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 FDEA201103100932Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION SPOTS ENTIRE LENGTH. REPAIRED NR 1 SLAT IAW SRM 51-70-10. MAJOR REPAIR .SDR SWAA111653Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED NR 2 SLAT PER EA.SDR SWAA111647Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT SKIN I/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.SDR USAA2011031091010Skin · crackedPHX - B2 - MAJOR REPAIR - RIGHT WING NR 6 SLAT OUTBOARD TRACK AREA - LOWER SURFACE IS CRACKED. REPAIRED NR 6 SLAT OUTBOARD TRACK AREA - LOWER SURFACE IAW B737 SRM 57-43-01 REPAIR 6.SDR UALA2011030901145Structure · damagedNR 4 LE SLAT AFT EDGE IS HITTING WING HOIST POINT. REMOVED, REPAIRED NR 4 SLAT AT SHOP 273. ACOMPLISHED INSTALLATION OF NR 4 SLAT. OPS CK'S AND RIG CK`S GOOD.SDR FDEA201103080905Skin · delaminatedDELAMINATION FOUND ON SLAT1 OTBD UPR T/E FROM OTBD END TO 250MM AND 40MM FROM T/E DIM 250MMX40MM, 15SQIN. REPAIRED IAW SRM 57-70-10CH REPAIR #4, 57-43-02 FIG 1 AND FIG 201REPAIR DOUBLER INSTALLED,SDR IPXA11565556Skin · crackedINSPECTION TYPE:C3 NR 1 SLAT COVE SKIN IS CRACKED AT THE INBD MAIN FLAP TRACK FITTING. R & R SKIN IAW SRM 51-40-02.SDR AALA20110316DWH07Skin · delaminatedDELAMINATION OF NUMBER 6 SLAT LOWER SKIN 3 INCHES INBOARD OF THE OUTBOARD EDGE. ACCOMPLISHED REPAIR PER EA COMP-57-01-5569.SDR FDEA201103040843Lug · crackedUPON REMOVAL OF RT WING OTBD HYD SYS NR 3 SLAT ACTUATOR, FOUND OTBD SLAT MECHANISM ASSY OTBD UPPER SUPPORT LUG CRACKED. OUTBOARD LUG BRACKET REMOVED AND REPLACED AS PER CMM 27-83-11 REVISION 69. FUNCTIONAL TEST OF THE SLAT CARRIED OUT AS PER AMM 27-82-02-4 RSDR AALA20110304TUL02Slat · corrodedCORROSION AROUND FASTENERS ON LEADING EDGE OF NUMBER 10 SLAT. INSTALLED STRAP DOUBLER PER EA 57-015594.SDR AALA20110316DWH05Wedge · dentedNUMEROUS DENTS ON ALL 12 WING LEADING EDGE SLAT WEDGES. ACCOMPLISHED REPAIR PER EA B767-57-015326.SDR SWAA111575Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT LOWER SURFACE CRACKED AT ACTUATOR. REPAIRED SLAT PER EA.SDR DALA1115229880Fitting · brokenRIGHT WING NR 4 SLAT OUTBOARD TRACK HAS BROKEN FITTING ON SLATSIDE. REMOVED AND REPLACED RT WING NR 4 SLAT PER WORKCARD 5740-9826M-RT CHECKS GOOD.SDR AALA20110302TUL01Rib · crackedRIGHT WING SLAT: HIGH FREQUENCY EDDY CURRENT SHOWS A CRACK INDICATION ON NUMBER 14 SLAT RIB. REPLACED NUMBER 14 RIB ON SLAT IAW ESO 80117.SDR IPXA11165519Skin · dentedINSPECTION TYPE:5YR, 10 DENTS ON LT WING NR 1 SLAT UPPER SURFACE. ACCOMPLISHED REPAIR ON LT WING NR 1 SLAT IAW EO A300-5750-41876-A.SDR SWAA111301Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING T/E NR 3 SLAT LOWER SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR SWAA111286Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT L/E LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.SDR DALA1118641819Wedge · chafedLT WING NR 5 SLAT WEDGE AREA T/E FOUND CHAFING. METAL HOT BOND REPAIR PERFORMED ON CHAFING AREA AS PER SRM 57-43-02 REPAIR I, FIG 201 AND SRM 51-70-10 REPAIR 4, FIG 201 AND 202.SDR