N445QX

Part: NONE — NONE · airframe 23,111 hrs · 24,809 cycles

FWD PAX DOOR LOWER THRESHOLD CORRODED BEYOND LIMITS. REPLACED FWD PAX DOOR LWR THRESHOLD IAW SRM 51-42-05-02-01, 51-42-75-02-01 AND 51-23-00-00-01 REV 21.

Part: SEAT TRACK — CORRODED · airframe 23,111 hrs · 24,809 cycles

SEAT RAIL 11 FROM FSX10.5-X102.5, Y9.250 IS CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 11 FROM FSX10.5-X102.5 Y9.250 IAW SRM 51-42-05-02-01, 51-41-05-00-01, 51-40-15-02-01, 51-40-07-01-01 REV 21.

Part: SEAT TRACK — CORRODED · airframe 23,111 hrs · 24,809 cycles

SEAT RAIL 10 FROM FSX-39.00-X10.5, Y9.250 IS CORRODED BEYOND LIMITS. REPAIRED SEAT RAIL 10 FROM FSX-39.00-X10.5 Y9.250 IAW SRM 51-42-05-02-01 51-41-05-00-01, 51-40-15-02-01, 51-40-07-02-01 REV 21.

Part: IGNITER — MALFUNCTIONED (APU) · airframe 22,975 hrs · 21,680 cycles

APU FAILED TO START - SMOKE OBSERVED FROM EXHAUST DURING START. PLACED ON MEL 49-00-1. CLEARED 8/27. INTERROGATED CDS, FOUND MULTIPLE HITS FOR FAULT "055/2 IGNITER PLUG B OPEN" IN FAULT HISTORY. REPLACED BOTH IGNITERS REF Q400 AMM 49-40-04-000-801 AND 49-40-04-400-801. OPS TEST GOOD. CLEARED MEL. RETURNED TO SERVICE.

Part: FEATHERING SYS — FAULTED (NR 2 PROPELLER) · airframe 22,935 hrs · 24,642 cycles

LAST 2 FLIGHTS #2 PROPELLER HAS FAILED TO FEATHER COMPLETELY ON SHUTDOWN. REMOVED FROM SERVICE. MET A/C, INTERROGATED CDS, FOUND FAULT CODE 144 A/B. C/W Q400 FIM TASK 61-20-03-810-821. CLEARED FAULTS, RAN #2 ENGINE TWICE. FAULT CODE 144 REMAINED CLEARED BOTH TIMES UPON SHUTDOWN. PHYSICAL INSPECTION OF THE #2 PROP WENT BACK TO FEATHER EACH TIME AT SHUT DOWN. NO CAUTION LIGHTS THAT WOULD BE ASSOCIATED ILLUMINATED. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (FEATHERING) · airframe 22,763 hrs · 24,469 cycles

#2 PROP DID NOT FULLY FEATHER DURING SHUTDOWN, NOTICED DURING WALK AROUND. NOTHING ABNORMAL FELT DURING SHUTDOWN. REMOVED FROM SERVICE. RAN #2 ENGINE, TOOK PROP IN AND OUT OF FEATHER MULTIPLE TIMES, PROPS NOW FULLY FEATHERED. SHUT DOWN #2 ENGINE. CONFIRMED PROP IN FULL FEATHER POSITION. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUIDE — MISSING (PAX DOOR) · airframe 22,628 hrs · 24,341 cycles

MCD MISSING RUBBER STOP/BUMPER FOR EXTERIOR HANDLE. REMOVED FROM SERVICE. REPLACED RUBBER BUMPER STOP AS REQUIRED. NO FURTHER ACTION REQUIRED. OPS CHECK GOOD. DOOR NOW OPEN AND CLOSES NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — OVERHEATED (LT MLG) · airframe 22,632 hrs · 24,345 cycles

DURING POST FLIGHT WALK AROUND, NOTICED SMOKE COMING FROM LEFT MAIN GEAR INBOARD TIRE. REMOVED FROM SERVICE. PERFORMED GVI OF BOTH WHEEL & BRAKE ASSY'S ON L/H MLG. NO SMOKE WAS OBSERVED COMING FROM WHEEL/BRAKE ASSY'S. CLEANED REMNANTS OF GREASE FROM THE #2 BRAKE ASSY. NO DEFECTS NOTED. A/C OK FOR SERVICE. PER MOM REQUEST, JACKED LMLG & CHECKED FOR ANY DEFECTS WITH BEARINGS. NONE FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 21,907 hrs · 23,613 cycles

EMERGENCY LIGHTING STRIP ON FLOOR JUST INSIDE MAIN CABIN DOOR LOOSE. REMOVED FROM SERVICE. RE-SECURED MCD ENTRANCE EMERGENCY LIGHTING STRIP FLOOR PATH REF AMM 33-51-16-400-801. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SHAFT SEAL — LEAKING (APU STARTER) · airframe 21,898 hrs · 23,601 cycles

AFTER APU START WHEN BLEED AIR WAS SELECTED ON, WHITE SMOKE NOTICED COMING FROM GASPERS IN FLIGHT COMPARTMENT.REF MCN 62172-01 ISSUE 2 PARA 2A-B 1A REPLACED APU STARTER SHAFT SEAL REF Q400 AMM TASK 24-33-01-000-801 AND 24-33-01-400-801. PERFORMED REMOVAL OF ODOR FROM AC DUCTS REF Q400 AMM TASK 21-00-00-160-801. LEAK CHECK GOOD AND NO ODOR NOTED. NOTE THAT THE APU STARTER SHAFT SEAL IS WHAT WAS REPLACED.

Part: CONTROL UNIT — INOPERATIVE (AC GENERATOR) · airframe 21,847 hrs · 23,554 cycles

ON DEPARTURE #2 AC GEN CAUTION ILLUMINATED. RAN CHECKLIST THE GEN DID NOT RESET. MONITORED THE LOAD ON ALL 3 PHASES OF THE #1 AC GEN. NO PHASE APPROACHED OVER LOAD. RETURNED TO FIELD. REMOVED FROM SERVICE. R&R AGCU #2. OPS CHECK GOOD. FAULT LIGHT EXTINGUISHED AND DID NOT RETURN. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 21,690 hrs · 23,412 cycles

PHOTO-LUMINESCENT STRIP NEAR SEAT 1B COMING LOOSE. REMOVED FROM SERVICE. CLEANED AND RE SECURED FLOOR PATH LIGHT STRIP AT 1B, IAW Q400 AMM 33-51-16-400-801. RETURNED TO SERVICE.

