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 K11A2022062900133Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 747 BETWEEN STRINGERS 8L AND 9LSDR K11A2022062900132Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 747 BETWEEN STRINGERS 8R AND 9RSDR K11A2022062900131Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 867 BETWEEN STRINGERS 8R AND 9RSDR DXTA2022060163100None · noneENGINE FOD: WHILE DEPARTING OUT OF FTW THE LEFT ENGINE INGESTED A LARGE BALLOON. A PIECE OF IT IS STILL STUCK BETWEEN THE FAN AND THE COWL. NO VIBRATIONS NOTED OR ANY ENGINE ABNORMALITIES.//CORRECTIVE ACTION//WE ARRIVED ONSITE AND DID THE INITIAL INSPECTION. WSDR IXXA2022060305Stringer · corrodedBULK CARGO FLOOR SUPPORT STRINGER CORRODEDSDR HNAA2022053100218None · nonePDIS 692 05-50 2708471 27MAY22 ROA CLOSE
SEVERE TURBULENCE ENCOUNTERED IN FLIGHT. (CAPTAIN ANSWERED 1.SEVERE 2. AUTOPILOT WAS ON 3. A/C OUT OF CONTROL - NO 4. CHNG IN ALT OR ATT - NO 5. VARIA IN AIRSPD - +/- 10 KNOTS 6. ANYTHING ELSE - NO 7. YESDR CALA2022053001372Coupling · corrodedFR 64 STRG 44 AND 43R COUPLINGS REMOVAL OF STRINGER COUPLINGS LOCATED AT STRG 43R-44 UNDER FR 64 REQUIRED FOR CORROSION EVALUATION ON FR 64 BUTTSTRAP AFT SIDE BETWEEN STRG 43R-44. AS NOTED ON LTPR NR# 5001146904-0030. EVALUATED CORROSION ON COUPLINGS ON STR''SSDR CALA2022053001368Stringer · corrodedSTRINGER 44 CORROSION BTWN FR64-65, DURING REMOVAL OF COUPLING AT FR 64 STRG 44 FOUND CORROSION SPOT ON STRINGER 44 WEB EVALUATION IS REQUIRED AS NOTED ON LTPR NR#5001146904-0040. PREFORMED REPAIR OF THE FR64 STR44 PER ECRA 5341-1316 AND EO-A32F-53-12768-00-FISDR CALA2022053001367Door Seal · corrodedCORROSION ON DOOR SEAL ATTACHEMENT HOLE UNDERNEATH GIRT BAR FITTING AT FR66 R2. (A3NB-53-3-6222, SEQ#1980, ZONE 262) LTPR NR# 5001144991-0010. REF LTPR BQN LOG 5001144991-0010. FOUND CORROSION ON DOOR SILL PERFORMED REPAIR IAW A320 SRM 53-41-14-300-001 REPAIR SDR HNAA2022052700216None · noneOIL LEAK COMING FROM THE #1 ENGINE. ALSO HAD FAINT OIL BURNING SMELL AT T/O POWER. CLEANED OIL FROM LOWER COWL AND GROUND RAN ENGINE WITH CREW. NO LEAKS NOTED IN LOWER COWL OR EXHAUST SECTION OF ENGINE. SUSPECT OIL IN COWLING IS FROM SERVICING. HOWEVER, OIL BSDR N6WA2022061506Attach Angle · corrodedR/H MLG TIRE BURST PANEL ANGLE HAS CORROSION. R&R R/H MLG TIRE BURST PANEL ANGLE IAW CRJ SRM 51-42-20 , SRM 51-23-00.SDR N6WA2022061505Attach Angle · corrodedL/H MLG TIRE BURST PANEL ANGLE HAS CORROSION.R&R L/H MLG TIRE BURST PANEL ANGLE IAW CRJ 700 SRM 51-42-20.SDR IXXA2022061003Pressure Web · corrodedCORROSION ON FWD SIDE OF AFT PRESSURE DOMESDR IPXA2022060182728None · noneINSPECTION TYPE:SEG4, DURING ACCOMPLISHMENT OF E.O.# B757-5310-73926-A. FOUND EXISTING REPAIR AT STA 1480, S-25R TO S-27R REQUIRE ENGINEERING ASSISTANCE FOR ALTERNATIVE INSPECTIONWORK PER UPS E.O. B757-5310-83543-A, UPS RCD 262045, AND VTMAE E.A. 757-5360-27-SDR JJBA20220518035None · noneDAMAGE TO LH LOWER COWLING ON THE FWD LEADING EDGE. BLENDED DAMAGE, INVESTIGATED DAMAGE - NO CRACKS NOTED. PERFORMED HFEC ON BLENDED AREA. NO CRACKS NOTED.SDR FDEA202205101175Flap · noneAGING AIRCRAFT INSPECTION ,EXISTING REPAIR LOCATED ON R/W I/B FLAP ,L/E NOSE PANEL ,I/B OF MFSTA 153.43,DOES NOT CONFORM WITH PREVIOUS REPAIR DOCUMENTS AND TO CURRENT SRM REPAIR 57-53-01-2R. REPAIRED PER B757 SRM 57-53-01-2RSDR CALA2022051101204None · corrodedCORROSION ON L1 INNER CHORD AT STA 330.62 (REF. AAR NR 99934740) .SDR CALA2022050601157None · corrodedREF AMES NR 0100-0200 ALC DOOR CUTOUT SILL PLATE UNDERSIDE FOUND TO BE CORRODED @ STA. 1400-1410 WHILE ACC OMPLISHING REPAIR @ STA. 1390. REMOVED AND REPLACE ALC UPPER CORD AT DOOR THRESHOLD, WITH NEW P ART P/N: 146N8522-51 IAW BOEING DRAWLING: 146N8522-REV A SDR CALA2022042901104None · noneDURING O2 SERVICING OF CREW OXYGEN, THE VERTICAL O2 BOTTLE SPARKED AND FLAMED ELECTRICALLY AT OPEN/CLOSE VALVE CAUSING BURNS TO LOCAL MATERIALS AND DESTROYING THE VALVE. DUE TO HEAT DAMAGE ACCOMPLISH THE FOLLOWING INSPECTIONS SRM 51-11-03-00A-284A-A SRM 51-13-SDR FDEA202204261333None · noneSUSPECTED REPAIR/SPLICE OUTER CREASE BEAM R/H STA 1400-1420 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.O # F-5310-T0368544, CREASE BEAM OUTBOARD CHORD, STA 1400-1420, S-17R, EXISTING UNAPPROVED REPAIR, PERMANENT REPAIR. MAJOR REPAIRSDR FDEA202204261326None · noneUNDOCUMENTED EXISTING REPAIR ON L/H WING INBD FLAP OUTBD TRAILING EDGE LWR SKIN ADJACENT NO 5 SPOILER PERFORMED WORK STEPS PER EA 000710. MAJOR REPAIR.SDR FDEA202204261325None · noneUNDOCUMENTED EXISTING REPAIR ON L/H WING INBD MAIN FLAP LWR SKIN APPROX WS 231.5 PERFORMED WORK STEPS PER EA 000711SDR FDEA202204261302None · noneUNDOCUMENTED EXISTING REOAIR/SPLICE AT AFT CARGO STA 1540-1560 RBL 13 THIS REPAIR COMPLY WITH SRM 53-60-53-2R, NO DAMAGE OR DEVIATIONS NOTED, AND PERFORMED REPAIR ASSESSMENT PER E.O F-5100-7-5001. MAJOR REPAIRSDR FDEA202204261301None · noneSUSPECTED REPAIR ON APU FIREWALL AT STA 1885.2 UPPER PART (APU SUPPORT STRUT L/H SIDE) THE REPAIR COMPLY WITH SRM 53-80-08-2R, NO DAMAGE OR DEVIATION NOTED, AND REPAIR EVALUATED PER EO F-5100-7-5001. MAJOR REPAIRSDR FDEA202204261300None · noneUNDOCUMENTED EXISTING REPAIR ON APU FIRE WALL AT STA 1885.2 LWR PART THIS REPAIR COMPLY WITH SRM 53-80-08-2R, AND NO DAMAGE OR DEVIATIONS NOTED, AND REPAIR ASSESSMENT PERFORMED PER E.O F-5100-7-5001. MAJOR REPAIRSDR FDEA202204261232Skin · noneUNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 LBL 7" DIMENSION 4.5"-5.0" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R.REF. SRM 53-80-01-2R REV. SDR FDEA202204261230Skin · noneUNDOCUMENTED EXISTING REPAIR BETWEEN STA 1918.9-1941 RBL 16.5" DIMENSION 4.3"-4.2" PERFORMED DVI INSPECTION PER SRM 51-10-08 AND TAP TEST PER SRM 51-10-06, FOUND EXISTING REPAIR WITHIN GOOD CONDITION AND PERFORMED PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R.RSDR FDEA202204251330None · noneCABIN STA 680 FOUND CORROSION ON BEAM EXISTING REPAIR LBL22-RBL12 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368538, SECTION 43, FLOOR BEAM ASSY, STA 680, UPPER CHORD, LBL 25 TO RBL 12, CORROSION, REPAIR MAJOR REPAIRSDR N6WA2022042202Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK FS477.00 TO FS693.00. R&R FLOOR SEAT TRACK @ FS477 TO FS693 IAW CRJ 700 AMM 53-00-49.SDR N6WA2022042201Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK FS349.00 TO FS477.00. R&R SEAT TRACK FROM FS349 TO FS477 IAW CRJ AMM 53-00-49.SDR IXXA2022042101None · damagedAREA OF CORROSION UNDER BUBBLED UP PAINT AT FWD LOWER CORNER OF APU INLET DOOR FRAME DURING BLEND OUT REVEALED 3/4 INCH CRACK IN SIDE FAIRING SKIN.SDR DALA2024031503361Skin · noneSHIP 6821 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 592742-14. CORRECTIVE ACTION: SEE LOGPAGE 0241621 FOR NEW TIME CONTROL LIMITS. (2204476)SDR DALA2024031303311None · noneSHIP 6821 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 592742-14 REV A. CORRECTIVE ACTION: REF ERA 592742-14AD. (2204475)SDR N6WA2022042103Support Angle · corrodedCORROSION FOUND ON 280 BEAM @ SHEARBOX AND COCKPIT FLOORBOARD ANGLE.R/R FLOOR ANGLE SUPPORT IAW CRJ SRM 51-42-21SDR FDEA202204150969Floorboard · damagedZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1610229 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202204150968Floor Panel · damagedZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1610312 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202204150966Floorboard · damagedZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1610228 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202204150965Floorboard · damagedZONE 220 FLOOR BOARD 221MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MAF ON VT MAE TRAVELER T22/1610230 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR N6WA2022041304Support Bracket · corrodedCORROSION ON BELLY AVIONICS COMP FLOORBOARD , FWD SUPPORT BRACKET AT FS280SDR N6WA2022041303Track · corrodedFWD CARGO BAY, AFT #3 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, AFT #3
TRACK IAW CRJ 700 AMM 25-51-02.SDR N6WA2022041302Track · corrodedFWD CARGO BAY, FWD #4 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, FWD #4
TRACK IAW CRJ 700 AMM 25-51-02.SDR N6WA2022041301Track · corrodedFWD CARGO BAY, FWD #3 TRACK HAS CORROSION. REMOVED AND REPLACED FWD CARGO BAY, FWD #3 TRACK IAW CRJ 700 AMM 25-51-02.SDR DALA2024081408117None · noneSHIP 3259 DISC: DTA MONITOR INSPECTION LOG REFERENCE ER/A 597426-14 SECTIONII REQUIRES DTA APPROVAL WITHIN 30,600 CYCLES AFTERSECTION I REPAIR. C/A: DISCONTINUE REVENUE SERVICE WITHIN THE NEXT 30,600 CYCLES AFTER SECTION I REPAIR PENDING A DAMAGE TOLERANCE ANDSDR DALA2024081408116None · noneSHIP 3259 DISC: DTA MONITOR INSPECTION LOG REFERENCE ER/A 597425-14 SECTION II REQUIRES DTA APPROVAL WITHIN 30,600 CYCLES AFTERSECTION I REPAIR. C. C/A: DISCONTINUE REVENUE SERVICE WITHIN THE NEXT 30,600 CYCLES AFTER SECTION I REPAIR PENDING A DAMAGE TOLERANCESDR FDEA202204061339None · noneEVALUATE REPLACED PART AT FRAME AT STA 231.25 BL-0 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368488, FRAME AT STA 231.5 BTWN LBL-20, RBL-20, REPLACEMENT OF NON SATISFACTORY FRAME REPAIR. MAJOR REPAIRSDR FDEA202204061328None · noneEVALUATE EXISTING REPAIR AT FRAME AT STA 1000 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-150687B, FRAME SPLICE REPAIR AT STA 1000 BETWEEN S-5L & S-5R. MAJOR REPAIRSDR FDEA202204061327None · noneEVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 340 RBL-53-LBL-53 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0368523, FLOOR BEAM AT STA 345, BTW LBL 53 TO RBL 53, SRM REPAIR WITH MINOR DEVIATIONS MAJOR REPAIRSDR FDEA202204061304None · noneEVALUATE EXISTING REPAIR AT FRAME AT STA 1020 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA # F-5310-150688 B, EXISTING REPAIR AT FRAME STA 1020 B/T STR 5L -5R. MAJOR REPAIRSDR FDEA202204061303None · noneEVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 377 LBL-45 PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA# F-5310-T0368447: EXISTING REPAIR AT STA 377, BETWEEN RBL17 AND LBL 45, TRACKING MAJOR REPAIRSDR FDEA202204061286None · noneEVALUATE EXISTING DOUBLER REPAIR AT FUSELAGE SKIN BETWEEN STA 1701-1720 STR 15L- 17L PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5330-T0368557, STA 1701-1720 S-15/S-16 L, EXISTING EXTERNAL REPAIR , DEVIATION FROM APPROVED DATA,
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