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 7C7A2019102200515Skin · noneTHE REMOVAL OF AN EXISTING STC VHF ANTENNA INSTALLATION ON BOTTOM FUSELAGE SKIN PANEL ASSEMBLY, LOCATED BETWEEN X291.40 - X312.35 AND BETWEEN STRINGERS 30P - 31P. PERMANENT REPAIR FOR THE REMOVED STC VHF ANTENNA IS INSTALLING A EXTERNAL DOUBLER WHICH WILL BE SDR AALA201910219040Engine · noneAIRCRAFT NOT GROUNDED: FLIGHT DIVERTED TO ATL ON ACCOUNT OF RIGHT ENGINE FUEL LEAK. RAMP REPORTS FUEL DRIPPING FROM #2 ENGINE DRAIN SHROUD. EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED #2 ENGINE ACTUATORS TEST IAW AMM 71-71-00, ALL TEST PASSED, NO LEAKS NOTEDSDR DALA2019102296078None · none(AIRCRAFT 6816, L/P 1321678) COMPLY WITH ERA 573400-14 REV B SECTION III. PERMANENT REPAIR. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE REPAIR REF ERA 573400-14 REV B SECTION III.SDR DALA2019102286076None · none(AIRCRAFT 668, L/P 1320475) DUE TO REPAIRS INSTALLED ON L/H SIDE OF A/C, UNABLE TO COMPLY WITH INSPECTION OF FUSELAGE SKIN LAP PER CARD 5331-01282-03. REPAIRS LOCATED: STA. 445-564, (ERA 498897-14) STA 588-596. CORRECTIVE ACTION: C/W PRI 498897-14 REV 2 RECEIVSDR CALA2019101801775None · noneSUPPORT TASK TAR DURING ACCOMPLISH EA 2500-07893 REV A OP 001, STA 753-848 BL 20 SEAT TRACK - REWORK FOUND EXISTING REPAIR AT LBL 33 STA 846 WILL INTERFERE WITH INTERCOSTAL INSTALLATION. PLEASE ADVISE. REF NR LP 9130872 CABIN STA 782 TO STA 911 LBL 33 FLOOR BESDR DALA2019102326103Structure · damagedFLT CREW SUSPECT LIGHTNING STRIKE ON RH SIDE. C/W LIGHTNING STRIKE INSPECTION PER B767 AMM 05-51-19-212-001. FOUND 16 RIVETS BURNT STA 196.5 / 212.5 / 220.5 / 236.5 / 246 / 266.5 / 267 / 317 / 325 / 347 / 355 / 368 ON RH SIDE FUSELAGE. DAMAGES WITHIN LIMITS PESDR R61A2019100491172Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 ST 26-27L. REMOVED AND REPLACED SHEAR CLIP FR17 ST 26-27L REF EMB SRM 51-40-08, 51-23-06,
CPM 51-25-00. A/C REMAINS IN CHECK.SDR R61A2019100491955Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 16 ST 25R-26R. REMOVED AND REPLACED SHEAR CLIP @ FR16 ST 25R-26R REF SRM 51-40-08, 51-23-06, CPM
51-25-00. A/C REMAINS IN CHECK.SDR DALA2019102426123None · none(AIRCRAFT 6816, L/P 1277371) REPLACE A SECTION OF FUSEALGE SKIN PANEL PER BOEING 757-200 SRM 53-30-01, REPAIR 2 TO ELIMINATE EXISTING REPAIR CORRECTIONS AND DTA REQUIREMENTS. ACCOMPLISH SECTION III OF ER/A 573400-14 REV. B AT NEXT C-CHECK OR WITHIN 60 DAYS WHISDR SWIA2019101846531Structure · damagedWHILE INCORPORATING SB 601R-57-046 REV C, FOUND 1EA. OVERSIZE (#14) FASTENER HOLE (C-CHECK) RO: 10/16/2019 REPAIRED IAW REO.SDR FDEA201908262020Access Panel · corrodedINTERNAL CORROSION ON DRAIN ACCESS PANEL DOUBLER R/R DOUBLE AND REPAIRED SHEAR TIE REF J.PF. (SEE NR0030). REMOVED AND REPLACED CRACKED INTERCOATAL REF NR00029 JPF. 475227 09-06-20119.SDR SWIA2019101746497Panel · damagedVISOR 326AR FAILED GAP CHECK. (C-CHECK) RO: 10/16/2019 PANEL 326AR FOUND TO BE OUT OF LIMITS IAW SRM.SDR SWIA2019101746496Panel · damagedVISOR 326AL FAILED GAP