N427QX

Part: NONE — NONE · airframe 31,364 hrs · 33,730 cycles

CARPET ZD&E NEEDS TO BE GLUED DOWN. POTENTIAL TRIPPING HAZARD. REMOVED FROM SERVICE. RE SECURED CARPET IN THE FRONT. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: NONE — NONE · airframe 31,308 hrs · 33,676 cycles

FUSELAGE DOORS WARNING LIGHT IN FLIGHT. RETURNED TO FIELD. REMOVED FROM SERVICE. FOUND AFT SERVICE DOOR NOT TO BE FULLY CLOSED. CLOSED AFT SERVICE DOOR. NO FURTHER DEFECTS TO BE NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 31,030 hrs · 33,390 cycles

WHEN ADVANCING POWER LEVERS FOR TAKEOFF ROLL, SPLR INBD HYD CAUTION ILLUMNATED. ABORTED TAKEOFF. UNDER MAINTENANCE CONTROL DIRECTION CONDUCTED SPGRG 27-06-01. WHEN SELECTING SPOILER SWITCH FROM FLIGHT TO TAXI, #1 HYD ISO VALVE CAUTION ILLUMINATED. MOMENTARILY. REMOVED FROM SERVICE. ON ARRIVAL TO A/C PERFORMED GVI OF SPOILER QUADRANT AREA (FLAPS DOWN) NO DEFECTS NOTED. OPERATED ROLL SPOILERS ON ELECTRIC PUMP'S NO DEFECTS NOTED. OPERATED AILERONS LEFT AND RIGHT NO DEFECTS NOTED. RAISED AND LOWERED FLAPS NO DEFECTS NOTED. #1 HYD QTY AT 50% SERVICED IAW Q400 TASK 12-10-29-611-801. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 30,797 hrs · 33,151 cycles

EXIT LENS AT TYPE II/III EMERGENCY EXIT FELL OFF. REMOVED FROM SERVICE. RE-SECURED EXIT LENS AT TYPE II/III EMERGENCY DOOR NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 30,382 hrs · 32,732 cycles

FA BREPORTS THE FA EMERGENCY LIGHT BUTTON COVER IS HANGING LOOSE. REMOVED FROM SERVICE. REMOVED FWD FA EMERGENCY LIGHT SWITCH, INSTALLED NEW SWITCH GUARD, RE-INSTALLED EMERGENCY LIGHT PUSH SWITCH IAW Q400 AMM TASKS 20-30-07-000-801 AND 400-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 30,273 hrs · 32,628 cycles

ON ADDING POWER DURING T/O, MASTER CAUTION CHIME,DID NOT SEE ANY CAUTION LIGHTS ILLUMINATE.UPON STOWING SPOILERS AFTER REJECTED TAKEOFF CLEARING RWY,MASTER CAUTION CHIME,AND MOMENTARY LIGHT ILLUMINATE SEE WHICH REDEPLOYED SPOILERS AND STOWED SEVERAL TIMES.CAUTION CHIMED ONCE MORE THEN WORKED AS NORMAL REMOVED FROM SERVICE. COMPLIED WITH FIM TASK 27-60-00-810-804 ROLL SPLR INBD PERFORMED OPS TEST OF THE GRND SPLR SYST27-62-00-710-801 OPS CHECKS GOOD,PERFORMED ALSO FO GRND SPLR SWITCHES IN THE PWR LEVER MODULE 27-62-00-710-803.OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: PEC — MALFUNCTIONED (AUTOFEATHER) · airframe 30,202 hrs · 32,560 cycles

DURING SYSTEMS CHECKS, THE #2 AUTOFEATHER TESTS FAILED. REMOVED FROM SERVICE. INTERROGATED CDS FOUND FAULT CODE 402B #2 PROP. C/W FIM REF : 61-20-09-810-812. REMOVED AND REPLACED PEC FOR #2 ENGINE REF: AMM TASK 61-20-36-000-801, 61-20-36-400-801 PARA 1-5,A AND CMC 671290-001 FOR HEAT SHRINK PROCEDURES. C/W REMAINDER OF STEPS FOR #2 PEC INSTALLATION IAW AMM TASK 61-20-36-400-801 AND REF MTC #6710006 FOR WORK PERFORMED. AUTOFEATHER #2 TESTS GOOD. FAULT CODES DID NOT RE-OCCUR. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST (NR 2) · airframe 30,190 hrs · 32,547 cycles

#2 AUTOFEATHER FAILED TEST FOR DAILY SYSTEM CHECK. REMOVED FROM SERVICE. PERFORMED OPS TEST OF THE PROP AUTOFEATHER SYSTEM IAW Q400 AMM 61-20-00-710-810. OPS TEST PASSED. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (SPOILER LIFT DUM) · airframe 30,099 hrs · 32,450 cycles

PRIOR TO ADDING POWER FOR TAKEOFF, OUTBOARD SPOILERS SPONTANEOUSLY RETRACTED ASSOCIATED INDICATIONS INCLUDED ROLL OUTBD LIGHT EXTINGUISHED (GLARESHIELD) AND MASTER CAUTION & ROLL SPLR OUTBD GND CAUTION ILLUMINATED. PILOT VISUALLY CONFIRMED THAT INBOARD SPOILERS DEPLOYED WHILE OUTBOARD SPOILERS RETRACTED. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED RIGHT HAND SIDE LIFT DUMP VALVES (OUTBOARD) IAW AMM 27-62-01-000/400-801. PERFORMED OPS TEST OF THE GROUND SPOILER SYSTEM IAW AMM 27-62-00-710-801. OPS TEST PASSED. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 29,698 hrs · 32,046 cycles

FA EMERGENCY SWITCH LIGHT DOES NOT ILLUMINATE. REMOVED FROM SERVICE. RE-LAMPED FWD FA EMERGENCY LIGHT SWITCH. SWITCH ILLUMINATES NORMALLY. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST (NR 1) · airframe 29,679 hrs · 32,028 cycles

DURING DAILY SYSTEM CHECK THE NR 1 A/F TEST FAILED. REMOVED FROM SERVICE. CHECKED FOR FAULT CODES, FOUND CODE 494. C/W Q400 FIM 61-20-10-810-826. CODE CLEARED, TEST PASSED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — FAILED (EMERGENCY EQUIP) · airframe 29,665 hrs · 32,010 cycles

FA ADVISES EMERGENCY EQUIPMENT DOOR UNDER FWD FA JUMPSEAT DOES NOT AUTOMATICALLY RETRACT. REMOVED FROM SERVICE. REMOVED AND REPLACED FWD FA UNDER SEAT SPRINGS REF Q400 CMM 25-21-47. OPS CK GOOD AT THIS TIME NO OTHER DEFECTS FOUND AT THIS TIME.

Part: DOOR — FAILED (EMERGENCY EQUIP) · airframe 29,665 hrs · 32,010 cycles

EMERGENCY EQUIPMENT COMPARTMENT DOOR UNDER LEFT REAR FA JUMPSEAT DOES NOT AUTOMATICALLY RETRACT. REMOVED FROM SERVICE. REMOVED AND REPLACED AFT LH SIDE FA UNDER SEAT COMPARTMENT DOOR SPRINGS REF Q400 CMM 25-21-48 OPS CK. GOOD NO OTHER DEFECTS FOUND AT THIS TIME.

Part: CONNECTOR — DAMAGED · airframe 29,383 hrs · 31,725 cycles

IN CRUISE FLIGHT (23,000) MASTER WARNING OCCURRED ALONG WITH "FUSELAGE DOORS". C/W E/A CHECKLIST. PRESSURIZATION REMAINED NORMAL THROUGHOUT FLIGHT. R-2 DOOR SHOWED UNSECURE ON DOORS SYS PAGE OF MFD. APPROXIMATELY 5 MINUTES LATER, MASTER WARNING & FUSELAGE DOOR WARNING EXTINGUISHED. DIVERTED. REMOVED FROM SERVICE. REFERENCE PRODUCTION WORK ORDER 292511 TASK CARD N/R-00001 FOR RE-TERMINATION AND RE-SEATING OF CONTACTS A, B, D, & E IN CONNECTOR 3261-J10 FOR PSEU FAULT: ASDRCL FAULT PROX SENS OPEN". CLEARED PSEU FAULTS. OPENED AND CLOSED AFT SERVICE DOOR SEVERAL TIMES. DOOR INDICATED CORRECTLY IN BOTH OPEN AND CLOSED POSITIONS. NO PSEU FAULTS RETURNED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: FASTENER — UNSECURE (CABIN) · airframe 28,496 hrs · 30,748 cycles

FLASHLIGHT AND LIFE VEST COMPARTMENT UNDER AFT CENTER FA JUMPSEAT DOES NOT SPRING CLOSED. REMOVED FROM SERVICE. RE SECURED SPRING RETAINING HARDWARE AT INBD SIDE OF AFT CTR FA LIFEVEST/FLASHLIGHT COMPARTMENT. DOOR SPRINGS CLOSED AS NORMAL. RETURNED TO SERVICE.

Part: PEC — MALFUNCTIONED (NR 1 PROPELLER) · airframe 28,220 hrs · 30,423 cycles

A/F ARM FAILED ON TAKEOFF ROLL, ABORTED TAKEOFF AT 70 KNOTS. A/F SELECT ONLY. RETURNED TO GATE. REMOVED FROM SERVICE. REMOVED & REPLACED #1 PEC IAW Q400 AMM TASK 61-20-36-000/400-801. PERFORMED OPS TEST OF AUTO FEATHER AND UP TRIM SYSTEM IAW Q400 AMM TASK 61-20-00-946-044. ALL OPS TEST GOOD. RETURNED TO SERVICE.

Part: PEC — MALFUNCTIONED (NR 2 PROPELLER) · airframe 28,206 hrs · 30,407 cycles

AUTOFEATHER FAILS TO TEST PROPERLY. #1 TORQUE SHOWS 100% & #2 TORQUE SHOWS 90% WHEN AUTOFEATHER TEST IS ACCOMPLISHED. POWER LEVERS ARE IN THE DISC POSITION AND AMBER FAILED MESSAGES APPEAR ON BOTH #1 & #2 ENGINES. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 PEC IAW AMM 61-20-36-000/400-801. ALL OPS TESTS AND CALIBRATION GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (NR 2 PROPELER) · airframe 28,206 hrs · 30,407 cycles

CREW REPORTS ABORTED TAKEOFF AT 60 KNOT DUE TO AUTOFEATHER FAILING TO ARM. ABORTED TAKE OFF. REMOVED FROM SERVICE. R&R #2 PEC OPS TEST PASSED. PROP OVERSPEED GOV CHECK PASSED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 28,206 hrs · 30,407 cycles

AUTOFEATHER DIDN'T ARM ON TAKEOFF IN SEATTLE. NOTICED AT V1, CONTINUED TAKEOFF. REMOVED FROM SERVICE. INTERROGATED CDF FOR FAULT CODES IAW Q400 AMM 77-31-00-710-803 FOUND FAULT CODES 494A B, 70AB, ON BOTH ENGINES, 398AB ON #2 ENGINE. COMPLIED WITH Q400 FIM PROCEDURE 61-20-08-810-818 FAULT CODES RESET COMPLIED WITH OPERATIONAL TEST OF PROPELLER AUTOFEATHER AND UPTRIM SYSTEM IAW 61-20-00-710-810 OF Q400 AMM REMAINING FAULT CODES CLEARED AFTER AUTO FEATHER PASSED, PERFORMED AUTOFEATHER TEST USING ENGINES AND ELECTRICAL MODE, PASSED IN BOTH. RECHECKED FAULT CODES NONE PRESENT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — FAILED · airframe 28,201 hrs · 30,402 cycles

WHILE CONDUCTING DAILY SYSTEM CHECKS, AUTO FEATHER FAILED. POWER LEVERS WERE IN DISC. REMOVED FROM SERVICE. NO CORRELATED FAULT CODES, REF. FIM TASK 61-20-00-810-805. PERFORMED OPS TEST OF THE AUTO FEATHER/UPTRIM SYS. IAW AMM 61-20-00-710-810. OPS TEST GOOD, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — NO TEST · airframe 28,168 hrs · 30,365 cycles

DURING DAILY SYSTEM CHECK THE AUTO FEATHER TEST FAILED TWICE. REMOVED FROM SERVICE. PERFORMED AF + UPTRIM OPS TEST IAW Q400 AMM 61-20-00-710-810. OPS TEST PASS. DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 200) · airframe 27,910 hrs · 30,067 cycles

ON CLIMB NOTICED DME 1&2 FLICKERING FROM DISPLAYING A DME DISTANCE FROM SEA TO DASHES. ADDITIONALLY THE TCAS FAIL MESSAGE WAS DISPLAYED INTERMITTENTLY AS THE DME DISPLAYED DASHED. UPON PULLING UP THE ELECTRICAL SYSTEM PAGE INITIALLY ALL INDICATIONS WERE NORMAL, BUT AS THE TCAS FAIL & DASHED DME DISPLAYED ALL INDICATIONS ON THE ELECTRICAL SYSTEM PAGE CHANGED TO DASHES. THIS ABNORMALITY WAS NOTED INTERMITTENTLY FOR THE FIRST 25 MINUTES OF THE FLIGHT. NO CAUTIONS OR WARNING LIGHTS ILLUMINATED DURING THIS EPISODE & NO OTHER ABNORMALITIES WERE OBSERVED. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. COULD NOT DUPLICATE ISSUE ON GROUND. AS PRECAUTIONARY MEASURE REMOVED EPCU IAW AMM 24-31-11-000-801. INSTALLED EPCU IAW AMM 24-31-11-400-801 OPERATIONAL TEST OF THE DC ELECTRICAL POWER CONTROL UNIT (EPCU) OPS TESTS GOOD. NO FURTHER DEFECTS NOTED. TASK 24-31-11-400-801. STEP 5.C. PERFORMED OPS TEST OF THE TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM TCAS IAW Q400 AMM TASK #34-43-00-710-801, OPS TESTS GOOD. CAPT'S SIDE DME READS .8NM AND FO'S SIDE READS .7NM RESPECTIVELY. INDICATIONS READ NORMAL AND ALL OTHER INDICATIONS DISPLAY NORMAL. NO DASHED OUT INDICATIONS, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 27,887 hrs · 30,039 cycles

EXIT SIGN AT 2E HAS FALLEN FROM ITS POSITION. REMOVED FROM SERVICE. ATTACHED THE EXIT SIGN COVER AT 2E. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: CONTACTOR — DAMAGED (ACCB) · airframe 27,814 hrs · 29,968 cycles

#1 AC GEN ILLUMINATED IN FLIGHT DURING CLIMB AT APPROXIMATELY 24,000 FT. PRIOR TO #1 AC GEN CAUTION, THE WNSHLD HOT (OR WNSHLD CTAL) CAUTION FLICKERED ON BRIEFLY (DID NOT RE-ILLUMINATE). WINDSHIELD HEAT WAS IN THE NORM POSITION STARTING AT 10,000 FT. PILOT STATIC 1/2/STBY HEATS WERE ALSO ON. ALL OTHER ICE PROTECTION SYSTEMS WERE OFF OR MANUAL. REMOVED AND REPLACED LH ACCB K1 CONTACTOR REF Q400 AMM 24-21-21-000-802 AND 24-21-21-400-802. OP TEST GOOD OF THE K1 CONTACTOR REF Q400 AMM 24-20-00-710-805.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 27,814 hrs · 29,989 cycles

#1 AC GEN CAUTION LIGHT ILLUMINATED BEGINNING INTERMITTENTLY AT APPROXIMATELY 20,000FT LIGHT EVENTUALLY REMIANED ILLUMIATED CONTINUOUSLY INCLUDING AFTER COMPLETION OF CHECKLIST. REMOVED FROM SERVICE. REMOVED AND REPLACED GCU #1 REF Q400 AMM 24-21-06-000-801 AND 24-21-06-400-801. OPERATIONAL TEST OF THE AC VARIABLE FREQUENCY GENERATION SYSTEM GOOD REF Q400 AMM 24-21-00-710-801. RETURNED TO SERVICE.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 27,808 hrs · 29,964 cycles

