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 CA060425002Rib · crackedRIGHT WING RIB AT STN 40.125 AFT UPPER FLANGE CRACKED ALONG BEND RADIUS.SDR SWAA061404Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED RT WING T/E FLAP RIB PER SRM AND CMM.SDR CA060508012Rib · crackedDURING COMPLETION OF INSPECTION REQUIRED BY PIPER SB 1161, A 2.5 INCH LONG CRACK WAS OBSERVED IN THE RT WING RIB AND 3 INCH LONG IN THE LT WING RIB AT STN 49.25. THE CRACKS WERE LOCATED IN THE BEND RADIUS UNDER THE MLG SIDE BRACE MOUNT (PN 95643-09). NEW RIBSDR 06FDEA1574Rib · gougedCOMPLY WITH EA 6-5740-92420 LT WING LEADING EDGE RIB GOUGED. COMPLIED WITH EA 6-5740-92420 LT WING LEADING EDGE GOUGED.SDR TRAX200600130Rib · crackedFOUND LT BATT RIB CRACKED. REPAIRED LT BATT RIB IAW REO 601R-57-51-046. KW 10175.SDR USAA060607Rib · crackedFOUND CRACK RT WING AT RIB 6 (WING STA 3621) STR R19-R20 . REPAIR KIT INSTALLED PER EA 97606 AND AIRBUS DWG B572-57026 ISSUE C, DEFECT SIZE: .040".SDR USAA060606Rib · crackedFOUND LT WING AT RIB 6 (WING STA 3621) BETWEEN STR 19 AND 20, CRACKED FUEL PIPE. REPAIR KIT INSTALLED PER EA 97607 AND AIRBUS DWG 572-57026 ISSUE 6, DEFECT SIZE: .040".SDR SWAA061338Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED MID FLAP OUTBOARD RIB PER SRM AND BOEING DRAWING.SDR 06FDEA1542Rib · crackedFOUND RT WING L/E CRACK 0.50" LONG ON RIB INSIDE L/E AT STA XORS 643. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1.SDR 06FDEA1538Rib · crackedFOUND 1 CRACK LT WING L/E INT SIDE 0.25" LONG ON RIB AT STA XORS 727. REPAIRED FORMER IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F176276/N00276 AND IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1.SDR 06FDEA1537Rib · crackedLT WING L/E INT SIDE FOUND CRACK 0.25" LONG ON RIB AT STA XORS 884. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 39 SHT 2 SECTION B-B VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F176275/N00275 AND IAW SRM 57-10-00 FIG 39 SHT 2 SECTION B-B VOL 1.SDR 06FDEA1534Rib · crackedRT WING L/E FOUND CRACK 1" LONG ON RIB INSIDE L/E AT STA XOS 923. REMOVED FASTENERS IAW SRM 51-33-01 PAGE 34-41. WRONG PART ARRIVED FROM BACKSHOP SCRAPPED WRONG PART. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176397-3A. REPAIR ANGLE AND F176397-6 FILLESDR 06FDEA1532Rib · crackedRT WING L/E FOUND CRACK .50" LONG ON RIB INSIDE L/E AT STA XOS 969. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1.SDR QXEA200601625Rib · crackedYYC - C3 RIGHT WING LEADING EDGE 611AR INBOARD AND OUTBOARD ALUMINUM END RIBS ARE CRACKED AT TOP AND BOTTOM ENDS. REPAIRED IAW RD 8/4-57-105.SDR CA060508011Rib · crackedDURING COMPLETION OF INSPECTION REQUIRED SB 1161, A 3 IN LONG CRACK WAS OBSERVED IN THE RT WING RIB AT STN 49.25. THE CRACK WAS LOCATED IN THE RIB BEND RADIUS UNDER THE MLG SIDE BRACE MOUNT (PN 95643-09). A NEW RIB WAS INSTALLED. BEFORE RE-INSTALLATION SHARSDR CA060508010Rib · crackedDURING COMPLETION OF INSPECTION REQUIRED SB 1161, A 2 INCH LONG CRACK WAS OBSERVED IN THE LT WING RIB AT STN 49.25. THE CRACK WAS LOCATED IN THE BEND RADIUS UNDER THE MAIN LANDING GEAR (MLG) SIDE BRACE ASSEMBLY (PN 95643-08). A NEW RIB WAS INSTALLED. BEFORESDR 2006FA0000432Rib · crackedRIB CRACKED IN FLANGE WHERE LANDING GEAR SIDE BRACE FITTING BOLTS. THE CRACK HAS BEEN NOTED ON LIKE MODELS (6 