N438QX

Part: NONE — NONE · airframe 27,134 hrs · 29,259 cycles

PROP DEICE CAUTION CAME ON RAN CHECKLIST IN EA. CAUTION WAS OUT THEN CAME BACK ON A FEW MINUTES LATER. ( PROP DEICE SYSTEM INOP ).

Part: SEAL — NONE (#2 ENGINE) · airframe 26,754 hrs · 28,870 cycles

#2 ENGINE SLOW TO COME OUT OF FEATHER. REMOVED FROM SERVICE. HAD CREW ENGINES #1 & #2. PERFORMED FUNCTIONAL TEST OF PROP TIME TO UNFEATHER IAW Q400 AMM TASK 61-20-00-720-802. ENGINE #1 WITHIN LIMIT. ENGINE #2 OUT OF LIMIT TAKING APPROX 45 SECONDS. FAILING FUNCTIONAL TEST. REPLACEMENT OF THE #2 PROP PISTON SEALS. ALL OPS CHECKS GOOD. TIME TO UNFEATHER NOW WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (#2 ENGINE) · airframe 26,742 hrs · 28,856 cycles

AFTER START UP, WHEN CONDITION LEVERS WERE ADVANCED FROM START & FEATHER, #2 ENGINE TOOK APPROX. 1 MIN TO COME OUT OF FEATHER. REMOVED FROM SERVICE. R&R #2 ENGINE OSG, OPS TESTS NORMAL. LEAK CHECK NORMAL. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN CABIN) · airframe 26,499 hrs · 28,608 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED FROM SERVICE. PERFORMED OPS TEST OF MAIN CABIN FWD PASSENGER DOOR IN REF WITH Q400 AMM TASK 51-11-00-710-802. ALSO OPENED AND CLOSED IT SEVERAL TIMES . NO ISSUES WAS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 26,226 hrs · 28,340 cycles

EMERGENCY EXIT SIGN IN AFT GALLEY NOT SECURE. REMOVED FROM SERVICE. RESECURE EMERGENCY EXIT SIGN AFT GALLEY NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PEC — MALFUNCTIONED (NR 2 PROPELLER) · airframe 26,177 hrs · 28,290 cycles

ON ENGINE START,PROPS BROUGHT OUT OF START/ FEATHER, #2 PROP TOOK OVER 50 SECONDS TO INCREASE TO THE GREEN ARC. REMOVED FROM SERVICE. TROUBLESHOOT CDS FOUND CODE 65, PERFORMED #2 ENGINE RUN OPS TEST FAILED TO FEATHER IAW Q400 FIM 61-20-02-810-834. C/W GREASE CK IAW Q400 AMM 61-10-00-640-801. REPLACED OVERSPEED GOVERNOR IAW Q400 AMM 61-20-26-000-801/400-801. PERFORMED OPS TEST, TEST GOOD IAW Q400 AMM 61-20-00-710-803 AND A FUNCTIONAL TEST IAW Q400 AMM 61-20-00-720-802 AND 61-20-00-710-803. FAULT CODE 64 NO LONGER PRESENT, RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,997 hrs · 28,108 cycles

FA FORWARD EMERGENCY LIGHT SWITCH, LIGHT NOT ILLUMINATED. REMOVED FROM SERVICE. RELAMPED FA FORWARD EMERGENCY LIGHT SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — SPARKS (GALLEY) · airframe 25,983 hrs · 28,094 cycles

CLIMBING THRU 10000' F/A REPORTED SPARKS COMING OUT OF AFT GALLEY PANEL; LEFT CENTER AND RIGHT CB'S OF "LIQUID WARMERS" AND AREA ENCOMPASSING SWITCHES OVER MAPCO "SUPER HOT" AS A PRECAUTION, F/A TURNED OFF ALL SWITCHES. AREA REMAINED HOT. NO VISIBLE SIGNS OF SMOKE OR FIRE. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED GVI OF THE MAPCO CONTROL PANEL, AND ALL ELECTRICAL CONNECTIONS, AND SURROUNDING AREA. PERFORMED OPS TEST OF THE GALLEY CONTROL PANEL IAW Q400 AMM TASK 25-34-00-710-801. LET THE LIQUID WARMERS RUN FOR ABOUT AN HOUR. FOUND NO ARCING OR SPARKING, OR ANY DEFECTS. THE SURFACE OF THE PANEL IS COOL TO THE TOUCH, AND NOT "SUPER HOT" OPS TEST PASSED. NO DAMAGE OR DEFECTS, OR SIGN OF SMOKE OR FIRE. REMOVED GALLEY CONTROL PANEL, FOUND NO DAMAGE, BURN EVIDENCE OR SIGNS OF FIRE. REINSTALLED PANEL, A/C OKAY FOR SERVICE. COULD NOT DUPLICATE.

Part: STARTER GEN — FAULTED (NR 2) · airframe 25,970 hrs · 28,083 cycles

ABORTED TAKEOFF BELOW 40 KTS DUE TO #2 DC GEN CAUTION . REMOVED FROM SERVICE. C/W Q400 FIM TASK 24-30-00-810-813 STEPS 1-4.A.(4). COULD NOT DUPLICATE #2 DC GEN CAUTION. REPLACED #2 DC STARTER/GENERATOR REF Q400 AMM 24-31-01-000-801 AND 24-31-01-400-801. OPS TEST GOOD. RETURNED TO SERVICE.

Part: APU — FIRE · airframe 25,737 hrs · 27,851 cycles

APPROXIMATELY A 4 FT FLAME SHOT OUT OF THE APU EXHAUST UPON START UP. REMOVED FROM SERVICE. C\W OPS TEST OF APU IAW AMM TASK 49-00-00-710-801. OPS TEST GOOD. OBSERVED APU DURING START UP. NO UNUSUAL FLAME OR SMOKE NOTED . NO FAULTS IN CDS. RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (DEICE SYSTEM) · airframe 25,564 hrs · 27,662 cycles

DEICE PRESS CAUTION CLIMBING OUT OF SEA. PRESSURE DOWN TO 12 PSI DURING TAIL SECTIONS. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED TACTILE INSPECTION OF INFLATED BOOTS ON TAIL SECTIONS, NO LEAKS FOUND. R&R LH LOW PRESSURE WARNING SWITCH AS A PRECAUTION, IAW Q400 AMM 30-11-31-000/400-801 OPS TEST PASSED. NO FURTHER DEFECTS NOTED. PER MOM A/C IS CLEARED FOR RETURN TO SERVICE.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 25,533 hrs · 27,634 cycles

FUSELAGE DOORS WARNING AT 9500'. MFD INDICATED AFT PAX DOOR RED. DOOR WARNING CYCLED SEVERAL TIMES DURING THE FLIGHT, BUT REMAINED STEADY FOR THE MAJORITY OF THE FLIGHT. RETURNED TO FIELD. REMOVED FROM SERVICE. FOUND INTERNAL DOOR L2 DOOR HANDLE NOT FULLY SEATED IN CLOSED POSITION. C/W OPS TEST OF AFT L2 DOOR IAW AMM 52-12-00-710-802. ALL TEST GOOD. NOT DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 25,295 hrs · 27,391 cycles

NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION AND CYCLED AFTER LANDING. REMOVED FROM SERVICE. INTERROGATED PSEU. REPLACED NOSE LANDING GEAR ALTERNATE LOCK ELECTRICAL HARNESS, IAW Q400 AMM TASKS 32-21-11-000-801 & 32-21-11-400-801. PERFORMED OPERATIONAL TEST OF LANDING GEAR PRIMARY EXTENSION & RETRACTION SYSTEM, IAW Q400 AMM TASK 32-31-00-710-801. OPERATIONAL TEST IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — INOPERATIVE (PNEUMATIC SYSTEM) · airframe 25,183 hrs · 27,278 cycles

AROUND 85 KTS BLEED HOT 1 AND 2 CAME ON. TEMP KNOB WAS 3 O'CLOCK. BLEED FLOW MIN FOR ENTIRE TAXI. DID E/A RESET BLEED NOT NR 1 AND NR 2 BOTH WENT OUT. ABORTED TAKE OFF. REMOVED FROM SERVICE. INTERROGATED CDS, FAULTS FOUND IN CURRENT LEG: 1007-R, 1006-R, NH NAPRSOV. REMOVED AND REPLACED RT ENGINE NACELLE SHUTOFF VALVE, IAW Q400 MM 36-11-19-00-801 AND 36-11-19-400-801. C/W OPERATIONAL TEST OF BLEED SYSTEM, IAW Q400 AMM 36-11-00-710-802. OPERATIONS CHECK GOOD. FAULTS DID NOT RETURN. OPERATED BOTH ENGINES AT NTOP FOR A TIMEFRAME OF THREE MINUTES, NO DEFECTS/FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (#1 ENGINE) · airframe 25,092 hrs · 27,183 cycles

JUST STARTED ADDING POWER FOR TAKEOFF-LOW POWER LOW AIRSPEED AND RECEIVED A POWERPLANT MESSAGE. ABORTED TAKEOFF, RETURNED TO GATE. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND CURRENT FAULTS 719A AND 719B FAULT CODES (3540). CLEARED FAULT ON NR 1 ENGINE (719A & 719B) FOR PURPOSES OF MTX TAXI TO HANGER. DUE TO RECENT HISTORY & TROUBLESHOOTING, R & R NR 1 ENGINE FUEL CONT ELECTRICAL HARNESS, IAW AMM 73-21-11-000-801/400-801 AS A PRECAUTIONARY MEASURE. PERFORMED ENGINE RUN AT POWER SETTINGS BETWEEN DISC & RATING. FAULTS 719A/B DID NOT REOCCUR. RETURNED TO SERVICE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 24,871 hrs · 26,939 cycles

OVERHEAD EMERGENCY EXIT SIGN IN AFT GALLEY IS LOOSE HANGING FROM CEILING. REMOVED FROM SERVICE. RESECURED OVERHEAD EMERGENCY EXIT SIGN AFT GALLEY AS REQUIRED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ROD — LACK OF LUBE (EXTENSION DOOR) · airframe 23,902 hrs · 25,857 cycles

ALTERNATE GEAR EXTENSION DOOR (FLOOR) HARD TO OPEN AND CLOSE. REMOVED FROM SERVICE. INSPECTED ALTERNATE GEAR EXTENSION DOOR. NO DEFECTS.CLEANED & LUBED ALTERNATE GEAR EXTENSION DOOR ACTUATOR ROD. DOOR OPENS AND CLOSES WITHOUT DIFFICULTY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (PROP DEICE) · airframe 23,860 hrs · 25,804 cycles

ON CLIMB OUT PROP DE-ICE CAUTION ILLUMINATED. DURING RUNNING OF PROP DE-ICE CHECKLIST, CAUTION LIGHT EXTINGUISHED AND RE ILLUMINATED. FINISHED CHECKLIST AND CAUTION ILLUMINATED AGAIN. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS WITH NO FAULTS FOUND. C/W FINC CK OF PROP DEICE IAW Q400 AMM 30-61-00-720-801, NO PROP DEICE CAUTION NOTED. FURTHER T/S'ING INCLUDES VISUAL CHECK OF #1 AND #2 PROP ASSY'S INCLUDING LEADING EDGES OF ALL BLADES, VISUAL CHECK OF DEICE HARNESSES AND BRUSH BLOCK'S. FOUND #2 PROP BLADES 3 AND 4 DEICE HARNESSES INTERMITTENTLY TO OPEN. REMOVED AND REPLACED #2 PROP BLADE 3 AND 4 DEICE HARNESS'S IAW Q400 AMM 61-10-06-000/400-805. C/W FUNC CK AND CALIBRATION OF PROP DEICE HEATER ELEMENTS IAW Q400 AMM 30-61-00-760-801. NO PROP DEICE CAUTION NOTED. ALL PHASES IOF #1 AND #2 AC GEN STEADY AT .19 LOAD. FUNC CK OF PROP DEICE SYSTEM PER Q400 AMM 30-61-00-720-801 CHECKS GOOD. RETURNED TO SERVICE.

