N262NN

Part: DOOR — STUCK (L1) · airframe 20,143 hrs · 13,326 cycles

INFO TO MAINTENANCE. 1L DOOR STUCK WHEN ARRIVING AT GATE. HARD TO OPEN OPS WAS ABLE TO OPEN THE DOOR. INFO TO MTX NOTED PIC#703129MOC#242727

Part: PRESSURE SWITCH — UNSERVICEABLE (BRAKE SYS) · airframe 17,291 hrs · 11,334 cycles

IN FLIGHT EICAS MSG PRKG BRK NOT RELEASED ILLUMINATED, EXECUTED QRH PROCEDURE. REMAINED ON. LANDING ROLLOUT EMER BRAKE FAULT ILLUMINTED. NO EMERGENCY DECLARED RAR EMERGENCY BRAKE PRESSURE SWITCH IAW AMM 32-44-09. OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,253 hrs · 9,946 cycles

SLAT/ FLAP LEVER WAS MOVED TO THE FLAP 1 POSITION ABOVE 240KTS AND IMMEDIATELY RETRACTED TO THE 0 POSITION APPROXIMATELY 2 SEC AND LATER TURN WAS A HIGH SPEED ANNUNIATION.-C/A-PERFORMED FLAP OVERSPEED PHASE I INSPECTION IAW ERJ AMM 05-50-07. NO DEFECTS NOTED AT THIS TIME. SEE ITEM 2

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,471 hrs · 9,406 cycles

L1 LIVE DOOR / SLIDE PARTIALLY DEPLOYED-C/A-L1 DOOR EMERGENCY SLIDE REMOVED AND DEPLOYED/OPS TEST C/W IAW E175 AMM 25-65-01 SEE ITEM 2 FOR CONTINUED DISCREPANCY

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,446 hrs · 9,388 cycles

CRG AFT FIRE SYS FAIL CRG FWD FIRE SYS FAIL-C/A-PERFORMED NORMAL APU SHUTOFF / RESTART IAW AMMM 49-00-00 NO DEFECTS NOTED AT THIS TIME

Part: CONTROL CABLE — MIGRATED (L2 SLIDE) · airframe 14,187 hrs · 9,183 cycles

L2 EMERGENCY SLIDE CABLE ASSEMBLY IS MIGRATING AT THE TOP NEAR THE SUPPORT BRACKET-C/A-REMOVED AND REINSTALLED L2 DOOR EMERGENCY SLIDE CABLE ASSEMBLY IAW EMB 175 AMM 52-12-40, MEASUREMENT CHECKS GOOD

Part: WINDSCREEN — BIRD INGESTION · airframe 11,698 hrs · 7,409 cycles

RETURN TO FIELD DUE TO MULTIPULE BIRD STRIKES FO WINDSHIELD EMERGENCY DECLARED LANDED SAFELY. -C/A-PEFORMED BIBRDSTRIKE INSPECTION IAW TASK CARD 05-50-02-200-801 NO DAMAGE NOTED AC OK FOR SERVICE

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 11,583 hrs · 7,336 cycles

AFT SERVICE DOOR EMERGENCY EXIT INDICATOR INOP-C/A-RAR EMERGENCY LIGHT POWER UNIT #4 IAW EMB AMM 33-50-01 OPERATIONAL TEST GOOD

Part: NONE — NONE · airframe 10,947 hrs · 6,939 cycles

ON TAKE OFF BLEED 1 AND 2 OVERPRESSURIZATION DECLARED EMERGENCY -C/A-T/S FAULT CODE 36111210AM1 FIM TASK 36-11-00-810-811-A BLOCK1,3,4,AND 9 FOUND TO BE TRANSITORY CONDITION OF TORQUE MOTOR CONTROLLER (LH) NO MESSAGE NOTED AIRCRAFT OK FOR SERVICE

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,463 hrs · 4,721 cycles

EXTERNAL FUSELAGE SKIN MULTIPLE LIGHTNING STRIKE DAMAGES BETWEEN FR 23-26 STGRS 26L-28L. C/A: ACCOMPLISHED PERMANENT REPAIR TO EXTERNAL FUSELAGE SKIN BETWEEN FR 23-26 STGR 26L-28L, IAW ENVOY ERS-EJ-53MR-4229.

