N421QX

Part: HANDLE — LACK OF LUBE · airframe 35,400 hrs · 37,903 cycles

AFT PASSENGER DOOR HANDLE FLAP STIFF. REMOVED FROM SERVICE. CLEANED/ LUBED AFT PAX DOOR HANDLE FLAPS. A/C OK FOR SERIVCE. NO PARTS REPLACED. RETURNED TO SERVICE.

Part: AILERON — WORN · airframe 34,868 hrs · 37,289 cycles

DURING PREFLIGHT WALKAROUND, FO NOTICED THE RIGHT AILERON LINKAGE AND FAIRING MAY HAVE INTERFERENCE WITH EACH OTHER. REMOVED FROM SERVICE. REMOVED AILERON PUSHROD FAIRING REF Q400 AMM TASK 27-12-06-000-801 STEP 3.D PANEL 632 GB . REINSTALLED R/H AILERON PUSHROD FAIRING PANEL 632GB. R/H AILERON LINKAGE NO LONGER HAS CONTACT WITH THE FAIRING. REF W/O 320462 N/R-00001, N/R-00002, AND TC RD84-57-5594 FOR WORK PERFORMED. RETURNED TO SERVICE.

Part: CARPET — LOOSE (CABIN FLOOR) · airframe 33,936 hrs · 36,262 cycles

CARPET@ROW 2D/E PULLING UP - CREATING A TRIP HAZARD. REMOVED FROM SERVICE. RE SECURED CARPET TAPE AT ROW 2D/E NO FURTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: NONE — LOOSE (ZONE 200) · airframe 33,829 hrs · 36,146 cycles

FLOOR LIGHT STRIP DETACHED BY FORWARD BAGGAGE COMPARTMENT. REMOVED FROM SERVICE. RESECURED FWD FLOOR LIGHT STRIP REF Q400 AMM 33-51-16-400-801. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 33,810 hrs · 36,127 cycles

FLOOR LIGHTING STRIP IN FRONT OF FWD GALLEY DETACHED. REMOVED FROM SERVICE. RESECURED FLOOR LIGHTING STRIP AS REQUIRED NO FURTHER DEFECTS NOTED. RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 33,669 hrs · 35,986 cycles

EMERENCY LIGHT NEXT TO FLIGHT ATTENDANT SEAT NEEDS TO BE RELAMPED. REMOVED FROM SERVICE. RELAMPED FWD FA EMERGENCY LIGHT NORM/ON SWITCH AS REQUIRED. NO FUTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 33,521 hrs · 35,824 cycles

AFTER TAKEOFF @ 1200 FT AGL FLAP POWER CAUTION ILLUMINATED AFTER ATTEMPTING TO RETRACT FLAPS. FLAPS REMAINED AT 15°. WE DID FLAP POWER CAUTION IN E&A FLAP POWER CAUTION EXTINGUISHED & RETRACTED TO 0° UPON LANDING ON TOUCHDOWN FLAP POWER CAUTION ILLUMINATED. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS FLAP DRIVE SYSTEM. HYDRAULIC PRESSURE LOSS MESSAGE PRESENT. RESET C/B - FLAPS CONT (L ESS - L7). CAWP FLAP POWER CAUTION LIGHT EXTINGUISHED. C/W OPERATIONAL TEST OF WING FLAPS REF Q400 AMM TASK 27-50-00-710-801. OP CK FAILED. FLAP POWER CAWP LIGHT ILLUMINATED. PERFORMED OPS TEST OF WING FLAPS. CHECK FAILED AND FLAP POWER CAUTION ILLUMINATED AFTER 4TH CYCLE W/ BOTH SPU AND MULE. HYD PRESS LOSS CODE POSTED. PERFORMED GVI OF PRESS SWITCH, FPU, AND WIRING. NO DEFECTS NOTED. C/W Q400 HYD PRESS LOSS FIM TASK 29-10-00-810-803 PARA 1-4A.(2),5. PERFORMED OPS TEST 5 FULL CYCLES. OPS TEST GOOD, FAULT CODE DID NOT RETURN. NO DEFECTS NOTED. REPLACED FPU PRESS SWITCH REF Q400 AMM TASK 27-52-01-000/400-802, OPS CHECK GOOD.