USAA2011030991008Panel · crackedMCN - C1 - MAJOR REPAIR - CRACK ON LEFT WING NR 2 SLAT COVE PANEL AT WS 580. REPLACED LEFT WING NR 2 SLAT COVE PANEL AT WS 580 IAW B757 SRM 51-40-02.SDR DALA1113470667Skin · chafedRIGHT WING NR 7 SLAT TRAILING EDGE LWR SURFACE HAS HEAVY CHAF MARKS FROM INBD EDGE TOWARD CENTER OF SLAT. REPAIRED IAW SRM 57-43-02 FIG 1.SDR DALA1113739874Structure · damagedON PREFLIGHT EXTERIOR INSPECTION, FOUND AREA BETWEEN SLATS 3 AND 4 ON THE RIGHT WING BINDING/DAMAGED UNDER DIRECTION OF MC COMPLIED WITH REPAIR INSTRUCTION ERA 48992 6-14. AIRCRAFT OK FOR SERVICE.SDR FDEA201102220691Rib · crackedLT WING NR 1 SLAT, ADJACENT TO T/E, INBD RIB FOUND CRACKED. CRACKED RIB REMOVED AND REPLACED WITH A NEW RIB AS PER SRM 51-31-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR USAA2011030190939Skin · debondedMCN - C3 - MAJOR REPAIR - NR 4 SLAT DISBONDED AT TRAILING EDGE WEDGE UPPER SURFACE AT WS 616. REPAIRED NR 4 SLAT TRAILING EDGE WEDGE UPPER SURFACE AT WS 616 IAW B767 SRM 51-70-10 REPAIR 4.SDR DALA1117860199Wedge · damagedRT WING NR12 SLAT WEDGE AREA UPPER SURFACE FOUND DENT AND HOLE. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 2 FIG 203.SDR IPXA11564918Structure · chafedINSP TYPE:C2, NR 8 SLAT LWR T/E IS CHAFED 34-36" OTBD FROM INBD END. CHAFED, OUT-OF-LIMITS, REMOVED DAMAGED SKIN AND CORE, INSTALLED FABRICATED CORE AND DOUBLER IAW SRM 51-70-10-2R AND SRM 57-43-02-1A-1.SDR IPXA11564917Structure · chafedINSP TYPE:C2, NR 8 SLAT LWR T/E IS CHAFED 27-33", INBD FROM OTBD END CHAFED OUT-OF-LIMITS, REMOVED DAMAGED SKIN AND CORE, INSTALLED FABRICATED DOUBLER IAW SRM 51-70-10-2R AND SRM 57-43-02-0I-1.SDR FOTR2101903974Cover · crackedLT WING L/E NR 2 SLAT TRACK COVER CRACKED. (OTBD TRACK) STOP DRILLED CRACK ON NR 2 SLAT IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 .080" PO 9007282 DIM. 6.2" X 7.1" IAW SRM 57-50-3. INSTALLED DOUBLER IAW SRM 57-50-3, FIG 1 AND 51-30-2. FASI NR SDR FOTR2101903892Skin · chafedLWR T/E INTERIOR LIP OF NR 8 SLAT CHAFED ALONG LENGTH OF SLAT. BLENDED CHAFED AREA ORIG MAT .070 WITH .039 REMAINING AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND 57-50-1 FIG 2. FABRICATED DOUBLER FROM 2024T3 .080 DIM. 6" X 4" PO 90010831 IAW SRM 57-50-3SDR UALA2011022100873Skin · dentedNR 4 SLAT UPPER SURFACE HAS NUMEROUS DENTS. MAJOR REPAIR ACCOMPLISHED: 15 EA DENTS A OVER Y RATIO WITHIN LIMITS OF SRM. NO CRACKS NOTED. NO ACTION REQUIRED. OK TO ARCHIVE. NR 4 SLAT WEDGE LWR SURFACE DOUBLER DISBONDED - INBD END. REPAIRED NR 4 SLAT T/E WEDGSDR SWAA111294Wedge · delaminatedDURING SCHEDULED MV3 CHECK, FOUND LT WING NR 3 SLAT L/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR 2011FA0000130Flap Track · corrodedLEFT HAND FLAP TRACKS HAD EXFOLIATION CORROSION AT THE UPPER END OF THE TRACK.SDR SWAA111109Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT I/B UPPER EDGE SURFACE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR SWAA111108Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT I/B UPPER EDGE SURFACE DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR SWAA111103Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED NR 2 SLAT PER SRM.SDR SWAA111094Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT O/B EDGE UPPER SURFACED DELAMINATED. REPAIRED NR 3 SLAT PER SRM.SDR SWAA111067Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR FDEA201102180781Spar · corrodedNR 5 SLAT FRONT SPAR HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-43-02. CUT OUT DAMAGED AREAS IAW SRM 51-70-11. FABRICATED REPAIR PARTS IAW SRM 51-70-11. INSTALLED REPAIR PARTS IAW SRM 51-70-11.SDR IPXA11564921Wedge · chafedINSPECTION TYPE:2C14, NR 3 SLAT LOWER SURFACE OF THE T/E WEDGE HAS "OUT OF LIMITS" CHAFING DAMAGE 21" TO 34" INBD OF THE OTBD END. REMOVED DAMAGE AND REPAIRED WITH HOT BOND IAW SRM 51-70-10.SDR SWAA111166Skin · crackedNR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER EA.SDR 2011FA0000116Structure · crackedPERFORMED INSP IAW SAFETY COMUNIQUE NR 313. FOUND RT FLAP L/E CRACKED (ABOUT 1.5 INCH LONG) IN THE VICINITY OF THE "FLAP ACTUATOR BRACKET". FURTHER FOUND NOSE RIB CRACKED AS WELL. REMOVED FLAP FOR REPAIRS.SDR FDEA201102170600Fillet · crackedRT WING L/E CRUISE PERFORMANCE FILLET NEAR UPPER JOINT FOUND CRACKED. FILLET DOUBLER REPAIRED AS PER SRM 57-40-71 REPAIR 1 FIGURE 201 REVISION 45. OPERATIONAL TEST OF THE SLAT CARRIED OUT AS PER AMM 27-80-00-860-801 REVISION 69.0 FOUND SATISFACTORY. REPAISDR FDEA201102170599Rib · crackedLT WING L/E NR 1 SLAT INBD RIB AREA FOUND CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201102170598Rib · crackedRT WING L/E NR 1 SLAT INBD RIB AREA FOUND CRACKED. REPAIRED AS PER DRAWING ARB7128 REVISION L AND SRM 51-31-01 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 45.SDR SWAA111055Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA111028Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 4 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 4 SLAT PER EA.SDR SWAA111018Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING NR 4 SLAT ON I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR NOCA01111Roller · lack of lubeFLAP/SLAT ELEC STATUS MESSAGE. RETRACTED SLATS AT 260 KNOTS TRANSIT FOR 20 SECONDS. ACFT DIVERTED. FLAP/SLAT OVERSPEED PICKED UP BY AFIRS. ACCOMPLISHED PHASE 1 AND PHASE 2 INSPECTION OF L/E SLAT LEFT AND RIGHT PER MM 05-51-08, NO DISCREPANCIES FOUND. INSPSDR DALA1113625523Skin · puncturedPUNCTURE ON SLAT 5, T/E WEDGE LOWER SURFACE, 30 INCHES FROM INBD END 093-03. REPAIRED DISCREPANT AREAS ON NR 5 SLAT T/E WEDGE, UPPER AND LOWER SURFACE IAW SRM 51-70-10, PG 212, PARA 7, PG 214, PARA 8, SRM 57-43-02 P11, ITEM 6, SRM 51-70-10, P237-244, PARA 14 SDR QXEA2011021700165Structure · chafedC6 CHECK - RT SLAT 2 AND 3 HAVE EVIDENCE OF CHAFING AT WS 178, 178+70 AND 178+129, 178+138 AND WS 294. BLENDED AREAS IAW SRM 51-12-00-001-001-A01. PERFORMED FPI IAW SRM NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11SDR SWAA111422Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER AFT T/E SKIN I/B OF AUX TRACK CRACKED. REPAIRED SKIN PER SRM.
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