N431QX

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 27,516 hrs · 29,445 cycles

WHEN SELECTING GEAR UP GOT MASTER CAUTION AND NR 2 ENG HYD, NR 2 HYD PRESS AND NR 2 RUD HYD CAUTIONS. NR 2 HYD PRESS INDICATED ZERO. GEAR STAYED DOWN AND PTU FAILED. COMPLIED WITH NR 2 ENG HYD PUMP CHECKLIST AND PULLED HYD PWR XFER CB. WITHIN 5 MIN CAUTIONS EXTINGUISHED AND GEAR RETRACTED. RETURN TO FIELD LDG WT 59000 LBS. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND A LARGE AMOUNT OF AIR IN THE NR 2 HYD SYSTEM. PERFORMED AMM TASK 29-10-00-870-802 PARA 1-3, 4A. AND 4B., AND 5; BLEEDING OF NR 2 HYDRAULIC SYSTEM USING THE SPU AND PTU. PERFORMED THE FUNCTIONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM IAW AMM TASK 32-30-00-720-801, AND TASK CARDS 6071001 AND 6120001. FUNCTIONAL CHECK IS GOOD. RESET HYD PWR XFER CB. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — DETACHED (CABIN) · airframe 27,489 hrs · 29,412 cycles

AMBIENT LIGHTING STRIP DETACHED FROM IN FRONT OF TYPE II/III EMERGENCY EXIT. REMOVED FROM SERVICE. REATTACHED FLOOR EMERGENCY LIGHTING STRIP WITH CARPET TAPE AS REQUIRED. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,378 hrs · 29,285 cycles

FOWARD F.A. EMERGENCY LIGHT BUTTON LIGHT BULB INOP. REMOVED FROM SERVICE. RELAMPED - OPS CHECK GOOD. RETURNED TO SERVICE.

Part: SIGN — UNKNOWN (CABIN) · airframe 27,257 hrs · 29,156 cycles

FORWARD OVERHEAD EXIT SIGN INOPERATIVE. REMOVED FROM SERVICE. VERIFIED CORRECT OPERATION OF FWD OVERHEAD EXIT SIGN. NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 27,105 hrs · 28,988 cycles

TRACK LIGHTING STRIP IS LOOSE BY THE LAVATORY. REMOVED FROM SERVICE. RESECURED FLOOR TRACK LIGHTING STRIP BY LAVATORY. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — NOT SEATED (O2 MASK) · airframe 26,566 hrs · 28,375 cycles

ALL THREE FLIGHT DECK O2 MASKS HAVE NO PRESSURE. REMOVED FROM SERVICE. GVI OF AREA AROUND CREW O2 BOTTLE. FOUND MALE BAYONET FITTING FOR HOSE WAS NOT SEATED. RESEATED. OPS TEST OF CREW OXYGEN SYSTEM IAW AMM TASK 35-10-00-710-801 RESULTS GOOD, NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 26,124 hrs · 27,897 cycles

F/A REPORTED THE FWD CABIN EMERGENCY LIGHTS SWITCH, LIGHT WAS DARK. REPLACED THE LAMPS IN THE LIGHT SWITCH. CHECKED GOOD. RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,118 hrs · 27,892 cycles

AFT CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND THE NR 3 POWER SUPPLY BATTERIES DRAINED. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-01-000-801, AND AMM 33-51-01-400-801. R & R THE BATTERY PACKS IAW AMM 33-51-00-820-801. OPS TESTED GOOD.

Part: PCU — MALFUNCTIONED (NR 2 ENGINE) · airframe 28,024 hrs · 30,044 cycles

SHORTLY AFTER TAKEOFF THE NUMBER 2 TORQUE WAS SUPPOSED TO BE AT 90% AND WAS AT 94%, THE RPM WAS SUPPOSED TO BE 100% AND WAS 98%. NO SURGES, NO CAUTIONS. HAPPENED WHILE CLIMBING THROUGH 100. FOLLOWED ENGINE FAILURE CHECKLISTS AND MANUALLY SHUTDOWN #2 ENGINE. AIRCRAFT WAS CONFIGURED FOR NORMAL TAKEOFF. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 PCU.

Part: BRAKE — SMOKE (MLG) · airframe 28,024 hrs · 30,044 cycles

AFTER LANDING RIGHT HAND MLG BOTH BRAKES EXCESSIVELY HOT AND SMOKING. NO ADVERSE BRAKING AND/OR STEERING NOTED WHILE TAXIING. REMOVED FROM SERVICE. CLEANED AND INSPECTED WHEEL ASSY'S. NO HEAT DAMAGE OR DISCOLORATION NOTED. THERMAL RELIEF PLUGS DID NOT RELEASE TIRE PRESSURE. WHEELS WAS NOT OVERHEATED AS DETERMINED BY CMM 3-1573 TASK 32-48-32-280-801-A STEP 5.D.(1). NOTE: BRAKE ASSY'S SHOWED NO SIGNS OF HEAT DAMAGE OR DEFECTS. NO PARTS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,406 hrs · 27,147 cycles

DURING DEPARTURE CHECKLIST, NOTICED SEVERAL EMERGENCY LIGHTS OUT, WOULD NOT ILLUMINATE WHEN SELECTED ON FROM FLIGHT DECK OR CABIN. REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-51-01-000-801, AND 33-51-01-400-801. OPS CHECKED GOOD IAW 33-51-00-710-803. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (RT MLG) · airframe 24,801 hrs · 26,511 cycles

RIGHT MAIN LANDING GEAR UNSAFE LIGHT AND GEAR DOWNLOCK ILLUMINATED WITH LANDING GEAR HANDLE DOWN COMPLIED WITH ALL EMERGENCY CHECKLIST AND LIGHTS REMAINED ILLUMINATED. CREW PERFORMED ALTERNATE GEAR EXTENSION. REMOVED FROM SERVICE. RETERMINATION OF CONNECTOR 3261-544 AND REPLACEMENT OF NR 2 MLG DOWNLOCK 2 ELECTRICAL HARNESS. OPS TESTED GOOD NUMEROUS TIMES IAW AMM 32-34-000-710-801, AND 32-31-00-710-801. ALL INDICATIONS ARE NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: KNOB — OUT OF ADJUST (MLG CNTRL PANEL) · airframe 24,741 hrs · 26,453 cycles

DURING TAKEOFF, THE LANDING GEAR LOCK RELEASE STUCK IN THE DOWN POSITION. REMOVED FROM SERVICE. AFTER INSPECTION OF LANDING GEAR CONTROL PANEL, FOUND THE RED GEAR LOCK RELEASE KNOB, STICKING ON PANEL. ADJUSTED THE RED KNOB. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,570 hrs · 26,276 cycles

LT & RT REAR EMERGENCY LIGHTS & BOTH EXIT SIGNS ON AFT PAX DOOR & RT SERVICE DOOR INOPERATIVE. REMOVED & REPLACED THE NR 4 BATTERY PACKS IAW AMM 33-51-0-000/400-801, ALL EXIT AND EGRESS SIGNS AND LIGHTS POWER ON. OPERATIONAL TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,570 hrs · 26,276 cycles

CEILING EMERGENCY LIGHTS AT X083.90 & X211.67 INOP. RELAMPED CEILING EMERGENCY LIGHTS OPS CHECK GOOD IAW 33-51-00-710-803.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,495 hrs · 26,201 cycles

EMERGENCY LIGHT SYSTEM FAILS THE 10 MINUTE FUNCTIONAL CHECK. REPLACED ALL BATTERIES IAW MTC 335000203.

Part: WIRE HARNESS — FAILED (DE-ICE SYSTEM) · airframe 23,391 hrs · 25,051 cycles

DESCENDING OUT OF FL 180 WE EXPERIENCED DUAL A/C GEN CAUTION LIGHTS AND CAUTION LIGHTS OF ALL A/C CONSUMERS. RAN E&A CHECKLIST RESET PROCEDURE AND EXTINGUISHED ALL CAUTION LIGHTS. NO OTHER ABNORMALITIES OBSERVED. LANDING UNEVENTFUL. FOUND NR 1 ENGINE NR 2 PROP BLADE AND NR 2 ENGINE NR 4 PROP BLADE DE-ICE WIRE HARNESS OUT OF CONTINUITY. REPLACED BOTH HARNESSES. OPERATIONAL CHECK OF THE AC SYSTEM CHECKS GOOD IAW AMM 24-21-00-710-801. RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (ZONE 200) · airframe 22,621 hrs · 24,227 cycles

TAKEOFF WARNING HORN SOUNDED DURING T/O AT ABOUT 50-60 KTS. ABORTED THE TAKEOFF AND CLEARED RUNWAY. CONTACTED DISPATCH & MX CONTROL. PERFORMED THE T/O ABORT CHECKLIST. AFTER CONSULTATION WITH MX CONTROL, WE DECIDED TO ATTEMPT ANOTHER T/O. AIRCRAFT WAS CONFIGURED PROPERLY. WARNING HORN WENT OFF AGAIN, AT 90-95 KNOTS. WE AGAIN COMPLETED THE T/O ABORT CHECKLIST AND AGAIN THE A/C WAS CONFIGURED PROPERLY. COMPLIED WITH OPS CHECK OF TAKEOFF WARNING SYSTEM IAW AMM TASK 31-52-00-710-801. OPS CHECK GOOD. COMPLIED WITH FIM TASK 31-52-00-810-802 FAULT ISOLATION STEPS A 1 THRU 8, ALL VALUES NORMAL REF FIM 31-52-00-810-802 4A (9)-5B. FOUND CONTINUITY BETWEEN 9811.J5001 (PIN 46) & GROUND. FOUND CONTINUITY BETWEEN CONFIG CONNECTORS & FCECU. WING FLAP INDICATION GOOD, FLAP DRIVE TRANSDUCER VALVES GOOD. R&R FCECU AS PRECAUTIONARY MEASURE IAW AMM 27-00-01-000-802/400-802, OPS CHECKS FOR FCECU GOOD. PERFORMED OPS TEST OF T/O WARNING SYSTEM IAW AMM 31-52-00-710-801, OPS CHECK GOOD. OBSERVED T/O WARNING HORN SILENT AS APPROPRIATE. NO FURTHER DEFECTS NOTED. NO RELEVANT CDS FAULTS FOUND. RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (BS 604) · airframe 22,562 hrs · 24,168 cycles

CORROSION ON SHEAR TIE BS 604.5 STRINERS 31-32R. FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00 REPAIR-09. REPAIRED IAW SRM 53-00-00-18.

Part: SHEAR TIE — CORRODED (BS 301) · airframe 22,562 hrs · 24,168 cycles

CORROSION ON SHEAR TIE BS 301 STRINGERS 31-32L FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00 REPAIR -09. REPAIRED IAW SRM 53-00-00-02-18.