A/C GEN CAUTION ILLUMINATED FLICKERED ABOUT 10 TIMES BEFORE STAYING ON. REMOVED FROM SERVICE. INTERROGATED CDS AND NO FAULTS WERE LOGGED. INTERROGATED EPCU, FAULT 27 LOGGED. CHECKED NR 1 AC GEN CHIP DETECTOR, NO CHIPS NOTED. OPS TESTED AC GEN SYSTEM, OPS CHECK GOOD IAW AMM 24-21-00-710-81. AS PRECAUTION, MTX REQUEST R&R OF NR 1 AC GEN GCU. R&R NR 1 AC GEN GCU IAW Q400 AMM TASK 24-21-06-000-801/400-801.OPS CHECKS GOOD.NO FURTHER DEFECTS NOTED. INNTERROGATED EPCU AND FOUND NO FAULTS REMAIN. RETURNED TO SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 27,809 hrs · 29,965 cycles

NR 1 AC GEN ILLUMINATED. REMOVED FROM SERVICE. C/W FIM TASK 24-20-00-810-801. NO FAULTS FOUND. R&R NR 1 AC GEN IAW MTC 6242101. AC GEN OPS CHECK GOOD. RETURNED TO SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (NR 1 ENGINE) · airframe 27,809 hrs · 29,966 cycles

ON CLIMB OUT, NR 1 AC GEN CAUTION LIGHT ILLUMINATING ON AND OFF RAPIDLY ABOUT 50 TIMES. THEN IT REMAINED ILLUMINATED FOR A BIT AND WE RAN THE CHECKLIST. SOMETIMES WHEN THE NR 1 AC GEN LIGHT WAS FLASHING, WSHD CTRL WAS FLASHING AS WELL. REMOVED FROM SERVICE. CONTINUITY AND INSULATION RESISTANCE CHECKS OF WIRING BETWEEN THE NR 1 AC GEN AND THE NR 1 AC GCU; AND BETWEEN NR 1 AC GEN AND LT ACCB. AND REPLACEMENT OF THE NR 1 AC GEN CONTROL HARNESS IN THE LEFT NACELLE. AND FOR OPERATIONAL TEST OF THE AC VARIABLE FREQ GENERATION SYSTEM. OPERATIONAL TEST WAS GOOD AT VARIOUS POWER SETTINGS. DURING OPS CK, OPERATED WINDSHIELD HEAT, NO "WSHLD CTRL" MESSAGE ILLUMINATED. RETURNED TO SERVICE.

Part: STEP — BROKEN (CABIN DOOR) · airframe 27,743 hrs · 29,889 cycles

RAMP REPORTS FLIP STEP ON MAIN CABIN DOOR BROKEN. REMOVED FROM SERVICE. INSPECTION FOUND THE FOLDING PORTION OF MCD TOP STEP TO BE BROKEN FROM ITS POTTED INSERTS. REMOVED BROKEN PORTION OF THE STEP, BROKEN HARDWARE. INSTALLED SERVICEABLE FLIP STEP ASSY ON MCD. DOOR OPENS AND CLOSES AS IT SHOULD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,526 hrs · 29,633 cycles

AFTER PUSHBACK WITH BOTH ENGINES STARTED AND READY TO TAXI AFT FA CALLED REPORTING THE SMELL OF SMOKE. THE SMELL REMAINED AND DID NOT DISSIPATE WHILE WE RETURNED TO GATE. AIRCRAFT DOWN FOR REPAIRS.

Part: ECU — MALFUNCTIONED (BLEED AIR SYS) · airframe 26,999 hrs · 29,040 cycles

AFTER TAKE-OFF NR 2 BLEED HOT CAUTION ILLUMINATED. CAUTION LIGHT WAS RESET VIA E&A CHECKLIST BUT RE-ILLUMINATED. BLEED HOT CAUTION NOT ILLUMINATED WITH BLEED SELECTED OFF. BLEED FLOW WAS SELECTED TO MIN FOR APPROPRIATE TIME FRAME PRIOR TO DEPARTURE (BLEED SYSTEM). REMOVED FROM SERVICE. ECS ECU REMOVAL AND REPLACEMENT. PERFORMED OPERATIONAL TEST OF THE BLEED AIR SYSTEM AS PER AMM TASK 36-11-00-710-802. NO BLEED HOT CAUTIONS ILLUMINATED AT ANY TIME. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (COCKPIT TEMP) · airframe 26,900 hrs · 28,940 cycles

CABIN PACK HOT CAUTION LIGHT ILLUMINATED DURING CRUISE AT 15,000. PER E/A CHECKLIST, TURNED OFF CABIN PACK. CAUTION LIGHT STILL ILLUMINATED AT PARKING. APPROXIMATELY 10 - 15 MINUTES AFTER THAT CHECKLIST CABIN PRESSURE MASTER WARNING ILLUMINATED. STARTED E/A CHECKLIST BUT QUICKLY DESCENDED THROUGH 9,000 FT. DURING APPROACH, THE LIGHT EXTINGUISHED. AIRCRAFT REMAINED UNPRESSURIZED TO TOUCHDOWN. REMOVED FROM SERVICE. CDS SHOWS FAULTS 7105, 7106, AND 7107. R & R THE CABIN COMPRESSOR OUTLET TEMP SENSOR IAW AMM 21-51-91-000-801/400-801. OPS TESTED THE ECS TEMP CONTROL IAW AMM 21-61-00-710-803. OPS TESTED GOOD FOR FLIGHT DECK CONTROL. NO CABIN PACK HOT CAUTION. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (MULTIPLE) · airframe 26,890 hrs · 28,927 cycles

GOING THROUGH 90 KTS ON TAKEOFF, ELEVATOR FEEL, PITCH TRIM, RUDDER CONTROL, SPOILER OTBD, CAUTION LIGHTS ILLUMINATED. LIGHTS STAYED ON UNTIL ABORTED TAKEOFF THROUGH 60 KTS, WHERE THEY EXTINGUISHED. NO EXCESSIVE BRAKING OCCURRED DURING ABORTED TAKEOFF. REMOVED FROM SERVICE. INTERROGATED CDS WITH NO CURRENT FAULTS FOUND. FOUND ADU DISCREPANCY, IOP2 AND ADU DISCREPANCY, IOP1 IN FAULT HISTORY. INSPECTED THE PITOT PROBES IAW AMM 34-11-06-200-801 WITH NO DEFECTS NOTED. PERFORMED AN OPS TEST OF BOTH ADUS IAW MTC 6341101, OPS TESTED GOOD, NO FAULTS IN CDS. PERFORMED OPS TEST OF BOTH IOPS IAW MTC 6314101. OPS TESTED GOOD, NO FAULTS. COMPLIED WITH AN OPS CHECK OF REDUNDANCY BETWEEN THE ADU, AHRS, AND DISPLAY IAW 34-11-00-710-802 WITH NO DEFECTS. CLEANED PITOT AND STATIC LINES IAW 34-11-00-170-801. OPS TESTED THE FLAPS, TESTED GOOD IAW AMM 27-50-00-710-801, NO FAULTS IN CDS. AIRCRAFT REMAINS CAT III QUALIFIED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 26,936 hrs · 28,862 cycles

EMERGENCY LIGHT SWITCH INSIDE THE MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED FROM SERVICE. REPLACED THE LAMPS IN THE SWITCH. SWITCH ILLUMINATES NORMALLY. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,564 hrs · 28,543 cycles

WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. FOUND THE AFT TWO CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECK GOOD.

Part: FUEL — ODOR (CABIN & COCKPIT) · airframe 26,007 hrs · 27,956 cycles

AT TOP OF DESCENT, B FA REPORTED A RAW FUEL ODOR EMANATING FROM THE VENTS. THE ODOR ALSO NOTED IN THE FLIGHT DECK VENTS. AFTER TURNING OFF THE NR 2 BLEED, THE ODOR DISSIPATED. LANDING UNEVENTFUL. COMPLIED WITH AMM 21-00-00-160-901. REMOVAL OF ODOR FROM THE AIR CONDITIONING DUCTS. NO ODORS NOTED. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 25,896 hrs · 27,829 cycles

AFT PAX DOOR FORWARD UPPER DOOR ROLLER HANGING UPON FORWARD LATCH ROLLER TRACK. ADJUSTED UPPER FORWARD ROLLER (G6) DOOR NOW CLOSES AND OPENS EASILY. REMOVED DOOR FRAME PANELS, DOOR LINER AND AFT STOWAGE CLOSET. RIGGED AFT PAX DOOR. REINSTALLATION OF DOOR FRAME PANELS, DOOR LINER, AND AFT STOWAGE CLOSET. NO PARTS REPLACED.

Part: GENERATOR — FAILED (NR 1) · airframe 25,647 hrs · 27,571 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. GENERATOR REPLACED IAW W/O 233733. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,548 hrs · 27,471 cycles

CABIN EMERGENCY LIGHTING SWITCHLIGHT DOES NOT ILLUMINATE IN THE NORMAL POSITION. RE-LAMPED CABIN EMERGENCY LIGHTING SWITCHLIGHT. LAMP TEST GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 25,375 hrs · 27,285 cycles

DURING CLIMB, LOST THE NR 2 ENGINE OIL PRESSURE AND NR 2 ENGINE ROLLED BACK. SHUTDOWN ENGINE INFLIGHT AND RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED THE NR 2 ENGINE. REPLACED THE NR 2 AC GENERATOR, OIL COOLER, BETA TUBE, AND OIL COOLER HOSES FOR POSSIBLE CONTAMINATION, AND PROP DOME CLEANING. OPS AND LEAK CHECKED GOOD. RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — DIRTY (NLG) · airframe 25,318 hrs · 27,227 cycles

AFTER TAKEOFF, THE NOSE GEAR WAS SLOW TO RETRACT. MAIN GEAR RETRACTED NORMALLY. THE NOSE GEAR DOOR LIGHT AND UNSAFE LIGHT REMAINED ON FOR 4-5 SECONDS. FINALLY RETRACTED WITH ALL LIGHTS OUT. LDG GEAR INOPERATIVE CAUTION LIGHT REMAINED EXTINGUISHED. PERFORMED ALTERNATE GEAR EXTENSION AS A PRECAUTION. ALTERNATE EXTENSION WAS NORMAL. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INSPECTED NOSE LANDING GEAR, AND FOUND CONTAMINATS BETWEEN PROXIMITY SENSOR AND TARGETS, CLEANED. COMPLIED WITH A FUNCTIONAL TEST OF LANDING GEAR IAW 32-31-00-720-801, FUNTIONAL TESTED GOOD. PSEU FAULT HISTORY SHOWED NG LK 2 NEAR, NG LK 1 NEAR, FLIGHT LEG HISTORY SHOWED NG DR CL,FAULT UNREASONABLE FAR, NG WOW 2 FAULT UNREASONABLE NEAR, NG WOW 1 FAULT UNREASONABLE NEAR. CLEARED FAULT HISTORY IAW FIM 32-00-00-810-815, PARA 1-4A (1)(B), PARA 5A (5)-5, (10), AND PARA 6. NO DEFECTS NOTED. FAULTS DID NOT RETURN. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: BLADE — FAILED (BLADE HEAT) · airframe 25,232 hrs · 27,142 cycles

PROPELLER DEICE CAUTION LIGHT ILLUMINATED AND STAYED ILLUMINATED DURING NR 2 PROPELLER CYCLE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. R & R THE NR 2 PROPELLER NR 5 BLADE. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NR 2 FUEL HEATER) · airframe 25,015 hrs · 26,908 cycles

AT 25000 FT, DURING CRUISE, THE FIRE BELL CAME ON . NO OTHER FIRE INDICATIONS VISIBLE ALL ENGINE INDICATIONS WERE NORMAL EXCEPT NR 2 FUEL TEMP SHOWED +99 DEGREES. IAW THE ABNORMAL FUEL TEMP CHECK LIST, TURNED ON THE NR 2 FUEL BOOST PUMP, NR 2 FUEL TEMP CAME BACK DOWN TO THE NORMAL RANGE BUT WOULD CLIMB BACK TO 71 DEGREES SHORTLY AFTER TURNING THE NR 2 BOOST PUMP OFF. REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENG FUEL HEATER THERMAL ACTUATOR IAW AMM TASK 73-11-05-000/400-801, LEAK CHECKED GOOD. RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (FUEL HEATER) · airframe 25,002 hrs · 26,894 cycles

AT 25000 FT, DURING CRUISE, THE FIRE BELL CAME ON . NO OTHER FIRE INDICATIONS VISIBLE. ALL ENGINE INDICATIONS WERE NORMAL, EXCEPT THE NR 2 FUEL TEMP SHOWED +99 DEGREES,. IAW THE ABNORMAL FUEL TEMP CHECK LIST, TURNED ON THE NR 2 FUEL BOOST PUMP, NR 2 FUEL TEMP CAME BACK DOWN TO THE NORMAL RANGE. WOULD CLIMB BACK TO 71 DEGREES SHORTLY AFTER TURNING THE NR 2 BOOST PUMP OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE FUEL HEATER THERMAL ACTUATOR IAW AMM 73-11-05-000/400-801. LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: IO CARD — MALFUNCTIONED (ZONE 100) · airframe 24,671 hrs · 26,543 cycles

DURING CLIMB OUT AT APPROXIMATELY 15,000 FT MSL, THE FUEL TEMP ON THE NR 2 ENGINE WENT FROM NORMAL TO +99 AND TURNED RED WITH THE BELL SOUNDING LIKE THE ENGINE FIRE BELL WAS ON CONTINUOUSLY. AFTER APPROXIMATELY 2 MINUTES THE FUEL TEMP WENT BACK TO NORMAL AND THE BELL QUIT. THERE WERE NO OTHER INDICATIONS OF A PROBLEM. DURING THE TIME THE FUEL TEMP WAS HIGH. ACCOMPLISHED THE EMERGENCY CHECKLIST WITH NO CHANGE IN THE TEMP INDICATION. LANDING UNEVENTFUL. AIRCRAFT REMOVED FROM SERVICE. RAN NR 2 ENGINE WITH NO FAULTS. STARTED NR 1 ENG WITH NR 2 ENGINE RUNNING, DASHES APPEARD FOR NR 2 FUEL TEMP OIL PSI IO, NR 2 FAILED MESSAGE ON ED. REMOVED AND REPLACED THE NR 2 IO MODULE IAW MTC 6314101. OPS TESTED GOOD DURING ENGINE RUN. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (FUEL TEMP) · airframe 24,602 hrs · 26,477 cycles

NR 2 FUEL TEMPERATURE ON EICAS DISPLAY INDICATED 99 DEGREES FOR 5 MINUTES WITH ASSOCIATED FIRE BELL. FIRE BELL SILENCED WHEN INDICATION CHANGED BACK TO WHITE. INSPECTED, FOUND ISSUE TO BE INDICATION. NO HISTORY IN THE PAST 2 MONTHS. REMOVED AND REPLACED FUEL TEMP SENSOR IAW MM 73-31-09-000-801, AND 73-31-09-400-801. OPS AND LEAK CHECKED GOOD.

