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 08FDEA02583Skin · chafedRIGHT WING CENTER FLAP UPPER SKIN HAS A WORN AREA APPROXIMATELY 70 INCH FROM THE INBD END AND 23 INCHES FROM THE AFT EDGE. BLENDED AREA AND FOUND AREA OUT OF ALLOWABLE LIMITS IAW A300-600 SRM 57-50-00; FIG SHEET 5; NOTE 1. FABBED REPAIR DOUBLER; TREATED; PRSDR SWAA083614Slat · crackedDURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR ASAA0843314Skin · chafedSLAT LOWER SURFACE IB END IS CHAFED. REMOVED DAMAGED AREA FABRICATED A DOUBLER AND BONDED THE REPAIR SRM 51-70-10 REPAIR 4.SDR ASAA0843252Skin · dentedRT OB AFT FLAP LOWER SURFACE IS DENTED. INSTALLED BONDED DOUBLERS IAW SRM 51-70-10.SDR ASAA0843305Skin · dentedNR 6 SLAT HAS 3 DENTS IN T/E WEDGE UPPER SURFACE 19-32" FROM IB END PREPAIRED DAMAGED AREA FABRICATED REPAIR PARTS & BONDED IAW SRM 51-70-10, REPAIR 4.SDR SWAA083470Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT INBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR USAA920081244Skin · crackedBFM - C2 - MAJOR REPAIR - LT WING LEADING SLAT NR 2 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING HAS A CRACK. REPAIRED LT WING LEADING EDGE SLAT NR 1 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING IAW B737 SRM 51-20-05. (S)SDR SWAA083406Slat · debondedDURING SCHEDULED SPV CHECK, FOUND RH WING #6 L/E SLAT INBOARD END DISBONDED. REPAIRED SLAT PER SRM.SDR USAA920081245Skin · delaminatedBFM - C2 - MAJOR REPAIR - LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN APPROX 28 INCHES FROM INBOARD AND 8 INCHES FROM AFT EDGE HAS DELAMINATION. REPAIRED LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN IAW B757 SRM 57-43-02 & 5SDR SWAA083273Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA.SDR DL757080865Skin · chafedLT WING NR 3 SLAT AT T/E AREA HAS CHAFING 2 EA LOCATIONS. REPAIRED CHAF IAW SRM 51-70-10.SDR ASAA0843060Skin · dentedNR 6 SLAT HAS 3 DENTS ON TOP SURFACE. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR IXX2008F00047Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RSDR CALA0800585Skin · crackedNUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 454. TRIMMED OUT CRACKED SKIN AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-43-01, FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02.SDR CALA0800584Skin · crackedNUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 424 AND 426. TRIMMED OUT CRACKED SKIN AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-43-01 FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02.SDR IXX2008F00042Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPSDR IXX2008F00037Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, SDR IXX2008F00036Skin · misrepairedDURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA ASDR IXX2008F00031Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING, FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RESDR USAA920081214Skin · delaminatedBFM - C2-MAJOR REPAIR - TAXK CARD NR JL-900-09000 - RIGHT WING NR 6 SLAT HAS AREA OF DELAMINATION. REPAIRED RIGHT WING NR 6 SLAT IAW SRM 57-43-01 AND 51-70-10. (K)SDR DL757081676Structure · unknownSUPPLEMENTAL SDR RT WING NR 7 SLAT TRAILING EDGE WEDGE REPAIR IAW ERA 468804-14, C/W ERA 468804-14.SDR USAA920081201Skin · debondedMCN - C-21 - MAJOR REPAIR - NR 6061316 - DISBOND TOP NR 5 SLAT STA 254. REPAIRED DISBOND TOP NR 5 SLAT WEDGE, SLAT STA 254 IAW B737, SRM 51-70-10-2R4 REPAIR 4. (K)SDR USAA920081175Skin · debondedMCN - MAJOR REPAIR - A CHECK WINGLET MOD - RT WING NR 10 SLAT TRAILING EDGE HAS 2 AREAS THAT ARE DEBONDED, SS 790 AND SS 802. REPAIRED RT WING NR 10 SLAT TRAILING EDGE, SS 790 AND SS 802 IAW B757 SRM 51-70-10 REPAIR 2 AND 4. (S)SDR USAA920081167Wedge · delaminatedPHX - MAJOR REPAIR - B CHECK - LT WING NR 2 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LT WING NR 2 SLAT TRAILING EDGE WEDGE IAW DRAWING 65C26602. (S)SDR USAA920081166Wedge · delaminatedPHX - MAJOR REPAIR - B CHECK - LT WING NR 3 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LEFT WING NR 3 SLAT TRAILING EDGE WEDGE IAW DRAWING 65C26603. (S)SDR USAA920081165Wedge · delaminatedPHX - MAJOR REPAIR - B CHECK - LT WING NR1 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LT WING NR 1 SLAT TRAILING EDGE WEDGE IAW DRAWING 65C26601. (S)SDR DHL2008F00024Bracket · crackedLT WING NR 1 KRUEGER FLAP ACTUATOR INBOARD AND OUTBOARD ATTACH BRACKETS ARE CRACKED IN THE CORNERS. REMOVED