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 CA060810004Rib · cracked(CAN) DURING NR 3 INSPECTION CRACK LOCATED IN (D) RIB JUST OB OF WING STRUT. LT WING. (TC NR 20060810004)SDR TRAX200600540Rib · crackedRANRC NR 163// RT BATT RIB CRACKED.SDR 06FDEA2669Rib · damagedFOUND RIB AT BL 70.5 FASTENER HOLE REWORK AND REPAIR. COMPLIED WITH WRI 57-10/0252 EO. 7-5710-7-2308I PART 2.SDR TRAX200600528Rib · crackedFOUND LT MLG WHEEL WELL BATTERY RIB IS CRACKED.SDR 06FDEA2605Frame · crackedLT WING L/E STA XORS 164 LOWER SECTION FOUND 1EA CRACK ON FORMER 1 INCH LONG. FORMER REPAIRED IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. PARTS FABRICATED IAW SRM 57-00-01 SHT 2 VOL 1.SDR SWAA062522Rib · crackedDURING SCHEDULED 8Y CHECK, FOUND RT WING OUTBOARD DEFLECTION CONTROL RIB CRACKED AT WBL 413 UPPER RADIUS. REPAIRED RIB PER SWA EA.SDR CA060716001Rib · cracked(CAN) WING CENTER RIBS AT STATION 190.0 IN BOTH WINGS WERE FOUND CRACKED AT THE TRAILING EDGE WERE THEY ATTACH TO THE AUX REAR SPAR OF THE WING. STN 190.0 IN THE OB AILERON HINGE ATTACH POINT. IT IS SUSPECTED THAT AT SOME TIME THIS AIRCRAFT WAS SUBJECTED TO WISDR UPS06847527Rib · crackedINSPECTION TYPE:C1-3 LT CENTER WING L/E UPPER RIB CRACKED AT XFS 497. STOP DRILLED CRACKED RIB AT LT L/E WING STA XFS 497 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED DOUBLERS ON RIB AT LT L/E WING STA XFS 497 IAW SRM 57-03-03 FIG 5, AND SRM 51-1-20D.SDR UPS06847447Rib · crackedRT CENTER L/E UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK ON RIB AT LT L/E STA XFS 415 IAW SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E STA XFS 415 IAW SRM 57-03-03 FIG 5 AND SRM 57-02-00.SDR UPS06847444Rib · crackedLEFT WING CENTER L/E RIB CRACKED AT XFS 328. STOP DRILLED CRACK AT LT WING L/E RIB AT STA XFS 328 IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E WING STA XFS 328 IAW SRM 57-03-03 FIG 5, AND SRM 57-02-00.SDR UPS06847438Rib · crackedLT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK ON RIB ANGLE IAW SRM 57-2-0 AT STA XFS 304. FABRICATED AND INSTALLED REPAIR ANGLES AT STA L/WING STA XFS304 IAW SRM 57-02-0, AND 51-01-20D.SDR 06FDEA02514Rib · crackedLT WING NR 16 SLAT TRACK I/B RIB FOUND CRACKED. LT WING NR 16 SLAT TRACK ASSY REMOVED AND NR 8 SLAT CABLES NR 67 AND NR 68 DISCONNECTED FOR REMOVAL AND REPLACEMENT OF NR 16 SLAT I/B RIB AS PER SRM 51-31-01 VOL.II. SLAT TRACK ASSY NR 16 REINSTALLED AND NR 8 SSDR 06FDEA02513Rib · crackedRT WING NR 16 SLAT TRACK I/B RIB FOUND CRACKED. RT WING NR 16 SLAT TRACK ASSY REMOVED AND NR 8 SLAT CABLES NR 67 AND NR 68 DISCONNECTED FOR REMOVAL AND REPLACEMENT OF NR 16 I/B RIB AS PER SRM 51-31-01 VOL II. SLAT TRACK ASSY NR 16 REINSTALLED, NR 8 SLAT CABLSDR 06FDEA02526Rib · damagedEXISITING REPAIR AT RT WING LEADING EDGE XCW130 RIB INSTALLATION. EXISTING REPAIR AT RT WING LEADING EDGE XCW 130 RIB INSTALLATION EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 378545-14 EO 1-5100-7-5001A-PT1, TITLE: "SDR UPS06847573Rib · brokenINSPECTION TYPE:C1-3 RT CENTER L/E RIB BROKEN AT STA XW 408. REMOVED AND REPLACED RT CENTER L/E RIB AT STA XW 408 IAW SRM 51-03-00-0, 51-1-20D AND DWG 5769857.SDR