# Service difficulty reports: N380WL, cancelled Mar 21, 2006

A list on [N380WL, cancelled Mar 21, 2006](https://openairdocs.org/deregistered/N380WL-2006-03-21.md).

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

- [SDR PIDA06007](https://openairdocs.org/sdr/PIDA06007.md): Attach Angle · cracked · Jan 15, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Attach Fittings
  > UPPER O/B ATTACH ANGLE FOR THE LEFT RAM AIR DUCT IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-02 AND 51-40-00.
- [SDR PIDA06004](https://openairdocs.org/sdr/PIDA06004.md): Skin · cracked · Jan 12, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AT BS 380 ABOVE STR 4 RT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.
- [SDR PIDA06005](https://openairdocs.org/sdr/PIDA06005.md): Skin · cracked · Jan 10, 2006 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AT BS 500A ABOVE STR 4 LT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.
- [SDR PIDA06002](https://openairdocs.org/sdr/PIDA06002.md): Actuator · broken · Dec 31, 2005 · N380WL · Boeing 7373G7 · Drag Control Actuator
  > LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94.
- [SDR PIDAS06002](https://openairdocs.org/sdr/PIDAS06002.md): Actuator · broken · Dec 31, 2005 · N380WL · Boeing 7373G7 · Drag Control Actuator
  > LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94.
- [SDR PIDA20050201](https://openairdocs.org/sdr/PIDA20050201.md): Autopilot Sys · malfunctioned · Dec 23, 2005 · N380WL · Boeing 7373G7 · Autopilot System
  > B-CHANNEL AUTO PILOT CAPTURES PRESELECTED ALTITUDE 300 FEET HIGH ON DESCENT BELOW FLIGHT LEVEL 20,000. A-CHANNEL WORKS FINE. PLACED B-AUTO PILOT ON MEL 22-1.
- [SDR PIDA20050200](https://openairdocs.org/sdr/PIDA20050200.md): Control Panel · malfunctioned · Dec 21, 2005 · N380WL · Boeing 7373G7 · Autopilot System
  > AUTO PILOT LEVELING OFF 300 FEET ABOVE SELECTED MCP ALTITUDE. REPLACED MODE SELECT PANEL PER MM 22-11-00. OPS CHECKS OK.
- [SDR PIDA20050193](https://openairdocs.org/sdr/PIDA20050193.md): Lap Joint · cracked · Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > DURING "A CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST AFT OF BS 440.
- [SDR PIDA20050192](https://openairdocs.org/sdr/PIDA20050192.md): Lap Joint · cracked · Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > DURING "A CHECK, FOUND TWO CRACKS ABOVE STR 10 RT SKIN LAP, ONE JUST AFT OF BS 500A AND ONE JUST FORWARD OF BS 500B.
- [SDR PIDA20050191](https://openairdocs.org/sdr/PIDA20050191.md): Lap Joint · cracked · Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > DURING A-CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST FORWARD OF BS 520.REPAIRED PER SRM 53-00-01.
- [SDR PIDA20050194](https://openairdocs.org/sdr/PIDA20050194.md): Skin · cracked · Nov 22, 2005 · N380WL · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > DURING "A" CHECK, FOUND CRACK IN FUSELAGE SKIN JUST BELOW STR 22RT BETWEEN BS 727D AND BS 727E.
- [SDR PIDA20050182](https://openairdocs.org/sdr/PIDA20050182.md): Power Lever · out of adjust · Oct 24, 2005 · N380WL · Boeing 7373G7 · Auto Throttle System
  > LEFT POWER LEVER DID NOT GO TO FLIGHT IDLE WITH LEVEL CHANGE SELECTED, THUS RESULTING IN ASYMMETRICAL THRUST. PERFORMED CABLE LUB PER MM 12-26-00.
- [SDR PIDA20050050](https://openairdocs.org/sdr/PIDA20050050.md): Engine · bird ingestion · Jun 6, 2005 · N380WL · Boeing 7373G7 · Engine (Turbine/Turboprop)
  > INGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22, 23, AND 24. ALL ENGINE PARAMETERS AND VIBRATION CHECKS NORMAL ON ENGINE RUN.
- [SDR 380WL0002](https://openairdocs.org/sdr/380WL0002.md): Indicator · malfunctioned · Mar 7, 2005 · N380WL · Boeing 7373G7 · Visual Omnirange (VOR) System
  > NR 2 NAV-ILS, FLAGS WHEN IN VOR/ILS/AP MODE. PLACED ON MEL 22-15-7 AND 8. PERFORMED TROUBLE-SHOOTING PROCEDURE FOR VOR/ILS SYSTEM PER MM 34-31-00. NO DEFECTS NOTED. CLEARED MEL.
- [SDR 380WL0003](https://openairdocs.org/sdr/380WL0003.md): Cable · out of rig · Mar 5, 2005 · N380WL · Boeing 7373G7 · Auto Throttle System
  > AUTOTHROTTLE KICKS OFF DURING FLIGHT. RIGGED LEFT THROTTLE FLEX CABLE PER MM 76-11-00. AUTOTHROTTLE CHECKS GOOD.
- [SDR 380WL0001](https://openairdocs.org/sdr/380WL0001.md): Computer · malfunctioned · Aug 20, 2004 · N380WL · Boeing 7373G7 · Auto Throttle System
  > AUTO THROTTLE DOES NOT ACHIEVE REQUESTED TAKE OFF THRUST AND DISENGAGES DURING ALL PHASES OF FLIGHT. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-10. TEST NORMAL.

## 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 = 'N380WL' AND deregistration_id = 'N380WL-2006-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N380WL-2006-03-21/reports

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