N625QX
Registered owner: HORIZON AIR INDUSTRIES INC, WA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FLIGHT 2332. PARTIAL SLIDE DEPLOYMENT OM MAIN CABIN (L1) DOOR. NO INFLATION. REMOVED FROM SERVICE.REMOVED FWD PAX DOOR BUSTLE IAW AMM 25-23-04-000-801-A. REMOVED FWD PAX DOOR EMERG. EVACUATION SLIDE ASSY IAW AMM 25-65-01-000-801-A. SAFETY PINS INSTALLED. REMOVED L1 DOOR GIRT BAR IAW AMM 52-11-41-000-801-A. FOUND L1 DOOR ASSIST BOTTLE DISCHARGED. PERFORMED FERRY FLIGHT FOR REPAIRS. INSTALLED NEW EMERGENCY EVACUATION SLIDE ASSEMBLEY TO L1 DOOR. REF AMM 25-65-01-400-801-A. REPLACED PNEMUATIC ASSEMBLEY DIAPHRAGM AND SHEAR PIN. REF AMM 52-11-56-000-801-A AND AMM 52-11-53+-400-801-A STEPS 1-8(L). CHARGED L1 DOOR PENUMATIC ASSY (REF AMM 52-11-53-400-801-A STEP 9. NFDN. RETURNED TO SERVICE.
FLIGHT 2405. BIRD STRIKE CAPTAINS WINDSHIELD AT 2500 FEET ON DEPARTURE . RETURNED TO FIELD DUE TO REDUCED VISIBILITY. LANDED NORMALLY. REMOVED FROM SERVICE. C/W E175 AMM 05-50-02-200-801-A. CLEANED BIRD REMAINS. FOUND NO DAMAGE TO A/C AFTER INSPECTION. NO FURTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE. NO PARTS REPLACED.
AT FL 330, RIGHT BEFORE DESCENT, STRONG THUMPING FELT IN FLOOR. IT FELT LIKE IT WAS NEAR THE FLIGHT DECK. THIS LASTED APPROX 10 MIN. AFTER THAT THE REST OF THE DESCENT WAS NORMAL UNTIL PASSING 10,000 FT. THUMPING IN FLOOR RESTARTED FOR SEVERAL MIN. BOTH F/A'S SAID THAT THEY COULD HEAR AND FEEL THE THUMPING ABOUT AT ROW 4. REMOVED FROM SERVICE. PERFORMED RIGGING AND FUNCTIONAL TEST OF NLG UPLOCK 2 SENSOR AND REPLACEMENT OF SENSOR. WIRING CHECKS PSEM2 TO NLG UPLOCK2 SENSOR PLUG, AND REPLACEMENT OF PSEM2. OPERATIONAL CHECK FLIGHT FAILED. AIRCRAFT REMAINS OUT OF SERVICE.
FUEL LEAK AT THE RIGHT HAND WING ROOT / WHEEL WELL AREA. AREA HAD A PREVIOUS REPAIR APPLIED. AIRCRAFT REMOVED FROM SERVICE AND IS CURRENTLY BEING REPAIRED.
