# Service difficulty reports: N176YV

A list on [N176YV](https://openairdocs.org/aircraft/N176YV.md).

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

Page 1 of 2 · 57 reports

- [SDR AMWA88439BC](https://openairdocs.org/sdr/AMWA88439BC.md): Battery · failed · Nov 6, 2007 · N176YV · Beech 1900D · Battery/Charger System
  > DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REMOVED AND REPLACED BATTERY AND CLEARED DISCREPANCY.
- [SDR AMWA88091BC](https://openairdocs.org/sdr/AMWA88091BC.md): Battery · discharged · Oct 18, 2007 · N176YV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY REPLACED BY MAINTENANCE, DISCREPANCY CLEARED. THIS TYPE ANNUNCIATOR DISCREPANCY IS CONSIDERED A NUISANCE ITEM AND DISTRACTION TO CREW.
- [SDR AMWA87824](https://openairdocs.org/sdr/AMWA87824.md): Hsi · odor · Oct 4, 2007 · N176YV · Beech 1900D · Directional Gyro and Indicating System
  > ELECTRICAL ODOR REPORTED IN COCKPIT ON CLIMBOUT. RETURNED TO FIELD AND MAINTENANCE VERIFIED THAT PROBLEM ORIGINATING IN CAPTAIN'S EHSI. REMOVED AND REPLACED UNIT, OPERATIONAL CHECK WAS SATISFACTORY.
- [SDR AMWA0828013](https://openairdocs.org/sdr/AMWA0828013.md): Spar Cap · corroded · Oct 2, 2007 · N176YV · Beech 1900D · Wing Spar
  > BIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR.
- [SDR AMWA0828013B](https://openairdocs.org/sdr/AMWA0828013B.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED LT AND RT FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 213.25.
- [SDR AMWA0828013J](https://openairdocs.org/sdr/AMWA0828013J.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 408.25.
- [SDR AMWA0828013D](https://openairdocs.org/sdr/AMWA0828013D.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 243.25, RT.
- [SDR AMWA0828013C](https://openairdocs.org/sdr/AMWA0828013C.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT FS 228.25.
- [SDR AMWA0828013G](https://openairdocs.org/sdr/AMWA0828013G.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 318.25.
- [SDR AMWA0828013H](https://openairdocs.org/sdr/AMWA0828013H.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 363.25.
- [SDR AMWA0828013K](https://openairdocs.org/sdr/AMWA0828013K.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 438.25.
- [SDR AMWA0828013I](https://openairdocs.org/sdr/AMWA0828013I.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 378.25.
- [SDR AMWA0828013F](https://openairdocs.org/sdr/AMWA0828013F.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 303.25.
- [SDR AMWA0828013E](https://openairdocs.org/sdr/AMWA0828013E.md): Frame · chafed · Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, Frame
  > REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING AT FS 258.25.
- [SDR AMWA0828013A](https://openairdocs.org/sdr/AMWA0828013A.md): Skin · damaged · Oct 2, 2007 · N176YV · Beech 1900D · Wing, Plate/Skin
  > RT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR.
- [SDR AMWA84517](https://openairdocs.org/sdr/AMWA84517.md): Annunciator · worn · May 9, 2007 · N176YV · Beech 1900D · Landing Gear Retraction/Extension System
  > UPON DEPART GEAR RETRACTED NORMALLY. NO PROBLEMS UNTIL GEAR EXTENSION. COULD NOT DETERMINE IF GEAR WAS COMPLETELY DOWN. FLEW BY TOWER AND THEY SAID IT APPEARED ONE OF THE GEAR WAS NOT COMPLETELY DOWN. PERFORMED MANUAL EXTENSION, BURNED OFF ADDITIONAL FUEL
