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 SWIA201541482Skin · chafedRIGHT APRON SKIN FOUND TO BE CHAFED OUT OF LIMITS. REPAIRED THE RT APRON SKIN PANEL IAW REO AND SRM.SDR DALA2015100906105Not Reported · not reportedPOSSIBLE LIGHTNING STRIKE. NO ELECTRICAL ANOMOLIES, ALL SYSTEMS APPEARED NORMAL. INSPECTED IAW AMM 05-51-19, ON SECTION 41, NOTED 9 CONTACT POINTS ON RT SIDE. 219568. COMPLIED WITH TEMPORARY REPAIR IAW ERA 540249-14, REV ORIG AT LOCATION ID NRS 1, 3, 4, 5, 6,SDR 2015FA0000460Pump · inoperativeA FUEL PUMP O/H FAILED WITH JUST 59.7 HOURS ON IT. ANOTHER UNIT O/H BY THIS COMPANY FAILED AT 65.8.SDR DALA2015092105722Structure · crackedCRACKS FOUND ON FRAME CUTOUT. REMOVED AND INSTALLED REPAIR PARTS IAW SRM 55-30-05 AND PRI/ERA 539470-14, REV 5.SDR A6WA201542990Unknown · noiseAFTER TAKEOFF AT APPROX 6000 FT, FLIGHT CREW NOTICED AN INTERMITTENT THUMP OCCURRING, FELT MOSTLY IN THE FLOORBOARDS. FLIGHT ATTENDANT REPORTS THE NOISE WAS PRESENT SOONER THAN FLIGHT CREW NOTICED IT. MOST NOTICEABLE IN FWD CABIN AREA. NO ABNORMAL INDICATIOSDR DALA2015093005888Not Reported · not reportedERA 538560-14, SECTION 1 COMPLIED WITH. DAMAGE APPEARS TO BE MORE EXTENSIVE THAN THE ORIGINAL LOG.SDR DALA2015073004752Tab · not reportedBUSHING GEARED TAB ATTACH POINTS WERE REPLACED. FITTING ON GEARED TAB ATTACH POINTS WAS REMOVED AND NEW FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW CMM 27-30-1, AMM 20-30-01-201, SRM 51-10-4, 51-10-3, PAR 21 AND 14 AND 51-30-2. FREE PLAY WAS CORRSDR WX0A2015072700061Unknown · oscillatesDURING CRUISE AT 38000 FT, AIRCRAFT OSCILLATED IN YAW WITH A FREQUENCY OF ABOUT 1/2 A SECOND, FROM LEFT TO RIGHT, RUDDER TRIM INDICATOR SHOWED LEFT. LEFT RUDDER TRIM VARYING BETWEEN L0.8 TO L1.2 128000 LBS M0.78 SMOOTH AIR AUTO PILOT 1 ON ENGINE VIB NORMAL, FSDR 2WAA20150709001Structure · damagedBIRD STRIKE ON T/O, LOSS OF AIRSPEED ON RT SIDE INTERMITTENT ON LT SIDE AIRSPEED. FOUND EVIDENCE OF BIRD STRIKE AT RADOME, PITOT TUBES, WING L/E. INSPECTED AND CLEANED AREAS IAW AMM 12-22-01. NO DENTS OR DEFECTS NOTED. OVERWEIGHT LANDING, OVER BY 200 LBS. ASDR ASOA2015061913149Skin · chafedPANEL 443BB HAS CHAFE DAMAGE. BLENDED CHAFE DAMAGE TO A SMOOTH CONTOUR ON PANEL 443BB IN REF TO SRM 51-12-00-001-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 54-12-01-101-001-A01.SDR DALA2015051403264Structure · damagedFOUND 2 HOLES ON LOWER FIXED L/E FOR HORSE COLLAR TO BE OVERSIZED AND OUT OF ROUND ON UPPER ROW. C/W PRI 535916-14, REV 1 AND ER/A 535916-14AD ORIGINAL.SDR DALA2015051103359Battery Pack · inoperativeRIGHT EMERGENCY ESCAPE TEST 1 INOPERATIVE. MAINTENANCE REPLACED RT POWER SUPPLY TO BATTERY