# Service difficulty reports: N155ZV, cancelled May 6, 2011

A list on [N155ZV, cancelled May 6, 2011](https://openairdocs.org/deregistered/N155ZV-2011-05-06.md).

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

- [SDR AMWA1019019](https://openairdocs.org/sdr/AMWA1019019.md): Spar · cracked · Nov 8, 2007 · N155ZV · Beech 1900D · Wing Spar
  > DURING DETAIL INSPECTION, RT AFT SPAR FLANGE AT WS117.5 WAS FOUND TO BE CRACKED FROM RIVET TO EDGE OF FLANGE. MAINTENANCE OBTAINED APPROVED DATA, PERFORMED REPAIR AND CLEARED DISCREPANCY.
- [SDR AMWA1001016](https://openairdocs.org/sdr/AMWA1001016.md): Skin · dented · Nov 8, 2007 · N155ZV · Beech 1900D · Wing, Plate/Skin
  > RT CENTER LEADING EDGE AT APPROXIMATELY WS 54.45 HAD BIRD STRIKE DAMAGE EXCEEDING STRUCTURAL REPAIR MANUAL LIMITS. OBTAINED APPROVED DATA, REPAIRED LEADING EDGE AND CLEARED DISCREPANCY.
- [SDR AMWA87352](https://openairdocs.org/sdr/AMWA87352.md): Indication Sys · smoke · Sep 11, 2007 · N155ZV · Beech 1900D · Flight Environment Data
  > ON TAXI OUT CAPT NOTED SMOKE AND ELECTRICAL ODOR WHICH APPEARED TO BE COMING FROM CAPT'S EFIS SYSTEM. CREW DECIDED TO RETURN TO GATE WITH NO FURTHER INCIDENT. CND ON GROUND, SYSTEM OPS CHECKS NORMAL. REMOVED AND REPLACED CAPT EFIS SCREEN FOR PRECAUTIONARY M
- [SDR AMWA15036A](https://openairdocs.org/sdr/AMWA15036A.md): Frame · chafed · Jul 10, 2007 · N155ZV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R.
- [SDR AMWA15036C](https://openairdocs.org/sdr/AMWA15036C.md): Skin · chafed · Jul 10, 2007 · N155ZV · Beech 1900D · Wing, Plate/Skin
  > FRICTION CHAFFING CREATED WORN SEGMENTS ON THE RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 6772-1 REV 1R.
- [SDR AMWA15036B](https://openairdocs.org/sdr/AMWA15036B.md): Skin · chafed · Jul 10, 2007 · N155ZV · Beech 1900D · Wing, Plate/Skin
  > FRICTION CHAFFING CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 677201 REV 1R.
- [SDR AMWA15036](https://openairdocs.org/sdr/AMWA15036.md): Spar · corroded · Jul 9, 2007 · N155ZV · Beech 1900D · Wing Spar
  > CORROSION LT AND AFT MAIN SPAR FLANGE. REPAIRED IAW ENGINEERING REPORT NR 6772-3 REV A DATED JUN 25, 2007.
- [SDR AMWA81813](https://openairdocs.org/sdr/AMWA81813.md): Landing Gear · malfunctioned · Jan 3, 2007 · N155ZV · Beech 1900D · Landing Gear Retraction/Extension System
  > WHEN GEAR WAS EXTENDED FOR LANDING, THE RT MAIN GEAR DID NOT SHOW DOWN AND LOCKED. THE CREW DECLAIRED AN EMERGENCY AND FOLLOWED EMERGENCY PROCEDURES, BY PUMPING THE GEAR DOWN. THE AIRCRAFT THEN LANDED SAFELY WITH NO FURTHER INCIDENT.
- [SDR 1060918030](https://openairdocs.org/sdr/1060918030.md): Oil System · low pressure · Sep 18, 2006 · N155ZV · Beech 1900D · Turbine Engine Oil System
  > AFTER TAKEOFF ON CLIMBOUT LEFT OIL PRESSURE ANNUNCIATOR ILLUMINATED & OIL PRESSURE WAS BELOW 60 PSI ON INDICATOR AT 3500 LB TORQUE. CREW SHUT ENGINE DOWN AND RETURNED TO FIELD WITHOUT FURTHER INCIDENT. NOTE: INFORMATION IN COMPUTER BLOCKS IS FOR GAS GENERATO
- [SDR 76087](https://openairdocs.org/sdr/76087.md): Trim Panel · loose · Feb 27, 2006 · N155ZV · Beech 1900D · Passenger/Crew Doors