FLIGHT 2274. FLIGHT DECK DOOR IS DIFFICULT TO OPEN.REMOVED FROM SERVICE. CLEANED FLIGHT DECK DOOR LATCH. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2012. FLIGHT DECK DOOR DIFFICULT TO OPEN.. REMOVED FROM SERVICE. CLEANED FLIGHT DECK DOOR LATCH, OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2295. POWERED UP AIRCRAFT WITH APU IMMEDIATE PACK 2 FAIL EICAS MESSAGE SO WE RAN CHEKLIST IN QRH WITH ANOTHER PACK 2 FAIL MESSAGE. FA'S SMELLED BURNING SMELL IN MAIN CABIN. RAMP REPORTS SMOKE COMING OUT OF PACK 2 EXAUST VENT UNDER FWD CARGO BAY. WITH PACK 2 SELECTED OFF, NO SMOKE OR SMELL. REMOVED FROM SERVICE. PERFORMED GVI OF RAM AIR INLET. NO SIGNS OF INGESTION. REMOVED PANEL 191AR & PERFORMED GVI OF PACK 2 AREA. NO STRUCTURAL OR ELECTRICAL DAMAGE NOTED. REMOVED CLAMPS ON RAM AIR OUTLET DUCT FLEXIBLE CONNECTION REF AMM 21-51-00-000-801-A. RAM AIR OULTLET DUCT & HEAT EXCHANGER HAVE RESIDUE INSIDE. REMOVED CLAMPS ON PACK OUTLET DUCT REF AMM 21-51-21-00-801-A. NO RESIDUE NOTED. RESECURED ALL DUCT CLAMPS REF AMM 21-51-00-400-801-A & 21-51-21-400-801-A. RESECURED PANEL 191AR. SMOKE & SMELL STOPPED WITH PACK 2 OFF. REF LP 108729 FOR DEFFERAL OF PACK 2. RETURNED TO SERVICE.
FLIGHT 2155. FLIGHT DECK DOOR IS DIFFICULT TO OPEN FROM INSIDE THE FLIGHT DECK. REMOVED FROM SERVICE. PERFORMED GVI OF FLIGHT DECK DOOR, FOUND DEBRIS IN MECHANICAL LATCH. CLEANED MECHANICAL LATCH AS REQUIRED, DOOR NOW OPENS AND CLOSES SMOOTHLY AS REQUIRED. RETURNED TO SERVICE. NO PARTS REPLACED.
FLIGHT 2016. REJECTED TAKEOFF AT APPROX. 100 KTS IAS DUE TO IAS MISMATCH FLAG ON AIRSPEED DIFFERENCE WAS APPROX. 10-15 KTS BETWEEN AIRSPEED INDICATORS CO PILOT IAS SHOWED APPROX. 80 KNOTS AT THE "80" CALL, PILOT SIDE SHOWED APPROX. 70 KNOTS. RETURNED TO GATE. FOLLOWED BY CFR. REMOVED FROM SERVICE. DURING INSPECTION OF PROBES FOUND DEBRIS IN #1 PITOT/STATIC/AOA SENSOR. PER MC REPLACED THE SENSOR REF. AMM 34-13-01-000/400-801-A. OPS TEST GOOD. THIS AIRCRAFT REMAINS CAT III, PLACARD IN COCKPIT SHOWS CAT III. MC NOTIFIED. PERFORMED HIGH ENERGY STOP CONDITION TASK, REF. AMM 05-50-12-200-801-A. NO DEFECTS NOTED. RETURNED TO SERVICE.
L1 DOOR DOES NOT OPEN NORMALLY. REQURIED UPWARD PRESSURE ON LATCH TO OPEN FROM THE OUTSIDE. REMOVED FROM SERVICE. C/W E175 FIM TASK 52-11-00-810-806+-A PARA 4.B. L1 DOOR OPERATES NORMAL, NO FAULT CODES NOTED. ALL L1 DOOR INDICATIONS ARE NORMAL. A/C OK FOR SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.
CENTER FUSELAGE 3 AFT CARGO LOWER SKIN FR 75 BETWEEN SRGR 29R AND STGR 29L THERE IS A CORRODED FLOOR SUPPORT. INSTALLED REPLACEMENT FLOOR SUPPORT CENTER FUSELAGE III AFT CARGO FR75 BETWEEN STGR 29R AND STGR29L REF EMB SRM 51-40-08. SEE WIPS AND TASKS FOR WORK PERFORMED
CENTER FUSELAGE 3 AFT CARGO LOWER SKIN FR76 AND BETWEEN STGR 29L AND 28L CORRODED SHEAR CLIP. REMOVED AND REPLACED THE SHEAR CLIP AT FR76 BETWEEN STGR 29L AND 28L. REF EMB SRM 51-40-08.