- [SDR AWM083022](https://openairdocs.org/sdr/AWM083022.md): B-Nut · loose · Mar 3, 2007 · N176YV · Beech 1900D · Landing Gear Brake System
  > WHEN CREW ARRIVED AT DESTINATION THEY CALLED INTO MAINT CONTROL AND WROTE UP THE LT BRAKES NOT GETTING FULL BRAKING ACTION. TIGHTENED B-NUT, CLEANED AND BLED BRAKES, OPS CK NORMAL.
- [SDR AMW082983BC](https://openairdocs.org/sdr/AMW082983BC.md): Battery · false indication · Mar 1, 2007 · N176YV · Beech 1900D · Battery/Charger System
  > WHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACE
- [SDR AMWA82619BC](https://openairdocs.org/sdr/AMWA82619BC.md): Battery · discharged · Jan 22, 2007 · N176YV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.
- [SDR AMW1061218001](https://openairdocs.org/sdr/AMW1061218001.md): Sensor · failed · Dec 12, 2006 · N176YV · Beech 1900D · Landing Gear Position and Warning
  > DURING A LANDING GEAR RETRACT CHECK, IT WAS NOTICED THAT SPARKS AND SMOKE WAS EMITTING FROM THE LIQUID LOW LEVEL SENSOR INSTALLED ON THE LANDING GEAR POWER PACK. THE SENSOR WAS REPLACED AND NO FURTHER PROBLEMS WERE NOTICED.
- [SDR AMW78306](https://openairdocs.org/sdr/AMW78306.md): Fuel Cap · missing · Jul 7, 2006 · N176YV · Beech 1900D · Fuel Storage
  > LT FUEL CAP CAME LOOSE ON CLIMB OUT AND WEDGED IN BETWEEN WING AND AILERON. EXTRA TRIM WAS REQUIRED FOR CLIMB, BUT AILERONS REMAINED FULLY CONTROLLABLE IN FLIGHT. THE CREW RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND PERFORMED AILE
- [SDR 1060607019](https://openairdocs.org/sdr/1060607019.md): Web · worn · Jun 13, 2006 · N176YV · Beech 1900D · Nacelle/Pylon, Bulkhead/Firewall
  > HOLE WORN ON WEB OF LT FIREWALL. LOOSE FASTENER FOUND TO HAVE CAME LOOSE AND WORE OUT THE HOLE. EXTRA CARE HAS BEEN TAKEN TO ENSURE THE FASTENER TO BE CHECKED FOR PROPER TORQUE. HOLE REPAIRED IAW MFG FR-CO-01357 REV 1.
- [SDR 1060406014A](https://openairdocs.org/sdr/1060406014A.md): Spar · corroded · Apr 26, 2006 · N176YV · Beech 1900D · Wing Spar
  > BIO CORROSION LT MAIN SPAR CAP FLANGE AT WS 124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1
- [SDR 1060406014](https://openairdocs.org/sdr/1060406014.md): Spar · corroded · Apr 26, 2006 · N176YV · Beech 1900D · Wing Spar
  > BIOCORROSION RT MAIN SPAR CAP FLANGE AT WS124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1
- [SDR 74809](https://openairdocs.org/sdr/74809.md): Fire Loop · failed · Dec 19, 2005 · N176YV · Beech 1900D · Fire Detection
  > WHILE IN ROUTE, THE LT T-HANDLE ILLUMINATED. CREW COMPLIED WITH EMERGENCY CHECKLIST AND DIVERTED DECLARED EMERGENCY AND LANDED SAFELY WITH NO FURTHER INCIDENT. IT WAS THEN FERRIED, MAINTENACE REMOVED AND REPLACED LT FWD FIRE LOOP ASSY.
- [SDR 74784](https://openairdocs.org/sdr/74784.md): Brake · weak · Dec 18, 2005 · N176YV · Beech 1900D · Landing Gear Brake System
  > WHILE TAXING IN, THE CREW NOTICED THE BRAKES WERE SPONGEY. THE AIRCRAFT WAS THEN FERRIED AND MAINTENANCE BLED THE BRAKES. NO PARTS USED.
- [SDR 74798](https://openairdocs.org/sdr/74798.md): Master Cylinder · failed · Dec 18, 2005 · N176YV · Beech 1900D · Master Cylinder/Brake Valve
  > DURING TAXI IN, THE CREW REPORTED THE BRAKES FEELING SPONGY. THEN FERRIED TO ICT WHERE MAINTENANCE REMOVED AND REPLACED THE MASTER CYLINDER.
