N733FD
Service difficulty reports · 203
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 = 'N733FD' 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 = 'N733FD' 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 07FDEA04258Skin · delaminatedCORROSION AND DELAMINATION FOUND AT RT WING TE PANEL ASSY TO PREVIOUS REPAIRS REPAIR PERFORMED BY DAMAGE REMOVAL, BONDING REPAIR AND INSTALLING OF NEW ANGLES AND DOUBLERS IAW EA 6-5720-112455 AND RAS/BAE/1003755/2006 ISS A.SDR 07FDEA04256Window Frame · corrodedFOUND CORROSION AT LT SLIDING WINDOW IN 2 AREAS REPAIR PERFORMED BY BLEND OUT THE CORROSION AND NDT FOR CRACK FREE IAW EA 6-5612-112518 AND RAS 054295/005/2007.SDR 07FDEA04255Skin Panel · corrodedCORROSION FOUND UNDER LT WING TIP STATIC DISCHARGER NR 1. REPAIR PERFORMED BYBLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112474 AND RAS/FOK/178/2007 ISS A.SDR 07FDEA04254Skin Panel · corrodedCORROSION FOUND UNDER RT WING TIP STATIC DISCHARGER NR 1 AND NR 2 REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING A PATCH IAW EA 6-5730-112504 AND RAS/FOK/179/2007 ISS A.SDR 07FDEA04253Skin · wornFOUND ELONGATED HOLES ON RT WING BOTTOM SKIN AFT OF REAR SPAR. REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A.SDR 07FDEA04252Skin · wornFOUND ELONGATED HOLES ON LT WING BOTTOM SKIN AFT OF REAR SPAR REPAIR PERFORMED BY OVERSIZING AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY EA 6-2910-112501 AND RAS/BAE/1005314/2007 ISS A.SDR 07FDEA04196Diaphragm · dentedFOUND DENTS AND NICKS IN DIAPHRAGM C 53-54, TR1-2RT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW EA 6-5315-112500 AND RAS 053448/012/2007 ISS A .SDR 07FDEA04195Diaphragm · dentedFOUND DENTS AND NICKS IN DIAPHRAGM C 48-49, TR2-3 LT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING A DOUBLER IAW EA 6-5315-112500 AND RAS 053448/012/2007 ISS A .SDR 07FDEA03596Rib · chafedFOUND CHAFING MARK ON LT WING INTERMEDIATE RIB AT WIAX 21.9. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5751-112495 AND RAS/BAE/1005322/2007 ISS A.SDR 07FDEA03594Fitting · chafedDEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A.SDR 07FDEA03593Fitting · chafedDEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A.SDR 07FDEA03402Floorbeam · corrodedFOUND CORROSION ON CARGO FLOOR STRUCTURE ANGLE SECTION FRAME 60, Y-1470, RHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA03401Floorbeam · corrodedCORROSION ON CARGO FLOOR CROSSBEAM FRAME 56 AND 58, Y-800, RHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.SDR 07FDEA03400Floorbeam · corrodedCORROSION ON CARGO FLOOR CROSSBEAM FRAME 62, AD TO Y800, LHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.SDR 07FDEA03399Floorbeam · corrodedCORROSION ON CARGO FLOOR CROSSBEAM FRAME 63, Y-500 TO Y-800, RHS. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.SDR 07FDEA03398Skin · chafedCHAFING MARK (18 BY 17 MM) FOUND AT WING L/E SKIN RT BETWEEN TRACK 3 AND WOFX-48.9. REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE IAW EA 6-5741-112506 AND RAS/BAE/1005353/2007 ISSUE A.SDR 07FDEA03210Skin · chafedABRASION FOUND NOSE SKIN OF RT SLAT NR 2 RIB 21-22. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5743-112508 AND RAS/FOK/189/2007 ISS "A".SDR 07FDEA03209Stringer · corrodedFOUND CORROSION ON STRG 56 RT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-112511 AND RAS/DATLS/003803/2007 ISS "A".SDR 07FDEA03208Stringer · corrodedFOUND CORROSION ON STRG 56 LT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-112511 AND RAS/DATLS/003803/2007 ISS "A".SDR 07FDEA03207Stringer · corrodedFOUND CORROSION ON STRG. 56 LT, FRAME 57.3-61. REPAIR PERFORMED BY REMOVAL OF CORROSION AND ROTO TEST IAW EA 6-5317-112511 AND RAS/DATLS/003803/2007 ISS "A".SDR 07FDEA03206Skin · chafedFOUND DEEP CHAFING MARKS IN LOWER SKIN OF TRIM TANK CENTER BOX UNDER THE WATER DRAIN INTAKE, INSIDE THE CENTER BOX. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5511-112507 AND RAS/CASA/5733/2007 ISS "A".SDR 07FDEA02992Frame · damagedFOUND SCRATCHED AND DENTED RUN OUT OF FRAME 74 AT P'26-27, RHS. REPAIR PERFORMED BY REWORK IAW EA 6-5318-112466 AND RAS/DAHAM/4022689/2007 ISSUE "A".SDR 07FDEA02981Beam · corrodedCORROSION ON FWD CARGO DOOR SILL BEAM AT FRAME LOCATIONS 25 AND 25A. REPAIR PERFORMED WITH CUTOUT OF UPPER FLANGE AND INSTALLATION OF A MACHINED ANGLE IAW TD/K7/S1/08107/2007 IN EA 6-5313-112452, APPROVED BY RAS/DABRE/7008107/2007 ISSUE "B".SDR 07FDEA02979Attach Fitting · corrodedCORROSION ON INNER SIDE OF LT ELEVATOR ATTACH FITTING NR 4. REPAIR PERFORMED BY REMOVING CORROSION AND FLAP PEENING OF REWORKED AREA IAW RAS/CASA/5708/2007 ISSUE: A AND EA 6-5520-112509.SDR 07FDEA02976Structure · corrodedSTRUCTURE CORRODED BETWEEN C65- 70, P 56-57 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02951Fitting · corrodedCORROSION ON CARGO DOOR CORNER FITTING C 25A REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02950Fitting · corrodedCORNER FITTING FWD CARGO DOOR C 20 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02949Stiffener · corrodedCORROSION ON STIFFENER C12-12A LAVATORY SERVICE BOX PANEL REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02948Frame · corrodedCORROSION ON FRAME C 12-12A LAVATORY BOX PANEL REPAIR PERFORMED B REPLACEMENT OF PART.SDR 07FDEA02947Skin · dentedSLAT 32 RT DENT IN SKIN, RIB 48 DENT IS ACCEPTABLE AS IT IS, FASTENER CHANGED TO TO NAS1739E5, APPROVED BY EA 6-5740-112472 AND RAS/FOK/183/2007 ISS A.SDR 07FDEA02946Spar · crackedCRACKS FOUND ON CENTER SPAR WEB AND DOUBLER C44 (AROUND HOLE 1 (LT) ,5 (LT) , 8 (RT)) REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND DOUBLER CUT-OUT IAW SB A300-53-242, APPROVED BY EA 6-5710-112510 AND RAS 053726/005/2007 ISS A.SDR 07FDEA02945Beam · corrodedCORROSION ON AFT CARGO DOOR SILL BEAM, C59-62 REPAIR PERFORMED BY REPLACEMENT OF UPPER FLANGE OF SILL BEAM IAW SRM 53-17-18 AND DRAWING 17R53970133, APPROVED BY EA 6-5317-114839 AND RAS/DATLS/0003813/2007 ISS B.SDR 07FDEA02944Attach Fitting · crackedCRACK IN ATTACHMENT FITTING FOR CROSSBEAM C62. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02908Attach Fitting · damagedIMPACT DAMAGE TO LT MLG FITTING LUG REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW SRM 51-73-10, APPROVED BY EA 6-5751-112498 AND RAS/BAE/1005258/2007 ISS A.SDR 07FDEA02920Beam · corrodedCORROSION ON BULK CARGO DOOR SILL BEAM REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02919Beam · corrodedSEVERAL CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM, OUT OF LIMIT IAW SRM 53-10-00. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10, SRM 53-17-18 FIG 207 AND DRAWING R539-70133-000.SDR 07FDEA02918Crossbeam · corrodedFOUND CORROSION ON CROSSBEAM C 61 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02917Crossbeam · corrodedCORROSION ON CROSSBEAM C61 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA02912Stringer · corrodedCORROSION ON STRINGER P56 RT, C63-69 AND P56 LT, C65-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.SDR 07FDEA02910Floor Support · corrodedCORROSION ON FLOOR SUPPORT CC11-14, Y232 SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207.SDR 07FDEA02909Floor Support · corrodedCORROSION ON SUPPORT FLOOR, C12A-15A RT, Y-1959 SPLICE REPAIR PERFORMED IAW. SRM 53-12-15 FIG 207.SDR 07FDEA02907Skin · corrodedCORROSION FOUND ON BULK CARGO DOOR CUT OUT INTERNAL DOUBLER REPAIR PERFORMED BY BLEND OUT THE CORROSION AND FLAP PEENING IAW EA 6-5317-112502 AND RAS/DATLS/0003796/2007 ISS A.SDR 07FDEA02906Structure · chafedSCRUB MARKS ON RT AFT EMERGENCY EXIT CROSS SHEET REPAIR PERFORMED BY BLEND OUT IAW SRM 51-73-10, APPROVED BY EA 6-5316-112503 AND RAS/DAHAM/4022567/2007 ISS A.SDR 07FDEA02810Angle · corrodedANGLE FRONT SIDE AND L-SHEET REARSIDE AT FR 92 ARE CORRODED REPAIR IN ACCORDANCE WITH EA 6-5319-112453 AND RAS/DAHAM/4022472/2007 ISSUE "B" PERFORMED.SDR 07FDEA02746Crossbeam · corrodedAFTER BLENDING CORROSION ON CROSSBEAM C67 RT, Y-1200 WAS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.SDR 07FDEA02742Support · crackedCRACKED SUPPORT STRUT BETWEEN C77-78 AT P'48 RT, SHOWN IN SRM53-18-18/FIG 5/ITEM 70. REPAIR PERFORMED BY REPLACEMENT OF SUPPORT STRUT IAW SRM 51-72-10.SDR 07FDEA02741Stringer · corrodedCORRODED STRINGER P'53 IN FWD CARGO COMPARTMENT BETWEEN C28-29. REPAIR PERFORMED BY REPLACEMENT IAW SRM 53-10-14/FIG 201.SDR 07FDEA02692Angle · corrodedCORRODED PROFILE ANGLE FOUND BETWEEN C63-67, RT. REPAIR PERFORMED BY BLEND OUT, REMAINING THICKNESS WAS OUT OF LIMIT AND PART IS REPLACED.SDR 07FDEA02691Web · crackedSEVERAL CRACKED WEBS FOUND BETWEEN TRACKS 1-2 AND 3-4 LT/RT AT C47. WEB P/N: A538-32100 A538-32103. REPAIR PERFORMED BY DRILLING CRACK STOP HOLES AND INSTALLING DOUBLERS IAW RAS 053425/005/2007, ISSUE "A" AND EA 6-5315-112499.SDR 07FDEA02690Skin · corrodedCORROSION FOUND ON EXTERNAL STRAP (P/N: A539-78233-200) NEAR C69 AND P'47, RT. REPAIR PERFORMED BY BLEND OUT CORROSION, REMAINING THICKNESS OUT OF LIMIT, APPROVED BY RAS/DAHAM/4022567/2007 ISSUE "A" AND EA 6-5317-112473.
Back to N733FD