N727FD
Service difficulty reports · 185
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N727FD' AND registry_match = 'registration' 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 n_number = 'N727FD' AND registry_match = 'registration' 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 07FDEA03373Skin · misrepairedFOUND OLD FLUSH REPAIR ON LT SLAT NR 2 LOWER SKIN, BETWEEN TRACK 5-6 WITH POOR EDGE MARGIN. FLUSH DOUBLER REPAIR PERFORMED IAW EA 6-5743-95844 AND RAS/FOK/264/2005 ISSUE C.SDR 07FDEA03371Skin · misrepairedFOUND OLD REPAIR ON NOSE SKIN OF RT CENTER FLAP, RIB 18-20, NOT CONFORM TO SRM 57- 50-00/FIG 208 (ONE RIVET ROW ON EACH SIDE MISSING). REPAIR RENEWED IAW SRM 57-50-00/PB 200 / FIG 208.SDR 07FDEA03368Skin · damagedFOUND TWO OLD REPAIRS ON RT SLAT NR 1 IN BAD CONDITION, BETWEEN RIB 10-13, L/E AREA. ONE FLUSH DOUBLER REPAIR BETWEEN RIB 10-13 PERFORMED IAW EA 6-5740-95838 AND RAS/FOK/265/2005 ISSUE A.SDR 07FDEA03367Skin · unknownUNKNOWN REPAIR FOUND AT LT SLAT NR 2 NEAR JACKSCREW NR 3 ATTACH FITTING. REPAIR WAS RENEWED WITH DOUBLER IAW EA 6-5743-92228 AND RAS/FOK/279/2005 ISSUE A.SDR 07FDEA03361Skin · unknownTEMPORARY REPAIR FOUND ON LT INNER FLAP, UPPER SKIN AT RIB 27, STRG 2.1-2.2 (RAS/FOK/146/2005 ISS A, WITH 5 FC). DOUBLER REPAIR RENEWED IAW EA 6-5750-95842 AND RAS/FOK/260/2005 ISSUE C.SDR 07FDEA03360Skin · damagedON OLD REPAIR ON NOSE SKIN, INNER RIB 7-9 OF SLAT NR 2 FOUND MISDRILLED HOLE. AFTER REMOVAL OF SKIN INSERT FOUND THREE RIBS DAMAGED. FLUSH SKIN REPAIR RENEWED IAW EA 6-5740-95837 AND RAS/FOK/267/2005 ISSUE A.SDR 07FDEA03359Skin Panel · wornELONGATED HOLES IN LT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN, RIB 8. REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALLING BUSHES IAW DRW, R571- 50532, APPROVED BY EA 6-5720-95853 AND RAS/BAE/1002114/2006 ISSUE A.SDR 07FDEA03358Door Frame · crackedCRACKED FRAME SEGMENT ON BEAM 8 OF AFT CREW DOOR RT. REPAIR PERFORMED BY REPLACEMENT OF FRAME SEGMENT IAW SRM 51-72-10.SDR 07FDEA03357Frame · chafedFOUND WEAR MARK ON INNER FLANGE OF FRAME 38.1 BETWEEN STRG 14-15 RT. REPAIR PERFORMED BY INSTALLING INTERNAL ANGLE AND ADDITIONAL SHIM AS PER PRINCIPLES GIVEN IN SRM 53-10-13/FIG 202, APPROVED EA 6-5314-95855 AND RAS/DABRE/7005992/2005.SDR 07FDEA03356Beam · corrodedFOUND CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59A-60A AND FRAME 63-63A. REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT INSPECTION FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-92211 AND RAS/DAHAM/4020122/2005 ISSUE A.SDR 07FDEA03355Tee Fitting · corrodedFOUND CORROSION ON T-SECTION BETWEEN STRG 50-55 LT AT FRAME 39. ON PRESSURE BULKHEAD, SMALL CRACKS HAVE BEEN FOUND. THE REPAIR CONSISTS IN