JASC 5101
Service difficulty reports · 482
Reports filed under 5101 · Aircraft 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 = '5101' 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 = '5101' 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 IXXA2022020902None · corrodedCABIN FLOOR PANEL SUPPORT IS CORRODED, FROM STA.1480 RBL85, TO STA.1560 RBL78SDR DALA2021101406360None · noneBIRD STRIKE ON LEFT NOSE FUSELAGE. IMPACT DENT FWD FR12 MEASURING 2.5INCH X 0.5 INCHES AND 0.0005 DEEP. DENT IS 10 INCHES ABOUT CUTOUT PANEL. DENT IS NOT PERMITTED PER A220 ASRP 53-11-01-06AAA-661A-A . C/W 10X DVI OF DENT FOR CRACKS, NO DAMAGE FOUND. COMPLIED SDR QXEA2020010200002Structure · vibrationSEVERE ICE ENCOUNTER FL 230 DESCENDED LOWER. AIR FRAME VIBRATION FROM 230 TO 146 SHIELD ICE 10K. AUTOPILOT OFF PROPS 1020. ELEVATOR FEEL SLUGGISH. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CONSULTED REPORTING FLIGHT CREW FOR FURTHER DETAILS, NO AIR FRAME OR PRSDR AALA201907299044Unknown · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS TOGA CONFIG 1 TAKEOFF 25R PHX OAT 43Ï¿½C JUST PRIOR TO V1, AIRCRAFT EXPERIENCED EXTREME JOLT FELT BY ENTIRE CREW SENSED SIGNIFICANT FORCE TO LEFT. NO ECAM TRIGGERED AND NO COMPRESSOR STALL SOUNDS. FORCE WAS OF SHORT DURATIOSDR DXTA2019030402106Unknown · vibrationAIRFRAME VIBRATION - IN CRUISE FLIGHT AT FL410 WE EXPERIENCED AN AIRFRAME VIBRATION. IT SOUNDED LIKE A PUMP RUNNING ON AND OFF AND SOUNDED LIKE A DEEPER BASS TYPE OF NOISE. THIS NOISE WAS VERY PRONOUNCED WITH OR WITHOUT HEADSETS. CREW LOOKED AT WINGS AND THERESDR ABXR0201902010048Hanger Assy · corrodedSUPPORT HANGER (CHORD) EXFOLIATEDSDR SWIA2018102345165Not Reported · vibrationAT 12000 THE AIRCRAFT STARTED TO PRODUCE HEAVY UNUSUAL VIBRATION IN THE HULL THE AND A VERY LOUD VIBRATING NOISE. WE DECLARED EMERGENCY AND RETURNED TO FIELD. NO MASTER WARNING AND NO MASTER CAUTIONS MESSAGES AND ALL ENG VIBRATIONS WERE WITHIN NORMAL RANGE. (FSDR SWIA2018103145194Panel · crackedPANEL 822DRW HAS CRACK IN COMPOSITE. (C-CHECK) RO: 10/24/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822DRW IN REFERENCE TO AMM 50-31-00.SDR SWIA2018410315193Panel · cracked822ARW PANEL HAS CRACK IN COMPOSITE.(C-CHECK) RO: 10/25/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822ARW IN REFERENCE TO AMM 50-31-00.SDR JJBA20170830015Plate · crackedSTRESS PANEL 523AT LADDER PLATE HAS GOUGES AND CHAFFING DAMAGE, STRUCTURES TO ACCESS AND REPAIR AS NECESSARY. LADDER PLATE HAS BEEN REPAIRED.SDR COZA20160825091Spar · corrodedCORROSION WAS FOUND ON THE FORWARD SIDE OF THE RIGHT WING SPAR AT THE NR 2 FORWARD BOOST PUMP. THE CORROSION WAS LOCATED DIRECTLY ABOVE AND BELOW THE PUMP RADIATING OUT FROM THE BONDING JUMPER ATTACH POINTS. THE CORROSION WAS REMOVED, SPAR NDT'D AND REMAININSDR WX0A2015102972979Structure · vibrationCLIMBING