N439QX

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 27,066 hrs · 29,106 cycles

DURING CLIMB OUT OF SEA THROUGH 15,000 THE FLT DATA RECORDER, THEN AVIONICS, THEN ELEVATOR FEEL CAUTION LIGHTS ILLUMINATED. THE AUTOPILOT REVERTED TO BASIC MODES, THE CA PFD V-SPEEDS AND MDA DISAPPEARED BUT NOT ON THE FO PFD. THIS SEQUENCE HAPPENED 4 TIMES. THE ASSOCIATED CHECKLIST IN THE E+A WERE REVIEWED BUT NOT APPLICABLE. FLIGHT DIVERTED TO PDX WITH NO FURTHER ISSUES. REMOVED FROM SERVICE. REPLACED IOP #1 IAW MTC 6314101. OPS CHECKS GOOD PERFORMED LLM RTS TEST IAW MTC 6314101. OPS CHECKS GOOD AIRCRAFT REMAINS CATEGORY III QUALIFIED. COCKPIT PLACARD REMAINS CAT III. MAINTENANCE CONTROL NOTIFIED. NO FAULTS FOUND IN CDS. COULD NOT DUPLICATE DISCREPANCY UNLESS IOP/IOM #1 BREAKER WAS PULLED. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — INOPERATIVE (ZONE 200) · airframe 26,646 hrs · 28,673 cycles

AFTER DEPARTURE FROM GEG APPRX 3K. CREW NOTED A HIGH CABIN TEMP- NOTICED THE CABIN WAS NOT PRESSURIZING DUE TO NO BLEED FLOW- CHECKLIST WAS FOLLOWED. SWITCHED TO RAM AIR. BLEEDS WERE TURNED OFF AS WELL AS PACK SWITCHES TO OFF THEN PAC SWITCHES TO AUTO + BLEEDS BACK ON. BLEED FLOW BEGAN AND A/C PRESSURIZED. NO OTHER ISSUES WERE NOTED DURING EVENT. NO PAC OR CABIN DUCTS HOT. NO CAUTIONS WERE OBSERVED. FLIGHT WAS CONDUCTED NORMALLY TO SEA. REMOVED FROM SERVICE. FOUND ECS FAULT CODE 3004, PERFORMED Q400 FIM TASK 21-60-00-810-809 AS REQUESTED. NO ADDITIONAL DEFECTS NOTED. RETURNED TO Q400 FIM TASK 21-60-00-810-809 FOR ECS FAULT CODE 3004. AS DIRECTED R+R PACK FLOW CONTROL AND SHUTOFF VALVE IAW Q400 AMM TASK 21-52-01-000/400-801. PACK FLOW CONTROL AND SHUT OFF VALVE OPS TEST PASSED. PRESSURIZED AIRCRAFT FOR MAINTENANCE REF Q400 AMM TASK 21-00-00-863-801. PRESSURIZATION CHECKS GOOD. NO LOSS OR FLUCTUATIONS IN PRESSURIZATION NOTED. FAULT CODE 3004 DID NOT RETURN. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — FAILED (NR 2) · airframe 26,270 hrs · 28,291 cycles

#2 PFD WENT BLANK IN FLIGHT RAN E&A CHECKLIST, DISPLAY CAME BACK. REMOVED FROM SERVICE. RESET #2 PFD IAW Q400 SPGRG 31-10-01 AS DIRECTED BY M/C 21443 GPM 8.2.2.4. DISPLAY RESTORED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST · airframe 26,258 hrs · 28,280 cycles

A/F TEST FOR FO DAILY CHECKS #2 FAILED #1 ABORT. REMOVED FROM SERVICE. CYCLED POWER ON A/C. C/W OPS TEST OF PROP AUTOFEATHER UPTRIM IAW Q400 AMM TASK 61-20-00-710-810. OPS TEST GOOD. AUTOFEATHER PASSED. NO FAULTS IN CDS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,053 hrs · 28,079 cycles

EMERGENCY EXIT LIGHT BY FWD FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. CHECKED WIRING BETWEEN POWER SUPPLY 1 AND P18. FOUND WIRE 31A-22-2 BROKEN. SPLICED WIRE PER Q400 WIRE MANUAL 20-16-10. OPS TEST GOOD.

Part: PEC — MALFUNCTIONED (#2 ENGINE) · airframe 26,002 hrs · 28,028 cycles

WHILE TESTING A/F DURING THE DAILY SYSTEMS CHECKS, #1 ENGINE INDICATES "ABORT" AND #2 ENGINE "FAILED" TEST CONDUCTED TWICE W/ POWER LEVERS IN DISC. REMOVED FROM SERVICE. CDS REPORTED FAULT CODES 494 CH A AND CH B AND 72 CH B #2 PROP. PER Q400 FIM TASK 61-20-02-810-836 AND 61-20-10-810-826, REMOVED AND REPLACED #2 PEC IAW Q400 AMM TASKS 61-20-36-000-801 AND 61-20-36-400-801. ALL OPERATIONAL CHECKS GOOD IAW TASK CARD 6710006. NO CDS FAULTS NOTED POST OP'S CHECKS. AIRCRAFT OKAY FOR SERVICE.

Part: AUTOFEATHER SYS — NO TEST (NR 1) · airframe 25,995 hrs · 28,021 cycles

A/F TEST FAILS TEST, #1 ENGINE ABORT, #2 ENGINE FAILED. REMOVED FROM SERVICE. INTERROGATED CDS . FOUND FAULT 72 CH B ON # 2 ENG DISPLAY. REF Q400 FIM TASK 61-20-02-810-836. CLEARED FAULT AND C/W OPS TEST OF AUTOFEATHER & UPTRIM SYSTEM PER AMM 61-20-00-710-810. TEST PASSED THREE TIMES. FAULT DID NOT RETURN. NO FURTHER DEFECTS.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOFEATHER SYS) · airframe 25,970 hrs · 27,996 cycles

AUTO FEATHER TEST "ABORT FAILED" AMBER MESSAGE ON ED. REMOVED FROM SERVICE. FOUND FAULT CODE 494 ON #2 ENG. PERFORMED FIM Q400 61-20-10-810-826. CLEARED CODE. PERFORMED A/F TEST. TEST PASSED. VERIFIED NO CODES AFTER TEST, NO FURTHER MAINT ACTIONS REQUIRED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 25,850 hrs · 27,875 cycles

MASTER WARNING FUSELAGE DOOR CLIMBING OUT OF BOI. AFT PASSENGER DOOR . FA SAID IT DIDN’T LOOK COMPLETELY CLOSED . AT FL 210. PRESSURIZATION NORMAL. DIVERTED TO ALW. FLIGHT LANDED SAFELY. REMOVED FROM SERVICE. UPON ARRIVAL TO AIRCRAFT FOUND L2 DOOR HANDLE NOT SEATED. COMPLIED WITH AMM TASK 52-12-00-8-710-802 FOR OPERATIONAL TEST OF THE AFT PASSENGER DOOR . ALL INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION OF THE DOOR AND SURROUNDING STRUCTURE WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 25,784 hrs · 27,814 cycles

AT CRUISE, FUSELAGE DOOR MASTER WARNING ILLUMINATED. AFT PASSENGER DOOR SHOWED OPEN. PRESSURIZATION WAS NORMAL THROUGHOUT REMAINDER OF FLIGHT. FA'S NOTED THE HANDLE WAS NOT PUSHED IN ALL THE WAY. DIVERTED. EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. FOUND DOOR HANDLE NOT PUSHED IN ALL THE WAY. PERFORMED OPERATIONAL TEST OF AFT PASSENGER DOOR IAW Q400 AMM 52-12-00-710-802. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: DITCHING DAM — MALFUNCTIONED · airframe 25,669 hrs · 27,707 cycles

FLIGHT ATTENDANT REPORTS DITCHING DAM IS NOT STAYING UP. FALLS DOWN WITH LIGHT TURBULANCE. REMOVED FROM SERVICE. STOWED AIRSTAIR DITCHING DAM AND PERFORMED OPERATIONAL CHECK, IAW Q400 AMM 25-62-01-710-801, OPERATIONS CHECKS GOOD. OK FOR SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PEC — MALFUNCTIONED (NR 2) · airframe 24,723 hrs · 26,717 cycles

NR 2 AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. TAKEOFF ABORTED 80 KTS GROUNDSPEED REACHED. NO EXCESSIVE BRAKING. REMOVED FROM SERVICE. REPLACED NR 2 PEC. A/C OK FOR CONTINUED SERVICE.

Part: AUTOFEATHER SYS — FAULTED (NR 2) · airframe 24,720 hrs · 26,714 cycles

DURING DAILY SYSTEMS NR 2 ENG FAILED AUTO FEATHER CHECK. REMOVED FROM SERVICE. FOUND FAULT CODES 494AB, 228AB, AND 206AB IN CDS FOR NR 2 ENG. C/W FIM 61-20-10-810-826. PERFORMED OPS TEST OF PROP AUTO FEATHER AN UPTRIM SYSTEM IAW AMM 61-20-00-710-810. TEST FAILED ON NR 2 SIDE. SAME CODES. CYCLED A/C POWER. CODES REMAIN. CLEARED PEC FAULTS IAW AMM 61-20-36-070-801. ALL CODES EXCEPT 494 CLEARED. PERFORMED AF TEST AGAIN PER AMM 61-20-00-710-810. TEST PASSED. CLEARED PEC FAULTS AGAIN. 494 NO LONGER SHOWS. RAN NR 2 ENG TWICE WITH NO ISSUES. PERFORMED LAST AF TEST PER SAME AMM. TEST PASS AGAIN. NO FAULTS. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,601 hrs · 26,575 cycles

DURING OPS CHECK OF EMERGENCY LIGHTS NOTED THAT CABIN EMERGENCY EGRESS LIGHTS IN PANELS 235CZ, 235DZ AND FWD RH EMER. EXIT DOOR ARE INOP. R/R'ED EMERGENCY LIGHT BATTERY R2 FROM ABOVE PAX CEILING PANEL 235CZ IAW Q400 AMM TASKS 33-51-01-000-801, 33-51-01-400-801, EMERGENCY LIGHT SYSTEM OPS CHECKS GOOD.

