N436QX

Part: INTERCOSTAL — DAMAGED (ZONE 800) · airframe 28,633 hrs · 30,985 cycles

RAMP REPORTS AFT CARGO DOOR WILL NOT CLOSE. REMOVED FROM SERVICE. PERFORMED GVI OF AFT CARGO DOOR AND FOUND MISALIGNED AND DOOR HANDLE HAD MINIMAL ROTATION. PERFORMED DOOR RESET AND OPS TEST PER AMM 52-31-00-710-801 AND 52-31-00-840-801 WITH NEGATIVE RESULTS. DOOR IS MISALIGNED AND HANDLE BARELY ROTATES. PERFORMED DOOR RESET IAW 52-31-00-840-801. COULD NOT GET HANDLE TO MOVE. REMOVED DOOR LINERS AND FOUND MECHANISM OVER ROTATED AND STRUCTURE DADMAGED. DAMAGE TO INTERCOSTAL. AIRCRAFT DOWN FOR REPAIRS.

Part: SENSOR — FAULTED (AFT PAX DOOR) · airframe 28,173 hrs · 30,518 cycles

ON TAKEOFF, FUSELAGE DOORS WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF. REMOVED FROM SERVICE. INTERROGATED PSEU, FOUND APDRLK SENSOR FAULTED. C/W MEL 52-10-5(A) MTX PROCEDURE INCLUDING DISCONNECTION OF AFT PAX DOOR LOCK SENSOR VIA CLIPPING AND STOWING WIRE. CONTINUE MEL. AIRCRAFT RETURNED TO SERVICE

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,796 hrs · 30,138 cycles

SEAT RAIL 11 FROM FSX10.50-X102.50, Y9.250 IS CORRODED BEYOND LIMITS. SEAT RAIL 11 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-05-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,796 hrs · 30,138 cycles

SEAT RAIL 10 FROM FSX-39.00 -X10.50, Y9.250 CORRODED BEYOND LIMITS. SEAT RAIL 10 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-05-00-01, 51-42-75-02-01.

Part: SPAR — CRACKED (ELEVATOR) · airframe 27,796 hrs · 30,138 cycles

RH 2 ELEVATOR PCU TO H-STAB REAR SPAR FITTING IS CRACKED. RH 2 ELEVATOR PCU H-STAB REAR SPAR FITTING REPLACED. REFER TO HRZ WO 284143 TC SB84-55-09/B FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 668-783) · airframe 27,796 hrs · 30,138 cycles

SEAT RAIL 9 FROM FSX668.00-X783.00 CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 9 IAW SRM 51-42-05-02-01, AND 51-4015-02-01.

Part: SEAT TRACK — DAMAGED (BS 571-670) · airframe 27,796 hrs · 30,138 cycles

SEAT RAIL 8 FROM FSX571.5-X670,Y-9.250 BLENDED BEYOND LIMITS. REPLACED SEAT RAIL 8 IAW SRM 51-42-05-002-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (BS 670-698) · airframe 27,796 hrs · 30,138 cycles

EQUIPMENT RAIL 23 FROM FSX670-X698 IS CORRODED BEYOND LIMITS. REPLACED EQUIPMENT RAIL 23 IAW SRM 51-42-05-02-01, 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (BS 670-698) · airframe 27,796 hrs · 30,138 cycles

EQUIPMENT RAIL 25 FROM FSX670-X698,Y-24 IS CORRODED BEYOND LIMITS. REPLACED EQUIPMENT RAIL 25 IAW SRM 51-40-07-02-01, 51-42-05-02-01, 51-42-45-02-01.

Part: PROCESSOR — MALFUNCTIONED (I/O UNIT) · airframe 27,746 hrs · 30,092 cycles

ENROUTE AT FL 240 RECEIVED TCAS FAIL ELEV FEEL CAU, DEICE PRESS CAU, IOP2 FAIL MESSAGES.DIVERTED LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS & FOUND "NO DATA FROM IOP2" REPLACED IOP2 PER FIM TASK 31-41-06-810-806 & MTC 6314101 OPS TEST GOOD AIRCRAFT REMAINS CAT III STATUS PLACARD REFLECTS CAT III MTX CTL NOTIFIED. RETURNED TO SERVICE.

Part: FILTER — NOT REPORTED · airframe 27,654 hrs · 30,015 cycles

CLIMBING THROUGH 17000 EXPERIENCED A FLT COMPARTMENT & CABIN DUCT HOT LIGHTS WITH A CABIN PRESS LIGHT. CABIN WOULD NOT PRESSURIZE NORMALLY,(CABIN CLIMBING) RAN DUCT HOT CHECK LIST, TRIED MANUAL PRESSURIZATION TO NO EFFECT, RECYCLED FLT COMPARTMENT PACK SWITCH FROM NORMAL TO OFF TO AUTO AND SYSTEM RESTARED NORMAL PRESSURIZATION FOR REMAINDER OF FLIGHT. REMOVED FROM SERVICE. CDS SHOWS FAULTS 7111 FLT DECK OVER TEMP 1 AND 7114 FD OVR TMP 4 IN FAULT HISTORY. NO CURRENT FAULTS. C/W FIM TASK 21-60-00-810-803. OS TEST OF ECS TEMP CONTROL. TEST GOOD WITH NO FAULTS. CABIN PRESS CAUTION AND PRESSURIZATION ISSUES ARE NORMAL OPERATION WHEN FAULT 7111 FLT DECK OVR TEMP 1. THIS FAULT SHUTS DOWN THE ACM. ECS TEMP CONTROL TEST GOOD WITH NO DEFECTS FOUND. REF AMM 21-61-00-710-803. C/W FIM TASK 21-60-00-810-870 AND 873. REPLACED PACK FLOW CONTROL/SHUT OFF AND FD PACK BYPASS VALVE FILTERS. ECS OPS TEST GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 26,881 hrs · 29,248 cycles

FLIGHT ATTENDANT ADVISE FLOOR STRIP LIGHTING IN FRONT OF 1 AB IS DETACHED. REMOVED FROM SERVICE. RESECURED FLOOR STRIP, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 26,776 hrs · 29,120 cycles

EMERGENCY FLOOR PATH LIGHT AT FORWARD CARPET IS DISCOLORED. REPLACED FLOOR PATH LIGHTING STRIP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,776 hrs · 29,120 cycles

MULTIPLE EMERGENCY LIGHTS IN AFT CABIN DO NOT ILLUMINATE DURING 10 MINUTE SELF TEST. REPLACED BATTERY PACK.

Part: DITCHING DAM — UNWANTED DEPLOY (PAX DOOR) · airframe 26,747 hrs · 29,089 cycles

RAMP AGENT ADVISED MAIN CABIN DOOR DITCHING DAM DEPLOYED. REMOVED FROM SERVICE. STOWED DITCHING DAM AT L1 DOOR, NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,612 hrs · 28,944 cycles

DURING CLIMB, FAULT LIGHT ON PRESSURIZATION CONTROLLER ILLUMINATED AND CABIN STARTED TO DEPRESSURIZE. FAULT LIGHT EXTINGUISHED APPROXIMATELY 20 SECONDS LATER WITH NO CREW INPUT, AND CABIN PRESSURE RETURNED TO NORMAL RANGE, AND WAS NORMAL FOR REMAINDER OF FLIGHT. WHILE FAULT LIGHT WAS ILLUMINATED, A RUSHING AIR SOUND WAS HEARD ON THE FLIGHT DECK WHICH STOPPED WHEN THE FAULT LIGHT EXTINGUISHED. REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, REF Q400 AMM TASKS 21-31-06-000-801 AND 21-31-06-400-801 (DUE TO HISTORY OF CPC THAT WAS ON AIRCRAFT WHEN FAULT OCCURRED). CPC OPERATIONS CHECK GOOD. GROUND PRESSURIZED AIRCRAFT, REF AMM TASKS 21-00-00-863-801/802. PRESSURIZATION CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: STOP — DAMAGED (PAX DOOR HANDLE) · airframe 26,282 hrs · 28,688 cycles

FORWARD PASSENGER DOOR HANDLE STOP GUIDE BUMPER TORN. REMOVED FROM SERVICE. REPLACED MAIN CABIN DOOR HANDLE BUMPER. RETURNED TO SERVICE.

Part: INDICATOR — INOPERATIVE (CABIN PRESSURE) · airframe 26,155 hrs · 28,451 cycles

CABIN DIFF DURING FLIGHT INDICATED 0. CABIN ALT REMAINED AT = 3000' DURING FLIGHT A DESCENT. CABIN RATE OF CLIMB INDICATED 0 DURING FLIGHT. NO FAULT ON CPC. AIRCRAFT WAS PRESSURIZED. (CABIN DIFF PRESSURE INDICATOR - UNPRESSURIZED). REMOVED FROM SERVICE. FOR R&R OF CABIN INDICATION MODULE. PERFORMED FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL IAW AMM 21-31-00-720-801. CABIN DIFF PRESSURE INDICATES NORMALLY. PLACARDS REMOVED, CLEARS MEL. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,151 hrs · 28,444 cycles

CLIMBING THROUGH F210 A RUSHING AIR SOUND WAS HEARD IN THE FLT DECK. ACFT STARTED TO SLOWLY DEPRESSURIZE. THE FAULT LIGHT ILLUMINATED ON THE CPC. WE STARTED A DESCENT. AFTER DESCENDING APPROX 2,000' THE FAULT LIGHT EXTINGUISHED AND CABIN PRESSURE RETURNED TO NORMAL. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R&R CPC CONTROLLER AS PRECAUTIONARY. OPS CK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STOP — RECESSED (PAX DOOR HANDLE) · airframe 26,097 hrs · 28,385 cycles

DURING WALK AROUND, NOTICED MCD HANDLE TO BE RECESSED. REMOVED FROM SERVICE. REMOVED AND REPLACED THE MCD HANDLE BUMPER . OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,979 hrs · 28,257 cycles

RH FWD EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RH FWD EXTERIOR EMERGENCY LIGHT IAW Q400 33-51-11-000/400-801.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 25,335 hrs · 27,530 cycles

