N637QX

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 17,550 hrs · 12,395 cycles

FLIGHT 2223. MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED FROM SERVICE. PERFORMED FUNCTIONAL CHECK OF L1 DOOR PER AMM 52-11-20-720-801-A. CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FUEL SYS — FAULTED · airframe 16,221 hrs · 11,301 cycles

FLIGHT 2104. REJECTED TAKEOFF FOR FUEL FEED 2 FAULT. WHENEVER N2 WENT ABOVE 65% FAULT WOULD RETURN. RAN CHECKLIST & FAULT DID NOT RETURN. REJECTED TAKEOFF WAS INITIATED AS POWER WAS BEING SET. MAX SPEED WAS APPROX 10KTS. RETURNED TO GATE AND REMOVED FROM SERVICE. INTERROGATED CMC AND FOUND NO FAULT CODES. C/W E175 FIM 28-21-00-810-815-A THROUGH STEP 5.D.(1).(A). AND FOUND TO BE A TRANSITORY CONDITION OF THE FUEL FEED SYSTEM. FUEL FEED 2 FAULT REMAINS EXTINGUISHED. NO FURTHER DEFECTS NOTED. NO BRAKE HOT CAUTION. BRAKE TEMPS REMAINED WITHIN LIMITS. PERFORMED GVI OF BRAKES AND FOUND NO DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: OVEN — DIRTY (ZONE 900) · airframe 15,826 hrs · 10,987 cycles

FLIGHT 2116. BURNING SMELL COMING FROM G2 OVEN WHILE IN USE REMOVED FROM SERVICE. CLEANED G2 OVEN AS REQUIRED, NOTED REMAINS OF BURNT FOOD. OPS CHECK GOOD REF E175 AMM TASK 25-37-02-720-802-A. RETURNED TO SERVICE.

Part: BLADES — DAMAGED (NR 1 ENGINE) · airframe 15,517 hrs · 10,736 cycles

FLIGHT 2248. DURING TAKE OFF ROLL HIT A BIRD ON THE LEFT ENGINE. DECLARED EMERGENCY WITH ATC AND RETURNED TO THE FIELD. LANDING UNEVENTFUL. FIRE DEPARTMENT MET AIRCRAFT AS PRECAUTION. FOUND EVIDENCE ABOUT BIRD STRIKE ON ENG #1. SEVERAL FAN BLADES DAMAGED. REMOVED FROM SERVICE. PERFORMED BIRDSTRIKE INSPECTION IAW E175 AMM 05-50-02-200-801-A AND BORESCOPE INSP OF #1 ENGINE IAW GE LMM 72-00-00-220-802. #1 ENGINE FAN BLADES #9,10,11,12 DAMAGED. REPLACED #1 ENG FAN BLADES #9,10,11,12,23,24,25,26 REF GE LMM TASK 72-21-00-800-803. #1 ENGINE FAN BLADE #6 DAMAGED. MEASURED DAMAGE AT #6 BLADE LEADING EDGE ON #1 ENGINE IAW GE LMM 72-21-00-200-803 STEP 3 A. TABLE 801. FOUND TO BE DEFORMATION AND IN LIMITS. MARKED FAN BLADE W/ MARKER. DURING #1 ENGINE BORESCOPE FOUND NICK ON STAGE 7 COMPRESSOR ROTOR BLADE AT LEADING EDGE. MEASURED NICK ON #1 ENGINE STAGE 7 COMPRESSOR ROTOR BLADE AT LEADING EDGE IAW GE LMM 72-00-00-220-802 5.C. TABLE 804. FOUND TO BE IN LIMITS. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: ARM — DAMAGED (ZONE 800) · airframe 15,363 hrs · 10,599 cycles