Part: ENGINE — POWER LOSS · airframe 24,279 hrs · 26,129 cycles

TAKEOFF TORQUE NOT OBTAINED ON EITHER ENGINE. PERFORMED TAKEOFF ABORT AT 100 KIAS. NTOP POWER SETTING WAS 90%. TAKEOFF TORQUE ON ENGINE NR 1 WAS 88% AND TAKEOFF TORQUE ON NR 2 ENGINE WAS 87%. PERFORMED NR 1 & NR 2 ENGINE POWER ASSURANCE CHECKS. BOTH CHECKS GOOD. CDS REPORTS NO FAULT CODES, AIRCRAFT OK FOR CONTINUED SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 23,828 hrs · 25,670 cycles

RAMP REPORTED THE AFT PAX DOOR IS STUCK IN THE OPENING AND WILL NOT OPEN OR CLOSE. UNSTUCK AFT PAX DOOR. PERFORMED GVI OF THE DOOR NO DEFECTS NOTED. OPS TEST GOOD IAW AMM TASK 52-12-00-710-802. DOOR OPENS AND CLOSES NORMAL. DOOR SEAL CLEANED AND LUBED PER AMM TASK 12-20-01-640-806.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 22,937 hrs · 24,743 cycles

CLIMBING AT 17,000, AIRCRAFT DID NOT PRESSURIZE. DECLARED AN EMERGENCY AND PERFORMED A EMERGENCY DESCENT. PRESSURIZATION ISSUE WAS RESOLVED AND THE FLIGHT CONTINUED ON.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 22,523 hrs · 24,289 cycles

FORWARD EMERGENCY DOOR EXIT UPPER DOOR DISPLAY SHOWS LOCKED WITH THE DOOR REMOVED FROM THE AIRCRAFT. FERRIED FOR REPAIRS. FOUND EMERGENCY EXIT DOOR PROXIMITY SENSOR OUT OF RIG. RIGGED SENSOR WITH NEW LOCKPIN INSTALLED IAW Q400 AMM TASK 52-71-01-830-805. OPERATIONAL TEST GOOD. RETURNED TO SERVICE.

Part: STRINGER — CORRODED · airframe 22,446 hrs · 24,209 cycles

CORROSION UNDER STAND-OFF ON STRINGER 31R. FOUND TO BEYOND LIMITS IAW SRM 53-10-03-01-01. STRINGER REMOVED AND REPLACED IAW SRM 53-10-03. NDT CARRIED OUT IAW NDTM6, 51-00-08-250-801.

Part: SHEAR WEB — CORRODED (BS 714-783) · airframe 22,446 hrs · 24,209 cycles

AFT CARGO SHEAR WEB BS 714 - 783 HAS CORROSION IN MULTIPLE LOCATIONS. SHEAR WEB REMOVED AND REPLACED IAW SRM 51-42-05-51-40-15, 51-42-75 AND 51-42-45.

Part: CARGO TRACK — CORRODED (BS 670-782) · airframe 22,446 hrs · 24,209 cycles

LEFT AFT INBD CARGO TRACK IN AFT CARGO BAY FROM BS 670 - 782, LBL 10 CORRODED BEYOND LIMITS. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15, AND 51-42-75.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,446 hrs · 24,209 cycles

RT INBD SEAT TRACK 11 CORRODED BEYOND LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-15, 51-41-05 AND 51-42-05.

Part: THRESHOLD — CORRODED (FWD CARGO DOOR) · airframe 22,446 hrs · 24,209 cycles

FWD CARGO DOOR LWR THRESHOLD PANEL AND CHANNEL CORRODED IN MULTIPLE LOCATIONS. THE THRESHOLD PANEL AND EDGE CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15, 51-41-05, AND 51-42-45.

Part: THRESHOLD — CORRODED (EMERGENCY EXIT) · airframe 22,446 hrs · 24,209 cycles

TYPE 2 EMERGENCY EXIT THRESHOLD BEAM HAS CORROSION IN MULTIPLE LOCATIONS. THRESHOLD BEAM REMOVED AND REPLACED IAW SRM 51-42-05, 51-42-45.

Part: STRINGER SPLICE — CORRODED (BS 234) · airframe 22,446 hrs · 24,209 cycles

STRINGER SPLICE BS 234.4 STRINGER 25L CORRODED IN MULTIPLE AREAS. THE STRINGER SPLICE REPLACED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 570-670) · airframe 22,446 hrs · 24,209 cycles

LEFT INBD AFT CABIN SEAT TRACK BS 570 - 670, LBL 10 CORRODED BEYOND LIMITS. THE SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-05 & 51-40-15.

Part: STRAP — CORRODED (BS 730-783) · airframe 22,446 hrs · 24,209 cycles

SHEAR WEB DOUBLER STRAP AT AFT CARGO DOOR SILL BS 730 - 783, LBL 30 CORRODED BEYOND LIMITS. THE SHEAR WEB DOUBLER STRAP WAS REMOVED AND REPLACED IAW SRM 51-42-05.

Part: STIFFENER — CORRODED (BS 783) · airframe 22,446 hrs · 24,209 cycles

ANGLE STIFFENER AT BS 783.1 FROM AFT SHEAR WEB TO VERTICAL WEB BL 0 - LBL 40 CORRODED BEYOND LIMITS. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,446 hrs · 24,209 cycles

RIGHT INBD SEAT TRACK 10 CORRODED BEYOND LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-15, 51-40-05, 51-42-05.

Part: FLOORBEAM — DAMAGED (BS 712) · airframe 22,446 hrs · 24,209 cycles

FLOORBEAM AND ANGLE AT BS 712.375 BENEATH SEAT TRACK NR 9 DAMAGED. FLOORBEAM REPLACED IAW SRM 51-42-05. ANGLE REPLACED IAW TASK CARD R/D 8/4-53-7648.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,446 hrs · 24,209 cycles

LEFT INBD FWD CABIN SEAT TRACK NR 5 BETWEEN FS 34 - 102.50 RBL 10 HAS DEEP CORROSION ON OUTBD FLANGE. REMOVED AND REPLACED IAW SRM 51-42-05, 51-40-15, 51-41-05, SRM 51-40-07.

Part: STRINGER SPLICE — CORRODED (BS 18.4) · airframe 22,446 hrs · 24,209 cycles

CORROSION FOUND ON STRINGER SPLICE 32R BS 18.400 UNDER WIRE HARNESS. REMOVED STRINGER SPLICE IAW SRM 51-42-05. INSTALLED A NEW STRINGER SPLICE IAW SRM 51-42-05.

Part: WEB — DAMAGED (BS 728-747) · airframe 22,446 hrs · 24,209 cycles

WEB AND STIFFENER BENEATH SEAT TRACK BS 728.102 - 747.602 DAMAGED. WEB REPLACED IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 591-670) · airframe 22,446 hrs · 24,209 cycles

RIGHT OTBD AFT CABIN SEAT TRACK FROM BS 591.50 - 670 RBL 40, CORRODED BEYOND LIMITS. SEAT TRACK REMOVED IAW SRM 51-40-15 AND SRM 51-42-05. A NEW SEAT TRACK DRILLED AND REAMED IAW SRM 51-40-07-02-01. THE NEW SEAT TRACK WAS INSTALLED IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-42-45.

Part: SEAT TRACK — CORRODED (BS 612-670) · airframe 22,446 hrs · 24,209 cycles

RIGHT INBOARD AFT CABIN SEAT TRACK NR 15 BETWEEN BS 612 AND 670 CORRODED BEYOND LIMITS. THE SEAT TRACK WAS REPLACED IAW DRAWING 85338210, AND SRM 51-42-05-81-40-15.

Part: ENGINE — LEAKING (NR 2) · airframe 21,707 hrs · 23,416 cycles

AFTER STARTING NR 2 ENGINE TO DO 80 PERCENT NH RUN-UP, SELECTED NR 2 BLEED ON AND THE FLIGHTDECK AND CABIN HAD A STRONG ODOR OF BURNING OIL COMMING FROM THE VENTS. REMOVED THE NR 2 ENGINE P2.2 EXHAUST DUCT, INSPECTED FOR LEAKS, NO LEAKS FOUND. REINSTALLED NR 2 ENGINE P2.2 EXHAUST DUCT, IAW AMM TASKS 36-11-26-000-801, 36-11-26-400-801. GROUND RAN ENGINES WITH BLEEDS ON, FLIGHTDECK AND CABIN FILLED WITH SMOKE WITHIN 2 MINUTES. SMOKE IS COMING FROM NR 2 ENGINE. REPLACED ENGINE.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,656 hrs · 23,373 cycles

FWD PAX AIRSTAIR INBD AFT ANGLE CORRODED. FWD PASSENGER AIRSTAIR INBD AFT ANGLE, PN 85217097-102, INSTALLED REF SRM 51-41-02. NEW ANGLE, PN 85217097-102, LOCATED AND DRILLED REF SRM 51-40-07. FILLET SEAL APPLIED IAW SRM REF 51-23-00-00-00-01.

Part: LIGHT — UNSECURE (CABIN FLOOR) · airframe 21,375 hrs · 23,114 cycles

FLOOR PATH LIGHTING STRIP IN ROW 1 LOOSE. RESECURED STRIP. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 21,297 hrs · 23,041 cycles

EMERGENCY LIGHT NEAR MAIN CABIN DOOR IS DETACHED. SECURED EMERGENCY LIGHT AND RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 21,151 hrs · 22,891 cycles

EMERGENCY LIGHT STRIP BY MAIN CABIN DOOR, DETACHED FROM THE FLOOR. ATTACHED LIGHT STRIP. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,883 hrs · 22,613 cycles

F/A REPORTS HAZE IN CABIN AFTER ENGINE START. NO ODOR NOTED. RAN ENGINES AT GATE WITH BLEEDS ON AT VARIOUS TEMP AND FLOW SETTINGS. COULD NOT DUPLICATE DISCREPANCY. PERFORMED OPS TEST OF BLEED AIR SYS IAW AMM TASK 36-11-00-710-801. OPS TEST PASSED. NO HAZE OR UNUSUAL ODOR IN CABIN. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: IGNITER — FAILED (APU) · airframe 20,498 hrs · 22,203 cycles

FAILED ATTEMPT TO START APU. GROUND PERSONNEL REPORT SMOKE COMING FROM APU EXHAUST. REPLACED BOTH IGNITORS IAW AMM TASK 49-40-04-000-801 & TASK 49-40-04-400-801, OPS TESTED GOOD, RETURNED TO SERVICE.

Part: PLACARD — DAMAGED (CABIN) · airframe 20,185 hrs · 21,860 cycles

PLACARD AT THE AFT GALLEY EMERGENCY STOWAGE COMPARTMENT IS UNREADABLE. REPLACED PLACARD. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,479 hrs · 21,103 cycles

ON DESCENT, CREW, CAPTAIN & F/O, SMELLED FAINT SMOKE ODOR ABOUT 1 MIN LATER F/A CALLED AND SAID THEY HAD SMOKE IN THE CABIN. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. ACCOMPLISHED ECS HEALTH CHECK. ACCOMPLISHED REMOVAL ODOR FROM ACFT DUCTS. OPS CK OF RECIRCULATING FAN AND ALL INTERIOR LIGHTS, NO DEFECT FOUND ACFT OK FOR CONTINUED SERVICE.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 19,160 hrs · 20,760 cycles

MAIN CABIN DOOR IS HARD TO OPEN AND ALSO MAKES A GRINDING SOUND IN OPERATION. FOUND CABIN DOOR TO OPEN OK. OPENED DRAIN BELOW MAIN CABIN DOOR AND DRAINED WATER. NOISE WENT AWAY. NO FURTHER DEFECTS NOTED. AS A PRECAUTIONARY MEASURE REMOVED AND REINSTALLED THE FORWARD LOWER WARDROBE IAW AMM TASK 25-20-03-000-803 AND 25-24-03-400-803 TO CHECK FOR ANY OBSTRUCTION TO THE DOOR MECHANISM. NONE FOUND. RETURNED TO SERVICE.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 19,106 hrs · 20,696 cycles

IN CRUISE AT 14,000 FT NOTICED NR 1 ITT RUNNING 100 DEGREES ABOVE NR 2. BEGAN NOTICING ODOR. ABOUT 2 MINUTES "CABIN PACK HOT" CAUTION ILLUMINATED. COMPLIED WITH CHECKLIST AND SHUTDOWN CABIN PACK. DECENDING THROUGH 7,000 FT. ALL CABIN PRESSURE WAS LOST. DIFFERENTIAL WENT ZERO AT 7,000. ECS ECU AND NR 1 BLEED STAGE PRESSURE SWITCH WERE REPLACED. ALL OPS CHECKS WERE COMPLETED AND CHECKED GOOD. RETURNED TO SERVICE.

Part: BRACKET — MISINSTALLED (NLG) · airframe 18,579 hrs · 20,110 cycles

DURING GEAR RETRACTION, AFTER THE MAINS FINISHED RETRACTING THE NOSE GEAR REMAINED IN TRANSIT FOR SEVERAL SECONDS AND THEN WITH HESITATION RETRACTED. ALTERNATE LANDING GEAR EXTENSION WAS COMPLIED WITH. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND NLG K2 PROXIMITY BRACKET INSTALLED ON NLG INCORRECTLY. FUNCTIONAL TEST OF MLG PRIMARY RETRACTION AND EXTENSION SYSTEM PERFORMED WITH NO DEFECTS NOTED. GEAR TRANSITION TIMES WERE NORMAL WITH NO HESITATION. IAW AMM TASK 32-31-00-720-801. RETURNED TO SERVICE.

Part: LANDING GEAR — SLOW · airframe 18,392 hrs · 19,919 cycles

DURING DEPARTURE, RETRACTING LANDING GEAR NOSE GEAR SLOW TO RETRACT, APPROXIMATELY 5 SECONDS AFTER MAIN GEAR LIGHTS EXTINGUISH THEN NOSE GEAR LIGHT EXTINGUISHED. SELECTING GEAR DOWN, NORMAL EXTENSION AND NORMAL TIME. PREFORMED VISUAL INSPECTION OF NLG HYD COMPONENTS, NO LEAKS AND NO DEFECTS NOTED. COMPLIED WITH FUNCTIONAL TEST OF THE LANDING GEAR PRIMARY RETRACTION SYSTEM IAW AMM TASK 32-31-00-720, APPLICABLE STEPS FOR ACFT. FOUND RETRACTION AND EXTENSION TIMES TO BE WITHIN SERVICABLE LIMITS, NO DEFECTS NOTED DURING LANDING GEAR "SWINGS". RETURNED TO SERVICE.

Part: PLACARD — MISSING (CABIN) · airframe 18,162 hrs · 19,682 cycles

F/A REPORTED THAT THE PLASTIC COVER FOR THE EMERGENCY EXIT PLACARD IS MISSING. PERFORMED GVI OF ACFT, COULD NOT FIND MISSING LENS COVER. DURING INSPECTION FOUND FWD EMERGENCY EXIT LIGHT ASSY BROKEN ON EMERGENCY EXIT. R & R EMERGENCY EXIT LIGHT ASSY WITH NEW FROM STOCK. OPS CHECK GOOD. ACFT OK FOR CONTINUED SERVICE. PLASTIC COVER WAS REPLACED WITH NEW FROM STOCK.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 16,682 hrs · 18,073 cycles

PAX DOOR FWD MACHINED CORNER, FOUND TO BE CRACKED. INSTALLED PAX DOOR FWD MACHINED CORNER IAW SRM 51-42-05-02-01.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 16,682 hrs · 18,073 cycles

CORROSION FOUND ON FWD PAX DOOR THRESHOLD AND THRESHOLD PLATE. REMOVED THRESHOLD AND THRESHOLD PLATE ASSY IAW SRM 51-42-05. INSTALLED NEW THRESHOLD AND NEW THRESHOLD PLATE ASSY IAW SRM 51-42-05-02-01 4, D.

Part: SEAT TRACK — CORRODED (NR 13) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 13 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-41-00 AND SRM 51-42-05, STEP 4E, 1-8. INSTALLED SEAT TRACKIAW SRM 51-42-05, STEP 4D AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (NR 12) · airframe 16,682 hrs · 18,072 cycles

SEAT TRACK, NR 12 CORRODED. REMOVED SEAT TRACK IAW SRM 51-42-05, STEP 4E, SRM 51-40-15, STEP 6M, & SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 11 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, PROCEDURE E 1-8 AND SRM 51-40-15 PG 213 PROCEDURE M 1-5. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, SRM 51-40-15 STEP 6H0J AND SRM 51-41-00.

