N745FD

Service difficulty reports · 216

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 = 'N745FD' 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.

SDR 08FDEA01740Cover · corrodedFOUND CORROSION ON COVER PLATE C 73, P9 LT REPAIR PERFORMED BY REMOVING CORROSION IAW SRM 51-74-10, NDT FOR CRACK FREE, FLAP PEENING AND RENEWING THE RIVETS IAW RAS/EFW/9000027/2008 ISS B, APPROVED BY EA 6-5318-117153.May 3, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01739Skin · crackedFOUND ON LT ASA BOOSTER DOOR A CRACK IN HOLE FOR RUBBER STRIP ATTACHMENT. REPAIR PERFORMED BY CUT OUT AND INSTALLING A FILLER AND DOUBLER IAW, RAS/BAE/1006711/2008 ISS A, APPROVED BY EA 6-5751-117144.May 3, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA01694Skin · wornFOUND ELONGATED HOLES ON RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS/BAE/1006364/2008 ISS A AND EA 6-2900-114925.Apr 30, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA01693Skin · wornFOUND ELONGATED HOLES ON LT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS /BAE/1006364/2008 ISS A AND EA 6-2900-114925.Apr 30, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA01692Skin · wornFOUND ELONGATED HOLES ON LT/RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-29-6057, APPROVED BY EA 6-2900-114925.Apr 30, 2008 · N745FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA01691Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 5 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01690Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 4 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01689Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 3 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01688Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 3 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01687Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 4 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01686Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER 5 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53/401.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01685Spar · chafedCHAFING MARKS AND ABRASION ON NR 2 LT SPOILER OUTBOARD SPAR REPAIR PERFORMED BY CUT THE DAMAGED AREA AND INSTALLING A DOUBLER IAW RAS 70503484/017/2008 ISS, APPROVED BY EA 6-5771-115271.Apr 30, 2008 · N745FD · Airbus A300B4622R · SpoilersSDR 08FDEA01684Skin · damagedFOUND ELONGATED HOLE ON NOSE SKIN FOLDING NOSE RT SLAT NR 1. REPAIR PERFORMED BY REPLACEMENT OF SKIN IAW SRM 51-72-10, APPROVED BY EA 6-5742-115273.Apr 30, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01683Skin · misrepairedFOUND ON SLAT RT NR 1 FOLDING NOSE OLD REPAIR NOT ACCOMPLISHED IAW SB 57-6067 AND DRAWING R578-40005. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-57-6067, APPROVED BY EA 6-5742-115273.Apr 30, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01682Skin · misrepairedFOUND ON SLAT LT NR 1 FOLDING NOSE OLD REPAIR NOT ACCOMPLISHED IAW SB 57-6067 AND DRAWING R578-40005. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-57-6067, APPROVED BY EA 6-5742-115273.Apr 30, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01681Skin · crackedFOUND DURING PERFORMANCE OF EO 6-5750-7-5000 PT 4 SEVERAL CRACKED HOLES IN INNER FLAP RT, LOWER SIDE, REPAIR PERFORMED BY REPLACEMENT OF RT INNER FLAP IAW AMM 27-50-11 PB400.Apr 30, 2008 · N745FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA01612Spar · crackedCRACK FINDING ON LT PYLON NR 2 LOWER SPAR AT RIB 10. REPAIR PERFORMED BY CUTTING AREA AND INSTALLING A DOUBLER IAW DRAWING R546-10342 ISS A , APPROVED BY RAS/AS/0040/2008 AND EA 6-5451-115284.Apr 28, 2008 · N745FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA01563Angle · damagedFOUND DURING ACCOMPLISHMENT OF WIC 6-5310-7-5001 PART 2 SEVERAL FASTENER WITH LARGER DIAMETER AS REQUIRED IAW SB A300-53-6063. REPAIR PERFORMED BY REAM UP THE HOLES AND PERFORM REPAIR INSTRUCTION IAW SB A300-53-6048 AND -6063, APPROVED BY RAS 70504678/020/200Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01561Angle · damagedFOUND DURING ACCOMPLISHMENT OF WIC 6-5310-7-5001 PART 2 SEVERAL FASTENER WITH LARGER DIAMETER AS REQUIRED IAW SB A300-53-6063. REPAIR PERFORMED BY REAM UP THE HOLES AND PERFORM REPAIR INSTRUCTION IAW SB A300-53-6048 AND -6063, APPROVED BY RAS 70504678/020/200Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01559Structure · chafedFOUND CHAFING MARKS ON SLAT NR 3 TRACK 10 OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE DAMAGE AND INSTALLING AN EXTERNAL PATCH IAW RAS FOK/049/2008 ISS A, APPROVED BY EA 6-5744-117139.Apr 25, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01558Skin · damagedTOOLING MARK FOUND ON SKIN AT C 58-59, P 13 RT REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/EFW/9000021/2008 ISS B, APPROVED BY EA 6-5316-117141.