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 DL72S951612Angle · crackedNR 3 SLAT LWR CHORD ANGLE CRACKED .50 INCH BELOW TAI DUCT. FOUND DURING E-2 LTR CK TPA MM. REPAIRED PER MM 57-54-0 PG 807A.SDR 95ZZZM1Skin · delaminatedON 4-18-95, THE PILOT IN COMMAND OF A/C FOUND NR 6 LE SLAT DELAMINATED DURING PREFLIGHT AT CVG. MAINTENANCE CONTROL CONTACTED AN EMERGENCY MAINTENANCE CREW TO EVALUATE THE DAMAGE. PER BOEING SPECS, THE AIRCRAFT WAS FERRIED TO MCO FOR MAINTENANCE. THE NR 6 LSDR DL757951844Te Wedge · delaminatedDURING SHOP INSPECTION, RT WING NR 10 L/E SLAT WAS FOUND WITH DELAMINATION TO THE T/E WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR DL72W951602Angle · crackedNR 2 SLAT, ANGLE CRACKED UNDER I/B STOP PAD. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-54-0 PG 12.SDR DL757951726Wedge · wornLOWER AFT EDGE IS WORN ON NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 REF AD 90-23-06. FOUND AND REPAIRED DURING HMV.SDR DL72L951774Bracket · crackedFOUND ON CV2 CK, .5 INCH VISIBLE CRACK ON NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET IN LOWER RADIUS. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72L951730Rib · crackedFOUND ON CV2 CHECK, (1) .25 INCH VISIBLE CRACK ON NR 5 SLAT L/E RIB O/B OF ACTUATOR ROD. (2) 2.0625 INCH CRACKS ON NR 5 SLAT L/E RIB I/B OF ACTUATOR ROD. REPAIRED PER M/M 57-54-0 PAR 3.SDR DL72S951548Rib · crackedUPON SHOP INSPECTION, 4TH RIB FROM INBOARD FOUND CRACKED, RT WING NR 6 L/E SLAT. REPAIRED PER SRM 57-54-00.SDR DL72S951540Skin · crackedFOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E SLAT AFT SKIN ATTACH ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S951496Rib · crackedDURING SHOP, INSPECTION RT WING NR 5 L/E SLAT WAS FOUNED WITH RIB NR 12 CRACKED. REPAIRED PER MM 57-54-00.SDR DL72W951555Skin · crackedSKIN CRACKED, NR 4 SLAT HAS 6 CRACKS AT FENCE ATTACH POINTS. REPAIRED PER MM 57-54-0 PG 817. FOUND AT HMV.SDR DL72W951531Skin · crackedAT HMV, FOUND RT WING NR 5 L/E SLAT WITH CRACKS IN THE SKIN AT WING FENCE ATTACH HOLE. REPAIRED PER MM 57-54-0 PG 817.SDR DL72W951462Rib · crackedRIB CRACKED NR 2 L/E SLAT NR 3 RIB CRACKED (MARKED). STOP DRILLED CRACK AS PER SRM 57-50-3. FABRICATED DOUBLER AS PER SRM 57-50-3 FIG 9 SHEET 1 AND 2.SDR DL72W951461Rib · crackedRIB CRACKED NR 2 L/E SLAT NR 4 RIB CRACKED (MARKED). STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 57-50-3 FIG 9.SDR DL72S951695Frame · crackedAT HMV, FOUND NR 2 SLAT O/B END 2ND FRAME FROM END CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S951694Frame · crackedAT HMV, FOUND NR 3 L/E SLAT NR 7 FRAME CRACKED INSIDE L/E. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S951692Frame · crackedAT HMV, FOUND NR 3 L/E SLAT OB FRAME CRACKED. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S951561Rib · crackedDURING HMV, FOUND NR 1 SLAT I/B END 2ND FRAME CRACKED. REPLACED RIB PER MM 57-54-00.SDR DL72S951491Slat · crackedFOUND DURING A-2 LETTER CHECK, .5 INCH CRACK AT I/B STOP PAD NR 6 SLAT. REPAIRED PER MM 57-54-0.SDR DL72W951463Rib · crackedRIB CRACKED NR 2 L/E SLAT NR 5 RIB FROM INBD END CRACKED FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9. FOUND AT HMV.SDR DLM88951556Skin · damagedDURING HMV, FOUND 2 REPAIRS ON BOTTOM OF NR 2 SLAT INTERFERE WITH L/E OF WING. REPAIRED PER SRM 57-09 PG 35 REF.SDR DL76S951575Te Wedge · delaminationDURING LTR CHECK, THE NR 1 L/E SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROXIMATELY 5 INCHES IN DIAMETER AND IS LOCATED 75 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIRED PER DSDR DL72S951423Angle · crackedTHE NR 8 L/E SLAT LWR FWD SKIN ATTACH ANGLE CRACKED AT ANTI-ICE AIR DUCT CUTOUT. REPAIRED PER SRM 57-54-0. FOUND DURING D-2 LTR CK TPAMM 4/6/95.SDR UPS202932Te Skin · crackedDURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT T/E. INSTALLED REPAIR PER SRM 51-40-2, 51-30-2, MM 51-20-21, 51-20-71.SDR UPS202927Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT RIB AT SS 63, FWD UPPER CORNER. REPAIRED PER SRM 57-50-3.SDR UPS202926Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT AT RIB SS 182, AFT CORNER WHERE LWR CHORD ATTACHES TO RIB. REPAIRED PER SRM 57-50-3.SDR UPS202898K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 6 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE UNDER THE UPPER LUG. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.SDR UPS202897K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 5 K-FLAP OUTBOARD HINGE LUG OUTBOARD FACE UNDER BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.SDR UPS202896K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 4 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE BOTH MOUNT BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.SDR UPS202895K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 3 K-FLAP OUTBOARD HINGE LUG UPPER AND LOWER BOLTS ON OUTBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01.SDR UPS202894K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 2 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE AT BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW OHM 57-51-11 AND MM 27-81-01.SDR UPS202893K-Flap · corrodedDURING 'D' CHECK, MAINTENANCE FOUND PITTING CORROSION ON THE NR 1 K-FLAP AT CENTER ATTACH LUG ON UPPER INBOARD, UPPER OUTBOARD AND LOWER INBOARD MOUNT BOLT AREAS. MAINTENANCE REPLACE THE NR 1 K-FLAP IAW MM 27-81-01.SDR UPS202875Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT RADIUS OF THE RIB AT SS 140 FORWARD END AT RIB, UPPER FLANGE RADIUS AREA. MAINTENANCE REMOVED THE RIB, FABRICATED NEW RIB AND FINAL INSTALLATION IAW SRM 51-10-2 AND 51-20-151.SDR UPS202873Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT MOST INBOARD RIB (SEAL RETAINER RIB AT SLAT STATION 120). MAINTENANCE REMOVED THE CRACKED RIB, INSTALLED NEW RIB AND FINAL INSTALLATION IAW SRM 51-30-2 AND 51-30-5.SDR UPS202871Skin · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE SKIN OF THE NR 6 SLAT BETWEEN STATION 166.5 AND STATION 161.5 AT FORWARD FASTENERS. MAINTENANCE REMOVED THE FASTENERS, STOP DRILLED, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-20-04, 51-10-2 AND MM 51SDR UPS202870Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT STATION 97.5 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER AND FINAL INSTALLATION IAW SRM 51-30-02 AND 51-50-3.SDR UPS202869Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 105 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-02 AND 57-50-3.SDR UPS202868Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 112 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-2 AND 57-50-3.SDR UPS202856Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 4 SLAT END RIB AT SLAT STATION ZERO. MAINTENANCE REMOVED AND INSTALLED A NEW RIB ASSEMBLY PER SRM 51-10-1.SDR UPS202855Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SLAT RIB AT SS 225 LOWER AFT CORNER. MAINTENANCE REPAIRED THE RIB USING DOUBLER PER 727 SRM 57-50-3.SDR UPS202854Skin · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 188.5 AND SS 195.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.SDR UPS202853Skin · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TPI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 176 AND SS 182. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.SDR UPS202852Skin · crackedDURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT ATTACHING FASTENER BETWEEN SS 147 AND SS 154.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B.SDR DL72S951413Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 5 O/B RIB FOR ACTUATOR ROD END CRACKED. REPAIRED PER MM 57-54-0 PG 3, FOR RT WING NR 5 L/E SLAT.SDR UPS202812Flap · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP JUST O/B OF THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR 727-57-1340.SDR DL72S951407Rib · crackedRIB NR 18 CRACKED NEXT TO NUTPLATE. INSTALLED DOUBLER PER MM 57-54-0 FIGURE 805. DURING SHOP INSPECTION OF RT WING NR 5 L/E SLAT.SDR UPS202796Skin · damagedDURING 'C' CHECK, MAINTENANCE FOUND NR 7 SLAT TRAILING EDGE SKIN AT I/B SLAT HOOK IS DAMAGED FROM LOOSE FASTENERS. INSTALLED REPAIR PER UPS ENGINEERING FILE NR B272-57-1339.SDR DL72W951379Rib · crackedDURING SHOP INSP, NR 18 RIB WAS FOUND CRACKED. REPAIRED PER SRM 57-50-3 FIG 9, FOR LEFT WING NR 4 L/E SLAT.SDR DL72W951378Rib · crackedDURING SHOP INSP, RIBS 12 WAS FOUND TO BE CRACKED. REPAIRED PER SRM 57-54-0 FIG 804, FOR LT WING NR 4 SLAT.SDR DL72W951377Ribs · crackedDURING SHOP INSP, RIBS 2, 8, 9, 21 WERE FOUND TO BE CRACKED. REPAIRED RIBS PER SRM 57-54-0 FIG 814. DURING SHOP INSPECTION OF NR 4 L/E SLAT.
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