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 AALA202305025867Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 LOWER AFT BOLT AT WS 14057 AND RIB 26. REPLACED BOLT PER TASK CARD 26C61057005.SDR DALA2023050103361Unknown · unknownERA608364-14AD SECTION I ISSUED FOR CORROSION FINDINGS ON LH WING SLAT TRACKS 1-11. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II EVERY 850FH FROM SECTION I UNTIL SECTION III. SECTION III REQUIRED PRIOR TO 8500FH FROM SECTION I. ASSOCIATED AA 5742-01028 ADDSDR AALA202305020863Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #11 UPPER BOLT AT WS 12277 AND RIB 23. REPLACED BOLT PER TASK CARD 26C61057005.SDR SWAA2023060241688Panel · crackedRT WING L/E PANEL 621PB FWD CORNER IS CRACKED (MARKED)<[01] IDENTIFIED PANEL 621PB IAW SRM 57-41-01-0I-4 FIGURE 3 TABLE 3 ITEM 1.<BR>DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-05-2R-6 PESDR SWAA2023053041885Skin · cracked#1 SLAT LEADING EDGE NOSE SKIN IS CRACKED JUST I/B OF ACTUATOR FITTING<CUT AND REMOVED 3EA CRACKS ON SKIN AS FOLLOWS; -O/B 2ND FWD FASTENER ON ACTUATOR RIB FITTING IAW SRM 57-42-01-2R-8 REPAIR 8 REQUIREMENTS.<BR>-O/B 1ST FASTENER ON I/B DOWN STOP RIB IAW SRM 5SDR AALA202305027820Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #8 LOWER FORWARD BOLT AT WS 9235 AND RIB 17. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202304256115Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #4 LOWER BOLT AT WS 3059 AND RIB 6. REPLACED BOLT PER AMM 27-84-63.SDR FDEA202304220745Skin · dentedRIGHT WING #11 SLAT UPPER SURFACE HAS A LARGE SMOOTH DENT 3" FORWARD OF TRAILING EDGE AND 50" FROM OUTBOARD EDGE AS MARKED. 0000493008 : CRAIL, ROGER L - 23-APR-2023 03:10 REPAIRED SLAT REF B767 SRM 51-70-10-2R. E.A. H-5750-T0374154 P1 WINGS - FLIGHT SURFASDR SWAA2023053130242Bracket · elongatedELONGATED HOLE SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING 2023-258140<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT LT WING IAW B737-700 SRM 52-10-02 ITEM 9.;[02] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE ATSDR YENA2023005020469Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF BOTTOM SKIN PANEL NO3 BTW GEAR RIB 5 AND RIB 5A ON LH WING (CPCP RELATED MPD TASK 575167-01); PERFORMED REPAIR ON UPPER SURFACE OF BOTTOM SKIN PANEL NO 3 BTW GEAR RIB 5 AND RIB 5A ON LH WING TOOL USED DIGITSDR DALA2023042603265Unknown · unknownER/A 608198-14AD ISSUED FOR DAMAGE TO THE RH WING SLAT TRACKS #1-10. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 608198-14AD SECTION II EVERY 850FH FOLLOWING THE ACCOMPLISHMENT OF SECTION I. ACCOMPLISH SECTION III WITHIN 8500FH FOLLOWING THE ACCOMPLISHMENT OSDR AALA202304250739Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #4 UPPER BOLT AT WS 3059 AND RIB 6. REPLACED BOLT PER AMM 27-84-63.SDR DALA2023042403169Unknown · unknownSHIP 6801 A. A. - A.D. DISBOND (2.200 IN X 1.100 IN) ON ISS 257 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC: 00050 ON ISS 257 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER REPAIR PER B757- SDR SWAA2023053129767Bracket · crackedCRACK SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING 2023-258133<[01] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING IAW B737-700 SRM 51-40-02;[02] REPLACED SUPPORT BRACKET LOCATED IFSS 193 IB LEADING EDGE AT RT WING IAW B737SDR DALA2023042603264Unknown · unknownERA 608151-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VISIT. FOLLOW ON ACTION IS REQUIRED. LH WING SLAT TRACKS 2, 4-10 ARE AFFECTED. ACCOMPLISH ERA 608151-14AD SECTION II EVERY 850 FH AFTER SECTION I.ERA 608151-14AD SECTION IIS TIME LIMITED TO 8500 FH. SDR SWAA2023053029181Skin · crackedCRACK SLAT 7 LOWER SKIN LOCATED SLAT STATION 322.71 AT RT WING 2023-282292<[01] P/N: NORTEC 500D; S/N: N500X12101V022233; CAL DUE: 30-AUG-23.;[02] REPAIRED SLAT 7 LOWER SKIN LOCATED SLAT STATION 322.71 AT RT WING IAW SRM B737-700 57-42-01-2R-8 REPAIR 8 ;FIGURESDR IPXA2023051293204Slat · damagedINSPECTION TYPE:3CL/H WING #5 SLAT I/B UPPER CORNER HAS KNIFE EDGE DAMAGED.REMOVED, FABRICATED AND REPLACED TRAILING EDGE AT THE L/H WING #5 SLAT IAW VTSAA EA 011-5740-01-A9954 I/R, UPS EO MD11-5750-86857-A DATED 05/12/23 (MINOR)SDR DALA2023042403166Unknown · unknownSHIP 188 ON WALK AROUND, FOUND RIGHT WING LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621KB MISSING. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE ACCESS DOOR AS PER B767-300 AMM 57-41. OK TO CONTINUE SVC. (5118165)SDR DALA2023042103131Unknown · unknownSHIP 1702 FOUND #11 SLAT LUBRICATION ACCESS PANEL MISSING. CORRECTIVE ACTION: REINSTALLED #11 SLAT LUBRICATION ACCESS PANEL PER B767-300 AMM 57-41. CDL AND PLACARD REMOVED. OK TO CONTINUE. (9896232)SDR VNAA202318040002Slat · gougedFOUND LH SLAT #1 TO HAVE GOUGE NEAR MIDDLE ON BOTTOM SIDE.SDR IPXA2023061209056Flap · damaged#15 LEADING EDGE FLAP DENT***SM40/LMX20*** ALL STEPS COMPLIED WITH IAW EO-87340-REQ1. REFERENCE T3F18E001ZAFL.SDR SWAA2023042028553Angle · crackedA -204 DOT 01; LH WING L/E ATTACH ANGLE CRACKED AT FASTENER HOLE; STA 500D; STR. 19L; 6' OUTBOARD OF FUSELAGE SKIN<[01] REMOVED L/H WING L/E ATTACH ANGLE STA 500D STR 19L;6 OUTBOARD OF FUSELAGE SKIN I/A/W SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED ALL FASTENERSDR DALA2023042003130Unknown · unknownERA 608052-14AD SECTION I ISSUED FOR CORROSION TO RH SLAT TRACKS. ACCOMPLISH SECTION II EVERY 850 FH UNTIL SECTION III. SECTION III REQUIRED PRIOR TO 8500FH FROM SECTION I ACCOMPLISHMENT. ASSOCIATED AA 5742-01028 ADDED FOR AC 8143 ASSOCIATED ER/A 00-608052 ADDSDR SWAA2023052327569Slat · crackedL/W NO-1 SLAT NOSE L/E SKIN CRACKED @ ACTUATOR RIB ATTACHED POINT OUB MKD DOT<[01] ACCOMPLISHED PART TRANSACTION.;[02] REMOVED AND REPLACED L/W #1 SLAT ASSY IN REFERENCE AMM 27-81-000-801 AND AMM 27-81-21-400-801.;[03] RII -- VERIFIED L/W #1 SLAT ASSY REPLACEMSDR AALA202304263943Support Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING LEADING EDGE SLAT #7 OUTBOARD AUXILIARY TRACK SUPPORT BRACKET LOCATED AT OUTBOARD FRONT SPAR STATION (OFSS) 564.5. REPLACED SUPPORT BRACKET PER SRM 51-10-02-OG AND DWG 112A2003#DL.SDR DALA2023041803074Unknown · unknownSHIP 672 A. A.