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 DHL2006805508Skin · damagedLT OTBD SLOT VANE HAS AN INTERIM REPAIR AT STA XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-07-06, EO NR AST060903 DATE 09-06-06. REMOVED INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. TRIMMED OUT DAMAGED AREA IAW EO NR AST060SDR DHL2006805507Skin · damagedRT OTBD WING SLOT VANE HAS AN INTERIM REPAIR AT STA XOLD 6.224. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 09-07-06, EO NR AST060904 DATE 09-07-06. REMOVED INTERIM REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. TRIMMED OUT DAMAGED AREA IAW EO NR AST0SDR USAA061178Wedge · delaminatedUPPER SURF OB END OF NR2 SLAT AT WEDGE. REMOVED DAMAGED CORE INSTALLED NEW CORE IAW SRM 51-70-10 DEFECT SIZE: 7.5 INCHES X 5.0 INCHES.SDR USAA061180Wedge · debondedDEBONDED UPPER SURF IB END OF NR 2 SLAT AT WEDGE REMOVED DAMAGED CORE, RECORED AND INSTALLED DOUBLER IAW SRM 51-70-10 DEFECT SIZE: 6.0 INCHES X5.0.SDR SWAA063528Skin · crackedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SURFACE CRACKED AT OB AUX TRACK LOCATION. REPAIRED SLAT IAW SRM.SDR QXEA200602582Skin · nickedC3 PDX - LEFT WING CENTER SLAT LOWER SURFACE HAS 1" LINE OF SMALL NICKS. REPAIRED IAW SRM 57-42-01 AND SRM 51-20-006.SDR QXEA200602581Skin · nickedC3 PDX - LEFT WING INBOARD SLAT HAS 2 NICKS. REPAIRED IAW SRM 57-42-01 AND SRM 51-20-00.SDR SWAA063479Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED UPPER OUTBOARD CORNER. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR 06FDEA03324Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG.402-408 AND FOUND WITHIN DAC DWG ARC0503 LIMITS. ORIGINAL THK I/B 0.408" REMSDR 06FDEA03323Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.2695" FINAL 1.314" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSDR 06FDEA03321Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.1885" FINAL 1.2155" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSDR 06FDEA03320Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE LOWER MOUNT SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 AND WITHIN DAC DWG ARC 0502 LIMITS. SHIMS FABRICATED AND INSTALLED SDR SWAA063466Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED. REPAIRED NR 5 L/E SLAT SKIN PER SRM.SDR IXXA06SMN294SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT VANE SKIN HOLES ELONGATED AT STATION XS 250.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, INTERNSDR USAA061150Skin · delaminatedLOCATION: NR 9 SLAT IB AND OB END, UPPER SURFACE FAB'D DOUBLER, APPLIED SEALANT AND TOPCOAT IAW SRM 51-70-10 & 51-70-10 DEFECT SIZE: .100 INCH W X .008 INCH D DENT AND 2 INCHES L X 2 INCHES W X .016 INCH D DELAMINATION..SDR AWXA200601642Skin · crackedMCN - MAJOR REPAIR RIGHT WING NR 6 SLAT SKIN SLAT LOWER SURFACE SKIN HAS 3 CRACKS, SLAT STA 254.5-256.5. REPAIRED RIGHT WING NR 6 SLAT BOTTOM SKIN, SLAT STA 254.5-256.5 IAW B737-300 SRM 57-43-01-2R6 FIG 201.SDR AWXA200601641Skin · crackedMCN - LEFT WING NR 1 SLAT SKIN SLAT LOWER SURFACE SKIN HAS 3 CRACKS, SLAT STA 294-297. REPAIRED LEFT WING NR 1 SLAT BOTTOM SKIN, SLAT STA 294-297 IAW B737-300 SRM 57-43-01-2R6 FIG 201.SDR 06FDEA03237Panel · crackedLEFT WING NR 2 SLAT TRAILING EDGE PANEL OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR AWXA200601612Hinge · brokenMAJOR REPAIR - LOG PAGE NR 7234081. LT KRUGER OUTER DOOR CRACKED AND HINGE BROKEN. DEFFERRED TO CDL 57-41-1, C1. REPLACED LEFT KRUGER OUTER DOOR & HINGE I/A/W B737-300 AMM 57-20-00.SDR 2006FA0001102Bolt · loose(REF NR: ATC0712) DURING AN A-CHECK INSPECTION OF RT WING LEADING EDGES. THE OB TRACK ATTACHMENT BOLT ON THE NR 6 SLAT WAS FOUND TO BE LOOSE AND ALSO THE SPLIT PIN WAS MISSING. A NON ROUTINE CARD, WO 3956/06 HAS BEEN RAISED TO FIT THE SPLIT PIN AND RECTIFY TSDR 0601939605Rod End · brokenAS THE AIRCRAFT WAS ON APPROACH FOR LANDING AT BIS THE SLAT DEPLOYMENT WAS ASYMMETRICAL AND THE AIRCRAFT EXPERIENCED AND UNCOMMANDED ROLL. CREW RETRACTED THE LEADING EDGE DEVICES AND RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT MSP. MAINTENANCE FOUNDSDR HALA0600717Rib · crackedANGLE CRACKED IN FIXED L/E FWD OF RIB ON OB SIDE OF NR 8 SLAT, OB ROTARY ACTUATOR. REMOVED ANGLE IN L/E OB NR 8 ROTARY ACTUATOR, REPLACED ANGLE AND INSTALLED ALL BUT (3) RIVETS, COMMON TO SKIN IAW SRM 51-40-01. INSTALLED (3) FASTNERS COMMON TO L/E SKIN IAW SSDR SWAA063233Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT LOWER SKIN CRACKED AT AFT INBOARD END. REPAIRED SKIN PER SRM.SDR USAA061101Skin · crackedFOUND CRACK NR 1 SLAT SKIN 43" INBOARD FROM INBOARD END ON LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .25".SDR USAA061079Skin · crackedFOUND CRACK LEADING EDGE SKIN, JUST AHEAD AND INBOARD OF OUTBOARD AUX TRACK. INSTALLED DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .25".SDR SWAA063222Flap · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E KRUEGER FLAP CRACKED AT INBOARD ACTUATOR ROD END CUTOUT. REMOVED AND REPLACED KRUEGER FLAP PER MM.SDR AWXA200601571Slat · crackedMCN - FOUND 2 CRACKS, BOTTOM NR 5 SLAT BELOW OUTBD MAIN TRACK, SLAT STA 230 - 232. REPAIRED 2 CRACKS BOTTOM NR 5 SLAT BELOW OUTBD MAIN TRACK, IAW B737-300 SRM 57-43-01-2R6, FIG 201.SDR 06FDEA03101Skin · chafedRT WING DROOP LE INBD SKIN FOUND CHAFE MARK (DROOP LE ASSY P/N ARB3027-502). REMOVED FOR REPAIR AS PER SRM 51-31-01 VOL.II. REINSTALLED RUBSTRIP AFTER REPAIR AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.SDR 06FDEA03100Skin · chafedLT WING DROOP LE OUTER SKIN INBD AND OUTBD EDGE FOUND CHAFE MARK, (DROOP LE ASSY P/N ARB3027-501). REPAIR CARRIED OUT AS PER E.A.1-5740-102167.SDR PIDR2006011Skin · crackedNUMBER THREE SLAT LOWER SKIN IS CRACKED AT THE ACTUATOR. REPAIRED PER SRM 57-43-01.SDR QXEA200602409Skin · damagedPDX- C3 CHECK- LEFT WING NR 1 SLAT AFT TRAINING EDGE IS DAMAGED AT WS 108. BLENDED OUT DAMAGE WITHIN LIMITS IAW REO 670-57-42-088/1. TREATED AND PAINTED AREA.SDR QXEA200602378Skin · chafedPDX - C3 CHECK, RIGHT WING INBOARD SLAT LOWER AFT EDGE CHAFED AT WS 68. BLENDED AND POLISHED AREA, MATERIAL LOSS .004, WITHIN LIMITS OF SRM 57-41-01-101-001-A01. TREATED AND PAINTED AREA. NO PARTS REPLACED.SDR 06FDEA03050Skin · damagedFOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR, DISCREPANCY REPORT 43000001-391SDR UPS06847787Rib · crackedINSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 460 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 460 IAW SRM 57-02-00 FIG 002.SDR 