PHOTO LUMINESCENT STRIP PEELING UP NEXT TO 2 D/E. REMOVED FROM SERVICE. RE SECURED PHOTO LUMINESCENT STRIP AS REQUIRED.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 25,302 hrs · 27,495 cycles

PHOTO- LUMINESCENT STRIP FORWARD OF ROW 2 SEAT E,D IS LOOSE. REMOVED FROM SERVICE. RE SECURED ROW 2 E,D STRIP IN REF WITH Q 400 MCN 625721-1 ISSUE 4 NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 24,835 hrs · 26,958 cycles

FLOOR MOLDING LOOSE AT SEATS 2E/D. REMOVED FROM SERVICE. RESECURED EMERGENCY FLOOR PATH LIGHTING AT SEAT 2D/E IAW AMM 33-51-16-400-801. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — CHAFED (HYDRAULIC SYS) · airframe 24,640 hrs · 26,740 cycles

AFTER TAXI-OUT, BEFORE TAKING THE RUNWAY, #2 ENG HYD PUMP CAUTION ILLUMINATED. ONE MINUTE LATER, #2 HYDRAULIC PRESSURE FELL TO ZERO AND SPLR OUTBD, ROLL SPLR OUTBRD HYD AND #2 RUD HYD CAUTIONS ILLUMINATED. SIMULTANEOUSLY, WE LOST STEERING AND GOT A PTU FAIL ON THE SWITCHLIGHT. WE RAN THE APPROPRIATE E/A CHECKLIST WHICH DIRECTED US TO PULL HYD PWR XFER C/B. ALSO #2 HYD ISO VLV CAUTION ILLUMINATED. REMOVED FROM SERVICE. #2 HYD SOV IS CLOSED WITH FIRE T HANDLE PUSHED IN AND FLUID QTY FULL. DURING TROUBLESHOOTING FOUND PIN A AT #2 RESERVOIR QTY SWITCH CONNECTOR TO HAVE 110 OHMS TO GROUND. MANIPULATED WIRE HARNESS NEAR CONNECTOR AND GROUND WENT AWAY. FOUND WIRE 2911-W3A-22WHT/BLK CHAFED THRU APP 3 FT FROM CONNECTOR 2911-P18 ENVIRONMENTALLY SPLICED WIRE 2911-W3A-22 WHT/BLK AND REPLACED AND RETERMINATED CONNECTOR 2911-P18 IAW WM 29-11-00 AND 20-15-05. OPS CK OF SELECTOR VALVE CHECKED GOOD. REPLACED #22 EDP REF AMM TASK 29-11-01-000-801 AND 29-11-01-400-801, AS PRECAUTIONARY MEASURE. NO CONTAMINATION FOUND ON EDP CASE DRAIN FILTER OR SYSTEM CASE DRAIN FILTER. NO ROTATING GROUP FAILURE. PERFORMED OPS CHECK OF PTU REF AMM TASK 29-11-61-710-801. NO DEFECTS NOTED. EDP OPS AND LEAK CHECKS GOOD. HYD PWR XFER C/W RESET. AIRCRAFT RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (ZONE 200) · airframe 24,600 hrs · 26,694 cycles

T/O WARN HORN BEEPED ONCE AT V1 109 KNOTS. REMOVED FROM SERVICE. REPLACED FCECU. OPERATIONAL CECHK FLIGHT GOOD. RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,599 hrs · 26,693 cycles

ON TAKE OFF ROLL T/O WARN HORN BEEPED ONE TIME AT APPROX 100KTS. REMOVED FROM SERVICE. FOLLOWED FIM IAW FIM 31-52-00-810-802. SECTION 3. A (1-2). OPS TEST PASSED. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE., NO PARTS REPLACED.

Part: LATCH — DAMAGED (FUEL PANEL) · airframe 24,355 hrs · 26,394 cycles

DURING ARRIVAL CHECK, NOTICED THE REFUEL/DEFUEL ACCESS DOOR LATCHED BELOW FLUS WHEN LATCHED AND ABOUT 25% OF THE LEFT LATCH CLOSE PLATE IS BROKEN OFF. REPLACED THE LEFT AND RIGHT LATCHES ON THE REFUEL/DEFUEL ACCESS DOOR IAW SRM 51-42-05 REPAIR 01.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 24,199 hrs · 26,213 cycles

#1 AC GEN CAUTION LILGHT ILLUMINATED AFTER APPLICATION OF TAKEOFF POWER. TAKEOFF ABORTED AT 60 KNOTS. REMOVED FROM SERVICE. FOUND EPCU FAULT CODE 27. INTERROGATED CDS FOR CHIP DETECTOR FAULTS. NO FAULTS FOUND. REMOVED AND REPLACED #1 AC GEN IAW Q400 MTC 6242101. PERFORMED LEAK CHECK AND OPS TEST. BOTH CHECK GOOD. #1 AC GEN LIGHT REMAINED EXTINGUISHED. INTERROGATED EPCU FOR FAULTS. NO FAULTS FOUND. NO FURTHER DEFECTS NOTED. INTERROGATED CDS FOR FAULTS.NO FAULTS FOUND. RETURNED TO SERVICE.

Part: BEARING — FAILED (MLG) · airframe 24,017 hrs · 25,987 cycles

INBD ANTISKID CAUTION ILLUMINATED AFTER NORMAL LANDING, F/A REPORTED SMOKE FROM RIGHT LANDING GEAR ON TAXI IN. FIRE OBSERVED FROM RIGHT BRAKE BY PASSENGERS AND GROUND PERSONAL. CFR RESPONDED TO AIRCRAFT. FIRE WAS OUT BY THE TIME CFR ARRIVED. STATION OPERATIONS REPORTED HYDRAULIC FLUID AND BRAKE PARTS ON THE RUNWAY. AIRCRAFT WAS TOWED FROM TAXIWAY TO THE GATE. REMOVED FROM SERVICE. POST FLIGHT INSPECTIONS SHOWS #3 MAIN WHEEL OUTBOARD HUB BEARING HAS SIGNIFICANT DAMAGE. REMOVED #3 WHEEL ASSY REF AMM 32-24-01-00-801 AS 90460. PERFORMED INSPECTION OF #2 MLG REF AMM 05-50-17-210-80. REPLACED #3 WHEEL ASSY , REF MTC 6324101. ALSO REPLACED #3 TIRE, #3 BRAKE, #3 WHEEL SPEED TRANSDUCER, #3 ALG AXLE. ALL DAMAGED BY WHEEL BEARING FAILURE. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 23,866 hrs · 25,807 cycles

PLASTIC GUARD OVER F/A EMERGENCY LIGHT SWITCH BY MAIN CABIN DOOR BROKEN. REMOVED FROM SERVICE. PERFROMED REMOVAL & INSTALLATION OF FOWARD LOWER WARDROBE WITH WARDROBE INSERT TO FACILITATE OTHER MTX IAW AMM TASK 25-24-03-000-803/400-803. R&R PLASTIC GUARD OVER FA EMERGENCY LIGHT SWITCH, OPS CHECK GOOD. NO FUTHER DEFECTS. RETURNED TO SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 23,326 hrs · 25,171 cycles

DURING CLIMB THROUGH 11000FT WE GOT CABIN PRESS WARNING. RAN CHECKLIST AND NORMAL DESCENT. ALSO GOT FAULT LIGHT ON PRESSURIZATION CONTROL PANEL. RAN CHECKLIST, WENT MANUAL AND BACK TO AUTO. FAULT LIGHT CLEARED BUT MAN DIFF WAS STILL AT ZERO. CABIN ALT RATE MAINTAIN SAME ALT AS AIRCRAFT. EMERGENCY WAS DECLARED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED DOOR SEALS, NO DEFECTS FOUND, PRESSURIZED A/C NO LEAKS FOUND. INTERROGATED CDS + FOUND CBPC OUTFLOW VALVE FAIL MSG. REPLACED OUTFLOW VALVE PER AMM TASKS 21-31-16-00-801 + 21-31-16-400-801 OPS CHECK GOOD. UNABLE TO DUPLICATE PROBLEM, OUTFLOW VAVLE REPLACED AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (LT MLG DOWNLOCK) · airframe 23,169 hrs · 24,964 cycles

AFTER GEAR SELECTION, AMBER "L DOOR" AND RED "LEFT" INDICATOR PER E/A CHECKLIST, LANDING GEAR ALTERNATE EXTENSION INDICATOR LIGHT IDICATED 3 GREEN, "GEAR SAFE FOR LANDING". REMOVED FROM SERVICE. CYCLED A/C POWER @ GATE. RED LIGT GEAR INDICATOR EXTINGUISHED AND LEFT GREEN INDICATOR ILLUMINATED. L DOOR AMBER LIGHT REMAINED ON. GEAR PINS INSTALLED.UPON A/C ARRIVAL @ GATE, L/H AFT GEAR DOORS WERE OPEN. REPLACED L/H MLG #1 DOWNLOCK SENSOR. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 22,892 hrs · 24,683 cycles

PROP DEICE CAUTION ILLUMINATED IN FLIGHT WHEN NR 1 PROP WAS SELECTED ON ( PROP DEICE SYSTEM INOP ). DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED GROUND RUN & C/W OPS. CHECK OF PROP. DEICE SYSTEM. FOUND PROP. DEICE CAUTION LIGHT ILLUMINATING DURING NR 2 PROP CYCLE. C/W AMM TASK 30-61-00-760-801. FOUND NR 1 & NR 4 DEICE LEADS WITH HIGHER RESISTANCE ON NR 2 PROP. REMOVED & REPLACED NR 2 PROP DEICE LEADS ON NR 1 & NR 4 BLADES. IAW AMM TASK 61-10-06-000/-400-805. FUNCTIONAL CHECK GOOD. CLEARS MEL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 22,844 hrs · 24,627 cycles

NR 4 EMERGENCY LIGHT POWER SUPPLY FAILED DISCHARGE TEST. R&R NR 4 EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-000/400-801. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED HOT) · airframe 22,416 hrs · 24,150 cycles

