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 SWAA110431Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA110430Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR DALA1105889886Structure · damagedNR3 RT WING L/E SLAT DAMAGE. REPLACED NR 3 RT WING SLAT IAW AMM 27-80-01.SDR DALA1105879886Structure · damagedNR 2 RT WING L/E SLAT DAMAGE. REPLACED NR 2 RT SLAT IAW 27-80-01-401 SLAT, NR 2 RT, OFF 09-2780-9-0012 00007, ON 09-2780-9-0012 00027. CORRECTED.SDR DXTA2011012504433Slat · damagedON FLAP-SLAT RETRACTION AFTER TAKEOFF, THE YELLOW NIPS LIGHT REMAINED ON. IWA THE CHECKLIST, RE-EXTENDED SLATS-FLAPS, EXTENDED NORMALLY AND NIPS LIGHT WENT OUT. RETRACTED FLAPS-SLATS AND NIPS LIGHT REMAINED ON. UPON INVESTIGATION, THE RT SLAT HAS A WRINKLE INSDR IPXA1664496Rib · crackedINSPECTION TYPE:C, RT WING - NR 10 SLAT INBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.063" APPROX. RIB AT OSS 723.9 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & RSDR IPXA1664495Rib · crackedINSPECTION TYPE:C, RT WING- NR10 SLAT OTBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.006" APPROX. RIB AT OSS792.94 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & REPSDR IPXA1664497Rib · crackedINSPECTION TYPE:C, RT WING L/E OSS 648.595, NR 9 SLAT OTBD ACTUATOR OTBD SUPPORT RIB FWD FLANGE LWR AREA FOUND CRACK. RT WING L/E OSS648.595 NR 9 SLAT OTBD ACTUATOR OTBD SUPT RIB FLANGE REPAIRED IAW HX RS R57-00-36911, REV A & EO B767-5710-41209-A, ORG MAT'LSDR AALA20110119TUL12Joint · wornLEFT WING KNUCKLE JOINT WORN OUTBOARD END OF NUMBER 4 SLAT. REPLACED WORN OUTBOARD KNUCKLE JOINT RIB NUMBER 4 LEFT SLAT PER ESO 80117.SDR AALA20110119TUL10Slat · crackedRIGHT WING: PREVIOUS BLEND OUT ON NUMBER 7 SLAT 33 INCHES FROM OUTBOARD END AND 10 INCHES FROM TRAILING EDGE WEDGE. INSTALLED REPAIRED PER AARD 57-43-00-01.SDR AALA20110119TUL09Slat · crackedPREVIOUS BLEND OUT ON NUMBER 7 SLAT 33 INCHES FROM OUTBOARD END AND 6.5 INCHES FROM THE TRAILING EDGE WEDGE. INSTALLED REPAIR PER AARD 57-43-00-01.SDR AALA20110119TUL08Skin · crackedCRACK IN SKIN AROUND FASTENER ON TOP OF SLAT EVEN WITH SPAR 46 INCHES FROM OUTBOARD END. REPAIRED CRACK IN SKIN PER AARD 57-43-00-01.SDR IPXA1164806Skin · gougedINSPECTION TYPE:10YR, RT WING MID SLAT INBD EDGE LWR SURFACE HAS A GOUGE ACCOMPLISHED REPAIR ON RT WING NR2 SLAT INBD LWR EDGE IAW EO A300-5750-41493-A.SDR DALA1107421820Skin · detachedRT WING NR9 SLAT WEDGE UPPER SURFACE INBD EDGE SKIN DETACHED METAL. HOT BOND REPAIR PERFORMED IAW SRM 57-43-52. REPAIR 1, FIG 201 AND SRM 51-70-10 REPAIR 4, FIG 202.SDR FDEA201101170204Skin · gougedLT WING NR 2 SLAT, INBD END LOWER SURFACE HAS GOUGES. REMOVED AND REPLACED LEFT WING NR 2 SLAT IAW AMM 27-80-12-04. OPS CHECK GOOD.SDR IPXA1664493Skin · crackedINSP TYPE:C RT WING - NR 10 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 792.5 ORG MAT'L 7075T6-0063" CRACK LENGTH 0.154" DAMAGE CUTOUT 8.875" X 7.125" THIS CLASSIFIED AS MAJOR REPAIR WITH 7075T6-SDR IPXA1664492Skin · crackedINSP TYPE:C RT WING - NR10 SLAT INBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIR IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 723.9 ORG MAT'L 7075T6-0063" CRACKED LENGTH 0.503" DAMAGE CUTOUT 8.875"X 7.25" THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 707SDR IPXA1664491Skin · crackedINSPECTION TYPE:C, RT WING NR9 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. RT WING NR9 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.5955" DAMAGE CUTOUT IS 8.875" X 7.375". THISSDR