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.

SDR DL72S981918Rib · crackedUPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. REPAIRED PER ERA 332223-14.Sep 15, 1998 · N408DA · Boeing 727232SDR ABXA9801000Rib · crackedRIGHT WING LEADING EDGE LOWER RIB CRACKED FORWARD OF ACCESS PANEL, STATION XFS 766.250. REPAIRED IAW SRM 57-3-1, 51-1-20D, 51-1-8 AND DWG 576947122.Sep 15, 1998 · N844AX · Doug DC861SDR SWAA982077Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND UPPER I/B, T/E PANEL RIB CRACKED. REPAIRED PER BOEING SRM.Sep 10, 1998 · N307SW · Boeing 7373H4SDR ABXA9800953Rib · crackedRIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END, STATION XFS 635.000. REPAIRED IAW DWG KO5056 AND DC8 SRM 57-2-0.Sep 10, 1998 · N844AX · Doug DC861SDR ABXA9800952Rib · crackedRIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END, STATION XFS 628.750. REPAIRED IAW DWG KO5056 AND DC8 SRM 57-2-0.Sep 10, 1998 · N844AX · Doug DC861SDR ABXA9800948Rib · crackedRIGHT WING LOWER LEADING EDGE RIB IS CRACKED FORWARD OF ACCESS PANEL AT STATION XFS622.5. REPAIRED IAW DC8 SRM 57-2-0.Sep 10, 1998 · N844AX · Doug DC861SDR CALA9801655Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT WING TIP RIB UPPER FLANGE BY INBOARD AFT CORNER OF FUEL VENT OUTLET. THE CRACK WAS STOP DRILLED IAW SRM 51-30-2. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.Sep 9, 1998 · N93738 · Boeing 727224SDR DHL9870837CRib · crackedAT C-CHECK, STA 546 RT WING RIB LOWER ANGLE CRACKED AT SECOND FROM FWD STR BOLT HOLE. STOP DRILLED CRACK, HFEC, REMOVED AND REPLACED RIB PER S/B 57-0127. N/R 2454Sep 8, 1998 · N708DH · Boeing 72725SDR DHL9870836CRib · crackedAT C-CHECK, RT WING LOWER RIB ANGLE CRACKED AT 3RD FROM AFT STRINGER BOLT HOLE. STOP DRILLED CRACK, HFEC, REPLACED WING RIB PER S/B 57-0127. N/R 2455Sep 8, 1998 · N708DH · Boeing 72725SDR CALA9801640Rib · crackedINSPECTION FOUND A 2.75 AND 1 INCH CRACK IN RIB INSIDE RT WINGTIP, ACCESSED THROUGH PANEL NR 8811. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.Sep 8, 1998 · N93738 · Boeing 727224SDR C2XA98IA350Rib · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING OUTBOARD LEADING EDGE ATTACH RIB ON THE FRONT SPAR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIB IAW ATR SRM 57-20-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Sep 8, 1998 · N14815 · Aerosp ATR42320SDR ABXA9800961Rib · crackedRIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END AT STATION XRS678.750. REPAIRED IAW DC9 SRM 57-20.Sep 4, 1998 · N844AX · Doug DC861SDR ABXA9800960Rib · crackedRIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END AT STATIONS XFS 733.000. REPAIRED IAW DC8 DWG K05056.Sep 4, 1998 · N844AX · Doug DC861SDR ABXA9800958Rib · crackedRIGHT LEADING EDGE UPPER RIB IS CRACKED AT AFT END AT STATION XFS728.750. REPAIRED IAW DC8 DWG KO5056.Sep 4, 1998 · N844AX · Doug DC861SDR DLL14981828Rib · crackedTHE RT WING IWS 503 RIB UPPER CAP, LT WING IWS 555 RIB UPPER CAP WERE BOTH FOUND CRACKED. ALL CRACKED PARTS WERE REPLACED.Sep 3, 1998 · N741DA · Lkheed 1011385115SDR DHL9870824CRib · crackedAT C-CHECK, RT WING L/E RIB O/B SIDE SLAT STA 0.260 HAS SEVERAL CRACKS IN REPAIR ANGLE. REPLACED ANGLE 16 X 1 X 1 PER SRM 51-10-1. N/R 2386Sep 3, 1998 · N708DH · Boeing 72725SDR DHL9870822CRib · crackedAT CHECK, RT WING HAS CRACK AT L/E RIB STA 260 FASTENER UPPER COVE AREA INSIDE. REMOVED ANGLE REPAIR, STOP DRILLED, HFEC INSPECTION, INSTALLED REPAIR PER SRM 51-40-3. N/R 2381Sep 3, 1998 · N708DH · Boeing 72725SDR UPS98827670Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB AT STA XS484.895 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 1, 1998 · N709UP · Doug DC871FSDR DLL14981827Bulkhead Fitting · crackedTHE RT WING PYLON BACKUP FITTING BULKHEAD WAS FOUND CRACKED. A DOUBLER REPAIR IS INSTALLED.Sep 1, 1998 · N741DA · Lkheed 1011385115SDR DHL9870831CRib · crackedAT C-CHECK, INSPECTED LOWER RIB CHORDS AT WS 601.5 PER S/B 57-0127. FOUND LOWER FLANGE OF RIB CRACKED AT STR 8. STOP DRILLED AND INSTALLED ANGLE REPAIR PER SRM 57-10-5, 22.5 X 2. N/R 1615Sep 1, 1998 · N708DH · Boeing 72725SDR UPS98827653Rib · crackedINSPECTION TYPE:C LT WING L/E RIB AT W/S XFS 297.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Aug 28, 1998 · N706UP · Doug DC871FSDR CALA9801563Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING TIP RIB AT PANEL NR 8110. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 26, 1998 · N14788 · Boeing 727232SDR AU981086Rib · damaged(AUS) LEFT WING RIBS LOCATED IN THE LEFT WHEEL WELL DISTORTED AND RIVETS SHEARED.Aug 24, 1998 · Piper PA34200TSDR DL72S981724Rib · crackedUPPER CHORD OF THE LT WING RIB AT WS 171.5 WAS FOUND W/CRACKS. THE CRACKS WERE LOCATED EMANATING FROM FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER WING STRINGERS 17 AND 20. REPAIRED PER ERA 332081-14.Aug 21, 1998 · N405DA · Boeing 727232SDR CALA9801482Rib · gougedINSPECTION FOUND A GOUGE IN LT WING LEADING EDGE RIB INBOARD OF NR 3 SLAT. A REPAIR ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-21-31.Aug 18, 1998 · N14245 · Boeing 7372C0SDR UPS98227517Rib · crackedINSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CRACKED. REPLACED RIBS IAW SRM AND DRAWING 657276, REINSTALLED NR 4 SLAT EYE BOLT IAW MM 27-81-32.Aug 14, 1998 · N905UP · Boeing 72751CSDR DL72S981676Rib · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. THE CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE 2 FWD MOST FASTENER HOLES AND TRAVELS DOWN, THRU THE ENTIRE THICKNESS OF THE HAug 14, 1998 · N405DA · Boeing 727232SDR AU981046Rib · cracked(AUS) RIGHT WING RIB DOUBLER CRACKED. CRACK LENGTH APPROXIMATELY 9.525MM (0.375 INCH).Aug 14, 1998 · Cessna 402ASDR AU981045Rib · cracked(AUS) LEFT WING RIB DOUBLER REPAIR CRACKED.Aug 14, 1998 · Cessna 402ASDR UPS98227564Rib · crackedINSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727-5710-0314.Aug 12, 1998 · N905UP · Boeing 72751CSDR UPS98227561Rib · crackedINSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314 FIG 13.Aug 12, 1998 · N905UP · Boeing 72751CSDR ABXA9800772Rib · crackedRIGHT WING LEADING EDGE AT STATION 316.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DRAWING K 05056 AND DC8 SRM 51-1-20D.Aug 11, 1998 · N803AX · Doug DC862SDR ABXA9800771Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 360.250 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.Aug 11, 1998 · N803AX · Doug DC862SDR ABXA9800777Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 560.00 UPPER LEADING EDGE RIB IS CRACKED. REPAIRED IAW DC8 SRM 57-3-2 AND DWG K 5056.Aug 5, 1998 · N803AX · Doug DC862SDR ABXA9800775Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 722.