N430QX

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 31,580 hrs · 33,798 cycles

ON APPROACH, WE GOT A FLAP POWER CAUTION IMMEDIATELY AFTER SELECTING FLAPS 5. FLAPS STOPPED AT ABOUT 1 DEGREE. WE WENT MISSED APPROACH AND RAN THE FLAP POWER CAUTION CHECKLIST, THE RESET PROCEDURE WAS UNSUCCESSFUL. WE DIVERTED .FLAP INDICATION REMAINED AT 1 DEGREE REGARDLESS OF SELECTED SETTING. LANDING UNEVENTFUL REMOVED FROM SERVICE. PERFORMED FIM TASK 27-50-00-810-802 STEP 1-3, FLAP POWER CAUTION DID NOT RETURN. NO FURTHER MAINTENANCE PROCEDURE IS NECESSARY. RETURNED TO SERVICE.

Part: RESERVOIR — FAULTED (HYD SYSTEM) · airframe 31,209 hrs · 33,240 cycles

ON TAKE OFF, LANDING GEAR WAS SLOW TO RETRACT MADE LOUD SQUEALING NOISE, SEQUENCING ON THE RETRACT WAS OFF, & THE ROLL SPOILER OUTBOARD CAUTION & #2 HYD ISO VALV CAUTION BOTH ILLUMINATED. AFTER THE GEAR WENT UP, BOTH LIGHTS EXTINGUISHED & EVERYTHING APPEARED NORMAL. ON ARRIVAL, GEAR WAS SELECTED DOWN, & THE EXACT SAME THING HAPPENED AGAIN. 3 GREEN WAS INDICATED ON THE MAIN GEAR SELECTOR, & A NORMAL LANDING WAS ACCOMPLISHED. REMOVED FROM SERVICE. REPLACED #2 HYD SYSTEM ISOLATION VALVE AND #2 HYD SYSTEM RESERVOIR. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: PRESSURE SWITCH — UNKNOWN (HYD SYSTEM) · airframe 30,993 hrs · 33,202 cycles

DURING TAKEOFF SEQUENCE WHEN GEAR HANDLE WAS SELECTED UP "#2 HYD ISO VLV"AND "ROLL SPOILER OUTBD HYD" CAUTION LIGHTS ILLUMINATED. AFTER GEAR FINISHED RETRACTING, ALL CAUTION LIGHTS EXTINGUISHED. RETURNED TO FIELD. WHEN GEAR WAS EXTENDED FOR LANDING "#2 HYD ISO VLV" CAUTION LIGHT AGAIN ILLUMINATED. GEAR LIGHTS WERE ALL RED FOR APPROX 8 SECONDS. AFTER LEVEL OFF ON MISSED APPROACH GEAR LIGHTS TURNED GREEN AND CAUTION LIGHT EXTINGUISHED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. VERIFIED HYDRAULIC QUANTITIES WITHIN LIMITS. GROUND RAN #2 ENG AND OPERATED ELEVATOR, RUDDER, AND SPOILERS SIMULTANEOUSLY. NO DEFECTS NOTED. R+R #2 HYD ISO VALVE PRESSURE SWITCH AS PRECAUTIONARY PER Q400 AMM 29-30-11-000-801 AND 29-30-11-400-801. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS PER Q400 AMM 32-31-00-710-801. HYDRAULIC MULE WAS OPERATED IN BOTH OPEN LOOP AS WELL AS CLOSED LOOP TO ISOLATE #2 HYD RESERVOIR. ALL GEAR SWINGS OPERATED NORMALLY. ACTUATED ALL APPLICABLE SYS 2 FLIGHT CONTROLS DURING GEAR SWINGS TO AID IN BLEEDING SYSTEM AS PRECAUTIONARY. FINAL QUANTITY DIFFERENTIAL BETWEEN PRESSURIZED AND UNPRESSURIZED WAS 5%. COULD NOT DUPLICATE #2 HYD ISO OR ROLL SPOILER OUTBD HYD CAUTION LIGHTS. NO FURTHER DEFECTS NOTED. OPERATIONAL CHECK FLIGHT GOOD. RETURNED TO SERVICE. .

Part: LAMP — INOPERATIVE (WARNING LIGHT) · airframe 30,845 hrs · 33,056 cycles

UPON ENTERING RUNWAY FOR TAKEOFF- FO NOTICED #2 ENG FUEL VALVE INOP. CANCELLED T/O CLEARANCE. RETESTED LAMPS W CAUTION ADVISORY TEST SWITCH. #2 ENG VALVE LAMP INOP. ABORTED TAKE OFF. REMOVED FROM SERVICE. RELAMPED #2 ENGINE FUEL VALVE OPEN LIGHT. LIGHT OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE.

Part: STRIP — UNSECURE (CABIN) · airframe 30,683 hrs · 32,897 cycles

FA REPORTS TRANSITION STRIP BY FORWARD JUMPSEAT LOOSE AND IS A TRIPPING HAZARD. REMOVED FROM SERVICE. REMOVED AND REPLACED ANTI-SKID TAPE ON FORWARD CENTER AISLE THRESHOLD STRIP. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 30,306 hrs · 32,517 cycles

AT THE VERY BEGINNING OF THE TAKE OFF ROLL #2 DC GEN CAUTION ILLUMINATED CHECKLIST DID NOT CORRECT ISSUE DC CAUTION REMAINS ILLUMINATED . TAKEOFF ABORTED. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 DC GCU PER Q400 AMM 24-31-06-000-801 AND 24-31-06-400-801. OPS CHECKED SYSTEM PER Q400 AMM 24-31-00-710-802. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: ANTI-SKID TAPE — PEELING (PAX DOOR) · airframe 29,989 hrs · 32,207 cycles

FA REPORTS ANTI-SLIP SURFACE AT TOP OF MAIN CABIN DOOR STAIRS IS PEELING UP, POSSIBLE TRIP HAZARD. REMOVED FROM SERVICE. SECURED NEW ANTI SLIP TAPE ON TOP MCD STAIR. NO FURTHER ACTION. RETURNED TO SERVICE.

Part: NONSKID — UNSECURE (AIRSTAIR) · airframe 29,733 hrs · 31,959 cycles

FLOOR GRIP TAPE ON TOP AIRSTAIR LOOSE TRIPPING HAZARD. REMOVED FROM SERVICE. RESECURED GRIP TAPE WITH NEW ONE IAW MCN 625743-01 ISSUE #2 NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 29,244 hrs · 31,445 cycles

EMERGENCY LIGHTS ILLUMINATE WITH EMERGENCY LIGHTS SWITCH IN "ARM" POSITION. REMOVED FROM SERVICE. FOUND CIRCUIT BREAKER "E3-EMERGENCY LIGHTS RELAY" OPEN. RESET CIRCUIT BREAKER, PER GPM 9.2.2.1. OPERATIONS TEST OF EMERGENCY LIGHTS GOOD, PER AMM 33-51-00-710-803. CIRCUIT BREAKER REMAINS CLOSED. RETURNED TO SERVICE.

Part: TRANSDUCER — INOPERATIVE (WHEEL SPEED) · airframe 29,021 hrs · 31,204 cycles

DURING LANDING ROLLOUT LEFT BRAKE CAME ON MUCH LATER THAN THE RIGHT BRAKE DID. BRAKE PEDDLE ON LEFT BRAKE NEEDED TO BE PUSHED FARTHER THAN THE RIGHT BRAKE FOR SAME EFFECT. REMOVED FROM SERVICE. REPLACEMENT OF THE NR 2 WHEEL SPEED TRANSDUCER AND FUNCTIONAL TEST. TESTED GOOD, REF Q400 AMM 32-46-00-720-802. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (LT FLAP POSITION) · airframe 28,914 hrs · 31,094 cycles

FLAP POWER CAUTION LIGHT CAME ON AFTER ENGINE START. RAN CHECK LIST IN RED BACK 8.28, TOOK OFF. AFTER FLAPS WERE RETRACTED AND INDICATOR READ ZERO THE FLAP POWER CAUTION CAME BACK ON, RETURNED TO FIELD AND DID A NO FLAP LANDING. REMOVED FROM SERVICE. REPLACED LEFT POSITION TRANSDUCER, FUNCTIONAL TEST GOOD. CAUTION AND FAULT DID NOT RETURN, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUIDE STOP — DAMAGED (DOOR) · airframe 28,818 hrs · 30,999 cycles

MCD STOP GUIDE (BUMPER) HAS A SMALL CRACK. REMOVED THE MCD STOP GUIDE REF Q400 AMM 52-11-11-000-801 STEP 3I INSTALLED A NEW FROM STOCK BUMPER REF Q400 AMM 52-11-11-400-801 STEP 4I. BUMPER REMAINS SERVICEABLE AFTER 10 CYCLES OF OPENING/CLOSING DOOR HANDLE.

Part: BUMPER — DAMAGED (PAX DOOR) · airframe 28,770 hrs · 30,947 cycles

MAIN CABIN DOOR HANDLE STOP GUIDE BUMPER DAMAGED, FOUND DURING PARKING. REMOVED AND REPLACED MCD DOOR HANDLE STOP GUIDE BUMPER WITH SERVICEABLE IAW AMM 52-11-11-000/400-801 AND MCN 6520839-01 ISS NR 1.

Part: SPRING — INOPERATIVE (EMER EQUIP DOOR) · airframe 28,311 hrs · 30,418 cycles

FWD FA EMERGENCY EQUIPMENT FLOOR DOOR SPRING INOP. REMOVED FROM SERVICE. REPLACED SPRINGS ON FWD FA EMERGENCY EQUIPMENT DOOR. SPRINGS OPERATE NORMALLY. RETURNED TO SERVICE.

Part: MANIFOLD — MALFUNCTIONED (NLG STEERING) · airframe 28,302 hrs · 30,406 cycles

AFTER CHECKLIST NOSE WHEEL CAUTION LIGHT CAME ON AFTER START NOSE WHEEL STEERING FAILED. RAN SPGRG 32-01-01 PER MAINT. STILL ILLUMINATED. WHEN TURNED ON, NOSE WHEEL COULD FEEL A THUD. REMOVED FROM SERVICE. REPLACED SCU, NWS MANIFOLD, & NWS HARNESS. OPS CHECKED GOOD. STEERING CAUTION EXTINGUISHED & DID NOT RETURN. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 28,130 hrs · 30,200 cycles

UPON ROLLING ONTO THE RUNWAY FOR TAKEOFF, "RA1 FAIL" WAS ANNUNCIATION ON THE ED. TAKEOFF ABORTED. REMOVED FROM SERVICE. SYSTEM PLACED ON MEL. CLEARED BY PERFORMING Q400 FIM 34-44-00-810-809. NO PRESENT FAULTS, PERFORMED RA1 TRANSCEIVER OPS TEST REF Q400 MTC 6344401. OPS TEST GOOD, NO FAULTS OR DEFECTS NOTED. A/C IS CAT III, COCKPIT PLACARD READS CAT III, MTX CTRL 46053 NOTIFIED, CLEAR MEL, PLACAREDS REMOVED, C/B PUSHED IN. RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 28,007 hrs · 30,062 cycles

FA EMERGENCY LIGHT SWITCH GUARD IS BROKEN. REMOVED FROM SERVICE. FOUND PIN DETACHED FROM RECEPTACLE FOR THE SWITCH GUARD @ FA EMERGENCY LIGHT SWITCH. RE SECURED PIN TO RECEPTACLE AS NEEDED NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BUMPER — MISSING (CABIN DOOR) · airframe 27,856 hrs · 29,885 cycles

MAIN CABIN DOOR OUTER HANDLE BUMPER STOP MISSING. REMOVED FROM SERVICE. REMOVED OLD BUMPER HARDWARE & INSTALLED NEW BUMPER FROM STOCK. REF -8 400 AMM TASKS 52-11-11-000/400-801. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNION — LEAKING (HYD SYSTRM) · airframe 27,826 hrs · 29,859 cycles

ENGINE #2 HYD PUMP FAILURE IN FLIGHT. DIVERTED. LANDING UNEVENTFUL. REPAIRED HYDRAULIC LEAK IN RIGHT WHEEL WELL. EDP PRESSURE LINE. NOTICED PITTING IN BULKHEAD FITTING IN WHERE LINE SEATS APPROX 20% OF THE WAY AROUND LOWER SIDE. REPLACED #2 ENGINE EDP PRESSURE RIGID LINE FORM NACELLE MID FRAME FLEX LINE CONNECTION TO AFT FIREWALL CONNECTION. REF MM TASK 29-00-00-400-802. PRESSURIZED LINE FROM EDP TO FILTER MANIFOLD WITH 3000 PSU FROM GHPU NO LEAKS NOTED. RETURNED TO SERVICE.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 27,613 hrs · 29,599 cycles

ROW 2DE EMERGENCY FLOOR PATH LIGHTING STRIP BROKEN. AIRCRAFT REMOVED FROM SERVICE. REPLACED PHOTOLUMINESCENT STRIP BY SEAT 2DE. NO OTHER DEFECT NOTED. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 27,209 hrs · 29,138 cycles

MULTIPLE NO AIII LIGHTS, CONFIGURATION CHECKED OUT AND LIGHTS RESOLVED THEMSELVES. AT MINS, APCH WARN ILLUMINATED. A/C AVIONICS WERE PROPERLY CONFIGURED. CONDUCTED MISSED APPROACH. LIMITATIONS DID NOT APPEAR TO HAVE BEEN EXCEEDED. ( HGS INOP-UNUSABLE ). PLACED ON MEL 32-30-2A. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,946 hrs · 28,849 cycles

FORWARD NR 1 LT AND RT BATTERY PACKS INOP. REMOVED AND REPLACED LT NR 1 AND RT NR 1 BATTERY PACKS IAW AMM 33-51-00-820-801. OPS TEST GOOD. NO FURTHER DEFECTS NOTED.