Part: SEAT TRACK — CORRODED (NR 7) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 7 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, STEP 4-E, 51-40-15, STEP 6-M & 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 PROCEDURE 4-D(3-10), 51-40-15 STEPS 1-6 J (1-7) & 51-41-00.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 2 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, 51-40-15, 51-42-60 AND 51-42-90. INSTALLED NEW SEAT TRACK IAW SRM 51-42-45, SRM 51-42-05.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 16,682 hrs · 18,073 cycles

AFT SERVICE DOOR EDGE BEAM, FOUND CORRODED. REMOVED BEAM IAW SRM 51-42-05. INSTALLED NEW BEAM IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (NR 18) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 18 CORRODED. REMOVED SEAT TRACK IAW SRM 51-42-05, PAR E AND 51-40-15 PAR M. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05. REPAIR 01 SRM 51-42-45, REPAIR 01 AND SRM 51-40-15, REPAIR 0.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 16,682 hrs · 18,073 cycles

AFT SERVICE DOOR EDGE BEAM, FOUND CORRODED. REMOVED BEAM IAW SRM 51-42-45, SRM 51-42-05. INSTALLED NEW BEAM IAW SRM 51-42-45, SRM 51-40-45 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (NR 10) · airframe 16,682 hrs · 18,073 cycles

NR 10 SEAT TRACK CORRODED. R & R SEAT TRACK IAW SRM 51-42-05, PROCEDURE G 1-10 AND E 1-8 AND SRM 51-40-15, PROCEDURE H 1-5, I 1-3 AND J 1-8.

Part: SEAT TRACK — CORRODED (BS 228-570) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK 313 HAS NUMEROUS AREAS OF PITTING CORROSION FROM FS 228.00 TO FS 570.00. REMOVED CORROSION AT NUMEROUS AREAS ON SEAT TRACK NR 13 REF 53-20-49, REPAIR-02, FIG 201, SRM. EVALUATED SEAT TRACK 13 ORIG MATERIAL THICKNESS FROM TOP TO BOTTOM SECTION OF THE SEAT TRACK CLAW IS .460", MATERIAL LOSS AFTER BLENDOUT IS BET .005" TO .020" DEPTH THE MAX ALLOWABLE BLENDOUT LIMIT IS ONLY .015". IAW SRM 53-20-49, FIG 201, SHEET 2, REWORKED AREAS IS OUT OF LIMITS EVALUATED AND MEASURED USING TUC6161 DEPTH GAGE. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (BS 228-570) · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 7 HAS NUMEROUS AREAS OF PITTING CORROSION FROM FS 228.00-FS 570.00. REMOVED PITTING CORROSION AT NUMEROUS AREAS ON SEAT TRACK 7, REF SRM 53-20-49. EVALUATED SEAT TRACK NR 7 ORIGINAL MATERIAL THICKNESS FROM TOP TO BOTTOM SECTION OF THE SEAT TRACK CLAW IS .460", MATERIAL LOSS AFTER BLENDOUT IS BET .005" TO .025IN. DEPTH THE MAX ALLOWABLE BLENDOUT LIMIT IS ONLY .015" IAW SRM 53-20-49. REWORKED AREAS IS OUT LIMITS EVALUATED AND MEASURED USING TUC6161 DEPTH GAGE. REPLACEMENT COMPLIED WITH ON BTAC NRI JOB 5415611, OP 133.

Part: SEAT TRACK — CORRODED · airframe 16,682 hrs · 18,073 cycles

SEAT TRACK NR 1 HAS NUMEROUS AREAS OF PITTING CORROSION FROM FS 32.400-FS 229.50. REMOVED CORROSION FROM 5 EA LOCATIONS ON SEAT TRACK NR 1, REF SRM 53-20-49, REPAIR-02. CONTINUED REMOVAL OF CORROSION ON SEAT TRACK NR 1 REF SRM 53-20-49, REPAIR-02. SEAT TRACK NR 1 FOUND OUT OF LIMITS IAW SRM 53-20-49, REPAIR-02. BLENDED 0.022" ON TOP OF CLAW, MAX ALLOWED 0.015", TOOL TUC4745. REPLACEMENT OF SEAT TRACK NR 1 PERFORMED ON JOB 5415611 OP 137.

Part: GUARD — MISSING (EMERGENCY LIGHT) · airframe 16,433 hrs · 17,792 cycles

GUARD MISSING ON THE CABIN EMERGENCY LIGHT SWITCH. REPLACED THE SWITCH BODY IAW AMM 33-51-05-000-801 AND INSTALLED NEW IAW AMM 33-51-05-400-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 16,231 hrs · 17,568 cycles

DURING APPROACH, PASSING 4000FT, AFTER DISENGAGING AUTO-PILOT. LEFT OTBD SPOILER DEPLOYED UNTIL TOUCHDOWN. ON TOUCHDOWN ALL SPOILERS DEPLOYED NORMAL. WHEN FLIGHT/TAXI SWITCH SELECTED TO TAXI, ALL SPOILERS RETRACTED NORMAL. SPOILER DEPLOYED WITH IAS BELOW 170 KNOTS IT WAS VISUALLY CONFIRMED THAT THE SPOILER WAS DEPLOYED ABOUT HALFWAY AND DIDN'T CHANGE POSITION WITH CONTROL INPUTS. NO OTHER CONDITION OR ADVISORY LIGHTS ILLUMINATED. INTERROGATED CDS NO FAULTS FOUND IN CDS PERFORMED OPS TEST OF THE SPOILER SYS IAW AMM 27-61-00-710-801. OPS TEST SATISFACTORY. NO UNCOMMANDED OTBD SPOILER DEPLOYMENT DURING OPS TEST. REMOVED LT OTBD SPOILER POWER CONTROL UNIT IAW AMM TASK 27-61-16-000-801. REPLACED W/ SERVICABLE POWER CONTROL UNIT IAW AMM TASK 27-61-16-400-801. OPS CHECK OF ROLL SPOLIER SYS GOOD IAW AMM TASK 27-61-00-710-801. RETURNED TO SERVICE.

Part: GLOWSTRIP — DAMAGED (ZONE 200) · airframe 14,941 hrs · 16,188 cycles

PHOTOLUMINESENT BASE LAYER DISCOLORING AT LOCATION 2B,10C,AND 20B SEAT ROWS. REPLACED GLOWSTRIP AT ROW 2B, 12D, 20B IAW AMM TASK 33-51-16-000-801 AND TASK 33-51-16-400-801 MCN NR 625721-1. RETURNED TO SERVICE.

Part: TRANSCEIVER — FAILED (VHF 2) · airframe 14,432 hrs · 15,622 cycles

IN FLIGHT, UNABLE TO COMMUNICATE ON VHF 2 (BOTH ARCDU'S). TRANSMIT LIGHT APPEARED DURING EACH TRANSMISSION. ATC FACILITIES COULD HEAR THIS RADIO DURING RADIO CHECKS. ON RETURN TO DEPARTURE, UNABLE TO RECEIVE ATIS WEATHER ON VHF 2. PERFORMED SELF TEST ON NR 2 COMM TRANSCEIVER, SELF TEST INDICATED TRANSCEIVER FAILURE. R & R NR 2 COM TRANSCEIVER WITH SERVICEABLE IAW AMM TASK 23-11-01-000-801/23-11-01-400-801. OPS TEST 23-11-00-710-801 CHECKS GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (AFT SERVICE) · airframe 14,284 hrs · 15,454 cycles

AFT SERVICE DOOR STIFF. LUBED AFT SERVICE DOOR. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: FLAP TRACK — GOUGED (LT WING TE FLAP) · airframe 14,074 hrs · 15,239 cycles

LT NR 3 FLAP TRACK LOWER RAIL GOUGED AT 0 DEGREE POSITION. BLENDED AREA OF CONCERN IAW SRM 51-50-50-02-03 TO A SMOOTH CONTOUR. BLEND AT 0 DEGREE POSITION (2.1"-2.5" FROM FWD EDGE OF LOWER FLAP TRACK) MEASURES 1.0"L X .4"W X .002" DEEP INTO THE CARBON/CARBIDE COATING ONLY. THERE IS NO DAMAGE FOUND TO THE UNDERLYING MATERIAL. BLEND IS WITHIN LIMITS IAW SRM 57-50-50-02-03. PERFORMED NDT INSPECTION OF THE LT NR 3 LOWER FLAP TRACK REPAIR AREA IAW NDT MANUAL PT 1 51-00-06-910-801 EDDY CURRENT METHOD. NO DEFFECTS NOTED. COMPLETED REPAIR PROCEDURE OF LT NR 3 FLAP TRACK LOWER RAIL AT 35 DEGREE POSITION IAW SRM 57-50-50-02-03.

Part: FLAP TRACK — GOUGED (LT WING TE FLAP) · airframe 14,074 hrs · 15,239 cycles

LT NR 3 FLAP TRACK LOWER RAIL GOUGED AT 0 POSITION. BLENDED AREA OF CONCERN IAW SRM 51-50-50-02-03 TO A SMOOTH CONTOUR. BLEND AT 0 POSITION (2.1"-2.40" FROM FWD EDGE OF LOWER FLAP TRACK) 1.0"L X .3"W X .001" DEEP INTO CARBON CARBIDE COATING ONLY (NO DAMAGE TO UNDERLYING METAL. BLEND IS WITHIN LIMITS IAW SRM 57-50-50-02-03. PERFORMED NDT INSPECTION OF THE LT NR 3 LOWER FLAP TRACK REPAIR AREA IAW NDT MANUAL PT 1 51-00-06-910-801 EDDY CURRENT METHOD. NO DEFFECTS NOTED. COMPLETED REPAIR PROCEDURE OF LT NR 3 FLAP TRACK LOWER RAIL AT 0 POSITION IAW SRM 57-50-50-02-03.

Part: FLAP TRACK — GOUGED (RT WING TE FLAP) · airframe 14,074 hrs · 15,239 cycles

RT NR 3 FLAP TRACK LOWER RAIL GOUGED AT 35 DEGREE POSITION. BLENDED AREA OF CONCERN IAW SRM 51-50-50-02-03 TO A SMOOTH CONTOUR. BLEND AT 35 DEGREE POSITION (24.4"-26.3" FROM FWD EDGE OF LOWER FLAP TRACK) MEASURES 1.90"L X .4"W IS THROUGH THE CARBON/CARBIDE COATING. THERE IS NO DAMAGE FOUND TO THE UNDERLYING MATERIAL. BLEND IS WITHIN LIMITS IAW SRM 57-50-50-02-03. PERFORMED NDT INSPECTION OF THE RT NR 3 LOWER FLAP TRACK REPAIR AREA IAW NDT MANUAL PT 1 51-00-06-910-801 EDDY CURRENT METHOD. NO DEFFECTS NOTED. COMPLETED REPAIR PROCEDURE OF RT NR 3 FLAP TRACK LOWER RAIL AT 35 DEGREE POSITION IAW SRM 57-50-50-02-03.

Part: FLAP TRACK — GOUGED (RT WING TE FLAP) · airframe 14,074 hrs · 15,239 cycles

LEFT NR 3 FLAP TRACK LOWER RAIL GOUGED AT 35 DEGREE POSITION. BLENDED AREA OF CONCERN IAW SRM 51-50-50-02-03 TO A SMOOTH CONTOUR. BLEND AT 35 DEGREE POSITION (24.35"-26.2" FROM FWD EDGE OF LOWER FLAP TRACK) MEASURES 1.85"L X .4"W IS THROUGH THE CARBON/CARBIDE COATING. THERE IS NO DAMAGE FOUND TO THE UNDERLYING METAL. BLEND IS WITHIN LIMITS IAW SRM 57-50-50-02-03. PERFORMED NDT INSPECTION OF THE LT NR 3 LOWER FLAP TRACK REPAIR AREA IAW NDT MANUAL PT 1 51-00-06-910-801 EDDY CURRENT METHOD. NO DEFFECTS NOTED. COMPLETED REPAIR PROCEDURE OF LT NR 3 FLAP TRACK LOWER RAIL AT 35 DEGREE POSITION IAW SRM 57-50-50-02-03.

Part: SPACER — MISSING (EMERGENCY EXIT) · airframe 14,030 hrs · 15,190 cycles

FORWARD LOWER EMERGENCY EXIT DOOR IS MISSING SPACER. ALSO DOOR HANDLE BELL CRACK AND HANDLE WERE CORRODED. REPLACED SPACER IAW AMM 52-23-01-400-801. REMOVED CORROSION FROM EFFECTED AREAS.

Part: DOOR — LACK OF LUBE · airframe 14,010 hrs · 15,168 cycles

F/A REPORTS THAT THE AFT SERVICE DOOR CAN NOT BE OPENED FROM THE OUTSIDE. CLEANED AND LUBED THE AFT SERVICE DOOR. DOOR OPENS AND CLOSES AS NECESSARY. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: EXTINGUISHER — MALFUNCTIONED (ZONE 100) · airframe 13,997 hrs · 15,154 cycles

MASTER WARNING BTL LOW (APU) LIGHT FLASHING INTERMITTENTLY AND CHECK FIRE DETECT LIGHT. C/W OPS TEST OF THE APU FIRE DETECTION SYS. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY WHILE MANIPULATING WIRES TO APU FIRE BOTTLE. R & R APU FIRE EXTINGUISHER BOTTLE AS A PRECAUTIONARY MEASURE IAW AMM TASKS 26-23-01-000-801 AND 26-23-01-400-801. OPS CHECK GOOD. RETURNED TO SERVICE, MEL CLEARED.

Part: SHAFT — LACK OF LUBE (DOOR HANDLE) · airframe 13,424 hrs · 14,540 cycles

AFT SERVICE DOOR HARD TO OPEN AND CLOSE. LUBRICATED OUTSIDE HANDLE SHAFT. PERFORMED OPS CHECK IAW AMM 52-41-00-710-801. OPS CHECKED GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: BYPASS VALVE — MALFUNCTIONED (ZONE 400) · airframe 12,866 hrs · 13,943 cycles

ON CLIMB OUT, NR 1 OIL TEMP CLIMBED TO 113 FOLLOWED HIGH OIL TEMP CHECKLIST AND REDUCED TORQUE BY 20 PERCENT AND LATER TEMP REDUCED TO 107 AND BELOW. ALL OTHER LIMITATIONS WERE NOT EXCEEDED. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS, FOUND NO FAULTS. EMU POWERPLANT EXCEEDANCE WAS 113.7 C FOR 588 SEC. AND WAS IN AREA A OF CHART 603 IAW AMM TASK 05-11-00-992-802. PERFORMED OPS TEST OF OIL COOLER FLAP DOOR ACTUATOR IAW AMM TASK 79-21-31-710-801. OPS CHECK GOOD. R & R OIL COOLER BYPASS VALVE IAW AMM TASK 79-21-06-000-801/79-21-06-400-801. OPS CHECK GOOD. LEAK CHECK GOOD. ALL TEMPS STAYED WITHIN LIMITS. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (OIL PRESSURE) · airframe 12,478 hrs · 13,548 cycles

NR 2 ENGINE OIL PRESSURE INTERMITTENTLY HIGH 72-106 PSI. RETURNED TO FIELD. LANDING UNEVENTFUL. INTEROGATED CDS. FOUND FAULT CODE 944 ON NR 2 ENGINE CHANNEL A AND B. IAW FIM TASK 79-20-00-810-886 PARA 4A. CLEARED FAULT CODE AND GROUND RAN ACFT IAW AMM TASK 71-00-00-768-805. FAULT CODE DID NOT RETURN. IAW MX REQUEST R & R NR 2 ENG OIL PRESSURE TRANSDUCER IAW AMM TASK 79-31-01-000-801/400-801. RAN ACFT AND PERFORMED AMM TASK 71-00-00-780-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: CONTROL CABLE — OUT OF ADJUST (BRAKES) · airframe 12,335 hrs · 13,391 cycles

BRAKES WERE VERY WEAK ON LANDING ROLLOUT, POST TOUCHDOWN. REPORTED AS WEAK ON BOTH PILOT AND F/O LANDINGS. ADJUSTED CABLE TENSION AT BRAKE CONTROL VALVE AS WELL AS FUNCTIONAL TEST OF MAIN BRAKE SYS. ALL TEST OK. RETURNED TO SERVICE.

