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 UPS02438958Rib · corrodedINSPECTION TYPE: C LT WING L/E RIB AT ILES 802.5 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR C/OUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUSDR UPS02438965Rib · corrodedINSPECTION TYPE: C, LT WING L/E RIB AT ILES 765.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.018 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT ASDR UPS02438964Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT ILES 1523.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.032 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT SDR UPS02438963Rib · corrodedINSPECTION TYPE:C, RT WING L/E RIB AT OLES 1421.35 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.031 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT ASDR UPS02438962Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.050 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT SDR UPS02438961Rib · corrodedINSPECTION TYPE: C RT WING L/E RIB AT ILES 1014.95 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT ASDR UPS02438960Rib · corrodedINSPECTION TYPE: C, LT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUTOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 1 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS SDR UPS02438959Rib · corrodedINSPECTION TYPE: C, LT WING LEADING EDGE RIB AT ILES 842.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.024 INCH X 0.5 INCH X 0.5 INCH, EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERIM CORROSION REPAIRSDR SWIA200210996Frame · crackedRIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED AT UPPER AND LOWER TERMINATION. REPAIRED RIGHT INBOARD LEADING EDGE INBOARD PER SRM 51-30-01, 51-10-02.SDR ABXA020157Rib · crackedNR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR SWIA200211019Rib · crackedRIGHT AND LEFT INBOARD LEADING EDGE RIBS EACH HAVE A CRACK. DOUBLER ADDED TO MENTIONED AREA IAW SRM 120 51-10-02.SDR QXEA0201369Rib · chafedCKB - RIGHT HAND LEADING EDGE INBOARD RIB HAS A HOLE CHAFED THROUGH EDGE. REPAIRED IAW HORIZON AIR EA 6-57-36 AND WVAC EO DH8S-57-0448.SDR QXEA0201370Rib · crackedCKB - LEFT HAND CENTER LEADING EDGE INBOARD RIB IS CRACKED IN TWO PLACES AND OUTBOARD RIB HAS ONE CRACK. REPAIRED IAW HORIZON AIR EA 6-57-28 AND WVAC EO DH8S-57-0428.SDR ABXA020038Rib · cracked4 EACH LEADING EDGE NOSE RIBS BETWEEN TRACKS 10 AND 11, HAD CRACK INDICATIONS AT AFT EDGES. REPAIRED NOSE RIBS AT STATIONS XRS 466-473-479-491 IAW REA D957-44307-MR.SDR ABXA020037Rib · crackedCRACK INDICATION ON AFT END OF LEADING EDGE NOSE RIB, INBOARD OF NR 10 SLAT TRACK. REPAIRED NOSE RIB IAW REA D957-44307-MR.SDR CALA0200327Rib · deformedINSPECTION FOUND THE R/H WING LEADING EDGE RIB DEFORMED INBOARD OF #4 SLAT TRACK(4TH RIB I/B). THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR AUS20020579Rib · corroded(AUS) RH WING CORRODED IN AREA OF LOWER AFT INBOARD CORNER. CORROSION AFFECTED LOWER WING SKIN, REAR SPAR AND THE UPPER SURFACE OF THEHORIZONTAL LEG OF THE CENTRE WING MAIN RIB.SDR COOSDR020163Rib · corrodedRIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95, AT LEFT WING, BUTTOCK LINE 70.5.SDR COOSDR020162Rib · corrodedRIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95 AT LEFT WING, BUTTOCK LINE 70.5.SDR 2002F00728Rib · crackedAT C-CHECK, FOUND RIGHT WING TIP RIB CRACKED AT WBL 62.5. (M)SDR DHL2002802520Former · crackedRIGHT WING O/B LEADING EDGE FORMER WITH .25 INCH CRACK AT STA XFS 672.