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 SWAA2016062453205Rib · crackedLEFT WING RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED CHORD IAW EA.SDR SCNA20160522064Rib · brokenRIGHT WING DEFLECTION, RIB LOWER ATTACH POINT IS BROKEN. REMOVED BROKEN LUG, EDDY CURRENT AFFECTED AREA, NO DEFECTS NOTED, ROTORY FLAP PEENED REPAIR AREA, TREATED AND PRIMED, DRILLED REPAIR FITTING AND INSTALLED.SDR SCNA20160522063Rib · wornLEFT WING DEFLECTION RIB LOWER ATTACH POINT IS WORN. LT WING DEFLECTION RIB LOWER ATTACH POINT IS WORN, REMOVED WORN EXISTING LUG, EDDY CURRENT AFFECTED AREA, NO DEFECTS NOTED, ROTORY FLAP PEENED AREA. TREATED & PRIMED, DRILLED REPAIR FITTING AND INSTALLED.SDR SCNA20160522062Rib · wornLEFT WING DEFLECTION, RIB UPPER ATTACH POINTS ARE WORN. LT WING DEFLECTION RIB UPPER ATTACH POINTS ARE WORN, BLENDED WORN AREA, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA, DRILLED & FABRICATED FILLER, DOUBLER, SERRATED PLATE, HFEC FOUND NO DEFECTS NOTED,SDR FDEA201605161598Support · crackedLEFT WING OTBD LE SKIN INTERNAL SUPPORT FORMER ASSEMBLY, FOUND CRACK AT STATION XOS 585. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G. NEW FORMER FABRICATED IAW DWG ARB 2931 REV H & PROTECTED IAW SRM 51-21-01-0G. NEW FORMER INSTALLED IAW SRM 51-31-01-0G. REPSDR SWAA2016061352764Rib · crackedRIGHT WING INBD OF DEFLECTOR, RIB CRACKED AT THE UPPER PANEL'S MID STIFFENER. R & R RIB IAW SRM AND DWG.SDR FDEA201605131575Former · crackedRIGHT WING FIXED LE SKIN SUPPORT FRAME, FORMER, FOUND CRACK AT STATION XOS 584. CRACKED SUPPORT FRAME, FORMER, REMOVED IAW SRM 51-31-01-OG & FABRICATED NEW FORMER IAW DWG ARB 2931 REV H. INSTALLED NEW FORMER AT RT WING FIXED LE SKIN IAW SRM 51-33-01-OG AT XOSDR FDEA201605131546Former · crackedLEFT WING FIXED LE COMPARTMENT FORMER FOUND CRACKED, AT STATION XOS 560. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G. NEW FORMER FABRICATED IAW DWG ARB 1162 REV S & PROTECTIVE TREATMENT CARRIED OUT IAW SRM 51-21-01-0G. NEW FORMER INSTALLED IAW SRM 51-34-01-0SDR 17GR2016051600001Rib · crackedPERFORMING INSPECTION AS PART OF SB 1161, DISCOVERED CRACKS IN BOTH WHEEL WELLS. CRACKS WERE VISIBLE WITHOUT NDT INSPECTION. THE WERE RADIATING FROM THE LOWER CORNER UP.SDR IPXA2016052003635Rib · crackedINSPECTION TYPE: 3C, LT WING FIXED L/E RIB AT XOS.1026 IS CRACKED AT THE LOWER FLANGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L/E RIB AT IAW DWG ARB2920 AND SRM 51-33-01.SDR DALA2016051103859Rib · crackedCRACKED RIB ON LT WING L/E BS XRS 324. STOP DRILL ON RIB IAW SRM 51-01, PAR 21, REPAIR. PARTS WERE FABRICATED IAW 57-06 B, FIG 18, REPAIR. PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5.SDR SWAA2016051051672Rib · crackedRIGHT WING FIXED TE VERTICAL SUPPORT RIB CRACKED AT RSS 277. R & R RIB IAW SRM.SDR