Part: NONE — CRACKED (LH) · airframe 7,463 hrs · 4,721 cycles

L/H ENHANCED WING TIP SPAR 1 CRACKED AT LIGHTNING HOLE-C/A-COMPLETE:REPAIRED LH ENHANCED WING TIP SPAR 1 IAW ENVOY EO# EJ-5700-004.

Part: NONE — NONE · airframe 7,463 hrs · 4,721 cycles

R/H ENHANCED WING TIP SPAR 1 CRACKED AT LIGHTNING HOLE-C/A-COMPLETE:REPAIRED RH ENHANCED WING TIP SPAR 1 IAW ENVOY EO# EJ-5700-004.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,838 hrs · 1,239 cycles

PAX 8D STATED SMELLS HYDRAULIC FLUID IN CABIN DURING FLT AND TAXI. RAN HYD SYST, OPERATED DIF CONTROLS, AND FOUND NO EVIDENCE OF SMELL OF HYD IN CABIN AREA OR AROUND SEAT 8D.

Part: AILERON — UNKNOWN · airframe 282 hrs · 178 cycles

BINDING IN FLIGHT CONTROLS NOTICED AT FL335 TEMP WAS -47C @ FL335 NARRATIVE: AFTER PROLONGED STABLE CRUISE FLIGHT AT FL390 DESCENT WAS GIVEN TO FL330 AT FL335 WE ENCOUNTERED LIGHT TURBULANCE IN CONJUNCTION WITH A TURN AS YOKES WAS DISPLACED LEFT TO RAISE RIGHT WING FROM TURN A TACTILE THUD WAS FELT IN COCKPIT FLOORBOARD AND A VISIBLE RACHETING/JOLT WAS SEEN IN CONTROL COLUMN AS THE FLIGHT CONTROLS. PERFROMED A GVI OF THE AILERON PCU AND MOVED CONTROL COLUMNS FOR BINDING. NO DISCREPANCIES FOUND ALL WORK IAW AMM 27-10-00. REINSTALLED AILERON PCU PANEL 641BB IAW AMM 27-12-01.

Part: CONTROL UNIT — FAILED (AILERON FEEL) · airframe 130 hrs · 86 cycles

FLIGHT CONTROL BINDING AT CRUISE ALTITUDE & ON DESCENT. CONTROL COLUMN RESTRICTED FROM RETURNING TO THE NEUTRAL POSITION. PERFORMED OPERATIONAL TEST OF AILERON SYSTEM IAW AMM 27-11-00, AND REMOVED AND REPLACED THE AILERON FEEL UNIT IAW 27-11-05 OPS CHECKED GOOD.

Part: CONTROL COLUMN — BINDING · airframe 126 hrs · 84 cycles

DURING DESENT, CONTROL COLUMN ON BOTH SIDES STUCK IN A TURN . SNAPPED THOUGH BIND. REPEATED IN A LEFT TURN , CONTINUED UNTILL THE ACFT SLOWED TO 220. BOTH COLUMNS WOULD BIND IN BOTH LT AND RT TURNS . IT TOOK GOOD AMOUNT OF PRESSURE TO SNAP PAST THE BIND ON BOTH SIDES . THE BINDING WOULD HAPPEN WITH AUTOPILOT ON OR OFF. PERFORMED AN ADJUSTMENT OF THE RT UPPER AND LT FUSELAGE SECTOR AILERON TORQUE TUBE IAW ERS-EJ-2700-123 AND OPS CHECKED IAW AMM 27-10-00-710-801 OPS CHECKED GOOD. PERFORMED AN NSTALLATION AND CLEARENCE CHECK OF THE LEFT AILERON FUSELAGE SECTOR TORQUE TUBE IAW ERS-EJ-2700-123.