# Service difficulty reports: N146ZV, cancelled Jul 7, 2010

A list on [N146ZV, cancelled Jul 7, 2010](https://openairdocs.org/deregistered/N146ZV-2010-07-07.md).

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

- [SDR AMWA88513BC](https://openairdocs.org/sdr/AMWA88513BC.md): Battery · discharged · Nov 10, 2007 · N146ZV · Beech 1900D · Battery/Charger System
  > AFTER TAKEOFF, HAD BRIEF BATTERY CHARGE ANNUNCIATOR ILLUMINATION. THEN, AFTER NEXT TAKEOFF ANNUNCIATOR REMAINED ILLUMINATED AND WAS ACCOMPANIED BY BATTERY AMMETER AND BOTH GENERATOR LOAD METERS CYCLING. AMMETER CYCLED FROM 0 TO 30A AND LOAD METERS CYCLED FROM
- [SDR AMWA88479BC](https://openairdocs.org/sdr/AMWA88479BC.md): Circuit Board · inoperative · Nov 8, 2007 · N146ZV · Beech 1900D · Battery/Charger System
  > DURING FLIGHT BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED A-130 PC BOARD AND CLEARED DISCREPANCY.
- [SDR AMWA88382BC](https://openairdocs.org/sdr/AMWA88382BC.md): Battery · malfunctioned · Nov 3, 2007 · N146ZV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT MULTIPLE TIMES. BATTERY WAS REPLACED BY MAINTENANCE AND DISCREPANCY CLEARED.
- [SDR AMWA88325BC](https://openairdocs.org/sdr/AMWA88325BC.md): Battery · malfunctioned · Oct 31, 2007 · N146ZV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR ILLUMINATED MULTIPLE TIMES DURING FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. THIS TYPE DISCREPANCY IS CONSIDERED A DISTRACTION TO THE CREW AND A NUISANCE ITEM.
- [SDR AMWA88093BC](https://openairdocs.org/sdr/AMWA88093BC.md): Battery · discharged · Oct 18, 2007 · N146ZV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. BATTERY WAS REPLACED AND DISCREPANCY WAS CLEARED. THIS TYPE ANNUNCIATOR DISCREPANCY IS CONSIDERED A NUISANCE ITEM AND DISTRACTION TO CREW.
- [SDR AMW070223021](https://openairdocs.org/sdr/AMW070223021.md): Skin · dented · Mar 15, 2007 · N146ZV · Beech 1900D · Rudder, Plate/Skin
  > (2) DENTS IN RUDDER; (1) ON THE LT SIDE AND (1) ON THE RT LOWER END CAP. REPAIRED IAW 1900-27-00-0001.
- [SDR AWM070223021A](https://openairdocs.org/sdr/AWM070223021A.md): Frame · chafed · Mar 6, 2007 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..
- [SDR AWM070223021B](https://openairdocs.org/sdr/AWM070223021B.md): Frame · chafed · Mar 6, 2007 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..
- [SDR AWM070223021C](https://openairdocs.org/sdr/AWM070223021C.md): Frame · chafed · Mar 6, 2007 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > RT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR (MAR 5, 2007)..
- [SDR AMW070219056](https://openairdocs.org/sdr/AMW070219056.md): Spar · cracked · Feb 19, 2007 · N146ZV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STAB MAIN SPAR CENTER WEB (4 EA) 0.5 INCH LONG CRACKS EXTENDED OUT FROM DEICE TUBE HOLE. FABRICATED/INSTALLED WEB PATCH.
- [SDR AM1070103027](https://openairdocs.org/sdr/AM1070103027.md): Support Beam · damaged · Jan 6, 2007 · N146ZV · Beech 1900D · Rudder Structure
  > PROBLEM DISCOVERED DURING MAINTENANCE INSPECTION. RUDDER BELLCRANK SUPPORT BEAM REPAIRED IAW AERODESIGN AIRCRAFT ENGINEERING, INC REPORT NR 6496-1 REV. 1 SHEET 1 THROUGH 33. DATED 01/04/2007.
