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 EISA96234Rib · crackedFOUND RIGHT WING RIB CRACKED AT 3RD LOWER STRINGER FROM AFT SPAR, WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER SRM 57-10-05. (M)SDR EISA96215Rib · crackedFOUND RIGHT WING LE NOSE RIB CRACKED BEYOND DOUBLER AT WS 330. FABRICATED AND INSTALLED LONGERON DOUBLER PER SRM 51-20-6, 51-50-34 AND 51-30-02. (M)SDR DHL9672203CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 601.5 HAS CRACK IN LOWER CHORD AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 9 INCHES BY 4 INCHES.SDR DHL9672202CRib · crackedAT C-CHECK, LOWER ANGLE CRACKED ON RT WING RIB AT STA 629 AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 9 INCHES BY 4 INCHES.SDR MALA965124Rib · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND AT WS 27.03 RT AFT WING RIB TRAILING EDGE (PN 27-31523), A 0.375 INCH CRACK. COMPLETED REPAIR PER FAC SRM 57-90-10, PAGES 3-6, REV. NOVEMBER 1, 1994, BY FABRICATING AND INSTALLING A 0.050 INCH BY 4.00 INCSDR 97ZZZM514Rib · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 738.5 LOWER RIB FLANGE IS CRACKED AT STRINGER NR 8 ATTACH POINT. STOP DRILLED CRACK IAW B 727 SRM 51-10-1. FABRICATED CHANNEL FROM 7075-0 .080 4 INCH BY 15 INCH IAW B727 SRM 57-SDR MWEA96505Rib · corrodedDURING INSP, LT WING RIB STA 164 BOTTOM INBD FLANGE AT STRINGER 16 WAS FOUND CORRODED. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0667/DLP DATED 9 AUG 96.SDR DLL10962259Rib · crackedLT WING PYLON SUPPORT UPPER RIB CAP AT IWS 529-555 HAS A CRACKED CASTELLATION. THE DAMAGE WAS CUT OUT AND REPLACED.SDR DHL9670828CRib · crackedAT C-CHECK, RIGHT WING RIB UPPER CHORD AT BL 70.5 HAS CRACK WITH PREVIOUS STOP DRILL. HFEC, HFEC FASTENER HOLES COMMON TO REPAIR AREA. INSTALLED REPAIR PER S/B 57-0112.SDR UPS96221155Ribs · crackedINSPECTION TYPE-C, RT WING NR 5 SLAT, OUTBD AND INBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED RIBS AND FABRICATED REPLACEMENT RIBS IAW DWG 65-17276 AND INSTALLED IAW SRM 51-30-02.SDR DHL9670817CRib · crackedAT C-CHECK, FOUND WING RIB ON LEFT WING STA 629.0 HAS CRACKS AT STRINGERS 8 AND 10. THREE AT TOP AND TWO AT BOTTOM. REPLACED RIB PER S/B 57-0127.SDR DHL9670815CRib · crackedAT C-CHECK, CRACKS FOUND AT WING STA 738.5 RIB AT LWR STR 6 AND UPPER STR 14. STOPPED DRILLED CRACKS, INSTALLED REPAIR AT STR 14 PER SRM 57-10-5, 10 INCHES LONG. INSTALLED REPAIR AT STR 6 PER SRM 57-10-5, 10 INCHES LONG.SDR DHL9670810CRib · crackedAT C-CHECK, WING RIB AT STA 601.5 HAS CRACKS AT LOWER STR 6, 8 AND TOP STRINGER 11. REMOVED AND REPLACED WING RIB AT STA 601.5 PER S/B 57-127.SDR DHL9670809CRib · crackedAT C-CHECK, INSPECTION REVEALED WING RIB AT WS 656.5 HAS CRACK AT LOWER STR 6, 8 AND TOP STR 9 AND 13. REMOVED AND REPLACED RIB PER S/B 57-127.SDR DHL9670803CRib · crackedAT C-CHECK, RIGHT WING RIB CRACKED AT WS 546.5 STR 7 AND STR 8. STOP DRILLED CRACKS, INSTALLED RIB REPAIR PER S/B 57-0127, 3.125 INCHES BY 17 INCHES.SDR AALA961344Rib · corrodedAFW - FOUND AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-932. (M)SDR CALA9601432Rib · crackedINSPECTION FOUND A .50 INCH CRACK IN BOTTOM OF RIB INSIDE OF RIGHT NAV LIGHT COMPARTMENT (RT WING TIP). THE RIB WAS REMOVED . A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM'S 51-10-1 AND 51-40-2. A DOUBLER WAS ALSO INSTALLED TO REPAIR CRACKED WEB IN SAME ARESDR DLL10962263Rib · crackedBOTH SIDES IWS 503 RIB UPPER CAP WAS FOUND WITH SEVERAL ATTACH TAB CRACKS IN THE TYPICAL LOCATIONS AFT OF STR 24, AS WELL AS FWD OF STR 24. THESE FWD CRACKS NECESSITATED THE COMPLETE REPLACEMENT OF THE UPPER CAPS.SDR DHL9670823CRib · crackedAT C-CHECK, RIB CRACKED AT WS 738.5, 2 CRACKS IN LOWER FLANGE AT STR 6 AND BETWEEN STR 6 AND 8 AND UPPER RIB AT STR 12. REMOVED AND REPLACED RIB PER 57-127.SDR DHL9670819CRib · crackedAT C-CHECK, INSPECTION OF RIGHT WING SHOWS CRACKS AT STR 11 AND 15 UPPER AND 8 AND 9 LOWER, STA 629.0. REMOVED AND REPLACED RIB PER S/B 57-127.SDR DHL9670808CRib · crackedAT C-CHECK, INSPECTION REVEALED CRACKS AT RIB UPPER FLANGE AT STR 13 AND 14 AND LOWER FLANGE AT STR 8 WS 686.5. INSTALLED REPAIRS PER S/B 57-0127, UPPER REPAIR 15 INCHES BY 3.5 INCHES, LOWER DOUBLER 8 INCHES BY 3.5 INCHES.SDR DHL9670805CRib · crackedAT C-CHECK, WING RIB CRACKED AT LOWER FLANGE AT STA 601.5, STR 7. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR AT LOWER FLANGE PER SRM 57-10-5, 15 INCHES BY 5 INCHES.SDR UPS96821285Rib · crackedINSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS550 UPPER, XFS 565 LOWER, XFS565 UPPER, XFS570 UPPER, XFS575 UPPER, XFS580 UPPER AN D XFS585 UPPER RIBS. REPAIRED PER MM 57-00-00 FIG 801SDR UPS96821284Rib · crackedINSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS985 LOWER, XFS 600 UPPER, XFS605 UPPER, XFS610 UPPER, XFS615 UPPER, XFS625 UPPER AN D XFS645 UPPER RIBS. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821265Rib · crackedINSPECTION TYPE: CS2. RT WING LEADING EDGE UPPER RIB CRACK AT STA XFS560. REPAIRED RIB PER MM 57-00-00 FIG 801.SDR UPS96821264Rib · crackedINSPECTION TYPE: CS2. LT WING LEADING EDGE 9 EA RIBS CRACKED AT WS XFS730, XFS750, XFS755 , XFS760, XFS765, XFS775, XFS780, XFS785 AND XFS800. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821234Rib · crackedINSPECTION TYPE-CS2, RT WING LEADING EDGE 4 RIBS CRACKED AT STA XFS820, XFS800, XFS695 AND XFS680. REPAIRED RIBS PER MM 57-00-00, FIG 801.SDR MALA965110Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND AT WS 27.03 RIGHT AFT WING RIB TRAILING EDGE (P/N 27-31523), A .25 INCH CRACK. COMPLETED REPAIR PER FAC SRM 57-90-10 PAGES 3-6, REV NOV 1/94 BY INSTALLING A 4 INCH BY 2.5 INCH REPAIR DOUBLER TO AFFECTED SDR DHL9672242CRib · crackedAT C-CHECK, CRACKED RIB UPPER CHORD AT BL 70.5. STOP DRILLED CRACKS, HFEC AND INSTALLED REPAIR KIT PER S/B 57-0112.SDR DHL9670826CRib · crackedAT C-CHECK, LEFT WING RIB UPPER CHORD AT BL 70.5, SHOWED CRACK INDICATIONS IN VERTICAL FLANGE DURING HFEC INSPECTON. TRIMMED AREAS PER BOEING INSTRUCTIONS. HFEC TRIMMED EDGES AND FASTENER HOLES COMMON TO REPAIR AREA. INSTALLED REPAIR PER S/B 57-112 AND BOEISDR DLL10962062Rib · crackedA CRACK WAS FOUND ON THE LEFT HAND WING IWS 503 UPPER RIB CAP CASTELLATION. ER/A 271804-14AD WAS WRITTEN TO ACCOMPLISH RIB REPLACEMENT AT NEXT AIRCRAFT HMV. REV A OF THIS ER/A DEFERS THIS REPLACEMENT TO THE NEXT AIRCRAFT HMV.SDR UPS96821059Ribs · crackedINSPECTION TYPE CS2, 4 RIBS CRACKED LT WING LEADING EDGE AT WS XFS780, XFS800, XFS740 AND XFS 710. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821060Ribs · crackedINSPECTION TYPE CS2, 4 RIBS CRACKED AT LT WING LEADING EDGE WS XFS 623, XFS 633, XFS 648 AND XFS 653. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821062Ribs · crackedINSPECTION TYPE CS2, THREE RIBS CRACKED AT RT WING LEADING EDGE ST XFS 304, XFS 310 AND XFS 341. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR UPS96821063Ribs · crackedINSPECTION TYPE CS2, LT WING LEADING EDGE ASSY 1 EA RIBS CRACKED AT WS XFS 580, XFS 620, 4 EA RIBS CRACKED AT WS XFS 766, 3 EA RIBS CRACKED AT WS XFS 800 AND 2 EA RIBS CRACKED AT WS XFS 820. REPAIRED RIBS PER MM 57-00-00 FIG 801.SDR AALA961274Rib · corrodedAFW - AFTER REMOVING CORROSION, FOUND REMAINING METAL BEYOND SRM LIMITS ON RIB. REPAIR PER MRB 757-916. (M)SDR ABXA9700130Rib Clip · gougedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LOWER CLIP GOUGED AT BULKHEAD 20 RIGHT BETWEEN STRINGERS 14 TO 15. BLENDED GOUGED IAW DC-9 SRM 57-03, 51-10-3B.SDR ABXA9700135Rib Tee Cap · corrodedDURING C-CHECK, FOUND CORROSION ON RIGHT WING RIB UPPER CAP. REPAIRED IAW ABX REA D95-15855-MR.SDR CALA9601228Rib · crackedINSPECTION FOUND A 10 INCH CRACK IN OUTBOARD RIB AT NR 5 SLAT ACTUATOR ATTACH POINT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9601230Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND LOWER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9601229Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND UPPER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WAS CUT OUT. REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.SDR ABXA9700112Rib · damagedDURING C-CHECK, FOUND RIGHT WING RIB LOWER T-CAP WITH A .50 DIAMETER HOLE DRILLED IN IT. REPAIRED IAW ABX REA D957-15864-MR.SDR EISA96128Rib · crackedRIGHT WING LEADING EDGE WING AT APPROX WS 340, PREVIOUS REPAIR DOUBLER CRACKED. FABRICATED NEW WEB ANGLE AND INSTALLED PER SRM 51-10-02. (M)SDR 96ZZZX4406Rib · crackedWHILE PERFORMING ANNUAL INSPECTION, THE WING TRAILING EDGE RIBS AND ATTACHING CLIPS AT STA'S 64, 74, AND 89 WERE FOUND CRACKED ON LEFT AND RIGHT WINGS. SUBMITTER STATED IT APPEARED DURING REMOVAL THE RIBS WERE STRESSED TO OBTAIN PROPER ALIGNMENT. THIS AREA ISDR 96ZZZX4405Rib · crackedWHILE PERFORMING ANNUAL INSPECTION, THE WING TRAILING EDGE RIBS AND ATTACHING CLIPS AT STA'S 64, 74, AND 89 WERE FOUND CRACKED ON LEFT AND RIGHT WINGS. SUBMITTER STATED IT APPEARED DURING REMOVAL THE RIBS WERE STRESSED TO OBTAIN PROPER ALIGNMENT. THIS AREA ISDR 96ZZZX4404Rib · crackedWHILE PERFORMING ANNUAL INSPECTION, THE WING TRAILING EDGE RIBS AND ATTACHING CLIPS AT STA'S 64, 74, AND 89 WERE FOUND CRACKED ON LEFT AND RIGHT WINGS. SUBMITTER STATED IT APPEARED DURING REMOVAL THE RIBS WERE STRESSED TO OBTAIN PROPER ALIGNMENT. THIS AREA ISDR CALA9601242Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN RIB OF NR 5 SLAT ACTUATOR ATTACH POINT INBOARD SIDE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3.SDR QXEA9600275Rib · crackLEFT WING LEADING EDGE SECTION 511AL .5 INCH CRACK NOTED IN OUTBOARD RIB UPPER FLANGE AT THE LAST FASTENER LOCATION. CRACK FOUND DURING C-CHECK. CRACK STOP DRILLED AND DOUBLER INSTALLED PER EA 7-57-49.SDR UPS96220754Rib · crackedINSPECTION TYPE-C, A PREVIOUS REPAIR WAS DISCOVERED TO THE RBL 70.5 RIB CHORD AT 135 760. HOWEVER, A CRACK HAD PROGRESSED SINCE THE ORIGINAL REPAIR INSTALLATION. REPAIR PER CARRIED OUT PER SB727-53-0112 (UPS EO 7275710-1271) WITH DEVIATIONS OUTLINED IN SRS ESDR MWEA96368Rib · crackedDURING D-CHECK, RT WING NR 1 SLAT INBD IDLER TRACK OUTBD RIB WAS FOUND CRACKED. REPLACED RIB SET IAW SRM 57-01, PAGE 1 AND 2.
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