Part: SEAT TRACK — CORRODED (BS 102-228) · corrosion level 2 · airframe 22,562 hrs · 24,168 cycles

LEFT INBD CABIN SEAT TRACK FROM BS 102.50 - 228.50, LBL 10 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REMOVED IAW SRM 51-42-05, 51-40-15, AND REPLACED IAW SRM 51-42-05, AND 51-40-15.

Part: THRESHOLD — CORRODED · airframe 22,562 hrs · 24,168 cycles

AIRSTAIR DOOR THRESHOLD CORRODED. BLENDED AND MEASURED BEYOND LIMITS IAW SRM 53-20-23-02-01. REMOVED AND REPLACED IAW SRM 51-40-07-02-01. IAW SRM 51-42-05-02-01, 51-23-00-00-01 & 51-25-10-02-01.

Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · airframe 22,562 hrs · 24,168 cycles

EMERGENCY EXIT DOOR THRESHOLD FOUND SEVERELY CORRODED. 10 REMOVED AND REPLACED IAW SRM 51-42-05 AND SRM 51-42-45.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 22,562 hrs · 24,168 cycles

RIGHT INBD CABIN SEAT TRACK NR 10 FROM X -39.00 TO X 10.50 RBL 10 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REPLACED IAW SRM 51-42-05, 51-40-15, & DWG 85328210.

Part: SEAT TRACK — CORRODED (BS 32-229) · airframe 22,562 hrs · 24,168 cycles

LEFT OTBD CABIN SEAT TRACK BS 32.40 - 229.50, LBL 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, AND 51-40-15.

Part: DOUBLER — CORRODED (LAVATORY DOOR) · airframe 22,562 hrs · 24,168 cycles

LAVATORY DOOR ACCESS DOUBLER CORRODED BEYOND LIMITS. REPAIRED IAW SRM 51-42-05, AND SRM 51-23-00.

Part: STRINGER SPLICE — CORRODED · airframe 22,562 hrs · 24,168 cycles

CORROSION FOUND ON STRINGER SPLICE AT X FS -18.00 ON STR 32P. REMOVED STRINGER SPLICE @ FSX -18.00, STR 32P IAW DHC-8-400 SRM 51-40-70 + 51-42-05. FIT, DRILLED + INSTALLED NEW STRINGER SPLICE @ FSX -18.00, STR 32P IAW DHC-8-400 SRM 51-40-07, 51-42-05, 51-23-00 + 51-25-10.

Part: SEAT TRACK — CORRODED (BS 570-610) · airframe 22,562 hrs · 24,168 cycles

INBD CABIN SEAT TRACK FROM BS 570 TO 612 RBL 10, FOUND CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 & 51-40-07.

Part: SEAT TRACK — CORRODED (BS 612-670) · airframe 22,562 hrs · 24,168 cycles

SEAT TRACK 15 FROM BS 612 TO 670 INBD RBL 10, FOUND TO BE CORRODED BEYOND LIMITS IAW SRM 53-20-49 FIG 201 SHEET 6 REPAIR 02. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-07, 51-40-05, 51-40-15, 51-41-05 AND 51-25-10.

Part: SHEAR WEB — CORRODED (BS 697-714) · corrosion level 2 · airframe 22,562 hrs · 24,168 cycles

AFT CARGO FWD SHEAR WEB AT BS 697.6 - 714.6, LBL 10 - 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR WEB IAW DHC-8-400 SRM 51-40-07 + 51-42-05, SRM 51-42-05, 51-40-15, 51-42-45, AND DWG 85339527.

Part: SEAT TRACK — CORRODED (BS 570-670) · airframe 22,562 hrs · 24,168 cycles

LEFT OUTBD AFT CABIN SEAT TRACK FROM BS 570 TO 670 LBL 10, CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-07 & 51-42-05.

Part: SHEAR WEB — CORRODED (BS 714-783) · airframe 22,562 hrs · 24,168 cycles

AFT CARGO AFT SHEAR WEB AT BS 714 - 783, LBL 10 - 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-40-07 + 51-42-05, SRM 51-42-05, 51-40-15, 51-42-45, & DWG 85339627.

Part: CARGO TRACK — CORRODED (BS 668-782) · airframe 22,562 hrs · 24,168 cycles

LEFT INBD AFT CARGO TRACK BS 668 TO 782 LBL 10 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-41-00, 51-42-05 & 51-25-10.

Part: SEAT TRACK — CORRODED (BS 571-668) · airframe 22,562 hrs · 24,168 cycles

LEFT OTBD CABIN SEAT TRACK NR 3 FROM BS 571.50 - 668. LBL 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-42-45, 51-40-15.

Part: STRINGER — CORRODED (BS 258-281) · airframe 22,562 hrs · 24,168 cycles

STRINGER 24L BETWEEN BS 258.5 - 281 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-15, 51-42-05.

Part: SHEAR TIE — CORRODED · airframe 22,562 hrs · 24,168 cycles

CORROSION ON SHEAR TIE BETWEEN STRINGERS 28 AND 29R. FOUND OUT OF LIMITS IAW SRM 53-00-00-02-09. REPAIRED IAW SRM 53-00-00 REPAIR 18.

Part: SEAT TRACK — CORRODED (BS 102-229) · airframe 22,562 hrs · 24,168 cycles

RIGHT OTBD SEAT TRACK FROM BS 102.5 TO 229.5, RBL 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-51-42-05, 51-42-45.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 22,562 hrs · 24,168 cycles

RIGHT OTBD SEAT TRACK BS 229.5 - 571.5, RBL 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-10, 51-42-05, 51-42-45.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,562 hrs · 24,168 cycles

RIGHT INBD FWD CABIN SEAT TRACK NR 11 FROM BS 10.50 TO 102.50, RBL 10 FOUND TO BE CORRODED BEYOND LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-42-05, 51-40-15, AND DWG 85328210.

Part: CONTROL PANEL — FAILED (MLG) · airframe 22,372 hrs · 23,953 cycles

LANDING GEAR LOCK RELEASE LEVER STUCK AND WOULD NOT ALLOW GEAR LEVER TO GO DOWN. NOTED THAT THE LOCK RELEASE LEVER WOULD MOVE WITH ONLY DOWN MOTION (NO SIDE PRESSURE). GEAR DID COME DOWN WITHOUT INCIDENT. LANDING UNEVENTFUL. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW AMM TASKS 32-31-01-000-801 AND 32-32-01-400-801. FUNCTIONAL TEST GOOD IAW TASK 32-31-01-720-801. NO OTHER DEFECTS NOTED. ACFT OKAY FOR CONTINUED SERVICE.

Part: HINGE — LACK OF LUBE (ACCESS DOOR) · airframe 22,108 hrs · 23,678 cycles

FLOOR ACCESS PANEL FOR ALTERNATE GEAR EXTENSION IS DIFFICULT TO OPERATE. LUBED THE RELEASE DOOR HINGE, DOOR OPERATES SMOOTHLY. RETURNED TO SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,106 hrs · 23,675 cycles

DURING TAKEOFF, THE NR 1 ENGINE ITT WAS AT 790 DEGREES DURING THE TAKEOFF ROLL AND ROSE ABOVE 810 DEGREES AFTER ROTATION. PULLED THE CONDITION LEVERS BACK TO 900 RPM AND ITT DROPPED TO 770 DEGREES. ON AVERAGE, NR 1 ITT WAS 60 DEGREES HIGHER THEN NR 2. ALSO SHOWING A FUEL BURN 90 LBS PER HOUR MORE ON THE NR 1 ENGINE. OIL TEMP WAS 5 DEGREES HIGHER. PERFORMED GROUND IDLE RUN OF ENGINE WITH FLIGHT CREW AND RECORDED EMU AND ECS DATA. REPLACED THE NR 1 HPSOV IAW AMM 36-11-09-000-800/400-801. ALSO REPLACED THE P2.7 INTERSTAGE BLEED VALVE. COMPLIED WITH POWER ASSURANCE RUNS IAW MTC 3710005. CHECKED GOOD. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 21,720 hrs · 23,276 cycles

F/A EMERGENCY SWITCH GUARD IS BROKEN. REPLACED SWITCH GUARD. CHECKS GOOD. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 21,023 hrs · 22,527 cycles

DURING ENGINE RUN FOR ACFT CHECK NR 2 ENGINE, TOOK 33 SECONDS TO UNFEATHER. C/W FIM TASK 61-20-00-810-803 TO STEPS 5, 5. R & R OVERSPEED GOVERNOR IAW TASK 61-20-26-000-801 & 400-801, PARA 1-5 C. PERFORMED FUNCTIONAL TEST OF THE PROPELLER TIME TO UNFEATHER TEST IAW TASK 61-20-00-720-801, CHECK GOOD. PERFORMED OPS TEST OF THE PROPELLER OVERSPEED GOVERNOR IAW AMM TASK 61-20-00-710-803. OPS TEST GOOD. PERFORMED ENGINE LEAK CHECK IAW AMM TASK 71-00-00-790-801. NO ENGINE OIL LEAK NOTED. NO FURTHER DEFECTS NOTED. REF AMM TASK 61-20-26-400-801, STEPS 5 D & E COMPLETE.

Part: CONTROLLER — FAILED (ANTI ICE SYS) · airframe 20,953 hrs · 22,456 cycles

WINDSHIELD CENTRAL ILLUMINATED, WHEN WINDSHIELD HEAT WAS SELECTED TO NORM. CAPTAIN`S WINDOW WAS COLD. FO`S WINDOW WAS WARM. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R LT WINDSHIELD ANTI-ICE CONTROLLER IAW AMM TASK 30-41-01-000-801/400-801 SYS OPERATES NORMALLY. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED (NR 1) · airframe 20,904 hrs · 22,398 cycles

NR 1 ENGINE FAILS DAILY AUTOFEATHER CHECK. FOUND FAULT CODES 400 IN CDS. NR 1 PEC, C/W FIM TASK 61-20-09-810-806. CLEARED ALL FAULTS AND C/W PROP AUTOFEATHER AND UPTRIM OPS CHECK REF AMM TASK 61-20-00-710-801, ALL TESTS PASSED AND FAULT CODES REMAINED CLEARED. NO FURTHER DEFECTS NOTED.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 20,740 hrs · 22,216 cycles

EMERGENCY LIGHT SWITCH ON WING DRAFT BULKHEAD, NORMAL, LIGHT SEGMENT DIM. REPLACED THE LAMP, NO HELP, REPLACED SWITCH IAW AMM 33-51-05-000-801 AND 33-51-05-400-801.

Part: ECU — BURNED (NLG STEERING) · airframe 20,138 hrs · 21,549 cycles

NOSE WHEEL STEERING INOPERATIVE. FOUND NOSE WHEEL STEERING ECU TO BE BURNED INTERNALLY. REPLACED UNIT IAW AMM TASK 32-51-01-000-801-400/801. CHECKS GOOD, RETURNED TO SERVICE.