Part: CONTROL PANEL — WARNING MESSAGE (ZONE 200) · airframe 23,488 hrs · 25,359 cycles

MASTER WARNING ON TAKEOFF AS THE F.O. MOVED THE LANDING GEAR HANDLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW Q400 AMM TASKS 32-31-01-000-801 AND 32-31-01-400-801. FUNCTIONAL TEST GOOD. CONTROL PANEL WAS REPLACED AS PRECAUTIONARY MEASURE. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (PAX DOOR) · airframe 23,221 hrs · 25,043 cycles

GROUND CREW REPORTS MCD DIFFICULT TO OPEN UNKNOWN SUBSTANCE ON DOOR SEAL. REMOVED FROM SERVICE. C/W OPERATIONAL TEST OF MAIN CABIN DOOR. OPS CKS GOOD. COULD NOT DUPLICATE. OK FOR CONTINUED SERVICE IAW AMM TASK 52-11-00-710-802. NO PARTS REPLACED.

Part: LEVER — BINDING (SERVICE DOOR) · airframe 23,196 hrs · 25,016 cycles

AFT SERVICE DOOR OUTSIDE LOCK HANDLE FORCE FEELS EXCESSIVE. FOUND AFT SERVICE DOOR TRIP LEVER IS BINDING FOR THE LIFT AND LATCH. COMPLETED RIGGING OF VENT DOOR MECHANISM, Q400 AMM TASK 52-00-00-830-801 PAR E. OPERATED DOOR FROM INTERIOR AND EXTERIOR AND CONFIRMED NORMAL DOOR OPERATION AND FEEL. STARTED THE ADJUSTMENT OF THE LIFT AND LATCH REF Q400 AMM TASK 52-00-00-830-803 PAR 1-4.B.C.E.F, AND PAR 5.A. COMPLETED Q400 AMM TASK 52-00-00-830-803. PER 5B AND C, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,436 hrs · 24,076 cycles

CABIN EMERGENCY POWER SUPPLY 3 APPEARS TO HAVE DEAD BATTERIES. R&R EMG. LIGHT POWER SUPPLY UNIT #3 IAW Q400 AMM 33-51-01-000/400-801. FUNC CHECK GOOD. CLEAR DEFECT.

Part: RESERVOIR — CONTAMINATED (HYDRAULIC SYS) · airframe 22,232 hrs · 23,824 cycles

WHILE PULLING INTO THE GATE BRAKES FELT MUSHY. THE HARDER YOU PRESS THE SOFTER THEY FELT TILL THEY GRAB. REMOVED FROM SERVICE. PERFORMED GVI OF BOTH LT & RT BRAKES & NR 1 & NR 2 HYDRAULIC SYS. NO LEAKS OR DEFECTS NOTED. PERFORMED NR 1 SYS RESERVOIR BLEEDING IAW AMM 29-10-00-870-079. PERFORMED NR 2 SYS RESERVOIR BLEEDING IAW AMM 29-10-00-870-077. DURING TAXI CHECK, BRAKES CHECK GOOD, OPERATED NORMALLY, NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PIN — CORRODED (FIRE BOTTLE) · airframe 22,215 hrs · 23,804 cycles

ON FINAL APPROACH - CHECK FIRE DETECT WARNING - RAN CHECK LIST APU FIRE BOTTLE INDICATES LOW. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PLACED ON MEL 26-20-1. RETURNED TO SERVICE. MEL CLEARED 3/12. FOUND PINS ON 2600 J12 OF APU BOTTLE CONNECTOR FOR PRESSURE SWITCH TO BE CORRODED. INSPECTED 2600-P12 NO DEFECTS NOTED_ REF WM 26-23-00. R&R'D APU FIRE EXT. BOTTLE REF. AMM 26-23-01-000-801 & 26-23-01-400-801. OPS TEST GOOD. M PROC REVERSED. THIS CLEARS MEL/DMI. RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 21,954 hrs · 23,495 cycles

DURING LANDING ROLLOUT ABOVE 60 KNOTS, THE BRAKES WOULD COME ON AND THEN RELEASE IN INTERVALS OF APPROX 1-2 SECONDS. REMOVED FROM SERVICE. PERFORMED TAXI OF AIRCRAFT, OPERATED BRAKES MULTIPLE TIMES AND COULD NOT DUPLICATE BRAKING ISSUE. PERFORMED FUNCTIONAL TEST OF ANTI-SKID SYSTEM IAW AMM 32-46-00-720-802. FUNCTIONAL TEST GOOD. ALSO PERFORMED BITE TEST IAW AMM 32-46-00-720-801. BITE CHECK GOOD. NO CDS FAULTS. NO DEFECTS NOTED AT THIS TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,669 hrs · 23,161 cycles

WHEN PERFORMING EMERGENCY LIGHT OPERATIONAL CHECK, THE AFT 3 AISLE LIGHTS AFT CENTER AND AISLE EXIT SIGN AND EXIT SIGN ON FORWARD FACE OF GALLEY ARE INOP. REPLACED POWER SUPPLY.

Part: CONTROL MODULE — MALFUNCTIONED (TE FLAPS) · airframe 20,900 hrs · 22,300 cycles

ON APPROACH, FLAP POWER CAUTION LIGHT ILLUMINATED WHEN FLAPS WERE SET TO 5. FLAP POSITION REMAINED AT 0. FLAP POWER CAUTION RESET WAS ACCOMPLISHED IAW THE CHECKLIST. ON SECOND ATTEMPT, CAUTION LIGHT STAYED DARK AND FLAP EXTENDED AS USUAL, THROUGH ALL FLAP RANGES. INSPECTED FLAPS. NO DEFECTS NOTED. FLAPS WERE LOWERED TO 5. REMOVED FROM SERVICE. FOUND IN CDS FLAP HISTORY PG. ARMING SWITCH FAULT IAW FIM 27-50-00-810-802. PARA 1C, ARMING SWITCH AS ONE OF THE CONDITION FOR FLAP POWER CAUTION. REMOVED AND REPLACED FLAP CONTROL MODULE IAW AMM 27-51-06-000-801, 27-51-06-400-801. PERFORMED AN OPS TEST IAW 27-21-16-710-802. OPS TESTED GOOD. PERFORMED FLAP MOVEMENT THROUGH FULL TRAVEL 5 TIMES WITH ENGINE POWER. NO FLAP POWER CAUTION, FAULTS OR DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER UNIT — MALFUNCTIONED (TE FLAPS) · airframe 20,891 hrs · 22,292 cycles

DURING APPROACH, THE FLAP POWER CAUTION LIGHT ILLUMINATED WHEN FLAPS WERE SELECTED TO 5 DEG. PERFORMED THE FLAP POWER CAUTION RESET PER CHECKLIST AND THE LIGHT EXTINGUISHED. ON SECOND ATTEMPT TO SET FLAPS THE FLAP POWER CAUTION LIGHT DID NOT ILLUMINATE BUT FLAPS STAYED AT ZERO DEG. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FERRIED FOR REPAIRS. REMOVED AND REPLACED THE FLAP POWER UNIT IAW AMM 27-52-01-000/400-801. FUCTIONAL TEST NORMAL. RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 20,210 hrs · 21,526 cycles

DURING TAXI OUT, THE ENGINE ADPT HEAT 1 AND PUSHER SYSTEM FAIL CAUTION LIGHTS ILLUMINATED. AFTER A COUPLE MINUTES THE ENG ADPT HEAT 2, # 1 STALL SYST FAIL, # 2 STALL SYST FAIL, PITOT HEAT 2 CAUTION LIGHTS ILLUMINATED. FOUND CIRCUIT BREAKERS FUEL AUX PUMP 1, FUEL AUX PUMP 2 INTK LIP HTR ENG 2, INTK LIP HTR ENG 1 L WINDOW HEAT, R AOA VANE HEAT, R WSHLD HEAT, L WSHLD HEAT ALL POPPED.EMOVED FROM SERVICE. AFTER CLOSING CIRCUIT BREAKERS ONE BY ONE, SMOKE AND SPARKS AFTER THE NR 2 INTAKE HEAT CB PUSHED IN AND ALL CB ABOVE TRIPPED. FOUND ARCED AND BURNED WIRE BUNDLE UNDER PANEL 133AZ. REPAIRED DAMAGED WIRE BUNDLE, IAW WM 20-16-10-20. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,097 hrs · 21,409 cycles

FORWARD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY PACKS IAW AMM 33-51-00-820-801. CHCEKED GOOD.

Part: PCU — INOPERATIVE (NR 1) · airframe 20,056 hrs · 21,365 cycles

PROPELLERS OUT OF FEATHER, NR 1 TORQUE 11 PERCENT, NR 2 TORQUE 1 PERCENT, NR 1 POWER LEVER SLOW TO RESPOND. REMOVED FROM SERVICE. INTERROGATED CDS, FAULT CODES 132 CH B & 224 CH A & B POSTED ON THE NR 1 ENGINE. REMOVED & REPLACED THE NR 1 PCU IAW AMM 61-21-11-00-801/400-801, MCN 671290-001 ISSUE 6, MTC 6610001 & 6610002. FAULT CODES CLEARED & REMAINED CLEAR AFTER ENGINE RUN. OP CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 19,959 hrs · 11,266 cycles

DURING TAXI, THE NR 1 ENGINE TORQUE WOULD NOT REDUCE BELOW 9% TORQUE. NR 1 ENGINE HAD NO REVERSE CAPABILITY WHEN ATTEMPTING TO USE REVERSE TQ REMAINED AT 95 TQ ALSO NR 1 PROPELLER DID NOT INDICATE. PROPELLER GROUND RANGE INDICATIONS WHILE NR 2 PROPELLER DID INDICATE CORRECT. GROUND RANGE NO POWERPLANT OR PEC CAUTIONS WERE INDICATED BOTH POWER LEVERS WERE AT 1020 AND VERIFIED THERE. NO CIRCUIT BREAKERS WERE SEEN AS TRIPPED. REMOVED FROM SERVICE. COMPLIED WITH CDS FAULT RETRIVAL FOUND FAULT CODE 132 NR 1 PEC CHANNEL A . COMPLIED WITH FIM 61-20-03-810-816 UP TO STEP 5A(A), COMPLIED WITH PEC, FAULT CLEARED IAWS AMM 61-20-36-070-801. COMPLIED WITH TWO ENGINE STARTS, RAN TAXI CHECK, FAULT DID NOT RETURN. ACFT RETURN TO SERVICE.

