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 2007UALA01102Control Panel · failedRTFL DUE TO MODE CONTROL PANEL FAILURE. [SUP 5-1-07] FOUND FAILED MODE CONTROL PANEL. REPLACED FLIGHT CONTROL COMPUTER. SHOP FOUND A "CHECK SUM ERROR" IN COMPUTER.SDR 2007UALA00786Unknown · vibrationHIGH FREQUENCY VIBRATION STARTED 23,500- 330 KNOTS WENT AWAY 24,500-300 KNOTS RETURNED AGAIN 25,000-315 KNOTS AND STOPPED 30,500-290 KNOTS .76 MACH. VIBRATION VERY NOTICEABLE THROUGHOUT CABIN. FLT CONTROLS SEEMED OK. CREW REPORTED UP & DOWN OSCILLATION THRSDR 2007UALA00785Unknown · vibrationHIGH FREQ LATERAL VIBRATION FROM TAIL OF ACFT DURING CLIMBOUT. VIBRATION DECREASES WITH DECREASE IN AIR SPEED. [SUP 06-01-07] REPLACED YELLOW HYDRAULIC SYSTEM RT ELEVATOR SERVO VALVE AFTER FINDING OSCILLATIONS TO BE OUT OF LIMITS.SDR DXTA200702021Unknown · unknownON CLIMB OUT, GOING THRU FL180 AND LATER FL 240. WE FELT BUMP FROM GEAR RE-RETRACTING. BOTH WERE AUDIABLE THUMPS. FOUND ALL THREE UP-LOCK SWITCHES OUT OF RIG AND NOSE GEAR EMERGENCY RELEASE CABLE TENSION WAS TOO TIGHT. MADE NECESSARY ADJUSTMENT IAW GEAR BUMPSDR 07FDEA00777Skin · unknownTHE MAIN CARGO DOOR HAS 4 EXTERNAL DOUBLERS ON ITS INTERNAL SKIN ALONG THE TOP EDGE AT STATIONS 520, 540, 560, AND 580. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00776Frame · unknownFOUND AFT PIT FRAME REPAIR, STA 970, ABOVE S23L TO S24L. COMPLY WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00775Frame · unknownFOUND AFT PIT FRAME REPAIR STA 950, ABOVE S24L TO S25L. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00774Stringer · unknownAFT PIT, FUSE STRINGER REPAIR STA 1130- 1166,S29. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00773Stringer · unknownAFT PIT, FUSE STRINGER REPAIR, STA 1070- 1090,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00766Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1237, RBL 20, WL 189. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00760Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1238, RBL20, WL 183. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2.SDR HALA0700095None · noneETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG R ENG OH LP 2 DISPLAYED. DOWN POWER AIRCRAFT, RERACKED R ENG OH LP 2 CARD ON P54, RESTORED POWER, EICAS STATUS MESSAGE CLEARED.SDR HALA0700088None · noneETOPS SIGNIFICANT SYSTEM, " AIL LOCK LGT ILLUM AT ALL SPEEDS EICAS MSG AILERON LOCKOUT DISPLAYED. TROUBLE SHOT PER FIM 27-11-00. SYSTEM CK'S OUT OK. AIL LOCK LIGHT AND EICAS MSG EXTINGUISHED. OK FOR SERVICE.SDR COMA0770018None · noneFLIGHT 5526 - ELEVATOR SPLIT CAUTION MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED AIRCRAFT, NO FAULTS IN MDC, NO HISTORY IN TRAX OR AIRCRAFT LOG BOOK. PERFORMED OPS CHECK WITH NO DEFECTS FOUND.SDR 2007UALA00578Unknown · smokeSMOKE COMING FROM FWD OUTFLOW VALVE AFTER ENGINE START.SDR HALA0700053None · noneLIGHTNING STRIKE ON CLIMB-OUT. ACCOMPLISHED HAL M251-767 "INSP OF AIRCRAFT AND OPERATIONAL CHECK OF RADIO AND NAVIGATION SYSTEMS AFTER LIGHTNING STRIKE". CHECKED GOOD, OK FOR SERVICE.SDR VNAA0702009Unknown · unknownCREW REPORTED A LOUD NOISE COMING FROM THE F/O'S SIDE AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT HAND FORWARD FUSELAGE AREA. SUSPECT COMM DOOR LEFT OPEN BUT WAS NOT OPEN UPON ARRIVAL TO AIRCRAFT. NO DEFSDR YENA2007010None · noneA/C RETURNED TO GATE DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND FIRE AND SMOKE DAMAGE TO OVERHEAD BIN AT ROW 18/19 LEFT CAUSED BY CAMERA EQUIPMENT BATTERY SHORTED IN PAX CARRY ON BAG. DAMAGED AREA WAS INSPECTED AND FOUND NO DAMGE TO STRUCTURE. AREA WAS CLSDR 07FDEA00402Unknown · unknownPREVIOUS COMPOSITE REPAIR FOUND LOCATED ON THE RT ELEVATOR LOWER SURFACE TRAILING EDGE STA 473. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 55-21-11 AND EA 6-5510-10668SDR IXXA07SMN090SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED SKIN WITH EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA ASDR 07FDEA00365Unknown · unknownON DEP AT 200'AGL (APPROX) RED WINDSHEAR WARNING LIGHT AND AURAL WARNING. PERFORMED ESCAPE MANV. FIREWALL POWER SET FOR ABOUT 3-5 SECONDS. WINDSHEAR WARN STOPPED AND LIGHT WENT OUT. RETURNED TO MEM. NO ENG PARAMETERS APPEARED TO BE EXCEEDED. AIRSPEED WASDR 07FDEA00327Unknown · unknownIN FLIGHT AIRCRAFT WANTED TO TURN RIGHT. REQUIRED 3 UNITS AILERON DEFLECTION TO FLY STRAIGHT. REQUIRED 14 UNITS OF RIGHT RUDDER TRIM TO LEVEL OUT AILERONS. NO CHANGES FROM CLIMB POWER TO IDLE POWER. NO CHANGE YAW DAMPERS ON OR OFF. NO CHANGES AUTOPILOT OSDR 07FDEA00326Unknown · unknownOLD REPAIR ON RT INBOARD FLAP AT LOWER AND UPPER SKIN BETWEEN RIB 12/14 TRAILING EDGE (PATCH REPAIR). REPAIR WAS PERFORMED IAW RAS/FOK/060/2003 ISSUE A.SDR 07FDEA00273Crossbeam · noneOLD REPAIRS ON CROSSBEAM C60 WITHOUT ANY OLD RECORDS CROSSBEAM WAS REPLACED BY NEW PART IAW SRM 51-72-10.SDR REXA200700013Unknown · unknownAFTER ESTABLISHING CRUISE ALTITUDE OUT OF DTW, THE FLIGHT CREW WAS ALERTED TO HIGHER THAN NORMAL N1 VIBRATION ON THE LEFT ENGINE. WHEN VIBRATION LEVELS CONTINUED TO INCREASE, THE QRH CHECKLIST WAS COMPLETED AND THE ENGINE WAS SHUT DOWN. THE FLIGHT CREW DECLASDR 07FDEA00137Skin · misrepairedPREVIOUS REPAIR, LEFT OF AFT PAX DOOR EXTERIOR SKIN LWR AFT CORNER HAS EXTERNAL REPAIR DOUBLE MEASURING 9.2IN BY 7.3IN. PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT PAX DOOR EXTERIOR SKIN LOWER AFT CORNER WAS DETERMINED NOT TO BE IAW A310 SRM 52-10-00 FIG 203, SDR N921R53309None · noneFUSELAGE STA 8 NLG WW DOOR JAMB LT CORNER SKIN WITH TEMPORARY REPAIR. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 53-07030-1 REV NEW 01-25-09 PAGE 1/3. ISSUED FAA FORM 8110-3. CPCP 4000 0551SDR 06FDEA04394Skin · misrepairedREPAIR LOCATED JUST AFT OF STA 1070 BETWEEN STR 20L-21L AND BETWEEN STA 1050-1070, BETWEEN STR 20L-21L. FOUND NOT TO BE INSTALLED USING APPROVED DATA. FOUND TO BE WITHIN 3" OF REPAIR AT STA 1050-1070, STR 1050-1070, STR 21L-22L, NO FASTENERS ABOVE REPAIR AT SDR 06FDEA04391Skin · misrepairedREPAIR LOCATED AT MED UPPER SKIN FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00910 AND SRM 52-00-3 FIG 3/4 DAMAGE HAS NOT BEEN CUT OUT PER SRM. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER REF SRM 52-00-3 FIG 3 PRIMED AND PASDR 06FDEA04390Skin · misrepairedREPAIR LOCATED ON RT WING NR 5 SLAT INBD TRACK FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00930 AND CMM/SRM, THERE IS NO JUSTIFIED DOCUMENT FOR INSTALLATION OF STAINLESS DOUBLER IN THIS LOCATION ACCOMPLISHED REPAIR OF NR 5 SLAT SKIN EXTENSIONSDR 06FDEA04389Skin · misrepairedEXT REPAIR LOCATED JUST AFT OF STA 700, STR 26L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00936 AND SRM 53-30-3 FIG 24, DOUBLER MISSING FASTENERS IN REPAIR AREA, RADIUS FILLER ALSO BENT. REMOVED DOUBLER, FABRICATED NEW DOUBLER AND FILLER. SDR 06FDEA04388Skin · misrepairedEXTERNAL REPAIR LOCATED AT STA 710, STR 28R FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00937 AND SRM 53-30-3 INCORRECT BLIND FASTENERS ARE INSTALLED ON REPAIR. REMOVED BLIND FASTENERS BS 710 STR 28R AND REINSTALLED SOLID FASTENERS REF SRM 51SDR 06FDEA04387Skin · misrepairedEXT REPAIR LOCATED AT APPROX STA STA 470-490 BETWEEN STR 21R-22R FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM # N00923 AND SRM 53-30-3 FIG 1 UPPER AND LOWER FASTENER ROWS