JASC 5100
Service difficulty reports · 4,244
Reports filed under 5100 · Standard Practices/Structures, newest first.
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 jasc_code = '5100' 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.
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 jasc_code = '5100' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR O9IA20131008544Insulation · misinstalledSMOKE SEEN COMING FROM IN FRONT OF DIVAN SEAT. INVESTIGATION REVEALED POOR INSULATION COVERING THE LT WING/STAB HEAT DUCT PIPE. THIS PIPE WAS REWRAPPED WITH INSULATION MATERIAL. RESULTANT CHECK FLIGHT WAS SATISFACTORY.SDR DALA1504320981Unknown · unknownFWD, MID, AFT CARGO DOORS REPAIRED IAW AA 5230-01159.SDR CALA2013100791779Fluid · leakingFLUID STREAM BENEATH TAIL CONE ON LT SIDE.SDR DALA1503399228Door Frame · unknownFUSELAGE, AFT CARGO DOORWAY, LOWER JAMB BEAM, L-28R CORROSION REPAIRED IAW ERA 398119-14.SDR A6WA2013100104210Drag Angle · crackedCRACKED DRAG ANGLE. R & R DRAG ANGLE.SDR SCNA20131010174Rub Strip · crackedNR 2 INBD UPPER RUB STRIP CRACKED. R & R UPPER RUB STRIP.SDR NE2R2013FA0000539Housing · misrepairedA CRACK SEVERAL INCHES LONG WAS FOUND IN THE STATOR HOUSING. IT HAD BEEN STOP-DRILLED AND FILLED WITH SOME TYPE OF SEALANT. IT WAS NOT INITIALLY APPARENT DUE TO SEVERAL LAYERS OF PAINT OVER THE HOUSING. THE STATOR HOUSING SHOULD HAVE BEEN REPLACED AT SOME ESDR ASMF201309009Unknown · unknownCAPTAIN REPORTED THAT DURING DESCENT, A STRONG NOISE IN COCKPIT FWD COMPARTMENT WAS HEARD. MX PERFORMED A PRESSURIZATION VALVE AND OUTFLOW VALVE EXTERIOR VISUAL INSPECTION AND BITE TO CONTROLLER NR 2 IAW AMM 21-31-00, ALL CORRECT.SDR CALA2013082190621Fluid · leakingCLEANED UP RED FLUID OFF THE BELLY FROM THE AFT CARGO DOOR TO THE REAR OF THE AIRCRAFT. FOUND RED-FLUID UNDER THS ACTUATOR, FLUID IS LEAKING OUT ACCESS PANEL BOTTOM OF TAIL & RUNNING FORWARD. CLEANED OFF RED FLUID FOUND NO LEAK OR TROUBLE. AUDIO CONTROL PANSDR CALA2013081990533Panel · damagedOTBD NR 1 SAIL TAIL DOOR HAD POPPED RIVETS ON L/E APPROX 1 FT FROM LOWER EDGE. INSTALLED PANEL.SDR CALA2013081290326Unknown · vibrationAIRFRAME VIBRATION.SDR ASOA20130806352Flange · corrodedC-CHECK, THE RT ENGINE HAD MINIOR CORROSION AT THE 12 O'CLOCK POSITION. MX REMOVED THE LIGHT CORROSION IAW SRM 51-10-03. RESTORED SURFACE PROTECTION IAW CPM 51-21-04. ALLOWABLE DAMAGE IAW EC7230-01075. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END SDR ASOA20130806351Flange · corrodedC-CHECK, THE LEFT ENGINE HAD SURFACE CORROSION AT THE 12 O'CLOCK POSITION. MX REMOVED THE SURFACE CORROSION ON REAR FLANGE IAW SRM 51-10-03. RESTORED SURFACE PROTECTION REF CPM 51-21-04. ALLOWABLE DAMAGE IAW EC 7230-01075. ALL WORK ACCOMPLISHED AND WILL BESDR CHQA20130724186Unknown · unknownCREW REPORTED AN ABNORMALLY LOUD NOISE FROM THE NOSE AREA OF THE ACFT AFTER GEAR RETRACTION. NOISE PRESENT FOR REMAINDER OF FLIGHT. ALL 3 LANDING GEAR SHOWED UP AND LOCKED AND LOWERED AS NORMAL DURING GEAR EXTENSION. LANDED WITHOUT INCIDENT. MX INSPECTED THESDR BSYR201307222052Unknown · unknownENROUTE, PILOT FELT A JOLT AND RPM FLUCTUATION. DIVERTED AND LANDED