Part: HANDLE — OUT OF POSITION (CARGO DOOR) · airframe 19,292 hrs · 20,570 cycles

DURING TAKE OFF ROLL, AT ABOUT 70KTS, THE FUSELAGE DOORS MASTER WARNING. TAKEOFF WAS ABORTED & CHECKLIST WAS RUN. FOUND THE AFT CARGO DOOR HANDLE TO BE AJAR, CONSITENT WITH DOORS SYS PAGE INDICATING THE AFT CARGO DOOR OPEN. INSPECTED AFT CARGO DOOR IAW AMM 05-52-00-000-000, AND 05-0029 WITH NO DEFECTS NOTED. FUSELAGE DOOR WARNING REMAINED EXTINGUISHED. RETURNED TO SERVICE.

Part: LENS — BROKEN (ANTI COLLISION) · airframe 19,163 hrs · 20,438 cycles

ANTI COLLISION LENS ON BELLY IS BROKEN. REMOVED FROM SERVICE. R & R THE ANTI-COLLISION LIGHT IAW AMM 33-44-06-000-801, & 33-44-06-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (COCKPIT FLOOR) · airframe 18,941 hrs · 20,215 cycles

ALTERNATE GEAR EXTENSION DOOR WILL NOT OPEN FULLY. REMOVED FROM SERVICE. CLEANED AND LUBRICATED THE GEAR EXTENSION DOOR IN COCKPIT FLOOR. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — TORN (DE-ICE SYSTEM) · airframe 18,903 hrs · 20,173 cycles

DE-ICE PRESS CAUTION LIGHT ILLUMINATED IN CLIMB THROUGH FL180. RAN CHECKLIST, NOTICED SECOND FROM WINGTIP BOOT WAS NOT ILLUMINATING. DE-ICE PRESS CAUTION REMAINED ON. RETURNED TO FIELD. LANDING UNEVENTFUL. AIRCRAFT REMOVED FROM SERVICE. RAN ENGINES AND OPERATED AIRFRAME DEICE SYSTEM. DISCREPANCY DUPLICATED. NOTED CDS FAULT LOW PRESSURE 2B FAIL. REMOVED LE 613 AR REF AMM TASK 57-23-01-000-801, FOUND AIR LINE TO BOOT TORN. REPLACED LINE WITH NEW FROM STOCK. REINSTALLED LE 613 AR IAW AMM TASK 57-23-01-400-801. OPS TEST GOOD. ALL BOOTS INFLATE, NO DEICE PRESS CAUTION, NO FAULTS IN CDS. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (TRANSDUCER) · airframe 18,755 hrs · 20,011 cycles

ON APPROACH AT ABOUT FL 240, THE NR 3 HYD QTY INDICATION WENT FOM 75% TO ZERO PERCENT FOR ABOUT 5 MINUTES AND RETURNED TO 75%. LANDING UNEVENTFUL. AT GATE IN INDICATES 75% NO CAUTION OR WARNING LIGHTS EMERGENCY CHECKLIST INDICATED NO CREW ACTION. AIRCRAFT REMOVED FROM SERVICE. INSP #3 HYD SYS IAW AMM 29-12-00-210-802 FOUND RESEVIOR QTY TRANSDUCER CONNECTOR LOOSE AND DIRTY. CLEANED AND SECURED THE CONNECTOR. PERFORMED AN OPS CHECK IAW AMM 29-12-01-710-801. OPS CHECKED GOOD. COULD NOT DUPLICATE FAULT. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 18,637 hrs · 19,886 cycles

AFTER PUSHBACK, PUT BOTH CONDITION LEVERS TO MAX IAW FLOW, NR 2 PROPELLER CAME OUT OF FEATHER BUT NR 1 PROP STAYED AT 190 FOR AT LEAST FOUR MINUTES. ONLY CAME OUT OF FEATHER WHEN POWER WAS ADDED. AIRCRAFT REMOVED FROM SERVICE. NO FAULTS IN CDS. REMOVED AND REPLACED NR 1 ENGINE OVERSPEED GOVERNOR IAW MM 61-20-26-000-801, AND 61-20-26-400-801 AS A PRECUATION. OPS AND LEAK CHECKED GOOD. COMPLIED WITH MULTIPLE PROPELLER UNFEATHERING ACTIONS. ALL NORMAL IAW MM 61-20-00-720-801. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 18,124 hrs · 19,320 cycles

DURING WALK THROUGH, FOUND THREE PIECES OF EMERGENCY LIGHT STRIPS DETACHED FROM FLOOR NEAR MCD AND FWD GALLEY AREA, SECURED THE LIGHT.

Part: TRANSDUCER — FAILED (AOA) · airframe 18,009 hrs · 19,182 cycles

DURING CLIMBOUT "PUSHER SYSTEM FAIL" CAUTION ILLUMINATED, RETURNED TO FIELD, LANDING UNEVENTFUL. AFTER LANDING ASSOCIATED 1 & 2 STALL SYST FAIL ILLUMINATED. INTERROGATED CDS FOUND RIGHT AOA FAIL. R&R RT AOA TRANSDUCER IAW AMM 27-33-26-000/400-801. FUNCTIONAL TEST GOOD. NO FAULT FOUND ON CDS. RETURNED TO SERVICE.

Part: AOA — FAILED · airframe 17,913 hrs · 19,081 cycles

PUSHER SYSTEM FAIL CAUTION ILLUMINATED DURING CRUISE FLIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS AND FOUND LEFT VANE HEATER MESSAGE. REMOVED AND REPLACED LT AOA TRANSDUCER. IAW AMM TASK 27-33-26-000-801/400-801. COMPLIED WITH MCN 627255-01 ISSUE NO. 01. FUNCTIONAL TEST GOOD. REF AMM TASK 27-33-26-720-801. LEFT VANE HEATER FAULT DID NOT RETURN IN CDS. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN FLOOR) · airframe 17,844 hrs · 19,015 cycles

GLOW STRIP NEAR RO 2 IS LOOSE. CLEANED FLOOR AND STRIP APPLIED TAPE AND SECURED. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN FLOOR) · airframe 17,843 hrs · 19,013 cycles

GLOW STRIP ADJACENT TO MAIN CABIN DOOR IS LOOSE. SECURED GLOW STRIP WITH APPROPRIATE TAPE. RETURNED TO SERVICE.

Part: SENSOR — DIRTY (NLG DOOR) · airframe 17,784 hrs · 18,951 cycles

DURING GEAR EXTENSION, AMBER NOSE GEAR LIGHTS REMAINED ILLUMINATED. ALL 3 GEAR DOWN LIGHTS WERE ILLUMINATED. AT GATE FOUND THE NOSE GEAR DOORS CLOSED. OPENED NOSE GEAR DOOR, FOUND NLG DOOR CL PROBE SENSOR DIRTY, CLEANED SENSOR, RAN NR 2 ENGINE, DOOR CLOSED AND INDICATED CLOSED. RETURN TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 17,567 hrs · 18,735 cycles

NOSE DOOR LIGHT REMAINED ON AFTER GEAR SELECTED DOWN FOR LANDING. AT GATE NOSE DOOR APPEARS CLOSED. INTEROGATED PSEU AND RETREIVED FAULT HISTORY NGDRCL UNREASONABLE FAR. FERRY FOR REPAIRS. CHECKED PSEU FAULT HISTORY SHOWS NGDRCL UNREASONABLE FAR ON FLIGHT LEG-01 ADJUSTED NGDRCL PROX SENSOR IAW AMM TASK 32-61-00-280-801.

Part: DOOR SEAL — MALFUNCTIONED (DOOR) · airframe 17,476 hrs · 18,641 cycles

AIRPLANE DID NOT PRESSURIZE ON CLIMB OUT FA REPORTED SEEING DAYLIGHT AROUND THE MAIN CABIN DOOR CABIN PRESS WARNING CHECKLIST WAS ACCOMPLISHED. RETURNED TO FIELD. LANDING UNEVENTFUL. PER PILOT VERBAL DOOR SEAL DID INFLATE ON INBOUND FLT C/W GVI OF MCD AND OTHER DOOR SEALS NO DEFECTS NOTED PRESSURIZED AIRCRAFT ON GROUND REF AMM 21-31-00-710-803 PRESSURIZATION OPS NORMAL AIRCRAFT RTS ALSO DRAINED DOOR SEAL ACCUM NO MOISTURE WAS PRESENT. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND DWG:85361501 REV D.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07-02-01, SRM 51-42-05-02-01, 51-41-00-00-01, 51-40-15-002-010, AMM 20-10-01-430-801 TABLE 1, TABLE 3 AND DWG:8532821 REV E.

