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 FDEA202010112495Bracket · crackedLT NR 4 SLAT TRACK LEADING EDGE COVER PLATE HAS A CRACKED LT BRACKET. REMOVED AND REPLACED CRACKED LT BRACKET ON LT NR 4 SLAT TRACK LEADING EDGE COVER PLATE, REF SRM 51-31-01 VOL II.SDR FDEA202010092456Wedge · delaminatedLT WING LEADING EDGE, NR 2 SLATS WEDGES DELAMINATED AT INBOARD SIDE UPPER SURFACE. REPAIRED LT WING LEADING EDGE, NR 2 SLATS WEDGE DELAMINAITED AT INBOARD UPPER SURFACE, IAW B767 SRM B767 SRM 57-43-02, 51-70-10-2R AND B767 AMM 51-21-01.SDR DALA2020101203343Skin · dentedLT WING NR 4 SLAT DENTED ON INBOARD END. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SLAT NR 4 LT WING, AS PER A330 SRM.SDR SWIA202053953Slat Track · wornLT SLAT TRACK 2-1 HAS WEAR GROVE ON LOWER SURFACE, MARKED 2 AREAS. C-CHECK RO 11/11/2020. REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE WITHIN LIMITS, REF. MHI RJ REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH SKYWEST TSDR SWAA2021072620160Skin · crackedCRACK ON LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB ON #4 SLAT. / REMOVED; INSTALLED SERVICEABLE # 4 SLAT; ADJUSTED AND FUNCTIONAL TESTED IAW MM 27-81-21-000-801; MM 53-81-21-400-801 AND MM 27-81-00-820-803 ADJUSTMENT AND FUNCTIONAL CHECKSDR UIEA2020092802100Structure · corrodedCORRODED SLAT. REPLACED SLAT, IAW B767 AMM 27-81-02.SDR SWAA2021071322442Slat · out of adjustREMOVE AND REPLACE SLAT 2 AT LT WING (FOR STRUCTURAL REPAIR BEYOND LIMITS IN L179668) / REMOVED AND REPLACED L/E SLAT #2 LT WING IAW B737-700 AMM 27-81-21-400-801. PERFORMED ADJUSTMENT AND TEST OF L/E SLAT #2; LT WING IAW B737-700 AMM 27-81-00-820-803 TEST OK.SDR K11A2020092100019Structure · corrodedRT WING LEADING EDGE NR 4 INTERNAL SIDE HAS CORROSION AT ATTACHMENT POINT OUTBOARD LOWER BONDING STRAP.SDR K11A2020092100014Structure · corrodedRT WING #5 LEADING EDGE FLAP HAS CORROSION AT ATTACH POINT FOR INBOARD LOWER BONDING WIRE.SDR FDEA202009182251Panel · crackedLT WING NR 2 SLAT LOWER COVE PANEL HAS EVIDENCE OF A CRACK ON INBOARD SIDE INBOARD MAIN TRACK ATTACH POINT TO SLAT REMOVED. FABRICATED AND INSTALLED NEW COVE PANEL, IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 114N4076 REV C. PERFORMED SATISFACTORY OPERATISDR FDEA202009182252Skin · chafedLT WING NR 5 SLAT LOWER SURFACE L/E AREA DAMAGE 2 (EA), PLACE AS MARK STREAMER ATTACH. REPAIRED NR 5 SLAT LOWER SURFACE 1EA AREA 89.5" FROM O/B, IAW B767 SRM 57-43-02-2R REPAIR 1 AND 51-70-10-2R REPAIR 4 FIG. 202; 1EA AREA 47.5" FROM O/B FOUND MISSING PAINT NSDR FDEA202009142209Rib · crackedRIGHT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT XIS 150.7474 ALIGNMENT PIN AREA FOUND CRACK. RIGHT HAND WING NUMBER 1 SLAT ASSEMBLY (INCLUDES SLAT AND CRUISE PERFORMANCE FILLET). REMOVED AND REPLACED, AS PER AMM 27-80-20-4. REFERENCE TO WRISDR ABXR2020091400088Wedge · corrodedRIGHT WING NR 9 SLAT UPPER WEDGE INNER IS CORRODED IN SEVERAL AREAS. NR 9 SLAT FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED NR 9 SLAT WITH SERVICEABLE UNIT, IAW B767 AMM 27-81-02 PARA 3, H.SDR ABXR2020091400087Angle · corrodedRIGHT WING NR 8 SLAT CORRODED AT THE TIA ATTACH POINT TO SLAT. BLENDED CORROSION ON CHORD SPLICE ANGLE ON NR 8 SLAT AT TAI ATTACH POINT. REMOVED .020 FROM NOMUAL .100 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-43-02 FIG 101 DETAIL V. REMOVED AND REPLACED ASDR FDEA2020091432191Skin · chafedRIGHT WING SLAT NR 11, T/E LOWER SURFACE CHAFE AT O/B TRACK. REPAIRED RT