Part: LATCH — STICKING (COCKPIT DOOR) · airframe 23,612 hrs · 25,390 cycles

FLT DECK DOOR LATCH STICKS IN THE UNLATCHED POSITION. REMOVED FROM SERVICE. CLEAN AND LUBED DOOR LATCH STRIKER. OPS CHECK GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 23,488 hrs · 25,251 cycles

DURING GEAR RETRACTION SPOILER OUTBOARD CAUTION ILLUMINATED FOR THE DURATION OF THE CYCLE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. AIRCRAFT DOWN FOR REPAIRS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,435 hrs · 25,184 cycles

EMERGENCY LIGHT EXIT SIGN AT MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY RT & LT #1 IAW AMM 33-51-01-000-801 & 33-51-01-400-801. OPS CK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEARING — FAILED (MLG WHEEL) · airframe 23,406 hrs · 25,159 cycles

WHILE TROUBLESHOOING ANTI-SKID SYSTEM, FOUND THE NR 1 MAIN GEAR WHEEL BEARING HAD FAILED.

Part: AXLE — CORRODED (LEFT MLG) · airframe 23,379 hrs · 25,124 cycles

LEFT MAIN LANDING GEAR #1 OUTBOARD AXLE HAS EXCESSIVE PITTING AND CORROSION AT THE OUTBOARD SIDE NEXT TO THE INBOARD BEARING JOURNAL. REPLACED #1 AXLE IAW AMM Q400 32-11-04-400-801.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 23,071 hrs · 24,755 cycles

AFTER GEAR RETRACTION GOT MASTER WARNING CAUTION AND AT LEAST THREE CAUTION LIGHTS. LIGHTS WENT OUT AFTER GEAR RETRACTION (2-3 SECONDS) F/O OBSERVED "SPOILER OUTBD" AND "ROLL SPLR INBD HYD CAUTIONS SPEED ABOUT 140 KIAS. REMOVED FROM SERVICE. INTEROGATED CDS AND FOUND NO CURRENT OR LOGGED FAULTS. C/W OPS TEST OF ROLL SPOILER SYSTEM IAW Q400 AMM 27-10-00-870-079 . OPS TEST GOOD. C/W BLEEDING OF 1 HYD SYSTEM AND 2 HYD SYSTEM IAW Q400 AMM 29-10-00-870-079 AND 29-10-00-870-077. C/W WITH OPERATIONAL TEST OF ROLL SPOILER SYSTEM IAW AMM 27-60-00-710-801. OPS TEST GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LATCH — INOPERATIVE (LAVATORY DOOR) · airframe 21,976 hrs · 23,467 cycles

PAX TRAPPED IN LAV, ABLE TO OPEN DOOR AT FLIGHT LEVEL 210. ( LAVATORY WASTE SYSTEMS - LAVATORY UNUSABLE ). REMOVED FROM SERVICE. REMOVED AND REPLACED LAV DOOR KNOB LATCH ASSY OPS CHECK GOOD NO FUTHER DEFECTS NOTED. CLEAR MEL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DETERIORATED (CABIN) · airframe 20,940 hrs · 22,309 cycles

EMERGENCY FLOOR -PATH -LIGHT ASSY BY COCKPIT DOOR IS DETERIORATED. REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY FLOOR-PATH-LIGHT ASSY REF Q400 AMM TASK 33-51-16-000-801 AND 33-51-16-400-801. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — STUCK (RUDDER PEDAL ADJ) · airframe 20,662 hrs · 22,003 cycles

FIRST OFFICER`S RUDDER PEDAL ADJUSTMENT HANDLE WILL NOT TURN, RUDDER PEDALS WILL NOT TRAVEL FORE OR AFT. REMOVED FROM SERVICE. PERFORMED A GVI FOR FOD, NO FOD OR DEFECTS NOTED. RELEASED THE FO'S ADJUSTMENT HANDLE, VERIFIED FULL RUDDER PEDAL ADJUSTMENT TRAVEL. LUBRICATED THE RT ADJUSTMENT HANDLE BEVEL GEAR. PERFORMED AN OPS TEST OF RUDDER CONTROL SYSTEM, IAW AMM 27-20-00-710-803. OPS TESTED GOOD. FO'S RUDDER PEDAL ADJUSTMENT HANDLE WORKS WITHOUT DEFECT. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 20,637 hrs · 21,976 cycles

AFTER TAKE OFF, FUSELAGE DOORS MASTER CAUTION ILLUMINATED FOR CARGO DOOR OPEN. DIVERTED. LANDING UNEVENTFUL. INSPECTED THE AFT CARGO DOOR AND FOUND THE HANDLE OUT. SECURED THE CARGO DOOR HANDLE. OPS CHECKED GOOD IAW 52-31-00-710-801 AND DOOR INSPECTED IAW 52-0028. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 19,823 hrs · 21,087 cycles

ON DEPARTURE, FUSELAGE DOOR WARNING LIGHT ILLUMINATED. VERIFIED AFT CARGO DOOR OPEN INDICATED ON DOOR PAGE. ACFT NOT PRESSURIZING. DECLARED EMERGENCY AND RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED, FOUND THE AFT CARGO DOOR HANDLE POPPED, INSPECTED, PERFORMED OPS TEST IAW AMM 52-31-00-710-801. OPS TESTED GOOD, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 19,763 hrs · 21,023 cycles

FUSELAGE DOORS WARNING LIGHT ILLUMINATED FLIGHT. AFT BAGGAGE DOOR INDICATED OPEN ON DOORS SYS PAGE. REMOVED FROM SERVICE. FOUND AFT BAG DOOR HANDLE OUT UPON ARRIVAL. PERFORMED INSP. OPS TEST GOOD, NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST (NR 1 ENGINE) · airframe 19,517 hrs · 20,790 cycles

AUTOFEATHER TEST FAILED ON THE NR 1 ENGINE. REMOVED FROM SERVICE. INTERROGATED CDS. FOUND FAULTS 204A/B. CLEARED FAULTS. PERFORMED OPERATIONAL TEST OF THE AUTOFEATHER SYSTEM IAW AMM 61-20-00-710-805. NR 1 ENGINE PASSED, NO FAULTS IN CDS. RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 19,468 hrs · 20,732 cycles

AUTO FEATHER DID NOT ARM ON TAKEOFF ROLL. AFTER LANDING PERFORMED A/F TEST, A/F TEST ON NR 1 ENGINE FAILED. REMOVED FROM SERVICE. C/W FIM TASK FOR CLEARING FAULT CODE 204. REPLACED NR 1 PEC IAW AMM 61-20-36-000/400-801. FAULT CLEARED, OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 19,415 hrs · 20,678 cycles

ON TO AF SELECT DID NOT ARM. TAKEOFF ABORTED. AS INSTRUCTED BY MTX CONTROL ACCOMPLISHED AF TEST NR 1 ORIO AF TEST FAILED. REMOVED AIRCRAFT FROM SERVICE. CYCLED POWER ON AIRCRAFT PERFORMED OPS CHECK PROCEDURE. PROP AUTOFEATHER SYSTEM IAW AMM 61-20-00-710-805. AUTOFEATHER SYSTEM PASS WITH NO DEFECTS NOTED. CREW ALSO PERFORMED GROUND RUN AND AUTOFEATHER SYSTEM PASS WITH NO DEFECTS . COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — UNSECURE (SERVICE DOOR) · airframe 18,948 hrs · 20,190 cycles

PASSING FL 210 AFT SERVICE DOOR ACTIVATED FUSEAGE MASTER WARNING. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. AIRCRAFT REMOVED FROM SERVICE. FOUND AFT SERVICE DOOR EXTERIOR HANDLE NOT FLUSH. COMPLIED WITH OPS TEST OF SERVICE DOOR, OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED IAW AMM 52-41-00-720-801. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BOLT — LOOSE (WINDOW) · airframe 18,613 hrs · 19,644 cycles

LOUD HISSING SOUND BY FO'S SIDE WINDOW, STARTING AT ABOUT 1.5 PSI DIFFERENTIAL AND NOT SUBSIDING. CABIN PRESSURIZATION NORMAL. DIVERTED. LANDING UNEVENTFUL. FOUND MULTIPLE OUTER SCREWS LOOSE ON AFT SIDE OF FO`S SIDE WINDOW. TORQUED SCREWS IAW AMM TASK 56-10-06-400-801. PRESSURIZED ACFT IAW AMM TASK 21-00-00-863-801. NO LEAKS NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,577 hrs · 19,806 cycles

FORWARD F/A EMERGENCY LIGHT SWITCH NOT ILLUMINATED. RELAMPED. CHECKS GOOD. RETURNED TO SERVICE.

Part: DOOR — MULTIPLE FAIL · airframe 18,272 hrs · 19,494 cycles

AFT GALLEY SERVICE DOOR IS DIFFICULT TO OPEN. REMOVED AND REPLACED THE IDLER LINK AND PIVOT ASSY BEARINGS. REMOVED AND REPLACED VENT DOOR SPRINGS AND HANDLE SHAFT GUIDE ASSY. CHECKED GOOD. RETURNED TO SERVICE.

