JASC 5753
Service difficulty reports · 31,513
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 IPXA13578873Skin · damagedLEFT OTBD FLAP HAS A HOLE IN UPPER SURFACE 1.8" DIA 5.5" FROM OTHER DAMAGE. REPAIRED IAW EOB757-5750-51094-A.SDR A6WA20134M1040Skin · dentedLEFT INBD FLAP HAS A DENT ON THE INBD T/E LOWER SIDE. REPAIR NR 3 OF SRM 57-22-00 NON FLUSH SKIN REPAIR.SDR SWIA201333909Vane · chafedLT INBD FLAP VANE HAS CHAFING DAMAGE ON LE INBD SIDE. C-CHECK REPAIRED LT INBD FLAP VANE INBD LE IAW REO.CSDR SWIA201333908Vane · chafedLT INBD FLAP VANE MIDDLE OF LE HAS CHAFING DAMAGE. C-CHECK REPAIRED LT INBD FLAP VANE MIDDLE LE IAW REO.SDR SWIA201333907Vane · chafedLT INBD FLAP VANE HAS CHAFING DAMAGE ON LE OTBD SIDE. C-CHECK LT INBD FLAP VANE OTBD LE WAS BLENDED IAW REO.SDR SWIA201333906Vane · chafedRT INBD FLAP VANE LE HAS CHAFING DAMAGE INBD SIDE. C-CHECK REPAIRED RT INBD FLAP VANE INBD LE IAW REO.SDR SWIA201333903Plate · chafedRT INBD FLAP, INBD HINGE ARM & INBD AFT LUG PLATE IS CHAFED. CHAFED BLENDED CHAFE MARK ON RT INBD FLAP, INBD HINGE ARM & INBD AFT LUG PLATE IAW REO.SDR 2013FA0000361Bracket · crackedDURING WALK-AROUND INSPECTION OF ACFT, FOUND THE RT OTBD FLAP TRACK NOSE ROLLER BRACKET CRACKED AT RADIUS. INSTALLED NEW NOSE ROLLER BRACKET USING MFG BULLETING 60-27-22.SDR SWAA2013061917340Skin · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED ON UPPER INBD SIDE. R & R AFT FLAP ASSY. IAW MM.SDR UALA2013061404141Skin · dentedRIGHT INBD MAIN FLAP LOWER SURFACE HAS A DENT 3 INCHES WIDE BY 5 INCHES LONG BY .083" DEEP. FOUND WITHIN LIMITS IAW SRM 57-53-01. REPAIRED RT INBD MAIN FLAP LWR SURFACE IAW SRM 51-71-10 REPAIR 4, FIG 202, SHEET 3.SDR SWAA2013061817239Skin · delaminatedRT WING INBD FORE FLAP INBD LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR FDEA201306141286Skin · damagedRIGHT WING INBD T/E FLAP DAMAGED AFT EDGE.SDR FDEA201306141291Hinge · corrodedLEFT WING OTBD FLAP FWD (WING) HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR IPXA13M79197Vane · delaminatedINSPECTION TYPE:4C, RT WING INBD FLAP VANE IS DELAMINATED AT STA. XIFH 191 LOWER SURFACE. REMOVED DAMAGE AND REPAIRED IAW SRM 57-50-80, EA 011-5753-01- A4734, REV IR AND EO MD11-5750-51342-A.SDR IPXA13M79111Vane · delaminatedINSPECTION TYPE:4C LT IB FLAP VANE LOWER SKIN DELAMINATED AT XIFH 186, 13" FROM T/E REPAIRED LT IB FLAP VANE SKIN PER MD11 SRM 57-50-80 REPAIR 2 FIG.201 (MAJOR)SDR SWAA2013061917349Flap · delaminatedRIGHT WING INBD AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2013061817260Spindle · corrodedRT WING NR 7 SPINDLE LOWER SURFACE ROOT CORRODED. R&R NR 7 FLAP SPINDLE CARRIAGE PER MT.SDR C77A20130616028Flap Track · wornRT NR 4 OTBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .007". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.2, REV IR.SDR C77A20130616027Flap Track · wornRIGHT NR 4 INBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .007". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.2, REV IR.SDR C77A20130616026Flap Track · wornRIGHT NR 3 OTBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .003". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.2, REV IR.SDR C77A20130616025Flap Track · wornRIGHT NR 3 INBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .003". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.2, REV IR.SDR C77A20130616024Flap Track · wornRIGHT NR 2 OTBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .002". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.2, REV IR.SDR C77A20130616023Flap Track · wornLEFT NR 4 INBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .005". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616022Flap Track · wornLEFT NR 3 OTBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .002". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616021Flap Track · wornLEFT NR 3 INBD FLAP TRACK, PN 170-39315-001 HAS WIDTH REDUCTION MATERIAL LOST .002". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM, PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616020Flap Track · wornLEFT NR 2A OTBD FLAP TRACK HAS THICKNESS REDUCTION MATERIAL LOST .011". SRM LIMIT: 0.008" ETD PERM REPAIR LIMIT: 0.024". BLENDED WORN AREA IAW SRM, PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616019Flap Track · wornLT NR 2A INBD FLAP TRACK, HAS THICKNESS REDUCTION MATERIAL LOST .012". SRM LIMIT: 0.008" ETD PERM REPAIR LIMIT: 0.024". BLENDED WORN AREA IAW SRM PART II 51-10-03, ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616018Flap Track · wornLEFT NR 2 OTBD FLAP TRACK, PN 170-39312-003 HAS WIDTH REDUCTION MATERIAL LOST .002". SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II 51-10-03 IAW ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR C77A20130616017Flap Track · wornLEFT NR 2 INBD FLAP TRACK HAS WIDTH REDUCTION MATERIAL LOST .002" SRM LIMIT: 0.000" ETD PERM REPAIR LIMIT: 0.039". BLENDED WORN AREA IAW SRM PART II, 51-10-03 IAW ETD 2011-170/01072B AND EA E175-57-159.1, REV IR.SDR FDEA201306131271Skin · debondedLEFT WING INBD FLAP, TOP OTBD PANEL LOWER SURFACE, DISBONDED. REPAIRED SKIN IAW SRM 51-70-10. REPAIR 4. MAJOR REPAIRSDR SWIA201334030Skin · chafedRT WING, RIGHT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK OTBD. C-CHECK REMOVED CHAFED OUT OF LIMITS VANE CAP & INSTALLED NEW LE SKIN VANE CAP, PN 601R14303-44S ON RT INBD FLAP VANE OTBD SECTION IAW REO.SDR SWIA201334029Skin · chafedRT WING, RT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK AT CENTER. C-CHECK BLENDED CHAFE ON RT INBD FLAP VANE FOREFLAP CENTER SECTION IAW REO.SDR ASOA2013071508644Hinge · chafedLT INBD FLAP, INB HINGE, AFT INBD LUG PLATE IS CHAFED. DAMAGE APPROX .100"L X .030"W X .015"D. REPAIRED IAW REO 601R-57-52-1536 IAW SRM 51-12-00. MAJOR REPAIR.SDR WX0A201306270018Vane · chafedRT WING OTBD FLAP INBD VANE L/E DOUBLER CHAFED THROUGH 8" FROM INBD END STA X05 164. REMOVED DAMAGED AREA. FABRICATED DOUBLER, HOT BOND REPAIR AND PERMANENT REPAIR ACCOMPLISHED.SDR DALA13028791806Skin · delaminatedLEFT WING INBD MAIN FLAP AFT UPPER SKIN FOUND DELAMINATED. SKIN REPAIRED IAW SRM 51-70-03, PAR 5A.SDR SWIA201334033Vane · chafedLT INBD FLAP VANE LE CHAFED ON INBD ACTUATOR ROD END. C-CHECK BLENDED CHAFED AREA ON LT INBD FLAP VANE LE INBD SECTION IAW REO.SDR SWIA201334032Vane · chafedLT INBD FLAP VANE LE CHAFED AT CENTER ACTUATOR ROD END. C-CHECK BLENDED OUT CHAFED AREA ON LT INBD FLAP VANE LE CENTER SECTION IAW REO.SDR SWIA201334031Vane · chafedLT INBD FLAP VANE LE CHAFED AT OTBD EDGE NEXT TO ACTUATOR ROD END. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE LE AT OTBD EDGE NEXT TO ACTUATOR ROD END IAW REO.SDR IPXA3578761Skin · damagedNR 10 SLATE WEDGE UPPER SKIN DAMAGED 50 INCHES FROM INBD EDGE 4 INCHES FROM T/E. REPAIRED IAW EO B757-5750-51028-A.SDR IPXA3578760Skin · damagedRT INBD MAIN FLAP HAS ONE INCH DENT AND DELAMINATED. REPAIRED IAW EO B757-5750-510007-A.SDR UALA2013061304093Bolt · wornLT INBD AFT FLAP, INSTALLATION BOLTS FOR AFT FLAP PUSH RODS AND SUPPORT TRACKS ARE WORN REPLACE AS REQUIRED. REPLACED HARDWARE AND TRACK. VERIFIED NEW HARDWARE AND SUPPORT TRACKS INSTALLED IAW AMM AND IPC 27-51-02-010C.SDR USAA2013070200019Skin · delaminated2S CHECK - DELAMINATION ON RT WING OTBD FLAP LOWER SURFACE BETWEEN RIB 15 TO RIB 17 APPROX 42" FROM OTBD EDGE & 1" FROM T/E. REPAIRED RT WING OTD FLAP LOWER SURFACE IAW EA 504140.SDR SWAA2013061217117Skin · delaminatedLEFT WING INBD T/E FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR IPXA3B78743Skin · dentedINSPECTION TYPE:3C, LEFT WING INBD FORE FLAP LOWER SURFACE FOUND DENTED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, REV 66.SDR IPXA3B78742Skin · dentedINSPECTION TYPE:3C, RT WING INBD FORE FLAP LOWER SURFACE FOUND DENTED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, REV 66.SDR SWAA2013062417473Flap · crackedRT WING O/B AFT FLAP O/B CENTER TRACK LOSE OUT FILLER CRACKED. R&R AFT FLAP IAW SRM & AMM.SDR IPXA13B78730Wedge · delaminatedINSPECTION TYPE:3C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE FOUND DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 66.SDR IPXA13B78729Wedge · puncturedINSPECTION TYPE:3C, RT WING INBD FORE FLAP T/E WEDGE LWR SURFACE PUNCTURED. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 66.SDR IPXA13B78728Wedge · puncturedINSPECTION TYPE:3C, RT WING INBD FORE FLAP T/E WEDGE LWR SURFACE FOUND PUNCTURED. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV.SDR IPXA13B78727Wedge · delaminatedINSPECTION TYPE:3C, LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE FOUND DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 66.
Back to JASC 5753