Part: DIAPHRAGM — CRACKED · airframe 17,305 hrs · 18,464 cycles

DIAPHRAGM PN 85414131-101 AT RIB STA XN197.81 HAS CRACK IN OUTBD FLANGE. REMOVED OB DIAPHRAGM PN:85414117 FOM TO ACCESS REMOVAL REF SRM 51-42-005 AND 51-40-15. INSTALLED OB DIAPHRAGM PN:85414117 REF SRM 51-42-05-02-01 AND 51-40-15-02-01. REMOVED DIAPHRAGM PN:85414131-101 AT RIB STA XN 197.81 REF SRM 51-40-15 AND 51-42-05. INSTALLED DIAPHRAGM PN:85414131-101 REF SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED SOLID RIVETS ON NEW DIAPHRAGM PN:85414131-101 AT STA XN 197.81 AND OB DIAPHRAGM PN:855414117 REF SRM 51-42-05. INSTALLED ON NEW DIAPHRAGM PN:85414131-101 AND PN:855414117 REF SRM 51-42-05-02-01 AND 51-40-15-02-01. RESTORE FINISH ACCOMPLISHED ON TC 6-54-441 LT ITEM 12.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK 11 PN 85328210-115 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED SEAT RAIL 11 PN 85328210-115 IAW SRM 51-40-15-02-01 & 51-41-00-00-01. INSTALLED SEAT TRACK 11 PN 85328210-115 BTWN STAX 0.400 & F.S.X94.800 REF SRM 51-41-00-00-01 & DWG 85328201 REV "E' DATE 2013/01/19. REMOVED SEAT RAIL SPLICE BETWEEN SEAT RAIL 11 & 12 IAW SRM 51-40-15-02-01. INSTALLED SEAT TRACK SPLICE COMMON TO SEAT TRACKS 11 & 12 REF SRM 51-42-05-02-01, 51-40-15-02-01 & DWG 85328201 REV "E" DATE 2013/01/19. REMOVED WEB FROM EA RAIL 11 STA 19.400-32.400 IAW SRM 51-42-05-02-01. INSTALLED FASTENERS AT ST-19.4 WEB COMMON TO SEAT TRACK 11 REF SRM 51-42-05-02-01 & DWG 85328201 REV "E" DATE 2013/01/19. REMOVED CABLE TIES 3EA BETWEEN STA 32.400 71.200, 2EA STA 94.800-116.000, 1EA STA. 116.00-136.000 IAW WM 20-12-10-201. INSTALLED CABLE TIE WRAPS BTWN F.S.X-32.400 F.S.X71.200 (3EA), STA 94.800 - F.S.X116.000 & 1EA AT F.S.X116.0 TO F.S.X136.00 REF WM 20-12-10-201 (2EA AT F.S.X94.800-F.S.X116.000). DISPLACED DRIP TRAY TO FOM REF SRM 51-40-15. INSTALLED DRIP TRAY COMMON TO SEAT TRACK 11 & 12 REF SRM 51-41-00-00-01. LOCATED & DRILLED NEW SEAT TRACK PN 85328210-115 & ATTACHED WIRE CLIPS TO SEAT TRACK REF SRM 51-40-07 & 51-42-05. COMPLIED WITH FORM M-184.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK NR 8 PN 85338210-109 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED SEAT TRACK NR 8 PN 85338210-109 REF SRM 51-42-05-00-01, 51-41-00-00-01, 51-40-10-02-01. INSTALLED SEAT TRACK NR 8 PN: 85338210-109 REF SRM 51-40-15, 51-42-05, 51-41-05 DWG 85338201 REV "F" 2011/04/20. REMOVED SPLICES PN 85338216-101, 85338215-101 COMMON TO SEAT TRACKS NR 7 AND NR 8 REF SRM 51-41-00-00-01, 51-42-05-00-01, 51-40-10-02-01. SPLICES PN 85338216-101, 85338215-101 COMMON TO SEAT TRACKS NR 7 AND NR 8 ARE INSTALLED ON JOB 5424331 OP 140 (SEAT TRACK NR 7 R&R). REMOVED SPLICES PN 85338216-101, 85338215-101 COMMON TO SEAT TRACKS NR 8 AND NR 9 REF SRM 51-41-00-00-01, 51-42-05-00-01, 51-40-10-02-01. INSTALLED SPLICES COMMON TO SEAT TRACK NR 8 & NR 9 PN: 85338216-101, 85338215-101 REF SRM 51-42-05, 51-40-15 DWG 85338201 REV "F" 2011/04/20. LOCATED & DRILLED SEAT TRACK NR 8 PN: 85338210-109 REF SRM 51-40-07 DWG 85338201 REV "F" 2011/04/20. COMPLIED WITH FORM M-184.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,305 hrs · 18,464 cycles

SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 AND 51-40-15, AND AND DRAWING 85338251 REV A.

Part: WARNING LIGHT — MALFUNCTIONED · airframe 17,140 hrs · 18,284 cycles

CPCS FAULT LIGHT ILLUMINATED IN FLIGHT. CYCLED DUM/MAN/AUTO SELECTOR PER "FAULT ANNUNCIATION ON PRESSURIZATION CONTROLLER" EMERGENCY CHECKLIST. FAULT LIGHT EXTINGUISHED AND AUTO PRESSURIZATION OPEARATED NORMALLY. INFORMATION ONLY. ACCOMPLISHED FSM CPCS FAULT RESET VERIFICATION PROCEDURE. FAULT ANNUNCIATION DID NOT RE-ILLUMINATE. RETURNED TO SERVICE.

Part: BRAKE — SMOKE (NR 2) · airframe 16,289 hrs · 17,388 cycles

DURING WALK AROUND POSTFLIGHT, NOTICED NR 2 BRAKE SMOKING. ALL OPS DURING LANDING ROLLOUT NORMAL. COMPLIED WITH ANTI-SKID FUNCTIONAL CHECK, NO DEFECTS NOTED. REPLACED THE NR 1 AND 2 BRAKE ASSY'S. COMPLIED WITH RIGGING CHECK OF MAIN BRAKE CONTROL CABLES, NO DEFECTS NOTED, NO ADJUSTMENTS REQUIRED.

Part: RESERVOIR — CONTAMINATED (HYDRAULIC SYS) · airframe 16,089 hrs · 17,168 cycles

BRAKES SOFT AND LESS EFFECTIVE THAN NORMAL. PERFORMED GVI OF MLG BRAKES AND BRAKE LINES OF NR 1 AND NR 2. NO DEFECTS NOTED. BRAKE PINS APPEARED NORMAL, BLED NR 1 AND NR 2 HYDRAULIC SYSTEMS RESERVOIR, REF AMM TASKS 29-10-00-870-801/802. TAXIED ACFT OPERATED MLG BRAKES IN SEVERAL INTERVALS. MLG BRAKES OPERATED NORMALLY. NO OTHER DEFECTS NOTED. C/W MQAR DOWNLOAD, REF MCN NR 64602-14.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 15,796 hrs · 16,846 cycles

EMERGENCY LIGHTS ABOVE THE MAIN CABIN DOOR AND THE COCKPIT ENTERANCE ARE NOT WORKING. REPLACED THE BATTERY PACK AT POSITION RT1 IAW AMM 33-51-00-820-801. CHECKS GOOD.

Part: BRAKE SYS — WEAK (MLG) · airframe 15,623 hrs · 16,640 cycles

ON LANDING FO NOTED THAT THE BRAKES DID NOT SEEM TO BE RESPONDING TO PEDAL INPUTS. CAPTAIN NOTICED THAT BRAKES DID NOT SEEM TO GRAB. AT THE GATE THE BRAKES FELT SPONGY. ACFT DID NOT PULL IN ANY DIRECTION. FOUND ALL BRAKES ROUGHLY THE SAME TEMPERATURE UPON ARRIVAL. TAXIED ACFT. CONFIRMED BRAKES SOMEWHAT WEAKER THAN NORMAL, GRABBY AND PEDALS A LITTLE SPONGY. C/W GVI OF PEDAL LINKAGE UNDER PANEL 121AL. NO DEFECTS NOTED. BLED ALL FOUR BRAKES IAW AMM 32-42-00-870-801. REMOVED AIR FROM ALL 4 BRAKE ASSEMBLIES. BRAKES 1 AND 3 HAD LARGER QUANTITIES OF AIR. TAXI TESTED ACFT. FOUND BRAKES WORKING NORMALLY FROM BOTH POSITIONS. NO FURTHER DEFECTS NOTED.

Part: TARGET — UNKNOWN (EMERGENCY EXIT) · airframe 15,456 hrs · 16,468 cycles

TYPE II/III FOWARD RT DOOR INDICATOR RT AT 23000 AT FUSELAGE DOORS WARNING ILLUMINATED PRESSURIZATION NORMAL INDICATIONS EXTINGUISHED DESCEDING THROUGH 14K. FWD RT EMERGENCY DOOR PROXIMITY SENSOR TARGET ASSY. ALL OPS CKS GOOD ACFT OK FOR CONTINUE SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 15,121 hrs · 16,117 cycles

EMERGENCY LIGHT STRIP AT ROW 1 LOOSE. SECURED THE EMERGENCY LIGHT AND RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,043 hrs · 16,049 cycles

F/A EMERGENCY LIGHT SWITCH, BACK LIGHT NOT WORKING, RELAMPED. RETURNED TO SERVICE.

Part: FIRE BOTTLE — READS LOW (APU BAY) · airframe 14,817 hrs · 15,812 cycles

MASTER WARNING, CHECK FIRE DETECTOR. APU BOTTLE, LOW LIGHT ILLUMINATED AT 25,000 AND -42 DEGREES C. REPLACED APU FIRE BOTTLE IAW AMM TASK 26-23-01-000-801/400-801. OPS TEST GOOD NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,794 hrs · 14,711 cycles

RIGHT EMERGENCY LIGHTS AND CEILING PANEL LIGHTS DS2 AND DS3 GO OUT AFTER 3 MINUTES OF OPERATION. FOUND PIN 2 VOLTAGE AT 24VDC BUT SHOULD BE 28 VOLT +/- 2. CHARGED POWER SUPPLIES AND CHECKED CHARGINE SYSTEM. ALL CHECKS GOOD.

Part: SKIN — DENTED (BS 258) · airframe 13,788 hrs · 14,708 cycles

LEFT FUSELAGE SKIN AT APPROX 7" AFT OF BS 258, STR 11-13P HAS 21 DENTS. REMOVED DAMAGE ON LT FUSELAGE AT APPROX 7" AFT OF FS 258.00, STR 12P REF RD8/4-53-6968, ISSUE 1. RECEIVED TC RD8/4-53-6968/3. C/W ET INSP ON CUTOUT IAW RD8/4-53-6968, ISSUE 1. REMOVED ALL EXISTING FASTENERS COMMON TO REPAIR DOUBLER NR 1 IAW RD 8/4-53-6968, SHEET 4. NO DAMAGE TO UNDERLYING STRUCTURE. FABRICATED REPAIR PACKER NR 1 USING MATERIAL, PN 2024-T3 0.063" PO: T20092 IAW RD 8/4-53-6968, SHEET 4. LOCATED AND DRILLED REPAIR DOUBLER NR 1, REF SRM 51-40-07 AND RD8/4-53-6968 ISSUE 1. REMOVED DOME NUT ASSY, PN 853077381-107 BTW FS X258.00 AND X281.00 ON STRINGER 13P IAW SRM 51-42-05. INSTALLED DOME NUT ASSY BETWEEN FS X258.0 AND FS X281.0 ON STR 13P, REF SRM 51-42-05, REPAIR-01. REMOVED STIFFENER, PN: 85307748-003 BETWEEN FS X258.00 AND X281.00 AND BETWEEN STR 13P AND STR 16P IAW SRM 51-42-05. INSTALLED STIFFENER, PN 85307748-003 BETWEEN FS X258.0 AND X281.0 AND BETWEEN STRINGER 13P AND 16P REF SRM 51-42-05, REPAIR-01. PERFORMED ET INSP IAW STEP 4 OF RD8/4-53-6968 ISSUE 1. COMPLETED FABRICATING REPAIR DOUBLER NR 1 REF RD8/4-53-6968, ISSUE 2. ALODINED AND PRIMED REPAIR DOUBLER NR 1 IAW RD8/4-53-6968 ISSUE 2. INSTALLED COUNTERSINK FILLERS ON OUTER SKIN OUNTERSINKS UNDER REPAIR DOUBLER NR 1 AREA REF RD8/4-53-6968, ISSUE 1 STEP B. INSTALLED RIVETS BETWEEN STR 11 AND STR 13, BS X258.0 AND BS X269.0, REF RD8/4-53-6968 ISSUE 1. INSTALLED DOUBLER NR 1 REF RD8/4-53-6968, ISSUE 2. RESTORED FINISH TO EXTERNAL SURFACE OF REPAIRED AREA REF RD NR 8/4-53-6968 ISSUE 2, SHEET 6, ITEMS 14 AND 16. RESTORED FINISH TO INTERNAL SURFACE OF REPAIRED AREA REF RD8/4-53-6968 ISSUE 2, SHEET 6, STEP 15 AND 17. TC COMPLIED WITH RD8/4-53-6968/3 ON JOB 5424325, OP 122.