PACK AND RELAY. SYSTEM OPERATION IS NORMAL.SDR 2015FA0000163Structure · corrodedEXTENSIVE CORROSION IN FUSELAGE AND WINGS, ESPECIALLY THE LEFT WING. THE PLANE WAS SO BADLY CORRODED IT LOOKED AS IF THE PLANE HAD BEEN IMMERSED IN SALT WATER AND THE COST OF THE REQUIRED REPAIRS WOULD EXCEED THE VALUE OF THE PLANE. IN ADDITION, THE LEFT WINGSDR SIMA20150416001Duct · unknownAT 27,000 DURING CLIMB, FLIGHT CONTROLS SHOOK VIOLENTLY & A BUZZING NOISE. ACFT WAS TAKEN OFF AUTO PILOT, CONDITION CONTINUED. DURING DESCENT GOT WORSE. DECLARED AN EMERGENCY, AND LANDED. R & R RT SUPPLY DUCT FROM RT DTCV TO HEAT EXCHANGER.SDR CA150421007Nut · damaged(CAN) TWO ANCHOR NUTS WERE FOUND BROKEN, CRACKED AND MISSING THE RETENTION SPRING.SDR ASOA2015040312536Megaphone · crew errorF/A REPORTS THAT MEGAPHONE IS INOPERATIVE. FOUND VOLUME TURNED DOWN ON MEGAPHONE. OPS CHECK GOOD IAW AMM 25-61-00.SDR HNAA2015032300103Unknown · unknownTROUBLE SHOOT EMERGENCY LIGHTS FLICKERS IN FLIGHT.....INSPECTED WIRING AT 9811TB14 5,6 AND 7. INSPECTED CONNECTOR M9811 J/P. SHOOK WIRING BEHIND LAV WALL, UNDERFLOOR CROSSOVER AND CABIN CEILING THROUGH ROWS 1 THRU 9. NO DISCREPANCIES NOTED.SDR DALA2015032402342None · noneDURING ATG4 WI-FI MODIFICATION IAW EA 06-468901-03, REV H, ME 13, EXISTING REPAIR DOUBLERS WERE FOUND AT THE FWD ANTENNA LOCATION, STA 508-520, S-28L, S-28R. THE EXISTING REPAIRS ARE LOCATED APPROXIMATELY 1) 2.25" FWD, 8.0" OTBD, AND 16.0" AFT OF THE NEW ATG4SDR DALA2015032002267None · noneSCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY: NR FOR ADDITIONAL INFORMATION 006-0001:5724-01010-04B/001, 00213. COMPLETED AMDS CARD 5724-01010-06 BECAUSE OF CRACKED FASTENER HOLE.SDR DALA2015032002266None · noneIAW STEP 4B OF CARD 5724-01010-03B, ACCOMPLISH SECTION 05, LH, PRIOR TO FURTHER FLIGHT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY: NR FOR ADDITIONAL INFORMATION 005-0001:5724-01010-03B/005 00211 COMPLETED AMDS CARD 5724-01010-05 BECAUSE OF CRACKED FSDR SWIA201540958Hinge Pin · migratedFLOTATION VALVE HINGE PIN MIGRATED FROM HINGE. C-CHECK, RO 4/1/15, INSTALLED HITCH PINS AND WASHERS TO PREVENT ROTATION VALVE HINGE PIN FROM MIGRATING REF STS EA.SDR DALA2015031802243None · noneFOLLOWUP TO N/R 229, LOG 1847754, ERA 514345-14AD. ACCOMPLISHED ER/A 514345-14AD, REV B SECT III ON STA R80 RT FRAME BETWEEN STR 10R & STR 14R. REF LOG PAGE 1847754SDR IPXA2015031787128Hook And Loop · looseEVAS VELCRO ON GLARESHIELD COMING LOOSE AT CAPT POSITION, REF EO M-2560-54394-B, INSTALLED NEW HOOK AND LOOP AS REQUIRED.SDR IPXA2015031887160None · noneCAPT EVAS WAS REMOVED FROM CONTAINER. WAS NOT DEPLOYED. R & R CAPT EVAS IAW AMM 25-69-00-401. PN