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 CALA2022112303208None · nonePERFORM EA 5310-04554 REV B OP 006 REF. ACCOMPLISHED EA 5310-04554 REV."B" OP-006,NO CRACKS,CONFIGURATIO N "A" ON JOB CARD SEQ#1433 WORKSDR ASAA2022112140903None · noneTHE FLIGHT ATTENDANT REPORTED L2 DOOR WAS DIFFICULT TO OPEN. GROUNDED - YES. PERFORMED OPERATIONAL CHECK OF L-2 DOOR NO DEFECTS NOTED DOOR OPERATES NORMAL C/W OPS CK OF R-2 DOOR BOTH DOOR OPERATE SAME A/C OK FOR SERVICE REF B737-9 AMM 52-13-00.SDR DALA2022112107483None · noneSHIP 3351 LH FRONT FIXED SGS WINDOWS REQUIRES DETAILED INSPECTION AND ELECTRICAL TEST MEASUREMENT PER AMDS 5611-01020-02A. CORRECTIVE ACTION: LH FRONT FIXED SGS WINDOWS REQUIRES DETAILED INSPECTION AND ELECTRICAL TEST MEASUREMENT PER AMDS 5611-01020-02A. (2503SDR DALA2023012600651None · noneSHIP 3308 DURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED AN ERROR REFERENCING AN INCORRECT FIGURE VIEW WITHIN THE WORK STEPS. CORRECTIVE ACTION: ACCOMPLISHED VASDR DALA2023012400576None · noneEM 5716-01017 WAS WRITTEN TO PERFORM THE ACTIONS REQUIRED BY AD 2019-16-07. DURING ACCOMPLISHMENT OF EM -01 AND -02 WORK CARDS, WHICH INCLUDE SB A330-57-3115 AND SB A330-57-3131 INSTRUCTIONS, CERTAIN STEPS FROM THE MODIFICATION SB WERE FOUND TO HAVE AN IMPROPSDR DALA2023011200232None · noneTO CONVERT EX LION AIRCRAFT TO DELTA STANDARDS ACCOMPLISH ALTERATIONS PER VA 97741MA REV IR.SDR DALA2022122308346None · noneDURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461-01, MTC HAS REPORTED AN ERROR REFERENCING AN INCORRECT FIGURE VIEW WITHIN THE WORK STEPS. THIS VA IS ISSUED TO ADDRESS THE WORK CARD UPSDR DALA2022120507761None · noneSHIP 3305 EM 5716-01017 WAS WRITTEN TO PERFORM THE ACTIONS REQUIRED BY AD 2019-16-07. DURING ACCOMPLISHMENT OF EM -01 AND -02 WORK CARDS, WHICH INCLUDE SB A330-57-3115 (INSP) AND SB A330-57-3131 (MOD) INSTRUCTIONS, CERTAIN STEPS FROM THE MODIFICATION SB WERE FSDR DALA2022120207714None · noneDURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED THAT WORK COULD BE ACCOMPLISHED MORE EFFICIENTLY IF CERTAIN STEPS THAT ACCOMPLISH THE MODIFICATION OF DIFFERENT ASDR DALA2022120207721None · noneDURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED AN ERROR REFERENCING AN INCORRECT FIGURE VIEW WITHIN THE WORK STEPS. CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99SDR DALA2022111807444None · noneER/A 584898-14 HAS BEEN REVISED TO 'C' DOCUMENTING THE SECTION I II PERMANENT REPAIR PERFORMED DURING CCK IN MCI. FOLLOW ON ACTIO N IS REQUIRED. SECTION III IS LIMITED TO 6 MONTHS (182 DAYS) FROM 17NOV22. ER/A TO BE REVISED INCORPORATING DAMAGE TOLERANCE EVALUSDR CALA2022111603147None · noneINSTALLED LOCKOUT PIN FOR #1 ENGINE TRUST REVERSER HCU. PLZ REMOVE AND RETURN TO TOOLING AFTER INSTALL IS COMPLETE. REMOVED T/R LOCKOUT PIN.SDR DALA2022120707879None · noneFUSELAGE FRAME BS 1360, S25L TO S27L. EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 