Part: MOTOR — FAILED (NLG STEERING) · airframe 19,324 hrs · 20,659 cycles

AFTER LANDING, UNABLE TO STEER ACFT, DID NOT RECEIVE NOSEWHEEL STEERING CAUTION. NWS GEARBOX TORQUE MOTOR ASSY R & R IAW AMM TASKS 32-51-31-000-801, 32-51-31-400-801, 32-51-26-000-801, 32-51-26-400-801, 32-51-36-000-801, 32-51-36-400-801. STEERING OPERATIONAL AND FUNCTIONAL CHECKS GOOD.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 18,085 hrs · 19,340 cycles

"NORMAL" INDICATION INOPERATIVE IN THE FWD F/A EMERGENCY LIGHT SWITCH. REPLACED THE LAMP IAW AMM 20-30-07-960-801. CHECKED GOOD.

Part: CONTROL UNIT — NO TEST (AUTOFEATHER) · airframe 17,467 hrs · 18,682 cycles

NR 1 ENGINE AUTOFEATHER FAILED TEST. FERRIED FOR REPAIRS. ALL WIRING CONTINUITY CHECKS PERFORMED, R & R NR 1 PEC. A/F TEST WORK NORMALLY, REF AMM TASK 61-20-36-400-801. THIS COMPLETE THIS REPAIR.

Part: CONTROLLER — MALFUNCTIONED (NR 1 AUTOFEATHER) · airframe 17,467 hrs · 18,682 cycles

NR 1 ENGINE AUTOFEATHER TEST FAILED. REPLACED NR 2 PEC ALL TEST PASS INCLUDING AUTOFEATHER/UPTRIM CHECK. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST · airframe 17,421 hrs · 18,633 cycles

AUTOFEATHER TEST DID NOT PASS. ACFT WAS STATIC, ENGINES NOT RUNNING. NO PRESENT FAULTS, COMPLIED WITH AMM TASK 61-20-00-710-801. OPS TEST OF PROPELLER AUTOFEATHER AND UPTRIM SYSTEM, SYSTEM OPS TEST NORMAL ACFT RETURN TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT SERVICE DOOR) · airframe 17,388 hrs · 18,598 cycles

DOOR WARNING LIGHT ILLUMINATED AT 1500 MSL AFTER TAKEOFF. AFT SERVICE DOOR INDICATED IT WAS NOT SECURE, PRESSURIZATION WAS NORMAL. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED STATIC AND DYNAMIC GVI OF AFT SERVICE DOOR. NO DEFECTS NOTED. COMPLIED WITH OPS TEST IAW AMM 52-41-00-710-801. OP'S TESTED GOOD. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 17,266 hrs · 18,477 cycles

AUTOFEATHER DID NOT ARM ON TAKE OFF. AUTOFEATHER WAS SELECTED. ABORTED TAKE OFF. BELOW 60KTS. COMPLIED WITH OPS TEST OF PROP AUTOFEATHER & UPTRIM IAW AMM 61-20-00-710-801. AUTOFEATHER TEST SHOWED FAIL FOR NR 1 & ABORT FOR NR 2. INTERROGATED EMU FOR FAULTS, FOUND CODE 494. C/W FIM TASK 61-20-10-810-826 FOR FAULT CODE, FAULT CLEARED, A/F TEST PASSED FOR NR 1 & NR 2 ENGINE. PERFORMED BETA CAL IAW AMM 61-20-36-720-801. GROUND RAN ACFT, PERFORMED OPS TEST OF A/F SYS IAW 61-20-00-710-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 17,266 hrs · 18,477 cycles

CLIMBING THRUGH 800' FUSELAGE DOOR WARNING SOUNDED. AFT SERVICE DOOR SHOWED NON-SECURED FOR ENTIRE DURATION OF FLIGHT. RETURNED TO FIELD. LANDING UNEVENTFUL. INSPECTED THE AFT SERVICE DOOR LIFT AND LATCH CRANK AND ROLLERS, ALSO GUIDE ROLLERS AND TRACKS, INTERLOCK CAM ASSY. NO DEFECTS NOTED.ALSO INSPECTED THE VENT DOOR SEAL, DOOR SEAL NO DEFECT NOTED. COMPLYED WITH A FUNCTIONAL TEST OF THE AFT SERVICE DOOR REF AMM TASK 52-41-00-720-801 FUNCTIONAL TEST GOOD NO DEFECTS NOTED. ALSO CLEANED AND LUBED DOOR SEALS, EXTERNAL HANDLE AND SHAFT. RETURNED TO SERVICE.

Part: PUMP — FAILED (FEATHERING) · airframe 16,975 hrs · 18,171 cycles

NR 2 ENGINE FAILED OPS CHECK OF PROPELLER ALTERNATE FEATHER IAW T/C 612000202. THE MAINTENANCE UNFEATHER FUNCTION FAILED IAW STEPS 2D, 2E, 2F, ALL OTHER FUNCTIONS NORMAL. REPLACED ALTERNATE FEATHER PUMP. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: SIGN — DETACHED (ROW 2E) · airframe 16,865 hrs · 18,048 cycles

ROW 2E EXIT SIGN OVER EMERGENCY EXIT DOOR DETACHED. SECURED EXIT SIGN. RETURNED TO SERVICE.

Part: BEARING — DAMAGED (PAX DOOR HANDLE) · airframe 16,857 hrs · 18,040 cycles

MAIN CABIN DOOR HANDLE HARD TO OPEN FROM THE INSIDE AS REPORTED BY THE F/A. REPLACED FORWARD PASSENGER DOOR EXTERNAL HANDLE TAPER PINS, EXTERNAL HANDLE SHAFT BEARINGS, GAS STRUT ASSIST CABLE, AND GAS STRUT ASSIST CABLE PULLEY, FORWARD PASSENGER DOOR OPS TEST GOOD NUMEROUS TIMES IAW MM TASK 52-11-00-710-802. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (NR 1) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 1 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-15 PAR M AND SRM 51-42-05 PAR E. INSTALLED NEW SEAT TRACK IAW SRM 51-40-15 AND SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 2 BS 229.5 571.5, FOUND CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM 51-40-15 AND SRM 51-42-05.

Part: SKIN — DENTED (BS 291-301) · airframe 16,716 hrs · 17,890 cycles

NUMEROUS DENTS FUSELAGE SKIN BETWEEN BS 291-301, S9-13L. CUT EXTERNAL JOINT STRAP, IAW RD 8/4-53-61-31, ISSUE 1 4/15/14. PERFORMED E/T INSPECTION ON EXTERNAL JOINT STRAP, NO DEFECTS NOTED. REPAIRED IAW SRM 51-42-05 AND SRM 51-40-15, AMM 25-80-01-000-801, AMM 25-80-01-400-801, AMM 56-20-01-000-801, AMM 56-20-01-400-801, AND SRM 51-25-05, PG 207 ITEM (F) 1-4.

Part: CHANNEL — CORRODED (CARGO DOOR SILL) · airframe 16,716 hrs · 17,890 cycles

CORROSION FOUND ON CHANNEL, UNDER FWD BAG DOOR SILL. FOUND OUT OF LIMITS IAW SRM 53-20-25. REMOVED CHANNEL, IAW SRM 51-42-05, REPAIR-01. INSTALLED CHANNEL IAW SRM 51-42-05 AND DWG 85329602.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TACK NR 11 FOUND CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-15, 51-42-05, AND SRM 51-40-15. INSTALLED SEAT TRACK IAW SRM 51-41-00 AND SRM 51-42-05, STEP 4.D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 13 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, SRM 51-41-00, SRM 51-40-15. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, SRM 51-41-00, SRM 51-40-15.

Part: BRACKET — CRACKED (WING) · airframe 16,716 hrs · 17,890 cycles

OTBD UPPER RIB MOUNTING BRACKET CRACKED. REMOVED CRACKED REPAIR BRACKET FROM L/E 511AL OTBD UPPER RIB IAW SRM 51-42-05. PROCEDURE E STEPS 1-8, FABRICATED NEW REPAIR ANGLE OTBD UPPER RIB IAW SRM 57-40-00, REPAIR 07. APPLIED ALODINE AND PRIMER TO NEW REPAIR ANGLE IAW SRM 57-40-00, REPAIR 07. INSTALLED NEW REPAIR ANGLE ON L/E PANEL OTBD UPPER RIB IAW SRM 57-40-00.

Part: SKIN — DAMAGED (BS 258) · airframe 16,716 hrs · 17,890 cycles

LIGHTING STRIKE DAMAGE ON LT FUSELAGE SKIN ON STR 27P 1" AFT OF X258.50. REMOVED RIVET ON LT FUSELAGE SKIN AT STR27P, FS.258.50 IAW SRM 53-00-00, PGS 101-102. INCREASED RIVET HOLE SIZE FROM 5/32 (.159) TO 3/16 (.193) IAW SRM 53-00-00, PAR 7A, 7B. C/W ET INSP ON REWORKED AREA REF NDTM, PT1 51-00-06. NO DEFECTS NOTED. INSTALLED RIVET AT STA X258.50 ON STR 27P REF: SRM 51-42-05, REPAIR-01 AND SRM 53-00-00 ALLOW DAMAGE-01.

Part: HINGE — CORRODED (PAX DOOR) · airframe 16,716 hrs · 17,890 cycles

FWD PASSENGER DOOR HINGE SHAFT IS FOUND TO BE CORRODED. DOOR HINGE SHAFT REMOVED, IAW AMM 52-11-26-000-801. INSTALLED NEW DOOR HINGE SHAFT IAW AMM 52-11-26-400-801, C

Part: HINGE — CORRODED (PAX DOOR) · airframe 16,716 hrs · 17,890 cycles

FWD PASSENGER DOOR HINGE SHAFT CRANK IS FOUND TO BE CORRODED. REMOVED FWD PAX DOOR HINGE SHAFT CRANK REF AMM 52-11-26-000-801. INSTALLED NEW FWD PAX DOOR HINGE SHAFT CRANK REF AMM 52-11-26-400-801. COMPLETED CPCP FORM M-184.

Part: YOKE — CHAFED (RT MLG) · airframe 16,716 hrs · 17,890 cycles

RT MLG YOKE ASSY HAS CHAFING ON OTBD FWD SIDE OF YOKE APPROXIMATELY 9" TO 10" FROM CENTERLINGE OF TOP LUG OF YOKE ASSY. CHAFING DAMAGE ON OTBD FWD SIDE OF RT MLG YOKE REMOVED REF HORIZON TASK CARD SB84-26-11, REV A DATED 4/5/14. PERFORMED P/T INSP. ON RT MLG OTBD FWD SIDE OF YOKE BLEND OUT IAW SB84-26-11, W/O 163201, DATED 4/5/14 AND ASTM E14171E1417M-13, REV 13, DATED 8/12/13 NO DEFECTS NOTED. NDT REPORT ATTACHED. 4FLAP PEENDED REWORKED AREA OF OTB FWD SIDE OF RT MLG YOKE REF HORIZON TC SB84-26-11, REV A. CLEANED AND RESTORED FINISH TO REWORKED AREA OF OTBD FWD SIDE OF RT MLG YOKE REF HORIZON TC SB84-26-11. STAMPED YOKE WITH SB IAW HORIZON TC SB84-26-11, REV A.