Part: BATTERY PACK — NONE (ZONE 200) · airframe 33,519 hrs · 35,832 cycles

AFT CABIN OVERHEAD CEILING EMERGENCY EXIT AND AFT R/H DRAFT BULKHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED EPSU BATTERY PACKS AT AFT LOCATION LH3 AND RH3 REF AMM TASK 33-51-01-000-801 AND 33-51-01-400-802. OPS CHECKS GOOD

Part: BRAKE — FIRE (NR 3) · airframe 33,416 hrs · 35,728 cycles

DURING POST FLIGHT WALK-AROUND, SAW #3 BRAKE SLIGHTLY ON FIRE. FIRE AND SMOKE CLEARED BEFORE AIRPORT FIRE AND RESCUE SHOWED UP. TIRE AND BRAKE LOOK OK. REMOVED FROM SERVICE. PERFORMED GVI OF THE MAIN LANDING GEAR WHEEL ASSY, #3 TIRE AND BRAKES IAW AMM TASK 32-40-00-210-802 AND TASK 32-40-00-210-803. REMOVED MLG TIRE HUB CAP IAW Q400 AMM TASK 32-40-00-210-802, STEP 4 (A) (1-3) AND INSPECTED WHEEL BEARING ASSY, NO DEFECTS NOTED. CLEANED MLG WHEEL AND REMOVED EXCESSIVE GREASE. INSTALLED #3 MLG TIRE HUB CAP IAW Q400 AMM TASK 32-41-01-400-801, STEP 4(B) (25-27). NO DEFECTS OR FIRE DAMAGE NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (LT MLG) · airframe 32,960 hrs · 35,273 cycles

LEFT MAIN GEAR OUTBOARD WHEEL/TIRE HAS SMOKE COMING OUT FROM CENTER AREA OF WHEEL MEDIUM TO SLIGHTLY MORE BREAKING APPLIED ON LANDING. REMOVED FROM SERVICE. INSPECTED THE #1 WHEEL AND BRAKE ASSY WITH NO DEFECTS NOTED. INTERROGATED THE CDS FOR ANY FAULT ON THE ANTISKID SYSTEM WITH NONE FOUND. OPERATED THE BRAKES SEVERAL TIMES WITH NO ABNORMALITIES NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITCH TRIM) · airframe 32,892 hrs · 35,205 cycles

DURING CLIMBOUT AT APPROX 200 KTS AUTO PILOT NOT ENGAGED PITCH TRIM CAUTION ILLUMINATED RAN ETA CHECKLIST PITCH TRIM WOULD NOT FUNCTION. DIVERTED, LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS FOUND FCECU FAILURE 67,63,E7,&E3 PERFORMED FIM TASK 27-00-00-810-805 ALL FAULTS CLEARED AND DID NOT RETURN OPS CK PITCH TRIM ELEVATOR SYS CKS GOOD 27-32-00-710-802 RETURNED TO SERVICE.

Part: SEAT TRACK — DAMAGED (BS 229-571) · airframe 32,650 hrs · 34,979 cycles

SEAT RAIL 19 FROM FSX229.5-X571.5,Y40.950 BLENDED BEYOND LIMITS. REMOVED AND REPLACED SEAT RAIL 19 FROM FSX229.5-X571.5, Y40.950 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-42-05-02-01, 51-41-15-02-01, 51-42-45-02-01 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — DAMAGED (BS 668-783) · airframe 32,650 hrs · 34,979 cycles

SEAT RAIL 9 FROM FSX668.00-X783.00,Y -9.250 BLENDED BEYOND LIMITS. REMOVED AND REPLACED SEAT RAIL 9 FROM FSX668.00-783.00, Y9.250 IAW SRM 51-40-07-02-01, 51-40-15-02-01, 51-42-05-*02-01 AND AMM 20-10-01-430-801.

Part: SEAT TRACK — DAMAGED (BS 32-229) · airframe 32,650 hrs · 34,979 cycles

SEAT RAIL 1 FROM FSX32.4-X229.5,Y-40.950 BLENDED BEYOND LIMITS. 1 SEAT RAIL (FS X32.4-X229.5, Y-40.95) REMOVED IAW SRM TASK 51-42-05-02-01, 51-42-45-02-01, 51-40-15-02-01. NEW SEAT RAIL 1 INSTALLED IAW SRM TASKS 51-40-07-02-01, 51-40-02-01-, 51-42-05-02-01, 51-42-45-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,650 hrs · 34,979 cycles

SEAT RAIL 10 FROM FSX-39.00-X10.50, Y9.250 IS CORRODED BEYOND LIMITS. REPLACED SEAT RAIL 10 IAW 51-42-05-02-01. 51-40-15-02-01, AND 51-41-05-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,650 hrs · 34,979 cycles