FLIGHT 2159. AIRCRAFT WAS OUT OF SERVICE FROM 10/3/24 TO 10/10/24. CSA SLAMMED THE DOOR WHILE CLOSING IT. A PIECE OF A RUB STRIP BROKE OFF AND FLEW INTO THE FORWARD GALLEY. THE DOOR IS NOW WEDGED AND UNABLE TO BE OPENED OR CLOSED" REMOVED FROM SERVICE. DURING ARRIVAL OF A/C FOUND TOP AFT SECTION OF DOOR WAS FILLED AFT FWD LOWER SECTION WAS TILETED FWD. ABLE TO OPEN STUCK DOOR PERFORMED GVI OF L1 DOOR AND SURROUND. FOUND 1 INCH CHUNK OF LINER MISSING AT TOP POSITION OF DOOR. ALSO FOUND AFT CENTERING PAD WORN & SUSPECT POSSIBLE MISALIGNMENT. REF WO 345314. NR 3, 5, 6, 12, 13, 14, 15, 16, 17, 18, 19 AND 20 FOR TROUBLE SHOOTING, FINDINGS, AND REPLACEMENT OF L1 DOOR ARM ASSEMBLY, FULL L1 DOOR RIG AND FURTHER WORK PERFORMED. NO FURTHER DEFECT NOTED. DOOR FUNCTION GOOD. RETURNED TO SERVICE. PHENOLIC BUSHING FOUND WORN IN THE SUPPORT ARM ATTACHMENT ARM.

Part: INDICATOR — OUT OF ADJUST (ZONE 800) · airframe 15,216 hrs · 10,505 cycles

L1 DOOR STATUS INDICATOR ONLY PARTIALLY INDICATING ARMED OR DISARMED. PLACED ON MEL MEL CLEARED BY ADJUSTED INDICATOR REF E175 AMM 52-11-00-820-801-A SUBTASK 52-11-00-820-033-A STEP 9V(6)(A-C). RETURNED TO SERVICE.

Part: SLIDE — MALFUNCTIONED (ZONE 800) · airframe 13,823 hrs · 9,380 cycles

DURING L1 DOOR EVACUATION SLIDE SAFETY PIN INSTALLATION, LOWER SAFETY PIN WAS FOUND HARD TO INSTALL DUE TO INCORRECT POSITON OF SLIDE PACKBOARD LATCH.FORCED PACKBOARD LATCH BACK INTO PLACE IN ORDER TO INSTALL PIN. INSTALLED LOWER SLIDE SAFTEY PIN ON L1 DOOR REF AMM TASK 52-00-23-900-801-A. PERFORMED GVI OF PACKBOARD LATCH RELEASING CABLE AND FOUND MINOR SIGNS OF WEAR ON CABLE. DETERMINED LENGTH OF PACKBOARD LATCH RELEASING CABLE NOT TO BE CAUSE OF ISSUE. REMOVED FORWARD PASSENGER DOOR EMERGENCY SLIDE IAW TASK # 25-65-01-000-801-A. INSTALLED SERVICEABLE EVACUATION SLIDE ASSY REF 175 AMM TASK 25-65-01-400--801-A

Part: LATCH — MALFUNCTIONED (L1 DOOR) · airframe 13,817 hrs · 9,376 cycles

L1 DOOR SHOWED PARTIAL GREEN ON LEFT LATCH INDICATOR WHEN SHUT (LATCH ON DOORFRAME). ASKED GATE AGENT TO REOPEN DOOR AND THEY WERE UNABLE TO. VENT FLAP ACTIONS OK, MAIN HANDLE ONLY MOVES UP APPROX. 2" FROM THE OUTSIDE. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. REPLACED L1 DOOR LATCH SENSOR ASSY AND ACCOMPLISHED TO 202403080151 FOR DOOR ADJUSTMENTS. RETURNED TO SERVICE.

Part: FITTING — OUT OF ADJUST (L1 GIRT BAR) · airframe 13,764 hrs · 9,337 cycles

FOUND L1 DOOR GIRTBAR AFT FLOOR FITTING OUT OF ADJUSTMENT. (L1 DOOR HARD TO OPEN). REMOVED FROM SERVICE. ADJUSTED L1 DOOR AFT GIRTBAR FLOOR FITTING. REF E175 AMM TASKS 53-10-21-0000/400-804-A. OPERATIONAL AND ADJUSTMENT CHECK GOOD. REF AMM TASK 52-11-00-820-A. RETURNED TO SERVICE.

