JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 AWXA200400280Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 4 CRACKS WERE FOUND ON NR 2 SLAT LOWER SKIN BELOW INBOARD AUXILIARY TRACK WBL 294.40. MAINTENANCE CUT OUT DAMAGE ON NR 2 SLAT LOWER SKIN WBL 294.40; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-3SDR AWXA200400267Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK THE NR 1 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED OUTBOARD OF THE INBOARD AUXILIARY TRACK. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 SLAT WEDGE LOWER SURFACE; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS ISDR AWXA200400253Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 6 CRACKS WERE FOUND ON NR 1 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 445. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 1 SLAT LOWER SKIN WBL 445; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206 PSDR AWXA200400248Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 3 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 232.40. MAINTENANCE CUT OUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 232.40; FABRICATED A FILLER AND SPLICE PLATE PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 5SDR CALA0400142Skin · crackedINSPECTION FOUND 0.2 INCH CRACKS AT THREE FASTENERS IN NR 3 SLAT LOWER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.SDR SWAA040520Skin · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER SKIN. REPAIRED NR 2 L/E SLAT PER RA.SDR 04FDEA00434Hinge · corrodedLEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED.SDR 04FDEA00433Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00432Hinge · corrodedLEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED.SDR 04FDEA00419Rib · crackedLT WING CRACK ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-0SDR 04FDEA00420Skin · crackedLT WING NR 2 SLAT CRACK AT 02 PLACES; 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLASDR 04FDEA00427Skin · crackedLEFT WING - NR 2 SLAT WITH CRACK AT 02 PLACES: 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING SDR ASAA0480077Splice Plate · bentOKC - DURING HV1 CHECK, FOUND RIGHT WING 0 TO 1 SLAT SPLICE PLATE UPPER END IS BENT. REPLACED SPLICE PLATE PER SRM 51-10-4 AND 57-50-13. (M)SDR IXXA0400061SPlate · elongatedDURING A ROUTINE C-CHECK INSPECTION FOUND LT OB SLOT VANE UPPER SURFACE ELONGATEED HOLES STA X0200 67.000 (ON REPAIR DOUBLER). REPAIR WAS ACCOMPLISHED. FASTENERS AND THE EXISTING REPAIR DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1 AND 51-3-0 PG 1. DAMAGED SKISDR UPS04241969Web · crackedINSPECTION TYPE: C, NR 1 KRUEGER FLAP ACTUATOR TRUNNION CAP SUPPORT WEB I/B & O/B CRACKED. NR 1 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAP SUPPORT WEB IAW SRM 51-20-1. INSTALLED 31 K-FLAP ACTUATOR TRUNNION SUPPORT CAP WEB PER BOEING DRSDR UPS04241980Web · crackedINSPECTION TYPE: C, CRACKS ON NR 5 K-FLAP ACTUATOR I/B & O/B TRUNNION CAPS SUPPORT WEBS AT UPPER & LWR CORNERS. NR 5 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAPS SUPPORT WEBS IAW SRM 51-20-1 & DRG 65-16269. INSTALLED TRUNNION CAPS SUPPOSDR CALA0400103Panel · crackedINSPECTION FOUND TWO 1.5 INCH CRACKS IN RT WING FIXED UPPER LEADING EDGE PANEL AT NR 4 SLAT ACTUATOR, SLAT STA 65.92. THE LEADING EDGE PANEL WAS REPAIRED IAW ECRA 5721-01116.SDR UIEA200400011Stiffener · crackedDURING D-CHECK AT SIN, FOUND NR 16 KRUEGER FLAP INBOARD STIFFENER CRACKED. TRIMMED OUT CRACKED SEGMENT OF STRINGER FLANGE TO REMOVE DAMAGE. NDT INSPECT STRINGER TO INSURE CRACK AND DEFECT FREE CONDITION. INSTALLED ALUMINUM REPAIR ANGLE AND ALUMINUM FILLER TSDR 2004F00173Doubler · crackedAT C-CHECK, FOUND RIGHT WING NR 8 SLAT ACTUATOR ATTACH OUTER OUTBOARD FRAME LAYER IS CRACKED WING LEADING EDGE CAVITY. FABRICATE, PRIMED AND INSTALL NEW DUOBLER REPAIR AT RIGHT WING NR 8 SLAT ACTUATOR. (M)SDR DHL2004806572Skin · corrodedITEM REF. NR. 0738: LT WING CENTER L/E OB. VANE SLOT CORRODED AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-8, DWG U80-R08. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OSDR CALA0400070Skin · delaminatedINSPECTION FOUND O/B CORNER OF NR 2 SLAT SKIN DELAMINATED. REPAIRED IAW SRM 51-70-10.SDR 04FDEA00252Skin · crackedFOUND LT WING LEADING EDGE SLAT NR 9 TRACK LOCATION WITH ACCESS CUTOUT FWD MOST CRACKED (OUTBOARD MOST REFUELING PANEL). LT WING - LEADING EDGE SLAT NR 9 TRACK LOCATION CUT-OUT FWD CRACK AREA REPAIR CARRIED-OUT AS PER SRM 51-33-01 VOL. II AND SRM 51-35-01 VOLSDR SWAA040309Skin · crackedDURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED OUTBOARD END. REPAIRED SKIN PER SRM.SDR SWAA040308Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN ON TRAILING EDGE INBOARD AFT CORNER DELAMINATED. REPAIRED L/E SLAT PER EA.SDR SWAA040289Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR DL757040107Wedge · dentedNR 1 SLAT TRAILING EDGE WEDGE DENTED 50 INCHES FROM I/B END. REPAIRED PER SRM 51-70-10.SDR QXEA200400078Spar · wornPDX- STEP WORN INTO LOWER FLANGE OF LEFT WING FORWARD SPAR AT INBOARD END OF LEADING EDGE 511AL STA YW58.5. REPAIRED IAW RD8-57-811 AND RD8-57-2054.SDR SWAA040262Slat · crackedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SLAT CRACKED AT INBOARD END. REPAIRED SLAT CRACK PER RA.SDR ASAA0580020Skin · gougedOKC - HV-CHECK, LEFT INBOARD FLAP LOWER SURFACE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER. (M)SDR CALA0400055Skin · crackedINSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 57-43-01.SDR SWAA040231Wedge · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR AWXA200400150Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-13 CHECK FOUND THE NR 6 SLAT WEDGE DELAMINATED AT THE INBOARD END, WS 254 RT. MAINTENANCE REMOVED DAMAGED NR 6 SLAT SKIN AT WS 254; FABRICATED A REPAIR DOUBLER; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10 FIG 31, PG 88 F, G, SDR SWAA040201Arm · brokenNR 4 KRUEGER FLAP ACTUATOR ARM BROKEN. REMOVED AND REPLACED KRUEGER FLAP ACTUATOR ARM PER MM.SDR DHL2004806556Attach Fitting · crackedLEFT WING STUB WING INTERNAL PART FITTING CRACKED 4.000 AT STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM SDR DHL2004806550Door · crackedLEFT INBOARD SLOT UPPER DOOR WITH 0.750 CRACK IN IT. REMOVED AND REPLACED LEFT INBOARD SLOT UPPER DOOR IAW MM 27-80-1 PG 201-204. REFER TO NR 2228 FOR OPS CHECK.SDR AWXA200400143Skin · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON LT WING NR 3 SLAT SKIN AT CUTOUT FOR ACTUATOR WS 152. MAINTENANCE BLENDED OUT CRACKED SKIN AT CUTOUT LT WING NR 3 SLAT WS 152; PERFORMED HFEC INSPECTION OF BLEND OUT TO VERIFY NO CRACKS EXISSDR MEX2004026Skin · damagedDURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND THE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT.SDR SWAA040165Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE UPPER INBOARD SURFACE DELAMINATED. REPAIRED SLAT WEDGE PER EA.SDR DL764040042Flap · bird strikeLEFT OUTBOARD FLAP BIRD STRIKE CAUSING DELAMINATION. PER SRM WILL REQUIRE MAJOR REPAIR. REMOVED DAMAGE AND LAYERED UP REPAIR PER SRM 57-53-01 AND 51-70. OK TO INSTALL REPAIR QC1446. INSTALLED REPAIR PER SRM 51-70-1. OK TO REFINISH REPAIR QC1446. RESTOREDSDR CALA0400027Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 4 SLAT SKIN LOWER SURFACE O/B OF ACTUATOR ATTACH. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 57-43-01.SDR DL75K040036Wedge · dentedFOUND ON PSV - 3 DENT ON NUMBER 2 SLAT WEDGE 48 INCHES FROM INBOARD EDGE. REPAIRED PER SRM 57-43-02D AND OPERATION 1000.SDR SWAA040136Wedge · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SA-M 604.SDR 2004UALA00047Wedge · dentedT/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE.SDR DL757040017Skin · wornNR 9 SLAT WORN ON LOWER SURFACE. REPAIRED PER SRM 51-70-10 PERMANENT REPAIR.SDR 04FDEA00069Slat Track · crackedLEFT WING LEADING EDGE - NR 16 SLAT TRACK INTERNAL STRUCTURE CRACKED AT INBOARD TRACK BRACKET. LT WING LEADING EDGE NR 16 SLAT TRACK INTERNAL STRUCTURE I/B RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND EA 1-5750-74279, WINGS - LEFT HAND SLAT - FABRISDR 04FDEA00075Hinge Bracket · crackedLEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. LT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.SDR 04FDEA00076Hinge Bracket · crackedRT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. RT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 V2.SDR 04FDEA00077Hinge Bracket · crackedLEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND 01 EA BRACKET CRACKED AT OUTBOARD SIDE APPROX 12 INCHES FROM FLAP LOWER SURFACE, 24 INCHES FROM FWD EDGE OF HINGE. LT INBD FLAP OTBD HINGE (FLAP SIDE) OTBD SIDE LOWER AREA 01 BRACKET EDGE CRACK TRIMMED OUT FSDR 04FDEA00078Slat Track · crackedRIGHT WING - NR 16 SLAT TRACK LEADING EDGE INBOARD BRACKET CRACKED. RT WING NR 16 SLAT TRACK LEADING EDGE INBD BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL IISDR DHL2004806531Skin · crackedRIGHT INNER WING OUTBOARD EXTENDED L/E SLOT SKIN CRACKED 4.000 AT STA XILD 42.000. REMOVED CRACKED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6AL 0.071) IAW SRM 57-3-3 PG 11. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE IAW SRM
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