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 AALA2018051749012Bolt · corrodedCORROSION FOUND ON THE SLAT TRACK NR 9 FORWARD BOLT ON LEFT WING. REPLACED THE BOLT IAW AMM 27-84-66.SDR AALA2018051649023Bolt · corrodedCORROSION FOUND ON SLAT TRACK NR 12, LOWER FORWARD BOLT ON THE LEFT WING. REPLACED THE BOLT IAW AMM 27-84-67-000-001-A, AND AMM 27-84-67-400-001.SDR SWAA2022021624555Panel · elongated:RIGHT WING LEADING EDGE PANEL 621FB HAS ELONGATED FASTENER HOLE / REPAIRED PANEL PER SRM 51-70-05. REFOILED PER SRM 51-70-14 AND RESTORED FINISH PER MM 51-21-99.SDR SWAA201805161612Skin · delaminatedLEFT WING FIXED LEADING EDGE COMMON TO THE NR 3 SLAT DELAMINATED. REPAIRED THE SLAT IAW EA.SDR SCNA2018043000081Skin · crackedDURING A WALK AROUND, FOUND A CRACK IN THE NR 8 SLAT CENTER LINE 3/8 INCH ON ONE SIDE AND 1/8 INCH ON THE OTHER OF RIVET HOLE AT SLAT ACTUATOR MOUNT AREA. REMOVED AND REPLACED THE NR 8 LEADING EDGE SLAT.SDR CALA2018043001202Skin · dentedRIGHT WING NNR 3 SLAT UPPER L/E SKIN DENTED. REPAIRED THE DENT IAW SRM 57- 40-00-300-108.SDR SCNA20180426080Structure · crackedFOUND A CRACK ON THE NR 2 LT LE SLAT. LENGTH OF CRACK IS 1.125 INCH. THE CRACK IS ACCEPTABLE TO FLY FOR 50FC. REMOVED AND REPLACED THE NR 2 LT L/E SLAT. OK FOR SERVICE.SDR DALA201804302919Roller · missingEMERGENCY LANDING DUE TO A LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATING DURING A GO AROUND. NR 3 LEADING EDGE SLAT HAD AMBER LIGHT, THE REST WERE GREEN. AFTER TOUCH DOWN, THE NR. 3 LEADING EDGE SLAT TURNED GREEN, MADE FLAPS 15 FOR EMERGENCY LANDING. REMOVESDR DALA2018042102799Wedge · delaminatedRIGHT WING NR 8 SLAT UPPER WEDGE HAS A DELAMINATED SPOT AT THE INBD END, EXTERIOR SURFACE. REPAIRED IAW SRM 51-70-10.SDR V0XD20180420004Bracket · crackedLEFT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577 REV -, SRM 51-23-00, 51-26-00, AND NDTM PART 01, 51-20-006.SDR V0XD20180420003Bracket · crackedRIGHT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577, REV -, SRM 51-23-00, AND NDTM PART 01 51-20-006.SDR AALA201804249015Bolt · corrodedCORROSION FORWARD BOLT OF SLAT TRACK 11 ON RIGHT WING BETWEEN WS 1228 TO 1287, BETWEEN RIBS 23 TO 24. REPLACED FORWARD BOLT OF SLAT TRACK 11 ON RIGHT WING IAW AMM 27-84-67.SDR SWAA2018042421361Skin · damagedNR 3 L/E SLAT HAS A CREASE ON UPPER SURFACE AT OTBD AUX TRACK CUTOUT. R & R THE SLAT IAW MM.SDR DALA2018042002723Skin · damagedNR 5 SLAT HAS DAMAGE. INSTALLED A PERMANENT REPAIR IAW SRM 51-10-06, REPAIR 1, SRM 57-43-01, ALLOWABLE DAMAGE 1, FIG 101, AND SRM 51-70-10, REPAIR GENERAL, AND REPAIR 3.SDR FDEA201804191065Skin · crackedLEFT WING NR 8 L/E SLAT LOWER SURFACE SKIN FOUND CRACKED ABOUT 2 INCHES IN LENGTH AT XOS 1055.SDR AALA2018051709031Bolt · corrodedCORROSION FOUND ON THE BOLT AT THE NR 1 SLAT TRACK UPPER FORWARD, RIGHT WING. REPLACED THE BOLT IAW AMM 27-84-63.SDR AALA2018042659023Bolt · corrodedCORROSION FOUND ON SLAT TRACK NR 6 BOLT RT WING. REPLACED THE BOLT IAW AMM 27-84-64.SDR DALA2018041802614Skin · chafedNR 8 