CHECK. (C-CHECK) RO: 10/16/2019 PANEL 326AL FOUND TO BE OUT OF LIMITS. ORDERED AND RECEIVED AND INSTALLED NEW PANEL IAW SRM.SDR FDEA2019082862020Access Panel · corrodedINTERNAL CORROSION ON DRAIN ACCESS PANEL DOUBLERSDR CVGA20190826001Unknown · unknownCREW REPORTED NO ROTATION AT VR. ABORTED TAKEOFF, HOWEVER, WAS UNABLE TO STOP BEFORE OVER-RUNNING THE RUNWAY. CREW EVACUATED ALL PASSENGERS AND ALL WERE ACCOUNTED FOR. AIRCRAFT SUSTAINED FIRE DAMAGE FOLLOWING THE EVENT.SDR SWIA2019100246383Panel · damagedPNL 684AB HAS ELONGATED SCREW HOLE. REPLACED UNSERVICEABLE PANEL 684AB IAW SRM.SDR FDEA201908071844Floor Support · noneEXISTING REPAIR FOUND ON FLOOR SUPPORT STRUCTURE BS 570 APPROX. LBL 10. REPAIR REQUIRES EVALUATION TO
DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA EVALUATION CARRIED OUT OF
EXISTING REPAIR ON FLOOR SUPPORT STRUCTURE AT BSSDR SWIA2019100246375Skin · chafedFUEL ACCESS CUTOUT 510AB SHOWS SIGNS OF CHAFFING (C-CHECK) RO: 09/28/2019 / REMOVED DAMAGE RESTORED FINISH IAW REO.SDR AALA2019080769019Unknown · vaporAIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER TAKE OFF FROM DFW, TRAILING FUEL VAPER NOTED OFF RIGHT WING TIP. MAINTENANCE FOUND NO EVIDENCE OF FUEL AT RIGHT WING TIP IAW AMM 28-11-00. OK FOR SERVICE.SDR SWIA2019080146108Unknown · unknownON DEPARTURE AIRCRAFT MADE A SUDDEN AND ABRUPT VEER TO THE LEFT. BLOWN TIRE WAS SUSPECTED. ON LANDING, HIGHER THAN NORMAL VIBRATION FELT FROM MAIN LANDING GEAR. FLT 3482. TROUBLESHOT AN ABRUPT VEER TO THE LEFT ON DEPATURE, WHERE A BLOWN TIRE WAS SUSPECTED.SDR 2020FA0000398Servo · overtorquedFOLLOWING A FATAL ACCIDENT, TESTING OF THE CLUTCH TENSION OF THE PITCH SERVO REVEALED THE BREAKAWAY FORCE NEEDED WAS 45 LBS. THE SPECIFIED REQUIRED CLUTCH TENSION BREAKAWAY FORCE SETTING IS 13 +/- 2 LBS. THIS SETTING IS ACHIEVED BY TIGHTENING THE CASTLE NUT SDR VNAA2019061871101Unknown · unknownIMMEDIATELY AFTER LIFT-OFF, CREW HEARD LOUD NOISE THEN VIBRATION. CREW DECIDED TO RETURN TO CLT. UPON CHECKING THE SYSTEMS, THEY FOUND THAT THE ADG HAD DEPLOYED. AIRCRAFT LANDED OVERWEIGHT, BUT WITHOUT INCIDENT AND WAS ABLE TO TAXI TO THE GATE UNDER ITS OWN POSDR SIMA201906110005Unknown · oscillatesMAX ABORT T.O AIRCRAFT OSCILLATING ABOVE 90-100 MPH, A/C PULLS TO THE RIGHT DURING TAXI. PERFORMED GVI OF MLG IAW AMM 32-11-00 PERFORMED OPS CHECK OF BRAKES IAW AMM 32-43-00.OPS CHECK GOOD. INSPECTED NLG TORQUE LINKS AND TIRES IAW CRJ 700 AMM 32-42-01 AND 32-SDR YV3R201906200123Connector · unlockedCUSTOMER REPORTED CONNECTOR ASSEMBLY P/N: C628-6 UNLOCKS AT RANDOM TIMES.SDR YV3R2019060620114Panel · crackedCUSTOMER REPORTED PANEL ASSEMBLY P/N: A305-6 IS CRACKED.SDR ASMF20190613011Aileron · handler errorDURING TAXING, THE RIGHT WING AILERON WAS HIT BY LIFT TRUCK. MAINTENANCE PERSONNEL PERFORMED GROUND HANDLING EQUIPMENT HITS AIRPLANE CONDITIONAL INSPECTION IAW AMM DMC-B787-A-05-51-58-00A-280A-A, DETECTING RH WING AILERON WITH DAMAGES, THE RH WING OUTBOARD LOWSDR DALA2023011700330None · noneSECTION I REPAIR TO LT VERTICAL STABILIZER SKIN PANEL