- [SDR 71037](https://openairdocs.org/sdr/71037.md): Brake · malfunctioned · May 26, 2005 · N176YV · Beech 1900D · Landing Gear Brake System
  > ON TAXI TO GATE BRAKES WERE SPONGY. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THEREFORE NO PARTS WERE USED.
- [SDR 70122](https://openairdocs.org/sdr/70122.md): Brake · dirty · Apr 4, 2005 · N176YV · Beech 1900D · Brake
  > AFTER ARRIVING AT GATE IN DFW, CREW REPORTED LEFT BRAKE WEAK. MAINTENANCE CLEANED THE BRAKES. THEREFORE NO PARTS WERE USED.
- [SDR 68837](https://openairdocs.org/sdr/68837.md): Brake · failed · Feb 1, 2005 · N176YV · Beech 1900D · Brake
  > AFTER TAXI IN LEFT BRAKE WEAK. REMOVED AND REPLACED LT BRAKE.
- [SDR 67819](https://openairdocs.org/sdr/67819.md): Brake Assy · smoke · Dec 21, 2004 · N176YV · Beech 1900D · Brake
  > AFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME.
- [SDR 64107](https://openairdocs.org/sdr/64107.md): Socket · dirty · Aug 21, 2004 · N176YV · Beech 1900D · Landing Gear Position and Warning
  > DISPATCH RECEIVED A CALL FROM MGW STATION THAT THEY HAD BEEN CONTACTED BY FLT 4740 AND INFORMED THAT THE AIRCRAFT DID NOT HAVE 3 GOOD DOWN AND LOCK INDICATIONS FOR MAIN LANDING. CREW WAS ADVISED TO FOLLOW CHECKLIST AND DIVERT. THEY LEARNED LATER THAT CREW HAD
- [SDR 63455](https://openairdocs.org/sdr/63455.md): Uplock Switch · failed · Jul 29, 2004 · N176YV · Beech 1900D · Landing Gear Position and Warning
  > AFTER TAKEOFF WHEN GEAR WAS RETRACTED THE LANDING GEAR IN-TRANSIT LIGHT REMAINED ILLUMINATED. CREW CONTACTED DISPATCH AND MAINTENANCE CONTROL. CREW WAS TOLD TO DIVERT. AIRCRAFT THEN DIVERTED, LANDED WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED RT UPLOCK
- [SDR 63428](https://openairdocs.org/sdr/63428.md): Brake Assy · malfunctioned · Jul 28, 2004 · N176YV · Beech 1900D · Brake
  > WHILE TAXING IN AFTER LANDING IN TPA. CAPTAIN FELT THAT THE LT BRAKE FELT SPONGY. THEN CALLED MAINTENANCE. BRAKES WAS BLEED, OPS CK NORMAL.
- [SDR 59816](https://openairdocs.org/sdr/59816.md): Nut · loose · Mar 18, 2004 · N176YV · Beech 1900D · Brake
  > ON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE. IT WAS TIGHTENED.
- [SDR 57453](https://openairdocs.org/sdr/57453.md): Brake · inoperative · Dec 29, 2003 · N176YV · Beech 1900D · Brake
  > UPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.
- [SDR AMWA44](https://openairdocs.org/sdr/AMWA44.md): Rib · cracked · Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46, STRG 101-640000-42 ON RT SIDE AND STRG P/N 101-640000-41, STRG P/N 101-640000-37 (4EA CRACKS TOTAL ON THIS RIB)
- [SDR AMWA43](https://openairdocs.org/sdr/AMWA43.md): Rib · cracked · Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 STRG P/N 101-640000-42 BOTH RT SIDE AND STRG P/N 101-640000-37 STRG P/N 101-640000-45 ON LT SIDE (4 EA TOTAL CRACKS ON THIS RIB)
- [SDR AMWA42](https://openairdocs.org/sdr/AMWA42.md): Rib · cracked · Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER.
- [SDR 53866](https://openairdocs.org/sdr/53866.md): Printed Ckt Board · faulty · Aug 26, 2003 · N176YV · Beech 1900D · Landing Gear Retraction/Extension System
  > UPON APPROACH TO VPS LANDING GEAR WOULD NOT EXTEND. A SECOND ATTEMP WAS MADE WITH THE SAME THING NO DOWN AND LOCKED INDICATION FLY BY OF TOWER AT VPS. CONFIRMED GEAR WAS NOT DOWN. GEAR WAS THEN PUMPED DOWN AND LOCKED CONFIRMED BY GEAR DOWN AND LOCK INDICATI