WITHOUT INCIDENT. OPENSDR UALA2013071705016Drain Mast · faultyFWD DRAIN MAST FAILED MESSAGE DISPLAYED ON CIDS PANEL WITH A CAUTION LIGHT. R & R FWD DRAIN MAST IAW MM. OPS CHECKED NORMAL.SDR DALA1504603244None · noneREFUEL APERTURE/WING ELECTRONIC BOND IDENTIFIED AS A MAJOR IAW AA 5724-01007.SDR UIEA2013071500366Indicator · missingLAV H MISSING TEMPERATURE INDICATOR ON WASTE DISPOSAL CHUTE (OUTSIDE). INSTALLED NEW TEMPERATURE INDICATOR ON WASTE DISPOSAL CHUTE (OUTSIDE) ON LAV H IAW AMM 11-35-02.SDR HNAA2013071000404None · noneAISLE EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. CYCLED SWITCH, FOUND LIGHT TO BE OPERATIONAL, OPS CHECKED GOOD.SDR HNAA2013071000403None · noneLEFT AFT EGRESS LIGHT BULB IS INOPERATIVE. CYCLED SWITCH, FOUND LIGHTS TO BE OPERATIONAL. OPS CHECKED GOOD.SDR 2013FA0000449Structure · corrodedDURING A PRELIMINARY MX INSPECTION, FOUND ACFT TO HAVE EXCESSIVE CORROSION ON AIRFRAME. MOVED THE RUDDER FULL DEFLECTION AND CONTROL ROD END ON PUSH PULL TUBE SNAPPED AT EXPOSED THREADED PORTION. FOUND SEVERAL STEEL PARTS THAT HAVE CORROSION, ALONG WITH THESDR 2013FA0000301Shaft · mismanufacturedNEW SHAFT FROM MFG IS .010 UNDER DIAMETER. PART IS USED TO COMPLY AD10-15-10.SDR DALA1503213253None · noneREFUEL APERTURE/WING ELEC BOND INSPECT, IDENTIFIED AS MAJOR IAW AA 5724-01007.SDR L7OA201305142002Unknown · unknownDURING TAKE OFF ROLL RT WING DIP DOWN. PILOT VERBALLY REPORTED LOUD THUMP/SUSPECTED TIRE FAILURE. INSPECTED RT LANDING GEAR STRUT, BRAKE AND MAIN WHEEL. FOUND NO DEFECTS, COULD NOT DUPLICATE PROBLEM DONE IAW AMM 32-00-00-201 & 12-00-00-201.SDR UALA2013050203067Unknown · unknownLOUD FLAPPING NOISE AT L2 DOOR. INSPECTED DOOR, SEAL AND AND FRAME. NO DISCREPANCIES NOTED AND NO EVIDENCE OF ANY OBJECT FLAPPING ON THE EXTERIOR OF THE FUSELAGE. SUSPECT NOISE IS ASSOCIATED WITH BLOWN APU DUCT THAT CAUSED DEFINING NOISE IN AFT GALLEY. THE SDR 2013FA0000249Filter · failedFOUND SEAM IN FILTER ELEMENT SEPARATED. NO TEARING OF THE MATERIAL WAS EVIDENT.SDR UALA2013031301484Circuit Card · unknownCPU CARD HAS AN INTERNAL FAULT, CMC MESSAGE ACTIVE. REPLACED CPU CARD IN P110 PANEL.SDR ASAA2013021693910None · noneHF NR 1 INOPERATIVE. BITE TEST NR 1 HF TRANSCEIVER NO FAULTS NOTED REF MM 23-11-00-710-801, PERFORMED HF COMM SYS TEST 23-11-00-730-801. OPS CK GOOD NO HISTORY 90 DAYS.SDR CA130215013Rod · damaged(CAN) VPS 20.03, REQUIRES THAT FPI BE PERFORMED BEFORE ANY SURFACE TREATMENT WHICH COULD RESULT IN OBSCURING OF CRACKS. VPS 20.03 DOES ALLOW FPI TO BE PERFORMED AFTER METAL SMEARING OPERATIONS PROVIDED THE PARTS ARE DEOXIDIZE ETCHED PRIOR TO FPI TO REMOVE A MSDR 2013FA0000082Channel · corrodedDURING REMOVAL OF INSULATION PANEL CHANNEL WAS FOUND WITH RUST AND WAS TREATED AND REPAIRED IAW EO PA-28-181.SDR 2013F00059Unknown · unknownPASSENGERS AND F/A HAVE REPORTED A LOUD SQUEAL IN THE AFT PORTION OF THE ACFT.SDR DXTA2013020605272Unknown · vibrationFIVE SECONDS AFTER APPLICATION OF TAKEOFF POWER, MULTIPLE LOUD NOISES WITH THE ENTIRE ACFT SHAKING AND VIBRATIONS WHERE FELT.SDR TRBA20130201001Unknown · unknownDURING TAKEOFF ROLL, FELT AND HEARD A NOISE AROUND THE NOSE