JASC 5712
Service difficulty reports · 6,967
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 ASOA201710047018Rib · crackedLEFT WING RIB 21 CRACKED. CUT OUT THE SECTION AND INSTALLED FILLER AND DOUBLER.SDR FDEA201709112862Frame · crackedRT WING LEADING EDGE FRAME ARB1161-15 AT STA XRS 269 IS CRACKED. RT LEADING EDGE FORMER REPAIRED PER EA 8-5710-T0335774.SDR C77A20170830001Rib · crackedTHE RIB THAT IS BEING REPLACED AS PART OF THE SERVICE BULLETIN WAS FOUND CRACKED DURING AN INSPECTION WHILE AT BASIC CHECK. BY ACCOMPLISHING SB 170-57-0047, THIS EO ALSO PROVIDES A REPAIR BY REPLACEMENT OF THE CRACKED RIB. ENGINEERING HAS CLASSIFIED THIS REPAISDR AALA201708289022Rib · crackedCRACK ON RIGHT WING SPAR NR 1 LEADING EDGE RIB 17. REPLACED THE RIB IAW DRAWING 190-31005-409.SDR SWAA2017100216797Frame · crackedLT WING FIXED LEADING EDGE CRACKED AT WBL 71.24. R&R FRAME IAW SRM AND DWG.SDR HYIA20170819001Rib · crackedDURING INSPECTION, A CRACK WAS FOUND EMANATING FROM AN AFT TRUNNION SUPPORT FASTENER HOLE ON THE RT CLOSE OUT RIB (P/N 5122155-56.) THE CRACK MEASURED 2.5 INCHES IN LENGTH. UPON REMOVAL OF THE RIB, ALL OF THE AFT TRUNNION SUPPORT FASTENER HOLES WERE FOUND ELOSDR SWAA2017082215845Rib · crackedLT WING LATERAL WEB CRACKED ATTACHED TO TRAILING EDGE PANEL JUST INBOARD OF LT DEFLECTION RIB. R & R THE RIB IAW SRM AND DWG.SDR DALA2017081006105Rib · crackedDURING SLAT DOOR MECHANISM REMOVAL PER CARD 00229 CRACKED RIB WAS FOUND. RIB WAS REPLACED PER SRM 51-40-05, 51-41-02, 51-41-05, SOPM 20-10-7, AND IPC 57-41-57-01 FIG 101.SDR FQAR20170808076Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE RIGHT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTSDR FQAR20170808075Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE LEFT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTESDR SWIA201743679Rib · corrodedRIGHT WING BATT RIB CORRODED AT WS 53.60. INSTALLED A NEW RIB AT WS 53.6 AND REAR SPAR IAW SRM. LEAK AND OP CHECK GOOD.SDR SWAA2017092016486Rib · crackedRT WING OUTBOARD RIB CRACKED AT NO STEP PANEL OUTBOARD ATTACH POINT. R&R RIB IAW SRM.SDR IPXA2017081320453Rib · crackedINSPECTION TYPE:3CL/H WING L/E RIB/FORMER IS CRACKED AT XFS 1192. REMOVED, FABRICATED AND REPLACED THE LT WING LE RIB IAW DWG ARB2920, AND SRM 51-31-01.SDR FQAR20170802072Channel · crackedA CHANNEL IN THE LEFT WING WAS FOUND CRACKED. CHANNEL IS LOCATED INBOARD ON THE WING'S LOWER SURFACE AND IS RIVETED TO SKIN PANEL.SDR FQAR201708002072Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE RIGHT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTSDR FQAR20170802071Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE LEFT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTESDR GTIA2017072902110Rib · gougedRT WING RIB 23 GOUGE STA 1228. BLEND OUT REPAIR AS PER EO 5721-1738.SDR AALA201708029034Rib · crackedAIRCRAFT IN BASE MAINTENANCE. RIGHT WING LEADING EDGE RIB 17 CRACKED. REPLACED RIB PER SRM 51-41-00, 51-41-02, 51-43-03, 51-43-04 AND DRAWING 190-31005-409.SDR AALA20170728007Rib · corrodedCORROSION ON RIGHT WING TRAILIING EDGE AILERON