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 DL76S962716Skin · delaminatedTHE NR 8 L/E SLAT T/E WEDGE WAS FOUND WITH UPPER SKIN DELAMINATION. THE DELAMINATED AREA WAS TRIMMED OUT AND REPAIRED PER SRM 57-43-02, FIG 201.SDR CKSA96356Slot Vane · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT VANE TRAILING EDGE DAMAGED. REMOVED AND REPLACED LEFT HAND OUTBOARD SLOT VANE TRAILING EDGE IAW DAC DRAWING NR 5769933, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82130.SDR CKSA96349Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND WING INBOARD SLOT DOOR IAW DMM 27-80-1 PAGE 201, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81808.SDR CKSA96345Plating · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: SKIN UNDER OUTBOARD SLOT PANEL DAMAGED APPROXIMATELY 1 HOLE. REMOVED AND REPLACED PLATING IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82012.SDR CKSA96343Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT LEADING EDGE DAMAGED. REPAIRED PER SRM 57-2-1 FIGURE 2H, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82125.SDR CKSA96332Door · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND OUTBOARD SLOT DOOR IAW DC-8 MM 27-41-2, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81805.SDR CKSA96330Door · missingDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR LEADING EDGE MISSING. REPAIR DONE ON RO#230452 INSTALLED IAW DC-8 SRM 51-1-20D AND 51-3-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81809.SDR MZZA96195Skin · corrodedTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING L/E NR 1 SLAT LOWER SKIN AROUND SCREW HEADS AT BS 421. THE CORRODED SKIN WAS CLEANED AND REPAIRED PER B727 SRM 57-50-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIRSDR DL72W962659Angle · crackedFOUND DURING A-2 LETTER CHECK, 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B UPSTOP PAD. REPAIRED PER M/M 57-54-0PAR 12.SDR CALA9700398Skin · rippledINSPECTION FOUND RIPPLING ONE FOOT IN DIAMETER IN RT WING NR 1 SLAT AT INBOARD END. THE RIPPLED AREA WAS CUT OUT, A SKIN INSERT, SPLICE STRAPS, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, FIGURE 43 AND 51-31-01.SDR DL72K962633Skin · crackedLOWER SKIN CRACKED AT O/B END. REPAIRED SKIN PER M/M 57-54-00 FIG 801.SDR CALA9700102Skin · dentedINSPECTION FOUND A 5 INCH DIAMETER BY 0.060 DEEP DENT IN OUTBOARD RT WING NR 3 SLAT. A SKIN AND DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 11.SDR MZZA96165Skin · corrodedTNN - DURNIG 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING NR 1 L/E FLAP SKIN INTERIOR SURFACE AT LES 306. THE CORRODED SKIN WAS CLEAN UP AND REPAIRED PER B727 SRM 57-50-3, FIG 2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NRSDR CALA9601779Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 8 SLAT RIB, JUST INBOARD OF ANTI-ICE DUCT. THE CRACK WAS ROUTED OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9.SDR CALA9601740Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 SLAT OUTBOARD TRACK INBOARD ATTACH RIB AND A .5 INCH CRACK IN INBOARD TRACK OUTBOARD ATTACH RIB OF NR 6 SLAT. THE CRACKS WERE STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9601739Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING NR 5 SLAT ACTUATOR OUTBOARD ATTACH RIB AND A .5 INCH CRACK IN INBOARD ATTACH RIB OF NR 5 SLAT ACTUATOR. THE CRACKS WERE STOP DRILLED, ANGLE REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR 96ZZZX6027Slat · crackedDURING PHASE 1 INSPECTION FOUND LT FLAP SLAT 552S141-1 CRACKED AT WELDS AT SEVERAL PLACES. NO SPARES AVAILABLE, HAD TO BE REMOVED FOR REPAIR BY MANUFACTURER DUE TO BEING MADE FROM MAGNESIUM ALLOY. SPECIAL ATTENTION NEEDS TO BE PAID TO THIS UNIT DURING PHASE SDR P5CA9600966Bracket · brokenLEFT WING LEADING EDGE FLAP NR 11 HAS BROKEN BRACKET ON CONNECTION ROD FROM BULLNOSE TO SLAT. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-10-01.SDR CALA9601743Skin · crackedINSPECTION FOUND .25 INCH CRACKS AROUND RIVET HEADS OF LT WING NR 1 SLAT SKIN NEAR ACTUATOR. REPAIRED IAW ECRA 5700-01159.SDR DL72W962521Angle · crackedFOUND THE NR 1 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED BELOW THE INBD STOP PAD. REPAIRED PER MM 57-50- 4.SDR DL72K962537Skin · crackedFOUND CRACK ON CORNER END OF NR 3 L/E FLAP. REPAIRED PER M/M 57-53-0, PG 804.SDR DL72S962498Angle · crackedFOUND A .50 INCH CRACK NR 6 L/E SLAT COVE SKIN ATTACH ANGLE AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR. 12.SDR 96FDEA01664Bonding Jumper · corrodedNR 398 036, CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT. *S/D* REPAIRED NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT IAW FEDEX EA 7-5750-31262.SDR CALA9601866Skin · dentedINSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 12.SDR 96FDEA01648Bullnose · corrodedNR 0407 029, CORROSION ON NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER AND LOWER ATTACH POINT. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER ATTACHMENT POINTS IAW FEDEX SRM 57-50-3 AND FEDEX SR 27-57-010.SDR CALA9601697Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-3.SDR CALA9601696Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR DHL9672019CRib · crackedAT C-CHECK, NR 6 SLAT I/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1.SDR DHL9672010CRib · crackedAT C-CHECK, NR 3 SLAT I/B RIB CRACKED. REMOVED AND REPLACED RIB PER SRM 51-10-1.SDR DHL9672001CRib · crackedAT C-CHECK, NR 6 SLAT O/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1 AND 57-30-7.SDR 96FDEA01626Hinge Lug · corrosionNR 0399 018, CORROSION NR 1 K-FLAP CENTER HINGE LUG AT LOWER BOLT. *S/D* REMOVED CORROSION ON NR 1 K-FLAP CENTER HINGE LUG. REPAIRED IAW FEDEX EA 7-5750-31276A. FUNCTIONAL TESTED NR 1 K-FLAP OK IAW FEDEX M/M 27-81-1.SDR 96FDEA01623Bonding Jumper · corrodedNR 0403 015, CORROSION ON NR 3 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* REPAIRED NR 3 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER ATTACH POINT PER FEDEX SRM 57-50-3 AND THE LOWER ATTACH POINT WAS FOUND TO BE WITHIN LIMITS PER FEDESDR 9622629618Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LEFT WING NR 1 SLAT OUTBOARD END FITTING. REPLACED FITTING PER SRM 51-30-2.SDR DHL9672003CFitting · crackedAT C-CHECK, LEFT WING L/E NR 4 SLAT ON I/B FLANGE CRACKED. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 57-50-3, 3 BY 3.SDR DHL9672012CAngle · crackedAT C-CHECK, NR 5 SLAT OUTBD END LOWER SKIN ANGLE TO OUTBD RIB CRACKED. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR PER SRM 51-40-4, REPAIR 1 BY 12 BY 3.5.SDR UPS96221515Skin · crackedINSPECTION TYPE: C. LT WING NR 4 SLAT SKIN TOP SIDE AT OTBD HOOK HAS SEVERAL CRACKS AROUND FASTENERS. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED PLATE PER SRM 57-50-3.SDR CALA9601670Skin · crackedINSPECTION FOUND A .125 INCH CRACK JUST INBOARD OF ACTUATOR, IN LOWER SKIN OF RT WING NR 5 SLAT PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159.SDR 96FDEA01647Bullnose · corrodedNR 0397 030. CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE I/B LINKAGE ATTACH POINT. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE. FUNCTIONAL TESTED. WORK DONE IAW FEDEX M/M 27-81-1.SDR 96FDEA01596Bonding Jumper · corrodedNR0318 - 002, CORROSION (C 57-562-01-02) NR 4 K-FLAP O/B RIB AT PREVIOUS BONDING JUMPER ATTACH POINT. *S/D* FOUND TO BE OUT OF LIMITS. REPAIRED NR 4 K-FLAP O/B RIB AT BONDING JUMPER ATTACH POINT IAW FEDEX SRM 57-50-3.SDR CALA9601873Skin · dentedINSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43.SDR UPS96221449Rib · crackedINSPECTION TYPE: SI. NR 1 SLAT FIRST RIB INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 SLAT FIRST RIB INBOARD OF TAIL DUCT PER SRM 57-30-3.SDR DL72S962508Rib · crackedRIB ON RT WING SLAT ACTUATOR WAS FOUND CRACKED. REPAIRED RIB PER M/M 57-54-00, FIG 809.SDR DL72S962507Rib · gougedRIGHT WING SLAT OUTBOARD TRACK BOLT HOLE DAMAGED. REPAIRED RIB PER M/M 57-54-00, FIG. 809.SDR DL72S962506Skin · crackedLOWER INBOARD END OF RIGHT WING SLAT WAS CRACKED. REPAIRED PER M/M 57-54-0, FIG. 801.SDR UPS96221450Rib · crackedINSPECTION TYPE: SI. NR 1 SLAT, NR 2 RIB FROM INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 SLAT NR 2 RIB FROM INBOARD OF TAIL DUCT PER SRM 57-50-3.SDR UPS96221453Jumper · corrodedINSPECTION TYPE: SI. NR 6 K-FLAP BULLNOSE BONDING JUMPER O/B UPPER ATTACH BOLT HAS PITTING AROUND BOLT HEAD. BLEND CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-50-0. K-FLAP ASSY WAS REPLACED ON NRC 597765.SDR UPS96221451Rib · crackedINSPECTION TYPE: SI. NR 3 SLAT OUTBOARD END RIB IS CRACKED IN RADIUS. REMOVED AND REPLACED NR 3 SLAT O/B END RIB IAW SRM 51-30-2, 51-10-1.SDR COMA9610307Flap · chafingNACELLE FLAP DISAGREEMENT WARNING WHEN FLAPS LOWERED. FOUND RT NACELLE FLAP CHAFING AT THE OUTBD HINGE. REPLACED FLAP.SDR CALA9601598Skin · crackedINSPECTION FOUND THREE 1 INCH CRACKS IN RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACKS WERE STOP DRILLED. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.SDR CALA9601597Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER OUTBOARD AREA OF RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.
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