Part: BRAKE — SMOKE (MLG) · airframe 26,818 hrs · 28,710 cycles

DURING PREFLIGHT, NOTICED NR 1 BRAKE SMOKING. PERFORMED GVI OF MAIN LANDING GEAR WHEEL ASSY AND BRAKES IAW AMM TASK 32-40-00-210-802 AND TASK 32-40-00-210-803 NO DEFECTS NOTED. PERFORMED TASK 32-40-00-210-805 FOR BRAKE FUSE PLUGS NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SPLICE — DEFECTIVE (BLEED AIR SYS) · airframe 26,615 hrs · 28,477 cycles

AFTER TAKEOFF NR 1 BLEED HOT ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. SPLICES E2 AND E3 REPLACED AT ECS CONTROL BOX. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 26,401 hrs · 28,231 cycles

ON TAKE OFF THE MASTER WARNING LIGHT CAME ON , AND DOOR LIGHT ON PANEL WAS ON - ABORTED TAKE OFF AND RAN CHECK LIST FOR DOOR OPEN ON GROUND. TAKE OFF ABORT WAS 50 KTS AND NO EXCESSIVE BRAKING WAS USED. REMOVED FROM SERVICE. PERFORMED GVI OF ALL DOORS & FOUND AFT PAX DOOR HANDLE NOT FLUSH. PERFORMED OPERATIONAL TEST OF THE AFT PAX DOOR IAW AMM TASK 52-12-00-710-802. OPS TEST GOOD, DOOR HANDLE FLUSH. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SHUTOFF VALVE — UNKNOWN (NR 1 ENGINE) · airframe 26,365 hrs · 28,181 cycles

AT START OF TAKEOFF ROLL, THE NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. ABORTED THE TAKEOFF. REMOVED FROM SERVICE. INTERROGATED CDS & FOUND FAULT CODE 1203 L P2.2 SOV. CLEARED FAULT, PERFORMED OPS TEST OF BLEED AIR SYSTEM IAW AMM 36-11-00-710-802. FAULT DID NOT RETURN. AS A PRECAUTION, R & R THE NR 1 ENGINE P2.2 SHUTOFF VALVE IAW AMM 36-11-31-000/400-801. 83394 6/20/18, COMPLIED WITH FIM 36-10-00-810-869. FOUND CONNECTOR 2121-P3, WORN AND LOOSE. REMOVED AND REPLACED THE CONNECTOR IAW WM 20-17-24. AS A PRECAUTIONARY, REMOVED AND REPLACED THE LT BLEED AIR OVERTEMP SWITCH IAW AMM 36-11-16-000-801, AND 36-11-16-400-801. FAULT 1AO1 IN HISTORY. COMPLIED WITH OPS TEST OF THE BLEED AIR SYSTEM IAW AMM 36-11-00-710-802. TOOK POWER LEVERS UP TO TAKE-OFF POWER WITH BLEEDS ON. NO DEFECTS NOTED. NO CAUTION OR FAULTS RETURNED. AIRCRAFT RETURNED TO SERVICE.

Part: AXLE — CORRODED (MLG) · airframe 26,226 hrs · 28,028 cycles

NR 2 MLG AXLE HAS CORROSION AND PITTING DAMAGE EXCEED 0.005 INCHES ON NON-WEAR SURFACES. REPLACED THE AXLE IAW AMM 32-11-04-400-801.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED OVERHEAT) · airframe 26,225 hrs · 28,027 cycles

NR 1 BLEED HOT CAUTION ILLUMINATED APPROXIMATELY 1000 FEET AFTER TAKE-OFF WITH BLEED SELECTOR ON MIN. AFTER COMPLETING NR 1 BLEED HOT CAUTION CHECKLIST, THE NR 1 BLEED HOT CAUTION ILLUMINATED AGAIN DURING CRUISE FLIGHT, ABOUT 30 MINUTES AFTER BLEED SELECTOR ON NORM. REMOVED FROM SERVICE. COMPLIED WITH FIM 36-20-00-810-801, PARA 1-3 A, 1-4.A & PARA 5. NO BLEED HOT CAUTION AND NO FAULTS. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (NR 1 BLEED) · airframe 26,158 hrs · 27,954 cycles

NR 1 BLEED HOT CAUTION ILLUMINATED. COMPLIED WITH E/C. LIGHT LLUMINATED AGAIN. CDS SHOWS FAULT CODE LT BLEED OVERTEMP, STATUS MESSAGE IN FAULT HISTORY. COMPLIED WITH FIM 36-10-00-810-852. AIRCRAFT PASSED THE OPERATIONAL TEST OF THE BLEED AIR SYSTEM IAW AMM 36-11-00-710-802 AND NO FAULT CODES POSTED IN CDS. REMOVED AND REPLACED THE LT RTD SENSOR IAW AMM 36-11-16-000-802 AND 36-11-16-400-802, OPS CHECKED GOOD. NR 1 BLEED HOT CAUTION DID NOT ILLUMINATE. RETURNED TO SERVICE.

Part: BOOT — FAILED (LT DE ICE) · airframe 25,975 hrs · 27,161 cycles

LEFT DEICE BOOT 513AL BALLONED AND POPPED IN FLIGHT. CONFIRMED DAMAGE ON THE GROUND. REMOVED FROM SERVICE. R & R THE LT WING LE 513AL IAW AMM 57-23-01-000-801, AND 57-23-01-400-801. OPS TESTED GOOD. RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 25,972 hrs · 27,758 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE, DURING TEST, ROWS 2, 6, 10, 14, AND 18. REPLACED THE BATTERY PACKS.

Part: ENGINE — MALFUNCTIONED · airframe 25,860 hrs · 27,635 cycles

BOTH NR 1 AND 2 ENGINES OVERTORQUE AND OVERTEMP LIMITS. OUTSIDE OF LIMITS, BOTH ENGINE CHANGED.

Part: LIGHT — LOOSE (CABIN) · airframe 25,749 hrs · 27,531 cycles

EMERGENCY LIGHT STRIP AT ROW 2 IS LOOSE. RESECURED AS REQUIRED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROLLER — MALFUNCTIONED (PROPELLER) · airframe 25,751 hrs · 27,552 cycles

DURING TAKE OFF ROLL, NR 1 PROPELLER SPEED LOW AT 980-990 RPM. TAKE OFF ABORTED. REMOVED FROM SERVICE. RAN THE NR 1 ENGINE AT RATING, NOTED NP AT 950. RESTARTED AND RAN AT RATING. SAME RESULTS. R & R THE NR 1 PEC IAW AMM 61-20-36-000-801 AND 61-20-36-400-801. OPS TESTED GOOD IAW MTC 6710006. RAN THE NR 1 ENGINE AT RATING ON TWO SEPERATE STARTS. NP STABLE AT 1020. NO FAULTS IN CDS. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN FLOOR) · airframe 25,687 hrs · 27,456 cycles

FLOOR EMERGENCY LIGHT IN FWD GALLEY UNATACHED. SECURED THE LIGHT AND SEALED. NO OTHER DEFECTS NOTED. IAW 25-14-01-400-801 & MCN 625721-1 ISSUE 3. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — FALSE INDICATION · airframe 25,614 hrs · 27,377 cycles

AUTOFEATHER SELF TEST WILL NOT TEST. REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF THE PROPELLER AUTO FEATHER AND UP TRIM SYSTEM IAW AMM 61-20-00-710-801. OPS TESTED GOOD, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (DEICE BOOTS) · airframe 25,293 hrs · 27,054 cycles

ENROUTE, RECEIVED A DEICE PRESSURE CAUTION. CONDUCTED THE APPLICABLE CHECKLIST. THE CAUTION LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. PRESSURE REMAINED NORMAL. RETURN TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. NO FAULT NOTED IN CDS. GVI DEICING BOOTS. NO DEFECT NOTED. COMPLIED WITH A FUNCTIONAL TEST OF THE PNEUMATIC DEICING SYSTEM WITH ENGINE IAW AMM 30-11-00-710-807. FUNCTIONAL CHECKED GOOD. VISUALLY VERIFIED ALL BOOTS INFLATING. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (SERVICE DOOR) · airframe 24,566 hrs · 26,311 cycles

FUSELAGE DOOR WARNING FLICKERED THEN REMAINED STEADY AT FL210. DOOR WAS AFT SERVICE DOOR, RETURNED TO FIELD. NO ISSUES WITH PRESSURIZATION NOTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. UPON ARRIVAL, FOUND AFT HALF OF DOOR HANDLE NOT FULLY FLUSH ON AFT SERVICE DOOR. PERFORMED GVI OF AFT SERVICE DOOR AND HANDLE, NO DEFECTS NOTED, CLEANED AND LUBED EXTERNAL DOOR HANDLE, NO LONGER ABLE TO DUPLICATE AFT HALF OF DOOR HANDLE STICKING OUT. CONFIRMED THROUGH PSEU, FAULT HISTORY DID FLAG "ASDRLK" UNREASONABLE FAR. CONFIRMED INDUCTANCE VALUES WITHIN LIMITS, WHEN DOOR CLOSED AND LOCKED, REF Q400 AMM TASK 32-61-00-280-801. PERFORMED OPS TEST OF AFT SERVICE DOOR, PER AMM TASK 52-41-00-710-801, OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 23,889 hrs · 25,623 cycles

"ON" BACKLIGHTING OF EMERGENCY LIGHT SWITCH BY FWD FA SEAT WILL NOT REMAIN ILLUMINATED. REPLACED THE LAMP.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,781 hrs · 25,512 cycles

CLIMBING THROUGH 10,500 FT, RECEIVED A CABIN PRESSURE MASTER WARNING. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS, FOUND CPC FOR VALVE DATA FAIL AND CP CONTROLLER FAILED. REPLACED THE AFT OUTFLOW VALVE IAW AMM 21-31-16-000-8010, AND 21-31-16-400-801. FAULTS REMAINED IN CDS. UNABLE TO CLEAR FAULTS. PART DID NOT FIX DISCREPANCY. REPLACED CABIN PRESSURE CONTROLLER IAW AMM 21-31-06-000-801, AND 21-31-06-400-801. COMPLIED WITH A FUNCTIONAL TEST IAW AMM 21-31-00-720-801. FAULTS REMAINED CLEAR IN CDS AND DID NOT REOCCUR. COMPLIED WITH A PRESSURIZATION OF THE ACFT IAW AMM 21-00-00-863-801. TESTED GOOD. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 23,658 hrs · 25,381 cycles

PHOTO LUMINESCENT STRIP ON FLOOR IN FRONT OF ROW 1AB IS NOT ATTACHED TO THE FLOOR. REATTACHED LUMINESCENT STRIP TO THE FLOOR AS REQUIRED IN FRONT ROW 1AB AS REQUIRED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GLOWSTRIP — DETACHED (CABIN FLOOR) · airframe 23,600 hrs · 25,314 cycles

GLOW STRIP NEAR MAIN CABIN DOOR CAME OFF. SECURED GLOW STRIP WITH APPROPRIATE TAPE. RETURNED TO SERVICE.

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 23,437 hrs · 25,140 cycles

NR 2 HYD PUMP CAUTION INFLIGHT. NR 2 HYD QUANTITY INDICATION ZERO ESTIMATE 30 MIN OPERATING TIME W/O FLUID. EMERGENCY DECLARED AND CFR CALLED. PERFORMED ALTERNATE GEAR EXTENSION. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 2 MLG RETRACTION ACTUATOR EXT/ RET HOSES & NR 2 ENGINE DRIVEN PUMP. C/W GEAR SWINGS, OPS CHECKS,CHECKS GOOD. RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 23,061 hrs · 24,769 cycles

CHECK PFD 1 ON PFD, CHECK ED ON MFD, CHECK PFD 1 ON MFD, CHECK ED ON ED. CYCLED POWER OF NR 1 MFD BY SWITCH. ALL FAULTS CLEARED. C/W MFD1, PFD1, ED OP'S CHECK IAW MTC 6316101, 6316104. AMM TASK 31-61-01-710-803. C/W CAT III RTS TEST PER TASK MTC 6316101, 6316104. AIRCRAFT REMAINS CAT III. AIRCRAFT PLACARD READ CAT III. NO RELATED FAULT FOUND IN CDS. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: PROCESSOR — MALFUNCTIONED (ZONE 100) · airframe 22,842 hrs · 24,535 cycles

IOP2 FAIL ED MESSAGE & AVIONICS CAUTION MESSAGE. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERAGATED CDS AND FOUND " NO DATA FROM IOP2". REMOVED & REPLACED NR 2 IOP IAW MTC 6314101 FLT. RETURNED TO SERVICE.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 22,693 hrs · 24,373 cycles

"LIFT HERE" PLACARD IS MISSING FROM THE FORWARD EMERGENCY EXIT. REPLACED PLACARD AS REQUIRED. RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 22,528 hrs · 24,202 cycles

ON APPROACH WHEN FLAPS SELECTED TO 15 TO 35, THE FLAP POWER CAUTION ILLUMINATED AND THE FLAPS STUCK AT 15 DEGREES. LANDED AT 15 DEGREES FLAPS WITHOUT INCIDENT. REPLACED THE FLAP CONTROL UNIT IAW AMM 27-51-010-000-801/400-801. RETURNED TO SERVICE.

