# Service difficulty reports: N705A, cancelled Mar 6, 2004

A list on [N705A, cancelled Mar 6, 2004](https://openairdocs.org/deregistered/N705A-2004-03-06.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR TC8A00011](https://openairdocs.org/sdr/TC8A00011.md): Engine · failed · Jun 28, 2000 · N705A · Boeing 72721C · Engine (Turbine/Turboprop)
  > #1 ENGINE FAILED. RETURNED TO TOL.
- [SDR TC8A00010](https://openairdocs.org/sdr/TC8A00010.md): Pump · failed · Jun 20, 2000 · N705A · Boeing 72721C · Fuel Boost Pump
  > ON 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.
- [SDR TC8A00009](https://openairdocs.org/sdr/TC8A00009.md): Start Valve · closed · Jun 17, 2000 · N705A · Boeing 72721C · Engine Start Valves/Controls
  > NR 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.
- [SDR TC8A00005](https://openairdocs.org/sdr/TC8A00005.md): Indicator · inaccurate · Apr 19, 2000 · N705A · Boeing 72721C · Directional Gyro and Indicating System
  > CAPT''S ATTITUDE INDICATOR SHOWS 5 DEGREES BANK.
- [SDR TC800005](https://openairdocs.org/sdr/TC800005.md): Indicator · inaccurate · Apr 19, 2000 · N705A · Boeing 72721C · Directional Gyro and Indicating System
  > CAPT''S ATTITUDE INDICATOR SHOWS 5 DEGREES BANK.
- [SDR TC8A00004](https://openairdocs.org/sdr/TC8A00004.md): Hydraulic System · low · Apr 5, 2000 · N705A · Boeing 72721C · Hydraulic Power System
  > DURING TAXI, SYS A-HYD FLUCTUATION IN INDIC. SERVICED A-HYD SYS, OPS CHECK GOOD IAW B727 MM 12-12-0.
- [SDR TC8A00003](https://openairdocs.org/sdr/TC8A00003.md): Outflow Valve · leaking · Mar 2, 2000 · N705A · Boeing 72721C · Pressure Regulator/Outflow Valve
  > UNABLE 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. PER
- [SDR TC8A00001](https://openairdocs.org/sdr/TC8A00001.md): Bulb · inoperative · Jan 21, 2000 · N705A · Boeing 72721C · Exterior Lighting
  > OUTBOARD LANDING LIGHT ON RT WING INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD IAW B727 MM 33-42-0.
- [SDR TC8A99027](https://openairdocs.org/sdr/TC8A99027.md): Wire · failed · Nov 5, 1999 · N705A · Boeing 72721C · Directional Gyro and Indicating System
  > ON 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.
- [SDR TC8A99026](https://openairdocs.org/sdr/TC8A99026.md): Nav Receiver · failed · Oct 6, 1999 · N705A · Boeing 72721C · VHF Communications System
  > DURING 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.
- [SDR TC8A99025](https://openairdocs.org/sdr/TC8A99025.md): Connector · wet · Sep 18, 1999 · N705A · Boeing 72721C · Hydraulic Pump, Auxiliary
  > NR 2 B-PUMP C/B WILL NOT RESET. BMM 29-12-0, OPERATION OF B-PUMP. EXCESSIVE MOISTURE ON PUMP CONNECTION.
- [SDR TC8A99024](https://openairdocs.org/sdr/TC8A99024.md): Pitot Tube · obstructed · Aug 13, 1999 · N705A · Boeing 72721C · Pitot/Static System
  > AT 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.
- [SDR TC8A99023](https://openairdocs.org/sdr/TC8A99023.md): Pitot Tube · obstructed · Aug 7, 1999 · N705A · Boeing 72721C · Pitot/Static System
  > ON 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 PITOT
- [SDR TC8A99022](https://openairdocs.org/sdr/TC8A99022.md): Union · failed · Aug 7, 1999 · N705A · Boeing 72721C · Pitot/Static System
  > AFTER 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 B727
- [SDR TC8A99021](https://openairdocs.org/sdr/TC8A99021.md): Generator · malfunctioned · Jul 13, 1999 · N705A · Boeing 72721C · AC Generator-Alternator
  > UNABLE TO PARALLEL NR 2 GENERATOR. TRANSFERRED TO DMI 9233 AS PER TCA B727 MEL 24-1, SPECIAL PROCEDURES 24-1 PLACARDS INSTALLED.
- [SDR TC8A99016](https://openairdocs.org/sdr/TC8A99016.md): Clamp · loose · May 6, 1999 · N705A · Boeing 72721C · Pneumatic Distribution System
  > KMSP-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. LI

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N705A-2004-03-06/reports

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