HINGE RIB NR 5 BETWEEN SPAR STATIONS 1233 AND 1235. REPAIRED IAW SRM 57-51-02-2R-3.SDR HYIA20170719003Rib · crackedDURING A ROUTINE INSPECTION, SIX CRACKS WERE FOUND IN THE LT CLOSE OUT RIB (P/N 5122155-55.) THESE CRACKS WERE LOCATED AT EACH OF THE SIX VERTICAL ATTACHING HOLES OF THE FORWARD ROW OF THE AFT TRUNNION SUPPORT. EACH CRACK IS TWO INCHES IN LENGTH. UPON REMOVASDR HYIA20170719002Rib · crackedDURING A ROUTINE INSPECTION, A CRACK (.250 IN LENGTH) WAS FOUND IN THE RT CLOSE OUT RIB (P/N 5122155-56.) THIS CRACK WAS FOUND IN THE FORWARD LOWER MOST HOLE OF THE FORWARD TRUNNION SUPPORT. UPON REMOVAL, ALL FASTENERS HOLES WERE FOUND TO BE WITHIN TOLERANCE SDR HYIA20170719001Rib · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND EMANATING FROM A FWD TRUNNION SUPPORT FASTENER HOLE ON THE RT CLOSE OUT RIB (P/N 5122155-56.) THE CRACKS MEASURED .250 IN LENGTH. UPON REMOVAL OF THE CLOSE-OUT RIB, IT WAS DETERMINED THE AFT ROW OF FASTENER SDR GTIA2017071702072Rib · corrodedCORROSION FOUND ON RIB 5-6, DRY BAY AREA L140MM X W35MM. PERFORMED A DOUBLER REPAIR IAW EO 5721-1732.SDR KO0R201707120040Rib · crackedRIGHT WING FIXED LEADING EDGE RIB AT WING STATION 725 IS CRACKED IN THE LOWER AFT RADIUS.SDR KO0R201707120039Rib · crackedRIGHT WING LEADING EDGE RIB IS CRACKED AT WING STATION 800SDR FDEA201707111910Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. THE RIB DOUBLER WAS REMOVED IAW SRM 51-31-01-0G . A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REV K, AND INSTALLED IAW SRM 51-31-01-0G, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707111909Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. THE RIB DOUBLER WAS REMOVED IAW SRM 51-31-01-0G. A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954 REV K, AND INSTALLED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR ABXA20170705077Rib · corrodedCORROSION ON LOWER AIR LOAD RIB AT LEFT WING LEADING EDGE STATION 938. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.SDR HYIA20170705004Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED IN THE RT CLOSEOUT RIB AT RWS 106.79. ON REMOVAL, IT WAS NOTED THAT THE FASTENER HOLE WHERE THE CRACK STARTED FROM WAS NO LONGER IN TOLERANCE FOR THE LOCK FASTENER THAT WAS PREVIOUSLY INSTALLED THERE.SDR AALA20170704006Rib · corrodedCORROSION ON LEFT WING TRAILIING EDGE OUTBOARD AILERON HINGE RIB NR 1 AT BONDING JUMPER ATTACH AREA. REPAIRED IAW SRM 57-51-02-2R-3.SDR AALA20170704005Rib · corrodedCORROSION ON LEFT WING TRAILIING EDGE OUTBOARD AILERON HINGE RIB NR 5 AT BONDING JUMPER ATTACH AREA. REPAIRED IAW SRM 57-51-02-2R-3.SDR C77A20170630002Rib · crackedLEFT WING INTERNAL BETWEEN SPAR II AND SPAR III, A CRACK WAS FOUND AT THE 3RD FASTENER HOLE FROM THE AFT ON THE UPPER FLANGE OF RIB 10, EXTENDING 2 WAYS FROM A FASTENER HOLE. THE TOTAL LENGTH OF THE (2) CRACKS IS APPROX. 0.400". PERFORMED SERVICE BULLETIN SDR C77A20170630001Rib · crackedINTERNAL OF RT WING, BETWEEN SPAR II AND SPAR III, A CRACK WAS FOUND AT THE THIRD FASTENER HOLE FROM THE AFT ON THE UPPER FLANGE OF RIB 10, EXTENDING 2 WAYS FROM A FASTENER HOLE.