  > AFTER ARRIVAL INTO PIT, THE CREW REPORTED THAT THE DOOR WOULD NOT OPEN FROM THE OUTSIDE. THE CREW THEN OPENED THE DOOR FROM THE INSIDE NORMALLY. MAINTENANCE RE-SECURED TRIM PIECE AND TRIM BACK.
- [SDR 1051229025](https://openairdocs.org/sdr/1051229025.md): Spar Cap · corroded · Feb 15, 2006 · N155ZV · Beech 1900D · Wing Spar
  > CORROSION ON LT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTION
- [SDR 1051229028A](https://openairdocs.org/sdr/1051229028A.md): Spar Cap · corroded · Feb 15, 2006 · N155ZV · Beech 1900D · Wing Spar
  > BIO CORROSION ON RIGHT WING MAIN SPAR CAP FLANGE NEAR WS 124588. MAINTENANCE FOUND DURING INSPECTION.
- [SDR 1051229028](https://openairdocs.org/sdr/1051229028.md): Spar Cap · corroded · Feb 15, 2006 · N155ZV · Beech 1900D · Wing Spar
  > BIO CORROSION ON LEFT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTION.
- [SDR 62795](https://openairdocs.org/sdr/62795.md): Wire · damaged · Jul 5, 2004 · N155ZV · Beech 1900D · Landing Gear System Wiring
  > AFTER TAKEOFF, GEAR HANDLE WAS PLACED IN UP POSITION. LANDING GEAR INTRANSIT LIGHTS AND AURAL HORN DID NOT EXTINGUISH AIRCRAFT RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. REPAIRED BROKEN WIRES AT TB152 AND REPAIRED BAD SPLICES AT A406 PCB.
- [SDR 57841](https://openairdocs.org/sdr/57841.md): Downlock · inoperative · Jan 12, 2004 · N155ZV · Beech 1900D · Landing Gear Position and Warning
  > AFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQUIRED. OPS CK GOOD.
- [SDR MASA97154](https://openairdocs.org/sdr/MASA97154.md): Actuator · failed · Sep 17, 1997 · N155ZV · Beech 1900D · Landing Gear Actuator
  > AIRSHUTTLE 5547 - BWI-BDR - UPON DESCENT IN BDR, THE CREW SELECTED GEAR DOWN AND DID NOT GET GEAR DOWN AND LOCKED INDICATION. THE CREW DECLARED AND EMERGENCY AND LANDED IN BDR WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACTUAT
- [SDR 97ZZZX3305](https://openairdocs.org/sdr/97ZZZX3305.md): Attach Bracket · excess wear · Jul 11, 1997 · N155ZV · Beech 1900D · Trailing Edge Flaps
  > FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING.
- [SDR 97ZZZX3304](https://openairdocs.org/sdr/97ZZZX3304.md): Attach Bracket · excess wear · Jul 11, 1997 · N155ZV · Beech 1900D · Trailing Edge Flaps
  > FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING.
- [SDR MASA97034](https://openairdocs.org/sdr/MASA97034.md): Windshield · warped · Jun 2, 1997 · N155ZV · Beech 1900D · Flight Compartment Windows
  > DURING MAINTENANCE, COPILOT'S WINDSHIELD WOULD NOT HEAT WHEN LOW WAS SELECTED. T/S SYSTEM AND FOUND THE WINDSHIELD WAS FAULTY. MAINTENANCE REMOVED AND REPLACED THE RT WINDSHIELD IAW BMM, OPS CHK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (X)
- [SDR 95ZZZX4168](https://openairdocs.org/sdr/95ZZZX4168.md): Rivets · loose · Jun 22, 1995 · N155ZV · Beech 1900D · Wing Miscellaneous Structure
  > RIVETS LOCATED IN RT WING OUTBOARD OF NACELLE TOP SPAR AREA LOOSE CAUSING FUEL LEAK. VERY COMMON OCCURRENCE WITH APPROXIMATELY A 6-10 RIVET LENGTH ALONG TOP WING SPAR.

## 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 = 'N155ZV' AND deregistration_id = 'N155ZV-2011-05-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N155ZV-2011-05-06/reports

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