Part: ACTUATOR — BYPASSING (NLG LOCK) · airframe 22,438 hrs · 24,110 cycles

AT TAKE OFF WHEN GEAR HANDLE WAS SELECTED UP, THE NOSE GEAR YELLOW DOOR LIGHT AND RED NOSE LIGHT REMAINED ILLUMINATED. NON NORMAL VIBRATION AND NOISES WERE NOTED. INDICATED NOSE GEAR STILL DOWN. KEPT AIR SPEED BELOW 195K. RETURNED TO FIELD. NO AN OVERWEIGHT LANDING. NOT A HARD LANDING. ALTERNATE GEAR EXTENSION CHECK LIST WORKED FINE. VERY LITTLE PRESSURE WAS REQUIRED ON NOSE GEAR PULL HANDLE. REMOVED AND REPLACED NLG LOCK ACTUATOR. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 22,278 hrs · 23,942 cycles

NR 1 HYD ISO VALVE CAUTION, ROLL SPOILER INBD CAUTION, NR 1 HYD QTY 0. AFTER LANDING NR 1 ENGINE HYD PUMP CAUTION. AFTER INITIAL INVESTIGATION REPORTS NR 1 LT SIDE WHEEL WELL COVERED IN FLUID. PERFORMED GVI OF LT NACELLE AND LT GEAR WELL. ISOLATED FLUID LEAK TO LT GEAR WELL. NOT ABLE TO LOCATE LEAK VISUALLY. HYD PRESS NEEDS TO BE PRESENT TO FIND LEAK. FOUND LEAK FROM CHAFE ON NR 1 EDP PRESSURE LINE IN WHEEL WELL JUST BELOW ISOLATION VALVE, CASE DRAIN ADEL CLAMP BOLT HEAD RUBBING CAUSING DAMAGE. REPAIRED NR 1 EDP PRESSURE LINE IAW TASK 20-20-21-350-801 BY SPLICING IN NEW SECTION OF LINE USING PERMA SWAGE FITTINGS. OPS AND LEAK CHECKS GOOD. NO CAUTION LIGHTS ILLUMINATED DURING ENGINE RUNS. ALSO REPLACED THE ENGINE DRIVEN PUMP.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,205 hrs · 23,865 cycles

CLIMBING ENROUTE, FAULT ANNUNCIATOR ON PRESSURIZATION CONTROLLER ILLUMINATED. CYCLED DUMP, MANUAL, AND AUTO SELECTOR TO MANUAL AND BACK TO AUTO AFTER TWO SECONDS AS DIRECTED BY EMERGENCY CHECKLIST. FAULT ANNUNCIATOR ILLUMINATED ONCE AGAIN. CPC PANEL FAULT LIGHT NOT ILLUMINATED ON ARRIVAL. INTERROGATED CDS, FOUND NO FAULTS. CHECKED PIN 13 OF CABIN PRESSURE CONTROLLER CONNECTOR 2131-P1 FOR PROPER CONFIGURATION. CONNECTOR IS PROPERLY CONFIGURED. REMOVED & REPLACED AFT OUTFLOW VALVE IAW AMM 21-31-16-000-801 AND 21-31-16-400-801. FUNCTIONAL TEST OF PRESSURIZATION CONTROL IS GOOD. FAULT LIGHT REMAINED EXTINGUISHED. RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (BS 783) · airframe 22,124 hrs · 23,776 cycles

AFT CARGO FLOOR SUPPORT BS 783 - Y 9.25 HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 53-40-15 REPAIR -01 AND FOUND OUT OF LIMITS. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-42-05-02-01, DWG 85339601, REV D AND DWG:85339281 REV C.

Part: SHEAR WEB — CORRODED (BS 697) · airframe 22,124 hrs · 23,776 cycles

FOUND CORROSION ON AFT CARGO FLOOR SHEAR WEB AT BS 697.6, Y 25. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — DAMAGED (NOT REPORTED) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK 12 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, AND DWG 85328201 REV E.

Part: SEAT TRACK — DAMAGED (NOT REPORTED) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK 13 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-00-00, AND DWG:85361501 REV E.

Part: FRAME — CORRODED (BS 624) · airframe 22,124 hrs · 23,776 cycles

FOUND EVIDENCE OF CORROSION ON FRAME BETWEEN STRINGERS 31-32R, BS 624.5. REMOVED THE CORROSION IAW SRM 53-00-00-02-09. FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK DAMAGED. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05, 51-41-00, 51-40-15, AND SRM 51-40-07-02-01.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK DAMAGED. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-41-00, 51-42-05, AND 1-40-15.

Part: DOUBLER — CORRODED (ZONE 200) · airframe 22,124 hrs · 23,776 cycles

FOUND CORROSION ON MACHINE DOUBLER AT LAVATORY SERVICE DOOR. FOUND OUT OF LIMITS IAW SRM 52-42-10-02-01 FIG. 201. REPLACED THE DOUBLER IAW SRM 51-42-05-02-01.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK DAMAGED. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05-02-01 AND 51-40-15-02-01, 51-41-05-00-01. AND DWG 85328201 REV E.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 22,124 hrs · 23,776 cycles

FWD PAX DOOR THRESHOLD CORRODED ON UPPER SURFACE. REMOVED AND REPLACED THE THRESHOLD IAW SRM 51-42-05 REPAIR -01 PAR 4E. ITEMS 1 THR 8, AND DWG 85329531 , REV A.

Part: STIFFENER — DAMAGED (BULKHEAD) · airframe 22,124 hrs · 23,776 cycles

FOUND DAMAGED ON BEAM COMMON TO PILOT'S BULKHEAD AND SEAT TRACK 10. REMOVED BULKHEAD STIFFENER IAW SRM 51-42-05. LOCATED AND DRILLED IAW SRM 51-40-07 REPAIR -01. INSTALLED A NEW STIFFENER IAW 51-42-05 REPAIR 01. RESTORED FINISH IAW SRM 51-25-10 REPAIR -01 AND 51-25-15 REPAIR -01.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15 REPAIR -01, 51-42-05 REPAIR -01 AND 51-41-00 STRUCT INDENT -01. .

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK 11 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 REPAIR-01, 51-41-00 AND DWG 8532801 REV D.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00 STRUCT IDENT-01, SRM 51-42-05 REPAIR-01 SRM 51-40-07 REPAIR-01, AND SRM 51-40-07 REPAIR-01.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK 14 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 REPAIR-01, SRM 51-40-015 REPAIR-01 AND SRM 51-41-00.

Part: SEAT TRACK — DAMAGED (ZONE 100) · airframe 22,124 hrs · 23,776 cycles

SEAT TRACK 15 DAMAGED. REMOVED & REPLACED SEAT TRACK IAW SRM 51-42-05 REPAIR -01, SRM 51-40-15 REPAIR -01 & SRM 51-41-00.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,077 hrs · 23,730 cycles

AUTOFEATHER TEST FAILED. INTERROGATED CDS, FOUND FAULTS 30 AND 901 ON NR 1 ENGINE AND 456 CHA AND B NR 2 ENGINE. CLEARED FAULTS, FAULT 30 REMAINED ON NR 1 ENGINE. R & R NR 1 FADEC IAW AMM TASKS 73-21-01-000-801 AND 73-21-01-400-801, ALL FAULTS CLEARED. PERFORMED OPS TEST OF AUTOFEATHER AND UPTRIM SYS IAW AMM TASK 61-20-00-710-801. OPS TEST GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (PROPELLER) · airframe 22,023 hrs · 23,666 cycles

BEFORE TAKEOFF THE NR 1 ENGINE FEATHERED, FOLLOWED BY A POWERPLANT MESSAGE. REPLACED THE NR 1 ENGINE PEC IAW AMM 61-20-36-000-801 AND 61-20-36-400-801. PRIOR TO REMOVAL, FOUND FAULT CODES 270, 402, 338 ON CHANNEL A. CLEARED ALL FAULT CODES. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (SWITCH) · airframe 22,013 hrs · 23,656 cycles

EMERGENCY LIGHT PANEL AT FORWARD F/A STATION HAS BURNED OUT LIGHT. REPLACED THE LAMP IN THE SWITCH. TESTED GOOD. RETURNED TO SERVICE.

Part: ANTENNA — MALFUNCTIONED (VHF SYS) · airframe 21,928 hrs · 23,570 cycles

NR 1 COMM UNUSEABLE ON 126.6 MHZ. NR 2 OK ON 126.6. RETURNED TO FIELD, LANDING UNEVENTFUL. REPLACED NR 1 VHF COMM ANTENNA IAW AMM 23-11-26. CHECKS GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,560 hrs · 23,163 cycles

AFT LT EMERGENCY LIGHT INOPERATIVE, SHARK LIGHT. REPLACED THE LAMP IAW AMM 33-51-11-00-801 AND 33-51-11-400-801. CHECKS GOOD. RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,560 hrs · 23,163 cycles

EMERGENCY LIGHTS FAILED OPS CHECK IAW SCHEDULED TASK CARD 335000202-60045. REPLACED ALL 8 POWER SUPPLIES IAW AMM 33-51-00-400-801 AND 33-51-01-000-801. OPS CHECK GOOD.

Part: FADEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 21,094 hrs · 22,651 cycles

UPTRIM MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AT ABOUT 70 KNOTS. PERFORMED EMU DOWNLOAD IAW MAINTENANCE 6773101. INTEROGATED CDS AND FOUND FAULT CODE 771A IAW MAINTENANCE CONTINUED. CHANGED FADEC ON NR 2 ENGINE IAW AMM 73-21-01-000-801 AND 73-21-01-400-801. OPS CK GOOD IAW AMM 71-00-00-868-805 AND 61-20-00-710-801. RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (PARK BRAKE) · airframe 20,671 hrs · 22,191 cycles

T/O WARNING TEST ACCOMPLISHED ON TAXI OUT WAS OK. WHILE HOLDING SHORT OF THE RUNWAY WITH PARK BRAKE ON, CLEARED FOR TAKEOFF PARK BRAKE WAS RELEASED WHILE ROLLING ONTO THE RUNWAY, PARK BRAKE CAUTION, ILLUMINATED THEN WHEN OUT. TAKEOFF WARNING TEST ACCOMPLISHED AND IT FAILED. R & R PARKING BRAKE CONTROL QUADRANT, REF AMM TASK 32-44-21-000-801, 32-44-21-400-801. FUNCTIONAL TEST GOOD. C/W OPS TEST OF THE TAKE OFF WARNING SYSTEM REF AMM TASK 31-52-00-710-801. OPS TEST GOOD, NO OTHER DEFECT NOTED.

Part: WARNING HORN — FALSE ACTIVATION (PARKING BRAKE) · airframe 20,225 hrs · 21,708 cycles

ON INITIAL TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED WITH THE PARK BRAKE OFF, THE PARK BRAKE CAUTION LIGHT WAS ILLUMINATED. THE TAKEOFF WAS ABORTED UNDER 20 KTS. RETURNED TO GATE. PERFORMED OPS TEST OF THE TAKEOFF WARNING SYSTEM. SYSTEM OPERATES NORMALLY AT THIS TIME WITH NO DEFECTS NOTED. AFTER TALKING WITH THE CAPTAIN IT WAS DETERMINED THE PARKING BRAKE WAS RELEASED TO LIGHTLY UPON POWERING UP FOR TAKEOFF NOT ALLOWING THE CAUTION LIGHT SUFFICIENT TIME TO EXTINGUISH CAUSING THE WARNING HORN TO SOUND. PARKING BRAKE OPERATIONALLY CHECKED GOOD AND WAS ABLE TO DUPLICATE THE REPORTED HORN BY LIGHTLY RELEASING THE BRAKE AND NOT WAITING FOR LIGHT TO EXTINGUISH BEFORE ADVANCING THROTTLES. ALL SYSTEMS FUNCTION NORMALLY IAW AMM TASK 31-52-00-710-801. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SWITCH — INOPERATIVE (NR 2 BYPASS) · airframe 19,949 hrs · 21,418 cycles

NR 2 ENGINE INTAKE BYPASS DOOR SWITCH INOPERATIVE. RETURNED TO FIELD DUE TO POTENTIAL ICING ENROUTE. LANDING UNEVENTFUL. REPLACED SWITCH. RETURNED TO SERVICE.

