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 ASAA2013120112257Skin · chafedRIGHT WING OTBD FOREFLAP INBD L/E IS CHAFED. R & R RT WING OTBD FOREFLAP INBD L/E SKIN IAW SRM 51-40-02-0G-0.SDR SWAA2013121823491Cover · crackedRT WING FLAP BETWEEN INBD & OTBD FLAP VANE JOINT COVER CRACKED. R & R COVER IAW SRM.SDR SWIA201335696Panel · chafedLT INBD FLAP VANE LE INBD PANEL CHAFED. C-CHECK BLENDED LT INBD FLAP VANE LE INBD PANEL IAW REO.SDR SWIA201335695Panel · chafedLT INBD FLAP VANE LE CNTR PANEL IS CHAFED. C-CHECK BLENDED LT INBD FLAP VANE LE CNTR PANEL IAW REO.SDR SWIA201335694Panel · chafedLT INBD FLAP VANE LE OTBD PANEL IS CHAFED. C-CHECK BLENDED LT INBD FLAP VANE LE OTBD PANEL IAW REO.SDR SWAA2013121623361Strip · crackedRT WING NR 6 FLAP TRACK STRIP CRACKED. R & R STRIP IAW SRM.SDR SWAA2013121623287Fitting · crackedRT WING MID FLAP INBD TORQUE TUBE SUPPORT INBD FITTING FWD LOWER HOLE CRACKED. R & R MID FLAP IAW MM.SDR SWAA2013120923067Plate · brokenRT WING INBD MID FLAP INTERNAL STRUCTURE PLATE BROKEN. R & R PLATE IAW CMM.SDR SWAA2013121123194Stiffener · crackedLT WING NR 3 FAIRING INBD SIDE FLAP TRACK STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.SDR SWAA2013120422981Angle · crackedRT WING NR 6 FLAP TRACK INTERNAL ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.SDR CALA2013120293382Seal · missingRT WING FLAP CANOE SEAL MISSING. RT WING MIDDLE FLAP CANOE 632CB OTBD SEAL PORTION REMOVED & EIGHT RIVETS REMOVED IAW CDL 27AC.SDR REXA2013112702218Panel · chafedTASK CARD 188 RT WING FLAP PANEL 684FT CHAFED, OUT OF LIMITS. REPLACED RT WING FLAP PANEL 684FT. PAINTED WITH GRAY A023 IAW CRJ900 SRM 57-52-01-001-A01. IAW CRJ900 AIPC 57-51-32. REPLACED HINGE NUT PLATE RIVETS IAW CRJ900 57-52-01-001-A01 TASK 51-23-00-001SDR SWAA2013120222847Angle · crackedNR 6 CANOE FAIRING THE OTBD ANGLE AT THE FORE FLAP CRACKED. R & R ANGLE IAW SRM.SDR C77A20131127019Flap Track · wornRIGHT WING FLAP TRACK NR 2 OTBD, PN 170-39312-004, IS WORN OUT OF LIMITS THICKNESS REDUCTION D .014 INCHES IAW EMB 175 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-610 IAW EMBRAER ETD 2013-170-058596, ETD 201SDR C77A20131127018Flap Track · wornRIGHT WING FLAP TRACK NR 2 INBD, PN 170-39313-004, WORN OUT OF LIMITS THICKNESS REDUCTION D .016 INCHES IAW EMB 175 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-609 IAW EMBRAER ETD 2013-170-058596, ETD 2011-1SDR C77A20131127017Flap Track · wornLEFT WING FLAP TRACK NR 2A OTBD, PN 170-39321-003, WORN OUT OF LIMITS THICKNESS REDUCTION D .014 INCHES IAW EMB 175 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-510 IAW EMBRAER ETD 2013-170-058596, ETD 2011-1SDR C77A20131127016Flap Track · wornLEFT WING FLAP TRACK NR 2A INBD, PN 170-39320-003, WORN OUT OF LIMITS THICKNESS REDUCTION D .011 INCHES IAW EMB 175 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-509 IAW EMBRAER ETD 2013-170-058596, ETD 2011-1SDR C77A20131127015Flap Track · wornLEFT WING FLAP TRACK NR 1 OTBD, PN 170-39310-003, WORN OUT OF LIMITS WIDTH REDUCTION W .005 INCHES IAW EMB 175 SRM 57-52-03 TABLE 102. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-505 IAW EMBRAER ETD 2013-170-058596, ETD 2011-170/01SDR C77A20131127014Flap Track · wornLEFT WING FLAP TRACK NR 1 INBD, PN 170-39310-004, WORN OUT OF LIMITS THICKNESS REDUCTION D.023 INCHES IAW EMB 175 SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW EMBRAER SRM PART II 51-10-03 ON WORK ORDER 738778-504 IAW EMBRAER ETD 2013-170-058596, ETD 2011-170SDR SWIA201335590Vane · chafedLT INBD FLAP VANE, LE IS CHAFED, INBD SIDE. C-CHECK REPAIRED CHAFE ON INBD SIDE OF LT INBD FLAP VANE LE IAW REO.SDR SWIA201335589Vane · chafedLT INBD FLAP VANE, LE IS CHAFED, CENTER. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE LE CENTER IAW REO.SDR SWIA201335588Vane · chafedLT INBD FLAP VANE, LE IS CHAFED, OTBD SIDE. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE LE IAW REO.SDR SWIA201335587Skin · chafedLT INBD FLAP, OTBD VANE ACTUATOR, FLAP UPPER SKIN IS CHAFED ON INTERNAL SURFACE. C-CHECK REPAIRED LT INBD FLAP, AT OTBD VANE ACTUATOR INNER SURFACE IAW REO.SDR FDEA201311222852Vane · delaminatedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION AT XIFH 160 TO XIFH 187. FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 77.0 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 77.0 FOUND SATISFACTORY. REPAIR CLASDR EE4Y2013120500145Skin · dentedLEFT WING, MID FLAP, L/E DENTED WBL 117. REPAIRED.SDR R61A201311221262Bearing Support · corrodedDURING HEAVY CHECK, RT WING FLAP BEARING SUPPORTS ARE CORRODED BETWEEN F5, F6. MX R & R BEARING SUPPORTS IAW AMM 27-51-04.SDR 7AHR20131129002Support Fitting · corrodedLEFT HAND OTBD TE FLAP SUPPORT FITTING ASSEMBLY & MOUNTING STUDS HAD PITTING CORROSION DAMAGE AT C CHECK INSPECTION BEYOND ALLOWABLE LIMITS.SDR DALA13062610181Skin · puncturedRT WING I/B AFT FLAP LOWER SURFACE FOUND PUNCTURED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01.SDR SWIA201335492Vane · chafedLT INBD FLAP VANE IS CHAFED AT OTBD EDGE. C-CHECK REPLACED LT INBD FLAP VANE IAW SRM.SDR SWIA201335491Vane · chafedLT INBD FLAP VANE IS CHAFED AT MID EDGE. C-CHECK BLENDED LT INBD FLAP VANE CHAFE IAW REO.SDR SWIA201335490Vane · chafedLT INBD FLAP VANE IS CHAFED AT INBD EDGE. C-CHECK BLENDED LT INBD FLAP VANE CHAFE IAW REO.SDR SWIA201335489Vane · chafedRT INBD FLAP VANE IS CHAFED AT OTBD EDGE. C-CHECK BLENDED RT INBD FLAP VANE CHAFE IAW REO.SDR SWIA201335488Vane · chafedRT INBD FLAP VANE IS CHAFED AT MID EDGE. C-CHECK BLENDED RT INBD FLAP VANE CHAFE IAW REO.SDR SWIA201335487Vane · chafedRT INBD FLAP VANE IS CHAFED AT INBD EDGE BLENDED RT INBD FLAP VANE CHAFE. ORIGINAL THICKNESS .050. REMAINING THICKNESS .043. MATERIAL LOSS .007. FOUND TO BE WITHIN LIMITS IAW REO.SDR DALA13062581501Skin · delaminatedLT WING I/B AFT FLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED IAW SRM 51-70-10, AND 57-53-01.SDR IPXA2013112000899Skin · dentedRT WING INBD AFT FLAP DENTED. REMOVED UPPER SKIN 4.75 INBD OTBD AND 1.5 INCHES FORE AND AFT 98.5 INCHES FROM INBD EDGE 3.5 INCHES FROM LOWER EDGE. REPAIRED IAW EO B747-5750-52765-A.SDR IPXA2013112000890Skin · damagedRT WING INBD AFT T/E FLAP LOWER SKIN DAMAGED, 173.5 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52715-B.SDR IPXA2013112000886Skin · damagedRT WING INBD AFT FLAP T/E SKIN DAMAGED 119.9 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52717-A.SDR IPXA2013112000885Skin · damagedRT WING INBD AFT FLAP T/E LWR SKIN DAMAGED 113.4 IN FROM INBD EDGE. REPAIRED IAW EO B747-5750-52708-A.SDR IPXA2013112000884Skin · damagedRT WING INBD AFT EDGE LWR SKIN DAMAGE 149.5 IN FROM INBD EDGE. REPAIR IAW EO B747-5750-52716-A.SDR IPXA2013112000882Wedge · damagedRT WING INBD AFT FLAP T/E WEDGE DAMAGED 98.75 AND 100.75 FROM INBD EDGE. REPAIRED IAW EO B747-5750-52709-A.SDR SWAA2013112222729Flap Track · corrodedLT WING NR 2 TE FLAP TRACK CORRODED ON UPPER SURFACE. R & R FLAP TRACK ASSEMBLY IAW MM.SDR SWAA2013112122649Angle · crackedLT WING NR 3 FLAP TRACK FAIRING INTERNAL AREA ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.SDR IPXA2013112000878Skin · damagedRT WING I/B FLAP COVE PANEL HAS .1250" HOLE 120" FROM INBD EDGE. REPAIR IAW EO B747-5750-52755-A.SDR IPXA2013112000877Skin · damagedRT WING INBD FLAP COVE PANEL HAS .1250 INCH HOLE, 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52758-A.SDR IPXA2013112000876Skin · damagedRT WING INBD MID FLAP COVE PANEL HAS .1250 INCH HOLE 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52756-A.SDR IPXA2013112000879Skin · damagedRT WING INBD MID FLAP HAS .1250" HOLE IN COVE PANEL INNER SKIN 83 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52720-A.SDR ASAA2013111796692Structure · chafedLT WING OTBD FOREFLAP L/E INBD CORNER IS CHAFED. FABRICATED, DRILLED AND INSTALLED NEW REPAIR DOUBLER ON LT OTBD FORELFAP INBD L/E IAW SRM 57-53-01-2R-1, FIG 201.SDR SWAA2013120222856Skin · crackedLT WING INBD MAIN FLAP TE WEDGE LOWER SURFACE CRACKED AT 12-INCH INBD OF OTBD AFT FLAP TRACK. REPAIRED SKIN IAW SRM & EA.SDR SWAA2013112222728Frame · crackedRT OTBD MID FLAP INBD CARRIAGE A-FRAME ARM ASSEMBLY CRACKED. R & R FRAME ASSEMBLY IAW SOPM.
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