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 ASAA2015051312192Rib · crackedLT WING RIB AT WBL 135, LOWER RIB CHORD BETWEEN STR 2 AND 3 IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO LT WING LWR RIB CHORD, WBL 135 IAW EA 400, 57EA 15246.SDR AALA20150511003Rib · crackedLEFT WING NR 4 SLAT INBD LE RIB, MACHINED AREA FOR RIBLET REPAIR SHOWS CRACK INDICATION AT THE AFT SIDE. R & R RIB IAW SRM 51-30-05.SDR SWAA2015060340337Rib · crackedRIGHT WING RIB CRACKED AT WBL 114, STRINGER 2. REPAIRED RIB IAW EA.SDR IPXA2015051489068Rib · crackedINSPECTION TYPE:3C, RT WING L/E INTERNAL RIB CRACKED IN RADIUS, STA 855. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW DWG ARB2922 AND SRM 51-31-01.SDR CA150703001Rib · corroded(CAN) DURING THE 8 YEAR INSPECTION, WE FOUND RIB NR 16 ON BOTH WING CORRODED. DAMAGE WAS OUT OF THE SRM REPAIR AUTHORITY, REPAIRED.SDR FDEA201504291320Rib · crackedRIGHT WING TIP FENCE FAIRING AROUND FASTENER HOLES CRACKED AT WY501. REPLACED IAW SRM 51-40-21.SDR VGCA20150428002Rib · crackedLEFT WING DRY BAY RIB 2 CRACKED.SDR ABXA20150427058Rib · corrodedNUMBER 8 FLAP SUPPORT 3 & 4 TENSION BOLT HOLES HAVE DEFECT INDICATIONS WITH ROTARY SCAN, POSSIBLE CORROSION. NR 8 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN 113T1345-44, PART NAME, NR 8 RIB, CORRODED LEVEL 2, FROM NR 8 FLAP SUPPORT. ACFT WAS GSDR AALA20150507007Rib · crackedRIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED AT XIS 134.546. REPAIRED RIB IAW EA 250763 DATED 5 7 2015.SDR DALA2017040602932Panel · crackedINSPECTION REPORTED A CRACK BETWEEN WSTA 285 AND WSTA 313 ON LT WING FUEL TANK AUXILIARY STRUCTURE DRY BAY BARRIER PANEL. REF ERA 532885-14 REV A. REF LOG PAGES 1919279 AND 2961772.SDR AALA20150423004Rib · crackedRIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW MCM CARD 5798-06 & EA 250469.SDR ASOA20150413094Rib · crackedDURING C-CHECK, RIB 21 ON RT WING INSIDE PANEL 651CB IS CRACKED. MAINTENANCE REPAIRED RT WING RIB 21 IAW EC 5720-01201. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20150407014Rib · crackedRIGHT WING RIB 5 HAS A 1 INCH CRACK LOCATED 1ST LARGE CUT OUT FROM AFT EDGE, 7:OO POSITION, OTBD SIDE. COMPLIED WITH REPLACEMENT OF RT WING RIB 5 IAW EO EM-57MR-595.SDR FDEA201504051155Rib · corrodedLEFT MLG FWD LUG HAS CORROSION ON BOTH FACES & BORE COMPLIED WITH EA 6-5710-T0316549, REPAIR OF RIB 5 FWD LUG LT.SDR FDEA201504021142Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0316574 REV NO POS P1.SDR U2RA201504010001Rib · crackedRIGHT WING RIB SUPPORT AT MID SPAR IN NR 3 MAIN TANK WING STA 1140, CRACKED. CRACK