Part: FITTING — DAMAGED (L1 DOOR SLIDE) · airframe 13,482 hrs · 9,096 cycles

MCD, (L1), AFT ESCAPE SLIDE FITTING ASSY, APPEARS TO HAVE A WEAK SPRING. REF E175 IPC, 53-10-21-15, FIG 70. REMOVED AND REPLACED THE AFT ESCAPE SLIDE FLOOR FITTING ASSY WITH NEW FROM STOCK REF E175 AMM TASK #53-10-21-000-804-A, AND 53-10-21-400-804-A.

Part: FITTING — MALFUNCTIONED (GIRT BAR) · airframe 13,478 hrs · 9,093 cycles

DOOR HANDLE ON MAIN CABIN DOOR (L1) IS DIFFICULT OT RAISE. REMOVED FROM SERVICE. REF W/O 337575 N/R-00002 FOR REPLACEMENT OF AFT SLIDE FLOOR FITTING ASSY. ALSO FOUND EXCESSIVE EPOX FROM PREVIOUS REPAIR ON UPPER CENTER ARMING WINDOW. REMOVED EXCESSIVE EPOXY. DOOR OPERATES NORMALY. REF AMM 52-11-00-910-801-A PAR 4C. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

FORWARD PAX DOOR SLIDE BACKING PLATE CRACKED. REMOVED AND REPLACED FWD PASSENGER DOOR SLIDE ASSEMBLY ON RACK, RE-INSTALLED GIRT BAR ON SLIDE. REF AMM 25-65-01, 52-11-41.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

BOTH LANDING GEAR EMERGENCY CLOSED LOOP CABLES ADJUSTMENT OUT OF LIMITS. RIGGED BOTH LANDING GEAR EMERGENCY CLOSED LOOP CABLES REF AMM 32-34-09.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

L1 DOOR FWD EVACUATION SLIDE FITTING SPRING BROKE AND RUSTY HARDWARE AND AFT FITTING HARDWARE RUSTY. REMOVED AND REPLACED HARDWARE ON L1 DOOR FWD AND AFT EVACUATION SLIDE FLOOR FITTING AS MARKED. REF AMM 53-10-21. REMOVED AND REPLACED SPRING ON L1 DOOR FWD FLOOR FITTING. REF AMM 53-10-21. ADJUSTMENT CHECK OF BOTH FITTINGS GOOD. REF AMM 52-11-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

AFT PASSENGER DOOR SLIDE MECHANISM CABLE CASING IS SEPARATED AT UPPER END. REPAIRED AFT PASSENGER DOOR SLIDE MECHANISM CABLE CASING AT UPPER END PER HORIZON COC AMM 52-12-40. ADJUSTMENT CHECK GOOD. REF AMM 52-12-52.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

FWD PAX DOOR SLIDE MECHANISM CABLE CASING IS SEPARATED AT UPPER END. REPAIRED FWD PAX DOOR SLIDE MECHANISM CABLE CASING AT UPPER END PER HORIZON COC AMM 52-11-40.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,467 hrs · 9,087 cycles

FWD SERVICE DOOR SLIDE MECHANISM CABLE CASING IS SEPARATED AT UPPER END. REPAIRED FWD SERVICE DOOR SLIDE MECHANISM CABLE CASING AT UPPER END PER HORIZON COC AMM 52-41-40.

Part: MODULE — MALFUNCTIONED (APU FUEL) · airframe 13,284 hrs · 8,931 cycles

AT APPROX. 300' AGL, THE APU FAILED. AT 400' ICASS MESSAGE APU FAIL MESSAGE ILLUMINATED. RETURNED TO FIELD. L;ANDING UNEVENTFUL. REMOVED FROM SERVICE. REF W/O 335965 TASK CARD: ECMP-APS2300 FMA R/R FOR WORK PERFORMED. REPLACED APU FUEL MODULE ASSY. RETURNED TO SERVICE.