Part: CONTROLLER — FAILED (NR 2 PROPELLER) · airframe 18,057 hrs · 19,262 cycles

POWERPLANT MESSAGE ON ED AT CRUISE. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND FAULT IN EMU NR 2 PROP 12B, 456A & B, 30B. UNABLE TO CLEAR FAULTS. REMOVED AND REPLACED NR 2 PEC IAW AMM TASK 61-20-36-000-801, AND 61-20-36-400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 18,050 hrs · 19,255 cycles

EMERGENCY LIGHT IS LOOSE. SECURED THE LIGHT. ACFT OK FOR SERVICE.

Part: AILERON — ICED (RIGHT) · airframe 18,029 hrs · 19,238 cycles

AFTER ENGINE START, RELEASED THE CONTROL LOCK AND PERFORMED A CONTROL CHECK IAW NORMAL PROCEDURES, DISCOVERED A ROLL CONTROL BIND. PULLED THE ROLL DISCONNECT AND DISCOVERED THE CAPTAIN'S CONTROLS ARE FREE BUT THE FO'S CONTROLS ARE STILL BINDING. ON ARRIVAL, PERFORMED GVI OF FLIGHT CONTROLS, FOUND ICE ACCUMULATION ON THE RT AILERON AND RT WING TIP AREA. REMOVED ICE AND INSPECTED AREA FOR DAMAGE. NONE NOTED. INTERROGATED CDS, NO FAULTS LOGGED. PERFORMED OPERATIONAL TEST OF THE AILERON CONTROL SYSTEM IAW AMM TASK 27-10-00-710-801. SYSTEM CHECKED GOOD. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED IAW GPM 9.2. RETURNED TO SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (COCKPIT) · airframe 17,835 hrs · 19,013 cycles

WHEN APU BLEED AIR IS TURNED ON, THE LAV SMOKE DETECTOR GOES OFF AFTER ABOUT 3 MINUTES. ONCE BLEED AIR IS TURNED OFF DETECTOR STOPS AFTER ABOUT 2 MINS. RAN APU WITH BLEED AIR ON FOR APPROX 1 HR. SET ECS TO FULL HOT THEN PREFORMED AN ECS PURGE ENGINE RUN. NO ODOR, THE LAV SMOKE DETECTOR DID NOT GO OFF. CHECKED CDS FOR FAULTS. NO FAULTS. CHECKED APU OIL LEVEL. OIL LEVEL NORMAL. CHECKED APU EXTERNAL FOR LEAKS. NO LEAKS NOTED. APU AND BLEED AIR SYSTEM OPS NORMAL. COULD NOT DUPLICATE.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 17,622 hrs · 18,795 cycles

DURING PREFLIGHT, NR 2 PROP DID NOT APPEAR TO BE FULLY FEATHERED. REMOVED THE NR 2 OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801. REPLACED #2 ENGINE OSG IAW AMM TASK 61-20-26-400-801. OPS TEST GOOD. LEAK CHECK GOOD. PERFORMED FUNTIONAL TEST OF PROP TIME TO UNFEATHER IAW AMM TASK 61-20-00-720-801, FUNCTIONAL TEST GOOD. PERFORMED #2 PROP FEATHER CHECK IAW AMM TASK 71-00-00-868-819, CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 17,595 hrs · 18,768 cycles

EMERGENCY POWER SUPPLY PS1 ILLUMINATE AFTER POWER TURNED OFF & SWITCH IN THE OFF POSITION. R & R THE POWER SUPPLY IAW AMM 33-51-01-000/400-801. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

RT IB AFT SEAT TRACK 15 FROM FS 612.00 TO FS 670.00, RBL 10 CORRODED BEYOND LIMITS. RT IB AFT SEAT TRACK 15 FROM FS X612.00 TO FS X670.0 RBL 10 REMOVED IAW SRM 51-41-05. NEW SEAT RAIL 15 PN 85338210-115 DRILLED IAW SRM 51-40-07. NEW SEAT RAIL 15 PN 85338210-115. INSTALLED FROM FS X 612.0 TO FS X670 RBL 10 IAW SRM 51-42-05. SRM 51-40-15 AND SRM 51-41-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

LT OB SEAT RAIL 2 IS CORRODED BEYOND LIMITS IAW SRM 53-20-49 REPAIR 02. LT OB SEAT RAIL 2 REMOVED IAW SRM 51-42-05, 51-42-45,51-40-15, 51-41-15. TEMPLATED DAMAGED LT OB SEAT RAIL 2 FROM FS 229.50 TO 571.50 & TRANSFERRED HOLES TO NEW RAIL PN 85361561-103SP IAW SRM 51-40-07-02-01. NEW SEAT RAIL 2 PN 85361561-103SP. INSTALLED FROM FS X229.50 SRM 51-40-15 AND SRM 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

LT AFT INBD AFT CARGO SEAT RAIL 9 FROM FS 670.0 TO FS 782.0 LBL 10 CORRODED BEYOND LIMITS. REMOVED LT AFT INBOARD SEAT RAIL 9 FROM FS X670.0TO FS X 782.0 LBL 10 IAW SRM 51-42-05, 51-41-00. NEW SEAT RAIL 9 PN 85338210-111 DRILLED USING TEMPLATE IAW SRM 51-40-07-02-01. NEW SEAT RAIL 9 PN 85338210-111 INSTALLED FROM FS X670 TO FS X782.0 LBL 10 IAW SRM 51-42-05 AND SRM 51-40-15. ALT FASTENERS INSTALLED ON TOP FLANGE FROM FS X 670 TO FS X 714 COMMON TO WEB REFERENCE TASK CARD RD 8/4-53-7852 FOR WORK ACCOMPLISHMENT.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

PAX DOOR THRESHOLD MEMBER CORRODED BEYOND LIMITS AS PER SRM 53-20-23 REPAIR 02. PAX DOOR THRESHOLD MEMBER PN 85329539-105 REPLACED IAW SRM 51-42-05.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

FWD BAGGAGE DOOR LWR SILL THRESHOLD CHANNEL AND PLATE CORRODED BEYOND LIMITS. REMOVED FWD BAG SILL PANEL PN 85329603-101 AND LWR EDGE CHANNEL ASSY PN 85329603-101 AND LWR EDGE CHANNEL ASSY PN 85329604-001 IAW SRM 51-40-07-02-01, 51-42-05 AND 51-42-45-02-01. INSTALLED NEW FWD BAG SILL AND LWR EDGE CHANNEL ASSY IAW SRM 51-42-05, 51-40-15, 51-40-10, 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

RT OB FWD SEAT TRACK 18 FROM FS 102.50 TO FS 229.50 RBL 40 CORRODED BEYOND LIMITS. REMOVED 18 SEAT TRACK (RT OUTBD FWD CABIN) FROM FS 102.50 TO FS 229.50 RBL 40 IAW SRM 51-40-15, 51-42-05 AND 51-42-45. DRILLED USING TEMPLATE NEW SEAT RAIL 18 PN 85328261-105SP IAW SRM 51-40-NEW SEAT RAIL PN 85328261-105SP SEAT RAIL 18 INSTALLED AT FS 102.50 TO FS 229.50 RBL 40 IAW SRM 51-40-15, 51-42-05 AND 51-42-45.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,591 hrs · 18,767 cycles

LH IB FWD SEAT TRACK #5 FROM FSX 39.00 TO FSX 102.50 LBL 10 CORRODED BEYOND LIMITS. LH FWD INBD CABIN SEAT RAIL #5 FROM FSX-39 TO FS X 102.50 LBL 10 REMOVED IAW SRM 51-42-05, 51-40-15 (HI-LITES) AND 51-41-00 (BOLTS). TEMPLATED OLD LH FWD INBD SEAT RAIL #5 FROM FS X-39 TO FSX 102.50 LBL 10 & TRANSFERED HOLES TO NEW RAIL PN 85328210-119 IAW SRM 51-40-07-02-01. LH FWD INBD CABIN SEAT RAIL #5 PN 85328210-199 FROM FS X -39 TO FS X 102.50 LBL 10 INSTALLED NEW IAW SRM 51-42-05 (RIVETS), 51-40-15 (HI-LITES) AND SRM 51-41-00 (BOLTS).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,591 hrs · 18,767 cycles

RT OB MID CABIN SEAT TRACK 19 FROM FS 229.50 TO FS 571.50, RBL 40 CORRODED BEYOND LIMITS. RT OB MID CABIN SEAT TRACK 19 REMOVED IAW SRM 51-42-05, 51-42-45, 51-40-15-51-41-15. NEW SEAT RAIL 19 PN 85361561-104SP DRILLED USING TEMPLATE IAW SRM 51-40-07. NEW RT OB MID CABIN SEAT TRACK 19 PN 85361561-104SP INSTALLED FROM FS 229.50 TO FS 571.50 RBL 40 IAW SRM 51-40-15, 51-42-05 AND 51-42-45.

