# N886GA: 1990 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2024-06-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 29, 2024
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- 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: 49931
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 7, 2013
- Certificate issued: June 6, 2019
- Last registry action: August 11, 2023
- Mode S code: AC34B6
- 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/N886GA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=886GA
- Page: https://openairdocs.org/deregistered/N886GA-2024-06-29

From the FAA registry file of October 31, 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 (91, newest 50)

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

- [SDR WX0A2018071773354](https://openairdocs.org/sdr/WX0A2018071773354), Jul 15, 2018: AHRS. MALFUNCTIONED. EMERGENCY DECLARED, MULTIPLE NAV SYSTEM FAILURES. R&R NR 2 AHRU.
- [SDR JR2R20170428268](https://openairdocs.org/sdr/JR2R20170428268), Apr 28, 2017: SKIN. DENTED. DENT IN FUSELAGE SKIN AT BS 1380, LONGERON 2L HAS A GOUGE IN THE CENTER THAT IS FLOURESCING, FOUND DURING FPI. INSTALLED REPAIR IAW SRM 53-04-2, FIG 4, PARA 3.C
- [SDR JR2R20170427223](https://openairdocs.org/sdr/JR2R20170427223), Apr 27, 2017: LONGERON SPLICE. CORRODED. IN TAILCONE AREA, LEFT SIDE AFT OF ACM THERE IS INTERGRANNULAR EXFOLIATION CORROSION BELOW LEFT ACM WALKWAY AT STA 1430 LONGERON 22 APPROX. REMOVED AND REPLACED
- [SDR WX0A2015110572986](https://openairdocs.org/sdr/WX0A2015110572986), Oct 31, 2015: SENSE LINE. LOOSE. TAIL COMPARTMENT, TEMP HIGH ANNUNCIATOR ILLUMINATED ON CLIMB THROUGH FL260. QRH 21.4 WAS RUN, ANNUNCIATOR EXTINGUISHED 1 MIN 45 SEC AFTER LT ENG THROTTLE WAS BR
- [SDR WX0A2015102972966](https://openairdocs.org/sdr/WX0A2015102972966), Oct 13, 2015: DOUBLER. CORRODED. FORWARD LAVATORY SERVICE LANDING STATION 237 - 256, LONGERON 20L - 21L. REPAIRED FWD LAVATORY SERVICE DOOR CUT OUT DOUBLER IAW EA 40-2015-177 DATED 10 15 2015 M
- [SDR WX0A2015081672797](https://openairdocs.org/sdr/WX0A2015081672797), Aug 8, 2015: SPOILER. DEFECTIVE. WITH SPEED BRAKES EXTENDED AT 320 KTS ACFT HAS A MODERATE ROLL RATE TO THE RT. LESS NOTICEABLE AT 250 KTS, BUT ACFT STILL ROLLS RT. OPERATIONS CHECKED SPOILER A
- [SDR WX0A2015072700063](https://openairdocs.org/sdr/WX0A2015072700063), Jul 24, 2015: CLAMP. DAMAGED. TAIL COMPARTMENT TEMP HIGH DURING CRUISE, AFTER TURNING ON AIRFOIL ANTI-ICE. FOUND NR 1 PACK CLAMP DAMAGED AT HEAT EXCHANGER. ITEM PLACED ON MEL 21-01 SIT 1 CAT
- [SDR WX0A2015072372752](https://openairdocs.org/sdr/WX0A2015072372752), Jul 20, 2015: ACM. SEIZED. SMOKE & HAZE ACCUMULATED IN THE CABIN FROM ROW 10 TO THE REAR OF THE ACFT. CRUISE ALTITUDE WAS 33000. FLIGHT TIME WAS 45 MIN INTO THE FLIGHT. IN CONJUNCTION WIT
- [SDR WX0A2015081172790](https://openairdocs.org/sdr/WX0A2015081172790), Jun 26, 2015: DUCT. BLOWN. JUST AFTER DEPARTURE THE CREW RECEIVED TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. THE CREW FINISHED THE MEMORY ITEMS & STARTED EXECUTING QRH 21.4 TAIL COMPARTMENT 
- [SDR WX0A2015062672698](https://openairdocs.org/sdr/WX0A2015062672698), Jun 24, 2015: WARNING SYSTEM. FALSE ACTIVATION. TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR ON CLIMB OUT. COMPLIED WITH QRH. LIGHT OUT APPROX 2 MIN AFTER APU SHUTDOWN, DID NOT RETURN. REF WO 00260062-1 & WO 002600
- [SDR WX0A2015061972669](https://openairdocs.org/sdr/WX0A2015061972669), Jun 15, 2015: ENGINE. OVERTEMP. ON TAKEOFF NR 1 ENG OVER TEMP, 632 EGT FOR 25 SECONDS EPR 1.91 OAT 42C N1 92 N2 95 MAX POWER PACK ON. REF WO 00259024. R & R LT ENG. ACFT OK FOR SERVICE.