Part: TRACK — LOOSE (DITCHING DAM) · airframe 19,449 hrs · 20,895 cycles

DITCHING DAM LOCK ON THE LOWER PART OF THE TRACK IS LOOSE. FOUND DITCHING DAM HANDLE COVER OPEN. CLOSED THE COVER. OPS CHECK IAW AMM 25-62-02-710-802, CHECKS GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,433 hrs · 20,879 cycles

F/A REPORTS THAT THE F/A PANEL EMERGENCY LIGHTS SWITCH, GREEN IS NOT ILLUMINATED. REPLACED THE LAMP. OPERATES NORMALLY. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,309 hrs · 20,752 cycles

BOTH F/A REPORTED SMOKE ODOR BRIEFLY AFTER TAKEOFF AND AGAIN ON LANDING. NO VISIBLE SMOKE. C/W FIM TASK 21-20-00, MCN 62172-01, PERFORMED ENGINE RUNS WITH BOTH ENGINES AND PERFORMED ECS TEST OF AC, HEAT SYS. NO ABNORMAL ODORS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: SEAL — FAILED (PROP PISTON) · airframe 18,883 hrs · 20,291 cycles

NR 2 PROPELLER TOOK 43 SECONDS TO UNFEATHER AFTER ENGINE START. REPLACED NR 2 PROPELLER PISTION SEAL AS THE LAST ACTION. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,812 hrs · 20,213 cycles

THE EMERGENCY LIGHTS FAIL TASK 33-51-00-710-803. THEY FLICKER WHEN ILLUMINATED. R & R NR 3 EMERGENCY LIGHTS POWER SUPPLY IAW AMM TASKS 33-51-01-000-801 & 33-51-01-400-801. R & R LT & RT BATTERIES IN NR 3 POWER SUPPLY IAW AMM TASK 33-51-00-820-801. COMPLIED WITH OPS CHECK OF THE EMERGENCY LIGHT SYSTEM IAW AMM TASK 33-51-00-710-803. OPS CHECKS GOOD.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 18,812 hrs · 20,212 cycles

NR 2 ENGINE TAKES LONGER THAN NORMAL TIME TO COME OUT OF FEATHER WITH POWER LEVERS AT FLIGHT IDLE. IAW MAINTENANCE REQUEST, R & R NR 2 OSG AS PRECAUTIONARY MEASURE WITH NEW FROM STOCK IAW AMM 61-20-26-400-801 AND 61-20-26-000-801. OPS CHECK GOOD. DURING INSTALLATION, REF HS 61-0038 FOR HEAT SHRINK. PERFOMRED FUNCTIONAL TEST OF PROP TIME TO UNFEATHER IAW AMM 61-20-00-720-801. UNFEATHER TIME WITHIN LIMITS. PERFORMED ENGINE LEAK CHECK IAW AMM 71-00-00-790-801, LEAK CHECK GOOD. RETURNED TO SERVICE.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 18,729 hrs · 20,121 cycles

MASTER WARNING CABIN PRESSURE, RAN CHECKLIST AS APPROPRIATE, DECENDED TO 10,000 FT. MANUAL PRESSURIZATION CONTROLLED CABIN. NO RAPID DECOMPRESSION AND NO FUSELAGE DOOR WARNING LIGHT. LANDING UNEVENTFUL. NO FAULTS FOUND IN CDS. FOUND LOOSE AND DAMAGED SEAL ON AFT BAGGAGE DOOR. R & R AFT BAGGAGE DOOR SEAL IAW AMM 52-31-26-000-801 AND 52-31-26-400-801. OPS CHECKS GOOD. C/W FIM 21-30-00-810-801 AND PERFORMED FUNCTION TEST OF THE PRESSURE CONTROL SYSTEM IAW AMM 21-31-00-720-801. TEST PASS. "CABIN PRESS" DID NOT ILLUMINATE. NO FAULTS IN CDS. LEAK CHECK OF AFT BAGGAGE DOOR SEAL GOOD. PRESSURIZED ACFT IAW AMM 21-00-00-863-801 AND 21-00-00-863-802. ACFT HELD PRESSURE. LEAK CHECK GOOD ON AFT BAGGAGE DOOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,636 hrs · 20,022 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY FLOOD LIGHT IS INOPERATIVE. REPLACED THE LAMP.

Part: WARNING MESSAGE — FALSE ACTIVATION (PROP DE ICE) · airframe 18,403 hrs · 19,777 cycles

PROPELLER DE-ICE CAUTION ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. ACCOMPLISHED RESET PROCEDURE IAW FSM PROPELLER DEICE RESET PROCEDURE. PROPELLER DE-ICE CAUTION EXTINGUISHED. RETURNED TO SERVICE.

Part: HF COMM — MALFUNCTIONED · airframe 17,995 hrs · 19,358 cycles

UNABLE TO HEAR ON COMM 1 & 2 WHILE FLYING IN PRECIPITATION. RETURNED TO FIELD. LANDING UNEVENTFUL. C/W TROUBLESHOOTING IAW WHILE DOING BONDING CHECK OF RADOME FOUND VALUES HIGH AT TEST POINT TP51 AND TP57 WHILE REMOVING RADOME NOTICED HARDWARE AT TP51 AND 57 LOOSE. CLEANED RADOME DIVERTER STRIPS MOUNTING PADS AND REINSTALLED RADOME IAW AMM 53-12-01-400-801, C/W BONDING CHECK IAW SRM 51-80-00-02-02 AND TEST POINTS WITHIN VALUES. C/W VISUAL INSPECTION OF BONDING STRAPS AND STATIC DISCHARGERS WITH NO DEFECTS NOTED. C/W OPS CHECK OF VHF COM 1 AND 2 IAW AMM 23-11-00-710-801. OPS CHECK GOOD AND OK FOR RETURN TO SERVICE.

Part: SWITCH — MALFUNCTIONED (OVERTEMP) · airframe 17,448 hrs · 18,780 cycles

NR 1 BLEED, HOT CAUTION MESSAGE DURING CLIMBOUT. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. FOUND ECS FAULT HISTORY NR 1 ENGINE 1A01. LT BLEED TEMP AND 7001 LT BLEED OVERTEMP. R & R NR 1 ENGINE BLEED OVERTEMP SWITCH IAW AMM TASK 36-11-16-000-801 AND 36-11-16-400-801. OPS CHECKED GOOD. COMPLIED WITH OPS TEST OF THE BLEED AIR SYS REF AMM TASK 36-11-00-710-802. OPS TESTED GOOD. NR 1 BLEED HOT CAUTION REMAINED EXTINGUISHED. RETURNED TO SERVICE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 17,202 hrs · 18,512 cycles

FORWARD LT AND RT EMERGENCY LIGHT POWER SUPPLIES FAILED DURING OPERATIONAL TEST. REPLACED POWER SUPPLY UNIT IAW AMM 33-51-01.

Part: GEARBOX — LEAKING (NR 2 ENGINE) · airframe 16,968 hrs · 18,260 cycles

NR 2 ENGINE WOULD NOT UNFEATHER AFTER START. INTERROGATED CDS NO CODES FOUND IAW AMM 61-20-00-710-804. R & R OSG IAW AMM 61-20-26-000/400-801 NO HELP. LEAKAGE NOTED AT OSG. REMOVED OSG IAW AMM 61-20-26-00-801. REINSPECTED AND CLEANED SURFACE NO OBSTRUCTION FOUND. INSTALLED OSG IAW AMM 61-20-26-400-801 NO HELP LEAK PERSISTS. CHECKED HUB GREASE LEVEL IAW AMM 61-10-640-501 LEVEL GOOD. REPLACED OSG AGAIN IAW AMM 61-20-26-000/400-801 OPS CHECKED GOOD, LEAK STILL PRESENT. CLEANED ALL REMAINING COATING OFF RGB PRIOR TO INSTALLATION DID NOT HELP LEAK. OPEN.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 16,393 hrs · 17,637 cycles

SEAT TRACK 10 FOUND CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 16,393 hrs · 17,637 cycles

CORROSION FOUND BELOW AFT PAX DOOR HINGE TUBE AFT BAY IN FOUR PLACES. BLENDED AFFECTED AREA IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-02-01. EDDY CURRENT INSPECTION FOR SURFACE CRACKS PERFORMED IAW NTM PART 6-51-00-02. NO CRACKS NOTED.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 16,393 hrs · 17,637 cycles

PASSENGER DOOR LOWER THRESHOLD PLATE CORRODED. REMOVED THRESHOLD PLATE IAW SRM 51-42-45-02-01 & 51-42-05-02-01. 1. INSTALLED NEW THRESHOLD IAW SRM 51-42-05-02-01. APPLIED PRIMER AS REQUIRED IAW SRM 51-42-05-02-01 AND 51-25-10-02-01.

Part: WEB — CORRODED (CARGO BAY) · airframe 16,393 hrs · 17,637 cycles

AFT CARGO BAY SHEAR WEB UNDER PANEL 144HZ HAS CORROSION. BLENDED WEB IAW SRM 53-40-43-02-01. PERFORMED ULTRASONIC THICKNESS INSPECTION IAW NTM PART 4 51-00-02 AND FOUND TO BE WITHIN LIMTIS IAW SRM 53-40-43-02-01.

Part: WEB — CORRODED (CARGO BAY) · airframe 16,393 hrs · 17,637 cycles

AFT CARGO BAY FLOOR WEB CORRODED. BLENDED IAW SRM 53-40-43-02-01. PERFORMED FPI OF BLENDED AREA IAW NDTM 51-00-01, NO DEFECTS NOTED. BLENDS FOUND TO BE WITHIN LIMITS IAW SRM 53-40-43-02-01. PERFORMED ECI ON BLENDED AREA, NO CRACKS FOUND AT THIS TIME IAW NDTM PART 6 51-00-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 16,393 hrs · 17,637 cycles

CORROSION FOUND UNDER FWD PAX DOOR LOWER AFT CORNER FITTING. BLENDED AFFECTED AREA IAW SRM 53-00-00-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-02-01. EDDY CURRENT INSPECTION FOR SURFACE CRACKS PERFORMED IAW NTM PART 6 51-00-02. NO CRACKS NOTED.

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · airframe 16,393 hrs · 17,637 cycles

FWD PAX DOOR SUPPORT ANGLE AFT OF MACHINED WEB IS CORRODED. REMOVED ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. DRILLED UP NEW ANGLE IAW SRM 51-40-07-02-01. INSTALLED NEW ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. PRIMED RIVETS IAW SRM 51-42-05-02-01. NO FURTHER ACTION REQUIRED.

Part: THRESHOLD — CORRODED · airframe 16,393 hrs · 17,637 cycles

THRESHOLD MEMBER CORRODED BEYOND LIMITS. REMOVED THRESHOLD MEMBER IAW SRM 51-42-45-02-01 AND 51-42-05-02-01. INSTALLED NEW THRESHOLD IAW SRM 51-42-05-02-01.

Part: BRACKET — CORRODED · airframe 16,393 hrs · 17,637 cycles

BRACKET CORRODED INBD HINGE SHAFT FWD OF MACHINED WEB. REMOVED ANGLE IAW SRM 51-42-05-02-01. DRILLED NEW BRACKET IAW SRM 51-40-07-02-01. INSTALLED BRACKET IAW SRM 51-42-05-02-01.

Part: SKIN — CORRODED · airframe 16,393 hrs · 17,637 cycles

WING PANEL 524FT HAS SEVERAL AREAS OF SUSPECTED CORROSION. BLENDED OUT CORROSION IAW SRM 51-20-00-00-02. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-35-02-02.

Part: SUPPORT BRACKET — CORRODED (DOOR HINGE) · airframe 16,393 hrs · 17,637 cycles

CORROSION FOUND UNDER THE FWD PAX DOOR HINGE SHAFT ON A SUPPORT BRACKET BS 26.900 JUST FWD OF THE MACHINED WEB. REMOVED BRACKET IAW SRM 51-42-05-02-01. DRILLED NEW BRACKET IAW SRM 51-40-07-02-01. INSTALLED NEW BRACKET IAW SRM 51-42-05-02-01 AND 51-42-45-02-01.

Part: SUPPORT BRACKET — CORRODED (PAX DOOR HINGE) · airframe 16,393 hrs · 17,637 cycles

CORROSION FOUND UNDER THE FWD PAX DOOR HINGE SHAFT ON A SUPPORT BRACKET STA 26.400 JUST AFT OF AFT MACHINED WEB. REMOVED LOWER ANGLE JUST AFT OF AFT MACHINED WEB BECAUSE OF EXCESSIVE CORROSION IAW SRM 51-42-05-02-01. DRILLED UP BRACKET IAW SRM 51-40-07-02-01. INSTALLED NEW BRACKET IAW SRM 51-42-05-02-01. PRIMED RIVETS IAW SRM 51-42-05-02-01. NO FURTHER ACTION REQUIRED.

Part: BEAM — CORRODED (DOOR SILL) · airframe 16,393 hrs · 17,637 cycles

FOUND LOWER SILL BEAM AT EMERGENCY EXIT CORRODED. REMOVED SILL BEAM IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. INSTALLED SILL BEAM IAW SRM 51-42-05-02-01 AND 51-42-45-02-01.

Part: PANEL — CORRODED (WING) · airframe 16,393 hrs · 17,637 cycles

WING SKIN MATING SURFACE UNDER PANEL 524CT HAS SEVERAL AREAS OF CORROSION. BLENDED CORROSION IAW SRM 57-20-35-02-02. PERFORMED ECI ON BLENDED AREAS. NO CRACKS FOUND IAW NDTM PART 6 51-00-01.

Part: CHANNEL — CORRODED (THRESHOLD) · airframe 16,393 hrs · 17,637 cycles

FWD PAX DOOR THRESHOLD CHANNEL CORRODED BEYOND LIMITS. REMOVED THRESHOLD CHANNEL IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. DRILLED NEW CHANNEL IAW SRM 51-40-07-02-01. INSTALLED CHANNEL IAW SRM 51-42-05-02-01.

