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 08FDEA01428Rib · corrodedTHE RIB 5 FWD BORE ON THE LT MLG IS CORRODED ON THE INSIDE, FOUND AFTER BUSHING WAS REMOVED. THE MAX DIAMETER OF 4.8405 HAS BEEN REACHED REMOVED LEVEL 1 CORROSION, AND REPAIRED LT MLG RIB 5 IAW FED EX EA 6-5710-118108. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNSDR 08FDEA01423Rib · damagedDURING MD10 ACF MODIFICATION ON WING LT SIDE OUTBOARD SLAT NR 3 FOUND RIB P/N ARB1666-501 WITH EA 7 HOLES OVALIZED. REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG ARB1666.SDR 08FDEA01391Rib · crackedRIGHT WING LEADING EDGE RIB FOUND CRACKED AT INBOARD OF SLAT TRACK NR 16. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. SLAT CABLES 83 AND 84 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 2008UALA02132Rib · crackedNR 1 MAIN FUEL TANK WBL 135 RIB WHERE L2 STRINGER PASSES THROUGH THE LWR CHORD ANGLE CUTOUT, CHORD IS CRACKED IN UPPER FWD RADIUS. MAJOR REPAIR ACCOMPLISHED: PERFORMED S/B REPAIR CONSISTING OF NEW "T" AND FILLER ASSY.SDR 2008UALA02131Rib · crackedNR 2 MAIN FUEL TANK, WBL 135 RIB WHERE L2 STRINGER PASSES THROUGH THE LWR CHORD ANGLE CUTOUT, CHORD IS CRACKED IN UPPER-FWD RADIUS. MAJOR REPAIR ACCOMPLISHED: PERFORMED S/B REPAIR CONSISTING OF NEW "T" AND FILLER ASSY.SDR 08FDEA01378Rib · damagedFOLDING SLAT NR 1 RT , FOUND MISDRILLED HOLE DURING EMBODIMENT OF SB 57-6067 REPAIR PERFORMED DURING EMBODIMENT OF SB 57-6067 BY INSTALLING OVERSIZED BLIND RIVET AND 4,00MM RIVETS IN OFFSET HOLES IAW RAS/BAE/1006919/2008 ISS A, APPROVED BY EA 6-5742-115256.SDR TRAX200800490Rib · crackedLEFT BATTERY RIB IS CRACKED. REMOVED TWO SUPPORT BRACKETS FOR F.O.M. C/W REO 601R-57-51-046 REPAIR TO LT BATTERY RIB ASSY WS 53.60. OK TO INSTALL SUPPORT BRACKETS. INSTALLED SUPPORT BRACKETS IAW SRM 51-41-04. C/W ASA REO 601R-57-51-046.SDR DLM88080544Rib · crackedDURING HMV A CRACK WAS FOUND ON RT WING LEADING EDGE RIB AT STA XRS=271. RIB WAS REPAIRED IAW SRM 57-06 BD FIG 801D.SDR DLM88080532Rib · crackedDURING HMV, A CRACK RIB WAS FOUND AT RIGHT WING FIXED LEADING EDGE AT STA XRS=164. RIB WAS REPLACED IAW SRM 51-30-5,51-30-2 AND DWG 9937517 REVE-J.SDR DLM88080492Rib · crackedDURING HMV A CRACKED RIB WAS FOUND AT LEFT WING FIXED LEADING EDGE STA XIS=136 LOWER SIDE. RIB WAS REPAIRED IAW ER/A 466349-14 REV ORIG.SDR 2008FA0000289Bulkhead · crackedDURING ROUTINE INSP, FOUND PART CRACKED. CHECKED (2) OTHER CARDINALS THAT HAPPENED TO BE IN OUR SHOP AND FOUND (1) OF THEM TO HAVE A SIMILAR CRACK. THIS SECTION OF THE BULKHEAD IS THE ATTACH STRUCTURE FOR THE LOWER ATTACH ANGLE FOR THE IB FLAP DRIVE BELLCRANSDR 2008FA0000288Bulkhead · crackedDURING ROUTINE INSPECTION, FOUND PART CRACKED. CHECKED (2) OTHER CARDINALS THAT HAPPENED TO BE IN OUR SHOP AND FOUND (1) OF THEM TO HAVE A SIMILAR CRACK. THIS SECTION OF THE BULKHEAD IS THE ATTACH STRUCTURE FOR THE LOWER ATTACH ANGLE FOR THE IB FLAP DRIVE BESDR 08FDEA01165Rib · crackedRT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED RIB IAW SRM 57-00-01 FIG 10 VOL I.SDR 08FDEA01146Rib · damagedDURING SB 28-6028 EMBODIMENT, 2 HOLES WERE MIS-DRILLED IN RIB 2 AFT WEB, BOTH WINGS. REPAIR PERFORMED BY INSTALLATION OF RIVETS TO FILL MIS-DRILLED HOLES, WITH REMAINING ACTIONS AS PER SB, ALL IAW EA6-5720-115257 AND RAS/BAE/1006544/2008 ISSUE A.SDR A6WA200840260Rib · corrodedLT INBOARD LEADING