Part: STOP — MISSING (PAX DOOR) · airframe 20,811 hrs · 22,486 cycles

MAIN CABIN DOOR EXTERIOR HANDLE STOP GUIDE IS MISSING. REMOVED FROM SERVICE. INSTALLED NEW STOP GUIDE IAW Q400 AMM 52-11-11-400-801, PARA 4,I. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BUTTON — JAMMED (CABIN DOOR) · airframe 20,709 hrs · 22,374 cycles

RAMP REPORTED THAT WHEN TRYING TO PRESS THE MAIN CABIN DOOR RELEASE BUTTON (OUTSIDE OF AC) THAT THE BUTTON JAMS ON THE MCD LEVER. UNABLE TO OPEN FROM OUTSIDE. REMOVED FROM SERVICE PERFORMED OPS TEST OF THE MAIN CABIN DOOR IAW Q400 AMM 52-11-00-710-802. OPS TEST GOOD. NO FURTHER DEFECTS NOTED.E. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 20,452 hrs · 22,074 cycles

PHOTO LUMINESCENT STRIP COMING UP IN FWD CABIN. REMOVED FROM SERVICE. RESECURED PHOTO LUMINESCENT STRIP@FWD CABIN AREA. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 20,230 hrs · 21,805 cycles

FLOOR LEVEL LIGHTING STRIP AT MAIN CABIN DOOR LOOSE. REMOVED FROM SERVICE. RESECURED FLOOR LEVEL LIGHTING STRIP AT SEAT 1A/B. FUNCTIONS AS REQUIRED/ NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 19,977 hrs · 21,520 cycles

EMERG LIGHTING STRIP BY MAIN CABIN DOOR LOOSE. REMOVED FROM SERVICE. RESECURRED EMERG LIGHTING STRIP BY MCD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LANDING GEAR — SLOW (NOSE) · airframe 19,906 hrs · 21,433 cycles

ON FINAL AS FIRST OFFICER SELECTED GEAR DOWN, THE AMBER N.DOOR AND RED NOSE LIGHTS REMAINED ILLUMINATED FOR 12-15 SECONDS BEFORE THEY EXTINGUISHED AND THE GREEN NOSE LIGHT ILLUMINATED. NOSE GEAR LAGGED BEHIND MAIN GEAR EXTENSION BY 10 SECONDS. GEAR LOCKED DOWN BY 15 SECONDS AND LANDED WITHOUT ISSUE. AIRCRAFT REMOVED FROM SERVICE. FERRIED FOR REPAIRS. CURRENTLY OUT OF SERVICE FOR REPAIRS.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 19,893 hrs · 21,419 cycles

WHEN LANDING SELECTED DOWN, NOSE TOOK ABOUT 5 SECONDS LONGER TO EXTEND THAN NORMAL AND LOUD NOISE WHEN LOCKING DOWN. NORMAL INDICATION FOR LANDING. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED PSEU NO CURRENT FAULTS. CK'ED RIGGING AND INDUCTANCE VALUES FOR EACH PROX SENSOR ALL VALUES FOR EACH ARE WITHIN LIMITS. C/W A GVI OF NOSE GEAR NO DEFECTS FOUND. REPLACED NOSE GEAR DOOR SOLENOID SEQUENCE VALVE OPS CK GOOD. NO DEFECTS NOTED. OPERATIONAL CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG DOOR) · airframe 19,876 hrs · 21,400 cycles

AFTER GEAR WAS SELECTED DOWN, RECEIVED RED UNSAFE LIGHT ON NOSE W/AMBER N.DOOR LIGHT AFTER L AND R MAIN INDICATED DOWN AND LOCKED, ABOUT 15 SECONDS LATER NOSE GEAR EXTENDED AND LOCK, AND GREEN INDICATOR ILLUMINATED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED NLG DOOR ACTUATOR OPS CHECK GOOD OK FOR SERVICE.

Part: BUMPER — DETERIORATED (CABIN DOOR) · airframe 19,185 hrs · 20,557 cycles

VERY DIFFICULT TO GET MAIN CABIN DOOR HANDLE TO OPEN FROM OUTSIDE. REMOVED FROM SERVICE. FOUND EXTERNAL MCD HANDLE STOP DETERIORATED CAUSING HANDLE TO FOUL AGAINST COVER ON TOP. REPLACED RUBBER BUMPER - NO FURTHER DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — INOPERATIVE (LT MLG) · airframe 19,042 hrs · 20,372 cycles

LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION.ALTERNATE GEAR EXTENSION PERFORMED. AFTER LANDING LEFT MAIN GEAR LIGHT ILLUMINATED, AFTER PARKING AT THE GATE THE LIGHT EXTINGUISHED. LANDING WAS UNEVENTFUL. REMOVED FROM SERVICE.REMOVED AND REPLACED LANDING GEAR CONTROL PANEL AS A PRECAUTIONARY MEASURE. REMOVED PANEL IAW AMM TASK 32-31-01-000-801. INSTALLED IAW Q400 AMM TASK 32-31-01-400-801. TEST GOOD. DUE TO USE OF ALTERNATE EXTENSION C/W AMM 32-34-00-710-802 PAR 4A (12)-(17). RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,613 hrs · 19,859 cycles

A FEW SECONDS AFTER SELECTING APU BLEED AIR OPEN, CABIN DUCT HOT AND FLT COMPT DUCT HOT ILLUMINATED AND CABIN FILLED WITH VISIBLE SMOKE AND OIL SMELL. EMERGENCY SERVICES DISPATCHED AND PASSENGERS DEPLANNED THROUGH MAIN CABIN DOOR. REMOVED FROM SERVICE. OPERATED APU WITHOUT BLEED AIR, APU OPERATED NORMALLY. TURNED APU BLEED ON AND BOTH CABIN AND FLT DECK DUCT HOT CAUTION ILLUMINATED WITH A SLIGHT OIL SMELL IN THE CABIN. SHUTDOWN APU. RAN ENGINES AND SELECTED BLEEDS INDIVIDUALLY. NO CAUTION LIGHTS AND NO OVERHEAT CONDITIONS WITH EITHER #1 OR #2 BLEED SELECTED. ALSO, NO OIL SMELL NOTED. COULD NOT DUPLICATE WITH ENGINE BLEED AIR. SHUTDOWN ENGINES. ALSO, DURING ENGINE RUN, NOTICED CAB AND FLT DECK TEMPS COULD NOT BE CONTROLLED IN AUTO MODE. PLACED APU ON MEL. PLACED CABIN TEMP CONTROL (AUTO) ON MEL. PLACED FLIGHT DECK TEMP CONTROL (AUTO) ON MEL. RETURNED TO SERVICE.

Part: UNKNOWN — HAZE (CABIN & COCKPIT) · airframe 18,403 hrs · 19,600 cycles

AFTER TURNING ON APU BLEED AIR THE CABIN AND FLIGHT DECK FILLED WITH MIST / HAZE ( APU INOP ). REMOVED FROM SERVICE. PLACED ON MEL. RETURNED TO SERVICE.

Part: APU — ODOR · airframe 18,341 hrs · 19,523 cycles

DURING BOARDING APU SELECTED BL AIR, SMELT SMOKE, FLT COMP TEMP INCREASING, FLT COMPT PACK HOT MASTER CAUTION RAN EA CHECKLIST ( APU BLEED AIR SYSTEM INOP ). PLACED ON MEL. RETURNED TO SERVICE.

