# N127ZV: 1994 Beech 1900D, registration cancelled 2013-08-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 19, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162) - Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Serial number: UE-127 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: December 17, 1994 - Last registry action: July 22, 2010 - Mode S code: A07006 - Location: [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery) - Owner type: Individual - Owner's area on the map: 32.3391° N, 86.4011° W: Placed by OpenAirDocs at the center of ZIP code 36108, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N127ZV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=127ZV - Page: https://openairdocs.org/deregistered/N127ZV-2013-08-19 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Beech 1900D: https://openairdocs.org/model/beech-1900d.md ## Service difficulty reports (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AMWA071130025](https://openairdocs.org/sdr/AMWA071130025), Dec 10, 2007: DOUBLER. CHAFED. AFT ACM SCREEN ASSEMBLY CHAFING INTO DOUBLER P/N 114-120022-11 IN RT WING CENTER SECTION AT WS 67.05. REPAIRED IAW SRM 51-40-02 AND CLEARED DISCREPANCY. - [SDR AMWA88803BC](https://openairdocs.org/sdr/AMWA88803BC), Nov 27, 2007: BATTERY. DISCHARGED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED FOR A SHORT TIME. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. - [SDR AMWA88437BC](https://openairdocs.org/sdr/AMWA88437BC), Nov 6, 2007: BATTERY. FAILED. DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. - [SDR AMWA88061](https://openairdocs.org/sdr/AMWA88061), Oct 16, 2007: SKIN. CORRODED. SURFACE TYPE CORROSION FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN IN AIRCRAFT BELLY. FS213.25 STR 13R-15R, STR 14L-16, 228.25 STR 13R-16. INSPECTED, CLEANED, AN - [SDR AMWA87942BC](https://openairdocs.org/sdr/AMWA87942BC), Oct 10, 2007: BATTERY. DISCHARGED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY WAS REPLACED AND DISCREPANCY WAS CLEARED. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS CONSIDERED A NUIS - [SDR AMWA85129BC](https://openairdocs.org/sdr/AMWA85129BC), Jun 5, 2007: CHARGER. LOOSE. AFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISA - [SDR 85129BC](https://openairdocs.org/sdr/85129BC), Jun 5, 2007: CHARGER. LOOSE. AFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISA - [SDR AMWA84103](https://openairdocs.org/sdr/AMWA84103), Apr 20, 2007: UNKNOWN. UNKNOWN. AFTER TAKEOFF THE CABIN DOOR ANNUN ILLUMINATED. RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. OPERATED DOOR NUMEROUS TIMES. OPS CHECKED GOOD. - [SDR AMW107001001](https://openairdocs.org/sdr/AMW107001001), Jan 11, 2007: SKIN PANEL. CRACKED. DURING THE INSPECTION PHASE OF A NR 4 DETAILED INSPECTION, A 2.5 INCH SPANWISE CRACK WAS FOUND ON THE UNDERSIDE OF THE RT WING AT WING STATION B.L. 29.06. NO SB - [SDR AMW1061010024](https://openairdocs.org/sdr/AMW1061010024), Jan 10, 2007: SPAR CAP. CORRODED. DURING STRUCTURAL INSPECTION, MAINTENANCE FOUND SOME BIO-CORROSION ON LT WING MAIN SPAR LOWER CAP BETWEEN WS 114 AND WS 124. REPAIRED IAW MFG FR-CO-01443 REV. 4 - [SDR AMWA079616](https://openairdocs.org/sdr/AMWA079616), Sep 16, 2006: POWERPACK. UNDERSERVICED. AFTER DEPARTURE, THE CREW RETRACTED THE GEAR AND THE INTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW THEN CYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. CR - [SDR AMW078387](https://openairdocs.org/sdr/AMW078387), Jul 12, 2006: WARNING LIGHT. INOPERATIVE. UPON GEAR EXTENSION FLIGHT CREW DID NOT GET THE 3 GREEN GEAR DOWN AND LOCK ANNUCIATION. CREW DECLARED EMERGENCY, EQUIPMENT WAS CALLED OUT, AIRCRAFT LANDED SAFEL - [SDR AMWA78291](https://openairdocs.org/sdr/AMWA78291), Jul 6, 2006: SWITCH. OUT OF RIG. CREW OBSERVED THE PAX DOOR ANNUNICATOR ILLUMINATE INTERMITTENTLY WITH PAX DOOR CLOSED. THE AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND - [SDR 77773](https://openairdocs.org/sdr/77773), Jun 2, 2006: INDICATOR. MALFUNCTIONED. UPON APPROACH CREW EXTENDED THE LANDING GEAR AND DID NOT GET A GREEN DOWN AND LOCK INDICATION ON ANY OF THE THREE LANDING GEAR DOWN AND LOCK INDICATORS, FOLLOWE - [SDR 76473](https://openairdocs.org/sdr/76473), Mar 20, 2006: ACTUATOR. CRACKED. UPON ARRIVAL, CREW REPORTED EVIDENCE OF HYDRAULIC FLUID COMING FROM RIGHT WHEEL WELL. CONTRACT MAINTENANCE WAS CALLED AND REPORTED HYDRAULIC FLUID LEAKING FROM - [SDR 73619](https://openairdocs.org/sdr/73619), Oct 19, 2005: BOLT. UNKNOWN. AFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOLT IN RIGHT SQUAT SWITCH. - [SDR AMWA73619](https://openairdocs.org/sdr/AMWA73619), Oct 19, 2005: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 1051101026](https://openairdocs.org/sdr/1051101026), Oct 1, 2005: SPRING. BROKEN. FLIGHT CREW REPORTED THAT WHILE ON THE GROUND WHEN THE CONTROL YOKE WAS LET LOOSE IT WOULD FLOP OVER TO THE RIGHT. MAINTENANCE PERSONNEL FOUND THE AFT AILERON/R - [SDR 73127](https://openairdocs.org/sdr/73127), Sep 23, 2005: TERMINAL. CRACKED. DURING A ROUTINE INSPECTION, INSPECTION PERSONNEL FOUND THE RT ENGINE BETA CABLE FRONT PUSH PULL TERMINAL CRACKED AROUND THE ENTIRE CIRCUMFERENCE. IT IS UNKNOWN - [SDR 69932](https://openairdocs.org/sdr/69932), Mar 23, 2005: HANDLE. UNSECURE. UPON PREFLIGHT WALK AROUND INSPECTION, CREW NOTICED 6F EMERGENCY DOOR EXTERIOR HANDLE POPPED OUT. MAINTENANCE RESECURED DOOR WITH NO FURTHER INCIDENT. THEREFORE - [SDR 68374](https://openairdocs.org/sdr/68374), Jan 11, 2005: INDICATOR. READS LOW. AFTER T/O AND APPROXIMATELY 10 MINUTES INTO FLIGHT. CREW NOTICED RIGHT HAND ITT INDICATOR DROPPED TO ZERO. TOOK INSTRUCTIONS RTF ABQ LANDED AND TAXIED TO GATE W - [SDR 62912](https://openairdocs.org/sdr/62912), Jul 8, 2004: OXYGEN MASK. DEPLOYED. PAX O2 MASKS DEPLOYING UPON AIRCRAFT CLIMB. FLIGHT CREW UNAWARE IF MASK DEPLOYMENT UNTIL LANDING IN ABQ. RESECURED PAX O2 MASK - [SDR AMWA41](https://openairdocs.org/sdr/AMWA41), Sep 7, 2003: RIB. CRACKED. RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-37 LT SIDE (1EA CRACK ON THIS RIB) - [SDR AMWA40](https://openairdocs.org/sdr/AMWA40), Sep 7, 2003: RIB. CRACKED. RIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-46 ON RT SIDE STRG P/N 101-640000-41 STRG P/N 101-640000-37 LT SIDE (4EA CRACK ON THIS R - [SDR AMWA39](https://openairdocs.org/sdr/AMWA39), Sep 7, 2003: RIB. CRACKED. RIB 69.184 CS CRACKED AT STRG P/N 101-640000-45 (1EA CRACK ON THIS RIB) LT SIDE. - [SDR AMWA38](https://openairdocs.org/sdr/AMWA38), Sep 7, 2003: RIB. CRACKED. RIB AT CS 24.973 CRACKED AT STRG P/N 101-640000-39 LT SIDE (1EA CRACK ON THIS RIB). - [SDR 047254](https://openairdocs.org/sdr/047254), Jan 26, 2000: ELEVATOR. ROUGH. WHILE ON FLIGHT 2629 DEPARTING, THE CREW PERFORMED AN ELEVATOR CHECK. THEY FELT ROUGHNESS IN THE ELEVATOR SYSTEM. THE CREW RETURNED TO THE GATE. MAINTENANCE PER - [SDR MASA99012](https://openairdocs.org/sdr/MASA99012), Jan 20, 1999: TUBE. CRACKED. FLT 5409 - BOS-BGR - AFTER TAKEOFF, CAPTAIN NOTED THE NR 1 ENGINE OIL PSI WAS DECREASING. THE CAPTAIN SHUT DOWN THE NR 1 ENGINE AS A PRECAUTIONARY MEASURE. CREW - [SDR 97ZZZX3291](https://openairdocs.org/sdr/97ZZZX3291), Jul 11, 1997: ATTACH BRACKET. EXCESS WEAR. 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 13 ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20021019030019I](https://openairdocs.org/incident/20021019030019I), Oct 19, 2002: Beech 1900D (N127ZV), Little Rock, AR, Minor damage. (-23) On October 19, 2002 at 0858 central daylight time a Beechcraft 1900D reported sheet metal peeling off the right engine. The aircraft made an uneventful… --- 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.