Part: SEAT TRACK — CORRODED · airframe 17,591 hrs · 18,767 cycles

LH IB AFT SEAT TRACK (SEAT RAIL #25) FROM FSX 668.00 TO FSX 698.00 CORRODED BEYOND LIMITS. REMOVED SOLID & CHERRY MAX RIVETS FROM LH IB AFT SEAT TRACK FROM FSX 668.00 TO FS X698.00 IAW SRM 51-42-05-02-01 & 51-42-45-02-01. TEMPLATED RIVET HOLES FROM OLD PART TO NEW SEAT RAIL #25 IAW SRM 51-40-07-02-01. RE-INSTALLED SOLID & CHERRY MAX RIVETS AND NEW LH IB AFT SEAT TRACK PN# 85337843-103 SP IAW SRM 51-42-05-02-01 & 51-42-454-02-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,591 hrs · 18,767 cycles

RH IB FWD SEAT TRACK #11 FROM FSX 10.50 TO FSX 102.50 RBL 10 CORRODED BEYOND LIMITS. RH IB FWD SEAT TRACK 11 FROM FSX 10.50 TO FSX 102.50 RBL 10 REMOVED IAW SRM 51-42-05 (RIVETS) SRM 51-40-15 (HI-LITES) AND SRM 51-41-00. TEMPLATES OLD RH IB FWD SEAT TRACK #11 FROM FSX 10.50 TO FSX 102.50 RBL 10 AND TRANSFERRED HOLES TO NEW RAIL PN 85328210-115 IAW SRM 51-40-07-02-01. RH IB FWD SEAT TRACK #11 FROM FSX 10.50 TO FSX 102.50 RBL 10 INSTALLED IAW SRM 51-42-05 (RIVETS), SRM 51-40-15 (HI-LITES) AND SRM 51-41-00 (BOLTS).

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 17,591 hrs · 18,767 cycles

AFT BAGGAGE FLOOR SHEAR ANGLE @ X 783.102 IS CORRODED. AFT BAGGAGE FLOOR SHEAR WEB ANGLE FSX 783.102 REMOVED & NEW ANGLE PN 85339286-115 INSTALLED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 17,591 hrs · 18,767 cycles

RH IB FWD SEAT TRACK #12 FROM FSX 102.50 TO FSX 228.50 RBL 10 CORRODED BEYOND LIMITS. RH IB FWD SEAT TRACK #12 FROM FSX 102.50 TO FS X 228.50 RBL 10 REMOVED IAW SRM 51-42-05 (RIVETS) SRM 51-40-15 (HI-LITES) AND SRM 51-41-00 (BOLTS). TEMPLATE OLD RH IB FWD SEAT TRACK #12 FROM FSX 102.50 TO FSX 228.50 RBL 10 AND TRANSFERRED HOLES TO NEW RAIL PN 85328210-112 IAW SRM 51-40-07-02-01. RH IB FWD SEAT TRACK #12 FROM FSX 102.50 TO FSX 228.50 RBL 10 INSTALLED IAW SRM 51-42-05 (RIVETS), SRM 51-40-15 (HI-LITES) AND SRM 51-41-00 (BOLTS).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 17,591 hrs · 18,767 cycles

RH IB FWD SEAT TRACK (RAIL #10) FROM FSX 39.00 TO FSX 10.50, RBL 10 CORRODED BEYOND LIMITS. RH IB FWD SEAT TRACK (RAIL #10) FROM FSX 39.00 TO FSX 10.50, RBL 10 REMOVED IAW SRM 51-42-05 (SOLIDS), 51-40-15 (HI-LITES) & 51-41-00 (BOLTS). TEMPLATED OLD RH IB FWD AT TRACK (RAIL #10) FROM FSX-39.00 TO FSX 10.50, RBL 10 & TRANSFERRED HOLES TO NEW RAIL PN 85328210-121 IAW SRM 51-40-07-02-01. RH IB FWD SEAT TRACK (RAIL #10) FROM FSX -39.00 TO FSX 10.50, RBL 10 INSTALLED NEW IAW SRM 51-42-05 (RIVETS), 51-40-15 (HI-LITES) & 51-41-00 (BOLTS).

Part: BRAKE — CONTAMINATED (RT MLG) · airframe 16,802 hrs · 17,952 cycles

RIGHT INBOARD BRAKE WAS SMOKING AFTER LANDING. NORMAL BRAKING USED AT LANDING. REMOVED THE NR 3 TIRE AND FOUND GREASE ON INSIDE OF THE HUB AND BRAKE. ALSO INNER GREASE SEAL HAD DISLOGDED. REPLACED TIRE ASSEMBLY. RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 16,197 hrs · 17,293 cycles

DURING EMERGENCY LIGHT FUNCTIONAL CHECK, FOUND FORWARD EMERGENCY LIGHTS UNABLE TO STAY ON. REPLACED LT AND RT NR 1 BATTERY PACKS IAW AMM 33-51-00. CHECKS GOOD.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 15,997 hrs · 17,077 cycles

EMERGENCY LIGHT STRIP AT ROW 1 IS LOOSE. SECURED THE LIGHT STRIP. CHECKED GOOD. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 15,983 hrs · 17,057 cycles

AFTER ENGINE START NR 1 PROPELLER TOOK AT LEAST 1 MINUTE LONGER TO COME OUT OF FEATHER THAN THE NR 2 ENGINE. PRESSED EVENT MARKER. PROPELLER DID EVENTUALLY COME OUT OF FEATHER ON ITS OWN. NR 1 PROPELLER GREASE LEVEL A LITTLE LOW, SERVICED NR 1 PROP W/GREASE IAW AMM TASK 61-10-00-640-801, TIME TO UNFEATHER NR 1 PROP FAILS IAW AMM TASK 61-10-00-640-801 LONGER THAN 1 MINUTE. R & R NR 1 OSG. R & R NR 1 PROP PISTON SEAL. NR 1 PROP GOES TO FEATHER AS REQUIRED AND COMES OUT OF FEATHER AS REQUIRED.

Part: CONDITION LEVER — MALFUNCTIONED · airframe 15,909 hrs · 16,966 cycles

DURING T/O ROLL, RT ABOUT 80 KTS, WE HEARD A BEEP, FOLLOWED BY THE T/O WARNING HORN A FEW SECONDS LATER. ABORTED THE T/O AROUND 90 KTS USING REVERSE POWER AND MODERATE BRAKING. THE T/O WARNING TEST WAS NORMAL DURING TAXI OUT AND AFTER RUNNING THE E & A CHECKLIST. THE ACFT CONFIGURATION WAS CORRECT AND THERE WERE NO OTHER ASSOCIATED CAUTIONS OR WARNINGS. OP'S CHECK OF TAKEOFF WARNING SYSTEM, R & R OF CONDITION QUADRANT, R & R NR 1 IOP. OP'S TEST GOOD. R & R NR 1 IOP, PERFORMED LLM RTS TEST IAW MAINTENANCE 6314101. RETURNED TO SERVICE.

Part: PROCESSOR — MALFUNCTIONED (INPUT OUTPUT) · airframe 15,638 hrs · 16,678 cycles

TAKEOFF WARNING HORN SOUNDED AS POWER WAS ADVANCED FOR TAKEOFF. TEST WAS SUCESSFUL AND ALL PARAMETERS WERE SET NORMAL. REPLACED THE NR 2 INPUT-OUTPUT PROCESSOR IAW MAINTENANCE 6314101. OPS CHECKS GOOD IAW AMM 31-41-00-710-802. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PROP DE ICE) · airframe 15,638 hrs · 16,678 cycles

TAKEOFF WARNING HORN ON TAKEOFF ROLL. ALL ITEMS IN PROPER CONFIGURATION MAX AIRSPEED 48 KNOTS WITH LIGHT BRAKING FLAPS AT 15 DEGREES SLOWING TO 10 KNOTS WE GOT A PROP DE-ICE CAUTION. AFTER CLEARING THE RUNWAY AND JOINING THE TAXIWAY THE PROP DE-ICE CAUTION WENT OUT. PERFORMED FUNCTIONAL TEST OF THE TAKEOFF AND WARNING SYS. REF AMM 31-52-00-720-801. SYS OPERATES AS DESCRIBED. FUNCTIONAL TEST OF T/O WARN SYS GOOD. PERFORMED THE FUNCTIONAL TEST OF THE PROP DE-ICE SYS. SYSTEM OPERATES AS DESCRIBED. FUNCTIONAL CHECK GOOD. REF AMM 30-61-00-720-801. PROP DEICE CAUTION DID NOT RETURN. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: PROPELLER — VIBRATION (NR 2) · airframe 15,060 hrs · 16,064 cycles

ENROUTE, ONCE CLEAR OF ICING CONDITIONS WE PICKED UP CONSTANT STRONG VIBRATION FROM BOTH ENGINES. AIRFRAME MODE SELECT SWITCH WAS SET TO FAST WITH ENGINE INTAKE BYPASS DOORS OPEN. ALL INDICATIONS ON ED WERE NORMAL. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. AFTER DISCOVERED MULTIPLE CHUNKS OF ICE ON THE RUNWAY AFTER LANDING AND WERE ON RAMP AFTER PARKING. ALL AIRFRAME AND PROP DEICE INDICATIONS WERE NORMAL. VIBRATION CLEARED UP ON APPROACH. C/W INSP AFTER REPORT OF EXCESSIVE OR UNUSUAL VIBRATION TASK 05-50-12-200-801. MINOR REPAIRS WERE REQUIRED ON NR 2 PROP ASSY, NO OTHER DEFECTS NOTED. C/W A/F DEICED OPS CHECK, TASK 30-11-16-710-801, NO FAULTS NOTED. C/W PROP DEICE FUNCTIONAL TEST TASK 30-61-00-720-801. NO FAULTS NOTED. RETURNED TO SERVICE.

