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 COEA0501753Unknown · unknownON TAKEOFF THE AIRCRAFT WOULD NOT GAIN ALTITUDE. AIRCRAFT CLEARED THE AIRPORT PROPERTY AND IMPACTED THE GROUND JUST AFTER THE FENCE. (K)SDR DXTA200501156None · noneCLEAR AIR TURBULENCE, NO WARNING, 16000 FT LEVEL FLIGHT, ABOUT 260 KTS, AUTOPILOT DISENGAGED, ATTITUDE REMAINED LEVEL, ALTITUDE +/- ABOUT 100, FORCED VIOLENTLY AGAINST SEAT BELTS, CREW HIT CEILING, TOILET SEAT FLIPPED INTO AISLE, EVENT LASTED LESS THAN 5 SECONSDR 05FDEA04352Repair · unknownRT HORIZONTAL STAB CENTER SECTION ON SKIN PANEL UPPER AFT SIDE FOUND 1 REPAIR DOUBLER DIM 16" BY 11" BEWTEEN STA XE 72 AND STA XE 83. STRIPPED PAINT IAW SRM 51-21-01 PAR 32C VOL 2. PERFORMED NDT INSPECTION IAW NDT SPM 06-10-01.006 AND 04-00-06 REPAIR PREVISDR 2006FA0000137Nut · failedNUT, PN MS21042L3 (PN130909N29) FAILED AND TAPERED PIN PN AN 38629A CAME OUT OF ADAPTER NP 1158110473 IN LT WING ROOT. THE ADAPTER DISENGAGED FROM THE TORQUE TUBE SHAFT PN 1018100211, THE LT MAIN GEAR COULD NOT LOCK DOWN. THE NUT HAD ONLY 160.4 HOURS ON IT FSDR 05FDEA04336None · noneFOUND PREVIOUSLY REPAIR AT RT WING NR 6 KRUEGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, NUMBERS OF FASTENER AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIEDSDR 05FDEA04309None · noneLT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.25 INCHES BY 1.75 INCHES AT STA XORS 532. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3.SDR 050143850Bolt · corrodedDURING REMOVAL OF PROP TO ACCESS BELTS, FOUND ONE PROP BOLT SEVERELY PITTED. ONLY THE ONE BOLT SHOWED ANY SIGNS OF CORROSION. BOLT HAD ONLY 350 HOURS FROM ORIGINAL FACTORY INSTALL. BOLT WAS REPLACED AND DIGITAL PHOTO'S WERE SUPPLIED MFG TECH SERVICES.SDR AU510001766Hinge Pin · loose(AUS) 103VU PANEL HINGE PIN LOOSE. NO CONTACT WITH ADJACENT ELECTRICAL HARNESS. FOUND DURING INSPECTION IAW AD/A320/175.(AD/SB DESC: AD/A320/175 ) (CASA NR 510001766)SDR AU510001551Screw · missingLT THRUST REVERSE LEVER COULD BE LIFTED WITH FORWARD THRUST LEVER OFF IDLE. THE THRUST LEVER TOP COVERS WERE REMOVED AND IT WAS FOUND THAT THE AFT TWO FASTENERS OF THE LEFT THRUST LEVER BAULK RAIL INSTALLATION WERE MISSING. THIS ALLOWED THE LEFT THRUST REVERSDR 507512092005Insulation · odorACRID ODOR FROM LEFT PILLAR BETWEEN LT WINDSHIELD AND SIDE WINDOW.SDR 2006FA0000006Valve · out of rigTHE NEW VALVE RECEIVED FROM THE MFG WAS INTERNALLY CLOCKED INCORRECTLY. AFTER INSTALLATION, NO FUEL WAS AVAILABLE FROM EITHER THE ON OR CROSSFEED PORTS. AFTER MALVE REMOVAL, IT WAS CONFIRMED THAT THE VALVE REMAINED IN THE OFF POSITION REGARDLESS OF MOVMENT TSDR DHL2005803546Doubler · crackedNR 2 ACCESS DOOR FRAME INTERNAL DOUBLER 0.75" CRACKED WORN & BROKEN (STA -156.000 TO -165.