Part: POWER UNIT — MALFUNCTIONED (TE FLAP) · airframe 18,245 hrs · 19,411 cycles

FLAP POWER CAUTION AFTER SELECTING FLAPS 15 FLAPS REMAINED AT FLAPS 10, FLAPS CONT CIRCUIT BREAKER RESET AS PER FLAP POWER CAUTION CHECKLIST. PERFORMED 2ND BREAKER RESET AS PER MAINTENANCE WITH SAME RESULT. PERFORMED MISSED APPROACH THEN RETURNED TO FIELD. LANDING UNEVENTFUL. NORMAL BREAKING ACTION ON NO FLAP (0) LANDING. REMOVED FROM SERVICE. NO FAULTS IN CDS. C/W FIM 27-50-00-810-802. PERFORMED OPS TEST OF FLAPS SEVERAL TIMES IAW AMM 27-50-00-710-801. NO DEFECTS NOTED AT THIS TIME. REMOVED FPU IAW AMM 27-52-01-000-801 UP TO STEP 4A(1), TEMPORARILY REINSTALLED PANEL 262HT.-JK 24015 1/29/19. CONTINUED WITH FPU REMOVAL REF AMM 27-52-01-000-801 STEP 4A(2) TILL END AND INSTALLED NEW FPU REM AMM 27-52-01-400-801. RII STEPS C/W. OPS TEST GOOD. FLAP POWER CAUTION MESSAGE DID NOT RETURN. A/C RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 18,214 hrs · 19,374 cycles

ON CLIMBOUT OF KGEG THE LAVATORY SMOKE DETECTOR WENT OFF. F/A "A" INVESTIGATED AND THE LAV WAS UNOCCUPIED, NO SIGNS OF SMOKE, FIRE OR HEAT. NO ONE HAD VISITED THE LAV, NO SIGN OF ANY TAMPERING OR OTHER PRODUCTS LIKE HAIRSPRAY THAT COULD TRIGGER IT. F/A "A" TOUCHED THE SMOKE DETECTOR AND THE ALARM STOPPED. WE RAN THE LAVATORY SMOKE DETECTOR CHECKLIST TO COMPLETION AND MADE THE DECISION AS A CREW TO CONTINUE AFTER TALKING WITH MCC. REMOVED FROM SERVICE. REMOVED LAV SMOKE DETECTOR REF Q400 26-12-11-000-801. INSTALLED LAV SMOKE DETECTOR W/NEW FROM STOCK REF 26-12-11-400-802. OPS CHECK PASS. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 18,160 hrs · 19,308 cycles

PRIOR TO BOARDING THE SMOKE DETECTOR IN THE LAV STARTED GOING OFF. REMOVED FROM SERVICE. PERFORMED GVI, NO DEFECTS NOTED. PERFORMED OPS CHECK OF LAV SMOKE DETECTOR IAW MM 26-12-11-710-801. OPS CHECK GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 18,103 hrs · 19,239 cycles

WHEN AT CRUISE ALTITUDE THE CA WINSHIELD FROSTED OVER AND THE CB POPPED. REMOVED FROM SERVICE. R+R NR 1 ANTI-ICE CONTROLLER REF AMM 30-41-01-000-801/400-801. OPS CHECK GOOD. C/B REMAINS PUSHED IN. RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 18,102 hrs · 19,238 cycles

CA WINDSCREEN COMPLETELY FROSTED OVER ON APPROACH. NO CAUTION LIGHT ILLUMINATED. REMOVED FROM SERVICE. FOUND 115VAC CIRCUIT BREAKER "L WSHLD HT" OPEN. RESET BREAKER PER GM 9.2.2.1. PREFORMED OPS TEST OF PILOT WINDSHIELD ANTI-ICING SYSTEM IAW AMM 30-41-00-710-801. OPS TEST GOOD. BREAKER REMAINS SET. RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (NLG) · airframe 17,911 hrs · 19,017 cycles

NOSE WHEEL DOOR DID NOT CLOSE AFTER TAKE OFF. AMBER N DOOR LIGHT ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. SWUNG THE NOSE GEAR PER Q400 AMM TASK 32-31-00-867-802 15 TIMES, COULD NOT DUPLICATE. AS A PRECAUTIONARY MEASURE, REMOVED NLG DOOR SOLENOID SEQUENCE VALVE REF Q400 AMM 32-31-71-000-801, & INSTALLED SERVICEABLE SOLENOID SEQUENCE VALVE REF AMM 32-31-71-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (PAX DOOR) · airframe 17,762 hrs · 18,861 cycles

CRACK ON BEAM, BETWEEN FASTENERS, LOCATED ON AFT PASSENGER DOOR WHERE VENT DOOR STOP FITTING BRACKET ATTACHES. CARRIED OUT REMOVAL OF AFT PASS DOOR IAW AMM 52-12-00-000-801. INSTALLED NEW BEAM PN 85217419-105 ON AFT PAX DOOR IAW SRM 51-23-00-00-01, 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01 AND 51-42-15-02-01. REFERENCE WO 248435 NR-00485 FOR REINSTALL OF AFT PAX DOOR.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

AFT BAGGAGE FWD SHEAR WEB CORRODED BEYOND LIMITS. CORRODED AFT BAGGAGE, FWD SHEAR WEB REMOVED AND REPLACED WITH NEW PART IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 8 FROM FSX570.00-X670.00 IS CORRODED IN SEVERAL PLACES. REMOVED SEAT RAIL NR 8 FROM FSX570.00 TO FSX670.00 IAW SRM 51-40-15, 51-40-00 AND 51-42-05. INSTALLED SEAT RAIL NR 8 FROM FSX270.00 TO FSX670.00 IAW SRM 51-40-15, 51-41-00, AND 51-42-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 9 FROM FSX670.00-X782.00 IS CORRODED BEYOND LIMITS. SEAT RAIL NR 9 REPLACED IAW SRM 51-42-05, 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 7 FROM FSX228.50-X570.00 IS CORRODED. SEAT RAIL NR 7 REPLACED IAW SRM 51-40-15-02-01, 51-41-05-00-01 AND 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 15 FROM FSX612.00-X670.00 IS CORRODED. SEAT RAIL NR 15 FROM FSX612.00-FSX670 REMOVED IAW SRM 51-42-05, 51-40-15 AND 51-41-00. SEAT RAIL NR 15 FROM FSX612.00-FSX670 INSTALLED IAW SRM 51-42-05, 51-40-15 AND 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 14 FROM FSX570.00-X612.00 IS CORRODED. SEAT RAIL NR 14 REMOVED IAW SRM 51-42-05, 51-40-15. SEAT RAIL NR 14 INSTALLED IAW SRM 51-42-05, AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 2 FROM FSX229.50-X571.50 IS CORRODED IN SEVERAL PLACES. CORRODED SEAT RAIL NR 2 FROM FSX 229.50-FS X571.50 REMOVED AND REPLACED IAW SRM 51-42-05, 51-42-45, 51-41-15 AND 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 13 FROM FSX228.50-X570.00 IS CORRODED IN SEVERAL PLACES. CORRODED SEAT RAIL NR 13 FROM FSX 228.50- FS X270.00 REMOVED AND REPLACED IAW SRM 51-42-05, 51-42-45, 51-41-15 AND 51-40-15.