Part: SKIN — DENTED (BS 301) · airframe 13,788 hrs · 14,708 cycles

LEFT FUSELAGE AT APPROXIMATELY 10" FWD OF FS 301.00, STR 10P-11P HAS DENT. REMOVED DAMAGE ON LT FUSELAGE AT APPROX 10" FWD OF F.S. 301.00 STR 10P REF RD8/4-53-6968, ISSUE 1 DATED 17 JULY 2015. RECEIVED T/C RD8/4-53-6968/3. C/W ET INSP ON CUTOUT IAW RD8/4-53-6968 ISSUE 1, DATE 7/17/15. NO DEFECTS NOTED. REMOVED ALL EXISTING FASTENERS COMMON TO REPAIR DOUBLER NR 2 IAW RD8/4-53-6968, SHEET 4, NO DAMAGE TO UNDERLYING STRUCTURE. FABRICATED REPAIR PACKER NR 2 USING MATERIAL, PN 2024-T3, 0.063", PO: T20092 IAW RD8/4-53-6968, SHEET 4. FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER NR 2 REF RD8/4-53-6968 ISS. 2 SHEET 4 & SHEET 5, STEP 6 & 7 DATED 7/20/15 MATERIAL 2024-T3 0.063", PO T20092. INSTALLED REPAIR COUNTERSINK UNDER REPAIR DOUBLER NR 2 AREA REF RD8/4-53-6968 ISSUE 2 DATED 7/20/15, STEP 8. REMOVED 5 CLIPS AND 1 STANDOFF TO FOM AT FS X281.0 TO FS X301.0 AND STR 9P TO 11P, REF SRM 51-42-05, REPAIR-01. INSTALLED 5 CLIPS AND 1 STANDOFF AT FS X281.0 TO X301.0 STR 9P TO 11P, REF SRM 51-42-05, REPAIR-01. REMOVED 6 EA BOLTS FROM SIDEWALL TRACK MOUNTS AT FS X258.0 TO FS X301.0 TO FOM REF SRM 51-41-00, STRUCT IDENT-01. INSTALLED 6 EA BOLTS AT SIDEWALL TRACK MOUNTS AT FS X258.0 TO FS 301.0 REF SRM 51-41-00, STRUCT IDENT-01. INSTALLED RIVETS ON DOUBLER NR 2 COMMON TO STR 9P, 10P, AND 11P AND COMMON TO FRAME FS X281.0 AND FS X301.0 AND PACKER NR 2, REF RD8/4-53-6968 ISSUE 2 DATED 7/20/15. INSTALLED DOUBLER NR 2, REF RD8/4-53-6968, ISSUE 1, DATE 7/17/15. RESTORED FINISH TO EXTERNAL REPAIR REF RD8/4-53-6968 ISSUE 2, DATED 20 JULY 2015, SHEET 6, ITEMS 14 AND 16. RESTORED FINISH TO INTERNAL SURFACE OF THE REPAIR AREA REF RD8/4-53-6968 ISSUE 2, DATED JULY 20 2015, SHEET 6 STEP 15 AND 16. TC COMPLIED WITH RD8/4-53-6968/3.

Part: RELIEF VALVE — FAILED (ZONE 200) · airframe 12,807 hrs · 13,674 cycles

CRUISING AT FL 250, HAD NR 1 HYD ISO VALVE AND NR 1 RUD HYD CAUTION LIGHTS ILLUMINATED. PERFORMED THE NR 1 HYD ISO VALVE CAUTION CHECK LIST NR 1 HYD PRESS REMAINED NORMAL. THE NR 1 HYD QTY WAS AT 40 PERCENT ON APPROACH WHILE SELECTING FLAPS, GOT A FLAP POWER CAUTION AND NOTED NR 1 HYD PRESSURE AT ZERO AND NR 1 HYD QTY AT ZERO. PERFORMED ZERO FLAPS LANDING. LANDED WITHOUT INCIDENT. LET THE ACFT ROLL TO A STOP ON RUNWAY, EMERGENCY BRAKE NOT APPLIED TO STOP ACFT TOWED TO GATE WITHOUT FURTHER INCIDENT. PERFORMED GVI OF NR 1 MLG AREA AND NACELLE. NO DPI’S POPPED AND NO LEAKS NOTED. PERFORMED GVI OF AFT ACCESSORY COMPARTMENT, FOUND RESIDUAL HYD FLUID, NO EVIDENCE OF LEAKS NOTED FROM HYD LINES. REMOVED FDR/CVR COVER AND CLEANED AREA OF RESIDUAL HYD FLUID PERFORMED GVI OF VERTICAL/ HORIZONTAL STABILIZER FOR LEAKS. NO LEAKS NOTED, OPENED PANEL 322DL FOR INSPECTION OF RUDDER PCU FOR LEAKS, NO LEAKS NOTED. CLOSED PANEL 322DL AND SEALED. SERVICED THE NT 1 HYD SYS IAW AMM TASK 12-10-29-611-801. PERFORMED BLEED OF NR 1 HYD SYS IAW AMM 12-10-00-870-801. REMOVED PANEL 263CL AND PERFORMED GVI OF NR 1 HYD ISOLATION VALVE NO LEAKS NOTED CLOSED PANEL 263CL AND SEALED. PRESSURIZED NR 1 HYD SYSTEM WITH STANDBY PUMP, INITIAL QTY WAS 90 PERCENT DROPPED TO 60 PERCENT. AFTER THIS THERE WAS A 5 PERCENT DROP EVERY 30 SECONDS IN HYD QTY. FOUND PUDDLE ON HYD FLUID COMING FROM DRAIN HOLE ON BELLY OF FUSELAGE UNDERNEATH CENTER WING AREA TO AFT LT SIDE DRAIN CONNECTED TO NR1 HYD BALANCE RELIEF VALVE. INSP OF NR 1 EDP AFTER OPERATION WITHOUT SUFFICIENT HYD FLUID IAW AMM TASK 05-54-00-280-801 FOR MAINT CONVENIENCE. R & R NR1 EDP IAW TASK 29-11-01-400-801. R & R HYD SYS BALANCE RELIEF VALVE IAW TASK 29-11-51-000/400-801.

Part: PROXIMITY SENSOR — DIRTY (PAX DOOR) · airframe 12,725 hrs · 13,594 cycles

PRIOR TO TAKEOFF CABIN DOOR, REAR, WARNING INDICATION LIGHT CAME ON. RETURNED TO GATE. CLEANED AND LUBED PROXIMITY SENSOR TO DOOR. OPS CHECK GOOD AT THIS TIME. REF AMM 52-42-00-710-801. FUSELAGE WARNING DID NOT RETURN. RETURNED TO SERVICE.

Part: STRINGER — CORRODED (BS 136-156) · airframe 11,727 hrs · 12,497 cycles

BUCKTAIL CORRODED ON STRINGER 26 RT BETWEEN BS 136 - 156. REMOVED CORRODED RIVETS, IAW SRM 51-42-05, REPAIR-01. REPLACED CORRODED RIVETS IAW SRM 51-42-05, REPAIR-01.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 11,727 hrs · 12,497 cycles

ANGLE SHEAR WEB, PN 85339286-115 LOCATED IN THE AFT CARGO COMPARMENT Z100.00, Y0.00 TO Y-25.00, X783.102 IS CORRODED AROUND NUTPLATE. SUBMITTED TO ENGINE FOR DISPOSITION. RECEIVED EO 53-L02834 9/11/14. C/W TASK CARD 53-L02834. PERFORMED ET INSP ON SHEAR ANGLE WEB CUT OUT IAW EO: 83-L02834, REV DATED 9/11/14 AND NDTM 51-00-06. NO DEFECTS NOTED. COMPLETED STEPS 1-8 AND 11 IAW EO 83-L02834, DATED 9/11/14. COMPLETED STEPS 9, 10 AND 12 IAW EO 83-L02834 DATED 9/11/14. REMOVED FLOOR ACCESS PANEL TO PN:83395612-1076, REF AMM 53-41-01-000-801. CLOSED PANEL, PN:83395612-1076 / 144JZ IAW AMM 53-41-01-400-801. REMOVED 90° CAP ANGLE IN AFT BAGGAGE TO FOM REF AMM 53-41-01-000-801. CLOSED 90° CAP ANGLE IN AFT BAGGAGE REF AMM 53-41-01-400-801, REMOVED FLOOR PANEL 145DZ TO FOM REF AMM 53-41-01-000-801. CLOSED FLOOR PANEL 145DZ REF AMM 53-41-01-400-801. C/W REPORT M-184 AS REQUIRED.

Part: SEAT TRACK — CORRODED (NR 19) · airframe 11,727 hrs · 12,497 cycles

SEAT TRACK NR 19 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, SRM 51-42-45 & SRM 51-42-15.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 11,727 hrs · 12,497 cycles

SEAT TRACK NR 10 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-00 AND SRM 51-42-05, REPAIR -01, AND SRM 51-40-07.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 11,727 hrs · 12,497 cycles

SEAT TRACK, NR 11 CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-05 & 51-40-15.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 11,727 hrs · 12,497 cycles

FWD BAGGAGE LOWER SURFACE EDGE CHANNEL HAS EVIDENCE OF CORROSION. RECEIVED, DRILLED AND LOCATED NEW BAGGAGE DOOR LOWER SURROUND EDGE CHANNEL, IAW SRM 51-40-07. INSTALLED 20 NUTPLATES ONTO NEW LOWER EDGE SURROUND CHANNEL WET WITH SEALANT, IAW TASK CARD 6/53-1158-438QX AND SRM 51-42-05.

Part: STRINGER — CORRODED (BS 564-584) · airframe 11,727 hrs · 12,497 cycles

EVIDENCE OF SURFACE CORROSION DETECTED ON STRINGER 26L BETWEEN BS 564.5 - 584.5. REMOVED CORROSION SRM 51-21-00, STEP 4A,2, NO MATERIAL LOSS. RESTORED PROTECTIVE FINISH IAW SRM 51-25-25-02-01, SRM 51-25-10-02-01 AND SRM 51-25-02-02-01 5(F)1.

Part: STRINGER — CORRODED (BS 116-136) · airframe 11,727 hrs · 12,497 cycles

STRINGER 26R CORRODED BETWEEN BS 116 - 136. REPAIRED IAW SRM 51-42-05, REPAIR -01.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 11,727 hrs · 12,497 cycles

LT WING FUEL ACCESS PANEL 522BT HAS NUMEROUS COUNTERSINKS WITH PITTING CORROSION. COUNTERSUNK HOLES TO MAX DEPTH. EVIDENCE OF CORROSION STILL REMAILS. OUT OF LIMITS REF SRM 57-10-35, REPAIR -03. 2 CONSECUTIVE HOLES OUT OF LIMITS. NO REPAIR ALLOWED REF SRM 57-10-35, REPAIR 04. ORDERED AND RECEIVED NEW FUEL PANEL 522BT, PN:85713037-953, C/W M-184.

