ENVOY AIR INC.

Operated by Envoy Air Inc. (per NTSB report)

Operated by Envoy Air Inc. (per NTSB report)

The flight crew’s misidentification of the intended landing runway, which resulted in an approach to and landing on the wrong runway due to their planned continuation bias. Contributing to the incident was the flight crew’s decision to continue the approach without the correct ILS frequency in the FMS. Also contributing was air traffic control’s failure to notify the flight crew that the were lined up with the incorrect runway contrary to FAA directives.

Operated by Envoy Air (per NTSB report)

An encounter with clear air turbulence.

Operated by Envoy Air (per NTSB report)

Operated by Envoy Air Inc. (per NTSB report)

The ramp agent’s cognitive impairment, which resulted in her (1) inconsistent behavior with trained procedures and prelanding briefings, (2) presence on the left side of the airplane while the left engine was still operating, and (3) subsequent ingestion into the engine.

Operated by Envoy Air (per NTSB report)

An abrupt jerk of the airplane as the captain applied the parking brake during the tow that caused a flight attendant to fall and break her wrist.

Operated by Envoy Air Inc (per NTSB report)

an encounter with convectively induced turbulence while overflying an area of known convective activity.

Operated by Envoy Air Inc. (per NTSB report)

The flight crew’s inability to maintain the airplane on the runway centerline after touchdown due to the reduced braking action resulting from the deteriorating weather conditions, which caused the airplane’s departure from the runway surface. Contributing to the accident were the delay in performing the runway assessment for undetermined reasons and failure to close the runway. Also contributing to the accident was the controller’s failure to advise the accident flight crew that braking action was no longer consistent with the previously published notice to air mission, which described braking action as good across all three runway zones.

Operated by ENVOY AIR INC (per NTSB report)

The local controller failing to follow established facility directives and issuing a clearance for takeoff from a runway not under his control.

Sanction: $11,000 · case closed 2016-06-03

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 29,766 hrs · 19,782 cycles

CATERING TRIED TO OPEN L2 DOOR AND THEY COULDN'T OPEN IT FROM OUTSIDE. OPERATED L2 DOOR IAW AMM 52-12-00 AND FOUND NO DEFECTS

Part: FLASHLIGHT ASSY — ODOR (ZONE 200) · airframe 30,267 hrs · 35,423 cycles

PAINT ODOR OF ELECTRICAL SMOKE IN COCKPIT AND NEAR ROW 8 ACCOMPLISHED TRIAD WORK SCOPE. R & R OF AFT CABIN FLASHLIGHT ASSY. NO BURNING ODOR OR ABNORMAL ODORS NOTED AT THIS TIME.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 25,637 hrs · 17,317 cycles

BIRD STRIKE ON TAKEOFF NR 1 ENG FROM KHPN. HIGH VIBRATION ON CLIMB AS WELL AS APPROACH BACK INTO KHPN. EMERGENCY DECLARED. PERFORMED BIRD STRIKE W/C INSPECTION PER ENVOY W/C EA05-50-200-801A. ON ENG NR 1 FOUND BLADE DEFORMATION TO BE OUT OF LIMIT SEE LOG PG 116602880/1 FOR CORRECTIVE ACTION

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 18,502 hrs · 12,594 cycles

EMERGENCY PHOTOLUMINESCENT STRIPS LIGHTS FWD CABIN BY CLOSET INOPERATIVE. R & R FWD MOST PHOTOLUMINESCENT STRIP LIGHT BY CLOSET IAW AMM 33-50-21.