- [SDR AMWA81587](https://openairdocs.org/sdr/AMWA81587.md): Latch · malfunctioned · Dec 24, 2006 · N146ZV · Beech 1900D · Passenger/Crew Doors
  > ON PREFLIGHT, CREW COULD NOT GET CABIN DOOR TO LATCH. MECHANIC SECURED THE DOOR AND THE AIRCRAFT WAS FERRIED. MORE TO BE ADDED WHEN ADL IS RECEIVED.
- [SDR AMWA081062](https://openairdocs.org/sdr/AMWA081062.md): Actuator · inoperative · Nov 30, 2006 · N146ZV · Beech 1900D · Landing Gear Steering System
  > DURING TAXI OUT, THE NOSE WHEEL STEERING FAILED MANUAL CASTER MODE, SINCE CAPT. KNEW THAT CONDITION WAS DEFERRABLE HE CONTINUED ON TO THE NEXT STATION. AFTER ARRIVING, DURING WALK AROUND INSPECTION HE DETECTED THE FAILURE OF THE ACUATOR. PROCEDURE 32-4 WAS PER
- [SDR AMWA080101](https://openairdocs.org/sdr/AMWA080101.md): Switch · out of adjust · Oct 11, 2006 · N146ZV · Beech 1900D · Trailing Edge Flap Control System
  > FLAP HANDLE WAS SELECTED TO 17 DEGREES AND THEY WENT TO 35 DEGREES UNCOMMANDED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND ADJUSTED FLAP SWITCH, OPS CHECKED NORMAL NO PARTS WERE USED.
- [SDR AMWA080040](https://openairdocs.org/sdr/AMWA080040.md): Control System · out of adjust · Oct 9, 2006 · N146ZV · Beech 1900D · Trailing Edge Flap Control System
  > ON APPROACH, CREW PLACED THE FLAP HANDLE TO 17 DEGREES. THE FLAPS CONTINUED TO EXTEND TO 35 DEGREES THUS CAUSING THE OVERSPEED OF THE FLAPS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CAME AND C/W WITH THE FLAP INSPECT IAW BMM 05-50-00 PG 201.
- [SDR AMW060705011A](https://openairdocs.org/sdr/AMW060705011A.md): Skin · bird strike · Jul 7, 2006 · N146ZV · Beech 1900D · Wing, Plate/Skin
  > BIRD STRIKE DAMAGE TO LT WING CENTER LEADING EDGE. DAMAGE 6IN X 3IN X 1IN DEEP. DAMAGE REPAIRED IAW AIR MIDWEST TO 1900-57-20-0006.
- [SDR 105092102690](https://openairdocs.org/sdr/105092102690.md): Stringer · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 3R AT FS 163.9. CRACKED. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. THEREFORE NO PARTS WERE USED.
- [SDR 105092102666](https://openairdocs.org/sdr/105092102666.md): Frame · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > FOUND CRACKED INNERSKIN AND FRAME (ASD) STA 150.6. MAINTENANCE REPAIRED THE PROBLEM.
- [SDR 1050921026131](https://openairdocs.org/sdr/1050921026131.md): Splice Plate · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Miscellaneous Structure
  > FOUND FS 434 CRACKED SPLICE PLATE SIDEWALL. MAINTENANCE REPAIRED THE SPLICE PLATE SIDEWALL.
- [SDR 1050921026160](https://openairdocs.org/sdr/1050921026160.md): Stringer · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 3R AT FS 163.9 CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.
- [SDR 1050921026090](https://openairdocs.org/sdr/1050921026090.md): Stringer · corroded · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > CORRSION FOUND ON FASTENERS FS 150-183 AND STRINGER 1-3R. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE.
- [SDR 1050921026120](https://openairdocs.org/sdr/1050921026120.md): Angle · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Miscellaneous Structure
  > FOUND LEFT FS 400 1 FT ABOVE FLOOR CRACKED. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED.