QXEA2016051100307Rib · crackedLEFT WING L/E 511AL HAS CRACKED RIB DOUBLERS 1EA INBD AND 1EA OTBD. DISBONDED L/E DE-ICE BOOT TO GAIN ACCESS TO RIB REPAIR REF AMM 30-11-76-000-801 4.A, 1. BONDED EXISTING DEICE BOOT ON CORNER AT L/E REF AMM 30-11-76-400-801. PG 408, PROCEDURE 4.C.1. REMOVESDR DALA2016050603706Rib · crackedCRACKED RIB AND RIB CLIP ON RT WING L/E BS XRS 267 APPROXIMATELY. RIB DOUBLER AND CLIP WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR QXEA2016052300321Rib · crackedLEADING EDGE 611AR, INBD RIB, EXISTING REPAIR ANGLE AT BOTTOM CORNER FOUND CRACKED. REMOVED CRACKED EXISTING REPAIR ANGLE FROM BOTTOM CORNER OF L/E PANEL 611AR REF SRM 51-42-05, 51-40-15. INSTALLED NEW REPAIR ANGLE BACK INTO L/E PANEL 611AR ON BOTTOM CORNER RESDR QXEA2016052300322Rib · crackedCRACK FOUND ON OTBD LOWER DOUBLER ON 511AL L/E RIB. REMOVED CRACKED OB LOWER DOUBLER FROM 511AL L/E RIB. REF SRM 51-42-05, 51-40-15. INSTALLED NEW DOUBLER, REF SRM 57-40-00, REPAIR-07, SECTION 7, "PROCEDURE" PG 202, STEPS 3 THROUGH 10, PG 203+204 RESPECTIVELYSDR YADA20160428001Rib · corrodedCORROSION FOUND BY X-RAY INSPECTION ON LOWER FLANGE LT ENG RIB PN 118-110050-5, ADJACENT TO FWD SPAR LOWER CAP. BLENDED & TREATED AREA.SDR ABXA20160423082Rib · corrodedTHE NR 7 OTBD ACTUATOR SUPPORT RIB HAS CORROSION IN THE ACTUATOR BORE. FINAL BORE SIZE IS 5.995 CLEAN & ROUND, NO DEFECTS NOTED, REA FORTHCOMING. REMOVED CORROSION FROM NR 7 OTBD ROTARY ACTUATOR SUPPORT, FINAL BORE SIZE 5.995". PERFORMED SURFACE SCAN IAW NDSDR ASAA2016041916604Rib · crackedRT WING RT WS 135 RIB CHORD CRACKED. ACFT GROUNDED. REPAIRED RT WS 135 RIB CHORD IAW EA 400-57EA-17072.SDR DALA2016041702971Rib · crackedCRACKED RIB ON RT WING FIXED L/E BS XRS 324. THE RIB WAS REPAIRED IAW SRM 57-06 B, D, FIG 18.SDR DALA2016041602965Rib · corrodedCORROSION AND WEAR ON BORES OF LT WING SLAT PANEL NR 2, RIBS BS XOS=196, XOS=240 AND XOS=286. RIBS BORES WERE REPAIRED WITH NEXT FINAL DIMENTIONS: XOS=196, 4 HOLES: 0.938" XOS=240, 2 HOLES: 0.940" XOS=286, 2 HOLES:1.123" AND REPAIR BUSHINGS WERE FABRICATED SDR IPXA2016050402914Rib · crackedINSPECTION TYPE:2C, LT WING NR 1 SLAT L/E FILLET ASSY RIB CRACKED AT BS XIS 150.74. R & R LT WING NR 1 SLAT L/E FILLET ASSY IAW AMM 27-80-21-400-801.SDR ABXA20160329070Rib · corrodedNUMBER 1 FLAP SUPPORT TE OTBD ACTUATOR BORE HOLE HAS AREAS OF CORROSION. DEFECT NOTED IAW JC S57-798-24-01. REPAIRED BORE HOLE IAW REA B657-61988-MR. CORROSION REMOVED IAW SRM 51-10-02. CORRODED LEVEL 2, PN 113T1345-19, PART NAME RIB HALF, SN NSN, WS LOCATSDR ABXA20160329069Rib · corrodedNUMBER 2 FLAP SUPPORT TE INBD ACTUATOR BORE HOLE HAS CORROSION & TOOLING MARKS, DEFECTS NOTED IAW JC S57-798-24-01 STEP 2 & 3. REPAIRED IAW REA B657-61989-MR. CORRODED LEVEL 2, PN 113T1345-25, PART NAME RIB HALF, SN NSN, WS LOCATION