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW ABX DWG K 05056 AND DC8 SRM 51-1-20D.Aug 5, 1998 · N803AX · Doug DC862SDR TWAA9812704Rib · damagedDURING MAINT, FOUND RT WING RIB DAMAGED AT SLAT TRACK OPENING XOS=610, IDLER TRACK NR 15. REMOVED AND REPLACED RIBS PER SRM 51-20-2, 51-30-5, AND 51-30-8, AND STANDARD MAINTENANCE PRACTICES.Aug 2, 1998 · N9620D · Doug DC983SDR QXEA9801181Rib · chafedLEADING EDGE RIB BETWEEN PANEL 92J AND 62A IS CHAFED IN SEVERAL PLACES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 A-C AND HORIZON AIR EA 4-57-1573.Jul 31, 1998 · N498US · Fokker F28MK4000SDR CA980818010Rib · cracked(CAN) ON WALK-AROUND, FOUND INSPECTION DOOR PANEL AT RIGHT HAND WING LOWER LEADING EDGE, LOWER SURFACE, OUTBOARD OF NR 3 PYLON AT DROOP LEADING EDGE WITH PULLED SCREWS AND WORN HOLES. FURTHER INSPECTION REVEALED RIB, ARB2339-4, ANGLE ARB3013-13, SILL ARB1334-Jul 31, 1998 · Doug DC1030SDR ABXA9800749Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XS 250-089 IS CRACKED ABOVE PNEUMATIC DUCT. FABRICATED REPAIR ANGLE IAW DC8 SRM 57-2-0.Jul 30, 1998 · N803AX · Doug DC862SDR ABXA9800748Rib · crackedRIGHT WING LEADING EDGE AT STATION XS 250-089 UPPER RIB IS CRACKED ABOVE PNEUMATIC DUCT. FABRICATED REPAIR ANGLE IAW DC8 SRM 57-2-0.Jul 30, 1998 · N803AX · Doug DC862SDR ABXA9800747Rib · crackedRIGHT WING LEADING EDGE AT STATION XILAI 7-295 THE UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DC8 SRM 51-1-8.Jul 30, 1998 · N803AX · Doug DC862SDR 99ZZZX708Rib · crackedDURING A PHASE INSPECTION, FOUND A 1.25 INCH CRACK IN THE RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS APPROXIMATELY 1.25 INCHES IN LENGTH. STOP DRILLED BOTH ENDS OF CRACK PER CESSNA INSTRJul 28, 1998 · N2628M · Cessna 441SDR 98ZZZX3059Rib · crackedDURING A PHASE INSPECTION, A CRACK WAS FOUND IN THE RIGHT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS AND IS APPROXIMATELY ONE INCH IN LENGTH. CRACK WAS STOP DRILLED AT BOTH ENDS PER CESSNA Jul 27, 1998 · N441RK · Cessna 441SDR UPS98827414Rib · crackedINSPECTION TYPE:C RT WING T/E RIB AT STA XW 3.00, IS CRACKED IN 4 PLACES. REPAIRED AREA IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827401Rib · crackedINSPECTION TYPE:C RT WING L/E AT STA XFS 329.000- THE LWR L/E RIB IS CRACKED AT MID SPAN. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827316Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 810.000. REPAIRED IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827315Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 772.5. REPAIRED IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827313Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS XFS 397.75 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827308Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS XFS 597.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871FSDR UPS98827306Rib · crackedINSPECTION TYPE-C, RT WING L/E AT WS XFS 697.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Jul 25, 1998 · N715UP · Doug DC871F
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