REQUIRES SECTION II REPETITIVE VISUAL INSPECTIONS EVERY C-CHECK OR 24 MONTHS (WHICHEVER OCCURS FIRST). THIS REWORK IS ACCOMPLISHED PER ERA 577568-14. ACCOMPLISHED DVI PER ERA577558-14, REV 0, SECTION II, SDR AALA201904229005Unknown · unknownAIRCRAFT WAS GROUNDED: ABORTED T/O BELOW 60 KTS. NO BRAKES APPLIED, THRUST REVERSER, LONG ROLL OUT. AS PRECAUTIONARY MAINTENANCE ACCOMPLISHED GEN VISUAL INSP OF TIRES/WHEELS ASSYS. NO DISCREPANCIES NOTED.SDR AALA201904169004Not Reported · not reportedAIRCRAFT NOT GROUNDED: PILOT REPORTS TAKEOFF REJECTED AT 60 KTS WT 152.6 MEDIUM BRAKING. MAINTENANCE ACCOMPLISHED CARD 05-96-17, NO DEFECTS NOTED.SDR SWIA201904095733Unknown · fireRTG DUE TO EFAD BATTERY ISSUE ON TAXI OUT. FLIGHT ATTENDANTS REPORTED FIRE WAS CONTAINED WITH WATER, FIRE CONTAINMENT BAG AND HALON EXTINGUISHER. DECLARED EMERGENCY AND INSTRUCTED FIRE DEPARTMENT TO MEET US AT GATE. RECEIVED SMOKE AFT LAV WARNING MESSAGE DUE TSDR DALA2024031903492None · noneSHIP 699 ACCOMPLISH SECTION II FRAME INSPECTIONS OF ER/A 556014-14. THE SUBJECT ER/A IS AT REV A. CORRECTIVE ACTION: REF ERA 556014-14AD. (1013115)SDR DALA2023011700329None · noneAD 2018-11-14 AMOC APPROVAL REQUIRES REPETITIVE INSPECTIONS EVERY 12000 CYCLES OR 32000 HOURS (WHICHEVER OCCURS FIRST) PER ERA 576744-14AD. ACCOMPLISHED REPETITIVE INSPECTION AS PER ER/A 576744-14AD REV B SECTION II . FOUND NO CRACK.SDR 2020FA0000094Collar · missingSWITCH PIN GUIDE COLLAR FOUND MISSING. ALLOWS SWITCH PIN TO WOBBLE IN SWITCH HOUSING. HARD TO SEE UPON INSPECTION.SDR DALA202203801499None · noneSHIP 3323 PD: REPAIRED PER SRM 57-40-00-300-007 SRI INSPECTION REQUIRED PER 57-40-00-205-007 TABLE 006. SPECIAL DETAIL INSTRUCTIONS PER 2.A. ( 3 ). ( C ). SDR RECORDABLE PER A330 REPORTING REQUIREMENTS TABLE PAGE 12 TASK 57-40-00-300-007. CA: REPAIRED PER SRM SDR 2020FA0000127Belt · brokenCLUTCH BELTS BROKE IN FLIGHT. REASON UNKNOWN.SDR CA190307005Leaf Spring · cracked(CAN) WHILE CREW WAS LOWERING FORWARD BELLY COWLING, INSIDE THE HANGAR, A LOUD BANG OCCURRED AND THE COWLING WAS PULLED OUT OF THEIR HANDS. THE RIGHT HAND ANTI-VIBRATION WEIGHT ASSEMBLY FELL ON THE FLOOR. UPON FURTHER INSPECTION A LEAF WAS FOUND TO HAVE CRACKESDR ASMF201904230014None · noneDURING TRANSIT CHECK, DOOR 2 SLIDE RAFT LH SLIDE WAS DEPLOYED. MAINTENANCE PERSONNEL REPLACED THE DOOR 2 SLIDE RAFT LH SLIDE I.A.W. DMC-B787-A-25-66-01-01B-720A-A, ALL CORRECT.SDR DALA2023012300506None · noneSHIP 191 AD 2018-11-14 AMOC APPROVAL REQUIRES REPETITIVE INSPECTIONS EVERY 12000 CYCLES OR 32000 HOURS (WHICHEVER OCCURS FIRST) PER ERA 574676-14AD. CORRECTIVE ACTION: ER/A 574676-14AD REVISED TO REV. A. ACCOMPLISH ER/A 574676-14AD REV A SECTION II INSPECTIONSSDR SIMA201812264001Oil System · within limitsHIGH SPEED ABORT TAKEOFF AT 80KTS DUE TO #2 ENGINE OIL PRESSURE BEING IN THE CAUTION RANGE IN TAKE OFF POWER. PRESSURE WAS ABOUT 150-155 PSI AFTER ABORT ALL INDICATION WAS IN TH GREEN.CORRECTIVE ACTION PERFORMED POWER ENGINE WITH CREW OIL PRESSURE INDICATION MSDR GTIA2018112972981Panel · looseDURING CLIMB