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12/06/05, DWG AA33-53-R09 REV IR DATE 11/22/05 REMOVED LT/RT NOSE AIR SCOOP IAW SRM 51-3-0. REMOVED EXISTING EXTERSDR 2005FA0001576Manual · incorrectTHIS ENG MODEL HAS BEEN INSTALLED ON THIS AC. FG OAW TRAD STC SA02238AT. THIS STC HAS NO REFERENCES FOR A GROUND PWR ASSURANCE RUNS. NO GRAPHS ARE AVAILABLE THROUGH STC TO CHART ENG PARAMETERS FOR ACCEPTABLE GROUND PERFORMANCE DATA ON THIS INSTALLATION. IT SDR 2005FA0001629Grip · crackedCRACK INDICATION REVEALED AT THE 8TH THREAD IB FROM END. INSPECTION METHOD: EDDY CURRENT. (K)SDR 2005FA0001627Link · crackedCRACK INDICATION REVEALED TRANSVERSE BETWEEN HOLES. INSPECTION METHOD: FLOURESCENT PENETRANT. (K)SDR 2005FA0001565Gear · unknownGEARSDR CA051125005Clamp · unsecure(CAN) DURING A ROUTINE PHASE CHECK A CLAMP WAS FOUND UNSECURED IN THE EE BAY JUST ABOVE THE SHIP BATTERY. CLAMP REMOVED. A FLEET CAMPAIGN IS IN PROGRESS TO CHECK FOR FOD IN THE EE BAY.SDR KBM2005F00358Switch · inoperativePSI SWITCH INOPERATIVE, REMOVED AND REPLACED. (K)SDR 05FDEA03861Insulation · burnedIN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERELY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC DUCT. REPLACED INSULATION BLANKETS PER REF: MM 25-28-00. NEED LEAK CHECK 97846. LEAK CHECKED #1 SYSTEM PNEUMATIC DUCT AT CASDR VNAA0511010Unknown · noneTHE AIRCRAFT STRUCK A BIRD ON TAKEOFF ROLL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IAW CRJ700 AMM 05-51-25-210-801-A01. NO DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR KBM2005F00340Hose · leakingHOSE- UNIT IS SWOLLEN AND LEAKING, REMOVED AND REPLACED. (K)SDR VNAA0511008Unknown · noneTHE CREW REPORTED ENCOUNTERING SEVERE TURBULENCE DURING DESCENT BETWEEN FL230 AND FL210. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED AN EXTREME TURBULENCE / MANEUVER INSPECTION IAW CRJ200 AMM 05-51-03-210-801. NO DEFECTS WERE FOUND. THE AIRCSDR CA051104008Washer · damaged(CAN) PARTIAL POWER LOSS IN-FLIGHT. UPON INSPECTION, CONTRACT AMO FOUND A WASHER LODGED UNDER AN INTAKE AND EXHAUST VALVE, CAUSING ZERO COMPRESSION. ON DISASSEMBLY, SCREW FOUND IN SCAT HOSE LEADING FROM CARB HEAT INTAKE PORT TO HEAT MUFF. LIKELY SCREW AND WASSDR ASAA0540523Repair · temporaryYXX - TEMP REPAIR AT STRINGER 25 LEFT BS 837, AFT CARGO DOOR CUTOUT LOWER CORNER. REMOVED AND REPLACED REPAIR WITH PERM REPAIR PER B737-2000 SRM 53-00-01 FIG 201. (M)SDR 9132005Step · damagedRETRACTABLE STEP ASSEMBLY MECHANISM IS ATTACHED TO THE LANDING GEAR STRUT BY A STEEL BRAIDED CABLE WITH METAL CLAMP. CLAMP AROUND STRUT ROTATED ALLOWING EXCESSIVE SLACK IN THE CABLE. WHEN THE LT LANDING GEAR WAS EXTENDED IT CAME IN CONTACT WITH THE RETRACTABSDR 05FDEA02788Insulation · burnedCAC, FUSELAGE INSULATION BLANKETS SEVERLY