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 SWAA2014082731292Flap · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2014082631217Skin · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.SDR USAA2014081900005Flap · crackedFTIS VISIT TWO CRACKS OF 0.75 INCHES & 2.5 INCHES ON RT WING TE FLAP LE AT APPROX 2 INCHES FROM OTBD END & BETWEEN RIB 9 & 10. REPAIRED RT WING TE FLAP LE IAW SRM 57-53-00-201 & 51-23-11.SDR CA140814003Skin · debonded(CAN) DURING THE PREFLIGHT WALKAROUND THE CREW DISCOVERED DAMAGE AND DELAMINATION OF THE R/H OUTBOARD TRAILING EDGE FLAP. INSPECTION REVEALED THE SKIN HAD DISBONDED FROM THE HONEYCOMB CORE THAT RESULTED IN IT DEPARTING THE AIRCRAFT. IT IS UNKNOWN THE EXACT PHASDR REXA2014080900823Panel · chafedRIGHT FLAP VANE PANEL 684ET CHAFED OVER RIVET HEAD. MATCH DRILLED NEW FLAP VANE PANEL 684ET IAW SRM 51-40-11-001-001-A01. PANEL TO BE INSTALLED ON TALLY CARD 296 OPS 192. PN OFF CC670-14027-3 & PN ON CC670-14027-3.SDR REXA2014080900822Panel · chafedLEFT FLAP VANE PANEL 584ET CHAFED ACROSS RIVET HEAD. MATCH DRILLED NEW FLAP VANE PANEL 584ET IAW SRM 51-40-11-001-001-A01. NEW PANEL TO BE INSTALLED ON TALLY CARD 225 OPS 192.SDR R61A201408090972Nut · corrodedDURING HEAVY CHECK, LT WING FLAP TRACK SUPPORT NR 3 FWD ATTACHMENT NUT IS CORRODED. MAINTENANCE R & R LT WING FLAP TRACK NUT IAW AMM 57-57-31.SDR R61A201408090971Pin · corrodedDURING HEAVY CHECK, LT FLAP TRACK SUPPORT NR 4 FORWARD ATTACHING PIN IS CORRODED. MX R & R LT FLAP TRACK PIN IAW AMM 57-57-31.SDR LR7A2014080900479Skin · crackedDURING AN A-1 INSPECTION, FOUND A THREE INCH CRACK IN LOWER SKIN FACE OF LT OTBD FLAP. FLAP STATION 276. REPAIRED IAW SMP 583, FIG 51-140-12.SDR R61A201408081022Support · corrodedDURING HEAVY CHECK, BEARING SUPPORT BETWEEN FLAP TORQUE TUBES 5 & 6 RT WING ARE CORRODED. MX R & R BEARING SUPPORT BETWEEN FLAP TORQUE TUBES 5 & 6 RT WING IAW AMM 27-51-04, REF CONTINUATION C1 VVP-027603-2014/568 FOR WORK DETAILS. PN 1702961 BEARING SUPPORT.SDR AALA20140815003Panel · gougedLEFT MAIN FLAP GOUGE IN THE LE PANEL. INSTALLED DOUBLER IAW SRM 57-53-01-2R-2 & EA B757-57-036154.SDR R61A201408080979Bushing · corrodedDURING HEAVY CHECK, LIGHT CORROSION FOUND INSIDE BUSHING ON RT FLAP TRACK. MX R & R BUSHING IAW AMM 20-10-08.SDR IPXA2014090284113Skin · puncturedINSPECTION 10S2, LEFT OTBD AFT FLAP IS PUNCTURED AT WBL 467.00.140-42. REPAIRED IAW EO B757-5750-55372-ASDR SWIA201439184Vane · chafedLEFT FLAP VANE INBD CHAFED. R & R L/E CAP WITH NEW L/E CAP IAW REO AND SRM.SDR SWAA2014081130760Flap · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW MM.SDR DALA2015071207881Flap · damagedFOUND SMALL PIECE OF METAL PROTRUDING FROM LOWER INBD FLAP RIGHT SIDE. INSTALLED REPAIR IAW ERA 528174-14 REV ORIGINAL SEC II .SDR FDEA201408062085Hinge Fitting · corrodedLEFT WING INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND MINOR SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMITS AS PER CMM 57-44-07 REVISION 62. EXISTING HOLE DIAMETER = 2.554 