N874NN
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
50 reports on file, 2013-06-22 – 2026-08-17.
Part: OIL COOLER — INOPERATIVE (ZONE 300) · airframe 44,360 hrs · 19,184 cycles
AIRCRAFT WAS GROUNDED: APU WAS RUNNING AND THE LIGHT EXTINGUISHED. AFTER 15 MINUTES APU SHUTDOWN AND THE R IGHT SOURCE OFF LIGHT CAME BACK ON. AFTER QRH PERFORMED DUE TO SOURCE OFF LIGHT, APU WAS RUNNING AND THE LIGHT EXTINGUISHED. AFTER 15 MINUTES APU SHUTDOWN AND THE RIGHT SOURCE OFF LIGHT CAME BACK ON. QRH PERFORMED AND DIVERTED TO THE NEAREST SUITABLE (NAS) FOLLOWING THE CHECKLIST. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED APU OIL COOLER IAW AMM 49-91-41.
Part: ANGLE — CRACKED (ZONE 100) · airframe 43,476 hrs · 18,805 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER UPPER ATTACH ANGLE LOCATED IN ECS BAY AT STA 663 AND LBL 45. REPAIRED ANGLE PER SRM 57-10-10-2R-5.
Part: DOUBLER — WORN (ZONE 100) · airframe 43,476 hrs · 18,805 cycles
AIRCRAFT IN BASE MAINTENANCE: WEAR TO ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER AT STA 224.8 BETWEEN S22R AND S23R. REPAIRED DOUBLER PER SRM 53-10-15-2R.
Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 43,476 hrs · 18,805 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER AT STA 663.75, BETWEEN RBL 31.83 AND RBL 40. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2.
Part: VAPOR BARRIER — DEGRADED (ZONE 100 - FUSE) · airframe 43,476 hrs · 18,805 cycles
AIRCRAFT IN BASE MAINTENANCE: EXISTING REPAIR ON LEFT HAND WHEEL WELL VAPOR BARRIER IS DEGRADED LOCATED 28 INCHES OYTBOARD OF KEEL BEAM AT BS 663 LBL 31.83 TO LBL 45.64. APPLIED PERMANENT REPAIR ON LEFT HAND VAPOR BARRIER. PER B737-NG AARD 57-10-10-9 AND B737-NG SRM 57-10-10-2R.
Part: DOOR FRAME — GOUGED (ZONE 200) · airframe 43,476 hrs · 18,805 cycles
AIRCRAFT IN BASE MAINTENANCE: FORWARD ENTRY DOOR AFT FRAME ROLLER GUIDE GOUGED. REMOVED AND REPLACED FORWARD ENTRY DOOR AFT FRAME ROLLER GUIDE. PER B737-NG SRM 51-40-02-OG.
Part: DOOR — BINDING (ZONE 800) · airframe 43,108 hrs · 18,645 cycles
AIRCRAFT WAS NOT GROUNDED: AFTER LEFT LAVATORY DOOR IS DIFFICULT TO OPEN. VERIFIED AFT LEFT LAVATORY DOOR BINDING. (OPEN).
Part: DOOR — BINDING (ZONE 800) · airframe 43,108 hrs · 18,645 cycles
AIRCRAFT WAS NOT GROUNDED: AFTER LEFT LAVATORY DOOR IS DIFFICULT TO OPEN. VERIFIED AFT LEFT LAVATORY DOOR BINDING. **SUPPLEMENTAL REPORT FOR (AALA202603130592) SUBMITTED 03/13/2026 BY DFW: READJUSTED BENT TRIM AS REQUIRED. OPS CHECK GOOD.
Part: SILL DRAIN — ODOR (ZONE 200) · airframe 43,061 hrs · 18,624 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS COMPLAINED OF A VOMIT SMELL AFTER DEPARTURE. CLEANED L1DOOR DRAIN. PER AMM 38-31-00.
Earlier reports · 2013–2025 · 41 reports
2025
Part: LIGHT — NO TEST (ZONE 200) · airframe 41,248 hrs · 17,745 cycles
AIRCRAFT IN BASE MAINTENANCE: DURING PS CHECK FOUND R1 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. VERIFIED R1 DOOR EMERGENCY EXIT SLIDE LIGHT IS WORKING, PER AMM 33-51-04. OPERATIONAL CHECK GOOD. NO FURTHER DEFECTS NOTED.
Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 41,172 hrs · 17,712 cycles
AIRCRAFT WAS NOT GROUNDED: GIRT BAR ON R1 DOOR SERVICE DOOR WAS HARD TO PUT ON POSITION AND REMOVE. REPOSITIONED GIRT BAR FOR DOOR 1R. PER AMM 25-66-01.
2024
Part: STOP FITTING — FAULTED (ZONE 200) · airframe 38,874 hrs · 16,626 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR JAMMED SHUT. MAINTENANCE (REF MIC#1668014), REPLACED DOOR STOP PLUNGER AND PERFORMED OPERATIONALTEST OF DOOR STOP PLUNGER IAW AMM 52-51-00
2023
Part: DOOR — STICKING (ZONE 900 - LAV/G) · airframe 35,532 hrs · 15,026 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR STICKING. MAINTENANCE LUBED AFT LEFT LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT AFT EXTERIOR L2 EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LEFT AFT L2 EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04.
Part: PANEL — CRACKED (ZONE 200 - FUSE) · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN MAIN CABIN FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL LOCATED AT BS 540 FROM LBL 1 TO LBL 21. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05.
Part: SHIELD — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR RIGHT HAND TRANSITION SHIELD LOCATED FROM BS 767 TO BS 787 AT S27R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1 R1.
Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727 PLUS 4 INCHES TO BS 887, AT S25L AND LBL 23. REPLACED TRANSITION PANEL PER AARD 51-00-05-1 R1.
Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 727 PLUS 4 INCHES TO BS 767, AT S27R AND RBL 23. REPLACED TRANSITION PANEL PER AARD 51-00-05-1 R1.
Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 35,233 hrs · 14,870 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 500I PLUS 10 INCHES TO BS 500H AT LBL 33. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5 AND DWG DBF2137 AND AARD 51-00-05-1.
Part: DOOR — UNSERVICEABLE (ZONE 900 - LAV/G) · airframe 34,472 hrs · 14,502 cycles
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN / CLOSE. REMOVED AND REPLACED LAVATORY DOOR ASSEMBLY PER CMM 25-40-64. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
2022
Part: LOCK — LACK OF LUBE (L4 DOOR) · airframe 33,155 hrs · 13,893 cycles
AIRCRAFT WAS NOT GROUNDED: L4 DOOR LOCK DIFFICULT TO OPERATE. LUBRICATED DOOR LOCK. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — NONE (ZONE 200 - FUSE) · airframe 33,131 hrs · 13,882 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT PUSH TO TEST INOPERATIVE. REPLACED FLASHLIGHT PER IPC 25-64-51-89A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-00.
Part: WINDSHIELD — DELAMINATED (ZONE 200 - FUSE) · airframe 32,567 hrs · 13,614 cycles
AIRCRAFT WAS GROUNDED: FLIGHT DECK L1 WINDSHIELD DELAMINATION. REMOVED AND REPLACED CAPTAIN'S WINDOW IN ACCORDANCE WITH JOB CARD 08L21056003 OPERATIONS CHECKS AND LEAKS CHECKS OK.
Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 32,059 hrs · 13,358 cycles
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT CABIN ENTRY DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED AFT RIGHT EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51-00.
Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 32,059 hrs · 13,358 cycles
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR STICKS. LUBRICATED LAVATORY DOOR AND RAILS PER AMM 20-30-21.
Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 31,954 hrs · 13,312 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY EXIT LIGHT LENS MISSING. REPLACED LENS PER AMM 33-51-0I.
Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 31,686 hrs · 13,194 cycles
AIRCRAFT WAS NOT GROUNDED: L1 FLIGHT ATTENDANT OUTBOARD FLASHLIGHT INOPERATIVE. REPLACED BATTERY PER AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: SHAFT — LOOSE (ZONE 800 - DOORS) · airframe 31,132 hrs · 12,959 cycles
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS THE DOOR HANDLE AT ENTRY DOOR 4L HAS EXCESSIVE MOVEMENT UP AND DOWN WHEN DOOR IS CLOSED AND LOCKED. TROUBLE SHOOTING L4 DOOR PER FIM 52-10-00-810-808. FOUND THE HANDLE CAM LOOSE ON THE HANDLE SHAFT. RE TORQUED THE HANDLE CAM PER AMM 52-13-11 AND 20-50-11. REMOVED AND REINSTALLED SLIDE PER JOB CARD 08L22125001.