Part: SHIELD — DENTED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

DENT AFT OF ICE SHIELD ON RT SIDE OF ACFT WITH CORRESPONDING PAINT CHIP. DENT IS WITHIN THE ALLOWABLE LIMITS OF RD8/4-53-5577, ISSUE 1, 7/12/13.

Part: YOKE — CHAFED (RT MLG) · airframe 16,716 hrs · 17,890 cycles

RT MLG YOKE ASSY HAS CHAFING ON INBD FWD SIDE OF YOKE APPROX 9" TO 10" FROM CENTER LINE TOP LUG OF YOKE ASSY. CHAFING DAMAGE ON INBD FWD SIDE OF RT MLG YOKE REMOVED REF HORIZON TC SB84-26-11. PERFORMED P/T INSP. ON RT MLG INBD FWD SIDE OF YOKE BLEND OUT IAW SB84-26-11. NO DEFECTS NOTED NDT REPORT ATTACHED. FLAP PEENED REWORKED AREA INBD FWD SIDE OF RT MLG YOLK REF HORIZON TASK CARD SB84-26-11 REV A DATED 4/5/14. CLEANED AND RESTORED FINISH TO REWORKED AREA ON INBD FWD SIDE OF RT MLG YOKE REF HORIZON TC SB84-26-11, REV A DATED 4/5/14. STAMPED YOKE WITH SB NR IAW HORIZON TC SB84-26-11.

Part: THRESHOLD — CORRODED (MAIN CARGO) · airframe 16,716 hrs · 17,890 cycles

MAIN CARGO DECK THRESHOLD PLATE CORRODED. FOUND OUT OF LIMITS. REMOVED THRESHOLD PLATE IAW SRM 51-42-05-020-01 4(E). INSTALLED NEW THRESHOLD PLATE IAW SRM 51-42-05, REPAIR-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 12 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-41-00. INSTALLED NEW SEAT IAW SRM 51-42-05, STEP 4D & SRM 51-41-00.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 14 CORRODED BEYOND LIMITS. R & R SEAT TRACK IAW SRM 51-40-15 PROCEDURE 6 A-G, SRM 51-42-05, PROCEDURE D 1-10 AND E 1-8 AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 15 CORRODED BEYOND LIMITS. SEAT TRACK REMOVED IAW SRM 51-42-05. LOCATED, DRILLED AND DEBURRED NEW SEAT TRACK, IAW SRM 51-40-07. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01, STEP 4D (3-10) AND SRM 51-41-00-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 8 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-07 & 51-42-05. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, REPAIR 01, SRM 51-41-00 AND DWG 85338201, 51-40-15, REPAIR 01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 16 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-41-00, 51-42-05. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM'S 51-42-05.

Part: STRINGER — CORRODED (25) · airframe 16,716 hrs · 17,890 cycles

CORROSION ON STRINGER 25 LOWER CORNER BETWEEN FS 26.7 AND 32.4.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 16,716 hrs · 17,890 cycles

MAIN CARGO DOOR THRESHOLD CORRODED. REMOVED CORRODED THRESHOLD, IAW SRM 51-42-05-02-01-4 (E). INSTALLED NEW THRESHOLD IAW SRM 51-42-05, PAR B, C AND D, PN 85329540-001. COMPLIED WITH FORM M-184.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X26.700, ANGLE BETWEEN STR 23 AND STR 25 COMMON TO WEB AND FUSELAGE IS CORRODED. REMOVED ANGLE IAW SRM 51-42-05. INSTALLED NEW ANGLE IAW SRM 51-42-05,

Part: STRINGER CLIP — CORRODED (FRAMES 26-32) · airframe 16,716 hrs · 17,890 cycles

STRINGER CLIP S25L, CORRODED BETWEEN FRAMES 26.7 AND 32.4. R & R CORRODED STRINGER CLIP IAW SRM 51-42-05, PROCEDURE D, STEPS 1-10 AND PROCEDURE E STEPS 1-8.

Part: SUPPORT ANGLE — CORRODED (FRAME 32) · airframe 16,716 hrs · 17,890 cycles

TOP ANGLE SUPPORT WEB COMMON TO FRAME 32.4 IS CORRODED. REMOVED CORRODED SUPPORT ANGLE , IAW SRM 51-42-15-02-01 5(G). INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-15-02-01 5(F).

Part: STRINGER CLIP — CORRODED (S25L) · airframe 16,716 hrs · 17,890 cycles

STRINGER CLIP CORRODED S25L . R & R STRINGER CLIP IAW SRM 51-42-05, PROCEDURE D 1-10 & E 1-8.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X19.50, STR 25P ANGLE COMMON TO PARTIAL WEB AND INTERCOSTAL IS CORRODED. REMOVED ANGLE AT FS X19.50, STR 25P COMMON TO PARTIAL WEB AND INTERCOSTAL REF SRM 51-42-05. INSTALLED NEW ANGLE AT FS X19.50, STR 25P COMMON TO PARTIAL WEB AND INTERCOSTAL REF SRM 51-42-05, PROCEDURE D, STEPS 1-10C. LOCATED AND DRILLED NEW ANGLE, PN 85329548-101, REF SRM 51-40-07. COMPLIED WITH FORM M-184.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X26.700, STR 25P ANGLE COMMON TO WEB AND INTERCOSTAL IS CORRODED. REMOVED ANGLE IAW SRM 51-42-05. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-07. INSTALLED NEW ANGLE IAW SRM 51-42-05, PROCEDURE D, STEPS 1-10.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X6.70 ANGLE COMMON TO WEB ABD INTERCOSTAL STR 25P IS CORRODED. REMOVED AT X 6.70 ANGLE COMMON TO WEB AND INTERCOSTAL AT 25P REF SRM 51-42-05. INSTALLED NEW ANGLE AT FS X6.700 COMMON TO WEB AND INTERCOSTAL AT STR 25P REF SRM 51-42-05, PROCEDURE D, STEPS 1-8. LOCATED AND DRILLED NEW ANGLE, PN 85329576-103, REF SRM 51-40-07. COMPLIED WITH FORM M-184.

Part: STRUCTURE — CORRODED (BS 71-94) · airframe 16,716 hrs · 17,890 cycles

EVIDENCE OF CORROSION AROUND RIVET HEADS COMMON TO STRINGER 24R BETWEEN BS 71.2-94.8 . RT FUSELAGE JUST BELOW EMERGENCY DOOR THRESHOLD. REMOVED CORROSION. FOUND WITHIN LIMITS IAW SRM 53-20-17.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X6.70 ANGLE BETWEEN STRINGERS 23 AND 25 COMMON TO WEB AND FUSELAGE IS CORRODED. REMOVED ANGLE AT FS X 6.70 BETWEEN STR 23P AND 25P COMMON TO WEB AND FUSELAGE REF SRM 51-42-05. INSTALLED NEW ANGLE AT FS X6.700 BETWEEN STR 23P AND STR 25P TO WEB AND FUSELAGE REF SRM 51-42-05, PROCEDURE D, STEPS 1-8. LOCATED AND DRILLED NEW ANGLE PN 85329542-017 REF SRM 51-40-07. COMPLIED WITH FORM M-184.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 16,716 hrs · 17,890 cycles

AT FS X1.00 TO FS 32.40, Y-27.00 CHANNEL IS FOUND TO BE CORRODED. REMOVED CORRODED CHANNEL IAW SRM 51-42-05-02-01 4(E). INSTALLED A NEW CHANNEL, IAW SRM 51-42-05-02-01 4(D). LOCATED AND DRILLED FASTENER HOLES ON THE NEW CHANNEL IAW SRM 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 19 BS 229.5 - 571.5 HAS LIGHT CORROSION. BLENDED AND POLISHEDTO REMOVE ALL THE DAMAGE ON SEAT TRACK IAW SRM 53-20-49, REPAIR 02, STEP 6A, FIG 201. FOUND OUT OF LIMITS IAW SRM 53-20-49, REPAIR 02, FIG 201, SHEET 3. REMOVED SEAT TRACK IAW SRM 51-42-05, STEP 4E. INSTALLED SEAT TRACK IAW SRM 51-42-05, STEP 4D.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 8 HAS CORROSION IN NUMEROUS PLACES. BLENDED IAW SRM 53-20-49, REPAIR 02, STPE 6A, FIG 201, SHEET 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-49, REPAIR 02, FIG 201, SHEET 2. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (BS 32-229) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 1 BS 32.4 - 229.5 HAS LIGHT CORROSION. BLENDED AND POLISHED TO REMOVE ALL THE DAMAGE ON SEAT TRACK IAW SRM 53-20-49, REPAIR 02, STEP 6A, FIG 201. FOUND OUT OF LIMITS IAW SRM 53-20-49, REPAIR 02 FIG 201, SHEET 3. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 18 HAS LIGHT CORROSION. BLENDED AND POLISHED IAW SRM 53-20-49, REPAIR 02, STEP 6A, FIG 201. FOUND OUT OF LIMITS IAW SRM 53-20-49, REPAIR 02, FIG 201, SHEET 3. REMOVED SEAT TRACK IAW SRM 51-40-15 PROCEDURE M STEPS 1-5, SRM 51-42-05, PROCEDURE E STEPS 1-8 AND SRM 51-41-05. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07, REPAIR-01, 201-204. INSTALLED NEW SEAT TRACK IAW SRM 51-40-15, REPAIR -01, PG 211, PARA H, SRM 51-42-05, REPAIR 01, SRM 51-41-05 STRUCT SRM 51-23-00 AND 51-40-15.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 10 HAS CORROSION IN NUMEROUS PLACES. BLENDED IAW SRM 53-20-49, REPAIR 02, STEP 6A, FIG 201. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-49. REPAIR 02, FIG 201, SHEET 2. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,716 hrs · 17,890 cycles

SEAT TRACK NR 12 HAS CORROSION IN NUMEROUS PLACES. BLENDED IAW SRM 53-20-49 REPAIR 02, STEP 6A, FIG 201. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-49, REPAIR 02, FIG 201, SHEET 2. SEAT TRACK REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,011 hrs · 17,125 cycles

AFT CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY POWER SUPPLY UNITS IAW AMM TASK 33-51-01-400-801.