BURNED AROUND SYS 1-2 AND SYS 1-3, PNEUMATIC AIR DUCT. CHECKED PNEUMATIC SYSTEMS PER JRH AND LEAK CHECKED,OP'S AND LEAK CHECHED OK.FOUND INSULTION BLANKETS SECURED & TOUCHING DUCT. NEW INSULTATION BLANKETS INSTALLED ISDR DXTA200500956Unknown · unknownAT FL400 IN CRUISE A LOUD THUMP WAS HEARD AND FELT IN THE NOSE AREA. ITEM IS UNDER INVESTIGATION.SDR AWXA200501029Structure · vibrationLAX - AIR TURN BACK - FLT 106 - AFTER TAKEOFF, CREW REPORTED AIRFRAME VIBRATIONS. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED AND OPERATED ALL FLIGHT CONTROLS. PERFORMED YAW DAMPER BITE TESTS AND CHECKED STANSDR 05FDEA02407None · noneTHIS INSTRUCTION TO REPLACE BOTH EXISTING ILS RECEIVERS WITH MMR AND ASSOCIATED WIRING. ACCOMPLISH EA 1-3431-82825.SDR 05FDEA02406None · noneIAW DWG SR11340052 SHT 10, 307.203, 307.204, THERE IS ALL WIRE INSTALLED. ACCOMPLISH EA 1-3431-82825.SDR 2005UALA00741Pdu · vibrationRETURNED TO FIELD DUE TO AIRCRAFT VIBRATION. TE FLAP PDU DID NOT FUNCTION PROPERLY. REPLACED SUBJECT PDU.SDR 05FDEA01754Insulation · burnedIN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERLY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC AIR DUCT. BLANKETS ARE REMOVED FOR BLANKETS MOD WILL BE INSTALLED AND SECURED ON EA 8-2580-86498, SEQ NR 780, EMP.97433, QC.9SDR 2005FA0001608Bolt · brokenBOLT BROKEN. (K)SDR LNX2006F000AAUnknown · unknownDURING ENROUTE CRUISE FLIGHT, THE LT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW MONITORED AND FOUND NO ADDITIONAL DISCREPANCY. THE FLIGHT CONTINUED TO ITS DESTINATION WITHOUT INCIDENT. UPON INVESTIGATION. THE MAINTENANCE CREW FOUND METAL PARTICLES INSDR VGC2005F00001Unknown · unknownNR 2 FUEL PUMP FAILED. RT DC GENERATOR OFF LINE, FOLLOWED BY LT DC GENERATOR OFF LINE. (ELECTRIC ODOR NOTED). TRU TO EMERGENCY SELECTED FOR DC BUSS POWER. PRECAUTIONARY LANDING MADE. (K)SDR S2YA05025Control Panel · inoperativeDURING TAXI THE CREW GOT A LAVATORY SMOKE DETECTOR INDICATION. CRASH-FIRE-RESCUE MET THE AC AT THE GATE AND THE PASSENGERS WERE DEPLANED. MECHANIC INSPECTED THE AC AND FOUND NO INDICATION OF FIRE OR SMOKE. MECHANIC REPLACED THE OXYGEN/ECS WITH APU PANEL ANDSDR 05FDEA00538Repair · unknownCOMPLY WITH AGING 9 - AGING INSPECTION, NR 2 PYLON - FERRULE PRECOOLER AT AFTER SIDE OF UPPER SIDE WITH REPAIR (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 54-51-11, CONFIG 2, FIG 201SDR MASA200500111Unknown · unknownASH 7111 CLE TO IAD ABORTED TAKEOFF DUE TO THE AIRCRAFT PULLING TO THE LEFT WITH FULL RIGHT RUDDER DEFLECTION. 