JASC 5730
Service difficulty reports · 27,262
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 DALA2014111106067Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1355C. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS SDR DALA2014111106066Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1367C. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS DOOR WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLE WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAXIMUM DIAMESDR DALA2014111106065Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1371C. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MESURED MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .5SDR DALA2014111106063Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1363, 1462C, MRB 57-31-082. CORROSION ON COUNTERSINK HOLE AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWED IS 0.0532" AND MAX DISDR DALA2014111106062Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1464C. CORROSION ON COUNTERSINK HOLES SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER, ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS .56SDR DALA2014111106061Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1470C. CORROSION ON COUNTERSINK HOLE AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURE MAX DIAMETER ALLOWABLE IS 0.532" IN AND MAX DIAMETER MEASURE IS 0SDR DALA2014111106060Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1365C. CORROSION ON SETTLMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1365C WAS REMOVED IAW SRM 51-22-2A, COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWED IS .532" ANSDR SWIA201440208Skin · dentedRIGHT WING L/E HAS A SMALL DENT WITH A SLIGHT CREASE 57" OTBD OF WS149.58. COMPLIED WITH TEMPORARY REPAIR IAW SRM PERMANENT REPAIR DUE AT NEXT C-CHECK. C-CHECK, HAND DRESSED DENT ON RT WING CENTER L/E PANEL BACK TO ORIGINAL CONTOUR IAW REO.SDR SWIA201440055Panel · chafedRIGHT WING BUTTE PANEL 694PB HAS CHAFE DAMAGE ON UPPER SURFACE. REPAIRED PANEL IAW EA.SDR SWIA201440040Skin · debondedRT WING OTBD L/E 630KL IS DEBONDED. BONDED RT WING OTBD L/E, 630KL IAW REO.SDR SWIA201440038Skin · debondedRT WING INBD L/E 620JL IS DEBONDED. BONDED RT WING INBD L/E IAW REO.SDR FDEA201411074077Skin · delaminatedLEFT WING FIXED TE, OTBD OF OTBD FLAP, 2 AREAS OF SKIN SEPARATION, RIVETS POPPED. REPAIRED IAW EA 6-5730-T0313385. CLASSIFIED AS MAJOR CAT A REPAIR.SDR SWAA2014112634511Skin · crackedLEFT WING LE LOWER SKIN CUT OUT CRACKED AT STATION 666. REPAIRED SKIN IAW SRM.SDR AALA20141107003Skin · corrodedCORROSION ON LOWER CTR WING SKIN RT SIDE UNDER DRAG LINK. REMOVED CORROSION.SDR AALA20141107002Skin · corrodedCORROSION ON LOWER CTR TANK WING SKIN LT SIDE UNDER DRAG LINK. REMOVED CORROSION & REPAIRED AREA IAW ENGINEERING AUTHORIZATION B737-57-037009.SDR SWIA201440122Skin · damagedPANEL 622AR HAS ONE ELONGATED HOLE ON BOTTOM OF SKIN NEAR THE L/E, ON OTBD SIDE OF SLAT TRACK 1-2, HEAD OF SCREW GOES THROUGH THE HOLE. C-CHECK, RO 11/24/14, REPAIRED PANEL 622AR IAW STS EA.SDR DALA2014110705980Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1303C, MRB 57-31-082, LW, AYP, CARD 170, ZONE 10. LT WING FUEL ACCESS DOOR NR 1303C WAS REPLACED IAW SRM 51-22-2A, DUE TO BLEND OUT IS NOT PERMITTED UPPER ACCESS DOOR, PN 3912757 IAW SDR UIEA2014110600582Panel · damagedFUEL LEAK OTBD NR 2 ENG PYLON LOWER WING PANEL 641FB. R & R PANEL & GASKET.SDR FDEA201411053516Former · crackedRIGHT WING FIXED LE SUPPORT FORMER FOUND CRACKED AT XOS 584. FORMER REMOVED AND REPLACED IAW SRM 51-33-01. FORMER FABRICATED IAW DRAWING ARB2931 REVISION H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201411053515Skin · crackedRIGHT WING FIXED LE NR 15 SLAT TRACK CUT OUT FOUND CRACKED XOS 944. REPAIRED IAW SRM 57-40- 02 FIGURE 201, REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201411053514Skin · crackedLEFT WING FIXED LE PANEL 519CB FWD CORNER CUT OUT FOUND CRACKED XOS 610. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201411053513Panel · crackedLEFT WING LE PANEL 518FB FWD CORNER CUT OUT FOUND CRACKED XOS 500. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201411053531Skin Panel · delaminatedLEFT WING TAKEOFF, TE PANEL TOP SKIN PANEL ARC0728-501 DELAMINATED AROUND FASTENERS. REPAIRED LT WING TE PANEL ARC0728-501 IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.SDR ASOA2014112611799Access Panel · crackedRT WING BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. COMPLIED WITH STS EA 32-2014-188. EA 30-2014-188 HAS BEEN ACSDR YENA20141103238Skin · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AT LT WING T/E SKIN AT RIB 7, 8, 15, 16 & 17. REMOVED CORROSION AT LT WING T/E SKIN FOR RIBS 6-9 AND 15-17 IAW A14-714-01.SDR FDEA201411023455Skin · crackedRIGHT WING OTBD FIXED LE, BOTTOM PANEL LAND CRACKED JUST INBD FROM FUEL FILL VLV ACCESS PANEL, MARKED, APPROX AT STATION XORS 885. INSTALLED REPAIR DOUBLER IAW SRM VOLUME I CHAPTER 57-10-00 FIGURE 49.SDR DALA2014103005924Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1454C, MRB 57-31-082, RW, AYP, CARD 174, ZONE 10. CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES WERE REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .532" AND SDR DALA2014103005910Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1307C, MRB 57-31-082, LW, AYP CARD 172, ZONE 10, CORROSION ON FUEL ACCESS PLATE 1307C ON SETTLEMENT AREA AND COUNTERSINK HOLES WAS REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETERSDR DALA2014103005909Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1377C, MRB 57-31-082, LW, AYP, CARD 167, ZONE 10. CORROSION ON SETTLEMENT AREA AND CORROSION HOLES WERE REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .532 AND MAXSDR AALA20141028011Access Panel · corrodedCORROSION ON RT LE AT ACCESS PANEL 621CB BELOW SLAT TRACK. ACCOMPLISHED REPAIR IAW EA B737-57-037145.SDR REXA2014102900906Skin · corrodedLEFT WING LOWER PLANK FUEL ACCESS PANEL 550BB AT WS 54.897 CUT OUT CORRODED 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR IPXA2014103184759Skin Splice · crackedINSPECTION 3C, LEFT WING FIXED L/E INNER SKIN SPLICE STRAP CRACKED AT STA XOS 667.6792. R & R LT WING FIXED L/E INNER SKIN SPLICE IAW SRM 51-33-01.SDR ASOA2014112511789Strap · crackedRT WING LOWER SURFACE CRACK AT WS 148.019. R & R JOINT STRAP IAW SRM 51-42-21 AND 51-42-06. REMOVED JOINT STRAP AND WAS FOUND CRACKED REPLACED JOINT STRAP IAW SRM 51-42-21 51-42-06.SDR REXA2014102900905Skin · corrodedLEFT WING LOWER PLANK FUEL ACCESS PANEL 550HB AT WS 294.048 CUT OUT CORRODED 0.002 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR SWIA201439751Access Panel · damagedFUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTED, INBD & OTBD ENDS. C-CHECK, FUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTING REPAIRED IAW REO.SDR SWIA201440140Panel · damagedBLOWN OUT SCREW HOLE ON LOWER ROW OF L/E PANEL 632AR. REPAIRED THE L/E PANEL IAW EA.SDR SWAA2014102933423Skin · corrodedLEFT WING UPPER SKIN CORRODED AT STATION 198 TE. REPAIRED SKIN IAW EA.SDR SWIA201440152Skin · corrodedLEFT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE SKIN IAW SRM AND FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440150Skin · corrodedLEFT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE RT WING LOWER SKIN AND FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440147Skin · crackedRIGHT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE RT WING LOWER SKIN. FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440145Skin · corrodedRIGHT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE RT WING LOWER SKIN IAW SRM. FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440143Skin · corrodedRT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE RT WING LOWER SKIN. AND FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440141Skin · corrodedRT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED CORROSION FROM THE RT WING SKIN IAW SRM. FOUND TO BE WITHIN LIMITS IAW EA.SDR SWIA201440139Skin · corrodedRT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED THE CORROSION IAW SRM. BLENDED AREA IS WITHIN LIMITS IAW EA.SDR SWIA201440137Skin · corrodedRIGHT WING LOWER SKIN HAD EVIDENCE OF CORROSION. REMOVED THE CORROSION IAW SRM AND EA.SDR SWIA201440135Skin · corrodedRIGHT WING LOWER SKIN HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM AND STS EA.SDR IXXA20150331096Skin Panel · corrodedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. CORROSION AT WS 800 UPPER SURFACE. REPAIRED LT WING UPPER SKIN PANEL & WS 800 IAW ENGINEERING DOCUMENT 47089REA22.SDR ASMF201501007Skin · dentedDURING TRANSIT CHECK, IT WAS DETECTED A LIGHTNING STRIKE IN THE RIGHT LOWER WING SKIN. PERFORMED A LIGHTNING STRIKE INSPECTION IAW AMM DMC-B787-A-05-51-19-00C-280B-A, DETECTING A DENT IN THE STATION 268.70 BETWEEN STRINGER L 13-14, RIB 3-4 WITH DAMAGES OF 2.0SDR SWIA201439765Skin · damagedRIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640CT HAS FRETTING. C-CHECK, FRETTING TO RT UPPER WING SKIN AT PANEL 640CT REPAIRED IAW EA.SDR SWIA201439764Skin · damagedRIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640BT HAS FRETTING. C-CHECK FRETTING TO RT UPPER WING SKIN AT PANEL 640BT REPAIRED IAW EA.
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