Part: MECHANISM — OUT OF RIG (VENT DOOR) · airframe 15,690 hrs · 16,775 cycles

MASTER WARNING FUSELAGE DOOR IN FLIGHT AT FL 190. SERVICE DOOR INDICATED OPEN IN FLIGHT. PRESSURE BUMP WHEN DOOR OPENED, THEN PRESSURIZATION NORMAL FOR REST OF FLIGHT. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. RIGGED THE VENT DOOR MECHANISM OF THE AFT SERVICE DOOR. OPS CHECKED GOOD. PRESSURIZED ACFT IAW MOM, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CAM — CHIPPED (PAX DOOR) · airframe 15,556 hrs · 16,645 cycles

FUSELAGE DOOR WARNING AFTER TAKEOFF SERVICE DOOR INDICATED, PRESSURE NORMAL. RETURNED TO FIELD, LANDING UNEVENTFUL. FOUND AFT SERVICE DOOR HANDLE NOT FLUSH, VENT WAS OK. PERFORMED GVI OF AFT SERVICE DOOR LOCKING MECHANISM IAW AMM TASK 52-41-00-210-802. FOUND LOWER CAM FOLLOWER CHIPPED, REMOVED AND REPLACED LOWER CAM FOLLOWER IAW AMM TASKS 52-41-11-000-801 AND 52-41-11-400-801, PARA 4K-L. PERFORMED OPS CHECK OF AFT SERVICE DOOR IAW AMM TASK 52-41-00-710-801. OPS CHECK GOOD. PRESSURIZED ACFT FUSELAGE DOOR WARNING DID NOT RETURN. NO PRESENT FAULTS IN PSEU. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — FAILED (MLG) · airframe 15,370 hrs · 16,449 cycles

AFTER TAKEOFF, WE SELECTED THE GEAR UP, THE NOSE GEAR CAME UP, NO LIGHTS, BUT THE LT AND RT MAINS DID NOT RETRACT. HAD THE HANDLE LIGHT AND DOOR, PLUS GEAR LIGHTS RED AND CAUTION. AFTER 5 TO 7 MINUTES THE MAINS CAME UP. DID ALTERNATE EXTENSION IAW MC. GEAR CAME DOWN NORMAL, DID NOT EXCEED 185 KIAS AFTER TAKE OFF AND LANDING. REPLACED NLG WOW1, WOW2,CENTERING,TAXI LIGHT HARNESS ASSY. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 15,121 hrs · 16,182 cycles

AUTOFEATHER TEST ON PREFLIGHT, NR 1 ENGINE INDICATION FAILED, NR 2 ENGINE INDICATION ABORT. CDS SHOWS FC 494 A & B AND 228B NR 1 ENG C/W FIM 61-20-10-810-826 & 61-20-05-810-832. FAULTS CLEARED. AUTOFEATHER TESTED GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — FAILED · airframe 15,039 hrs · 16,101 cycles

NR 1 PROPELLER AUTOFEATHER CONTROL FAILS DAILY TEST. INTEROGATED CDS FOUND FAULT 228B ON NR 1 ENGINE C/W FIM TASK 61-20-65-810-832, FAULT CODE CLEARED A/F TEST PASSED. RETURNED TO SERVICE.

Part: APU — UNKNOWN · airframe 14,689 hrs · 15,747 cycles

FAILED APU START ATTEMPT. STRONG FUEL ODOR IN COCKPIT & FUEL SPILLED ON GROUND UNDER APU. INTERROGATED CDS, FOUND IGNITION FAULT. PERFORMED START OF APU WITH NO DEFECTS. OK FOR SERVICE. COULD NOT DUPLICATE.

Part: STRUCTURE — MALFUNCTIONED (GLARE SHIELD) · airframe 13,664 hrs · 14,690 cycles

CAPT SIDE GLARESHIELD VINYL, BLOCKS VIEW OF ENGINE FIRE WARNING ON GLARESHIELD WHEN SEATED AT PROPER POSITION. R & R EYEBROW PIECE CAPT SIDE ON GLARESHIELD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (PROPELLER) · airframe 13,661 hrs · 14,686 cycles

WITH POWER LEVERS AT DETENT TORQUE ON NR 2 ENGINE WAS ABOVE TARGET AND PROPELLER RPM WAS 970. INTERROGATED CDS FOR FAULTS. NO FAULTS INDICATED. GROUND RAN ACFT, ON APPLICATION OF HIGH POWER WAS ABLE TO DUPLICATE DISCREPANCY ABOUT THREE TIMES AND THEN COULD NOT DUPLICATE AFTER THAT. R & R NR 2 ENGINE OVERSPEED GOVERNOR IAW AMM TASKS 61-20-26-000-801 AND 61-20-26-400-801. NR 2 OVERSPEED GOVERNOR CHANGED AS A PRECAUTION. GROUND RAN ACFT AT HIGH POWER AGAIN. PROP SPEED INDICATED NORMAL AND ENGINE TORQUE INDICATED NORMAL. ALL OPS CHECKED ARE GOOD. NO LEAKS NOTED. COMPLIED WITH ENGINE TREND DOWNLOAD IAW TASK CARD 6773101. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 13,657 hrs · 14,681 cycles

EXIT SIGN LENS AND ROW 2 BULKHEAD FELL OFF. INSTALLED LENS. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (BRAKES) · airframe 13,407 hrs · 14,439 cycles

DURING LANDING, BRAKES ARE INEFFECTIVE. ON POST INSPECTION, IT APPEARS INSIDE WHEELS BRAKE ARE INOPERATIVE. ZERO HEAT GENERATED. OUTER WHEELS EXTREMELY HOT. INTERROGATED CDS NO FAULTS FOUND. INSPECTED NR 2 & NR 3 WHEEL SPEED TRANSDUCERS. FOUND NR 2 TRANSDUCER TO BE BINDING. R & R NR 2 WHEEL SPEED TRANSDUCER IAW AMM TASK 32-46-11-000-801 AND 32-46-11-400-801. OPS/FUNCTIONAL TEST GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: SEAL — LOOSE (PAX DOOR) · airframe 13,190 hrs · 14,213 cycles

RUBBER SEAL LOOSE ON THE MAIN CABIN DOOR DITCHING DAM. RESECURED THE RUBBER SEAL ON THE MCD OVERHEAD DITCHING DAM. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: STRINGER — DAMAGED (32 RIGHT) · airframe 13,042 hrs · 14,042 cycles

APPROXIMATELY 1 INCH AFT OF FS -54 O/B OF STRINGER 32S FOUND LIGHTNING DAMAGE. DRILLED OUT DAMAGE IAW SRM 51-40-07-02-01. FOUND AREA TO BE OUT OF LIMITS DUE TO CHEM MILLED STEP PROXIMITY IAW SRM 53-10-31-02-02. CONFIRMED AREA CRACK FREE.

Part: STRINGER — DAMAGED (32 RIGHT) · airframe 13,042 hrs · 14,042 cycles

APPROXIMATELY 5 INCHES FORWARD OF FS -39 OTBD OF STRINGER 32S, FOUND LIGHTNING DAMAGE. REMOVED DAMAGE FROM SKIN IAW SRM 53-10-31-02-02. CONFIRMED CRACK FREE. INSTALLED RIVET IN HOLE IAW SRM 53-10-02-02. APPLIED INTERIOR AND EXTERIOR SURFACE PROTECTION.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 13,042 hrs · 14,042 cycles

FOUND LIGHTNING DAMAGE ON THE LT ELEVATOR AT THE OTBD CORNER OF THE T/E. CUT OF DAMAGED SKIN UPPER AND LOWER IAW SRM 55-20-30-02-01. REMOVED DAMAGED TIP BLOCK. REPLACED TIP BLOCK. CONFIRMED SKIN TO BE CRACK FREE. FABRICATED REPAIR PACKERS IAW SRM 55-20-30-02-01. FABRICATED REPAIR DOUBLERS IAW SRM 55-20-30-02-01. INSTALLED REPAIR IAW TEMP REV 55-003 OF SRM 55-20-30-02-01. ALODINED PRIMED AND PAINTED AREAS.

Part: STRINGER — DAMAGED (33) · airframe 13,042 hrs · 14,042 cycles

APPROXIMATELY 2 INCHES AFT OF FS -19 AT STRINGER 33, FOUND LIGHTNING DAMAGE. REMOVED DAMAGE BY DRILLING HOLE .166" IAW SRM 53-00-00-02-08. CONFIRMED CRACK FREE. INSTALLED REPAIR FASTENER IAW SRM 53-00-00-02-08. APPLIED INTERIOR AND EXTERIOR SURFACE PROTECTION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,042 hrs · 14,042 cycles

LIGHTNING STRIKE DAMAGE AT THE FUSELAGE BELLY 6" AFT OF STATION -69 BETWEEN STRINGERS 33 AND 32S. BLENDED DAMAGE IAW RD 8/4-53-505. BLENDED DAMAGE IS 4" AFT OF STATION -69, REMOVED DAMAGE 6" AFT OF STATION -69 BY DRILLING IAW RD 8/4-53-2037. VERIFIED TO BE CRACK FREE. WITHIN LIMITS. INSTALLED RIVET IAW SRM 51-25-10-02-01. APPLIED CPC.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 13,042 hrs · 14,042 cycles

LIGHTNING STRIKE DAMAGE TO THE FUSELAGE BELLY AT STATION -111 BETWEEN STRINGERS 33 AND 32S. REMOVED DAMAGED RIVET IAW SRM 51-42-05-02-01. VERIFIED TO BE CRACK FREE. INSTALLED RIVET. APPLIED SURFACE PROTECTION AND APPLIED CPC.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,042 hrs · 14,042 cycles

LIGHTNING STRIKE DAMAGE TO THE FUSELAGE BELLY AT STATION -20 BETWEEN STRINGERS 33 AND 32S. REMOVED DAMAGE IAW RD 8/4-53-505. BLEND WITHIN LIMITS, VERIFIED TO BE CRACK FREE. APPLIED ALODONE TOPCOAT.

Part: STRINGER — DAMAGED (32 RIGHT) · airframe 13,042 hrs · 14,042 cycles

APPROX 3 INCHES FORWARD OF FS -69.4 OTBD OF STRINGER 32S FOUND LIGHTNING STRIKE DAMAGE. REMOVED DAMAGE TO SKIN IAW SRM 53-10-31-02-02. CONFIRMED CRACK FREE. INSTALLED RIVET AND INSTALLED SURFACE PROTECTION. APPLIED PRIMER PAINT AND CPC.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,042 hrs · 14,042 cycles

APPROXIMATELY 8 INCHES FORWARD OF FS 1 INBD OF STRINGER 32, FOUND LIGHTNING DAMAGE. REMOVED DAMAGE FROM SKIN IAW SRM 53-20-31-02-01. CONFIRMED CRACK FREE. INSTALLED RIVET IN HOLE IAW SRM 53-10-31-02-02. APPLIED INTERIOR AND EXTERIOR SURFACE PROTECTION.

Part: SIGN — MISINSTALLED (CABIN) · airframe 13,006 hrs · 14,004 cycles

ROW 2 BULKHEAD EXIT SIGN LOOSE. REMOVED INCORRECT FASTENERS & INSTALLED NEW FROM STORES. OPS CHECK OF EMERGENCY LIGHTING IS GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED

NR 1 PROP FEATHER TEST FAILED. CHECKED CDS FOR FAULT CODES, NONE FOUND. OPS TEST OF THE PROPELLER AUTOFEATHER & UPTRIM SYS IAW AMM 61-20-00-710-801. CHECKED GOOD, NO DEFECTS NOTED. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: LIGHT — NO TEST (ZONE 200) · airframe 12,590 hrs · 13,584 cycles

FLOOR PATH LIGHTING INBD OF FORWARD CARGO BAY FAILED 10 MINUTE ILLUMINATION TEST. REPLACED EFFECTED FLOOR STRIP.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 12,509 hrs · 13,525 cycles

CABIN FLOOR PATH LIGHTING DETERIORATED AT SEGMENTS 1, 2, 4, 6, 7, 8, 10, 11, AND FORWARD CARGO BAY AREA. REPLACED EFFECTED EMERGENCY LIGHT STRIPS.