THE TOTAL LENGTH OF THE (2) CRACKS IS APPROX. 0.670". REPAIR MAJOR. PERFORMEDSDR JR2R20170630142Rib · crackedRIGHT WING LEADING EDGE RIB HAS A CRACK INBOARD OF SLAT TRACK NR 9 BETWEEN XFS 151.125 - 145. REMOVED AND REPLACED THE RIB IAW SRM 57-06B, FIG 18.SDR FDEA201706271769Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 673 RIB DOUBLER CRACKED. RIB DOUBLER REMOVED IAW SRM 51-33-01-0G, AND A NEW DOUBLER WAS FABRICATED IAW DRAWING ARB3954, REVISION K. THE DOUBLER WAS INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJSDR FDEA201706271773Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 668 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01-0G, DRAWING ARB3954, REV K. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR C77A20170615009Rib · crackedRIGHT WING, BETWEEN SPAR II AND SPAR III, A CRACK WAS FOUND AT THE THIRD FASTENER HOLE FROM THE AFT ON THE UPPER FLANGE OF RIB 10, EXTENDING 2 WAYS FROM A FASTENER HOLE. MAJOR REPAIR, PERFORMED SERVICE BULLETIN 170-57-0047 BY REPLACING THE EXISTING RIB.SDR AALA201706129053Rib · crackedCRACK ON RIGHT WING LEADING EDGE RIB 17 AT YA8551. REPLACED THE RIB IAW DRAWING 190-31005-409.SDR AALA201706129052Rib · crackedCRACK ON LEFT LEADING EDGE RIB 17 AT -YA8551. REPLACED THE RIB IAW DRAWING 190-31005-49.SDR RAIA201706090001Rib · crackedRIGHT SPAR 1 WING RIB NR 9 HAS CRACK AT SCREW HOLE. REPAIRED THE RIB.SDR SWAA2018121427683Rib · crackedLT WING TRAILING EDGE RIB CRACKED IN RADIUS JUST OUTBOARD OF OUTBOARD FLAP WS 512. REPAIRED RIB PER EA.SDR COEA2017052733923Rib · corrodedRIGHT REAR RIB 23 HAS AREAS OF CORROSION. REPAIRED IAW ES-2409/17.SDR JR2R20170526055Rib · crackedLEFT WING FIXED LEADING EDGE RIB UPPER END CAP/CABLE FAIRLEAD IS CRACKED AT W.S. XOS 219. REPAIRED LT WING FIXED LEADING EDGE RIB UPPER END CLIP /CABLE FAIRLEAD AT WING STA. XOS 219 I.A.W. MD-80 SRM 57-06B FIG. 17SDR U2RA201706090004Web · crackedDURING ACCOMPLISHMENT A D CHECK INSPECTION, FOUND RIGHT WING TRAILING EDGE SUPPORT RIB WEB CRACKED AT INBOARD SIDE OF THE NR 7 GROUND SPOILER. - REMOVED AND REPLACED RIGHT WING TRAILING EDGE SUPPORT RIB WEB IAW SRM 51-40-02.SDR C77A20170524002Rib · crackedRIGHT WING INTERNAL BETWEEN SPAR II AND SPAR III, A CRACK WAS FOUND IN THE UPPER FLANGE OF RIB 10. REPLACED THE RIB IAW SB 170-57-0047.SDR DALA2017052404145Rib · crackedCRACK RIB WAS FOUND NEAR STA XRS=414 AT FRONT SPAR WING RT SIDE. RIB NEAR STA XRS=414 AT FRONT SPAR WING RT SIDE WAS REPAIRED PER SRM 57-06B FIG 12 SHEET 2. 51-30-2 AND 51-30-5.SDR AALA20170523002Rib · corrodedCORROSION ON LEFT WING TRAILIING EDGE AILERON HINGE RIB NR 3 AT BONDING JUMPER ATTACH AREA. REPAIRED IAW SRM 57-51-02-2R-3.SDR GTIA2017051901931Rib · gougedFOUND A GOUGE ON THE RT WING WS 1228 RIB 23. REPAIRED IAW EO 5721-1720, REV 00, AND TD 80304436/005.SDR FQAR20170517025Rib · crackedDURING A ROUTINE INSPECTION, A RIB IN THE RIGHT WING WAS FOUND WITH A SMALL CRACK. RIB IS AFT OF MAIN WING SPAR, IS THIRD RIB OUT FROM FUSELAGE, AND IS IMMEDIATELY INBOARD OF LANDING GEAR UPPER STRUT. CRACK WAS LOCATED IN UPPER FLANGE OF RIB WHERE RUB IS RIVETSDR ABXA20170511056Rib · crackedCRACK IN LEADING EDGE RIB AT RIGHT WING STATION 500. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
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