Part: PLATE — LOOSE (ZONE 800) · airframe 12,298 hrs · 13,346 cycles

CLIMBING THROUGH 10,000, INFORMED THAT SOMETHING APPEARED TO BE STICKING OUT DOOR , AND F/A COULD SEE OUT OF DOOR. DOOR SECURED AND ACFT WAS PRESSURIZING AT 11,000. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND AFT SERVICE DOOR KICK PLATE HAD FALLEN DOWN BETWEEN DOOR SEAL AND LOWER DOOR THRESHOLD. RESECURED AFT SERVICE DOOR LOWER KICK PLATE. DID NOT NOTE ANY DAMAGE. SEAL REMAINED INTACT. PERFORMED PRESSURIZATION FOR MX IAW AMM TASK 21-00-00-863-801 AND 21-00-00-863-802. PRESSURE HELD STEADY NO LEAKS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CAM — WORN (PAX DOOR) · airframe 11,806 hrs · 12,829 cycles

AFT PASSENGER DOOR WILL NOT OPEN. INSPECTED AFT PAX DOOR, FOUND INTERLOCK CAM ASSY WORN. R & R AFT PAX DOOR INTERLOCK CAM ASSY. PERFORMED OPS TEST OF THE AFT PAX DOOR IAW TASK 52-12-00-710-802. OPS CHECK GOOD NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: SHAFT — FAILED (DOOR HANDLE) · airframe 11,760 hrs · 12,783 cycles

REAR PASSENGER DOOR HARD TO OPEN. PERFORMED GVI OF THE AFT PAX DOOR AND SURROUNDING AREA, NO DEFECTS NOTED. CONFIRMED THE AFT PAX DOOR CLOSES AND LOCKS NORMALLY. CONFIRMED ALL DOOR INDICATIONS OPERATED NORMALLY. REPLACED AFT PAX DOOR HANDLE SHAFT & BEARINGS IAW AMM, FUNCTIONAL TESTED, PRESSURE AND LEAK TESTED GOOD, DOOR OP'S SMOOTHLY. RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 11,233 hrs · 12,241 cycles

F/A COMPLAINS THAT THE AIRSTAIR DOOR IS HARD TO OPEN & CLOSE. THE LEVER IS HARD TO PUSH UP& DOWN. INSPECTED FWD PASSENGER DOOR (AIRSTAIR DOOR) & DRAIN PLUGS. DRAINS DID HAVE A GOOD AMOUNT OF WATER. SO LET DRAINS DRAIN. OPS CHECK OF PASSENGER DOOR GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,099 hrs · 12,110 cycles

F/A'S REPORT A BURNING RUBBER ODOR AROUND THE MID-CABIN AREA. THIS WAS FIRST NOTICED DURING CRUISE FLIGHT. ODOR WAS NOTICED BY SERVERAL PASSENGERS, AND WAS INTERMITTENT IN NATURE. THE OVERHEAD LIGHTS WERE OFF WHEN THIS HAPPENED. ODOR WAS NEVER NOTICED BY THE PILOTS. OPERATED EACH ENGINE INDIVIDUALLY WITH BLEEDS ON AT VARIOUS TEMP SETTINGS FOR SEVERAL MINUTES. NO UNUSUAL ODORS WERE NOTED. THERE WERE NO CURRENT ECS FAULTS. THERE IS NO HISTORY OF CABIN SMELLS WITHIN THREE MONTHS. NO OTHER DEFECTS WERE NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FWD BAG DOOR CUTOUT BOTTOM EDGE OF CUTOUT HAS CORROSION. REMOVED CORROSION FROM EDGE CHANNEL IAW SRM 51-21-00-00-01, FOUND TO BE OUT OF LIMITS IAW SRM 53-20-25-00-01. REMOVED DOOR CHANNEL IAW 51-42-05-02-01. MATCH DRILLED NEW EDGE CHANNEL IAW SRM 51-42-05-02-01. INSTALLED NEW EDGE CHANNEL ANGLE IAW SRM 51-42-05-02-01.

Part: SUPPORT — CORRODED (THRESHOLD) · airframe 10,744 hrs · 11,707 cycles

FORWARD PAX DOOR THRESHOLD SUPPPORT IS CORRODED ON THE LOWER SIDE. REMOVED CORROSION IAW SRM 51-21-00-00-02. MEASURED BLEND, MIN REMAINING THICKNESS .037", FOUND TO BE OUT OF LIMTS IAW RD 8/4-53-1660. REMOVED CORRODED THRESHOLD SUPPORT IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. LOCATED AND MATCH DRILLED REPLACEMENT THRESHOLD SUPPORT IAW SRM 51-42-05-02-01. INSTALLED THRESHOLD SUPPORT IAW SRM 51-42-05-02-01 AND 51-40-15-02-01.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 10,744 hrs · 11,707 cycles

COCKPIT SEAT TRACK DAMAGED. SMOOTHED OUT DAMAGE IAW SRM 51-14-00-02-01 AND 53-10-49-02-01. FOUND SEAT RAIL CAP CRACKED REF SRM 53-10-49-02-01 STEP 5H MIN REMAINING THICKNESS (OTBD EDGE OF TRACK CAP) .168" REF NTM 51-00-02-250-801 PT4 REV 6. DAMAGE WITHIN LIMITS OR RD 8/4-53-3867. COMPLIED WITH TASK CARDS RD 8/4-53-3867 AND 6-53-1008.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

INNER ANTENNA SKIN DOUBLER STR 33-32S, FR 71.2-94.8 IS CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-01. MIN REMAINING THICKNESS .034". RECEIVED AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3891. COMPLIED WITH RD 8/4-53-3891 AND TASK CARD RD 8/4-53-3891.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME X28.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD LT PAX DOOR THRESHOLD. REMOVED CORROSION FROM FLANGE ANGLE IAW SRM 51-21-00-00-01. FOUND TO BE OUT OF TOLERANCE IAW SRM 53-20-23-00-01. FABRICATED NEW FLANGE FROM 7075 T6 .050 IAW TASK CARD 6-53-1006. INSTALLED FLANGE IAW SRM 51-42-5-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME X8.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD LT PAX DOOR THRESHOLD. REMOVED CORROSION FROM FLANGE ANGLE IAW SRM 51-21-00-00-01. FOUND TO BE OUT OF TOLERANCE IAW SRM 53-20-23-00-01. FABRICATED NEW FLANGE FROM 7075 T6 .050 IAW TASK CARD 6-53-1006. INSTALLED FLANGE IAW SRM 51-42-5-02-01.

Part: STRINGER — CORRODED (BS 373.150 S31L) · airframe 10,744 hrs · 11,707 cycles

STRINGER 31P END TIE AFT SIDE OF FR 373.150 HAS CORROSION AROUND A FASTENER. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01. REMOVED STRINGER TIE END IAW SRM 51-42-05-02-01. RECEIVED NEW STRINGER END TIE LOCATED AND MATCHED DRILLED TO A/P IAW SRM 51-40-07-02-01. INSTALLED STRINGER END TIE IAW SRM 51-40-00-00-01, 51-42-15-02-01 AND 51-40-15-02-01.

Part: ROLLER — GOUGED (CARGO DOOR) · airframe 10,744 hrs · 11,707 cycles

AFT LT BAGGAGE DOOR FWD LOWER ROLLER FITTING HAS GOUGES. REMOVED CAM FOLLOWER FROM ROLLER ASSY IAW AMM 52-31-24-000-801. REMOVED FWD LOWER ROLLER FITTING IAW AMM 52-31-24-000-801. MATCH DRILLED NEW FITTING TO DOOR IAW SRM 51-40-07-02-01. INSTALLED FITTING IAW AMM 52-31-24-400-801.

Part: STRINGER CLIP — CORRODED (BS 373.15 S31L) · airframe 10,744 hrs · 11,707 cycles

STRINGER 31P END TIE ON AFT SIDE OF FR 373.150 HAS CORROSION AROUND A FASTENER. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01. REMOVED AFFECTED FASTENER IAW SRM 51-40-15-02-01, REMOVED STRINGER END TIE IAW SRM 51-42-05-02-01. RECEIVED NEW STRINGER END TIE, LOCATED AND MATCH DRILLED TO AP IAW SRM 51-40-07-02-01. INSTALLED STRINGER END TIE IAW SRM 51-40-00-00-01, 51-42-15-02-01 AND 51-40-15-02-01.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 10,744 hrs · 11,707 cycles

TOP SIDE OF LT OTBD FLAP HAS CHAFE MARKS ON INBD SIDE. BLENDED CHAFE MARKS IAW RD 8/4-57-1594. BLENDED AREAS OUT OF LIMITS LIMITS IAW RD 8/4-57-1594. RECEIVED AND COMPLIED WITH RD 8/4-57-1631 FROM ENGINEERING.

Part: PANEL — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 262FT FORE MATING SURFACE HAS FRETTING. BLENDED DAMAGED AREAS IAW RD 8/4-53-521, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH REPAIR IAW RD 8/4-53-521.

Part: PANEL — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 261LT FORE AND AFT MATING SURFACE HAS FRETTING. REMOVED FRETTING DAMAGE IAW RD 8/4-53-521. COMPLIED WITH RD 8/4-53-521.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 262FT FORE MATING SURFACE HAS FRETTING. BLENDED DAMAGE AREAS IAW RD 8/4-53-521. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLETED REPAIRS IAW RD 8/4-53-521.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 261FT FWD MATING SURFACE HAS FRETTING. BLENDED DAMAGED AREAS IAW RD 8/4-53-521, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH REPAIR IAW GENERIC PERMANENT REPAIR IAW RD 8/4-53-521.

Part: SKIN — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 261HT AFT MATING SURFACE HAS FRETTING. BLENDED DAMAGE AREAS IAW RD 8/4-53-521. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLETED REPAIRS IAW RD 8/4-53-521.

Part: PANEL — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 261LT FORE AND AFT MATING SURFACE HAS FRETTING. BLENDED DAMAGE AREAS IAW RD 8/4-53-521. MINIMUM REMAINING THICKNESS .093" FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLETED REPAIRS IAW RD 8/4-53-521.

Part: PANEL — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 261HT AFT MATING SURFACE HAS FRETTING. BLENDED DAMAGE FROM PANEL REF RD 8/4-53-521 AND FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH GENERIC PERMANENT REPAIR FOR CHAFING PANEL IAW RD 8/4-53-521.

Part: PANEL — DAMAGED · airframe 10,744 hrs · 11,707 cycles

PANEL 262HT FWD MATING SURFACE HAS FRETTING. BLENDED DAMAGED AREAS IAW RD 8/4-53-521, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH REPAIR IAW GENERIC PERMANENT REPAIR RD 8/4-53-521.

Part: PANEL — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

PANEL 262HT FWD MATING SURFACE HAS FRETTING. BLENDED DAMAGE AREAS IAW RD 8/4-53-521. MINIMUM REMAINING THICKNESS .098" FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLETED REPAIRS IAW RD 8/4-53-521.

Part: PANEL — DAMAGED · airframe 10,744 hrs · 11,707 cycles

PANEL 262AT FWD MATING SURFACE HAS FRETTING. BLENDED DAMAGED AREAS IAW RD 8/4-53-521, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH REPAIR IAW GENERIC PERMANENT REPAIR RD 8/4-53-521.

Part: PANEL — DAMAGED · airframe 10,744 hrs · 11,707 cycles

PANEL 261CT FWD MATING SURFACE HAS FRETTING. BLENDED DAMAGED AREAS IAW RD 8/4-53-521, FOUND TO BE WITHIN LIMITS OF RD 8/4-53-521. COMPLIED WITH REPAIR IAW GENERIC PERMANENT REPAIR IAW RD 8/4-53-521.

Part: SUPPORT BRACKET — CORRODED · airframe 10,744 hrs · 11,707 cycles

RELAY SUPPORT BRACKET ABOVE STR 32S IS CORRODED FR 94.8 TO 116.0. REMOVED CORROSION IAW SRM 51-21-00-00-01. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED BRACKET IAW SRM 51-42-05-02-01. FABRICATED NEW BRACKET IAW TASK CARD 6-53-1010. COMPLIED WITH TASK CARD 6-53-1010.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FORWARD PAX DOOR THRESHOLD TOP PLATE IS CORRODED. REMOVED THRESHOLD TOP PLATE IAW SRM 51-40-07-02-01. MEASURED CORRODED MEMBER AND FOUND OUT OF LIMITS IAW RD 8/4-53-1660. RECEIVED REPLACEMENT THRESHOLD , PREPARED THRESHOLD FOR INSTALLATION AND INSTALLED IAW SRM 51-42-05-02-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

CORROSION FOUND ON VERTICAL ANGLE AT STA 6.700 ABOVE STR 25P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-23-00-01. REMOVED ANGLE IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. FABRICATED ANGLE IAW TASK CARD 6-53-1011. INSTALLED ANGLE IAW SRM 51-42-05-02-01. COMPLIED WITH TASK CARD 6-53-1011.

Part: PLATE — CORRODED (THRESHOLD) · airframe 10,744 hrs · 11,707 cycles

FORWARD PAX DOOR THRESHOLD TOP PLATE IS CORRODED. REMOVED THRESHOLD TOP PLATE IAW SRM 51-40-07-02-01. MEASURED CORRODED THRESHOLD MEMBER, MINIMUM REMAINING THICKNESS .046", FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-1660. PREPARED FOR INSTALLATION AND INSTALLED NEW THRESHOLD IAW SRM 51-42-05-02-01, AND 51-42-05-02-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

CORROSION FOUND ON VERTICAL ANGLE AT STATION 6.700 ABOVE STGR 25P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. FABRICATED ANGLE IAW TASK CARD 6-53-1011. INSTALLED ANGLE IAW SRM 51-42-5-02-01. COMPLIED WITH TASK CARD 6-53-1011.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

CORROSION FOUND ON VERTICAL ANGLE AT STA 26.700 ABOVE STR 25P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-23-00-01. REMOVED BRACKET IAW SRM 51-51-42-05-02-01 AND 51-40-15-02-01. FABRICATED NEW PART IAW TASK CARD 6-53-1011. INSTALLED PART IAW SRM 51-42-05-02-01. COMPLIED WITH TASK CARD 6-53-1011.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FORWARD NUTPLATE ANGLE AND INTERCOSTAL FOR ANTENNA STR 33-32S, FR 71.2-94.8 ARE CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3891. MINIMUM REMAINING THICKNESS .121". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3891. RESTORED SURFACE PROTECTION IAW RD 8/4-53-3891. COMPLIED WITH TASK CARD RD 8/4-53-3891.

Part: SUPPORT — CORRODED (THRESHOLD) · airframe 10,744 hrs · 11,707 cycles

EMERGENCY EXIT THRESHOLD SUPPORT IS CORRODED BY THE LOWER FITTINGS AND ON THE LOWER SIDE. REMOVED CORROSION IAW SRM 51-21-00-00-02. MEASURED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-21-00-01. REMOVED THRESHOLD SUPPORT IAW SRM 51-42-05-02-01, 51-42-15-02-01 AND 51-41-05-00-01. PREPARED FOR INSTALLATION AND INSTALLED NEW SUPPORT IAW SRM 51-40-07-02-01, 51-42-05-02-01 AND 51-42-45-02-01. APPLIED CPC IAW AMM 51-25-01-390-801.