IPXA1664490Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 49 AT OSS 641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.554" DAMAGE CUTOUT 8.875"X 7.375" THIS CLASDR FDEA201101170203Skin · gougedRT WING FIXED L/E INBD OF THE PYLON AND OTBD OF THE NR 3 SLAT TRACK THERE ARE APPROX 11 GOUGES FROM BUTTON HEADS INSTALLED ON THE BOTTOM SKIN OF SLAT RIB 8. R & R SLAT IAW AMM 27-80-11-04. SLAT TEST GOOD IAW AMM 27-80-11-04. REMOVED SKIN SECTION IAW SRM 51-SDR AALA20110117TUL05Skin · crackedRIGHT WING HAS CRACK IN THE NUMBER 9 SLAT COVE SKIN AT THE OUTBOARD DRIVE TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER ON SKIN PER AARD 57-43-00-4.SDR AALA20110117TUL04Slat · corrodedRIGHT WING CORROSION ON THE NUMBER 9 SLAT 43 INCHES FROM THE INBOARD END. REMOVED DAMAGE AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20110117TUL03Slat · corrodedRIGHT WING CORROSION ON THE NUMBER 9 SLAT 29 INCHES FROM THE OUTBOARD END. CUT OUT AREA OF CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR USAA2011020390506Slat · debondedMCN - C1 - MAJOR REPAIR - DISBOND ON NR 5 SLAT OUTBOARD UPPER TRAILING EDGE BETWEEN OSS528.75 TO OSS531.75. REPAIRED NR 5 SLAT OUTBOARD UPPER TRAILING EDGE BETWEEN OSS528.75 TO OSS531.75 IAW B767 SRM 51-70-10 REPAIR 4.SDR USAA2011020390505Slat · debondedMCN - C1 - MAJOR REPAIR - DISBOND ON NR 4 SLAT OUTBOARD UPPER TRAILING EDGE BETWEEN OSS678.74 TO OSS682.74. REPAIRED NR 4 SLAT OUTBOARD UPPER TRAILING EDGE BETWEEN OSS678.74 TO OSS682.74 IAW B767 SRM 51-70-10 REPAIR 4.SDR UALA2011011700279Skin · dentedNR 6 L/E SLAT T/E COMPOSITE WEDGE HAS DENT OUT OF LIMITS. DENT IS 2.5 BY 2 INCH MAX ALLOWABLE IAW NOTE K IS 2 INCH, AND IS DELAMINATED FROM UPPER SKIN AREA 2.5 BY 2 INCH. REF UA-EVA-80482 AND MM 57-53-93-603 TIME LIMITED REPAIR IAW PARA 11. INJECTION REPAIRSDR UIEA2011011400004Skin · damagedDURING A-CHECK BEING PERFORMED-UPPER L/E PANEL - EXTERNAL SKIN WITH DELAMINATION/DAMAGE (REF FIG 1). (PERMANENT REPAIR PERFORMED IAW THE SRM 51-40-09, FIG 18 (SHEETS 1-5) AND PREPREG 250A F CURE IAW SRM 51-40-12. THE REPAIR ACCOMPLISHED IN PART 1 OF THIS EO SDR SWAA110328Slat · wornDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT CAN LOWER SURFACE WORN. REMOVED AND REPLACED CAN PER MM.SDR FDEA201101130171Skin · dentedNR 1 SLAT UPPER SURFACE, WS 711.5, HAS A TEMP REPAIR OR A DENT. (CURRENT SRM REQUIRES PERM. REPAIR AT C-CHECK) REPAIRED NR1 L/E SLAT IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSION IS 3" DIAMETER. SLAT ASSY PN IS: 114N4002-133, SN: A1-0143. REPAIR WASDR FDEA201101130169Skin · noneNR3 L/E SLAT UPPER SURFACE WS 509.5 HAS A TEMP REPAIR. (CURRENT SRM REQUIRES PERM REPAIR AT C-CHECK) REPAIRED NR3 SLAT ASSY IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSIONS ARE 3" DIAMETER. THE SLAT PN IS: 114N4004-165A, SN: A1-0122. THE REPAIR WAS PSDR SWAA110330Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR SWAA110329Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 3 SLAT I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.SDR SWAA110221Skin · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 SLAT SKIN LOWER SURFACED CRACKED. REPAIRED SKIN PER SRM.SDR DALA1106950198Skin · delaminatedLT WING NR 5 SLAT WEDGE AREA LWR SURFACE OTBD EDGE FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 57-43-02, REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.SDR DALA1106850198Wedge · deformedLT WING NR 5 SLAT WEDGE AREA LWR SURFACE INBD EDGE FOUND DEFORMED. METAL HOT BOND REPAIR PREFORMED IAW