INCHES. FINAL HOLE DIAMETER = 2.5625 INCHES. MAXIMUM ALLOWABLE DIAMETER = SDR FDEA201408062087Vane · delaminatedLEFT WING INBD FLAP VANE FOUND DELAMINATED AT LOWER SURFACE AS MARKED. AREA REPAIRED AS PER SRM 57-50-80 FIGURE 201 REPAIR 2 PARAGRAPH 2A(2)A(2) REV 56 AND EA 1-5750-T0310448 PART 1 TITLE: "WINGS - FLIGHT SURFACES - LT WING - INBD FLAP VANE ASSY - LOWER SURFASDR FDEA201408062086Skin · damagedTO COMPLY WITH WORK CARD T1-5750-T0302286 PART 2 TITLE WINGS, FLIGHT SURFACES, RT INBD FLAP SKIN DAMAGE. INSTALL PERMANENT REPAIR. EA 1-5750-T0302286 PART 2 TITLE: "WINGS-FLIGHT SURFACES - RT INBD FLAP SKIN DAMAGE" HAS BEEN COMPLIED WITH. REPAIR CLASSFIED SDR FDEA201408062098Support Fitting · crackedLEFT WING OTBD FLAP INBD HINGE FWD SUPPORT RT FITTING PN ARB2431-509 HAS A CRACK ON FWD END. COMPLIED WITH IN EA T 8-5710-T310392 P1/SEQ 809.SDR FDEA201408062097Support Fitting · crackedLEFT WING OTBD FLAP INBD HINGE FWD SUPPORT LT FITTING PN ARB2431-507 HAS A CRACK ON FWD END. COMPLIED WITH IN EA T 8-5710-T310392 P1/SEQ 809.SDR SWAA2014082531186Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED. REPAIR AFT FLAP IAW SRM.SDR AALA20140805007Wedge · puncturedLEFT WING OTBD FLAP, TE WEDGE LOWER SIDE HAS 1.5 INCH PUNCTURE. ACCOMPLISHED BONDED REPAIR SRM 51-70-05.SDR FDEA201408052082Skin · damagedRIGHT OTBD AFT FLAP BOTTOM PUNCTURED & TOP CRACKED OTBD OF OTBD FAIRING. REPAIRED OTBD AFT FLAP TE IAW SRM 57-53-01 & SRM 51-70-04 PARA B & PARA G FIG 9. TOP SURFACE REPAIR DIMENSIONS ARE 11.75 X 6 INCHES & DIMENSION OF LOWER SURFACE REPAIR IS A 2 INCH CIRCLSDR IPXA2014080483860Skin · damagedLEFT OTBD T/E FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B757-5750-55118-A.SDR IPXA2014080483857Skin · damaged.2500" PUNCTURE IN LOWER SKIN OF COVE PANEL ON RT MID FLAP. R & R IAW EO B747-5750-55132-A.SDR IPXA2014080483856Panel · damaged.2500 INCH PUNCTURE IN LOWER SKIN OF COVE PANEL ON RT MID FLAP R & R IAW EO B747-5750-55131-A.SDR SWAA2014081930990Flap · delaminatedLEFT WING TE OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR FDEA201408012034Skin · delaminatedLEFT WING INBD TE AFT FLAP UPPER SURFACE TABS DELAMINATED AT APPROX WS 200. REMOVED DAMAGED AREA. SANDED, CLEANED & PREPPED. APPLIED REPAIR, REFINISHED & TOP COATED IAW SRM 51-70-04 PARA 4G AMM 51-21-10-7.SDR REXA2014080100507Skin · dentedFOUND A DENT IN THE LT INBD FLAP LOWER SKIN. REPAIRED IAW EA CRJ957-02766.SDR SWAA2014080430587Skin · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED ON INBD LOWER SURFACE. R & R AFT FLAP IAW AMM.SDR FDEA201407312025Skin · gougedLEFT WING OTBD MAIN FLAP UPPER SURFACE LE GOUGED. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01 FIG 101 DETAIL VI. REPAIRED & INSTALLED FILLER & DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 2. MAJOR REPAIR.SDR CA140801004Nut · missing(CAN) EXITING THE ACFT CREW NOTED RT INBD FLAP FAIRING DROOPING. INVESTIGATION FOUND FAIRING PUSHROD DISCONNECTED, FOUND HARDWARE IN FAIRING, EXCEPT THE NUT WHICH WAS MISSING. INSPECTED OTHER FLAP FAIRINGS PUSHRODS ROD ENDS BOLTS, FOUND 3 MISSING COTTER PINSSDR SWAA2014092332233Hinge Fitting · crackedLEFT WING OTBD FORE FLAP OTBD TRACK HINGE FITTING FWD FASTENER HOLE CRACKED. R & R FORE FLAP IAW EA.SDR SWAA2014082031049Support Fitting · corrodedLEFT WING NR 4 FLAP TRACK AFT SUPPORT FITTING CORRODED. REPAIRED FITTING IAW CMM.SDR REXA2014073000797Skin · dentedLEFT WING INBD FLAP LOWER SKIN HAS DENT AT FLS63.50. DENT MEASUREMENTS ON LT WING INBD FLAP LOWER SKIN FLS63.50 WAS 2.40 INCHES L X 1.79 INCHES W X .100 INCHES D. DAMAGE RESPECT SUBMITTED IAW CRH 900 SRM 57-52-01-101-001-A01. REQUIRED DENT ON LT WING INBD LSDR SWAA2014080130536Skin · wornLEFT WING OTBD MID FLAP LEADING WORN. R & R MID FLAP IAW MM.SDR SWAA2014080130519Flap · delaminatedLEFT WING OTBD AFT FLAP INBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR K11A2014120400006Skin · damagedLEFT INBD FLAP DAMAGED OTBD L/E, 1 X 1.SDR SWAA2014092432263Skate Angle · crackedRIGHT WING NR 7 FWD FLAP TRACK FAIRING OTBD SKATE ANGLE CRACKED AT REAR SPAR. REPAIRED ANGLE IAW SRM.SDR SWIA201439096Skin · damagedHAIL DAMAGE ON TOP OF LEFT INBD FLAP. C-CHECK, REPAIRED LT INBD FLAP IAW SRM AND EA.SDR FDEA201407291995Skin · dentedRIGHT WING INBD FLAP UPPER SURFACE FOUND NUMEROUS DENTS. REPAIRED IAW EA 1-5750-T0309945B PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.SDR SWAA2014091531923Doubler · delaminatedRIGHT WING INBD FORE FLAP UPPER SURFACE DOUBLER DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWIA201439042Skin · chafedLT INBD FLAP AFT SKIN CHAFE INNER SIDE BY LT NR 2 VANE ACTUATOR. C-CHECK COMPLIED WITH EA.SDR REXA2014072700794Access Panel · chafedTASK CARD 900-27-580-101 LT INBD FLAP VANE ACCESS PANEL 584ET CHAFFED ACROSS RIVET HEAD. LOCATED & INSTALLED TWO EACH NUTPLATES IAW SRM 51-42-06-001-001-A01. PRIMED NEW PANEL IAW SRM 51-25-06-001-001-A01. TOP COATED PANEL IAW SRM 51-25-16-001-001-A01.SDR QXEA2014072900620Rub Strip · wornLEFT INBD FLAP, NR 1 FLAP TRACK FWD AND AFT RUB PADS WORN. REMOVED WORN PADS IAW AMM 27-54-01-000-802, STEPS 4A(1)-(3) 4C(1)-(2) & 4F(1)-(2) 4D(1)-(3). INSTALLED NEW RUB PADS IAW AMM 27-54-01-400-802 STEPS 3B(1)-(4) 4E(1)-(4) & 4I(1)-(7) 4C(1)-(7).SDR FDEA201407251962Skin · chafedRIGHT WING OTBD TE MAIN FLAP NOSE SKIN LE FOUND CHAFED AT 2.5 INCHES FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0309844 P1. REPAIR CLASSIFIED AS MAJOR.SDR ASAA2014072508799Skin · chafedLEFT INBD MID FLAP UPPER SKIN IS CHAFED ON INBD EDGE. ACFT GROUNDED. CHAFE ON LT INBD MID FLAP UPPER SKIN WAS ON EXISTING REPAIR. REPAIRED UPPER SKIN IAW SRM 57-53-01-2R-3.SDR IPXA2014080683861Skin · damagedRT INBD FLAP UPPER SKIN HAS A DENT/GOUGE BETWEEEN RIB 17 AND 18 AND STR 2.1 TO 2.3 ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 17 AND 18 AND STR 2.1 TO 2.3 IAW SRM 57-50-00, PARA 4E, FIG 205.SDR SWAA2014080130518Flap · delaminatedRIGHT WING OTBD FLAP AT INBD EDGE CORNER DELAMINATED. REPAIRED FLAP IAW SRM.
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