603580-14AD. (2497638)SDR DALA2022111707412None · noneSHIP 6802 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA ON STA 1360 LH AT AFT COMPARTMENT CARGO COMPARTMENT. FRAME ON STA 1360 LH AT AFT COMPARTMENT CARGO WAS REPAIRED PER ER/A 603580-14AD REV. ORIGINAL. (2497902)SDR FDEA202211152794None · noneDURING ACCOMPLISHMENT OF EO F-5310-E0347443 AN EXISTING REPAIR WAS FOUND AT STA 1360 INBD OF S26L THAT REQUIRES FURTHER INSPECTION PER EO. COMPLIED WITH EA # F-5310-145326D P6, FUSELAGE-MAINFRAME-LOWER CARGO FRAME REPAIRS AT BS 1320, S26L, BS 1340, S-26L, SDR YENA2022111601129None · noneFLT #101, (AIR RETURN) GEAR WAS DOWN FROM CLIMB UP TO 18000' MAX SPEED WAS 250KTS, 180,000 MAX OUT PER AMM 05-51-12-200-001-S, A/C SPEED INDICATED BY DFDR NEVER EXCEEDED VLE WHILE GEAR REMAINED DOWN AND LOCKED AND WILL NOT REQUIRE ANY INSPECTION. AS PRECAUTIOSDR SWIA2022122967044None · noneCOMPLY WITH: ERJ3095-23 - RE-MODIFICATION OF AFT ATG ANTENNA RETRO-FIT -105 INSTALLATION ON / ERJ175 WIFI ATG4 SYSTEM REV B PART(S) 0 COMPLIED WITH: ERJ3095-23 - RE-MODIFICATION OF AFT ATG ANTENNA RETRO-FIT -105 INSTALLATION ON / ERJ175 WIFI ATG4 SYSTEM SDR ASAA2022111440771None · noneHGS/AUTOLAND EVAL UNABLE TO BE COMPLETED DUE TO ATC. GROUNDED - YES. ACCOMPLISHED LAND VERIFY TEST B737-900 AMM 22-11-00/201. ALL TESTS PASSED. ACCOMPLISHED HGS SYS TESTS. HGS 4000 SMM 34-36-00. ALL TEST PASSED.SDR CALA2022111103100None · noneDISPLACE SEAT ROW 15 ABC TO FOM - REINSTALL ON THIS CARD (IDT) - SUPPORT TASK NSA EMX NR 00013 REMOVED AND REINSTALLED SEAT ROW 15ABC IAW B737NG AMM 25-22-00-0 SYSTEM IAW B737NG AMM 23-34-00-710-801. IN SEAT POWER SUPPLY SYS CHECKED EMERGENCY LIGHT SEAT 15 ABCSDR FDEA202211102748None · noneCTR CARGO COMPT - FRAME AT STA 1661 L48R REQUIRED TO BE SPLIT FOR ACCESS TO LONGERON REPAIR. TOP STRAP OF REPAIR NEEDS TO BE INSTALLED REF SRM 53-00-07-2R NOTE 15-C STEP 1(REF. N1289) INSTALLED STRAP AT FRAME STA 1661 IN BETWEEN L47R AND L48R REF MD11 SRM SDR DALA2022122708389Not Reported · not reportedDURING ENTRY INTO SERVICE WORK PER AA 2500-01852 SECTION 01 ERRORS IN PART NUMBER CALL OUTS WERE DISCOVERED. UTILIZE VA 97739 REV IR WHEN COMPLETING AA 2500-01852 SECTION 01.SDR DALA2022111407328None · noneERA 603429-14 SECTION I ISSUED FOR LIGHTNING STRIKE DOUBLER REPAIR AT FR24, STR9R FOLLOWING FERRY FLIGHT FROM SLC PER ERA 603446-14. FOLLOW ON ACTION IS REQUIRED. SECTION I REPAIR LIMITED TO 8000 FH FROM TIME OF ACCOMPLISHMENT. SECTION II IS TBD AND ERA REVISISDR DALA2022111107288None · noneSHIP 3221 NEED TO COMPLY WITH DTE ERA 585867-14 REV C SECTION VII. CORRECTIVE ACTION: COMPLIED WITH ERA. (2487679)SDR DALA2022111107287None · noneNEED TO COMPLY WITH DTE ERA 585867-14 REV C SECTION VI MONITOR INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA. (2487660)SDR IXXA2022110800005None · none#7 SLAT HAS COMPOSITE DAMAGE MARKED LOWER TRAILING EDGE.SDR CALA2022110403035None · noneADDITIONAL DATA IS NEEDED TO EVALUATED ON EXISTING DOUBLER AS PER ECRA 5330-06364 (LP 6821164) SEE AEROMAN NON ROUTINE 2022-359932 INSPECTION REQUIREMENTS FOR REINFORCING REPAIR GENERATE ANOTHER DIP THAT REFERENCE THE LOGPAGE 78,000 FC BUT BEFORE AIRCRAFT REACSDR FDEA202211022711None · noneAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY BETWEEN XFS = 228.840 AND XFS = 246.301. EXISTING REPAIR DOUBLER AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY BETWEEN XFS=228.840 SDR CALA2022110203023None · noneREF LOG 9823382 A/C REQUIRES PHASE 2 INSPECTION OF HORIZONTAL STABILIZER AND ELEVATORS WITHIN 15 FLIGHT CYCLES AS AMM 05-51-19-00A-311A 05-51-19-00A-311A REF LOG 9823382 A/C REQUIRES PHASE 2 INSPECTION OF HORIZONTAL STABILIZER AND ELEVATORS WITHIN 15 FLIGHT CYSDR DXTA2022103173060Unknown · unknownA VIBRATION OF UNDETERMINED LOCATION. COULD BE FELT THROUGH OUT THE ENTIRE AIRCRAFT. SEEMS TO LESSEN WITH SPEED BUT NEVER GOES AWAY. VIBRATION OCCURRED CLIMBING OUT OF 3000 WITH THE FLAPS & GEAR UP. REMAINED THROUGHOUT THE ENTIRE FLIGHT UNTIL LANDING. BUT IT SDR ANCF20221102032None · nonePILOT REPORT
31.OCT.2022 WO 16'683'222=> OVER WEIGHT LANDING
OVER WEIGHT LANDING DUE TO MEDICAL EMERGENCY LAN WEIGHT 70.0TONS MAX LDGW 67.4 TONS VERT SPEED LESS THAN 300
ACTION TAKEN
01.NOV.2022 WO 16'683'222=> IN ACCORDANCE WITH AIRBUS REFERENCE: 811353SDR DALA2022122708399None · noneCOMPLY WITH VA 99348MA. COMPLIED WITH.SDR DALA2022120807893None · noneEM 5311-0124 REQUIRED UPDATES. CORRECTIVE ACTION: ACCOMPLISHED VA 99348MA SECTION I IN CONJUNCTION WITH EM 5311-01244-01A AND -01B. (2472159)SDR DALA2022103107028None · none(LOG 2472323) EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. BS 500B TO BS 500C BTW STR 24R TO STR 26R AT LOWER FUSELAGE. VERIFIED THAT REPAIR ON EXTERNAL LOC SKIN BS 500B TO BS 500C BTW STR 24R TO STR 26R AT LOWER FUSELAGE WELL MEETS THE GENERALREQUIRESDR DALA2022102806991None · noneDURING LAST H-CHECK (03JAN2019) AT STAG, ER/A 574045-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 0182. ACCOMPLISH ER/A 574045-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR.SDR FDEA202210262736None · noneAGING AIRCRAFT ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON O/B SIDE AT RIB 8A POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETESDR FDEA202210262735None · noneAGING AIRCRAFT ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON I/B SIDE AT RIB 8A POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETESDR R61A2022110300685None · noneREPUBLIC EO 170AD-53-10-0010 STEP 5.C SOLID RIVETS - PROTRUDING HEAD CANNOT BE INSTALLED PER GUIDANCE IN SERVICE BULLETIN 170-53-0051 REV 3 FIG 4 PARAGRAPH 1 (B) 2. ROUTINE TASK CARD COMPLIED WITHSDR DALA2022103107030None · none(LOG 2469749) DURING INSPECTION FOUND FUSELAGE / STA 727C FS 727D / S-2L - S-3L / VIASAT INSTALL / EXISTING DOUBLER. REPAIRED PER ERA 603295.SDR DALA2022103107023Access Panel · corroded(LOG 2468545) DURING INSPECTION FOUND CORROSION ON FUEL ACCESS PANEL 632QB, 632CB, 632FB, 631BB, 632NB, 532NB, 532CB, 532DB, 531BB, 532JB, 532GB, 632EB, 632KB, 632HB, 532HB, 632MB, 112W8201-3. REMOVED CORROSION PER B737-900ER SRM 57-20-01-2R-1 REPAIR 1 PAR. 4 SDR FDEA202210242753None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR24L~26L,FR72~73. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600 SRM 5SDR FDEA202210242734None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR26R~29R,FR77~78. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERMINED SDR ABXA20221122135None · noneDURING AIRCRAFT C-CHECK, CORROSION WAS FOUND IN THE BETWEEN BS 1307 & 1285, S36L. THERE IS A PREVIOUS EXTERNAL REPAIR DOUBLER AT BS 1300, S36L WAS REMOVED FOR DISPLACEMENT OF THE SKIN P/N 146T3211-1. THE MINIMUM REMAINING THICKNESS IS 0.045” THEREFORE IS OUTSDR DALA2022111807441None · noneSHIP 655 ER/A 475076-14AD REV. D; B757 FUSELAGE / SKIN / STA. 590- 661 / STR 14L-19L / SPLICE. CORRECTIVE ACTION: REF ERA 475076-14 (2461137)SDR DALA2023012600673None · none(LOG 2456800) AS PART OF CONVERION OF FORMER AIRCRAFT ACCOMPLISH VA 97737 REV IR IN CONJUNCTION WITH AA2560-01569-01B. ACCOMPLISHED VA 97737MA REV B IN CONJUNCTION WITH JOB CARD 2560-01569-01B.SDR DALA2022120407737None · nonePERFORM INSPECTION ATTACH FITTING ON SERVO CONTROL ACTUATOR SPOILER 1 LH WING AND SPOILER 1, 2, 3, 4, 5, 6 RH WING ALL ATTACH FITTING. ERA 602649-14AD HAS BEEN COMPLIED WITH PRI 602649-14 MATCHES PERFORMED ALL INSPECTION REQUIRED LOCATED ON ATTACHFITTING ON SDR FDEA202210182588None · noneREPAIR (REPLACEMENT) AT RIGHT HAND WING LEADING EDGE CAVITY FORMER AT FORMER XOS 963. EXISTING REPAIR AT RIGHT HAND WING LEADING EDGE CAVITY FORMER AT XOS 963 EVALUATED AND FOUND PART MARK NOT VISIBLE. EXISTING FORMER REMOVED AND REPLACED IN ACCORDANCE WSDR DALA2022120107684None · noneACCOMPLISH ER/A 602362-14 SECTION 01 AT THE NEXT C-CHECK OF THE AIRCRAFT. ACCOMPLISH ER/A 602362-14 SECTION 01 AT THE NEXT C-CHECK OF THE AIRCRAFT. ASSOCIATED ER/A 00-602362 ADDED FOR AC 8129. ACCOMPLISHED AND RECORDED WTBF MODIFICATION PER PRI 602362-14 REV 0SDR DALA2022101806744None · noneSHIP 655 DURING INTERNAL INSPECTION OF THE BROADCAST TV, DOUBLER OF REPAIR DISABLE THE INSPECTION AREA IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC:00677 INSPECTIONS WERE PERFORMED PER PRI 602592- 14 REV 0. AND ERA 602592-14 REV ORIGINAL. (2454596)SDR CALA2022101402799None · corrodedFWD CARGO FRAME 25 STRINGER 41RT-42RT CLEAT HAS CORROSION PER HA ECO LCQ N/R 9296371/20371 GEN BY V052030SDR DXTA2022101371990None · noneMAIN DOOR VISUAL INDICATOR: DOOR CLOSES AND "CLICKS" LOCKED WITH NO CAS MESSAGE OF DOOR OPEN. ALL 6 SIGHT GLASS WINDOWS DO NOT SHOW GREEN OR WHITE STRIPES. PERFORMED MULTIPLE OPS CHECKS OR MAIN CABIN DOOR WITH NO DEFECTS NOTED AT THIS TIME. ALL HATCHED VISU
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