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 SWAA2022011948202Skin · crackedRT WING LOWER SURFACE L/E; #6 SLAT NOSE SKIN AT ACTUATOR RIBS. CRACK AROUND FASTENER SKIN. CRACK CONFIRMED IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT 2ND FWD O/B FASTENER. CRACK LENGTH :0.157. REMOVED INBD CENTER, OTBD COVE SKIN & PARTIAL FLEX SSDR AALA202112217505Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #11 ATTACHMENT BOLT BETWEEN WS 12277 AND WS 12870 BETWEEN RIB 23 AND RIB 24. REPLACED BOLT PER AMM 27-84-67-000-001.SDR SWAA2022010546694Skin · crackedCRACK LOWER SURFACE SLAT 3 LEADING EDGE NOSE SKIN AT ACTUATOR LT WING ; 2021-536388 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138003; DUE DATE: 05-MAR-22; [02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 210138203; DUE DATE:SDR SWAA2022010546691Skin · crackedCRACK LOWER SURFACE SLAT 6 LEADING EDGE NOSE SKIN AT ACTUATOR RT WING. PERFORMED HAND LAY OUT ON LOWER SURFACE SLAT 6 LEADING EDGE NOSE SKIN AT ACTUATOR RT WING IAW SRM 57-42-01-2R-8 REPAIR 8 FIGURE 202 SHEET 3 THIS REPAIR IS APPLICABLE AS PER APB 57-42-01 PASDR SWAA2021122746805Panel · pulledR/W L/E PANEL 621LB HAS SEVERAL PULLED FASTENER HOLES. DAMAGE AT SEVERAL FASTENER HOLES EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A(5). DAMAGE IS PER SRM 51-70-05-2R-6 AS DIRECTED BY SRM 57-41-01-2R-1. REMOVED 2 EACH BACKPLATES TO FACSDR FDEA202111172882Skin · delaminatedRH WING INBOARD MAIN FLAP LEADING EDGE WITH DELAMINATION. RH WING INBOARD MAIN FLAP LEADING EDGE WAS REPAIRED I.A.W. S.R.M. 57-53-01-2R PAG. 5 FIG. 201 TABLE 1 AND 51-70-03-0G PAG. 36 FIG. 5 REV. 81 AUG 15/2021SDR AALA202111167667Slat · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING SLAT 2 TRACK 6 SPHERICAL BEARING ATTACHMENT FITTING BUSHING CRACKED. REPLACED SLAT 2 PER JOB CARD 26C62057009.SDR R61A2021120100962Skin · crackedR/H WING #3 SLAT FOUND CRACKED AT O/B SLAT TO TRACK FITTING. REMOVED AND REPLACED SLAT IAW 27-81-07-400-801-ASDR SWAA2021121343272Skin · crackedCRACK AROUND THE FASTENER AT NO.8 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. EDDY CURRENT INSPECTED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. EXTENT OF CRACK NOTED APPROXIMATELY .100 INCHES IN LENGTH. INSTALLED REPAIR PARTS IAW SDR SWAA2021121343273Skin · crackedCRACK AROUND THE FASTENER AT NO.5 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. EDDY CURRENT INSPECTED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. EXTENT OF CRACK NOTED APPROX .100 INCHES. REMOVED DAMAGED PART IAW SRM 57-42-01-2R-8, STSDR DALA2021111506991None · noneSHIP 689 CORROSION ON LEADING EDGE AREA AT SLAT # 5. CORRECTIVE ACTION: SUMMARY OF NRC 00326: LEADING EDGE SLAT # 5 WAS REPLACED PER AMDS. (2015016)SDR AALA202111238249Slat · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT WING #7 INBOARD SLAT SKIN AT WING STATION ISS 186 7 INCHES FORWARD OF THE AFT EDGE. REPAIRED SLAT SKIN PER SRM 57-43-01-2R PROCEDURE 6 REPAIR 6 AND EA 328949.SDR IPXA2021111976138Angle · crackedINSPECTION TYPE:A300RT WING KRUGER FLAP SUPPORT WEB HAS A CRACKREMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2021111976137Angle · crackedINSPECTION TYPE:A300LT WING KRUGER FLAP SUPPORT WEB HAS A CRACKREMOVED AND REPLACED IAW SRM 51-40-21SDR 2021F00399None · dentedREPAIR OF RH WING LEADING EDGE DENTS. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ32339M1 DATED: 11/9/2021, WING (RIGHT) LEADING EDGE DAMAGE/GOUGE.SDR JR2R20211110148Skin · dentedLH #1 SLAT LE SKIN HAS BIRD STRIKESDR DALA2021110806838Flap · debondedSHIP 3256 DEBONDED OB FLAP AFT EDGE LOWER SKIN ON LH WING. CORRECTIVE ACTION: R/R OB FLAP ON L/H WING PER DELTA WORK CARD 2750-1020-LT. OK FOR SERVICE. (2009198)SDR DALA2021110806878None · noneSHIP 1811. FOUND OUT L/H WING NO.1 SLAT UPR SURFACE DELAMINATION , 15" TO O/B EDGE,2" TO AFT EDGE. CORRECTIIVE ACTION: L/H WING NO.1 SLAT UPR SURFACE T/E REPAIRED AT 15" TO O/B EDGE,2 " TO AFT EDGE AS PER B767-400 SRM 57-43 & SRM 51-70 & SRM 51-70. (2007621)SDR SWAA2022011040649Skin · crackedLT WING #1 SLAT HAS LWR SKIN CRACKED AT 3 EACH FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97. 3-23 ; / [01] REMOVED 3EA. FASTENERS FOR NDT. INSPECTION IAW. B-737-700 SRM. 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] PERFORMED HFEC INSP. ON SKISDR SWAA2022011040652Skin · cracked#7 SLAT THE LOWER SURFACE OF THE WING LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR RIBS APPEARS TO BE CRACKED ON THE SKIN AROUND 3RD OB FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71. ; DOT 8-32 / [01] REMOVED ACCESS PANEL 624 DR. AND 1EA. FASSDR AALA202111057337Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 LOWER ATTACHMENT BOLT BETWEEN WS 700 AND WS 1406 BETWEEN RIB 2 AND RIB 3. REPLACED BOLT PER AMM 27-84-63-400-002-A.SDR AALA202111053548Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 MIDDLE AFT ATTACHMENT BOLT BETWEEN WS 700 AND WS 1406 BETWEEN RIB 2 AND RIB 3. REPLACED BOLT PER AMM 27-84-63-400-002-A.SDR ASMF2021120800324Skin · damagedTHREE DENTS ON SLAT NUMBER 1 SKIN. DURING TRANSIT CHECK, IT WAS DETECTED THREE DENTS ON SLAT NUMBER 1 SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 3 DENTS ON SLAT 1 WITH MULTIPLE DAMAGES ON LE FRONTAL AREA LOCALIZED BETWEEN STA 1151.75 AND STA 1SDR DALA2021111006925None · noneSHIP 3225 SLAT NUMBER 5 REMOVED FROM AIRCRAFT. CORRECTIVE ACTION: NEW SLAT INSTALLED AND RIGGED PER A320 AMM 27-84-67. OK FOR SERVICE. (2003115)SDR SWAA2021112938659Panel · crackedR/W LOWER LEADING EDGE; PANEL 621FB; CRACKED AND DELAMINATED ON CORNER ; / [01] PREPARED DAMAGED AREA; REPAIR AREA IS FULLY DRY NO WATER NOTE AT ACCESS PANEL 621FB. REF B737-700 SRM 51-70-04-2R-13 PARAGRAPH 4 B AND C.; [02] VERIFIED STEP 1; [03] OK TO APPLY RESDR SWAA2021122138636Slat · crackedRIGHT WING MOVEABLE L/E SLAT NR 5 NOSE SKIN, ACTUATOR RIB APPEAR SMALL