- A.D. DISBOND ON EXTERNAL DOUBLER ON OSS 305, LOWER SURFACE LE SLAT 4 TRAILING EDGE WEDGE LH WING. CORRECTIVE ACTION: SUMMARY OF NRC00079: EXTERNAL DOUBLER ON OSS 305 , LOWER SURFACE LE SLAT 4 TRAILING EDGE WEDGE LH WING WAS REPAIRED PER B757-20SDR DALA2023041803072Unknown · unknownSHIP 672 A. A. - A.D. DISBOND (1.500 LENGHT X 1.200 WIDTH) ON ISS 272 LOWER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC00078: TRAILING EDGE WEDGE ON ISS 272 LOWER SURFACE SLAT 5 WAS REPAIRED PER B757-200 SRM. (2718765)SDR DALA2023041703030Unknown · unknownER/A 607970-14AD ISSUED FOR DAMAGE TO THE RH WING SLAT TRACKS #1-11. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISHED ER/A 607970-14AD REV O SECTION 1. (LP# 2719959)SDR DALA2023041703029Unknown · unknownER/A 607969-14AD ISSUED FOR DAMAGE TO THE LH WING SLAT TRACKS #1-11. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISHED ER/A 607969-14AD REV O SECTION 1. (LP# 2719850)SDR DALA2023050403482Slat · corroded(LOG 2718077) DURING INSPECTION FOUND RH WING #7 SLAT LOWER SURFACE AND UPPER SURFACE OF THE TE WEDGE HAS SEVERAL AREAS WITH EVIDENCE OF CORROSION. REMOVED AND REPLACED #7 SLAT IAW AMDS T/C: 2780-4522-06. ALL MAINTENANCE ACCOMPLISHED ON AMDS T/C: 2780-4522-06.SDR AALA202304177695Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #3 FORWARD BOLT AT WS 2508 AND RIB 5. REPLACED BOLT PER AMM 27-84-63.SDR SWAA2023053126632Skin · crackedCRACK LEADING EDGE SLAT 1 LOWER SURFACE NOSE SKIN AT ACTUATOR RIB SS 451.97 AT LT WING 2023-257784<[01] TOOL P/N: NORTEC 500D; S/N: N500X12101V022233; CAL DUE: 30-AUG-23.;[02] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00KH2JC;[03] CORRECTED ITEM 2: FAULT RESOLVEDSDR SWAA2023051126803Fitting · crackedCRACK SLAT 2 SKIN ACTUATOR FITTING AREA AT SLAT STATION 322.71 AT LT WING 2023-247593<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200053402; DUE DATE: 13-MAY-23;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE DATE SDR SWAA2023051126804Fitting · crackedCRACK SLAT 5 SKIN ACTUATOR FITTING AREA AT SLAT STATION 85.19 AT RT WING 2023-247594<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200053402; DUE DATE: 13-MAY-23;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE DATE 3SDR IPXA2023042592989Bracket · corrodedINSPECTION TYPE:3CWHILE WORKING NR-488740 NEED TO REMOVE L/H WING O/B FLAP I/B HINGE FOR REPLACEMENT.REPLACED CORRODED HINGE BRACKET ASSY ON THE L/H WING O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)SDR DALA2023041703028Unknown · unknownERA 607881-14AD SECTION I ISSUED FOR CORROSION TO RH SLAT TRACKS FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 607881-14AD REV O SECTION I FOR R/H SLAT TRACK CORROSION BLENDING. (TIME LIMITED REPAIR) RII STEP 3 WAS COMPLIED WITH ON LOG 2716878 AND N/R 22. (LP# 2SDR DALA2023041703027Unknown · unknownERA 607882-14AD SECTION I ISSUED FOR CORROSION TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED.ACCOMPLISHED ERA 607882-14AD REV O SECTION I FOR L/H SLAT TRACK CORROSION BLENDING. (TIME LIMITED REPAIR) RII STEP 3 WAS COMPLIED WITH ON LOG 2716782 AND N/R 