LENGTH APPROXIMATELY 4". R & R RIB SUPPORT NR 112U9200.SDR AALA20150331005Former · crackedRIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WC 57-98-06.SDR DALA2015040102546Rib · crackedCRACKED RT WING L/E RIB STA XRS 271. RIB WAS REPLACED IAW SRM 51-30-2; 51-30-5 AND DWG 9937588-4, REV G.SDR R61A201503300224Rib · corrodedDURING HEAVY CHECK, FIXED T/E RIB 10 LT WING REQUIRES ALTERNATE MEANS OF REPAIR. MX FIXED T/E RIB 10 LT WING REQUIRES ALTERNATE MEANS OF REPAIR, IAW SB 170-57-0047, ALSO ETD 2015-170-028796, REV H. CONTINUATION CARD C1-C3 FOR DETAILS OF WORK. ACFT REMAINS USDR DALA2015033102507Rib · crackedCRACKED RIB AND CLIP ON LT WING L/E STA XRS 430. NO CRACKS WERE FOUND ON THE CLIP. REPLACED RIB, TREATED AND PAINTED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38.SDR USAA2015033100015Rib · corrodedCORROSION FOUND ON FASTENER NUT ON RIB 5 AREA IN THE RT WING UNDER PANEL 674AB. REMOVED CORROSION & REPAIRED IAW EA 106551.SDR USAA2015033100014Rib · corrodedFOUND CORROSION AROUND FASTENERS AT FALSE SPAR BOX BETWEEN RIB 4 & 5 INSIDE LT WING ACCESS PANEL 574AB. REMOVED CORROSION & REPAIRED IAW EA 106552.SDR USAA2015033100013Rib · corrodedCORROSION AROUND FASTENERS ON RT WING MLG RIB 5 LOWER FLANGE. REMOVED CORROSION & REPAIRED IAW EA 209622.SDR USAA2015033100012Rib · corrodedCORROSION AROUND FASTENERS ON LT WING MLG RIB 5 LOWER FLANGE. REMOVED CORROSION & REPAIRED IAW EA 209635.SDR FDEA201503281110Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION ON FWD FACE & IN BORE. COMPLIED WITH EA 6-5710-T0316490 REV NO POS P1. WINGS, BASIC WING STRUCTURE CORROSION REPAIR OF RIB 5 FWD LUG. MAJOR REPAIR.SDR DALA2015032902471Rib · corrodedCPCP CORROSION ON BORE INNER AND OUTER SURFACE OF RIBS FROM STA XOS=530,580 AND 610 AT LT SLAT PANEL NR 5. CORROSION ON INNER AND OUTER SURFACE OF RIBS FROM XOS = 530 AND 610 WERE REMOVED IAW SRM 51-10-3, PAR 26 WAS ACCOMPLISHED ORIGINAL THICKNESS ON RIB AT SSDR SWAA2015033037958Rib · crackedRIGHT WING DEFLECTION CONTROL RIB CRACKED. R & R RIB IAW SRM.SDR DALA2015032702449Rib · corrodedCORROSION ON BORES OF RIB FROM STA XOS= 380 AT LT SLAT PANEL NR 4. DAMAGE ON RIB STA XOS=380 WAS REPAIRED IAW ETI-88-15-098, REV ORIGINAL AND ER/A 533324-14 REV ORIGINAL.SDR DALA2015032702448Rib · corrodedCORROSION ON BORES OF RIB FROM STA XOS= 286 AT LT SLAT PANEL NR 2. DAMAGE ON BORES OF RIB STA XOS=286 WAS REPAIRED IAW ETI-88-15-099, REV ORIGINAL AND ER/A 533325-14, REV