FROM WS 613 - 613. ACFT SDR ABXA20160329068Rib · corrodedNUMBER 2 FLAP SUPPORT TE OTBD ACTUATOR BORE HOLE HAS CORROSION & TOOLING MARKS, DEFECTS NOTED IAW JC S57-798-24-01 STEP 2 & 3. REMOVED CORROSION FROM BORE IN 20BD ACTUATOR BORE IAW SRM 51-10-02. FINAL SIZE 6.048, REAMED DAMAGE HOLE IAW REA B657-61989-MR. INSDR ABXA20160329067Rib · corrodedNUMBER 1 TE FLAP SUPPORT, INBD ACTUATOR, BORE, HOLE HAS EVIDENCE OF CORROSION DEFECT. NOTED REF JC S57-798-24-01 STEP 2 & 3. REPAIRED IAW REA B657-61988-MR. CORRODED LEVEL 2, PN 113T1345-21, PART NAME RIB HALF, SN NSN, WS LOCATION AT LT WS 795. ACFT WAS GNSDR ABXA20160329052Rib · corrodedRIGHT WING LE AIR LOAD RIB CORRODED AT WS 479. R & R RT WING LE AIR LOAD RIB AT WS 479 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-14, PART NAME STRUT RIB, SN NSN, WS LOCATION FROM WS 479 - 479. ACFT WAS GNDED.SDR SWAA2016041450926Rib · crackedLEFT WING INSPAR RIB WEB CRACKED ON RIB WEB ON WBL 198.60, AT LEVEL OF S 5 FUEL TANK. REPAIRED WEB IAW EA.SDR FDEA201603241028Support Rib · crackedLEFT WING FIXED LE COMPARTMENT, SUPPORT RIB FOUND CRACKED, AT XOS 685. R & R WITH NEW FABRICATED SUPPORT RIB IAW SRM 51-31-01-0G. NEW SUPPORT RIB FABRICATED IAW DWG ARB2924 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603241027Rib · crackedLEFT WING FIXED LE SKIN SUPPORT RIB FOUND CRACKED, AT XOS 753. R & R WITH NEW FABRICATED SUPPORT RIB IAW SRM 51-31-01-0G. NEW SUPPORT RIB FABRICATED IAW DWG ARB2923 REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR ABXA20160323051Rib · corrodedLEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 575, OTBD OF NR 4 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R AIR LOAD RIB AT OSS 575 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2209-17, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 575 -SDR FDEA201603220977Former · crackedRIGHT WING LE FORMER, AT XOS 1025, FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G & FABRICATED NEW FORMER IAW DWG ARB2920 REV BB. INSTALLED NEW FORMER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SIMA20160320001Rib · crackedDURING MBV INSPECTION, QA FOUND A CRACK ON THE LT WING RIB 5. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R LT WING RIB 5 IAW ERS-EM-57MR-592. REPAIR MATERIALS, RIB 5 PN 145-67083-601.SDR SIMA20160318009Rib · crackedLEFT WING SPAR NR 1 RIB 9, LOWER FLANGE CRACK AT FASTENER HOLE AREA. ACCOMPLISHED REPAIR TO LT WING SPAR NR 1 RIB 9, LOWER FLANGE AT FASTENER HOLE AREA IAW ERS-EM-57MR-605. SEE WIPS & TASK FOR DETAILS.SDR SIMA20160316007Rib · chafedLEFT AIL PCA SYS NR 1 RETURN BLUE FLEXIBLE HOSE IS CHAFING ON LOWER RIB INSIDE 551CB. REPAIRED LT WING 21 CHAFE IAW ERS-EM-57MR-594.SDR SWAA2016032150058Rib · crackedRIGHT WING RIB AT WBL 413 CRACKED, AT UPPER BEAM. REPAIRED RIB IAW EA.SDR UVVR2016031500042Rib · chafedRIGHT FLAP OTBD L/E VANE IS CHAFING ON WING RIB WHEN FLAPS ARE RETRACTED. FLAPS WERE FOUND TO BE PROPERLY RIGGED. SUSPECT WING RIB TO BE MFG INCORRECTLY.SDR UVVR2016031500041Rib · chafedLEFT FLAP OTBD L/E VANE IS CHAFING ON WING RIB WHEN FLAPS ARE RETRACTED. FLAPS WERE FOUND TO BE PROPERLY RIGGED. SUSPECT WING RIB TO BE MFG INCORRECTLY.SDR SWAA2016041851036Rib · crackedLEFT WING RIB CRACKED AT WBL 135.50, AFT LOWER END. REPAIRED RIB IAW EA.SDR ABXA20160307050Rib · corrodedLEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 884, OTBD OF NR 2 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R RIB IAW SRM 51-40-02 7D & DWG 114T222. CORRODED LEVEL 2 PN 114T2222-15, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 884 - 88SDR IPXA2016041001914Rib · crackedINSPECTION TYPE:3C, RT CRUISE PERFORMANCE FAIRING IS CRACKED ON WEB/RIB. REPAIRED RT CRUISE PERFORMANCE FAIRING WEB/RIB IAW EA 011-5754-01-A6178, REV I/R AND EO MD11-5750-60451-A.SDR IPXA2016041001909Rib · crackedINSPECTION TYPE:C3, LT CRUISE PERFORMANCE FAIRING OTBD WEB/RIB IS CRACKED. REPAIRED LT CRUISE PERFORMANCE FAIRING OTBD WEB/RIB IAW EA 011-5754-01-A6159 REV. I/R AND EO MD11-5750-60452-A.SDR DALA2016030601679Rib · crackedCRACKED RIB BS XOS.553 AT RT WING FIXED L/E IN REF CARD 89, ZONE 10. RIB WAS REPAIRED IAW ER/A 543160-14 AND SRM 51-10-2, 51-10-3 PAR 14 AND 21, SRM 57-06A.SDR DALA2016030401647Rib · crackedCRACKED RIB BS XOS=455 AT LT WING FIXED L/E IN REF CARD 55, ZONE 10, CARD 172, ZONE 10. RIB WAS REPAIRED IAW SRM 51-30-2, 51-30-5, ETI 88-16-085 R2 AND ER/A 543174-14, REV ORIGINAL.SDR FDEA201603020779Rib · crackedRIGHT WING LE COMPARTMENT, SKIN SUPPORT RIB FOUND CRACKED, AT XOS 667.6. R & R WITH NEW FABRICATED RIB IAW SRM 51-31-01-0G. NEW RIB FABRICATED IAW DWG ARB2930 REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2016032850273Rib · crackedRIGHT WING RIB CRACKED EXISTING FILLER INTERNAL AREA ON WBL 114.00, STRINGER 2R UPPER CHORD REAR SPAR. REPAIRED RIB IAW EA.SDR FDEA201603010727Rib · crackedLEFT WING FIXED LE COMPARTMENT, RIB FOUND CRACKED, AT XORS 490. R & R WITH NEW FABRICATED RIB IAW SRM 51-31-01-0G. NEW RIB FABRICATED IAW DWG ARB2931 REV H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603010726Doubler · crackedLEFT WING FIXED LE COMPARTMENT, RIB INTERNAL DOUBLER FOUND CRACK, AT XORS 801. R & R WITH NEW RIB DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201603010725Doubler · crackedRIGHT WING LE COMPARTMENT, RIB INTERNAL DOUBLER FOUND CRACK, AT STATION XORS 562. R & R WI RIB DOUBLER IAW SRM 51-31-01-0G. NEW RIB DOUBLER FABRICATED IAW DWG RB3954 REV K. CLASSIFIED AS MAJOR IAW GMM 6-2-100..SDR DALA2016102807820Angle · corrodedRIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.
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