SLAT TRACK T/E WEDGE LOWER SURFACE SKIN CHAFED AT FWD OF INBD SLAT TRACK. FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A PERMANENT REPAIR AW SRM 57-43-02, AND 51-70-10, REPAIR 4.SDR DALA2018041402481Skin · wornLEFT WING NR 5 SLAT T/E WORN, 17 INCHES FROM THE OTB EDGE. REPAIRED IAW SRM 51-70-10.SDR AALA201804239062Bolt · corrodedCORROSION FOUND ON THE SLAT TRACK NR 8 UPPER FORWARD BOLT, RIGHT WING. REPLACED THE BOLT IAW AMM 27-84-65.SDR DALA2018041402570Skin · crackedNR 1 SLAT COVE SKIN IS CRACKED AT INBD SIDE OF INBD SLAT TRACK FITTING. REPAIRED THE SLAT COVE SKIN AT OSS 736.70 IAW ER/A 556511-14, REV, ORIGINAL.SDR DALA2018041402569Skin · debondedRIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 58 INCHES FROM INBD END IS DEBONDED. REPAIRED THE SKIN IAW B757 57-43-02, REPAIR 1, AND SRM 51-70-10, REPAIR 3 & 4.SDR AALA201804239059Bolt · corrodedCORROSION FOUND ON THE BOLT ATTACHMENT OF SLAT TRACK NR 12 LOWER FWD ON THE LEFT WING. REPLACED THE BOLT IAW AMM 27-84-67.SDR AALA201804239058Bolt · corrodedCORROSION FOUND ON THE SLAT TRACK NR 12, LOWER AFT BOLT ON THE LEFT WING. REPLACED THE BOLT IAW AMM 27-84-67.SDR AALA201804239054Bolt · corrodedCORROSION FOUND ON THE SLAT TRACK NR 6, LOWER FORWARD BOLT, ON THE LEFT WING. REPLACED THE BOLT IAW AMM 27-84-64.SDR CALA2018041301164Skin · chafedLEFT WING, NR 3 SLAT LOWER SKIN, WS 537 AND 453 CHAFED. FOUND TO BE OUT OF LIMITS IAW 57-43-02, FIG 101. REPAIRED THE SKIN IAW EC/RA 5740-02861, REV-, AND REV A.SDR CALA2018041201151Skin · chafedLEFT WING NR 2 SLAT HAS TWO CHAFES ON THE BOTTOM SIDE OF THE SLAT AT WS 623 AND 590. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, REPAIRED IAW EC/RA 5740-02862, REV.SDR CALA2018041201150Skin · chafedLEFT WING NR 4 SLAT LOWER SIDE, UPPER EDGE CHAFED AT WS 397.5. FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101. REPAIRED IAW EC/RA 5740-02860, REV.SDR CALA2018041001145Skin · crackedNR 10 SLATHAS A CRACK IN THE SKIN. REPAIRED THE SLAT IAW SRM 57-43-01, PG 201-205.SDR SWAA2022021470026Slat · crackedREMOVE AND INSTALL NEW #2 SLAT DUE TO CRACK AT ACTUATOR RIB AND AFT EDGE WORN. / REMOVED AND INSTALLED #2 SLAT SERVICABLE SLAT IAW AMM 27-81-21-000-801 AND 27-81-21-400-801. ADJUSTMENTS AND OPPS CHECKS GOOD. SEE SAM 326 FOR FURTHER SIGN OFFS. (POS:#2; TAG NO:3SDR SWAA201805161608Skin · crackedRIGHT WING NR 6 SLAT, NOSE SKIN CRACKED ON LOWER SURFACE AT ACTUATOR RIB. REPAIRED THE SKIN IAW SRM.SDR SWAA2018041121126Skin · crackedRIGHT WING NR 6 SLAT SKIN CRACKED AT SLAT ACTUATOR FITTING FASTENER SLAT STA. 202.45. R & R THE NR 6 SLAT IAW AMM.SDR SWAA2018051421873Skin · crackedRT WING NR 6 SLAT LEADING EDGE NOSE SKIN CRACKED AT SLAT STA 202.45. REPAIRED SKIN IAW ER AND EA.SDR SWAA2018051621983Skin · crackedLEFT WING NR 1 SLAT LEADING EDGE NOSE SKIN CRACKED AT SLAT STA. 451.97 ACTUATOR RIB FASTENER. REPAIRED THE SKIN IAW ER AND EA.SDR SWAA2018041121127Skin · crackedRIGHT WING NR 8 SLAT SKIN CRACKED AT SLAT ACTUATOR FITTING FASTENER SLAT STA 451. R & R THE SLAT IAW AMM.SDR