Part: IGNITER — FAILED (APU) · airframe 12,381 hrs · 13,386 cycles

APU FAIL LIGHT ILLUMINATED DURING START ATTEMPT WITH A SIGNIFICENT AMOUNT OF FUEL DUMPED ON THE GROUND UNDER THE TAIL SECTION. HEAVY FUEL ODOR INSIDE ACFT. R & R IGNITOR PLUGS WITH NEW IAW AMM TASK 49-40-04-000-801/49-40-04-400-801. PERFORMED START PROCEDURE INSPECTION OF APU IAW TASK 49-00-00-869-801. CHECKED GOOD, NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (NR 2) · airframe 12,204 hrs · 13,205 cycles

DURING ROLLOUT AND TAXI-IN ACFT SEEMED TO BE PRODUCING THRUST WITH POWER LEVERS AT FULL DISC POSITION. CONSTANT BRAKING WAS NEEDED TO CONTROL SPEED. AFTER SHUTDOWN NR 2 PEC CAUTION & POWERPLANT MESSAGE. REPLACED NR 2 PCU & JUNCTION BOX DB3-K2 DAUGHTER BOARD 3 IAW TASKS 61-20-11-000-801 & 61-20-11-400-801 & 20-30-16-960-801 & 24-50-60-400-801 OF AMM. ALL OPS CHECKS GOOD. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (ZONE 400) · airframe 12,161 hrs · 13,163 cycles

AFTER LANDING, DURING TAXI , PROPS DIDN'T SEEM TO COME OUT OF FLT IDLE TO DISC FOR A MINIMUM OF 20 SECS, POSSIBLY LONGER. ACFT TAXIED AT FASTER THAN NORMAL SPEED & ACCELERATED IF BRAKES WERE NOT APPLIED WITH POWER LEVERS IN DISC POSITION. AFTER 20 OR MORE SECONDS, PROPS FINALLY ATTAINED DISC POSITION. NOISE CHANGE INDICATION ONLY. PSEU & CDS SHOW NO RELATED FAULTS. GROUND RUN IN & OUT OF FEATHER, COULD NOT DUPLICATE DISCREPANCY. REPLACED PEC NR 2 AS A PRECAUTIONARY MEASURE IAW AMM 61-20-36-000-801 & 61-20-36-400-801. OPS TESTED GOOD. RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 11,842 hrs · 12,788 cycles

FWD AND AFT EMERGENCY EVAC LIGHTS ARE INOPERATIVE INTERMITTENTLY. REPLACED BATTERY PACKS FOR LIGHTS. OPS CHECKED GOOD.

Part: PROPELLER — MALFUNCTIONED · airframe 11,735 hrs · 12,678 cycles

ON LANDING, PROPELLERS DID NOT APPEAR TO GO TO DISCING, HAD TO RIDE BRAKES EVEN IN FULL DISC ON TAXI. NR 2 PROP GROUND RANGE LIGHT WAS NOT ILLUMINATED EVEN AT FULL DISC. JUST SHORT OF PARKING IT WENT BACK TO NORMAL. NO FAULTS NOTED. GROUND RAN BOTH ENGINES AND CYCLED PROPS IN AND OUT OF BETA RANGE SEVERAL TIMES. BOTH NR 1 AND NR 2 PROP BETA RANGE LIGHTS ILLUMINATED AND EXTINGUISHED NORMALLY. CHECKED FOR FAULTS AGAIN, NONE FOUND. NO DEFECTS NOTED AT THIS TIME. NO PREVIOUS HISTORY. ALSO, NO SIGNS OF ANY GREASE LEAKING AROUND NR 2 PROP. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONNECTOR — UNSECURE (SMOKE DETECTOR) · airframe 11,447 hrs · 12,403 cycles

DURING DAILY SYS TEST, NR 1 AFT BAGGAGE SMOKE DETECTOR DID NOT TEST. RESEATED NR 1 AFT BAG SMOKE DETECTOR ELECTRICAL CONNECTOR. C/W, OPS TEST OF THE BAGGAGE SMOKE DETECTOR IAW AMM TASK 26-12-06-710-801. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: DOOR — FROZEN (MAIN PAX) · airframe 11,132 hrs · 12,060 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. REMOVED ICE & MOISTURE FROM PART AROUND MCD SEAL. INSPECTED SEAL. N/D/N. C/W OPS CK OF MCD IAW TK 52-11-00-712-802. NO DEFECTS NOTED. ACFT OK FOR CONT SERVICE. NO PARTS REPLACED.

Part: ANGLE — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

CORROSION FOUND ON WING BULKHEAD ANGLE OF THE BULKHEAD ASSY LOWER INBD EDGE. CORROSION BLENDED TO LIMITS IAW RD 8/4-25-262. COMPLIED WITH TASKCARD RD 8/4-25-262.

Part: ANGLE — CORRODED (BS 783.102) · airframe 10,870 hrs · 11,793 cycles

ANGLE AT STA X783.102 CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-40-07-02-01. BLENDED CORROSION AROUND FASTENER HOLE ON ANGLE . REMOVED .023 FROM AROUND FASTENER HOLE. STARTING THICKNESS OF .080, REMAINING THICKNESS OF .057. BLEND AREA OF 2.0" X .7500". REAMED FASTENER HOLE TO .312 WORK DONE IAW SRM 51-21-00-00-02. PERFORMED FPI ON BLENDED AREA AROUND FASTENER HOLE ON ANGLE IAW CHAPTER 8 NO DEFECTS NOTED. INSTALLED ANGLE IAW SRM 51-42-05-02-0. APPLIED SEALANT TO BLENDED AREA IAW RD 8/4-53-4095. ALL WORK DONE IN COMPLIANCE WITH TASK CARD RD 8/4-53-4095.

Part: PANEL — DAMAGED (LT NACELLE) · airframe 10,870 hrs · 11,793 cycles

LT AFT NACELLE PANELS 414AR AND 424AL AFT END ARE CHAFED FROM EXHAUST. REPAIRED IAW RD 8/4-54-012.

Part: SKIN — CHAFED (RT NACELLE) · airframe 10,870 hrs · 11,793 cycles

INBD AND OTBD UPPER RT NACELLE PANELS ARE CHAFING ON EXHAUST ASSY. REPAIRED IAW RD 8/4-54-012.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 10,870 hrs · 11,793 cycles

FLOOR SUPPORT PLATES UNDER FLOORBOARD 233AZ ARE CORRODED. FABRICATED AND INSTALLED NEW SUPPORT PLATES IAW TASK CARD 6-53-1036 AND SRM 51-42-05-02-01. TREATED AND PRIMED PER TC 6-53-1036, 51-21-10-02-01 AND 51-25-10-02-01.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 10,870 hrs · 11,793 cycles

MAIN PASSENGER DOOR THRESHOLD CORRODED. REMOVED SILL IAW SRM 51-42-05-00-01. BLENDED CORROSION, BUT FOUND TO BE THROUGH SILL AND OUT OF LIMITS. DRILLED NEW THRESHOLD IAW SRM 51-40-07-02-01. INSTALLED SILL AND ORIGINAL RUB STRIP IAW SRM 51-42-05-02-01.

Part: CHANNEL — CORRODED (PAX DOORWAY) · airframe 10,870 hrs · 11,793 cycles

UPON REMOVING THE PASSENGER DOOR THRESHOLD FOUND CORROSION ON THE THRESHOLD CHANNEL. BLENDED CORROSION IAW SRM 53-20-23-02-01. WITHIN LIMITS. PERFORMED LPI ON BLENDED AREAS OF PAX DOOR THRESHOLD, NO EVIDENCE OF CORROSION OR DEFECTS. WORK DONE IAW NDT MM CH 8. ALODINED, PRIMED AND PAINTED PAX DOOR THRESHOLD PER SRM TASK 53-20-23-02-01.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 524FT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624AT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: UNKNOWN — CORRODED (BS 783.102) · airframe 10,870 hrs · 11,793 cycles

MULTIPLE AREAS OF CORROSION FOUND AT STA X783.102. REMOVED CORROSION AT STA X783.102 IAW SRM 51-21-00-00-02. CLEANED, TREATED WITH ALODINE AND PRIMED CORRODED AREA AT STATION X 783.102 IAW RD 8/4-53-4068. ALL WORK PERFORMED DONE IN COMPLIANCE WITH TASK CARD RD 8/4-53-4068.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORRODED MOUNTING ANGLE UNDER AIR STAIRS. BLENDED CORROSION, ORIGINAL THICKNESS IS .090", REMOVED .010", IAW SRM 51-21-00-00-02. PERFORMED LPI ON ANGLE, NO CRACKS FOUND IAW CH 8 TOC. ALODINED AND APPLIED EPOXY PRIMER IAW RD 8/4-52-696. INSTALLED AFT MOUNT ANGLE IAW AMM 20-10-01-430-801. WORK DONE IAW RD 8/4-52-696.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624AT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. ACCESS PANEL 524CT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624FT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624BT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. ACCESS PANEL 524DT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624CT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624DT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445 AND TASK CARD RD 8/4-57-1692.

Part: PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. PANEL 624ET HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. ACCESS PANEL 524AT HAS SURFACE CORROSION. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACCESS PANEL 524BT HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (WING) · airframe 10,870 hrs · 11,793 cycles

ACFT IS DOWN FOR C-CHECK. ACCESS PANEL 524ET HAS SURFACE CORROSION ON PANEL AND ITS MATING SURFACE. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442 AND RD 8/4-57-445.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 10,870 hrs · 11,793 cycles

AFT SERVICE DOOR EDGE CHANNEL IS CORRODED. REMOVED FASTENERS AND NUTPLATES AND EDGE CHANNEL, BLENDED OUT CORROSION. SENT ENGINEERING REQUEST TO MFG. FABRICATED EDGE CHANNEL IAW SRM 53-40-21. TREATED AND PRIMED IAW SRM 51-20-00-00-01. INSTALLED NUTPLATES IAW SRM 51-42-05-02-01. INSTALLED FASTENERS IAW SRM 51-42-05, 51-42-45 AND 51-42-60. COMPLIED WITH AND ALL WORK DONE IAW TASK CARD 6-53-1031.

