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 2008UALA06457Panel · damagedNR 1 L/E SLAT INBOARD SECTION OF FIBERGLASS CLOSURE PANEL MISSING APPROX 30 INCHES. PANEL RECEIVED, NEED 8 HOURS TO INSTALL.SDR CALA0801061Skin · delaminatedRIGHT WING NUMBER 5 SLAT OUTBOARD EDGE ON TRAILING EDGE WEDGE SEALANT MISSING, CHECK FOR DELAMINATION. REPAIRED DAMAGE AT OUTBOARD TRAILING EDGE WEDGE NUMBER 5 SLAT PER B737-500 SRM 51-70-10.SDR ASAA0843759Skin · gougedNUMBER 2 SLAT LOWER TRAILING EDGE GOUGED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.SDR USAA2008120892195Panel · crackedMCN - MAJOR REPAIR - C12 CHECK - RIGHT WING NR 9 SLAT COVE PANEL AT WS 653 CRACKED. REPLACED RIGHT WING NR 9 SLAT COVE PANEL AT WS 653 IAW BOEING DWG 114N4076.SDR 08FDEA04780Skin · chafedRIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122632. REPAIR CLASSIFIED AS MSDR 08FDEA04779Skin · chafedLEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122631. REPAIR CLASSIFIED AS SDR FDEA200811054724Skin · crackedLT WING L/E FOUND CRACK ON SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 39. VOL I.SDR FDEA200811054718Angle · crackedLT WING SLATS FOUND CRACK ON ANGLE OTBD SIDE NR 2 SLAT. REPAIRED ANGLE IAW SRM 57-00-01 FIG 3 SHT 2 VOL I.SDR FDEA200811054728Switch · misalignedNR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4.SDR ASAA0843722Skin · dentedNR 4 SLAT T/E WEDGE UPPER SURFACE IS DENTED. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR 08FDEA04718Angle · crackedLH WING SLATS FOUND CRACK ON ANGLE OUTBOARD SIDE NR 2 SLAT.SDR SWAA086072Skin · crackedDURING SCHEDULED SPV CHECK, FOUND NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR DHLA2008745678Skin · crackedNR 5 L/E SLAT SKIN CRACKED AT TRACK, SLAT STA 90.25 ACCOMPLISHED REPAIR TO NR 5 SLAT SKIN PER EO COO-2-57-344-08 DATED 10/08/08. REFERENCE FAA FORM 8110-3 DATED 10/12/08 AND EVA B257-00136 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 6-327SDR 08FDEA04673Angle · crackedLT WING OTBD LE APPROX CLOSE OUT WEB UPPER ANGLE IS CRACKED REMOVED DAMAGED ANGLE. INSTALLED NEW ANGLE, IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR UALA2008112006594Panel · damagedNR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGE BY AIRSTAIR.SDR ASAA0843811Skin · delaminatedNR 3 SLAT T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. PREPPED DELAMINATED AREAS FABRICATED AND INSTALLED REPAIR CORE FILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 4.SDR SWAA086023Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA086022Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA085972Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0843786Skin · chafedNUMBER 4 SLAT TE WEDGE LOWER SKIN IS CHAFED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR FILLER AND DOUBLERS PER SRM.SDR ASAA0843749Skin · dentedNR 5 SLAT UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR SWAA085895Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND NR 2 SLAT T/E WEDGE DELAMINATED AT UPPER SURFACE. REPAIRED WEDGE PER SRM.SDR UPS08854141Skin · damagedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-08 LT OUTBOARD VANE SKIN PLATING EO DC8-5100 -30418-C APPX H STEPS 4, 5, 6 & 7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FSDR 22AA20081006Slat · damagedON SERVICE CHECK, RT WING SLAT NR 8 LEADING EDGE DAMAGE. FOUND BIRD STRIKE ON RT WING SLAT NR 8 LEADING EDGE; INSPECTED RT WING SLAT NR 8 LEADING EDGE IN ACCORDANCE WITH DC10 M/M 05-62-00. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATISDR SWAA085818Wedge · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING LEADING EDGE NR 3 SLAT I/B UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA085811Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING L/E NR 3 SLAT INBOARD UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA085800Skin · crackedDURING SCHEDULED 14Y CHECK, FOUND NR 2 SLAT L/E LOWER SKIN CRACKED I/B OF ACTUATOR. REPAIRED SKIN PER SRM.SDR CALA0801008Skin · delaminatedLEFT WING NUMBER 2 SLAT INBOARD AND OUTBOARD WEDGE SEALANT DAMAGED, NEED TO CHECK FOR DELAMINATION. REMOVED AND REPLACED DELAMINTED SKIN AND CORE ON LEFT WING NUMBER 2 SLAT PER SRM 51-70-10 AND APPLIED PROTECTIVE FINISH PER CAL ECRA 5100 500128 REV Q.SDR SWAA085844Slat · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA085847Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT AFT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA085788Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM.SDR UPS08854140Structure · damagedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-05 LT SLOT VANE XFS 239.0 EO DC8-5100-30418 -C APPX H STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED REPLACEMENT REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DC-8 SRM 57-03-03 FIG 10 SHEET 1 ANSDR ASAA0843767Skin · dentedNUMBER 9 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.SDR ASAA0843745Skin · damagedRIGHT FIXED LEADING EDGE DAMAGED, NO SPECIFICS AT NR 4 K FLAP ACTUATOR LOWER EDGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 57 41 01.SDR USAA920081997Skin · delaminatedCLT Q3 MAJOR REPAIR NR 03C40257009/009 DELAMINATED AREA ON NR 5 SLAT TRAILING EDGE WEDGE OTBD END. REPAIRED NR 5 SLAT TRAILING EDGE IAW B737 SRM 51-70-10, REPAIR NR 4.SDR USAA920081933Panel · crackedCLT C3 MAJOR REPAIR NR 19C51057012/001 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 30 INCHES FROM OTBD END. REPAIRED NR 1 SLAT CLOVE PANEL AT OTBD SLAT TRACK IAW BOEING DRAWING NR 114N075-11.SDR USAA920081934Pcu · crackedCLT C3 MAJOR REPAIR NR 19C51057012/004 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 27 INCHES FROM OTBD END. REPAIRED NR 1 SLAT COVE PANEL AT OTBD SLAT TRACK IAW BOEING DRAWING NR 114NO75-11.SDR UALA2008111306195Slat · damagedNR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGED BY AIR STAIR. SLATS REPLACED.SDR 2008UALA06195Slat · damagedNR 1 AND NR 2 LEADING EDGE SLAT DAMAGE.SDR SWAA085654Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM.SDR FDEA200810184424Panel · crackedNR 2 L/E SLAT COVE PANEL, INBD OF OTBD MAIN TRACK IS CRACKED. REMOVED AND REPLACED COVE PANEL IAW SRM 51-40-02 AND DRAWG NR 114N4076.SDR 08FDEA04424Panel · crackedNR 2 LEADING EDGE SLAT COVE PANEL, INBD OF OTBD MAIN TRACK IS CRACKED. REMOVED AND REPLACED COVE PANEL IAW SRM 51-40-02 AND DRAWING, NR 114N4076.SDR 08FDEA04415Slat Track · gougedLEFT WING NR 18 SLAT TRACK UPPER CLOSE OUT PANEL IS GOUGED. REMOVED AND INSTALLED DOOR ASSY IAW SRM 51-31-01. CLEANED, WELDED & INSPECTED REF. DPS 10.225. ALODINED & PRIMED IAW SRM 51-21-01.SDR AALA200820021Skin · crackedNR 10 SLAT ASSY SKIN CRACKED. REPAIR DOUBLER INSTALLED IAW AARD 57-43-00-04SDR AALA200820020Skin · corrodedNR 10 SLAT ASSY SKIN CORRODED. REPAIR DOUBLER INSTALLED IAW ECO B757-57-004757 DATED 10/16/2008.SDR DHLA20087651016Casting · crackedUPON VISUAL INSPECTION FOUND THE NR 6 K-FLAP CENTER HINGE CASTING OUTBOARD SIDE AT THE ATTACH POINT FOR THE ACTUATOR ROD END CRACKED APPROX 2 INCHES IN LENGTH. K-FLAP IS TO BE CHANGED. REMOVED PART NUMBER IS 65-16227-18 SERIAL NUMBER BN1869. UNKNOWN IS THE SDR UPS08M53782Skin · crackedINSPECTION TYPE:1C CRACK FOUND ON LT WING DROOP L/E UPPER SKIN O/B SIDE. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 30.SDR DHLA2008745523Rib · crackedRT WING NR 5 L/E SLAT HAS A CRACKED RIB, AT SLAT STA 150. REMOVED AND REPLACED RIB MEMBER, BY FABRICATION, AND ASSOCIATED TRACK FITTING PER B727 SRM 57-50-2 FIG 2, 51-10-1, AND 51-30-2. REF N/R 4987-6-173.SDR USAA920081921Skin · delaminatedBFM MAJOR REPAIR C3 CHECK NR 6013567 LT WING NR 3 SLAT UPPER SURFACE DELAMINATED OTBD END. REPAIRED LT WING NR 3 SLAT UPPER SURFACE OTBD END IAW B767 SRM 57-43-01.SDR USAA920081920Skin · delaminatedBFM MAJOR REPAIR C3 CHECK NR 6013566 RT WING NR 8 SLAT UPPER SURFACE DELAMINATED 2 INCHES FROM INBD TRAILING EDGE WEDGE. REPAIRED RT WING NR 8 SLAT UPPER SURFACE 2 INCHES FROM INBD TRAILING EDGE WEDGE IAW B767 SRM 57-43-01.
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