# N877GA: 1994 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2022-10-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 1, 2022
- Status when cancelled: Registration expired, pending cancellation
- 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 series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 53467
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 28, 2005
- Certificate issued: June 6, 2019
- Last registry action: December 22, 2020
- Mode S code: AC10EE
- 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/N877GA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=877GA
- Page: https://openairdocs.org/deregistered/N877GA-2022-10-01

From the FAA registry file of October 29, 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 (70, newest 50)

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

- [SDR JR2R20171014211](https://openairdocs.org/sdr/JR2R20171014211), Oct 14, 2017: FRAME ANGLE. CRACKED. RIGHT CANTED FRAME ANGLE CRACKED, AFT SIDE. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM 51-10-4.
- [SDR JR2R20171014210](https://openairdocs.org/sdr/JR2R20171014210), Oct 14, 2017: FRAME ANGLE. CRACKED. LEFT CANTED FRAME ANGLE CRACKED LT AFT SIDE. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM 51-10-4.
- [SDR JR2R20141012185](https://openairdocs.org/sdr/JR2R20141012185), Oct 12, 2017: WINDOW FRAME. CRACKED. RT WINDOW FRAME CRACKED UPPER FWD CORNER. REPAIRED THE WINDOW FRAME IAW SRM 53-05, FIG 122.
- [SDR JR2R20171011209](https://openairdocs.org/sdr/JR2R20171011209), Oct 11, 2017: GUARD. CRACKED. AFT ACCESSORY COMPARTMENT EMERGENCY EGRESS CATWALK FWD OUT BOARD HINGED WALK GUARDS CRACKED. REPAIRED AFT ACCESSORY EMERGENCY EGRESS CATWALK FWD OUT BOARD HINGE
- [SDR WX0A2016020473087](https://openairdocs.org/sdr/WX0A2016020473087), Feb 3, 2016: SERVO VALVE. FAILED. THE CREW WAS USING AUTO BRAKES FOR LANDING. THE AUTO BRAKES WERE DISENGAGED BETWEEN 120 - 100 KTS BY APPLYING MANUAL BRAKING. WHEN THE AUTO BRAKE SYS WAS DISENG
- [SDR WX0A072960](https://openairdocs.org/sdr/WX0A072960), Oct 21, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE ROW 8 INOPERATIVE. R & R EMER LIGHT BULB ABOVE ROW 8 IAW 33-53-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A072899](https://openairdocs.org/sdr/WX0A072899), Sep 25, 2015: WARNING SYSTEM. FALSE ACTIVATION. AFTER GEAR RETRACTION, RT MAIN GEAR UNSAFE LIGHT, REMAINED ON. FOLLOWED QRH 32.9, RED GEAR LIGHT ON WITH GEAR HANDLE UP. AFTER GEAR EXTENSION & RETRACTION, RED 
- [SDR WX0A2015092172879](https://openairdocs.org/sdr/WX0A2015092172879), Sep 21, 2015: SWITCH. DEFECTIVE. AUTO BRAKES DISENGAGE ON TOUCHDOWN. R & R AUTO BRAKE DISCONNECT SWITCH S1-441 IAW AMM 32-44-00-2-0. OPERATIONS CHECKED GOOD.
- [SDR WX0A2015092172876](https://openairdocs.org/sdr/WX0A2015092172876), Sep 20, 2015: SWITCH. DEFECTIVE. LANDING GEAR HORN WOULD NOT SILENCE ON VARIOUS CONFIGURATIONS, FLAP & SLATS 0, SLATS EXTENDED FLAPS 15. R & R LG SILENCE HORN SWITCH. OPERATIONS CHECKED GOOD IA
- [SDR WX0A2015091872866](https://openairdocs.org/sdr/WX0A2015091872866), Sep 15, 2015: BATTERY. DISCHARGED. TAIL COMPARTMENT CEILING EMER EXIT LIGHTS INOPERATIVE. R & R BATTERIES IN POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.
- [SDR WX0A2015082472830](https://openairdocs.org/sdr/WX0A2015082472830), Aug 23, 2015: UNKNOWN. MALFUNCTIONED. AT FL 290, THE FLOW LIGHT ON & THE CABIN BEGAN CLIMBING AT 1000 FEET A MINUTE. CREW ASKED FOR A DESCENT & EXECUTED QRH 21.7 CABIN PRESS OFF SCHEDULE OR ERRATIC 
- [SDR WX0A2015081772812](https://openairdocs.org/sdr/WX0A2015081772812), Aug 14, 2015: UNKNOWN. ODOR. ON TAKEOFF ROLL, THE FLIGHT ATTENDANTS REPORTED THE SMELL OF FUMES. BOTH PILOTS SMELT THE SAME FUMES. CABIN & FIRE QRH & AIR CON SMOKE & FUMES QRH COMPLETED. NO
