JASC 5712
Service difficulty reports · 6,970
Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712' 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 = '5712' 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 SWIA200413294Rib · crackedLT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). COMPLIED WITH 1 THROUGH 9 OF REO 601R-57-51-046. FAB. PARTS FROM 56144-4 ANGLE .063 AND 7075T6 .050, PO 358501/1. PERFORMED REPAIR NR 1.SDR SWIA200413293Rib · crackedRT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED DAMAGE AND INSTALLED REPAIR PARTS DOUBLER AND FILLER IAW REO 601R-57-51-046 REPAIR 1.SDR 04FDEA01116Rib · crackedRIGHT WING - NR 16 SLAT TRACK INBOARD RIB SUSPECTED CRACK AS MARKED. RIGHT WING - NR 16 SLAT TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL 2.SDR 04FDEA01113Rib · crackedRIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.SDR 04FDEA001113Rib · crackedRIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.SDR GTIA040478Rib · crackedRT WING L/E COMPARTMENT STA XRS267, L/E SUPPORT RIB IS CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.SDR 05FDEA00012Rib · crackedWINGS - RT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-75716.SDR 05FDEA00011Rib · crackedWINGS - LT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-571-75732.SDR UIEA200400054Rib · crackedFOUND LEFT WING LE PARTIAL RIB AT ILES 414.5 HAS A 4.5 INCH CRACK LONGITUDAL ACROSS ITS WEB JUST BEHIND THE FORWARD RIB SECTION. CRACKED WEB REPAIRED PER SRM 51-40-02. (M)SDR UIEA200400055Rib · crackedFOUND RT WING LEADING EDGE RIB AT ILES 330 FOUND WITH A 1.25 INCH LONG CRACK ON THE WEB ALONG THE LOWER ANGLE AT AFT EDGE. REPLACED CRACKED LEADING EDGE RIB WEB WRT SRM 51-30-02. (M)SDR SWIA200413251Rib · crackedRIGHT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION.SDR SWIA200413249Rib · crackedLEFT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION.SDR ASAA0440115Rib · crackedGYR - FOUND LEFT WING INTERNAL RIB AT WING STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOEWR CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M)SDR ASAA0440105Rib · crackedGYR - FOUND LEFT WING INTERNAL RIB AT STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOWER CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M)SDR SWIA200413332Rib · crackedLT INBOARD LEADING EDGE RIB HAS A SMALL CRACK. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT ADDED AT AFFECTED AREA OF LT LEADING EDGE RIB IAW EMB120 SRM 51-10-02 PG 2 SEC 2B.SDR ASAA0440103Rib · crackedGYR - FOUND WING RIB LOWER CHORD IS CRACKED APPROXIMATELY .5 INCH LONG, CHORD TO SKIN ATTACH TEE AFT OF STRINGER. REPLACED DAMAGED RIB LOWER CHORD. (M)SDR 2004UALA00315Rib · damagedLEFT WING RIB 5 FITTING INBOARD REAR SPAR FASTENER 4 FROM THE TOP, NUT SHEARED OFF. BOLT LIKELY SHEARED AT THE TIME OF INSTALLATION. NO DAMAGE TO ADJACENT FASTENERS, FASTENER HOLES OR FITTING COMMON TO PROBLEM HOLE WAS NOTED INDICATING THAT SHEARING DID NOT OCSDR ASOA04269Rib · crackedDURING A C-CHECK IN MCN, THE LEFT WING BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT WING BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)SDR 2004FA0000391Rib · crackedRAMP INSP FOUND OIL CANNING IN LT WING OF HIGH TIME. WING WAS INSPECTED AND ONLY DEFECT FOUND WAS LWR FLANGE ON 4 OF INTERSPAR RIBS WERE CRACKED AT STRINGER PASS-THROUGH. CRACK WAS .5-.75 INCHES LONG AND USUALLY EXTENDED PAST FIRST RIVET. AFTER REPAIRING IAWSDR UPS04842238Rib · crackedINSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS04842114Rib · crackedINSPECTION TYPE: C3, RT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS04842110Rib · crackedINSPECTION TYPE: C3, RIGHT WING O/B LEADING EDGE RIB IS CRACKED AT XFS 603.75. CRACK TERMINATES AT FASTENER HOLE, NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS04842109Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT PNEUMATIC DUCT SUPPORT AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842115Rib · crackedINSPECTION TYPE: C3, RT WING LE LOWER RIB IS CRACKED AT XFS 335.25. CUT OUT DAMAGE, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-2-0 FIG 2.SDR UPS04842113Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 810. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842112Rib · crackedINSPECTION TYPE: C3, LEFT WING LEADING EDGE UPPER RIBS ARE CRACKED AT XFS 747.5 AND XFS 753.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842111Rib · crackedINSPECTION TYPE: C3, RT WING LEADING EDGE UPPER RIB IS CRACKED AT XFS 803.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842108Rib · crackedINSPECTION TYPE:C3 RIGHT WING L/E LOWER RIB IS CRACKED AT XS 429 AT I/B END OF SLOT HOUSING. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS04842107Rib · crackedINSPECTION TYPE:C3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS04842106Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 304 AT PNEUMATIC DUCT SUPPORT. CUT OUT AND STOPDRILLED CRACKED AREA, NDT VERIFIED NO CRACKS AT STOPDRILLS AND CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.SDR 04FDEA00779Rib · crackedLEFT WING LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND CRACKED. LT WING LEADING EDGE RIB AT SLAT TRACK NR 16 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II.SDR 04FDEA00767Rib · gougedEA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098-25. COMPLIED WITH EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098.25.SDR DHL2004803515Rib · crackedLT OUTER WING OTBD L/E RIB CRACKED 0.250 AT XFS 741.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SSDR DHL2004803511Rib · crackedLT OUTER WING OB L/E FORMER CRACKED 0.250 (UPPER PART) STA XFS. 835.000 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 FABRICATED DOUBLER (2024T3 AL,0.032) IAW SRM 57-2-0 PAGES 9, 10. CLEANED TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IASDR DHL2004803508Rib · crackedLT OUTER WING OB L/E FORMER CRACKED 0.250 AT XFS 822.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SDR DHL2004803507Rib · crackedLT OUTER WING OB. L/E FORMER CRACKED 0.250 AT XFS 760.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SDR SWAA040877Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING AT WBL 114, S2, UPPER RIB CRACKED. REPAIRED RT WING RIB PER ER.SDR 04FDEA01858Rib · crackedRIGHT AND LEFT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED, REPAIR ANGLE AND DOUBLER INSTALLED TO RESTORE STRENGTH IAW FEDEX EA 8-5710-75729 (REF FEDEX NRC N0732, N0626).SDR SWAA040821Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD AT WS 135.5, BETWEEN S-2 AND S-3, CRACKED. REPAIRED LT WING RIB CHORD PER ACO.SDR 04FDEA00631Rib · crackedLEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) MOST UPPER AFT FAIRING SUPPORT BRACKET FOUND CRACKED. REPAIRED AS PER EA 1-5750-75304, TITLE: WINGS - T/E FLAPS - LEFT I/B FLAP - O/B HINGE BRACKET FAIRING - CRACK REPAIR.SDR 2004FA0000336Rib · crackedFOUND OIL CANNING IN LT WING OF HIGH TIME WHEN LIFTING AFT END OF TIP TANK. WING WAS INSPECTED AND ONLY DEFECT WAS LWR FLANGE ON 4 OF INTERSPAR RIBS WERE CRACKED, STRINGER PASS-THROUGH. CRACK WAS .5-.75 INCHES LONG, EXTENDED PAST FIRST RIVET. AFTER REPAIRINGSDR 04FDEA00543Rib · crackedRIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACKED. RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR ASAA0480116Rib · crackedOKC - DURING HV6 CHECK, FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP RIB IS CRACKED AT RIVET HOLE. REPLACED DAMAGED END CAP RIB PER SRM 51-30-2. (M)SDR GLBA20030575Link · crackedRIB LINK CRACKED ON RT NAC FLAP, R&R RT RIB LINK ON NACCLLE FLAP PN 120-34222-010SDR 04FDEA00426Rib · crackedLT WING, CRACK FOUND ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM SDR UPS04841857Rib · crackedINSPECTION TYPE: C3, RT WING O/B LEADING EDGE LOWER RIB IS CRACKED AT XFS 825. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR SWAA040385Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING WBL 135, RIB LOWER CHORD CRACKED. REPAIRED CHORD PER ER.SDR ABXA040066Rib · crackedRT WING LE HAD CRACKED RIB AT LOWER NUTPLATES FOR NR 2 IB SLAT TRACK RIB. FOUND 4 CRACKS, REPAIRED IAW REA D957-49005 AND INSTALLED NUTPLATES IAW DC-9 SRM 51-30-2.SDR UPS04241932Rib · crackedINSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00.SDR UPS04841848Rib · crackedINSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.
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