20. (LP# 27SDR IXXA2023041102Rib · crackedCRACK AT FIXED LEADING LWS 549SDR DALA2023050503524Unknown · unknownERA607871-14AD SECTION I ISSUED FOR CORROSION AND WEAR TO L WING SLAT TRACKS 1-10. FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 60781-14AD REV O SECTION I, L/H SLAT TRACK CORROSION BLENDING (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED ON LOG 2714780 N/R 22SDR DALA2023050503522Unknown · unknownERA607872-14AD SECTION I ISSUED FOR CORROSION TO RH WING SLAT TRACKS. FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 607872-14AD REV O SECTION I, R/H SLAT TRACK CORROSION BLENDING (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED ON LOG 2714772 N/R 23. (LP# 27136SDR SWAA2023041925268Panel · elongatedL/H WING PANEL 521CB HAS ELONGATED FASTNER HOLE.<[01] REPAIRED L/H WING PANEL 521CB IAW SRM 51-70-04;[02] INSPECTION C/W.SDR EE4Y2023041017577Slat · damagedDURING THE STRUCTURAL INSPECTION, WAS FOUND THE SLAT #1 RH WITH AN EXISTING REPAIR. AS PER PREVIOUS OPERATOR RECORDS, THE REPAIR WAS INSTALLED AS A TEMPORARY REPAIR. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-002312 REV.: / AND MEMO FORM SDR DALA2023041102849Unknown · unknownAIRCRAFT 8127, AD/ERA REQUIRES L/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. SDR DALA2023041102848Unknown · unknownAIRCRAFT 8127, AD/ERA REQUIRES R/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17 AND ERA 607782 AND THE "SLAT CONTOUR CHECK" AS DESCRIBED SDR DALA2023040902735Unknown · unknownSHIP 3093 LEFT WING #2 SLAT INBOARD TRAILING EDGE DAMAGE. CORRECTIVE ACTION: REPAIRED PER A321 SRM 57-43-21. (4115914)SDR DALA2023041102793Unknown · unknownSHIP 1708 RH WING NO.8 SLAT UPPER SURFACE AT 33" FROM I/B SIDE FOUNG DENT. CORRECTIVE ACTION: RH WING NO.8 SLAT UPPER SURFACE REPAIRED AT 33" FROM I/B SIDE AS PER B767-300 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4. (2707660)SDR SWAA2023051823385Panel · crackedRT WING L/E PANEL 621CB FWD O/B CORNER IS CRACKED<OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).REMOVED INNER SURFACE DAMAGED PLIES AND CLEANED REPAIR AREA FABRICATED REPAIR PLIES FROM BMS 5-129 TY2 GR05 LOT#1521552-3; BMS 8-79 CL3 ST120 LOT#152013SDR DALA2023040502665Unknown · unknownSHIP 6701 UPON COMPLETION OF THE ULTRASONIC LOW FREQUENCY BOND TEST AT THE NO 2 LEADING EDGE SLAT TRAILING EDGE WEDGE FOUND 2 EA AREAS OF DISBOND AT THE UPPER OB SURFACE. CORRECTIVE ACTION: REPAIR NO.2 LE SLAT TE WEDGE #2 EACH DISBONDS UPPER OB SKIN IAW B757 SSDR DALA2023050503523Unknown · unknownERA 607663-14AD SECTION I ISSUED FOR CORROSION TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED. ERA 607663-14AD SECTION I COMPLETED, RII SLAT RIGGING ACCOMPLISHED ON LOG 2703468 AND N/R 30. (LP# 2702474)SDR IPXA2023042893022Slat · gougedINSPECTION TYPE:3CR/H #6 SLAT INNER SKIN IS GOUGED BETWEEN STA XOS=848.175 AND XOS=868.476 .REPAIRED GOUGED SKIN AT THE R/H #6 SLAT INNER SIDE BETWEEN STA XOS=848.175 AND XOS=868.476 IAW VTSAA EA 011-5710-01-A9923 IR AND UPS EO MD11-5750-86650-A DATED 04/24/23
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