE IT ATTACHES TO CYLINDER FITTING. THIS IS A BAD TYPE END ON LINE. SUGGEST MORE SECURITY OF PRIMER LINES AT MORE PLACES, TO MINIMIZE Nov 7, 2006 · N2059E · Cessna 172N · Aircraft Fuel Distribution SystemSDR CA061031002Bulkhead · cracked(CAN) BULKHEAD WAS INSTALLED IAW CESSNA SK172-156A INSTRUCTIONS. BULKHEAD HAS CRACKS CURVING AROUND BOLT HOLES ABOUT HALF INCH AWAY FROM THE HOLE EDGE AT THE INNER BEND RADIUS. NOTE: THIS IS THE FOURTH OR FIFTH IDENTICALLY CRACKED BULK HEAD FOUND ON AS MANY OOct 27, 2006 · Cessna 172N · Propeller Hub SectionSDR 2006FA0000897Cylinder · separatedPILOT EXPERIENCED A NOTICEABLE POP SOUND IN ENGINE COMPARTMENT FOLLOWED BY ROUGHNESS. SOON AFTER THE ENGINE OIL PRESSURE STARTED TO DETERIORATE AND PILOT ELECTED TO SHUTDOWN ENGINE AND STOPPED PROPELLER FROM TURNING BY PUTTING AIRCRAFT IN NOSE HIGH ATTITUDE. Aug 25, 2006 · N733EN · Cessna 172N · Reciprocating Engine Cylinder SectionSDR CA060804008Cylinder Head · cracked(CAN) ALL 4 CYLINDERS HAVE CRACKS THAT BEGIN AT THE INNER MOST EXHAUST FLANGE STUD AND MOVING TO THE EXHAUST VALVE SEAT, THEN 180 DEGREES ACROSS THE EXHAUST VALVE SEAT TO THE UPPER SPARK PLUG HOLE. SN. E36-10511 E36-10244 E36-10426 E36-10496 NOTE: THIS MAKESAug 1, 2006 · Cessna 172N · Reciprocating Engine Cylinder SectionSDR 2007FA0000025Seat Back · brokenINSPECTED SEATS IAW AD 87-20-03R2 FOUND PILOTS SEAT BOTTOM ASSY BROKEN AT LEFT FWD ATTACH POINT AND RT FWD CRACKED. (K)Jul 25, 2006 · N733BE · Cessna 172N · Flight Compartment EquipmentSDR CA060711008Bulkhead · cracked(CAN) THE SPINNER FORWARD BULKHEAD WAS INSTALLED NEW ONE YEAR EARLIER, WITH THE NEW HEAVIER MATERIAL SPINNER IAW SNL03-9 (ALTERNATE PROPELLER SPINNER INSTALATION) THE FWD BULKHEAD HAS CRACKS OF APPROXIMATLY 1.5 INCHES EACH COMING ACROSS EACH PROP BOLT HOLE ATJul 10, 2006 · Cessna 172N · Propeller Spinner SectionSDR CA060530006Engine · failed(CAN) ON TAKE-OFF THE AIRCRAFT WOULD NOT DEVELOP FULL POWER SO THE PILOT ABORTED THE TAKE-OFF. AIRCRAFT WAS BROUGHT INTO THE HANGER AND AME'S REMOVED COWLING AND REMOVED VALVE COVERS. IT WAS NOTED THAT ALL THE CLEARANCES ON THE VALVES WERE TOO LOOSE. AIRCRAFTMay 25, 2006 · Cessna 172N · Engine (Reciprocating)SDR 2006FA0000521Crankcase · crackedDURING A 100 HR INSPECTION, AN OIL LEAK WAS NOTED AROUND THE L/H FORWARD CRANKCASE AROUND THE UPPER CRANKCASE BOLT (PN 6-34A WITH PN LW-11866 NUT). THE ENGINE WAS CLEANED AND A DYE PENETRANT INSPECTION PERFORMED. A CRACK ROUGHLY 4 INCHES LONG WAS FOUND RUNNIMay 18, 2006 · N1962F · Cessna 172N · Reciprocating Engine Power SectionSDR 2006FA0000551Bulkhead · crackedDURING AN ANNUAL INSPECTION OF THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND 3 OF THE BOLT HOLES OF THE FORWARD SPINNER BULKHEAD. THE PROBLEM CAUSE IS THAT THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS BEING TIGHTENED AGAINST THE