2021
Part: CONTROL UNIT — FAULTED (AUTOBRAKE) · airframe 29,026 hrs · 11,980 cycles
AIRCRAFT WAS NOT GROUNDED: AUTOBRAKE DISARM LIGHT ILLUMINATED, FLIGHT REJECTED TAKEOFF. REPLACED ANTISKID/AUTOBRAKE CONTROL UNIT IAW AMM 32-42-21, OPS CHECKED GOOD.
2020
Part: ANGLE — LOOSE (R1 GIRT BAR) · airframe 27,975 hrs · 11,522 cycles
AIRCRAFT WAS NOT GROUNDED. 1R DOOR GIRT BAR CLIP IS VERY LOOSE. REPOISTIONED CLIP, PER AMM 25-66-01.
Part: HOLDER — LOOSE (GIRT BAR) · airframe 27,909 hrs · 11,495 cycles
AIRCRAFT WAS NOT GROUNDED. SLIDE GIRT BAR CLIP LOOSE ON FWD SERVICE DOOR. ADJUSTED GIRT BAR CLIP, IAW AMM 25-66-00. OPERATIONS CHECK GOOD.
Part: MODULE — MALFUNCTIONED (MLG HANDLE) · airframe 27,250 hrs · 11,201 cycles
AIRCRAT WAS GROUNDED, LANDING GEAR WOULD NOT RETRACT, CREW CONFIRMED MANUAL EXTENSION DOOR WAS CLOSED AND CYCLED GEAR HANDLE AND LANDING GEARS RETRACTED. AIRCRAFT RETURNED TO DEPARTURE, LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REMOVED, AND REPLACED THE LANDING GEAR CONTROL LEVER MODULE AND ACCOMPLISHED LANDING GEAR SWING.
Part: LANDING GEAR — MALFUNCTIONED · airframe 27,233 hrs · 11,190 cycles
AIRCRAFT WAS GROUNDED: AFTER TAKE OFF LANDING GEAR WOULD NOT RETRACT. FOLLOWED QRH PROCEDURE. AFTER EMERGENCY GEAR DOOR CYCLED AND VERIFIED CLOSED, GEAR CYCLED NORMALLY AND OPERATED NORMALLY FOR LANDING. ACCOMPLISHED OPERATIONAL CHECK OF LANDING GEAR IAW B737-NG AMM 32-32-00. OPERATIONAL CHECKED GOOD. NO FAULTS FOUND AT THIS TIME.
Part: PANEL — CRACKED (FUSELAGE) · airframe 26,967 hrs · 11,069 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540 AND RBL 2. REPLACED FLOOR SUPPORT BREAK ASSEMBLY PANEL IAW 51-00-05-1.
Part: PANEL — CRACKED (FUSELAGE) · airframe 26,967 hrs · 11,069 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540 AND LBL 2. REPLACED FLOOR SUPPORT BREAK ASSEMBLY PANEL IAW 51-00-05-1.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,890 hrs · 11,031 cycles
AIRCRAFT NOT GROUNDED - RIGHT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED, NO HELP. REMOVED AND REPLACED POWER SUPPY (M1671) PER AMM 33-51-06, OPERATIONAL CHECKS GOOD.
Part: WINDOW — DELAMINATED (COCKPIT) · airframe 26,347 hrs · 10,793 cycles
AIRCRAFT IN BASE MAINTENANCE: LOWER OUTER CORNER OF THE R1 WINDSHIELD HAS MILKY DELAMINATION. **SUPPLEMENTAL REPORT: REPLACED WINDSHIELD PER TASK CARD 08L2156004 ** (CLOSED).
2019
Part: BOTTLE — READS HIGH (DOOR SLIDE) · airframe 23,824 hrs · 9,676 cycles
AFT LT DOOR SLIDE PRESSURE WAS HIGH. REMOVED AND REPLACED DOOR SLIDE IAW AMM 25-94-12.