DALA2018040602229Slat Track · wornWEAR ON THE SLAT TRACK DOOR NR 8 AT THE LT WING. SLAT TRACK DOOR WAS REPLACED IAW ER/A 540095-14MA, REV A, SECTION II.SDR CALA2018040601117Wedge · delaminatedON VISUAL INSPECTION OF THE NR 3 SLAT TRAILING EDGE WEDGE, FOUND AN AREA OF DELAMINATION, 40 INCHES FROM THE INBD END, 6.5 INCHES FROM THE TOP, ABOUT 4 INCHES IN DIAMETER. REMOVED AND REPLACED THE NR 3 SLAT IAW MM 27-81-02.SDR DALA2018040504206Door · damagedLEFT NR 1 SLAT OUTBOARD TRACK DOOR DAMAGED. REMOVED DOOR AND FORWARD TO CDL 57-47-01. MCC NOTIFIED. MCC PLACARD INSTALLED. EA 5929781-2.SDR SWAA2018043021546Skin · crackedLT WING LOWER SURFACE NR 3 SLAT SKIN AT FASTENERS HOLE CRACKED. REPAIRED SKIN IAW SRM.SDR 2018F00149Skin · damagedDAMAGE TO SLAT SKIN AND GOUGE TO INBOARD HLE SKIN P/N 6722402-41. ACCOMPLISHED ENGINEERING LETTER DQ11736M1.SDR 2018FA0000127Skin · damagedDAMAGE TO SLAT SKIN AND GOUGE TO INBOARD HLE SKIN P/N 6722402-41. ACCOMPLISHED ENGINEERING LETTER DQ11736M1.SDR FDEA201804020828Skin · crackedCRACK GOING OUT FROM SKIN AFT SIDE OF THE NR 1 SLAT FROM FASTENER. COMPLIED WITH EA F-5750-T0339279 P1. FABRICATED TWO REPAIR DOUBLERS, FILLERS & INSTALLED IAW SRM 57-43-01-2R, REPAIR 4.SDR SWAA2018043021555Skin · crackedRT WING NR 5 SLAT NOSE SKIN LOWER SURFACE AT ACT RIB FASTENER HOLE CRACKED. REPAIRED NR 5 SLAT SKIN IAW SRM.SDR FDEA201803300806Skin · dentedLEFT WING L/E SLAT HAS DENT ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 57 & 60 INCHES. REPAIRED IAW SRM 51-70-10, REPAIR 2, SRM 57-43-02-2R, AND EA H-5750-T0339161, P1. MAJOR REPAIR.SDR FDEA201803270789Skin · dentedRIGHT WING L/E NR 10 SLAT HAS DENTS ON T/E WEDGE UPPER SKIN FROM INBD BETWEEN 62 INCHES & 71 INCHES. REPAIRED THE SLAT IAW SRM 51-70-10-2R, REPAIR 2, MAJOR REPAIR.SDR DALA2018032801988Wedge · debondedRIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 58 INCHES FROM INBD END IS DEBONDED. REMOVED A 2INCH DIAMETER CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCH DIA AND CORE PLUG IAW 57-43-02, REPAIR 1, AND SRM 51-70-10, REPAIR 3, & 4.SDR DALA2018032801987Wedge · debondedRIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 31 INCHES FROM INBD END IS DEBONDED. REMOVED A 2 INCH DIA CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCHES IN DIAMETER AND CORE PLUG IAW SRM 57-43-02, REPAIR 1, AND SRM 51-70-10 REPAIR 3SDR FDEA201803270792Pulley Bracket · gougedLEFT WING SLAT CABLE RUBBING INTO PULLEY BRACKET JUST OUTBOARD OF THE DRIVE ASSEMBLY BEHIND THE NR 3 & 4 SLAT SPLIT. OCCURRED DUE TO THE CABLE NOT RIDING INSIDE OF PULLEY TRACK. THE PULLEY GUIDE PIN WAS FOUND DANGLING UNSECURE AT THE BRACKET. REPLACED NEW ASDR DALA2018032902022Skin · wornDURING INSPECTION, FOUND WEAR ON THE NR 7 SLAT, LOWER SKIN, AT THE WEDGE AREA, ON THE RT WING. MAINTENANCE REPAIRED THE SLAT SKIN.SDR DALA2018032902021Skin · wornDURING INSPECTION, FOUND WEAR ON THE NR 6 SLAT LOWER SKIN, AT THE WEDGE AREA ON THE RT WING. MAINTENANCE REPAIRED.
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