- [SDR 1050921026072](https://openairdocs.org/sdr/1050921026072.md): Frame · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > FOUND FRAME ANGLE AT FS 456 CRACKED. MAINTENANCE INSPECTED AND NO CRACKS WERE NOTED. THEREFORE NO PARTS WERE USED.
- [SDR 1050921026071](https://openairdocs.org/sdr/1050921026071.md): Stringer · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 12 AT FS 456 RT CRACKED. MAINTENANCE REPAIRED STRINGER WHILE AIRCRAFT WAS IN STRUCTURAL REPAIR.
- [SDR 1050921026](https://openairdocs.org/sdr/1050921026.md): Frame · cracked · Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Frame
  > CRACKED INNER SKIN AND FRAME. MAINTENANCE REPAIRED IAW SRM 51-70-00 AND 51-70-15. MORE INFORMATION WILL BE AVAILABLE AT A LATER TIME.
- [SDR 67974](https://openairdocs.org/sdr/67974.md): Wire · chafed · Dec 26, 2004 · N146ZV · Beech 1900D · Landing Gear Door Retract Section
  > DEPARTING OMA RETRACTED GEAR, C/B TRIPPED. RESET C/B, GEAR THEN RETRACTED, C/B TRIPPED AGAIN. DID NOT RESET 2ND TIME PER CHECK LIST. DIVERTED TO HON MANUAL EXTENSION. MX THEN SECURED LANDING GEAR AND TOWED A/C TO GATE. REPAIRED CHAFED WIRE ON HYDRO GROUND
- [SDR 67554](https://openairdocs.org/sdr/67554.md): Yaw Damper · malfunctioned · Dec 12, 2004 · N146ZV · Beech 1900D · Rudder Control System
  > WHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND CONTINUED FLIGHT WITH NO FURTHER INCIDENT. PERFORMED TAXI TEST. INSPECTED, OPS CHECK NORMAL AT THIS TIME.
- [SDR 58580](https://openairdocs.org/sdr/58580.md): Brake · malfunctioned · Feb 4, 2004 · N146ZV · Beech 1900D · Brake
  > WHILE AIRCRAFT ARRIVED IN FARMINGTON, NEW MEXICO ON FLIGHT 715 THE PARKING BRAKE WHEN APPLIED THE PEDALS WERE MUSHY. MAINTENANCE BLED THE BRAKES. THE AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE USED.
- [SDR 57947](https://openairdocs.org/sdr/57947.md): Brake · malfunctioned · Jan 15, 2004 · N146ZV · Beech 1900D · Landing Gear Brake System
  > BRAKES MUSHY ON CAPT'S SIDE WHEN THE PARKING BRAKE WAS SET. BLEED THE BRAKES.
- [SDR 52268](https://openairdocs.org/sdr/52268.md): Indicator · inoperative · Jul 5, 2003 · N146ZV · Beech 1900D · Landing Gear Position and Warning
  > UPON ARRIVAL, ON FLIGHT 700, THE LANDING GEAR HANDLE DOWN, NO GREEN INICATORS ON. THE RIGHT MAIN MANUAL EXTENSION WAS PERFORMED. FLYBY TOWER CONFIRMED GEAR APPEARED DOWN. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GEAR D
- [SDR AMW3](https://openairdocs.org/sdr/AMW3.md): Intercostal · failed · Nov 27, 2002 · N146ZV · Beech 1900D · Fuselage Miscellaneous Structure
  > AFTER TAKE OFF THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS WER
- [SDR AMW4](https://openairdocs.org/sdr/AMW4.md): Intercostal · cracked · Nov 27, 2002 · N146ZV · Beech 1900D · Cargo/Baggage Doors
  > AFTER TAKE OFF FROM HOT SPRINGS ARKANSAS, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO #2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AN
- [SDR AMW2](https://openairdocs.org/sdr/AMW2.md): Intercostal · failed · Nov 27, 2002 · N146ZV · Beech 1900D · Cargo/Baggage Doors
  > AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS W
- [SDR AMW1](https://openairdocs.org/sdr/AMW1.md): Intercostal · failed · Nov 27, 2002 · N146ZV · Beech 1900D · Cargo/Baggage Doors
  > AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS WERE NO
- [SDR 045447](https://openairdocs.org/sdr/045447.md): Intercostal · failed · Nov 27, 2002 · N146ZV · Beech 1900D · Cargo/Baggage Doors
  > AFTER TAKE OFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A STRONG VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS
- [SDR AMWA14](https://openairdocs.org/sdr/AMWA14.md): Pressure Panel · chafed · Nov 18, 2002 · N146ZV · Beech 1900D · Fuselage, Powerplant Attach Fittings
  > WHILE PERFORMING AND "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THE LT/RT PRESSURE PLATES EXHIBIT RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE CHAFING. NO TEARDOWN REPORT WILL BE REQUIRED.
