# N424NV: 1986 Mcdonnell Douglas DC-9-83 (MD-83), registration cancelled 2022-05-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 7, 2022
- Status when cancelled: Second renewal notice
- Airframe: [Mcdonnell Douglas DC-9-83 (MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022085)
- Engine: [Pratt & Whitney JT8D-219](https://openairdocs.org/engine/pratt-whitney-jt8d-219) (registry code 51694)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (OpenAirDocs)
- Serial number: 49421
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 5, 2011
- Certificate issued: June 6, 2019
- Last registry action: June 25, 2020
- Mode S code: A50BBB
- Owner when cancelled: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N424NV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=424NV
- Page: https://openairdocs.org/deregistered/N424NV-2022-05-07

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 Mcdonnell Douglas DC-9-83 (MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (44)

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

- [SDR JR2R10082017350](https://openairdocs.org/sdr/JR2R10082017350), Oct 8, 2017: BEAM. CORRODED. FOUND THE DOOR FRAME BEAM TO BE CORRODED. REMOVED AND REPLACED THE BEAM IAW SRM 51-30-5.
- [SDR JR2R2017100331](https://openairdocs.org/sdr/JR2R2017100331), Oct 7, 2017: RIB. CRACKED. VERTICAL STAB LOWER L/E FIFTH RIB UP FROM BOTTOM, CRACKED AT LOWER ATTACHED FASTENER, RT SIDE. REMOVED AND REPLACED DAMAGED THE RIB IAW 51-30-2, FIG 19-20, AND 
- [SDR JR2R20171007333](https://openairdocs.org/sdr/JR2R20171007333), Oct 7, 2017: RIB. CRACKED. VERTICAL STAB LOWER L/E, FOURTH RIB, UP FROM BOTTOM CRACKED AT LOWER ATTACHED FASTENER, RT SIDE. REPAIRED THE RIB IAW 55-02, FIG 27, SHEET 3 AND 4. INSTALLED IA
- [SDR JR2R20171007332](https://openairdocs.org/sdr/JR2R20171007332), Oct 7, 2017: RIB. CRACKED. VERTICAL STAB LOWER L/E, THIRD RIB UP FROM BOTTOM, CRACKED AT LOWER ATTACH FASTENER LT SIDE. REMOVED AND REPLACED DAMAGED RIB IAW SRM 51-30-2, FIG 19-20, AND 51
- [SDR JR2R20171007326](https://openairdocs.org/sdr/JR2R20171007326), Oct 7, 2017: SKIN. CORRODED. FUSELAGE SKIN CORRODED. REPAIRED THE SKIN IAW EA 42-2017-024.
- [SDR JR2R20171006092](https://openairdocs.org/sdr/JR2R20171006092), Oct 6, 2017: SKIN. CORRODED. FORWARD LAVATORY SERVICE DOOR EXTERNAL SKIN CORRODED BETWEEN SKIN AND INTERNAL DOUBLER. REPAIRED FWD LAV SERVICE DOOR FWD LOWER CORNER FUSELAGE CUTOUT IAW EA 25
- [SDR JR2R10171006124](https://openairdocs.org/sdr/JR2R10171006124), Oct 6, 2017: DOOR. CRACKED. LEFT WING OTBD BUTTE DOOR, OTBD SIDE CRACKED. REMOVED AND REPLACED BUTTE DOOR IAW SRM 51-30-5, PARA 7.
- [SDR JR2R20171005252](https://openairdocs.org/sdr/JR2R20171005252), Oct 5, 2017: ANGLE. DAMAGED. AFT CARGO ANGLE CRACKED OR HAS DEEP GOUGE BS 1154, STRINGER 21R. REMOVED AND REPLACED THE ANGLE IAW SRM 51-30-5.
- [SDR JR2R20171004194](https://openairdocs.org/sdr/JR2R20171004194), Oct 4, 2017: STIFFENER. CRACKED. AFT FUSELAGE FRAME CRACKED ON AFT SIDE OF FRAME INNER LIP AROUND FASTENER. REMOVED AND REPLACED EXISTING CRACKED REPAIR STIFFENER IAW MD80 SRM 51-30-5.
- [SDR JR2R20171004123](https://openairdocs.org/sdr/JR2R20171004123), Oct 4, 2017: ATTACH BRACKET. CRACKED. LT WING TRAILING EDGE OUT BOARD BUTE DOOR ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED LT WING TRAILING EDGE OUT BOARD BUTE DOOR ATTACH BRACKET IAW SRM 51-30
- [SDR JR2R201100817344](https://openairdocs.org/sdr/JR2R201100817344), Oct 3, 2017: SKIN. CRACKED. CRACK FOUND IN THE SKIN AND DOUBLER AT LOWER AFT CORNER OF AIRSTAIR DOOR.