2017
Part: FLOORBEAM — CORRODED (BS 500I) · corrosion level 2 · airframe 18,131 hrs · 7,221 cycles
CORROSION FOUND ON THE FORWARD CARGO FLOORBEAM ANGLE AT BS 500I FROM THE LEFT TRANSITION PANEL TO THE RIGHT TRANSITION PANEL. REMOVED AND REPLACED FLOORBEAM ANGLE IAW 51-00-05-1 AND DRAWING 143A9485.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 18,131 hrs · 7,221 cycles
CABIN FLOOR SUPPORT CRACKED BETWEEN BS 312 AND 328, LBL46. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-00-05-1 AND DRAWING 141A5400.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 18,082 hrs · 7,198 cycles
FLOOR LEVEL EXIT SIGN MISSING BY THE R2 DOOR. REPLACED THE EMERGENCY EXIT SIGN LENS. OK FOR SERVICE IAW AMM 33-51-01.
Part: BRACKET — LACK OF LUBE (ZONE 800) · airframe 17,337 hrs · 6,878 cycles
AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR BRACKET IS TOO TIGHT. LUBRICATED GIRT BAR FLOOR MOUNTED BRACKET. OPERATIONAL CHECK GOOD.
Part: SIGN — BROKEN (CABIN) · airframe 17,095 hrs · 6,776 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN NEAR AFT ENTRY DOOR IS BROKEN. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
2016
Part: LENS — BROKEN (CABIN) · airframe 16,763 hrs · 6,643 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT AISLE LIGHT LENS COVER AT 24DEF IS BROKEN. REPLACED LENS COVER IAW AMM 33-51-02. OPERATIONAL CHECK GOOD.
Part: WINDOW — FAULTY (COCKPIT) · airframe 16,541 hrs · 6,546 cycles
AIRCRAFT WAS GROUNDED. ORD, AIR INTERRUPT, ORD-TUS. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CLIMB THE CAPTAINâS NR 2 WINDOW BEGAN TO PRODUCE A VERY LOUD. MAINTENANCE REMOVED AND REPLACED THE CAPTAINâS NR 2 WINDOW IAW MCM 56-94-01.
Part: LANDING GEAR — MALFUNCTIONED · airframe 15,732 hrs · 6,200 cycles
DURING CLIMB LANDING GEAR FAILED TO RETRACT. INDICATION SHOWED ALL GEAR DOWN WITH RED/DISAGREE LIGHTS ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED BITE CHECK PROCEDURE IAW TASK 32-09-00-810-801 WITH NO FAULTS FOUND. INSPECTED WIRING WITH NO DEFECTS FOUND. PERFORMED LANDING GEAR OPERATIONAL TEST 12 TIMES IAW TASK 32-32-00-70-801 WITH NO FAULTS FOUND.
2015
Part: SKIN — CRACKED (FUSELAGE) · airframe 12,768 hrs · 5,012 cycles
AIRCRAFT HAS AN AREA OF DAMAGE TO THE FUSELAGE SKIN AT THE APU ACCESS DOOR FWD HINGE, BETWEEN STATION 1093 & 1103. TEMPORARY REPAIR PREVIOUSLY ACCOMPLISHED ON FMR 3HF53E94F. PERMANENT DOUBLER REPAIR ACCOMPLISHED IAW SRM 53-80-01-2R.
Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 11,306 hrs · 4,447 cycles
AIR INTERRUPT, EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. FLAPS WOULD NOT EXTEND PAST 5, ALTERNATE EXTENSION NORMAL. REPLACED LT FLAP POSITION TRANSMITTER IAW MM 27-55-01. SYS CHECKED NORMAL.
2014
Part: LENS — UNSECURE (EXIT SIGN) · airframe 7,721 hrs · 3,060 cycles
EXIT SIGN LENS AT RT NR 2 DOOR NOT SECURE. REPLACED RT NR 2 DOOR EXIT SIGN ASSEMBLY, OPERATIONS CHECKED NORMAL.
2013
Part: SOCKET — DIRTY (EXTERIOR LIGHT) · airframe 5,828 hrs · 2,326 cycles
EXTERIOR EMERGENCY LIGHT BEHIND RIGHT NR 2 DOOR INOPERATIVE. CLEANED BOTH THE CONTACT SOCKET & THE BULB. OPERATIONS CHECKED NORMAL.