JASC 5744
Service difficulty reports · 2,731
Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 = '5744' 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 = '5744' 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 AALA980722Post · corrodedTUL - RIGHT INBOARD FLAP TRACK NR 2 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5. REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL 22. TREATED, PRIMED, AND PAINTED SRM 51-21-01 VOL II. TST: 91,033.07 HOURS. CYCLES: SDR AALA980721Post · corrodedTUL - RIGHT INBOARD FLAP TRACK NR 4 ATTACH POST FORWARD BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 105. REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED, AND PAINTED/SRM 51-21-01 VOL II. TST: 91,033.07 HOURS. SDR AALA980720Post · corrodedTUL - RIGHT INBOARD FLAP TRACK NR 3 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5. REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED/PAINTED, SRM 51-21-01 VOL II. TST: 91,033.07 HOURS. CYCLES: 18,1SDR CALA9800558Attach Fitting · corrodedINSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING AT BOTTOM OF WING CORRODED AT INBOARD FACE. THE FITTING WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 20-50-01.SDR CALA9800505Bracket · crackedINSPECTION FOUND A 2 CRACK IN BOTH INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACHES INSIDE LEADING EDGE. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. THE FLAP ACTUATOR WAS REMOVED AND REINSTALLED IAW MM 27-8SDR UPS98226019Fitting · frettedINSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 4 T/E FLAP TRACK FWD ATTACH FITTING FRETTED ON INBOARD SIDE OF TRACK ATTACH POINT. REMOVED FITTING AND ROUTED TO MACHINE SHOP. FITTING REWORKED PER ER NO 98-2216.SDR UPS98826057Fitting · crackedINSPECTION TYPE-C, LT WING T/E, THE LWR REAR SPAR TO AUX SPAR TIE FITTING AT THE STA 98 FLAP HINGE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5642205.SDR UPS98225857Fitting · corrodedINSPECTION TYPE-SI, NR 1 FLAP TRACK FWD FITTING IS CORRODED AROUND MOUNT HOLE. REPLACED FITTING PER SRM 51-10-1, NEW FITTING SETUP AND MACHINED PER BOEING DRAWING 65-17357.SDR UPS98225767Fitting · corrodedINSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 5 FLAP TRACK ON WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALLED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01.SDR UPS98225766Fitting · corrodedINSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 4 FLAP TRACK, WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALLED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01.SDR DHL9880609CFitting · crackedAT C-CHECK, LT FLAP HINGE SUPPORT FITTING AT STA 97 NR 2 HOLE HAS CRACK. REAMED HOLE AND HFEC NO FURTHER CRACK FOUND PER DC-8 MM 51-3-4.SDR 99ZZZX1206Flap Track · wornFOUND FLAP TRACKS WORN BY ROLLERS. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED, BOTH FLAPS. THIS IS SECOND AIRCRAFT IN 2 MONTHS.SDR 99ZZZX1205Flap Track · wornFOUND FLAP TRACKS WORN BY ROLLERS. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED, BOTH FLAPS. THIS IS SECOND AIRCRAFT IN 2 MONTHS.SDR DHL9880607CFitting · crackedAT C-CHECK, RT WING I/B AILERON L/E DAMPER BRACKET CRACKED. REMOVED AND INSTALLED NEW FITTING PER SRM 51-1-21.SDR DL72K980079Flap Track Shim · migratedDURING INSPECTION PER DAL SI 4-58662-12AD (AD 90-07-05), THE LAMINATED SHIM OF THE RT INBD FLAP TRACK WAS FOUND MIGRATED BEYOND THE .25 ALLOWED LIMIT. THE MIGRATED SHIM WAS REINSTALLED PER AD REQUIREMENTS AND ACCOMPLISHED PER ER/A 363668-14AD.SDR MZZA98025Fittings · corrodedKUL - LEFT OUTBOARD FOREFLAP, OUTBOARD STABILIZING TRACK FITTING INBOARD