EDGE OUTBOARD SIDE UPPER RIB CORROSION. (M) CORROSION REMOVED IAW SRM 51-21-06. (K)SDR A6WA200840257Rib · corrodedLT SIDE OUTBOARD LEADING EDGE UPPER RIB INBOARD SIDE CORROSION. (M) LT SIDE OB LEADING EDGE UPPER RIB CORROSION REMOVED IAW SRM 51-21-06. (K)SDR A6WA200840262Rib · corrodedRIGHT WING INBOARD L/E OUTSIDE UPPER RIB CORRODED WS 148. CORROSION REMOVED IAW SRM 51-21-06. (M)SDR A6WA200840261Rib · corrodedFOUND CORROSION ON RIGHT OUT LE, WS 249 INBOARD SIDE UPPER RIB. (M) CORROSION REMOVED IAW SRM 51-21-06 AND TREATED IAW SRM (51-21-11) (51-25-06).SDR TRAX200800456Rib · crackedAAR - 1023 - LEFT BATT RIB CRACKED. REMOVED LEFT BATT RIB DOUBLER LOCATED HOLES IN NEW SERVICEABLE BATT RIB DOUBLER IAW CRJ 200 SRM 51-40-11. OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW 51-25-06. OK TO INSTALL. INSTALLED NEW SERVICEABLE BATT RIB DOUBSDR TRAX200800455Doubler · crackedAAR - 7006 - RIGHT BATT RIB CRACKED. UPON FURTHER EVALUATION, FOUND RIGHT BATT RIB PREVIOUS REPAIR DOUBLER TO BE CRACKED. REMOVED CRACKED REPAIR DOUBLER FROM RIGHT BATT RIB & DUPLICATED SERVICEABLE REPAIR DOUBLER FROM P/N S6144-4 .063 IAW REO 601R-57-51-046.SDR 08FDEA01055Rib · crackedRT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED FORMER IAW SRM 57-00-01 FIG 10 SHT 1 VOL I.SDR 08FDEA01054Rib · crackedRT WING L/E INT ZONE FOUND CRACK ON RIB AND MISSING GANG CHANNEL ON RIB. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.SDR 2008UALA01521Rib · crackedLEFT WING TANK LOWER RIB CRACKED WS 135.5 APPROX 12" FWD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED BY REMOVING DAMAGE AND VERIFYING DAMAGE REMOVAL WITH HFEC. REPAIRED RIB.SDR 2008UALA01520Rib · crackedRIGHT WING TANK RIB CRACKED AT WS 135.5 APPROX 12" FWD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED BY REMOVING DAMAGE AND VERIFYING DAMAGE REMOVAL WITH HFEC. REPAIRED RIB.SDR 08FDEA01024Rib · crackedLT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED OUTBD OF NR 12 SLAT TRACK. INSTALLED REPAIR ARB-4352-35, PO 612903.1 IAW SRM 57-20-00 FIG 1 VOL I & 53-33-01 VOL II. MINOR REPAIR.SDR 08FDEA01023Rib · crackedLT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED INBD OF THE NR 15 SLAT TRACK. REMOVED AND REPLACED RIB ARB-4352-35, PO 612712.1 IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR.SDR 08FDEA01022Rib · crackedLT WING L/E INTERNAL RIB UPPER AFT EDGE REPAIR DOUBLER IS CRACKED INBD OF THE NR 16 SLAT TRACK. REPAIRED RIB & INSTALLED CUP ARB 1292-39, PO 612641.1; IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR.SDR TAMF20080019SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER CHORD AT STA 441.60. CORRECTIVE ACTION: RIB WAS FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214240, DRAWING 114T2200 AND SRM 51-40-02 PG 1-7.SDR TAMF20080018SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER SHROUD AT STA 933.73 AND 938.73. (2) RIBS WERE FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214294 AND PO214297, DRAWINGS 117T2224 AND 114T2223 AND SRM 51-40-02/1-3 AND 7.SDR TAMF20080017SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER CHORD STA 779.44 AND 784.44. (2) RIBS WERE FABRICATED AND INSTALLED IAW P0214296 AND P0214326, AND DRAWINGS 114T2217 AND 114T2218 AND SRM 51-40-02 PG 1-7.SDR SWAA081372Rib · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135, STR 2. REPAIRED CHORD PER ACO.SDR 08FDEA00864Rib · crackedLEFT WING, LEADING EDGE RIB FOUND CRACKED AT XOS 795. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB2922. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA00862Rib · crackedLT WINGLET RIB CRACKED REPLACE, REPAIR RIB.SDR 08FDEA00694Rib · wornFOUND WEAR IN RT MLG RIB 5 LUGS, FORWARD RIB 5 REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALLING OVERSIZE BUSH IAW DRAWING R572-49221.SDR 08FDEA00676Rib · chafedFOUND CHAFING MARKS ON LT WING LEADING EDGE STRUCTURE, SLAT JACK NR 1 INNER RIB HOLE EDGE. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1006441/2008 ISS A, APPROVED BY EA 6-5741-114935.SDR UPS08851996Rib · crackedINSPECTION TYPE:C3 UPPER RIB CRACKED AT END IN LEFT WING O/B LEADING EDGE NEAR STA XFS 809. FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, 57-2-00, 57-3-0 FIG 19.SDR UPS08851794Rib · crackedINSPECTION TYPE:C3 INNER RIB CRACKED AT AFT END IN LT WING OB LE IB SECTION NEAR STA XFS6 03. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-2 1, 51-1-21D, 51-1-8, 57-2-00.SDR UPS08851785Rib · crackedINSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB LE IB SECTION NEAR STA XFS6 27, UPPER STOPPED DRILLED CRACK. FABBED AND INSTALLED REPAIR DOUBLER.SDR UPS08851769Rib · crackedINSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB L/E IB SECTION NEAR STA X FS 609, UPPER STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLERS ON L/W OB LEADING EDGE UPPER RIB AT XFS609 IAW SRM 57-3-3 FIG 6, SRM 57-2-0 FIG 2, 51-1-8SDR 2008FA0000179Rib · corrodedCOMPLIANCE WITH AD 2002-26-02 DETECT AND CORRECT CORROSION IN WING CENTER SECTION. FOUND 5 RIVETS CORRODED OFF THE LOWER CENTER RIB ON THE RT WING WALKWAY BOX.SDR 2008UALA01105Rib · crackedRT WING RIB AT WBL 135.5 IS CRACKED AT AFT LOWER RIB CLIP NR 13349-6000-0033. ACP'D PER EVA 080161. MAJOR REPAIR: REPAIR ACCOMPLISHED.SDR DHL2008805518Frame · crackedRT FLAP WELL UPPER FORMER CRACKED 1" STA XW 5.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL2024T3 0.063") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ASDR DHL2008805531Frame · crackedNR 4 STUB WING UPPER FORMER CRACKED 0.500" STA XFS 541.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8SDR 08FDEA00542Rib · crackedRIGHT WING, UPON REMOVAL OF NR 1 SLAT INBOARD CRUISE PERFORMANCE FILLET FOR NR 1 SLAT INBOARD LEADING EDGE METAL SEAL REPLACEMENT, FOUND OUTBOARD RIB NEAR ALIGNMENT AREA CRACKED. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS SDR S9BA20080010Rib · corrodedCPCP INSP, RT WING FWD RIB AT STA.85 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.
SDR S9BA20080009Rib · corrodedCPCP INSPECTION, RT WING FWD RIB AT STA 72.5 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.SDR 2008UALA00721Rib · crackedLEFT WING WBL 135.5 AFT RIB LOWER FITTING CRACKED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR.SDR G60A200800021Rib · crackedRT WING REFUEL/DEFUEL BAY OUTBD RIB LWR AFT END CRACKED 1.5 INCH.SDR 08FDEA00345Rib · crackedRIB NR 25 FOUND TO BE CRACKED. REPLACE DAMAGED RIB.SDR GLBA20061055Rib · crackedLT RIB NR 21 AT WS YA-6750 BETWEEN WING FRONT SPAR AND THE WING AUXILLARY SPAR, CRACKED FWD AND AFT OF STRINGER NR 1. CRACKS APPROX .375 INCH IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PIECE IAW SRM 57-20-07 REPAIR PIECE CUT FROM NEW RIB
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