ON TAKE OFF ROLL, DUAL NR 1 AND 2 BLEED HOT CAUTION LIGHTS ILLUMINATED. SPEED LESS THEN 50 KIAS, TAKEOFF ABORTED. RAN THE CHECKLIST POST ABORT. BOTH LIGHTS EXTINGUISHED AND DID NOT REAPPEAR. REMOVED FROM SERVICE. CDS FOUND NO CURRENT FAULTS. PERFORMED FIM 36-20-00-810-805, NR 1 AND 2 BLEED HOT CAUTION. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: BUMPER — BROKEN (PAX DOOR) · airframe 22,340 hrs · 24,058 cycles

MAIN CABIN DOOR WILL NOT OPEN. REMOVED FROM SERVICE. FOUND EXTERIOR DOOR HANDLE RUBBER BUMPER BROKEN. REPLACED BUMPER IAW AMM 52-11-11-400-800, PAR 1-3 G AND 5. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

CORROSION IN MULTIPLE LOCATIONS ON SEAT TRACK 2 FROM FS X 229.50 TO FS X 571.50 LBL Y40. SEAT TRACK 2 FROM FSX 229.50- X571.50 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01 & 51-42-045-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

CORROSION IN MULTIPLE LOCATION ON SEAT TRACK 13 FROM FS 228.50 TO FS 570 RBL 9.25. REMOVED AND REPLACED SEAT TRACK 13 FROM FS 228.50 TO FS 570 RBL 9.25 IAW SRM 51-42-05, 51-40-15, 51-41-05, 51-40-07.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

FWD BAGGAGE DOOR SILL CORRODED IN SEVERAL AREAS. FWD BAGGAGE DOOR SILL REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-15-02-01 & 51-42-45-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

CORROSION IN MULTIPLE LOCATIONS ON SEAT TRACK 18 FROM FS X 102.50 TO FS X 229.50 RBL Y 40. REMOVED AND REPLACED SEAT TRACK 18 FROM FSX 102.5 TO FSX 229.5 RBL Y 40 IAW SRM 51-40-15-02-01, 51-42-05-02-01 AND 51-42-45-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

CORROSION IN MULTIPLE LOCATIONS ON SEAT TRACK 20 FROM FS X 571.50 TO FS X 670 RBL Y 40. SEAT TRACK 20 FROM FSX 571.50 TO FSX 670 RBL Y 40. REMOVED AND REPLACED WITH NEW SERVICEABLE PART IAW SRM 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,327 hrs · 24,046 cycles

CORROSION ON SEAT TRACK 10 FROM FS X -39 TO FS X 10.50 RBL Y 9.25. SEAT TRACK 10 REMOVED AND REPLACED WITH NEW SERVICEABLE PART AT FS X -39 TO FS X 10.50 RBL Y 9.25 IAW SRM 51-40-15-02-01, 51-42-08-02-01, AND 51-41-05-00-01. BONDING CHECK OF THE GROUNDING POINTS ON THE NEW INSTALLATION CARRIED OUT IAW AMM 51-80-00-260-818.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 22,105 hrs · 23,790 cycles

FWD CARGO DOOR WARNING LIGHT AFTER TAKE OFF. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. UPON INSPECTION FOUND FWD CARGO DOOR HANDLE NOT SECURE. PERFORMED OPS TEST OF FWD BAG DOOR IAW TASK 52-32-00-710-801 NO DEFECTS NOTED. O.K. FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 21,938 hrs · 23,606 cycles

EMERGENCY LIGHT STRIP IN FROUNT OF ROW 2 D & E DETACHED. REINSTALLED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-16-400-801. RETURNED TO SERVICE.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 21,718 hrs · 23,390 cycles

COVER ON THE FLOOR GLOW STRIP BROKEN. SECURED THE COVER. NO OTHER DEFECTS. RETURNED TO SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 21,718 hrs · 23,390 cycles

EMERGENCY LIGHT LENS BROKEN IN MID CABIN BY SEAT 8AB. REMOVED AND REPLACED IAW AMM 33-51-00-210-801. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (ROW 2ED FLOOR) · airframe 19,603 hrs · 20,898 cycles

FLOOR TRACK LIGHT IS LOOSE. SECURED THE LIGHT AT ROW 2ED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WHEEL — VIBRATION (NLG) · airframe 20,423 hrs · 22,085 cycles

ON DEPARTURE BETWEEN 90-100 KTS, THERE WAS SIGNIFICANT NOSE WHEEL VIBRATION. AFTER THE GEAR DOOR HAD CLOSED, VIBRATION STOPPED AFTER 8 SECONDS. NOTICED SEVERE VIBRATION DURING INTIAL BRAKING UPON LANDING. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 AND NR 2 NLG WHEEL AND TIRE ASSY'S IAW TASK CARD 6324102. NO OTHER DEFECTS NOTED.RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (AUTOFEATHER SYS) · airframe 19,696 hrs · 21,302 cycles

DURING DAILY CHECK, THE NR 1 AUTOFEATHER TEST INDICATED ABORT IN AMBER. NO FAULTS IN CDS PERTAINING TO AUTOFEATHER SYSTEM. COMPLIED WITH AN OPS CHECK OF PROPELLER AUTOFEATHER SYSTEM IAW MM 61-20-00-710-805. OPS CHECKED GOOD. FAULT DID NOT RETURN. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 19,482 hrs · 21,088 cycles

LUMINESCENT LIGHTING STRIP AT 2D&E LOOSE. RE-SECURED LUMINESCENT LIGHTING STRIP AT 2D&E. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (WHEEL SPEED) · airframe 19,353 hrs · 20,948 cycles

DURING TAKEOFF AT 40 KTS, OUTBOARD ANTISKID CAUTION ILLUMINATED. ABORTED THE TAKE OFF AND RETURNED TO GATE. REMOVED THE RT OTBD. MAIN SHEEL HUBCAP INSPECTED AND REINSTALLED HUBCAP. NO DEFECTS NOTED. WHEEL SPEED GENERATOR WAS NOT REMOVED IAW APPLICABLE PORTIONS OF AMM TASK 32-46-11-000-801 AND 32-46-11-400-801 NR 59880. INTEROGATED CDS AND FOUND FAULT FOR LT OTBD WHEEL SPEED TRANSDUCER. REMOVED AND REPLACED THE NR 1 WST AND HUB CAP DUE TO DAMAGE IAW AMM TASK 32-46-11-000-801,32-46-11-400-801. CLEARED CDS FAULT AND NO OTHER DEFECTS FOUND AT THIS TIME OPS TESTED GOOD. COMPLIED WITH FUNCTIONAL TEST OF THE ANTI-SKID CONTROL SYSTEM USING BUILT IN TEST IAW 32-46-00-720-801 FUNCTIONAL TESTED GOOD.

Part: AILERON — OUT OF RIG (WING) · airframe 19,234 hrs · 20,619 cycles

AIRCRAFT ROLLS TO THE LEFT WITH CONTROL YOKES NEUTRAL FUEL WAS BALANCED AND TRIM NEUTRAL THIS OCCURRED WITH AP ON AND OFF. LANDING UNEVENTFUL. RIGGED AILERON SYSTEM IAW AMM 27-10-00-830-805. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 18,230 hrs · 19,705 cycles

FORWARD EMERGENCY LIGHT SWITCH BY MAIN CABIN DOOR INOPERATIVE. REPLACED THE LAMPS IN THE SWITCH. CHECKED GOOD. RETURNED TO SERVICE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 18,076 hrs · 19,528 cycles

PRESSURIZATION FAULT AFTER TAKEOFF. CYCLED SELECTOR PER THE EMERGENCY CHECKLIST AND FAULT LIGHT WENT OUT AND SYSTEM OPERATED NORMALLY. ACCOMPLISHED THE FSM CPCS FAULT RESET PROCEDURE. FAULT DID NOT RETURN. RETURNED TO SERVICE.

Part: DOOR — BINDING (AFT PAX) · airframe 17,077 hrs · 18,441 cycles

AFT PASSENGER DOOR STICKING. RESET THE AFT PASSENGER DOOR IAW AMM TASK 52-00-00-810-801. DOOR CHECKS GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,053 hrs · 18,409 cycles

AT CRUISE 19,000 SMELLED SMOKE ODOR WITH NO VISIBLE SMOKE IN COCKPIT - F/A'S DID NO ODOR. NO ABNORMAL INDICATIONS IN COCKPIT. COMPLETED AIR CONTAMINATION CHECKLIST FORM M-744. PERFORMED GVI OF COCKPIT, FWD CABIN, LAVAORY AND FWD BAGGAGE COMPARTMENT. NO DEFECTS NOTED. CHECKED NR 1 AND NR 2 ENGINE OIL QUANTITY. NO DEFECTS NOTED. C/W REMOVAL OF ODOUR FROM AIR CONDITIONING DUCTS IAW AMM TASK 21-00-00-160-801. RAN APU WITH BLEED AIR SELECTED ON AND RECURIC FAN SELECTED ON FOR 20 MINUTES. NO ABNORMAL ODORS NOTED. GROUND RAN BOTH ENGINES, BLEED 1 AND 2 SELECTED ON, RECURIC FAN SELECTED ON, PACKS IN AUTO. RAN ENGINES FOR APPROX 25 MINUTES AT VARIOUS POWER SETTINGS FROM DISC TO RATING. NO ABNORMAL ODORS NOTED. RETURNED TO SERVICE.