Part: RAIL — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

EQUIPMENT RAIL NR 23 FROM FSX670.00-X698.00 IS CORRODED BEYOND LIMITS AT FWD ANCHOR NUT ATTACHMENT. EQUIPMENT RAIL NR 23 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-05-00-01 AND 51-42-75-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 16 FROM FSX670.00-X782.00 IS CORRODED BEYOND LIMITS. SEAT RAIL NR 16 FROM FS670-FSX782 REMOVED IAW SRM 51-42-05, 51-40-15 AND 51-41-00. SEAT RAIL NR 16 FROM FSX670-FSX782 INSTALLED IAW SRM 51-42-05, 51-40-15 AND 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 18 FROM FSX102.50-X229.50 IS CORRODED IN SEVERAL PLACES. REPLACED SEAT RAIL NR 18 FROM FSX102.50-X229.50 IAW SRM 51-42-15-02-01, 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 1 FROM FSX32.40-X229.50 IS CORRODED IN SEVERAL PLACES. REMOVED SEAT RAIL NR 1 FROM FSX 32.40-FSX 229.50 IAW SRM 51-42-05, 51-40-15 AND 51-42-45. INSTALLED SEAT RAIL NR 1 FROM FSX 32.40-FSX 229.50 IAW SRM 51-42-05, 51-40-15 AND 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

SEAT RAIL NR 10 FROM FSX-39.00-X10.50 IS CORRODED. SEAT RAIL NR 10 REMOVED IAW SRM 51-42-05, 51-40-15. SEAT RAIL NR 10 REPLACED IAW SRM 53-20-49-02-04, 57-41-05-00-01, 51-42-05-02-01 AND 51-40-15-02-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 17,762 hrs · 18,861 cycles

LAV DOUBLER CORRODED. LAV DOUBLER REPLACED IAW SRM 51-42-05-02-01.

Part: CONTROL CABLE — OUT OF RIG (AILERON) · airframe 16,516 hrs · 17,495 cycles

AIRCRAFT REQUIRES SIGNIFICANT (EXCESSIVE) RIGHT AILERON TRIM (ALMOST 1 FULL TICK-MARK) AND RIGHT RUDDER TRIM TO FLY WINGS LEVEL TRIMMED ON CLIMB OUT AND CRUISE. REQUIRES 15 DEGREES RIGHT YOKE CONTROL TO LIFT OFF LEVEL ON TAKE OFF. ALL TRIM MUST BE REMOVED SLAVING BELOW 160 KTS ON AP0PROACH FOR TRIMMED LEVEL FLIGHT. REMOVED FROM SERVICE. SPOILER AND AILERON CABLE TENSION LOW. CABLE ADJUSTMENTS WERE PERFORMED FOR SPOILERS & AILERONS ON FUSELAGE & WINGS. REF FIM TASK 27-13-00-810-801 PARAGRAPH 1 THRU 4A (14). TEST FLIGHT GOOD. RETURNED TO SERVICE

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 16,340 hrs · 17,310 cycles

FLOOR EMERGENCY LIGHT STRIP NEXT TO MCD IS LOOSE. REMOVED FROM SERVICE. SECURED THE EMERGENCY LIGHT, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: NOT REPORTED — MALFUNCTIONED (NR 1 PROPELLER) · airframe 16,297 hrs · 17,265 cycles

NR 1 PROP FAILS TO MANUALLY UNFEATHER PER EC 612000202 STEP 2E (PROP MTX UNFEATHER(S) INOP). PLACED ON MEL 61-20-1. RETURNED TO SERVICE.

Part: LIGHT — DELAMINATED (CABIN) · airframe 1,960 hrs · 982 cycles

ROW 2 D/E FLOOR PATH LIGHTING STRIP DELAMINATED. REMOVED FROM SERVICE. REPLACED STRIP IAW AMM 33-51-16-000-801. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 15,779 hrs · 16,714 cycles

CLIMBING THRU 15,000 FT, THE NR 2 ENGINE SURGED FROM 87 TO 84 PERCENT TORQUE FOR A MOMENT. EVENT MARKER WAS PUSHED SHORTLY AFTER. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED NACELLE SHUTOFF VALVE IAW AMM 36-11-19-000-801, & 36-11-19-400-801. VALVE OPS CHECKED GOOD ON GROUND ENGINE RUN. NO TORQUE OSCILLATIONS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (PTU) · airframe 15,719 hrs · 16,648 cycles

PTU CONTROL FAIL ADVISORY LIGHT ILLUMINATED AFTER TAKEOFF, EVERYTHING FUNCTIONED NORMALLY. RETURNED TO FIELD. LANDING UNEVENTFUL. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL TEST OF PTU IAW AMM 29-11-61-710-801, COMPLIED WITH F/C IAW AMM 29-11-61-720-801, NO DEFECTS WERE NOTED. NO HISTORY 90 DAYS. COMPLIED WITH VISUAL INSPECTION OF PTU COMPONENTS, AND WIRING, FOUND BACKSHELL LOOSE ON PTU PRESSURE SWITCH. SECURED THE CONNECTOR BACKSHELL AND REPLACED PTU PRESSURE SWITCH IAW AMM 29-30-11-000-801. OPS AND TESTED. LEAK CHECKED. SYSTEM OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 15,676 hrs · 16,603 cycles

NR 2 FEATHER PUMP FAILS OPERATIONAL CHECK AFTER PCU CHANGE. REPLACED FEATHERING PUMP. CHECKS GOOD.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 15,648 hrs · 16,579 cycles

WHILE CLIMBING THROUGH 13000 FT, THE NR 2 ENGINE SURGED ONCE WITH A 3 TO 5 PERCENT TORQUE FLUCTUATION AND A NOTICEABLE YAW AND SOUND CHANGE. REMOVED FROM SERVICE. ACCOMP T/C 73000Q01. NO FAULT CODES POSTED. ACCOMPLISHED A GVI ON THE NR 2 ENGINE. NO OBVIOUS DEFECTS. R & R THE NR 2 FADEC IAW 73-21-01-000/400-801. OPS TESTE GOOD IAW 71-00-00-868-805 APPLIED SECTIONS. NO FAULT CODES REPOSTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 14,952 hrs · 15,825 cycles

EMERGENCY LIGHT BY FWD GALLEY CUPBOARD COMING UP. SECURED THE LIGHT. RETURNED TO SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 14,689 hrs · 15,544 cycles

DURING APPROACH, GEAR DOWN LANDING CHECKLIST, GEAR CAME DOWN, THREE GREEN WITH THREE AMBER LIGHTS WHICH REMAINED ON NO OTHER LIGHTS ASSSOCIATED. REPLACED THE LANDING GEAR SELECTOR VALVE, FUNCTIONAL AND LEAK CHECKED. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 12,637 hrs · 13,367 cycles

AFT CARGO DOOR WARNING ON CLIMB OUT. RETURNED TO FIELD. LANDING UNEVENTFUL. C/W INSPECTION OF THE AFT BAGGAGE DOOR HANDLE LOCK MECHANISM IAW HS 52-0028 AND HS 52-0032, NO DEFECTS NOTED. C/W OPERATIONAL TEST OF THE AFT BAGGAGE DOOR IAW AMM TASK 52-31-00-710-801. OPS TEST GOOD. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 12,350 hrs · 13,037 cycles

AT 10,000 FT FUSELAGE DOOR WARNING LIGHT. AFT CARGO DOOR SHOWED UNSAFE IN MFD. RETURN TO FIELD. LANDING UNEVENTFUL. AFTER LANDING AFT BAGGAGE COMPARTMENT DOOR EXTENDED IN HORIZONTAL POSITION. PERMORMED OPERATIONAL TEST OF AFT BAGGAGE DOOR IAW AMM TASK 52-31-00-710-801. NO DEFECTS NOTED. ALSO C/W HS 52-0028 AND HS 52-0032. RETURNED TO SERVICE.

