# Service difficulty reports: N358BE, cancelled Mar 19, 2004

A list on [N358BE, cancelled Mar 19, 2004](https://openairdocs.org/deregistered/N358BE-2004-03-19.md).

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

- [SDR PLGA001017](https://openairdocs.org/sdr/PLGA001017.md): Strut · discharged · Oct 17, 2000 · N358BE · Saab 340B · Main Landing Gear Strut/Axle/Truck
  > BOS-BGR - FLT 4709 - DURING TAKEOFF, THE OUTSIDE AIR TEMP LIGHT ILLUMINATED UPON GEAR RETRACTION. ALSO, NOTED AN INTERMITTENT CONFIGURATION WARNING WHEN THE PROPELLER WAS SELECTED BELOW MAX RPM. CREW FOLLOWED THEIR CHECKLIST AND RETURNED TO BOS WHERE THE AIR
- [SDR PLGA000527](https://openairdocs.org/sdr/PLGA000527.md): Transducer · failed · May 27, 2000 · N358BE · Saab 340B · Hydraulic Pressure Indicator
  > FLT 4761 - BTV-BOS, CREW NOTED THE HYDRAULIC LIGHT HAD COME ON. IT WAS ALSO NOTED THAT THE MAIN AND OUTBOARD PRESSURE INDICATORS WERE READING LOW AND THAT AUTO MODE WAS NOT WORKING. THE FLIGHT CREW MANUALLY LOWERED THE LANDING GEAR, DECLARED AN EMERGENCY AND
- [SDR PLGA000402](https://openairdocs.org/sdr/PLGA000402.md): Uplock Switch · failed · Apr 2, 2000 · N358BE · Saab 340B · Landing Gear Position and Warning
  > YOW-BOS - FLT 4837 - AFTER DEPARTURE, WHEN THE GEAR WAS SELECTED UP THE HYDRAULIC AUTO MODE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE HYDRAULIC PUMP WAS SELECTED TO OVERRIDE AND THE GEAR CAME UP, BOTH THE INTRANSIT LIGHT STAYED ILLUMINATED. GEAR WAS SE
- [SDR PLGA991216](https://openairdocs.org/sdr/PLGA991216.md): Connector · loose · Dec 16, 1999 · N358BE · Saab 340B · Compressor Bleed Valve
  > BOS - FLT 4855 - DURING FLIGHT, THE RIGHT LOW PRESSURE BLEED VALVE WAS NOT FUNCTIONING AND STUCK OPEN. AIRCRAFT RETURNED TO BOS. AFTER TROUBLESHOOTING MAINTENANCE, FOUND THE CONNECTOR AT THE RIGHT BLEED VALVE LOOSE. THE CONNECTOR WAS RESECURED, REQUIRED OP
- [SDR PLGA991006](https://openairdocs.org/sdr/PLGA991006.md): Duct · failed · Oct 6, 1999 · N358BE · Saab 340B · Air Intake Anti/De-Ice System
  > BOS-SYR - FLT 4776 - CREW NOTED THAT THE LEFT INTAKEO LIGHT ILLUMINATED WHEN SYSTEM WAS SELECTED ON. ATTEMPTS FAILED IN TRYING TO RESET THE SYSTEM PER THE CHECKLIST. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DUCT PARTICL
- [SDR PLGA990721](https://openairdocs.org/sdr/PLGA990721.md): Flex Line · failed · Jul 21, 1999 · N358BE · Saab 340B · Hydraulic System, Main
  > BTV - FLT 6881 - AFTER TAKEOFF FROM BTV, THE MAIN HYDRAULIC PRESSURE DROPPED AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE CREW USED THE EMERGENCY GEAR EXTENSION SYSTEM TO LOWER THE GEAR AND THE AIRCRAFT RETURNED TO BTV AND LANDED SAFELY. MAINTENANCE FOUND THE
- [SDR PLGA990216](https://openairdocs.org/sdr/PLGA990216.md): Transponder · failed · Feb 16, 1999 · N358BE · Saab 340B · ATC Transponder System
  > LGA - FLT 6514 - CREW REPORTED NR 2 TRANSPONDER FAILED ALONG WITH TCAS. NR 1 TRANSPONDER ALREADY MEL'D. A/C RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM. A/C RETURNED TO SERVICE. (M)
- [SDR PLGA990106](https://openairdocs.org/sdr/PLGA990106.md): Valve · defective · Jan 6, 1999 · N358BE · Saab 340B · Cabin Temperature Control System
  > BOS - FLT 6232 - AFTER TAKEOFF, CREW NOTED LT DUCT OVERTEMP LIGHT ILLUMINATED. CREW UNABLE TO CONTROL CABIN TEMP IN AUTO AND MANUAL MODES. A/C RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DUAL TEMP CONTROL VALVE. A/C RETURNED TO SE