UPS06847524Rib · crackedINSPECTION TYPE:C1-3 RT CENTER LE UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK ON UPPER RIB AT XFS 297 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED DOUBLERS AT RT WING STA XFS 297 IAW SRM 57-02-00 FIG2, AND SRM 57-03-00 FIG 13.SDR TRAX200600483Rib · crackedFOUND RIGHT BATTERY RIB CRACKED.SDR ABXA060228Strap · corrodedUPPER SPAR CAP STRAP AT RT WING STA 792 HAD INTERGRANULAR CORROSION. REPAIRED AREA IAW REA B657-54341.SDR UPS06447478Rib · crackedNR 1M FUEL TANK WS 862 RIB LOWER CHORD AT STR 6 FOUND CRACK, CRACK LENGTH 1/2"). LWR CHORD REPAIRED AS PER SRM 57-10-05 FIG 3SDR UPS06447679Rib · crackedINSPECTION TYPE:C RT WING L/E SUPPORT RIB FOUND CRACKED AT WS 767 JUST BEHIND NR 17 VC FLAP I/B ROTARY, CRACK LENGTH 0.3" TO 4.5" RESP. RHW L/E SUPPORT RIB AT WS 767 BEHIND NR 17 VC FLAP O/B ROTARY ACTUATOR AREA REPAIRED AS PER RS R57-41-35530 CONTINUE INSPECSDR UPS06447601Rib · crackedINSPECTION TYPE:C LT WING L/E UPPER SUPPORT RIB FOUND CRACKED AT WS 970 BEHIND NR 7 VC FLAP I/B CRACK LENGTH 0.5 TO 3.5 INCH. LT WING L/E UPPER SUPPORT RIB AT WS 970 BEHIND NR 7 VC FLAP I/B AREA REPAIRED AS PER RS R57-41-35528 CONTINUE INSPECTION IS REQUIRED SDR SWAA062317Rib · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING FUEL CELL INTERIOR MAIN BOX UPPER RIB CRACKED AT WBL 114, STR 1. REPAIRED RIB PER ER.SDR TRAX200600456Rib · crackedFOUND RT BATT RIB CRACKED.SDR 06FDEA2410Rib · crackedRT WING FIXED L/E RIB LWR CHORD IS CRACKED, LOCATED OUTBD OF KRUGER FLAP ACTUATOR.SDR HALA0600500Rib · corrodedFOUND CORROSION ON LEFT WING AT LES 485 UPPER RIB FLANGE. REMOVED CORROSION AT LES 485 UPPER RIB FLANGE 16 INCH BY .75" WIDE AND .002" DEEP. FOUND TO BE WITHIN LIMITS PER SRM 57-41-09/101. ALODINED AND APPLIED DECORATIVE FINISH IAW MM 51-21-04-377-001 AND MSDR HALA0600502Rib · corrodedFOUND CORROSION ON LT WING AT LES 456, UPPER RIB FLANGE. REMOVED CORROSION ON UPPER FLANGE LES 456 15" LONG .75" WIDE .003" DEEP. FOUND TO BE WITHIN LIMITS PER SRM 57-41-09/101. ALODINED AND RESTORED FINISH IAW MM51-21-04-377-001 AND MM51-221-10-307-020.SDR CA060626001Rib · cracked(CAN) DURING SCHEDULED INSPECTON, MAINTENANCE FOUND THE NR 1 LEADING EDGE SLAT ACTUATOR WING RIB ATTACH POINT CRACKED. CRACKED MOUNT SUPPORT REPLACED.SDR 06FDEA2150Rib · crackedLT WING NR 16 SLAT TRACK I/B RIB FOUND CRACKED 0.5 INCHES LONG. RIB REMOVED AND INSTALLED NEW RIB PER SRM 51-31-01 VOL.II. MAJOR REPAIR CLASSIFIED PER GMM 6-2-100.SDR 06FDEA2087Rib · crackedRIGHT WING L/E COMPT RIB FOUND CRACKED AT 20 INCHES O/B OF SLAT TRACK NR 12. REMOVED AND INSTALLED NEW RIB AS PER SRM 51-33-01 AND 51-35-01 VOL.II. MINOR REPAIR CLASSIFIED AS PER GMM 6-2-100.SDR SWAA061824Rib · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING RIB UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED WING CHORD PER ER.SDR DHL2006873530Rib · crackedNR 4 RIGHT STUB WING RIB 4 INCH CRACK STA XOLDO 67.750 (MAJOR REPAIR). REMOVED CRACKED RIB IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EA5SDR TRAX200600257Rib · crackedLT BAT RIB CRACKED.SDR TRAX200600220Rib · crackedRT BATT RIB CRACKED. REPAIRED RT BATT RIB IAW R.E.O. 601R-57-51-046 (CLOSED)SDR SWAA061588Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED WING RIB PER SRM.SDR UPS06146861Rib · crackedINSPECTION TYPE:5YR LT WING KRUEGER FLAP AREA RIB 2 IS CRACKED/CHAFED THRU. FABRICATED AND INSTALLED REPAIR IAW UPS ENGINEERING FILE NUMBER A300-57-20019 AND SAA EA 300-5741-01-A0184.SDR CA060505003Rib · crackedRIB ASSEMBLY ON WING CRACKED AT ATTACHMENT POINT TO SPAR. SPAR WAS UNDAMAGED BUT TRACK WAS REPLACED. AIRCRAFT HAS 10870.3 HOUR ON IT AT TIME OF REPAIR POSSIBLE TIME FATIGUED PART.SDR SAI050601Cap · crackedDURING THE ROUTINE CQB 03-1 400 HR EDDY CURRENT INSPECTION A CRACK IN THE UPPER LEFT CANTED RIB NEAR THE AFT SIDE OF THE FORWARD MAIN SPAR BEHIND THE HYDRAULIC COMPONENTS AT APPROX FS 179.6. THE CRACK WAS APPOX 1-1.5 INCHES LONG. THE CAP WAS REPLACED PER CESSDR SAI050602Cap · crackedCRACK FOUND DURING ROUTINE CQB 03-1 EDDY CURRENT INSPECTION OF RIGHT UPPER CANTED RIB CAP APPROX 1.5 INCHES FS 179.6. THE UPPER CANTED RIB CAP WAS REPLACED PER CQB 03-1 AND SK441-110B WITH IMPROVED PART 5790066-11. DURING REINSTALLATION OF HI-LOKS AND RIVETSSDR UPS06446996Rib · crackedINSPECTION TYPE:C LEFT WING - SURGE TANK WS 1516 RIB LWR STR 6 & 9 SUSPECT CRACK. CRACK LENGTH 1.125 INCH. LEFT WING WS 1516 RIB LWR STR -9 AREA REINSPECTED BY NDT, NO CRACK REVEALED AND STR -6 AREA REPAIRED AS PER SRM 57-10-05 FIG 4.SDR UPS06446995Rib · crackedINSPECTION TYPE:C RIGHT WING SURGE TANK WS 1516 RIB UPPER CHORD STR 8 FOUND CRACKED. CRACK LENGTH 0.625 INCH. RIGHT WING SURGE TANK WS 1516 RIB UPPER CHORD STR 8 AREA REPAIRED AS PER SRM 57-10-05 FIG 3.SDR UPS06446994Rib · crackedINSPECTION TYPE:C RIGHT WING SURGE TANK WS 1516 RIB LOWER CHORD STR 6 AND STR 8 FOUND CRACKED. CRACK LENGTH 0.75 INCH & 1 INCH. RIGHT WING SURGE TANK WS 1516 RIB LOWER CHORD STR 6 TO THE FWD END AREA REPAIRED AS PER SRM 57-10-05 FIG 4.SDR TRAX200600184Rib · crackedRT WING BAT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046 (CLOSED)SDR TRAX200600183Rib · crackedLT WING WHEEL WELL BATT RIB CRACKED.SDR 061157Rib · chafedRIGHT WING L/E RIB AT FSSI 1022 IS CHAFED.SDR 061156Rib · chafedRIGHT WING L/E RIB AT FSSI 887 IS CHAFED.SDR A6WA200640163Rib · crackedFOUND LT WS 53.60 BATT RIB ASSEMBLY HAS A .5 INCH CRACK AT TOP CORNER. REPAIRED BATTERY RIB BY REMOVING DAMAGED AREA AND INSTALLING REPAIR ANGLE DOUBLE AND FILLER IAW BOMBARDIER REO 601R-57-51-046 REV B. (M)SDR UPS06146859Rib · crackedFOUND LT WING KRUEGER FLAP WELL RIB CRACKED. REMOVED AND REPLACED RIB PER A300 SRM 51-40-21 AND 51-40-00.SDR 2006UALA00864Rib · damagedRIB FOR LT LEADING EDGE LOCATED AT THE WING TIP IS CRACKED. REPAIR ANGLES INSTALLED.SDR 06FDEA1624Rib · crackedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: LT WING STA XORS 345, BETWEEN STR 13-14, TOP OF THE RIB, CRACK 1 INCH LONG. PERFORMED REPAIR IAW FEDEX EA 8-5710-96133.SDR UPS06846783Rib · crackedFOUND LT LEADING EDGE AT STA XFS 841.250 RIB IS CRACKED. STOP DRILLED CRACK AT LT L/E AT STA XFS 841.250 IAW SRM 57-02-00-0 FIG 002. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLERS IAW DWG 5769470, AND SRM 57-02-00, AND SRM 51-1-21
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