Part: ACCESS PANEL — CORRODED (LT WING)

LEFT WING FUEL ACCESS PANEL 521BT HAS NUMEROUS COUNTERSINKS WITH PITTING CORROSION. REMOVED CORROSION WITHIN MAX ALLOWABLE DEPTH OF COUNTERSINK. EVIDENCE OF CORROSION STILL REMAINS. OUT OF LIMITS REF SRM 57-10-35, REPAIR -03 AND SRM 57-10-35, REPAIR -04 DUE TO HAVING 2 CONSECUTIVE HOLES OUT OF LIMITS. ORDERED AND RECEIVED NEW FUEL PANEL 521BT, PN:85713034-001.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 11,727 hrs · 12,497 cycles

LT WING FUEL ACCESS PANEL 523AT HAS NUMEROUS COUNTERSINKS WITH PITTING CORROSION. COUNTERSINK HOLES TO MAX ALLOWABLE DEPTH. EVIDENCE OF CORROSION STILL REMAINS OUT OF LIMITS REF SRM 57-10-35, REPAIR 03. 2 CONSECUTIVE HOLES OUT OF LIMITS. NO REPAIR ALLOWED REF SRM 57-10-35, REPAIR 04. ORDERED AND RECEIVED NEW FUEL PANEL 523AT PN 85713043-953, FUEL PANEL 523AT INSTALLED ON JOB 5424310, OP 3147. COMPLIED WITH M-184.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 11,727 hrs · 12,497 cycles

LEFT WING FUEL ACCESS PANEL 522AT HAS NUMEROUS COUNTERSINKS WITH PITTING CORROSION. COUNTERSUNK HOLES TO MAX ALLOWABLE DEPTH. EVIDENCE OF CORROSION STILL REMAINS, OUT OF LIMITS REF SRM 57-10-35, REPAIR -03, 2 CONSECUTIVE HOLES FOUND TO BE OUT OF LIMITS. NO REPAIR ALLOWED, REF SRM 57-10-35, REPAIR. NR 04. ORDERED AND RECEIVED NEW FUEL PANEL 522AT PN:85713035-953, COMPLIED WITH M-184.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 11,727 hrs · 12,497 cycles

LEFT WING FUEL ACCESS PANEL 522CT HAS NUMEROUS COUNTERSINKS WITH PITTING CORROSION. COUNTERSUNK HOLES TO MAX ALLOWABLE DEPTH. EVIDENCE OF CORROSION STILL REMAINING. OUT OF LIMITS REF SRM 57-10-35, REPAIR NR 3, 2 CONSECUTIVE HOLES OUT OF LIMITS. NO REPAIR ALLOWED REF SRM 57-10-35, REPAIR -04. ORDERED AND RECEIVED NEW FUEL PANEL 522CT PN:85713039-953, PANEL 522CT INSTALLED ON JOB 5424310, OP 3145.

Part: STRINGER SPLICE — CORRODED (BS 116) · airframe 11,727 hrs · 12,497 cycles

STRINGER SPLICE 24R CORRODED BS 116. FOUND OUT OF LIMITS IAW SRM 53-20-17. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-05, REPAIR -01, SRM 51-42-05, PAR 4D, 51-40-15 PARA 6H, 6J, SRM 51-40-07, REPAIR -01, SRM 51-20-00 PG.14, 51-25-25 PG 201-204, AND SRM 51-25-05, PG.206-207, ITEM (F)1-4.

Part: STRUCTURE — CORRODED · airframe 11,727 hrs · 12,497 cycles

CLIPS CORRODED COMMON TO STR 24, RT AT FS 136.00, FS 156.000, FS 176.000 AND FS 194.000. COMPLIED WITH M-184 FORM 4 CLIPS FOUND OUT OF LIMITS, NO REPAIR ALLOWED REF SRM 53-20-15 STRUCT IDENT-01. REMOVED 4 EA CLIPS AT STR 24S FS X136.000, FS X156.000, FS X176.000 AND FS X194.000, REF SRM 51-42-05, REPAIR-01. INSTALLED 4EA NEW CLIPS AT STR 24S, RT AT FRAME STATIONS FS 136.00, FS 156.00, FS 176.00, FS 194.00 IAW SRM 51-42-05, PAR 4D. FABRICATION OF 4 CLIPS AT STRINGER 24 RT AT FRAME STATIONS 136.00, 156.00, 176.00, 194.00. FABRICATED ON JOB 5424315, OP 138. LOCATED AND DRILL 4 EA CLIPS AT STR 24S FS X136.000, X156.000, X176.000 AND FS X194.000 REF SRM 51-40-07. RESTORED INTERIOR FINISH AT STR 24R AT FRAME STATIONS 136.00, 156.00, 176.00, 194.00 IAW SRM 'S 51-20-00, PG 14, 51-25-25, PGS 201-204.

Part: BRACKET — BROKEN (EXHAUST DUCT) · airframe 11,727 hrs · 12,497 cycles

RT ENGINE FORWARD EXHAUST ASSY HAS A BROKEN BRACKET. TRIMMED AWAY CRACKED AND DAMAGE AREA IAW SRM 54-45-25, REPAIR-26, PROCEDURE 7, STEP A. C/W LPI ON REWORKED AREA REF NDTM PT1 51-00-08. NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR FILLER IAW SRM 54-45-25, REPAIR-26, PROCEDURE 7, STEPS C THRU F USING MIL-T-9046 TITANIUM SHEET PO T25325/4 AND CP TITANIUM ROD PO 102315-4.

Part: SEAT TRACK — CORRODED (NR 15) · airframe 11,727 hrs · 12,497 cycles

SEAT TRACK NR 15 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, SRM 51-42-05-02-01, SRM 51-40-15-02-01, AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (NR 8) · airframe 11,727 hrs · 12,497 cycles

SEAT TRACK NR 8 CORRODED. REMOVED AND REPLACED THE SEAL TRACK IAW SRM 51-42-05, 51-40-15, 51-41-00, SRM 51-42-05 & 51-41-00, AND SRM 51-4007.

Part: GUSSET — CORRODED · airframe 11,727 hrs · 12,497 cycles

TWO GUSSETS CORRODED AT BS 77.8 AND 88.2 COMMON TO EXIT BEAM. REMOVED AND REPLACED THE GUSSETS IAW SRM 51-42-05 AND SRM 51-40-07.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 11,727 hrs · 12,497 cycles

AFT SERVICE DOOR INNER EDGE BEAM IS CORRODED. REMOVED AND REPLACED THE BEAM IAW DWG 85339543, REV-A, NDTM PT1 51-00-06, SRM 51-40-07, SRM 51-21-10-02-01, SRM 51-25-10-02-01, AND DWG 85339541, REV B.

Part: THRESHOLD — CORRODED · airframe 11,727 hrs · 12,497 cycles

THRESHOLD SHOWS EVIDENCE OF CORROSION. FOUND OUT OF LIMITS IAW TC 6-53-1160. REMOVED AND REPLACED THE THRESHOLD IAW SRM 51-42-05 PROCEDURE 4E, SRM 51-42-05, AND SRM 51-40-07.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 11,727 hrs · 12,497 cycles

AFT SERVICE DOOR HAS OUTER EDGE BEAM CORRODED. LOCATED AND DRILLED NEW OUTER EDGE BEAM IAW SRM 51-40-07. INSTALLED NUT PLATES IAW DWG 85339541, REV -B.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 11,727 hrs · 12,947 cycles

TWO GUSSETS CORRODED AT BS 77.8 AND 88.2 COMMON TO EXIT BEAM. REMOVED AND REPLACED THE GUSSETS IAW SRM 51-42-05, SRM 51-42-05, AND SRM 51-40-07.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 11,727 hrs · 12,497 cycles

AFT SERVICE DOOR HAS OUTER EDGE BEAM CORRODED. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-07 AND DWG 85339541, REV -B.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 11,727 hrs · 12,497 cycles

THRESHOLD PLATE SHOWS EVIDENCE OF CORROSION. FOUND OUT OF LIMITS IAW TC 6-53-1160. REMOVED AND REPLACED THE THRESHOLD PLATE IAW SRM 51-42-05, PROCEDURE 4-E, SRM 51-42-05, AND SRM 51-40-07.

Part: SUPPORT — CORRODED · airframe 11,727 hrs · 12,497 cycles

CENTER FUSELAGE AIRSTAIR DOOR REMOVABLE DRAFT BULKHEAD SUPPORT ASSY SHOWS EVIDENCE OF CORROSION. REMOVED SURFACE CORROSION AND FOUDN WITHIN LIMITS IAW SRM 51-21-00 4(A) 1 TO 2 PAGE 2 AND DWG 8Z4844, DETAIL-103 RELEASE P REV-A. RESTORED PROTECTIVE FINISH TO SUPPORT ASSY IAW SRM 51-21-00 4(A)2D AND DWG 8Z4844, DETAIL-03 RELEASE P REV-A.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 11,727 hrs · 12,497 cycles

INNER EDGE CHANNEL AFT PAX DOOR IS CORRODED. REMOVED INNER EDGE CHANNEL IAW DWG 85329514 AND SRM 51-40-07. LOCATED & DRILLED NEW INNER EDGE CHANNEL IAW SRM 51-40-07. INSTALLED INNER EDGE CHANNEL IAW SRM 51-42-05 AND DWG 85334541, REV-B 96/10/02 AND SRM 51-42-45.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 11,727 hrs · 12,497 cycles

AIRSTAIR DOOR SURROUND ANGLES HAVE EVIDENCE OF CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE ANGLES IAW SRM 51-42-05, STEP 4E.

Part: ANGLE — CORRODED · airframe 11,272 hrs · 12,497 cycles

ANGLE AT X26.70 BETWEEN STRINGERS 23-25L CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00 4, A 5 AND DWG 85329542, REL P REV. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-05-02-01 4(E).

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 11,727 hrs · 12,497 cycles

OUTER EDGE CHANNEL AFT PAX DOOR CORRODED. LOCATED AND DRILLED NEW OUTER EDGE CHANNEL IAW SRM 51-40-07. INSTALLED CHANNEL IAW SRM 51-41-05.

Part: ANGLE — CORRODED · airframe 11,727 hrs · 12,497 cycles

ANGLE AT X 6.700 BETWEEN STRINGERS 23 - 25L CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00 4, A 5 AND DWG 85329542. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-05-02-014 E.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 11,359 hrs · 12,099 cycles

GUARDED LIGHT SWITCH FOR EMERGENCY LIGHTS, GREEN NORMAL PART OF SWITCH LIGHT NOT ILLUMINATED. REPLACED THE LAMP, SWITCH OPERATES NORMAL NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (SWITCH) · airframe 11,359 hrs · 12,099 cycles

GUARDED SWITCH LIGHT MARKED "EMERGENCY LIGHTING" NEXT TO FORWARD F/A JUMP SEAT GREEN "NORMAL" PART OF SWITCH LIGHT NOT ILLUMINATED. RELAMPED "NORMAL" PART OF SWITCH, SWITCH OPERATES NORMAL, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (AFT PAX DOOR) · airframe 11,303 hrs · 12,044 cycles

F/A STATED WIND NOISE, SQUEAL FROM AFT PAX DOOR UPPER AFT CORNER OF DOOR. CABIN PRESSURIZATION WAS NORMAL. DIVERTED, LANDING UNEVENTFUL. CHECKED CDS AND NO FAULTS NOTED. COMPLIED WITH A GVI OF THE AFT PASS DOOR SEAL, DOOR FRAME AND VENT DOOR SEAL. COMPLIED WITH A PRESSURIZATION AND DEPRESSURIZATION CHECK IAW AMM 21-00-00-863-801/802 & RIL 84-21-012. RAN PRESSURIZATION DIFF TO 5.5 PSI. NO DOOR SQUEAL NOTED. ACFT OK FOR CONT SERVICE.