Part: BRAKE — OVERHEATED (ZONE 700) · airframe 14,937 hrs · 15,940 cycles

LEFT MAIN GEAR IS PUTTING OFF A WHITE SMOKE, ON POST FLIGHT INSPECTION. DEBRIEFED FLIGHT CREW, DETERMINDED SMALL AMOUNT OF WHITE SMOKE TO BE COMING FROM BRAKE ON NR 2 MLG WHEEL, LT INBD. PERFORMED GVI OF MLG WHEELS, TIRES AND BRAKES. ALL BRAKES ARE APPROXIMATELY THE SAME TEMPERATURE. FLIGHT CREW REPORTS NO UNUSUAL BRAKING CHARACTERISTICS. PERFORMED INSPECTION AFTER APPLICATION OF EXCESS BRAKING. INSPECTION INCLUDES REMOVAL OF MLG WHEEL/TIRE ASSEMBLIES, PERFORMED ON BOTH LT MLG WHEELS ONLY AND FUNCTIONAL CHECK OF MLG BRAKE SYSTEM. ALL CHECKS GOOD, INSPECTION REVEALS NO DEFECTS ON WHEELS/TIRES, BRAKES. INSPECTION PERFORMED IAW AMM 05-50-56-210-801. ACFT RETURNED TO SERVICE.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 14,681 hrs · 15,658 cycles

AFTER TAKEOFF AT GEAR RETRACTION NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. ALT GEAR EXTENSION EXCUTED AND RETURN TO FIELD. LANDING UNEVENTFUL. REPLACED NLG SOLENIOD SEQUENCE VALVE, AND FLUSHED NLG HYDRAULIC LINES, AND REPLACMENT OF GEAR HANDLE. OPS AND LEAK CHECK GOOD. RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CARGO BAY) · airframe 14,458 hrs · 15,434 cycles

F/A REPORTS BURNING ODOR IN AFT GALLEY AREA. F/A SMELL VERIFIED WITH AFT PAX DOOR CLOSED, RECIRCULATING FAN BOTH ON & OFF, BLEED AIR BOTH ON & OFF. ODOR APPEARED TO BE COMING FROM AFT MOST VENTED CEILING PANEL IN AFT GALLEY. UPON FURTHER INVESTIGATING FOUND AFT CARGO AFT LIGHT ASSY HAD PREVIOUSLY BEEN R & R. AFTER REVIEWING EO 6-33-94, IT WAS DETERMINED THAT THE INCORRECT LIGHT BULB HAD BEEN USED SUBSEQUENTLY CAUSING TO MUCH HEAT AND CAUSING THE RTV SEALANT TO GIVE OFF BURNING ODOR. CORRECT LIGHT BULB, 305, WAS INSTALLED AND CURED THE BURNING ODOR. WAS ABLE TO DUPLICATE THE BURNING SMELL NUMEROUS TIMES BY RE-INSTALLING THE INCORRECT LIGHT BULB AND WAITING A FEW MINUTES TO HEAT UP. IT WAS DETERMINED THE NEW LIGHT ASSY PREVIOUSLY INSTALLED HAD INCORRECT BULB INSTALLED IN THE ASSY FROM THE MFG AND IT WASN'T UNTIL WE FOUND THE EO IN THE IPC THAT IT WAS DETERMINED TO BE THE WRONG BULB CAUSING EXCESS HEAT. AS PRECAUTIONARY MEASURE, R & R AFT CARGO LIGHT ASSY WITH CORRECT HARDWARE AND BULB IAW AMM 33-31-01-000-801/400-801 AND MCN'S 63374-01, 63397-1 AND 63375-01.

Part: LIGHT — ARCED (CARGO BAY) · airframe 14,455 hrs · 15,432 cycles

F/A'S REPORT A SLIGHT ELECTRICAL ODOR IN THE AFT MAIN CABIN AROUND ROW 18 AND AFT GALLEY AREA. C/W TROUBLESHOOTING ELECTRICAL ODOR IN THE ACFT REF MCN 62172-01, STEP 1A. FOUND AFT CARGO AFT LIGHT ASSY ARCING WITHIN ASSY. R & R AFT CARGO AFT LIGHT ASSY, REF AMM TASK 33-31-01-000-801, 33-31-01-400-801, OPS CHECK GOOD. GROUND RUN ENGINE AND APU WITH BLEED AIR. NO ELECTRICAL ODOR NOTED IN AFT CABIN. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,375 hrs · 15,360 cycles

HOT PLASTIC ODOR COMING FROM ROW 17 ON BACK FROM THE ACFT, APU, BLEED AIR, RECIRC FAN WERE ALL ON. NO OTHER ODOR WAS NOTICED FORWARD OF THAT AREA. COMPLIED WITH AIR CONTAMINATION CHECKLIST FORM M-744 AND REFERED TO FIM 21-20-00, MCN 62172-01. COMPLIED WITH GVI OF BOTH MAPCO'S, AFT GALLEY CEILING LIGHTS, AFT CARGO COMPARTMENT AND AFT CARGO BAY LIGHTS. NO DEFECTS, ODORS OR DISCOLORATION NOTED. DID FIND FRESH SEALANT APPLIED TO BOTH AFT PASS DOOR AND AFT SERVICE DOOR SUROUNDS, WHICH DO GIVE OFF A SLIGHT ODOR. ONLY ODOR NOTED BY FOUR DIFFERENT MECHANICS. F/A DID NOT HAVE THE AFT GALLEY GASPER OPEN AT TIME OF WRITE UP AND BOTH DOORS CLOSED. NO OTHER DEFECTS NOTED. ACFT OK FOR CONTINUE SERVICE.

Part: TRIM PANEL — MALFUNCTIONED (ZONE 200) · airframe 13,942 hrs · 14,931 cycles

AFTER TAKE OFF, EXPERIENCED A SUDDEN RWD ROLL INPUT THROUGH THE YOKE. HELD WINGS LEVEL MANUALLY. THEN NOTICED AILERON TRIM INDICATED FULL SCALE RWD. RETRIMMED TO NEUTRAL. AILERON TRIM SYS OPERATED NORMALLY FOR THE REST OF THE FLIGHT. REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW AMM TASKS 27-13-16-000-801 & 27-13-16-400-801. OPS CKS ARE GOOD. RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 13,437 hrs · 14,387 cycles

AFT CARGO DOOR WARNING IN FLIGHT LOST PRESSURIZATION. RETURNED TO FIELD. LANDING UNEVENTFUL. UPON ARRIVAL OF ACFT NOTED AFT CARGO PIT DOOR HANDLE POPPED OUT. REMOVED INTERIOR COVER FOR AFT PIT DOOR HANDLE MECHANISM AND PERFORMED GVI OF HANDLE, NO DEFECTS NOTED. OPERATED DOOR SEVERAL TIMES, HANDLE REMAINED SECURE. RE-INSTALLED INTERIOR COVER FOR AFT CARGO PIT DOOR HANDLE MECHANISM. PERFORMED OPS TEST OF AFT BAGGAGE DOOR IAW AMM TASK 52-31-00-710-801, TEST GOOD. PRESSURIZED ACFT TO 5 DIFF. IAW AMM TASKS 21-00-00-863-801 AND 21-00-00-863-802. NO PRESSURE LOSS, NO DOOR WARNING, AFT BAG PIT DOOR HANDLE REMAINED SECURE. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: SEAL — DIRTY (PAX DOOR) · airframe 12,607 hrs · 13,501 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE USING NORMAL PROCEDURES. INSPECTED PAX DOOR SEAL. CLEANED AND LUBED SEAL. PRESSURIZED SEAL. F/A OPEN & CLOSE DOOR, CHECKED GOOD. OK FOR CONTINUED SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 12,492 hrs · 13,375 cycles

AFTER ROTATION, MASTER WARNING FOR CARGO DOOR ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. UPON ARRIVAL AT GATE FOUND AFT CARGO DOOR HANDLE NOT COMPLETLY IN DETENT PERFORMED. OPS TEST OF AFT CARGO DOOR IAW AMM TASK 52-31-00-710-801. NO DEFECTS NOTED GROUND PRESSURIZED ACFT IAW AMM TASK 21-00-00-863-801 AND 21-00-00-863-802 NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,332 hrs · 13,219 cycles

FWD F/A'S EMERGENCY LIGHT SWITCH "ON" PORTION BURNED OUT. RELAMPED FWD F/A EMERGENCY LIGHTS SWITCH. LAMPS TEST GOOD. RETURNED TO SERVICE.

Part: RUB STRIP — WORN (FLAP TRACK) · airframe 11,802 hrs · 12,657 cycles

LEFT INBD FLAP, NR 1 FLAP TRACK FWD AND AFT RUB PADS WORN. REMOVED WORN PADS IAW AMM 27-54-01-000-802, STEPS 4A(1)-(3) 4C(1)-(2) & 4F(1)-(2) 4D(1)-(3). INSTALLED NEW RUB PADS IAW AMM 27-54-01-400-802 STEPS 3B(1)-(4) 4E(1)-(4) & 4I(1)-(7) 4C(1)-(7).

Part: SEAT TRACK — CORRODED (NR 2) · corrosion level 2 · airframe 11,802 hrs · 12,657 cycles

NR 2 SEAT TRACK CORRODED OUT OF LIMITS. . REMOVED SEAT TRACK IAW SRM 51-42-05 AND INSTALLED NEW IAW SRM 51-42-05, SRM 51-40-15, SRM 51-42-45, & SRM 51-40-07.

Part: SEAT TRACK — CORRODED (NR 8) · airframe 11,802 hrs · 12,657 cycles

NR 8 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01, STEP 4E, 1 THRU 7, 51-40-15-02-01 [TR51-020] STEP 6, M 1 THRU 4, SRM 51-40-07, STEP 5, B 1 THRU 6, SRM 51-42-05-02-01, STEP 4D, 4 THRU 9, SRM 51-40-15 AND SRM 51-42-05.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 11,802 hrs · 12,657 cycles

NR 10 SEAT TRACK CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00, PG 1, 51-42-05 IAW 4E 51-40-15, PER 6H2.