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND SRM 51-1-2SDR DHL2002802519Former · crackedLEFT WING O/B LEADING EDGE FORMER WITH .5 INCH CRACK AT STA XFS 635.000. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 SDR DHL2002802514Former · crackedLEFT WING CTR L/E FORMER WITH CRACK AT STA XFS 335.000. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 5702-0 PG 9-10. INSTALLED DOUBLER PER SRM 51-1-21 PG 1.SDR AUS20021025Rib · corroded(AUS) RH WING UPPER SKIN SUPPORT RIB CORRODED UNDER P' CLAMP LOCATED AT OUTBOARD END OF NO6 LEADING EDGE FLAP - ZONE 64 STN WS 330.5. FOUND DURING CPCP INSPECTION.SDR DHL2002802508Former · crackedITEM: N/R 1913 LH WING OUTBD L/E- FORMER AT STA. XFS803.750 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10, FABRICATED DOUBLER WITH 2024T3AL .050 IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED AND PRIMED , IAW SRM 51-1-8B INSTALLED DOUBLERSDR DHL2002802501Former · crackedITEM: REF: N/R 1747 RH WING L/E FORMER CRACKED .250 UPPER PART XFS622.500CORR: REMOVED FASTNERS IAW SRM 51-1-20D PG.1 . STOP DRILLED CRACK IAW SRM 57-2-0 PG/ 9-10. FABRICATED REINFORCING ANGLE( 2024T3.050) IAW SRM 57-2-0 PG. 9-10 , CLEANED , TREATED AND PRIMEDSDR MWEA020367Fitting · crackedCENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 RIGHT. -- REMOVED AND INSTALLED FITTING.SDR QXEA0201365Rib · crackedCKB - RIGHT HAND CENTER LEADING EDGE HAS CRACKS ON THE END RIBS. ONE ON THE OUTBOARD RIB AND TWO ON THE INBOARD RIB. REPAIRED IAW HORIZON AIR EA 6-57-11 AND EO DH8S-57-0394.SDR QXEA0201364Rib · crackedCKB - LEFT HAND CENTER LEADING EDGE HAS CRACKS ON THE END RIBS. ONE ON THE OUTBOARD RIB AND TWO ON THE INBOARD RIB. REPAIRED IAW DHC8S-57-0394 AND HORIZON AIR EA 6-57-11.SDR DHL2002802507Former · crackedITEM: N/R 1915 LH WING OUTBD. L/E - FORMER AT STA.XFS841.000 WITH .500 CRACK IN IT.CORR.: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10 . FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10 , CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B. INSTALLED DOSDR DHL2002802505Former · crackedITEM: REF.: N/R 1916 LH WING OUTBD L/E - FORMER @ STA. XFS791.000 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10 , FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B , INSTALLED DOSDR DHL2002802506Former · crackedITEM:N/R 1914 LH WING OUTBD. L/E- FORMER AT STA. XFS825.000 WITH .500 CRACK IN IT.CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10, FABRICATED DOUBLER WITH 2024T3AL.050 IAW SRM 57-2-0 PG. 9-10, CLEANED , TREATED ,AND PRIMED IAW SRM 51-1-8B , INSTALLED DOUBLESDR UPS02438706Rib · corrodedINSPECTION TYPE:C RT WING- NR 18 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 8 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02.SDR UPS02438705Rib · corrodedINSPECTION TYPE:C RT WING- NR 25 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT BOLT HOLE FOUND SURFACE CORROSION. FROM NR 1 - NR 8 BOLT HOLE. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02.SDR UPS02438704Rib · corrodedINSPECTION TYPE:C RT WING- NR 20 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5, NR 8 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.SDR UPS02438703Rib · corrodedINSPECTION TYPE:C RT WING- NR 25 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 6 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.SDR UPS02438701Rib · corrodedINSPECTION TYPE:C RT WING- NR 22 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5 & 6 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434" WITH NR 4, 5, 6 OVERSIZED ECCENTRICALLY. RT WING- NR 22 L/E FLAP I/BSDR UPS02438700Rib · corrodedINSPECTION TYPE:C RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.434" - 0.500". RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACEDSDR UPS02438699Rib · corrodedINSPECTION TYPE:C RT WING- NR 23 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434". RT WING - NR 23 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB REPLACSDR UPS02438698Rib · corrodedINSPECTION TYPE:C RHW- NR 24 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT BOLT HOLES NR 1 & 8 - 0.434", NR 2 & 3 - 0.530", NR 7 - 0.465", NR 4 - 0.404", NR 5 - 0.437" , NR 6 - 0.404". RT WINSDR UPS02438697Rib · corrodedINSPECTION TYPE:C RHW - NR 24 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 2, 3, 5 - 8 BOLT HOLE FOUND SURFACE CORROSION. CORROSION BLEND OUT FINAL SIZE NR 2 & 3 - 0.388", NR 7 & 8 - 0.498". RT WING - NR 24 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB REPLACESDR MALA020327Rib · crackedDURING 4K-CHECK IN CWA, LT LEADING EDGE 511BL HAS CRACKED RIBS. MAINTENANCE FABRICATED REPAIR ANGLES FROM LOT 415071 AND COMPLETED REPAIRS, IAW SRM 57-10-30, TO RIBS AS REQUIRED.SDR UPS02438696Rib · corrodedINSPECTION TYPE:C RHW- NR 22 L/E FLAP O/B ROTARY ACTUATOR MOUNTING RIB SURFACE CORRODED. CORROSION BLEND OUT AT SURFACE AT MOUNT BOLT HOLES NR 1 & 2 - 0.025" AT BOLT HOLES BORE NR 1 TO 6 - FINAL DIA 0.312" NR 7 - 0.371", NR 8 - 0. 312" RT WING NR 22 L/E FLAPSDR QXEA0200825Rib · corrodedPDX - RT WING RIB AT YW369.0, OUTBOARD SIDE HAS TWO SMALL AREAS OF CORROSION. REPAIRED IAW HORIZON AIR EA 2-57-164.SDR UPS02238318Rib · crackedINSPECTION TYPE:C, 3 SUPPORT RIBS CRACKED ON T/E PANEL BELOW NR 8 SPOILERS. RIBS REPLACED IAW SRM 51-30-2 & DRG 65-21656.SDR AUS20020451Rib · damaged(AUS) WING RIB LOCATED THIRD OUTBOARD FROM THE WING ROOT CONTAMINATED WITH MOISTURE. FOUND DURING INSPECTION IAW AD/CA25/7-1.SDR 2002UALA00749Rib · crackedLT WING TRAILING EDGE WBL 445.95 RIB LOWER TEE CHORD 65B08150-99 HAS A CRACK IN THE VERTICAL FLANGE BETWEEN 2 FASTENERS. DAMAGE CAN BE VIEWED FROM OUTBOARD END OF INBOARD FLAPWELL BELOW 65B07818 MIDFLAP DEFLECTOR RAMP. MAJOR REPAIR WAS ACCOMPLISHED ON THE LESDR DHL2002726513Rib · crackedDURING C-CHECK, RT WING FIXED L/E RIB HAS A CRACK AT WS 572. CUT OUT DAMAGED AREA IAW B-727 SRM 51-40-3. FABRICATED AND INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND 51-40-3.SDR MWEA020237Clip · inadequateREMOVED ATTACH FITTING AT BULKHEAD XRS 69, BETWEEN STRINGER 21 THROUGH 22 RIGHT WING TO FACILITATE OTHER MAINTENANCE. -- NEW CLIP NEEDED DUE TO BUILD UP OF REPAIR ON STRINGER. FABRICATED AND INSTALLED CLIP.SDR CA020430003Rib · failed(CAN) RT WING STA 172.00 - DURING INSTALATION OF AUXILIARY WING TANKS, AN INSPECTION ACCESS HOLE WAS CUT IN LOWER RING SKIN AT STA. 169.00 SURVEILLANCE INSPECTON OF THE WING RIB AT STA 172.00 REVEALED AN EXTENSIVE COMPRESSION FAILURE ALONG THE ENTIRE LENGTH O
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