N27304
Registered owner: UMB BANK NA 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.
10 reports on file, 2008-09-23 – 2026-06-24.
Part: PROCESSOR — FAULTY (WX RADAR) · airframe 10,787 hrs · 3,758 cycles
WX RADAR INOP PER FIM TASK 34-41 TASK 836, REMOVED AND REPLACED WEATHER RADAR PROCESSOR PER AMM 34-41-42. PERFORMED OPS CHECKED. CHECKS GOOD NO FAULTS NOTED. READY FOR CONTINUED SVC.
Part: ANTI-ICE SYSTEM — FAULTED · airframe 10,699 hrs · 3,724 cycles
BLEED CTRL ICING INHIB L INHIBIT FUNCTION FROM THE AIR SUPPLY CONTROLLER (ASC) TO ENGINE ANTI ICE (EAI) SYSTEM HAS FAILED.FROM AHM: ENGINE-1 INTERMEDIATE DUCT PRESSURE SENSOR SIGNAL IS OUT OF RANGE DETECTED BY: INTEGRATED AIR SYSTEMS CONTROLLER (IASC)-LEFT. 1AE. L ENGINE HP VLV IS SECURED CLOSED. MAINTENANCE MESSAGE : 36-21010. INITIAL EVAL MAINTENANCE MESSAGE OCCURED DURING THE CLIMB FLIGHT PHASE. REF FIM 36-21 TASK 801 STEP D (1) FAULT ISOLATION PROCEDURE (CLIMB) REPLACE PRESSURE REGULATION SHUTOFF VALVE. PART NIS GUM. ENG 1 PRSOV REPLACED REF L/P 9218750. ENG 1 HPSOV REACTIVATED REF AMM 36-00-00-440-803. FAULT MSG 36-11020 'ENG 1 HPSOV NOT IN COMMANDED POSITION' IS LATCHED. NO OTHER FAULTS PRESENT. REQUIRES PNEUMATIC ENGINE ON- SYSTEM TEST REF FIM 36-11 TASK 802. REPLACED E1 HPSOV REF AMM 36-11-07. INSTALL LEAK CHECK GOOD. LRU REPLACEMENT TEST AND PNUEMATIC ENGINE ON SYSTEM TEST FAILED. NO HELP. FAULT REMAINED.
Part: PUMP — FAULTED (NR 2 ENGINE) · airframe 8,949 hrs · 3,055 cycles
NUMBER 2 ENG DRIVEN HYD PUMP LOW PRESSURE, FOLLOWED BY LOSS OF SYSTEM B WHEN STARTED SERVICING B SYS RESERVOIR. FOUND HYD FLUID COMING OUT OF DRAIN MAST NR 2 ENG. REMOVED NR2 ENG HYD PUMP IAW AMM 29-11-11 UP TO ITEM G (10). CONTINUED INSTALLATION OF ENG 2 EDP IAW AMM 29-11-11-400-801 UP TO STEP 3H (10). R & R EDP CASE DRAIN FILTER ELEMENT IAW AMM 29-11-51-400-801, FOUND NO DEBRIS OR CONTAMINATION ON FILTER. R & R SYS B EDP CASE DRAIN FILTER IAW AMM 29-11-41-000-801, FILTER WAS CLEAN. IAW AMM 29-11-11-400-801.
Part: GIRT BAR — FOD (ZONE 800) · airframe 8,378 hrs · 2,866 cycles
2R GIRT BAR BLOCKED WILL NOT DISARM REMOVED DEBRIS FROM GIRT BAR CATCH. VERIFIED PROPER DOOR GIRT BAR OPERATION NO DEFECTS NOTED. OK TO CONTINUE. REF AMM 25-66-01-200-802. OK TO CONTINUE.
Part: TIRE — DAMAGED (ZONE 700) · airframe 8,172 hrs · 2,803 cycles
NUMBER 3 MAIN TIRE FLAT SPOT. REMOVED NR 3 MAIN TIRE R & R NR 3 MLG TIRE IAW AMM 32-45-11.
Part: BRAKE — CRACKED (ZONE 700) · airframe 8,172 hrs · 2,803 cycles
NUMBER 3 MLG BRAKE PADS CRACKED/DAMAGED. REMOVED AND REPLACED NR 3 BRAKE IAW AMM 32-41-41.
Part: MODULE — FAULTY (ZONE 100) · airframe 6,919 hrs · 2,394 cycles
MASTER CAUTION FIRE WARNING BELL CUTOUT MULTIPLE 6 PACK LIGHTS ILLUMINATED WITH ODOR DEBRIEFED CREW NO FIRE OR SMOKE NOTICED OR VISIBLE. PERFORMED CONDITIONAL INSP PER AMM 05-51-56. INSPECTED FWD GALLEY AREA INCLUDING COFFEE MAKERS AND OVENS NO ISSUES FOUND. RAN ACFT AIR COND PACKS AND NO FUMES OR SMOKE FOUND. PERFORMED FIRE OVERHEAT TESTS AND UNABLE TO DUPLICATE. SUSPECT INTERMITTANT FAULT ASSOCIATED WITH ENGINE AND APU FIRE DETECTION CONTROL MODULE. REMOVED AND REPLACED MODULE REF AMM 26-10-01. OPS CK GOOD. NO FURTHER FAULTS FOUND. OK TO CONTINUE.
Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 6,881 hrs · 2,379 cycles
DOOR 1L SLIDE PACK GRATE PROTECTION FLAP STUCK INSIDE HOUSING. REPOSITIONED PROTECTION FLAP AS REQUIRED ON BOTTOM OF SLIDE PACK. OK FOR SERVICE PER AMM 25-66-01. REPOSITIONED PROTECTION FLAP AS REQUIRED ON BOTTOM OF SLIDE PACK. OK FOR SERVICE PER AMM 25-66-01
Part: BATTERY — UNKNOWN (INTERNAL) · airframe 1,752 hrs · 583 cycles
FIRST CLASS SEATS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY M2816 PER AMM 33-51-06. OPS CHECKS GOOD OK TO CONTINUE. PARTS USED: 29-3351-3-0031,QTY :1
Part: COMPUTER — FAILED (STALL WARNING) · airframe 13,235 hrs · 12,225 cycles
STALL FAIL MESSAGE ON CLIMB OUT, COMPLIED WITH QRH. ACCOMPLISHED FIM 27-30-00 LRU DIAGNOSTICS REFLECTS SPC2 INTERNAL FAILURE. REMOVED, REPLACED, AND TESTED SPC COMPUTER IAW AMM 27-35-01, OPS CHECK GOOD. (K)