CENTER FUSELAGE 3 AFT CARGO DOOR CUTOUT FWD FINGER DOUBLER CORRODED AT FR 77. REMOVED AND REPLACED THE CENTER FUSELAGE 3 AFT CARGO DOOR CUTOUT FWD FINGER DOUBLER AT FR 77 REF SRM 51-40-08. SEE WIPS AND TASKS FOR WORK PERFORMED.
CENTER FUSELAGE 3 FR 87 R/H REAR BEAM CORRODED. REMOVED AND REPLACED THE CENTER FUSELAGE 3 FR 87 R/H REAR BEAM. REF EMB SRM 51-40-08. SEE WIPS AND TASKS FOR WORK PERFORMED.
#1 ENGINE FIRE EXTINGUISHING SYSTEM FUSELAGE TEE VALVE FAILED FUNCTIONAL TEST. REMOVED AND REPLACED #1 ENGINE FIRE EXTINGUISHING SYSTEM FUSELAGE TEE VALVE, CHECKED FOUND OK. REF AMM 26-21-00 AND 26-21-13.
FLIGHT 9988. STUCK MIC COM 1, INTERCOM TRANSMITTING OVER PA. CONSTANT TRIPPLE CHIME IN THE CABIN. REMOVED FROM SERVICE. FOUND FAULT CODE 23511002CMC C/W FIM TASK 23-51-00-810-865-A. PERFORMED OPS CHECK OF AIRBORNE AUDIO SYS IAW AMM TASK 23-51-00-710-801-A OPS CHECK FAILED FAULT PERSISTS. REPLACED #1 NIM, UPLOADED SOFTWARE AND PERFORMED OPERATIONAL TESTS, ALL CHECK GOOD A/C AND PLACARD REMAIN CAT III QUALIFIED.REPLACED #1 NIM, UPLD SOFTWARE AND PERFORMED ALL OPS CHECK PER E175 AMM TASKS 34-02-04-000-801 & 34-02-04-400-801. RETURNED TO SERVICE.
ON TAKEOFF ABOVE 1000' WE HAD A BIRDSTRIKE ON THE #1 ENGINE. LP VIBRATION WAS NOTED AT 4.1 OR HIGHER. NOTICABLE VIBRATION AND SOUND. FOUND DAMAGE TO MULTIPLE #1 FAN BLADES WITH EVIDENCE OF A BIRD STRIKE IN THE NACELLE & ON THE FLAP BEHIND MLG #1 SIDE. VIBRATION NORMAL BELOW 50% N1. DECLARED EMERGENCY. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED BIRDSTRIKE INSPECTION ON AIRCRAFT AND REMOVED BIRD REMAINS IAW E175 AMM 05-50-02-200-801-A. NO EVIDENCE OF #1 ENGINE CORE INGESTION. FOUND DAMAGE TO #1 ENGINE FAN BLADES #23, 27, 28, 1, 2, 3 AND 4. REMOVED AND REPLACED #1 ENG FAN BLADE & PIN SET (REF T/C E175-72-00-00-QE03). VIBE CHECK GOOD, NFDN. RETURNED TO SERVICE.
FLIGHT 2047. ESCAPE ROUTE LIGHT STRIP ADJACENT TO 2C IS DAMAGED LESS THAN 10% OF THE LIGHT STRIP. ALSO DAMAGED AT 1D 1A 2A 2C 1C. REMOVED FROM SERVICE AND PLACED ON MEL. CLEARED BY REPLACING PHOTOLUMINESCENT INDICATOR LIGHT STRIPS ADJACENT T IAW E175 AMM 33-50-21-000/400-801-A OPS TEST GOOD NFDN PLACARDS REMOVED MTX CTRL NOTIFIED THIS CLEARS DEFECT. RETURNED TO SERVICE.
