N7949A
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.
23 reports on file, 2022-04-04 – 2026-08-20.
Part: BRAKE — FIRE (ZONE 700) · airframe 58,134 hrs · 28,396 cycles
AFTER BRAKE RELEASED, MECHANIC REPORTED A BRAKE FIRE. DEPLOYED EXTINGUISHER. ARFF RESPONDED WITH NO FURTHER ACTION. SAID MX TEMP BOTH SIDES WAS 230-240 DEGREES. REMOVED NR 1& 2 WHEEL AND BRAKE ASSYS. PERFORMED MINIMUM WORK SCOPE AFTER HOT BRAKE INSPECTION IAW AMM 05-51-07-000-901.
Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 58,044 hrs · 28,351 cycles
NR 1 ENGINE, RT FIRE CORE LOOP UPPER POSITION WITH BROKEN TERMINAL. REPLACED AND TESTED #1 ENGINE RH FIRE CORE LOOP UPPER POSITION TERMINAL LUGS IAW B737-800 AMM 26-11-02-960-801 PARAG 2.A THRU G(1) THRU I (9)(B) K AND L SATISFACTORY CONDITION.
Part: NUT PLATE — DAMAGED (SLIDE BRACKET) · airframe 58,044 hrs · 28,351 cycles
FORWARD GALLEY SERVICE DOOR, ESCAPE SLIDE BRACKET ASSY FWD AND AFT POSITION WITH NUTPLATES DAMAGED. REPLACED NUTPLATES ATTACHED WITH SOLID RIVETS IAW B737-800 AIPC 52-41-00-01B SHEET 003 AND 004 ITEM 260 AND 325(REV 121 DATED 06-15-2026 AND FASTENER INSTALLATION AND REMOVAL IAW B737-800 BCF SRM 51-40-02-0G-0 PARAG 4.E AND B (REV 26 DATED 03-10-2026)
Part: FRAME — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
FAS#4686 AFT CARGO RH SIDE STA 727H FRAME HAS OVERSIZED HOLE AT ZEE CHANNELS. C\W EA 26009 REV IR FUSELAGE / FRAME WEB IB CHORD / AT BSTA 727I / BTW LH AND RH S-25 & S-26 / OVERSIZED HOLES FAS#4686
Part: FRAME — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
AFT CARGO LH AND RH SIDES STA 767 FRAME HAS OVERSIZED HOLES AT ZEE CHANNEL - - REMOVED AND REINSTALLED AFT CARGO FLOOR PANELS IAW B737 AMM 25-52-10 FAS#4686
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
AFT CARGO RT SIDE FRAME STA 727F HAS OVERSIZED HOLE AT ZEE CHANNEL. COMPLIED WITH EA 26006 REV IR FUSELAGE/FRAME WEB IB CHORD, AT BS 727F, BTW S-25R&S-26R OVERSIZED HOLE.
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
AFT CARGO LH AND RH SIDES STA 787 FRAME HAS OVERSIZED HOLES AT ZEE CHANNEL - - C\W EA 26003 REV IR FUSELAGE FRAME WEB IB CHORD AT BSTA 727J BTWN LH AND RH S-25 & S-26 / OVERSIZED HOLES FAS#4686
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
AFT CARGO LH AND RH SIDES STA 727J FRAME HAS OVERSIZED HOLES AT ZEE CHANNEL -- C\W EA 26001 REV IR FUSELAGE / FRAME WEB IB CHORD / AT BSTA 747 / BTW S25L & S-26L AND BTW S-25R & S-26R / OVERSIZED HOLES FAS#4686
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 57,115 hrs · 27,901 cycles
AFT CARGO LH AND RH SIDES STA 727I HAS OVERSIZED HOLES AT ZEE CHANNEL - - C\W EA 26002 REV IR FUSELAGE / FRAME WEB IB CHORD / AT BSTA 787 / BTW S-25L & S-26L / OVERSIZED HOLES FAS#4686
Earlier reports · 2022–2025 · 14 reports
2025
Part: PITOT HEAD — DAMAGED (ZONE 100) · airframe 61,712 hrs · 40,315 cycles
DEFECT 75617: MULTIPLE BIRDS HIT IMMEDIATELY AFTER ROTATION. LOST CA AIR SPEED. CA ALTITUDE SLOWLY CREPT AS WE BEGAN APPROACH. ENGINES WENT TO EEC MODE - RESOLUTION: R AND R CA SIDE PITOT PROBE PER AMM 34-11-01, LEAK CHECK GOOD. PER AMM 34-11-00-790-810. A/C OK FOR SERVICE. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-18, NO OTHER DEFECTS FOUND.
Part: PITOT HEAD — DAMAGED (ZONE 100) · airframe 5,566 hrs · 27,148 cycles
MULTIPLE BIRDS HIT IMMEDIATELY AFTER ROTATION. LOST CA AIR SPEED. ALTITUDE SLOWLY CREPT AS WE BEGAN APPROACH. ENGINES WENT TO EEC MODE - RESOLUTION: R AND R CA SIDE PITOT PROBE PER AMM 34-11-01, LEAK CHECK GOOD. PER AMM 34-11-00-790-810. A/C OK FOR SERVICE. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-18, NO OTHER DEFECTS FOUND.