CUTTING OUT THE TEE AND INSTALLING A NEW TEE WITH AN ANGLE AND A STRAP. A SPECIFIC REPAIR HAS BEEN INSTALLED FOLLOWINGSDR 07FDEA03354Stiffener · corrodedFOUND CORROSION ON T-SECTION BETWEEN STRG 50-55 LT AT FRAME 39. ON PRESSURE BULKHEAD, SMALL CRACKS HAVE BEEN FOUND. THE REPAIR CONSISTS IN CUTTING OUT THE TEE AND INSTALLING A NEW TEE WITH AN ANGLE AND A STRAP. A SPECIFIC REPAIR HAS BEEN INSTALLED FOLLOWINGSDR 07FDEA03353Sill · damagedCORROSION, MISDRILLED HOLES AND CRACKS ON THE UPPER FLANGE OF THE FWD CARGO DOOR SILL BEAM BETWEEN FRAME 20-26. REPAIR PERFORMED BY REPLACEMENT OF FWD CARGO DOOR SILL BEAM UPPER FLANGE PER DRW R537-06091 ISSUE B WITH DEVIATIONS NOTED IN RAS/DABRE/7005974/2005SDR 07FDEA03352Fitting · corrodedCORROSION ON CORNER FITTINGS AT FRAME 58, STRG 44 LT AND RT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF BOTH FITTINGS LT AND RT IAW SRM 51-72-10.SDR 07FDEA03351Fitting · corrodedCORROSION ON CORNER FITTING AT FRAME 63, STRG 44 LT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW SRM 51-72-10.SDR 07FDEA03350Floorbeam · corrodedCORROSION ON CROSSBEAM FRAME 67 RT, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.SDR 07FDEA03349Fitting · dentedDENTED MILLED CORNER FITTING AT C 25, STRG 41-43 LT, OUT OF LIMIT IAW SRM 53-10-00. REPAIR PERFORMED BY REPLACEMENT OF CORNER FITTING IAW SRM 51-72-10.SDR 07FDEA03348Floorbeam · misrepairedOLD REPAIR AT CROSSBEAM FRAME 63 IS NOT PERFORMED IAW SRM 53-10-15/FIG 207. SPLICE REPAIR RENEWED IAW SRM 53-10-15/FIG 207.SDR 07FDEA03347Floorbeam · corrodedCORROSION ON TOP CAP BEAM FRAME 66 RHS, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-74-10.SDR 07FDEA03345Floorbeam · corrodedCORROSION AT TOP CAP BEAM FRAME 58 LT AND RT. SPLICE REPAIR ON TOP CAP BEAM FRAME 58 LT AND RT PERFORMED IAW SRM 53-10-15/FIG 207.SDR 07FDEA03344Shear Plate · crackedCRACKED SHEAR PLATE AT FRAME 79, STRG 26 LT AND RT. REPAIR PERFORMED BY INSTALLATION OF NEW PART IAW SRM 51-72-10.SDR 07FDEA03343Skin Panel · chafedFOUND CHAFING MARK ON INTERNAL SURFACE OF RT WING TOP SKIN PANEL NR 3 BETWEEN RIB 27-28 NEAR FRONT SPAR. REPAIR PERFORMED BY BLEND OUT, HFEC INSPECTION FOR CRACK FREE AND FLAP PEENING IAW EA 6-5720-95843 AND RAS/BAE/1001878/2005 ISSUE A.SDR 07FDEA03342Skin Panel · corrodedFOUND CORROSION ON TOP SKIN PANEL NR 3 LT, NEAR RIB 25-28 AT T/E, OUT OF SRM LIMIT. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT OF AFFECTED FASTENERS AND FLAP PEENING IAW EA 6-5720-92224 AND RAS/BAE/1001906/2005 ISSUE A.SDR 07FDEA03341Skin · damagedDENT WITH A CHAFING MARK WAS FOUND ON THE RT SLAT NR 1, LOWER SKIN T/E HONEYCOMB TAIL, NEAR RIB 21-23. REPAIR PERFORMED BY SKIN INSERT AND REPAIR PATCH IAW TD FOK/273/2005 ISS B, APPROVED BY EA 6-5742-95845 AND RAS/FOK/237/2005 ISS. B.SDR 07FDEA03340Cover · corrodedCORROSION ON TORSION BOX COVER PLATE AT FRAME 57, STRG 15 RT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW EA 6-5316-92212 AND RAS/DAHAM/4020097/2005 ISS B.SDR 07FDEA03339Frame · corrodedCORROSION ON FRAME 57 INNER FLANGE AT STR 14 RT. REPAIR PERFORMED BY REWORK IAW EA 6-5316-92212 AND RAS/DAHAM/4020097/2005 ISS B.SDR 07FDEA03338Skin · misrepairedFOUND OLD INTERNAL DOUBLER WITH CUT OUT ACC SRM IN OUTER SKIN AT FRAME 19, STRG 17 RHS. INNER DOUBLER IS NOT COMPATIBLE WITH PTOF CONVERSION. REPAIR PERFORMED BY RENEWING INTERNAL DOUBLER BY AN EXTERNAL ONE IAW DWG BEA 14095229-02 AND RAS/DABRE/70059934/200SDR 07FDEA03337Rib · damagedLT SLAT 1 TRAILING EDGE LOWER SKIN DAMAGE AT INNERRIB 23, AREA AT T/E PROFILE. REPAIR IS PERFORMED WITH SKIN INSERT AND REPAIR PATCH IAW TD FOK/262/2005 ISSUE B.SDR 07FDEA03334Fitting · crackedFOUND CRACK IN HOLES H, G, Q, S AND T OF ANGLE FITTING IN CENTER WING BOX AT FRAME 47 RT DURING SB A300-57-6086, -6050, AND -6049. REPAIR PERFORMED BY OVERSIZING THE HOLES IN ALL LAYERS ON A STEP BY STEP BASIS, ROTO TEST INSPECTION AT EACH STEP AND INSTALLINGSDR 07FDEA03333Fitting · crackedFOUND CRACK IN HOLE G/T OF ANGLE FITTING IN CENTER WING BOX AT FRAME 47 LT DURING SB A300-57-6086, -6050, AND -6049. REPAIR PERFORMED BY OVERSIZING THE HOLES IN ALL LAYERS ON A STEP BY STEP BASIS, ROTO TEST INSPECTION AT EACH STEP AND INSTALLING OVERSIZED FSDR 07FDEA03332Floor Support · corrodedSTRONG CORROSION ON LONGERON (CABIN FLOOR STRUCTURE) BETWEEN FRAME 11 AND 14, Y730 LHS. REPAIR PERFORMED BY INSTALLING PROFILES IAW SRM 53-12-15 / FIG 207.SDR 07FDEA03329Structure · corrodedUPPER HOIST POINT OF DORSAL FIN IS DAMAGED BY EROSION. SURFACE REPAIRED AS PER GUIDELINES OF SRM 51-77-11 PARA 3 A., USING PASTE ADHESIVE AS PER SRM 51-77-10 PARA 5 B (1) IAW. EA 6-5318-92211 AND RAS/DAHAM/4020086/2005 ISS A.SDR 07FDEA03328Skin Panel · corrodedCORROSION SPOTS ON EXTERNAL SKIN PANEL BETWEEN FRAME 78-88, STRG 5 LT TO 5 RT. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC AND ROTO TEST INSPECTION, INSTALLING AN EXTERNAL REPAIR DOUBLER AND FLAP PEENING IAW TD/K4/S1/20147/2005/A APPROVED BY EA 6-5319-92222 ANSDR 07FDEA03327Coupling · corrodedTHE COUPLING BETWEEN LT FWD AND AFT DORSAL FIN CONNECTING STRIPS IS CORRODED. REPLACEMENT OF LHS AREA CONNECT STRIPS COUPL, C76, IAW SRM 51-72-10.SDR 07FDEA03326Skin · misrepairedWASHERS USED BY OLD REPAIR ON RUDDER ARE NOT CONFORM TO SRM 55-41-12/PB 201/FIG 216. DELAMINATION, CORRODED AND TOO SHORT FASTENERS. DELAMINATION OF GFRP FITTING CONNECTION REPAIR PERFORMED AT ALL HINGE FITTINGS IAW SRM 55-41-12/FIG 216.
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