Part: SEAT TRACK — CORRODED (NR 7) · airframe 11,802 hrs · 12,657 cycles

NR 7 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05, REPAIR-01, SRM 51-40-15 REPAIR-01, SRM 51-41-00 F AND SRM 51-40-07.

Part: SKIN — CORRODED (FUSELAGE) · airframe 11,802 hrs · 12,657 cycles

LAVATORY SERVICE PANEL LIP SKIN HAS CORROSION. REMOVED CORROSION IAW SRM 52-42-10, PAR 1A AND FIG 201 SHT 2. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND SRM 51-25-10-02-01. FILLED THE BLEND OUT FLUSH WITH EPOXY ADHESIVE IAW SRM 52-42-10 STEP 7A(6). APPLIED TOP COAT TO REPAIRED AREA IAW SRM 51-25-05, ITEM (F) 1-8.

Part: DOOR SILL — CORRODED (EMERGENCY EXIT) · airframe 11,802 hrs · 12,657 cycles

EMERGENCY EXIT LOWER SILL EDGE BEAM SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED THE SILL BEAM IAW SRM 51-42-05, SRM 51-41-00, SRM 51-40-05, AND 51-42-05.

Part: STOP FITTING — CORRODED (EMERGENCY EXIT) · airframe 11,802 hrs · 12,657 cycles

EMERGENCY EXIT LOWER DOOR STOP FITTINGS AND SERRATED PLATES SHOW SIGNS OF CORROSION. REMOVED STOP FITTINGS FWD AND AFT IAW SRM 51-41-00. INSTALLED NEW STOP FITTINGS FWD AND AFT IAW SRM 51-41-00. REMOVED SERRATED PLATES IAW SRM 51-41-00. INSTALLED NEW SERRATED PLATES FWD AND AFT IAW SRM 51-41-00.

Part: GUSSET — CORRODED (EMERGENCY EXIT) · airframe 11,802 hrs · 12,657 cycles

EMERGENCY EXIT DOOR LOWER GUSSETS SHOW SIGNS OF CORROSION AT BS 78.20 AND 88.30. REMOVED THE GUSSETS IAW SRM 51-40-05. INSTALLED NEW GUSSETS IAW SRM 51-42-05 & SRM 51-42-45.

Part: SEAT TRACK — CORRODED (NR 1) · airframe 11,802 hrs · 12,657 cycles

NR 1 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-15, 51-42-05 & 51-42-45, SRM 51-40-07, DRAWING 85328251, REV A, SRM 51-42-05, STEP 4D, & SRM 51-40-15.

Part: SEAT TRACK — CORRODED (NR 19) · airframe 11,802 hrs · 11,657 cycles

NR 19 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-05 REPAIR -1, SRM 51-40-15, REPAIR -01, SRM 51-42-05, REPAIR -01, AND DWG 85361551, REV-B.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 11,802 hrs · 12,657 cycles

FWD PAX DOOR THRESHOLD SHOWS EVIDENCE OF CORROSION. REMOVED THRESHOLD IAW SRM 51-42-05 AND INSTALLED NEW IAW SRM 51-42-05 AND SRM 51-40-07.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 11,802 hrs · 12,657 cycles

FWD PAX DOOR FWD ANGLE AT STA X6.7 STR 25 SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED ANGLE IAW SRM 51-42-05, SRM 51-42-05-02-01, STEP 4D (3-10), SRM 51-40-07 AND SRM 51-40-15, STEP 6 H2.

Part: ANGLE — CORRODED (FWD PAX DOOR) · airframe 11,802 hrs · 12,657 cycles

FWD PAX DOOR AFT ANGLE AT STA 26.7 SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED ANGLE IAW SRM 51-42-05, SRM 51-42-05-02-01, STEP 4D (3-10), SRM 51-40-07, & SRM 51-40-15.

Part: ANGLE — CORRODED (FWD PAX DOOR) · airframe 11,802 hrs · 12,657 cycles

FWD PAX DOOR FWD ANGLE AT STA 6.7 STRINGERS 23-25 SHOW EVIDENCE OF CORROSION. REMOVED AND REPLACED ANGLE IAW SRM 51-42-05, SRM 51-42-05-02-01, STEP 4.D(3-10) AND SRM 51-40-07.

Part: ANGLE — CORRODED (FWD PAX DOOR) · airframe 11,802 hrs · 12,657 cycles

FWD PAX DOOR AFT ANGLE AT STA 26.7 STRINGERS 23-25 SHOWS EVIDENCE OF CORROSION. REMOVED AND REPLACED ANGLE IAW SRM 51-42-05, SRM 51-42-05-02-01, STEP 4.D(3-10), AND SRM 51-40-07.

Part: MODULE — MALFUNCTIONED (FLT MANAGMENT) · airframe 11,341 hrs · 12,151 cycles

WITH AUTOPILOT ENGAGED AND NAVIGATING DIRECTLY TO FMG VOR, AND DESCENDING AT APROXIMATELY 1700 FT PER MINUTE, A MOMENTARY AILERON MISTRIM MESSAGE APPEARED AND THE AIRPLANE BEGAN TO GO INTO A 15-20 DEGREE RT BANK AND PROCEED OFF COURSE. AFTER DISCONECTING THE AUTOPILOT THE AIRPLANE RESISTED MANUAL ROLL CONTROL FROM ME FOR ABOUT 1-2 SECONDS AND THEN ROLL CONTROL BECAME NORMAL AND THE AIRPLANE FLEW NORMALLY HAND-FLOWN. THE FMS COMMAND BARS GAVE PROPER COMMANDS TO CORRECT COURSE DURING THIS EVENT WHICH LASTED 5-8 SECONDS. LANDING UNEVENTFUL. INTERROGATED CDS, NO CURRENT FAULT OR FAULTS IN HISTORY FOUND. PERFORMED FREEDOM OF MOVEMENT CHECK IAW AMM TASK 27-10-00-710-801, 27-13-00-710-802, AND 27-61-00-710-801. ALL CONTROL SURFACES HAVE FULL MOVEMENT OF TRAVEL. FERRIED AIRCRAFT. C/W TO 201405051546, WIRING CHECKS GOOD. REMOVED FGM 1 IAW TC 6221101. INSTALLED SERVICEABLE FGM IAW TC 6221101. PERFORMED LLM RTS TEST IAW TASK CARDS 6221101 FOR NR 1 AND NR 2 FGM'S. RETURNED TO SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 11,297 hrs · 12,106 cycles

THE ACFT FAILED TO FOLLOW AN FMS RIGHT TURN TO DOWNWIND AT SEA. ONE SECOND LATER THE AUTOPILOT DISCONNECT WARNING SOUNDED WITH ASSOCIATED LIGHTS. A/P DISCONNECT BUTTON WAS PUSHED TO SILENCE THE WARNING WHILE AN ATTEMPT TO FLY THE ACFT BACK ON COARSE BY HAND WAS NEGOTIATED BY THE CONTROLS BEING LOCKED. NUMEROUS ATTEMPTS AT PUSHING THE A/P DIS BUTTON ON THE YOKE DID NOT RELEASE THE CONTROLS. ONE SECOND LATER THE ACFT WAS IN A 5 DEGREE LEFT BANK AND STILL DECENDING WITH THE CONTROLS LOCKED. APPROXIMATLY 5 SECONDS LATER THE CONTROLS ABRUPTLY RELEASED WITH A RIGHT TURN AND FLEW NORMALLY TO TOUCHDOWN. NO CAUTION OR WARNING LIGHTS ILLUMINATED ON THE ANNOUNCIATOR PANEL OTHER THAN ASSOCIATED WITH A/P DISCONNECT, AND THE A/P WAS NEVER RE-ENGAGED. R & R ROLL ACTUATOR CAPSTAN & ROLL ACTUATOR, PERFORMED GVI OF AILERON CABLES. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL & VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED. OPS CHECK FLIGHT GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 10,790 hrs · 11,534 cycles

F/A REPORTS SMALL PIECE OF EMERGENCY LIGHT DETACHED. CLEANED FLOOR AND APPLIED EMERGENCY LIGHT STRIP IN FRONT OF SEAT 2D. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (SEAT 2D) · airframe 10,758 hrs · 11,500 cycles

EMERGENCY LIGHT LOOSE BY SEAT 2D. REPLACED EMERGENCY LIGHT. RETURNED TO SERVICE.

Part: ROD END — CORRODED (EMERGENCY EXIT) · airframe 9,956 hrs · 10,626 cycles

LOWER EMERGENCY EXIT DOOR FORWARD SHOOT BOLT ROD END AND HARDWARE HAS CORROSION. REPLACED ROD END AND HARDWARE IAW TASK 52-23-01-400-801.

Part: SWITCH — FAILED (PITCH TRIM) · airframe 9,852 hrs · 10,515 cycles

PITCH TRIM CAUTION ON TAKEOFF, ABORTED TAKEOFF AT ABOUT 60 KNOTS. REPLACED PILOTS PITCH TRIM SWITCH. RETURNED TO SERVICE.

Part: HINGE — WEAK (STOWAGE BOX) · airframe 9,747 hrs · 10,405 cycles

F/A REPORTED THE STOWAGE COMPARTMENT DOOR UNDER THE JUMPSEAT WILL NOT "SPRING" CLOSED. REPLACED BOTH SPRING HINGE ASSEMBLIES AS REQUIRED, CHECKS NORMAL. REF CMM 25-21-47, RETURNED TO SERVICE.

