N322FE, cancelled May 4, 2006
Service difficulty reports · 19
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 = 'N322FE' AND deregistration_id = 'N322FE-2006-05-04' 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 = 'N322FE' AND deregistration_id = 'N322FE-2006-05-04' 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 2004F00236Fuse Link · shearedRT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546.SDR 2004F00237Sleeve · crackedNR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502.SDR 2004FA0000678Fuse Pin · shearedRT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.SDR 2004FA0000679Attach Fitting · corrodedLOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.SDR 01FDEA00218Pin · defectiveNOSE GEAR DID NOT RETRACT ON T/O. REMOVED AND REPLACED NOSE GEAR PIN. AC OK TO CONTINUE.SDR 00FDEA00400Stiffener · corrodedSNRM 0327 LOWER AUX FUEL TANK AFT BULKHEAD, LT MOST VERTICAL STIFFNER FOUND WITH CORROSION. R&R PER 51-31-01, 21-11-06-2.SDR 00FDEA00399Support Bracket · crackedSNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01.SDR 00FDEA00403Skin · crackedSNRM 0196 LT WING OB FLAP UPPER SKIN SURFACE FOUND CRACKED APPROX 3 5/32 INCHES. R&R PER SRM 51-31-01, 57-10-00, 57-52-02.SDR 00FDEA00402Skin · crackedSNRM 0198 LT WING IB FLAP UPPER SKIN FOUND PATCH REPAIR CRACKED APPOX 6 INCHES. R&R PER CMM 57-52-01.SDR 00FDEA00401Skin · crackedSNRM 0222 LT WING L/E LOWER ACCESS PANEL CUTOUT NR 526AB FWD SIDE FOUND CRACKED. R&R PER SRM 51-31-01.SDR 00FDEA00398Channel · corrodedSNRM 0252 AFT FUSELAGE WATER TANK BAY STA 1996, FUSELAGE FRAME AFT LWR CHANNEL TOP SURFACE CORRODED, LONGERON 50 RT TO LT. R&R CHANNEL & STRAP PER SRM 53-30-00 FIG 8, VOL 1.SDR 98FDEA00413Fire Bottle · dischargedENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGUISHER SYSTEM HAD DISCHARGED THRU APU PORT (NR 2 ENG FIREX CONTAINER 1). REPLACED NR 2 ENG FIREX CONTAINER 1 PER M/M 26-21-02 AND SQUIB FOR SDR 98FDEA00250Slider · brokenSHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREADY CONFIGURED FOR LANDING, LANDED SUCCESSFULLY, NO FURTHER PROBLEMS. DOOR 4L SWITCH NOT WORKING DUE TO TRACK CAM AND SLIDER BROKEN. REPLACESDR 96FDEA01489Hi-Lock Collars · missingSNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352.SDR 96FDEA01490Tension Strap · crackedSMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I.SDR 96FDEA01435V-Panel · missingUPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00.SDR 95FDEA01428Duct · failedDURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 DEGREES HIGHER THAN ENG NR 2 AND NR 3. AT APPROX 300 FEET NR 1 FIRE WARNING AND BELL RECEIVED. ACSDR 95FDEA00214Fire Warning · malfunctionedTHE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, REMOVED AND REPLACED LIGHT ASSY. OPS CKD GOOD.SDR 95FDEA00005Duct · failedENG FIRE IN NR 2 ENG SHORTLY AFTER ROTATION. OBSERVED EGT REACHED 899 DEG. MEMORY ITEMS ACCOMP, CKLT PROCED COMPLIED WITH, RETURNED TO OAK FOR UNEVENTFUL LANDING (FIRE HANDLE PULLED, BOTTLE NOT DISCHARGED). REPLACED 14TH STAGE LWR CROSSOVER DUCT, LPT COOLIN
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