N776MS
Registered owner: WILMINGTON TRUST COMPANY TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ENVOY AIR INC. (SIMA) | Operator | on 2023-08-14 | 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.
11 reports on file, 2023-05-02 – 2026-07-30.
Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 55,452 hrs · 36,734 cycles
L1 DOOR DIFFICULT TO OPEN AND STICKS ACCORDING TO GATE AGENT WHO REQUESTED IT BE LOOKED AT BY MX. OPENED & CLOSED L1 DOOR MULTIPLE TIMES IN REF WITH AMM SDS 52-11-00.FOUND DOOR TO BE WORKING NORMALLY. NO DEFECTS NOTED.
Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 55,268 hrs · 36,564 cycles
BRAKE RT & LT FAULT MESSAGE DISPLAYED ON EICAS WHEN MLG EXTENDED. WENT AROUND AND RAN QRH PROCEDURE. BOTH LEFT AND RIGHT BRAKE PEDALS WERE VERY DULL AND AIRCRAFT WAS STRUGGLING TO STOP WITH FULL PRESSURE APPLIED AND BRAKES DID NOT SEEM TO BE APPLYING EVENLY AS AIRCRAFT WAS PULLING LEFT AND RIGHT WHEN BRAKING. EXITED THE RUNWAY AND AIRCRAFT WAS TOWED TO THE GATE. EMERGENCY DECLARED. CMC FAULT CODE 32411020BCM. PERFORMED MAIN BRAKE PRESS TRANSDUCER FUNCTIONAL CHECK, MAIN BRAKE AND EMER/PARK BRAKE OPS CHECKS AND PERFORMED LOW AND HIGH-SPEED TAXI CHECKS WITH FLIGHT CREW PER EMB 170 AMM 32-41-00-720-802-A, 32-41-00-710-801-A, AND 32-44-00-710-801-A. FUNCTIONAL, OPS, AND TAXI CHECKS GOOD, NO DISCREPANCIES NOTED
Part: BLEED AIR SYS — LEAKING (NR 1 ENGINE) · airframe 50,617 hrs · 32,430 cycles
ENG 1 BLEED LEAK IN FLIGHT, FL280 FOLLOWED QRM PROCEDURES, AND UNABLE TO MAINTAIN CABIN PRESSURE DUE TO PACK 2 MEL. RETURN TO ORD EMERGENCY DECLARED/NO OVERWEIGHT LANDING/NO MASK DEPLOYMENT. T/S AML 5133549, FOUND E1 PRECOOLER LEAK AT TOP OF OUTLET DUCT. REMOVED AND REPLACED #1 ENGINE PRECOOLER IAW ERJ170 AMM 36-11-08 OPS TEST GOOD.
Part: ANTI-ICE VALVE — LEAKING (WING) · airframe 50,597 hrs · 32,412 cycles
BLEED 2 LEAK ON CLIMBOUT PASSING THROUGH 10,000 FT DECLARED EMERGENCY. OVERWEIGHT LANDING NO INJURIES REPORTED. WHILE TROUBLESHOOTING BLEED TWO LEAK, FOUND FILTER ON ANTI ICE VALVE TO BE LEAKING BLEED AIR. REFERENCE AML PAGE 5133527 ITEM 1 RAN FIM 36-11-00-810-837-A AND FIM 36-21-00-810-804-A AT TO/GA TEST PASSED NO LEAKS DETECTED. RAN OPERATION CHECK OF BLEED 2 SYSTEM IAW AMM 36-11-00 TEST PASSED. RAN BLEED 2 NAPRSOV AND HPSOV IBIT CHECK .TEST PASSED. NO LEAKS DETECTED.
Part: SHEAR TIE — CORRODED (FRM 78) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
SHEAR CLIP AT FR 78 BTWN STGRS 28L-29L CORRODED.(LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED SHEAR CLIP AT FR 78 BTWN STGRS 28L-29L IAW EMB 170 SRM 51-40-08.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
FLOOR BOARD SUPPORT AT FR 78 BTWN STGRS 29L-29R CORRODED (LEVEL 2 CORROSION).-C/A-REMOVED AND REPLACED FLOOR BOARD SUPPORT AT FR 78 BTWN STGR 29L-29R IAW EMB 170 SRM 51-40-08.
Part: FLOOR SUPPORT — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
FWD GALLEY RH FLOOR SUPPORT HAS EVIDENCE OF CORROSION BETWEEN FR 17 AND FR 18.(LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED FWD GALLEY RH FLOOR SUPPORT BETWEEN FR 17 AND FR 18 IAW EMB 170 SRM 51-40-04
Part: SHEAR PANEL — CORRODED (LH FWD GALLEY SH) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
SSI 53-10-027 FWD GALLEY LH SHEAR PANEL BETWEEN FR 19 AND FR 20 HAS EVIDENCE OF CORROSION. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED FWD GALLEY LH SHEAR PANEL BETWEEN FR 19 AND FR 20 IAW EMB 170 SRM 51-40-08.
Part: FLOOR SUPPORT — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
SSI 53-10-027 FWD GALLEY RH SHEAR PANEL BETWEEN FR 12 AND FR 14 CORRODED.(LEVEL2 CORROSION)-C/A-REMOVED AND REPLACED FWD GALLEY RH SHEAR PANEL BTW FR 12-14 IAW EMB 170 SRM 51-40-08.
Part: SEAT TRACK — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 49,025 hrs · 31,158 cycles
SSI 53-10-027 LH LOWER INBD SEAT TRACK BEAM HAS EVIDENCE OF CORRODED BETWEEN FR 19 AN FR 20 (LEVEL 2 CORROSION).-C/A-REMOVED AND REPLACED LH LOWER INBD SEAT TRACK BEAM BTW FR 19-20 IAW EMB 170 SRM 51-40-08.
Part: PROXIMITY SENSOR — FAILED (#1) · airframe 48,158 hrs · 30,452 cycles
TROUBLESHOOTING LOG PG 4980597 ITEM 1 "AFTER TAKE OFF, GEAR LEVER COULD NOT BE MOVED UP. NO EICAS MESSAGE NOTED." - FOUND NLG WOW SENSOR 1 HARNESS CORRODED AT WOW PROXIMITY SENSOR 1 CANON PLUG.-C/A-RAR NLG WOW SENSOR 1 HARNESS IAW EMB 170 AMM 32-00-01. OPS CHECK GOOD. REF LOG PG 4980597 ITEM 1.