- [SDR WX0A2015081672806](https://openairdocs.org/sdr/WX0A2015081672806), Aug 13, 2015: PROXIMITY SENSOR. FAILED. AFTER GEAR RETRACTION WE HAD RT RED GEAR LIGHT WITH GEAR HANDLE UP. AFTER QRH PROCEDURE, NOW HAD RT GEAR & NOSE GEAR RED LIGHT WITH GEAR HANDLE UP. ALSO HAD AN 
- [SDR WX0A2015081172787](https://openairdocs.org/sdr/WX0A2015081172787), Jul 3, 2015: SENSOR. OUT OF ADJUST. AT APPROX 2000 FEET ON APPROACH, SPOILER DEPLOYED, LIGHT ILLUMINATED. COMPLETED 360' TURN & LIGHT REMAINED ON. AFTER RESTARTING, APPROACH LIGHT ILLUMINATED INTE
- [SDR WX0A2015070672720](https://openairdocs.org/sdr/WX0A2015070672720), Jul 2, 2015: UNKNOWN. ODOR. IAW FLIGHT ATTENDANTS, ALL, THEY COULD SMELL A CHEMICAL, BURNT, FOUL SMELL ALL THROUGHOUT THE CABIN FROM TAKE OFF POWER TO ABOUT 15 MIN AFTER TAKEOFF. TAKE OFF 
- [SDR WX0A2014122272309](https://openairdocs.org/sdr/WX0A2014122272309), Oct 15, 2014: LIGHT. INOPERATIVE. LEFT FWD OVERWING EMER EXIT SIGN HAS ONE LAMP OUT. RELAMPED LIGHT FIXTURE IAW AMM 33-50-00. CHECKED GOOD AT THIS TIME.
- [SDR WX0A072199](https://openairdocs.org/sdr/WX0A072199), Oct 13, 2014: MANIFOLD. DEFECTIVE. ON LANDING AUTO BRAKES DISARMED AUTOMATICALLY UPON TOUCHDOWN WITH AUTO BRAKES SET AT MED. TROUBLE SHOT IAW AMM 32-44-00. FOUND LAND MANIFOLD BAD. REPLACED LAND 
- [SDR WX0A071974](https://openairdocs.org/sdr/WX0A071974), May 30, 2014: SKIN. SCRATCHED. UPPER ETERNAL FUSELAGE SKIN SCRATCHED OUT OF LIMITS AT STATION 349 UNDER VHF ANTENNA. BLENDED TO REMOVE DAMAGE, HFEC INSPECTED WITH NO CRACKS NOTED. FABRICATED 
- [SDR WX0A071852](https://openairdocs.org/sdr/WX0A071852), Feb 15, 2014: BATTERY. DISCHARGED. EMERGENCY AISLE LIGHTS INOPERATIVE 28 - 29. REPLACED BATTERIES IN BATTERY PACK FOR EMERGENCY AISLE LIGHTS 28 - 29. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.
- [SDR WX0A07177](https://openairdocs.org/sdr/WX0A07177), Dec 15, 2013: BATTERY. DISCHARGED. COCKPIT OVERHEAD LIGHTS DO NOT COME ON WITH EMERGENCY LIGHT TEST. R & R BATTERIES FOR EMERGENCY LIGHTS IN FWD SECTION IAW AMM 33-50-00, OPERATIONS TESTED GOOD.
- [SDR WX0A071778](https://openairdocs.org/sdr/WX0A071778), Dec 14, 2013: BATTERY. DISCHARGED. MID CABIN OVERWING EXIT DOOR AFT EMERGENCY LIGHT LOWER INOPERATIVE, BATTERIES ARE OUT OF DATE. R & R BATTERY IAW AMM 33-53-00, OPERATIONS CHECKED GOOD.
- [SDR WX0A071766](https://openairdocs.org/sdr/WX0A071766), Dec 2, 2013: BATTERY PACK. DISCHARGED. IN ACCORDANCE WITH MEL 25-09 SIT 1 DMI 5542, AFT CABIN FLASHLIGHT NOT BLINKING. R & R AFT CABIN FLASHLIGHT BATTERY PACK IAW AMM 25-60-00, OPERATIONS CHECKED GOO
- [SDR WX0A201310280038](https://openairdocs.org/sdr/WX0A201310280038), Oct 26, 2013: BATTERY PACK. INOPERATIVE. CENTER ISLE EMERGENCY LIGHTS AT 29 &31 INOPERATIVE. REPLACED BATTERY PACK BATTERIES FOR 29-31, OPS CK GOOD REF AMM 33-53-00.
- [SDR WX0A201308130066](https://openairdocs.org/sdr/WX0A201308130066), Aug 11, 2013: FLASHLIGHT. INOPERATIVE. FWD F/A STATION UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.
- [SDR WX0A2013070800028](https://openairdocs.org/sdr/WX0A2013070800028), Jun 28, 2013: BATTERY PACK. INOPERATIVE. DURING A ROUTINE OVERNIGHT SERVICE CHECK, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND 
- [SDR WX0A071599](https://openairdocs.org/sdr/WX0A071599), May 31, 2013: FRAME. CORRODED. AFT CARGO COMPARTMENT FS FRAME 1309 LOWER FLANGE IS CORRODED BETWEEN LONGERON 28R TO 28L. REPAIRED DAMAGED AREA OF FRAME.
- [SDR WX0A071598](https://openairdocs.org/sdr/WX0A071598), May 29, 2013: DOOR FRAME. CRACKED. VENTRAL DOOR SURROUND REVEAL CRACK IN UPPER LEFT CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER.