Part: COVER — BROKEN (LIGHT SWITCH) · airframe 9,585 hrs · 10,232 cycles

SAFETY COVER ON EMERGENCY LIGHT SWITCH BROKEN. REPLACED COVER. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 9,585 hrs · 10,231 cycles

SAFETY COVER ON EMERGENCY LIGHTING BROKEN. R & R SAFETY GUARDING COVER ON EMERGENCY LIGHTING SWITCH. OPS CHECK OF SWITCH GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (PROPELLER) · airframe 8,842 hrs · 9,437 cycles

NR 1 PROPELLER WILL NOT COME OUT OF FEATHER AFTER ENGINE START. INTERROGATED CDS. NO FAULTS. PERFORMED FUNCTIONAL TEST OF PROPELLER TIME TO UNFEATHER IAW AMM 61-20-00-720-801 AND OPS TEST OF PROPELLER OVERSPEED GOVERNOR IAW AMM 61-20-00-710-803. BOTH OPS & FUNCTIONAL TEST GOOD. PROP NR 1 UNFEATHERS AND FEATHERS WITHOUT FAIL NUMEROUS TIMES. PROPELLER ALSO UNFEATHERS NORMALLY WITH MANUAL UNFEATHER. COULD NOT DUPLICATE PROBLEM. AS PRECAUTIONARY MEASURE REMOVED OSG IAW AMM 61-20-26-000-801. INSTALLED SERVICEABLE OSG IAW AMM 61-20-26-400-801 AND HS 61-0038. OPS TEST GOOD. NO FAULT CODES NOTED. RETURNED TO SERVICE.

Part: BULKHEAD — SCRATCHED · airframe 8,617 hrs · 9,178 cycles

ON FWD BULKHEAD, FACING MAIN CABIN DOOR, THE BULKHEAD IS SCRATCHED AND CUT SHOWING POSSIBLE CONTACT WITH MAIN CABIN DOOR. R & R FORWARD DRAFT BULKHEAD IAW AMM 25-24-06. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,871 hrs · 8,374 cycles

F/A EMERGENCY LIGHT SWITCH LIGHT INOPERATIVE. LAMPED AND OPS TESTED GOOD. RETURNED TO SERVICE.

Part: TMU — MALFUNCTIONED (DE ICE SYS) · airframe 7,609 hrs · 8,105 cycles

DE-ICE PRESSURE CAUTION ILLUMINATED. DE-ICE PRESSURE NORMAL. DE-ICE PRESSURE CAUTION ILLUMINATION ERRATIC THROUGH ALL CYCLES. DIVERTED, LANDING UNEVENTFUL. ATTEMPTED TO RETRIEVE CDS DATA. UNABLE TO ACCESS ICE PROTECTION SYS. (REF FIM 30-10-00-801). GROUND RAN ENGINE AND PERFORMED TEST OF AIRFRAME DEICE SYS IAW AMM 30-11-00-720-801. SYS CHECKED GOOD IN MANUAL MODE. DOES NOT OPERATE IN AUTO MODE. INSPECTED C/P'S AND WIRING AT TMU. NO DEFECTS FOUND. R & R TMU IAW A30-11-01-000-801 & 30-11-01-400-801. NO FAULTS IN CDS. SYS TEST GOOD. RETURNED TO SERVICE. COULD NOT DUPLICATE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 7,408 hrs · 7,899 cycles

F/A REPORTS "EMERGENCY LIGHTING' GUARDED SWITCH LIGHT "NORMAL" SEGMENT IS NOT GREEN AS IT SHOULD BE. R & R FWD EMERGENCY LIGHT SWITCH IAW AMM TASK 33-51-05-000-801/400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,812 hrs · 7,310 cycles

SEVERAL CENTER AND FORWARD OVERHEAD SIGN BULBS ARE INOPERATIVE. RELAMPED.

Part: SWITCH — DAMAGED (EMERGENCY LIGHTS) · airframe 6,730 hrs · 7,223 cycles

EMERGENCY LIGHT SWITCH COVER ADJACENT TO FWD F/A JUMP SEAT DAMAGED. R & R MAPCO SWITCH COVER BY DOOR. OPS CHECK GOOD, A/C OK FOR SERVICE.

Part: AMPLIFIER — MALFUNCTIONED (ZONE 200) · airframe 6,382 hrs · 6,867 cycles

CHECK FIRE DET MASTER WARNING LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED NR 1 FAULT A AND FAULT B LIGHTS ILLUMINATED. R & R FIRE CONTROL AMPLIFIER IAW AMM 26-10-01-000-801 AND 26-10-01-400-801. C/W OP TEST OF NACELLE FIRE DETECTION SYS, BAGGAGE SMOKE DETECTORS, APU FIRE DETECTION SYS, AND OP CHECK OF THE FUEL AND HYD SHUTOFF VALVES. ALL SYS OP TEST GOOD. MASTER WARNING CHECK FIRE DET & NR 1 FAULT A & B LIGHTS EXTINGUISHED. RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED · airframe 5,878 hrs · 6,339 cycles

SEAT TRACK 5 HAS MINOR CORROSION AFT OF STATION 32.4. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE. ALODINED AREA. APPLIED ADHESIVE IAW RD 8/4-53-44.

Part: SKIN — DAMAGED (CENTER WING) · airframe 5,878 hrs · 6,339 cycles

FRETTING DAMAGE ON CENTER WING PANEL 262HT BOTTOM L/E. REMOVED DAMAGE IAW RD 8/4-53-521. CONFIRMED CRACK FREE AND WITHIN LIMITS. REINSTALLED CAMLOCK FASTENERS.

Part: MOUNT BRACKET — CORRODED (WING) · airframe 5,878 hrs · 6,339 cycles

FRETTING DAMAGE ON CENTER WING T/E MOUNTING BRACKET FOR PANEL 262HT. REMOVED FRETTING DAMAGE IAW RD 8/4-53-457 ISSUE 2. MATERIAL LOSS IS OUTSIDE OF LIMITS AFTER REWORK. FILLED BLENDED AREA WITH EPOXY TO BRING UP TO ACCEPTABLE LIMITS IAW RD 8/4-53-4411. ALODINED AND PRIMED AREA AND APPLIED TEFLON TAPE.

Part: SKIN — CORRODED (BS 94.8-116) · airframe 5,878 hrs · 6,339 cycles

SKIN STRAP AND SPLICE PLATE AT STATION 94.8-116 IS CORRODED AT STRINGER 31P-32P. BLENDED AND REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING MATERIAL WITHIN LIMITS AND CONFIRMED TO BE CRACK FREE. ALODINED PRIMED AND PAINTED EFFECTED AREA.

Part: SKIN — CORRODED (CENTER WING) · airframe 5,878 hrs · 6,339 cycles

CORROSION DAMAGE ON CENTER WING PANEL 262AT BOTTOM L/E. REMOVED DAMAGE IAW RD 8/4/53-521. REMOVED MATERIAL WITHIN LIMITS AND CONFIRMED CRACK FREE. INSTALLED CAMLOC FASTENERS.

Part: FRAME — CORRODED (BS 489.5) · airframe 5,878 hrs · 6,339 cycles

BS 489.5 FRAME FLANGE CORRODED AT STRINGER 31-32P. REMOVED CORROSION IAW RD 8/4-53-234. REMOVED MATERIAL OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLANGE IAW RD 8/4-53-017. CONFIRMED CRACK FREE, ALODINED PRIMED AND PAINTED.

Part: SEAT TRACK — CORRODED (BS 664.5) · airframe 5,878 hrs · 6,339 cycles

SEAT TRACK 15 IS CORRODED AROUND BS 664.5. REMOVED CORROSION, FOUND WITHIN LIMITS OF RD 8/4-53-4406. ALODINED AND FILLED BLENDOUTS.

Part: SEAT TRACK — CORRODED (BS 750-783) · airframe 5,878 hrs · 6,339 cycles

CORROSION ON SEAT TRACK 9 AROUND 2 FASTENER HOLES ON THE LT FLANGE LOCATED AT STATION 750 AND 783. FOUND TO BE OUTSIDE OF LIMITS 100 PERCENT MATERIAL LOSS. REPLACED THE SEAT TRACK IAW SRM 51-42-05-02-01.

Part: FRAME — CORRODED (BS 547) · airframe 5,878 hrs · 6,339 cycles

FRAME BS 547, FLANGES ARE CORRODED AT STRINGER 33-31S. REMOVED RIVETS TO CLEAN UP CORROSION. REMOVED CORROSION IAW RD 8/4-53-2344. REMAINING MATERIAL WITHIN LIMITS AND CONFIRMED CRACK FREE. INSTALLED RIVETS. .

Part: FRAME — CORRODED (BS 489.5) · airframe 5,878 hrs · 6,339 cycles

FRAME 489.5, FLANGE IS CORRODED AT STRINGER 33-32S. REMOVED CORROSION IAW RD 8/4-53-2344. REMOVED MATERIAL WITHIN LIMITS AND CRACK FREE. ALODINED PRIMED AND PAINTED AREA.

Part: FRAME — CORRODED (BS 301) · airframe 5,878 hrs · 6,339 cycles

FRAME 301, FLANGE IS CORRODED AT STRINGER 33-32S. REMOVED CORROSION IAW RD 8/4-53-2344. MATERIAL REMOVED WITHIN LIMITS AND CRACK FREE. ALODINED PRIMED AND PAINTED AREA.

Part: FRAME — CORRODED (BS 321) · airframe 5,878 hrs · 6,339 cycles

FRAME 321, FLANGE IS CORRODED AT STRINGER 33-32S. REMOVED CORROSION IAW RD 8/4/53-2344. REMOVED MATERIAL WITHIN LIMITS AND CONFIRMED CRACK FREE. ALODINED PRIMED AND PAINTED AREA.

