Owner type
Corporation
Serial number
17000050
Year built
2004
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 2, 2004
Certificate issued
January 25, 2023
Expires
January 31, 2030
Mode S code
AA8075

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.

On this page

Airworthiness directives that may apply · 98

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1988In forceSuperseded2026
ADs by the year they took effect: 134 ADs
19881
19972
19993
20002
20014
20022
20033
20045
20057
20069
200715
20088
20094
201014
20115
20124
20135
20142
20161
20175
20182
20192
20205
20213
20227
20235
20242
20255
20262
See all 135 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 11

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR SIMA20260730003Door · no discrepancyL1 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.Jul 30, 2026 · N776MS · Emb ERJ170100SE · Passenger/Crew DoorsSDR SIMA20260704001Warning Message · false activationBRAKE 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 ASJul 4, 2026 · N776MS · Emb ERJ170100SE · Landing Gear Brake SystemSDR SIMA20240701002Bleed Air Sys · leakingENG 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. REMOVJul 1, 2024 · N776MS · Emb ERJ170100SE · Engine Bleed Air SystemSDR SIMA20240623001Anti-Ice Valve · leakingBLEED 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 36-11-00-810Jun 23, 2024 · N776MS · Emb ERJ170100SE · Airfoil Anti/De-ice SystemSDR SIMA20231001004Floor Support · corrodedFLOOR 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.Oct 1, 2023 · N776MS · Emb ERJ170100SE · Fuselage Miscellaneous StructureSDR SIMA2023101601003Shear Tie · corrodedSHEAR 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.Oct 1, 2023 · N776MS · Emb ERJ170100SE · Fuselage Internal Mounting StructureSDR SIMA20230928006Seat Track · corrodedSSI 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.Sep 28, 2023 · N776MS · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20230928005Floor Support · corrodedFWD 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 51-40-04Sep 28, 2023 · N776MS · Emb ERJ170100SE · Fuselage Miscellaneous StructureSDR SIMA2023101928004Floor Support · corrodedSSI 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.Sep 28, 2023 · N776MS · Emb ERJ170100SE · Fuselage Miscellaneous StructureSDR SIMA2023101628003Shear Panel · corrodedSSI 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.Sep 28, 2023 · N776MS · Emb ERJ170100SE · Fuselage Miscellaneous StructureSDR SIMA20230502001Proximity Sensor · failedTROUBLESHOOTING 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 CHEMay 2, 2023 · N776MS · Emb ERJ170200LR · Landing Gear Position and Warning

STCs that may be installed · 48

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 48 STCs