- [SDR WX0A2015081272792](https://openairdocs.org/sdr/WX0A2015081272792), Jun 12, 2015: ENGINE. OVERTEMP. ON TAKEOFF LT ENG EGT 636 FOR APPROX 9 SEC N1 94% N2 97 & EPR 1.98 OAT 34C OIL TEMP WENT TO 136 DEGREE. DURING THE TAKEOFF ROLL THE CREW NOTED THE EGT ON THE LT
- [SDR WX0A2015061072649](https://openairdocs.org/sdr/WX0A2015061072649), Jun 6, 2015: GROUND STUD. LOOSE. FORWARD ENTRY DOOR EMER LIGHT INOPERATIVE WITH SWITCH ON. COMES ON WITH FWD ENTRY DOOR LIGHT. FOUND GND STUD LOOSE ON LIGHT ASSEMBLY. SECURED GND STUD IAW SWPM 
- [SDR WX0A2015052072605](https://openairdocs.org/sdr/WX0A2015052072605), May 19, 2015: LIGHT. INOPERATIVE. FORWARD ENTRY EMER LIGHTS INOPERATIVE. RELAMPED THREE EACH 43 LIGHT BULBS. BULBS ILLUMINATE ONLY WITH FWD ENTRY LIGHTS ON, REF LOG PAGE 553552 IAW AMM 33-53-01.
- [SDR WX0A2015050172567](https://openairdocs.org/sdr/WX0A2015050172567), Apr 30, 2015: SLIDE. UNSECURE. R1 SLIDE FELL OFF WHEN DOOR WAS OPENED. R & R R1 SLIDE IAW TASK CARD 25-058-017.
- [SDR WX0A2015030972456](https://openairdocs.org/sdr/WX0A2015030972456), Mar 4, 2015: LIGHT. INOPERATIVE. EMERGENCY EXIT FLOOR IDENTIFIER LIGHT AT ROW 24DEF REQUIRES RELAMP. RELAMPED IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A2015030972455](https://openairdocs.org/sdr/WX0A2015030972455), Mar 4, 2015: LIGHT. INOPERATIVE. EMERGENCY EXIT FLOOR IDENTIFIER LIGHT AT ROW 25 DEF INOPERATIVE. RELAMPED IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A2015022372430](https://openairdocs.org/sdr/WX0A2015022372430), Feb 19, 2015: LIGHT. INOPERATIVE. FOUND ON WAKE UP, TAIL CONE EMER CTR LIGHT INOPERATIVE. RELAMPED TAIL CONE EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.
- [SDR WX0A2015021672417](https://openairdocs.org/sdr/WX0A2015021672417), Feb 8, 2015: NOSE COWL. CORRODED. NUMBER 2 ENG NOSE COWL CORROSION BLEND OUT AT 6 O'CLOCK POSITION ON INNER LIP ATTACH POINT OUT OF LIMITS. R & R NR 2 ENG NOSE COWL IAW AMM 71-10-01.
- [SDR WX0A2015013072381](https://openairdocs.org/sdr/WX0A2015013072381), Jan 24, 2015: LIGHT. INOPERATIVE. EMERGENCY EXIT REMOVABLE LIGHT AT L1 DOOR INOPERATIVE. REPLACED BULB IAW AMM 33-53-00.
- [SDR WX0A2015012672379](https://openairdocs.org/sdr/WX0A2015012672379), Jan 24, 2015: LIGHT. INOPERATIVE. EMERGENCY EXIT REMOVABLE LIGHT AT L1 DOOR INOPERATIVE. REPLACED BULB IAW AMM 33-53-00.
- [SDR WX0A2014090972147](https://openairdocs.org/sdr/WX0A2014090972147), Sep 6, 2014: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY PACK IN TAIL SECTION INOPERATIVE. R & R EMER LIGHT BATTERY PACK IN TAIL SECTION IAW AMM 35-53-01. OPERATIONS CHECKED GOOD.