#2 ENGINE STARTER CONTROL VALVE FOUND PUNCTURED AT HOUSING. R&R #2 ENGINE STARTER CONTROL VALVE IAW E175 CF34-8 LMM 80-00-00-800-801. LEACK CHECK GOOD. A/C CLEAR TO RTS.
FA REPORTED R1 DOOR SLIDE GAUGE OUT OF VIEW/ HARD TO READ. REMOVED FROM SERVICE. REPLACED R1 FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE ASSY IAW E175 AMM 25-65-01-000-801-A/400-801-A. NO FURTHER DEFECTS. RETURNED TO SERVICE.
AUTOTHROTTLES DISCONNECTED (UNCOMMANDED) 3 TIMES DURING DESCENT, BETWEEN FL240 AND 16000 FT, AT 270 KIAS. PLACED ON MEL 22-30-00B. MEL CLEARED BY REPLACING TRUST CONTROL QUADRANT AND PERFORMED LLM RTS TEST IAW AMM 76-11-01-000/400-801 AND 22-11-00-710-801. A/C REMAINS CAT III QUALIFIED. COCKPIT PLAC REMAINS CAT III. M/C NOTIFIED. CLEAR DEFECT.
FLIGHT CONTROLS NOT MOVING NORMALLY DURING AFTER START CHECK. RUDDER STIFF AND CHATTERING. REMOVED FROM SERVICE. DUE TO RECENT HISTORY, BLED #1 HYD SYS, REF AMM TASK 29-10-00-870-803-A. C/W OPS TEST OF RUDDER CONTROL SYSTEM PER AMM TASK 27-20-00-710-802-A. NO DEFECTS NOTED. RETURNED TO SERVICE.
DURING FLIGHT CONTROL CHECK; THE CAPTAINS YOKE GRINDS WHEN LEFT AILERON INPUT IS RELEASED. REMOVED FROM SERVICE. INSPECTED CAPTAINS AILERON CONTROL CABLE AND FOUND A ZIP TIE IN THE CAPTAINS YOKE. REMOVED ZIP TIE, NO MORE GRINDING NOTED. AILERONS MOVE NORMALLY REF E175 AMM 27-11-01-400-801A. RETURNED TO SERVICE.
ON LANDING ROLLOUT ENG1 NO DISPATCH AND ENG 1 FADEC FAULT ILLUMINATED. REMOVED FROM SERVICE. R&R #1 ENG FADEC IAW CF34-8 LMM 73-00-00-800-801 #1 ENG OPS TEST GOOD NO MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE.
R2 DOOR FWD COMMAND RAMP HAS SURFACE CORROSION AND CORRODED HARDWARE. TREATED SURFACE CORROSION ON R2 DOOR FWD COMMAND RAMP AND HARDWARE IN REF TO SRM 51-12-00.
R1 DOOR FWD COMMAND RAMP HAS SURFACE AND HARDWARE CORROSION. TREATED SURFACE CORROSION AT R1 DOOR FWD COMMAND RAMP AND HARDWARE IN REF TO SRM 51-12-00.
CORROSION ON CENTER FUSELAGE III GUSSET AT FR 90 AND Y= +10. REMOVED AND REPLACED GUSSET AT CENTER FUSELAGE III FR 90 AND Y +10 IAW SRM 51-40-02, 51-40-08.
CORROSION ON CENTER FUSELAGE III RH LONGITUDINAL BEAM AT FR 87 AND Y= +10. REMOVED AND REPLACED CENTER FUSELAGE III RH LONGITUDINAL BEAM AT FR 86 TO-FR 89 AND Y +10 IAW SRM 51-40-02, 51-40-03,51-40-08.