Part: FMU — MALFUNCTIONED (#2 ENGINE) · airframe 12,793 hrs · 8,540 cycles

ENGINE #2 NO DISPATCH MESSAGE AFTER ENGINE START. PLACED FADEC SYSTEM ON MEL (IGNITORS). CLEARED BY REPLACING THE FUEL METERING UNIT IAW AMM 73-21-03-000/400-801-A. CHECKS GOOD. MEL CLEARED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,652 hrs · 8,441 cycles

MOMENTRY LAV SMOKE EICAS MASTER WARNING ILLUMINATED IN FLIGHT. NO INDICATIONS OF FIRE, SMOKE, VAPE, SMOKE OR TAMPERING. REMOVED FROM SERVICE. C/W OPS CHECK OF AFT LAVATORY SMOKE DETECTOR IAW E175 AMM 26-14-01-700-801-A. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FADEC — MALFUNCTIONED (#2 ENGINE) · airframe 12,366 hrs · 8,200 cycles

ENGINE 2 NO DISPATCH DURING START OF #2 ENGINE. PLACED ON MEL 73-21-01A. MEL CLEARED 7/5 BY REPLACING #2 FADEC REF E175 AMM 73-21-01-000/400-801-A. OPS CHECK GOOD. CLEARED DEFECT. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 200) · airframe 11,877 hrs · 7,777 cycles

THRUST CONTROL QUADRANT REQUIRES REPLACEMENT PER TO 20230411418. R AND R THRUST CONTROL QUADRANT IAW E175 AMM 76-11-01-000/400-801. PERFORMED LLM RTS TEST IAW E175 AMM 76-11-01-400-801 AND E175 AMM 76-11-01-720-802. AIRCRAFT REMAINS CAT III QUALIFIED. COCKPIT PLACARD REMAINS CAT III MAINTENANCE CONTROL NOTIFIED.

Part: ACTUATOR — MALFUNCTIONED (ZONE 200) · airframe 11,501 hrs · 7,434 cycles

RUDDER TRIM MIGRATING LEFT AND RIGHT BELLOW 230 KIAS. NO MISBEHAVIOR ABOVE 230. NO EICAS MESSAGES OR OTHER FAULT. REMOVED FROM SERVICE. INTERROGATED CMC FOUND NO FAULT CODES, PERFORMED GVI OF RUDDER AND TRIM, FOUND NO DEFECTS, PERFORMED RUDDER TRIM ACTUATOR FUNCTIONAL TEST IAW E175 AMM TASK 27-24-01-720-801-A, RUDDER TRIM INDICATOR ON EICAS MOVES AS REQUIRED FHDB DOWNLOAD PERFORMED AND SENT, IAW E175 AMM TASK 45-45-00-00-970-801-A, PER MTX REQUEST, NO FURTHER DEFECT NOTED. REPLACED RUDDER TRIM ACTUATOR.

Part: PUMP — LEAKING (NR 1 ENG FUEL) · airframe 11,036 hrs · 6,996 cycles

FOUND THE #1 ENGINE FUEL PUMP TO BE LEAKING. REMOVED FUEL PUMP IAW E-175 A,, TASK 73-11-01-000-801-A. INSTALLED SERVICEABLE PUMP IAW E175 AMM 73-11-01-400-401-A. LEAK CHECKS GOOD.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 10,953 hrs · 6,914 cycles

A FOOT LONG PIECE OF FLOOR EMERGENCY GLOW STRIP CAME OFF. REMOVED FROM SERVICE. RE SECURED FLOOR STRIP LIGHTING. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: NONE — NONE · airframe 9,273 hrs · 5,320 cycles

FA REPORTS AFT RIGHT DOOR DISARMING LEVER DIFFICULT TO DISARM. REMOVED FROM SERVICE. UPON ARRIVAL @ A/C F/A COULD NOT DUPLICATE DIFFICULTY ARMING AND DISARMING AFT RIGHT DOOR. PERFORMED GVI OF DOOR AND ARM/DISARM HANDLE. DOOR ARMED AND DISARMED WITH NORMAL EFFORT. A/C OK FOR RTS NO DEFECTS FOUND ON GVI.

Part: NONE — NONE · airframe 9,273 hrs · 5,720 cycles

FA REPORTS FWD RIGHT DOOR DISARMING LEVER DIFFICULT TO DISARM. REMOVED FROM SERVICE. UPON ARRIVAL AT A/C F/A COULD NOT DUPLICATE ARMING AND DISARMING OF RIGHT FWD DOOR PERFORMED GVI OF DOOR AND ARM / DISARM HANDLE WITH NO DEFECTS FOUND DOOR ARMED AND DISARMED WITH NORMAL EFFORT A/C OK FOR RTS.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 7,450 hrs · 4,532 cycles

LAV SMOKE MASTER WARNING NO SIGN OF FIRE PAX WAS IN LAV WHICH SMELLED LIKE VAPE. REMOVED FROM SERVICE. INSPECTED FWD LAV INCLUDING THE TRASH CAN FOR ANY DEFECT. NONE FOUND. PERFORMED TEST OF THE LAV SMOKE DET SYSTEM IAW AMM TASK 26-14-01-700-801-A WITH NO DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE .

Part: WIRE HARNESS — MISROUTED (FUEL QTY IND) · airframe 7,442 hrs · 4,528 cycles

FUEL QTY INDICATION HARNESS FOUND ROUTED WITH AFT SPOILER CNTL MODULE FROM MODULE INTO THE WHEEL WELL. REROUTED THE FUEL QTY INDICATION HARNESS PER E175 AMM 28-41-06-400-801-A, AND SWPM 20-45-30

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 7,067 hrs · 4,293 cycles

FA REPORTS R1 DOOR ARMING HANDLE STIFF WHEN DIS-ARMING DOOR ON ARRIVAL. REMOVED FROM SERVICE. ADJUSTED BOTH EVACUATION SLIDE FITTINGS ON GALLEY FLOOR IAW E175 AMM TASKS 53-10-25-000-804-A AND 400-804-A. ARM/DISARM HANDLE OPERATES SMOOTH AND EASY. RETURNED TO SERVICE.

Part: ARMING LEVER — STICKING · airframe 6,997 hrs · 4,247 cycles

R1 ARMING LEVER STICKS. REMOVED FROM SERVICE. CLEANED FWD SERVICE DOOR GIRT BAR ANCHORS AS REQUIRED. ARMING LEVER MOVES SMOOTHLY. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SPRING — DAMAGED (GIRT BAR) · airframe 6,895 hrs · 4,200 cycles

FWD SERVICE DOOR EMERGENCY SLIDE ARMING LEVER IS VERY DIFFICULT TO ENGAGE. REMOVED FROM SERVICE. C/W INSTRUCTIONS PER E175 AMM SDS 52-41-00 FOR ARMING AND DISARMING OF THE FWD SERVICE DOOR EMERGENCY SLIDE ARMING LEVER. LEVER OPERATES AS INTENDED. NO DEFECTS NOTED. REFERENCE W.O. 296936, T/O # 00003 FOR TECH ORDER FINDINGS OF DIMENSIONAL CHECK OF THE GIRT BAR SPRINGS, REFERENCE N/R-00004 FOR SLIDE REMOVAL & REINSTALL AND REFERENCE N/R-00005 FOR FORWARD & AFT SPRINGS FOR GIRT BAR ON THE FWD SERVICE DOOR. REF W/O 296936 N/R -00005 FOR REPLACEMENT OF GIRT BAR SPRINGS. AIRCRAFT RETURNED TO SERVICE.

Part: TRACK — DIRTY (GIRT BAR) · airframe 6,868 hrs · 4,183 cycles

FRONT #2 SIDE DOOR ARMING LEVER TAKES SIGNIFICANT FORCE TO ARM. REMOVED FROM SERVICE. CLEANED GIRT BAR TRACK AS REQUIRED CYCLES ARM/DISARM LEVER, NO DEFECTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CABLE — OUT OF POSITION (R1 GIRT BAR) · airframe 6,809 hrs · 4,147 cycles

R1 DOOR VENT FLAP HANDLE NOT FLUSH WITH ARMING LEVER. REMOVED FROM SERVICE. INSPECTED AND FOUND AFT BUSTLE DETACH CABLE INTERFERING WITH THE MOVABLE INDICATION TO LENS FOR THE AFT GIRT BAR. REMOVED BUSTLE, DISCONNECTED BOTH GIRT BAR CABLES AND REROUTED TO CONFORM TO FIG 410 SHEET 1 OF AMM TASKS, RECONNECTED CABLES AND REINSTALLED BUSTLE; IAW ERJ AMM TASKS 25-65-01-000-801-A PARA 1-5.A.(2), & FIG 401 SHEET 1, AND 25-65-01-400-801-A PARA 6.C.(1)-(3) NAD REF FIG 401 SHEET 1. NO ADJUSTMENTS MADE. RETURNED TO SERVICE.