GEAR AREA, ABORTED TAKEOFF AND TAXIED TO THE RAMP. NO VISIBLE DAMAGE WAS FOUND ANY WHERE ON THE ACFT. TWO PASSENGERS SEATED ON SEATS 10C & 10D REPORTED SEEING A SMALL BALL OF FIRE JUST BEFORE THE ABSDR 2013FA0000191Shutoff Valve · failedDURING ELECTRICAL CONNECTION OF THE VALVE TO THE BENCH TEST, OPEN POSITION IS INDICATED ON THE BENCH TEST WHILE THE VALVE IS NOT USED AND IS ON CLOSED POSITION.SDR SIMA20130121008Unknown · unknownFLIGHT 2910, CREW REPORTED AT 30,000 FT, HEARD A LOUD BANG. ALL INSTURMENT INDICATIONS NORMAL & A SMOOTH CRUISE CONDITION NOTED. UNABLE TO POSITIVELY IDENTIFY NOISE & SUSPECTED THAT A TIRE MAY HAVE BURST IN THE WHEEL WELL. DECLARED AN EMERGENCY & PERFORMESDR ASMF201303002Unknown · vibratesTHE ACFT TO LANDING DUE TO A STRONG NOISE AND VIBRATION IN THE NLG AND RT TREND. MX PERSONNEL PERFORMED A NLG REVISION IAW MM 32-00-00, NO DETECTING FAILURE. AS A PRECAUTIONARY ACTION, IT WAS PERFORMED SERVICE TO THE NLG SHOCK STRUT IAW MM 12-15-41, ALL CORRECSDR ASAA2012121993502Unknown · unknownOFFSET LIGHT ON CAPTS FMC CONTROL PANEL WILL NOT DIM. TESTED CAPTS FMC IAW MM 34-61-00 FMC, LCD CDU, LAMP TEST. SYS OP CHECKED GOOD, NO HISTORY IN THE LAST 60 DAYS.SDR YYFA20121212001Unknown · unknownWHEN OPENING AFT STAIRS A PUDDLE OF FUEL ON THE GROUND.SDR ASAA2012112893383Unknown · unknownF/A REPORT EMERGENCY EXIT LIGHTS CAME ON FOR ABOUT 5 SECONDS. AFTER ENGINE START TURNING NR 1 GENERATOR ON AND DURING LANDING ROLL OUT WITH THRUST REVERSERS OUT. PERFORMED EMERGENCY LIGHT OPS TEST IAW 33-51-00, GROUND RAN NR 1 AND NR 2 ENGINES IAW 71-00-00,SDR LCFA2012F00259Bearing Support · brokenROD END BEARING, FOUND BROKEN AFTER COMPLETION OF FLIGHT, ON POST INSPECTION.SDR SWIA201232293Axle · corrodedCORROSION FOUND NR 1, 2, 3, 4 AXLE ROOT. (C-CHECK) REMOVED CORROSION IAW REO.SDR CA121102007Pressure Switch · unknown(CAN) CAUTION ANNUNCIATOR LIGHT FLASHING ON & OFF WITH SYSTEM SELECTED OFF.SDR DALA1503429228Skin · unknownHS UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.SDR ASAA2012081392714Unknown · leakingFOUND OIL LEAKING FROM MIDDLE DRAIN OF APU IAW 05-60-00-280-801CSTEP A.(2) (C) APU REQS REPLACEMENT. BLACK LIGHT TEST OF SWABS FROM LOAD COMPRESSOR DRAIN DID NOT PROVIDE CONCLUSIVE EVIDENCE OF OIL CONTAMINATION. RAN APU WITH RT PACK ON FOR 30 MINUTES. NO ASDR UALA2012080604207Strap · brokenCOCKPIT TIE DOWN STRAP BROKEN. SUPPLEMENTAL DATA UPDATE, REPLACED STRAP.SDR 2012FA0000630Unknown · fireACFT WAS COMPLETELY DESTROYED AS A RESULT OF AN IN-FLIGHT FIRE AND RESULTING POST CRASH FIRE. THE FIRE APPEARS TO HAVE STARTED IN THE COCKPIT FROM AN UNKNOWN IGNITION SOURCE AND FED BY GASOLINE.SDR IU6R201206123572Housing · crackedVALVE BROKEN AND CRACKED, PIN HOLE FOUND ON HOUSING.SDR DALA1503519228Skin · unknownHORIZONTAL STABILIZER RT UPPER AFT SKIN FASTENER HOLES WITH SHORT E/D & BUSHING REPAIRS IAW ERA 491786-14, LOG 0613380, 0938307.SDR DALA1503499228Skin · unknownFUSLAGE, SKIN, STA 1475 BETWEEN L1-L2L & L1-L2R REPAIRED IAW ERA 491769-14, LOG 0613380,0938307.SDR CA120822016Panel · bulged(CAN) LEFT INBD TKS PANEL BULGED.
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