Part: ANGLE — CORRODED · airframe 16,393 hrs · 17,637 cycles

AFT CARGO FLOOR SHEAR WEB ANGLE HAS SUSPECTED CORROSION. BLENDED ANGLE IAW SRM 53-40-15-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-02-01. BLENDED AREA ALODINED IAW SRM 51-21-10-02-01, PRIMED IAW SRM 51-25-10-02-01 AND PAINTED IAW SRM 51-25-15-02-01. PERFORMED ECI ON ANGLE. NO CRACKS FOUND IAW NDTM PN 6 51-00-01.

Part: FLOOR SUPPORT — CORRODED · airframe 16,393 hrs · 17,637 cycles

CORROSION ON FLOOR SUPPORT ANGLE. REPLACED FLOOR SUPPORT ANGLE IAW SRM 53-40-43-02-01.

Part: SEAT TRACK — CORRODED (BS 211) · airframe 16,393 hrs · 17,637 cycles

RT OTBD SEAT TRACK CORRODED AT BS 211. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREA IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 241-396) · airframe 16,393 hrs · 17,637 cycles

LT OTBD SEAT TRACK HAS CORROSION AT BS 241, 255, 272, 303, 318 AND 396. BLENDED CORROSION AT IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (NR 16) · airframe 16,393 hrs · 17,637 cycles

SEAT TRACK NR 16 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 16,393 hrs · 17,637 cycles

SEAT TRACK NR 11 FOUND TO BE CORRODED BEYOND LIMITS. REMOVED NR 11 SEAT TRACK IAW SRM 51-41-00-00-01, 51-42-05-02-01 AND 51-40-15-02-01. DRILLED NEW FASTENER HOLES IN NEW TRACK PN 85328210-115, DEBURRED AND COUNTERSUNK AS NECESSARY. ALL WORK DONE IAW SRM 51-40-07-02-01 AND 51-40-05-00-01. INSTALLED BOLTS FOR SEAT TRACK NR 11 IAW SRM 51-41-00-00-01. INSTALLED SOLID RIVETS AT AFT SERVICE SPLICE IAW SRM 51-42-05-02-01. INSTALLED HI-LITES AND SOLID RIVETS AT AFT SEAT TRACK SPLICE AND CENTER SECTION IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. INSTALLED SOLID RIVETS FWD SPLICE SECTION OF NR 11 SEAT TEACK IAW SRM 51-42-05-02-01. INSTALLED FWD SPLICE SECTION OF SEAT TRACK NR 11 IAW SRM 51-40-15-02-01. LOCK FASTENER INSTALLATION ACCOMPLISHED IAW SRM 51-40-15-02-01, TR 51-020. APPLIED PRIMER TO NECESSARY FASTENERS IAW SRM 51-25-10-02-01. APPLIED TOPCOAT TO NECESSARY FASTENERS IAW SRM 51-25-15-02-01. APPLIED SELF LEVELING GREEN SEALANT TO SEAT TRACK NR 11 FROM FORWARD END OF TRACK NR 11 TO FS X83.00 IAW AMM 53-23-01-400-801 HS 53-0003.

Part: SEAT TRACK — CORRODED (BS 578-656) · airframe 16,393 hrs · 17,637 cycles

LEFT INBD SEAT TRACK CORRODED AT BS 578-656. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMTIS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION OF ABOVE AREAS IAW NTM PART 6, 51-00-02. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 16,393 hrs · 17,637 cycles

SEAT TRACK NR 11 FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-00-00-01, 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (NR 16) · airframe 16,393 hrs · 17,637 cycles

SEAT TRACK NR 16 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED NR 16 SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND AMM 20-10-01-430-801.

Part: TRAY — CORRODED (E/E BAY) · airframe 16,393 hrs · 17,367 cycles

CORROSION ON AVIONICS TRAYS AND BOLTS AT BS 19.4 ABOVE STR 33. REMOVED AND REPLACED CORRODED SCREWS AND WASHERS IAW SRM 51-41-00-00-01. CLEANED AVIONICS TRAYS OF CORROSION IAW SRM 51-21-00-00-02. NO CORROSION DAMAGE NOTED.

Part: SEAT TRACK — CORRODED (BS 272 - 549) · airframe 16,393 hrs · 17,637 cycles

LEFT INBD SEAT TRACK CORRODED BS 272 - 549. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 589) · airframe 16,393 hrs · 17,637 cycles

RIGHT INBD SEAT TRACK CORRODED AT BS 589. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 148) · airframe 16,393 hrs · 17,637 cycles

LT OTBD SEAT TRACK CORRODEDA T BS 148. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-40-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 179) · airframe 16,393 hrs · 17,637 cycles

LEFT INBD SEAT TRACK CORRODED AT BS 179. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 216) · airframe 16,393 hrs · 17,637 cycles

RIGHT INBD SEAT TRACK CORRODED AT BS 216. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE FREEDOM OF MOVEMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 620) · airframe 16,393 hrs · 17,637 cycles

RT INBD SEAT TRACK CORRODED AT BS 620. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 722.102) · airframe 16,393 hrs · 17,637 cycles

CORROSION FOUND ON LT SEAT TRACK AT Y9.25, BS 722.102. BLENDED CORROSION IAW SRM 53-40-49-02-02 AND 53-40-49-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-40-49-02-01 AND 53-40-49-02-02. ALODINED BLENDED AREA IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 247-372) · airframe 16,393 hrs · 17,637 cycles

RIGHT OTBD SEAT TRACK CORRODED BS 247,279 & 372. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-40-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREA IAW SRM 51-21-10-02-01.

Part: SEAT TRACK — CORRODED (BS 371 AND 557) · airframe 16,393 hrs · 17,637 cycles

RIGHT INBD SEAT TRACK CORRODED AT BS 371 AND 557. 1. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREA IAW SRM 51-21-10-02-01.

Part: PANEL — CORRODED (WING) · airframe 16,393 hrs · 17,637 cycles

PANEL 624AT HAS CORROSION ON MATING SURFACE. BLENDED OUT DAMAGED AREA IAW SRM 57-20-35-01-01 BETWEEN STA YW237.399 AND YW201.069. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-35-01-01. PERFORMED ECI ON BLENDED AREA. NO CRACKS FOUND IAW NDTM PART 6 51-00-01.

Part: PIVOT ASSY — CORRODED (CARGO DOOR) · airframe 16,393 hrs · 17,637 cycles

FWD BAGGAGE DOOR PIVOT ASSY HAS SIGNS OF CORROSION. CLEANED AND INSPECTED FORWARD BAGGAGE PIVOT ASSY IAW SRM 51-26-00-02-01. FOUND CORRODED AND SEIZED BEARING. PIVOT ASSY HAD NO FURTHER EVIDENCE OF CORROSION. NEW BEARING ON ORDER. R & R SEIZED BEARING LOCATED ON FWD BAGGAGE DOOR PIVOT ASSY IAW CMM 52-12-06. PROOF LOAD TEST STILL REQUIRED. BEARING FAILED PROOF LOAD TEST IAW SRM 51-22-40-51-0002. REMOVED AND CLEANED AND REINSTALLED BEARING IAW CMM 52-12-06. PROOF LOADING STILL REQUIRED. PERFORMED PROOF LOAD IAW SRM 51-22-40 HS 51-0002 AND IAW 52-12-06-3-C, 10 THRU 3, C, 12. PROOF TEST PASSED.

Part: SWITCH — BROKEN (EMERGENCY LIGHT) · airframe 15,875 hrs · 17,095 cycles

FORWARD EMERGENCY LIGHTING SWITCH DOES NOT ILLUMINATE. REPLACED THE SWITCH. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: DISPLAY — INOPERATIVE (ZONE 200) · airframe 15,611 hrs · 16,793 cycles

PFT BLANKED OUT SHOWED "T" AND STAYED OFF FOR APPROX THREE MINUTES "PFD MON 1 FAIL" MESSAGE ON ED. DISPLAY RETURNED TO NORMAL AFTER ABOUT 3-4 MIN. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 PFD IAW MX 6316104 AS PRECAUTIONARY MEASURE. CLEANED PFD FILTER. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 15,383 hrs · 16,562 cycles

AUTOFEATHER SELECT BUTTON WILL NOT TEST WITH THE CAUTION ADVISORY TEST. PERFORMED GVI AND FOUND C/B F3 POPPED,"CAUTION ADV." NO HISTORY OF CIRCUIT BREAKER F3 WAS FOUND WITHIN THE LAST 14 DAYS. RESET CIRCUIT BREAKER IAW GPM 9.2.2 LAMP CHECKED GOOD. AUTOFEATHER TEST GOOD. NO OTHER DEFECTS NOTED. CIRCUIT BREAKER REMAINS SET. RETURNED TO SERVICE.

Part: HANDLE — OUT OF ADJUST (SERVICE DOOR) · airframe 15,376 hrs · 16,555 cycles

FOUND AFT SERVICE DOOR EXTERIOR HANDLE NOT RESTING IN THE DOOR CUT OUT WHEN THE DOOR IS CLOSED AND LOCKED FROM INSIDE THE ACFT. REMOVED THE LINER IAW AMM 25-26-26-000-801. ADJUSTED HANDLE OPEN STOP.

Part: STOP — WORN (EMEGENCY EXIT) · airframe 13,863 hrs · 14,978 cycles

DURING THE OPENING OF THE FORWARD EMERGENCY TYPE II EXIT, THE LOWER DOOR WAS UNABLE TO BE LOCKED TO THE WATER LANDING (DITCHING) POSITION. FOUND STOP TO BE WORN ON DOOR. REPLACED EXIT STOP IAW SRM 51-42-05.

Part: SWITCH — DIRTY (POWER LEVER) · airframe 13,216 hrs · 14,330 cycles

ON LANDING THE GROUND SPOILERS FAILED TO DEPLOY. FLIGHT/TAXI SWITCH WILL NOT REMAIN IN THE TAXI POSITION. CLEANED NR 1 & NR 2 POWER LEVER 12 DEGREE SWITCHES IN POWER LEVER MODULE IAW CMM 76-10-01 PG 401 & 402. PERFORMED FUNCTIONAL TEST OF THE GROUND SPOILER SYS IAW AMM TASK 27-62-00-720-801. FUNCTIONAL TESTED GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,857 hrs · 13,969 cycles

EMERGENCY LIGHT SWITCH ON, FORWARD F/A CONTROL PANEL IS NOT ILLUMINATING. RELAMPED, OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (ZONE 200) · airframe 12,675 hrs · 13,773 cycles

THE EMERGENCY FLOOR PATH LIGHTING DISCOLORED IN FRONT OF THE BAGGAGE DOOR (FWD) AND ALSO IN FRONT OF ROW 1. REPLACED AS REQUIRED IAW TC 6-33-70.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 12,556 hrs · 13,651 cycles

ENROUTE AT 25,000 FT, THERE WAS A LOUD SQUEAL FROM THE TYPE II/III EXIT DOOR ON THE FO'S SIDE. RETURNED TO FIELD, LANDING UNEVENTFUL. R & R RT FWD LOWER EMERGENCY EXIT DOOR SEAL IAW MM TASK 52-23-06-000-801 AND TASK 52-23-06-400-801. PRESSURIZATION LEAK CHECKED GOOD. NO LEAKS OR NOISE DETECTED. RETURNED TO SERVICE.