06FDEA03020Hinge Bracket · corrodedRT WING OUTBD FLAP (FLAP SIDE) OUTBD HINGE PIVOT PIN ATTACHMENT INBD BORE FOUND CORROSION. RT AFT O/B FLAP O/B HINGE PIVOT I/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG 626-627. ORIGINAL THK 1.340" FINAL 1.3425" MAX ALLOWABLE 1.150SDR 06FDEA3019Hinge Bracket · corrodedRIGHT WING INBD FLAP (WING SIDE) OUTBD PIVOT HOLES SPOT FACE FOUND CORRODED (OUTBD HINGE BRACKET P/N ARC0154-502).SDR 06FDEA3020Hinge Bracket · corrodedRT WING OUTBD FLAP (FLAP SIDE) OUTBD HINGE PIVOT PIN ATTACHMENT INBD BORE FOUND CORROSION (OUTBD HINGE BRACKET P/N ARC1991-14).SDR AWXA200601522Skin · crackedMCN - CRACK ON NR 2 SLAT, COVE SKIN, OSS 677. REMOVED AND REPLACED NR 2 SLAT COVE SKIN, OSS 677, IAW B757-200, SRM 51-30-01-06, FIG 7, AND 51-40-02-06, PAR 5, 6 FIGS 9, 10, 11, AND BOEING DWG, 114N4077.SDR AWXA200601520Skin · crackedMCN - CRACK ON NR 3 SLAT COVE SKIN, OSS 472. REMOVED AND REPLACED NR 3 SLAT COVE SKIN AT OSS 472, IAW B757-200, SRM 51-40-02-06, PAR 5, 6, FIGS 9, 10, 11, 51-30-01-06, FIG 7, AND BOEING DWG, 114N4076.SDR F3LA200600095Slat Track · damagedDURING C-4 CHECK, INSPECTION REPORTED LT WING, NR 1 SLAT I/B SLAT TRACK CUTOUT DAMAGED. REMOVED DAMAGED AREAS AND PERFORMED HFEC INSPECTION. NO FAULTS OR CRACKS NOTED. APPLIED ALODINE TREATMENT EPOXY PRIMER AND PAINT TO AFFECTED AREAS. REFERENCE A319 SRM 5SDR 06FDEA02998Rib · crackedSNRM N01252: RHW LE SLAT TRACK NR 16 I/B RIB FOUND CRACKED. SNRM N01252: CRACKED RHW LE SLAT TRACK NR 16 I/B RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR UPS06847768Rib · crackedINSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-3-3, 57-02-00, 51-1-21 AND 51-1-20D.SDR 06FDEA2998Rib · crackedRT WING LE SLAT TRACK NR 16 I/B RIB FOUND CRACKED.SDR UPS06847796Rib · crackedINSPECTION TYPE:C3 LT CENTER L/E WING RIB CRACKED AROUND FASTENER HOLE AT XFS-448. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED ANGLE REPAIR LT CENTER L/E WING RIB AT XFS-448 IAW SRM 53-03-03-0 FIG 005 AND SRM 51-1-20D.SDR UPS06847790Rib · crackedINSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 409. STOP DRILLED CRACKED RIB AT LT L/E RIB STA XFS 409 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 409 IAW SRM 57-02-00 FIG 002.SDR UPS06847788Rib · crackedINSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 491. STOP DRILLED CRACKED RIB AT LT L/E UPPER RIB AT STA XFS 491 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 491 IAW SRM 57-02-00 FIG 002.SDR UPS06847765Rib · crackedINSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 310. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.SDR SWAA063049Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR UPS06847798Rib · gougedINSPECTION TYPE:C3 RT CENTER L/E WING UPPER RIB HAS DEEP GOUGE AT XFS 435 BLENDED GOUGE IAW SRM 57-02-00 FIG 2 SHEET 2 (OUT OF LIMITS). FABRICATED AND INSTALLED DOUBLER IAW SRM 57-3-3 FIG 5, SRM 57-02-00 AND SRM 51-1-20D AT RT CENTER L/E UPPER RIB XFS 435SDR UPS06847797Rib · crackedINSPECTION TYPE:C3 RT CENTER L/E WING UPPER RIB CRACKED AT XFS.404. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-02-00-0,SRM 51-1-20D, AND SRM 51-1-21 AT RT CENTER L/E UPPER RIB XFS.404.
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