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 USAA920080418Wedge · debondedCLT - MAJOR REPAIR - Q5 CHECK - LEFT WING NR 3 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-03.SDR USAA920080417Wedge · debondedCLT - MAJOR REPAIR - Q5 CHECK - LEFT WING NR 1 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND. REPAIRED LEFT WING NR 1 SLAT TRAILING EDGE WEDGE IAW B737 SRM 57-70-10.SDR DHL2008752502Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TSDR DHL2008752503Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT NR 5 L/E SLAT MATERIAL USED SDR DHL2008752501Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TSDR DHL2008752570Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR DHL2008752550Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR DHL2008752500Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL SDR USAA920080407Wedge · debondedMCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND, SS 126.9. REPAIRED RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE, SS 124.90 - SS 128.40 IAW B737 SRM 51-70-10-2R.SDR USAA920080330Skin · crackedPHX - MAJOR REPAIR - NR 4321748, RIGHT WING NR 6 SLAT LOWER SURFACE CRACKED. REPLACED RIGHT WING NR 6 SLAT IAW B737 AMM 27-81-00.SDR DHL2008765033Rib · crackedDURING C CHECK, NR 2 SLAT INBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED INNER SKIN PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED DAMAGE INBOARD RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5 AND 51-40-1. TREATED AND PRIMED HOLES AND AREA IAWSDR USAA920080486Angle · crackedMIA - MAJOR REPAIR - C4 CHECK, LEFT WING LEADING EDGE NR 6 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES CRACKED, LES 280. REPLACED LEFT WING LEADING EDGE NR 6 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES, LES 280 IAW BOEING DRAWING 114T3100 AND B767 SRM 51-10-02.SDR USAA920080485Angle · crackedMIA - MAJOR REPAIR - C4 CHECK - RIGHT WING LEADING EDGE NR 7 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES CRACKED, LES 227 - LES 321. REPLACED RIGHT WING LEADING EDGE NR 7 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES, LES 227 - LES 32 IAW BOEING DRAWING 114T3100 ANSDR USAA920080368Skin · delaminatedCLT - MAJOR REPAIR - Q3 CHECK - NR JK-12-57502C/20, RIGHT WING NR 4 SLAT TRAILING EDGE DELAMINATED. REPAIRED RIGHT WING NR 4 SLAT TRAILING EDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-03.SDR ASAA0872704Skin · crackedNR 2 LEADING EDGE SLAT HAS 1, 4 INCH CRACK ADJACENT TO ACTUATOR MOUNT FASTENER. SLAT SKIN REPAIR COMPLETED.SDR ASAA0872703Skin · crackedNR 7 LEADING EDGE SLAT HAS 1, 4 INCH CRACK ADJACENT TO ACTUATOR MOUNT FASTENER. SLAT SKIN REPAIR COMPLETED.SDR ASAA0842679Wedge · delaminatedLEFT WING NR 1 SLAT T/E WEDGE AREA OF DELAMINATION ON O/B UPPER SUFACE. REMOVED DAMAGED AREA OF DELAMINATION, FABRICATED CORE AND REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 201 PAR 9G 217 218 PAR 8 214 PAR 15 20 PGS 241 242 254 257.SDR USAA920080347Skin · crackedCLT - MAJOR REPAIR - C2 CHECK - NR JK-10-5725C-C1, LEFT WING NR 1 SLAT LOWER SURFACE SKIN CRACKED. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE SKIN IAW B737 SRM 57-43-01 REPAIR 6.SDR SWAA080568Slat · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR SWAA080560Slat · crackedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR ASAA0842634Wedge · delaminatedNR 5 SLAT HAS DELAM AT I/B AFT CORNER. REPAIRED NR 5 SLAT AT I/B END IAW B737 400 SRM CH 51 70 10 REPAIR 4.SDR DHL2008765024Skin · crackedDURING C CHECK, NR 4 SLAT UPPER SKIN CRACKED AT INBOARD HOOK MOUNT SCREW WS 390. STRIPPED AREA IAW B727 MM 51-20-1, C/S HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. CRACKS TERMINATE IN STOP DRILL HOLES. FABRICATED REPAIR PLATE MATERIAL USED 7075-T6 0.125" PO NR SDR C77A200800005Slat Track · obstructedDURING FLIGHT INBOUND, PILOT SENT ACARS MESSAGE OF SLAT FAIL. A/C PERFORMED A ZERO FLAP LANDING, AND THE PILOT AS NOTED THE BRAKES HAVING A HIGH TEMP. AC PROCEEDED TO GATE UNDER ITS OWN POWER. MAINT THEN PERFORMED THE SLAT-ACE 1 AND 2 TESTS. ALL TESTS COMPLETESDR ASAA0842674Skin · delaminatedLEFT WING NR 1 L/E SLAT LOWER SURFACE O/B SIDE DELAMINATED. REMOVED DAMAGE DELAMINATION UNDER 2" DIAMETER, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.SDR ASAA0842618Panel · chafedNR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP LOCATION CHAFING DAMAGE. ON NR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP REPAIR IAW B737 400 SRM 57 43 01 FIG 201.SDR USAA920080367Skin · crackedCLT - MAJOR REPAIR - Q3 CHECK - NR JK-12-57102C/19, RIGHT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED RIGHT WING NR 5 SLAT LOWER SKIN IAW B737 SRM 57-43-01.SDR USAA920080366Skin · crackedCLT - MAJOR REPAIR - Q3 CHECK - NR JK-11-57101/3, LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED LEFT WING NR 3 SLAT LOWER SKIN IAW B737 SRM 57-43-01.SDR USAA920080365Skin · crackedCLT - MAJOR REPAIR - Q3 CHECK - NR JK-11-27300/1, LEFT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED LEFT WING NR2 SLAT LOWER SKIN IAW B737 SRM 57-43-01 REPAIR 6.SDR SWAA080446Slat · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E EDGE. REPAIRED SLAT PER SRM.SDR 08FDEA00260Skin · dentedRT WING, NR 5 L/E SLAT HAS DENTS 5EA ON L/E SKIN. CUT OUT DAMAGED AREA, FABERICATED DOUBLERS, SPLICE PLATE, BAFFLES, SEAL, FILLER AND INSTALLED REPAIR IAW SRM 57-10-00 FIG.II, VOL I, SRM51-21-01 VOL II AND SRM 51-35-02 VOL II.SDR ASMF200801003Slat · damagedDURING TAXING, AC HIT WITH LT SLAT NR 1 ON THE LT WING OF THE AIRCRAFT REGISTRATION N774AM. DETAILED INSPECTION WAS PERFORMED ON LT WING TIP DETECTING A STRUCTURAL DAMAGE ON SLAT NR 1 OF 17 INCHES LENGTH AND 11 INCHES WIDTH, OUT OF LIMITS, LOCATED BETWEEN STATSDR ASAA0842660Wedge · delaminatedNR 1 SLAT HAS DELAM AT O/B AFT END. REPLACED NR 1 SLAT DELAMINATED AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4.SDR DHL2008749008Attach Fitting · crackedRT WING NR 5 SLAT ACTUATOR ATTACH FITTING CRACKED AT INBOARD SIDE, INSIDE LEADING EDGE STRUCTURE. FABRICATED NEW RIBS (2 EACH) IAW SRM 57-50-2 FIGURE 2, 51-20-1 FIGURE 1 AND SRM 51-20-1 FIGURE 2. IAW ER 2-37163-801 REV A. INSTALLED NEW RIBS AT NR 5 SLAT ISDR ASAA0842635Wedge · delaminatedNR 5 SLAT HAS DELAM AT O/B AFT END. REPAIRED NR 5 SLAT AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4.SDR DHL2007873519Frame · crackedLT WING L/E CONSTANT SECTION UPPER FORMER CRACKED 1 1/4" STA XCW 69.000. REMOVED CRACKED FORMER IAW SRM 51-1-20D, SRM 51-3-0. FABRICATED NEW FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FIG. 1, DOUGLAS DWG 5769646. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAWSDR 08FDEA00208Skin · noneSLAT NR 7 TRAILING EDGE WEDGE EXTERNAL DOUBLER, REF: ENTRY NR R15 IN 4X-BY EXTERNAL DAMAGE RECORD SHEET. THE TEMPORARY REPAIR DOUBLER AT SLAT NR 7 TRAILING EDGE WEDGE OUTER SURFACE SKIN REMOVED. COMPLIED WITH ATTACHMENT B OF EO F-5100-7-5001 P1. REPAIR DOSDR DHL2008765032Rib · crackedDURING C CHECK, NR 2 SLAT OUTBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 2 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLED ACCESS PANSDR DHL2008765030Rib · crackedDURING C CHECK, CRACK INDICATION ON NR 4 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 4 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLESDR DHL2008765025Skin · crackedDURING C CHECK, CRACKED ON NR 3 SLAT UPPER SURFACE AT INBOARD SLAT HOOK MOUNT SCREW WS 520. REMOVED HOOK FROM AREA IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR AT NR 3 SDR DHL2008765031Rib · crackedDURING C CHECK, CRACK INDICATION ON PREVIOUS REPAIR OF NR 3 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED NR 3 SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED CRACKED RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB IAW SRM 51-3SDR DHL2008765018Structure · gougedDURING C CHECK, RIGHT WING NR 6 SLAT TRAILING EDGE GOUGED AT HOOK FITTINGS WS 150 APPROXIMATE. REMOVED HOOK FITTING FROM ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIGURE 10. TREATED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTASDR DHL2008765017Skin · crackedDURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DRILLED 3 EACH CRACKED PLACES AROUND RIVETS AT INBOARD END WS 150 (DIAMETER 0.190") IAW SRM 51-10-1 AND 57-50-3 FIGURE 12. HFEC C/W AROUND STSDR DHL2008765007Skin · dentedDURING C CHECK, RT WING WS 760 NR 8 SLAT UPPER SURFACE HAS A DENT AROUND FASTENER. EVALUATED AND FOUND DENT OUT OF LIMITS IAW SRM 57-50-1 FIG 2 DUE TO DENT BEING ON FASTENER. CUT OUT DAMAGED AREA DIMENSION 1.75" BY 1.125" IAW SRM 57-50-3 FIG 1. FABRICATED DSDR USAA920080349Skin · delaminatedMCN - MAJOR REPAIR - C20 CHECK - NR 6033405, DISBOND ON THE LEFT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91. REPAIRED LEFT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91 IAW B737 SRM 51-70-10-2R4.SDR USAA920080185Web · crackedPIT - MAJOR REPAIR - C4 CHECK - RIGHT WING 6 SLAT WEB CRACKED, FSS 550. REPAIRED RIGHT WING 6 SLAT WEB, FSS 550 IAW USAIRWAYS EA 110396.SDR USAA920080184Web · crackedPIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 599. REPAIRED RIGHT WING 9 SLAT WEB, FSS 599 IAW USAIRWAYS EA 110393.SDR 08FDEA00130Wedge · damagedEXISTING REPAIR, SLAT NR 6 TRAILING EDGE WEDGE EXTERNAL DOUBLER (REF: 4X-BY EXTERNAL DAMAGE RECORD SHEET ENTRY NR R4) TO EVALUATE EXISTING REPAIR. ACCOMPLISHED EVALUATION IAW ATTACHMENT B OF EO F-5100-7-5001 P1. EXISTING REPAIR DOUBLER AT NR 6 SLAT IS AN ISDR USAA920080175Web · crackedPIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 692. REPAIRED RIGHT WING NR 9 SLAT WEB, FSS 692 IAW USAIRWAYS EA 110393.SDR DL76G081133Skin · damagedFOUND ON W/A NR 6 SLAT DAMAGE. REPLACED PNL 511 CB.SDR DHL2008782001Angle · crackedUPON INSPECTING THE LEADING EDGE, FOUND WHAT APPEARS TO BE A CRACK ON THE LEFT WING INBOARD MOUNT BRACKET FOR NR 4 LE SLAT ACTUATOR. THE CRACK TRAVELS FROM THE RADIUS TOWARDS THE BOLT AT APPROX WING STATION 393. ANGLE WILL BE REPLACED WITH NEW PART.
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