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 MASA20220204097None · noneSLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PRSDR MASA20220128095None · corrodedSLAT TRACK 3-2 OF SLAT #3 ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.SDR DALA2022012400485None · noneSHIP 3231 FOUND ACCESS PANEL 622WB MISSING ON RIGHT WING OUTBOARD OFF PYLON. CORRECTIVE ACTION: INSTALLED NEW PANEL. OK FOR SERVICE. (8312807)SDR SWAA2022012160962Support Angle · crackedCRACK SUPPORT ANGLE LOCATED ABOVE FUEL BOOST PUMP IFSS 120 FRONT SPAR AT LT WING. REPLACED SUPPORT ANGLE LOCATED ABOVE FUEL BOOST PUMP IFSS 120 AT RT WING IAW B737-700 SRM 51-40-02; DWG 112A2004, SHEET 1, REV A AND SRM 57-20-10-1A-3.SDR LR7A2022011303074Skin · crackedDURING SCHEDULED DAILY INSPECTION FOUND CRACK ON LEFT WING LEADING EDGE AT OWS126L FS437 WL268 / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. LP 51785.SDR MASA20220113046None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113045None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113044None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113043None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113042None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113041None · corrodedRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR MASA20220113040None · noneRH SLAT TRACKS 1-1, 1-3, 2-1, 2-2, 3-1, 3-2 AND 3-3 FOR THE RH WING SLAT #1, #2 AND #3 WERE FOUND TO HAVE CORROSION DAMAGE ON LOWER SURFACES AS SHOWN IN FIGURES 1 THRU 3. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) CRJ900 ILLUSTRATED PARSDR DALA2022011600295None · noneER/A 590172-14 HAS BEEN UPDATED TO REV. A TO INCORPORATE REVISED REO APPROVAL. THE NEW APPROVAL INTRODUCES ADDTIONAL TIMECONTROL AND INSPECTION REQUIREMENTS. FOLLOW ON ACTION IS REQUIRED. ER/A 590172-14 REV. A SECTION III IS TO BE ACCOMPLISHED WITHIN 3 0000FC SDR TAMF20220112019Slat · dentedDURING THE “48 HOURS” AIRCRAFT SERVICE CHECK, A DENT WAS FOUND ON LH WING SLAT NUMBER 4.
PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH AIRBUS RDAF REF. 81011880/020 AND AIRBUS A330 SRM TASK 57-40-00-283-005SDR SWAA2022021459372Plate · crackedCRACK SLAT 6 PLATE ON AUXILIARY TRACK POSITION LOWER AT RT WING (1 EA) ; 2022-11246 / [01] REMOVED AND REPLACED SLAT 6 PLATE ON AUXILIARY TRACK POSITION LOWER AT RT WING (1 EA) IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02; [02] REMOVED AND REPLACED SLATSDR SWAA2022021558981Skin · crackedCRACK LOWER SKIN SLAT 1 AT LEVEL OF ACTUATOR FITTING SLAT STATION 451.97 AT LT WING ; 2022-12108 / [01] TOOL USED PN NORTEC 600D SN 200048001 DUE DATE 24-FEB-22; [02] PERFORMED PERMANENT REPAIR PARTS -1 DOUBLER -2 FILLER AND FASTENERS LOC. LOWER SKIN SLAT 1 ATSDR SWAA2022021558983Skin · crackedCRACK SLAT 4 LOWER SKIN AT LEVEL OF ACTUATOR FITTING SLAT STATION 85.19 AT LT WING ; 2022-12123 / [01] TOOL USED PN NORTEC 600D SN 200048001 DUE DATE 24-FEB-22; [02] PERFORMED PERMANENT REPAIR PARTS -1 DOUBLER -2 FILLER AND FASTENERS LOC. SLAT 4 LOWER SKIN AT SDR CALA2022010700053Skin · debondedNO.6 SLAT LOWER SURFACE MID AREA FOUND 1EA DISBOND. L/H WING NO.6 SLAT WEDGE ASSY REPLACED AND INSTALLED AS PER ECRA 5743-01626 REV -. RII BY TA507. REF TO ECRA:5743-01626,SDR EE4Y2022010514831None · noneDURING STRUCTURE INSPECTION, CUSTOMER FOUND THE LH WING, LEADING EDGE SECTION ON SLAT #2 O/B TRACK CUT OUT