THROUGH FL300 AT .77 WE ENCOUNTERED AIRFRAME VIBRATION. IAW QRH 56.18 WE DISCONNECTED AUTOPILOT 1 & APPLIED LT RUDDER, WHICH DAMPENED THE VIBRATION. UPON DELETION OF VIBRATION WE RE-CONNECTED AUTOPILOT 1 WHILE CRUISING AT FL 250 & M.78 WE RE-ENCOUNTSDR WX0A2015061972670Unknown · vibrationCLIMBING OUT OF ABOUT 20000 FEET, SPEED ABOUT 295 VTS, VS ABOUT 2000 FEET, WE EXPERIENCED SIGNIFICANT ACFT VIBRATION. VIBRATION WAS MORE PRONOUNCED IN AFT OF ACFT. ACCORDING TO AFT FA IT WAS INTENSITY OF VIBRATION THEY HAVE NEVER FELT BEFORE. WE WERE IN CLEASDR CALA2015022000121Unknown · vibrationPRONOUNCED AIRFRAME VIBRATION AFTER GEAR & FLAP RETRACTION. NOTICEABLE VIBRATION IN YOKE & ON FLOOR. FELT SPOILERS WEAR PARTLY UP. ENG INDICATIONS NORMAL. TROUBLE SHOT AIRFRAME VIBRATION IAW AMM 05-51-67. NO DEFECTS NOTED ON GND. THIS SUBMISSION FOR MRR SDR AALA20150119013Unknown · vibrationAIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB AN AIRFRAME VIBRATION FELT ON THE RT SIDE OF THE CABIN FROM ROW 9 FWD TO THE COCKPIT. PERFORMED TSM 05-50-00 INSPECTED WING ROOT, LG DOORS, FLAP PLAY & FLIGHT CONTROSDR SIMA20141204003Unknown · vibrationUNUSUAL HARMONIC TYPE VIBRATION FELT 4 TIMES IN THE DECENT. PERFORMED INSPECTION OF THE ACFT IAW WC 05-005 PART 1. NO DEFECTS NOTED. REFER LOG PAGE 3556786 FOR FCF.SDR WX0A2014120272290Unknown · vibrationEXCESSIVE AIRFRAME VIBRATION CLIMBING FROM 26500 ' TO 32500 ' VIBRATION REPORTED GREATER IN THE TAIL OF THE ACFT. DID NOT HEAR VIBRATION. VIBRATION WAS IN A SIDE TO SIDE MOTION, YAW. ACFT WEIGHT 138,000 LBS, AIR SPEED 290 KNOTS, 7.4 MOCK. NR 1 ENG N1 89.3,SDR IXXA20150101036Stringer · corrodedCORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R OUT OF LIMITS. REPAIRED CORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R IAW 47089REA02.SDR SIMA20140802002Unknown · vibrationCLIMBING THROUGH FL 358 A CONTINUOUS & CONSTANT FLIGHT CONTROL VIBRATION WAS FELT THROUGH THE FLIGHT CONTROL COLUMN. THE VIBRATION WAS ONLY FELT ALONG THE HORIZONTAL STABILIZER AXIS. OCCASIONALLY THERE WAS A STRONGER VIBRATION PERIODICALLY FELT. THE VIBRATISDR USAA2014061300027Unknown · vibrationDURING CLIMB THRU FL280 AT MACH 79 STRONG AIRFRAME VIBRATION IN VERTICAL AXIS, UP & DOWN MOTION, AT APPROX RATE OF 2 - 3 CYCLES PER SECOND, HAD TO SLOW BELOW 280 KNOTS MACH 76 TO STOP MOTION. REPLACED SEALS ON HYD ACCESS PANELS & AFT CARGO DOOR SEALS. REPLACESDR SIMA20130618003Tape · departedSPEEDTAPE ON C/A SIDE HUMP SEAL CAME OFF ON THE CLIMBOUT FOLLOWED BY STRONG BURNED PLASTIC SMELL IN ACFT, REF TO NRWC 646-DFW-01255 AND 646-DFW-01259. REAPLLIED SPEED TAPE ON CAPT HUMP SEAL AND PERFORMED NR 1 ENGINE INLET INSPECTION. NO DAMAGE FOUND.SDR SWIA201231907Drag Angle · crackedCRACK ON AFT DRAG ANGLE. (C-CHECK) REPLACED DRAG ANGLE SECTION IN REFERENCE TO REO.SDR SWIA201231667Panel · chafedPANEL 326CL