CRACK AND FASTENERS HEADS PULLED. FABRICATED AND LOCATED NEW FASTENER HOLES AT REPAIR DOUBLER IAW SRM 57-42-01-2R-8. CUT OUT DAMAGED AREA IAW SRM 57-42-01-2R-8. PERFORMED HFEC AT CUT OSDR SWAA2021110238256None · cracked#1 SLAT SKIN CRACKED AT LOWER SURFACE PROPAGATING FROM FWD AND AFT SIDES OF 1 FASTENER LOCATED NEAR ACTUATOR ATTACHMENT; CRACK MEASURES .500 FWD AND .250 AFT OF FASTENER ; / [01] C/W TASK CARD; [02] C/W WITH EA 21-157-03206 ON NUMBER 1 SLAT.SDR SWAA2021110238255None · cracked#1 SLAT SKIN CRACKED AT LOWER SURFACE PROPAGATING FROM FWD AND AFT SIDES OF 1 FASTENER LOCATED NEAR ACTUATOR ATTACHMENT; CRACK MEASURES .250 FWD AND .500 AFT OF FASTENER ; #1 SLAT SKIN CRACKED AT LOWER SRFACE PROPAGATING FROM FWD AND AFT SIDES OF 1 FASTENER LOSDR SWAA2021111738462Panel · delaminatedRIGHT WING L/E PANEL 621JB IS DELAMINATED AT LEADING EDGE. / REPAIRED RIGHT WING L/E PANEL 621JB EROSION STRIP AT LEADING EDGE IAW B737 SRM 57-41-01-2R-6SDR AALA202110280537Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #12 LOWER FORWARD ATTACHMENT BOLT BETWEEN WS1346 AND WS14459, BETWEEN RIB 25 TO RIB 27. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR AALA202110284347Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #12 UPPER FORWARD ATTACHMENT BOLT BETWEEN WS13464 AND WS14459, BETWEEN RIB 25 TO RIB 27. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR SWAA2021102532174Slat · delaminatedPAINT PEELING AND/OR DELAMINATION ON UPPER RIGHT WING OUTBOARD OF SLATS AND NEAR FORWARD LEADING EDGE OF WING. TOUCHED UP PAINT ON UPPER RIGHT WING OUTBOARD OF SLATS AND NEAR FORWARD LEADING EDGE OF WING IAW AMM 51-21-99-300-801.SDR SWAA2021112331826None · crackedCRACK LOWER SURFACE SLAT 5 AT RT WING ; 2021-486529 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138503; CAL DUE DATE: 05-MAR-22; [02] CALIPER P/N 500-752-20 S/N B21038259 DUE DATE 10 AUG 22; [03] RADIUS GAUG P/N 2204A57 S/N AE-408657 DUSDR SWAA2021112331092None · crackedCRACK LOWER SURFACE SLAT 1 AROUND OF FASTENER; ACTUATOR AREA LT WING ; 2021-486451 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 190023010 AND DUE DATE: 01-DEC-21.; [02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 190023010 AND DUE DATE: 01-DEC-21.; [03SDR AALA202110292366Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #12 UPPER AFT ATTACHMENT BOLT BETWEEN WS13464 AND WS14459, BETWEEN RIB 25 TO RIB 27. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR IPXA2021102875404Skin · corrodedINSPECTION TYPE:4CRT WING UPPER FORWARD SKIN HAS CORROSION BETWEEN STA.XORS 212 AND XORS 216 STRINGER 16.REPAIRED CORRODED RT WING UPPER SKIN IAW SRM 57-00-01 FIG. 1 AND 51-30-00 (MINOR).SDR AALA202110283974Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 LOWER ATTACHMENT BOLT BETWEEN WS5512 AND WS6699, BETWEEN RIB 10 TO RIB 12. REPLACED BOLT PER AMM 27-84-64-400-002-A.SDR DALA2021101906454None · noneSHIP 6823 DISBOND (1.600 IN. X 0.900 IN.) ON