WING NR 11 SLAT T/E LOWER SURFACE CHAFE AT O/B TRACK WITH 250 DEG METAL BOND, IAW B767 SRM 57-43-01-01 FIG 1 DETAIL NR 1, 57-43-02-01 FIG 1 DETAIL NR 4, 57-43-02-2R REPAIR 1 DETAIL NR SDR SWIA202053428Roller · out of toleranceLT WING SLAT TRACK ROLLER 3-2 OUTBOARD FWD OUT OF LIMITS. C-CHECK RO 10/16/2020. REPLACED LT WING OUTBOARD FWD SLAT TRACK SIDE ROLLER, REF CRJ700 AMM.SDR SWIA202053427Roller · out of toleranceLT WING SLAT TRACK ROLLER 1-2 INBOARD FWD OUT OF LIMITS. C-CHECK RO 10/16/2020. REPLACED LT WING 1-2 INBOARD FWD SLAT TRACKSIDE ROLLER, REF CRJ700 AMM.SDR SWIA202053426Roller · out of toleranceLT WING SLAT TRACK ROLLER 1-2 INBOARD AFT OUT OF LIMITS. C-CHECK RO 10/16/2020. REPLACED LT WING 1-2 INBOARD AFT SIDE ROLLER, REF CRJ700 AMM.SDR SWIA202053425Roller · out of toleranceRT SLAT TRACK 1-2 FWD OUTBOARD ROLLER IS OUT OF LIMITS. C-CHECK RO 10/16/2020. REMOVED AND REPLACED RT WING SLAT TRACK 1-2 FWD OUTBOARD ROLLER, REF CRJ 700 AMM. TORQUED NUTS TO 25IN/LBS AND SAFETIED. T/W: TUC8221 DUE CAL: 31 OCT 2020. RT WING SLAT TRACK 1SDR YENA2020091400456Skin · crackedDURING HEAVY MAINTENANCE, CRACK LEADING EDGE EXTERNAL SKIN SLAT TRACK 5 AREA ON LT WING, REF: ARM W/O 2020-277/1 N/R 2020-245048 TECH 8622918 INSP 8612311. ACCOMPLISHED REPAIR BETWEEN RIB 19-20, IAW AEROMAN EA 57-0594-20 REV 1 (COVER AND PART 1) EMBREAR ETD 2SDR IPXA2020092260512Skin · damagedINSPECTION TYPE: 2C LT WING NR 3 SLAT LOWER SKIN HAS DEEP CHAFE DAMAGE. REMOVED AND REPLACED LT WING NR 3 SLAT ON NRC 432092.SDR FDEA2020090982145Skin · chafedRT WING NR 8 SLAT T/E LOWER SURFACE CHAFED AT INBOARD AUX TRACK. REPAIRED RT WING NR 8 SLAT T/E LOWER SURFACE, IAW B767 SRM 57-43-02-2R REPAIR 1, 51-70-10-2R FIG. 202.SDR SWAA2021081614181Bracket · crackedCRACK SLAT 7 AUXILIARY TRACK BRACKET LOCATED AT SLAT STATION 373 AT RT WING / REPLACED BRACKET LOCATED SLAT 7 AUXILIARY TRACK AT SLAT SATATION 373 AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 114A5020 SHEET 6 REV DSDR FDEA202009032088Skin · chafedLEFT WING #5 SLAT WING STATION OSS 441 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4.SDR FDEA202009032087Skin · chafedLEFT WING #5 SLAT AT WING STATION OSS 499 IS CHAFFED ON LOWER SURFACE DUE TO WORKING RIVETS REPAIRED LEFT WING #5 SLAT IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4SDR DALA2020090432952Doubler · debondedDURING INSEPCTION FOUND DISBOND OF 2.2" LENGTH AND 2.0" WIDTH AT EXTERNAL DOUBLER ON THE OUTSIDE OF THE LOWER SKIN OF SLAT 4 TRAILING EDGE WEDGE APPOXIMATELY STA OSS306. REPAIRED PER ERA 587580-14.SDR DALA2020090432951Skin · dentedDURING INSPECTION FOUND DENTS ON RIGHT WING SLAT 6 WEDGE #24, 37 AND 39 OUT OF LIMITS. DENTS REPAIRED PER SRM 51-70-10.SDR DALA2020090432950Skin · dentedDURING INSEPCTION FOUND DENTS OUT OF LIMITS ON LH WING SLAT PANEL # 3, WEDGE AREA, ZONE 1 DENT #21, ZONE 2 DENT #49 AND 78, DENTS WERE REPAIRED PER SRM 51-70-10.SDR DALA2020090402956Skin · dentedDURING INSPECTION NOTICED DENT #2 OF SLAT PANEL #8 UPPER SURFACE (WEDGE AREA) OUT OF LIMITS. REPAIRED DENT PER SRM 51-70-01SDR IPXA2020082859590Skin · delaminatedINSPECTION TYPE:SEG, #9 LEADING EDGE SLAT SHOWS DISBOND. REPAIRED SLAT IAW B757 SRM 51-70-10-2R PER SRM 57-43-02-2R-1 SEE E.O. B757-SDR DALA2020082802913Skin · debondedMAINTENANCE FOUND 3 DISBONDS ON T.E SLAT WEDGE 8 UPPER SURFACE AT OSS=452, OSS=453, OSS=560. DISBONDS REPAIRED PER RM 51-70-10. (LP 1603359)SDR FDEA2020082631996Skin · chafedLT WING NR 5 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED NUMEROUS SPOTS. REMOVED FINISH AT AREA AS MARKED OF NR 5 SLAT TRAILING EDGE WEDGE. LOWER SKIN, FOUND 1EA AREA OF 4 EA. REQUIRE REPAIR, REPAIRED IAW B767 SRM 57-43-02-1A. REMOVED DAMAGE 1EA AREA AND REPASDR N6WA20200824003Slat · damagedRIGHT WING INBD SLAT WAS DAMAGED DURING MAINTENANCE AND REPAIRED IAW STS EA70-2020-141.SDR DALA2020082102832Wedge · debondedDISBOND WAS FOUND ON SLAT T.E. WEDGE 2 AT OSS=580 REPAIRED PER SRM 57-43-02 AND 51-70-10SDR P5CA2020082200287Flap · inflt separationFLAPS DRIVE DISPLAYED WHEN FLAP 1 SELECTED. STATUS MESSAGE FLAP SYSTEM MONITOR. WALKAROUND FOUND #6 LE VC FLAP PANEL MISSING #1 INBD T/R DAMAGE. INSPECTION OF ADJACENT ARE FOUND DAMAGED AT ILES 1100 LE PANEL.(INSTALLED MISSING #6 LE FLAP PANEL / IAW B747 AMM 2SDR FDEA202008171959Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING (1 EA) REPLACED BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING IAW AMM 27-80-14- 04.SDR FDEA2020081871927Bolt · corrodedONE CORRODED BOLT ATTACHMENT ON SLAT TRACK NR 7 LOWER POSITION OF THE LT WING. REPLACED THE BOLT IAW AMM 27-80-14-04.SDR SWIA202052800Skin · chafedRT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REMOVED CHAFING IN SEVERAL AREAS ON RT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE, REF CRJ700 SRM. COMPLIED WITH ALL STEPS OF MHIRJ REO.SDR SWIA202052799Skin · chafedRT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.SDR SWIA202052798Skin · chafedRT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.SDR SWIA202052796Skin · chafedLT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REWORKED CHAFE DAMAGE TO LT SLAT NR 2 TRAILING EDGE, PER REO.SDR SWIA202052795Skin · erodedLT SLAT NR 3 LEADING EDGE HAS EROSION THE ENTIRE LENGTH. C-CHECK RO 9/27/2020. REMOVED EROSION DAMAGE FROM LT SLAT NR 3 LEADING EDGE, REF MHIRJ REO. SEE CONTINUATION FOR WORK DETAILS.SDR U2RA202009200016Spindle · gougedWHILE ACCOMPLISHING TASK CARD 744-27-0003 FOUND LT INBOARD FLAP FWD SPINDLE BEARING HOUSING GOUGED NEAR FAIL-SAFE LINK. REPAIRED PER VT-SAA EA 747-5740-56-A8471 REV A.SDR SWAA2020090908785Skin · crackedCRACK AROUND THE FASTENER AT NR 6 SLAT RIGHT WING LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIBS, MARKED. REMOVED THE DAMAGE PART AT NR 6 SLAT RT WING LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB AND INSTALLED REPAIR PARSDR UIEA2020081341692Skin · damagedNR 8 SLAT INBD LE HAD DAMAGE 8"X 6" AND A DEPTH OF 1.5". REPAIRED THE NR 8 SLAT IB LE IAW FAS EA 20009-IR.SDR ABXR2020081100074Wedge · corroded#9 SLAT UPPER TE WEDGE AFT SURFACE IS CORRODED IN NUMEROUS AREAS. REPAIRED DAMAGE ON 39 SLAT TE WEDGE IAW SRM 57-43-02 REPAIR 1,51-70-10 PARA 7, 8, 14, 15, 18, 20, 21, 22.SDR FDEA202008101848Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE(#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 1SDR FDEA202008101847Bracket · corrodedLEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE(#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA202008101846Bracket · corrodedLEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE CORRODED. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGEPIVOT HOLE BORE(#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATESDR U2RA202009200019Spindle · gougedWHILE ACCOMPLISHING TASK CARD 744-27-0003 FOUND RT INBOARD FLAP NR 5 FWD SPINDLE BEARING HOUSING GOUGED NEAR FAIL-SAFE LINK. REPAIRED PER VT-SAA EA 747-5740-56-A8471 REV A.
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