- [SDR WX0A2016040473128](https://openairdocs.org/sdr/WX0A2016040473128), Apr 2, 2016: ACTUATOR. INOPERATIVE. IN CRUISE, TRANSFER LOCKOUT, LIGHT ILLUMINATED. QRH 21.10 COMPLIED & LIGHT REMAINED ILLUMINATED. TROUBLE SHOT & TESTED SYS IAW AMM 21-32-00. BIT CHECK OF NR 1 C
- [SDR WX0A2016040573129](https://openairdocs.org/sdr/WX0A2016040573129), Mar 31, 2016: SPAR CAP. CRACKED. LEFT WING FWD SPAR, LOWER CAP UPPER SURFACE, FWD FLANGE CORRODED AT STATION XFS 570. DURING REPAIR, A .200"" CRACK WAS NOTED, BETWEEN TWO FASTENER HOLES. DAMAGE
- [SDR JR2R20160331508](https://openairdocs.org/sdr/JR2R20160331508), Mar 31, 2016: SPAR CAP. CRACKED. LEFT WING FWD SPAR LOWER CAP, UPPER SURFACE FWD FLANGE CORRODED AT STATION XFS 570. DURING THE REPAIR, A .200" CRACK WAS NOTED, BETWEEN TWO FASTENER HOLES. DAMA
- [SDR JR2R20160331493](https://openairdocs.org/sdr/JR2R20160331493), Mar 31, 2016: FLOOR PANEL. CORRODED. FLOOR PANEL AT R1 DOOR GIRT BAR FLOOR LATCHES CORRODED OUT OF SRM 53-01 LIMITS. REPLACED FLOOR PANEL WITH SERVICEABLE PART IAW SRM 51-10-4.
- [SDR WX0A2015113000025](https://openairdocs.org/sdr/WX0A2015113000025), Dec 1, 2015: LAMP. INOPERATIVE. EMERGENCY EXIT LAMP INOPERATIVE AT ROW 26. REPLACED THE LAMP IAW AMM 33-53-00, OPS CHECKED GOOD.
- [SDR WX0A2015113000022](https://openairdocs.org/sdr/WX0A2015113000022), Nov 26, 2015: SMOKE DETECTOR. FALSE ACTIVATION. AFTER LANDING, SMOKE ALARM FOR AFT RT LAV WENT OFF, F/A REPORTS NO EVIDENCE OF SMOKE OR FIRE. PLACED AFT RT LAV SMOKE DETECTOR ON MEL 26-07 S1, AUTHORIZATION NR
- [SDR WX0A2015062672701](https://openairdocs.org/sdr/WX0A2015062672701), Jun 25, 2015: WARNING SYSTEM. FALSE ACTIVATION. TAIL COMPARTMENT HIGH LIGHT ON OAP AT ROTATION QRH 21.4. LIGHT EXTINGUISHED AFTER 60 SEC. REF WO 00260196-1 & 0020196-2. COMPLIED WITH TC 21-059-010 & TC 21-059
- [SDR WX0A2015062672696](https://openairdocs.org/sdr/WX0A2015062672696), Jun 25, 2015: BATTERY. DISCHARGED. FOUND ON WAKE UP, FWD CABIN EMER LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.
- [SDR WX0A2015061072642](https://openairdocs.org/sdr/WX0A2015061072642), Jun 5, 2015: A/C PACK. ODOR. FLIGHT ATTENDANT'S REPORTED A STRONG PLASTIC BURNING SMELL SHORTLY AFTER TAKEOFF. VERIFIED ODOR COMING FROM LT PACK DURING POWER RUNS. DEFERRED LT PACK IAW MEL 
- [SDR WX0A2015040872519](https://openairdocs.org/sdr/WX0A2015040872519), Apr 4, 2015: POWER SUPPLY. INOPERATIVE. FORWARD WING EMER EXIT LIGHTS INOPERATIVE. R & R EMER EXIT LT POWER SUPPLY IAW 33-53-01. FWD WING EMER EXIT LTS CHECKED GOOD.
- [SDR WX0A2015040872509](https://openairdocs.org/sdr/WX0A2015040872509), Apr 2, 2015: LIGHT. BROKEN. TAIL COMPARTMENT RT AFT EMER EXIT LIGHT INOPERATIVE & ASSEMBLY BROKEN. R & R RT AFT TAIL COMPARTMENT E & E LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL IAW AMM 33-
- [SDR WX0A2015030472445](https://openairdocs.org/sdr/WX0A2015030472445), Mar 3, 2015: LIGHT. INOPERATIVE. RIGHT EXTERIOR EMER EXIT LIGHT INOPERATIVE. REPLACED RT OVERWING EMER EXIT LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A2015022372434](https://openairdocs.org/sdr/WX0A2015022372434), Feb 21, 2015: FLAP. CRACKED. LEFT OTBD FLAP TE CRACKED. REPAIRED DAMAGED SECTION OF LT OTBD FLAP TE IAW SRM 57-03.
- [SDR WX0A2014102172214](https://openairdocs.org/sdr/WX0A2014102172214), Oct 10, 2014: PROXIMITY SENSOR. FAULTY. GEAR RETRACTION ON TAKEOFF RT GEAR INDICATION REMAINED RED WITH GEAR HANDLE UP. RAN QRH 32.9, HYD PRESS & QTY NORMAL. R & R RT MLG UPLOCK & DOWNLOCK PROXIMITY S