ORIGINAL.SDR FDEA201503261091Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION ON FWD & AFT FACE & IN THE BORE COMPLIED WITH EA 6-5710-T031347. REPAIR OF RIB 5 FWD LUG RT.SDR R61A201503250226Rib · crackedDURING HEAVY CHECK, LT WING, RIB 10 CRACKED CHORD WISE JOINT, SPLICE GOING FWD, CRACK LIKE INDICATIONS IN FASTENER HOLE JUST OTBD OF SKIN SPLICES IAW ETD 2013-170-000186. MAINTENANCE REPAIRED HOLE IAW ETD 2015-170-028597. FINAL HOLE SIZE .503 INSTALLED BUSHISDR R61A201503250225Rib · crackedDURING HEAVY CHECK, RT WING AFT RIB 10 HOLE IN INBD LOWER FLANGE JUST FWD OF SPAR 2 IS CRACKED CRACKS RADIATING INBD AND OTBD FROM HOLE. MAINTENANCE REPAIRED HOLE IAW ETD 2015-170-028597 FINAL HOLE REAMED TO 504 INSTALLED BUSHING. C1-C2 FOR WORK DETAILS. ACSDR DALA2015032602387Rib · corrodedCORROSION ON BORE/INNER AND OUTER SURFACE OF RIBS FROM STA XIS=83,136 AND 186 AT SLAT PANEL LT NR 1. CORROSION ON OUTER SURFACE OF RIBS WERE REMOVED IAW SRM 51-10-3. RIBS WERE MESURED AS FOLLOWS ORIGINAL THICKNESS IS 0.320" REMAINING THICKNESS IS 0.277", THESDR DALA2015032502361Rib · corrodedCORROSION ON BORED, INNER AND OUTER SURFACE ON RIBS FROM STA XOS=286, 332 AND 380 AT LT SLAT PANEL. DAMAGES ON RIBS STA XOS= 286; 332, 380 WERE REPAIRED IAW ER/A 533332-14, REV ORIGINAL AND ETI 88-15-104, REV 1.SDR DALA2015032302311Rib · damagedDURING MAINTENANCE ACTIVITIES. DAMAGE BORES ON RIBS STA XOS 286, 332 AND 380 AT RT SLAT PANEL NR 3. DAMAGE ON RIB STA XOS=332 WAS REWORKED AND MEASURED WITH ID 0.938, 4 HOLES, THEREFORE LIMITS OF MAXIMUM REWOK HOLE DIAMETER IAW SRM 57-02, PAR 9 C (1). BUSHINGSDR DALA2015032302310Rib · corrodedINITIAL CORROSION FWD BORE ON RIB STA XOS 380 AT SLAT PANEL NR 4 RT WING. DAMAGE ON RIB STA XOS= 380 WAS REMOVED AND MEASURED, WITH ID 1.1265 ON FWD HOLE, THEREFORE OUT LIMIT OF MAXIMUM REWORK HOLE DIAMETER, THEREFORE WAS REPAIRED WITH AND ER/A 533326-14, REVSDR DALA2015032302309Rib · corrodedINITIAL CORROSION AFT BORE ON RIBS STA XOS 429 AT SLAT PANEL NR 4 RT WING. DAMAGE ON AFT BORE WAS REPAIRED IAW AND ER/A 533326-14 REV, ORIGINAL.SDR FDEA201503201034Rib · corrodedOPEN R MOD TYPE T MOD NR 6-5710-T0316275 REV NR PS P1 WINGS, BASIC WING STRUCTURE, TERMINATING ACTION OF RIB 5 FWD LUG RT COMPLY WITH EA 6-5710-T0316275 REV NR POS P1. COMPLIED WITH EA 6-5710-T0316275 P1 WINGS BASIC WING STRUCTURE & TERMINATING ACTION OF RSDR IXXA20150320049Cap · corrodedAIRCRAFT GNDED FOR HVY MX. UPPER CAP ON LE RIB AT LES 261 CORRODED 4 INCHES FROM FRONT SPAR ON INBD SIDE. REMOVED, REPAIRED & INSTALLED UPPER RIB CAP LES 261 IAW SRM 57-41-09 & 51-40-02.SDR ABXA20150318034Repair · crackedFOUND A CRACK ON RT WING LE STATION 651 ON A PREVIOUS REPAIR OF A STRUT RIB. R & R AIR LOAD