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 FDEA201603090874Skin · delaminatedRIGHT INBD TE MAIN FLAP, UPPER OTBD ACCESS PANEL, UPPER SURFACE FOUND WITH MULTIPLE DENT MARKS & MULTIPLE DELAMINATED AREA. DAMAGED AREAS REMOVED, CLEANED & DRIED USING 150 DEG F PROCESS IAW SRM 57-53-01-2R DETAIL 1 REV 116 & SRM 57-70-10-2R REV 116. REPAIR SDR FDEA201603090871Attach Bracket · corrodedLEFT WING INBD FLAP, DRIVE LINK ATTACHMENT BRACKET, BRACKET BORE FOUND CORRODED. BORE REAMED IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0323874 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR UIEA2016031000146Skin · dentedLEFT INBD TE FLAP, UPPER SURFACE HAS A DENT 86" IN FROM O/BEND. REMOVED DAMAGE PREPPED FOR & APPLIED REPAIR IAW SRM 51-70-10 REPAIR 2. PAINTED REPAIR IAW AMM 51-24-22.SDR SWAA2016040850711Flap Track · corrodedLEFT WING NR 4 FLAP TRACK CORRODED. REPAIRED FLAP TRACK IAW CMM.SDR ASAA2016030816132Skin · chafedLEFT WING INBD T/E MIDFLAP UPPER SURFACE INBD END IS CHAFED. ACFT GROUNDED. REMOVED CHAFE ON LEADING INBD T/E MIDFLAP UPPER SURFACE SKIN, CHECKOUT OF LIMITS IAW SRM 57-53-01-A-1, FIG 101. R & R LEFT WING INBD T/E AND FLAP UPPER SURFACE SKIN SEGMENT IAW SRM 5SDR SWIA201642005Skin · chafedRIGHT INBD FLAP VANE L/E SKIN CHAFED AT OTBD END. REMOVED BAD RT INBD FLAP VANE L/E SKIN AT OTBD END. INSTALLED SERVICEABLE VANE SKIN IAW SRM.SDR DALA2016030901781Skin · crackedCRACKED SKIN ON UPPER SURFACE OF RT OTBD FIXED GUIDE VANE INBD FLAP. UPPER SURFACE OF RT OTBD FIXED GUIDE VANE INBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR. II.SDR IPXA2016032201071Support Strap · corrodedINSPECTION TYPE:3C, RT WING INBD FLAP OTBD FAIRING SUPPORT STRAP CORRODED. R & R RT WING INBD FLAP, OTBD FAIRING SUPPORT STRAP AT BS XW 254 IAW SRM 51-35-01 AND DWG ARC2540.SDR DXTA2016030706203Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245 - .6255 PER DRAWING 1159WM20107. RT "D" TRACKSDR DXTA2016030706202Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .7495 - 07505 PER DRAWING 1159WM20105. RT "C" TRACKSDR DXTA2016030706201Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .8760 -.8770 PER DRAWING 1159WM20056. RT "B" TRACK SDR DXTA2016030706200Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "A" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 PER DRAWING 1159VVM20054. NEW UPPER FITSDR DXTA2016030706199Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 PER DRAWING 1159WM20107. REMOVED LT "D" SDR DXTA2016030706198Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .7495-.7505 PER DRAWING 1159WM20105. REMOVED LT "C" SDR DXTA2016030706197Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .8760-.8770 PER DRAWING 1159WM20056. LT FLAP TRACK "BSDR DXTA2016030806196Support Fitting · corrodedLEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF A FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 IAW DWG 1159WM20054. INSTALLED LT A TRACK SDR SWIA201641952Panel · damagedRT INBD FLAP PANEL HAS OUT OF LIMITS DAMAGE. REMOVED FLAP, PN CC670-14002-8, SN 15097 AND INSTALLED A SERVICEABLE RT INBD FLAP ASSY, PN CC670-14002-8 AND SN 15106 IAW AMM. OPS TEST GOOD AT THIS TIME.SDR DXTA2016030706196Support Fitting · corrodedLEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE.SDR REXA2016030700374Vane · chafedLEFT WING INBD FLAP VANE LE CHAFED IN 3 PLACES, INBD 1" X .750 X .004 DEEP, MID 1.0 X .600 X .004 DEEP, OTBD 1" X .500 X .003 DEEP. CONTINUATION CARD 8798011 OP 153. REPAIRED LT INBD FLAP VANE LE CHAFES IAW REO 601R-57-52-004 REV D.SDR IPXA2016030800493Skin · damagedLEFT INBD AFT FLAP LOWER SKIN DAMAGED, REPAIRED IAW EP B767-5750-59435-C.SDR FDEA201603070856Rib · crackedRIGHT WING INBD FLAP INTERNAL RIB, FOUND CRACK AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4. COMPLIED WITH EA 6-5750-T0323968 P1. REPLACED THE RT WING INBD FLAP INTERNAL RIB AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4.SDR DALA2016030701692Skin · wornWORN INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE. INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR II.SDR DALA2016030701688Skin · delaminatedDELAMINATED UPPER SURFACE ON INBD GUIDE VANE AT LT WING OTBD FLAP, POSITION 3, BS XV1=170. UPPER SURFACE ON INBD GUIDE VANE AT LT WING OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR II.SDR A6WA201643665Skin · dentedLEFT INBD FLAP, LOWER SKIN SURFACE AFT OF THE INBD HINGE ARM HAS 2 DENTS. REPAIRED LT FLAP, LOWER SKIN SURFACE AT INBD HINGE ARM IAW EA CRJ257-00305 REV A.SDR UIEA2016030700128Skin · dentedRIGHT WING NR 21, VC FLAP FOLDING NOSE SKIN DENT. REPAIRED IAW NR RI-57-44-11269 REV A.SDR IPXA2016030500354Angle · crackedINSPECTION TYPE: C10, CRACKED ANGLE, LT WING OTBD FLAP UPPERSIDE OF INBD LOCATION NEAR WS 538.2. REPLACED IAW SRM 51-40-02-0G, REV 64.00.SDR IPXA2016030500353Angle · crackedINSPECTION TYPE:C10, CRACKED ANGLE RT WING OTBD FLAP UPPER SIDE OF INBD LOCATION NEAR WS 720. REPLACE PARTS IAW SRM 51-40-02-0G, REV 64.00.SDR V0XD20160306049Skin · dentedLEFT INBD FLAP LOWER SURFACE HAS DENT OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 57-52-01, 51-42-06, 51-42-10, 57-52-01. NDT PERFORMED DATED 29 FEB 2016.SDR DALA2016030501669Skin · dentedDENTS ON UPPER SURFACE LT OTBD FLAP INBD GUIDE VANE AT BS XV1=190, XV1=187, XV1=160 AND XV1=161. DENTS XVI=160 AND XVI=161 WERE REPAIRED UNDER ERA 543162-14, REV. A.SDR HNAA2016030400071Support Bracket · corrodedNR 4 LT, INBD FLAP TRACK SUPPORT BRACKET HAS PITTING ON CAVITY FACE. R & R NR 4 FLAP TRACK SUPPORT BRACKET IAW MM 57-50-42.SDR HNAA2016030400070Flap Track · corrodedCORROSION ON LT WING, NR 4 FLAP TRACK, INBD SIDE, BEHIND THE TRACK SUPPORT BRACKET. R & R NR 4 FLAP TRACK IAW MM57-50-42.SDR SRXR2016FA0000110Fitting · gougedLEFT INBD MID FLAP OTBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED ON NRC A026329 IAW EA 747-5753-39-A6075, REV I/R AND FAA APPROVED 8110-3.SDR SRXR2016FA0000109Fitting · gougedLEFT INBD FLAP, INBD SPHERICAL BEARING GOUGED AT AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED ON NRC A026333 IAW VT EA 747-5753-39-A6075 IR AND FAA APROVED 8110-3.SDR SRXR2016F00073Fitting · gougedRIGHT INBD MID FLAP OTBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LOCK BOLT HOLE. REPAIR WAS ACCOMPLISHED IAW EA 747-5753-39-A6074 I/R AND FAA APPROVED 8110-3, DATED FEB 20, 2016, REF NRC A026319.SDR SRXR2016F00072Fitting · gougedRIGHT INBD MID FLAP, INBD SPHERICAL BEARING FITTING IS GOUGED OTBD OF SAFETY LINK. REPAIR WAS ACCOMPLISHED ON NRC A026314 IAW EA 747-5753-39-A6074, REV I/R AND FAA APPROVED 8110-3, DATED FEB 20 2016.SDR DALA2020121104049Structure · damagedDURING WALK AROUND FOUND LT OUTBOARD UPPER FLAP TRAILING EDGE DAMAGED. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-53-00 PARA 8. OK FOR SERVICE.SDR SWAA2016032850311Fairing · crackedRIGHT WING FLAP TRACK FAIRING 642BB INTERNAL CAVITY CRACKED. REPAIRED FAIRING IAW EA.SDR SWAA2016031449884Flap · delaminatedLEFT WING NR 1 OTBD AFT FLAP DELAMINATED AT INBD CORNER. R & R AFT FLAP IAW AMM.SDR DALA2016030401793Skin · puncturedRT WING INBD MAIN FLAP UPPER SKIN PUNCTURED 62" FROM INBD END/ 13" FROM T/E. ACCOMPLISHED REPAIR OF RT WING INBD MAIN FLAP UPPER SKIN, APPROXIMATELY A .5" CIRCLE, 62" FROM THE INBD END AND 13" FROM THE T/E IAW SRM 51-70-17.SDR DALA2016030401792Flap Track · corrodedNR 2 FLAP TRACK HAS RUST COMING OUT BETWEEN FLAP TRACK AND WING LOWER SURFACE AT AFT INBD CORNER ATTACH AREA. REPAIRED FLAP TRACK CORROSION IAW CMM 27-51-82. CORROSION IS LEVEL 1. REPAIRED ON NR 85. REMOVED/INSTALLED ON NR 275.SDR REXA2016030300353Vane · chafedRIGHT WING INBD FLAP VANE CHAFED IN 2 PLACES, INBD 1.0"" X .675 X .003 DEEP, MID 1.0"" X .500 X .003 DEEP. CONTINUATION CARD 8798011 OP 164. BLENDED CHAFE ON RT FLAP VANE INBD LOCATION IAW REO 601R-57-52-004. REPLACED SKIN ON MID LOCATION IAW SRM 51-40-11 &SDR DALA2016030401646Skin · delaminatedDELAMINATED UPPER SURFACE ON OTBD GUIDE VANE AT RT WING INBD FLAP. OTBD GUIDE VANE AT RT WING INBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR II.SDR SRXR2016F00069Fitting · gougedRIGHT INBD MID FLAP INBD SPHERICAL BEARING FITTING IS GOUGED ABOVE BEARING REF NRC A026313, REPAIR WAS ACCOMPLISHED IAW EA 747-5753-39-A6074.SDR SRXR2016F00068Bearing · gougedRIGHT INBD MID FLAP, INBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED IAW VT-SAA EA 747-5753-39-A6074 I/R AND FAA APPROVED 8110-3.SDR SWIA201641979Skin · chafedTHE LT INBD FLAP VANE L/E, CENTER VANE CAP CHAFED. REPLACED THE LT INBD FLAP VANE L/E, CENTER VANE CAP IAW SRM AND STS EA.SDR DALA2016030301790Nut · corrodedNR 6 WING FLAP NUT AND SCREW BALL HAS RUST, BROWN RESIDUE ON BALLSCREW. REPLACED NR 6 WING FLAP BALL SCREW REF AMM 27-51-21.SDR SWAA2016030449648Flap · delaminatedRIGHT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.SDR FDEA201603020804Panel · damagedPANEL RACK ZONE 60 RT WING INBD FLAP PANEL HAS TOOLING MARK ON AFT END OF PANEL, BETWEEN SCREW HOLES. COMPLIED WITH EA F-5750-T0323339 PT 1 DATED 02 18 16. WINGS, FLIGHT SURFACES, RT WING MAIN FLAP TOOLING MARK & BLEND. REF FAA FORM 8100-9 DATED 02 11 2016 SDR FDEA201603020766Bracket · corrodedRIGHT INB FLAP, OTBD HINGE FWD, ACTUATOR ATTACHMENT INBD LUG BORE, FOUND CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0323807 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201603020765Bracket · corrodedRIGHT INBD FLAP, OTBD HINGE FWD, ACTUATOR ATTACHMENT OTBD LUG BORE, FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0323807 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
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