JASC 5753
Service difficulty reports · 31,515
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 DHLA20087521022BWedge · delaminatedRIGHT WING INBD T/E FLAP ASSY MID FLAP T/E HAS AREA OF DELAMINATION AT OUTER T/E. 337 FILED AND MP9 FILED NR 26945. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 10, 14, 20, 22. REMOVED DAMAGED AREA APPROX 4 INCH BY 4 INCH AND FABRICATED SDR DHLA20087521022AWedge · delaminatedLEFT WING INBD T/E FLAP ASSY INBD MID FLAP T/E APPROX 64 INCHES FROM OUTBOARD EDGE HAS AREA OF DELAMINATION AT PREVIOUS REPAIR. 337 FILED AND MP9 NR 26944 FILED. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 9, 10, 14, 20, 22. AREA OF DAMSDR MALA080189Skin · gougedGOUGE NOTED IN LT FLAP UPPER SKIN. REPAIRED IAW EO S51031.SDR 2008UALA06213Skin · delaminatedRT OUTBOARD TRAILING EDGE FLAP OUTBOARD LOWER SURFACE DELAMINATED APPROX 72 SQ INCHES. REPLACED DAMAGED OUTBOARD AFT FLAP ON RT WING. OP CHECKED GOOD. ACFT OK FOR SERVICE.
SDR SWAA085681Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B FWD SIDE. REMOVED AND REPLACED FLAP PER MM.SDR 08FDEA04464Skin · delaminatedLT WING, INBD FLAP TRAILING EDGE UPPER SURFACE PREVIOUS REPAIR LOCATED 44.0 INCH FROM OTBD EDGE DELAMINATED APPROX 3.0 BY 3.0 IN SIZE. REMOVED EXISTING REPAIR BY A NEW REPAIR PER SRM 57-52-12 FIG 204.SDR 08FDEA04463Skin · delaminatedRT WING, INBD FLAP TRAIL EDGE LWR SURFACE PREVIOUS REPAIR LOCATED 17.0 INCHES FROM INBD EDGE, DELAMINATED APPROX 22.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER EA 6-5750-125477.SDR 08FDEA04462Skin · delaminatedLT WING, INBD FLAP TRAIL EDGE LWR SKIN PREVIOUS REPAIR LOCATED 54.5 INCHES FROM INBD EDGE DELAMINATED APPROX 3.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER SRM 57-52-12 FIG 204.SDR UPS08853786Doubler · gougedINSPECTION TYPE:SV LT WING OUTBOARD FLAP TOP SKIN HAS A REPAIR DOUBLER THAT IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-0 TR57- 84.SDR SWAA085645Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MID FLAP WEDGE PANEL DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA04448Skin · gougedRIGHT OUTBD FLAP L/E INBD END IS GOUGED IN THE EXTERNAL SKIN.SDR F3LA2008102200678Skin · dentedDURING C4/S1 C-CHECK, INSPECTION NOTED DENT ON OUTBOARD FLAP TRAILING EDGE LOWER SURFACE BETWEEN RIB 16 AND RIB 17 ON THE RIGHT WING. MAINTENANCE PERFORMED REPAIR IN ACCORDANCE WITH A319 SRM 57-53-00, PARAGRAPH 8N.SDR UPS08853769Doubler · gougedINSPECTION TYPE:SV REPAIR DOUBLER GOUGED. REF SURVEY SEQUENCE 715-W3-28. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0.SDR UPS08653694Flap · dentedINSPECTION TYPE:N/A RIGHT I/B MAIN FLAP DENTED OUT OF SRM LIMITS. REPAIRED PER EO B767-5750-30895-A.SDR ASM2008F00008Hinge · corrodedAFTER REWORK OF OB FLAP, IB AFT HINGE PN ARC 1984-501, IB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-04 PAGE 624 AND 625. FOUND 1.172" INSTEAD OF 1.150". BOECOM NR 1-1024128699-4 APPROVE TO INSTALL AN OS BUSHING.SDR 2008UALA06176Skin · chafedRIGHT WING INBOARD FORE FLAP OUTBOARD END UPPER SURFACE HAS CHAFED REPAIR. REMOVED DAMAGED REPAIR AND BONDED ON NEW REPAIR REO G12468, REV B.SDR 2008UALA06175Skin · debondedLEFT WING INBOARD FWD FLAP OUTBOARD END UPPER SKIN DISBONDED DOUBLER. REMOVED PREVIOUS REPAIR. BONDED ON NEW DOUBLER REF REO G12468 REV B.SDR 08FDEA04413Channel · crackedLEFT