Part: ARMING LEVER — FOD (ZONE 800) · airframe 6,799 hrs · 4,141 cycles

R1 DOOR ARMING LEVER NOT FULLY ENGAGING. REMOVED FROM SERVICE. C/W E175 FIM TASK 52-41-00-810-808-A STEPS 1-5A. FOUND DEBRIS & CONTAMINATION IN FORWARD SERVICE DOOR EVACUATION SLIDE FITTINGS. CLEANED & REMOVED ALL DEBRIS FROM DOOR FITTINGS. R1 DOOR ARMING LEVER OPERATES NORMALLY. A/C OK FOR CONTINUED SERVICE. NOTE: WHEN CLEANING THE CONTAMINATION FROM EVACUATION SLIDE FITTINGS OF R1 DOOR INSPECTED THEM IAW 53-10-25-200-804-A, NO DEFECTS NOTED.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 6,760 hrs · 4,116 cycles

FA REPORT ARMING LEVER ON RI DOOR NOT ARMING FULLY. REMOVED FROM SERVICE. REMOVED DEBRIS FROM GRIT BAR FLOOR FITTING ON R1 DOOR ARM/DISARM LEVER ENGAGES AND DISENGAGES PROPERLY NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN FLOOR) · airframe 6,044 hrs · 3,686 cycles

FLOOR PATH LIGHTING STRIP B IS CRACKED. REPLACED FLOOR PATH STRIP, IAW E175 AMM 33-50-21-000/400-801A.

Part: MANIFOLD — MALFUNCTIONED (NLG STEERING) · airframe 6,029 hrs · 3,677 cycles

RIGHT TURN TENDENCY ON TAXI AND ON ROLLOUT AFTER LANDING. FOUND HIGHER BRAKE TEMPS ON THE LEFT SIDE WHEEL BRAKES. REMOVED FROM SERVICE. SEARCHED STEERING MANIFOLD S/N: 01843 HISTORY AND FOUND IT HAD BEEN REMOVED FROM ANOTHER A/C FOR "RIGHT TURN TENDENCY DURING TAXI." C/W E175 MCN: E320065-01 ISSUE NO: 02, NO FINDINGS. ALL RECORDED VALUES ARE NOMINAL/NORMAL. R & R STEERING MANIFOLD, REF E175 AMM TASK 32-52-01-000/400-801-A. LEAK & OPERATIONS CHECKS ARE GOOD. DURING MTX TAXI NO UNUSUAL STEERING TURN TENDENCY WAS NOTED. THIS ACTION CLEARS LOG ENTRY. RETURNED TO SERVICE.

Part: SCREW — MISSING (DOOR HANDLE) · airframe 1,428 hrs · 898 cycles

EMERGENCY EQUIPMENT DOOR HANDLE BROKEN. DIFFICULT OPENING DOOR. REMOVED FROM SERVICE. INSTALLED MISSING SCREW ON DOOR LATCH. NO FURTHER DEFECTS NOTED. EMERGENCY EQUIPMENT DOOR OPERATES NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: PLACARD — UNSECURE (LANDING GEAR) · airframe 1,025 hrs · 671 cycles

EMERGENCY GEAR DOOR PLACARD. REMOVED FROM SERVICE. RESECURED LANDING GEAR EMERGENCY PLACARD TO EMERGENCY GEAR EXTEND DOOR. NO OTHER DEFECTS. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: LATCH — DEFECTIVE (COCKPIT DOOR) · airframe 893 hrs · 578 cycles

FLIGHT DECK DOOR LATCHING MECHANISM UNLOCKING/LOCKING DOOR INCORRECTLY ( FLIGHT DECK SECURITY DOOR AUTOMATIC LOCKING SYSTEM ). REMOVED AND REPLACED COCKPIT DOOR ELECTROMAGNETIC LATCH WITH NEW REFERENCE AMM TASK 52-51-03-400-801-A AND 52-51-03-000-801-A. PLACARDS REMOVED CIRCUIT BREAKER RESET MTX CONTROL NOTIFIED CLEARS DMI.