WINGS). ALL PREVIOUS NOTATIONS FOUND ON AC IN EXCESS OF 6000 HRS TO BE CAUSED BY AN IMPRESSION LEFT BY THE AN960-4 WASHER USED UNDER THE LOCKNUT. TSDR SWAA061295Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E MIDFLAP INBOARD END RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.SDR 2006FA0000433Rib · crackedINSPECTED RIB IAW SB 1161 AND FOUND RIB CRACKED. THE SAME RIB HAS BEEN FOUND CRACKED IN THE SAME LOCATION ON SIX OTHER WINGS. ALL OTHER WINGS HAD EXCESS OF 6000 HRS REPAIRED AND APPEARED TO HAVE BEEN INSTALLED CROOKED. THE ASSEMBLY PROCESS HAD THIS PART INSTSDR 2006FA0000437Rib · crackedDURING MODIFICATION OF AFT RIB IAW SB, 2 CRACKS WERE FOUND PROPAGATING FROM THE OB BOLT HOLE FOR THE ATTACHMENT OF (PN 9564307) BRACKET. (K)SDR TRAX200600053Rib · crackedRT BATTERY RIB CRACKED.SDR IXXA06RNG052SRib · crackedDURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STA XOLID 6.225. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-081 DATED MAYSDR IXXA06RNG051SRib · crackedDURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XFS 304.0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-077 DATED ASDR UPS06146734Rib · crackedINSPECTION TYPE:5 YR RT WING KRUGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED REINFORCABLE ANGLE IAW A300 SRM 51-40-21.SDR UPS06146722Rib · crackedLT WING NR 3 SPOILER LOCATION IN FLAP WELL INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL PER A300 SRM 51-40-00 AND 51-40-21.SDR UPS06146714Rib · crackedINSPECTION TYPE: 5YR, LT WING KRUGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED DOUBLER PER SRM 51-40-00 AND 51-40-21.SDR UPS06146685Rib · crackedRT WING NR 3 SPOILER LOCATION IN FLAP WELL INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL PER A300 SRM 51-40-21.SDR UPS06146684Rib · crackedRT WING T/E NR 4 SPOILER INTERCOSTAL CRACKED IN FLAPWELL. REMOVED AND REPLACED INTERCOSTAL PER A300 SRM 51-40-21.SDR 06FDEA1324Rib · crackedFOUND CRACKED INBOARD SUPPORT RIB AT RT WING SLAT TRACK NR 16. RIB REPLACED AS PER DRAWING ARB2850 AND ARB1129 AND ARB1323 AND SRM 51-31-01 VOL2 AND 51-33-01 VOL2 (MAJOR REPAIR).SDR 06FDEA1323Rib · crackedFOUND CRACKED INBOARD SUPPORT RIB AT LT WING SLAT TRACK NR 16. RIB REPLACED AS PER DOUGLAS DRAWING ARB2850 AND SRM 51-31-01 VOL2 AND SRM 51-33-01 VOL2 (MAJOR REPAIR).SDR USAA060576Rib · crackedLT WING, RIB 6 AT AFT APERTURE OF REFUEL PIPE ATTACHMENT HOLE CRACKED. REPAIR KIT P/N 57257026000 INSTALLED ON LT WING RIB 6 PER EA 96297 AND AIRBUS DWG R57257026 ISSUE C, DEFECT SIZE: 0.063 INCH.SDR DHL2006764515Rib · crackedREF ASTAR N/R 015815 DISCREPANCY: NR 6 SLAT OB ACT ROD END MOUNT RIB CRACKED REMOVED AND REPLACED RIB NR 6 SLAT OB ACT ROD END MOUNT PO NR 619549 P/N 65-17294-14 IAW B727 SRM 51-30-2.SDR USAA060523Rib · crackedRIB 6 RIGHT WING STA 3621 BETWEEN STR 19 & 20 CRACK. RIB 6 REPAIRED PER EA 97506, AIRBUS DWG R57257026, DEFECT SIZE: 0.050 INCH.SDR SWAA061043Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER SWA ACO.SDR ASOA06339Rib · crackedDURING A C-CHECK, THE RT SIDE BATT RIB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE BATT RIB IAW EO. (K)SDR UPS06846518Rib · crackedINSPECTION TYPE:C3 LT CENTER LE XRS 323 RIB IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-0, 57-3-1 AND 51-01-20D.SDR 06FDEA1042Rib · crackedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: XORS 345 BETWEEN STR 42 AND STR 43 RIGHT WING, REWORKED AREA 0.354 INCH X 0.354 INCH AND CRACK 0.275 INCH LONG ON RIB ANGLE. TRIMMED LEG CAP FLUSH TO HORIZONTAL LEG TO COMPLETELY REMOVE CRACK, AND INSTALLEDSDR 06FDEA1041Rib · crackedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: XORS 345 BETWEEN STR 42 AND STR 43 RIGHT WING, REWORKED AREA 0.354 X 0.354 INCH AND CRACK 0.275 INCH LONG ON RIB ANGLE. TRIMMED LEG CAP FLUSH TO HORIZONTAL LEG TO COMPLETELY REMOVE CRACK, AND INSTALLED T-ANSDR DHL2006750511Beam · crackedSTA 1183 BULKHEAD VERTICAL BEAM IS CRACKED AT AFT FLANGE INBD AND OUTBD SIDE RBL 36. STOP DRILLED 2 CRACKS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. REMOVED GILLINER SUPPORT STRUCTURE FOR ACCESS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. LOCATED AND DRSDR UIEA200600043Rib · crackedLT WING UPPER FIXED TRAILING EDGE PANEL OUTBOARD SUPPORT RIB HAS A CRACK IN THE WEB. REPAIRED IAW SRM 51-40-02 FIG 1.SDR UIEA200600027Rib · crackedRT WING DRY BAY - LOWER CHORD OF RIB AT WS 1516 IS CRACKED IN TWO PLACES. REPLACED LOWER CHORD OF RIB IAW SB 747-2221 FIG 5.SDR 2006FA0000717Rib · crackedDURING COMPLIANCE WITH SB, LT AND RT RIBS FOUND CRACKED AS SUSPECTED. INSTALLED REPAIR KITS. LT DRAG BRACE PIVOT, PN 39479002, ALSO FOUND CORRODED AND CRACKED. THIS IS NOT PART OF SB INSPECTION. (K)SDR UPS06446626Rib · crackedINSPECTION TYPE:C LHW NR 6 VC FLAP O/B ARM O/B RIB O/B SIDE CTR VERTICAL STIFFENER FASTENER HOLES CRACKED AT HOLES 1100, CRACK LENGTH 1.9". LHW NR 6 VC FLAP O/B ARM O/B RIB O/B SIDE CTR STIFFENER REPAIRED AS PER HX RS NR R57-41-35411 PERFORM DVI AT THE AFFECTSDR ABXA060170Rib · brokenRIGHT WING LEADING EDGE, OUTBOARD CLOSURE RIB, FORWARD EDGE OF THE HORIZONTAL FLANGE AT WING STA XS 526, BROKEN OFF. ACCOMPLISHED BLEND OUT REPAIR AT RIGHT WING LEADING EDGE CLOSURE RIB IAW REA D857-53072.SDR UPS06446631Rib · crackedRT WING NR 17VC FLAP O/B ARM O/B RIB ILES 766 TOP FLANGE I/B AND O/B SIDE FASTENER HOLE CRACK AT SEVERAL LOCATION. RHW NR 17 VC FLAP O/B ARM O/B RIB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR DHL2006750501Rib · crackedR/W L/E STA171 PANEL SUPPORT RIB CRACKED AT LIGHTING HOLE. REMOVED DAMAGED RIB AT R/W L/E STA 171, O/B OF DEFUEL VALVE IAW B727 SRM 51-30-2. FABRICATED RIB FROM 2024-T3 0.40 SIZE 15" BY 7" PO 9002715, IAW B727 SRM 51-20-1, AND SRM 57-20-2. TREATED AND PRIMESDR DHL2006760510Rib · crackedL/WING NR 1 L/E SLAT ACTUATOR ROD END I/B ATTACH BRACKET SHOWS CRACK. REMOVED AND REPLACED RIB AND SUPPORT CHANNEL L/WING NR 1 L/E SLAT ACTUATOR ROD END I/B IAW B727SRM 51-30-2, 51-10-1.SDR UPS06446640Rib · crackedINSPECTION TYPE:C RT WING NR 21 VC FLAP O/B ARM O/B ROTARY SUPPORT RIB O/B TOP FLANGE CRACKED AT ILES 1094 APP, CRACK LENGTH 1/4" TO 1.25". RT WING NR 21 VC FLAP O/B ARM O/B ROTARY SUPPORT RIB REPAIRED AS PER RS NR R57-41-35464 PERFORM DVI. REQUIRE AT THE AFSDR DJFA2006212Rib · crackedDURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING A PHASE A/B INSPECTION, A CRACK WAS DISCOVERED IN THE TRAILING EDGE OF RIGHT WING RIB OUTBOARD OF THE FLAP ACTUATOR.SDR USAA060407Rib · crackedIN SPAR LOWER AFT SUPPORT RIB 135.5 CRACKED. REPAIRED IAW 97467, DEFECT SIZE: 1.250 INCH.
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