Part: ACCESS DOOR — OPEN (ZONE 100) · airframe 55,023 hrs · 26,872 cycles
DEFECT 785302: GROUND POWER ACCESS DOOR LEFT OPEN FOR FLIGHT . RESOLUTION: PERFORMED SUBTASK 52-49-02-710-001 AMM. OK FOR SERVICE.NO DEFECTS NOTED
Part: ENGINE — VIBRATION (NR 1) · airframe 55,015 hrs · 26,867 cycles
DEFECT 785300: ENG.#1 VIB EXCEEDDED 4.0 SEVERAL TIMES DURING DECENT BELOW 10.000' VARIED FROM 0.3-5.0, ALERT SHOWED 4 TIMES. NO ABNORMAL VIBRATIONS FELT BY CREW. RESOLUTION: PERFORMED VIBRATION SERVEY IAW AMM 71-00-00-700-814-F00 VIBRATION NEVER EXCEEDED 0.3 FROM IDLE TO T/O THRUST OK FOR SERVICE
2024
Part: AILERON SYS — LACK OF LUBE · airframe 54,709 hrs · 26,720 cycles
DEFECT 777651: AILERONS REQUIRE EXCESSIVE FORCE TO CONTROL AIRPLANE IN ROLL AXIS. RESOLUTION: PERF AILERON CONTROL WHEEL FORCE TEST IAW AMM 27-11-00. FORCE REQUIRED IS WITHIN LIMITS ABOUT 1LBS BELOW TRESHOLD. PER FIM 27-11 TASK 804. PULLEYS AND CABLES ON BOTH WINGS LOOK GOOD. LUBRICATED LEFT & RIGHT AILERONS PER AD 2006-21-01, TASK CARD 270260100. FORCE TEST WITHIN LIMITS & ABOUT 5 LBS BELOW LIMIT, OK FOR SERVICE.
Part: BEARING — LACK OF LUBE (AILERON) · airframe 54,535 hrs · 26,639 cycles
DEFECT 735267: FLIGHT CONTROLS ARE EXTREMELY STIFF ON ROLL AXIS. - - RESOLUTION: INSPECTED AILERONS AND AILERON FEEL AND CENTERING UNIT SPRINGS IAW AMM 27-11-81. NO DEFECTS NOTED. LUBED AILERON POWER OUTLET LEVERS AND BEARINGS IAW AMM 12-22-11. PERFORMED OPS CHECK OF AILERONS IAW AMM 27-11-00. NO BINDING OR STIFF AILERONS NOTED. A/C OK FOR SERVICE
Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 53,492 hrs · 26,144 cycles
L1 DOOR SLIDE CYLINDER PRESSURE INDICATOR NEEDLE IS IN THE NO-GO BAND. REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY IAW B737-800BCF AMM 25-66-01.
Part: SKIN — CRACKED (RT WING) · airframe 53,492 hrs · 26,144 cycles
RIGHT WING, SLAT #8 ACTUATOR TO SLAT ATTACH POINT SKIN WITH CRACK. REPAIRED RH WING SLAT#8 SKIN SECTION FROM SLAT STA 442.595 TO SLAT STA 460-345 LWL SECTION DUE TO CRACK IAW B737-800 SRM 57-42-01-2R-8 RERPAIR 8 ALTERNATIVE 1 PARA 4.F.FIG 202.
Part: GIRT BAR — LOOSE (MAIN DOOR) · airframe 53,452 hrs · 26,124 cycles
GIRT BAR CLIP ON MAIN ENTRY DOOR IS LOOSE. MX ADVISED. REMOVED AND REPLACED DAMAGED RIVET AS NEEDED REF SRM 51-40-02. CHECKS GOOD. SLIDE PACK COVER WAS NOT REMOVED FOR REPAIR.
Part: SLIDE — DETACHED (DOOR) · airframe 53,062 hrs · 25,956 cycles
SLIDE FELL OUT OF BASTLE WHEN DOOR WAS OPENED. REPOSITIONED SLIDE PACK PER AMM 25-66-01. A/C READY FOR SERVICE.
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,392 hrs · 24,800 cycles
DEFECT 744233 ITEM 2: L1 GIRT BAR OUT OF SLIDE COMPARTMENT. RESOLUTION: RESECURED GIRT BAR IAW AMM 25-66-01. A/C OK FOR SERVICE.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,384 hrs · 24,796 cycles
L1 GIRT BAR EXTENDED OUT OF SLIDE COMPARTMENT . INSPECTED L1 GRIT BAR EXTENDED IAW AMM 23-66-01 NO DEFECTS NOTED AT THIS TIME AC IS OK FOR SERVICE.
2022
Part: SKIN — DENTED · airframe 49,018 hrs · 24,194 cycles
DEFECT: WHILE INVESTIGATING EXTERNAL FUSELAGE SKIN, FOUND DENT @STA.500B+2 2.0" ABOVE STRINGER 21R. RESOLUTION: REPAIRED DAMAGE TO EXTERNAL FUSELAGE SKIN AT STA 500 B+2, 2.0" ABOVE STR 21R IAW B737-800 REF SRM 53-00-01-2R-3 REPAIR #2. CATEGORY B REPAIR INSPECTION REQUIREMENTS -
Part: BATTERY PACK — INOPERATIVE
DEFECT: RH GALLEY EMERGENCY LIGHT INOP RESOLUTION: R&R RH EMERGENCY BATTERY PACK POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.