Part: STOP — WORN (PAX DOOR) · airframe 12,204 hrs · 13,255 cycles

MAIN CABIN DOOR HANDLE IS HARD TO UNLOCK FROM INSIDE. COMPLIED WITH FUNCTION CHECK OF DOOR, FOUND FORCE TO UNLOCK EXCEEDS 60 LBS; REPLACED NR 5 STOP PIN FOR WEAR, ADJUSTED DOOR STOP BOLTS, STOP GUIDES, & DOWN LIMIT STOP IAW AMM PRESSURIZATION, RUN, LEAK CHECKED GOOD, DOOR FUNCTIONAL CHECKED GOOD. RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 12,009 hrs · 13,037 cycles

LEFT REAR PASSENGER DOOR SEEMS HARD TO OPEN. CLEANED AND LUBED AFT PAX DOOR SEAL, OPEN AND CLOSED DOOR MULTIPLE TIMES , DOOR OPEN AND CLOSES NORMAL. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: HANDLE — ICED (PAX DOOR) · airframe 11,872 hrs · 12,882 cycles

F/A REPORT MAIN CABIN DOOR RELEASE HANDLE IS VERY DIFFICULT TO LIFT UP WHEN OPENING DOOR. CLEANED ICE FROM LOWER DOOR APERTURE. COMPLIED WITH LUBRICATION AND OPS CHECK OF DOOR HANDLE IAW MM 52-11-00-700-802. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — NONE · airframe 11,739 hrs · 12,739 cycles

DOOR VERY DIFFICULT TO OPEN FROM INSIDE. COMPLIED WITH FUNCTIONAL CHECK OF THE AIRSTAIR DOOR HANDLE FORCES IAW AMM 52-11-00-720-802, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (PROPELLER) · airframe 11,563 hrs · 12,565 cycles

"A/F TEST FAILED" CAUTION MESSAGE ON NR 1 ENGINE AFTER A/F TEST. CHECKED CDS, FOUND FAULT 400A ON NR 1 PEX REF FIM 61-20-09-810-806. FOUND NR1 PEC HAS PRIOR HISTORY OF SAME FAULT ON OTHER ACFT. R & R NR1 PEC IAW AMM 61-20-36-000-801/400-801. CHECKS GOOD IAW AMM 61-20-36-720-801 AND MX 6710006. C/W OPS TEST OF PROPELLER AUTOFEATHER AND UPTRIM SYS IAW AMM 61-20-00-710-801. CHECKS GOOD. NO FURTHER DEFECTS NOTED. RETUREND TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 11,522 hrs · 12,512 cycles

ON TAKEOFF ROLL WITH POWER LEVERS IN THE RATING DETENT, AUTOFEATHER FAILED TO ARM. AUTOFEATHER SWITCHLIGHT WAS DEPRESSED AND "SELECT" WAS ILLUMINATED. TAKEOFF WAS ABORTED ABOVE 60 KTS BUT LESS THAN 80 KTS. RETURNED TO THE GATE. INTERROGATED CDS FOR FAULTS. FOUND FAULT CODE 422 CHANNEL A&B ON NR 1 ENGINE. (UPTRIM A LOGIC FAULT). COMPLIED WITH AUTOFEATHER/ UPTRIM CHECK IAW AMM TASK 61-20-00-710-801. AUTOFEATHER/ UPTRIM TEST FAILED ON NR 1 ENGINE. IAW FIM TASK 61-20-09-810-813. R & R NR 1 PROP ELECTRONIC CONTROL UNIT IAW TASKS 61-20-36-000-801 AND 61-20-36-400-801. ALL OPS TESTS ARE GOOD. NO FAULT CODES INDICATED. OK FOR SERVICE. CHECKED DISCRETE SIGNAL FOR AUTOFEATHER SWITCH IN CDS. SWITCH OPERATES GOOD AND SIGNAL IN CDS IS GOOD. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 11,413 hrs · 12,423 cycles

AUTOFEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. INTERAGATED CDS FOUND FAULT CODES 494 & 422 ON NR 1 ENGINE. C/W FIM 61-20-10-810-826 FOR FAULT 494 FAULT CODE CLEARED. C/W FIM 61-20-09-810-813 FAULT CODE CLEARED OPS TEST GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — DAMAGED (ZONE 200) · airframe 10,766 hrs · 11,762 cycles

POSSIBLY ELECTRICAL ODOR EMANATING FROM REAR OF ACFT. INSPECTED CARGO PIT FOUND ODOR TO BE CENTERED AROUND THE FWD LAMP ASSY. BEGAN REMOVAL OF PANEL 251CZ REMOVED ENOUGH OF THE PANEL TO GRANT ACCESS FOR FURTHER INSPECTION REQUIRING THE REMOVAL OF THE AFT CARGO FWD SMOKE DETECTOR REF AMM TASM 26-12-01-000-801. FOUND OVERHEAD CARGO COMPARTMENT LIGHT ASSY PHENOLIC CAUSING THE ODOR. R & R AFT CARGO FWD LIGHT ASSY AS REQ REF AMM 33-31-01-000-801 & 33-31-01-400-801 NO FURTHER ODOR DETECTED, OPS CHECK GOOD. INSTALLED PANEL 251CZ AFT BAGGAGE COMPARTMENT LINERS REF AMM 25-52-19-400-801 1-4(A-5),5. REPLACED SMOKE DETECTOR. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,501 hrs · 11,466 cycles

CORROSION FOUND ON RT INBD SEAT TRACK AT X 1.00. BLENDED SEAT TRACK DAMAGE AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED RT INBD FWD SEAT TRACK IAW SRM 51-40-00-02-01. INSTALLED NEW SEAT TRACK IAW SRM 51-40-07-02-01 AND 51-40-15-02-01. APPLIED SELF LEVELING GREEN IAW SRM 51-21-10-02-01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 10,501 hrs · 11,466 cycles

CORROSION FOUND AT FS 32.400, Z100.032 WEB AT AFT SIDE OF FWD PASSENGER DOOR FLOOR LEVEL Y EQUALS 27L TO 38L. REMOVED ANGLE .013" MATERIAL REMOVED IAW SRM 51-21-00-00-02 AND 51-42-05-00-01. FABRICATED NEW ANGLE FROM 2024-T3 .050 IAW DWG 824844, SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED FABRICATED SUPPORT ANGLE IAW SRM 51-42-05 AND TC 6-53-1000, APPLIED PRIMER AND CIC IAW TC 6-53-1000. ALL WORK DONE IN CONFORMITY WITH TC 6-53-1000.

Part: TRAY — CORRODED (BATTERY BOX) · airframe 10,501 hrs · 11,466 cycles

STANDBY BATTERY TRAY NEEDS CLEANED PAINTED. CLEANED TRAY IAW SRM 51-26-00. REMOVED CORROSION IAW SRM 51-21-00. TREATED AND PRIMED IAW RD 8/4-53-3833. PERFORMED ECI ON TRAY, NO CRACKS FOUND IAW NDTM PSM 1-84-7A.

Part: PANEL — CORRODED (BS 784) · airframe 10,501 hrs · 11,466 cycles

FOUND CORROSION AROUND 2 PANEL SCREW HOLES AT FS X 784.102 FLOOR LEVEL Z100.032 Y6.250 AND Y20. BLENDED OUT CORROSION AND FOUND IN LIMITS IAW SRM 51-21-00 AND RD 8/4-53-3835.. ALODINED IAW SRM 51-21-10-01. ENGINEERING REQUEST SENT TO MFG. PERFORMED ECI ON BLENDED AREA. NO CRACKS FOUND AT THIS TIME IAW NDTM PSM 1-84-7A. APPLIED PRIMER TOP COAT AND CIC IAW RD 8/4-53-3835.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

CORROSION FOUND AT FORWARD PASSENGER DOOR THRESHOLD MEMBER. REMOVED THRESHOLD MEMBER IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW 51-21-00-00-02. LOCATED FASTENER HOLED FOR NEW THRESHOLD MEMBER IAW SRM 51-40-05-00-01 AND 51-40-07-02-01. INSTALLED ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. APPLIED TOPCOAT AND CIC IAW SRM 51-25-95 AND SRM 51-21-10-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

CORROSION FOUND AT X1.0 LT AND Z100 BETWEEN STR 23 & 24. REMOVED CORROSION IAW SRM 51-21-00. TREATED AFFECTED AREAS IAW SRM 51-21-10-02-01 PRIMED IAW SRM51-25-10-02-01, TOP COATED IAW SRM 51-25-25-02-01, APPLIED CIC IAW SRM 51-21-10-02-01. ALL WORK DONE IN CONFORMITY WITH RD 8/4-53-3831.

Part: FRAME — CORRODED (BS 281 S30-32R) · airframe 10,501 hrs · 11,466 cycles

FOUND CORROSION ON FRAME FS 281 BETWEEN STR 30 AND 32 RT SIDE. REMOVED CORROSION IAW 51-21-00-00-02. MAX MATERIAL REMOVED .003" IS WITHIN LIMITS IAW RD 8/4-53-2344. TREATED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. APPLIED TOP COAT AND CIC TO WORK AREA IAW RD 8/4-53-2344. ALL WORK PERFORM IN CONFORMITY WITH RD 8/4-53-2344.

Part: STRUCTURE — CORRODED · airframe 10,501 hrs · 11,466 cycles

CORROSION AT X 32.400 AND 2100 LT BETWEEN STR 23&24. REMOVED CORROSION IAW SRM 51-21-00-00-02. MAX MATERIAL REMOVED .021". TREATED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-25-02-01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-10-02-01. ALL WORK IN CONFORMITY WITH TC RD 8/4-53-3831.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

CHANNEL BELOW MAIN DOOR THRESHOLD CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-00-00-02. SENT TO ENGINEERING. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-1660. PERFORMED LPI IAW QX CHAP 8.2 NO DEFECTS NOTED. PERFORMED ECI ON ALL BLENDED AREAS IAW NDTM PSM 1-84-7A. ALODINED AFFECTED AREA IAW SRM 51-21-10-02-01, PRIMED IAW SRM 51-25-10-02-01.

Part: FRAME — CORRODED (BS 196) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 196 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .039, ORIGINAL THICKNESS .040", .001 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE RD 8/4-53-2344. TREATED WORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01. RIVETS INSTALLED ON WO Q-118955-R OP1.

Part: FRAME — CORRODED (BS 216 S30-32L) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 216 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. TOP COATED AND APPLIED CIC TO FASTENERS IAW RD 8/4-53-2344.

Part: STRUCTURE — CORRODED (BS 176) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 176 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED IAW SRM 51-21-10-02-01, 51-25-10-02-01. INSTALLED RIVETS IAW IAW SRM 51-42-05-02-01. PRIMED AND PAINTED RIVETS IAW RD 8/4-53-2344.

Part: SKIN — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

FOUND CORROSION ON FUSELAGE BELLY UNDER FWD DRAIN MAST ATTACH POINT. REMOVED SURFACE CORROSION FROM DRAIN MAST MOUNT IAW SRM 51-21-00. ALODINED IAW SRM 51-21-10-02-01. PAINTED IAW SRM 51-25-25-02-01.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 10,501 hrs · 11,466 cycles

CORROSION AROUND FLOOR PANEL SCREW HOLE AT FS X714.062 Z 100.032 Y23.5. BLENDED AREA IAW 51-21-00-00-02. FOUND OUT OF LIMITS IAW 53-40-43-00-01. ENGINEERING REQUEST SENT TO MFG. PAINTED AREA IAW SRM 51-25-15-02-01. PERFORMED ECI IAW NDTM PSM 1-84-7A. WORK FOUND ACCEPTABLE IAW RD 8/4-53-3836.

Part: FRAME — CORRODED (BS 156) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT F/S 156 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED, PAINTED AND APPLIED CIC TO WORKED AREA IAW RD 8/4-53-2344.

Part: STRUCTURE — CORRODED (BS 136) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 136 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED IAW SRM 51-21-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED RIVETS IAW RD 8/4-53-2344.

Part: STRUCTURE — CORRODED · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS ON ATTACH FLANGE OF RT STG 25, FROM X116.00 - X156.00. REMOVED 13 CORRODED RIVETS IAW SRM 51-42-05-00-01. AFTER FURTHER INSP, NO DAMAGE FOUND TO STRINGER. INSTALLED 13 NEW RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED FRAME IAW SRM 51-25-15-02-01. APPLIED MOISTURE DISPLACING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

CORROSION FOUND FROM FRAME X47.975 - X32.400 ON ATTACH FLANGE ON RT STR 31. REMOVED 4 RIVETS IAW SRM 51-42-06-00-01. BLENDED AREA IAW SRM 51-21-00-00-02. ENGINEERING REQUEST SENT. ULTRA SONIC THICKNESS EXAMINATION PERFORMED, MINIMUM REMAINING THICKNESS .068" SENT INFORMATION TO MFG. ALL BLENDS ARE ACCEPTABLE IAW RD 8/4-53-3816. TREATED AND PRIMED AREA IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALL WORK DONE IAW RD 8/4-53-3816. APPLIED TOPCOAT AND LPS HARD COAT IAW SRM 51-25-25-02-01 AND 51-21-10-02-01.

Part: FRAME — CORRODED (BS 258 S30-32L) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 258 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED, PAINTED AND APPLIED CIC IAW SRM 51-25-10-02-01, 51-25-15-02-01 AND MM 51-25-01-390-801.

Part: FRAME — CORRODED (BS 156) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT F/S 156 BETWEEN STR 30 AND 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION IAW SRM 51-26-10-02-01. ALL BLENDS WITHIN LIMITS RD 8/4-53-2344. TREATED BLENDED AREAS IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. PAINTED RIVETS IAW SRM 51-25-15-02-01. APPLIED MOISTURE DISPLACING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 321) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS FOUND AT FS 321 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WORKED AREA IAW SRM 51-21-10-02-01, 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND APPLIED CIC IAW RD 8/4-53-2344.

Part: SILL — CORRODED (CABIN) · airframe 10,501 hrs · 11,466 cycles

AFT SERVICE DOOR SILL PLATE CORRODED. CORROSION REMOVED IAW 51-21-00-00-02. SENT ENGINEERING REQUEST. AREA OUT OF LIMITS IAW SDR 53-40-21-00-01. LOCATED HOLES AND ROUGH CUT NEW SEAL PLATE IAW SRM 51-24-35-02-01. FABRICATED NEW SILL IAW EC 6-53-999. TREATED WITH ALUMINUM PREP AND ALODINE IAW 51-21-10-02-01. PRIMED FABRICATED SILL IAW SRM 51-25-10-02-01. INSTALLED SILL PLATE AND SLICE PLATES IAW SRM 51-40-05, 51-40-07, 51-40-15, 51-42-15 AND 51-42-05. APPLIED CIC TO WORKED AREA IAW SRM 51-21-00-00-01.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

LIGHT CORROSION FOUND UNDER AFT SERVICE DOOR SILL. REMOVED CORROSION IAW SRM 51-21-00. ENGINEERING REQUEST SENT. RECEIVED RD 8/4-53-3828. AREA IS OK AS IS. TREATED AND PRIMED AREA WORKED IAW SRM 51-25-10-02-01.