LUG AND MIDDLE STABILIZING TRACK FITTING INBOARD LUB CORRODED BEYOND LIMIT IAW SRM 57-40-00. FITTINGS REPLACED IAW SRM 51-30-2, TRACKS REFITTED AND FOREFLAP REFITTED. FUNCTIONAL CHECK SSDR 98ZZZM289Fittings · corrodedKUL - LEFT OUTBOARD FOREFLAP, OUTBOARD STABILIZING TRACK FITTING INBOARD LUG AND MIDDLE STABILIZING TRACK FITTING INBOARD LUB CORRODED BEYOND LIMIT IAW SRM 57-40-00. FITTINGS REPLACED IAW SRM 51-30-2, TRACKS REFITTED AND FOREFLAP REFITTED. FUNCTIONAL CHECK SSDR AU971485Bracket · cracked(AUS) LH AILERON CENTRE ATTACHMENT BRACKET CRACKED ON UPPER AND LOWER WEBS AT AILERON INPUT BELLCRANK PIVOT BOLT ATTACHMENT AREA.SDR 97FDEA00630Hinge · corrodedCORROSION ON NR 1 K-FLAP CENTER HINGE LUG ON AIRCRAFT SIDE UNDER BOTH I/B AND O/B LUG SCREWS. REMOVED AND REPLACED NR 1 K-FLAP CENTER HINGE FITTING.SDR UPS97824290Fitting · crackedDURING C CHECK INSPECTION, FOUND RT WING OTBD FLAP STA XF 408 (INBD) FLAP HINGE SUPPORT FITTING CRACKED. CRACK IS OUT OF SRM LIMITS. REMOVED SUPPORT FITTING AT STA 408, LOCATED, DRILLED AND INSTALLED NEW SUPPORT FITTING IAW DC8 SRM 57-1-0, 51-3-0.SDR AALA971441Fitting · corrodedTUL - DURING C-CHECK, FOUND CORROSION INSIDE FOUR BOLT HOLES ON NR 3 SUPPORT FITTING FOR INBOARD TRACK ON INBOARD END OF RIGHT INBOARD FLAP. REMOVED CORROSION AND INSTALLED BUSHINGS IN BOLT HOLES PER SRM AARD 57-20-00-10, REPAIR NR 10. (M)SDR UPS97223995Fitting · crackedINSPECTION TYPE:C, INBOARD SPOILER SUPPORT ATTACH FITTING FOR NR 6 FLAP TRACK CRACKED. FITTING REPLACED IAW SRM 51-30-2.SDR AALA971238Casting · corrodedTUL - INBOARD AILERON QUADRANT CASTING CORRODED AROUND LOWER BUSHING. BOTH UPPER AND LOWER. REMOVED AND REPLACED QUADRANT. CORROSION BEYOND MANUAL LIMITS. TST: 56,772 HOURS. CYCLES: 34,468. (X)SDR 97ZZZM1023Fitting · corrodedNR 7 FLAP TRACK REAR SPAR ATTACH FITTING HAS CORROSION IN OUTBOARD HOLE. REMOVED AND REPLACED FITTING PER SRM 51-40-02. (M)SDR ABXA9701112Fitting · corrodedDURING C-CHECK, FOUND THE LEFT FLAP INBOARD FWD HINGE FITTING CORRODED. REPLACED THE FWD HINGE FITTING IAW DC9 MM 57-40-01.SDR IXXA9700116Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING FLAP SUPPORT FITTING WAS FOUND CRACKED AT STATION 339.723. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SERVICE BULLETIN 27-249SDR 97ZZZM872Bracket · crackedRIGHT AILERON CENTER HINGE BRACKET WAS FOUND CRACKED AT HOLE FOR MOUNTING TO WING. REPLACED HINGE BRACKET.SDR DHL9780144CFitting · crackedAT C-CHECK, FLAP HINGE SUPPORT FITTING LEFT STA 97 I/B BOLT HOLE CRACK INDICATION. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING PER SRM 51-1-21.SDR MWEA97344Fitting · crackedDURING INSPECT, OTBD FLAP HINGE SUPPORT FITTING CRACKED FWD OF WING SPAR WEB. MAINT REPAIRED IAW DAC DRW 4911393 AND SRM 51-30-5.SDR DL757970796Fitting · wornTHE SIX BOLTS THAT ATTACH THE NR 3 FLAP INBD FLAP TRACK FWD SUPPORT FITTING TO THE MLG BEAM WERE FOUND TO BE LOOSE CAUSING THE BOLTS TO WEAR INTO THE BEAM AND THE FITTING. ALL SIX HOLES IN BOTH THE BEAM AND THE FITTING WERE FOUND TO BE EGG SHAPED. THE ORIG FSDR DHL9780146CFitting · crackedAT C-CHECK, FLAP HINGE SUPPORT FITTING RT STA 97 NR 2 BOLT HOLE O/B CRACK INDICATION. OVER SIZED BOLT HOLE .03125 PER JOB CARD 8-51-12-001.SDR DHL9780145CFitting · crackedAT C-CHECK, FLAP HINGE SUPPORT FITTING LEFT STA 219 O/B BOLT HOLE CRACK INDICATION. REMOVED FITTING, REAMED HOLES AND INSTALLED NEW FITTING PER SRM 51-3-0.SDR W8PA970229Fitting · crackedINBOARD FOREFLAP CENTER TRACK ATTACH FITTING CRACKED. REPLACED ATTACHED FITTING. (M)SDR ABXA9700439Fitting · corrodedDURING C-CHECK, FOUND CENTER FLAP HINGE ATTACH FORWARD FITTING CORRODED. REPLACED FITTING IAW DC9 MM.SDR HAL9738Casting · corrodedRIGHT WING INBD FLAP CASTING STA XRS 69 HAS LEVEL 2 CORROSION. REMOVED AND REPLACED CASTING ASSY PN 3914981-504. SRM 51-30-5 AND SRM 51-10-4. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)SDR HAL9739Casting · corrodedLEVEL 2 CORROSION ON LEFT WING INBOARD FLAP CASTING XRS 69. REMOVED AND REPLACED CASTING PER SRM 51-30-0, AND SRM 51-30-5. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)SDR HAL9745Fitting · corrodedLEFT WING FLAP NR 4 LEADING EDGE CAP INBOARD AND OUTBOARD ATTACH FITTINGS HAVE CORROSION. LEVEL 2 LEFT WING XRS 232. REMOVED BRACKETS. REMOVED CORROSION AND TREATED. BRACKET MATERIAL LOSS WITHIN LIMITS PER SRM 57-01, FIG 1. INSTALLED NEW CAP DOUBLERS PER SSDR 97ZZZX2687Fitting · corrodedLEFT WING FLAP NR 4 LEADING EDGE CAP INBOARD AND OUTBOARD ATTACH FITTINGS HAVE CORROSION. LEVEL 2 LEFT WING XRS 232. REMOVED BRACKETS. REMOVED CORROSION AND TREATED. BRACKET MATERIAL LOSS WITHIN LIMITS PER SRM 57-01, FIG 1. INSTALLED NEW CAP DOUBLERS PER SSDR 9703491211Casting · crackedDURING TRANSITION CHECK, FOUND CRACK IN THE LEFT INBOARD FLAP INBOARD TRACK ATTACH CASTING. REPAIRED PER EA 12-121503.SDR ABXA9700870Fitting · crackedDURING C-CHECK, THE AILERON CENTER HINGE ATTACH FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 MM 27-10-1.SDR UPS97221942Casting · corrodedINSPECTION TYPE-D, NR 7 FLAP TRACK FWD ATTACH CASTING ON WING HAS CORROSION. REPAIR CARRIED OUT IAW SRS EO 97-02-016, REF UPS ENGINEERING FILE NR 727-57-1775.SDR UPS97221890Casting · corrodedINSPECTION TYPE-D, EVIDENCE OF CORROSION ON NR 5 FLAP TRACK FWD ATTACH CASTING ON WING. CORROSION REMOVED IAW SRM 51-10-6. HFEC PER NDT PT6 51-00-00 F13 AND MPI PER BS6072 CARRIED OUT, NO FURTHER CORROSION. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS, REF UPSDR UPS97221938Fitting · corrodedINSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LWR SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED PER SRM 51-10-6. HFEC C/O PER NDT PT6 51-00-00 F13, MPI CO PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 2 WING MOUNTED FLAP C/OSDR UPS97221937Fitting · corrodedINSPECTION TYPE-D, NR 1 AND NR 2 FLAP TRACK ATTACH FITTINGS ON LOWER SURFACE OF WING, CORROSION AT ATTACH POINT. CORROSION REMOVED IAW SRM 51-10-6, HFEC C/O PER NDTPT6 51-00-00 F13, MPI C/O PER C/O PER BS 6072, NO CORROSION FOUND. REPAIR TO NR 1 WING MOUNTESDR UPS97821823Casting · crackedINSPECTION TYPE: C. RT WING T/E, OUTBOARD OF MLG TRUNNION AND FWD OF AUXILIARY SPAR, THE STA 98 FLAP HINGE LWR ATTACH CASTING CRACKED. REMOVED CRACKED CASTING, FABRICATED REPLACMENT CASTING INSTALLED CASTING PER SRM 51-1-20D, AND SRM 51-3-1.SDR ABXA9700180Fitting · gougedDURING C-CHECK, FOUND LEFT WING INBOARD SPOILER FITTING GOUGED. REPAIRED THE LEFT WING INBOARD FITTING IAW ABX REA D957-17399-MR.SDR RAAA96B1016Fitting · corrodedDURING SCHEDULED S5 INSPECTION PER CARD S5-21110, FOUND LT OUTBD AILERON HINGE ASSY SUPPORT FITTING CORRODED AT WS 727. REPLACED FITTING PER SRM 51-10.SDR RAAA96B1015Fitting · corrodedDURING SCHEDULED S5 INSPECTION PER CARD S5-21110, FOUND LT OUTBD AILERON HINGE ASSY SUPPORT FITTING CORRODED AT WS 693.5. REPLACED FITTING PER SRM 51-10.SDR UPS96221490Hinge · corrodedINSPECTION TYPE: SI. L/W I/B AILERON CENTER (WING SIDE) HINGE FITTING IS CORRODED. REPLACED L/W I/B AILERON CENTER (WING SIDE) HINGE FITTING IAW MM 27-10-01.SDR UPS96821460Fitting · crackedINSPECTION TYPE: C. LT WING STA XRS98 FLAP CARRIAGE FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.
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