- [SDR WX0A2014090472133](https://openairdocs.org/sdr/WX0A2014090472133), Aug 31, 2014: APU. LEAKING. IMMEDIATELY AFTER TAKEOFF ALL FLIGHT ATTENDANT`S & FIRST OFFICER`S SMELLED A STRONG CHEMICAL ODOR, SMELL DISSIPATED OVER 10 MINUTES. QRH 26.5 REFERENCED. PACKS 
- [SDR WX0A071866](https://openairdocs.org/sdr/WX0A071866), Feb 25, 2014: BATTERY. DISCHARGED. FWD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERIES AT FWD GALLEY POSITION IAW 33-53-00, OPERATIONS CHECKED GOOD.
- [SDR WX0A201309260005](https://openairdocs.org/sdr/WX0A201309260005), Sep 20, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OPS CHEC
- [SDR WX0A201309260004](https://openairdocs.org/sdr/WX0A201309260004), Sep 17, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OP
- [SDR WX0A201308130054](https://openairdocs.org/sdr/WX0A201308130054), Aug 1, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTER
- [SDR WX0A201308010042](https://openairdocs.org/sdr/WX0A201308010042), Jul 25, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R
- [SDR WX0A2013070800024](https://openairdocs.org/sdr/WX0A2013070800024), Jun 28, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R BATTERIES IN THE POWER SUPP
- [SDR WX0A2013041571558](https://openairdocs.org/sdr/WX0A2013041571558), Apr 1, 2013: BATTERY PACK. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A201301140085](https://openairdocs.org/sdr/WX0A201301140085), Jan 14, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BAT
- [SDR WX0A071474](https://openairdocs.org/sdr/WX0A071474), Jan 9, 2013: BULKHEAD. CRACKED. RIGHT CANTED BULKHEAD 1463 AS 2 EACH CRACKS AT LONGERON 17R AND 18R. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLERS AND SHIMS.
- [SDR WX0A071472](https://openairdocs.org/sdr/WX0A071472), Jan 9, 2013: DRAG ANGLE. CRACKED. LEFT CANTED BULKHEAD 1463 DRAG ANGLE CRACKED IN EXISTING DOUBLER. REMOVED AND REPLACED DRAG ANGLE AT 181.
- [SDR WX0A071471](https://openairdocs.org/sdr/WX0A071471), Jan 9, 2013: DRAG ANGLE. CRACKED. RIGHT CANTED BULKHEAD 1463 DRAG ANGLE CRACKED. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE AND INSTALLED.
- [SDR WX0A071418](https://openairdocs.org/sdr/WX0A071418), Nov 14, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071373](https://openairdocs.org/sdr/WX0A071373), Oct 31, 2012: BATTERY PACK. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071285](https://openairdocs.org/sdr/WX0A071285), Aug 28, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071276](https://openairdocs.org/sdr/WX0A071276), Aug 19, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071211](https://openairdocs.org/sdr/WX0A071211), May 26, 2012: POWER SUPPLY. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071147](https://openairdocs.org/sdr/WX0A071147), Mar 28, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE
- [SDR WX0A071146](https://openairdocs.org/sdr/WX0A071146), Mar 21, 2012: BATTERY. DISCHARGED. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TE

## 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 20120603010789I](https://openairdocs.org/incident/20120603010789I), Jun 3, 2012: Mcdonnell Douglas DC-9-83 (MD-83) (N424NV), Grand Island, NE, Minor damage. On June 3, 2012, at approximately 1231 CDT, the RH MLG on allegiant air, LLC, Mcdonnell Douglas MD-83, N424NV, became stuck in the mud as the PIC attempted to…

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