Part: BEARING — DAMAGED (SERVICE DOOR) · airframe 10,946 hrs · 11,658 cycles

SERVICE DOOR IS DIFFICULT TO OPEN. R & R AFT SERVICE DOOR HANDLE MECHANISM BEARINGS IAW AMM 52-41-01-000-802, 52-41-01-400-802. DOOR OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 10,569 hrs · 11,259 cycles

AT 23000 FT, FAULT ANNUNCIATOR ON PRESSURIZATION CONTROLLER. MANUAL MODE WORKED FINE. CDS REPORTS "INDICATOR MODULE FAIL" & AFT OUTFLOW VALVE FAIL MESSAGES-CLEARED IND MOD FAIL IAW FIM TASK 21-30-00-810-813. REPLACED AFT OUTFLOW VALVE IAW AMM TASKS 21-31-16-000-801 & 21-31-16-400-801. OPS CK GOOD-NO FURTHER FAULTS FOUND. RETURNED TO SERVICE.

Part: PROBE — UNKNOWN (ZONE 100) · airframe 10,549 hrs · 11,236 cycles

PROPELLER CAUTION LIGHT RAN CHECK LIST RESET THE CAUTION LIGHT WENT OUT NOTICED WITH PROPELLER DEICE ON NO ADVISORY LIGHTS AND NO ELETRICAL DRAW. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INTERROGATED CDS NO CURRENT FAULTS NOTED PERFORMED FUNCTIONAL TEST OF PROPELLERS DEICING SYS IAW AMM 30-61-00-710-801 FUNCTION CHECKED GOOD, ACFT OK FOR SERVICE. IAW MAINTENANCE REQUEST, R & R SAT PROBE IAW AMM 34-11-11-000/400-801. OPS CKS GOOD REPLACED FOR PRECAUTIONARY REASONS.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 10,337 hrs · 11,018 cycles

EMERGENCY LIGHT COME ON WHEN SELECTING EMER LIGHTS SWITCH TO ARM. F/A EMERGENCY LIGHT SWITCH NEAR F/A JUMPSEAT APPEARS TO BE INTERMITTENT. R & R OF EMERGENCY LT SWITCH IAW AMM TASKS 33-51-05-000-801 & 33-51-05-400-801. OPS TESTS GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 10,243 hrs · 10,920 cycles

PASSENGER BAG CAUGHT ON F/A'S EMERGENCY LIGHT SWITCH. SWITCH NOW STUCK IN "IN" POSITION. REPLACED EMERGENCY LIGHT SWITCH IAW IAW AMM 33-51-05-000-801 & 33-51-05-400-801. OPS TESTED GOOD IAW AMM TASK 33-51-00-710-801. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: TIRE — FAILED (NR 3 MLG) · airframe 8,443 hrs · 9,007 cycles

ON ROTATION FOR TAKEOFF, LOUD VIBRATION FELT ON ACFT, AFTER CONTACTING TOWER, THEY ADVISED REMNANTS OF TIRE WERE LEFT ON RUNWAY. C/W WITH INSPECTION OF ACFT AFTER FAILED TIRE, R & R NR 3 MAIN WHEEL ASSY, R & R RT MLG AFT INBD GEAR DOOR. R & R NR 2 PROP NR 1 BLADE ASSY, AC RELEASED FOR SERVICE.

Part: HANDLE — BINDING (AIRSTAIR DOOR) · airframe 8,215 hrs · 8,754 cycles

FUNCTIONAL TEST OF THE AIRSTAIR DOOR TASK 52-11-00-710-802, FAILS STEP 3 A (B). FORCE REQUIRED TO PUSH HANDLE TO THE FULL UNLOCKED POSITION MEASURED AT 63 LBS DOWN FOR REPAIRS.

Part: DOOR — BINDING (MAIN PAX) · airframe 8,215 hrs · 8,754 cycles

F/A REPORTS MCD HARD TO OPEN. FERRIED FOR REPAIRS. ACFT CURRENTLY OUT OF SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 8,188 hrs · 8,719 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED AND LUBED THE AIRSTAIR DOOR IAW TASK 52-11-00-640-801. PERFORMED AN OPS TEST IAW TASK 52-11-00-710-802. PERFORMED A FUNCTIONAL CHECK IAW TASK 52-11-00-720-802. "OPS CHECKED GOOD" NO EXCESSIVE FORCES NOTED. RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 7,830 hrs · 8,324 cycles

BRAKES WEAK ON LANDING ROLLOUT. NO CAUTION LIGHTS NOTED. REPLACED THE NR 2 OTBD WHEEL SPEED TRANSDUCER IAW AMM 32-46-11-000-801 AND 32-46-11-400-801. FUNCTIONAL CHECKED GOOD IAW 32-46-00-720-802. RETURNED TO SERVICE.

Part: WASHER — LOOSE (PAX DOOR) · airframe 7,477 hrs · 7,953 cycles

MAIN CABIN DOOR EXTERNAL HANDLE RUBBER BUMPER WASHER IS LOOSE. BONDED WASHER WITH ADHESIVE. NO DEFECTS NOTED. WASHER BONDED IAW MM 52-11-00-P 549. NOTE 1. RETURNED TO SERVICE.

Part: LIGHT — OVERHEATED (ZONE 200) · airframe 6,335 hrs · 6,763 cycles

F/A REPORTS ELECTRICAL BURNING ODOR IN AFT CABIN AREA. FOUND TO BE LIGHTS IN AFT CARGO COMPARTMENT. REPLACED BOTH AFT CARGO BAY LIGHT ASSYS & TERMINAL LUGS. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 6,276 hrs · 6,705 cycles

EMERGENCY FLOOR PATH LIGHT RUNNING IN FRONT OF THE FORWARD CARGO DOOR IS DETERIORATED. REPLACED IAW AMM 33-51-16-000-801 AND 33-51-16-400-801.

Part: RECEPTACLE — WORN (GALLEY) · airframe 6,222 hrs · 6,652 cycles

LEFT HOT JUG IN GALLEY HAS A ELECTRICAL BURNING SMELL COMING FROM IT. FOUND LT AFT GALLEY MAPCO CONNECTOR TO HAVE SIGNS OF WEAR WHERE PLUG CONNECTS MAPCO, AS WELL AS BURN MARKS ON BACKSIDE OF CONNECTOR. R & R LT MAPCO CONNECTOR AND LT MAPCO. NO BURNING ELECTRICAL SMELL NOTED AND NO OTHER DEFECTS NOTED. MADE SURE TO INSPECT RT AFT MAPCO IN AFT GALLEY AS WELL AS THE MAPCO CONTROL PANEL. NO OTHER DEFECTS NOTED ON EITHER. RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 5,786 hrs · 6,212 cycles

DENT IN LOWER FUSELAGE SKIN 6 INCHES FWD OF FRAME 32.4 MIDWAY BETWEEN STRINGERS. BLENDED SMALL GOUGE IAW RD 8/4-53-666. MIN REMAINING THICKNESS .084", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 PT 4 AND 51-00-01-250-801 PT 6. BLEND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-666. MATERIAL LOSS IS IN LIMITS IAW RD 8/4-53-4489,

Part: FLOOR SUPPORT — CORRODED (BS 783) · airframe 5,786 hrs · 6,212 cycles

AFT CARGO FLOOR SUPPORT AT BS 783 IS CORRODED INBD OF SEAT TRACK 16. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS .073". CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FOUND FLOOR SUPPORT WITHIN LIMITS IAW RD 8/4-53-4473. ALODINED, PRIMED AND PAINTED IAW RD 8/4-53-4473. APPLIED CPC IAW AMM 51-25-01-340-801.

Part: FLOOR SUPPORT — CORRODED (BS 783) · airframe 5,786 hrs · 6,212 cycles

AFT CARGO FLOOR SUPPORT AT STA 783 CORRODED INBD OF SEAT TRACK 9. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS .059". CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FLOOR SUPPORT WITHIN LIMITS IAW RD 8/4-53-4473. ALODINED, PRIMED AND PAINTED IAW RD 8/4-53-4473. APPLIED CPC IAW AMM 51-25-01-340-801.

Part: SEAT TRACK — CORRODED · airframe 5,786 hrs · 6,212 cycles

SEAT TRACK 5 HAS CORROSION BS 32.4-49.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. CONFIRMED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. SEAT TRACK 5 FOUND TO BE WITHIN LIMITS IAW TASK CARD RD 8/4-53-4497. ALODINED IAW TC RD 8/4-53-4497. APPLIED AV DEC TAPE AND SELF LEVELING GREEN IAW RD 8/4-53-4497. C/W TASK CARD 8/4-53-4497.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 5,786 hrs · 6,212 cycles

SEAT TRACK 10 HAS CORROSION UNDER FORWARD BAG PIT MOUNTS. REMOVED CORROSION IAW SRM 51-21-00-00-02. SEAT TRACK FOUND WITH IN LIMITS IAW RD 8/4-53-2358 AND RD 8/4-53-884. CONFIRMED CRACK FREE REF NTM 51-00-06-910-801. ALODINED AND FAST WELD SEAT TRACK IAW RD 8/4-53-2358. COMPLIED WITH RD 8/4-53-884 AND RD 8/4-53-2358.

Part: FRAME — CORRODED (BS 236 S31-32L) · airframe 5,786 hrs · 6,212 cycles

FRAME 236, FLANGE IS CORRODED STR 31P - 32P. REMOVED 3 RIVETS FOM AND BLENDED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .043", CONFIRMED CRACK FREE CONDITION REF NTM 51-00-04-910-801 AND 51-00-06-910-801. BLEND IS WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 258.5 S31-32L) · airframe 5,786 hrs · 6,212 cycles

FRAME 258.5, FLANGE IS CORRODED STR 31P -32P. REMOVED 2 RIVETS FOM AND BLENDED CORROSION ON FRAME IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .043", CONFIRMED CRACK FREE CONDITION REF NTM 51-00-06-910-801 AND 51-00-04-910-801 PT 1. FOUND BLEND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 301 S31-32L) · airframe 5,786 hrs · 6,212 cycles

FRAME 301 FLANGE IS CORRODED STR 31P - 32P. REMOVED 3 RIVETS FOM AND BLENDED CORROSION ON FRAME IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .044", CONFIRMED CRACK FREE CONDITION REF NTM 51-00-06-910-801 AND 51-00-04-910-801 PT 1. FOUND BLEND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 301 S31-33R) · airframe 5,786 hrs · 6,212 cycles

FRAME 301 FLANGES ARE CORRODED STR 31S - 33. REMOVED 4 RIVETS FOM AND BLENDED CORROSION ON FRAME IAW SRM 51-42-05-02-01 AND RD 8/4-53-2344. CONFIRMED CRACK FREE CONDITION, MIN REMAINING THICKNESS .046" REF NTM 51-00-06-910-801 AND 51-00-04-910-801 PT 1. FOUND FLANGE TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 281 S31-32L) · airframe 5,786 hrs · 6,212 cycles