Part: SKIN — DENTED (RUDDER) · airframe 16,786 hrs · 18,116 cycles

FORE RUDDER LT SIDE SKIN DENTED JUST UNDER TOP HINGE FOR TAIL RUDDER, MARKED. RECEIVED ENGINEERING DOCUMENTATION IAW TASK CARD RD 8/4-35-1240. C/W ET INSP IAW RD 8/4-55-1240, ISSUE 1, NO DEFECTS NOTED. RECEIVED HORIZON TASKCARD RD 8/4-55-1240. COMPLIED WITH HORIZON TASKCARD. RD 8/4-55-1240. RESTORED FINISH AS NEEDED TO REPAIRED AREA REF SRM 51-25-05, PG 206-207, ITEM (F) 1-4.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,786 hrs · 18,116 cycles

FOUND CORROSION ON COUNTERSINK AREA OF ACCESS PANEL. REPAIRED IAW SRM 54-10-35, REPAIR -03. STILL HAVE CORROSION AND GOUGE FOUND TO BE OUT OF LIMITS REF SRM 57-10-35, REPAIR -03 ITEM 6A. RECEIVED NEW FROM STORES PANEL 622AT. INSTALLATION ACCOMPLISHED.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON THE FORWARD PASSENGER DOOR LOWER MAIN SILL, PN 85329349 AT BS X 30.00. LAYER OUT PATTERN FOR LWR MAIN SILL FWD AND AFT REPAIR DOUBLERS REF SRM 53-20-17-02-02, FIG 201, SHEETS 3 AND SHEET 4. FABRICATED AFT LOWER EXTERNAL DOUBLER FROM 2024-T3.063", PO;TX-3823/1, AND LOCATED AND DRILLED REF SRM 53-20-17-02-02, FIG 201. FABRICATED AFT UPPER EXTERNAL REPAIR DOUBLER FROM 2024-T3.063, PO:TX-3823, LOCATED AND DRILLED, REF SRM 53-20-17-02-02. FABRICATED BOTH FWD LOWER AND UPPER REPAIR DOUBLERS FROM 2024-T3.063, PO:TX-3823, LOCATED AND DRILLED BOTH DOUBLERS, REF SRM 53-20-17-02-02. ALODINED AND PRIMED 4 EA REPAIR DOUBLERS REF SRM 51-25-10-02-01. REPAIRED THE EXISTING COUNTERSINKS REMAINING IN THE SKIN UNDERNEATH THE EXTERNAL REPAIR DOUBLERS, FWD AND AFT REF SRM 53-20-17-02-02, STEP 7.I. INSTALLED FWD AND AFT EXTERNAL REPAIR DOUBLERS REF SRM 53-20-17-02-02. SEALED AROUND EXTERNAL EDGES OF DOUBLERS REF SRM 51-23-00, SRM 53-20-17, STEP 7N, REPAIR 02. PRIMED EXTERNAL DOUBLERS FWD AND AFT REF SRM 53-20-17-02-02. PREPPED AND PAINTED FWD PAX DOOR LOWER EXTERIOR THRESHOLD AREA REF SRM 51-25-05, PG 206-207, ITEM (F)1-4. FABRICATED NEW LOWER MAIN SILL FROM NEW STR 25 STOCK, PN 85329349, LOCATED AND DRILLED, REF SRM 53-20-17, STEP 7E, INSTALLATION ACCOMPLISHED ON TASK CARD 6-53-1160 FWD PASSENGER DOOR JOB 5423635, OP 5464. INSTALLED LOWER MAIN SILL, PN 85329349-101, REF DWG 85329330, REV A.

Part: THRESHOLD — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EMERGENCY EXIT THRESHOLD BEAM ASSY CORRODED. LOCATED AND DRILLED EDGE BEAM FOR EMERGENCY EXIT DOOR, PN 85329514-101 REF SRM 51-40-07. APPLIED MOSITURE DIS PAINT ALLUMINIZED PAINT ON EDGE BEAM, PN 85329514-101, REF SRM 51-25-15. APPLIED AVDEC UNDER NUTPLATES AND INSTALLED NUTPLATES IAW SRM 51-42-75. TOUCHED UP MOISTURE DIS PAINT UNDER THRESHOLD PLATE AND APPLIED AVDEC IAW SRM 51-25-15 FROM STA X 71.200 TO X 94-800. INSTALLED 12 RIVETS THRU FUSELAGE INTO EDGE BEAM & 6 RIVETS GOING THRU EDGE BEAM INTO HOZ ANGLES IAW SRM 51-42-05. INSTALLED REMAINING EDGE BEAM FASTENERS REF SRM 51-42-05 AND DWG 85329511, REV D.

Part: RIB — CORRODED (DOOR FRAME) · airframe 16,786 hrs · 18,116 cycles

AFT PAX DOOR SURROUND STRUCTURE HAS CORRODED RIB, AT BS X690-25. REMOVED RIB IAW SRM 51-42-05, STEP 4E AND INSTALLED IAW SRM 51-42-05.

Part: RIB — CORRODED (DOOR FRAME) · airframe 16,786 hrs · 18,116 cycles

AFT PAX DOOR SURROUND STRUCTURE HAS CORRODED RIB, PN 85339514-101 AT BS -X676. REMOVED RIB, PN 85339514-101 AT AFT PAX DOOR SURROUND STRUCTURE REF SRM 51-42-05, STEP 4E. RIB, PN 85339514-101 ISSUED FROM STOCK AND LOCATED, DRILLED IAW SRM 51-40-07. RIB ON 85339514-101 INSTALLED IAW SRM 51-42-05.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON BULKHEAD ANGLE SUPPORT ASSY, BULKHEAD ANGLE SUPPORT ASSY. REMOVED REF SRM 51-42-05. NEW BULKHEAD ANGLE SUPPORT INSTALLED IAW SRM 51-42-05. NEW BULKHEAD ANGLE SUPPORT LOCATED AND DRILLED IAW SRM 51-40-07.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 19 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-15-02-01, 51-40-15-02-01 AND 51-42-05-02-01

Part: ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON FWD ANGLE AT BSX 6.700 ON MCD. REMOVED ANGLE, PN 85329576-103 FROM LOWER MAIN SILL AT BS X 6.700, REF SRM 51-42-05-02-01 AND SRM 51-40-05-02-01. RECEIVED LOCATED AND DRILLED AND INSTALLED ANGLE, PN 85329576-103, REF SRM 51-40-07-02-01, SRM 51-42-05-02-01, TASK CARD 6-583-1160 FWD PASSENGER DOOR.

Part: ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON ANGLE AT BS X6.700 ON MCD. LOCATED AND DRILLED AND INSTALLED ANGLE IAW SRM 51-40-07-02-01, SRM 51-42-05-02-01.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 7 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 AND SRM 51-41-00, REF DWG 85361501, REV E

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 11 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW DWG NR 85328201, REV E.

Part: ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON ANGLE AT BS X26.700 ON MCD. LOCATED AND DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-07-02-01, AND SRM 51-42-05-02-01.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON MACHINED INTERCOSTAL. RECEIVED NEW MACHINED INTERCOSTAL LOCATED AND DRILLED IAW SRM 51-40-07. APPLIED ALUMINIZED EPOXY PRIMER AND INSTALLED NEW MACHINED INTERCOSTAL IAW SRM 51-40-15-02-01 AND DWG 85329330, REV A.

Part: ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON ANGLE AT BS X 19.500 ON MCD. REMOVED ANGLE FROM PARTIAL WEB IAW SRM 51-42-05-02-01. INSTALLED NEW ANGLE ON PARTICAL WEB IAW SRM 51-42-05-01-01, STEP 4D 3-10. LOCATED, DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-40-07-02-01.

Part: ANGLE — CORRODED (ZONE 200) · airframe 16,786 hrs · 18,116 cycles

EVIDENCE OF CORROSION ON AFT ANGLE AT BS X 26.7 ON MCD. REMOVED ANGLE, PN 329576-104 FROM LOWER MAIN SILL AT BS X 26.7, REF SRM 51-42-05-02-01 AND SRM 51-40-15-02-01. RECEIVED, LOCATED AND DRILLED AND INSTALLED NEW ANGLE, PN 85329516-104, REF SRM 51-40-07-02-01, SRM 51-42-05-02-01, TASK 6-53-1160 FWD PASSENGER DOOR.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 15 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-41-00, 51-40-15, AND DWG NR 85338210, REV -C .

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 9 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07 AND DWG: 85338201.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,786 hrs · 18,116 cycles

SEAT TRACK NR 8 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 541-42-05-02-01, SRM 51-42-05-02-01 AND DWG: 85338210, REV -C.

Part: AILERON SYS — MALFUNCTIONED (RT WING) · airframe 16,782 hrs · 18,114 cycles

EXCESSIVE RT WING DOWN AILERON TRIM REQUIRED AS AIRSPEED INCREASES AMOUNT OF RT AILERON ALSO INCREASES. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. COMPLIED WITH FIM TASK 27-13-00-810-801, VERIFIED AILERON CABLE TENSIONS, VISUALY INSPECTED AILERON TRIM INPUT, PREFORMEND OPS CHECK OF AILERON TRIM SYS AND OPS CHECK OF AUTOPILOT PITCH AND ROLL ACTUATORS. NO DEFECTS NOTED. ALL OPS CHECKS GOOD IAW APPLICABLE AMM TASK. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (NR 2 ENGINE) · airframe 16,725 hrs · 18,051 cycles

NR 2 ENGINE DID NOT COME OUT OF FEATHER AFTER ENGINE START. INTEROGATED CDS, NO FAULTS FOUND, AS PERCAUTIONARY R & R NR 2 ENGINE OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801, 61-20-26-400-801, KR 44607 1-10-2016. PERFORMED OPS TEST OF THE PROPELLER OVERSPEED GOVERNOR IAW AMM 61-20-00-710-803, OPS CHECK GOOD, PERFORMED LEAK CHECK IAW AMM 71-00-00-790-801, NO LEAKS FOUND, NO FAULTS IN CDS, NO DEFECTS NOTED.

Part: SEAL — STICKING (PAX DOOR) · airframe 16,366 hrs · 17,642 cycles

AFT PAX DOOR HARD TO OPEN CLOSE. CLEANED AND LUBED AFT DOOR SEAL DOOR OPENS AND CLOSES PROPERLY AT THIS TIME. RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (PROPELLER) · airframe 16,225 hrs · 17,510 cycles

AUTOFEATHER DID NOT ARM ON TAKEOFF. ABORTED TAKEOFF. REPLACED THE NR 1 PEC IAW AMM 61-20-396-000/400-801. CLEARED FAULT CODES. RETURNED TO SERVICE.

Part: FAULT CODE — FALSE ACTIVATION (AUTOFEATHER SYS) · airframe 16,215 hrs · 17,497 cycles

AUTOFEATHER TEST FAIL MESSAGE FOR NR 2 ENGINE. FOUND LT PROP CODES 494A, 402, 408, 494 ON THE "B" CHANNEL. CLEARED CODES IAW FIM 61-41-00-810-807. NO FAULTS AFTER. TEST PERFORMS FINE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FAN — INOPERATIVE (TRU) · airframe 15,866 hrs · 17,131 cycles

AFTER PUSHBACK, PARKING BRAKE SET, PROPS OUT OF FEATHER APPROXIMATELY 20-30 SEC, NOTICED GRAY-WHITE SMOKE COMING FROM RT SIDE OF NOSE OUTSIDE OF COCKPIT, LASTING FOR APPROXIMATELY 15 SECONDS, AND LT SIDE OF COCKPIT FOR ABOUT 5 SECONDS. RETURNED TO THE GATE. CW GVI OF BATTERY COMPARTMENT NO DEFECTS. CW GVI OF OXYGEN COMPARTMENT AND NOSE WHEEL STEERING AREA NO DEFECTS. CW GVI OF DC CONTACTOR BOX FROM INSIDE, NO DEFECTS. CW GVI OF TRU'S AND UPPER DECK NEAR TRU'S. FOUND TRU FAN NOT WORKING AND REPLACED TRU. PREVIOUS NIGHT W/O FOUND AP OPERATION CK REQUIRED PITOT STATIC LUBE TO BE APPLIED TO PITOT HEADS. SUSPECT PITOT HEAT LUBE CREATING SMOKY APPEARANCE. WAS ABLE TO DUPLICATE CONDITIONS WITH PITOT STATIC LUBE. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GASKET — LEAKING (ENGINE) · airframe 15,859 hrs · 17,122 cycles

AT INITIAL CLIMBOUT, NR 1 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 67 PSI AND INTO THE YELLOW ARC OF 60 PSI. OIL PRESSURE STABILIZED AS CONDITION LEVERS WERE BROUGHT BACK TO 900 RPM AND 850 RPM. THE ENGINE WAS NOT SHUTDOWN. RETURNED TO FIELD. LANDING UNEVENTFUL. INSPECTED NR 1 ENGINE OIL LEVEL. FOUND OIL LEVEL BELOW SIGHT GLASS. SERVICED NR 1 ENGINE WITH 18 PINTS-REF AMM, TASK 12-10-71-210-802. CHECKED NR 1 ENGINE SCUPPER OVERFLOW DRAIN-FOUND ALL COMPARTMENTS WITH RESIDUAL OIL. MAINLY STARTER GENERATOR COMPARTMENT, CLEANED SCUPPER AND RAN ACFT AT HIGH POWER. DID NOT NOTE ANY FLUCTUATIONS OF OIL PRESSURE. AFTER SHUTDOWN INSPECTED NR 1 ENGINE OVERFLOW/SCUPPER. FOUND NR 1 DC STARTER GEN SECTION FULL OF OIL; WHILE OTHER COMPARTMENTS REMAINED DRY. R & R NR 1 ENGINE STARTER GENERATOR DRIVE OIL SEAL IAW TASK 79-22-79-000-801 AND REMOVAL AND REPLACEMENT OF NR 1 ENGINE STARTER GENERATOR IAW MTC 6243101. FOUND ORIGINAL GARLOCK SEAL O-RING DAMAGED, OPS CHECKS GOOD. LEAK CHECKS GOOD. INSPECTED NR 1 ENGINE OVERLFOW/SCUPPER-NO RESIDUAL OIL FOUND. RAN ENGINE AT HIGH POWER-80 PERCENT NH FOR 30 MIN. OIL PRESSURE REMAINED STABLE ON BOTH ENGINES AND DID NOT DROP BELOW 61 PSI. NO FAULTS FOUND IN CDS. AFTER SHUTDOWN PERFORMED ENGINE LEAK CHECK AND OIL LEVEL CHECK, BOTH CHECKS GOOD. NO LEAKS NOTED. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 15,855 hrs · 17,115 cycles

F/A REPORTS THAT THE FLOOR EMERGENCY LIGHTING AT ROW 2 RT SIDE IS DETACHED. REATTACHED THE LIGHTING STRIP. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CIRCUIT BOARD — BURNED (FUEL PANEL) · airframe 15,590 hrs · 16,836 cycles

FUELER REPORTED SMOKE FROM THE FUELING PANEL, EXTERNAL. NO SMOKE OBSERVED BUT OBSERVED FUEL DEFUEL SWITCH WAS FOUND TO BE LOOSE AND PUSHED IN. FOUND PART OF THE CIRCUIT BOARD IN THE REFUEL/DEFUEL CONTROL BOX BURNED. ALSO, PERFORMED GVI OF WIRES OF THE REFUEL/DEFUEL COMPARTMENT. NO DEFECTS FOUND. R & R THE REFUEL/DEFUEL CONTROL PANEL ON THE NR 2 ENGINE NACELLE IAW AMM TASKS 28-24-01-000-801, 28-01-400-801. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 14,510 hrs · 15,649 cycles

MAIN CABIN DOOR HARD TO OPEN. INSPECTED FOR DEFECTS, NO DEFECTS NOTED AT THIS TIME. CLEANED & LUBED DOOR SEAL DOOR OPENS NORMALLY. PERFORMED OPS TEST IAW AMM 52-11-00-710-801. RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,207 hrs · 15,326 cycles

F/A REPORTS STRONG CHEMICAL ODOR. PACK TEMP WAS 40 DEGREE C. SELECTED FULL COLD ON PACKS SMELL DISIPATED. AS TEMPS INCREASED ODOR INCREASED BUT WAS LESS PRONOUNCED. ON ARRIVAL NO ODORS DETECTED. PERFORMED GVI IN BOTH ENGINE NACELLES AND THE APU COMPARTMENT WITH NO DEFECTS NOTED. COMPLIED WITH MCN NR 62172-01 AND AMM TASK 21-00-00-160-801. NO ODORS DETECTED. FOUND FAULT CODE 1104 L-HPSOV IN CDS AND NO AIRFLOW WITH NR 1 BLEED ON AND NO RISE IN ITT. R & R THE LT HPSOV IAW AMM TASKS 36-11-09-000-801 & 36-11-09-400-801. PERFORMED OPS TEST OF THE BLEED AIR SYS IAW AMM TASK 36-11-00-710-801. OPS TESTS GOOD. NO ODORS DETECTED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LATCH — STICKING (ZONE 200) · airframe 13,749 hrs · 14,850 cycles

EMERGENCY STOWAGE COMPARTMENT UNDER AFT F/A JUMPSEAT, LATCH IS STICKING. REPLACED LATCH FOR EMERGENCY STOWAGE COMPARTMENT UNDER AFT F/A JUMPSEAT W/NEW FROM STOCK. LATCH SECURE AND NO LONGER STICKING. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE — DAMAGED (INDICATION SYS) · airframe 13,717 hrs · 14,818 cycles

BRAKING DURING LANDING POOR. TAXI IN OTBD ANTI-SKID CAUTION LIGHT ILLUMINATED FOR ABOUT THREE SECONDS THEN WENT OUT. TROUBLESHOT AND REPAIRED DAMAGED WIRE. SYSTEM FUNCTIONAL TESTED GOOD IAW AMM 32-46-00-720-802. RETURNED TO SERVICE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 13,600 hrs · 14,696 cycles

EMERGENCY EXIT LIGHT COVER FELL OFF. SECURED COVE. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 13,548 hrs · 14,642 cycles

AFT F/A REPORTS A FAINT ELECTRICAL OR HOT ODOR IN AFT GALLEY. INSPECTED AFT GALLEY AREA ELECTRICAL COMPONENTS. NO ODOR DETECTED. INSPECTED GALLEY COFFEE/WATER JUGS SOCKETS ASSY. NO DEFECTS NOTED. NO ODOR NOTED IN AFT CARGO PIT. INSPECTED IAW MCN 62172-01 AND FORM M-744. ACFT OK FOR CONTINUED SERVICE.

Part: LIGHT — ODOR (CARGO BAY) · airframe 13,523 hrs · 14,615 cycles

AFT F/A REPORTED FAINT ODOR OF SMOKE IN AFT GALLEY. RAMP INSPECTED AFT CARGO AREA AND REPORTED A SIMILAR ODOR. NO VISIBLE SIGNS OF SMOKE. FOLLOWED MCN 62172-01, ISSUE NR 2 TROUBLESHOOTING COMMON ODORS IN ACFT. PERFORMED GVI ON AFT CARGO BAY. FOUND FWD LIGHT FIXTURE TO HAVE SULFER ODOR. R & R FWD LIGHT ASSY IAW AMM TASK 33-31-01-000-801, 33-31-01-400-801, MCN 63374-01 AND 63375-01. LT SEEMED UNSUALLY HOT, REPLACED MAPCO AS PRECAUTION, REPLACED RING TERMINAL ON TERMINAL "A" OF LIGHT ASSY. RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPNER) · airframe 13,304 hrs · 14,375 cycles

AILERONS, WHEN TURNING RIGHT REQUIRES STRAINED PRESSURE AND SOME RESISTANCE SPEEDS ABOVE 200 KTS VERY NOTICEABLE. AILERON CABLE RUN INSPECTION, TENSION, AND RIGGING. FUNCTIONAL TEST OF ROLL SPOILERS AND TIGHTENING OF LEAKING B-NUT ON THE RT OTBD SPOILER. TEST FLIGHT FAILED. YAW DAMPER NOT CENTERED AND YAW DAMPER DISENGAGED MESSAGE DURING FLIGHT, DID NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-11-00-710-801, AND ALSO ROLL SERVO MOTOR. RETURNED TO SERVICE.

Part: STRUT — LACK OF LUBE (PAX DOOR) · airframe 13,302 hrs · 14,371 cycles

F/A REPORTS MAIN CABIN DOOR IS STICKING ABOUT .2500 TO .5 OF THE WAY DOWN, AFTER OPENING AND NEEDS ADDITIONAL FORCE TO OPEN. CLEANED & LUBED UPPER & LOWER STRUTS OPS CHECKED GOOD MCD OPERATES AS REQUIRED IAW AMM 52-11-00-710-802. RETURNED TO SERVICE.

Part: ACTUATOR — BYPASSING (NLG LOCK) · airframe 12,689 hrs · 13,734 cycles

ON LANDING GEAR EXTENSION, ON APPROACH THE NOSE GEAR DOORS TOOK LONGER THEN NORMAL TO INDICATE CLOSED ALL OTHER GEAR INDICATION WERE NORMAL. LANDING UNEVENTFUL. NLG LOCK ACTUATOR BYPASSING AT A HIGH RATE ROBBING DOOR ACTUATOR OF HYD PRESSURE. NLG LOCK ACTUATOR WAS REPLACED. RETURNED TO SERVICE.

Part: SPRING — FAILED (STORAGE DOOR) · airframe 12,476 hrs · 13,503 cycles

LEFT AFT F/A EMERGENCY STORAGE DOOR DOES NOT SPRING BACK UP. FOUND SPRINGS TO STORAGE DOOR WORN OUT. REPLACED SPRINGS. OPS CHECKED DOOR WAS GOOD.

Part: LATCH — BROKEN (JUMP SEAT) · airframe 12,106 hrs · 13,117 cycles

F/A REPORTED AFT JUMP SEAT UNDERNEATH DOOR DOES NOT CLOSE. BOTH LATCHES REMAINS OPEN. REPLACED LATCH ASSY WITH NEW AT AFT LT JUMPSEAT EQUIPMENT DOOR. CHECKS GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: PITOT LINE — RUPTURED (STANDBY) · airframe 12,077 hrs · 13,082 cycles

ON CLIMBOUT STANBY INSTRUMENT SHOWS ACFT AIRSPEED ABOVE VMO THE HIGHER AND FAST THE ACFT IS THE MORE PRONOUNCED THE VARITATION IS. INDICATES NORMAL ON GROUND. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R ISI R & R STBY PITOT/STATIC PROBE NOT HELP. FOUND RUPTURED STBY PITOT LINE, REPLACED LINE, OPS CHECK GOOD NO LEAKS. RETURNED TO SERVICE.

Part: HINGE — CORRODED (STOWAGE BOX) · airframe 11,778 hrs · 12,778 cycles

COMPARTMENT UNDER FORWARD F/A JUMP SEAT FALLS OPEN. FOUND HINGE TO BE DAMAGED AND RUSTED. REPLACED THE HINGE. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: COVER — DISLODGED (SWITCH) · airframe 11,677 hrs · 12,668 cycles

EMEGENCY LIGHTS PUSHBUTTON COVER HAS COME OFF, F/A "A", FORWARD LOCATION. RESECURED FWD EMEGENCY LIGHT COVER AS REQUIRED. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: MECHANISM — OUT OF RIG (PAX DOOR VENT) · airframe 11,585 hrs · 12,571 cycles

AFT PAX DOOR WARNING IN FLT. RAN APPROPRIATE CHECKLIST AND RETURNED TO FIELD. NO OTHER ISSUES. . LANDING UNEVENTFUL. RIGGED VENT DOOR MECHANISM OF AFT PAX DOOR. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: ROD — BROKEN (PAX DOOR) · airframe 11,443 hrs · 12,417 cycles

F/A REPORTED THE MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM THE INSIDE. REPLACED THE MAIN CABIN DOOR ROD ASSY FOR THE DOOR LIFT MECHANISM. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 11,120 hrs · 12,053 cycles

RIGHT INBD NR 10 SEAT TRACK AT X1. CORRODED. BLENDED CORROSION IAW SRM 53-20-49. FOUND BEYOND SRM LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, 51-40-15 AND 51-41-00. NEW SEAT TRACK INSTALLED IAW SRM 51-42-05, 51-40-15 AND 51-41-00.

Part: SUPPORT — CORRODED (BS 32.4) · airframe 11,120 hrs · 12,053 cycles

SUPPORT PLATE AT FS 32.40 LT INBD OF THRESHOLD MEMBER IS CORRODED. R & R IAW SRM 51-42-05.

Part: BRACKET — CORRODED (THRESHOLD) · airframe 11,120 hrs · 12,053 cycles

BRACKET AT FS 8.70 UNDER THRESHOLD MEMBER IS CORRODED. REMOVED BRACKET, IAW SRM 51-42-05, P.205 STEP 4.E & REPLACED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 11,120 hrs · 12,053 cycles

RIGHT INBD NR 11 SEAT TRACK AT STA X38.400 HAS CORROSION. BLENDED CORROSION IAW SRM 53-20-49, BLENDED BEYOND SRM LIMITS. SEAT TRACK REMOVED REF SRM 51-42-05 AND 51-40-15, 51-41-00. NEW SEAT TRACK INSTALLED IAW SRM 51-42-05, 51-40-15 AND 51-41-00.

Part: SUPPORT CHANNEL — CORRODED (THRESHOLD) · airframe 11,120 hrs · 12,053 cycles

PAX DOOR THRESHOLD MEMBER SUPPORT CHANNEL IS CORRODED. REMOVED SUPPORT CHANNEL IAW SRM 51-42-05. INSTALLED NEW SUPPORT CHANNEL, IAW SRM 51-42-05.

Part: SUPPORT CHANNEL — CORRODED (THRESHOLD) · airframe 11,120 hrs · 12,053 cycles

PAX DOOR THRESHOLD SUPPORT CHANNEL CORRODED. REMOVED CORRODED SUPPORT CHANNEL IAW SRM 51-42-05 PARA E 1-8. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 650) · airframe 11,120 hrs · 12,053 cycles

LT INBD NR 8 SEAT TRACK BS 650 HAS CORROSION. REMOVED CORROSION AND IS WITHIN LIMITS IAW SRM 53-30-49 AND 53-20-49.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

PAX DOOR THRESHOLD CORRODED. REMOVED THRESHOLD IAW SRM 51-42-05, PAR E 1-8 AND INSTALLED IAW SRM 51-42-05.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE AT FS X6.70 BETWEEN LOWER MAIN SILL AND STRINGER 24P IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-05 PG 205, PARA E 1-8. INSTALLED NEW ANGLE IAW SRM 51-42-05.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE, AT FS X6.70 AND LOWER MAIN SILL CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-05 AND SRM 51-40-15.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE AT FS X26.70 BETWEEN LOWER MAIN SILL AND STRINGER 24P IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-05, PG 205, PAR E1-8. REPLACED CORRODED ANGLE IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

PAX DOOR THRESHOLD CORRODED. REMOVED THRESHOLD IAW SRM 51-42-05, PG 205, PAR E 1-8. INSTALLED NEW THRESHOLD IAW SRM 51-42-05.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE AT FS X26.70 AND LOWER MAIN SILL CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-05 AND SRM 51-40-15.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE AT FS X26.70 AND LOWER MAIN SILL CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-05 AND SRM 51-40-15.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,120 hrs · 12,053 cycles

ANGLE AT FS X6.70 AND LOWER MAIN SILL CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (BS 650) · airframe 11,120 hrs · 12,053 cycles

LT INBD NR 8 SEAT TRACK BS 650 HAS CORROSION. REMOVED CORROSION IAW SRM 53-30-49 AND SRM 53-20-49. FOUND OUT OF LIMITS IAW SRM 53-20-49-02-02, REPLACED SEAT TRACK IAW SRM 51-42-05, 51-40-15 & SRM 51-40-15.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 11,120 hrs · 12,053 cycles

LT WING FUEL PANEL 524CT LANDING HAS FRETTING AT ONE FASTENER HOLE AT THE INBD END. BLENDED AWAY FRETTING AREA ON LT WING FUEL PANEL 524CT LANDING REF SRM 57-20-30, STEP 2.B. MATERIAL REMOVED 0.004 FOUND TO BE IN LIMITS, MAX ALLOWABLE DAMAGE IS .005 DEPTH AFTER BLENDING, REF SRM 57-20-30, STEP 2.B.

Part: PROPELLER — MALFUNCTIONED (FEATHERING) · airframe 11,074 hrs · 12,008 cycles

NR 1 PROPELLER WOULD NOT COME OUT OF FEATHER. R & R NR 1 ENGINE PROPELLER OVERSPEED GOVERNOR AS A PRECAUTION IAW MM TASK 61-20-26-000-801 + 61-20-26-400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: STEP — DELAMINATED (PAX DOOR) · airframe 10,817 hrs · 11,731 cycles

F/A REPORTS THAT THE MAIN CABIN DOOR IS STILL DIFFICULT TO OPEN. FERRIED ACFT FOR REPAIRS. FOUND LOWER STEP TO BE DELAMINATED. REPLACED LOWER STEP IAW AMM 52-11-01-801. RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 10,816 hrs · 11,731 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBED DOOR & PERFORMED OPS CK OF MCD DOOR IAW 52-11-00-710-802. OPS CHECKED GOOD.

Part: CAM — WORN (PAX DOOR) · airframe 10,393 hrs · 11,292 cycles

AFT PAX DOOR WILL NOT OPEN. FOUND INTERLOCK CAM ASSY ON AFT PAX DOOR WORN. R & R CAM ASSY WITH NEW . DOOR OPS CHECKED GOOD IAW AMM TASK 52-12-00-710-802. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED · airframe 9,728 hrs · 10,591 cycles

ON APPROACH, AT 200 FT, ACFT HAD A BIRD STRIKE, RECEIVING DAMAGE TO THE NOSE OF THE ACFT AND THE STABILIZERS. LANDING UNEVENTFUL. ACFT FERRIED FOR REPAIRS AND IS CURRENTLY DOWN FOR REPAIRS.

Part: PIVOT — LACK OF LUBE (PAX DOOR HANDLE) · airframe 9,413 hrs · 10,274 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE HANDLE. CLEANED & LUBED DOOR HANDLE PIVOT POINT OPS CHECK NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GOVERNOR — MALFUNCTIONED (ZONE 400) · airframe 3,992 hrs · 4,051 cycles

NR 1 PROPELLER UNUSUALLY SLOW TO COME OUT OF FEATHER AFTER ENGINE START. NO FAULTS FOUND IN EMU. R & R NR 1 OSG IAW AMM TASK 61-20-26-000-801 AND 61-20-26-400-801. OPS TEST GOOD PROPELLERS BOTH UNFEATHER IN 18 SECS. NO OTHER DEFECTS NOTED. LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (ZONE 400) · airframe 27,229 hrs · 28,464 cycles

ON LANDING, WHEN POWER LEVERS WERE BROUGHT TO DISC, THE NR 1 DID NOT GO INTO BETA, UNTIL JUST BEFORE STOPPING AT THE GATE THE POWER LEVERS WERE IN DISC THE ENTIRE TIME THE NR 1 PROP GROUND RANGE LIGHT DID NOT ILLUMINATE. THE ACFT PULLED TO THE RIGHT ON ROLL OUT. TORQUE, ITT, NH AND NL AND FF WERE ALL HIGHER ON NR 1, ALL WENT TO NORMAL JUST BEFORE STOPPING AT THE GATE NO OTHER MESSAGES OR CAUTION LIGHTS. R & R PCU. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (NR 2) · airframe 8,431 hrs · 9,246 cycles

ON TAKEOFF NR 2 PROPELLER NEVER REACHED 1020 RPM. PROPELLER REACHED 950 RPM AND TORQUE AT 92 PERCENT, NR 1 ENGINE RUNS NORMALLY AFTER SELECTION TO PROPELLERS 900 RMP EVERYTHING FUNCTIONED NORMALLY. REPLACED NR 2 OVERSPEED GOVERNOR IAW AMM TASK 61-20-26-000-801 AND 61-20-26-400-801. OPS AND LEAK CHECKED GOOD.

Part: PROPELLER — NO TEST (NR 1) · airframe 8,427 hrs · 9,244 cycles

NR 1 PROPELLER FAILS ALTERNATE FEATHER CHECK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,322 hrs · 9,154 cycles

FORWARD F/A POSITION THE NORMAL PORTION OF THE EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATE. RELAMPED. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 7,580 hrs · 8,391 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED DOOR AND PERFORMED OPS TEST OF FORWARD PASSENGER DOOR IAW TASK 52-11-00-710-802. DOOR OP'S CHECKED GOOD. ACFT OK FOR SERVICE.

Part: INDICATION SYS — MALFUNCTIONED · airframe 7,148 hrs · 7,927 cycles

WHEN SELECTED, AUTOFEATHER SWITCH INDICATES SELECT BUT ED DOES NOT SHOW "AF SELECT" PROBLEM OCCURED AFTER ACFT WAS DEICED. CW FIM TASK 61-41-00-810-813 PROP INDICATION ED INDICATION DISCREPANCY AND NO RELATED FAULTS NOTED. CW AMM TASK 61-20-00-710-801 OPS TEST OF PROP AUTOFEATHER AND UPTRIM SYS AND NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SUMMING UNIT — MALFUNCTIONED (RUDDER) · airframe 6,800 hrs · 7,563 cycles

IN LEVEL CRUISE FL250, POWER REDUCED AND RT RUDDER APPLIED. RUDDER PEDAL DEFLECTED A SMALL DISTANCE AND THEN STOPPED. FELT LIKE A LIMIT TO TRAVEL. PFCS SHOWED ABOUT A HALF A NEEDLE WIDTH OF DEFLECTION. RUDDER TRIM FELT LIKE IT WAS WORKING PROPERLY. CREW TRIED TO MOVE THE RUDDER & FELT THE LIMIT. RT & LT SIDES HAD SAME LIMIT RESULTS. CAPTAIN APPLIED PRESSURE TO RT RUDDER PEDAL UNTIL THERE WAS A PHYSICAL RELEASE & LARGE YAW OF ACFT. AFTER CENTERING RUDDER PEDALS, PRESSURE WAS AGAIN APPLIED AND LIMIT WAS FELT AGAIN. DURING APPROACH LIMIT TO RUDDER TRAVEL WAS GONE AT 7000'/200KIAS/-21C. RUDDER OPERATED SMOOTHLY FOR REMAINDER OF FLIGHT & DURING TAXI. REMOVED RUDDER FEEL & SUMMING UNIT IAW AMM TASK 27-22-06-000-801. INSTALLED IAW TASK 27-22-06-400-801. PERFORMED FREEDOM OF MOVEMENT CHECK OF RUDDER SYS ENSURING FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT. NO DEFECTS NOTED. OPS CHECKED GOOD. OCF FLIGHT GOOD. RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 5,263 hrs · 5,997 cycles

F/A REPORTED MAIN CABIN DOOR IS DIFFICULT TO OPEN. CYCLED MAIN CABIN DOOR SEVERAL TIMES , OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: DOOR — BINDING (MAIN PAX)

F/A REPORTS THAT MAIN CABIN DOOR IS DIFFICULT TO OPEN. CYCLED DOOR SEVERAL TIMES, OPS CHECKS GOOD. NO DEFECTS NOTED. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: COMPUTER — FAILED (AHRU) · airframe 4,946 hrs · 5,683 cycles

ELEVATOR FEEL CAUTION LIGHT ILLUMINATED IN CRUISE. RAN CHECKLIST SLOWED TO 200 KTS AND DIVERTED. CAPTAIN'S PFD AND MFD HAD "ATT FAIL ", "HDG FAIL", "IVSI FAIL" RED MESSAGED. FAILURE OCCURED AT 25,000 WITH -43 DEGREE C OAT. LANDING UNEVENTFUL. PERFORMED A CLEANING OF NR 1 AND NR 2 PITOT/STATIC SYS. C/W LEAK TEST IAW TC 6341102. ALL CHECKS GOOD. REPLACED NR 1 AHRU IAW TC 63421010. ALL CHECKS GOOD. RETURNED TO SERVICE.

Part: MOUNT — CORRODED (WING) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - FWD WING SPAR PANEL MOUNTING FLANGE, UNDER PANEL 261CT, HAS FRETTING. BLENDED OUT DAMAGE IAW RD 8/4-53-451 MINIMUM REMAINING THICKNESS .094" AND .072 REF NTM 51-00-02-250-801. CONFIRMED CRACK FREE IAW RD 8/4-53-451. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-1521. ALODINED, PRIMED AND APPLIED TEFLON TAPE IAW RD 8/4-53-451.

Part: SPAR — CHAFED (WING) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - AFT WING SPAR PANEL MONTING FLANGE FOR PANEL 262AT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.

Part: SEAT TRACK — CORRODED (BS 668) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - SEAT TRACK 8, AFT END AT STA 668.00 HAS AREA OF POSSIBLE CORROSION. BLENDED GOUGES ON TOP OF SEAT TRACK IAW RD 8/4-53-884. FOUND WITHIN LIMITS OF RD 8/4-53-884. COMPLETED REPAIR IAW RD 8/4-53-884.

Part: SPAR — CHAFED (WING) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262FT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.

Part: SPAR — CHAFED (WING) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262HT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. VERIFIED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - SEAT TRACK NR 11 FWD END HAS AREA OF POSSIBLE CORROSION. COMPLIED WITH RD 8/4-53-2358.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 4,936 hrs · 5,327 cycles

C1 CHECK - ACCOMPLISH TASK CARD RD8/4-53-3447/3: TEMP REPAIR FOR LIGHTNING STRIKE DAMAGE TO LWR FUSELAGE. COMPLIED WITH RD 8/4-53-3449/3.

Part: SEAT TRACK — GOUGED (BS 698) · airframe 4,936 hrs · 5,627 cycles

C1 CHECK - AFT BAGGAGE COMPARTMENT SEAT TRACK 9, FWD END AT STA 698.00 HAS GOUGES. BLENDED GOUGES ON TOP OF SEAT TRACK IAW RD 8/4-53-884. FOUND WITHIN LIMITS OF RD 8/4-53-884. COMPLETED REPAIR IAW RD 8/4-53-884.

Part: DOOR — BINDING (MAIN PAX) · airframe 4,425 hrs · 5,073 cycles

THE MAIN CABIN DOOR IS HARD TO OPEN FROM THE INSIDE AS REPORTED BY THE F/A. APPLIED LPS-2 LUBE TO THE DOOR STOPS AND HANDLES. DOOR OPS CHECKS GOOD IAW AMM TASK 52-11-00-710-802. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WIRE HARNESS — FAILED (PROP DE ICE) · airframe 3,173 hrs · 3,686 cycles

PROP DEICE CAUTION LIGHT INTERMITTENTLY COMES ON WHEN THE NR1 PROP HEAT ENERGIZES. WHEN THE NR 1 PROP HEAT QUITS THE CAUTION LIGHT GOES OUT. PERFORMED EMERGENCY/ABNORMAL CHECKLIST, DIDN'T HELP. ELECTRICAL PAGE SHOWED THAT THE PROP HEAT WAS DWG A LOAD OK. NR 2 PROP HEAT WORKED FINE. RETURNED TO THE FIELD. LANDING UNEVENTFUL. REMOVED NR1 PROP SPINNER, INSPECTED & FOUND NR 2 PROP HEAT DE-ICE HARNESS BURNED. REPLACED DE-ICE HARNESS IAW AMM TASK 61-10-06-400-805. PROP DE-ICE SYS OPERATIONALLY CHECKS NORMAL. REINSTALLED PROP SPINNER. RETURNED TO SERVICE.

Part: RUDDER — BINDING (ZONE 200) · airframe 3,153 hrs · 3,657 cycles

DURING APPROACH, RUDDER BOUND AND WOULDN'T MOVE TO THE LT WITH NORMAL RUDDER PEDAL FORCE. WHEN MORE RUDDER PEDAL FORCE WAS APPLIED THE RUDDER SUDDENLY "BROKE LOOSE" AND YAWED HARD TO THE LT. HAPPENED ONCE MORE TO THE RT. USED RUDDER TRIM FOR THE REMAINDER OF THE FLIGHT AS SUGGESTED BY FCIF. LANDING UNEVENTFUL. C/W GVI OF ENTIRE RUDDER CONTROL SYS, C/W RUD CTL SYS OPS CHECK, C/W FREEDOM OF MOVEMENT CHECK, REPLACED FDR, NO DEFECTS NOTED. FERRIE FOR REPAIRS. R & R RUDDER FELL/ TRIM / SUM UNIT IAW AMM 27-22-06-000-801 AND 27-22-06-400-801. OPS CHECK FLIGHT OK. RETURNED TO SERVICE.

