JASC 5754
Service difficulty reports · 17,348
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 DL767954159Te Wedge · delaminationRT WING NR 9 AND NR 11 SLAT TRAILING EDGE WEDGES HAVE AREAS OF DELAMINATION. ACCOMPLISHED REPAIRS PER DL ERA 272145-14AD.SDR CAL950997Skin · crackedHOU - INSPECTION FOUND CRACKS EXTENDING FROM RIVET HOLES OF NR 2 SLAT LOWER SKIN. THE CRACKS RAN FROM RIVET TO RIVET. ONE CRACK TOTALED 6 INCHES IN LENGTH AND THE OTHER TOTALED 5 INCHES IN LENGTH. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-01159 AND BOEINGSDR DL72S953985Rib · crackedUPON INSPECTION, FOUND A CRACK IN RIB 17. REPAIRED SRM 57-50-3, FOR NR 6 L/E SLAT PANEL.SDR DL72S953984Rib · crackedUPON INSPECTION, A CRACK WAS FOUND RIB 16. REPAIRED RIB PER MM 57-54-0 FIG 4, FOR NR 6 L/E SLAT PANEL.SDR DL72S953979Angle · crackedFOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 6 SLAT. REPAIRED PER M/M 57-54-0 FIG 816.SDR DL72S953978Angle · crackedFOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 7 SLAT. FASTENERS LOOSE OUTBD SLAT TRACK FAIRING NR 7 SLAT. REPAIRED PER M/M 57-54-0 2. REPLACED FASTENER.SDR 9515639601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO CRACKS IN THE LEFT WING NR 5 SLAT INBOARD IDLER TRACK ATTACH FITTING. REPLACED FITTING PER SRM 51-30-2.SDR DL72E953977Rib · crackedAT HMV, NR 4 SLAT RIB NR 18 CRACKED. REPAIRED PER MM 57-54-00.SDR UPS204774Flap · corrodedWHILE ON GROUND, MAINTENANCE REPLACED NR 3 K-FLAP, DUE TO CONDITION AND CORROSION. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.SDR DL72E960315Rib · crackedDURING SHOP INSPECTION, RIBS NR 2 AND NR 3 WERE FOUND TO BE CRACKED. REPAIRS WERE MADE AS PER M/M 57-54-0. ALSO, THE LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0, FOR NR 7 L/E SLAT.SDR UPS204800Attach Lug · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE HAS CORROSION AROUND LWR FASTENER HOLE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY. ARM ADDENDUM 727-5750-5542, 51-30-2, MM 27-81-01, 27-81-00.SDR UPS204799Attach Lug · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE IS CORRODED AT BOTH FASTENER HOLES. REMOVED AND REPLACED K-FLAP ASSY PER MM 27-81-01, 27-81-00, E.O. B727-5750-5542.SDR UPS204798Attach Lug · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 K-FLAP HAS PITTING CORROSION ON INBOARD ATTACH LUG OF BULLNOSE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY PER SRM 27-81-01, 27-81-00.SDR UPS204794Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP ACT. ATTACH FITTING ON ACFT SIDE CRACKED AT INBD UPPER ANGLE. REMOVED AND REPLACED UPPER LT ANGLE ON NR 2 K-FLAP SUPPORT PER SRM 57-40-00 AND 51-30-2.SDR DL72S953933Rib · crackedRIB CRACKED-NR 2 SLAT RIB MARKED NR 11 CRACKED AT LOWER ATTACH ANGLE. CORRECTION-FABRICATED REPAIR PER M/M 57-54-0, PG 805.SDR DL72S953927Cove Angle · crackedDURING F-1 LTR CHECK, FOUND NR 8 SLAT COVE ANGLE CRACKED BELOW ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0.SDR DL72S954042Rib · crackedATL - HMV, NR 6 SLAT I/B RIB AT INBOARD SLAT TRACK CRACKED IN LWR RADIUS. REMOVED FASTENERS FROM REPAIR AREA, FABRICATED REPAIR PER 57-54-0 FIG 805.SDR DL72E953976Angle · crackedNR 1 L/E FLAP ACTUATOR ATTACH ANGLE CRACKED I/B SIDE. WORKED AT HMV, REPAIRED ANGLE PER M/M 57-20-21.SDR 95FDEA01506Te Wedge · tornNR 7 SLAT T/E WEDGE IS TORN ABOVE I/B GUIDEHOOK. REPAIRED NR 7 SLAT T/E WEDGE IAW EA NR 7-5710-25887.SDR DL72S953956Skin · gougedDURING SHOP INSPECTION, NR 1 L/E SLAT WAS FOUND WITH LOWER SKIN GOUGED AT ACTUATOR ATTACH RIBS. REPAIRED PER SRM 57-50-3.SDR DL72E953915Angle · crackedDURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0.SDR CAL950928Skin · crackedHOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF SIX RIVETS ON NR 1 SLAT LOWER SKIN JUST OUTBOARD OF ACTUATOR ATTACH FITTING. TOTAL LENGTH OF CRACKS WAS 5.5 INCHES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C30133 AND ECRA 5750SDR CAL950927Skin · crackedHOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF TWO RIVETS ON NR 6 SLAT LOWER SKIN BETWEEN TAIL DUCT AND ACTUATOR. TOTAL LENGTH OF CRACKS WAS 1.125 INCHES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5750-01159. (X)SDR CAL950926Skin · crackedHOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF THREE RIVETS ON NR 6 SLAT LOWER SKIN AT INBOARD AUXILIARY TRACK. TOTAL LENGTH OF CRACKS WAS 2.5 INCHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-01159. (X)SDR 95UAL900170Support Rod Assy · failedSUPPORT ROD ASSY WAS FOUND FAILED AFTER FLIGHT. THERE WAS RESULTANT DAMAGE TO THE NR 20 LEADING EDGE VARIABLE CAMBER FLAP. SUPPORT, ROD ASSY AND VARIABLE CAMBER FLAP ASSY WERE REPLACED. FAILURE OF THE SUPPORT ROD WAS INITIATED BY FRETTING DAMAGE WITH A INSUSDR DL72S953923Skin · wornUPON HMV, FOUND SKIN WORN ON SECTION OF SKIN UNDER LIFT FENCE NR 4 SLAT. REPAIRED PER MM 57-54-0 PG 817.SDR DL72E953973Rib · crackedNR 5 SLAT-RIB NR 20 CRACKED UNDER LEADING EDGE AT NUTPLATE. WORKED AT HMV. REPAIRED PER M/M 57-54-00.SDR DL72E953972Heat Shield · crackedNR 6 SLAT-INTERIOR HEAT SHIELD CRACKED BETWEEN RIBS 11 AND 12. WORKED AT HMV. REPAIRED PER M/M 57-54-00, PG 804A.SDR DL72E953969Rib · crackedNR 4 SLAT-RIB NR 2 CRACKED. WORKED AT HMV. REPAIRED PER M/M 57-40-00, FIG 805.SDR DL72E953906Angle · crackedDURING A-1 LETTER CHECK, FOUND 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72E953905Angle · crackedDURING A-1 LETTER CHECK, FOUND .25 INCH CRACK NR 7 L/E SLAT COVE SKIN ATTACH ANGLE AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72S960061Fairing · crackedTHE O/B TRACK FAIRING WAS CRACKED. REPAIRED AS PER MM 57-54-0 FOR NR 3 L/E SLAT.SDR DL72S960036Cove Panel · crackedDURING A SHOP INSPECTION, A CRACK WAS FOUND ON A COVE PANEL LOCATED AT THE I/B UP STOP ATTACH POINT. A REPAIR WAS INSTALLED PER THE M/M 57-54-0, FOR NR 3 L/E SLAT.SDR DL72S960035Rib · crackedDURING A SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 RIB AT THE I/B TRACK ATTACH. A