HAS CHAFING. (C-CHECK) REPAIRED PANEL 326CL AS PER CRJ 200 SRM.SDR UALA2011102105700Unknown · vibrationLIGHT VIBRATION IN COCKPIT DURING CLIMB UP TO FL 300. FLT ATTENDANT REPORTED VIBRATION IN THE TAIL WAS STRONGER. ALL VIBRATION STOPPED AFTER FL300 WHILE STILL CLIMBING. ACCOMPLISHED VIBRATION TROUBLESHOOT IAW MT 53-005 REV G. ACCOMPLISHED ELEVATOR EXCESSIVESDR GNB2011F00001Web · crackedCRACKS FOUND FOR/AFT AREA PREVIOUSLY ADDRESSED IN MEB 84-12. REPAIR CONDUCTED IAW 8110-3 FAA APPROVED DATA, REF 135415A(14).SDR REXA201100183Panel · openLOUD NOISE COMING FROM THE NOSE OF THE A/C FOLLOWED BY A STALL FAIL MSG DURING INITIAL CLIMBOUT. FOUND PANEL 212BR OPEN. PERFORMED OPS CHECK ON STALL PROTECTION SYSTEM IAW 27-35-00.SDR YENA20091207167Unknown · vibrationFLT JB33 ROC-JFK PERFORMED AIR RETURN BACK TO ROC DUE TO AIRCRAFT VIBRATION ON CLIMBOUT WITH FLAPS 1 NEVER EXCEEDED 160 KTS, MID CABIN VIBRATION. MX PERFORMED INSPECTION OF LAVATORY A DRAIN LINE AND BRACKET, NOSE GEAR MAIN AND SECONDARY DOOR HINGES IAW AMM 52SDR UIEA201000121Support · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE LEFT I/B UPPER TRAILING EDGE FIXED PANEL O/B SUPPORT WEB (REFERENCE FIGURE 1). PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747SDR AALA200800198Skin · noneAFW - FUSELAGE SKIN AT STATION 1582 HAD A TEMPORARY REPAIR. AREA OF DISCREPANCY IS 3.8 INCH BY 2.7 INCH. ACCOMPLISHED PERMANENT REPAIR FOR FUSELAGE SKIN AT STATION 1582 STRINGER 25L.SDR 07FDEA03547Structure · corrodedCORROSION FOUND ON CONNECTING SECTION, C 55/58-59, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR NSVA20070225Unknown · unknownFLIGHT ATTENDANT REPORTING HISSING SOUND COMING FROM AROUND EMERGENCY EXIT ROW 7 PRESSURIZATION NORMAL. OPS CHECK PRESSURIZATION IAW AMM 21-32-00-05. COULD NOT LOCATE A HISSING SOUND AROUND EMERGENCY EXIT DOORS, NO FAULTS FOUND.SDR 07FDEA03415None · noneFOUND OLD EXTERNAL RIVETED DOUBLER ON RT INBOARD FLAP, OUTBOARD EDGE RIB 21, WITHOUT ANY RECORD. REPAIR RENEWED BY CUT OUT TO A REGULAR SHAPE AND INSTALLING A NEW DOUBLER, APPROVED BY EA 6-5752-95905 AND RAS/DABRE/7006189/2006 ISSUE A.SDR 2007UALA03448Unknown · damagedSTA 1682 RIGHT SIDE AT FLOOR LEVEL IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED A NEW REPAIR ANGLE & STRAP.SDR 2007UALA03405Unknown · vibrationLIGHT LATERAL AIRFRAME VIBRATION IN COCKPIT AND AFT GALLEY DURING CLIMB FL248-270.SDR 07FDEA03026Skin Panel · unknownFOUND OLD DOUBLER REPAIR AT FRAME 26-27, STRG 24-26 RT. THE REPAIR WAS PERFORMED IAW DRW: R537B1730-002 BUT FOUR HOLES HAVE DIA: 7, 5MM INSTEAD OF 4,8MM. REPAIR PERFORMED BY REAM UP THE DIAMETERS TO 8, 8-9, 0MM AND INSTALL FOUR SHOULDERED BUSHES IAW EA 6-5SDR FDKA200708396Insulation · burnedFDM 6003 JFK (0920 PHX LCL). CREW RETURNED TO THE FIELD DUE TO A STRONG SMOKE ODOR COMING FROM ROOF OF GALLEY. MX FOUND INSULATION