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 UPS98827305Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS XFS 778.750. REPAIRED IAW SRM 57-2-0.SDR UPS98827304Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS 691.250 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98827303Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.SDR UPS98827301Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS XFS385.25 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW 57-2-0.SDR UPS98827300Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB CRACKED AT WS XFS 847.5 UPPER AFT END. REPAIRED IAW SRM 57-2-0.SDR SWAA981477Rib · crackedDURING SCHEDULED C4 CHECK, FOUND CRACKED I/B AFT UPPER WING PANEL STUB RIB. REPAIRED PER BOEING SRM.SDR TWAA9812209Rib · crackedDURING CHECK-C, FOUND CRACK 17 IN LONG AT BOTTOM OF RT WING RIB WEB ANGLE, 27 IN O/B OF WING BODY FAIRING, FWD. REMOVED AND REPLACED WEB ANGLE AT O/B END OF WING BODY FAIRING, PER SRM 51-10-1, AND 51-40-3.SDR UPS98827516Rib · crackedINSPECTION TYPE-D, RT WING L/E AT STA XFS653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827256Rib · crackedINSPECTION TYPE-D, RT WING L/E AT WS XFS 822.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-1.SDR UPS98827293Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 297.500. REPAIRED IAW SRM 57-2-0.SDR UPS98827263Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED WS XFS 697.5. REPAIRED IAW SRM 57-2-0.SDR UPS98827260Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS 576.75. REPAIRED IAW SRM 57-2-0.SDR UPS98827254Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 283.250. REPAIRED IAW SRM 57-2-0.SDR AU980838Rib · corroded(AUS) LT AND RT WING NR 2 NOSE RIBS LOCATED AT STN 32.75 ADJACENT TO THE LEADING EDGE CABIN AIR DUCTS SEVERELY CORRODED. PART TOTAL CYCLES: 12,704.SDR UPS98227166Rib · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED ON RT WING RIB AT WS 656.5 STR 6 LOWER. REPLACED CRACKED RIB WITH NEW RIB PER EO B727-5710-1325.SDR UPS98227165Rib · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED ON LT WING RIB AT WS 6565 STR 6 LOWER. REMOVED CRACKED RIB REPLACED WITH NEW RIB IAW EO B727-5710-1325D.SDR DHL9872170DRib · crackedAT D-CHECK, LT WING TIP OUTER RIB HAS CRACK EXTENDING OUT FROM OVAL ACCESS PANEL OPENING, LOWER AFT CORNER. ACCOMPLISHED HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 4 X 10 X 1. N/R 1283.SDR DHL9872156DRib · crackedAT D-CHECK, LT WING TIP OUTER RIB CENTER VERTICAL SUPPORT BRACKET HAS CHAFED AREA OF FWD SIDE, SMALL BULB SEAL DETERIORATED TOP FLANGE OF BRACKET IS CRACKED WITH ONE NUT PLATE BROKEN OFF. REPLACED VERTICAL SUPPORT BRACKET AT LT WING TIP OUTER RIB PER SRM 51-3SDR DHL9872120DRib · corrodedAT D-CHECK, RT WING FIXED L/E SUPPORT RIB ON THE O/B SIDE AT FWD END IS CORRODED. FABRICATED AND AND INSTALLED ATTACH FITTING PER SRM 51-30-2. CUT OUT RIB SUPPORT AND INSTALLED RIB REPAIR PER SRM 51-40-2, 6 X 4'. N/R 2462.SDR C2XA98IA256Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE SUPPORT AT RIB NR 30 CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TCSDR CALA9801224Rib · crackedINSPECTION FOUND A 3.5 INCH CRACK IN LT WING LEADING EDGE RIB AT HI-LOK IN UNDERSIDE OF LEADING EDGE AT XOS 516. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED ON RIB IAW SRM 57-02, FIGURE 6 AND 51-10-3. THE RIB WAS REINSTASDR 98ZZZX2673Rib · crackedAT ANNUAL INSPECTION, FOUND THE NOSE RIB UNDER THE WING WALK AREA CRACKED IN TWO PLACES. REPLACED RIB.SDR AU980851Rib · corroded(AUS) LEFT AND RIGHT WING NR 2 NOSE RIBS LOCATED AT STN 32.75 ADJACENT TO THE LEADING EDGE CABIN AIR DUCTS SEVERELY CORRODED. PART TOTAL CYCLES: 12,650.SDR P2EA98124Rib · crackedSJO - DURING C-CHECK, WHILE REMOVING RT WING INBOARD MID-FLAP TO FACILITATE OTHER MAINTENANCE OBSERVED TWO RIBS CRACKED AT WBL 87.7. NEWS RIBS FABRICATED BY COOPESA MACHINE SHOP AS PER COOPESA EO NR C00-3-57-330-98. INSTALLED IAW SRM 51-10-1 PAGE 5 AND 51-30SDR CALA9801198Rib · crackedINSPECTION FOUND A .375 INCH CRACK IN UPPER OUTBOARD FLANGE OF RT WING RIB AT WS 171.5, STRINGER 16. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6.SDR P2EA98122Rib · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-10-5726C, A CRACK WAS FOUND ON A RIB OF THE RT WING, INBOARD MID-FLAP. THE CRACK WAS LOCATED AT WBL 83 AND WAS 1 INCH IN LENGTH. THE RIB WAS REPLACED IAW SRM 51-10-1 PAGE 6. RIVETS REPLACED IAWSDR UPS98827154Rib · crackedINSPECTION TYPE-C ,LT WING LE RIB UPPER ARM CRACKED BY AFT FASTENER AT WS XFS 572.500. REPAIRED IAW SRM 57-2-0.SDR UPS98827108Rib · crackedINSPECTION TYPE:C, LT WING L/E AT STA XFS703.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827107Rib · crackedINSPECTION TYPE:C, LT WING L/E AT STA XFS803.750, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827106Rib · crackedINSPECTION TYPE:C, LT WING L/E AT STA XFS810.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827105Rib · crackedINSPECTION TYPE:C, LT WING L/E AT STA XFS797.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827104Rib · crackedINSPECTION TYPE:C, LT WING L/E AT STA XFS760.00, THE L/E RIB IS CRACKED AT THE AFT END, STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98827148Rib · crackedINSPECTION TYPE-C, RT WING L/E LWR RIB AT WS XOLDI 6.225 IS CRACKED AT THE FWD END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769891.SDR UPS98827112Rib · crackedINSPECTION TYPE:C, RT WING L/E UPPER RIB AT STA XFS304.00 IS CRACKED AT THE FWD END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR TWAA9810610Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND A CRACK IN AFT FASTENER RIB, 18 IN OUTBOARD OF NR 5 SLAT CENTER TRACK RIB IN LE OF LEFT WING. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. REPLACED HI-LOKS PER SRM 51-30-5. REPLACED RIVETS PER SRM 51-30-5. (M)SDR ABXA9800717Rib · crackedLEFT WING LEADING EDGE LOWER RIB ARM CRACKED BY AFT FASTENER AT STATION XFS 816.250. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-21.SDR ABXA9800703Rib · crackedRIGHT WING LEADING EDGE AT STATION XOLDI 6.225, UPPER LEADING EDGE RIB HAS A 4 CRACK. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21.SDR ABXA9800683Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 778.750 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING K05056.SDR ABXA9800682Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 716.250 IS CRACKED AT AFT LOWER END. REPAIRED RIB IAW DRAWING K05056.SDR MWEA98735Rib · corrosionCORROSION WAS FOUND ON LT WING INTERNAL RIB AT STATION XRS 164 ON THE LOWER HORIZONTAL FLANGES. REMOVED CORROSION AND INSTALLED REPAIR STRAP USING APPROVED DATA.SDR MWEA98731Rib · corrosionLEFT WING RIB AT STATION XRS 69 HAS CORROSION ON LOWER RIB CAP. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR USING APPROVED DATA.SDR MWEA98657Rib · crackedFOUND 1 INCH CRACK ON LEFT WING NUMBER 2 SLAT DRIVE OUTBOARD RIB AT XRS 214. MTC FABRICATED AND INSTALLED NEW NOSE RIBS.SDR CALA9801065Rib · crackedINSPECTION FOUND THREE .75 INCH CRACKS IN RT WING LEADING EDGE RIBS AT STA XRS 276.5, XRS 270, AND XRS 289. THE RIBS WERE REMOVED AND NEW RIBS WERE INSTALLED IAW ECRA 5721-01008.SDR CALA9801028Rib · crackedINSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB ADJACENT TO OUTBOARD SLAT ACCESS PANEL, OUTBOARD SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-21-01, AND 51-31-01.SDR CALA9801027Rib · crackedINSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB IN FRONT OF NR 5 LEADING EDGE SLAT. THE RIB WAS REPAIRED IAW SRM 57-20-00, FIGURE 1 AND 51-31-01.SDR CALA9801026Rib · crackedINSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB IN BETWEEN XORS 855 AND XORS 917. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-01-01, AND 51-31-01.SDR UPS98827011Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XS467.323 IS CRACKED. REPAIRED IAW SRM 57-2-0.SDR UPS98826948Rib · crackedINSPECTION TYPE:D, RT WING L/E AT STA XFS291.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826947Rib · crackedINSPECTION TYPE:D, RT WING L/E AT STA XFS297.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98826946Rib · crackedINSPECTION TYPE:D, RT WING L/E AT STA XFS 397.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.
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