Part: GUSSET — CORRODED (BS 697) · airframe 10,744 hrs · 11,707 cycles

FLOOR GUSSET AT AFT END OF AFT PAX DOOR IS CORRODED STA X697. REMOVED CORROSION IAW SRM 51-21-00-00-02, MINIMUM REMAINING THICKNESS .064". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 8/4-53-3892. RESTORED SURFACE PROTECTION IAW RD 8/4-53-3892. COMPLIED WITH TASK CARD RD 8/4-53-3892.

Part: FRAME — CORRODED (BS 664.5) · airframe 10,744 hrs · 11,707 cycles

FRAME 664.5 FLANGES ARE CORRODED STR 33-31P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .062". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRD 8/4-53-2344. RESTORED SURFACE PROTECTION AND APPLIED CPC IAW RD 8/4-53-2344.

Part: FLOORBEAM — CORRODED (BS 697) · airframe 10,744 hrs · 11,707 cycles

FLOORBOARD ANGLE BY AFT PAX DOOR AFT END IS CORRODED FORWARD OF STA X697. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS .040". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3892. RESTORED SURFACE PROTECTION IAW RD 8/4-53-3892. COMPLIED WITH HORIZON TASK CARD RD 8/4-53-3892.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

AFT NUTPLATE ANGLE FOR ANTENNA STR 33-32S, FR 71.2-94.8 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .057". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRD 8/4-53-3891. RESTORED SURFACE PROTECTION AND APPLIED CPC IAW SRM 51-25-05-02-01 AND AMM 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (BS 697-714) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 9 HAS CORROSION AT STA X697-714. STARTED TO REMOVE DAMAGE, BUT FOUND TO BE OUT OF LIMITS. REPLACED THE NR 9 SEAT TRACK IAW SRM 51-42-05-02-01.

Part: WEB — CORRODED (BS 714-747) · airframe 10,744 hrs · 11,707 cycles

AFT CARGO LT UNDER FLOOR WEB HAS AREAS OF CORROSION AT STATION 714-747. REMOVED CORROSION IAW SRM 51-21-00-00-02 CONFIRMED CRACK FREE. REMAINING THICKNESS .048" WITHIN LIMITS. ALODINED AND PRIMED AREA.

Part: GUIDE — DAMAGED (PAX DOOR) · airframe 10,744 hrs · 11,707 cycles

AFT PAX DOOR CUTOUT FWD AND AFT MIDDLE ROLLER GUIDES HAS GROOVES WORN INTO TOP SIDE OF FITTINGS. BLENDED TO REMOVE GROOVES IAW RD 8/4-52-145. COMPLIED WITH RD 8/4-52-145.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 5 IS CORRODED. REMOVED CORROSION IAW RD 8/4-53-884. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK NR 5 IAW SRM 51-42-05-02-01. MATCH DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-07-02-01, 51-42-05-02-01, 51-40-15-02-01 AND 51-41-05-00-01..

Part: WEB — CORRODED (BS 714-747) · airframe 10,744 hrs · 11,707 cycles

AFT CARGO LT UNDERFLOOR WEB HAS AREA OF CORROSION STA 714-747. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. DAMAGE AND REMAINING THICKNESS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3872. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-45-02-01 AND RD 8/4-53-3872. COMPLIED WITH TASK CARD RD 8/4-53-3872.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FLOOR WEB ON SEAT TRACK 5 IS CORRODED STA 1.00 TO 19.000. REMOVED CORROSION FROM WEB IAW SRM 51-21-00-00-01. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-43-00-01. REMOVED WEB IAW SRM 51-42-05-02-01. FABRICATED NEW WEB IAW SRM 51-24-35-02-01 AND 51-40-07-02-01. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED WEB IAW SRM 51-42-05-02-01 AND TOPCOATED IAW SRM 51-25-15-02-01.

Part: ANGLE — CORRODED (BS 783.1) · airframe 10,744 hrs · 11,707 cycles

AFT CARGO LT FLOOR LEVEL ANGLE AT STA 783.1 IS CORRODED IN 3 AREAS. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. DAMAGE AND REMAINING THICKNESS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3872. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-45-02-01 AND RD 8/4-53-3872. COMPLIED WITH TASK CARD RD 8/4-53-3872.

Part: STRAP — CORRODED (THRESHOLD) · airframe 10,744 hrs · 11,707 cycles

AFT CARGO DOOR THRESHOLD STRAP HAS CORROSION AROUND 2 NUTPLATES. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. DAMAGE WITHIN LIMITS IAW RD 8/4-53-3872. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-45-02-01 AND RD 8/4-53-3872.

Part: WEB — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

AFT CARGO UNDERFLOOR WEB HAS AREAS OF CORROSION ON MOUNT SURFACE FOR PANEL 144JZ. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. DAMAGE AND REMAINING THICKNESS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3872. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW SRM 51-21-10-02-01, 51-25-45-02-01 AND RD 8/4-53-3872.

Part: PANEL — CRACKED (RT WING) · airframe 10,744 hrs · 11,707 cycles

RT INBD WING STRESS PANEL LANDING HAS 3 HOLES THAT HAVE CRACKS. REPAIRED IAW RD 8/4-57-526 AND RD 8/4-53-513.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 32.4 FLANGES ARE CORRODED AT STRINGER 28S. REMOVED CORROSION, BUT MATERIAL REMOVED WAS FOUND TO BE OUTSIDE LIMITS. FABRICATED AND INSTALLED NEW FRAMES IAW SRM 51-00-00-250-801. PRIMED AND TREATED NEW FRAMES AND RIVETS.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

STRINGER 24S SPLICE AT FR 116.0 HAS CORRODED FASTENERS AND POSSIBLE CORROSION. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .051", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3857. TREATED, PRIMED IAW SRM 51-21-10-02-01, 51-25-10-02-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FLOORBEAM 19.4 IS CORRODED BY THE FORWARD BAGGAGE DOOR. REMOVED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .089. CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS RD 8/4-53-3899. RESTORED SURFACE PROTECTION AND COMPLIED WITH REPAIR IAW RD 8/4-53-3899.

Part: FRAME — CORRODED (BS 341 S29-32L) · airframe 10,744 hrs · 11,707 cycles

FRAME 341 FLANGES ARE CORRODED AT STRINGER 32P-29P. REMOVED FLEX DUCT AND CLAMP FOM. REMOVED LIGHT CORROSION IAW AMM 51-22-44-000-801. REMAINING THICKNESS 0.51". CONFIRMED CRACK FREE. NO MATERIAL LOSS NOTED AND NO PITTING. ALODINED PRIMED AND PAINTED AREA. RE-INSTALLED REMOVED COMPONENTS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FLOORBOARD SUPPORT Z ANGLE HAS CORROSION AT AFT END OF SERVICE DOOR. REMOVED CORROSION IAW SRM 51-21-00-00-02. MATERIAL LOSS MINIMUM THICKNESS MEASURED .034". LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-40-43-00-01. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. RECEIVED RD 8/4-53-3869. LIMITS ALLOWED TO .034" MATERIAL LOSS FOUND WITHIN LIMITS IAW RD 8/4-53-3869. RESTORED SURFACE PROTECTION IAW RD 8/4-53-3869. COMPLIED WITH RD 8/4-53-3869.

Part: WEB — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FORWARD DRAFT BULKHEAD UNDERFLOOR SUPPORT WEB IS CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-01. REMOVED WEB IAW SRM 51-42-45-02-01, MINIMUM REMAINING THICKNESS .037", NOMINAL IS .050. FABRICATED NEW WEB IAW TASK CARD 6-53-1004. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW SUPPORT WEB IAW SRM 51-42-15-02-01 AND 51-42-05-02-01..

Part: STRINGER — CORRODED (FUSELAGE)

STRINGER 26S CORRODED FR 136 TO 156. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .066", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3879. ALODINED, PRIMED IAW SRM 51-21-10-02-01, 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 216 FLANGES ARE CORRODED STR 32P-29P. REMOVED CORROSION IAW RD 8/4-53-2344. CONFIRMED CRACK FREE IAW NTM 51-00-02-250-801 AND 51-00-01-250-801. ALL WORK ACCOMPLISHED IAW RD 8/4-53-2344.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

RT FLOORBOARD SUPPORT Z CHANNEL IS CORRODED FR 1.00 TO 47.00. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED BLENDS ARE CRACK FREE REF NTM 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3872. RESTORED SURFACE PROTECTION AS REQUIRED IAW RD 8/4-53-3870. COMPLIED WITH TASK CARD RD 8/4-53-3870.

Part: FRAME — CORRODED (FUSELAGE)

FRAME 341 FLANGES ARE CORRODED STR 32P-29P. REMOVED LIGHT CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. NO MATERIAL LOSS NOTED, SURFACE CORROSION WITH NO PITTING. TREATED, PRIMED AND PAINTED IAW RD 8/4-53-2344.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

SHEAR WEB PANEL 144GZ FOUND CORRODED UPON REMOVAL. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-21-00-00-02. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 51-21-00-00-02. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

STRINGER 31S CORRODED FR 604.5 TO 624.5. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3877. MINIMUM REMAINING THICKNESS .081", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. TREATED, PRIMED IAW RD 8/4-53-3877.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

STRINGER 26S CORRODED FR 156 TO 176. BLENDED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .062", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3879. ALODINED, PRIMED IAW SRM 51-21-10-02-01, 51-25-10-02-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

RT FLOORBOARD SUPPORT Z CHANNEL IS CORRODED FR 1.00 TO 47.00. REMOVED CORROSION IAW SRM 51-21-00-00-01. CONFIRMED BLENDES TO BE CRACK FREE REF NTM 51-00-01-250-801. REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-3870. RESTORED SURFACE PROTECTION AS REQUIRED IAW RD 8/4-53-3870. COMPLIED WITH TASK CARD RD 8/4-53-3870.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 136 FLANGES ARE CORRODED STR 30P-32P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .040", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED IAW SRM 51-21-10-02-01. APPLIED CPC IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 564.5) · airframe 10,744 hrs · 11,707 cycles

FRAME 564.5 FLANGES ARE CORRODED AND HAS MISSING FASTENER STR 31P-32P. BLENDED CORROSION IAW RD 8/4-53-2344. REMOVED RIVETS IAW SRM 51-41-05-02-01. MINIMUM REMAINING THICKNESS .051", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. INSTALLED 1 RIVET IAW SRM 51-42-05-02-01. PAINTED EXTERNAL SKIN IAW SRM 51-25-05-02-01.

Part: FRAME — CORRODED (BS 321) · airframe 10,744 hrs · 11,707 cycles

FRAME 321 FLANGE IS CORRODED STR 32P-31P. REMOVED CORROSION IAW 51-21-00-00-02. MINIMUM REMAINING THICKNESS .049", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND PAINTED AND APPLIED CPC IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 19.4 FLANGES ARE CORRODED STR 33-27S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .037", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED IAW 51-21-10-02-01 AND 51-25-10-02-01. APPLIED CPC IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 94.8 FLANGES 30P-30S ARE CORRODED. REMOVED CORROSION FROM AFFECTED FLANGES IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .038", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND APPLIED CPC IAW RD 8/4-53-2344.

Part: SEAT TRACK — CORRODED (BS 697-714) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 16 HAS CORROSION AND SCRATCHES STA X697-714. REMOVED CORROSION AND MEASURED, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK 16 IAW SRM 51-42-05-02-01. MATCH DRILLED, TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW SEAT TRACK NR16 IAW SRM 51-42-05-02-01.

Part: FRAME — CORRODED (BS 644 S30-33L) · airframe 10,744 hrs · 11,707 cycles

FRAME 644.5 FLANGES ARE CORRODED STR 33-30P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .056", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 624.5 S30-33L) · airframe 10,744 hrs · 11,707 cycles

FRAME 624.5 FLANGES ARE CORRODED STR 33-30P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS .055", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND APPLIED SURFACE PROTECTION IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 136) · airframe 10,744 hrs · 11,707 cycles

FRAME 136 FLANGES ARE CORRODED STR 30S-32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .045", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. DAMAGE AND REMAINING THICKNESS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND APPLIED CPC IAW RD 8/4-53-2344.

Part: FRAME — CORRODED · airframe 10,744 hrs · 11,707 cycles

FRAME 19.4 FLANGES STR 30P-32P ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .038", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS DETERMINED TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. PAINTED AND CPC IAW SRM 51-25-25-02-01 AND RD 8/4-53-2344.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

FOUND CORROSION IN COUNTERSINK HOLE DIAMETER PANEL 622CT. REPLACED PANEL 622CT WITH A SERVICEABLE PANEL.

Part: SEAT TRACK — CORRODED (BS 624.5-664.5) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK CORRODED FORWARD OF 624.5 TO AFT OF FR 664.5. BLENDED CORRODED AREA AND FOUND REMOVED MATERIAL EXCEEDED LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK 15 IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. PREPARED NEW SEAT TRACK FOR INSTALLATION IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED SEAT TRACK NR15 IAW SRM 51-42-05-02-01, 51-41-05-00-01, 51-40-15-02-01. ALODINE, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 71.2 FLANGES 30P-32P ARE CORRODED. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: STRINGER — CORRODED (BS 547-564 S31R) · airframe 10,744 hrs · 11,707 cycles

STRINGER 31S HAS CORRODED FASTENERS AND POSSIBLE CORROSION FR 547.0 TO 564.5. REMOVED 12 RIVETS IAW SRM 51-42-05-02-01 AND BLENDED CORROSION IAW SRM 51-21-00-00-01. FOUND WITHIN LIMITS RD 8/4-53-3878. TREATED AND PRIMED IAW SRM 51-21-10-02-01, 51-25-10-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. RESTORED FINISH IAW SRM 51-25-05-02-01 AND RD 8/4-53-3878.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 156 FLANGES ARE CORRODED STR 30S-32S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 509.5 FLANGES ARE CORRODED STR 30P-32P. REMOVED CORROSION FROM AFFECTED AREAS IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 116.0 FLANGES ARE CORRODED STR 32P-30P. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 301 FLANGES ARE CORRODED STR 33-31S. REMOVED CORROSION FROM AFFECTED AREAS AND COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 156 FLANGES ARE CORRODED STR 30P-32P. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 176 FLANGES ARE CORRODED STR 33-30P. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 301 FLANGES ARE CORRODED STR 30P-32P. REMOVED CORROSION FROM AFFECTED AREAS AND COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 584.5 FLANGES ARE CORRODED STR 33-30P. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 71.2 FLANGE IS CORRODED STR 31S-32S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 176 FLANGES ARE CORRODED STR 32S-30S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 584.5 FLANGES ARE CORRODED STR 33-30S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 281 FLANGES ARE CORRODED STR 30P-32P. REMOVED CORROSION IN AFFECTED AREAS AND REPAIRED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 196 FLANGE IS CORRODED STR 31P-30P. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 281 FLANGE IS CORRODED STR 32S-31S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 116.0 FLANGES ARE CORRODED STR 33-30S. REMOVED CORROSION FROM AFFECTED AREAS IAW RD 8/4-53-2344. COMPLETED REPAIRS IAW RD 8/4-53-2344.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

STRINGER 31P HAS CORRODED FASTENERS AND POSSIBLE CORROSION FR 604.5 TO 624.5. REMOVED FASTENERS IAW SRM 51-42-05-02-01. CORROSION LIMITED TO FASTENERS ONLY. INSTALLED FASTENERS IAW SRM 51-42-05-00-01. ALUMINIZED AND APPLIED CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801.