DO NOT EXTEND BEYOND INTERNAL STRUCTURE. REMOVED DOUBLER, FABRICATED DOUBLESDR 06FDEA04386Skin · misrepairedEXT REPAIR LOCATED AT APPROX STA 39-410 BETWEEN STA 21R- 22R FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM NR N00922 AND SRM 53-30-3 FIG 3 REPAIR HAS INSUFFICIENT FASTENER ROWS PAST INTERNAL STRUCTURE. REMOVED EXISTING SKIN REPAIR, INSTALLED NEW RESDR 06FDEA04385Skin · misrepairedREPAIR LOCATED AT STA 360 BETWEEN STR 15L-16L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM# N00920 AND SRM 53-30-3 FIG 2, REPAIR DOES NOT HAVE REQUIRED NUMBER OF FASTENER ROWS. REMOVED DOUBLER, EVALUATED REPAIR AND FOUND IT TO BE IAW WITH BACO DRASDR HALA0700003Skin · damagedDAMAGE TO A/C LEFT WING AT NR 1 AND NR 2 SLAT LEADING EDGE NOSE SKIN. MADE BY AIRSTAIR TRUCK. REMOVED AND REPLACED NR 2 SLAT IAW AMM 27-81-02-424-028. GROUND CKD OK.SDR 06FDEA04355Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1870, FS 34 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SSDR 06FDEA04352Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3249, FR 60 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAISDR 06FDEA04351Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3143, FR 55/58 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM RESDR 06FDEA04322Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON AFT CARGO DOOR SKIN FWD LWR SIDE, FS 3249, AND FR 60. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO AN SDR 06FDEA04321Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF FWD CARGO DOOR SKIN, FS 1605, AND FR 23-23A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO SDR 06FDEA04365Structure · misrepairedPREVIOUS REPAIR FOUND LOCATED ON THE LT CROSSBEAM FS 2082, FR 38 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIRSDR 06FDEA04360Structure · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1870, FR 34 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND REPAIRED PER SSDR 06FDEA04362Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT CROSSBEAM FS 1976, FR 36 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM AND NEW REPAIR PSDR 06FDEA04348Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON THE LT INBOARD FLAP LOWER SURFACE FWD OF T/E SECTION WS 139 AND RIB 3. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOTSDR DU4R2007002Floor Support · tool damageFLOOR SUPPORT STRINGER HAS DRILL BIT DAMAGE BS 594 LBL 11 FWD CARGO COMPT. CUT OUT DRILLED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED 2 ANGLES 9" BY 1" BY 1" FROM 7075-T6 .050" AND 2 ANGLES 10" BY 1" BY 1" FROM 2024-T3 .040" IAW B757 SRM 51-70-12, FIGSDR DU4R2007001Floor Support · damagedFLOOR SUPPORT STRINGER HAS DRILL BIT DAMAGE BS 590 LBL 11 FWD CARGO COMPT. CUT OUT DRILLED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED 2 ANGLES 10" BY 1" BY 1" FROM 7075-T6 .050" AND 2 ANGLES 8" BY 1" BY 1" FROM 2024-T3 .040" IAW B757 SRM 51-70-12, FIGSDR 06FDEA04247Unknown · unknownCALLED OUT A/C AFTER AN ABORTED T/O FOR A LOUD SQUEAL ON FLIGHTDECK AT 80 KTS. REQUESTED FLIGHT CREW UNPLUG PERSONAL HEADSET AND PLUG IN COMPANY HEADSET. CREW REQUESTED ANOTHER T/O ATTEMPT, A/C DEPARTED KIND.SDR SIMA200634602Unknown · noisyLOUD WHISTLING NOISE WAS EVIDENT ON CLIMB-OUT. FOUND GPU DOOR OPEN. SECURED DOOR AND FOUND NO EVIDENCE DAMAGE, RETURNED AIRCRAFT TO SERVICE.SDR QXEA200603147Valve · inoperativeSEA - ON FLIGHT 2396, DURING BAGGAGE FIRE EXITING TEST "VALVE OUTLET" LIGHT DOES NOT ILLUMINATE DURING AFT BAGGAGE FIRE TEST. MAINTENANCE REMOVED AND REPLACED AFT BAGGAGE PIT AIR OUTLET VALVE. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE.
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