Part: STRUCTURE — CORRODED (BS 783.102) · airframe 10,870 hrs · 11,793 cycles

MULTIPLE AREAS OF CORROSION FOUND AT STA X783.102. ACFT DOWN FOR C-CHECK. REMOVED CORROSION AND COMPLETED REPAIR IAW SRM 51-21-00-00-02 AND TASK CARD RD 8/4-53-4062.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. SEAT TRACK PN CORRODED. BLENDED MINOR CORROSION. BLEND IS WITHIN LIMITS IAW RD 8/4-53-884. TREATED IAW SRM 51-21-10-02-01. PERFORMED FPI ON BLENDED AREAS IAW CHAPTER 8, NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORROSION FOUND A RT INBD SEAT TRACK BETWEEN PILOTS BULKHEAD AND FS 70.5. BLENDED OUT CORROSION IAW SRM 51-21-00, FOUND WITHIN LIMITS SRM 53-20-49-02.

Part: SEAT TRACK — CORRODED (BS 70.5-428.5) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORROSION FOUND AT LT INBD SEAT TRACK BETWEEN FS 70.5 - 428.5. BLENDED AREAS OF CORROSION. MAX BLEND DEPTH OF .008. MAX LENGTH X WIDTH 8"X.5". REMAINING MATERIAL OF .412. WORK DONE IAW R/D 8/4-53-884. BLENDS FOUND WITHIN LIMITS. PERFORMED FPI IAW CH 8, NO DEFECTS NOTED. TREATED IAW RD 8/4-55-884.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C- CHECK. CORROSION FOUND AT LEFT INBD SEAT TRACK BETWEEN PILOTS BULKHEAD AND FS 70.5. BLENDED OUT CORROSION IAW SRM 51-21-00, FOUND WITHIN LIMITS SRM 53-20-49-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,870 hrs · 11,793 cycles

SEAT TRACK CORRODED. BLENDED OUT CORROSION IAW SRM 53-20-49-02-02 AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. INSTALLED NEW SEAT TRACK IAW SRM 51-40-07-02-01, 51-42-05-02-01 AND 51-41-00-00-01. PRIMED AND TOP COATED IAW 51-25-10-02-01 AND 51-25-15-02-01.

Part: SEAT TRACK — CORRODED (BS 428.5-644.5) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORROSION FOUND AT LT INBD SEAT TRACK BETWEEN FS 428.5 - 644.5. BLENDED OUT CORROSION IAW SRM 51-21-00, FOUND WITHIN LIMITS SRM 53-20-49-02.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 10,870 hrs · 11,793 cycles

RT OTBB FLAP CHAFED ON UPPER SKIN. BLENDED CHAFED AREA YW 194.5 TO 210, 15 INCHES FWD OF T/E OF RT INBD FLAP, WIDTH OF BLEND WAS .375/.002 MATERIAL REMOVED. BLENDED CHAFED AREA YW 227 TO 244 APPROX 13.5 INCHES FWD OF T/E OF FLAP, DEPTH OF BLEND WAS .004. BOTH BLENDED AREAS FOUND IN LIMITS IAW RD 8/4-57-1594. PERFORMED ECI , NO CRACKS FOUND AT THIS TIME IAW NDTM PSM 1-84-7A 51-00-06. PERFOMED ULTRASONIC DEBOND INSP, NO DISBOND NOTED. TREATED, PRIMED AND PAINTED.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 10,870 hrs · 11,793 cycles

AFT SERVICE DOOR EDGE CHANNEL IS CORRODED. BLENDED CORROSION ON SERVICE DOOR EDGE CHANNEL. FABRICATED EDGE CHANNEL IAW SRM 53-40-21. TREATED AND PRIMED IAW SRM 51-20-00-00-01. INSTALLED NUTPLATES IAW SRM 51-42-05-02-01, INSTALLED FASTENERS IAW SRM 51-42-05, 51-42-45 AND 51-42-60. WORK DONE IAW TASK CARD 6-53-1031.

Part: SEAT TRACK — CORRODED (BS 428.5-644.5) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORROSION FOUND A RT INBD SEAT TRACK BETWEEN FS 428.5 - 644.5. BLENDED OUT CORROSION IAW SRM 51-21-00, FOUND WITHIN LIMITS SRM 53-20-49-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,870 hrs · 11,793 cycles

SEAT TRACK CORRODED. BLENDED OUT CORROSION IAW SRM 53-20-49-02-02. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-844. REMOVED SEAT TRACK IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01. INSTALLED SEAT TRACK IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. TOP COATED IAW SRM 51-25-25-02-02.

Part: SEAT TRACK — CORRODED (BS 100.8-428.5) · airframe 10,870 hrs · 11,793 cycles

ACFT DOWN FOR C-CHECK. CORROSION FOUND A RT SEAT TRACK BETWEEN FS 100.80 - 428.5. BLENDED MULTIPLE AREAS OF CORROSION, MAX BLEND DEPTH .008 MAX LENGTH X WIDTH 8X.5", REMAINING MATERIAL .412. DONE IAW RD 8/4-53-884. BLENDS FOUND TO BE WITHIN LIMITS. PERFORMED FPI ON BLENDED TRACK IAW CH 8, NO DEFECTS NOTED. TREATED IAW RD 8/4-53-884.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,870 hrs · 11,793 cycles

SEAT TRACK CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05. LOCATED AND DRILLED SERVICEABLE TRACK IAW SRM 51-40-07-02-01 AND 51-40-05-00-01. INSTALLED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: FILTER — ODOR (CABIN) · airframe 9,906 hrs · 10,790 cycles

SAME ODOR DETECTED AS LOG PAGE DISCREPANCY 500901 (BURNING PLASTIC ODOR). ODOR WAS NOT AS STRONG AND DID NOT LAST AS LONG (APPROX 1 MINUTE) BUT WAS STILL DETETECTED. REPLACED THE RECIRCULATION FILTER IAW AMM TASK 21-22-22-000-801 AND 21-22-222-400-801 AND C/W SUBTASK 21-22-16-710-001 FOR OPS CHECK OF THE FAN, OPS CHECK GOOD. RETURNED TO SERVICE.

Part: FILTER — DIRTY (RECIRC FAN) · airframe 9,902 hrs · 10,787 cycles

DURING FINAL 10-15 MIN OF FLIGHT, ODOR DETECTED BY ALL 4 CREW AND PASSENGERS. SEEMED TO SMELL LIKE BURNING PLASTIC, SUSPECTED IT WAS COMMING FROM BLEED AIR/ ENVIROMENTAL SYS, ISOLATED TO RECIRCULATING FAN. PLACED RECIRCULATING FAN ON MEL 21-20-2. CLEARED BY: R & R RECIRCULATING FAN FILTER IAW 21-22-22-000-801 AND 21-22-22-400-801 PERFORMED OPS TEST OF RECIRCULATING FAN IAW 21-22-16-710-001. OPS CK GOOD, NO FURTHER ODOR NOTED. ALSO PERFORMED A GVI OF THE COFFEE WARMERS AND NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 9,696 hrs · 10,580 cycles

AFT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN FWD F/A SWITCH IS PUSHED. REPLACED THE BATTERY PACKS FOR POSITION 3 IAW AMM 33-51-00-820-801. OPS CHECKS GOOD.

Part: SWITCH — MALFUNCTIONED (OVERTEMP) · airframe 9,428 hrs · 10,319 cycles

NR 1 BLEED CAUTION LIGHT SHORTLY AFTER TAKEOFF. RETURN TO FIELD. LANDING UNEVENTFUL. NR 1 BLEED HOT CAUTION LIGHT STAYED ON WITH ENG OFF AND DUCT COLD. REPLACED NR 1 BLEED OVER TEMP SWITCH IAW MM 36-11-16-000-801/400-801. RETURNED TO SERVICE.

Part: DOOR — CONTAMINATED (MAIN PAX) · airframe 9,227 hrs · 10,099 cycles

UNABLE TO OPEN THE MAIN CABIN DOOR FROM THE INSIDE. REMOVED MOISTURE FROM THE DOOR SEAL AND FRAME AREAS. NO DAMAGE TO THE DOOR SEAL. DOOR OPERATES NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: THERMOCOUPLE — FAILED (APU ENGINE) · airframe 9,128 hrs · 9,990 cycles

APU FAILED TO START ON THE FIRST TRY. APU FAIL LIGHT ILLUMINATED. RAMP REPORTS LOTS OF SMOKE FROM THE APU EXHAUST AFTER FAILURE TO START. PLACED APU ON MEL 49-00-1. CLEARED BY: LOOKING AT CDS AND FOUND FAULT CODE 129-1 EGT T/C 2 OPEN. C/W FIM Q400 49-70-070810-810. FOUND NO DEFECTS WITH THE WIRING. REPLACED THE THERMOCOUPLE NR 2 IAW 49-70-07-000-801 AND TASK 49-70-07-400-801. OPS CHECKS GOOD. CLEARED MEL.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 7,635 hrs · 8,398 cycles

GREEN LIGHT MAIN GEAR INDICATOR STAYED ILLUMINATED AFTER GEAR RETRACTION. R & R LANDING GEAR CONTROL PANEL, IAW AMM TASK 32-31-01-000-801, 32-31-01-400-801, FUNCTIONAL TEST GOOD, IAW AMM TASK 32-31-01-720-801. INSPECTED LANDING GEAR HARNESS, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN CABIN) · airframe 6,869 hrs · 7,489 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. INSPECTED MCD SEAL AND HANDLE MECHANISM NO DEFECTS NOTED. PERFORMED OPS TEST OF THE FWD PASSENGER DOOR IAW AMM TASK 523-11-00-710-802. OPS TEST GOOD CLEANED DOOR SEAL. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: INSERT — LOOSE (PAX DOOR) · airframe 6,596 hrs · 7,168 cycles

MAIN CABIN DOOR WILL NOT OPEN. FOUND LOOSE SCREW IN AFT HANDRAIL LINKAGE. REPLACED THREADED INSERT. RETURNED TO SERVICE. DOOR CHECKS GOOD.

Part: NUT — MISSING (PAX DOOR) · airframe 6,554 hrs · 7,128 cycles

CAN NOT OPEN PASSENGER DOOR FROM THE INSIDE. FOUND AFT HANDRAIL THREADED BUSHING MISSING FROM CABIN DOOR STRUT. REPLACED. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE.

Part: BUSHING — MISSING (PAX DOOR) · airframe 6,484 hrs · 7,041 cycles

INBOUND FLIGHT CREW COULD NOT FULLY OPEN THE MAIN CABIN DOOR. INSPECTED AND FOUND MAIN CABIN DOOR HAND RAIL SUPPORT JOINT NUT TO BE MISSING. INSTALLED NEW THREADED NUT. IPC NR 52-11-21 FIG 1 ITEM NR 630 PN 85210276-101. OPS CHECK OF DOOR IS NORMAL. NO DEFECTS NOTED.