- [SDR WX0A071595](https://openairdocs.org/sdr/WX0A071595), May 23, 2013: DOOR FRAME. GOUGED. FORWARD CARGO DOOR HYDRO-FORMED FRAME HAS SEVERAL GOUGES AT AFT LOWER CORNER. FABRICATED REPAIR DOUBLER AND INSTALLED.
- [SDR WX0A071594](https://openairdocs.org/sdr/WX0A071594), May 23, 2013: DOUBLER. CHAFED. RIGHT L/B FLAP L/B VANE LEADING EDGE DOUBLER CHAFED. REPLACED DOUBLER.
- [SDR WX0A201305301593](https://openairdocs.org/sdr/WX0A201305301593), May 23, 2013: LONGERON SPLICE. CORRODED. FS 1461 LONGERON SPLICE 12L CORRODED. REPLACED LONGERON SPLICE.
- [SDR WX0A071592](https://openairdocs.org/sdr/WX0A071592), May 23, 2013: DOUBLER. CHAFED. RIGHT O/B FLAP L/B VANE LEADING EDGE DOUBLER CHAFED AT I/B CORNER. REPLACED DOUBLER.
- [SDR WX0A2013032171541](https://openairdocs.org/sdr/WX0A2013032171541), Mar 17, 2013: 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 WX0A071426](https://openairdocs.org/sdr/WX0A071426), Nov 28, 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 WX0A071384](https://openairdocs.org/sdr/WX0A071384), Nov 6, 2012: SKIN. CORRODED. AFT LAV SERVICE PANEL CUTOUT CORRODED BETWEEN FUSELAGE SKIN AND DOUBLER STATION 1309 JUST ABOVE LONGERON 22L.
- [SDR WX0A071411](https://openairdocs.org/sdr/WX0A071411), Nov 4, 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 WX0A071363](https://openairdocs.org/sdr/WX0A071363), Oct 21, 2012: CUSP WEB. CORRODED. CABIN FLOOR CUSP WEB CORRODED OUT OF LIMITS AT STA 370 RBL 47. REMOVED DAMAGED CUSP WEB, FABRICATED, LOCATED, DRILLED CUSP WEB DOUBLER AND INSTALLED IAW MD 80SR
- [SDR WX0A071352](https://openairdocs.org/sdr/WX0A071352), Oct 6, 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 WX0A071337](https://openairdocs.org/sdr/WX0A071337), Sep 25, 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 WX0A071336](https://openairdocs.org/sdr/WX0A071336), Sep 24, 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 WX0A071313](https://openairdocs.org/sdr/WX0A071313), Sep 12, 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 WX0A071254](https://openairdocs.org/sdr/WX0A071254), Jul 27, 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 WX0A071241](https://openairdocs.org/sdr/WX0A071241), Jul 6, 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 WX0A071162](https://openairdocs.org/sdr/WX0A071162), Apr 1, 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 WX0A070991](https://openairdocs.org/sdr/WX0A070991), Nov 6, 2011: VANE. GOUGED. RIGHT WING INBOARD FLAP VANE GOUGE AT XV2 223. PERMANENT REPAIR APPLIED 4" X 11" EXTERNAL DOUBLER FROM XV2 221 TO XV2 225 IAW BOEING MD80 SRM 57-03 PAGE 27 WITH
- [SDR WX0A070932](https://openairdocs.org/sdr/WX0A070932), Sep 5, 2011: 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 WX0A070931](https://openairdocs.org/sdr/WX0A070931), Sep 1, 2011: 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 WX0A070924](https://openairdocs.org/sdr/WX0A070924), Aug 2, 2011: LENS. MISSING. IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. FLOOR PATH LIGHTING STRIP IS MISSING THE LENS C
- [SDR WX0A070906](https://openairdocs.org/sdr/WX0A070906), Jul 25, 2011: UNKNOWN. ODOR. SMELL COMING FROM AIR CONDITIONING PACKS ON APU AIR, LEAK CHECKED APU AND VERIFIED ACM SERVICE LEVELS. INSPECTED COALESCER BAGS AND FOUND OK FOR CONTINUED SERVI
- [SDR WX0A070899](https://openairdocs.org/sdr/WX0A070899), Jun 30, 2011: 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 WX0A070876](https://openairdocs.org/sdr/WX0A070876), May 26, 2011: ENGINE. MALFUNCTIONED. DURING CLIMB, RIGHT ENGINE OIL TEMP BEGAN CLIMBING, FOLLOWED BY OIL QUANTITY FALLING. ENGINE WAS SHUTDOWN IN FLIGHT, OIL TEMP REACHED 199FT. REMOVED AND REPLACE