CORROSION ON CENTER FUSELAGE III RH INTERCOSTAL BETWEEN FR 90-FR 91 AND Y= +10. REMOVED AND REPLACED CENTER FUSELAGE III RH INTERCOSTAL SUPPORT ANGLE AT FR 90-FR 91 AND Y +10 IAW SRM 51-40-02, 51-40-08.
CORROSION ON CENTER FUSELAGE III RH SHEAR PANEL BETWEEN FR 87-88 AND Y= +12 SEVERAL SPOTS. REMOVED AND REPLACED CENTER FUSELAGE III RH SEAR PANEL AT FR 87-FR 88 AND Y +12 IAW SRM 51-40-02, 51-40-08.
EICAS MSG RECIRC SMOKE DETECT FAIL ( RECIRCULATION SYSTEM SMOKE DETECTOR â PACKS OPERATIVE ). REMOVED FROM SERVICE. C/W FIM TASK 21-26-00-810-813-A, REMOVED AND REPLACED SPDA 2 DISCRETE/IO MODULE, SLOT M11 IAW E175 AMM TASK 24-61-05-000/400-801-A. OPS TEST GOOD IAW E175 AMM TASK 24-42-02-860-801-A. SMOKE DETECT FAIL EICAS MSG WENT AWAY. C/W AMM TASK 28-41-00-210-801-A, GVI OF THE HARNESSES OF THE FUEL QTY INDICATION SYSTEM, NO DEFECTS NOTED, THIS ACTION CLEARS MEL 26-16-00(A), DEFECT # 966615. PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE.
R1 DOOR SLIDE DISLODGED. REMOVED FROM SERVICE. R1 DOOR SLIDE FOUND TO BE MOUNTED FIRMLY. NO SIGN OF BEING DISLODGED. FURTHER INSPECTION REVEALED THAT THE SLIDE PRESSURE GAUGE DOES NOT LINE UP WITH THE BUSTLE VIEWING WINDOW. REMOVED AND REINSTALLED BUSTLE. RETURNED TO SERVICE.
HEARD NOISE AT CRUISE, ASSURED IT TO BE SPEED TAPE OVER GROUND POWER PLUG . SUSPICION CONFIRMED ON POST FLIGHT WALK AROUND. REMOVED FROM SERVICE. REMOVED & REAPPLIED SPEED TAPE OVER EXTERNAL POWER ACCESS DOOR AS REQUIRED. CDL CLEARED ON LOGPAGE 918622 BY REMOVING SPEED TAPE & INSTALLED PANEL 125AL REF E175 AMM 06-41-00-800-801-A. REVERSED MTX PROCEDURES FOR CDL 53-03-01. THIS ACTION CLEARS DEFECT 918622. RETURNED TO SERVICE.
DURING LINE CHECK, FORWARD SERVICE DOOR EMERGENCY DOOR OPENING BOTTLE PRESSURE IS LOW. CHARGED THE FORWARD SERVICE DOOR PNEUMATIC BOTTLE ASSEMBLY IAW E175 AMM 52-41-51-614-801-A.
EMERGENCY EGRESS PATH LIGHTING ASSY E175 AIPC 33-50-21-01 SECTION "B", "C", "D", "K" DAMAGED. R & R SECTION "B", "C", "D", "K" OF PHOTOLUMINESCENT STRIP LIGHT IAW E175 AMM TASK 33-50-21-000/400-801-A AND REF E175 AIPC 33-50-21-01. OPS TEST GOOD.
LAV SMOKE WARNING CAS MESSAGE CAME ON DURING CRUISE. FA'S SAID NO PASSENGERS HAD BEEN IN EITHER LAV AND NO EVIDENCE OF SMOKE OF ANY KIND. CHECKLIST C/W MESSAGE EXTINGUISHED WITHIN 2 MINS OF COMING ON. NO OTHER INDICATIONS WERE NOTED THROUGHOUT FLIGHT. REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF THE LAV'S FWD AND AFT AND THE LAV TRASH CAN AREA AND THE SMOKE DETECTOR WITH NO DEFECTS FOUND. PERFORMED OPERATIONS CHECK OF THE LAV SMOKE DETECTOR SYSTEM IN ALL LAV'S, REF AMM TASK 26-14-01-700-801-A, WITH NO DEFECT NOTED. AIRCRAFT OK FOR CONTINUED SERVICE.