VERY STRONG VIBERATION WERE FELT. CLIMB SPEED WAS 332/.79. REDUCED SPEED TO 300/.78 VIBERATION DISAPPEARED, F/A REPORTED ALO THE SAME-T/S VIBERATION IAW TSM 05-5000-810-801-A FOUND PANEL 192BT LOOSE. TIGHTENED IAW 53-35-00SDR DALA201811206731Wing · mismanufacturedAIRBUS AOT A57P011-18-00 EXPLAINS THAT SOME WING RIB TO WING LOWER SKIN GAPS WERE NOT FILLED IN PRODUCTION AS REQUIRED. UNFILLED GAPS COULD ALLOW CONTACT AND SPARKS AND POTENTIAL EWIS CONCERNS. WORK TO BE COMPLETED, APPLY ADHESION PROMOTER, MIX AND POUR SEALANSDR UIEA2018111402606None · noneEVIDENCE OF BIRD INGESTION ON ENG #1 INLET COWL AT 1230 POSITION (FACING ENG) AND OUTLET GUIDE VANE AT 1130 POSITION(<P>COMPLETED GVI #1 ENGINE NOSE COWL AND ENGINE INTAKE AND FOUND EVIDENCE OF BIRD STRIKE AT 1230 POSITION ON INLET COWL IAW B767 AMM 05-51-18. SDR CALA2018111202354Floorbeam · mechanic errorREFER NR L/P 9131013 B767-53-3-6222 CABIN STA 256.25 RBL 59 FLR PNL SUPPORT BEAM FOUND EXTRA SCREW HOLE CABIN STA 256.25 RBL 59 FLOOR SUPPORT BEAM REPAIRED AS PER ECRA 5310-07545 REV- AND ATTACHED FORM 44.0008 ITEM 1-15 ACCOMPLISHED ADD EMP:V898555 RII APPROVESDR CALA2018111202353None · noneREF ECRA 5331-02292 AC 278, FUSELAGE SKIN BET. STA 500D & 500E A ND BET. STR 22R & STR 25R. PART 1 ITEM 18 ACCOMPLISH INSPECTION REQUIRMENTS ON OR BEFORE THE AC REACHING 50,000 TOTAL AC FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 47,000 CYCLES BU T SDR CALA2018111202352None · noneREF ECRA 5311-02041 AC 278 LOWER AUXILIARY SILL STR 23L OUTER CH ORD INTERIM REPAIR, PART 1, ITEM 19 - INITIAT A DIP TO ACCOMPLIS H INSPECTION REQUIRMENTS ON OR BEFORE THE AIRCRAFT REACHING 75,0 00 TOTAL AIRCRFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING SDR I5EA2018111200001None · noneDISCREPANCY: GROUND PERSONNEL REPORTED SMOKE COMING FROM A MOTORIZED W/C WHEELCHAIR, WHEN OPENING CARGO COMPARTMENT, WHEELCHAIR REMOVED, NO VISIBLE DAMAGE NOTICED BY FLIGHT CREW TO FORWARD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED CARGO DETECTION SYSTSDR CALA2018111202349Floor Support · none(B757-53-3-0488) HEAVY BLUE WATER ON FLOORBEAM STRUCTURE BELOW R 1 ENTRY FLOORBEAM AND ABOVE NLG WW UPPER WEB STA 350 TO STA 365 BL-0 TO RBL 25. REF VTSAA NR 0027692. CLEANED, NEUTRALIZED, PERFORMED DVI AND APPLIED CIC TO FLOOR BEA M STRUCTURE BELOW R1 ENTRY FSDR ANCF201811080015None · noneDURING CLIMB SEVERAL BIRDS STRIKES ON NOSE AND WINGS.SDR SIMA20181107002None · pilot errorAIRCRAFT NOT PRESSURIZING. CLIMBING THROUGH 10,000 FEET WE NOTICED CABIN ALTITUDE IN THE AMBER AND INDICATION AROUND 9400 FT. DESCEND BACK TO 10,000 AND RETURNED TO DFW. DID NOT TRY MANUAL PRESSURIZATION.-C/A-SUSPECT AIRCRAFT IN INCORRECT CONFIGURATION FOR CABSDR C77A2018110700001None · noneTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH THE INSTRUCTIONS THAT ARE SPECIFIC TO THE RH HORIZONTAL STABILIZER FROM SB 170-55-0014, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING HORIZONTAL STABILIZER RIBS 10A, 11A, AND 12A WITH NEW,
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