Part: SEAT TRACK — NOT REPORTED (ZONE 100) · airframe 11,911 hrs · 12,590 cycles

SEAT TRACK NR 11 REQUIRES REPLACEMENT, PN 85328210-115. REMOVED DRIP ANGLE COMMON TO SEAT TRACK NR 10 AND SEAT TRACK NR 11, REF SRM 51-42-05. INSTALLED DRIP ANGLE COMMON TO SEAT TRACK NR 10 AND NR 11 REF SRM 51-42-05. REMOVED FASTENERS IN TOP SIDE OF SPLICE FOR SEAT TRACK 10 AND 11 REF SRM 51-40-15-02-01. INSTALLED FASTENERS IN TOP SIDE OF SPLICE COMMON TO SEAT TRACK 10 AND 11, REF SRM 51-40-15, REPAIR-01. REMOVED 10 BOLTS EA FROM SEAT TRACK NR 11 SUPPORTS, REF SRM 51-41-00. INSTALLED 10 BOLTS ON SEAT TRACK NR 11 SUPPORTS, REF SRM 51-41-00. REMOVED AFT SPLICE COMMON TO SEAT TRACK NR 11 AND NR 12 REF SRM 51-42-05 AND SRM 51-40-15. INSTALLED SPLICE COMMON TO SEAT TRACK 11 AND 12 REF SRM 51-42-05, REPAIR-01. REMOVED 7 EA STAND OFFS FROM SEAT TRACK NR 11 REF SRM 51-42-05. INSTALLED 7 WIRE STAND OFFS ON SEAT TRACK NR 11 REF SRM 51-42-05. REMOVED SEAT TRACK NR 11 FOR REPLACEMENT, REF SRM 51-42-05, 51-4015 AND SRM 51-41-00. INSTALLED SEAT TRACK NR 11 REPLACEMENT, PN 85328210-115, REF SRM 51-42-05, 51-40-15, 51-41-00 DWG 85328201. LOCATED AND DRILLED SEAT TRACK NR 11 REF SRM 51-40-07, DWG 85328201. LOCATED AND DRILLED FWD SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11 REF SRM 51-40-07, DWG 85328201.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 11,911 hrs · 12,590 cycles

SEAT TRACK NR 7 REQUIRES REPLACEMENT, REMOVED SEAT TRACK IAW SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, 51-41-05, DWG 85361501. .

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 11,911 hrs · 12,590 cycles

SEAT TRACK NR 8 FOUND OUT OF LIMITS, PN 85338210-109. REMOVED SEAT TRACK NR 8, PN 85338210-109, REF SRM 51-42-050201, 51-40-07-02-01, 51-40-15-02-01. INSTALLED SEAT TRACK NR 8, PN 85338210-109, REF SRM 51-42-05-02-01, 51-41-00-00-01 AND DWG 85338201, REV E. LOCATED AND DRILLED SEAT TRACK NR 8, PN 8533210-109, REF SRM 51-40-07. COUNTERSINK REMAINING HOLES IN SEAT TRACK, REF SRM 51-40-07, PN 85338210-109, SEAT TRACK NR 8. COMPLETED COUNTERSINK IN SEAT TRACK NR 8, REF SRM 51-40-15-02-01. REMOVED SPLICE MEMBERS COMMON TO SEAT TRACKS 8 AND 9 REF SRM 51-40-15, 51-42-05. INSTALLED SPLICE MEMBERS COMMON TO SEAT TRACK NR 8 AND NR 9 REF SRM 51-42-05-02-01, 51-40-15-02-01 AND DWG 85338210, REV E. RESTORED FINISH REF SRM 51-25-15, 51-25-10.

Part: SEAT TRACK — NOT REPORTED (ZONE 100) · airframe 11,911 hrs · 12,590 cycles

SEAT TRACK NR 10 REQUIRES REPLACEMENT. REMOVED 10 EA FASTENERS INBD SIDE OF SPLICE COMMON TO TRACK 10 & 11 IAW SRM 51-40-15, REPAIR -01. REMOVED 4 EA BOLTS ATTACHING TO TRACK NR 10 IAW SRM 51-41-00 STRUCT IDENT -01, BS -5 TO 10.5. REMOVED 9EA WIRE BUNDLE CABLE TIES COMMON TO TRACK 10 REF WM 20-12-10. REMOVED SPLICE COMMON TO SEAT TRACK NR 10 AND NR 11, REF SRM 51-42-05, REPAIR 01. INSTALLED 4 EA BOLTS ATTACHING "X" MEMBERS TO SEAT TRACK NR 10, REF SRM 51-41-00, STRUCT IDENT -01. INSTALLED WIRE BUNDLE CABLES, 9 EA TO TRACK NR 10, REF SRM 51-41-00 STRUCT IDENT -01. REMOVED GROUND STUD COMMON TO TRACK 10 AT BS 17, REF SRM 51-41-00 STRUCT IDENT -01. INSTALLED GROUND STUD COMMON TO TRACK NR 10 REF SRM 51-41-00 STRUCT IDENT 01. REMOVED WIRE BUNDLE ATTACHMENT CLIP COMMON TO SPLICE FOR TRACK 10 AND 11, REF SRM 51-40-15, REPAIR -01. INSTALLED WIRE BUNDLE SUPPORT COMMON TO SEAT TRACK NR 10 & NR 11, REF SRM 51-42-05. REMOVED INBD SPLICE COMMON TO SEAT TRACK NR 10 & NR 11, REF SRM 51-42-05. INSTALLED INBD SPLICE COMMON TO SEAT TRACK 10 & 11, REF SRM 51-42-05, REPAIR -01. REMOVED OTBD SPLICE COMMON TO SEAT TRACK NR 10 & NR 11, REF SRM 51-42-05. INSTALLED OTBD SPLICE COMMON TO SEAT TRACK 10 & 11 REF SRM 51-40-15, REPAIR 01. REMOVED SEAT TRACK NR 10 REF SRM 51-42-05. DRILLED LOCATED AND INSTALLED NEW SEAT TRACK, PN 85328210-121, REF SRM 51-42-05 AND SRM 51-40-15, REPAIR 01. PERFORMED BONDING CHECK REF AMM 51-80-00, PG 299.306 & PG 299.307. BOND CHECK GOOD. RESTORED FINISH ON SEAT TRACK NR 10 & NR 11, REF SRM 51-25-25, 51-25-10.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 11,008 hrs · 11,642 cycles