WITH EXISTING REWORK. WAS REPAIRED INSTALLING AN INTERNAL REPAIR DOUBLER AS PER E.O# COO-EO-2021-14360-R00,ETD 2021-038880.SDR DALA2022010700141None · noneSHIP 6813 A.A. DISBOND OF 1.200 IN X 1.000 IN AT UPPER SKIN OSS 600 LE SLAT 9 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00032:DURING REPAIR PROCEDURE ON UPPER SKIN OSS 600 LE SLAT 9 TRAILING EDGE WEDGE PER B757-200 S.R.M. (2075374)SDR SWAA2022021458008Web · corrodedCORROSION WEB LOCATED INTERNAL CAVITY ACCESS PANEL 621GB LEADING EDGE AT RT WING ; 2021-585074 / [01] REPLACED WEB LOCATED INTERNAL CAVITY ACCESS PANEL 621GB LEADING EDGE AT RT WING IAW B737-700 SRM 51-40-02-0G AND AMM 28-21-00-400-801.; [02] REPLACED WEB LOCASDR DALA2022010700137None · noneSHIP 6822 DISBOND ON TRAILING EDGE WEDGE AFT EDGE INBD SIDE AT SLAT NO 7 RH WING (AD). CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00022: TRAILING EDGE WEDGE AFT EDGE INBD SIDE AT SLAT NO 7 RH WING WAS REPAIRED PER B-757-200 S.R.M. (2073374)SDR DALA2022010108189None · noneSHIP 181 FOUND LHW OB SLAT NO.2 UPR SUFACE BULGE FORM OB EDGE 10 INCHES. CORRECTIVE ACTION: LHW OB SLAT NO.2 UPR SUFACE FORM OB EDGE 10 INCHES REPAIRED: AS PER B767-300 SRM 51-70. (2067730)SDR A6WA202112288173Fitting · gougedCHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING. ****AIRCRAFT REMOVED FROM SERVICE ****** BLENDED CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING PN601R10315. CHAFE DIMENSIONS L = 0.500Ï¿½ X W = 1.750Ï¿½ X D = 0.020Ï¿½. PERFORMED HFECSDR DALA2021122808122None · noneSHIP 181 RHW NO.7 SLAT LEADING EDGE 01 EA DENT FORM I/B EDGE 88 INCH. CORRECTIVE ACTION: DENT AREA REPAIRED AND REPAIR PARTS MADE FORM ALCLAD SHT 7075T6- 0.063" AND ALCLAD SHT 7075T6-0.071" AS PER B767-300 SRM 57-43 (2066762)SDR DALA2021122808120None · noneSHIP 185 R/H WING #9 SLAT UPPER SURFACE FOUND CRACK AROUND THE FWD END#1 RIVET FROM 40 IN TO I/B EDGE. CORRECTIVE ACTION: REPAIRED AS PER B767-300 SRM 57-43 (2065867)SDR DALA2021122808119None · noneSHIP 185 R/H WING #10 SLAT UPPER SURFACE SUSPECT CRACK AROUND THE FWD END #1 RIVET FROM 40 IN TO I/B EDGE. CORRECTIVE ACTION: REPAIRED AS PER B767-300 SRM57-43. (2065854)SDR DALA2021122808116None · noneSHIP 185 R/H WING #9SLAT UPPER SURFACE FOUND CRACK AROUND THE FWD END #1 RIVET FROM 40 IN TO O/B EDGE. CORRECTIVE ACTION: REPAIRED AS PER B767-300 SRM57-43. (2065553)SDR DALA2021122408032None · noneSHIP 185 FOUND OUT SLAT NO.4 SKIN CRACK AROUND THE UPPER ROW FWD NO.1 RIVET HOLE AT 40INCHES TO OB EDGE. CORRECITIVE ACTION: CRACK AREA REPAIRED AS PER B767-300 SRM57- 43-01 (2061966)SDR DALA2021122408030None · noneSHIP 185 FOUND OUT NO.2 SLAT SKIN CRACK AROUND UPPER ROW FWD CRACK AREA REPAIRED AS PER B767-300 SRM57-43-01. (2061979)SDR DALA2021122408029None · noneSHIP 185 FOUND OUT NO.3 SLAT SKIN CRACK ADJACENT TO THE LOWER ROW MOST FWD RIVET AT 40INCHES TO IB EDGE. CORRECITIVE ACTION: CRACK AREA REPAIRED AS PER B767-300 SRM57- 43-01 (2061971)SDR SWAA2021122755019Web · crackedLEFT WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.SDR MASA20211221644Access Panel · noneTHE RH WING L/E SLAT# 2 ACCESS PANEL 63102 WAS FOUND TO HAVE AN ELONGATED FASTENER HOLE. PERFORMED PERMANENT REPAIR IAW CRJ900 IPC 57-42-32, FIG. 5, ITEM 125 (REV. 70DATED JUN. 25. 2021 ).SDR MASA20211221639None · noneTHE LH WING L/E SLAT 1 T/E WEDGE WAS FOUND WITH AN EXISTING DAMAGE BLENDOUT.AT THE AFT EDGE, BETWEEN SLAT TRACK 1-2 AND SLAT TRACK 1-3. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-00-00, 51-21-16, AND 51-13-02 TABLE 1. DEFECT LOCATION: LH WING LEADING EDGE SLSDR MASA20211221637None · noneTHE RH WING SLAT #3 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEMS 15,AND 90 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SLAT TRASDR DALA2021122307994None · noneSHIP 670 #2 SLAT T/E WEDGE UPPER SURFACE HAS (2) INDICATIONS OF DISBONDS. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON #2 SLAT T/E WEDGE IAW B757-200 SRM. (2058945)SDR MASA20211221636None · noneTHE RH WING SLAT #2 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 05, ITEMS 15, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SDR MASA20211221635None · noneTHE RH WING SLAT #1 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 01, ITEMS 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SDR MASA20211221628None · noneSLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEM 15, 90 (REV. 70 DATED 10 AUG 2021).SDR MASA20211221627None · noneSLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).SDR MASA20211221626None · noneSLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).SDR SWAA2022021054317Panel · delaminatedSUPPLEMENTAL INFORMATION: L/WING L/E ACCESS PANEL 521DB FWD I/B CORNER DELAMINATED ; / [01] PREPARED FOR REPAIR AT PANEL 521 DB AS PER B737-700 SRM 51-70-06-2R-6; [02] VERIFIED STEP 1. OK TO INSTALL REPAIR.; [03] REPAIRED AT PANEL 521 DB AS PER B737-700 SRM 51SDR SWAA2022020753919Skin · crackedR/WING #6 SLAT NOSE EXTERNAL SKIN AT ACTUATOR RIB HAS EVIDENCE OF CRACKS AT 5 EACH FASTENERS SLAT STATION 202.45 ; / [01] REMOVED FASTENER 5 EA AT RIGHT WING #6 SLAT NOSE EXTERNAL SKIN AT ACTUATOR RIB AS PER REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1SDR SWAA2022013156092Bracket · elongatedELONGATED HOLE SUPPORT BRACKET LOCATED INTERNAL CAVITY 511AT LEADING EDGE AT LT WING ; 2021-567078 / [01] REPLACED SUPPORT BRACKET LOCATED INTERNAL CAVITY 511AT LEADING EDGE AT LT WING IAW B737-700 SRM 51-10-02 AND 51-40-02; MATERIAL USED: PN#212A1214-1; PO#20SDR DALA2022121608151Slat · damagedSHIP 6709 # 5 LEADING EDGE SLAT UPPER WEDGE HAIL DAMAGED. CORRECTIVE ACTION: REF ERA 595672-14. (2050884)SDR AALA202201106730Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT #3 LOWER AFT BOLT. REPLACED BOLT PER AMM 27-84-65-400-002-A.SDR SWAA2022020252089Skin · crackedCRACK AROUND THE FASTENER AT NO.7 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. REMOVED PANELS 624CB; 624DB; 624EB AND FLEX SKIN AT SLAT #7 IAW SRM 51-40-02. FABRICATED REPAIR PARTS (1) DOUBLER; AND (2) FILLERS, AND APPLIED CHEMICAL CONVERSDR MASA20211213605None · damagedTHE RH WING SLAT 1 RIB AT SS 196.66 WAS FOUND WITH EXISTING MATERIAL REMOVAL COMMON TO THE SLAT DISCONNECT SENSOR STRIKE PIN. PERFORMED PERMANENT REPAIR IAW SRM 57-41-12-995-801, ITEM 28B (REV. 38 DATED JUL. 25, 2020).SDR AALA202112218164Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT #1 , TRACK #2 FORWARD LOWER BOLT. REPLACED BOLT PER AMM 27-84-61-200-001-A AND AMM 27-84-63-400-002-ASDR AALA202112214373Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE #1 SLAT, TRACK #3 ECCENTRIC BOLT . REPLACED BOLT PER AMM 27-84-61-200-001-A AND AMM 27-84-63-400-002-A.
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