- [SDR WX0A2014091072151](https://openairdocs.org/sdr/WX0A2014091072151), Sep 4, 2014: TRIM MOTOR. FAILED. AFTER TAKEOFF PRIMARY TRIM FAILURE. COMPLIED WITH QRH REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR IAW AMM 27-40-01. REF LOG PG 537838 FOR OPERATIONS CHECK
- [SDR WX0A072105](https://openairdocs.org/sdr/WX0A072105), Aug 22, 2014: POWER SUPPLY. INOPERATIVE. EXTERIOR EMER LIGHT WILL NOT ILLUMINATE. R & R BATTERY POWER SUPPLY FOR EXTERIOR EMER LIGHTS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A071935](https://openairdocs.org/sdr/WX0A071935), Apr 29, 2014: BATTERY. DISCHARGED. EMERGENCY EXIT SIGN IS INOPERATIVE AT RT FWD OVERWING EXIT. REPLACED BATTERIES IN RT FWD OVERWING EXIT SIGN IAW AMM 33-53-00, OPERATIONS CHECKED GOOD.
- [SDR WX0A071921](https://openairdocs.org/sdr/WX0A071921), Apr 19, 2014: SPAR. CRACKED. VERTICAL STABILIZER LE BOLT HOLE CRACKED ON RT SIDE JUST ABOVE SPLICE AT STATION 52.267. FRONT SPAR CAP FLANGE OVERSIZED FASTENER HOLE TO .325" FOR DAMAGE REMOV
- [SDR WX0A071920](https://openairdocs.org/sdr/WX0A071920), Apr 18, 2014: SKIN PANEL. CORRODED. RIGHT WING LOWER SKIN PANEL UPPER SURFACE CORRODED OUT OF LIMITS AT STATION XCW 114. REMOVED CORROSION DAMAGE & EXISTING MLG DOUBLER. FABRICATED TAPERED FILLER 
- [SDR WX0A071912](https://openairdocs.org/sdr/WX0A071912), Apr 15, 2014: PAN. GOUGED. FORWARD RT SERVICE DOOR JAMB PAN GOUGED, PERMANENT REPAIR. REPAIRED IAW STS EA 20-2014-060.
- [SDR WX0A071913](https://openairdocs.org/sdr/WX0A071913), Apr 13, 2014: SKIN. DENTED. RIGHT ELEVATOR CONTROL TAB DENTED OUT OF LIMITS ON UPPER SURFACE, STATION XHS 86. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER & HOT BONDED IAW SRM 51-70-2 PARA 1
- [SDR WX0A071909](https://openairdocs.org/sdr/WX0A071909), Apr 11, 2014: CHANNEL. CRACKED. KEEL BEAM INTERCOSTAL AT STATION 937 CRACKED IN 2 EA LOCATIONS. REPAIRED BEAM INTERCOSTAL CHANNELS AT STATION 937 IAW SRM 53-05 FIG 81.
- [SDR WX0A071910](https://openairdocs.org/sdr/WX0A071910), Apr 8, 2014: BEAM. CRACKED. L1 DOOR INTERNAL BEAM IN NR 8 HOLE CRACKED. STOP DRILLED CRACK, FABRICATED & INSTALLED DOUBLER IAW SRM 52-05.
- [SDR WX0A071878](https://openairdocs.org/sdr/WX0A071878), Mar 16, 2014: BATTERY. DISCHARGED. AFT FLIGHT ATTENDANT`S FLASHLIGHT BLINKING LIGHT IS DEAD. R & R BATTERY IAW MM 25-60-00.
- [SDR WX0A071795](https://openairdocs.org/sdr/WX0A071795), Dec 18, 2013: BATTERY. DISCHARGED. R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R ONE EACH BATTERY IN R1 DOOR EMERGENCY LIGHT IAW AMM 33-53-00, CHECKED GOOD.
- [SDR WX0A201310280039](https://openairdocs.org/sdr/WX0A201310280039), Oct 13, 2013: ENGINE. POWER LOSS. AT APPROXIMATELY 1000 FT AGL, RT ENGINE LOST POWER, AND INDICATED APPROXIMATE IDLE CONDITIONS, NO OVERWIEGHT LANDING MADE 124,000 LBS.