UPPER SURFACE OSS 818, AT LE SLAT 10 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00015: DISBOND ON UPPER SURFACE OSS 818, AT LE SLAT 10 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM. (1987935)SDR YENA2021102000687Slat Track · crackedDURING HEAVY MAINTENANCE, CRACK: LH WING L.E. SLAT TRACK #5 CUTOUT ; REF. TOMX NR 00206: R & R FIXED LEADING EDGE BTW RIB12 TO RIB17 @ LH WING IAW SRM 51-41-02 AND SRM 51-43-02.SDR DALA2021101506371None · noneSHIP 5642 LH WING #4 SLAT INBD UPPER TRAILING EDGE HAS EXPOSED COMPOSITE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON #4 SLAT T/E WEDGE UPPER SURFACE IAW B757-200 SRM. (1982230)SDR SWAA2021101428537Angle · crackedSUPPLEMENTAL INFORMATION: CRACK SLAT 1 ANGLE LOCATED AT THE END OF INBOARD SLAT TRACK AT LT WING 2021-460671 / REPLACED ANGLE LOC SLAT 1 AT END OF INBOARD SLAT TRACK LT WING I.A.W CMM B737-700 57-43-01 REPLACED ANGLE LOC SLAT 1 AT END OF INBOARD SLAT TRACK LT SDR SWAA2021111528655None · crackedCRACK EXTERNAL SKIN LOCATED SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING ; 2021-461484 / [01] REMOVED ACCESS PANEL 623DB AND FLEX SKIN LOC SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND SDR SWAA2021111528656None · crackedCRACK EXTERNAL SKIN LOCATED SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING ; 2021-461488 / [01] REMOVED ACCESS PANEL 522DB AND FLEX SKIN LOC SLAT 4 AT LEVEL SLAT STATION 85.19 LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND DAMAGSDR DALA2021101106221None · noneSHIP 194 LH WING #4 SLAT. CRACKED NOSE SKIN. CORRECTIVE ACTION: CRACKED NOSE SKIN REPAIRED AND ACCOMPLISHED AS PER PRI 594252-14. (1945826)SDR DALA2021101106224None · noneSHIP 194 DAMAGE WAS NOTED ON THE #4 SLAT SKIN. ER/A 594252-14 SECTION I REPAIR WAS ACCOMPLISHED, FOLLOW ON ACTION IS REQUIRED FOR SECTION II. CORRECTIVE ACTION: REF ER/A 594252-14 (1975413)SDR IPXA2021102375234None · crackedINSPECTION TYPE:CRH WING SLAT #9 OB TRACK PANEL COVER IS CRACKEDREMOVED AND INSTALLED REPLACEMENT COVER PER SRM 51-40-02-0GSDR IPXA2021102375233None · crackedINSPECTION TYPE:CRH WING SLAT #9 I/B TRACK PANEL COVER IS CRACKEDREMOVED AND INSTALLED REPLACEMENT COVER PER SRM 51-40-02-0GSDR DALA2021100606132None · noneSHIP 181 FOUND GAUGE ON R/H WING NO.8 SLAT AFT INNER SURFACE AT O/B AREA. CORRECTIVE ACTION: R/H WING NO.8 SLAT AFT INNER SURFACE AT O/B AREA REPAIRED AS PER B767-400 SRM 57-43-02-2R-1 AND SRM 51-70-10. (1973607)SDR FDEA202110052477Slat · damagedRH WING #11 SLAT HAS WHAT APPEARS TO BE A BULLET HOLE IN TOP SURFACE REPAIRED R/H WING #11 SLAT REF 767 SRM 57-43-02-2R AND 51-70-10.SDR DALA2021100706150None · noneSHIP 6807 A.A. DISBOND (1.700 IN X 1.300 IN) AT UPPER SURFACE OSS 827, LE SLAT 10 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 185: UPPER SURFACE OSS 827, LE SLAT 10 TRAILING EDGE WEDGE WAS REPAIRED PER B 757-200 SRM. (1971714)
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