REPAIR WAS INSTALLED PER THE M/M 57-54-0 PG 807, FOR NR 3 L/E SLAT.SDR DL72L953893Bracket · crackedDURING D-1 LETTER CHECK, FOUND NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED AT UPPER AND LWR CORNERS, I/B SIDE. REPAIRED PER M/M 57-20-21 PAR 12.SDR 95UAL900163Fillet · missingON ARRIVAL AT NRT, FOUND LEFT SLAT NR 1 DAMAGED AND FILLET MISSING. REPLACED FILLET. INSPECTED AREA AND REPAIRED MINOR DAMAGE TO SLAT. RELEASED COAT 3-8065 TO PERFORM A ONE TIME FLEET INSPECTION OF SLAT FILLET ATTACHMENTS.SDR 95ZZZX6151Slat · disbondedTHE NR 5 AND NR 8 SLAT WEDGES DISBONDED. THE DAMAGE WAS SUSPECTED TO BE CAUSED BY MOISTURE IN THE SLAT CORE AND SUBSEQUENT CORE CORROSION AND WHEN SLAT IS IN STOW POSITION, IT PUSHES TOO HARD ON LEADING EDGE FIXED PANEL AND GENERATES EXTRA BENDING FORCE TO TRSDR DL72S953856Flap · crackedDURING INSPECTION, FOUND NR 3 KRUEGER FLAP WITH TIME LIMITED REPAIR AT O/B GATE HINGE CUTOUT. REPAIRED PER MM 57-53-0.SDR UPS204592Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 48.25. REPAIRED RIB IAW 727 SRM 57-50-3. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER.SDR UPS204590Flap · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP. REPLACED NR 5 K-FLAP PER MM 27-81-01.SDR UPS204589Bolt · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SLAT IS CRACKED AT O/B GUIDE HOOK, UPPER ATTACH BOLT. REPAIRED NR 5 SLAT PER SRM 57-50-03.SDR UPS204588Skin · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND AND REPLACED NR 2 K-FLAP DUE TO CONDITION AND CORROSION. THE NR 2 K-FLAP WAS FOUND TO BE CORRODED OUT OF LIMITS. REPLACED NR 2 K-FLAP PER MM 27-81-01.SDR DLL10953994Rib · crackedNR 6 L/E SLAT RIB CRACKED. REPAIRED PER SRM 57-51-00 FIG 812, FOUND AT LETTER CHECK.SDR DL72S960030Ribs · crackedDURING INITIAL SHOP INSPECTION, FOUND RIBS NR 16 AND 17 CRACKED AT UPPER FORWARD CORNER. REPAIRED CRACKED AS PER MM 57-54-0.SDR DL72S953859Angle · crackedDURING F-1 LETTER CHECK, FOUND NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S953858Angle · crackedDURING F-1 LETTER CHECK, FOUND NR 7 L/E SLAT COVE SKIN ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR UPS204559Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB IN NR 5 SLAT 8 INCHES FROM I/B END (3RD RIB IN FROM I/B END MARKED). REPLACED RIB IAW SRM 51-30-2.SDR UPS204555Fitting · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UPPER FWD SIDE OF NR 2 K-FLAP OUTBOARD MOUNTING LUG WHILE WORKING NR 360298 (WINGS 203). REMOVED AND REPLACED NR 2 K-FLAP OUTBOARD MOUNTING FITTING PER SRM 51-30-2 AND MM 27-81-01.SDR UPS204554Web · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 7.25. REMOVED AND REPLACED NR 4 SLAT RIB AT SLAT STA 7.25 IAW SRM 51-10-1, 51-30-2.SDR UPS204553Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SLAT, RIB JUST I/B OF TAI T-DUCT, CRACKED AT FWD CORNER. REMOVED AND REPLACED NR 3 SLAT RIB JUST I/B OF TAI T-DUCT IAW SRM 51-10-1, 51-30-2.
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