All 70: https://openairdocs.org/deregistered/N877GA-2022-10-01/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA07LA068](https://openairdocs.org/ntsb/MIA07LA068), Mar 29, 2007: McDonnell Douglas DC-9-83 (MD-83) (N877GA), Sanford, FL, substantial damage. Probable cause: The flight crew's failure to complete the checklist and adhere to airplane placards. Contributing to the accident was a separation of a B-nut on the rudder power hydraulic shut off valve for…

## FAA accident and incident reports (3)

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 20160203005489I](https://openairdocs.org/incident/20160203005489I), Feb 3, 2016: Mcdonnell Douglas DC-9-83(MD-83) (N877GA), Allentown, PA, No damage. After touchdown in (abe), the crew heard a noise and felt a small yaw. Stopped the aircraft and found that both main tires had blown on the left side. This…
- [Incident 20110526012319I](https://openairdocs.org/incident/20110526012319I), May 26, 2011: Mcdonnell Douglas DC-9-83(MD-83) (N877GA), Pittsburgh, PA, No damage. During climb out, allegiant air LLC flight 607, N877GA. (MD-83) experienced an low oil pressure indication. Engine was shut down and aircraft returned to land…
- [Accident 20070329005549A](https://openairdocs.org/incident/20070329005549A), Mar 29, 2007: Doug DC983 (N877GA), Orlando, FL, Substantial damage. (-23) Complete loss of right side hydraulic pressure and quantity. Flight crew had to use alternate extension control lever to extend landing gear. Both main…

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