RIB LOWER CHORD AT STATION 651 IAW SRM 51-40-02 & DWG 114T2212. SDR INFO, CRACKED, LENGTH 1.2", PN 114T2212-6, PART NAME CHORD, SN N/A, STRINGER & WC LOCATION WS 651.SDR AALA20150316005Former · crackedRIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED DOUBLER & HAT BUSHING IAW WC 57-98-06.SDR DALA2015031702197Rib · damagedSCRATCH AFT BORE ON LT RIB STA XOS 580 AT SLAT PANEL NR 5 RT WING. DUE TO EXCEED ALLOWABLE LIMITS IAW SRM 57-02, PAR 9, TABLE 1 RIB XOS:580 N/P 9937564-2 THE SLAT PANEL NR 5 RT WITH N/P 5937563-502, N/S DL-64 WAS REPLACED.SDR DALA2015031702193Rib · scratchedSCRATCH ON LEFT FWD BORE OF RIB XOS 198 AT SLAT PANEL NR 2 RT WING. DAMAGE WAS REWORKED AND MEASURED, WITH DIAMETER INBD 0.940, 1 HOLE, THEREFORE WITHIN LIMITS OF MAXIMUM REWORK HOLE DIAMETER IAW SRM 57-02, PAR 9 C, 1. BUSHING WAS FABRICATED IAW SRM 57-02, PASDR QXEA2015031600117Rib · crackedUPPER REPAIR ANGLE ON THE OTBD CLOSING RIB ON L/E PANEL 611AR CRACKED. REMOVED UPPER REPAIR ANGLE ON THE OTBD CLOSING RIG ON L/E PANEL 611AR REF SRM 51-42-05. INSTALLED NEW UPPER REPAIR ANGLE ON OTBD CLOSING RIB ON L/E PANEL 611AR REF SRM 57-40-00 REPAIR-07, SDR QXEA2015031600116Rib · crackedUPPER AND LOWER REPAIR ANGLES ON THE INBD CLOSING RIB ON L/E PANEL 611AR IS CRACKED. REMOVED UPPER AND LOWER REPAIR ANGLES ON THE INBD CLOSING RIB ON L/E PANEL 611AR REF SRM 51-42-05, REMOVED CRACKED ANGLES. INSTALLED NEW UPPER AND LOWER REPAIR ANGLES ON THE SDR WVER0309201551507Rib · damagedDAMAGE WAS FOUND DURING REMOVAL OF SEALANT DURING INCORPORATION OF SB 670BA-57-015 AT RH RIB WS 48.95, JUST FWD OF REAR SPAR.SDR ASOA20150308064Rib · mechanic errorDURING C-CHECK THERE WAS MAINTENANCE INDUCED DAMAGE FROM MISDRILLING OUT FASTENERS TO LT WING RIB 1A, AT WING STATION Y-1085.00 LT. MAINTENANCE R & R THE RIB IAW EC5710-01242. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150305007Rib · crackedACFT IS IN C-CHECK WHEN INSPECTION FOUND A CRACK ON THE LT WING AT RIB NR 5 IN AREA FWD OF PREVIOUS SB MOD. CRACK RUNS FROM LOWER FLANGE OTBD THRU THE HYLOCK HOLE AND CONTINUOUS VERTICALLY 6". R & R THE NR 5 RIB IAW EC5710-01239. ALL WORK ACCOMPLISHED AND SDR UIEA2015030500165Rib · corrodedLEFT WING LES INTERNAL RIB IS CORRODED AT FWD UPPER CORNER & LOWER EDGE. R & R LES INTERNAL RIB WS 456 IAW REA 47136REA08, WORK ACCOMPLISHED SRM 51-40-02.SDR UIEA2015030500166Rib · corrodedLEFT WING LES INTERNAL RIB IS CORRODED ABOVE WIRE STANDOFF LOCATED AT APPROX LESS 479. FOUND CORROSION BEYOND LIMITS, REPAIRED AIR LOAD RIB IAW SRM 51-70-11.
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