N730FD

Service difficulty reports · 213

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 = 'N730FD' 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 08FDEA01347Skin · delaminatedFOUND WATER INGRESS DURING THERMOGRAPHIC INSPECTION ON RUDDER RT SIDE. REPAIR PERFORMED BY REMOVING SKIN AND CORE, DRY THE AREA, PERFORM REPAIR IAW SRM 51-77-10 IAW RAS/DAHAM/4024380/2008 ISS A, APPROVED BY EA 6-5540-115259.Apr 8, 2008 · N730FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA01247Pan · crackedINNER PAN OF SLAT NR 1 FOLDING NOSE IS CRACKED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB A300-57-6067.Apr 2, 2008 · N730FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA01249Skin · corrodedFOUND CORROSION UNDER STATIC DISCHARGER SUPPORT PLATE, LT WING TIP. REPAIR PERFORMED BY REMOVE OF CORROSION AND INSTALLING A REPAIR PATCH IAW, RAS /FOK/047/2008 ISS A, APPROVED BY EA 6-5730-117164.Apr 2, 2008 · N730FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA01248Skin · damagedFOUND SKIN PLATE DETACHED AT C20A, P28 RT REPAIR PERFORMED BY INSTALLING A REPAIR DOUBLER IAW RAS/EFW/9000018/2008 ISS. B, APPROVED BY EA 6-5313-115242.Apr 2, 2008 · N730FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA00814Skin Panel · dentedFOUND DENT AT SKIN PANEL C21-22, P 36-37 LT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/DABRE/7008975/2008 ISS A, APPROVED BY EA 6-5313-115243.Mar 10, 2008 · N730FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA00655Seat Track · corrodedFOUND CORROSION ON SEAT TRACK C14-19, Y450. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 29, 2008 · N730FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00654Seat Track · corrodedFOUND CORROSION ON SEAT TRACK C15A-19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Feb 29, 2008 · N730FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00559Frame · chafedFOUND SEVERAL CHAFING MARKS ON INNER FLANGE OF FRAME C28, P 13-22 LT. REPAIR PERFORMED BY BLEND OUT THE AREAS AND NDT FOR CRACK FREE IAW RAS/DABRE/7008942/2008 ISS A, APPROVED BY EA 6-5314-115244.Feb 22, 2008 · N730FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA00558Frame · chafedFOUND SEVERAL CHAFING MARKS ON INNER FLANGE OF FRAME C28, P 9-12 LT. REPAIR PERFORMED BY BLEND OUT THE AREAS AND NDT FOR CRACK FREE IAW RAS/DABRE/7008942/2008 ISS A, APPROVED BY EA 6-5314-115244.Feb 22, 2008 · N730FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA00557Skin Panel · dentedFOUND NICK/DENT AT EXTERNAL SKIN PANEL, C22-23, P52-53 LT REPAIR PERFORMED BY DRESS OUT THE DENT IAW SRM 51-73-00 AND SKIN REPAIR BY BUSH IAW SRM 53-10-12 FIG 221 SHEET 1.Feb 22, 2008 · N730FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA04190Shaft · failedON DEPT 18L(KMEM) RECEIVED ECAM FOR SLATS SYS 1/2 FAULT W/CORRESPONDING SLAT LIGHT ON FWD PANEL. RECYCLE UNSUCCESSFUL. FOLLOWED QRH. NORMAL LANDING LNG GW 281.0. VERIFIED LEFT AND RIGHT WING SLATS WERE FULL UP AT "0" DEGREES POSITION IN REF TO AMM 27-80-00Sep 23, 2007 · N730FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR 06FDEA03166Circuit Breaker · faultyCRUISE FLIGHT LEVEL 320, APPROX 1 HR AFTER BLOCK OUT: ECAM/SC : SMOKE DISCH AGENT 2 RED AGENT, 2 DISCH BLUE FWD AGENT 2 SELECTED (OVERHEAD PANEL) DISCH 2/DISCH AGENT 2 LIGHTS ILLUMINATED NO EVIDENCE OF SMOKE OR FUMES. POST FLT DISCOVERED CARGO COMPT BTL 2 C/BSep 2, 2006 · N730FD · Airbus A300B4622R · Extinguishing SystemSDR 05FDEA02704Warning Light · illuminatedNR 2 REVERSER UNLOCK CAME ON DURING TAKEOFF IMMEDIATELY AFTER BRAKE RELEASE AFTER 40 PERCENT BUT BEFORE STANDARD POWER. LIGHT WENT OUT WHEN THROTTLES PULLED TO IDLE MEL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06SEP05 "MEL 78-30-Aug 27, 2005 · N730FD · Airbus A300* · Engine Thrust Reverser
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