Part: FRAME — CORRODED · airframe 10,744 hrs · 11,707 cycles

FRAME 18.25, FLANGE, STR 33 - 32S CORRODED. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 216) · airframe 10,744 hrs · 11,707 cycles

FRAME 216, FLANGES ARE CORRODED STR 33-30S. BLENDED OUT ALL CORROSION IAW RD 8/4-53-2344. MATERIAL LOSS FOUND TO BE IN LIMITS OF RD. COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 547 S31-32L) · airframe 10,744 hrs · 11,707 cycles

FRAME 547 FLANGE IS CORRODED STR 32P- 31S. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 196, FLANGES ARE CORRODED STR 32S - 30S. REMOVED CORROSION FROM AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 604.5) · airframe 10,744 hrs · 11,707 cycles

FRAME 604.5 FLANGE IS CORRODED STR 29P- 30P. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 236) · airframe 10,744 hrs · 11,707 cycles

FRAME 236, FLANGE IS CORRODED STR 30P - 29P. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 258.5) · airframe 10,744 hrs · 11,707 cycles

FRAME 258.5, FLANGES ARE CORRODED STR 32P - 30P. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 413 S31-32R)

FRAME 413, FLANGE IS CORRODED STR 31S - 32S. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 1.00, FLANGE IS CORRODED STR 33 - 32S. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 1.00, FLANGE IS CORRODED STR 31P - 32P . BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 564.5 S32-33L) · airframe 10,744 hrs · 11,707 cycles

FRAME 564.5 FLANGE IS CORRODED STR 33-32P. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 469.5) · airframe 10,744 hrs · 11,707 cycles

FRAME 469.5 FLANGE IS CORRODED STR 31P- 32P. REMOVED CORROSION FROM AFFECTED AREA AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 604.5 S31-32L) · airframe 10,744 hrs · 11,707 cycles

FRAME 604.5 FLANGE IS CORRODED STR 31P-32P. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 489.5 S31-32R) · airframe 10,744 hrs · 11,707 cycles

FRAME 489.5 FLANGE IS CORRODED STR 31S - 32S. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 627.5 S31-32R) · airframe 10,744 hrs · 11,707 cycles

FRAME 624.5 FLANGE IS CORRODED STR 31S-32S. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 47.975, FLANGES STR 29S-30P ARE CORRODED. REMOVED CORROSION IN AFFECTED AREAS AND REPAIRED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 489.5 S29-30L) · airframe 10,744 hrs · 11,707 cycles

FRAME 489.5 FLANGE IS CORRODED STR 29P - 30P. BLENDED OUT CORROSION IN AFFECTED AREAS AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 621BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-441.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

FRAME 19.4 UPPER FLANGE IS CORRODED STR 33-32S. REMOVED CORROSION FROM FRAME IAW SRM 51-21-00-00-02. REMAINING THICKNESS .041", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. RESTORED SURFACE IAW SRM 51-25-15-02-01.

Part: PANEL — DAMAGED (RT WING) · airframe 10,744 hrs · 11,707 cycles

RT INBD WING STRESS PANEL LANDING HAS 3 HOLES THAT HAVE CRACKS. REMOVED DAMAGE AND BUSHED HOLES IAW RD 8/4-57-526 AND RD 8/4-57-513.

Part: BULKHEAD — MISINSTALLED (FUSELAGE) · airframe 10,744 hrs · 11,707 cycles

AFT TAIL COMPARTMENT INTERNAL AT THE PRESSURE BULKHEAD IS MISSING 4 RIVETS AT STR 29 LT. INSTALLED RIVETS IAW SRM 51-42-05-00-01.

Part: SEAT TRACK — CORRODED (BS 604.5-664.5) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 8 IS CORRODED FR 604.5 - AFT OF 664.5. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01, 51-41-00-00-01, 51-40-15-02-01 AND 51-42-05-02-01.

Part: CHANNEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WHILE ATTEMPTING TO CLOSE FUEL PANEL 522BT FOUND CORRODED NUTPLATE SHELL. REMOVED GANG CHANNEL AND REPLACED NUTPLATE WITH NEW IAW SRM 51-42-75-01-02. INSTALLED GANG CHANNEL IAW Q400 SRM 51-42-75-02-01.

Part: SKIN — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-441. COMPLETED REPAIR REF. RD-8/4-57-1626 AND 8/4-57-441.

Part: SKIN — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

622AT WING CUTOUT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW RD 8/4-57-441. TREATED AND PRIMED WORKED AREA IAW RD 8/4-57-441.

Part: SKIN — DAMAGED (WING) · airframe 10,744 hrs · 11,707 cycles

WING FUEL PANEL CUTOUT 624ET HAS PREVIOUS BLEND DAMAGE. PERFORMED OUT OF DAMAGED AREA REF NTM 51-00-02-250-801. CONFIRMED CRACK FREE REF RD 8/4-57-445. AREA FOUND TO BE WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-445.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 11 IS CORRODED. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-2358. REMOVED SEAT TRACK NR 11 IAW SRM 51-40-15-02-01 AND 51-42-05-02-01. INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-40-15-02-01 AND 51-42-05-02-01.

Part: PANEL — CRACKED (LT WING) · airframe 10,744 hrs · 11,707 cycles

LT INBD WING STRESS PANEL LANDING HAS 6 EA HOLES THAT HAVE CRACKS. REMOVED DAMAGE, REAMED AND BUSHED HOLES IAW RD 8/4-57-513.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 624BT HAS CORROSION ON MATING SURFACE. PANEL REPLACED WITH SERVICEABLE PANEL DUE TO OTHER DISCREPANCIES. (NON-ROUTINE 3 WO 106433).

Part: SEAT TRACK — CORRODED · airframe 10,744 hrs · 11,707 cycles

SEAT TRACK 10 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-2358. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-15-02-01, 51-42-05-02-01, 51-42-07-02-01, 51-41-05-00-01, AND 51-23-00-00-01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-05-02-01.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 524AT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. FOUND TO BE OUT OF LIMITS. REPLACED PANEL WITH SERVICEABLE PANEL.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 624CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND COMPLETED REPAIRS IAW RD 8/4-57-442.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 524ET HAS CORROSION. REMOVED CORROSION FROM THE PANEL IAW RD 8/4-57-442. MATERIAL REMAINING WITHIN LIMITS. HFEC CONFIRMED TO BE CRACK FREE.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 10,707 cycles

PANEL 624DT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442.

Part: PANEL — CORRODED · airframe 10,744 hrs · 11,707 cycles

PANEL 622BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-425 AND FOUND TO BE OUT OF LIMITS IAW RD. REPLACED PANEL WITH SERVICEABLE PANEL.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 524CT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442.

Part: STRINGER — CORRODED (BS 136-156 S25R) · airframe 10,744 hrs · 11,707 cycles

STRINGER 25S HAS POSSIBLE CORROSION FR 136 TO 156. REMOVED 17 CORRODED RIVETS SRM 51-42-05-02-01 AND FOUND CORROSION LIMITED TO FASTENERS ONLY. INSTALLED 17 NAS10975AD4.5 RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND PAINTED AS NECESSARY IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-05-02-01.

Part: STRINGER — CORRODED (BS 156-176 S25R) · airframe 10,744 hrs · 11,707 cycles

STRINGER 25S HAS CORRODED FASTENERS AND POSSIBLE CORROSION FR 156 TO 176. REMOVED 4 CORRODED RIVETS IAW SRM 51-42-05-02-01, FOUND CORROSION LIMITED TO RIVETS ONLY. INTALLED 4 NAS10975AD5 RIVETS IAW SRM 51-42-05-02-01. TREATED, PRIMED, PAINTED AND APPLIED CPC AS NECESSARY IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND AMM 51-25-01-3990-801.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 524AT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. FOUND TO BE OUT OF LIMITS IAW RD 8/4-57-442. REPLACED PANEL WITH SERVICEABLE PANEL.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524DT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624DT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624FT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624ET MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624BT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624AT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524CT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524ET MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIR IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 524DT LANDING HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-442.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524BT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524FT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 524AT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

WING CUTOUT FOR PANEL 624CT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 624ET HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND REPAIRED IAW RD 8/4-57-442.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 624AT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND REPAIRED IAW RD 8/4-57-442.

Part: STRINGER — CORRODED · airframe 10,743 hrs · 11,706 cycles

STRINGER 26S HAS POSSIBLE CORROSION FR 94.8-116.0. REMOVED 8 RIVETS IAW SRM 51-42-05-02-01, FOUND CORROSION LIMITED TO FASTENERS ONLY. INSTALLED 8 RIVETS IAW SRM 51-42-05-02-01. RESTORED FINISH IAW SRM 51-25-05-02-01 AND 51-25-15-02-01.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 524BT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 624FT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND REPAIRED IAW RD 8/4-57-442.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 622AT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-425.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 522BT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-425.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 522AT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-425.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 524FT LANDING HAS CORROSION. REMOVED CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 10,744 hrs · 11,707 cycles

ACCESS PANEL 522AT HAS 3 EA BAD NUTPLATES. REMOVED GANG CHANNEL IAW SRM 51-42-05-02-01. R & R 3 BAD NUTPLATES IAW SRM 51-42-75-02-01. INSTALLED GANG CHANNEL IAW SRM 51-42-05-02-01.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 10,744 hrs · 11,707 cycles

FUEL PANEL 622AT HAS 4 EA BAD NUTPLATES/SCREWS. REMOVED INBD NUTPLATE STRIP IAW SRM 51-42-05-02-01. R & R BAD NUTPLATES IAW SRM 51-42-05-02-01. INSTALLED GANG CHANNEL IAW SRM 51-42-05-02-01.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 10,744 hrs · 11,707 cycles

1 BAD NUTPLATE FOUND ON DRY BAY ACCESS PANEL 621BT. REMOVED GANG CHANNEL OTBD SIDE OF DRY BAY ACCESS PANEL 621BT CUTOUT IAW SRM 51-42-05-02-01. R & R 1 BAD NUTPLATE ON GANG CHANNEL IAW SRM 51-42-05-02-01. INSTALLED GANG CHANNEL IAW SRM 51-42-75-02-01.

Part: PANEL — CORRODED (WING) · airframe 10,744 hrs · 11,707 cycles

PANEL 622CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-425. FOUND TO BE OUT OF LIMITS. REPLACED WITH SERVICEABLE PANEL.

Part: PANEL — CORRODED (WING) · airframe 10,743 hrs · 11,706 cycles

PANEL 622CT LANDING HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW RD 8/4-57-432. REPLACED PANEL WITH SERVICEABLE PANEL.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 10,680 hrs · 11,640 cycles

F/A ADVISES THAT THE MAIN CABIN DOOR IS HARD TO OPEN AND TO CLOSE. CLEANED AND LUBED THE DOOR. OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS WERE REPLACED.

Part: SKIN — CRACKED (MLG DOOR) · airframe 10,515 hrs · 11,452 cycles

LT MAIN GEAR INBD DOOR OUTER SKIN IS CRACKED ABOVE THE AFT HINGE. INSTALLED NEW DOOR IAW AMM 32-12-01-400-801. RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 10,203 hrs · 11,154 cycles

PDX- AFT RIGHT EMERGENCY EGRESS LIGHT DID NOT ILLUMINATE WHEN SELECTED ON. FOULD POWER SUPPLY FAILED AT STA X692.22. REPLACED IAW AMM 33-51-01-000-801. CHECKS GOOD IAW AMM 33-51-01-400-801.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 9,888 hrs · 10,799 cycles

A8 CHECK- DURING THE OPS CHECK OF THE EMERGENCY LIGHT SYS, THE AFT EXIT SIGN OPERATES INTERMITTENTLY. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-000-801 AND 33-51-01-400-801. CHECKS GOOD.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 9,789 hrs · 10,694 cycles

RECEIVED WINDSHEILD CONTROL CAUTION, FO'S WINDSHEILD FOGGED UP. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. COMPLIED WITH FIM TASK 30-40-00-810-805 FOR WINDSHIELD CTRL CAUTION. NO FAULTS FOUND. CHECK WIRE CONNECTIONS AT FO'S WINDSHIELD AND FOUND NO DEFECTS. CHECK ELECTRICAL RESISTANCE OF FO'S WINDSHIELD IAW AMM TASK 30-41-00-760-801, NO DEFECTS FOUND. R & R NR 2 ANTI-ICE CONTROLLER WITH C/P 3041-P2 CONNECTED IAW AMM TASK 30-41-01-00-801 & 30-41-01-400-801 FOR PRECAUTIONARY MEASURE. OPS CHECK GOOD IAW AMM TASK 30-41-00-710-802. RETURNED TO SERVICE.

Part: BATTERY — FAILED (MEGAPHONE) · airframe 9,442 hrs · 10,318 cycles

AFT CABIN EMERGENCY MEGAPHONE BATTERY IS WEAK. REPLACED BATTERY WITH NO HELP. REPLACED THE MEGAPHONE ASSY AND BATTERY IAW AMM 25-62-21-00-400-802. OPS CHECKS GOOD.

Part: ACTUATOR — OUT OF ADJUST (LT MLG) · airframe 9,144 hrs · 10,009 cycles

AFTER GEAR RETRACTION THE LT AMBER AND LT REDLIGHT REMAINED ILLUMINATED FOR 5 TO 8 SECOMDS AND THEN WENT OUT. AIRSPEED WAS 180 KIAS WHEN LIGHTS WENT OUT. UNEVENTFUL LANDING. ADJUSTED LT MLG ACTUATOR IAW AMM TASK 32-31-11-830-801, ALL CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FMU — LEAKING (NR 1 ENGINE) · airframe 9,055 hrs · 9,920 cycles

ON POST FLIGHT FOUND FUEL DRIPPING FROM NR1 NACELLE DRAIN. DURING FLIGHT FUEL FLOW RATE IS SAME AS NR2 BUT QUANTITY SHOWS MORE LOSS ON NR1 SIDE. REMOVED, RE-ORINGED, REINSTALLED NR1 FMU IAW AMM 73-21-06-000-801 AND 73-21-06-400-801. RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 7,576 hrs · 8,269 cycles

UNABLE TO TURN OFF EMERGENCY LIGHTS. FOUND C/B FOR EMERGENCY LIGHTS POPPED RESET CB IAW GPM 9.2.2, NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PIVOT — LACK OF LUBE (PAX DOOR) · airframe 7,329 hrs · 7,975 cycles

BOI - F/A REPORTS THE MAIN CABIN DOOR IS HARD TO UNLATCH AND OPEN FROM THE INSIDE. PERFORMED GVI OF MCD FOUND NO OBVIOUS DEFECTS, CLEANED AND LUBED DOOR PIVOT POINTS PERFORMED OPERATIONAL TEST OF MCD IAW AMM TASK 52-11-00-710-802, DOOR FUNCTIONS NORMALLY. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: GOVERNOR — MALFUNCTIONED (ZONE 400) · airframe 7,225 hrs · 7,848 cycles

NR 2 ENG WON'T COME OUT OF FEATHER, NO OTHER CAUTIONS OR ABNORMALITIES. NO OVERTEMP OR OVER TORQUE. SHUTDOWN ENG. REPLACED NR 2 PROP OSG IAW TASK 61-20-000-801 & TASK 61-20-26-400-801. OPS CKS NORMAL. ACFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (MLG DOOR) · airframe 7,205 hrs · 7,825 cycles

LT AND RT MAIN GEAR DOORS CYCLED IN CRUISE FL220, 248KTS. CYCLED ONE TIME & TOOK 1-2 SECONDS. SLOWED BELOW 200 KTS , DID CHECK LIST & CONTACTED MX CONTROL. NORMAL GEAR EXTEND SPEED IS BELOW 200 KTS, ALT IS BELOW 185 KTS. CYCLE OCCURD 48 KTS ABOVE NORMAL GEAR OPS SPEED. LANDED WITHOUT INCIDENT AND TOWED OFF RUNWAY. COMPLIED WITH GENERAL VISUAL INSP OF THE MLG & DOORS IAW TASK 05-50-31-210-801. NO DEFECTS NOTED. FERRIED FOR REPAIRS. REPLACED RGDRCL SENSOR IAW 32-61-06-000-802/400-802. ADJ SENSOR TARGET IAW 32-12-01-830-801. OPS TEST GOOD OF MLG PRIMARY EXTENSION & RETRACTION IAW 32-31-00-710-801. RETURNED TO SERVICE.