ENROUTE THE MESSAGE "CHECKED" SHOWED ON THE ED & NR 2 MFD A, "CHECK PFD2" SHOWED ON THE NR 2 MFD & NR 2 PFD. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND ED/PFD2 MISMATCH IN LAST LEG FAULTS. C/W FIM TASK 31-61-01-810-807. PERFORMED OPS TEST OF MFD2, PFD2, AND ED, REF MAINTENANCE 6316101, MAINTENANCE 6316104, AND AMM 31-61-01-710-803. REMOVED ED FOR INSPECTION OF ELECTRICAL CONNECTORS AND COOLING DUCTS. NO DEFECTS NOTED. INSTALLED ED REF AMM TASK 31-61-11-000-801 AND 31-61-11-400-801. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 9,806 hrs · 10,366 cycles

ON TAKEOFF ROLL, AUTOFEATHER ARM MESSAGE DID NOT APPEAR AS POWER LEVERS WERE ADVANCED INTO THE RATING DETENT. TAKEOFF ABORT PERFORMED ABOUT 65 KTS. INTERROGATED CDS/EMU FOR PROP & POWERPLANT FAULTS.NO FAULTS NO FAULTS RECORDED PERFORM OPS TEST OF PROPELLER AUTOFEATHER/UPTRIM SYS IAW AMM TASK 61-20-00-710-801. TEST PASSED SATISFACTORY. OPS CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: PROPELLER — OUT OF BALANCE (ZONE 400) · airframe 9,721 hrs · 10,282 cycles

VIBRATION IN BOTH CONTROL YOKES STARTING AROUND 200 KTS INCREASING IN INTENSITY THRU 220 KTS SLOW TO BELOW 200 KTS. RETURNED TO FIELD LANDING UNEVENTFUL. TENSIONED AILERON CABLES, REPLACED WORN BUSHINGS IN RT INBD AND OTBD SPOILER LINKAGES, REPLACED NR 1 PROPELLER DUE TO OUT OF BALANCE. RETURNED TO SERVICE.

Part: STIFFENER — CRACKED · airframe 9,634 hrs · 10,184 cycles

FOUND CRACKED STIFFENER ON LT COWL PANEL 414AR. R & R THE STIFFENER IAW SRM 51-42-05, REPAIR-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 9,634 hrs · 10,184 cycles

EVIDENCE OF CORROSION FOUND ON ANGLE AIRSTAIR DOOR X6.700, STR 25. REMOVED AIRSTAIR DOOR ANGLE IAW SRM 54-42-05. INSTALLED AIRSTAIR DOOR ANGLE IAW SRM 51-42-05-02-01, STEP 4D(3-10).

Part: THRESHOLD — CORRODED · airframe 9,634 hrs · 10,184 cycles

THRESHOLD CHANNEL ON THE MCD IS CORRODED AROUND SEVERAL FASTENER HOLES. LOCATED AND DRILLED FASTENER HOLES ON NEW THRESHOLD CHANNEL. REF: SRM 51-40-07-02-01. INSTALLED THRESHOLD CHANNEL IAW SRM 51-42-05-02-01, STEP YD(3-10).

Part: ANGLE — CORRODED (FUSELAGE) · airframe 9,634 hrs · 10,184 cycles

EVIDENCE OF CORROSION FOUND ON ANGLE AIRSTAIR SURROUNDAT X6.700, STR 25. REMOVED AIRSTAIR SURROUND ANGLE IAW SRM 51-42-05 AND 51-40-15. INSTALLED AIR STAIR SURROUNDED ANGLE IAW SRM 51-42-05-02-01, STEP 4D (3-10) AND SRM 51-40-15-02-01 STEP 6, NR 2.

Part: PROBE — MALFUNCTIONED (FUEL) · airframe 9,540 hrs · 10,078 cycles

FUEL QUANTITY INDICATION ON RT WING TANK FLUCTUATED WHILE ENROUTE, SHOWING UP TO 2000 LBS LESS THAN THE LT WING TANK. ON DESCENT, RT TANK INDICATIONS JUMPED BACK TO NORMAL BALANCE LIMITS AFTER A BRIEF CROSS-FLOW OF 1-2 MINUTES. AT GATE AFTER SHUTDOWN, RT WING TANK INDICATOR SHOWS DASHES. REPLACED WING FUEL QUANTITY PROBE NR 6 AND NR 7 REF TO AMM TASK 28-40-31-000-801AND TASK 28-40-31-400-801 STEPS 1 THROUGH 5B. PERFORMED FUNCTIONAL TEST, CAPAITANCE, OF THE RT NR 6 AND 7 PROBES IAW AMM TASK 28-40-31-720-801 PARA 4 AND FOUND THEM TO BE WITHIN NORMAL RANGE. CLEARED FAULT CODE & DID NOT RETURN. NO FLUCTUATION NOTED. RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE · airframe 9,293 hrs · 9,810 cycles

AFT EMERGENCY EQUIPMENT BIN DOES NOT OPEN SMOOTHLY. CLEANED AND LUBED AFT LT EMEGENCY EQUIPMENT SLIDING DOOR. DOOR SLIDES NORMALLY. NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,289 hrs · 9,803 cycles

FORWARD F/A REPORTED SMELLING A BURNED RUBBER ODOR IN THE CABIN AROUND ROW 5. THIS WAS CONFIRMED BY MULTIPLE PASSENGERS AROUND ROW 5. COMPLETED FORM M-744, AIR CONTAMINATION, ODORS/SMELLS CHECKLIST, COMPLIED WITH MCN NR 62172-01 ISSUE NR 2, PARA 1.A.3, NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH FLIGHT CREW, AND OPERATED BLEED AIR/AIR CONDITIONING, NO DEFECT NOTED. PERFORMED GVI OF CABIN CEILING/SIDEWALL LIGHTS, PSU'S AND OVERHEAD BINS, NO DEFECTS NOTED. CONFIRMED WITH MAINTENANCE CONTROL NO PREVIOUS HISTORY WITHIN THE LAST 200 DAYS FOR ATA CHAPTERS 21, 24, 33, 36, 49. ACFT OK FOR CONTINUED SERVICE.

Part: WINDOW — LOOSE (COCKPIT) · airframe 9,013 hrs · 9,492 cycles

CRACKLNG NOISE DURING CLIMB AND DESCENT. NOISE APPEARED TO BE COMING FROM OVERHEAD AREA IN THE FLIGHT DECK. COMPLIED WITH GVI OF WINDSHIELD'S AND SIDE WINDOWS, NO DEFECTS NOTED. RETORQUE SIDE WINDOWS AND WINDSHIELDS IAW AMM 56-10-06, TASK 56-10-06-400-801 AND 56-10-01 TASK 56-10-01-400-801. FOUND RT SIDE WINDOW WITH SEVERAL LOOSE SCREWS LOWER ROW AND FOUND LT SIDE WINDOW WITH SEVERAL LOOSE SCREWS UPPER ROW. PRESURIZED ACFT AND NO NOISES ON FLIGHT DECK AT THIS TIME. RETURNED TO SERVICE.