AGAINST LIGHT ASSY IN GALLEY, REPOSITIONED INSULATION. NO FURTHER SMOKE SMELL FOUND.SDR DLM88071109Skin · noneTEMPORARY REPAIR ON STA 180 AND BETWEEN LONG 23 AND 25 RT. REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064056 ON HMV IN GDL.SDR DLM88071108Skin · noneTEMPORARY REPAIR ON STA 218 AND LONG 23-25 RT, REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064057 ON HMV IN GDL.SDR 2007UALA03083Unknown · vibrationACFT FLOWN AT 250 KTS/LWR ALTS TO REDUCE AIRFRAME VIBRATIONS EXPERIENCED AT HIGHER SPEEDS. 09-07-07 CHECKED ALL ACCESS PANEL DOORS FOR FIT AND FAIR, NOTHING NOTED.SDR 2007FA0000672Bridge · crackedON JULY 23, 2007 DURING A ROUTINE DYE-PENETRANT INSPECTION ON TG-10B (L-23 SUPER BLANIK, S/N 029013) CRACKS WERE DISCOVERED AT SEVERAL WELDS ON THE A741 210N BRIDGE ASSEMBLY. IT IS A MAINTENANCE MANUAL REQUIREMENT THAT THIS PART BE DYE-PENETRANT INSPECTED EVESDR K11A2008121172011Duct · damagedAREA OF DAMAGE LOWER RIGHT SIDE JUST AFT OF SOUND ATTENUATING MATERIAL TOP OF DUCT BEHIND INLET (S DUCT).SDR MWEA070157None · noneSM 2673 SOILD FASTENERS NEED TO BE INSTALLED PER ETA 0602B STEP 1 BETWEEN CENTER & FIRST OFFICER`S WINDOW AT THE NEXT HEAVY CHECK. INSTALLED FASTENERS.SDR 07FDEA02470Structure · unknownEXISTING DOUBLER EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1.SDR MALA070073Structure · damagedAIRCRAFT HAD ARRIVED TO MSP AFTER LANDING FLIGHT 2788 WITH PASSENGERS ON BOARD. AIRCRAFT TAXIED TO GATE AREA AND WAS WAITING AT CIRCLE 95. AIRCRAFT 8896 WAS PUSHED BACK AND LEAVING FROM B14 WHEN JET BLAST FROM THE CRJ PUSHED BAG CARTS FROM THE GOPHER AREA. SDR 07FDEA02191Skin · misrepairedOUTER FLAP RT, OLD STATIC DISCHARGER REPAIR FOUND NOT CONFORM TO RAS/FOK/110/2003 (DOUBLER THICKNESS). REPAIR PERFORMED BY INSTALLATION OF NEW DOUBLER IAW RAS/FOK/110/2003 ISSUE "A".SDR 2007UALA01904Unknown · vibrationVIBRATION NOISE ENCOUNTERED IN FLIGHT. REMOVED PANELS AND REPLACED SEALS AND FASTENERS. NO VIBES REPORTED FROM OUTBOUND CREWS.SDR 2007UALA01596Unknown · vibrationVIBRATION FELT DURING CLIMB IN MID-AFT CABIN AREA. AFTER LEVEL-OFF VIBRATION STOPPED. VIBRATION WAS FELT IN CLIMB AND DESCENT AND IT WAS A SIDE TO SIDE MOTION THAT GOT MORE PRONOUNCED WITH INCREASE IN SPEED.SDR 052107N151CSStructure · damagedON APPROACH, CREW ENCOUNTERED FLOCK OF GEESE RESULTING IN NUMEROUS STRIKES. ABORTED APPROACH, INITIATED AFM ABNORMAL CHECKLIST WITH NO ABNORMALITIES NOTED. DIVERTED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING AND EXITING AIRCRAFT, CREW NOSDR 2007UALA01560Unknown · vibrationAIRFRAME VIBRATIONS BEGIN IN CLIMB FL185 AND FADES OUT APPROX FL.SDR 2007UALA01595Unknown · vibrationVERY LIGHT LATERAL AIRFRAME VIBRATION IN CLMB AND CRUISE. GOES AWAY WITH AILERON INPUT. SAMC TEXT: FLT CREW REPORTED NO VIBRATION IN DESCENT.
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