Part: WIRE — DAMAGED (MLG) · airframe 7,118 hrs · 7,723 cycles

DURING CRUISE NOSE GEAR DOORS CYCLED, AND RT MAIN GEAR DOOR CYCLED. ACFT SPEED WAS 260K AND ALT 12000. CHECKLIST COMPLETED AND ALT EXTENSION PERFORMED. LANDING UNEVENTFUL. INTEROGATED PSEU AND FOUND FAULTS "LGWOW2 OPEN" AND "CH.A FAIL,CH. INOP" TROUBLESHOT TO SHORTED WIRES AT CONNECTOR PLUG 3261-P21 TO LGWOW2 PROX SENSOR. RETERMINATED WIRES IAW WM 32-61-01. FAULTS NO LONGER PRESENT AFTER WIRE REPAIR, REPLACED PSEU AS A PRECAUTIONARY MEASURE IAW 32-61-01-000-801/400-801. PERFORMED RETRACT AND EXTEND OF LANDING GEAR IAW 32-31-00-867-801, CHECKS GOOD. RETURNED TO SERVICE.

Part: DOOR — STUCK (MAIN PAX) · airframe 7,008 hrs · 7,600 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. OPERATED MAIN CABIN DOOR. OPEN AND CLOSED SEVERAL TIMES. OPS CHECKS NORMAL. NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 6,767 hrs · 7,324 cycles

AFTER START, NR 1 PROP RPM IS SLOW TO COME OUT OF FEATHER (15-20 SECONDS). UPON CDS CODE RETRIVAL FOUND, (CODE 132) FOR PROP 1. IAW FIM TROUBLE SHOOTING, REMOVED AND REPLACED OVERSPEED GOVERNOR IAW AMM TASK'S 61-20-26-000-801 AND 61-20-26-400-801. LEAK CHECK GOOD, OPS TEST GOOD, AND CODE DID NOT RETURN. ACFT OK FOR SERVICE.

Part: CONTROLLER — OUT OF ADJUST (PROP FEATHERING) · airframe 6,768 hrs · 7,325 cycles

AFTER PUSHBACK NR 1 PROP TOOK OVER A MINUTE TO UNFEATHER AFTER THE CONDITION LEVER WAS BROUGHT TO MAX. IT THEN TOOK ANOTHER 30 SECONDS TO FULLY UNFEATHER. PERFORMED FUNCTIONAL TEST OF THE PROP ELECTRONIC CONTROLLER - CALIBRATION PROCEDURE IAW AMM TASK 61-20-36-720-801, AND ADJUSTMENT OF THE PROP ELECTRONIC CONTROLLER SYNCHROPHASE TRIM IAW AMM TASK 61-20-36-820-801. ALL CHECKS GOOD. C/W FUNCTIONAL TEST OF THE PROP TIME TO UNFEATHER IAW AMM TASK 61-20-00-720-801. BROUGHT C/L FROM START/ FEATHER TO MIN AND MAX MULITIPLE TIMES. TIME TO UNFEATHER WAS WITHIN LIMITS OF LESS THAN 30 SECONDS. NO FURTHER DEFECTS NOTED. NO FAULTS LOGGED IN CDS. TIME FROM UNFEATHER (MIN) TO FEATHER (START/ FEATHER) IDENTICAL BETWEEN NR 1 AND NR 2 ENG. RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (ZONE 400) · airframe 6,752 hrs · 7,307 cycles

DURING CLIMB NR 1 PROP RPM FLUCTUATED FROM 850 TO 860 FOR APPROX FOR 3 SECONDS AND RETURNED TO 850 RPM. REPLACED NR 1 PCU IAW AMM TASK 61-20-11-000-801 AND 61-20-11-400-801 AND TASK CARDS NR 661001, 661002, 6710008, 6710005. OPS CKS GOOD. ALL INDICATIONS NORMAL, ACFT OK FOR SERVICE.

Part: DOOR — ICED (MAIN PAX) · airframe 6,642 hrs · 7,189 cycles

MAIN PASSENGER CABIN DOOR REPORTED TO BE HARD TO OPEN. REMOVED ICE FROM SEAL. DOOR OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 6,205 hrs · 6,673 cycles

PDX- CLIMBING THROUGH 22,000 FT, NOTICED NR 2 FUEL FLOW ABOUT 200 PPH HIGHER THAN NR 1, NR 2 ITT CLIMBED TO 827 DEG C. SHORTLY AFTER NR 2 BLEED HOT CAUTION ILLUMINATED. RETURNED TO FIELD & LANDING UNEVENTFUL. NO PRESENT EMU OR ECS FAULTS IN CDS. REPLACED NR 2 HP BLEED VALVE & 2.7 INTERCOMPRESSOR BLEED VALVE. OPERATION TEST OF BLEED AIR SYSTEM, BLEED AIR SYSTEM OPERATIONAL TEST GOOD. NR 2 ENGINE POWER ASSURANCE CHECKS GOOD BOTH CAPPED AND UNCAPPED. GROUND RAN NR 1 & 2 ENGINES AT HIGH POWER FOR 5 MIN WITH BLEEDS ON AND FLOW NORMAL. NO CAUTION LIGHTS ILLUMINATED AND ALL ENGINE INDICATIONS NROMAL DURING RUN. NO EMU OR ECS FRESENT FAULTS FOUND IN CDS AFTER RUN. RETURNED TO SERVICE.

Part: GOVERNOR — FAILED (NR 1 PROP) · airframe 6,142 hrs · 6,597 cycles

AFTER START NR 1 PROP WOULD NOT COME OUT OF FEATHER EVENTUALLY IT DID BUT VERY SLUGGISH. PROP DID NOT FEATHER AT SHUTDOWN. REMOVED NR 1 PROP OVERSPEED GOVERNER IAW Q400 AMM TASK 61-20-26-000-801. INSTALLED IAW TASK 61-20-26-400-801 OPS TEST GOOD. RETURNED TO SERVICE.

Part: UPLOCK ROLLER — SEIZED (LANDING GEAR) · airframe 5,627 hrs · 6,012 cycles

SEA - ON POST FLIGHT WALK AROUND NOTICE LEFT UPLOCK WHEEL BEARING IS STUCK TIGHT. REMOVED & REPLACED LEFT UPLOCK ROLLER IAW DASH-8 Q 400 AMM TASKS 32-31-21-000-802 32-31-21-400-802. LEFT UPLOCK ROLLER MOVES FREELY NOW, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: UPLOCK ROLLER — STIFF (LT MLG) · airframe 5,621 hrs · 6,006 cycles

SEA - LEFT MAIN LANDING GEAR UPLOCK ROLLER STIFF. LUBRICATED NR 1 MAIN LANDING GEAR UPLOCK ROLLER AS REQUIRED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 5,124 hrs · 5,381 cycles

LAX - JUST PRIOR TO APPLICATION OF TAKEOFF POWER ENGINE DISPLAY CYCLED OFF THEN ON. UNIT ON NORMALLY AFTER ACFT LEFT THE RUNWAY (TAKEOFF ABORTED). INSPECTED ENGINE DISPLAY GROUND STUDS FOR INTEGRITY, NO DEFECTS. CW OPS CHECK OF THE ENGINE DISPLAY IAW 31-61-01-710-803, NO DEFECTS NOTED. CYCLED ENGINE DISPLAY POWER OFF AND ON SEVERAL TIMES. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 5,005 hrs · 5,236 cycles

MSO - ON PREFLIGHT, FOUND LANDING GEAR ALTERNATE EXTENSION DOOR WOULD NOT FULLY OPEN. OPERATIONAL CHECK DOOR, DOOR OPENS COMPLETELY. NO FAULTS NOTED. LATER AS FOLLOW-UP TO FBO ACTION, REMOVED AND REPLACED SECONDARY MLG SELECTOR VALVE IAW MM TASK NR 29-21-06-000-801 AND NR 29-21-06-400-801. RIGGED VALVE IAW MM TASK NR 29-21-06-830-801. OPS AND LEAK CHECKS GOOD. RETURNED TO SERVICE.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 4,987 hrs · 5,209 cycles

PDX - C1 - LT INBD SEAT TRACK HAS MULTIPLE SMALL GOUGES FROM APPROX STA 32 TO 49. BLENDED OUT SMALL GOUGES REF RD 8/4-53-884, PAGE 6 NOTE 1 AND PAGE 2. MAX MATERIAL REMOVED IS .015 INCH AND FOUND TO BE WITHIN LIMITS REF RD 8/4-53-884 PAGE 2. HFEC INSPECTED AT BLENDED AREA FOR CRACK IAW NDTM PART 6, 51-00-01. NO CRACKS NOTED. COMPLETED STEPS 2 THROUGH 8 OF RD 8/4-53-884 ON PAGE 6.

Part: COMPUTER — FAULTED (HGS) · airframe 4,635 hrs · 4,804 cycles

BOI - HGS WOULD NOT GO INTO A3 MODE. ARMS OK BUT WILL NOT GO INTO A3. NO A3 MSG IN COMBINER OCCURRED GEG RUNWAY 3 MADE 2 APP BOTH FAILED RESET ALL PARAMETERS, NO RELIEF DIVERTED TO BOI SAME FAILURE ILS 10R. STANDARD LANDING. FOUND RECORDED FAULTS HGS COMBINER, FOUND SEVERAL HC FC34 FAULTS. REMOVED AND REPLACED HGS COMPUTER IAW CAT III MTC 6343501. TUNED LOCAL NAV TO CAPTURE AIII- HGS OP TESTS GOOD. A/C UPGRADED TO CAT III, PLACARD READS CAT III. MEL PLACARD REMOVED. MTX CONTROLLER NOTIFIED OF A/C STATUS CHANGE. RETURNED TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 4,187 hrs · 4,314 cycles

SEA - NOSE STEERING CAUTION LIGHT ILLUMINATED ON FINAL APPROACH BEFORE GEAR DOWN. CYCLED STEERING SWITCH AS PER CHECK LIST, BUT CAUTION LIGHT REILLUMINATED. ABORTED APPROACH. PERFORMED NORMAL GEAR EXTENSION AND LANDING. PERFORMED SCU INTERROGATION PER AMM TASK NR 32-51-01-742-801. CLEARED SCU NVM PER AMM TASK NR 32-51-01-743-801. ALL FAULTS CLEARED. PERFORMED NWS OPS CHECK PER AMM TASK NR 32-51-00-710-801. OPS CHECK GOOD. NO SCU FAULTS OR NWS CAUTION RE-OCCURRING. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 2,711 hrs · 2,718 cycles

SEA - EN ROUTE TO SEA, RUNAWAY RUDDER TRIM FULL RIGHT (FULL SCALE). WAS ABLE TO REVERSE WITH TRIM SWITCH. PULLED THE CIRCUIT BREAKER AT NEUTRAL POSITION. ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR (PN 399600-1007, SN 176) AND THE RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 2,493 hrs · 2,467 cycles

FLT 2459 - IN CRUISE THE NR 2 HYDRAULIC PUMP CAUTION ILLUMINATED FOLLOWED BY THE RUDDER CONTROL FOLLOWED BY THE NR 2 ISOLATION VALVE. NORMAL CHECKLIST DIRECTED PTU ON NR 1. HYDRAULIC FLUID HOT CAUTION LIGHT ON APPROACH. FLAPS SELECTED AND RECEIVED A FLAP POWER CAUTION LIGHT. LANDED WITH NO FLAPS, ALSO NO WHEEL BRAKES ON LANDING. STOPPED WITH THE EMERGENCY PARKING BRAKE. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PTU, PTU SELECTOR VALVE, HYDRAULIC RESERVOIR TEMP SWITCH. BLED THE NR 2 HYDRAULIC SYSTEM AND BLED NR 1 AND NR 2 HYDRAULIC SYSTEM, BLED BRAKES, AND TAXI CHECKED FOR NOSE WHEEL STEERING AND PARKING BRAKES. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — LEAKING (APU BAY) · airframe 2,409 hrs · 2,371 cycles

YYJ - FLIGHT 7400 - AFTER LANDING, THE FLIGHT ATTENDANT NOTICED A RAW FUEL SMELL IN THE AIRCRAFT. DURING TAXI AND SHUTDOWN THE SMELL INCREASED. MAINTENANCE RAN BOTH ENGINES FOR 10 MINUTES WITH THE BLEEDS ON AND NOTICED NO FUEL SMELLS. NOTICED LARGE AIR LEAK AT APU JOINT. PLACED APU ON MEL 49-00-1. RETURNED TO SERVICE. REPLACED THE APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (DE ICE SYS) · airframe 1,128 hrs · 1,086 cycles

SEA - ON FLIGHT 2268, DEICE PRESSURE CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND NOTED DECREASE IN PRESSURE AND THE NR 2 INTAKE BOOT LIGHT DID NOT ILLUMINATE DURING CYCLE. MAINTENANCE VISUALLY INSPECTED AIRFRAME BOOTS AND INTAKE BOOTS FOR DEFECTS. NONE FOUND. RAN ENGINES AND OPERATED DEICE SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PCU — MALFUNCTIONED (NR 2) · airframe 1,028 hrs · 992 cycles

SEA FLIGHT NR 2348: AFTER CONDITION LEVERS WERE ADVANCED TO MAX DURING ENGINE START, NR 2 PEC CAUTION LIGHT ILLUMINATED AND NR 2 PROP DID NOT GO ABOVE 190. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED NR 2 PCU. PCU RUNS PASSED POWER ASSURANCE. PASSED LEAK CHECK, GOOD FOR NR 2 ENGINE. NR 2 PEC CAUTION LIGHT DID NOT ILLUMINATE. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ACCUMULATOR — UNDERSERVICED (HYD SYSTEM) · airframe 744 hrs · 717 cycles

EUG FLIGHT NR 2280: NR 3 HYD CAUTION LIGHT ILLUMINATES DURING NR 3 HYD SYSTEM CHECK AFTER START. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE SERVICED NR 3 SYSTEM MAIN ACCUMULATOR IAW Q400 AMM TASK 12-30-00. PERFORMED ENGINE RUN, SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — UNKNOWN (NR 2 DC) · airframe 645 hrs · 627 cycles

BIL FLIGHT NR 2411: NR 2 DC GENERATOR CAUTION. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED THE NR 2 DC STARTER/GENERATOR IAW MTC 6243101 (1-4). OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 179 hrs · 178 cycles

SEA TO MSO FLIGHT 2340: POWER PLANT MESSAGE CAME ON AND REMAINED ILLUMINATED FOR REMAINDER OF FLIGHT. FLIGHT WAS DIVERTED TO GEG. MAINTENANCE FOUND FAULT CODE 158B IN CDS. CLEARED FAULT IAW FIM TASK 61-20-04-810-812. FAULT DID NOT REOCCUR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 119 hrs · 110 cycles

BZN FLIGHT NR 2381: WX FAIL MESSAGE ON MFD 1. RAN CHECKLIST. RECEIVED TEST PATTERN BUT NO RETURNS WITH WX FAIL MESSAGE AGAIN. MAINTENANCE REMOVED AND REPLACED WX RADAR TRANSCEIVER. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (RF ANTENNA) · airframe 123 hrs · 114 cycles

SEA FLIGHT NR 2466: WX FAIL DISPLAYED ON BOTH MFD'S. E/A CHECKLIST DID NOT RECTIFY. MAINTENANCE INSPECTED AND FOUND LOOSE PLUG TO RF ANTENNA. SECURED PLUG AND OPS CHECK WEATHER RADAR SYSTEM PER Q400 AMM TASK 34-41-00-710-802. OPS CHECK IS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.