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 MWEA011090Rib · gougedGOUGE ON INBOARD SLAT SUPPORT TRACK STATION 480.871. REMOVED AND REPLACED RIB.SDR UPS01836507Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836506Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE UPPER RIB RIB IS CRACKED AT XFS 691.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836505Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 697.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836504Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836503Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 609. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836502Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 616. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836501Rib · crackedINSPECTION TYPE:C2 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 641. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836500Rib · crackedINSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2SDR UPS01836382Rib · crackedINSPECTION TYPE:C2 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 622.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR AUS20010825Rib · cracked(AUS) WING RIBS LOCATED IN LH WHEEL BAY CRACKED AS INDICATED IN CESSNASERVICE LETTER ME76-2.SDR 2001FA0000259Rib · damagedFOUND LOOSE AND/OR MISSING NAILS AT RIB/FRONT SPAR CONNECTION. 2 RIBS ON RT WING AND 2 RIBS ON LT WING FOUND DAMAGED WHILE INSPECTING PER REGMENTS OF AD.SDR DHL2001803503Rib · brokenAT C CK; LH WING-CLOSING RIB BROKEN ON INBOARD AILERON RH LATERAL PART. REMOVED FASTNERS IAW SRM 51-1-21A, PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-1, PAR. 1, SRM 51-1-21A, PG 1. REF: N/R 0616. SDR CLSDR UPS01836352Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 678.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836351Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 397.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836322Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR 2001FA0000035Rib · crackedWHILE DOING A SCHEDULE VISUAL INSPECTION OF THE WING IT WAS NOTED A CRACK WAS IN RIB WEB. THE RIB IS LOCATED NEXT TO THE LAST OUTBOARD LEFT WING. CRACK IS 7 INCH LONG ALONG THE THE BOTTOM SIDE THEN TURNS UP AT BOTH ENDS FOR 1 INCH. REMOVED AND REPLACED WITHSDR RRXA11292Rib · chafedDURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO LT WING L/E RIB AT STA. XS250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2.SDR RRXA11291Rib · chafedDURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO LT WING CENTER L/E RIB AT STA. XS510, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0 FIG2A.SDR UPS01836074Rib · crackedINSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 722.5, XFS 728.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01836073Rib · crackedINSPECTION TYPE:C2,3 LEFT WING OUTBOARD L/E RIBS ARE CRACKED AT XFS 791.25, XFS 755.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01836072Rib · crackedINSPECTION TYPE:C2,3 LEFT WING O/B RIB IS CRACKED AT XFS 653. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01436144Rib · crackedINSPECTION TYPE:C RHW NR 3 FUEL TANK WS 557.42 WING INTERSPAR RIB WEB CRACK. REPAIR C/OUT AS PER SRM 57-10-05.SDR UPS01836066Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E HAS CRACKED UPPER RIB AT XFS 572.5, AND LOWER RIB AT XFS 566.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01836068Rib · damagedINSPECTION TYPE:C2,3 RIGHT WING OUTBOARD L/E RIB WEB IS TORN AT XW 761. REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 5769467 AND SRM 57-1-0, 51-1-21.SDR RRXA11187Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO LT WING L/E UPPER RIB AT STA. XFS 610, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0 SDR RRXA11184Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E LOWER RIB AT STA. XFS622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-3-0, 57-2-0 FIG.2.SDR AJP2001F00001Rib · crackedWHILE PERFORMING INSPECTION, SHORT CRACKS (.1250 - .3750) FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ISSUSTRATED IN SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW WHILE LANDING/ TAXIING. NO AD OR STR RELATED TO FAILURE.SDR AJP2001F00000Rib · crackedWHILE PERFORMING INSPECTION, SHORT CRACKS (APPROX .1250 - .3750), FOUND IN CENTER RIB, CRACKS ARE AS DESCRIBED AND ILLUSTRATED IN SB. SUSPECTED CAUSE: EXCESSIVE CYCLES, EXCESSIVE YAW, WHILE LANDING AND TAXIING. NO AD OR STC RELATIONSHIP ADDRESSES INSPECTIONSDR 20010515AP002Rib · crackedDURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CANTED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT APPROXIMATELY 1.375 INSDR 20010515AP001Rib · crackedDURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CANTED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT APPROXIMATELY 1.375 INSDR AALA20010988Rib · crackedTUL - FOUND DURING SCHEDULED C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LBL 70.5 UPPER RIB CHORD AT BS 760. INSTALLED THE PREVENTATIVE MODIFICATION 65C33202-99 PER BOEING 727 SB 727-57-0112 WITH DEVIATION PER ESO 11697 DATED 5-9-2001. (M)SDR AALA20011029Rib · crackedTUL - FOUND CRACK IN RADIUS AT LEFT STATION 760 RIB CHORD. ROUTED OUT DAMAGE. INSTALLED REPAIR PER S/B 727-57-0112 AND ESO 11697 DATED 5/9/01. (M)SDR 20010604CW001Rib · crackedDURING THE INSTALLATION OF SHOULDER HARNESS KITS, THE HEADLINER WAS REMOVED. CORROSION ON CARRY THRU SPAR FORE AND AFT TOP SPAR CAPS AND SKIN WAS NOTICED. CORROSION WAS ALSO PRESENT AT LEFT AND RIGHT ROOT RIBS. LEFT ROOT RIB HAD SMALL CRACK. NO FURTHER ACTSDR 2001UALA00656Rib · crackedNR 6 SLAT ACTUATOR ATTACHMENT INBOARD AND OUTBOARD RIBS ARE CRACKED. REPAIRED ATTACHMENT RIBS PER SM-0R 70-57-56-01-AR5.SDR IXXA0100057SRib · misdrilledDURING ROUTINE C-CHECK INSPECTION, MISDRILLED HOLES WERE DETECTED IN THE RIGHT WING LEADING EDGE RIB AT WING STATION 763, ACCESS PANEL 517B. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW REPAIR DOUBLER IN ACCORDANCE WITHSDR UPS01835921Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01835865Rib · crackedINSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 678.75, XFS 666.25, XFS 603.75. REPAIRED RIBS.SDR UPS01835861Rib · crackedINSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 603.75, XFS 616.25, XFS 622.5. REPAIRED RIBS.SDR UPS01835856Rib · crackedINSPECTION TYPE:C1,3 RT WING L/E. UPPER RIB IS CRACKED AT XILD .7095. REPAIRED RIBSDR UPS01835854Rib · crackedINSPECTION TYPE:C1,3 RT WING L/E. UPPER AND LOWER RIBS ARE CRACKED AT XFS 885. REMOVED, FABRICATED, AND REPLACED RIBS.SDR UPS01835818Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING OB. L/E. UPPER RIB IS CRACKED AT XFS 841.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR CALA0100437Rib · chafedRIGHT WING LEADING EDGE RIB INBOARD OF ANTI ICE DUCT IS CHAFED. REMOVED AND REPLACED RIB PER SRM 57-30-2, 51-30-2, AND 51-30-5.SDR UPS01835891Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 791.25. REPAIRED RIBSDR UPS01835867Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 810. REPAIRED RIB.SDR UPS01835866Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XOLD 067. REPAIRED RIBSDR UPS01835852Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 816.25. REPAIRED RIB.SDR UPS01835851Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 741.25. REPAIRED RIB.SDR UPS01835850Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB.SDR UPS01835849Rib · crackedINSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB
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