Part: FRAME — CORRODED (BS 94.8) · airframe 5,878 hrs · 6,339 cycles

FRAME 94.8, FLANGE IS CORRODED AT STRINGER 31P-32P. BLENDED AND REMOVED CORROSION IAW RD 8/4-53-2344. AREA CRACK FREE AND MATERIAL REMOVED WITHIN LIMITS. ALODINED AREA, PRIMED AND PAINTED.

Part: SEAT TRACK — CORRODED · airframe 5,878 hrs · 6,339 cycles

RT OTBD SEAT TRACK IS CORRODED JUST AFT OF THE EMERGENCY EXIT. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING MATERIAL WITHIN LIMITS. COMPLIED WITH RD 8/4-53-884 ISSUE 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,878 hrs · 6,339 cycles

SEAT TRACK 11 HAS MINOR CORROSION AT STATION 19.4. REMOVED CORROSION IAW SRM 51-21-00-00-02. WITHIN LIMITS AND CONFIRMED CRACK FREE. ALODINED EFFECTED AREA.

Part: SEAT TRACK — CORRODED · airframe 5,878 hrs · 6,339 cycles

RT OTBD SEAT TRACK IS CORRODED AT STA 373.15-388.0. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AREA CRACK FREE. MATERIAL LOSS WITHIN LIMITS.

Part: FRAME — CORRODED (BS 529.5) · airframe 5,878 hrs · 6,339 cycles

FRAME 529.5 FLANGES ARE CORRODED AT STRINGER 33-31S. REMOVED RIVETS FOR ACCESS. REMOVED CORROSION IAW RD 8/4-53-2344. MATERIAL REMOVED WITHIN LIMITS. CRACK FREE. REINSTALLED RIVETS. ALODINED PRIMED AND PAINTED AREA.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 5,878 hrs · 6,339 cycles

CORROSION ON SEAT TRACK 9 AT THE AFT END BOTTOM OF THE CLAW. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND TO THEN BE OUT OF LIMITS. REPLACED SEAT TRACK.

Part: FRAME — CORRODED (BS 604.5) · airframe 5,878 hrs · 6,339 cycles

FRAME 604.5, FLANGE IS CORRODED AT STRINGER 31P-32P. REMOVED RIVETS FOR ACCESS TO AREAS. REMOVED CORROSION IAW RD 8/4-53-2344. MATERIAL REMOVED WITHIN LIMITS AND CRACK FREE. RE-INSTALLED RIVETS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 5,878 hrs · 6,339 cycles

SEAT TRACK 10 HAS MINOR CORROSION AFT OF STA 1. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMOVED AREA WITHIN LIMITS. CRACK FREE. ALODINED AREA, COMPLIED WITH STEP 6 OF RD 8/4-55-2358.

Part: SEAT TRACK — CORRODED (BS 489.5) · airframe 5,878 hrs · 6,339 cycles

RIGHT OTBD SEAT TRACK IS CORRODED AFT OF STA 489.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMOVED MATERIAL WITHIN LIMITS. CONFIRMED CRACK FREE. ALODINE APPLIED.

Part: DOOR — DAMAGED (LT MLG) · airframe 5,878 hrs · 6,339 cycles

LEFT MLG, AFT LEFT DOOR HAS A RIVET WITH THE HEAD MISSING ON THE WHITE RUB PAD. REMOVED DOOR TO FOM, AND REMOVED SCUFF PLATE. REPAIRED IAW IAW RD 8/4-54-048 ISSUE 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 5,878 hrs · 6,339 cycles

FUSELAGE SKIN HAS CORROSION ON MATING SURFACE FOR NR2 VHF ANTENNA. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS .056, CONFIRMED AREA CRACK FREE REF NTM 51-00-02-250-801 AND NDTM 8.2.1. DAMAGE WITHIN LIMITS IAW RD 8/4-53-4415. ALODINED IAW RD 8/4-53-4415.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 5,878 hrs · 6,339 cycles

INTERIOR LOWER FUSELAGE ANTENNA DOUBLER STA 71.2-94.8 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. PERFORMED IT THICKNESS IAW NDTM 51-00-02-250-801. CONFIRMED AREA CRACK FREE REF NTM 51-00-06-910-801. AREA WITHIN LIMITS IAW RD 8/4-53-4415. ALODINED, PRIMED APPLIED ALLUMINIZED PAINT AND AV8 IAW RD 8/4-53-4415.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER FEEL) · airframe 5,506 hrs · 5,944 cycles

WHEN DESCENDING AT HIGH SPEEDS (270KIAS AT 14000') RUDDER APPEARS STIFF ; POPS-FREE. RUDDER OPERATES NORMALLY AT LOWER SPEEDS (IE250 & BELOW). LANDING UNEVENTFUL. INSPECTED AND FOUND RFTU WITH RESISTANCE TO MOVEMENT, REPLACED RUDDER FEEL UNIT AND PERFORMED DETAILED INSPECTION OF THE RUDDER CONTROL SYSTEM, ALL POST MX TEST CHECKED GOOD. TEST FLIGHT OK.

Part: LATCH — LACK OF LUBE (EMERGENCY EXIT) · airframe 4,433 hrs · 4,813 cycles

FWD NR 2 SIDE EMERGENCY EXIT DITCHING DAM HANDLE IS HARD TO OPERATE. CLEANED AND LUBED THE LATCH AND DOOR. OPS CHECKS GOOD. HANDLE OPERATES NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: VALVE — FAILED (ZONE 500) · airframe 3,602 hrs · 3,960 cycles

SUPPLEMENTAL INFORMATION- DEICE PRESS CAUTION LT SECOND BOOT LIGHT REMAINS ILLUMINATED FROM WING TIP. DIVERTED, LANDING UNEVENTFUL. TROUBLESHOT SYS TO NR 1 DDV BEING INOP. REPLACED NR 1 DDV IAW AMM 30-11-16. SYS TESTS GOOD. COMPLETED VISUAL INSP OF L/E DEICE BOOTS. NOTE: LE 513AL AND 331AL R & R DUE TO DETERIORATION OF SEAMS. RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (DE ICE SYSTEM)

DEICE PRESS CAUTION LT SECOND BOOT LIGHT REMAINS ILLUMINATED FRO WING TIP. DIVERTED, LANDING UNEVENTFUL. TROUBLESHOT SYS TO NR 1 DDV BEING INOP. REPLACED NR 1 DDV IAW AMM 30-11-16. SYS TESTS GOOD, COMPLETED VISUAL INSPECTION OF L/E DEICE BOOTS. ( NOTE: LE 513AL AND 331 AL R & R DUE TO DETERIORATION OF SEAMS.)

Part: SPOILER SYS — OUT OF ADJUST · airframe 2,697 hrs · 2,991 cycles

TAKEOFF WARNING HORN ON INTIAL TAKEOFF ROLL FLAPS 15 SPOILERS DOWN ELEVATOR TRIM SET CORRECT CONDITION LEVERS MAX WHEN CONDUCTING CHECKLIST AFTER ABORTED TAKEOFF WARNING HORN AGAIN OCCURED. REPLACED THE FLIGHT/ TAXI SWITCH IAW AMM TASK 27-62-03-000-801 &27-62-03-400-801. NO HELP. FOUND IN CDS RT INBD SPOILER SHOWED +1.10 ADJUSTED RT INBD SPOILER LVDT IAW AMM TASK 27-61-31-830-801. FUNCTIONAL TEST OF THE GROUND SPOILER SYS GOOD IAW AMM TASK 27-62-00-720-801 FUNCTIONAL TEST OF THE TAKE OFF WARNING SYS GOOD IAW AMM TASK 31-52-80-720-802. OK FOR CONTINUED SERVICE.

Part: SWITCH — MALFUNCTIONED (SPOILERS) · airframe 2,697 hrs · 2,991 cycles

AT THE START OF THE TAKEOFF ROLL, RECEIVED A T/O WARNING. ABORTED TAKEOFF. PLACED THE FLIGHT/TAXI SWITCH FOR THE SPOILERS ON MEL 27-60-2. 11/30 MEL CLEARED BY: REPLACING THE FLIGHT/TAXI SWITCH IAW AMM 27-62-03-000-801 AND 27-62-03-400-801 STEPS 1-5(B). COMPLETED THE INSTALLATION OF THE FLIGHT/TAXI SWITCH IAW AMM TASK 27-62-03-400-801 STEPS 5. C THRU E, FUNTIONAL TEST CHECKED GOOD,OK FOR CONTINUED SERVICE.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 2,247 hrs · 2,474 cycles

F/A'S EMERGENCY LIGHT SWITCH WILL NOT ILLUMINATE IN THE "NORMAL" POSITION. RELAMPED THE SWITCH. CHECKS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG DOOR) · airframe 863 hrs · 970 cycles

SEA - ON GEAR EXTENSION, R DOOR LIGHT FLASHED ON AND OFF FOR 10-15 SECONDS BEFORE GOING DARK. LANDING UNEVENTFUL. INSPECTED AND FOUND PSEU FAULT "RGDRCL" GAP TO LARGE. FERRY TO PDX FOR REPAIRS NR 32-61-00-280-801 AND FOUND TO BE LOW AT 7.89 MILIHENRIES. ADJUSTED RGDRCL PROX SENSOR S20 IAW MM TASK NR 32-61-06-830-801. PROX SENSOR S20 INDUCTANCE VALUE NOW GOOD WITH GEAR DOWN AND LOCKED OR UP AND LOCKED. LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM OPERATIONAL TEST GOOD SEVERAL TIMES IAW MM TASK NR 32-31-00-710-801. ALL INDICATIONS NORMAL DURING OPERATIONAL TESTS. RETURNED TO SERVICE.