N749FD
Service difficulty reports · 180
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 = 'N749FD' 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 = 'N749FD' 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 07FDEA04597Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 4-5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04596Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04595Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04594Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 11 REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04593Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04592Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 1-2, P4-6 REPAIR PERFORMED BY BLEND OUT CORROSION, REPAIR IAW SB 57-6047, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04591Hinge Fitting · corrodedFOUND CORROSION ON LT THS HINGE FITTING NR 2. REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTING THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A.SDR 07FDEA04590Hinge Fitting · corrodedFOUND CORROSION ON LT THS HINGE FITTING NR 7. REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTING THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A.SDR 07FDEA04589Hinge Fitting · corrodedFOUND CORROSION ON LT THS HINGE FITTING NR 1 REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTING THE AREA IAW EA 6-5516-106523 AND RAS/CASA/5537/2007 ISS A.SDR 07FDEA04588Rib · corrodedFOUND OLD REPAIR ON RT WING BOTTOM SKIN RIB 9 UNDER JOINT STRAP WITH NEW CORROSION AND FINDINGS REPAIR PERFORMED BY CORROSION BLEND OUT, NDT FOR CRACK FREE AND REPROTECTING THE AREA IAW EA 6-5720-106519.SDR 07FDEA04534Plate · delaminatedDELAMINATION ON LT WING OUTER SHROUD BOX FLAP DEFLECTOR PLATE, AROUND THE ROLLER SUPPORT. REPAIR PERFORMED BY REMOVING DAMAGED PLIES AND INSTALLING REPAIR PLIES USING PRINCIPLES OF SRM 51-77-12/PARA.2A(3), ALL IAW EA 6-5755-106530 AND RAS/BAE/1005093/2007 ISSSDR 07FDEA04518Stiffener · corrodedFOUND CORROSIONN ON T-STIFFENER C91. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA04517Skin Panel · corrodedFOUND ON LT OUTER WING ON MANHOLE FLANGE RIB 23-24 CORROSION. REPAIR PERFORMED BLEND OUT CORROSION IAW SRM 57-20-12 PARA 4 A, NDT FOR CRACK FREE IAW EA 6-5720-106525 AND RAS//BAE/1005053/2007 ISS A.SDR 07FDEA04516Skin Panel · damagedFOUND OLD REPAIR ON RT OUTER WING AT FASTENER HOLE 939, RIB 9-10 IN BAD CONDITION. REPAIR PERFORMED BY OVERSIZING THE HOLE AND INSTALLING NEW TAPER OK IAW EA 6-5720-106520 AND RAS/BAE/0564/2003 ISS B.SDR 07FDEA04515Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 20-21. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005302/2007 ISS A.SDR 07FDEA04514Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 13-14. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005302/2007 ISS A.SDR 07FDEA04513Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, FWD OF FRONT SPAR. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A.SDR 07FDEA04512Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, REAR SPAR AND AFT REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A.SDR 07FDEA04510Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 11-12, P15-16. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005301/2007 ISS A.SDR 07FDEA04505Spar · crackedFOUND CRACKS IN SEVERAL HOLES ON CENTER SPAR WEB C 44 REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL, BUSH AND NEW FASTENER INSTALLTION IAW EA 6-5710-106488 AND RAS 052365/022/2007 ISS A.SDR 07FDEA04503Skin Panel · corrodedFOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5. REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND INSTALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A.SDR 07FDEA04502Skin Panel · corrodedFOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5 REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND INSTALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A.SDR 07FDEA04501Skin · corrodedFOUND CORROSION ON AFT RUN OUT OF TOP SKIN PANEL NR 2, RT WING WITH ADDITIONAL CRACK FINDING AFTER CORROSION REMOVAL REPAIR PERFORMED BY CUT OUT THE DAMAGE AND INSTALLING A REPAIR DOUBLER IAW EA 6-5720-106529 AND RAS/BAE/1005083/2007 ISS A.SDR 07FDEA04500Plate · delaminatedFOUND DELAMINATION ON LT WING INNER SHROUD BOX DEFLECTOR PLATE AROUND ROLLER SUPPORT REPAIR PERFORMED BY BONDING REPAIR IAW EA 6-5755-112536 AND RAS//BAE/1005280/2007 ISS A.SDR 07FDEA04495Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-9 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR 07FDEA04494Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR 07FDEA04493Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-10 AND 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR 07FDEA04492Skin · chafedFOUND AT RT NR 1 SLAT SEVERAL CHAFING MARKS ON LOWER OUTBOARD SKIN PANEL. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING AN EXTERNAL DOUBLER IAW EA 6-5742-112470 AND RAS/FOK/174/2007 ISS A.SDR 07FDEA04444Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR U, NR I AND NR H WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04443Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING RT VERTICAL FLANGE FITTING HOLE NR A, NR E, NR F, NR G, NR P, NR Q AND NR S WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04442Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR G, NR S AND NR T WITH CORROSION. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CORROSION REMOVAL IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04441Fitting · corrodedFOUND AT C47 INTERNAL CENTER WING LT VERTICAL FLANGE HOLE NR I AND NR U WITH CORROSION. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND CUT EXTERNAL FITTING AT HOLE NR I IAW SB 57-6049 IAW EA 6-5710-106533 AND RAS 052780/019/2007 ISS A.SDR 07FDEA04439Angle · corrodedFOUND CORROSION AT PICK UP ANGLE C40-41LT REPAIR PERFORMED BY REPLACEMENT OF PICK UP ANGLE AND SPLICING WITH EXTERNAL REPAIR ANGLE AND INTERNAL STRAP IAW EA 6-5315-106521 AND RAS 052466/027/2007 ISS A.SDR 07FDEA04438Fitting · corrodedFOUND AT LT MLG FWD PINTLE PICK-UP FITTING TOOL MARKS AND BORE AND FASTENER HOLE CORROSION. REPAIR PERFORMED BY REPLACEMENT OF FWD PICK UP FITTING IAW DRAWING R572-40266. REPLACEMENT OF TENSION FITTING AND REWORK OF CORROSION IN FASTENER HOLE AND FREEZE BUSHSDR 07FDEA04436Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN AT RIB 7-8, CENTER SPAR STRINGER 13 REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5720-112460 AND RAS/BAE/1005212/2007 ISS A.SDR 07FDEA04435Skin · corrodedFOUND CORROSION ON RT WING BOTTOM SKIN RIB 1-2 IN FRONT OF FRONT SPAR NEAR TRACK NR 1 REPAIR PERFORMED BY REWORK OF CORROSION IAW EA 6-5720-112461 AND RAS/BAE/1005290/2007 ISS A.SDR 07FDEA03494Skin · damagedDURING ACCOMPLISHMENT OF EO 6-5750-7-500 FOUND AT RT INBOARD FLAP LOWER SKIN NUMEROUS HOLES WITH CRACK, TOOLING MARKS AND MISDRILLED. REPAIR PERFORMED BY RAISING THE HOLES UNTIL REMOVAL OF DAMAGES IAW EA 6-5752- 106527 AND RAS/FOK/141/2007 ISS A.SDR 07FDEA03492Skin · damagedDURING ACCOMPLISHMENT OF EO 6-5750-7-500 FOUND AT LT INBOARD FLAP LOWER SKIN NUMEROUS HOLES WITH CRACK, TOOLING MARKS AND MISDRILLED. REPAIR PERFORMED BY RAISING THE HOLES UNTIL REMOVAL OF DAMAGES IAW EA 6-5752- 106527 AND RAS/FOK/140/2007 ISS A.SDR 07FDEA03491Door · misrepairedOLD EXISTING REPAIR AT LT NLG DOOR NOT CONFORM TO TD 942.045310/008/2006 (MATERIAL THICKNESS 1,3MM INSTEAD OF 1,6MM) REPAIR RENEWED IAW EA 6-5282-106514 AND RAS 045310/014/2006.SDR 07FDEA03488Skin · corrodedFOUND CORROSION ON INNER SKIN DOUBLER C10A-11, P 54RH-54LH. REPAIR PERFORMED BY REMOVAL OF CORROSION, SMOOTH BLEND OUT AND INSTALLING OVERSIZE FASTENER IAW EA 6-5312-114837 AND RAS 053782/014/2007.SDR 07FDEA03483Skin Panel · corrodedFOUND ON WING BOTTOM SKIN LT, RIB 8 AN OLD CORROSION REPAIR AROUND HOLE 585 (DRAWING R571-401410 ) WITHOUT ANY DOCUMENTATION. REPAIR PERFORMED BY REWORK OF AREA AND FASTENER REPLACEMENT IAW EA 6-5720-106534 AND RAS/BAE/1005114/2007 ISS A.SDR 07FDEA03480Skin Panel · wornFOUND ELONGATED HOLES ON BOTTOM SKIN LT OUTER WING RIB 8 REPAIR PERFORMED IAW R571-50532 (REAM UP AND BUSHING INSTALLATION), APPROVED BY EA 6-5720-106531 AND RAS/BAE/1005033/2007 ISS A.SDR 07FDEA02991Skin Panel · chafedCHAFING MARKS WERE FOUND ON RT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORMED BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A".SDR 07FDEA02990Skin Panel · chafedCHAFING MARKS WERE FOUND ON LT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORMED BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A".SDR 07FDEA02989Fitting · damagedFOUND IN MANHOLE FITTING AN EXISTING POCKED REPAIR IN BAD CONDITION AT C38.2. REPAIR PERFORMED BY INSTALLING NEW FILLER IAW EA 6-5314-112469, APPROVED BY RAS/DABRE/70008163/2007 ISSUE "A".SDR 07FDEA02987Floorbeam · misrepairedFOUND A WRONG PERFORMED OLD TOP CAP BEAM REPAIR IN AFT CARGO COMPARTMENT, C61, RHS. REPAIR PERFORMED BY INSTALLING NEW SPLICE REPAIR IAW SRM 53-10-15 / FIG 207.SDR 07FDEA02986Skin Panel · corrodedFOUND CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-201 AT C39-40, P'28-29, RHS. REPAIR PERFORMED BY REWORK AND INSTALLING INTERNAL REPAIR DOUBLER IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A".SDR 07FDEA02985Skin Panel · corrodedEXTERNAL CORROSION AT UPPER FWD CORNER ON SKIN PANEL A538-12189-200 AT C39-40, P28-29, LHS. REPAIR PERFORMED BY REWORK IAW EA 6-5315-112437 AND RAS: 052738/008/2007 ISSUE "A".SDR 07FDEA02984Valve · corrodedHEAVY CORROSION ON SUPPORT VALVE BETWEEN C16A AND C17. REPAIR PERFORMED BY INSTALLING NEW SUPPORT VALVE IAW SRM 51-72-10.SDR 07FDEA02983Floorbeam · corrodedOLD WRONG PERFORMED TOP CAP BEAM REPAIR IN FWD CARGO COMPARTMENT, C30, RT. REPAIR PERFORMED BY INSTALLING NEW TOP CAP BEAM REPAIR IAW SRM 53-10-15/FIG 207.
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