BRACKETS (2 EACH) IAW B727 SRM 51-30-2. FABRICATED BRACKETS WITH 2024-T3 .036 3.5" X 7.5" PO 9006767 IAW BOEING ENGINEERING DOCUMENT 65-16275 AND B72 SDR ASAA0842996Skin · crackedRT WING NR 3 K FLAP LEADING EDGE GOUGED ON EXTERIOR 5.5 INCHES FROM LEADING EDGE AND 13.2 INCHES FROM IB END VERIFIED CRACK IN GOUGE STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW B737 400 SRM 57 43 02 FIG 201 REPAIR 2.SDR 08FDEA02052Skin · crackedNR 4 SLAT UPPER SURFACE ON AFT HOOK ATTACHMENT SCREW HAS SKIN CRACKED REMOVED HOOK AS REQ IAW B727 SRM 51-10-2. FAB REPAIR PLATE MAT USED 2024T3-.125 PO NR 810563. DIM (5" BY 4") IAW B727 SRM 57-50-3 FIG 10, TREATED AND PRIMED IAW B727 SRM 51-10-2, C/W HFEC SDR SWAA082894Slat · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA.SDR SWAA082893Slat · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA.SDR F3LA200800280Skin · puncturedDURING WALK AROUND MAINTENANCE NOTED A BIRD STRIKE ON THE LEFT OUTBOARD LEADING EDGE FLAP APPROXIMATELY SIX FEET FROM OUTBOARD END OF FLAP. ENGINE PARAMETERS WERE REPORTED NORMAL BY THE PILOT. MAINTENANCE REPAIRED THE LEFT OUTBOARD FLAP LEADING EDGE IN ACCORSDR DHL2008764530Rib · crackedWHILE AT C CHECK, NR 5 K-FLAP ACTUATOR SIDE MOUNTING RIBS I/B AND O/B CRACKED. REPAIRED RIBS IAW BOEING DWG 65-16269 REVC MATERIAL 2024T3 .063" DIM 7" BY 6 1/8 INCH PO NR 9006773.SDR SWAA082791Structure · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SWA EA.SDR DHL2008764515Rib · crackedNR 6 K-FLAP ACTUATOR SUPPORT SIDE I/B AND O/B RIBS CRACKED WS 304. REMOVED INBOARD AND OUTBOARD RIBS AND FAB NEW RIBS WITH 2024-T3-.063 INCH DIM 7 1/2 INCH BY 4 INCH AND PO 9006773 IAW BOEING ENGINEER DWG NR 65-16275.SDR SWAA082728Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR UPS08M52393Structure · crackedINSPECTION TYPE:C RT WING DROOP L/E UPPER SURFACE FOUND CRACKED FROM O/B END TO I/B ABOUT 2 INCHES LONG AS MARKED. CRACK STOP DRILLED PER SRM 57-10-00 FIG30 V.1R.40. HFEC INSP C/OUT PER D AC NDT SPM R.13 PART06-10-01-001 AT STOP DRILL HOLE FOUND NO CRACK EVISDR SWAA082677Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.SDR SWAA082678Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR USAA920081144Slat · delaminatedCLT - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 4 SLAT INBOARD END HAS DELAMINATION. REPAIRED RIGHT WING NR 4 SLAT INBOARD END IAW US AIRWAYS EA 100445.SDR USAA920081149Skin · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - NR 03C30257009/ 9, LEFT WING NR 3 SLAT UPPER SURFACE INBOARD END HAS DELAMINATION. REPAIRED LEFT WING NR 3 SLAT UPPER SURFACE INBOARD END IAW B737 SRM 57-43-02 AND 51-70-10 REPAIR 4.SDR USAA920081103Skin · debondedCLT - MAJOR REPAIR - C2 CHECK - RIGHT WING NR 5 SLAT UPPER SURFACE TRAILING EDGE IS DISBONDED. REPAIRED THE RIGHT WING NR 5 SLAT UPPER SURFACE TRAILING EDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-02.SDR SWAA082668Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0843029Wedge · chafedRIGHT WING NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFED THROUGH IN TWO PLACES ON AFT EDGE ONE EACH AT INBOARD AREA AND 1 EACH AT ACTUATOR AREA. PREPARED DAMAGED AREA. FABRICATED FILLERS AND DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR NR 4.SDR SWAA082530Skin · delaminatedDURING SCHEDULED CV CHECK, FOUND LT WING NR 4 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM.SDR USAA920081056Skin · crackedMCN - MAJOR REPAIR - C12 CHECK - LEFT WING NR 2 SLAT COVE PANEL CRACKED, SS 607. REPLACED LEFT WING NR 2 SLAT COVE PANEL CRACKED, SS 607 IAW B737 SRM 51-40-02.SDR ABXA080160Panel · crackedNR 4 SLAT INNER SURFACE PANEL CRACKED NEAR I/B TRACK. REMOVED AND REPLACED ON NR 0129 IAW B767. (A)SDR 2008UALA02715Doubler · crackedNR 1 SLAT JUST INBOARD OF REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED EXISTING DOUBLER AND DAMAGED AREA. INSTALLED REPAIR SPLICE AND FILLER.SDR 2008UALA02714Doubler · crackedNR 2 SLAT INBOARD OF EXISTING REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED THE EXISTING DOUBLER AND THE DAMAGED AREA. INSTALLED REPAIR SPLICE AND FILLER.SDR 070197Slat · damagedDURING A ROUTINE SERVICE CHECK INSPECTION BY ALLEGIANT AIR MAINTENANCE DEPARTMENT PERSONNEL DAMAGE TO THE RIGHT WING NR 4 SLAT WAS DISCOVERED CAUSED BY A BIRD STRIKE. THE NR 4 SLAT WAS REMOVED AND THE AIRCRAFT FERRIED FROM BELLINGHAM, WA TO LAS VEGAS, NV. A
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