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01557Skin · corrodedFOUND CORROSION ON SKIN C57 1-57.2, P21-22 LT REPAIR PERFORMED BY EXTERNAL DOUBLER INSTALLATION IAW RAS/EFW/9000024/2008 ISS B, APPROVED BY EA 6-5316-117143.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01556Structure · corrodedCORROSION AND LIGHTNING STRIKE FOUND ON RT WING TIP. REPAIR PERFORMED BY BLEND OUT AREA IAW RAS/FOK/037/2008 ISS A, APPROVED BY EA 6-5730-115275.Apr 25, 2008 · N745FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA01555Structure · corrodedCORROSION AND LIGHTNING STRIKE FOUND ON LT WING TIP (4 AREAS) REPAIR PERFORMED BY CUT OUT DAMAGED AREA 1 AND 4 AND INSTALLING AN EXTERNAL PATCH WITH SHIM, BLEND OUT AREA 2 AND 3 AND INSTALLING EXTERNAL PATCH UNDER STATIC DISCHARGER , APPROVED BY RAS/FOK/037/Apr 25, 2008 · N745FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA01553Structure · chafedFOUND CHAFING MARKS ON SLAT NR 1 RT, FOLDING NOSE AREA. REPAIR PERFORMED BY BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW RAS/FOK/032/2008 ISS A, APPROVED BY EA 6-5742-115274.Apr 25, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01552Structure · chafedFOUND CHAFING MARKS ON SLAT NR 1 LT, FOLDING NOSE AREA REPAIR PERFORMED BY BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW RAS/FOK/031/2008 ISS A, APPROVED BY EA 6-5742-115274.Apr 25, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01551Plate · corrodedFOUND CORROSION ON RUDDER LIGHTING PROTECTION PLATE RT SIDE. REPAIR PERFORMED BY REMOVAL OF CORROSION, LAMINATE THE DAMAGED AREA AND INSTALLING A NEW PLATE IAW RAS/DAHAM/4024150/2008 ISS A, APPROVED BY EA 6-5541-114926.Apr 25, 2008 · N745FD · Airbus A300B4622R · Rudder StructureSDR 08FDEA01550Plate · corrodedFOUND CORROSION ON RUDDER LIGHTING PROTECTION PLATE LT SIDE. REPAIR PERFORMED BY REMOVAL OF CORROSION, LAMINATE THE DAMAGED AREA AND INSTALLING A NEW PLATE IAW RAS/DAHAM/4024150/2008 ISS A, APPROVED BY EA 6-5541-114926.Apr 25, 2008 · N745FD · Airbus A300B4622R · Rudder StructureSDR 08FDEA01549Skin · damagedFOUND OLD LIGHTNING STRIKE REPAIR AT C 1-40 LT WITH BAD DOCUMENTATION. REPAIR PERFORMED BY CORRECTION IAW SRM 53-10-12 FIG 219 WITH 2 DEVIATION ON C8-9, P27LT. REPAIRED BY PERFORMING ROTO AND EC-TEST AND INSTALLING DAN5-6Y AND C11 P28 LT, WHICH WAS REPAIRED Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01548Frame · damagedFOUND DEFORMED FLANGE AT C 75, P26 RT REPAIR PERFORMED BY REWORK OUTER FLANGE TO ELIMINATE THE DEFORMATION, NDT FOR CRACK FREE IAW AS/EFW/9000019/2008 ISS A, APPROVED BY EA 6-5318-117150.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA01547Frame · damagedFOUND DEFORMED FLANGE AT C 74, P26-27 LT/RT REPAIR PERFORMED BY REWORK OUTER FLANGE TO ELIMINATE THE DEFORMATION, NDT FOR CRACK FREE IAW RAS/EFW/9000019/2008 ISS A, APPROVED BY EA 6-5318-117150.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA01546Sill · crackedCRACK FINDING ON C 60A-62 RT IN UPPER FLANGE OF AFT CARGO DOOR SILL BEAM REPAIR PERFORMED IAW SRM 53-17-18 WITH DEVIATION IN FASTENER USE (CHANGE FROM MS20426DD6 TO HL11VF5/NSA 5075-5) APPROVED BY RAS/EFW/9000020/2008 AND EA 6-5317-117138.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01545Angle · damagedFOUND ON C 12A PREVIOUSLY EMBODIED SB A300-53-6137, IMPROVMENT OF FITTING ON C12A, IN BAD CONDITION (ANGLE A536-10318-265. REPAIR PERFORMED IAW SRM 53-12-13 FIG 201 IAW RAS/70503839/019/2008 ISS A, APPROVED BY EA 6-5312-115285.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01544Stiffener · wornFOUND ON C12A PREVIOUSLY EMBODIED SB A300-53-6137, IMPROVEMENT OF FITTING ON C12A, IN BAD CONDITION (DAMAGED FASTENER, DENTS IN STIFFENER A536-10996-201. REPAIR PERFORMED BY REAM UP THE SEVERAL HOLES, INSTALL OVERSIZED FASTENER AND REPLACE STIFFENER IAW RAS/7Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01543Structure · wornFOUND ON LT INBOARD FLAP DURING ACCOMPLISHMENT OF SB A300-57-6100 SOME HOLES OVERSIZED. REPAIR PERFORMED BY VERIFICATION OF OVERSIZED HOLES IAW RAS/FOK/040/2008 ISS A, APPROVED BY EA 6-5752-115278.Apr 25, 2008 · N745FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA01542Fitting · crackedFOUND ON FWD CARGO DOOR HINGE FITTING AT C 23, A BROKEN ANTI-TWIST PLATE. REPAIR PERFORMED BY REMOVE THE BROKEN LOCKING DEVICE AND INSTALLING AN ANGLE BRACKET TO RESTORE THE LOCKING FUNCTION IAW RAS/DABRE/7009080/2008 ISS A, APPROVED BY EA 6-5313-115280.Apr 25, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA01541Bushing · corrodedFOUND CORROSION ON PYLON NR 2, RIB 12 OUTBOARD WING LUGS. REPAIR PERFORMED BY REPLACEMENT OF BUSHINGS IAW SRM 57-20-34 PB 200, APPROVED BY EA 6-5451-117148.Apr 25, 2008 · N745FD · Airbus A300B4622R · Wing, Attach FittingsSDR 08FDEA01540Bushing · corrodedFOUND CORROSION ON PYLON NR 2, RIB 12 OUTBOARD WING LUGS. REPAIR PERFORMED BY REPLACEMENT OF BUSHINGS IAW SRM 57-20-34 PB 200, APPROVED BY EA 6-5451-117148.Apr 25, 2008 · N745FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA01539Fitting · corrodedFOUND ON PYLON NR 2 CORROSION ON PYLON TO WING SHACKLES 6/7/8 OUT OF SRM 54-51-71 LIMIT. REPAIR PERFORMED BY SMOOTH BLEND OUT THE CORROSION, NDT FOR CRACK FREE IAW RAS/AS/0037/2008 ISS A, APPROVED BY EA 6-5451-117148.Apr 25, 2008 · N745FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA01415Structure · dentedFOUND DENT AND CORROSION SPOTS ON BULK CARGO DOOR, NEAR C 67, BEAM 5 REPAIR PERFORMED BY REWORK OF CORROSION IAW SRM 51-74-10 AND LET THE DENT AS IT IS, APPROVED BY RAS/DAHAM/4024431/2008 ISS B AND EA 6-5234-117140.Apr 15, 2008 · N745FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA01414Skin Panel · corrodedCOROSION FOUND ON SKIN PANEL, C39-40, P28-29 RT REPAIR PERFORMED IAW DRAWING R538-10690, APPROVED BY RAS 70503475/004/2008 AND EA 6-5315-115270.Apr 15, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01413Door Frame · crackedFOUND CRACK IN FRAME HEAD C61A OF AFT CARGO DOOR. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Apr 15, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA01281Structure · delaminatedWATER INGRESS FINDINGS DURING RUDDER THERMOGRAPHY INSPECTION -EO 6-5530-7-5004. REPAIR PERFORMED BY REMOVING OUTER SKIN AND CORE, DRY THE REPAIR AREA, REPLACE THE CORE AND PERFORM WET LAY UP- REPAIR IAW RAS/DAHAM/4024104/2008 ISS A, APPROVED BY EA 6-5540-1149Apr 3, 2008 · N745FD · Airbus A300B4622R · Rudder StructureSDR 08FDEA01280Attach Fitting · misalignedFOUND A CLIP AT C 76, P 33-34 LT WITH NOT ENOUGH EDGE DISTANCE. REPAIR PERFORMED BY MANUFACTURING AND INSTALLING OF NEW CLIP IAW RAS/EFW9000026/2008 ISS A, APPROVED BY EA 6-5318-117152.Apr 3, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA01279Attach Fitting · misalignedFOUND A CLIP AT C 76, P 33-34 RT WITH NOT ENOUGH EDGE DISTANCE. REPAIR PERFORMED BY MANUFACTURING AND INSTALLING OF NEW CLIP IAW RAS/EFW9000026/2008 ISS A, APPROVED BY EA 6-5318-117152.Apr 3, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA01246Floor Support · corrodedFOUND FLOOR SUPPORT CORRODED AT C11-13A, Y-730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Apr 2, 2008 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA01245Attach Fitting · damagedFOUND CLIP WITH MISDRILLED HOLES AT C70, P43 LT. REPAIR PERFORMED Y REPLACEMENT OF PART IAW SRM 51-72-10.Apr 2, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA01079Skin Panel · damagedDURING REMOVAL OF STRINGER 26 LT DRILLING MARK EXISTS BETWEEN C38.2-39. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 53-10-12 FIG 221.Mar 20, 2008 · N745FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA01078Fitting · corrodedFOUND CORROSION ON FITTING AT KRUEGER FLAP AREA LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Mar 20, 2008 · N745FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01077Fitting · corrodedFOUND CORROSION ON FITTING AT KRUEGER FLAP AREA RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Mar 20, 2008 · N745FD · Airbus A300B4622R · Leading Edge Devices
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