N705A, cancelled Mar 6, 2004

Service difficulty reports · 16

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 = 'N705A' AND deregistration_id = 'N705A-2004-03-06'
  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 TC8A00011Engine · failed#1 ENGINE FAILED. RETURNED TO TOL.Jun 28, 2000 · N705A · Boeing 72721C · Engine (Turbine/Turboprop)SDR TC8A00010Pump · failedON TAXI, LEFT AFT BOOST PUMP POPPED CB, COULD NOT RESET. TRANSFERRED TO DMI LIST DMI NR 0090 IAW MEL 28-4 COMPLIED WITH SP 28-1 PAR H, PLACARDS INSTALLED.Jun 20, 2000 · N705A · Boeing 72721C · Fuel Boost PumpSDR TC8A00009Start Valve · closedNR 2 START VALVE CLOSED BEFORE LIGHT OFF RETURNED TO RAMP. PERFORMED MANUAL START PROCEDURES ON NR 2 FIGURE, OPS CHECK NORMAL IAW FLIGHT MANUAL PG 3 NR 34.Jun 17, 2000 · N705A · Boeing 72721C · Engine Start Valves/ControlsSDR TC8A00005Indicator · inaccurateCAPT''S ATTITUDE INDICATOR SHOWS 5 DEGREES BANK.Apr 19, 2000 · N705A · Boeing 72721C · Directional Gyro and Indicating SystemSDR TC800005Indicator · inaccurateCAPT''S ATTITUDE INDICATOR SHOWS 5 DEGREES BANK.Apr 19, 2000 · N705A · Boeing 72721C · Directional Gyro and Indicating SystemSDR TC8A00004Hydraulic System · lowDURING TAXI, SYS A-HYD FLUCTUATION IN INDIC. SERVICED A-HYD SYS, OPS CHECK GOOD IAW B727 MM 12-12-0.Apr 5, 2000 · N705A · Boeing 72721C · Hydraulic Power SystemSDR TC8A00003Outflow Valve · leakingUNABLE TO MAINTAIN CABIN PRESSURE WITH ONE PACK VALVE OPERATING. REMOVED AND REPLACED LT OUTFLOW VALVE IAW B727 21-30-51, OPS CHECK AND LEAK CHECK NORMAL. REMOVED AND REPLACED EQUIPMENT COOLING FLOW CONTROL VALVE IAW B727MM 21-58-21, OP''S CHECK NORMAL. PERMar 2, 2000 · N705A · Boeing 72721C · Pressure Regulator/Outflow ValveSDR TC8A00001Bulb · inoperativeOUTBOARD LANDING LIGHT ON RT WING INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD IAW B727 MM 33-42-0.Jan 21, 2000 · N705A · Boeing 72721C · Exterior LightingSDR TC8A99027Wire · failedON TAXI OUT, FLAGS APPEARED ON NR 2 AND NR 2 CDI. REPAIRED WIRE AT NR 2 DG AND SECURED WIRING HARNESS. NR 2 DG, RMI AND CD, OPS CHECK NORMAL IAW B727 MM 34-21-0. NR 2 COMPASS SYSTEM NORMAL.Nov 5, 1999 · N705A · Boeing 72721C · Directional Gyro and Indicating SystemSDR TC8A99026Nav Receiver · failedDURING TAXI-OUT, CAPT'S VOR FLAG IN VIEW. REMOVED AND REPLACED NR 1 VHF NAV RCVR AND SYSTEM OPS GOOD IAW BMM 34-31-0.Oct 6, 1999 · N705A · Boeing 72721C · VHF Communications SystemSDR TC8A99025Connector · wetNR 2 B-PUMP C/B WILL NOT RESET. BMM 29-12-0, OPERATION OF B-PUMP. EXCESSIVE MOISTURE ON PUMP CONNECTION.Sep 18, 1999 · N705A · Boeing 72721C · Hydraulic Pump, AuxiliarySDR TC8A99024Pitot Tube · obstructedAT 80 KTS ON FIRST OFFICER AIRSPEED INDICATOR 0 KTS ON CAPTAINS AIRSPEED INDICATOR, ABORT TAKEOFF. PERFORMED PITOT STATIC LEAK TEST. FOUND OBSTRUCTION IN CAPTS PITOT TUBE. CLEARED TUBE, LEAK CHECK GOOD IAW MM CHAPT 34-11-0 AND FAR PART 43 APPENDIX E.Aug 13, 1999 · N705A · Boeing 72721C · Pitot/Static SystemSDR TC8A99023Pitot Tube · obstructedON TAKEOFF ROLL, CAPT AIRSPEED ALIVE BY 70 KNTS, FIRST OFFICER 0 KTS. ABORT AT 78 KTS IN ACCORDANCE WITH TRANSCONTINENTAL PROCEDURE. NORMAL TAXI IN. REMOVED PITOT LINE FROM AIRSPEED INDICATOR, CAPPED PITOT LINE AT MACH SPEED SWITCH. PRESSURIZED F/O'S PITOTAug 7, 1999 · N705A · Boeing 72721C · Pitot/Static SystemSDR TC8A99022Union · failedAFTER TAKEOFF, CAPT AND FIRST OFFICER AIRSPEED INDICATOR DIFFERENCE OF 50 KTS (FIFTY KNOTS). RETURN TO FIELD. INSPECTED F/O'S PITOT SYSTEM, REMOVED AND REPLACED UNION AT F/O'S PITOT PROBE. PERFORMED FULL RANGE PITOT STATIC LEAK CHECK IN ACCORDANCE WITH B727Aug 7, 1999 · N705A · Boeing 72721C · Pitot/Static SystemSDR TC8A99021Generator · malfunctionedUNABLE TO PARALLEL NR 2 GENERATOR. TRANSFERRED TO DMI 9233 AS PER TCA B727 MEL 24-1, SPECIAL PROCEDURES 24-1 PLACARDS INSTALLED.Jul 13, 1999 · N705A · Boeing 72721C · AC Generator-AlternatorSDR TC8A99016Clamp · looseKMSP-KMSP TRIP NR 03341. ENG NR 3 STRUT O/H OCCURED IN CLIMB, COMPLIED WITH ENG STRUT O/H CHECKLIST. ENG NR 3 FIRE WARNING LIGHT CAME ON DURING CLIMB, COMPLIED WITH ENG FIRE SEVERE DAMAGE SEPARATION CHECKLIST AND SHUT ENG DOWN AND FIRED THE EXTINGUISHER. LIMay 6, 1999 · N705A · Boeing 72721C · Pneumatic Distribution System
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