PROPELLER HUBMay 17, 2006 · N123GJ · Cessna 172N · Propeller Spinner SectionSDR 2006FA0000548Bulkhead · crackedDURING AN ANNUAL INSPECTION FO THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND 3 OF THE BOLT HOLWS OD THE FORWARD SPINNER BULKHEAD. THE PROBABLE CAUSE IS THAT THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS BEING TIGHTENED AGAINST THE PROPELLER HUMay 17, 2006 · N123GJ · Cessna 172N · Propeller Spinner SectionSDR CA060509002Switch · defective(CAN) PILOT WAS IN CRUISE WITH LANDING LIGHT ON, WHEN SHE SMELLED SMOKE AND NOTICED SMOKE COMING FROM LANDING LIGHT SWITCH. SMOKE STOPPED WHEN SWITCH TURNED OFF AND PILOT SQUAWKED 7700 FOR HELP AND SHE WAS ADVISED TO LAND. AGAIN IT WAS CONFIRMED THAT THE SWITCApr 28, 2006 · Cessna 172N · Exterior LightingSDR P742006F00000Clamp · defectiveTHE DEFECT INVOLVES THE CLAMP FOR THE COLLECTER TO TAIL PIPE SLIP JOINT. THE ALIGNMENT PIN OR THE CLAMP IS 40 PERCENT WORE THROUGH AT 100 HOURS OF OPERATION. (K)Apr 28, 2006 · N6391J · Cessna 172N · Engine Collector/Tailpipe/NozzleSDR 2006FA0000429Switch · stuckFLAP UP LIMIT SWITCH STUCK IN THE OPEN POSITION. (K)Apr 7, 2006 · N4668G · Cessna 172N · Trailing Edge Flap Control SystemSDR CA060406001Relay · defectiveRELAY IS USED TO POWER THE RADIO-NAVIGATION SYSTEM. ON A TRAINING FLIGHT INSTRUMENT APPROACH, SMOKE WAS NOTICED UNDER THE INSTRUMENT PANEL. THE APPROACH WAS ABORTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CARRIED OUT A DETAILED INSPECMar 29, 2006 · Cessna 172N · UHF Communications SystemSDR 2006FA0000381Strut · brokenLANDING GEAR BROKE JUST OUTSIDE OF THE GEAR BOLT. THE FACE OF THE CRACKED AREA APPEARS TO HAVE RUST ON IT THAT COULD INDICATE A PREVIOUS CRACK. (NE01200603823) (K)Mar 24, 2006 · N739YA · Cessna 172N · Main Landing Gear Strut/Axle/TruckSDR 2006FA0000462Bulkhead · crackedDURING ROUTINE PHASE INSPECTION FWD PROP BULKHEAD FOUND TO BE CRACKED NEAR SEVERAL MOUNTING BOLT HOLES. HAVE SEEN THIS SEVERAL TIMES BEFORE. SUSPECT DEFECT IN CURRENT MFG PROCESS. (K)Mar 16, 2006 · N734QQ · Cessna 172N · Propeller Spinner SectionSDR 2006FA0000241Harness · mismanufacturedTHE AIRCRAFT HAD MAGNETO LEADS THAT NEEDED TO BE REPLACED. A NEW HARNESS SET WAS RECEIVED AND WAS INSTALLED ON THE ENGINE. THE ENGINE RAN POORLY. FOUND (T-4). ALSO NOTED THAT THE SHIELD ON NR 1 BOTTOM WIRE HAD BEEN CUT DURING MANUFACTURER AND THE SHIELD WAMar 13, 2006 · N5228E · Cessna 172N · Ignition Harness (Distribution)SDR CA060224009Seat · crackedWHILE DOING 100HR INSPECTION ON AIRCRAFT AME WAS DOING THE SEAT RAIL INSPECTION NOTICED PILOTS SEAT WAS LOOSE WHEN HE MOVED IT BACK. ON FURTHER INSPECTION OF THE SEAT IT WAS DISCOVERED THAT ONE OF THE ATTACHMENT LEGS USED TO ATTACH THE SEAT TO THE PEDESTAL WASFeb 24, 2006 · Cessna 172N · Flight Compartment Equipment
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