# Service difficulty reports: N126YV, cancelled Jun 30, 2010 A list on [N126YV, cancelled Jun 30, 2010](https://openairdocs.org/deregistered/N126YV-2010-06-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AMWA89204](https://openairdocs.org/sdr/AMWA89204.md): Pcb · inoperative · Dec 20, 2007 · N126YV · Beech 1900D · Landing Gear Retraction/Extension System > LANDING GEAR GAVE NO REACTION WHEN GEAR HANDLE EXTENDED. MOVED FLAPS TO FULL DOWN, LANDING GEAR WARNING HORN SOUNDED. FOLLOWED EMERGENCY CHECKLIST AND MANUALLY EXTENDED THE GEAR AND GOT 3 GEAR SAFE INDICATION LIGHTS AND LANDED SAFELY. MAINTENANCE REPLACED A316 - [SDR AMWA28032](https://openairdocs.org/sdr/AMWA28032.md): Spar · sheared · Jul 5, 2007 · N126YV · Beech 1900D · Wing Spar > SHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R. - [SDR AMWA7026D](https://openairdocs.org/sdr/AMWA7026D.md): Rib · corroded · Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/Bulkhead > BIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R. - [SDR AMWA7026C](https://openairdocs.org/sdr/AMWA7026C.md): Skin · chafed · Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/Skin > FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R. - [SDR AMWA7026B](https://openairdocs.org/sdr/AMWA7026B.md): Skin · chafed · Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/Skin > FRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R. - [SDR AMWA7026A](https://openairdocs.org/sdr/AMWA7026A.md): Rib · corroded · Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/Bulkhead > BIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702-4 REV 1R. - [SDR AMWA7020E](https://openairdocs.org/sdr/AMWA7020E.md): Skin · cracked · Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED, LENGTH APPROX 1.5 INCHES. REPAIRED IAW REPORT #6702-3 REV 1R. - [SDR AMWA7020D](https://openairdocs.org/sdr/AMWA7020D.md): Skin · cracked · Jun 12, 2007 · N126YV · Beech 1900D · Wing, Plate/Skin > RT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 6702-2 REV 1R. - [SDR AMWA7020B](https://openairdocs.org/sdr/AMWA7020B.md): Frame · chafed · Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Frame > FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. - [SDR AMWA7020A](https://openairdocs.org/sdr/AMWA7020A.md): Frame · chafed · Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Frame > FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R. - [SDR AMWA7020C](https://openairdocs.org/sdr/AMWA7020C.md): Frame · chafed · Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Frame > FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW ACFT REPORT NR 6702-1 REV 1R - [SDR AMW082671](https://openairdocs.org/sdr/AMW082671.md): Actuator · false indication · Feb 15, 2007 · N126YV · Beech 1900D · Landing Gear Actuator > ON APPROACH TO LANDING THE NOSE GEAR INDICATOR D/N SHOW GEAR DOWN AND LOCKED. CREW PERFORMED EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. A FLY-BY OF THE TOWER CONFIRMED GEAR WAS DOWN. THE INTRANSIT LIGHT IN THE GEAR HANDLE WAS ALSO OUT. SO CREW LANDED S - [SDR AMWA82479BC](https://openairdocs.org/sdr/AMWA82479BC.md): Battery · discharged · Feb 5, 2007 · N126YV · Beech 1900D · Battery/Charger System > BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR THE DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. - [SDR AMWA81896](https://openairdocs.org/sdr/AMWA81896.md): Bulb · inoperative · Jan 7, 2007 · N126YV · Beech 1900D · Landing Gear Position and Warning > WHEN GEAR WS EXTENDED FOR LANDING, THERE WAS NO DOWN AND LOCKED INDICATION ON ANNUNCIATOR. CREW DECLAIRED EMERGENCY, AND FOLLOWED PROCEDURES. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED ANNUNCIATOR BULBS. PENDING ADL RETURN. - [SDR AMW1061011025](https://openairdocs.org/sdr/AMW1061011025.md): Spar Cap · corroded · Oct 13, 2006 · N126YV · Beech 1900D · Wing Spar > FOUND CHAFING AREA, LT WING LOWER MAIN SPAR CAR, FORWARD SURFACE AT APPROX. WS 72.0. REPAIRED IAW MFG FR-CO-01437 REV. 1. - [SDR AMWA078634](https://openairdocs.org/sdr/AMWA078634.md): Cable · broken · Jul 27, 2006 · N126YV · Beech 1900D · Passenger/Crew Doors > ON PREFLIGHT, THE CREW COULD NOT OPEN THE CABIN DOOR. MAINTENANCE WAS CALLED AND FOUND THE INNER FORWARD DOOR CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BROKEN CABLE AND CABLE GUIDE ASSY. - [SDR 1051213026A](https://openairdocs.org/sdr/1051213026A.md): Angle · cracked · Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous Structure > DURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED. - [SDR 1051213026](https://openairdocs.org/sdr/1051213026.md): Angle · cracked · Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous Structure > DURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED. - [SDR 71138](https://openairdocs.org/sdr/71138.md): Diode · faulty · Jun 2, 2005 · N126YV · Beech 1900D · Emergency Lighting > EMERGENCY COCKPIT LIGHTING ON, OFF HOT BATTERY BUSS, MAIN BATTERY SWITCH OFF AND SWITCH FOR FLIGHT INSTRUMENT INDIRECT LIGHTS ON. ELECTRICAL ODOR IN COCKPIT AREA. MAINTENANCE REMOVED AND REPLACED DIODE. - [SDR 71124](https://openairdocs.org/sdr/71124.md): Rheostat · burned · Jun 1, 2005 · N126YV · Beech 1900D · Passenger Compartment Lighting > CREW CALLED IN AND REPORTED THAT WITH COCKPIT EMERGENCY LIGHTS ON, BATTERY OFF, INDIRECT LIGHTING ON, THERE WAS AN ELECTRICAL BURNING ODOR. MAINTENANCE REMOVED AND REPLACED INDIRECT LIGHT RHEOSTAT SWITCH. - [SDR 68027](https://openairdocs.org/sdr/68027.md): Wheel · damaged · Dec 29, 2004 · N126YV · Beech 1900D · Nose/Tail Landing Gear > UPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STOPPED THE AIRCRAFT ON THE APRON WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY, NOSE GEAR ASSY, DRAG LEG ASSY. VISUALLY INS - [SDR 66764](https://openairdocs.org/sdr/66764.md): Light · loose · Nov 14, 2004 · N126YV · Beech 1900D · Exterior Lighting > DURING TAXI, CREW NOTED TAXI LIGHT JUMPING BACK AND FORTH. RETURNED TO GATE AND NOTED TAXI LIGHT HAD COME LOOSE AT MOUNTING POINT. NO FURTHER INCIDENT. REMOVED AND REPLACED LIGHT ASSY BULB AND HARDWARE, P/N A715-1, 130909B124, 130909B45, 130909N32. - [SDR 66269](https://openairdocs.org/sdr/66269.md): Yaw Damper · malfunctioned · Oct 29, 2004 · N126YV · Beech 1900D · Autopilot System > YAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETURNED TO GATE AND THE SYSTEM WAS DEFERRED WITH NO FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND YAW DAMPER OPS CK NORMAL. - [SDR 63720](https://openairdocs.org/sdr/63720.md): Wire · broken · Aug 7, 2004 · N126YV · Beech 1900D · Fire Protection System Wiring > AIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE BOTTLE, OPS CK NORMAL. - [SDR 61901](https://openairdocs.org/sdr/61901.md): Downlock Switch · malfunctioned · May 31, 2004 · N126YV · Beech 1900D · Landing Gear Position and Warning > WITH MAIN LANDING GEAR SELECTED DOWN THE LEFT MAIN LANDING GEAR WON'T INDICATE DOWN AND LOCKED. AIRCRAFT DIVERTED TO DUJ. EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LT MLG ACTUATOR/DOWNLOCK SWITCH CK GOOD. P/N 114-38 - [SDR 61743](https://openairdocs.org/sdr/61743.md): Control Unit · malfunctioned · May 25, 2004 · N126YV · Beech 1900D · Landing Gear Position and Warning > ON APPROACH FOR LANDING IN PFN, THE LT MAIN GEAR WON'T INDICATE DOWN AND LOCK. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED A125 PCB, OPS CHECK NORMAL. P/N 101-364578-9, S/N 671396. - [SDR 61073](https://openairdocs.org/sdr/61073.md): Connector · burned · May 3, 2004 · N126YV · Beech 1900D · Electrical Connectors > CREW REPORTED ON APPROACH ANNUNICATOR C.B. TRIPPED. IT WAS RESET AND POPPED AGAIN. THERE WAS A FAINT BURNED ODOR IN THE CABIN. LANDED WITH NO FURTHER INCIDENT. R&R FEED THRU CONNECTOR. - [SDR 56696](https://openairdocs.org/sdr/56696.md): Latch · broken · Dec 2, 2003 · N126YV · Beech 1900D · Passenger/Crew Doors > UPON ARRIVAL CREW HAD DOOR WARNING ANNUNCIATOR. IT WOULD NOT EXTUNGUISH. MAINT WAS CALLED AND FOUND LATCH CABLE BROKEN. CABIN DOOR INOPERATIVE CAMS ON AFT SIDE WILL NOT CLOSE. REMOVED AND REPLACED AFT DOOR LATCH CABLE. P/N 129-514059-25 - [SDR 54992](https://openairdocs.org/sdr/54992.md): Indicator · failed · Oct 6, 2003 · N126YV · Beech 1900D · Engine BMEP/Torque Indicating > RIGHT TORQUE GAUGE FAILED ON TAKE OFF DURING INITIAL POWER UP. RETURNED TO GATE AND CALLED MX. REPLACED GAUGE OPS CK GOOD P/N 114-3800-653 SN 390MU. - [SDR 52034](https://openairdocs.org/sdr/52034.md): Uplock Switch · faulty · Jun 28, 2003 · N126YV · Beech 1900D · Landing Gear Position and Warning > DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3GREEN) INICATIONS. LANDING NORMAL WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED ON T - [SDR 52034AMWA2](https://openairdocs.org/sdr/52034AMWA2.md): Valve · failed · Jun 28, 2003 · N126YV · Beech 1900D · Landing Gear Retraction/Extension System > DURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3 GREEN) INDICATIONS. LANDED NORMALLY WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED O - [SDR 049124](https://openairdocs.org/sdr/049124.md): Circuit Breaker · failed · Mar 24, 2003 · N126YV · Beech 1900D · Electrical Power System Wiring > AFTER TAKE OFF FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 706,WHEN THE LANDING GEAR WAS SELECTED UP, SMOKE WAS DETECTED FROM THE RIGHT HAND CIRCUIT BREAKER PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. THE CREW RETURNED TO FA - [SDR 57708](https://openairdocs.org/sdr/57708.md): Actuator · malfunctioned · Jan 7, 2003 · N126YV · Beech 1900D · Landing Gear Actuator > APPROACH, L/G HANDLE MOVED TO LWR GEAR, RED INTRANSIT LAMPS FLICKERED, 5-AMP L/G IND ON RT C/B PANEL POPPED. L/G EXTENDED, 3 GEAR DOWN LIGHTS FAILED TO ILLUM, WOULD NOT RESET. TOWER VERIFIED NOSE L/G EXTENDED. MALFUNCTION NOT DUPLICATED ON GROUND. L/G IND - [SDR 044989](https://openairdocs.org/sdr/044989.md): Fire Loop · broken · Nov 12, 2002 · N126YV · Beech 1900D · Fire Detection > DURING CREW CHANGEOVER IN ALBUQUERQUE, THE PILOTS DISCOVERED THAT THE LT FIRE HANDLE ILLUMINATED DURING PREFLIGHT CHECKS. THE LIGHT WOULD NOT EXTINGUISH. THE CORRECTIVE ACTION WAS THAT MAINTENANCE FOUND THE FORWARD LOOP BROKE. THEY INSTALLED A NEW LOOP. NO TEA - [SDR MASA98175](https://openairdocs.org/sdr/MASA98175.md): Switch · out of adjust · Sep 12, 1998 · N126YV · Beech 1900D · Propeller Feathering/Reversing > FLT 5331 - RDG-PHL - THE LEFT AUTOFEATHER WOULD NOT ARM ON TAKEOFF, AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR 97ZZZX3290](https://openairdocs.org/sdr/97ZZZX3290.md): Attach Bracket · excess wear · Jul 11, 1997 · N126YV · 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 95ZZZW464](https://openairdocs.org/sdr/95ZZZW464.md): De-Ice Boot · separated · Mar 11, 1995 · N126YV · Beech 1900D · Propeller Deice Boot Section > TWO PROP DE-ICE BOOTS SEPARATING FROM LEADING EDGE EROSION SHIELD. PAINT ON SHIELD SEPARATED FROM SHIELD. SUBMITTER SUGGEST IMPROVING PAINTING PROCEDURES ON PROP BLADES OR LEAVING PAINT OFF OR EROSION SHIELD. ## 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 = 'N126YV' AND deregistration_id = 'N126YV-2010-06-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N126YV-2010-06-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.