N105JS
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Aeromexico | Operator | on 2024-09-16 | Operator named in NTSB report |
Accident & incident history
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.
9 reports on file, 2021-08-20 – 2025-07-29.
Part: PRESSURE SYSTEM — FAILED (NR 2 ENGINE) · airframe 13,837 hrs · 5,752 cycles
ENGINE CONTROL LIGHT IS ON , ENG 2 . 737 IFIM TASK G73-20-00-810-858 PERFORMED , LIGHT RESET. PSS ENG 2 VISUAL INSPECCION WAS PERFORMED IAW AMM F73-21-00-200-801-G00. DATA ENTRY DATA PLUG CONFIGURATION CHECK WAS PERFORMED IAW AMM G73-21-09-700-801-G00. PSS WAS REPLACED IAW AMM 73-21-11. PS3 (PSS) SENSE LINE DRY OUT WAS PERFORMED IAW AMM 73-21-11-160-801-G00.
Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 200) · airframe 13,832 hrs · 5,750 cycles
RETURN TO BLOCK DUE TO ENGINE CONTROL LIGHT ON FOR ENG 2. IAW IFIM 73-21-00-810-826 PERFORMED TEST TO REC. MESSAGE UNCATCHED AND ERASED , MAINT LIGHT EXTINGUISHED.
Part: DOOR — GROUND DAMAGE (ZONE 800) · airframe 13,515 hrs · 5,620 cycles
DUE IMPACT OF SERVICE CART, CAUSE DAMAGE ON AFT CARGO DOOR
Part: PROXIMITY SWITCH — MISALIGNED (ZONE 800) · airframe 8,177 hrs · 3,516 cycles
AFT CARGO LIGHT COMES ON DURING T/O AROUND 65 KTS CAUSING A REJECTED TAKE OFF FRM 52761700
Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE) · airframe 6,862 hrs · 2,929 cycles
DURING ENGINE STAR ENGINE CONTROL LIGHT ENGINE 2 ILUMINATED FRM 73230152
Part: WARNING LIGHT — ILLUMINATED (ENGINE) · airframe 6,571 hrs · 2,809 cycles
ENGINE CONTROL LIGHT IS ON, ENGINE 2 - 732 302 52. MAINT LIGHT IS ON - 316 811 00.
Part: ENGINE — UNSERVICEABLE (ZONE 400) · airframe 6,554 hrs · 2,805 cycles
DURING FINAL APPROACH 3500FT AGL-77330252 VIBRATION INDICATION IS HIGH, ENGINE 2 (MOMENTARILY, APPROXIMATELY 7 SECONDS)
Part: SKIN — DENTED (BS 355 S17-18L) · airframe 422 hrs · 286 cycles
DURING TRANSIT CHECK, IT WAS DETECTED A DENT WITH NICK ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT WITH NICK ON FUSELAGE SKIN LOCATED AT BSTA 355.9 AND BETWEEN STRINGER S-17L AND S-18L WITH 1.53" LENGTH, 1.00" WIDE AND 0.010" DIAMETER; DAMAGE ON FUSELAGE SKIN AT BSTA 355.9 AND BETWEEN S-17L AND S-18L WAS REMOVED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, PARAGRAPH 4.B.(2)(B), FIGURE 103, DETAIL C; ULTRASONIC THICKNESS MEASUREMENT AND HIGH FREQUENCY EDDY CURRENT INSPECTION ON REWORKED AREA WERE PERFORMED IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1, FIGURE 103, DETAIL C AND B737 NDTM PART 4, 51-00-00 PROCEDURE 2 AND PART 6, 51-00-00 PROCEDURE 23; A CHEMICAL CONVERTION COATING WAS APPLIED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1 PARAGRAPH 2.E.(1); A DECORATIVE FINISH WAS APPLIED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, PARAGRAPH 2.E.(4) AND AMM 51-21-99-300-802, ALL CORRECT.
Part: SKIN — DAMAGED (BS 355 S17-18L) · airframe 421 hrs · 286 cycles
DURING TRANSIT CHECK, IT WAS DETECTED A DENT WITH NICK ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT WITH NICK ON FUSELAGE SKIN LOCATED AT BSTA 355.9 AND BETWEEN STRINGER S-17L AND S-18L WITH 1.53" LENGTH, 1.00" WIDE AND 0.010" DIAMETER; DAMAGE ON FUSELAGE SKIN AT BSTA 355.9 AND BETWEEN S-17L AND S-18L WAS REMOVED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, PARAGRAPH 4.B.(2)(B), FIGURE 103, DETAIL C; ULTRASONIC THICKNESS MEASUREMENT AND HIGH FREQUENCY EDDY CURRENT INSPECTION ON REWORKED AREA WERE PERFORMED IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1, FIGURE 103, DETAIL C AND B737 NDTM PART 4, 51-00-00 PROCEDURE 2 AND PART 6, 51-00-00 PROCEDURE 23; A CHEMICAL CONVERTION COATING WAS APPLIED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1 PARAGRAPH 2.E.(1); A DECORATIVE FINISH WAS APPLIED IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, PARAGRAPH 2.E.(4) AND AMM 51-21-99-300-802, ALL CORRECT.