Part: HINGE — LOOSE (ZONE 800) · airframe 8,712 hrs · 9,182 cycles

MAIN CABIN DOOR AFT HINGE ATTACH POINT IS LOOSE AT THE PIVOT POINT. REPLACED THE MAIN CABIN DOOR LAYSHAFT. OPS TESTS GOOD.

Part: BRAKE — SMOKE (ZONE 700) · airframe 8,613 hrs · 9,072 cycles

LEFT MAIN INBD BRAKE IS GIVING OFF A WHITE SMOKE AFTER LANDING, NORMAL BRAKING WAS USED. REMOVED NR 2 TIRE AND BRAKE ASSY FOUND EXCESSIVE GREASE BUILD UP ON BRAKE INNER HOUSING, INSTALLED SERVICABLE NR 2 TIRE AND BRAKE AS PRECAUTION IAW TC 6324101, 6324201 ACFT OK FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (SWITCH PANEL) · airframe 8,400 hrs · 8,825 cycles

FORWARD EMERGENCY LIGHT ON & OFF SWITCH INDICATOR LIGHT INOPERATIVE. FOUND BULBS BURNED OUT, SWITCH OPERATES NORMAL. REPLACED BURNED OUT BULBS AND OPERATES NORMAL ACFT OK FOR SERVICE.

Part: BRACKET — BROKEN (EMERGENCY EXIT) · airframe 7,537 hrs · 7,887 cycles

EMERGENCY EXIT DOOR DITCHING DAM HANDLE ACCESS DOOR BRACKET BROKEN. SECURED BRACKET TO DITCHING DAM HANDLE COVER ON THE EMERGENCY DOOR. RETURNED TO SERVICE.

Part: CONTROL PANEL — FAILED (RUDDER TRIM) · airframe 7,359 hrs · 7,688 cycles

AFTER TAKEOFF, THE RUDDER TRIM KNOB LOST ITS SPRING BACK TO CENTER ABILITY. RUDDER TRIM STILL WORKED FINE, BUT KNOB WOULD NOT RETURN TO 12 O'CLOCK WHEN RELEASED. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R AILERON/RUDDER TRIM CONTROL-PANEL IAW AMM TASK 27-13-16-000-801. PERFORMED OPS TEST OF THE RUDDER TRIM SYSTEM IAW AMM TASK 27-22-00-710-801. OPS TEST GOOD. PERFORMED OPS TEST OF THE AILERON TRIM SYS IAW AMM TASK 27-13-00-710-802. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LINKAGE — BROKEN (FLAP HANDLE) · airframe 7,189 hrs · 7,510 cycles

FLAP CONTROL HANDLE TRIGGER LINKAGE BROKEN. FLAP POWER CAUTION LIGHT ILLUMINATED. RETURNED TO FIELD, LANDING UNEVENTFUL. PERFORMED GVI AND FOUND FLAP LEVER TRIGGER GROMMET JAMMED INTERROGATED CDS FOUND HYDRAULIC PRESSURE LOSS IN CURRENT FAULTS REPLACED FLAP CONTROL MODULE IAW AMM TASK 27-51-06-000-801 AND 27-51-06-400-801. OPS TEST GOOD NO FURTHER DEFECTS NOTED C/W FIM TASK 27-50-00-810-802 OPS TEST GOOD CAUTION DID NOT RETURN NO FURTHER FAULTS NOTED IN CDS. RETURNED TO SERVICE.

Part: STARTER GEN — FAILED (NR 1 ENGINE) · airframe 6,338 hrs · 6,605 cycles

AFTER STARTING NR 1 ENGINE SELECT START SWITCH DID NOT DISENGAGE WITH START LIGHT REMAINING ILLUMINATED. STARTER/GENERATOR FAILED. SMOKE FROM COWL. RETURNED TO GATE. INTERROGATED EPCU. NO FAULTS. FOUND NR 1 STARTER GEN BURNED OUT. R & R NR 1 STARTER GEN IAW MX 6243101. DUE TO ACFT HISTORY AND IAW FIM TASK 80-00-00-810-803. R & R K1 AND K2 IAW AMM TASKS 24-31-31-000-801 AND 24-31-31-400-801. R & R ESC PANEL IAW AMM TASKS 80-00-01-000-801 AND 80-00-01-400-801. R & R NR 1 GCU IAW AMM TASKS 24-31-06-000-801 AND 24-31-06-400-801. ALL OPS TESTS GOOD. SET CLOCKS IAW AMM TASK 31-21-01-820-801. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: GUARD — BROKEN (EMERGENCY LIGHT) · airframe 5,525 hrs · 5,754 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH GUARD BROKEN. REPLACED GUARD IAW AMM 33-51-05-400-801. RETURNED TO SERVICE.

Part: BEARING — CORRODED (SERVICE DOOR) · airframe 5,294 hrs · 5,491 cycles

GROUND CREW AND F/A'S REPORT THAT THE AFT SERVICE DOOR CANNOT BE OPENED. INVESTIGATION FOUND FWD AND AFT LIFT AND LATCH TORQUE TUBE SUPPORT BEARINGS CORRODED. REPLACED BEARINGS, AND PERFORMED LIFT AND LATCH MECHANISM RIGGING. C/W FUNCTIONAL TEST OF THE AFT SERVICE DOOR IAW AMM TASK 52-41-00-720-801. FUNCTIONAL TEST GOOD.RETURNED TO SERVICE.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP DE ICE) · airframe 5,114 hrs · 5,276 cycles

AFTER SELECTING PROP DE-ICE GOT MASTER CAUTION: BOTH NR 1 & NR 2 AC GEN CAUTIONS (AND ASSOCIATED LIGHTS). AC GEN CHECKLIST COMPLIED WITH BOTH GENS RESET & AC CAUTION LIGHTS EXTINGUISHED. DID NOT HAVE OPPORTUNITY TO USE PROP DE-ICE A SECOND TIME. R & R NR 1 BRUSH BLOCK ASSY IAW AMM TASK 30-61-00-000-801/400-801, R & R NR 1 TMCU IAW AMM TASK 30-61-06-000-801/400-801, R+R ISOLATOR CONTACTOR 3061-K1 IAW AMM TASK 30-61-16-000-802/400-802. PERFORMED AN OPS TEST OF THE AC VARIABLE FREQUENCY GENERATION SYS IAW AMM TASK 24-21-00-710-801. ALL TESTED GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: DOOR — DAMAGED (MLG) · airframe 4,749 hrs · 4,905 cycles

FOUND ON PREFLIGHT DAMAGE TO BOTH AFT MLG DOORS NR 1 SIDE. REPLACED MLG DOORS IAW EA 6-32-445 QX, DAMAGE TO THE GEAR DOORS AS RESULT OF TIMING OF GEAR HANDLE MOVEMENT, ALL REQUIRED MX ACTIONS ARE COMPLETE, ACFT IS AUTHORIZED FOR RETURN TO REVENUE SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (PROP DEICE) · airframe 4,647 hrs · 4,801 cycles