OFF-ON: 107STC-267, SN OFF: 0009X06P, SN ON: 0008X09P. EFF REF IPC 25-60-00-90, ITEM 001.SDR 29GA2015032000001Door · handler errorGROUND DAMAGE DISCOVERED, AFT FUSELAGE BELOW CARGO DOOR BS 658.5 - 702. REPAIRED DAMAGED AREA OF FUSELAGE SKIN INSTALLED EXTERNAL DOUBLER AND REPAIRED FRAME SECTOR.SDR HNAA2015031600101None · nonePOSSIBLE ANIMAL STRIKE DURING ROLL OUT. INSPECTED PLANE AND FOUND NO EVIDENCE OF ANIMAL STRIKE.SDR DALA2015031702208None · handler errorLEFT WINGTIP SUSTAINED EXTENSIVE DAMAGE FROM ANOTHER ACFT. R & R WINGTIP IAW PRI 533962-14.SDR FDEA201503130910None · noneL1 DOOR WILL NOT ARM. OPERATED & ARMED L1 DOOR EMERGENCY SLIDE IAW AMM 52-11-00-6. OPS CHECKED GOOD.SDR ASOA2015040712547Skin · erodedPANEL 522 DB HAS SCREW HOLE DAMAGED AND L/E EDGE ERODED. REMOVED DAMAGE AT L/E EDGE AND AROUND SCREW HOLE, REF: SRM 51-12-00-001-001-AS01, TR 51-0050. RECEIVED AND COMPLIED WITH STS EA 32-2015-097. PERMANENT REPAIR. ALL STEPS COMPLETED. RECEIVED AND COMPSDR ASOA2015031312378None · noneMEGAPHONE REQUIRES REPLACMENT FOR LIFE LIMITS. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECK GOOD NO FURTHER DEFECTS NOTED.SDR RAIA201503110003Unknown · unknownPASSENGER REPORTED THERE WAS SOMETHING STREAMING FROM WING DURING CRUISE, RETURNED TO BLOCK. MAINTENANCE PERFORMED GVI OF WING FOR LEAKS, NO DEFECTS NOTED.SDR XV6A2015031100002Repair · unknownREF TECH W/O 1502527. R & R EXISTING REPAIR AT BS 727G IAW DWG 53-15046. EXISTING CATEGORY "C" REPAIR TIME LIMITED REPLACED BY CATEGORY "B" REPAIR.SDR ASOA2015031112343None · noneTO COMPLY WITH EC/TC EO 700-25-0166, MEGAPHONE REQUIRES REPLACEMENT. R & R MEGAPHONE IAW AMM 25-61-14. REF IPC 25-61-14, FIG 1, ITEM 5.SDR ASAA2015030810892Unknown · unknownEEC-ON -OTA 15'C-WIND CALM ENG ANTI-ICE-OFF-30.08 WING ANTI-ICE-OFF REDUCE POWER TAKEOFF 8 FMC COMPUTED DIFFERENT N1 TARGET VALUES OF 0.7 ENG 1 89.8 ENG NR 2, 89.1. ACFT GROUNDED. PREFORMED FIM TASK 34-61-839, AND SUB TASK MM 34-61-00-730-001. NO DEFECTS FOUSDR HALA2015030700034None · noneREPLACED TAILCONE SLIDE DUE TO PRECAUTIONARY, DID NOT DEPLOY. REPLACED TAILCONE SLIDE IAW AMM 25-61-02-400-801.SDR IPXA2015030786756Bulkhead Web · noneINSPECTION TYPE:C, D507181 NOSE WHEEL WELL BULKHEAD WEB REPAIR STA 395. REMOVED DOUBLER REPAIR ON D507181 NOSE WHEEL WELL BULKHEAD STA .395 IAW SRM 51-40-02-0G. NDT FOR CRACKS. HFEC IAW NTM 51-00-19, NO NOTED DEFECTS T12117. NDT ROTO PROBE OPEN HOLES. ROSDR DALA2015031902244None · noneATG ANTENNA DOUBLER WILL BE 6" FROM EXISTING REPAIR. C/W STA 1340 TO 1360, STR 29L TO 30 R FABRICATION AND INSTALLATION OF ATG ANTENNA DELETION DOUBLER REPAIR IAW ERA 527407-14, REV "O".SDR DALA2015030601920None · noneDURING THE LANDING, THE ACFT SKIDDED TO THE LT AND DEPARTED THE RUNWAY. MAINTENANCE AND DAMAGE EVALUATION IS IN PROGRESS.SDR DALA2015030601909Antenna · brokenDURING INSPECTION FOUND ANTENNA BROKEN AT FS 508, BL 0. FOUND CORROSION UNDERNEATH. MAINTENANCE REPAIRED IAW ERA 533778-14.SDR DALA2015031702211None · noneERA 533588, SECTION I ISSUED FOR REPAIR TO C2 BEAM.SDR DALA2015030401863None · noneDURING H-CK2, ER/A 532540-14, SECTION I INSTALLED AN SRM 53-04, PAR 57 EXCEPT FOR A MINOR DEVIATION. THE PURPOSE OF THIS LOGPAGE IS TO MONITOR THE SECTION II REPETITIVE INSPECTION. THIS CARD WAS ATTENDED WITH ER/A 532540-14, REV ORIG AND SRM 53-04, FIG 57.SDR QXEA2015030200107None · noneF/A REPORTS MAIN CABIN DOOR. HANDLE FEELS LOOSE. PERFORMED GVI OF MCD. NO DEFECTS NOTED. OPEN AND CLOSED MCD SEVERAL TIMES. DOOR OPERATES AND MCD SEAL PRESSURIZES PROPERLY. C/W AMM 52-11-00-710-502. NO DEFECTS NOTED.SDR HALA2015030100028None · noneMULTIPLE BIRD STRIKE AFTER T/O, EST AT 100' ALT GEAR FLAPS 5, NO ABNORMAL ENGINE INDICATIONS, NO UNUSUAL SMELLS, NO VIBRATION OR FLIGHT CONTROL PROBLEMS. ACCOMPLISHED AMM05-51-18-212-001 AND NO DISCREPANCIES NOTED; CLEANED AREA AS REQUIRED AND SAMPLES TAKENSDR IPXA2015030286602None · noneLEVEL 1 EMERGENCY LIGHT BATTERY 1 OPERATIVE, FORMED OPERATION TEST IAW AMM 33-50-00. OPS CK GOOD.SDR NACA201502260023None · noneREPLACE PATCHES ON RT STABILIZER L/E WITH FLUSH REPAIR. REPLACED PATCH WITH FLUSH FIT REPAIR, IAW ARM 55-10-3, FIG 2, REV 108. REFERENCE MCO 3008, W/O 1349438.SDR DALA2015022701715Web · handler errorFOUND WEB AT FR 34 MFG, PN D53231360200 DAMAGED BY IMPACT WITH JET TUG, SUPERTUG, INSTALLED NEW WEB ASST AT FRAME 34 IAW DWG C2D53233311, SHEET 2A.SDR DALA2015022701714Web · handler errorFOUND WEB AT FR 30 MFG, PN D5320258200 DAMAGED BY IMPACT WITH JET TUG, SUPERTUG, REPLACED WEB AT FR 30 IAW DWG C2D53233311, SHEET 2A.SDR DALA2015022601687None · noneERA478388-14, REV A, FS 1644 AT S-19L-S-20L/DENT REPAIR TIME LIMITED. OPENED AFT CARGO LT SIDEWALL, AFT CORNER, 719929 WIP. PERFORMED GVI AND HFEC OF REPAIR IAW ERA 478338-14, REV A, ORIGINAL INSPECTION INTRUCTIONS. NO DISCREPANCIES FOUND.SDR DALA2015022601701Access Panel · corrodedCORROSION ON COUNTERSINK, ON FUEL ACCESS DOOR 620 MB. REMOVED CORROSION. FABRICATED NEW BUSHING AND REWORKED AREA IAW SRM 57-00-04.SDR DALA2015022601663None · noneINADECUATE RIVETS ON STA 435 AND BETWEEN LONGERON 20 TO 24RT. FASTENERS WERE REMOVED. AREA WAS TREATED AND PAINTED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21. REPAIR WAS ACCOMPLISHED IAW ER/A 532510-14, REV ORIGINAL AND ETI-88-
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