- [SDR 98ZZZM891](https://openairdocs.org/sdr/98ZZZM891.md): Switch · malfunctioned · Oct 10, 1998 · N176YV · Beech 1900D · Detection System
  > FLT 5633 - RETURNED TO THE FIELD IN MCI WHEN THE LEFT FIRE LOOP LIGHT CAME ON IN FLIGHT. MCI MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY, BUT DID CHANGE THE T-HANDLE AND RETURNED THE AIRCRAFT TO SERVICE AFTER A TEST FLIGHT THAT PRODUCED NO DISCREPANCY. (
- [SDR 98ZZZM885](https://openairdocs.org/sdr/98ZZZM885.md): Switch · malfunctioned · Oct 10, 1998 · N176YV · Beech 1900D · Detection System
  > FLT 5665 - ICT-MCI - EN ROUTE, T-HANDLE AND FIRE LOOP ILLUMINATE INTERMITTENTLY. ICT MAINTENANCE FOUND AND REPAIRED CHAFFED WIRES UNDER THE LEFT FORWARD FLOORBOARD AND REPLACED THE LEFT FIRE LOOP TEST SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURT
- [SDR 98ZZZM883](https://openairdocs.org/sdr/98ZZZM883.md): Harness · loose · Oct 9, 1998 · N176YV · Beech 1900D · Detection System
  > FLT 5600 - RTF WHEN THE LT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. THE LEFT ENGINEWAS SHUT DOWN. EMERGENCY EQUIPMENT WAS CALLED. AIRCRAFT LANDED WITHOUT INCIDENT. ICT MAINTENANCE THEN RETURNED THE AIRCRAFT TO SERVICE. (M)
- [SDR 98ZZZM903](https://openairdocs.org/sdr/98ZZZM903.md): Fire Loop · malfunctioned · Oct 8, 1998 · N176YV · Beech 1900D · Detection System
  > FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)
- [SDR 98ZZZM902](https://openairdocs.org/sdr/98ZZZM902.md): Fire Loop · malfunctioned · Oct 8, 1998 · N176YV · Beech 1900D · Detection System
  > FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)
- [SDR 98ZZZM901](https://openairdocs.org/sdr/98ZZZM901.md): Fire Loop · loose · Oct 7, 1998 · N176YV · Beech 1900D · Detection System
  > FLIGHT 5609 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED. INTERMITTENTLY IN FLIGHT. MAINTENANCE FOUND LOOSE WIRE AT LOOP CONNECTOR. WIRE WAS RESOLDERED, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)
- [SDR 98ZZZM896](https://openairdocs.org/sdr/98ZZZM896.md): Skin · cracked · Mar 28, 1998 · N176YV · Beech 1900D · Trailing Edge Flaps
  > OVERNIGHT MAINTENANCE IN ICT FOUND A 1 INCH CRACK IN TOP SKIN.5 INCH FROM INBOARD AND 9.5 INCH FROM TE ON RHOB FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 98ZZZM434](https://openairdocs.org/sdr/98ZZZM434.md): Skin · loose · Jan 17, 1998 · N176YV · Beech 1900D · Trailing Edge Flaps
  > IN ICT AT OVERNIGHT DETAIL NR 1 INSPECTION, MAINTENANCE FOUND SEVERAL RIVETS LOOSE AND PULLED THROUGH THE SKIN ON THE BOTTOM SKIN OF RT INBOARD FLAP. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM1196](https://openairdocs.org/sdr/97ZZZM1196.md): Brackets · worn · Oct 1, 1997 · N176YV · Beech 1900D · Trailing Edge Flaps
  > FLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW TO 1900-27-50-0001. (M)
- [SDR 97ZZZM1195](https://openairdocs.org/sdr/97ZZZM1195.md): Brackets · worn · Oct 1, 1997 · N176YV · Beech 1900D · Trailing Edge Flaps
  > FLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW TO 1900-27-50-0001. (M)

Next page: https://openairdocs.org/aircraft/N176YV/reports.md?page=2

## 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 = 'N176YV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N176YV/reports

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