DURING OPERATIONAL CHECK NOTED THAT WHEN SOFTLY PRESSURE ARMING R2 AFT SERVICE DOOR RED INDICATION IS FULL IN WINDOW, WHEN NORMAL PRESSURE ARMING R2 DOOR RED INDICATION TAB OVERCLOCKS THE VIEWING WINDOW SHOWING HALF RED. VERIFIED R2 DOOR GIRT BAR ENGAGED THE SAME AMOUNT WITH BOTH "SOFT" AND NORMAL PRESSURE APPLIED TO ARMING HANDLE. TEMPORARILY REMOVED AFT GIRT BAR (REF. E175 AMM 52-42-41-000-801-A) AND ADJUSTED FLAG TO BE RED DURING BOTH STYLES OF DOOR ARMING (52-42-00-820-801-A). REINSTALLED GIRT BAR AND REMOVED EES SAFETY PIN (52-42-41-400-801-A).
LAVATORY SMOKE DETECTOR SOUNDED IN CRUISE. SOURCE UNKNOWN. NO VISIBLE SMOKE. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. C/W E175 AMM TASK 26-14-01-700-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. COULD NOT DUPLICATE. NO PARTS REPLACED.
FA REPORTS FWD GALLEY SERVICE DOOR R1 ARMING LEVER IS DIFFICULT TO MOVE EXTREMELY STIFF. REMOVED FROM SERVICE. VERIFIED R1 ARMING LEVER ARMED AND DISARMED AS REQUIRED. NO STIFFNESS NOTED. NO DEFECTS FOUND. ARMING LEVER MOVES SMOOTHLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
F/A REPORTS EMERGENCY STRIP ON FLOOR IS BLACK. REMOVED FROM SERVICE. CLEANED EMERGENCY STRIP ON FLOOR L/H SIDE AT SEAT 2A-4A.NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.
ILLUMINESCENT LIGHTING ON FLOOR NEXT TO 4A MISSING. REMOVED FROM SERVICE. REPLACED 3A + 4A PHOTOLUMINESCENT INDICATOR STRIP LIGHT IAW E17 AMM TASK 33-50-21-000-801-A + 33-50-21-400-801-A. PERFORMED OPS TEST IAW E175 AMM TASK 33-50-21-710-801-A. OPS TEST GOOD. RETURNED TO SERVICE.
WHEN PUSHING CONTROL COLUMN FORWARD THERE IS HEAVY VIBRATION/BINDING. ALSO INTERMITTENT POPPING. REMOVED FROM SERVICE. COMPLIED WITH MCN E270006 ISSUE 01. NO FAULT CODES DISPLAYED ON EICAS. CONTROL COLUMNS MOVE WITHOUT BINDING. PERFORMED GVI OF CTRL COLUMN TORQUE TUBE & ASSOCIATED COMPONENTS IN FWD-AFT MOTION, NO DEFECTS NOTED. VERIFIED CTRL COLUMN DAMPERS INDICATED FULL WITH REF E175 AMM 27-31-02-210-801-A. NO DEFECTS NOTED, AIRCRAFT IS SERVICEABLE FOR CONTINUED SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.