Part: SWITCH — MALFUNCTIONED (BLEED OVERTEMP) · airframe 5,871 hrs · 6,369 cycles

DURING CLIMB, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. PERFORMED EMERY/ABNORMAL CHECKLISTS. WITH NR 1 BLEED SWITCH OFF, NR 1 BLEED HOT CAUTION REMAINED ILLUMINATED. REMOVED AND REPLACED NR 1 ENG BLEED OVER TEMPERATURE SWITCH IAW AMM TASK 36-11-16-000-801, AND INSTALLED IAW AMM TASK 36-11-16-400-801. GROUND RAN ACFT, CAUTION LIGHT DID NOT RETURN. NO OTHER DEFECTS NOTED.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 5,847 hrs · 6,340 cycles

LAV SMOKE DETECTOR WENT OFF NO SMOKE NOTICED RESET LIGHT, TURNED GREEN. REPLACED LAV DETECTOR IAW AMM TASK 26-12-11-000-801 AND TASK 26-12-11-400-801. OPS CK NORMAL. RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 5,515 hrs · 5,918 cycles

SEA - MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED OPERATIONAL TEST OF FORWARD PASSENGER DOOR PER Q400 AMM 52-11-00-710-802. CHECKS GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 5,231 hrs · 5,621 cycles

SEA - AFT PASSENGER DOOR VERY HARD TO OPEN. CLEANED AND LUBRICATED DOOR SEAL. REF Q400 AMM TASK 12-20-01-640-811 PAR 4B. OPS CHECKS GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 5,158 hrs · 5,545 cycles

SEA - ON CLIMBOUT THROUGH 2700 FEET AT AROUND 270 KNOTS, THE MAIN GEAR RED UNSAFE LIGHTS CAME ON (AND GEAR HANDLE LIGHT) MOMENTARILY. PSEU CHECKED, RELATED CODES TO LANDING GEAR WERE RT MLG UPLK UNREASON FAR, LT MLG UPLK UNREASON NEAR, RT GEAR DOOR LK UNREASON FAR. CHECKED GAPS AND INDUCTANCE FOR RT AND LT MLG DOOR NO DISCREPANCIES NOTED. REMOVED AND REPLACED THE PSEU AS A PRECAUTIONARY MEASURE. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,978 hrs · 5,328 cycles

PDX -C1- SEAT TRACK NR 11 AT STA 71.2 HAS CORROSION ON TOP OF CLAW. REMOVED AND REPLACED SEAT TRACK REF D8 Q400 SRM 51-42-05.

Part: ALTIMETER — FAILED (RADIO) · airframe 4,702 hrs · 4,990 cycles

PDX - AFTER ADDING POWER FOR TAKEOFF JUST OVER THE GATE STICK PUSHER CAUTION LIGHT AND GPWS CAUTION LIGHTS ILLUMINATED ABORTED TAKEOFF AND RETURNED TO GATE. FIRST OFFICER RAD ALT TURNED RED FROM 0 TO RED RA. PLACED THE RADIO ALTIMETER ON MEL 34-40-6. RETURNED TO SERVICE. REPLACED THE NR 2 RAD ALT R/T. OPERATIONAL CHECKS GOOD.

Part: VALVE — FAILED (DE ICE SYS) · airframe 4,398 hrs · 4,656 cycles

GEG - "DEICE PRESS" CAUTION IN FLIGHT. NR 2 GREEN LAMP ON TAIL DOES NOT ILLUMINATE WHEN PRESSURIZED. DIVERTED TO GEG AND ACCOMPLISHED A UNEVENTFUL LANDING. REPLACED NR 6 DDV IAW AMM TASK 30-11-16-000-801, AND 30-11-16-400-801. FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: LATCH — FAILED (LANDING GEAR) · airframe 4,031 hrs · 4,235 cycles

SEA - DOOR TO ALTERNATE EXTENSION WILL NOT OPEN. INSPECTED AND FOUND LATCH BROKEN. REMOVED AND REPLACED LATCH, OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED

AUTO FEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. MAINT FOUND 64,70,494 ON ENG 1 CHAN A AND CODE 494 ON CHAN B. CLEARED PEC CODES IAW Q400AMM TASK 61-20-36-070-801 FOR BOTH ENGINES. PERFORMED OPS TEST OF AUTOFEATHER SYSTEM IAW AMM TASK 61-20-00-710-801. OPS TEST GOOD - TEST PASSED. GROUND RAN ACFT TO RATING PWR AND AUTO FEATHER ARMED AS REQUIRED. CHECKED CDS FOR CODES, NO CODES POSTED. RETURN TO SERVICE NO PARTS REPLACED. (K)

Part: WIRE HARNESS — FAULTY (NLG) · airframe 3,222 hrs · 3,349 cycles

SEA AFTER TAKEOFF FROM BOI, THE RT GEAR DOOR LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED TO SEA. PERFORMED AN EMERGENCY GEAR EXTENSION ON APPROACH TO SEA AND ACCOMPLISHED AN UNEVENTFUL LANDING. ACFT FERRY TO PDX FOR REPAIRS. IN PDX, MX FOUND MULTIPLE PSEU FAULTS IN MEMORY. REPLACED THE NOSE GEAR HARNESS AND THE PSEU AS A PRECAUTION. CHECKS GOOD. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 1,417 hrs · 1,385 cycles

PDX - FLIGHT NR 2250 - DURING CRUISE A MASTER WARNING LIGHT ILLUMINATED INDICATING THE FORWARD BAGGAGE DOOR UNSAFE. CHECK LIST RUN AND PRESSURIZATION WAS NORMAL. DIVERTED TO PDX FOR WORK. MAINTENANCE (INITIAL INSPECTION OF DOOR FOUND HANDLE IMPROPERLY STOWED) INSPECTED THE DOOR LINKAGE NO DEFECTS WERE NOTED. CLEANED AND LUBRICATED THE DOOR HANDLE SHAFT. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 1,417 hrs · 1,385 cycles

PDX - FLIGHT 2250 (RNO-SEA) - IN CRUISE FLIGHT RECEIVED A FORWARD BAGGAGE DOOR WARNING. DIVERTED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE CLEANED AND LUBRICATED THE DOOR HANDLE SHAFT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — NOT SEATED (CARGO DOOR) · airframe 892 hrs · 856 cycles

SMF - ON FLIGHT 2384, DIVERTED FLIGHT, CLIMBING THRU FL220 MASTER WARNING ANNUNCIATED SHOWING FUSELAGE DOOR R1 SHOWED UP ON DOOR PAGE MASTER WARNING INTERMITTENTLY KEPT CYCLING WITH NO CHANGE IN CABIN PRESSURE. MAINTENANCE FOUND CARGO DOOR HANDLE NOT FULLY SEATED IN LOCKED POSITION UPON ARRIVAL. PERFORMED OPERATIONAL TEST OF DOOR AND DOOR WARNING SYSTEM. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (GALLEY DOOR) · airframe 580 hrs · 553 cycles

LAX FLIGHT NR 2446: CLIMBING THROUGH 7000 FT, RECEIVED THE FUSELAGE DOORS MASTER WARNING. THE GALLEY SERVICE DOOR SHOWED OPEN ON DOOR PAGE. FA ADVISED DOOR HANDLE WAS OUT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE, DURING TAXI TO GATE, NOTICED AFT SERVICE DOOR EXTERNAL HANDLE EXTENDING OUT APPROX 1/4". PERFORMED OPS TEST OF AFT SERVICE DOOR. OPS CHECK GOOD. PRESSURIZED A/C IAW Q400 AMM TASK 21-00-00-863-801. AFT SERVICE DOOR REMAINED LOCKED. DEPRESSURIZED A/C IAW TASK 21-00-00-863-802. PERFORMED GVI OF AFT SERVICE DOOR. OPS TEST OF AFT SERVICE DOOR IAW TASK 52-41-00-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: STARTER GEN — WARNING LIGHT (NR 2) · airframe 360 hrs · 350 cycles

SEA FLIGHT NR 2241: NR 2 DC GEN CAUTION. AIRCRAFT RETURNS TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 DC STARTER/GENERATOR IAW TC 6243101 (1-4). GROUND RAN. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 233 hrs · 227 cycles

PDX FLIGHT NR 2326: ON START UP FOR TAXI, NR 2 DC GEN WOULD NOT COME ON-LINE. RAN CHECKLIST. NO HELP PER CHECKLIST. LEFT NR 2 DC GEN SWITCH OFF. MAINTENANCE CYCLED BUSS FAULT. RESET SWITCH AND C/W OPS TEST OF DC GEN SYSTEM IAW Q400 AMM TASK 24-31-00-710-802. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EXTERIOR) · airframe 61 hrs · 58 cycles

LAX FLIGHT NR 2334: DURING TAXI, NOTICED POSITION LIGHT NOT ON. TURNED ON SWITCH AND C/B POPPED. AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE REPLACED BULB AND PERFORMED OPS TEST IAW Q400 AMM TASK 33-42-00-710-801. NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 66 hrs · 62 cycles

LAX FLIGHT NR 2334: CABIN ALT CLIMBING EXCESSIVELY. NOTICED FAULT LIGHT ILLUMINATED ON PRESSURE CONTROLLER. RAN EMERGENCY CHECKLIST. HAD THEM RUNNING IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED AFT OUTFLOW VALVE IAW Q400 AMM TASK 21-31-10-000-801 AND 21-31-10-400-801. FUNCTIONAL TEST GOOD IAW 21-31-00-720-801. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — UNKNOWN (FUEL TANK LOW) · airframe 48 hrs · 45 cycles

LAX FLIGHT NR 2442: NR 1 FUEL TANK LOW CAUTION ON. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REFUELED AND DEFUELED A/C SEVERAL TIMES LEAVING 2000 LBS A SIDE. NO DEFECTS NOTED. OPERATION PERFORMED IAW Q400 MM TASK 12-10-28-650-802 AND 12-10-28-650-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (NACELLE) · airframe 52 hrs · 48 cycles

RNO FLIGHT NR 2444: NR 2 BLEED AIR CAUTION IS ON. DUCT TEMP WAS NORMAL. RAN CHECKLIST AND TURNED OFF NR 2 DUCT. CAUTION REMAINED ON AFTER LANDING AND SHUTDOWN. NO OTHER ABNORMAL INDICATIONS NOTED. MAINTENANCE REMOVED AND REPLACED NACELLE DUCT LEAK OVERTEMP SWITCH IAW TASK 36-11-21-000-801 AND 36-11-21-400-801. OPS CHECK GOOD. NR 2 BLEED HOT CAUTION LIGHT REMAINS NORMALLY OFF. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (OVERTEMP) · airframe 31 hrs · 24 cycles

SEA FLIGHT NR 2393: NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED WHILE IN CRUISE AT 10,000. ACCOMPLISHED NR 1 BLEED HOT CAUTION CHECKLIST AND ASSOCIATED RAM VENTILATION CHECKLIST. NR 1 BLEED HOT CAUTION LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT AND ALL GROUND UPS. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED AIR OVERTEMP SWITCH IAW Q400 36-11-16, PAGES 401-504. FUNCTIONAL CHECK GOOD. FAULTS CLEARED AND DID NOT REOCCUR. AIRCRAFT RETURNED TO SERVICE.