- [SDR WX0A201308130062](https://openairdocs.org/sdr/WX0A201308130062), Aug 5, 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 WX0A2013041171556](https://openairdocs.org/sdr/WX0A2013041171556), Apr 9, 2013: ENGINE. OVERTEMP. CLIMBING THROUGH 12000FT EXPERIENCED A LOUD BANG AND SHUTTER. RIGHT ENGINE EGT EXCEEDED 700 AND ROLLED BACK THROTTLE IS BOUND FROM 2" TO IDLE FUEL LEVER IS LOCK
- [SDR WX0A071479](https://openairdocs.org/sdr/WX0A071479), Jan 4, 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 WX0A2012122871467](https://openairdocs.org/sdr/WX0A2012122871467), Dec 28, 2012: SMOKE DETECTOR. FAULTY. FLIGHT CREW REPORTED, CARGO DETECTION SYSTEM AUDIBLE ALARM AND MASTER CAUTION/MASTER WARNING ANNUNCIATORS WHILE IN CLIMB COMPLETED. QRH FOLLOWED. NO SIGNS OF FI
- [SDR WX0A071403](https://openairdocs.org/sdr/WX0A071403), Nov 27, 2012: CUSP WEB. CORRODED. REPAIR DOUBLER IS CORRODED ON CUSP WEB BETWEEN FS 1060 TO 1079 ON LEFT SIDE. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED.
- [SDR WX0A071422](https://openairdocs.org/sdr/WX0A071422), Nov 26, 2012: CUSP WEB. CORRODED. PASSENGER CABIN RT CUSP WEB CORRODED AT FS 1030. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND RING DOUBLER AND INSTALLED.
- [SDR WX0A071401](https://openairdocs.org/sdr/WX0A071401), Nov 26, 2012: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED AT STATION 636. REPAIRED CORRODED WEB.
- [SDR WX0A071400](https://openairdocs.org/sdr/WX0A071400), Nov 26, 2012: CUSP WEB. CORRODED. PASSENGER CABIN RIGHT CUSP WEB CORREDED AT FS 389. REMOVED CORRODED CUSP, FABRICATED REPAIR DOUBLER AND INSTALLED.
- [SDR WX0A071399](https://openairdocs.org/sdr/WX0A071399), Nov 26, 2012: FRAME. GOUGED. CABIN LEFT FRAME GOUGED AT STATION 1212 NEAR LONGEON 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLER, STRAP AND INSTALLED.
- [SDR WX0A071396](https://openairdocs.org/sdr/WX0A071396), Nov 26, 2012: CUSP WEB. CORRODED. PASSENGER CABIN RIGHT CUSP WEB CORRODED AT FS 1030. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND RIGHT DOUBLER INSTALLED.
- [SDR WX0A071395](https://openairdocs.org/sdr/WX0A071395), Nov 26, 2012: SHEAR TIE. CORRODED. AFT CARGO PIT SHEAR TIE CORRODED AT STATION 1174 BETWEEN LONGERON 30 AND 29L. REMOVED DAMAGED AREA, FABRICATED SHEAR TIE AND REPAIR.
- [SDR WX0A071394](https://openairdocs.org/sdr/WX0A071394), Nov 26, 2012: CUSP WEB. CORRODED. RIGHT CUSP WEB CORRODED AT STATION 370. REPAIRED RIGHT CUSP WEB.
- [SDR WX0A071393](https://openairdocs.org/sdr/WX0A071393), Nov 26, 2012: FRAME. GOUGED. CABIN LEFT FRAME GOUGED AT STATION 1231 NEAR LONGERON 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLER, STAMP AND INSTALLED.
- [SDR WX0A071421](https://openairdocs.org/sdr/WX0A071421), Nov 25, 2012: CUSP WEB. CORRODED. CABIN LEFT CUSP WEB 3 AREAS OF CORROSION STATION 712 TO 786. CUT OUT DAMAGED AREAS, FABRICATED REPAIR FILLERS, RING DOUBLERS, REPAIR DOUBLERS AND INSTALLED.
- [SDR WX0A071397](https://openairdocs.org/sdr/WX0A071397), Nov 21, 2012: SKIN. CHAFED. FWD CARGO DOOR EXTERNAL SKIN CHAFED OUT OF LIMITS AT FWD LOWER CORNER. CUT OUT DAMAGED AREA, FABRICATED, DOUBLER, FILLER, LOCATED AND INSTALLED.
- [SDR WX0A071392](https://openairdocs.org/sdr/WX0A071392), Nov 21, 2012: CUSP WEB. CRACKED. CABIN LEFT CUSP WEB CRACKED AT STATION 810 LBL 55. CRACK MEASURES .400. CUT OUT CORROSION AND FABRICATED REPAIR DOUBLER DRILLED AND INSTALLED.

All 91: https://openairdocs.org/deregistered/N886GA-2024-06-29/reports.md

## 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 20121228028819I](https://openairdocs.org/incident/20121228028819I), Dec 28, 2012: Mcdonnell Douglas DC-9-82(MD-82) (N886GA), Fort Wayne, IN, No damage. At approx 1515EST local, gl-roc informed this office that at 1805Z, allegiant flt 959 enroute from ksbn to kpgd with 154 persons on board, had declared an…

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