2/15/05 MAINTENANCE PERFORMED NOSE WHEEL STEERING SYSTEM ECU ADJUSTMENT CHECK IAW CRJ 200 AMM 32-51-10, OPS CHECKED GOOD.SDR COMA0560107Unknown · unknownFLIGHT 5780 SEVERE TURBULANCE DURING FLIGHT, LASTED 15 TO 20 SECONDS. C/W TURBULANCE INSPECTION, NO DEFECTS FOUND.SDR ASAA0570001Repair · scheduled maintDURING MAINTENANCE CHECK FOUND TEMP REPAIR AT BS 394. INSTALLED PERMANENT REPAIR IAW SRM. (K)SDR PNSA041204Unknown · unknownCAPT MISTAKENLY HEARD AUTOCOARSEN FAIL CALLOUT BY SECOND IN COMMAND ON INITIAL TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AFTER TURNING OFF RUNWAY FAILURE LIGHT WAS CONFIRMED NOT TO BE ON. MAINTENANCE WAS CALLED BUT NO ACTION TAKEN. AIRCRAFT TAXIED BACK TO RUNWASDR UPS04143619Unknown · unknownCAPTAIN REPORTED A LOUD THUNK 5 TIMES IN FLIGHT. THE NOISE BECAME LOUDER AND EFFECTED THE AIRPLANE AND FLIGHT CONTROLS. AT THIS TIME AN INFLIGHT EMERGENCY WAS DECLARED. PERFORMED BOW TS 1883 REV 0098 WITH NO FAULTS NOTED.SDR QXEA200400930Structure · contaminatedTAKE-OFF WAS ABORTED WHEN THE AIRCRAFT FAILED TO ROTATE AT VR. THE TAKE-OFF WAS ABORTED AT 102KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED RESIDUAL TYPE IV DEICE FLUID FROM AIRCRAFT. THE AIRSPEED INDICATORS AND THESDR QXEA200400896Unknown · unknownSEA - FLIGHT 2413 - THE FLIGHT RETURNED TO THE GATE AFTER THE PUSHER SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE CIRCUIT BREAKERS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR QXEA200400846Unknown · unknownTHE TAKEOFF WAS ABORTED WHEN AFTER REACHING 102KTS, THE AIRCRAFT DID NOT ROTATE WHEN THE CONTROL YOKE WAS PULLED BACK. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE BEGAN WORKING ON THE AIRCRAFT TO DETERMINE THE CAUSE. THE AIRCRAFT IS DOWN FOR MAINTENANCSDR 04FDEA03185Unknown · unknownON DEPARTURE OUT OF ONT AT APPROX 1000 AGL GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. DIVERT TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIGHT CONTROL INSPECTION. PUSDR GYN2005F00000Air Filter · mismanufacturedMFG SWITCHED FROM PN 1J47 TO PN 2J47. THE PROBLEM IS THAT THE NEW STYLE FILTER IS SMALLER IN DIAMETER THAN THE OLD STYLE FILTER, AND WE HAVE NOT BEEN ABLE TO PURCHASE A (DG-47) ADEL CLAMP FROM ANY OF OUR SUPPLIERS. AS NOW, WE HAVE TO RESORT TO REDRILLING THESDR GNB2005F00000Line · crackedCRACKED PRESSURE LINE AT THE BEND. (SW01200502449) (K)SDR 2008FA0000716Spar · delaminatedDURING THE 6000 HR INSPECTION, DELAMINATION FOUND IN THE TOP AFT CORNERS OF THE SPAR BRIDGE, BOTH SIDES. AFTER FURTHER INVESTIGATION BY FACTORY PERSONNEL, CRACKS WERE FOUND DOWN THROUGH THE DIFFERENT LAYERS OF GLASS NOT THROUGH THE CARBON FIBER. RECOMMEND THATSDR BAQA2004628Antenna · damagedOVER THE PAST 24 MONTHS THIS AIRCRAFT HAS HAD 4 SETS OF NAV ANTENNAS INSTALLED. FAILURE MODE OF ANTENNA IS (RT ELEMENT BECOMES EXTREMELY WEAK) WHICH CAUSES NAV INDICATOR DISPLAY ERRORS OF UP TO 5 DEGREES, VISUAL INSPECTION INDICATES THAT RT NAVE ANTENNA ELEME
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