WING INBD FLAP OUT HINGE AFT FAIRING STRUCTURE ATTACH CHANNEL IS CRACKED AT THE UPPER INBD BOLT. REMOVED CRACKED CHANNEL REF SRM 51-33-01. FORMED, LOCATED & DRILLED CHANNEL REF DWG ARC 2594 & SRM 51-33-01. ALODINED, PRIMED & APPLIED TOP COAT REF SRM 5SDR 08FDEA04412Attach Angle · crackedLEFT WING INBD FLAP OTBD HINGE FAIRING STRUCTURE, FWD ATTACH ANGLE IS CRACKED FROM THE BOLT HOLES RUNNING TO THE OUTER EDGE. REMOVED ATTACH ANGLE REF SRM 51-33-01. FORMED, LOCATED & DRILLED NEW ATTACH ANGLE REF DWG ARC 2568. ALODINED & PRIMED ANGLE REF SRSDR 08FDEA04408Skin · crackedLEFT WING OTBD FLAP, INBD HINGE, AFT LOWER FAIRING IS CRACKED. REMOVED PANEL 535 JL IAW SRM 51-31-01. PANEL 535JL WAS CRACKED; WELDED PANEL 535JL IAW RS DPS 10.301 & DWG ARC 2147; REV " M ". WELS WAS CHECKED IAW DWG ARC 2147; REV " M " & DPS 4.707, NO CSDR 08FDEA04395Panel · chafedRIGHT WING INBD T/E FLAP PANEL 641 BR IS CHAFED. REPAIRED TWO AREAS OF CHAFING BY REMOVING DAMAGED AREAS & FABRICATING & BONDING A FILLER & DOUBLERS IAW SRM 51-71-00. REMOVED CAM LOCKS TO FACILITATE REPAIR & RE-INSTALLED IAW SRM 51-31-01. ALODINED, PRIMED, SDR SWAA085655Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA085622Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING O/B FLAP, AFT FLAP DELAMINATED AT INBOARD END ALONG T/E. REPAIRED FLAP PER SRM.SDR FDEA200810154352Skin · crackedLT WING L/E CRACK ON EXT LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.SDR SWIA200820185Structure · damagedFLT 6204 - DAMAGE FOUND DURING BURST/FLAT TIRE INSPECTION, TRAILING EDGE OF RIGHT INBOARD FLAP HAS DENT. INSTALLED NEW RIGHT INBOARD FLAP, PN CC670-14002-8, SN ON:15049, SN OFF: 10173.
SDR 08FDEA04370Skin · gougedLEFT OUTBD FLAP L/E IS GOUGED AT THE INBD END OF THE FLAP. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. LT WING OUTBD FLAP LE NOSE SKIN BETWEEN RIB NR 1 & 2 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. FABBED & INSTALLED OUTBD FLAP LE REPAIR IAW SRM 57-50-00. TSDR 08FDEA04351Skin · dentedRT WING INBD FLAP FOUND DEEP DENT ON UPPER SKIN 0.50 INCH BY 0.50 INCH DEEP .062 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1 VOL I.SDR SWAA085602Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LEFT WING O/B AFT FLAP INBOARD SIDE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED FLAP PER MM.SDR SWAA085579Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD AREA REPAIR DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA04347Skin · gougedLEFT CENTER FLAP L/E HAS A GOUGE IN THE EXTERNAL SURFACE LOCATED APPROX MIDWAY BETWEEN NR 3 & 4 FLAP TRACKS. REPAIRED LEFT CENTER FLAP L/E FROM RIB 16 TO RIB 17 IAW SRM 57-50-00.SDR 08FDEA04340Structure · crackedCRACK ON AFT STRUCTURE OF RT INBD FLAP WBL 114.2 FABRICATED AFT STRUCTURE REPAIR FILLER, ANGLE SPLICE, INSTALLED REPAIR SPLICE AND FILLER ON RT INBD FLAP IAW SRM 57-50-2, SRM 51-40-4, AND SRM 51-30-2.SDR UPS08153716Skin · chafedINSPECTION TYPE:1C3C LT WING CENTER FLAP UPPER MID SECTION REPAIR DOUBLER CHAFED. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER ON LT WING CENTER FLAP UPPER MID SECTION REF A300-600 SRM 57-50-00 FIG 205 AND SRM 57-50-00.SDR ASAA0843733Skin · delaminatedRT OUTBOARD AFT FLAP PREVIOUS REPAIR IS DELAMINATED ON INSIDE UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED REPAIR IAW B737 400 SRM 51 70 10.SDR USAA920081894Skin · debondedPHX-RON MAJOR REPAIR. RT WING TRAILING EDGE WEDGE DISBONDED APPROX 3 INCHES FROM TRAILING EDGE AND 40 INCHES FROM INBD EDGE. REPAIRED RT WING TRAILING EDGE IAW A320 SRM 57-53-00, PAGE 253, PARAGRAPH M. FIGURE 211.SDR UPS08653688Hinge Fitting · crackedINSPECTION TYPE:N/A RT WING I/B MAIN FLAP AFT I/B HINGE FITTING CRACK CRACK LENGTH .9375 INCH APPROX. RT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPLACED AS PER SRM 57-53-02-2R FIG 201.SDR ASAA0843664Skin · dentedLT INBOARD MID FLAP T/E WEDGE HAS MULTIPLE DENTS ON A PREVIOUS REPAIR ON THE LOWER SURFACE. REMOVED DAMAGED DOUBLER, FABBED REPLACEMENT DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 4.SDR UPS08653689Hinge Fitting · crackedINSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING CRACK. CRACK LENGTH .875 INCH APPROX. LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R FIG 201.SDR SWAA085560Wedge · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RIGHT WING I/B MID FLAP T/E WEDGE O/B END DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR UPS08854127Skin · gougedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-33 RT OUTBOARD FLAP UPPER SKIN REPAIR DOUBLER GOUGED JUST O/B OF FLAP STA 219 HINGE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-00 FIG 2A AND 57-07-01 FIG 4.SDR ASAA0843663Skin · dentedLT OUTBOARD FORE FLAP HAS MULTIPLE DENTS ON THE LOWER SURFACE INBOARD END. REMOVED DAMAGED AREAS, FABBED FILLERS AND DOUBLERS AND BONDED THE REPAIRS IAW B737 400 SRM 51 70 10 REP 4.SDR UPS08854021Panel · damagedINSPECTION TYPE:SP LT FLAP SURF BOARD PANEL HAS TWO DAMAGED SCREW HOLES. INSTALLED BONDED REPAIR IAW SRM 57-7-1, 51-1-9A PAR 11 FIG 9, 51-1-15 PAR 2.SDR DL757081547Panel · gougedRT INBD FLAP CENTER L/E PANEL IS GOUGED ON LOWER SURFACE INBD SIDE. BLENDED DAMAGED AREA IAW AMM 57-53-00. REMAINING SKIN THICKNESS .073. ORIGINAL IS .080, WITHIN LIMITS.SDR ASAA0843680Skin · dentedLEFT INBD AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11 IN THE SRM.SDR ASAA0843671Skin · dentedLT WING INBOARD MID FLAP WEDGE UPPER SURFACE HAS A DENT. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2.SDR 2008UALA06032Flap · damagedRIGHT WING INBOARD TRAILING EDGE FLAP HAS A 4 INCH SPLIT AT THE TRAILING EDGE WITH APPROX 3.5 INCHES OF DELAMINATION IN LENGTH. RT AFT FLAP ROUTED TO SHOP FOR REPAIR. FLAP REINSTALLED. OP CHECKS NORMAL.SDR KCSA081519Spar · damagedLT OTBD MID FLAP AFT SPAR HAS TOOLING DAMAGE. UNDER WBL 815 ACCESS PLATE. (K)SDR ASAA0843678Skin · dentedLT TRAILING EDGE FLAP LOWER SURFACE DENT AT 42 INCHES FROM INBOARD AND 3.5 INCHES FWD OF TRAILING EDGE. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11.SDR ASAA0843675Skin · chafedRT OUTBOARD FORE FLAP IS CHAFED ON THE OUTBOARD LEADING EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND INSTALLED IAW B737 400 SRM 57 53 01.SDR ASAA0843674Skin · dentedRT INBOARD AFT T/E FLAP UPPER SURFACE HAS 2 EA DENTS 3 INCHES OUTBOARD OF INBOARD EDGE. PREPPED DAMAGED AREAS, FABBED DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2.SDR ASAA0843673Skin · dentedLT INBOARD AFT FLAP HAS MULTIPLE DENTS ON THE UPPER SURFACE. REMOVED DAMAGED AREAS, FABBED FILLERS AND DOUBLER, AND BONDED REPAIRS 2 EA IAW B737 400 SRM 51 70 10 REP 4.
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