FRAME 281, FLANGE IS CORRODED STR 31P - 32P. REMOVED 4 RIVETS FOM AND BLENDED CORROSION ON FRAME IAW RD 8/4-53-2344. CONFIRMED CRACK FREE CONDITION, MIN REMAINING THICKNESS .044" REF NTM 51-00-06-910-801 AND 51-00-04-910-801 PT 1. FOUND FLANGE TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 258.5 S31-33R) · airframe 5,786 hrs · 6,212 cycles

FRAME 258.5 FLANGES ARE CORRODED STR 33-31S. REMOVED 6 RIVETS AND BLENDED CORROSION IAW RD 8/4-53-2344. MIN REMAINING THICKNESS .043", CONFIRMED CRACK FREE CONDITION REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FLANGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED, TOPCOATED AND CPC IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 5,786 hrs · 6,212 cycles

SEAT TRACK 11 HAS CORROSION BY THE FORWARD BAG BAY MOUNT. REMOVED CORROSION IAW SRM 51-21-00-00-02. SEAT TRACK FOUND TO BE WITH IN LIMITS IAW RD 8/4-53-2358 AND RD 8/4-53-884. CONFIRMED CRACK FREE REF NTM 51-00-06-910-801. ALODINED AND FAST WELDED SEAT TRACK IAW RD 8/4-53-2358. COMPLIED WITH RD 8/4-53-884 AND RD 8/4-53-2358.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,786 hrs · 6,212 cycles

SEAT TRACK 8 HAS A SMALL AREA OF CORROSION STA 644.5-664.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. SEAT TRACK FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. CONFIRMED BLEND CRACK FREE REF NTM 51-00-06-910-801. ALODINED SEAT TRACK IAW RD 8/4-53-884. COMPLIED WITH RD 8/4-53-884.

Part: SEAT TRACK — CORRODED (BS 644.5-664.5) · airframe 5,786 hrs · 6,212 cycles

SEAT TRACK 15 HAS MINOR CORROSION UNDER THE GALLEY MOUNTS 644.5-664.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. TRACK FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. CONFIRMED BLEND CRACK FREE REF NTM 51-00-06-910-801. ALODINED SEAT TRACK IAW RD 8/4-53-884. COMPLIED WITH RD 8/4-53-884.

Part: FRAME — CORRODED (BS 584.5) · airframe 5,786 hrs · 6,212 cycles

FRAME 584.5, FLANGES ARE CORRODED STR 33-31S. REMOVED RIVETS FOM AND BLENDED CORROSION REF RD 8/4-53-2344. CORNFIRMED CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED RIVETS, APPLIED ALUMINIZED COATING, CPC, PRIMER AND TOPCOAT IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 281) · airframe 5,786 hrs · 6,212 cycles

FRAME 281, FLANGE IS CORRODED STR 31S-32S. REMOVED RIVETS FOM AND BLENDED CORROSION REF RD 8/4-53-2344. CONFIRMED CRACK FREE AREA REF NTM 51-00-04-910-801 AND 51-00-06-910-801. FLANGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED RIVETS, APPLIED ALUMINIZED COATING, CPC, PRIMER AND TOPCOAT IAW RD 8/4-53-2344, SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (BS 604) · airframe 5,786 hrs · 6,212 cycles

FRAME 604.5 IS CORRODED STR 31P-32P. REMOVED RIVETS FOM, BLENDED AND REMOVED CORROSION IAW RD 8/4-53-2344 MIN REMAINING THICKNESS, CONFIRMED CRACK FREE AREA REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FRAME FLANGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED AND PRIMED IAW RD 8/4-53-2344. INSTALLED RIVETS, APPLIED ALUMINIZED TOP COAT AND CPC IAW RD 8/4-53-2344. PRIMED AND TOPCOATED IAW SRM 51-25-10-02-01 AND 51-25-05-02-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 3,879 hrs · 4,213 cycles

F/A "B" DETECTED A BURNING RUBBER ODOR NEAR REAR OF CABIN , FLOW CONTROL ON MAX TO COOL CABIN. LATER ON BOTH F/A'S SAW A KIND OF MIST INSIDE CABIN THAT DISAPATED. CONSULTED WITH FLIGHT CREW. NOTED " NO MIST NOTED IN CABIN" C/W SL DH8-400-SL-21-012A NO DEFECTS NOTED. NO ODOR IN CABIN NOTED. INTERROGATED CDS NO FAULTS NOTED. ACFT OK FOR CONT SERVICE. NO PARTS REPLACED.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 2,859 hrs · 3,157 cycles

PDX- FORWARD LEFT HAND EGRESS EMERGENCY LIGHT DOES NOT ILLUMINATE. FOUND THE EPS1 POWER SUPPLY DEPLETED. REPLACED POWER SUPPLY IAW Q400 AMM 33-51-01-000-801. OPERATIONAL CHECKS GOOD.

Part: MONITOR — FAILED (DE ICE SYSTEM) · airframe 2,851 hrs · 3,148 cycles

WHILE CLIMBING THROUGH APPROX 23,000 FT, -25 C, ICING CONDITIONS USING BOOTS GOT DEICE PRESS CAUTION LIGHT. PRESSURE APPEARED GOOD ON GAUGE, BOOTS CYCLING. RAN ENG CHECKLIST, TURNED BOOTS TO MANUAL. AFTER RESET CAUTION LIGHT REOCCURED. LT BOOTS ON, DESCENDED OUT OF ICE IMMEDIATELY IAW EMG CHECKLIST. RETURNED TO THE FIELD. LANDED UNEVENTFUL. INTERROGATED CDS, NO FAULTS FOUND. PERFORMED GVI OF L/E NO DEFECTS NOTED. GROUND RAN ENGINES AND PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYS IAW AMM 30-11-00-720-801, CYCLED PNEUMATIC SYS IN FAST, SLOW, AND MANUAL VARIOUS TIMES FOR 25 MIN AS A PRECAUTION IAW MX CONTROL. R & R TIMER MONITOR UNIT IAW AMM TASK 30-11-01-000-801, AND 30-11-01-400-801. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: OIL SYSTEM — FAILED (NR 2 ENGINE) · airframe 2,756 hrs · 3,039 cycles

ON CLIMBOUT FORM, NR 2 OIL WARNING LIGHT CAME ON AND NR 2 TQ WENT TO 106 PERCENT REDUCED PWR AND FOLLOWED ENG OIL CHECK LIST AT THE STOP & FEATHER POINT ENG SHUTDOWN BY ITSELF BEFORE WE COULD FINISH THE CHECK LIST. COMPLETED CHECK LIST AND RETURNED TO DEPARTURE. (AT THE TIME THE OIL WARNING LIGHT WAS ON THE OIL SYMBOLOGY WAS MISSING ONLY ARC DISPLAYED). LANDING WAS UNEVENTFUL. R & R NR 2 ENGINE IAW NR6710003 AND NR6710004. OPS AND LEAK CHECKS GOOD. ALSO REPLACED NR 2 OIL COOLER. ACFT RETURNED TO SERVICE.

Part: STRUT — DAMAGED (ZONE 700) · airframe 2,681 hrs · 2,947 cycles

FOUND DAMAGE AT RT MLG RT FWD STABILIZER STAY FWD LOWER EDGE APPROX 1" IN LENGTH AND .040 IN DEPTH. FERRIED FOR REPAIRS. REPLACED THE RT MLG STABILIZER STRUT IAW AMM 32-11-16-000-801. RETURNED TO SERVICE.

Part: GENERATOR — FAILED (ZONE 400) · airframe 1,463 hrs · 1,653 cycles

AT ROTATION NR 2 AC GEN CAUTION LIGHT ILLUMINATED. RESET NR 2 AC GEN IAW THE CHECKLIST AND THE CAUTION LIGHT WENT AWAY. RETURNED TO THE FIELD. LANDING UNEVENTFUL. REPLACED THE NR 2 ENGINE AC GENERATOR IAW MX 6242101. OPS CHECK GOOD, LEAK CHECK GOOD, NO OTHER DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE. MX ACTION PERFORMED AS A PRECAUTIONARY MEASURE. NO FAULT CODES NOTED IN EPCU.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER) · airframe 651 hrs · 760 cycles

AFTER LEVELING OFF AT 7000' ON DESCENT INTO AIRPORT/ADVANCED POWER TO MAINTAIN AIRSPEED ( APPROX. 225KTS) WHICH CAUSED ACFT TO BE UNCOORDINATED (BALL OUT TO RT SIDE) APPLIED RT TO RE-COORDINATE. INITIAL APPLICATION OF PRESSURE ON RUDDER (NORMAL PRESSURE) PRODUCED NO MOVEMENT WITH CONTINUED AND INCREASED PRESSURE RUDDER PEDAL BROKE FREE (POPPED FREE). NO OTHER OCCURANCES REMAINDER OF FLIGHT. AUTO PILOT WAS ENGAGED. LANDING UNEVENTFUL. REMOVED FLOORBOARDS AND PANELS TO GAIN ACCESS TO ENTIRE RUDDER CONTROL SYS, INSPECTED FOR CONDITION OF CABLES, PULLEYS AND FOR ANY POSSIBLE DEFECT. NO DEFECT NOTED. RII'S C/W. R & R ORIGINAL YAW DAMPER AFTER GVI NO DEFECT NOTED. NO DEFECTS WERE NOTED DURING ALL RIGGING & OPS CHECKS. PERFORMED OPS CHECK/TEST OF RUD. CONTROL SYS. NO DEFECTS NOTED. FREEDOM OF MOVEMENT CHECK FROM PILOT AND CO-PILOT POSITIONS, NO DEFECT OR JAMS NOTED. REPLACED RUDDER FEEL AND SUMMING UNIT ALL OPS CHECKS GOOD NO DEFECTS NOTED. CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (COMMS) · airframe 292 hrs · 335 cycles

BLEED OVER FROM NR 1 COMM 120.400 TO NR 2 COMM 132.000. BLEED OVER OCCURS WHEN TRANSMITTING ON 120.400 ONLY. BLEED OVER IS VERY CLEAR AND DISTRACTIONG ON THE NR 2 COMM. OUTSIDE THE SCOPE OF THE SL. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R VHF NR 1 AND VHF NR 2 TRANSCEIVERS AS PRECAUTIONARY MEASURE IAW AMM TASKS 23-11-01-000-801/400-801. WHILE PERFORMING GVI OF NR 1 AND NR 2 VHF COMM ANTENNAS FOUND HAIRLINE CRACKS AT BASE OF NR 1 ANTENNA. R & R NR 1 VHF COMM ANTENAS IAW AMM TASK NR 23-11-00-710-801. CONTACTED FOR DEPARTURE ON FREQUENCY 120.400 SEVERAL TIMES WITH NO BLEED OVER. ACFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 235 hrs · 259 cycles

BURNING ELECTRICAL ODOR IN AFT GALLEY. INSPECTED AFT GALLEY AND AFT CABIN FOR ELECTRICAL ODOR. COULD NOT DUPLICATE PROBLEM. NO OTHER DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE.