N435QX

Part: PEC — MALFUNCTIONED (NR 2) · airframe 30,661 hrs · 33,155 cycles

AUTO FEATHER DID NOT ARM WITH POWER LEVERS SET IN THE DETENT. REMOVED FROM SERVICE. CDS FAULT 400 - #2 PROP CHANNEL #1 AND #2. REMOVED AND REPLACED #2 PEC IAW FIM 61-20-09-810-806. OPS CHECK GOOD. FAULT DID NOT RETURN. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDSHIELD) · airframe 30,589 hrs · 33,065 cycles

WINDSHIELD CONT CAUTION INTERMITTENT DURING FLIGHT. RETURNED TO FIELD. REMOVED FROM SERVICE. PERFORMED OPS CHECK IAW Q 400 FIM 30-40-*00-810-805 THROUGH STEP 3.A.3(A) FAULTS DID NOT RETURN, CAUTION LIGHTS DID NOT ILLUMINATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HEATER — MALFUNCTIONED (WINDSHIELD) · airframe 30,589 hrs · 33,065 cycles

WINDSHIELD CTRL CAUTION AFTER SELECTING WINDSHIELD HEAT TO NORM @ 10000 FT. DIVERTED. REMOVED FROM SERVICE. C/W Q400 FIM TASK 30-40-00-810-805 RESISTANCE TO VOLTAGE CHECKS GOOD ON CART AND F.O. WINDSHIELD COULD NOT DUPLICATE HAS ENTRY. PRESSURIZED A/C FOR MTX REF Q400 AMM 21-00-01-869-801. DURING OPERATIONS TEST OF PILOT AND COPILOT WINDSHIELD ANTI-ICING SYS PER Q400 AMM TASK 30-41-00-710-801, 30-41-00-710-802. DURING PRESSURIZATION WINDSHIELD CTRL CAUTION ILLUMINATUED R&R 3041-K3 AND 3041-K4 RELAYS. PER Q400 AMM TASK 20-30-16-860-802 NO HELP. SWAPPED CANNON PLUGS ON ANTI-ICE CONTINUE. NO HELP. CANNON PLUG SWAPPED BACK TO ORIGINAL POSITION. WINDSHIELD CTRL CAUTION STILL ILLUMINATED WITH A/C PRESSURIZED CDS PABEL REMAINS RH WINDSHIELD CTRL FAIL. R&R COPILOT WINDSHIELD OPS CHECK AND PRESSURE CHECKS GOOD. RETURNED TO SERVICE.

Part: FLOOR PANEL — LOOSE (CABIN FLOOR) · airframe 30,181 hrs · 32,530 cycles

F/A REPORTS PHOTO-LUMINESCENT STRIP COMING LOOSE IN FORWARD CABIN. REMOVED FROM SERVICE. RE-SECURED LOOSE FLOOR PATH LIGHTING AT ROW 1AB REF Q400 AMM 33-51-16-400-801. RETURNED TO SERVICE.

Part: PAD — MISSING (ZONE 800) · airframe 30,068 hrs · 32,428 cycles

RUBBER BUMPER FOR MAIN CABIN DOOR OUTSIDE HANDLE FELL OFF. REMOVED FROM SERVICE. REPLACED MISSING BUMPER STOP IAW Q400 AMM TASK 52-11-11-400-81 PAR 4 J AND PAR 5. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 29,553 hrs · 31,864 cycles

APU START FAILED RAMP REPORTED EXCESSIVE AMOUNT OF SMOKE FROM APU ( APU INOP ). REMOVED FROM SERVICE. SUCCESSFULLY STARTED APU MULTIPLE TIMES. NO SMOKE PRESENT DURING OPERATION. NO PRIOR HISTORY OF APU FAILURE SINCE JANUARY. CLEARS MEL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 28,808 hrs · 31,084 cycles

FLUORESCENT STRIP ON FLOOR BY FWD CARGO DOOR POPPED OFF. REMOVED FROM SERVICE. RE-SECURED FLOOR STRIP. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 28,285 hrs · 30,589 cycles

AFT PASSENGER DOOR SIDE EMERGENCY LIGHT IS INOP. RELAMPED LIGHT WITH NO HELP. FOUND CANNON PLUG DISCONNECTED. RECONNECTED AND OPERATIONAL CHECKS GOOD IAW 25-26-28-400-801 AND 33-51-06-400-803.

Part: DOOR — MALFUNCTIONED (AFT PAX) · airframe 27,920 hrs · 30,165 cycles

FOUND AFT PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE USING THE INSIDE AND OUTSIDE HANDLES. PERFORMED OPERATIONAL CHECK OF THE DOOR IAW AMM 52-12-00-710-801, DOOR DOES NOT OPERATE SMOOTHLY. PERFORMED FUNCTIONAL TEST OF THE DOOR IAW AMM 52-12-00-720-801. FAILED F1 OPEN LOAD TEST WITH VARIOUS LOADS EXCEEDING 45 LBF. FAILED F2 CLOSED LOAD TEST WITH VARIOUS LOADS EXCEEDING 50 LBF. OUT OF SERVICE IN WORK. REPLACED VENT DOOR SPRINGS AND DOOR GUIDE, FUNCTIONAL TEST & RII. DOOR HANDLE FORCES ARE WITHIN LIMITATION. RETURNED TO SERVICE.

Part: STARTER GEN — MALFUNCTIONED (NR 1 ENGINE) · airframe 27,909 hrs · 30,156 cycles

#2 DC GEN CAUTION LIGHT ILLUMINATED ON TAKE OFF ROLL. TAKEOFF ABORTED. RETURNED TO GATE, REMOVED FROM SERVICE. PLACED ON MEL 24-30-6. CLEARED MEL 6/2/21 REF Q400 AMM TASK 24-31-01-000-801 REMOVED #2 DC STARTER/GEN. REF Q400 AMM TASK 24-31-01-400-801 INSTALLED NEW STARTER/GEN. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 27,634 hrs · 29,885 cycles

RAMP REPORTS AFT PASSENGER DOOR HARD TO OPEN. REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL CHECK OF THE AFT PAX DOOR IAW AMM 52-12-00-710-801. DOOR OPERATES NORMALLY. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 30,850 hrs · 33,263 cycles

FORWARD WING BULKHEAD EMERGENCY EXIT LIGHT LENS IS DISCOLORED. REPLACED LENS IAW CMM 25-52-13.

Part: SEAT TRACK — CORRODED (PASS CABIN) · airframe 27,503 hrs · 29,752 cycles

SEAT RAIL 11 FROM FSX10.50 -X102.50,YBL 40.950 IS CORRODED BEYOND LIMITS. SEAT RAIL 11 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01 REV 21 AND AMM 20-10-01-430-801 REV 71. PROTECTED SEAT RAIL IAW SRM 51-25-10-02-01, 51-25-15-02-01.

Part: SEAT — CORRODED · airframe 27,503 hrs · 29,752 cycles

SEAT RAIL 10 FROM FSX-39.00-X10.50, YBL 40.950 IS CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 10 IAW SRM 51-42-05-02-01, 51-40-15-02-01 REV 21, AND AMM TASK 20-10-01-430-801. PROTECTED SEAT RAIL IAW SRM 51-25-10-02-01, 51-25-15-02-01.

Part: SHEAR WEB — NOT REPORTED (ZONE 200) · airframe 27,503 hrs · 29,752 cycles

FWD SHEAR WEB FROM FSX697.60-X715.00 LH SIDE. REMOVED FWD SHEAR WEB FROM FSX697.60-X715.00 LH IAW SRM 51-40-07-02-01(REV 21). INSTALL NEW FWD SHEAR WEB FROM FSX697.60-X715.00 LH IAW SRM 51-42-05-02-01, 51-42-45-02-01, 51-42-75-02-01, 51-40-15-02-01(REV 21).

Part: SEAT — CORRODED · airframe 27,503 hrs · 29,752 cycles

SEAT RAIL 9, SIDE FLANGE CORRODED AROUND ANCHOR NUT HOLES AT APPROX FSX751 AND X775. REPLACED SEAT RAIL 9 PN 85338210-111 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-41-05-00-01 AND 51-42-05-02-01 REV NO 21.

Part: CHANNEL — CRACKED (LT FUS PANEL) · airframe 27,503 hrs · 29,752 cycles

CRACK ON UPPER CHANNEL OF LH UNDERWING TO FUSELAGE PANEL LANDING BETWEEN PANELS 263BL AND 263CL. CRACK DAMAGE AT FWD SECTION OF UPPER CHANNEL OF LH UNDER WING TO FUSELAGE PANELS REMOVED IAW RD84-53-10101. NDT CARRIED OUT BY SKY SERVICE (REF: WO# TWO33218) NO FAULTS FOUND. REPAIR ANGLE FABRICATED AND INSTALLED IAW RD84-53-10101.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 27,503 hrs · 29,752 cycles

SEAT RAIL 8 FROM FSX571.50-X670.00, Y-40.950 BLENDED BEYOND LIMITS. REMOVED CABIN FLOOR PANELS 141CZ, 141DZ, AND 141EZ IAW AMM 53-41-01-000-801 REV 71, AND AMM 53-33-01-000-801 REV 71. REPLACED SEAT RAIL 8 FROM FSX 571.5-X670.0 @ Y-40.95 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-41-05-00-01 AND 51-42-05-02-01 REV NO 21. INSTALLED CABIN FLOOR PANELS 141CZ, 141DZ, AND 141EZ IAW AMM 53-41-01-400-801 REV 71, AND AMM 53-33-01-400-801 REV 71, AND IN REFERENCE TO HORIZON COC HS 53-0005.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,503 hrs · 29,752 cycles

SEAT RAIL 16 FROM FSX670-X783.00,Y40.950 IS CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 16 FROM FS X670-X283.00 Y40.950 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01 (REV 21).

Part: SHEAR WEB — CORRODED (AFT) · airframe 27,503 hrs · 29,752 cycles

AFT SHEAR WEB FROM FSX715-X783,LH SIDE IS CORRODED BEYOND LIMITS. REPLACED AFT SHEAR WEB PN 85339627-111 FROM X715-X783. IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01 AND 51-42-45-02-01 REV NO 21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,502 hrs · 29,752 cycles

SEAT RAIL NR 1 FROM FS X32.4 TO X 229.5 Y-9 250 BLENDED BEYOND LIMITS. REPLACED SEAT RAIL NR 1 IAW Q400 SRM 51-40-07-02-01. 51-40-15-02-01, 51-42-05-02-01, 57-42-45-48-02-01.

Part: BRAKE — LEAKING (ZONE 700) · airframe 27,446 hrs · 29,695 cycles

ON POST FLIGHT FOUND LEFT MAIN GEAR RIGHT TIRE LEAKING SOME FLUID ONTO BRAKE CAUSING SMOKE. RIGHT INBOARD TIRE COVERED IN A OIL LIKE FLUID. REMOVED FROM SERVICE. INSPECTED NR 2 MLG WHEEL AND TIRE FOUND FLUID ON BRAKE, WHEEL, AND TIRE. REMOVED WHEEL AND TIRE, FOUND NO BURNING OR DISCOLORATION ON AXLE. SUSPECTED LEAKING BRAKE ASSEMBLY. REMOVED AND REPLACED BRAKE ASSEMBLY, IAW MTC 6324201. WHEEL AND TIRE ASSEMBLY WAS REMOVED AND REPLACED, IAW MTC 6324101. VERIFIED NO WHEEL BEARING FAILURE. RETURNED TO SERVICE.

Part: LANDING GEAR — CONTAMINATED (NR 2) · airframe 27,423 hrs · 29,669 cycles

ON PREFLIGHT WALKAROUND F/O FOUND SMOKE COMING FROM NR 2 MLG ASSEMBLY. UPON CLOSER INSPECTION FOUND FAIR AMOUNT OF FLUID ON INBOARD TIRE, THE NR 2 TIRE WAS STILL SMOKING 20 MINUTES AFTER INBOUND CREW SHUTDOWN AIRCRAFT. REMOVED FROM SERVICE. DETERMINED TO BE GREASE FROM PRIOR GEAR LUBES, CLEANED AFFECTED AREA, AS REQUIRED. PERFORMED GVI NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LANDING GEAR — CONTAMINATED · airframe 27,370 hrs · 29,620 cycles

ON WALKAROUND POST FLIGHT, FOUND SMOKE AROUND LEFT GEAR AREA. REMOVED FROM SERVICE. PREFORMED GVI OF WHEEL ASSEMBLY, FOUND TO BE CONTAMINATED WITH RESIDUAL FLUID AND GREASE. JACKED LMLG ASSEMBLY AND REMOVED HUBCAP, REF AMM 32-41-01-000-801. PERFORMED GVI, NO DEFECTS NOTED. CLEANED AREA AS REQUIRED. REINSTALLED AND SAFETIED HUBCAP AND DOWNJACKED, REF AMM 32-41-01-400-801. C/W GVI OF BRAKE LINES, IAW AMM TASK 32-40-00-210-804. NO DEFECTS NOTED THROUGHOUT INSPECTION, BELIEVE PAX OBSERVATION TO HAVE BEEN RESIDUAL FLUID AND GREASE. RETURNED TO SERVICE.

Part: BRUSH BLOCK — WORN (NR 1 PROPELLER) · airframe 27,141 hrs · 29,353 cycles

CLIMBING THROUGH 14,000 FT PROP DEICE CAUTION ILLUMINATED. PERFORMED E&A CHECKLIST, RESET UNSUCCESSFUL. PROP DE-ICE CAUTION REMAINED ILLUMINATED FOR DURATION OF FLIGHT. DIVERTED, LANDING UNEVENTFUL, REMOVED FROM SERVICE. INTERROGATED CDS, FOUND FC OPEN PHASE B ON NR 1 TMCU. DURING TROUBLESHOOTING, NOTED POSSIBLE WEAR ON CENTER SLIP RING OF NR 1 PROP, FOUND TO BE WITHIN LIMITS, PER DOWTY CMM 61-10-49. REPLACED NR 1 BRUSH BLOCK, PER AMM 30-61-00-000/400-801 AND C/W FUNC TEST OF PROPS ANTI-ICING, REF AMM 30-61-00-720-801. OPERATIONS CHECK GOOD. OPEN PHASE B FC AND PROP DE-ICE CAUTION LIGHT DO NOT RETURN. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG LOCK) · airframe 26,903 hrs · 29,094 cycles

UPON GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE & GEAR HANDLE DISAGREE LIGHT STAYED ILLUMINATED FOR ABOUT 30 SECONDS. MAIN GEAR OPERATED NORMAL. ALL OTHER PARAMETERS WERE NORMAL. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED NOSE LANDING GEAR LOCK ACTUATOR. LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM FUNCTIONAL TEST GOOD, SEVERAL TIMES, IAW DHC-8-400 MM TASK3 32-31-00-720-801. RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 26,162 hrs · 28,278 cycles

DURING THE LANDING GEAR EXTENSION THE LANDING GEAR NOSE DOOR REMAINED OPEN WITH AN AMBER INDICATION ON THE MAIN PANEL. CHECKING THE ALTERNATE GEAR LIGHTS, THE NOSE GEAR WAS NOT INDICATING DOWN AND GREEN. WE RAN THE LG ALT EXT. CHECKLIST 10.14. WE TAXIED UNDER OWN POWER TO THE GATE. REMOVED FROM SERVICE. REPLACEMENT OF FAILED NGLK2 SENSOR, OTHER TROUBLESHOOTING AND GEAR OPS CHECKS. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 25,865 hrs · 27,937 cycles

SEVERE ICE ENCOUNTER FL 230 DESCENDED LOWER. AIR FRAME VIBRATION FROM 230 TO 146 SHIELD ICE 10K. AUTOPILOT OFF PROPS 1020. ELEVATOR FEEL SLUGGISH. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CONSULTED REPORTING FLIGHT CREW FOR FURTHER DETAILS, NO AIR FRAME OR PROP DEICE SYSTEM ABNORMALITIES WHEN EXCESSIVE ICING WAS ENCOUNTERED. VIBRATION WAS NOT PRESENT AFTER EXITING ICING CONDITIONS. C/W OPERATIONAL CHECKS AT REQUEST OF MTX CTL OF THE AIRFRAME PNEUMATIC DEICE SYSTEM IAW Q400 AM TASK 30-11-00-720-801 AND OPERATIONAL CHECK OF PROP DEICE IAW Q400 TASK 30-61-00-720-801 AS A PRECAUTIONARY MEASURE. OPS CHECK GOOD. C/W GVI OF AIRFRAME AND HORIZONTAL STAB AND COMPLIED WITH OPERATIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM IAW 27-30-00-710-801. OK FOR CONTINUED SERVICE. RETURNED TO SERVICE.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 25,734 hrs · 27,784 cycles

ILLUMINATED EXIT SIGN ADJACENT TO THE TYPE 2/3 EMERGENCY EXIT DOOR SIGN IS LOOSE. LIGHT STILL ILLUMINATES PROPERLY. REMOVED FROM SERVICE. REPLACED LOWER FORWARD EMERGENCY EXIT DOOR SIGN AT TYPE 2/3 EMER DOOR IAW Q400 AMM 33-51-06-000-801/400-801. OPS TEST PASS. NO FURTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: LINER — OUT OF POSITION (PAX DOOR) · airframe 25,640 hrs · 27,682 cycles

F/A REPORTS THE AFT PASSENGER DOOR IS CREAKING. PRESSURIZATION IS NORMAL. REMOVED FROM SERVICE. FOUND UNDER HINGE COVER ASSY ON LOWER LINER (AFT PASSENGER DOOR) TO BE JAMMING UP, AND MAKING "CREAKING" NOISE ON MOVEMENT. REMOVED AND REPLACED LOWER LINER, REF Q400 AMM 25-26-21-000-801 STEP 4.C AND 25-26-21-400-801 STEPS 4.C, 5.B, 5.D, 5.J, 5.K. DOOR OPERATES AS REQUIRED AND OPS TEST GOOD. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 25,072 hrs · 27,020 cycles

ON TAKEOFF "LANDING GEAR INOP" ILLUMINATED WHEN GEAR HANDLE RAISED. N GEAR (AMBER) ON GEAR ADVISORY ILLUMINATED ALL OTHER LIGHTS DARK. RAN LANDING GEAR INOP CHECKLIST. WHEN WE GOT TO GEAR HANDLE DOWN PORTION ALL 3 GEAR DOWN LIGHTS ILLUMINATED . N DOOR REMAINED ILLUMINATED. WE STOPPED CHECKLIST THERE AS WE HAD 3 GREEN BOTH ON PANEL AND IN THE FLOOR (EXTENSION PANEL). F/A'S ADVISED THE MAINS WERE EXTENDED THE WHOLE TIME EVEN GEAR INDICATION WAS THAT THEY WERE UP. UPON LANDING WE HAD NO NOSE WHEEL STEERING, BUT "NOSE STEERING" NEVER ILLUMINATED. DECLARED EMERGENCY. RETURNED TO FIELD. LANDING UNEVENTFUL. FERRIED. REMOVED FROM SERVICE. REPLACED LANDING GEAR CONTROL PANEL. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM REF AMM TASK 32-31-00-710-801 PER MANAGEMENT REQUEST. OPS CHECKS GOOD. NO OTHER DEFECTS NOTED. NO FAULT IN PSEU. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 24,457 hrs · 26,269 cycles

FA REPORTS THAT THE INTERIOR HANDLE ON THE TYPE II/III EMERGENCY DOOR IS LOOSE. REMOVED FROM SERVICE. RESECURED H/W ON EMERGENCY DOOR HANDLE. DOOR OPERATES NORMALLY AS REQUIRED. NO OTHER DEFECTS NOTED. REMOVED AND REINSTALLED UPPER RT FWD DOOR IAW AMM TASK 52-22-00-000/400-801. RETURNED TO SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 23,993 hrs · 25,744 cycles

FLIGHT CREW EXPERIENCED 1 UNCOMMANDED AUTO PILOT DISENGAGE, 1 FAILURE TO CAPTURE ALT WHEN ALT SEL SELECTED, AND 1 UNCOMMANDED ALT OFF AFTER ALT CAPTURE. PLACED ON MEL 34-60-1B. C/W FIM 22-11-00-810-880 FOR AP DISENGAGE, AND INTEROGATED CDS PER AMM 45-00-34-742-801 FOR AP AND FD FAULTS, NONE FOUND. C/E HGS RTS PER MTC 6343510 CLEAR MEL.

Part: PROPELLER — OUT OF BALANCE (NR 2) · airframe 22,950 hrs · 24,547 cycles

AFTER TAKEOFF, AIRFRAME VIBRATION FELT IN CONTROL YOKE AS WELL AS PILOT SEAT. INTENSITY WAS CYCLICAL FROM LIGHT TO MODERATE AT ALL AIRSPEEDS AND ALTITUDES. GREATEST INTENSITY WAS FELT BELOW 6,000 FEET. DIVERTED, AND LANDED UNEVENTFUL. REMOVED FROM SERVICE. PERFORMED A PROPELLER BALANCING. FOUND THE NR 2 PROP IPS TO BE HIGH. R & R NR 2 PROPELLER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.

Part: DISCHARGE TUBE — DAMAGED (FIRE BOTTLE) · airframe 22,545 hrs · 24,082 cycles

FOUND FWD CARGO FIRE BOTTLE DISCHARGE TUBE DAMAGED. R & R THE FIRE BOTTLE DISCHARGE TUBE IAW 26-22-03-000-801, PARA 4A (6), AND AMM 26-22-03-400-801, PARA 1-4 (H).

Part: BULKHEAD — UNSECURE (CARGO BAY) · airframe 22,328 hrs · 23,861 cycles

FWD BULKHEAD CAME LOOSE AND OBSTRUCTS MCD. REMOVED FROM SERVICE. SECURED THE BULKHEAD WITH LATCHES. NO FURTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 22,134 hrs · 23,654 cycles

EMERGENCY LIGHTS SWITCH NEXT TO FORWARD FA HAS INOPERATIVE BACKLIGHTS. REPLACED THE LAMPS IN THE SWITCH.

Part: LIGHT — OBSTRUCTED (CABIN FLOOR) · airframe 22,084 hrs · 23,599 cycles

FORWARD GALLEY DOOR WILL NOT OPEN FULLY. FOUND FWD GALLEY LWR DOOR CONTACTING FLOOR LIGHT STRIP. REMOVED THE LIGHT STRIP AND FOUND EXCESSIVE FLOOR TAPE ATTACHED. APPLIED THE CORRECT FLOOR TAPE AND INSTALLED, SECURED WET FLOOR.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 21,976 hrs · 23,498 cycles

NR 2 SEAT TRACK FROM BS 229.5 - 571.5 WAS FOUND CORRODED. THE SEAT WAS REPLACED IAW SRM 51-42-15-02-01, 51-42-05-02-01, 51-42-45-02-01, AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 21,976 hrs · 23,498 cycles

SEAT TRACK NR 10 FROM -39.00 - 10.50 CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15.

Part: DOUBLER — CORRODED (LAVATORY) · airframe 21,976 hrs · 23,498 cycles

LAVATORY INTERNAL DOUBLER CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-05.

Part: BEAM — CORRODED (PAX DOOR) · airframe 21,976 hrs · 23,498 cycles

AFT PASSENGER DOOR NR 2 BEAM CORRODED. THE BEAM WAS REPLACED IAW SRM 51-42-05, 51-40-15, 51-41-05, 51-42-45. AND DWG 85217301

Part: RING ASSEMBLY — DAMAGED (GROUND AIR) · airframe 21,976 hrs · 23,498 cycles

GROUND AIR SERVICING CONNECTION POINT DAMAGED. GROUND AIR SERVICING RING PLATE REPLACED IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (FWD CARGO BAY) · airframe 21,976 hrs · 23,498 cycles

FWD CARGO DOOR THRESHOLD IS CORRODED. THE THRESHOLD WAS REPLACED IAW SRM 51-42-05-02-01, 51-42-45, & 51-42-75.

Part: FLANGE — CRACKED (KICKPLATE) · airframe 21,976 hrs · 23,498 cycles

PILOTS BULKHEAD KICKPLATE FLANGE CRACKED. THE KICKPLATE FLANGE WAS REPAIRED IAW SRM 53-10-25.

Part: SEAT TRACK — CORRODED · airframe 21,976 hrs · 23,498 cycles

SEAT TRACK NR 11 FROM 10.50 - 102.50 IS CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-15, 51-42-05.

Part: SEAT TRACK — CORRODED (BS 571-.5-668) · airframe 21,976 hrs · 23,498 cycles

SEAT TRACK NR 3 FROM BS 571.5 - 668 IS CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, AND 51-42-45-02-01.

Part: FRAME — CORRODED (BS 156) · airframe 21,976 hrs · 23,498 cycles

CORRODED FRAME FLANGE, BS 156 BETWEEN STRINGERS 30L- 30R. BLENDED THE FRAME FLANGE AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-02-09. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801.

Part: SEAT TRACK — CORRODED (BS 670-782) · airframe 21,976 hrs · 23,498 cycles

SEAT TRACK 16 FROM BS 670 - 782 CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-42-05, AND 51-40-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,976 hrs · 23,498 cycles

SEAT RAIL 9 FROM FS 670.00 - FS 782.00 IS CORRODED. SEAT RAIL 9 REMOVED SRM 51-42-05, 51-40-15. NEW SEAT RAIL 9 INSTALLED IAW SRM 51-42-05, 51-40-15.

Part: CIRCUIT BREAKER — OPEN · airframe 21,583 hrs · 23,109 cycles

AUTOFEATHER TEST FAILED, SHOWS ABORT BELOW BOTH A/F TEST. REMOVED FROM SERVICE. NOTED FADEC 2 DU ON ED AND FAULT CODE 30 B IN CDS. FOUND THE CIRCUIT BREAKER LT ESS K6 PROP 2 PEC B OPEN. RESET THE CIRCUIT BREAKER IAW GPM 9.2.2.1. NO MESSAGE ON ED, FAULT CODE 30 B CLEARED, CIRCUIT BREAKER REMAINS CLOSED, AND AUTOFEATHER TEST PASSED. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (AFT CARGO DOOR) · airframe 21,326 hrs · 22,857 cycles

DURING TAXI TO RUNWAY, AFT CARGO DOOR WARNING. ABORTED TAKE OFF. REMOVED FROM SERVICE. COMPLIED WITH INSPECTION OF AFT THE CARGO DOOR IAW 05-0029. NO DEFECTS FOUND. DOOR HANDLE OPERATE SMOOTHLY AND FREELY. OPS CHECK OF AFT CARGO DOOR GOOD IAW AMM 52-31-00-710-801. ACFT GOOD FOR CONTINUED SERVICED. AIRCRAFT RETURNED TO SERVICE.

Part: LATCH — UNSECURE (ZONE 800) · airframe 20,795 hrs · 22,286 cycles

DITCHING DAM SLOT ON THE MAIN CABIN DOOR DOES NOT LINE UP. AIRCRAFT REMOVED FROM SERVICE. FOUND FORWARD DRAFT BULKHEAD UPPER LATCHES NOT SECURED. SECURED LATCHES. CHECKS GOOD. LINES UP. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 20,531 hrs · 22,018 cycles

AFTER TAKEOFF, DOOR WARNING ILLUMINATED WITH AN ASSOCIATED, AFT CARGO DOOR UNSECURE INDICATION AT APPROXIMATELY 3000 FT. CABIN DID NOT APPEAR TO BE PRESSURIZING NORMALLY. RETURNED TO FIELD. LANDING UNEVENTFUL. ACFT TAXIIED BACK TO THE GATE WITH THE AFT BAGGAGE DOOR HANDLE UNLOCKED. CYCLED DOOR SEVERAL TIMES. NO DEFECTS NOTED. SECURED AFT BLOWOUT PANEL. PRESSURIZED AND DEPRESSURIZED ACFT IAW AMM 21-00-00-863-801/802. DOOR REMAINS SECURE. RETURNED TO SERVICE.

Part: HINGE FITTING — BROKEN (INTERIOR DOOR) · airframe 20,096 hrs · 21,563 cycles

FORWARD FA EMERGENCY EQUIPMENT COMPARTMENT DOOR SPRING HINGE NOT HOLDING DOOR CLOSED. REPLACED BOTH HINGE & SPRING ASSEMBLIES AND BOTH LATCHES. CHECKED GOOD. DOOR SPRINGS CLOSED AND LATCHES. NO FURTHER DEFECTS NOTED.

Part: ROLLER — LACK OF LUBE (GALLEY DOOR) · airframe 20,041 hrs · 21,513 cycles

AFT GALLEY SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED DOOR SEAL AND LUBRICATED GUIDE ROLLERS. DOOR OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: DISPLAY — FAILED (ZONE 200) · airframe 19,977 hrs · 21,448 cycles

NR 2 PFD MON FAILED MESSAGE ON ED WITH AFCS FAIL MSG ON NR 2 PFD WITH RED FFAIL INDICATIONS ON NR 2 PFD WITH AVIONICS CAUTION LIGHT AFTER TOUCH DOWN. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. FOUND NO DATA FROM PFD 2 IN CDS. REVERSION TO MFD 2 SHOWS PFD 2 DATA. REMOVED REPLACED AND LLM RTS NR 2 PFD IAW TC 6316104. AVIONICS CAUTION DOES NOT ILLUMINATE. CDS SHOWS NO AVIONICS FAULTS. CW GVI OF ALL PFD 2 GROUND WIRES NDN.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 19,854 hrs · 21,327 cycles

NR 1 AC GENERATOR MASTER CAUTION DURING CLIMB OUT. RETURN TO FIELD. LANDING UNEVENTFUL. FOUND EPCU FAULT 25, NO RELEVANT CDS FAULT. R & R THE NR 1 GENERATOR IAW MTC 6242101. OPS & LEAK CHECKED GOOD.

Part: LIGHT — DETACHED (CABIN) · airframe 19,788 hrs · 21,268 cycles

EMERGENCY LIGHT STRIP IN FRONT OF SEATS 2D & 2E IS LIFTING OFF THE CARPET. REMOVED & REPLACED THE EMERGENCY LIGHT ASSY IAW AMM TASK 33-51-16-000-801/400-801. RETURNED TO SERVICE.

Part: COVER — BROKEN (ZONE 200) · airframe 19,745 hrs · 21,228 cycles

EMERGENCY LIGHT SWITCH COVER BROKEN AT FORWARD FA STATION. REPLACED THE SWITCH COVER. CHECKS GOOD. RETURNED TO SERVICE.

Part: ANTENNA — FAULTY (LOC/VOR) · airframe 19,701 hrs · 21,176 cycles

BOTH VHF NAV 1 & 2 WOULD NOT RECEIVE. NO IDENTS OR NEEDLES. DME DISPLAYED WITHOUT IDENT. ON RETURN TO PDX DURING DESCENT BELOW 20,000' BOTH VHF NAVS BEGAN TO RECEIVE AND DISPLAY BTG WITH VERY FAINT IDENT. LANDING WEIGHT LESS THAN #62000. REMOVED AND REPLACED LT AND RT VOR/LOC ANTENNAS IAW MTC 6345102. OPS CHECK GOOD. A/C REMAINS CAT III QUALIFIED, PLACARD READS CAT III.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 19,489 hrs · 20,962 cycles

BATTERY PACK FOR THE FORWARD LT EMERGENCY LIGHT FAILS AN OPS CHECK. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-00-801 AND 33-51-01-400-801. CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (AFT PAX DOOR) · airframe 19,440 hrs · 20,918 cycles

AFT PASSENGER DOOR IS UNABLE TO BE OPENED FROM THE OUTSIDE. INSIDE WORKS FINE. LUBED THE EXTERNAL DOOR HANDLE SHAFT. C/W OPERATIONAL TEST IAW AMM 52-12-00-710-802. CHECKS GOOD. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,702 hrs · 20,158 cycles

EMERGENCY LIGHTS IN THE AFT FUSELAGE AND AFT DOOR ARE INOPERATIVE. REPLACED THE RT NR 4 EPSU BATTERY PACK IAW AMM 33-51-00-820-801. OPS CHECKED GOOD.

Part: AOA — OBSTRUCTED (STALL WARNING) · airframe 17,103 hrs · 18,436 cycles

ABORTED TAKEOFF FOR PUSHER FAIL CAUTION LIGHT. FOUND AOA COVER INTERFERING WITH AOA VANE. REPLACED COVER AND VANE. RETURNED TO SERVICE.

Part: STALL WARNING — MALFUNCTIONED · airframe 17,091 hrs · 18,424 cycles

ABORTED TAKEOFF 60-70 KNOTS FOR PUSHER SYS FAIL. PERFORMED AOA FUNCTIONAL TEST AND OPS TEST OF ELEVATOR CONTROL STICK PUSHER. NO FAULTS FOUND. RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (AFT PAX) · airframe 16,946 hrs · 18,264 cycles

F/A REPORTS THAT THE AFT PASSENGER DOOR IS DIFFICULT TO OPEN. LUBED THE CAM FOLLOWER NEEDLE BEARINGS. OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ENGINE — ODOR · airframe 16,811 hrs · 18,137 cycles

DESCENT THROUGH APROXIMATELY 130000" FOR LANDING. F/A REPORTED SMOKE IN THE CABIN. DECLARED EMERGENCY, RAN CHECK LIST. SMOKE CONTINUED TILL EVACUATION, ON RUNWAY. ENGINE POWER WAS APPROXIMATELY 20 PERCENT TORQUE. BLEED AUTO ICE PROTECTION ON. ACFT CURRENTLY OUT OF SERVICE FOR REPLACEMENT OF NR 2 ENGINE.

Part: FRAME — CORRODED (BS 216) · airframe 16,752 hrs · 18,077 cycles

CORROSION FOUND ON FRAME FLANGE AT BS 216 BETWEEN STRINGERS 31 & 32L. WITHIN LIMITS IAW SRM 53-00-00, REPAIR 09.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 13 CORRODED. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15, 51-41-00, AND DWG 8/5307071 REV A.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 8 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, SRM 51-42-05-02-01, SRM 51-40-15-02-01. SRM 51-42-05, SRM 51-41-00 AND DWG 85338201, REV E.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 7 REQUIRES REPLACEMENT, PN 85361510-103. REMOVED 2 DRIP ANGLES COMMON TO SEAT TRACK NR 6 AND NR 7, REF SRM 51-42-05-02-01. INSTALLED 2EA DRIP ANGLE COMMON TO SEAT TRACK NR 6 AND NR 7 IAW SRM 51-42-05. REMOVED 5 EA WIRE HARDNESS STANDOFF ON SEAT TRACK NR 7 IAW SRM 51-42-05. INSTALLED 5 EA WIRE HARDNESS STANDOFF ON SEAT TRACK NR 7 IAW SRM 51-42-05. REMOVED BONDING JUMPER ON SEAT TRACK NR 7 AT APPROXIMATELY X294.00 IAW SRM 51-41-00. INSTALLED BONDING JUMPER ON SEAT TRACK NR 7 AT APPROXIMATELY 294.00 IAW SRM 51-41-00. REMOVED ALL BOLTS ON SEAT TRACK NR 7 AND RIVETS COMMON TO TRACK AND WEB BETWEEN X469.5 AND X439.5 IAW SRM 51-42-05 AND SRM 51-41-00. INSTALLED NEW SEAT TRACK NR 7 IAW SRM 51-42-05, SRM 51-41-00 AND DWG 85361501, REV E LOCATED AND DRILLED NEW SEAT TRACK NR 7, PN 85361510-103, ALL BOLT HOLES AND HOLES COMMON TO WEBS REF SRM 51-40-07-02-01. LOCATED AND DRILLED SEAT TRACK NR 7 AT FWD AND AFT SPLICE LOCATIONS REF SRM 51-40-07, REPAIR-01, DWG 85361501, REV D. LOCATED AND DRILLED SEAT TRACK NR 7 DRIP ANGLE REF SRM 51-40-07-02-01, DWG 85361501, REV D. PERFORMED BONDING CHECK ON SEAT TRACK NR 7, REF AMM 51-80-00-760-830. REMOVED FWD SPLICE OF SEAT TRACK NR 7 IAW SRM 51-42-05 AND SRM 51-40-15. INSTALLED FWD SPLICE OF NEW SEAT TRACK NR 7 IAW SRM 51-42-05 AND SRM 51-40-15 AND DWG 85307071, REV A. REMOVED AFT SPLICE OF SEAT TRACK NR 7 IAW SRM 51-42-05 AND SRM 51-40-15. INSTALLED AFT SPLICE COMMON TO TRACK NR 7 AND NR 8 IAW SRM 51-42-05, SRM 51-40-15 AND DWG 85307071, REV A.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK, NR 5,CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-44-00, SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 11, CORRODED. REMOVED AFT SPLICE COMMON TO SEAT TRACK 11 AND 12, REF SRM 51-42-05-02-01 AND SRM 51-40-15-02-01. INSTALLED AFT SPLICE COMMON TO SEAT TRACK 11 AND 12 REF SRM 51-42-05 AND 51-40-15 AND DWG 85328201 2013-01-19. REMOVED DRIP ANGLE FROM BS 47-975 TO BS 176.0 COMMON TO SEAT TRACK 11 AND 12 REF SRM 51-42-05-02-01. DRIP ANGLE INSTALLED REF SRM 51-42-05-51-40-15, PN 85307495-112 COMMON TO SEAT TRACK NR 11 AND NR 12. DISPLACED 4 EA WIRE BUNDLES BTW STA 32.400 TO STA 47.975, 2EA WIRE BUNDLES BTW STA 71.200 TO 94.800, 1EA WIRE BUNDLES BETWEEN BS 94.800 TO 116.0 REF WM 20-12-10-201. INSTALLED 4 WIRE BUNDLES BETWEEN FS 32.4-47.9, 2 BUNDLES FS 71.2-94.8, 1 BUNDLES, FS 94.8-116.0, REF WM 20-12-10-201. REMOVED SEAT TRACK NR 11, PN 85328210-115, REF SRM 51-42-05-02-01 AND SRM 51-41-00-00-01. INSTALLED 3 EA TRACK NR 11, REF SRM 51-42-05 AND 51-41-00 AND DWG 85328201 2013-01-19. LOCATED AND DRILLED FRAME ATTACH POINTS AND WEB BETWEEN BS 1.000 TO BS 116.00, REF SRM 51-40-07-02-01. LOCATE AND DRILL AFT SPLICE 11 AND 12, REF SRM 51-40-07. INSTALLED FASTENERS ON SEAT TRACK NR 10 AND NR 11 SPLICE REF SRM 51-42-05, 51-40-15, DWG 85328201. RESTORED FINISH REF SRM 51-25-20.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 15, CORRODED. REMOVED SPLICE COMMON TO SEAT TRACK 14 AND 15, REF SRM 51-42-05-02-01 AND SRM 51-40-15-02-01. INSTALLED SPLICE COMMON TO SEAT TRACK NR 14 AND 15, REF SRM 51-42-05-02-01 AND SRM 51-40-15-02-01. REMOVED SEAT TRACK NR 15, PN:85338210-115, REF SRM 51-41-00-02-01 AND SRM 51-42-05-02-01. INSTALLED NR 15 SEAT TRACK, PN:85338210-115, REF SRM 51-42-05-02-01 AND SRM 51-41-00-02-01. RECEIVED NEW SEAT TRACK, PN:85338210-115, LOCATED AND DRILLED SEAT TRACK, REF SRM 51-40-07-02-01. REMOVED SPLICE COMMON TO SEAT TRACK NR 15 & 16, REF SRM 51-42-05-02-01 AND SRM 51-40-15-01-02. INSTALLED SPLICE COMMON TO SEAT TRACK NR 15 AND 16, REF SRM 51-42-05. RESTORED FINISH REF SRM 51-25-20, 51-40-15, DWG:85338201 REV E.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK, NR 2, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 16,752 hrs · 18,077 cycles

SEAT TRACK NR 10, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00 AND SRM 51-40-15.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 15,353 hrs · 16,568 cycles

AFTER SELECTING THE GEAR DOWN, THE RED NOSE UNSAFE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY 45 SEC TO 1 MIN BEFORE EXTENDING WITH FORCE. THE NOSE DOOR, AMBER LIGHT EXTINGUISHED APPROXIMATELY 30 SEC AFTER NOSE GEAR EXTENDED. LANDING UNEVENTFUL. INTERRROGATED PSEU AND FOUND 2 CURRENT FAULTS RGDRCL AND LGDRCL BOTH UNREASONABLE FAR. FERRIED FOR REPAIRS. VERIFIED PHYSICAL GAPS OF RGDRCL AND LGRDRCL WERE WITHIN LIMITS IAW AMM 32-61-06-830-801. VERIFIED INDUCTANCE VALUES OF RGDRCL AND LGDRCL WERE WITHIN LIMITS IAW AMM TASK 32-61-00-280-801. VERIFIED NO PRESENT FAULTS IN PSEU. NO OTHER DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 14,772 hrs · 15,937 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. C/W LUBRICATION OF THE AIRSTAIR DOOR IAW AMM TASK 52-11-00-640-802, TR 52-524. OPS CHECK GOOD. RETURN TO SERVICE.

Part: RIB — CORRODED (DOOR FRAME) · airframe 14,721 hrs · 15,881 cycles

RIB ON AFT PAX DOOR SURROUND STRUCTURE AT FS X676.375 IS CORRODED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-05.

Part: SKIN — DENTED (BS 307) · airframe 14,721 hrs · 15,881 cycles

DENT IN RT FUSELAGE SKIN BS 307.2 2.7" ABOVE STR 9, 0.035" DEEP. REPAIRED IAW TC RD8/4-53-6266/3.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR ANGLE, BS 26.7 FROM STR 23 - 25P FOUND CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-05.

Part: RIB — CORRODED (DOOR FRAME) · airframe 14,721 hrs · 15,881 cycles

RIB ON AFT PAX DOOR SURROUND STRUCTURE AT BS 669.3 IS CORRODED . REMOVED AND REPLACED THE RIB IAW SRM 51-42-05.

Part: BEAM — CORRODED (DOOR THRESHOLD) · airframe 14,721 hrs · 15,881 cycles

EDGE BEAM FOUND CORRODED AT SERVICE DOOR THRESHOLD. FABRICATED NEW INNER EDGE BEAM IAW DWG 85339543, REV A, SHT 1. INSTALLED IAW SRM 51-42-75 AND TC-6-53-1160.

Part: RIB — CORRODED (DOOR FRAME) · airframe 14,721 hrs · 15,881 cycles

RIB ON AFT PAX DOOR SURROUND STRUCTURE AT BS 683.45 IS CORRODED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-05.

Part: BEAM — CORRODED (DOOR THRESHOLD) · airframe 14,721 hrs · 15,881 cycles

EDGE BEAM FOUND CORRODED AT SERVICE DOOR THRESHOLD. FABRICATED NEW EDGE BEAM IAW DWG 85339542, SHT 1. INSTALLED IAW SRM 51-42-75.

Part: BEAM — CORRODED · airframe 147,221 hrs · 15,881 cycles

INNER EDGE BEAM IS CORRODED. LOCATED & DRILLED NEW INNER EDGE BEAM IAW SRM 51-40-07, STEP 5, B. INSTALLED SRM 51-42-75.

Part: CHANNEL — CORRODED · airframe 14,721 hrs · 15,881 cycles

CHANNEL IS CORRODED. INSTALLED NEW CHANNEL IAW SRM 51-42-75 STEP 5D(3).

Part: RIB — CORRODED (DOOR FRAME) · airframe 14,721 hrs · 15,881 cycles

RIB ON AFT PAX DOOR SURROUND STRUCTURE AT BS 690.525 IS CORRODED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-05.

Part: RIB — CORRODED (DOOR FRAME) · airframe 14,721 hrs · 15,881 cycles

RIB, ON AFT PAX DOOR SURROUND STRUCTURE AT BS 697.6 IS CORRODED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR THRESHOLD BS 6.7 - 26.7 FOUND CORRODED. REMOVED THE THRESHOLD IAW SRM 51-42-05-02-01, STEP 4E(1-2). LOCATED DRILLED AND DEBURRED NEW THRESHOLD IAW SRM 51-40-07-02-01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR ANGLE AT STA X6.7, STR 25P FOUND CORRODED. REMOVED ANGLE IAW SRM 51-42-05-02-01, STEP 4E(2-8). INSTALLED NEW ANGLE IAW SRM 51-42-05-02-01, STEP 4D(3-10).

Part: BEAM — CORRODED · airframe 14,721 hrs · 15,881 cycles

EDGE BEAM, HAS CORRODED ON EMERGENCY DOOR THRESHOLD. LOCATED AND DRILLED NEW EDGE BEAM IAW SRM 51-40-07-02-01. INSTALLED IAW SRM 51-42-05-02-01, STEP 4D (1).

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR THRESHOLD X1 - 32.4 FOUND CORRODED. LOCATED AND DRILLED NEW THRESHOLD IAW SRM 51-40-07, REPAIR-01. INSTALLED IAW SRM 51-42-05002-01 STEP 4D (3-10).

Part: ANGLE — CORRODED (PAX DOOR) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR ANGLE, AT BS 26.7, STR 25P FOUND WITH CORROSION. COMPLIED WITH FORM M-184. REMOVED ANGLE IAW SRM 51-42-05-02-01, STEP 4E(2-8). INSTALLED NEW ANGLE IAW SRM 51-42-05-02-01, STEP 4D, 3-10. LOCATED, DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-40-07-02-01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 14,721 hrs · 15,881 cycles

FWD PASSENGER DOOR ANGLE AT BS 6.7 FROM S23 - 25P FOUND CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-05-02-01.

Part: LIGHT — UNSECURE (CABIN) · airframe 14,390 hrs · 15,546 cycles

FLOOR EXIT LIGHTS AT ROW 1B ARE LOOSE. SECURED THE LIGHTS IAW AMM TASK 33-51-16-400-801. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: OUTLET — CRACKED (NR 1 EXHAUST) · airframe 14,373 hrs · 15,531 cycles

F/A REPORTED THAT A PIECE OF METAL IS VIBRATING ON TOP OF THE NR 1 ENGINE EXHAUST. FOUND TO BE NR 1 ENGINE EXHAUST OUTLET. REPLACED NR 1 ENGINE EXHAUST OUTLET IAW AMM 78-10-26-00-400-801. ALSO, REPAIRED FOULING CONDITION BETWEEN AFT UPPER COWLING AND THE AFT EXHAUST ASSY IAW SRM 54-45-10-02-01. NDT (HFEC) C/W IAW 1-84-7A PT 6 511-00-01 AND SRM 54-45-10, STEP 5A 4. NO CRACKS FOUND. RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (PTU) · airframe 13,957 hrs · 15,067 cycles

PTU SWITCH LIGHT STAYED ILLUMINATED AFTER TAKEOFF. RETURNED TO FIELD. LANDING UNEVENTFUL. TESTED RELAYS IN PTU AUTO SYSTEM. RELAY 2921-1-K3 FAILED TO CLOSE WHEN COMMANDED. REPLACED RELAY IAW 20-30-16-960-801. RELAY OPS GOOD IAW TABLE 201 OF 24-50-60-710-804. PTU FUNCTIONAL TESTED GOOD SEVERAL TIMES IAW 29-11-61-720-801. CHECKED GOOD. REPLACED PTU SELEECTOR VALVE IAW 29-11-66-000-801, 29-11-66-400-801. OPS AND LEAK CHECKED GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 13,879 hrs · 14,985 cycles

FORWARD F/A EMERGENCY LIGHTS SWITCH DOES NOT ILLUMINATE. REPLACED THE LAMP FOR THE SWITCH. CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,844 hrs · 14,955 cycles

UNKNOWN ODOR IN AFT GALLEY. ODOR DID NOT SEEM TO CHANGE WITH APU BLEEDS ON OR OFF, OR WITH RECIRCULATION FAN ON OR OFF. INSPECTED ACFT, NO DEFECTS NOTED. UNABLE TO LOCATE ODOR SOURCE.

Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 13,046 hrs · 14,089 cycles

NR 1 ENGINE FAILS OVERSPEED GOVERNOR TEST. REMOVED & INSPECTED NR 1 ENGINE OSG CONNECTOR AND FOUND IT TO BE LOOSE AND DIRTY, CLEANED & INSTALLED CONNECTOR. PERFORMED OSG TEST IAW MTC 61200019, OPS TEST GOOD. RETURNED TO SERVICE.

Part: VALVE — FAILED (DEICE SYS) · airframe 12,487 hrs · 13,492 cycles

DURING DEPARTURE, THE DE-ICE PRESSURE CAUTION ILLUMINATED. COMPLIED WITH EC. DE-ICE PRESSURE =19 PSI PHASE FLIGHT =CLIMB, THE INBD SECTION ON THE LT HORIZONTAL STAB WOULD NOT ILLUMINATE. IT TESTS OK. LIGHT MODE SWITCH=SLOW. RETURNED TO FIELD, LANDING UNEVENTFUL. PERFORMED TACTILE INSPECTION ON ALL L/E WHILE INFLATED WITH NO DEFECTS NOTED. INTERROGATED CDS AND FOUND "LOW PRESSURE 6B FAIL" R & R THE NR 6 DDV IAW AMM TASKS 30-11-16-000&400-801. CLEARED FAULT FROM CDS. PERFORMED OPERATIONAL TEST OF THE DUAL DISTRIBUTING VALVES IAW AMM TASK 30-11-16-710-801. OPS TEST GOOD, CAUTION DID NOT RETURN. NO FAULT CODES. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 12,400 hrs · 13,388 cycles

EMERGENCY LIGHT STRIP LOOSE AT FRONT OF PASSENGER CABIN. SECURED EMERGENCY LIGHT IAW AMM TASK 33-51-16-400-801. RETURN TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 12,400 hrs · 13,388 cycles

EMERGENCY LIGHT LOOSE AT FRONT OF PASSENGER CABIN. SECURED EMERGENCY LIGHT IAW AMM TASK 33-51-16-400-801. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 12,362 hrs · 13,349 cycles

AUTOFEATHER FAILED TO ARM DURING TAKEOFF. INTERROGATED CDS AND FOUND EMV FAULT CODES 204A+B. PLA STUCK ON, PERFORMED FIM TASK 61-20-05-810-819, NOTED THAT PLA HIGH & LOW SWITCHES CHANGE STATE FROM REVERSE TO RATING. PERFORMED TEST OF AUTOFEATHER SYSTEM ENGINES OFF IAW MM TASK 61-20-00-710-801 OPS GOOD. PERFORMED HIGH POWER GROUND RUN AND NOTED THAT AUTOFEATHER ARMS AT POWER. REPEATED NUMEROUS TIMES OPS CHECKS GOOD. EMU FAULTS DID NOT RETURN. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST · airframe 12,311 hrs · 13,303 cycles

ON DAILY SYSTEM CHECK, AUTOFEATHER TEST FAILED ON LEFT SIDE. INTERROGATED CDS AND FOUND NR 1 PEC FAULTS 204 A+B AND 484 A+B. CLEARED PEC FAULTS AND COMPLIED WITH FIM TASK 61-20-05-810-819 STEPS 1-5A (3) PLA HIGH MICROSWITCH OPS CHECKED GOOD. COMPLIED WITH ANOTHER AUTOFEATHER TEST IAW AMM TASK 61-20-00-710-801. TESTS GOOD. NO OTHER FAULTS NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: BUTTON — FAILED (EMERGENCY LIGHTS) · airframe 12,275 hrs · 13,264 cycles

F/A REPORTED THAT THE EMERGENCY LIGHT BUTTON CAME OUT. SECURED EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: GUARD — MISSING (EMERGENCY LIGHTS) · airframe 12,166 hrs · 13,143 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH GUARD IS MISSING. REPLACED MISSING SWITCH GUARD FOR F/A EMERGENCY LIGHTING SWITCH WITH NEW FROM STOCK. SWITCH AND GUARD SECURE. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 11,544 hrs · 12,489 cycles

THE EMERGENCY LIGHT GUARD AT THE FORWARD F/A POSITION IS DETACHED. REPLACED THE SWITCH GUARD. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 11,443 hrs · 12,374 cycles

ROW 2 EMERGENCY EXIT LIGHT LENS FELL OUT. REPLACED THE LENS FOR THE RT EMERGENCY EXIT SIGN. RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,228 hrs · 12,175 cycles

EVIDENCE OF CORROSION AROUND MARKER ANTENNA MOISTURE WELL. REMOVED ATTACH SCREWS AT MARKER ANTENNA IAW SRM 51-41-00-00-01. REMOVED SMALL AMOUNTS OF CORROSION FROM MARKER ANTENNA AREA IAW SRM 51-21-00 (A)(1)(2). PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01. (C). FOUND CORROSION ONLY TO BE TRANSFER FROM GASKET. NO CORROSION FOUND ON FUSELAGE SKIN. INSTALLED MARKER ANTENNA IAW AMM TASK 34-51-31-400-801. COMPLIED WITH HORIZON T/C 6345104, NO DEFECTS NOTED.

Part: NUT PLATE — CORRODED (CARGO DOOR FRAME) · airframe 11,228 hrs · 12,175 cycles

FWD CARGO DOOR FWD UPPER STOP FITTING NUTPLATES CORRODED. REMOVED TOP CENTER WEB IAW SRM 51-42-45-02-01, 51-42-05-02-01 & 51-42-15-02-01. REMOVED FWD CARGO DOOR FWD UPPER STOP FITTING 28 IAW AMM 52-32-19-000-801, SUBTASK 52-32-19-020-046. REPLACED NUTPLATES WITH A NUT AND WASHER AT LOCATIONS D & B IAW SRM 52-00-00-01-01 & INSTALLED STOP FITTING IAW AMM 52-32-19-400-801, SUBTASK 52-32-19-420-045. INSTALLED TOP CENTER WEB PANEL IAW SRM 51-42-45-02-01 & 51-42-05-02-01. INSTALLED HUCK BOLTS FASTENERS IAW SRM 51-42-15-02-01. APPLIED PRIMER TO FASTENERS IAW SRM 51-25-10-02-01.

Part: BRACKET — CORRODED (DOOR SEAL) · airframe 11,228 hrs · 12,175 cycles

AIRSTAIR DOOR SEAL BRACKET AT X 13.5, CORRODED. FABRICATED BRACKET, PN 85307741-131 IAW DLA-2081-334808. OK TO TREAT AND PRIME. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NUTPLATE IAW SRM 51-42-73-02-01. PRIOR TO STEP ONE, REMOVED BRACKET IAW SRM 51-42-02-01. INSTALLED BRACKET IAW SRM 51-42-05-02-01.

Part: SILL — CORRODED (EMERGENCY EXIT) · airframe 11,228 hrs · 12,175 cycles

FOUND SILL CORRODED. REMOVED EMERGENCY EXIT SILL IAW SRM 51-42-05-02-01. LOCATED AND DRILLED NEW SILL IAW SRM 51-40-07-02-01 AND INSTALLED IAW SRM 51-42-05-02-01 AND 51-42-15-02-01.

Part: ANTENNA — CORRODED (DME) · airframe 11,228 hrs · 12,175 cycles

EVIDENCE OF CORROSION AROUND NR 2 DME ANTENNA. REMOVED NR 2 DME ANTENNA IAW AMM 34-53-11-000-801. REMOVED SMALL TRACES OF CORROSION FROM DME ANTENNA AREA IAW SRM 51-21-00.(A)(1)(2). PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01 (C). INSTALLED DME ANTENNA IAW AMM TASK 34-53-11-400-801. IN REF TO STEP 3 REF IS SRM 51-21-00-00-01 (A)(2).

Part: STOP FITTING — CORRODED (CARGO DOOR) · airframe 11,228 hrs · 12,175 cycles

FWD CARGO DOOR AFT UPPER STOP FITTING NUTPLATE CORRODED. REMOVED STOP FITTING IAW AMM 52-32-19-000-80. INSTALLED STOP FITTING IAW AMM 52-32-19-400-801, SUBTASK 52-32-19-420-141.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 11,228 hrs · 12,175 cycles

SUPPORT ANGLE BY FWD PAX DOOR HAS SIGNS OF CORROSION. DRILLED OFF OLD ANGLE SUPPORT IAW SRM 51-40-07-02-01. LOCATED HOLES ON NEW ANGLE SUPPORT IAW SRM 51-40-07-02-01. COUNTER SUNK ALL HOLES USING A PILATED COUNTER SINK BIT. INSTALLED NEW ANGLE SUPPORT WET WITH SEALANT IAW SRM 51-42-05-02-01.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 11,228 hrs · 12,175 cycles

FWD PAX DOOR THRESHOLD HAS SIGNS OF CORROSION. REMOVED FWD PAX DOOR THRESHOLD IAW SRM 51-42-05-02-01. DRILLED UP NEW THRESHOLD, FWD CORNER FITTING, AND SEAL PLATE IAW SRM 51-40-07-02-01. INSTALLED FWD PAX DOOR THRESHOLD IAW SRM 51-42-05-02-01.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON FWD PAX DOOR SILL. REMOVED FWD PASSENGER AIRSTAIR DOOR ASSY IAW AMM 52-11-00-000-801. DRILLED OFF FWD PAX DOOR TOP SILL PLATE IAW SRM 51-40-07-02-01. DRILLED OFF PLASTIC STRIP ON TOP OF SILL PLATE IAW SRM 51-40-07-02-01. DRILLED HOLES FOR PLASTIC ABRASION STRIP ONTO SILL PLATE IAW SRM 51-40-07-02-01. RIVETED ABRASION STRIP ONTO SILL PLATE WET WITH SEALANT IAW SRM 51-42-05-02-01. REF WO Q-1483885-N, OP 298 FOR INSTALLATION OF THE SILL PLATE.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 11,228 hrs · 12,175 cycles

RT WING FUEL ACCESS PANEL 624AT OTBD PANEL RADIUS FOUND CORROSION. BLENDED AREA IAW SRM 57-20-35-02-02. MAX DEPTH .007 & WITHIN LIMITS. PERFORMED NDT INSPECTION OF THE RT WING FUEL PANEL 624AT IAW NDT MANUAL, PART 6 51-00-01. 25-801 & PART 1 51-00-06-910-801 EDDY CURRENT METHOD. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01. APPLIED PRIMER WHERE NECESSARY IAW SRM 51-25-10-02-01.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 11,228 hrs · 12,175 cycles

FWD CARGO DOOR HAS CORROSION ON 2 UPPER NUTPLATES FOR THE UPPER AFT ROLLER BEARING MOUNT. REPLACED NUTPLATE WITH A NUT AND WASHER IAW RD 8/4-52-1027.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 11,228 hrs · 12,175 cycles

FWD CARGO DOOR HAS CORROSION ON THREE NUTPLATES FOR THE UPPER FWD ROLLER BEARING MOUNT. REMOVED NUTPLATE AND REPLACED IT WITH A NUT AND WASHER IAW RD 8/4-52-1027.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,228 hrs · 12,175 cycles

RT INBD SEAT TRACK NR 10 FROM FS 39 - 10.5 CORRODED WITH PREVIOUS BLENDS. REMOVED SEAT TRACK IAW SRM 51-15-02-02-01 AND 51-42-05-00-01. INSTALLED NEW SEAT TRACK IAW SRM 51-41-05-00-01, 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,228 hrs · 12,175 cycles

RT INBD SEAT TRACK NR 11 FROM FS 10.50 THROUGH FS 102.50 CORRODED WITH PREVIOUS BLENDS. REMOVED RT INBD SEAT TRACK NR 11 IAW SRM 51-15-02-02-01 AND 51-42-05-00-01. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01. INSTALLED HILITES AND SOLID RIVETS OF NR 11 SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. APPLIED TOPCOAT AND AVDEC GREEN TO MOUNTS AT SEAT TRACK. APPLIED AV-DEC SELF LEVELING GREEN CORROSION INHIBITING COMPOUND INSIDE RAILS NR 11 IAW SRM 51-21-10-02-04.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 11,228 hrs · 12,175 cycles

RT WING LANDING FOR FUEL PANEL 624AT FOUND CORRODED OTBD RADIUS. BLENDED AREA IAW SRM 57-20-30-01-02. MAX DEPTH AT .008 FOUND TO BE OUT OF LIMITS. COMPLIED WITH NDT INSPECTION OF THE FUEL PANEL LANDING OF THE RT WING FOR PANEL 624AT IAW NDT MANUAL PART 1 51-00-01-250-801 EDDY CURRENT METHOD. NO DEFECTS NOTED. UPON FURTHER INVESTIGATION FOUND BLENDED AREA TO BE WITHIN LIMITS IAW SRM 52-20-35-02-05 TREAT AND PRIME AREA STILL REQUIRED. PRIMED AND ALODINE FUEL PANEL 624AT LANDING IAW 57-21-10-02-01 AND 51-25-10-02-01.

Part: PANEL — CORRODED (CARGO BAY) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON AFT CARGO PANEL 144HZ. REPLACED UNSERVICEABLE PANEL WITH NEW SERVICEABLE PANEL. COUNTERSUNK ALL FASTENER HOLES ON NEW 144HZ AFT CARGO PANEL IAW SRM 51-40-07-02-01. APPLIED ALODINE TO COUNTERSUNK FASTENER HOLE IAW SRM 51-21-10-02-01.

Part: PANEL — CORRODED (CARGO BAY) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON AFT CARGO PANEL 144GZ. DRILLED AND COUNTER SUNK HOLES IN REPLACEMENT PANEL 149GZ IAW SRM 51-40-07-02-01.

Part: PANEL — CORRODED (CARGO BAY) · airframe 11,228 hrs · 12,175 cycles

SUSPECTED CORROSION ON AFT CARGO PANEL 144JZ. DRILLED AND COUNTERSUNK HOLES IN REPLACEMENT PANEL 144JZ IAW SRM 51-40-07-02-01.

Part: PANEL — CORRODED (CARGO BAY) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON AFT CARGO PANEL 144LZ. DRILLED AND COUNTERSUNK HOLES IN REPLACEMENT PANEL IAW SRM 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (BS 325) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT I/B SEAT TRACK AT FS 325. BLENDED CORROSION AT R/H INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 624.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 624.5. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8 NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 536) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 536. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW 53-20-49-02-02. PERFORMED FPI ON BLENDED AREA IAW NDT MANUAL, PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 579) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 579. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL, PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 464) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 464. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW Q400 SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL, PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 381) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 381. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 480) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON RT INBD SEAT TRACK AT FS 480. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-020-01.

Part: SEAT TRACK — CORRODED (BS 608.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT FS 608.5. BLENDED SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL, PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 519) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 519. BLENDED SEAT TRACK IAW SRM 51-21-00-00-01. BLEND WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 639) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT FS 639. BLENDED SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 412) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 412. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8 NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 259.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT FS 259.5. BLENDED CORROSION AT LT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 457) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 457. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMTIS IAW SRM 53-20-49-02-02. PERFORMED FLPI OF BLENDED AREA IAW NDT MANUAL PART 8 NO DEFECTS NOTED. ALODINES IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 396.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT FS 396.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 272) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 272. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8, NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 426) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 426. REMOVED CORROSION IAW SRM 51-21-00-00-02. CORROSION WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 656.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT FS 656.5. BLENDED SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 433) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 433. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFOMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 388) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT BS 388. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 503.5-506) · airframe 11,228 hrs · 12,175 cycles

THREE SPOTS OF CORROSION ON LT INBD SEAT TRACK BETWEEN BS 503.5 - 506. BLENDED SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 489.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 489.5. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI OF BLENDED AREA IAW NDT MANUAL PART 8 NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 240) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 240. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI OF BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 496) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON RT INBD SEAT TRACK AT FS 496. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 626) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 626. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 296) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 296. BLENDED CORROSION AT RT INBD SEAT TRACK FSX296 IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 590) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 590. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART NO DEFECTS NOTED. PERFOMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 420) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT FS 420. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFOMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 783) · airframe 11,228 hrs · 12,175 cycles

SUSPECTED CORROSION FOUND ALONG LT INBD SEAT TRACK AT FS 783.102. BLENDED CORROSION AT LT INBD SEAT TRACK IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 783) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ALONG RT INBD SEAT TRACK AT FS 783.102. BLENDED CORROSION AT RT INBD SEAT TRACK AT IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-46-02-02. OK TO NDT. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 449.5) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT BS 449.5. BLENDED CORROSION AT RT INBD SEAT TRACK AT FSX449 IAW SRM 51-21-00-00-07. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 587) · airframe 11,228 hrs · 12,175 cycles

CORROSION FOUND ON LT INBD SEAT TRACK AT BS 587. BLENDED CORROSION AT LT INBD SEAT TRACK AT FSX587 IAW SRM 51-21-00-00-01. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. ALODINED IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 528) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON RT INBD SEAT TRACK AT BS 528. BLENDED CORROSION AT RT INBD SEAT TRACK IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. PERFORMED FLPI ON BLENDED AREA IAW NDT MANUAL PART 8. NO DEFECTS NOTED. PERFORMED ALODINE TREATMENT IAW SRM 51-21-10-02-01.

Part: FLOORBEAM — CORRODED (BS 783.102) · airframe 11,228 hrs · 12,175 cycles

CORROSION ON FLOOR ANGLE IN AFT CARGO COMPARTMENT AT FUSELAGE STA 783.102, LT SIDE. FOUND BEYOND LIMITS IAW SRM 53-40-15-02-01 AND 51-21-00-00-02. ALL WORK PERFORMED IAW TASK CARD RD8/4-53-4027.

Part: CONTROL CABLE — DAMAGED (AILERONS) · airframe 11,032 hrs · 11,959 cycles

IN FLIGHT, WITH THE AUTO-PILOT ON OR OFF AND THE AIRPLANE TRIMMED TO NEUTRAL FEEL, BOTH YOKES ARE CANTED TO THE RIGHT. ON THE GROUND WHEN DOING A CONTROL CHECK THE LEFT ROLL TAKES EXTRA RESISTANCE OR BINDS TO GET FULL DEFLECTION OF THE LT INBD AND OTBD ROLL SPOILER. R & R BOTH UPPER & LOWER, BOTH LT WING & RT WING AILERON CABLES, FREEDOM OF MOVEMENT CHECK PERFORMED INSURING FULL TRAVEL AND VERIFICATION OF DIRECTION OF TRAVEL. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 1 DC) · airframe 10,540 hrs · 11,453 cycles

AFTER LEVELING AT CRUISE ALTITUDE, FL220 NR1 AND NR2 DC GENERATOR CAUTION LIGHTS ILLUMINATED. COMPLIED WITH EMER/ABNORMAL CHECKLIST. NR 2 DC GENERATOR RESET. NR 1 DC GENERATOR FAILED TO RESET. COMPLIED WITH NR 1 DC GENERATOR CHECKLIST. NO ABNORMAL INDICATIONS FROM REMAINING ELECTRICAL SOURCES. PERFORMED OPS TEST OF THE MAIN 28VDC GENERATOR SYS REF AMM 24-31-00-710-802. VERIFIED NORMAL OPERATION OF NR 1 AND NR 2 DC GENERATOR SYSTEM. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,038 hrs · 10,920 cycles

F/A REPORTS THAT THE EMERGENCY LIGHTING SWITCH LIGHT DOES NOT ILLUMINATE. RELAMPED SWITCH LIGHT. OPERATES NORMALLY. RETURNED TO SERVICE.

Part: HINGE — CONTAMINATED (MLG DOOR) · airframe 9,965 hrs · 10,845 cycles

LANDING GEAR ALTERNATE EXTENSION DOOR ON FLIGHT DECK FLOOR DIFFICULT TO OPEN FULLY. FOUND DIRT AND DEBRIS IN THE HINGE AREA. CLEANED AND LUBED DOOR, OPERATES NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WINDSCREEN — LOOSE (CABIN) · airframe 9,241 hrs · 10,077 cycles

BULKHEAD IN FRONT OF SEAT 1A IS EASILY DISLOGED AT THE TOP CAUSING INTERFERENCE WITH THE MAIN CABIN DOOR. INSPECTION FOUND LATCHES FOR THE FWD DRAFT BULKHEAD IN THE UNSECURED POSITION. LOCKED THE LATCHES FOR THE FWD DRAFT BULKHEAD IN THE SECURED POSITION IAW AMM TASK 25-24-06-400-802. NO FUTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BYPASS VALVE — MALFUNCTIONED (OIL COOLER) · airframe 8,936 hrs · 9,767 cycles

AT APPROXIMATELY 16,000 FT, OIL TEMP 107 DEGREES AND CLIMBING SLOWLY. STARTED HIGH OIL TEMP CHECKLIST, OIL TEM CLIMBED TO 125 DEGREES. SHUTDOWN NR 1 ENGINE. LANDING UNEVENTFUL. INTEROGATED CDS AND FOUND NR 1 ENGINE PEAK VALUE 125.7 DEGRESS C AND AREA B 698 SECONDS. COMPLIED WITH AMM TASK 05-53-00-210-814. REPLACED NR 1 OIL COOLER BYPASS VALVE IAW AMM TASK 79-21-06-000-801/400-801. OPS CHECKED GOOD. NO LEAKS NOTED. ALSO REPLACED NR 1 OIL COOLER DOOR ACTUATOR. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 8,705 hrs · 9,530 cycles

OIL ODOR FROM VENTS ON FLT DECK, WITH ENGINES AT REDUCED POWER. ODOR CAME FROM VENTS AFTER REDUCING THROUGH 50 PERCENT TORQUE FOR APPROACH. NO SMOKE WAS APPEARENT. COMPLIED WITH ENGINE RUNS AND BOROSCOPE INSPECTIONS, FINDING NO EVIDENCE OF OIL OR DISCREPANCIES. NO CONTAMINATION FOUND IN CABIN. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 8,526 hrs · 9,339 cycles

EMERGENCY EXIT LIGHTS AT SEAT 19 E/D AND AFT CENTER CEILING LIGHT ARE INOPERATIVE. REPLACED BATTERY PACK. RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,523 hrs · 9,337 cycles

FORWARD 2 EMERGENCY LIGHT STRIPS INOPERATIVE. REMOVED EMERGENCY LIGHT STRIPS AT ENTRY TO COCKPIT AND IN FRONT OF FWD CARGO BAY. IAW AMM TASK 33-51-16-000-801, SUB TASK 33-51-16-020-004. INSTALLED NEW LIGHT IAW AMM TASK 33-51-16-400-801, SUB TASK 33-51-16-420-004. RETURNED TO SERVICE.

Part: AXLE — CORRODED (NR 1 MLG) · airframe 7,701 hrs · 8,492 cycles

DURING THE REMOVAL OF THE NR 2 BRAKE, FOUND LIFTING PAINT AND CORROSION ON THE NR 1 MLG INBD AXLE. REPLACED THE AXLE IAW AMM 32-11-04-400-801. RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 6,969 hrs · 7,728 cycles

EMERGENCY LIGHTS DISARMED CAUTION NOT ILLUMINATED WITH EMERGENCY LIGHTS OFF, BULB TEST OK. CYCLED ACFT POWER. EMERGENCY LIGHT CAUTION LIGHT ILLUMINATED. PERFORMED OPS TEST ODF THE EMERGENCY LIGHTS SYS IAW AMM 33-51-00-710-801. OPS CHECKED GOOD NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (NR 1 BRAKE) · airframe 6,156 hrs · 6,906 cycles

BRAKING ON LANDING POOR. ON POST FLIGHT FOUND NR1 BRAKE COLD TO THE TOUCH NR 2,3,4, BRAKES WARM. R & R LT OTBD WHEEL SPEED TRANSDUCER IAW AMM 32-46-11-000-801/400-801. NO FURTHER DEFECTS. TAXI CHECK GOOD. RETURNED TO SERVICE.

Part: STARTER GEN — FAILED (APU) · airframe 5,727 hrs · 6,484 cycles

THE APU WAS RUNNING AND THE AIRCRAFT WAS USING THE APU GEN FOR POWER. THE GROUND CREW NOTICED BLUE SMOKE AND A PLASTIC BURNING SMELL COMING FROM THE APU THE GENERATOR HAD GONE OFF LINE. SHUT THE APU DOWN. PLACED THE APU ON MEL 49-00-1. REPLACED APU STARTER/GEN IAW AMM TASK 24-33-01-000/400-801. OPS CKS GOOD NO SMELL OR BLUE SMOKE NOTED. CLEAR DMI. RETURNED TO SERVICE.

Part: STICK SHAKER — MALFUNCTIONED · airframe 5,381 hrs · 6,119 cycles

ON LANDING RECEIVED PUSHER SYS FAIL CAUTION LIGHT. DID NOT CLEAR WITH EMERGENCY CHECKLIST PROCEDURE. COMPLIED WITH SL DH8-400-SL-31-005 FOR NUISANCE PUSHER SYS FAIL CAUTION LIGHT. RESET BREAKERS AND ALL CHECKED GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 4,895 hrs · 5,625 cycles

C1 CHECK - AFT MATING SURFACE ON FUSELAGE FOR PANEL 261CT AND 261LT HAS FRETTING. REMOVED DAMAGE FROM FUSELAGE MATING SURFACE AS REQUIRED IAW RD 8/4-53-451. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-53-451. COMPLIED WITH REPAIR IAW RD 8/4-53-451.

Part: SKIN — CORRODED (FUSELAGE) · airframe 4,895 hrs · 5,625 cycles

C1 CHECK - FWD MATING SURFACE ON FUSELAGE FOR PANELS 262AT, 262FT AND 262HT HAS FRETTING. REMOVED DAMAGE FROM FUSELAGE MATING SURFACES AND FOUND TO BE WITHIN LIMITS OF RD 8/4-53-451 AND RD 8/4-57-1514. COMPLIED WITH REPAIRS IAW RD 8/4-53-451 AND 8/4-57-1514.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 4,895 hrs · 5,625 cycles

C1 CHECK - RT SEAT TRACK NR10 HAS EVIDENCE OF CORROSION. REMOVED CORROSION, MATERIAL LOSS .048" AND IS IN LIMITS IAW COMPLETED REPAIR IAW RD 8/4-53-2358.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 4,895 hrs · 5,625 cycles

C1 CHECK - RT SEAT TRACK NR11 HAS EVIDENCE OF CORROSION. REMOVED CORROSION, MATERIAL LOSS .012" AND IS IN LIMITS IAW COMPLETED REPAIR IAW RD 8/4-53-2358.

Part: ADAPTER — FAILED (ENGINE) · airframe 4,470 hrs · 5,153 cycles

ENGINE ADAPTER HEAT 1 CAUTION MSG, DUE TO WEATHER CONDITIONS, RETURNED TO THE FIELD. LANDING UNEVENTFUL. R & R NR1 ENG INTAKE ADAPTER HEATER IAW AMM TASKS 30-21-15-000/400-801. OPS TEST GOOD. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 4,310 hrs · 4,965 cycles

AUTOFEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. FOUND FAULT CODE 400 CH B NR2 PEC IN CDS. PERFORMED GVI OF NR 2 PEC, CONNECTOR PLUGS AND ASSOCIATED WIRING. NO DEFECTS NOTED. C/W NR2 PEC FAULT CLEAR IAW AMM TASK 61-20-36-070-801. C/W FIM TASK 61-20-09-810-806. PERFORMED AUTOFEATHER TEST SEVERAL TIMES IAW AMM TASK 61-20-00-710-801. TEST PASSED EVEYTIME. NO FURTHER DEFECTS NOTED AT THIS TIME. NO FAULT CODES LOGGED IN CDS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ACTUATOR VALVE — MALFUNCTIONED (THERMAL) · airframe 3,499 hrs · 4,096 cycles

FLIGHT NR 2 ENGINE FUEL INLET TEMP 72 DEGREE C RETURNED TO NORMAL IAW EAC. DIVERTED, LANDING UNEVENTFUL. REPLACED NR 2 ENG THERMAL ACTUATOR VALVE AND FUEL HEAT EXCHANGER OPS CHECKED AND LEAK CHECKED OK. RETURNED TO SERVICE.

Part: DOOR — UNKNOWN (L2) · airframe 3,381 hrs · 3,958 cycles

"L2" PASSENGER DOOR IS STICKY. INSPECTED "L2" DOOR FOUND NO DEFECT. LUBE DOOR MECHANISM LIFT AND LATCH, BULB SEAL ON THE VENT DOOR. FUCTIONAL TEST GOOD REF TASK 52-12-00-720-801. RETURNED TO SERVICE. NO PARTS REPLACED. COULD NOT DUPLICATE.

Part: SWITCH — MALFUNCTIONED (NR 1 OVERTEMP) · airframe 2,140 hrs · 2,515 cycles

NR 1 BLEED HOT CAUTION MESSAGE ON APPROACH , AT 5,000 FEET. ABORTED APPROACH AND RETURNED TO DEPARTURE. LANDING UNEVENTFUL. INTERROGATED CDS AND FOUND FAULT CODES 7001- L BLD OVR TEMP AND 7005- L BLD AND OT, C/W FIM TASK 36-046, REMOVED AND REPLACED NR 1 BLEED OVERTEMP SWITCH IAW AMM TASKS 36-11-16-00-801 AND 36-11-16-400-801, PERFORMED OPS CHECK FOR AMM TASK 36-11-16-720-801. OPS CHECH GOOD, CAUTION EXTINGUISHED, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: INDICATOR — MALFUNCTIONED (STNDBY AIRSPEED) · airframe 1,948 hrs · 2,298 cycles

ON TAKEOFF ROLL HAD AN INTERMITTENT IAS IN RED BOX & SSEC IN YELLOW BOX THAT EXTINGUISHED PRIOR TO VR. NOTICED ON CLIMB OUT AIRSPEED INDICATOR ON STANDBY INSTRUMENT WAS INDICATING 40 KTS TAS. THEN AT 10,000 FT IT WAS 15 TO 25 KTS TAS & THEN ON FINAL IT WAS INDICATING CORRECLY. REMOVED & REPLACED ISI. PURGED PITOT STATIC LINES FROM WATER CONTAMINATION. PERFORMED STANDBY PITOT STATIC LEAK CHECKS. LEAK CHECKS GOOD.PERFORMED OPERATIONAL TEST OF ISI. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (OIL PRESSURE) · airframe 1,601 hrs · 1,892 cycles

ABORTED TAKEOFF FOR NR 1 ENGINE OIL PRESSURE HIGH (73 PSI). PERFORMED ENG GRND RUN FOUND ENGINE OIL PRESSURE STABLE AT 70 PSI, WITHIN LIMITS IAW ENG OPERATING LIMITS IN AMM 05-11-00 PG 603. ACFT OK FOR CONTINUED SERVICE. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 1,066 hrs · 1,163 cycles

ACV - NO GREEN LIGHT FOR MAIN LANDING GEAR WHEN GEAR SELECTED DOWN. LEFT + NOSE NORMAL INDICATION. RIGHT MAIN NO LIGHT AT ALL. ALL THREE GREEN LIGHTS IN ALT LANDING GEAR EXTENSION BAY ILLUMINATED. LANDED WITHOUT INCIDENT. FOUND BURNED OUT LIGHT BULBS IN RT GEAR DOWN INDICATION. REPLACED EACH WITH MS25237-387, LIGHTS OPERATE NORMALLY. NO OTHER DEFECTS NOTED.

Part: WIRE HARNESS — OUT OF POSITION (PAX DOOR) · airframe 767 hrs · 850 cycles

PDX- FLIGHT ATTENDANT REPORTS REAR GALLEY PAX DOOR (L2) HARD TO OPEN/CLOSE. LOCK SENSOR HARNESS SNAGGED ON HINGE LINK AND DAMAGED, (CLEARED HARNESS FROM HINGE MECHANISM) OPS CHECKED DOOR, NO OTHER DEFECTS FOUND. UPPER DOOR LINER REMOVED FOR INVESTIGATION AND REINSTALLED AND SEALANT APPLIED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — SMOKE (GALLEY) · airframe 706 hrs · 786 cycles

LAX - FA'S NOTICE SMOKE ODOR NEAR REAR GALLEY OVERHEAD LIGHT ASSEMBLY. PERFORMED GVI OF THE AFT GALLEY AND ITS COMPONENTS, NO DEFECTS NOTED. NO SMOKE ODOR NOTED IN CABIN. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 559 hrs · 638 cycles

YYJ - AFTER ENGINE SHUT DOWN LEFT MAIN GEAR SAFE LIGHT WENT OUT AND AMBER AND RED GEAR LIGHT CAME ON WITH HANDLE ILLUMINATED. SECONDARY GEAR LIGHTS ALL ARE GREEN. INSTALLED MLG PINS AND ENGAGED NOSE GEAR LOCK. REMOVED AND REPLACED NR 1 DOWN LOCK ACTUATOR PROX SENSOR WITH NEW. OPS CHECK GOOD ACFT OKAY TO CONTINUE SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 441 hrs · 486 cycles

RDM - AUTO FEATHER DIDN'T NOT SELECT. AS DIRECTED BY MTX CONTROL PERFORMED PILOT AUTOFEATHER TEST. RECEIVED AUTOFEATHER TEST PASSED AUTOFEATHER NOW SELECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SENSOR — MALFUNCTIONED (AFT SERVICE DOOR) · airframe 166 hrs · 171 cycles

SEA- RT SERVICE DOOR CAUTION CAME ON, ON TAKEOFF ACFT WOULD NOT PRESSURIZE. RETURNED TO THE FIELD, LANDING UNEVENTFUL. REMOVED AND REPLACED AFT SERVICE DOOR LOCK SENSOR AND PRESSURIZATION CHECKS GOOD. RETURNED TO SERVICE.

Part: FEEL UNIT — MALFUNCTIONED (ZONE 300) · airframe 92 hrs · 96 cycles

RNO - WHEN PULLING POWER TOWARDS IDLE ON DESCENT AND ADDING THE REQUIRED LEFT RUDDER AT ABOUT 1-1 1/2 INCH TRAVEL THERE IS AN INCREASE IN PEDAL RESISTANCE FOR APPROXIMATELY THE SAME DISTANCE AND THEN AN ABRUPT RELEASE IN PRESSURE REQUIRED FOLLOWED BY NORMAL TRAVEL. UNEVENTFUL LANDING. FERRIED RNO-PDX FOR REPAIRS. DISCREPANCY IS ASSOCIATED TO RUDDER FEEL/SUMMING UNIT. REPLACED RUDDER FEEL SUMMING UNIT IAW AMM TASKS 27-22-06-000-801 AND 27-22-06-400-80. ALL CHECKS GOOD. NO DEFECTS NOTED. C/W FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED DIRECTION OF MOVEMENT, NO DEFECTS NOTED. RETURNED TO SERVICE.