JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 COMA0860133Skin Panel · chafedSKIN PANEL ON RIGHT LOWER WINGTIP FOUND CHAFED THRU AT WS 407. REPLACED DAMAGED SKIN PANEL.SDR COMA0860132Fairing · chafedRIGHT WING TIP FORWARD FAIRING CHAFED THRU ON BOTTOM AT WS 407. REPLACED RIGHT WINGTIP FORWARD.SDR ABXR080065Skin · corrodedLEFT WING UPPER TRAILING EDGE SKIN BULGED, RIVETS CUPPED FORWARD OF SPOILER BOARDS (CENTER). CUT OUT DAMAGE. INSTALLED NEW SECTION OF SKIN AND -9 DOUBLER IAW DC9 SRM 57-30-3, 57-01, FIG 3, 51-30-2 AND 51-30-5.SDR UIEA200800024Panel · crackedLT WING UPPER FIXED T/E PANELS AT STA WBL 445, 11.0 INCHES FROM TRAILING EDGE AND WBL 515, 6.0 INCHES FROM TRAILING EDGE HAVE A 1.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2 SHEETS 3 AND 5, PREPREG LAYUP 250 DEGREES F CURE PSDR KCSA081068Skin · corrodedFOUND CORROSION ON RT WING LOWER SKIN INBOARD BOOST PUMP ACCESS PANEL CUTOUT FLANGE AT WS 679.50.SDR UPS08851678Panel · delaminatedINSPECTION TYPE:C2 RIGHT WING O/B TRAILING EDGE PANEL UPPER FWD. SURFACE IS DELAMINATED. REPAIRED RIGHT WING O/B TRAILING PANEL SURFACE IAW DWG 5644654 AND SRM 51-1-9A.SDR C2XA08IA044Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THESDR C2XA08IA043Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THESDR C2XA08IA042Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THESDR C2XA08IA040Skin · crackedIAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH REINSPECTIONS TO BE MADE AT EVER 50FC, AND THE SDR UPS08851558Doubler · crackedWING INTERNAL DOUBLER CRACKED ABOVE NR 4 FILL VALVE. ACCOMPLISHED STEPS 6A1 THRU 6A4 ON PRELIMINARY EO NR DC8-5730-28500-A DATED 1-28-08. ACCOMPLISHED STEP 6AS-6AG. OK TO INSTALL REPAIR. COMPLETED REMAINING STEPS THRU 6A(9) OF EO DC8-5730-28500.SDR UIEA200800021Skin · crackedLT WING LEADING EDGE LOWER SURFACE, OUTBOARD FUELING DOOR FRAME CUT-OUT HAS A COMPOSITE CRACK AT OUTBOARD SIDE, FORWARD EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 3 AND 5 AND SRM 51-40-12, PREPREG 250 DEGREES F CURE. ALSO,SDR UIEA200800018Skin Panel · delaminatedRT WING LOWER FIXED LEADING EDGE HAS A 12.0 INCH LONG BY 10.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 18, SHEET 1, 2, AND 5, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4757A412.SDR 08FDEA00277Skin · crackedCRACK IN UPPER RIGHT WING OUTBD PANEL AT WBL 602.5, OF OUTBD AILERON REPAIRED UPPER WING OUTBD. PANEL AT WBL 602.5 REF EA NR 7-5720-113964. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR UPS08851575Skin · crackedINSPECTION TYPE:C2 LOWER SKIN HAS CRACK RUNNING OFF RIVET NR 1 PYLON STUB WING. REPAIRED LT OUTBD STUB WING LOWER SKIN REF SRM 57-02-01A-0 FIG 002.SDR 08FDEA00264Skin · dentedRIGHT WING TRAILING EDGE LOWER SKIN SURFACE DENTED INBD OF OUTBD MAIN FLAP INBD END. REMOVED PANELS TO FOM IAW MD/DC10 SRM 51-31-01 VOL II, CUTOUT DAMAGE AREA IAW MS/DC10 SRM 57-00-01 VOL I. MATERIAL ID FOR DOUBLER REPAIR 2024 T-3, .090 PO NR 575582.1, ISDR ABXA080053Skin · crackedLEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-01.SDR ABXA080052Skin · crackedLEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-1.SDR DHL2007873538Skin · crackedLT OUTER WING OTBD L/E UPPER SKIN CRACKED 1" AT STA XW 761.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM DATED 01-12-08 EVA D857-00037 REV IR DATED 01-08-08 REV IR SEMAN DWG NR ED-4670 DATED 12-12-07. REMOVED FASTENERS IAW SRM 51-1-21 SRM 51-1-20D.SDR DHL2007873531Skin · damagedLT WING INBD L/E LWR SKIN HOLES ELONGATED AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-11-08 EVA D857-00033 REV IR DATED 01-04-08 SEMAN DWG ED-4624 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION PLUS FABRICSDR 08FDEA00240Bracket · crackedRT WING O/B MOST UPPER TRAILING EDGE PANEL I/B SIDE SPOILER SEAL BRACKET CRACKED AT AFT EDGE AND AT SPOILER DOWN STOP PAD CUTOUT. REMOVED CRACKED BRACKET AND FABRICATED NEW SEAL DEPRESSOR BRACKET REF BOEING DRAWING 65-21657/ITEM NR 155 AND INSTALLED ON PANEL SDR IXXA08SMN031SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING ON LEADING EDGE OUTER UPPER PART AT STATION XFS 822.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. SDR IXXA08SMN028SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 420.000 STRINGER 5. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR APPLIED SEALANT ON BLEND SDR UPS08851544Structure · missingAPPROX 3/8 BY 1 INCH PIECE OF SHEETMETAL MISSING ON T/E OF WING. LOCATED ON LT WING INBD OF NR 3 SPOILER PANEL. ACCOMPLISHED EO DC8-5730-28460A.SDR 08FDEA00223Skin · crackedRT WING, LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER AS PER EA 1-5740-117298, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR ABXR080034Skin · crackedRIGHT WING LOWER TRAILING EDGE SKIN AFT OF INBOARD BUTE DOOR WAS CRACKED. REPAIRED SKIN IAW DC9 SRM 57-01, FIGURE 3.SDR DHL2007873537Skin · corrodedLT WING CTR L/E EXT SKIN SHOWS CORROSION AT STA XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA-FORM 8110-3 DATED 01-14-08 EVA D857-00034 REV IR DATED 01-05-08 SEMAN DWG ED-4677-1 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSISDR GLBA20061052Skin · crackedMAJOR REPAIR, LT IB LOWER WING SKIN CRACKED APPROXIMATELY .250 INCH IN LENGTH AT THE FORWARD IB CORNER OF FUEL ACCESS PANEL 522DB. MAINTENANCE STOP DRILLED CRACK AND PATCHED IAW SRM 57-20-01.SDR GLBA20061051Skin · crackedMAJOR REPAIR RT LOWER WING SKIN CRACKED APPROXIMATELY .9 INCH IN LENGTH AT THE FORWARD IB CORNER AND AFT OB CORNERS OF FUEL ACCESS PANEL 621AB. STOP DRILLED CRACKS AND PATCHED IAW SRM 57-20-01.SDR IXXA08SMN023SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTER FLAP LOWER PANEL SKIN DENTED AT STATION 164.000 TO STATION XF 186.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITSDR IXXA08SMN022SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING DENTED AT UPPER LEADING EDGE AT STA XFS 7.5000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK, NO CORROSION FOUND. PERFORMED MEASUREMENT DIAMETER FOUND WITHIN ALLOWABLE LIMITS APPLIED PRO-SEAL 735 IAW DC8SDR UPS08651477Panel · crackedLT WING LOWER T/E PANEL CRACKED AND WIGGLE PLATE BROKEN. REPLACED LT LWR WING PANEL 561 GB PER SRM 51-40-00, SEE LP 858182/1. INSTALLED NEW WIGGLE PLATE IAW B767 SRM 51-40-02.SDR 08FDEA00185Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL 541GB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541GB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541GB IAW AMM 28-11-SDR 08FDEA00184Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL 541HB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541HB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541HB IAW AMM 28-11SDR 08FDEA00183Access Panel · corrodedLEFT WING FUEL TANK ACCESS PANEL 542AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 542AB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 542AB IAW AMM 28-SDR 08FDEA00182Access Panel · corrodedLEFT WING FUEL TANK ACCESS PANEL 543AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 543AB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 543AB IAW AMM 28-SDR 08FDEA00181Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL 541DB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541DB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541DB IAW AMM 28-11SDR 08FDEA00180Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL 541FB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541FB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541FB IAW AMM 28-11SDR IXXA08SMN016SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 278.000 STRINGER10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. FILLED WITH SEALANT REWORKED AREA. PERFORMED NDSDR IXXA08SMN015SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 358.000 -371.000, STRINGER 5 TO STRINGER 8. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. FASDR IXXA08SMN009SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) MIDDLE DOOR, DELAMINATED SKIN. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN CENTER DOOR ON RIGHT MAIN LANDING GEAR FUSELAGE. PERFORMED OPERATIONAL CHECK FOR HYD SYSTEM LEAKS, GOOD IAW DC8 MINATESDR IXXA08SMN005SPanel · crackedDURING ROUTINE C CHECK INSPECTION, FOUND WING FUSELAGE PANEL NUMBER 716 FILLET PANEL RIGHT SIDE CRACKED AT STATION 690.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOLSDR IXXA08SMN004SPanel · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER PANEL DELAMINATED AT STATION XF 219 TO XF 339.000. REMOVED DAMAGED PANEL. INSTALLED NEW PANEL IAW DC8 SRM 51-3-0, 51-3-1.SDR 08FDEA00126Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 641JB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641JB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 641JSDR 08FDEA00127Panel · corrodedRT WING FUEL TANK ACCESS PANEL 641HB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641HB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG. 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 6SDR 08FDEA00125Panel · corrodedRIGHT WING TANK ACCESS PANEL 641GB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641GB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 64SDR 08FDEA00124Panel · corrodedRIGHT WING FUEL TANK PANEL 641FB HAS CORROSION ON THE LOWER SURFACE. REMOVED CORROSION ON PANEL 641FB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 641FB ISDR UPS08851541Skin · damagedINSPECTION TYPE:C2 LT WING OUTBD SLOT LWR ACCESS PNL HAS DOUBLE DRILLED HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT WING OUTBD SLOT LWR ACCESS PNL IAW SRM 57-02-00 FIG 002A AND DWG 5769928.SDR TRAX200800088Skin · crackedCRACK FOUND ON RIGHT WING LOWER SKIN AT RIB 19.
SDR IXXA08SMN002SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING CENTER LEADING EDGE OUTER LOWER SKIN AT STATION XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE ARE
Back to JASC 5730