WHEN MOVING CONTROL COLUMN FORWARD THERE IS A GRINDING/BINDING FEELING AND SOUND. BOTH FO AND CA SIDE. REMOVED FROM SERVICE. PERFORMED GVI OF VISIBLE COMPONENTS OF CONTROL COLUMN IN FLIGHT DECK + FWD AVIONICS BAY. DETERMINED NOISE TO BE LIKELY ORIGINATING FROM CONTROL COLUMN COMMAND POSITION SENSORS. PERFORMED GVI OF CONTROL COLUMN COMMAND POSITION SENSORS, FOUND LARGE AMOUNTS OF DUST AND DEBRIS ON THE INNER BARRELS. CLEANED AND POLISHED INNER BARRELS IAW E175 AMM 12-22-02-100-801-A AND RIGGED IAW E175 AMM 27-33-01-820-801-A. PERFORMED FLIGHT CONTROL RETURN TO SERVICE TEST IAW E175 AMM 27-00-00-070-801-A, AND FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECT NOTED PER GPM 9.2. AIRCRAFT RETURNED TO SERVICE.
GROUND PROXIMITY FLOOR LIGHTING NEAR SEAT 1A INOPERATIVE. REMOVED FROM SERVICE. R&R PHOTOLUMINESCENT INDICATOR STRIP LIGHT AT 1A IAW E175 AMM TASKS 33-50-21-000-801-A AND 33-50-21-400-801-A. OP CK GOOD. RETURNED TO SERVICE.
FOR APPROXIMENTLY 30 SECONDS LAV SMOKE MASTER WARNING. COMMUNICATED WITH FLIGHT ATTENDANT PASSENGER WAS IN LAV, PASSENGER EXITED LAV. LAV SMOKE MASTER WARNING CEASED. REMOVED FROM SERVICE. PERFORMED GVI OF LAVATORY & SURROUNDING AREA, NO SIGNS OF DAMAGE OR DEFECTS NOTED. C/W FIM TASK 26-14-00-810-803-A OPS TEST GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.
DURING CRUISE, A PASSENGER NOTED FLUID LEAKING AROUND RIGHT ENGINE PYLON. PILOTS CHECKED AND IT APPEARS TO BE FUEL. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE.
APPROXIMATELY 18 MINUTES AFTER TAKEOFF, F/A REPORTED MINOR MOISTURE VISIBLE ON RIGHT WING. MOISTURE LEVEL INCREASED WITH TIME UNTIL IT WAS STREAMING FROM WING. DIVERTED, LANDING UNEVENTFUL. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AFT FLAP COVER AREA AND INBD AND OUTBD OF ENG PYLON, FOUND RESIDUAL FUEL, NO ACTIVE LEAK NOTED. RAN ENG, NO LEAKS NOTED. FOUND 3 LOOSE FASTENERS ON FUEL ACCESS PANEL 621AB. SECURED FASTENERS. REMOVED AND INSPECTED PANELS 623AB AND 429XR TO INSPECT FOR LEAKS. NONE FOUND. REINSTALLED PANELS 623AB, 429XR. REMOVED PANELS 616BB, 616AB. FOUND LEAK COMING FROM FORWARD SPAR LOWER TANK SEALANT BETWEEN THE SLAT GEAR ARM AND ENGINE PYLONS. FOUND LEAK AT LOWER WING FORWARD SPAR OUTSIDE RIB 10. PERFORMED TEMP REPAIR TO LEAK IAW TC ETD2017-170-072887. FERRIED FOR REPAIRS. AIRCRAFT DOWN FOR REPAIRS.
FOUND FWD GIRT BAR RETAINING BRACKET ON BELLCRANK OF FWD SERVICE DOOR BENT. REMOVED FROM SERVICE. REMOVED SPRING PLATE ON FWD SERVICE DOOR. INSTALLED SERVICEABLE GIRT BAR SPRING PLATE AND DOUBLER IAW AMM 52-41-40-400-804A OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
R2 GIRT BAR INDICATION HALF RED, HALF WHITE. RETURNED TO SERVICE.
L2 DOOR EMERGENCY ESCAPE SLIDE INADVERTENTLY DEPLOYED, BUT DID NOT INFLATE. REMOVED SLIDE ASSEMBLY IAW AMM 25-65-01.