Part: FRAME — CORRODED (BS 116) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS ON FRAME AT X116.00 BETWEEN LT STR 31&30. REMOVED 5 RIVETS IAW SRM 51-42-05-00-01. REMOVED LIGHT CORROSION IAW SRM 51-21-00-02-01. BLENDED AREA WITHIN LIMITS OF RD 8/4-53-2344. ALL WORK DONE IAW RD 8/4-53-2344. TREATED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED 5 NEW RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED IAW SRM 51-21-15-02-01. APPLIED LPS NR 3 IAW RD 8/4-53-2344.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS ON ATTACH FLANGE OF RT STG 26 FROM X116.00 - X216.00. REMOVED 42 RIVETS IAW SRM 51-42-05-00-01. FOUND NO OTHER CORROSION. INSTALLED 42 NEW RIVETS IAW SRM 51-42-05. PRIMED AND PAINTED IAW AMM 51-25-26 AND 51-25-31-302-801. APPLIED LPS NR 3 IAW RD 8/4-53-2344.

Part: SEAT TRACK — CORRODED (BS 644.5-668.9) · airframe 10,501 hrs · 11,466 cycles

CORROSION ON FLOOR SEAT TRACK LT SIDE INBD FS X644.5 TO X668.9. BLENDED CORROSION FOUND TO EXCEED MAX LIMITS IAW RD 8/4-53-884. REMOVED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. PREPARED SEAT TRACK FOR INSTALL AND INSTALLED SEAT TRACK IAW 51-40-00-00-01, 51-42-00-00-02, 51-40-15-02-01, 51-42-00-00-01 AND 51-42-05-02-01.

Part: STRUCTURE — CORRODED (BS 176 S30-32L) · airframe 10,501 hrs · 11,466 cycles

CORRODED RIVETS ON FOUND AT F/S 176 BETWEEN STR 30&32 LT. REMOVED 6 RIVETS IAW SRM 51-42-05-00-01. FOUND CORROSION UNDER BUCK TAILS ON FRAME, BLENDED OUT CORROSION IAW SRM 51-26-10-02-01. ALL BLENDS WITHIN LIMITS RD 8/4-53-2344. TREATED BLENDED AREAS IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED 6 NEW RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED RIVETS IAW SRM 51-25-15-02-01. APPLIED MOISTURE DISPLACING COMPOUND IAW RD 8/4-53-2344.

Part: ATTACH FITTING — CORRODED (BS 584-644) · airframe 10,501 hrs · 11,466 cycles

CORROSION ALONG INBD ATTACH FLANGE ON LT STG 31 FROM X584.00 - X644.50. REMOVED CORROSION IAW SRM 51-21-00-00-02. TREATED AND PRIMED IAW SRM 51-25-10-02-01.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 10,501 hrs · 11,466 cycles

C2 - CORRODED RIVETS ON RT STG 31 ATTACH FLANGE BETWEEN X1.00 AND 19.400. REMOVED 19 EA RIVETS IAW SRM 51-42-05. FOUND NO EVIDENCE OF CORROSION UNDER RIVET HEADS IAW SRM 51-14-00. INSTALLED 19 EA RIVETS IAW SRM 51-42-05. TREATED, PRIMED AND PAINTED AREA IAW SRM 51-21-10, 51-25-10 AND 51-25-15.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 9,174 hrs · 10,084 cycles

EXCESSIVE BRAKING REQUIRED TO STOP. C/W BLEEDING OF THE BRAKE SYS. IAW AMM 32-42-00-870-801. C/W FUNCTIONAL TEST OF BRAKE SYS IAW AMM 32-42-00-720-801. CHECKS GOOD. C/W FUNCTIONAL TEST OF ANTI-SKID SYS IAW AMM 32-46-00-720-802. TESTS GOOD. C/W ANTI-SKID BUILT-IN TEST IAW AMM 32-46-00-720-801. TESTS GOOD. NO ANTI-SKID FAULTS FOUND IN CDS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ACTUATOR — MALFUNCTIONED (ZONE 700) · airframe 8,768 hrs · 9,657 cycles

WITH GEAR RETRACTION NOSE WHEEL REMAINED DOWN AND LOCKED FOR 23 SEC AFTER MAINS WERE UP AND LOCKED. NOSEWHEEL AMBER, RED AND UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR CAME UP BY ITSELF AND LIGHTS WENT DARK. ALTERNATE GEAR EXT. ACCOMPLISHED. LANDING UNEVENTFUL. FERRY FOR REPAIRS. REPLACED NLG ACTUATOR IAW AMM 32-31-51-000-801 & 32-31-51-400-801 OPS TEST GOOD RETURNED TO SERVICE.

Part: BLADE — CRACKED (PROPELLER) · airframe 8,170 hrs · 8,986 cycles

NR 2 PROPELLER BLADES HAVE CUFF CRACKS, ALL BLADES. REPAIRED CUFF CRACKS ON ALL 6 BLADES OF THE 2 PROPS IAW MFG PUB 1105 BLADE REPAIR MANUAL MINOR BLADE REPAIR NR 3 (F10). PLACED ON DMI. RETURNED TO SERVICE.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 7,357 hrs · 8,040 cycles

WEATHER RADAR DOES NOT PAINT GROUND CLUTTER OR WEATHER CORRECTLY. DUE TO THUNDERSTORMS, DIVERTED, LANDING UNEVENTFUL. R & R RADAR TRANSCEIVER IAW AMM 34-41-01, PGS 401-406. OPS TEST CKS GOOD IAW 34-41-00, PGS 516-520. RETURNED TO SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 6,998 hrs · 7,601 cycles

GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED. 3 RED LIGHTS ILLUMINATED, NO OTHERS ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION IAW E/A CHECKLIST PROCEDURE GEAR EXTENDED OK. LANDING UNEVENTFUL. FAULTS NOTED IN PSEU FLIGHT LEG 00" DIN01A FAULT UNREASON TRUE, DINO2A UNREASON FALS, LG DR CL FAR, RGDRCL FAR, NGDN2 FAR, NGDN1 FAR, NGDRCL FAR. FERRY FOR REPAIR. C/W RESISTANCE CHECKS AT LG SELECTOR VALVE(P54) FOUND HIGH RESITANCE AT EXTEND CONTACTS. R & R LANDING GEAR SELECTOR VALVE IAW AMM TASK 32-31-06-000-801/400-801. FUNCTION CHECKS GOOD. NO DEFECTS AND LEAKS CHECK GOOD. REF RIL'S 84-32-030 AND 84-32-006. FERRIED TO COMPLETE TASKS. ACFT RETURNED TO SERVICE.

Part: DOOR — UNSECURE (CARGO) · airframe 6,918 hrs · 7,502 cycles

MASTER WARNING FUSELAGE DOORS - REJECTED T/O AT 96KTS. UPON RETURN TO GATE BAG AFT DOOR HANDLE POPPED OPEN. DOOR STILL CLOSED. WT 48,000 LBS. NO BRAKES APPLIED. C/W INSP AND OPS TEST OF AFT CARGO DOOR HANDLE IAW AMM TASK 52-31-00-710-801. OPS TEST GOOD, TASKS 52-31-00 HS NR 52-0032 AND HS NR 52-0028 NO DEFECTS NOTED. OK FOR CONTINUED SERVICE. AMM HS NR 05-0019 C/W, NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 6,853 hrs · 7,419 cycles

LANDING GEAR DID NOT EXTEND NORMALLY- NO INDICATION THAT GEAR DOORS OPENED PERFORMED EMERGENCY CHECK LIST UTILIZED ALTERNATE GEAR EXTENSION. GEAR EXTENDED UTILIZING ALTERNATE GEAR EXTENSION. LANDING UNEVENTFUL. RETRIEVED PSEU FAULT CODES IAW AMM TASK 32-61-00-742-801, FOUND FAULTS DIN01A UNREASONABLE TRUE-00 (EXTEND COMMAND) DIN02A UNREASONABLE FALSE-00 (RETRACT COMMAND) DIN01B FAIL (LANDING ADV LAMP TEST 2). COMPLIED WITH DVI OF LANDING GEAR AND WHEEL WELLS WITH NO DEFECTS NOTED. COMPLIED WITH GVI AND COMPLIED WITH CONTINUITY CHECK FROM LANDING GEAR CONTROL PANEL CONNECTOR 3261-P55 PIN "P" AND GROUND STUD 3261-GS9 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LDG CONTROL PANEL IAW AMM 32-31-01-000-801 AND 32-31-01-400-801. FUNCTIONAL TESTS GOOD. RETURNED TO SERVICE.

Part: ELEVATOR SYSTEM — MALFUNCTIONED · airframe 6,847 hrs · 7,413 cycles

"ELEVATOR FEEL" CAUTION MESSAGE IN CRUISE AT 25,000 REMAINED ON FOR ENTIRE FLIGHT. DIVERTED. LANDING UNEVENTFUL. INTEROGATED CDS FOUND FAULT "LT FEEL ACTUATOR FAIL MESSAGE" ALSO FOUND CB H4 TRIPED. RE-SET H4 REF GMM 9.2.2. AND C/W FIM TASK 27-30-00-810-802 CLEARED FAULTS FROM CDS REFORMED OPS TEST OF ELEVATOR CONTROL SYS IAW TASK 27-30-00-710-801. OPS CHECKS GOOD NO FAULTS FOUND IN CDS, ACFT OK'D FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (BLEED SYS) · airframe 6,588 hrs · 7,107 cycles

ON T/O ROLL AT 70KTS, GOT THE NR 1 AND NR 2 BLEED HOT CAUTION LIGHT, AFTER FOLLOWING ABNORMAL CHECKLIST, BLEED, PRESSURIZATION ALL WORKING NORMALLY. INTERIGATED CDS, NO FAULTS FOUND, C/W OPS TEST OF THE BLEED AIR SYS IAW AMM TASK 36-11-00-710-802, OPS TEST GOOD , NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SOLENOID VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 6,536 hrs · 7,050 cycles

ATTEMPTED TO START APU, APU AUTO SHUTDOWN. RAMP REPORTED ALOT OF SMOKE. PLACED ON MEL 49-00-1. RETURNED TO SERVICE. MEL CLOSED ON 11-18-09. INTERROGATED CDS, FOUND CODE 102-3 ( UNDERSPEED) REMOVED AND REPLACED MAIN FUEL SOLENOID VALVE IAW AMM TASK 49-30-07-000-801 AND 49-30-07-400-801 C/W OP TEST OF APU IAW 49-00-00-710-801 OP CHECKS GOOD- (NOTE: TURBINE ROTATED FREELY NO TURBINE DRAG) C/W 3 START ATTEMPTS. ALL CHECKED GOOD. NO CURRENT FAULTS IN CDS. RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 ENGINE) · airframe 6,369 hrs · 6,863 cycles

POWERPLANT MESSAGE ON T/O ROLL AT 40KTS. INSPECTED AND FOUND FAULT 794 ON NR 1 ENG. PERFORMED FIM TASK 73-20-00-810-850 AND AMM TASK 71-00-00-868-806 WITH 2 SEPRATE STARTS. FAULT DID NOT RETURN. AIRCRAFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 6,077 hrs · 6,515 cycles

AN ELECTRICAL ODOR IN BACK BAGGAGE COMPARTMENT NEAR NR 1 SMOKE DETECTOR. REMOVED AND REPLACED NR 1 SMOKE DETECTOR AS A PRECAUTION IAW AMM 26-12-01-000-801 / 400-801 OPS TEST GOOD. ELECTRICAL ODOR STILL EXISTS. REMOVED FORWARD AFT BAGGAGE COMPARTMENT LIGHT ASSY IAW AMM TASK 33-31-01-000-801. INSTALLED SERVICABLE LIGHT ASSY IAW AMM TASK 33-31-01-400-801. OPS CHECK PASSED. LT LIGHTS IN AFT CARGO COMPARTMENT ON FOR APPROX. 30 MINUTES. NO ELECTRICAL ODOR PRESENT DURING OR AFTER OPS CHECK. RETURNED TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 6,043 hrs · 6,474 cycles

STRONG ODOR IN FLIGHT DECK EXTENDS BACK TO APPROXIMATELY ROW 5. INVESTIGATED ODOR, FOUND NR 1 ARCDU FAILED., REMOVED AND REPLACED NR 1 ARCDU IAW MTC 9238101. RETURNED TO SERVICE.

