N728FD
Service difficulty reports · 266
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 = 'N728FD' 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 = 'N728FD' 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 07FDEA03484Skin Panel · corrodedCORROSION ON FUSELAGE SKIN BETWEEN FRAME 30-31, STRG 54 LT TO RT. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5314-95877 AND RAS/DABRE/7006101/2005 ISSUE A.SDR 07FDEA03482Longeron · corrodedHEAVY CORROSION AT LONGERON BETWEEN FRAME 11-15A, Y953, CABIN FLOOR STRUCTURE. REPAIR PERFORMED IAW SRM 53-12-15 / FIG. 207.SDR 07FDEA03481Skin Panel · failedFOUND EXTERNAL DOUBLER REPAIR AT FRAME 72-73 BETWEEN STRG 43-44 LT, NOT CONFORM TO SRM 53-10-12/FIG 203. REPAIR PERFORMED BY INSTALLATION OF NEW DOUBLER IAW SRM 53-10-12/FIG 225.SDR 07FDEA03479Skin · damagedFOUND TWO MISDRILLED HOLES AT CIRCUMFERENTIAL LAP JOINT, FRAME 13, STRG 9 LT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW EA 6-5312-95874 AND RAS/AS/0012/2006 ISSUE A.SDR 07FDEA03475Angle · crackedDURING SB57-6086 AND SB57-6049, HOLES H, G, RT AND G, I , N, T ON LT HAVE BEEN FOUND CRACKED IN CENTER WING BOX, FRAME 47. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF NEW FASTENERS IAW EA 6-5710-95836 AND RAS/AS/0016/2006 ISSUE A.SDR 07FDEA03473Panel · delaminatedFOUND ON OUTBOARD T/E PANEL, LHS, DELAMINATION REPAIR PERFORMED BY REMOVING THE DELAMINATION AND INSTALLING NEW PLIES IAW EA 6-5751-95858 AND RAS /BAE/1002007/2005 ISS A.SDR 07FDEA03472Rib · crackedFOUND CRACK (3MM) ON MLG RIB 5, LHS, AT HOLE 47 (RAS/BAE/1001321/2005 GIVES A LIMIT OF 10 FC). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-92236 AND RAS/BAE/1001952/2005 ISS B.SDR 07FDEA00318Damper · damagedGEAR WOULD NOT RETRACT IN FLIGHT. SWITCHED POSITION DETECTORS, NO AVAIL. PLZ REFERENCE MTSI 32-30 / 1119 FOR ALL WORK ACCOMPLISHED REGARDS THIS ITEM. A/C LDG GEAR RETRACT SYS NOW ON MEL. REMOVED AND REPLACED BOGIE PITCH DAMPER/FLEW AC GEAR DWN ON MEL 32-3SDR 07FDEA00317Damper · dischargedL/G WOULD NOT RETRACT USING EITHER SYS 1 OR 2. CHECKED PROX DETECT CONTROL UNIT FOR FAILURES. NOTED THAT THE FAILURE CODE "BL" IS LOGGED. T/S AT THIS TIME PER TSM 32-30-00 PER AMM 32-10-00-6. CLEARED MEMORIZED FAULT ON PROX DETECTION UNIT WITH NO FURTHER SDR 07FDEA00335Damper · dischargedGEAR WOULD NOT RETRACT IN FLIGHT. SWITCHED POSITION DETECTORS, NO AVAIL. REFERENCE MTSI 32-30 / 1119. BWI MX, REMOVED AND REPLACED PROXIMITY DETECTOR UNIT 54GB AS PER A300 M/M 32-31-71-4. REMOVED AND REPLACED LT BOGIE PITCH DAMPER AS PER A300 M/M 32-11-15-SDR 07FDEA00334Damper · dischargedL/G WOULD NOT RETRACT USING EITHER SYS 1 OR 2. PERFORMED SERVICE OF LT BOOGIE PITCH DAMPER WITH NITROGEN PER AMM 12-12-32-0 PARAGRAPH 10. FOUND THAT PITCH DAMPER ONLY HAD A 400 PSI PRECHARGE. CURRENT LIMITS PER CHART FIG 11 IS 1300 PSI. RECHARGED PITCH DAMSDR 06FDEA04026Slat System · faultedSLATS SYSTEM 1 AND 2 FAULTED DURING EXTENSION. SLATS WOULD NOT EXTEND. RECYCLE DID NOT CORRECT THE FAULT. NO CORRESPONDING LIGHT ON SFPI. LANDED WITH SLATS 0. EMERGENCY DECLARED. BRAKE TEMPS 500 DEG MAX AFTER LANDING. T/S PER A300-600 TSM 27-80-02. FOUSDR 06FDEA03985Transmitter · malfunctionedDURING CRUISE, BRAKE PRESS WENT TO 3000 PSI DEPRESSED PEDDLES, CYCLED BRAKE/A/SKID AND CYCLED PARK BRAKE, NO CHANGE. ALSO YELLOW BRAKE TRIPLE PRESS BREAKER PER MAINT INSTRUCTIONS, NO CHANGE. WHEN MAIN GEAR TOUCHED DOWN PRESS RETURNED TO ZERO. FOUND BY TAKINSDR 06FDEA03967Unknown · malfunctionedDURING CRUISE BRAKE PRESS WENT TO 3000 PSI DEPRESSED PEDDLES, CYCLED BRK/A/SKID AND CYCLED PARK BRAKE. NO CHANGE, ALSO YELLOW BRAKE TRIPLE PRESS BREAKER PER MAINT INSTRUCTIONS, NO CHANGE. WHEN MAIN GEAR TOUCHED DOWN PRESS RETURNED TO ZERO. T/S SYSTEM REF M/SDR 06FDEA03630Computer · malfunctionedPDIS 728 77-10 0804 13OCT06 GSO RECD ENG 2 N1 MODE. ONLY MAINTENANCE - CLEARED ITSELF ON T/O ROLL RECD SAME WARNING. REFECT T/O AT 60KTS. FOLLOWED ALL ECAM/RED TABS. FADEC WAS SELECTED TO N1 MODE FOR BOTH ENGINES. FACT 13OCT06 04:47 GSO R REMOVED AND REPLASDR 06FDEA3002Engine · smokeAIR TURN BACK, AFTER TOWER REPORTED HEAVY SMOKE OUT OF THE RIGHT ENGINE. DECLARED EMERGENCY AND RETURNED TO LAND. THE ENGINE INSTRUMENTS APPEARED NORMAL. NORMAL LANDING AT 284000 LBS (NOT OVERWEIGHT. OBSERVED ON LANDING NO SMOKE NOTED. ON TAXI IN TO GATE,
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