- [SDR PLGA980710A](https://openairdocs.org/sdr/PLGA980710A.md): Circuit Breaker · tripped · Jul 10, 1998 · N358BE · Saab 340B · Trailing Flap Position Indicating System
  > BOS - FLT 4264 - WHEN FLAPS WERE SELECTED DOWN FOR LANDING AT BOS, THE CREW REPORTED THERE WAS NO FLAP INDICATION. CREW PERFORMED A MISSED APPROACH AND FOUND THE FLAP INDICATOR CIRCUIT BREAKER OPEN. THE BREAKER WAS RE-SET AND AIRCRAFT LANDED WITHOUT INCIDENT
- [SDR PLGA980621A](https://openairdocs.org/sdr/PLGA980621A.md): Hyd Line · leaking · Jun 21, 1998 · N358BE · Saab 340B · Hydraulic System, Main
  > PVD - FLT 4573 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, HYDRAULIC PUMP RAN CONTINUOUSLY AND HYDRAULIC FLUID QTY DECREASED. CREW SELECTED GEAR DOWN AND DIVERTED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG RETRACT ACTUATOR UP LIN
- [SDR PLGA980528A](https://openairdocs.org/sdr/PLGA980528A.md): Relay · failed · May 28, 1998 · N358BE · Saab 340B · DC Generating System
  > BOS - FLT 4253 - AFTER TAKEOFF, THE RIGHT MAIN ELECTRICAL BUS INTERMITTENTLY FELL OFF LINE. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TIME DELAY RELAY (PC72). SYSTEM TESTED GOOD. (M)
- [SDR PLGA971025B](https://openairdocs.org/sdr/PLGA971025B.md): Oil Press Light · illuminated · Oct 25, 1997 · N358BE · Saab 340B · Engine Oil Pressure
  > BOS - FLT 4219 - DURING TAKEOFF, THE CREW NOTED THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND WAS UNABLE TO DUPLICATE THE PROBLEM. AIRCRAFT RETURNED TO SERVICE
- [SDR PLGA9701183](https://openairdocs.org/sdr/PLGA9701183.md): Retract Mech · malfunctioned · Jan 18, 1997 · N358BE · Saab 340B · Landing Gear Retraction/Extension System
  > JFK - FLT 4337 - ON APPROACH TO JFK, CREW SELECTED GEAR DOWN. THE GEAR DID NOT EXTEND AND THE ELECTRIC HYDRAULIC PUMP DID NOT COME ON. THE CREW EXTENDED THE GEAR USING EMERGENCY PROCEDURES. CREW THEN SELECTED FLAPS DOWN AND THE FLAP SYSTEM OPERATED NORMAL.
- [SDR PLGA9606192](https://openairdocs.org/sdr/PLGA9606192.md): Cowl Door · not latched · Jun 19, 1996 · N358BE · Saab 340B · Engine Cowling System
  > PIT - FLT 4382 - AFTER TAKEOFF FROM PIT, THE RIGHT ENGINE FWD OUTBOARD COWLING DOOR OPENED. THE AIRCRAFT RETURNED TO PIT, LANDING WITHOUT INCIDENT. THE COWLING WAS TEMPORARILY REPAIRED AND THE AIRCRAFT THEN FERRIED TO PSM FOR PERMANENT REPAIR. (M)
- [SDR PLG2596E1](https://openairdocs.org/sdr/PLG2596E1.md): Upstop Pad · out of adjust · Feb 5, 1996 · N358BE · Saab 340B · Landing Gear Retraction/Extension System
  > PSM - FLT 4471 - ON CLIMB-OUT, THE LANDING GEAR INTRANSIT LIGHT STAYED ILLUMINATED, AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE AIRCRAFT RETURNED TO PSM AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE UPSTOP PAD ON THE LEFT HAND MAIN GEAR. TEST FLIGH
- [SDR 95ZZZX1529](https://openairdocs.org/sdr/95ZZZX1529.md): Prop Lead · failed · Feb 11, 1995 · N358BE · Saab 340B · Propeller Deice Boot Section
  > PQI - FLT 4599 - RT PROP DEICE FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO PQI LANDING WITHOUT INCIDENT. MEL'D PROP DEICE SYSTEM AND REPOSITIONED THE AIRCRAFT TO BOS. BOS MAINTENANCE REPLACED A DEFECTIVE PROP LEAD ON THE NR 3 BLADE AND RETURNED THE AIRCRAFT

## 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 = 'N358BE' AND deregistration_id = 'N358BE-2004-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N358BE-2004-03-19/reports

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