Part: DOOR — STIFF (PAX DOOR) · airframe 2,646 hrs · 3,100 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. CYCLED DOOR SEVERAL TIMES, NO DEFECTS NOTED, DOOR OPERATES NORMALLY, NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — STIFF (MAIN PAX) · airframe 2,432 hrs · 2,858 cycles

MAIN CABIN DOOR DIFFICULT TO OPERATE SLOW TO DROP/ HARD TO PULL UP. CLEANED & LUBED MAIN CABIN DOOR AS REQUIRED. OPENED & CLOSED DOOR MULTIPLE TIMES WITH NO DEFECTS NOTED. DOOR OPERATES NORMAL. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HINGE — LACK OF LUBE (MAIN PAX) · airframe 2,170 hrs · 2,540 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED AND LUBED DOOR HINGE POINTS AS REQUIRED. OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING MESSAGE — ILLUMINATED (PITCH TRIM) · airframe 1,766 hrs · 2,064 cycles

SMF- PITCH TRIM CAUTION MESSAGE AFTER TAKEOFF. RETURNED TO THE FIELD. LANDING UNEVENTFUL. C/W FIM TASK 27-30-00-810-803 AND AMM TASK 27-32-00-710-802 OPERATIONAL CHECK OF PITCH TRIM NORMAL NO FURTHER FAULTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 1,076 hrs · 1,233 cycles

LAX - MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR, TRACK AND SEAL. OPS TEST GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — STUCK (MAIN PAX) · airframe 1,011 hrs · 1,156 cycles

F/A REPORTS THAT MAIN CABIN DOOR HANDLE IS HARD TO MOVE AT FIRST. MAINTENANCE OPERATED DOOR NUMEROUS TIMES WITH NO DEFECTS NOTED. DOOR OPERATES NORMALLY. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WIRE HARNESS — MALFUNCTIONED (MLG DOOR) · airframe 977 hrs · 1,119 cycles

RIGHT MLG DOOR TOOK APPROX 45 SECONDS TO 1 MINUTE TO RETRACT AFTER GEAR EXTENTION. ALL GEAR INDICATIONS NORMAL AT THE TIME OF LANDING. FERRY TO PDX FOR REPAIRS. MAINTENANCE WAS ABLE TO DUPLICATE DISCREPANCY. RT MLG DOOR REMAINED OPEN AFTER GEAR EXTENTION REVIEWED PSEU FAULT CODE RGDLK2 UNREASONABLE FAR- TROUBLESHOT IAW FIM TASKS 32-34-01-810-803 & 32-73-11-810-836- REMOVED AND REPLACED RGDLK2 SENSOR HARNESS, AND AS PRECAUTION MESURE RGDLK1 SENSOR HARNESS IAW TASKS 32-61-06-000-802 & 32-61-06-400-802-- OPCK IAW TASK 32-31-00-710-801. OPERATIONAL CHECKS GOOD, NO PSEU FAULTS RECORDED. RETURNED TO SERVICE.

Part: GENERATOR — FAILED (ZONE 400) · airframe 447 hrs · 513 cycles

PDX - AT 65-70 KT THE NR 2 AC GEN CAUTION LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. RETURNED TO THE GATE. COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED NR 2 AC GEN AS A PRECAUTIONARY MEASURE DUE TO ABORTED TAKEOFF IAW AMM TASKS 24-21-01-000-801 AND 24-21-01-400-801. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (DOORS) · airframe 413 hrs · 469 cycles

GEG - "FUSELAGE DOORS" WARNING SYSTEMS PAGE DISPLAYS AND SHOWS AFT CABIN DOOR UNSAFE. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AND FOUND HANDLE PROTRUDING AFTER LANDING AT GATE. PERFORMED FUNCTIONAL CK IAW AMM 51-12-00-720-801. NO DEFECTS NOTED. NO PARTS REPLACED. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 372 hrs · 420 cycles

BOI - DURING CLIMB THRU 20,000 MASTER WARNING AND FUSELAGE DOOR LIGHT ILLUMINATED. STARTED LOSING PRESSURIZATION 1000FPM. DESCENDED TO 11,000 AND WERE ABLE TO HOLD PRESSURIZATION. DOOR PG SHOWS LEFT AFT PAX DOOR OPEN. CLIMBED BACK TO 17,000 AND DIVERTED TO BOI, THE CABIN ALT SHOWED 5000. ACCORDING TO THE CHART IT SHOULD BE AT 3000. LANDING UNEVENTFUL. C/W FUNCTIONAL TEST OF THE AFT PASSENGER DOOR IAW MM TASK 52-12-00-720-801, AFTER FINDING DOOR HANDLE NOT PROPERLY SEATED. DOOR LOCKS AND UNLOCKS PER SUBTASK 52-12-00-720-052 STEP 2A. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: HANDLE — BACKED OUT (ZONE 800) · airframe 330 hrs · 380 cycles

DURING CLIMBOUT GOT MASTER WARNING FUSELAGE DOORS AND FWB BAG DOOR INDICATED RED ON THE MFD. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED FWD BAG DOOR ON ARRIVAL AND FOUND EXTERNAL HANDLE NOT SEATED. PUSHED HANDLE IN AND VERIFIED CAUTION LIGHT EXTINGUISHED. OPS CHECK OF FWD BAG DOOR IAW TASK 52-32-00-710-801. AC OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: PROP HEAT — SPARKS · airframe 239 hrs · 259 cycles

ON APPROACH WITH PROP HEAT ON, HAD SPARKS COMING OUT OF BOTH PROPS CLOSE TO THE SPINNER. PERFORMED GVI OF PROPS, SPINNERS, BRUSH BLOCK ASSY. FOUND NO EVIDENCE OF SPARKING. RAN BOTH ENGINES WITH PROP HEAT FOR 15 MINUTES AND NO SPARKING OCCURRED. RE-INSPECTED PROPS, NO DEFECTS NOTED. FUNCTIONAL OF PROP DEICE C/W IAW AMM 30-61-00-720-801. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 214 hrs · 233 cycles

LAX - IN CLIMB OUT RECEIVED FUSELAGE DOORS WARNING LIGHT, CONFIRMED FWD BAG WAS NOT SECURE. PRESSURIZED NORMAL. RETURNED TO THE FIELD, LANDING UNEVENTFUL. ON ARRIVAL FOUND FORWARD CARGO DOOR HANDLE EXTRUDING FROM ITS SECURE POSITION, NOT FULLY FLUSHED. PERFORMED GVI OF FWD CARGO DOOR. NO DEFECTS NOTED. LUBED DOOR HANDLE MECHANISM. C/W OPERATIONAL TEST OF THE FORWARD BAGGAGE DOOR. OPS TEST GOOD PER AMM TASK 52-32-00-710-801. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 176 hrs · 188 cycles

GEG - LEFT AFT PAX DOOR LIGHT ILLUMINATED. DIVERTED TO GEG. ACCOMPLISHED AN UNEVENTFUL LANDING. CHECKED DOOR HANDLES ON AIRCRAFT UPON ARRIVAL. FOUND AFT PAX DOOR HANDLE NOT FULLY SEATED. COMPLIED WITH INSP IAW AMM 05-48-09-210-802 (GVI), NO DEFECTS NOTED. C/W OPERATIONAL CHECK FORM OUTSIDE AND INSIDE, IAW AMM 52-11-00. CHECKS GOOD. OK FOR SERVICE. NO PARTS REPLACED.

Part: PROXIMITY SENSOR — OUT OF RIG (MLG) · airframe 120 hrs · 125 cycles

BZN - STARTED ENGINES AT GATE. DISCONNECTED FROM GPU. AS SOON AS PUSHBACK COMMENCED, NOSE GEAR DOORS CYCLED OPEN AND CLOSED. NO CONTACT OF DOORS WITH LECTRO CART. VERIFIED ALL BATTERY SWITCHES ON. CONFERRED WITH MTX CONTROL. ELECTED TO CONTINUE PUSH BACK. AS SOON AS PUSHBACK WAS RE-STARTED NOSE GEAR DOORS CYCLED OPEN THEN CLOSED. INTERROGATED PSEU FOUND PRESENT FAULT "NGDN1 RIGGING NEAR GAP TOO LARGE." VERIFIED INDUCTANCE VALUE TOO LOW. PERFORMED RIGGING OF S9 PROX SENSOR IAW AMM TASK 32-61-06-830-801. PERFORMED INDUCTANCE VALUE CHECK OF PROX SENSOR IAW AMM TASK 32-61-00-280-801. PRESSURIZED HYD SYSTEM AND CYCLED GEAR DOORS SEVERAL TIMES. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONNECTOR — MALFUNCTIONED (TRANSDUCER) · airframe 41 hrs · 36 cycles

PDX - ON CLIMB-OUT OF SEA OIL PRESSURE NEEDLE HAD NO INDICATION AND NUMERICAL VALUE HAD DASHES. NO WARNING LIGHT ILLUMINATED. DESCENDING- NEEDLE AND NUMERICAL VALUE REAPPEARED WITH IN NORMAL PARAMETERS. NR 2 ENGINE. DIVERTED TO PDX. ACCOMPLISHED A UNEVENTFUL LANDING. UPON FURTHER INVESTIGATION, FOUND UNKNOWN FLUID IN THE OIL PRESSURE TRANSDUCER CONNECTOR AT TRANSDUCER, CLEANED CONNECTOR REMOVED AND REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSDUCER PER Q400AMM TASKS 79-31-01-000-801 AND 79-31-01-400-801, OPS TEST AND LEAK CHECK GOOD. PERFORMED AIRCRAFT TAXI CHECK TO REPLICATE DISCREPANCY FOR APPROX 15 MINUTES, DISCREPANCY DID NOT REOCCUR. RETURNED TO SERVICE.