Part: CONTROLLER — FAULTED (APU STARTER) · airframe 53,089 hrs · 34,798 cycles

APU FAILED TWICE IN FLIGHT. FIRST RESTART WAS SUCCESSFUL, RAN FOR ABOUT 15 MINUTES. FAILED AGAIN. WITH IDG 2 OUT, DIVERTED TO CVG. EMERGENCY DECLARED, T/S IAW FIM 49-10-00-810-810-A. R & R ELECTRONIC STARTER CONTROLLER IAW ERJ 170 AMM 49-42-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 52,559 hrs · 34,313 cycles

THE GATE AGENT REPORTS THAT THE MAIN BOARDING DOOR, SPECIFICALLY THE HANDLE, IS HARD TO OPEN/OPERATE. DOOR OPERATES AS INTENDED IAW AMM 52-11-00 COULD NOT DUPLICATE THE FAULT.

Part: LIGHT — INOPERATIVE (1DF AND 2DF) · airframe 24,573 hrs · 16,328 cycles

PHOTOLUMINESCENT STRIP IDICATOR BETWEEN SEAT 1DF AND 2DF DISCOLORED INOP. FOUND PHOTOLUMINESCENT STRIP IDICATOR BETWEEN SEAT 1DF AND 2DF DISCOLORED, RAR PHOTOLUMINESCENT STRIP IAW AMM 33-50-21, OPS CHECK GOOD.

Part: HINGE — LACK OF LUBE (ZONE 800) · airframe 26,531 hrs · 17,972 cycles

GATE AGENT REPORTS THAT DOOR MECHANISM IS DIFFICULT TO OPEN, ABNORMAL PRESSURE. L1 DOOR LUBRICATED DOOR HINGES. OPS CHKD GOOD IAW AMM 52-11-00

Part: FLASHLIGHT ASSY — INOPERATIVE (ZONE 200) · airframe 1,741 hrs · 1,200 cycles

AFT F/A EMERGENCY FLASHLIGHT RED LIGHT INOP FOUND AFT F/A EMERGENCY FLASHLIGHT RED LIGHT INOP, RAR FLASHLIGHT ASSY IAW 33-51-01 NO FURTHER DEFECTS NOTED.

Part: NONE — NONE (NONE) · airframe 16,727 hrs · 11,519 cycles

DIVERTED TWICE AND DECLARED EMERGENCY FOR LOW FUEL. MINIMUM FUEL IS NOT A MAINTENANCE ISSUE. MIN FUEL MEANS THAT HE WAS DECLARING BECAUSE THEY WERE OUT OF RESERVE FUEL FOR AN ALTERNATE DESTINATION. IF ATC REQUESTED THAT THEY HOLD OR DIVERT, THEY COULD RUN OUT OF FUEL.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,836 hrs · 18,526 cycles

AFT WET AREA FLOOR STRUCTURE CORROSION ON LT BEAM AT FR 87 Y -12". (MAJOR REPAIR) (LEVEL 2 CORROSION) MEASUREMENTS OF AFT WET AREA FL OOR STRUCTURE CORROSION ON LH BEAM AT FR 87 Y -12" MEASURES L=.2" W=.1" D=.025" FOUND TO BE OUT OF LIMITS PER EMB 175 SRM 53-23-10/AD02. LOCATED AND DRILLED NEW AFT WET AREA LH BEAM PN: 170-65669-003 PER EMB 175 SRM 51-40-02. INSTALLED L/H SHEAR PANEL IAW E-175 SRM 51-40-08 TOPCOATED FASTENERS IAW E-175 SRM 51-23-06 ENVOY ETN-EJ- 51-015. APPLIED CIC IAW E-175 CPM 51-25-00. INSTALLED STAINLESS STEEL STRIP IAW E-175 AMM 53-01-39-400- 804A. REMOVED AND REPLACED AFT WET AREA FLOOR STRUCTURE LH BEAM AT FR 87 Y -12" IAW E-175 SRM 51-40-08.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,836 hrs · 18,526 cycles

AFT WET AREA FLOOR STRUCTURE CORROSION ON RH BEAM AT FR 87 Y +12". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLEND MEASUREMENTS OF AFT WET AREA FLOOR STRUCTURE CORROSION ON RH BEAM AT FR 87 Y +12" MEASURE L=.3" W=.2" D=.022". PART IS OUT OF LIMITS PER EMB 175 SRM 53- 23-10/AD02. REMOVED AFT WET AREA FLOOR STRUCTURE RH BEAM IAW E-175 SRM 51-40-08. LOCATED AND DRILLED NEW FLOOR STRUCTURE IAW E- 175 SRM 51-40-02. (RH BEAM PN: 170-65669). NSTALLED RH SHEAR PANEL IAW E-175 SRM 51-40-08 TOPCOATED FASTENERS IAW E-175 SRM 51-23-06 ENVOY ETN-EJ- 51-015. TOPCOATED FASTENERS IAW E-175 SRM 51-23-06 ENVOY ET N-EJ-51-015 APPLIED CIC IAW E-175 CPM 51-25-00. INSTALLED STAINLESS STEEL STRIP IAW E-175 AMM 53-01-39-400- 804A. REMOVED AND REPLACED AFT WET AREA FLOOR STRUCTURE RH BEAM AT FR 87 Y+12 IAW E-175 SRM 51-40-08.

Part: GLOWSTRIP — WORN (ZONE 200) · airframe 24,537 hrs · 16,447 cycles

RIGHT DIAGONAL EMERGENCY PHOTOLUMINESCENT STRIP LIGHT BETWEEN SEATS 4 & 8 BEYOND WEAR LIMITS. REQUIRES REPLACEMENT. R & R RT DIAGONAL EMERGENCY PHOTOLUMINESCENT STRIP LIGHT BETWEEN SEATS 4 & 8 IAW AMM 33-50-21. CHKD GOOD.

Part: GLOWSTRIP — FADED (ZONE 200) · airframe 24,537 hrs · 16,447 cycles

FIRST FWD RT EMERGENCY PHOTOLUMINESCENT STRIP INDICATOR STRIP LIGHT. BY CAPTAINS CLOSET FILLED WITH MOISTURE FADED. REQUIRES REPLACEMENT. R & R FIRST FWD RT EMERGENCY PHOTOLUMINESCENT STRIP INDICATOR STRIP LIGHT (RED SQUARES) BY CAPTAINS CLOSET IAW AMM 33-50-21.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 24,537 hrs · 16,447 cycles

EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. R & R LT FWD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. NO OTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 26,134 hrs · 17,815 cycles

EMERGENCY LIGHT NOT WORKING ON THE MAIN CABIN CEILING. FLIGHT CREW PLACARD MEL 33-08 AUTH# 080540D-C

Part: WHEEL — DAMAGED (ZONE 700) · airframe 28,652 hrs · 19,835 cycles

EXCESSIVE SHIMMY IN NOSE GEAR AT HIGH SPEED ON TO/LNDG ROLL C/W LANDING GEAR SIGNIFICANT VIBRATION (SHIMMY) OF THE NLG IAW AMM 05-50-24-200-802-A SUBTASK 210-006-A. FOUND NLG LH TIRE WORN BEYOND LIMITS WITH FLAT SPOTS AND NLG RH TIRE WORN TO LIMITS. REFER TO NRWC 319-LIT-01884 AND NRWC 319-LIT-01885 FOR THE REPLACMENT OF NLG WHEEL AND TIRE ASSEMBLIES. NO FURTHER DEFECT NOTED.

Part: ENGINE — VIBRATION (NR 2) · airframe 24,898 hrs · 16,719 cycles

NR 2 ENG HIGH VIBRATION AT 4.0. NOTICED AFTER 80KTS. STAYED AT 4.0 IN AMBER. LEVELED AT 12000FT TO RUN QRH. AFTER RUNNING QRH STEPS ENG REMAINED 4.O - 4.2 AS WELL AS BEING ABLE TO FEEL A VIBRATION FROM THE ENG2 SIDE. ENG 2 DID RETURN TO GREEN WITH REDUCED THRUST SO WE KEPT IT REDUCED AND RETURNED TO DFW. DURING TAXI IN WE DID SEE A BRIEF RETURN TO 4.1 VIB IN ENG 2. TRANSFERRED TO NRWC 045-DFW-05383 ITEM-1. EMERGENCY DECLARED C/W E2 FAN BLADES AND PINS TROUBLESHOOTING IAW EA72-00-00-012 FOUND PINS NEEDED CHANGED REF NRWC 045-DFW-05384 FOR RAR OF PINS OPC CHECK GOOD HIGHEST VIB WAS 0.3AU @70% N1

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,668 hrs · 18,434 cycles

CENTER FUSELAGE III, SHEAR TIE CORRODED AT FR87, STR 28R. (MAJOR REPAIR) (LEVEL 2 CORROSION) EVALUATED CENTER FUSELAGE III SHEAR TIE CORRODED AT FR87, STR 28R HAS 100% MATERIAL LOSS IAW SRM 51-10-03 AND SRM 51-75-16. LOCATED AND DRILLED A NEW SHEAR TIE IAW SRM 51-40-02, APPLIED ALODIE, PRIMED, & PAINT IAW SRM 51-23- 04, SRM 51-23-05, & ETN-EJ-51-015, ETN-EJ- 51-025. R & R CENTER FUSELAGE III, SHEAR TIE AT FR87, STRS 27R-28R IAW SRM 51-40-08. LEVEL 2 CORROSION

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,668 hrs · 18,434 cycles

CENTER FUSELAGE III, SHEAR TIE CORRODED AT FR87 AND STGR 28R. (LEVEL 2 CORROSION). REMOVED AND REPLACED CENTER FUSELAGE III, SHEAR TIE AT FR87 AND STGR 27R-28R IAW EMB 175 SRM 51-40-08. SEE EAMS WO H10522 #1503 WIPS AND TASKS FOR ALL WORK ACCOMPLISHED.

Part: PICCOLO TUBE — FAULTED (ZONE 500) · airframe 29,748 hrs · 25,880 cycles

WING, NR 1 ENG ANTI ICE EICAS MESSAGE ILLUMINATED IN FLIGHT. EMERGENCY DECLARED, REMOVED AND REPLACED LT WING SLAT NR 2 PICCOLO TUBE IAW AMM 30-11-05 OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (NR 4 FLAP) · airframe 16,985 hrs · 11,339 cycles

SLAT/FLAP FAILURE ON CLIMB OUT GOING FROM 3 TO 2. EMERGENCY DECLARED. REPLACED LH OUTB FLAP 4L ACTUATOR IAW AMM 27-51-01. RIG & OPC OF FLAP SYSTEM GOOD IAW AMM 27-50-00 REF NRWC 090-MIA-03812 FOR ALL WORK PERFORMED

Part: ENGINE — POWER LOSS (NR 1) · airframe 19,558 hrs · 13,119 cycles

REJECTED T/O DUE TO ASYMMETRIC THRUST. TAKEOFF THRUST WAS SET AT TOGA TO START ROLL. NR 1 THRUST LEVER WAS SUBSEQUENTLY PUSHED THROUGH THE DETENT INADVERTENTLY. TO1 RSV WAS ACTIVATED. THRUST DIFFERENTIAL OF AROUND 7% N1 OBSERVED. DECISION MADE TO REJECT AS PM CALLED 80. NO ABNORMAL BRAKE INDICATIONS. MAX SPEED APPROX 83 KIAS. ENG TLA NOT TOGA EICAS MESSAGE ANNUNCIATED AND CLEARED. MAINTENANCE REQUEST ETN-EJ-72-001 APR EVENT DATA COLLECTION & ENGINE LIFING UPDATE BE COMPLETED. C/W ETN-EJ-72-001 NO ENGINE EXCEEDANCE RECORDED OK FOR SERVICE.

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 29,022 hrs · 25,467 cycles

L1 DOOR IS DIFFICULT TO OPEN. GATE AGENT STRUGGLED TO OPEN. LATCH POSSIBLY NOT COMPLETELY DISENGAGING ON THE RH SIDE OF DOOR C/W L1 DOOR EXTERNAL OPENING & CLOSING IN REF TO AMM SDS 52-11-00. NO FAULT NOTED DURING L1 DOOR OPERATION

Part: SKIN — DENTED (ZONE 200) · airframe 15,609 hrs · 10,731 cycles

FUSELAGE DENT AFT OF FWD PASSENGER DOOR BETWEEN FRAMES 20 AND 21, BETWEEN STGRS 11L AND 12L. (MJOR REPAIR) COMPLIED WITH HIDDEN DAMAGE INSPECTION OF AREA IAW EAMS QCM 1.16 REV 50. NO ADDITIONAL DEFECTS NOTED. CUT & REMOVED DAMAGE SPOT IN THE SKIN AT FR 20 - FR 21 STR 11L - 12L REF ETD2026-170-013290 REV . LOCATED DRILLED, DEBURRED & COUNTERSUNK REPAIR DOUBLER AND FILLER REF ETD2026-170-013290 REV.: A. TREATED REPAIR DOUBLER AND FILLER AND CUTOUT OF SKIN IAW SRM 51- 23-04 AND ETD2026-170-013290 REV.: A, PRIMED REPAIR DOUBLER AND FILLER AND CUT OUT OF SKIN IAW SRM 51-23-05, ETN-EJ-051-025 & ETD2029-170-013290 REV.A. FILLET SEALED AROUND REPAIR DOUBLER IAW ETD2026-170-13290 REV B. CLEANED, PREPPED, PRIMED AND RESTORED FINISH IAW SRM 51-23-06, ETN-EJ-51-015. INSTALLED FUSELAGE REPAIR DOUBLER AT FR 20 - FR21 AT STRG 11L - 12L REF ETD2026-170-013290 REV.: B.

Part: HANDLE — NO DISCREPANCY (ZONE 800) · airframe 54,535 hrs · 35,925 cycles

GATE AGENT SAID L1 DOOR HANDLE WAS VERY HARD TO OPEN, OPENED AND CLOSED L1 DOOR MULTIPLE TIME PER SDS 52-11-00.L1 DOOR OPERATED NORMALLY , NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (ROW 2) · airframe 23,824 hrs · 16,031 cycles

EMERGENCY LIGHT AT ROW 2 INOPERATIVE PER PS-2 FOUND CABIN EMERGENCY LIGHT INOP, RAR LIGHT IAW AMM 33-50-13, OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: SUPPORT FITTING — DAMAGED (ZONE 800 SLIDE) · airframe 28,552 hrs · 19,675 cycles

DAMAGE TO L1 DOOR FWD AND AFT SLIDE SUPPORT FITTINGS WHILE REMOVING EMERGENCY EVACUATION SLIDE PER WC 25-65-01-001. R & R EMERGENCY EVACUATION SLIDE ON L1 DOOR IAW ENVOY MTX WC EA25-65-01-001

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 28,200 hrs · 19,411 cycles

MAIN CABIN DOOR HARD TO OPEN/CLOSE. OPEN AND CLOSED MAIN CABIN DOOR SEVERAL TIMES IAW MTX GROUND HANDLING CHECKLIST. NO DEFECTS NOTED AT THIS TIME.

Part: A/C PACK — FAILED (NR 1) · airframe 23,756 hrs · 16,022 cycles

THROUGH FL 210 FIRECRACKER SMELL AND THIN VISIBLE SMOKE. SMOKE WENT AWAY AFTER 30 SECONDS BUT ODOR REMAINED. SAME CONDITIONS IN PAX CABIN AS REPORTED BY FLIGHT ATTENDANTS. GOT XBLEED SWITCH OFF MESSAGE DURING DESCENT. BRIEFLY GOT NAV 1 FAIL ON MCDU. PAX AND FA REPORTED A VIBRATION & AN UNIDENTIFIED SOUND FROM THE CLOSET AREA. DURING DESCENT ALSO GOT THE HISSING SOUND FROM THE CA DV WINDOW THAT WENT AWAY ABOUT 100 FT. ON THE GROUND AFTER APU START & ENG 2 SHUT DOWN , THE XBLEED SWITCH OFF MESSAGE RETURNED. CONFIGURATION WAS NORMAL FOR THE PHASE OF FLIGHT. CLIMB 1, APU OFF. IN ORDER TO COMPLY WITH TRIAD WORK, PERFORMED FIM TASK 21-20-00-810-801-A & FOUND PACK 1 FAILED ON EICAS, DURING COMPLIANCE. FOLLOWED ASSOCIATED FIM TASK 21-51-00-810-833-A. DURING COMPLETION OF THE FIM, CONDUCTED OPS TEST OF COOLING PACKS IAW AMM 21-00-00/200 AND FOUND VIOLENT BANG IN PACK 1 SYSTEM IN FWD SECTION OF ACM. AFTER DEACTIVATING PACK 1 FOR TROUBLESHOOTING PURPOSES, CONTINUED TO RUN ACFT ON PACK 2 FOUND SMOKE DISSIPATED & NO ABNORMAL NOISE HEARD. MEL 21-44 WAS ISSUED TO DEACTIVATE PACK 1. REF AML 107202210 FOR DEFERRAL OF PACK 1. REF AML PAGE 107202218 FOR ACTION TAKEN OF THE CA DV WINDOW HISSING NOISE.

Part: HANDLE — BINDING (ZONE 800) · airframe 27,638 hrs · 19,076 cycles

L1 OUTER DOOR HANDLE WAS REPORTED VERY HARD TO PULL UP. MADE DOOR DIFFICULT TO OPEN. PERFORMED GVI OF ADHESIVE TAPE ON L1 DOOR ARMING COVER IAW AMM 25-23-00. NO DEFECTS.

Part: DOOR — FAULTED (ZONE 800) · airframe 51,689 hrs · 33,035 cycles

L1 DOOR STUCK WON'T OPEN. DEPLANED THROUGH R1 DOOR. FIRE DEPARTMENT ASSIST IN DEPLANING. UPON INITIAL INSPECTION, FOUND L1 DOOR ARMING LEVER IN ARMED POSITION WITH GIRT BAR ENGAGED. DISARMED L1 DOOR IAW AMM SDS 52-11-00 AND VERIFIED GIRT BAR DISENGAGED. PERFORMED OPS CHK OF L1 DOOR EMERGENCY EVACUATION SLIDE HANDLE IAW AMM TASK 52-11-40-720-802-A . OPS CHK GOOD. NO DEFECTS NOTED. LEVER OPERATES WITH NO BINDING AND WITHOUT EXCESSIVE FORCE (16.3 LBS OF FORCE REQUIRED TO ARM, 19.3 LBS OF FORCE REQUIRED TO DISARM). T/S L1 DOOR IAW FIM TASK 52-11-00-810-808-A. NO FAULTS FOUND. OPENED AND CLOSED L1 DOOR EXTERNALLY AND INTERNALLY MULTIPLE TIMES IAW SDS 52-11-00. OPS CHK GOOD. NO DEFECTS NOTED. L1 DOOR OPERATES AS NORMAL OPENING AND CLOSING INTERNALLY/EXTERNALLY IAW AMM SDSD 52-11-00.

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: DOOR — LACK OF LUBE (ZONE 800) · airframe 54,374 hrs · 35,992 cycles

L1 DOOR HARD TO OPEN AND CLOSE LUBRICATED L1 DOOR AS REQUIRED. NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 40,913 hrs · 28,129 cycles

GATE AGENT SAID L1 DOOR WAS HARD TO OPEN L1 DOOR OPC OK IAW AMM 52-11-00

Part: MAU — FAILED · airframe 16,732 hrs · 11,372 cycles

AVNX MAU 1B FAIL IN FLIGHT. ASSOCIATED MESSAGES SPOILER FAULT AND SPDBRK FAIL. EMERGENCY DECLARED. PERFORM POWER DOWN POWER UP RESET PER QRH 7.2.1 AND 7.2.2. MESSAGE EXTINGUISH A/C OK FOR SERVICE. AND PERFORM QRH 7.3.22 AND AMM 27-00-00. OPS CHECK GOOD

Part: REINFORCEMENT — CRACKED (FR 8) · airframe 43,905 hrs · 35,830 cycles

SSI # 53-10-015 REINFORCEMENT BRACKET AT FR08 RH SIDE UNDER DV WINDOW IS CRACKED. (MAJOR REPAIR) REMOVED AND REPLACED REINFORCEMENT BRACKET AT FR08 RH SIDE UNDER DV WINDOW IAW ERJ 170 SRM 51-40-08.

Part: ROLLER — LACK OF LUBE (ZONE 800) · airframe 28,964 hrs · 25,409 cycles

L1 DOOR STRUGGLES TO OPEN FROM THE OUTSIDE. MULTIPLE ATTEMPTS REQUIRED TO OPEN. LUBRICATED ROLLERS AND CYCLED DOOR IAW AMM 52-11-00. DOOR OPENED NORMALLY

Part: HINGE — LACK OF LUBE (ZONE 800) · airframe 22,319 hrs · 14,890 cycles

GATE AGENT HAVING DIFFICULTY OPENING L1 DOOR LUBRICATED HINGE POINTS AND CYCLED DOOR IAW AMM 52-11-00. OPS CHECKED GOOD

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 46,310 hrs · 35,606 cycles

STRINGER SPLICE 09R IS CRACKED ON FWD END, AT FR 59. 0.25" IN LENGTH. (MAJOR REPAIR). R & R SPLICE, STRINGER 9/10R-JCT CTL II/III, AL OPS CHK GOOD.

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 46,310 hrs · 35,606 cycles

STRINGER SPLICE 09L IS CRACKED ON FWD END, AT FR 59. 0.25" IN LENGTH. (MAJOR REPAIR). R & R STRINGER 09-LHS-JCT, AL OPS CHKD GOOD.

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 46,310 hrs · 35,606 cycles

STRINGER SPLICE 10R IS CRACKED ON FWD END, AT FR 59. 0.25" IN LENGTH. (MAJOR REPAIR). R & R SPLICE, STRINGER 9/10R-JCT CTL II/III, AL OPS CHK GOOD.

Part: STRINGER — CRACKED (ZONE 200) · airframe 46,310 hrs · 35,606 cycles

STRINGER SPLICE 10L IS CRACKED ON FWD END, AT FR 59. 0.25" IN LENGTH. (MAJOR REPAIR). R & R STRINGER 09-LHS-JCT, AL OPS CHKD GOOD.

Part: WINDSHIELD — DAMAGED (ZONE 200) · airframe 55,129 hrs · 36,402 cycles

CAPTAIN`S WINDSHIELD BIRD STRIKE AT FL220 TRANSFERRED TO NRWC 792-ORD-02395 ITEM-1. R & R CAPTAIN COCKPIT WINDSHIELD IAW AMM 56-11-00. LEAK CHECKED GOOD.

Part: HOOK — FOD (ZONE 800) · airframe 2,134 hrs · 1,436 cycles

L1 DOOR DOES NOT OPEN ALL THE WAY UNLESS GUST LOCK IS PRESSED. INSPECTED L1 PASSENGER DOOR SUPPORT ARM HOOK MECHANISM IN REF TO AMM 52-11-30 AND CLEANED DIRT RESIDUE FROM HOOK AREA. OPERATINAL CHECK IS GOOD REF AMM 52-11-30.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 27,567 hrs · 19,021 cycles

AVNX MAU 3A FAIL RIGHT AFTER TAKEOFF. CAUSED MANY OTHER EICAS MESSAGES EMERGENCY DECLARED. C/W FIM TASK 31-42-00-810-812-A AND AMM 27-00-00/200 FLIGHT CONTROL RETURN TO SERVICE NO FAULTS FOUND OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 29,287 hrs · 19,526 cycles

ACRID, MUSTY ODOR PRESENT THROUGHOUT ACFT WHEN OPERATING PACKS, THE ODOR WAS MORE PREVALENT AT LOWER ALTITUDES. PER TRIAD WORK SCOPE STEP 6, PERFORM A GROUND RUN USING EACH ENGINE BLEED AIR AS A SOURCE FOR THE PACKS TO TRY DUPLICATE THE ISSUE, & ISOLATE WHICH ENG THE ODOR IS COMING FROM. REF NRWC 006-ORD-04211 ITEM'S NR 1, 2, AND 3, & NRWC 006 -ORD-04212, ITEM'S NR 1 & 2. VISUALLY CHECKED COCKPIT FLASHLIGHTS & DETERMINED THERE WERE NO SIGNS OF OVERHEAT AND / OR ODOR. COCKPIT FLASHLIGHTS OPS CHKD GOOD IAW AMM 33-51-00/600. UPON FLT CREW DEBRIEF, CREW DESCRIBED ODOR AS ELECTRICAL.TROUBLESHOT IAW FIM 21-20-00-810-801-A. CONDITION WAS FOUND TO BE TRANSITORY. NO FURTHER DEFECTS NOTED. PERFORMED 10 MIN GROUND RUN OF PACK SYSTEM UTILISING THE APU AS BLEED SOURCE. UNABLE TO DUPLICATE ODOR. PERFORMED ENG GROUND RUN IAW LMM 72-00-00-700-802, USING ENGINES AS BLEED SOURCE FOR PACK SYS. UNABLE TO DUPLICATE ODOR USING EITHER ENGS 1 OR 2. PERFORMED ENG HIGH POWER RUN IAW LLM 72-00-00-700-802. UNABLE TO DUPLICATE ODOR

Part: ENGINE — ODOR · airframe 44,521 hrs · 34,205 cycles

BURNING SMELL COMING FROM FLIGHT DECK WHOLE FLIGHT. FA STATED SMELLED IT IN THE CABIN. C/W EMB TRIAD WORK SCOPE FOR A/C N782SM FROM STEPS 1 TROUGH 8 . NO SMOKE OR BURNING SMELL FOUND OR NOTED .COMP WASH C/W WITH IN ABI LAST NIGHT REFERENCE NRWC 782-ABI-02917 AND 782-ABI-02918. SLIGHT SMELL OF COMP WASH SOAP BEFORE ENGINES RUN ,NO SMELL AFTER HIGH POWER RUNS.

Part: PIN — CORRODED (ZONE 700) · corrosion level 2 · airframe 27,836 hrs · 18,526 cycles

RIGHT MLG SHOCK STRUT FWD PINTLE PIN HAS CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED RH MLG FWD PINTLE PIN REF:EMB 175 AMM 32-11-01. PN OFF:1840- 0002 SN OFF:L2252 PN ON:1840-0002 SN ON:L 3201

Part: PIN — CORRODED (ZONE) · corrosion level 2 · airframe 27,836 hrs · 18,526 cycles

RIGHT MLG SHOCK STRUT AFT PINTLE PIN HAS CORROSION. (LEVEL 2 CORROSION) REMOVED AND REPLACED RH MLG AFT PINTLE PIN IAW AMM 32-11-01. PN OFF:1810- 0024 SN OFF:L1180 PN ON:1840-0024 SN ON:L 2194