PROP DE-ICE CAUTION LIGHT. SELECTED OFF & CAUTION LIGHT EXTINGUISED, SELECTED BACK ON AND PROP ADVISORY LIGHTS NEVER RE-ILLUMINATED. DIVERTED AND ACCOMPLISHED AN UNEVENTFUL LANDING. INTERROGATED CDS, NO FAULTS. CW FIM TASK 30-60-00-810-807. CW ELECTRICAL CONTINUITY CHECK OF NR 1 & NR 2 PROP DEICING HEATER ELEMENTS IAW AMM 30-61-00-760-801. NO DEFECTS. CW GVI OF BOTH NR 1 & NR 2 PROP DE-ICE LEADS & BRUSH BLOCKS. NO DEFECTS. CW FUNCTIONAL TEST OF THE PROP DE-ICE SYS IAW AMM 30-61-00-720-801. TEST PASS. IAW MAINT CONTROL. R & R NR 1 TMCU. REPLACED NR1 TMCU IAW AMM TASK 30-61-06-000-801 AND AMM TASK 30-61-06-400-801. CW CALIBRATION PROCEDURE FOR THE TMCU IAW AMM 30-61-06-820-801. NO DEFECTS NOTED. OK FOR CONTINUED SERVICE. REPLACED AS A PRECAUTIONARY MEASURE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 4,832 hrs · 4,538 cycles

F/A REPORTS FWD F/A SEAT EMERGENCY LIGHT SWITCH LIGHT INOPERATIVE. FOUND "NORMAL" PORTION OF EMERGENCY SWITCH LIGHT ADJACENT TO FWD F/A SEAT TO BE INOPERATIVE. LAMPED "NORMAL" PORTION OF SWITCH LIGHT. OPS CHECKED GOOD. EMERGENCY LIGHT ILLUMINATED PROPERLY AS WELL AS NORMAL PORTION. PERFORMED OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM TASK 33-51-00-710-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 4,167 hrs · 4,319 cycles

FORWARD EMERGENCY LIGHT SWITCH GUARD BROKEN. REPLACED SWITCH GUARD.

Part: SCREW — LOOSE (CABIN) · airframe 3,953 hrs · 4,102 cycles

PASSENGERS TRIPPING IN A LOOSE SCREW IN THE PASSENGER AISLE CARPET. REPLACED THE MISSING SCREW WITH A NEW SCREW. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PTU — FAILED (TE FLAPS) · airframe 3,916 hrs · 4,057 cycles

AFTER LANDING F/A NOTED SMOKE COMING FROM RT SIDE OF ACFT, HYD FLUID ALSO NOTED COMING FROM RT SIDE OF ACFT, ALSO NOTED PTU WAS STILL OPERATING WITH FLAPS AT 0. REPLACED PTU. FOUND PTU SHAFT SHEARED. LEAK COMING FROM PTU. R & R IAW AMM TASK 29-11-61-000-801, AND 29-11-61-400-80.1. PERFORMED SIMPLIFIED FLUSH OF NR 2 HYD SYS IAW TASK 29-10-00-617-803. SUB TASK 29-10-00-170-136 PARA D. OPS AND LEAKS ARE GOOD. NO FURTHER DEFECT NOTED. DEFERRED FULL SYS FLUSH. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 3,612 hrs · 3,731 cycles

FLOOR GLOWSTRIP NEAR FWD CABIN DOOR LOOSE. SECURED GLOW STRIP NEAR FWD CABIN DOOR , NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: UPLOCK — DIRTY (DOOR) · airframe 3,083 hrs · 3,199 cycles

DITCHING DAM DOOR KNOCKED DOWN BY PASSENGER WILL NOT SECURE IN PLACE. CLEANED UPLOCKS OF LINT/DEBRIS. PERFORMED OPS CHECK OF THE AIRSTAIR DOOR EMERGENCY DITCHING DAM IAW Q400 AMM TASK 25-62-01-710-801. OPS CHECKS GOOD. OPERATED SEVERAL TIMES AND DAM STAYED SECURE EVERY TIME. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: RELAY — BURNED (WINDSHEILD HEAT) · airframe 2,728 hrs · 2,842 cycles

WITH WINDSHIELD HEAT IN NORM, OUTSIDE AIR TEMP -7C, "WSHLD HOT" CAUTION ILLUMINATED IAW CHECKLIST, WINDSHIELD HEAT WAS PLACED IN "WARM UP" MODE. ABOUT 15 MIN LATER, "WINDSHIELD HOT" CAUTION ILLUMINATED AGAIN WITH OUTSIDE AIR TEMP +2C. DIVERTED FOR REPAIRS. C/W FIM TASK 30-40-00-810-801. NO FAULTS FOUND IN CDS. C/W OPS TEST IAW AMM 30-41-00-710-801/-802. UNABLE TO DUPLICATE DISCREPANCY. C/W RESISTANCE CHECK OF BOTH WINDSHIELDS IAW AMM 30-41-00-760-801. NO DEFECTS NOTED. INSPECTED CONTACTS ON RELAYS 3041-K1, K2, K3 AND K4. NO DEFECTS NOTED ON 3041-K2 AND K4. FOUND BURNT CONTACTS ON 3041-K1 AND K3. R & R 3041-K1 AND K3 IAW AMM 30-41-01-000-802/400-802. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. NO CDS FAULTS AFTER OPS CHECK. RETURNED TO SERVICE.

Part: HANDLE — BINDING (PAX DOOR) · airframe 1,229 hrs · 1,312 cycles

INSIDE HANDLE IS DIFFICULT TO MOVE TO THE OPEN POSITION. LUBRICATED AIRSTAIR DOOR IAW AMM TASK 52-11-00-640-801, AND C/W FUNCTIONAL CHECK OF THE AIRSTAIR DOOR IAW AMM TASK 52-11-00-720-802. HANDLE LOAD WAS 37 LBF FUCTIONAL CHECK PASSED. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DITCHING DAM — UNWANTED DEPLOY (PAX DOOR) · airframe 941 hrs · 995 cycles

MAIN CABIN DOOR DITCHING DAM DEPLOYED DURING PASSENGER BOARDING. RESTOWED MAIN CABIN DOOR DITCHING DAM. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: TRACK — LACK OF LUBE (PAX DOOR) · airframe 705 hrs · 744 cycles

F/A ADVISED THAT THE MAIN CABIN DOOR WILL OPEN, BUT IT DOES NOT LOWER EASY. CLEANED AND LUBED THE DOOR TRACKS. CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — BINDING (MAIN PAX) · airframe 111 hrs · 100 cycles

F/A ADVISED VERY DIFFICULT TO OPEN. DOOR "POPS" TO INITIAL POSITION OK BUT TO CONTINUE TO OPEN BEYOND THAT POINT WAS NOT POSSIBLE WITHOUT EXTERNAL ASSISTANCE. PERFORMED OPS TEST IAW AMM TASKS 52-11-00-710-802. NO DEFECTS NOTED. COULD NOT DUPLICATE. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 89 hrs · 78 cycles

F/A REPORTS "MAIN CABIN DOOR" DIFFICULT TO OPEN UP. PERFORMED OPS TEST OF IAW AMM 52-11-00-710-802. OPS TEST PASS. HAD NO DIFFICULTY OPENING OR CLOSING DOOR FROM INSIDE OR OUTSIDE. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.