SRM 57-43-02. REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.SDR DALA1102320124Wedge · delaminatedLT WING L/E NR2 SLAT WEDGE UPPER SURFACE FOUND DELAMINATED; CA: LT WING L/E NR2 SLAT WEDGE UPPER SURFACE, REPAIR FILLER AND DOUBLER FABRICATED IAW 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW DELTA PS 900-5-1, NR 4.SDR USAA2011020190480Skin · delaminatedCLT - Q3 - MAJOR REPAIR - DELAMINATION ON UPPER SURFACE OF NR 5 TRAILING EDGE SLAT 15.5 INCHES INBOARD FROM OUTBOARD EDGE & 5 INCHES FORWARD OF TRAILING EDGE. REPAIRED NR 5 SLAT TRAILING EDGE IAW B737 SRM 51-70-10 REPAIR 4.SDR USAA2011020190479Skin · crackedCLT - Q3 - MAJOR REPAIR - CRACKS ON NR 1 SLAT LOWER TRAILING EDGE SURFACE 43 INCHES OUTBOARD OF INBOARD EDGE. REPAIRED NR 1 SLAT LOWER TRAILING EDGE SURFACE 43 INCHES OUTBOARD OF INBOARD EDGE IAW B737 SRM 57-43-01 REPAIR 6.SDR IPXA11M64394Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPARTMENT, BEADED DOUBLER INBD OF SLAT TRACK NR 17, FOUND WITH SUSPECTED CRACK AT 2 LOCATIONS XOS 698.5-703. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG. 203.SDR ASAA1148837Slat · delaminatedNR 2 SLAT UPPER OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED SLAT IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1148836Slat · delaminatedNR 2 SLAT UPPER INBOARD TRAILING EDGE DELAMINATED ON PREVIOUS REPAIR. REPAIRED SLAT IAW B737 400 SRM 51 70 10 REPAIR 4SDR FDEA201101070073Skin · corrodedNR 3 SLAT LOWER SURFACE AT SEAM BETWEEN SLAT AND AERODYNAMIC SEAL HAS CORROSION. REMOVED CORROSION ON NR 3 SLAT LOWER SURFACE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L-139" X 1" X D=.063 ORIG MATERIAL .063 AFTER REWSDR DALA1109400178Wedge · delaminatedLT WING NR 2 SLAT WEDGE AREA UPR SURFACE (30IN FROM OTBD EDGE) FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AT DELAMINATION AREA IAW SRM 57-43-02, REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIG 201.SDR DALA1108920178Wedge · delaminatedLT WING NR 1 SLAT WEDGE AREA UPPER SURFACE (1 IN FROM OTBD EDGE) FOUND DELAMINATED METAL. HOT BOND REPAIR PERFORMED IAW SRM 57-43-02, REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIG 201.SDR FDEA201101070074Angle · corrodedNR 10 SLAT COVE ANGLE CORRODED. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. ORIG MATERIAL .063 AFTER REWORK .000 MATERIAL LOSS .063 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L= 131" X W=2" X D=.063. R & R COVE ANGLE IAW SRM 51-40-02. SDR UALA2011010600081Fitting · crackedCREW REPORTED EICAS STATUS MESSAGE FLAP-SLAT ELEC GROUND SEE`S VISIBLE HYD LEAK. REPLACED CRACKED FITTING ON THE FLAP-SLAT SHUTOFF VALVE MODULE. OPS NORMAL AND NO LEAKS NOTED.SDR FDEA201101050012Slat Track · crackedRT WING SLAT TRACK NR8 CUT OUT OTBD AREA CRACKED. REPAIRED AS PER E.A. 1-5740-143499. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR SWAA110086Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT INBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR QXEA2011011200021Skin · chafedC6 CHECK - LT NR 2 SLAT HAS A CHAFE ON THE INBD UPPER T/E. BLENDED CHAFE IAW SRM 51-21-06-00. ORIGINAL THICKNESS .100", REMAINING THICKNESS IS .098". CHAFE IS WITHIN LIMITS OF SRM 57-42-01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-00, 51-25-06-00 AND 5SDR IPXA11M64069Doubler · crackedINSPECTION TYPE:C3, LT WING FIXED L/E COMPARTMENT INBD OF SLAT TRACK NR 4 BEADED DOUBLER FOUND WITH CRACKS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.
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