Part: HANDLE — DISLODGED (CARGO DOOR) · airframe 5,079 hrs · 5,344 cycles

SEA - UPON ROTATION FUSELAGE DOOR WARNING LIGHT ILLUMINATED AND AIRCRAFT DID NOT PRESSURIZE. AFTER RETURN TO FIELD BAGGAGE DOOR HANDLE WAS STICKING OUT. MAINTENANCE PERFORMED A INSPECTION OF THE AFT CARGO DOOR AND OPERATIONAL TEST IAW AMM TASK 52-31-00-710-801. NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR — UNKNOWN (SERVICE) · airframe 5,072 hrs · 5,336 cycles

PDX - L2 - AFT SERVICE DOOR WILL NOT OPEN. MAINTENANCE OPERATED DOOR, NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 4,935 hrs · 5,169 cycles

PDX - C1 - THERE ARE THREE DENTS IN THE UPPER OUTBOARD SKIN OF THE MCD THAT REQUIRE A PERMANENT REPAIR. MAPPED AREA OF DENTS FOR ENGINEERING STARTED THE REPAIR ON THE MCD SHELL ASSY IAW RD 8/4-52-456 STEPS (1) AND (2). CONTINUED REPAIR OF MCD SHELL BY COMPLYING WITH RD8/4-52-456 STEP (3) AND (4). NFEC IAW NDTM PART 6 51-00-01 AND RD8/4-52-456(4), NO CRACKS NOTED. DRILLED HOLES IN MCD SHELL SKIN FOR REPAIR AS PER RD 8/4-52-456 NOTES 6 AND 7. FILLED COUNTERSINKS ON DOOR SKIN FABRICATED AND DRILLED DOUBLER FASTENER HOLES, AND ALODINED AND PRIMED DOUBLER IAW RD 8/4-52-456 NOTES (8) AND (9I) AND (9II) AND DRAWING ON SHEET 4. INSTALLED REPAIR DOUBLER BY FAY SEALING AND WET INSTALLING SOLID RIVETS IAW RD8/4-52-45 NOTES 10 AND 11. SEALED EDGES OF REPAIR DOUBLER AND CUT-OUT AND APPLIED CORROSION INHIBITOR TO INTERNAL SURFACES IAW RD 8/4-52-456 STEP 12 AND 13. INSTALLED MCD INNER SKIN PANEL IAW RD8/4-52-456 GENERAL NOTES STEP 2 AND SRM 51-42-05.

Part: SKIN — DAMAGED (TE FLAP) · airframe 4,935 hrs · 5,169 cycles

PDX - C1 - LT OTBD FLAP AT APPROX 30 INCHES FROM INBOARD END AND APPROX 14 INCHES UP FROM TRAILING EDGE ON THE TOP SURFACE HAS A CHAFE FORMING, CHAFE IS APPROX 3 INCHES IN LENGTH AND .100 INCH WIDE IN CENTER OF CHAFED AREA. BLENDED AREA IAW SRM 57-52-30-02 TO REMOVE DAMAGE AND FOUND BLENDED AREA TO BE OUT OF LIMITS IAW SRM 57-52-30-01. HFEC IAW -8 400 NDTM PART 6 51-00-01, NO CRACKS NOTED. UT BOND IAW -8 400 NDTM PART 1 51-00-04, NO DISBONDS NOTED. UT THICKNESS IAW -8 400 NDTM PART 51-00-04, HIGH .032 LOW .030 MAPPED AREA FOR ENGINEERING. INSPECTED AREA OF BLEND AND FOUND AREA TO BE WITHIN LIMITS IAW RD8/4-57-1146, REPAINTED BARE AREA IAW RD8/4-57-1146 TO COMPLETE REPAIR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 4,935 hrs · 5,169 cycles

PDX - C1 RT OTBD FLAP HAS TOP SKIN CHAFE APPROX 47 INCHES FROM THE INBD EDGE 34 INCHES LONG. BLENDED AREA OF CHAFE IAW SRM 57-52-30-02 TO REMOVE DAMAGE AND FOUND BLENDED AREA TO BE OUT OF LIMITS IAW SRM 57-52-30-01. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NOTED. UT BOND IAW NDTM PART 1 51-00-04, NO DISBONDS NOTED. UT THICKNESS IAW NDTM PART 1 51-00-04, HIGH .032 LOW .027. MAPPED FOR ENGINEERING, INSPECTED AREA OF BLEND AND FOUND IT TO BE WITHIN LIMITS IAW RD 8/4-57-1147. REPAINTED BARE AREA IAW RD8/4-57-1147 TO COMPLETE REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,935 hrs · 5,169 cycles

PDX - C1 CHECK, CORROSION PITS ON TOP OF RT INBOARD SEAT TRACK AT STATION 644.5. BLENDED AREA, MATERIAL REMOVED WAS 0.37 INCH AND OUT OF LIMITS. REPLACED SEAT TRACK.

Part: UNKNOWN — ODOR (CABIN AIR) · airframe 4,816 hrs · 5,030 cycles

PDX - APU AIR HAS UNUSUAL AND PERSISTANT ODOR. PLACED APU ON MEL 49-00-1. MEL CLEARED 3/11/09 INSPECTED APU COMPARTMENT. NO DEFECTS NOTED. RAN APU. NO UNUSUAL ODOR FOUND. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BOOT — FAILED (DE ICE SYSTEM) · airframe 4,777 hrs · 4,987 cycles

GEG- "DEICE PRESS" LIGHT ILLUMINATED IN FLT. RAN CHECKLIST LIGHT CONTINUED TO ILLUMINATE. PSI LOOKED GOOD. LEFT INBOARD DE-ICE BOOT/HORIZONTAL STAB, LIGHT ON THE ICE PROTECTION PANEL CONTINUED TO FLICKER WHILE CHECKLIST WAS BEING DONE. DIVERTED TO GEG. LANDING UNEVENTFUL. REMOVED AND REPLACED LT INBOARD HORIZONTAL STAB LEADING EDGE WITH NEW FROM STOCK IAW AMM 55-13-00-000-801 AND 55-13-00-400-801. OPS CHECK GOOD. "DE-ICE PRESS" CAUTION DID NOT ILLUMINATE. SEALANT PLACED ON DMI. RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (RADAR ALTIMETER) · airframe 4,631 hrs · 4,813 cycles

SEA - DURING APPROACH IN SEA A3 ARM WOULD CYCLE OFF THEN COME BACK ON AT LOC INTERCEPT, THEN AT GLIDESLOPE INTERCEPT IT WOULD GO NO A3. ATTEMPTED 2 APPROACHES ON 16C AND 1 APPROACH ON 16L AND SETUP AGAIN AT PDX 10R ALL RESULTS THE SAME. EVENT MARKER PUSHED. DIVERTED TO PDX, UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 RAD ALT COMPUTER IAW MTC 6344401 AND HGS COMPUTER IAW MTC 6343501 OPERATIONAL TEST GOOD. AIRCRAFT UPGRADED TO CAT III STATUS. AIRCRAFT PLACARD READS CAT III DMI PLACARDS REMOVED. RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 4,452 hrs · 4,635 cycles

NR 1 ARCDU FAILED UNABLE TO RESET PER CHECKLIST. CYCLED ARCDU 1 C/B'S L-ESS G2, R-MAIN E4, PERFORMED POWER ON BITE TEST, PERFORMED TEST THROUGH CDS, TEST OK, PERFORMED OPS TEST IAW MTC 6238101, ARCDU OPS TEST NORMAL. AIRCRAFT RELEASED THROUGH CONTACT WITH MTX CONTROL. OK FOR SERVICE. ACFT REMAINS CAT III, COCKPIT PLACARD READS CAT III. COULD NOT DUPLICATE, RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BLOWOUT PANEL — LOOSE · airframe 4,224 hrs · 4,370 cycles

DEPARTING BLI AT 1500 FT, HEARD A MUFFLED THUMP (AFT FA DESCRIBED A LOUD METALLIC THUMP). ACFT THEN DEPRESSURIZED. CABIN CLIMB FOLLOWED ACFT CLIMB RATE TO 7000 FT. FINISHED AFTER TAKEOFF FLOW AND WHEN SELECTING BLEED CONTROL FROM MIN TO NORM. THE CABIN STARTED TO RAPIDLY REPRESSURIZE AFTER 2 MINUTES, PRESSURIZATION RATE WAS NORMAL. REMAINED IN LEVEL FLT 7000. PRESSURIZATION WAS NORMAL ON DESCENT TO SEA. ON GROUND IN BLI BEFORE FLIGHT, THE A/C WAS PARKED WITH 40 KNOT DIRECT TAILWIND. FOUND AFT CARGO BAY AFT BLOW OUT PANEL OUT OF POSITION. RESECURED AS NECESSARY PRESSURIZED ACFT (REF AMM TASK NR 21-00-00-863-801) TO 5 DIFF + HELD FOR 5 MIN WITH NO DEFECTS OR LEAKS NOTED. DEPRESSURIZED A/C (REF AMM TASK NR 21-00-00-863-802) + RE-INSPECTED AFT CARGO BAY AFT BLOW OUT PANEL. PANEL REMAINED SECURE WITH NO FURTHER DEFECTS. INSPECTED AFT CARGO BAY DOOR, NO DEFECTS. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: GENERATOR — MALFUNCTIONED (AC SYSTEM) · airframe 3,960 hrs · 4,051 cycles

YKM- RECEIVED A NR 1 AC GENERATOR CAUTION LIGHT PRIOR TO 60 KNOTS ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AC GEN IAW TC 6242101.OPS CHECKED GOOD PER Q-400 AMM TASK 24-21-00-710-801. RETURNED TO SERVICE.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 3,178 hrs · 3,213 cycles

PDX - FLIGHT 2335. CREW REPORTED A BURNING ODOR IN THE AFT GALLEY AREA. MAINTENANCE FOUND THE SOURCE TO BE THE LT JUG. REPLACED THE LT JUG. OPERATIONAL CHECKS GOOD. ACFT RETURNED TO SERVICE. (S)

Part: COMPUTER — FAILED (NR 2 AHRS) · airframe 2,801 hrs · 2,819 cycles

BIL - FLIGHT 2598 (SEA-BIL) - RECEIVED A ELEVATOR CAUTION EN ROUTE. CONTINUE TO BIL. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 AHRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: AUTOFEATHER SYS — MALFUNCTIONED (PROPELLER) · airframe 2,257 hrs · 2,187 cycles

LAX- FLIGHT 2448 - DURING TAKEOFF ROLL, AUTO-FEATHER SYSTEM FAILED TO ARM. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE. MAINTENANCE FOUND FAULT CODES 402B AND 494 A/B. PERFORMED PEC FAULT CODE CLEARING PROCEDURE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: AUTOFEATHER SYS — MALFUNCTIONED (PROPELLER) · airframe 2,200 hrs · 2,128 cycles

YYJ - FLIGHT 2079 - ON TAKEOFF, AUTOFEATHER SYSTEM FAILED TO ARM. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE. MAINTENANCE FOUND FAULT CODE 941 IN THE SYSTEM AND CLEARED THE CODE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 2,185 hrs · 2,111 cycles

SEA- FLIGHT 2289 (SEA-EUG) - ABORTED TAKEOFF AT 85 TO 90 KNOTS AND RETURNED TO THE GATE FOR AUTOFEATHER SYSTEM NOT ARMING. MAINTENANCE FOUND FAULT CODE 494 AND PERFORMED FIM TASK 61-20-10-810-826. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONNECTOR — SMOKE (GPU) · airframe 1,933 hrs · 1,849 cycles

PDX - FLIGHT 2432, NOTICED GPU CONNECTOR SMOKING. MAINTENANCE FOUND GPU CONNECTOR FAULTY. NO AIRCRAFT DAMAGE NOTED. USED ANOTHER GPU. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 339 hrs · 305 cycles

LAX FLIGHT NR 2444: NR 3 HYD CAUTION LIGHT ILLUMINATED DURING PUSH BACK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE OPERATED NR 3 HYD ISO VALVE AND CYCLED ELEVATOR SEVERAL TIMES. C/W PRESSURIZATION CHECK OF NR 3 HYD SYSTEM IAW Q400 AMM TASK 29-00-00-863-803. OPS CHECK GOOD. CAUTION LIGHT REMAINED EXTINGUISHED. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (NR 2 PROPELLER) · airframe 180 hrs · 152 cycles

BOI FLIGHT NR 2237: NR 2 PROP FAILED TO COME OUT OF FEATHER FOR APPROXIMATELY 5 MINUTES AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 PROP OVER SPEED GOVERNOR WITH SERVICEABLE UNIT IAW Q400 TASK 61-20-26-000-801 FOR REMOVAL AND TASK 61-20-26-400-801 FOR INSTALLATION. C/W OPS CHECK OF THE OSG IAW TASK 61-20-00-710-803 OF Q400 AMM. OPS TEST GOOD. C/W FUNCTIONAL TEST OF THE PROP TIME TO UNFEATHER IAW Q400 MM TASK 61-20-00-720-801. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: GCU — MALFUNCTIONED (NR 2 AC GEN) · airframe 172 hrs · 148 cycles

SEA FLIGHT NR 2348: NR 2 AC GEN WOULD NOT COME ON LINE AFTER START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED RETRIEVAL OF DATA FROM EPCU. FOUND CODE 28 2AC GCU. REMOVED AND INSTALLED SERVICEABLE NR 2 AC GEN GCU IAW Q400 AMM 24-21-06-000-801 AND 24-21-06-400-801. PERFORMED OPS TEST IAW Q400 AMM 24-21-00-710-801. OPS TEST GOOD. NR 2 AC GEN COMES ON LINE AS REQUIRED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (HYD SYSTEM) · airframe 64 hrs · 51 cycles

SEA FLIGHT NR 2459: NR 2 RUD HYD CAUTION AND NR 2 HYD PRESS BLANK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND NR 2 HYD CIRCUIT BREAKER POPPED. RESET BREAKER AND GROUND RAN NR 2 ENGINE. NR 2 HYD CAUTION LIGHT EXTINGUISHED. OPS CHECK OF NR 2 HYD PRESSURE INDICATION AND OPERATION IS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.