- [SDR MASA99093](https://openairdocs.org/sdr/MASA99093.md): Switch · failed · Jun 7, 1999 · N146ZV · Beech 1900D · Propeller Feathering/Reversing
  > FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERRIED TO FMN, WHERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE LOW PRESSURE AUTOFEATHER SWITCH AND THE LEFT ENGINE HIGH
- [SDR 99ZZZM390](https://openairdocs.org/sdr/99ZZZM390.md): Switch · failed · Jun 7, 1999 · N146ZV · Beech 1900D · Propeller Feathering/Reversing
  > FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERRIED TO FMN, WHERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE LOW PRESSURE AUTOFEATHER SWITCH AND THE LEFT ENGINE HIGH
- [SDR MASA98027](https://openairdocs.org/sdr/MASA98027.md): Downlock Switch · failed · Feb 11, 1998 · N146ZV · Beech 1900D · Landing Gear Position and Warning
  > FLT 407 - ROW-ABQ - ON APPROACH TO ABQ WITH GEAR SELECTED DOWN, PILOT DID NOT HAVE GREEN NOSE INDICATION AND RED HANDLE WAS STILL ILLUMINATED. CREW DECLARED EMERGENCY, PERFORMED FLYBY OF TOWER TO VERIFY GEAR WAS DOWN, AND LANDED WITHOUT INCIDENT. MAINTENANCE
- [SDR MASA98024](https://openairdocs.org/sdr/MASA98024.md): Switch · out of adjust · Feb 9, 1998 · N146ZV · Beech 1900D · Landing Gear Position and Warning
  > FLT 551 - ALM-ABQ - CREW REPORTED WITH THE LNDING GEAR HANDLE IN DOWN POSITION, PILOT COULD NOT GET NOSE GREEN DOWN AND LOCKED INDICATION. RED GEAR HANDLE LIGHT WAS ILLUMINATED, BUT THERE WAS NO AUDIBLE WARNING. PILOT HAND PUMPED GEAR BUT DID NOT RECEIVE A G
- [SDR MASA98020](https://openairdocs.org/sdr/MASA98020.md): Bulb · failed · Feb 6, 1998 · N146ZV · Beech 1900D · Landing Gear Position and Warning
  > FLT 407 - ROW-ABQ - CREW REPORTED, NO LEFT MAIN GEAR INDICATION. CREW VISUALLY VERIFIED GEAR WAS DOWN. CAPTAIN PUMPED GEAR DOWN UNTIL FELT RESISTANCE. CREW DECLARED AN EMERGENCY AND PROCEEDED TO LAND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE
- [SDR MASA97215](https://openairdocs.org/sdr/MASA97215.md): Handle Assy · lack of lube · Oct 7, 1997 · N146ZV · Beech 1900D · Emergency Exits
  > DURING NIGHT MAINTENANCE, THE LT EMERGENCY EXIT WAS FOUND HARD TO OPERATE. MAINTENANCE LUBRICATED THE HANDLE ASSY. OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE. AC TTL HRS: 5,924. AC TTL CYCLES: 9,665. (X)

## 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 = 'N146ZV' AND deregistration_id = 'N146ZV-2010-07-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N146ZV-2010-07-07/reports

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