SEAT RAIL 11 FROM FSX10.50-X102.5,Y9.250 CORRODED BEYOND LIMITS. SEAT RAIL 11 REPLACED IAW SRM 51-42-05-02-01, 51-40-15-02-01, AND 51-41-05-00-01.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM) · airframe 31,491 hrs · 33,794 cycles

PITCH TRIM MASTER CAUTION AND AUTO TRIM FAIL ON FMA DURING CLIMBOUT . ELEVATOR TRIM INDICATOR SHOWED FULL NOSE UP. NO CIRCUIT BREAKERS POPPED. REMOVED FROM SERVICE. FOUND FAULTS ON CDS IFC FAILURE X2, FCECU FAILURE 67, 63, E7, AND E3 REF Q400 FIM 27-30-00-810-803. REPLACED THE FCECU Q400 AMM 27-00-01-000-802 AND 27-00-01-400-802 OPS TEST GOOD. PITCH TRIM MASTER CAUTION REMAINS EXTINGUISHED. NO FAULTS IN CDS. NO FURTHER DEFECTS NOTED. AUTO TRIM FAIL NO LONGER DISPLAYED. RETURNED TO SERVICE.

Part: BUMPER — DEFECTIVE (CABIN DOOR) · airframe 31,104 hrs · 33,392 cycles

RAMP PERSONNEL UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE, UNABLE TO GET FINGERS IN RECESS TO GRAB THE HANDLE FASTENER, OPENED DOOR FROM INSIDE. REMOVED FROM SERVICE. REPLACED BUMPER STOP ASSY REF MCN 6520839-01, DOOR OPENS FROM OUTSIDE AS NORMAL. OK FOR SERVICE AMM 52-11-11-420-008. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 30,492 hrs · 32,679 cycles

ON DESCENT PASSING APPROX 12000-13000 FEET CABIN PRESSURE WARNING ILLUMINATED. CABIN RATE OF CLIMB INDICATOR WENT FROM -2000FPM TO +3000 IN ABOUT A SECOND. WE CONTINUED DESCENT AND WARNING EXTINGUISHED AROUND 10000 FT. CABIN DID NOT REGAIN PRESSURIZATION IN AUTO OR MANUAL. IPC AND E+A CHECKLISTS FOLLOWED. UPON ARRIVAL GROUND CREW NOTED THAT MAIN CABIN DOOR HANDLE WAS OPEN BY A FINGER TIP OR TWO. REMOVED FROM SERVICE. CDS SHOWED CP CONTROLLER FAIL. R&R CPC IAW Q400 AMM 21-31-06-000/400-801. OPS TEST GOOD. FUNCTIONAL TEST OF PRESS CONTROL IAW Q400 AMM 21-31-00-720-801. TESTS GOOD. NO WARNINGS AND NO FAULTS CURRENTLY. NO FURTHER DEFECTS AT THIS TIME. THIS CLEARS DEFECT 902686. PLACARDS REMOVED. MTX CONTROL NOTIFIED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 30,492 hrs · 32,678 cycles

AT FWD FA STATION THE "NORMAL" PORTION OF THE EMERGENCY LIGHTING SWITCH IS NOT ILLUMINATED. SWITCH OPERATES AND "ON " PORTION DOES ILLUMINATE. REMOVED FROM SERVICE. RELAMPED "NORMAL" PORTION OF EMERGENCY LIGHTING SWITCH AS REQUIRED. SWITCH ILLUMINATES CORRECTLY. AIRCRAFT RETURNED TO SERVICE.

Part: SPRING — BROKEN (CABIN DOOR) · airframe 30,488 hrs · 32,674 cycles

MAIN CABIN DOOR UPPER LEVER SPRING BROKE.

Part: SENSOR — MALFUNCTIONED (INLET TEMP) · airframe 30,304 hrs · 32,452 cycles

IN"AUTO" WE COULDNT GET THE FC DUCT BELOW 85, IN MANUAL WE COULDN'T GET THE FC DUCT BELOW 40. ANYTIME WE RAISED THE FC DUCT ABOVE FULL COLD WE COULD SMELL HEAT. REMOVED FROM SERVICE. R/R PACK INLET TEMP SENSOR IAW Q400 AMM 21-52-11-000/400-801. PERFORMED OPS TEST OF ECS TEMP CONTROL IAW Q400 AMM 21-61-00-710-803. OPS TEST GOOD. FC DID NOT RETURN. A/C IS CLEARED FOR RETURN TO SERVICE.

Part: TMU — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 30,252 hrs · 32,389 cycles

DURING CLIMB AND AND CRUISE, DEICE TIMER CAUTION ILLUMINATED AND WENT DARK MULTIPLE TIMES. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED FROM SERVICE. REPLACED TMU IAW Q400 AMM 30-11-01-000/400-801 FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 29,986 hrs · 32,078 cycles

LANDING GEAR LOCK RELEASE REQUIRES EXCESSIVE FORCE TO MOVE DOWNWARD DURING LANDING GEAR EXTENSION. GEAR DOWN POSITION. REMOVED FROM SERVICE. INSPECTED LANDING GEAR CONTROL PANEL, FOUND SHEARED FACE PLATE FASTENER OBSTRUCTING HANDLE OPERATION BY MEANS OF SHIFTING FACEPLATE. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL ASSEMBLY IAW MM 32-31-01-000-801 AND 32-31-01-400-801. FUNCTIONAL CHECK CONTROL PANEL GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 29,725 hrs · 31,765 cycles

EMERGENCY EXIT FLOOR PATH STRIP AT MCD PULLED FROM FLOOR. DURING RON ARRIVAL CHECK FOUND FLOOR EMERGENCY EXIT STRIP AT MCD BETWEEN WET FLOOR & CARPET LIFTED OFF. WET FLOOR SEAL NOT DAMAGED. REMOVED EXIT STRIP CLEANED SURFACE & INSTALLED NEW EXIT STRIP. APPLIED SEALANT TO EDGES OF EXIT STRIP ON WET FLOOR. NO FURTHER DEFECTS FOUND.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 29,172 hrs · 31,096 cycles

EMERGENCY EXIT SIGN POPPED OFF AT ROW 2. REMOVED FROM SERVICE. INSPECTED EMERGENCY EXIT SIGN COVER, NO DAMAGE NOTED. REINSTALLED SAME COVER. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: VALVE — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 29,154 hrs · 31,072 cycles

DEICE PRESS CAUTION ILLUMINATED IN FLIGHT UPON SELECTING AIRFRAME SELECT MODE TO FAST. DIVERTED. LANDING UNEVENTFUL. REMOVED FROM SERVICE. CDS SHOWS NO FAULTS. PERFORMED FUNC TEST OF AIRFRAME PNEUMATIC DEICING SYS IAW AMM 30-11-00-720-801 TWICE. FIRST TIME FUNC TEST PASS. SECOND FUNC TEST FAILED WHEN FAST MODE SELECTED. OUTER LEFT WING BOOT LIGHT DID NOT ILLUMINATE FOLLOWED BY DEICE PRESS CAUTION, AND LOGGED A " LOW 1A PRESS" FAULT IN CDS." REPLACED #1 DDV IAW AMM 30-11-16-000/400-801. PERFORMED OPS TEST OF DDV'S IAW AMM 30-11-16-710-801. OPS TEST PASS, NO FAULTS RETURNED. RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,735 hrs · 30,557 cycles

EMERGENCY LIGHTS AT CENTER AISLE ROWS 10, 14 AND 18, CENTER AISLE AFT EXIT SIGN AND RT BULKHEAD EXIT SIGN ILLUMINATE WHEN A/C POWERS DOWN WITH EMERGENCY LIGHT SWITCHES IN OFF POSITION. REMOVED FROM SERVICE. REMOVED POSITION #3 EMERGENCY LIGHT BATTERY PACK. REPLACED CARRIER & INSTALLED ORIGINAL BATTERIES. INSTALLED BATTERY PACK AT POSITION #3. OPS TEST GOOD. REF AMM TASKS 33-51-01-000 / 400-801. RETURNED TO SERVICE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 28,703 hrs · 30,519 cycles

PLASTIC "EXIT" LIGHT COVER AT SEAT 2D/E FELL OFF, UNABLE TO STAY ON. REMOVED FROM SERVICE. REPLACED WITH NEW EXIT SIGN FROM STOCK. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 28,512 hrs · 30,293 cycles

EXIT SIGN BY TYPE II/III DOOR POPPED OFF. REMOVED FROM SERVICE. REINSTALLED EXIT DOOR LIGHT LENS. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 28,078 hrs · 29,817 cycles

FORWARD LOWER EXIT SIGN BROKEN AT THE TYPE II EMERGENCY EXIT. REPLACED.

Part: SWITCH — DEFECTIVE (CABIN) · airframe 27,974 hrs · 29,452 cycles

PILOT REPORTS WHEN A/C IS POWERED DOWN, EMERGENCY LIGHTS ILLUMINATE WHEN BATTERIES TURNED OFF AND EMERGENCY LIGHT SWITCH IN OFF POSITION. REMOVED FROM SERVICE. REMOVED & REPLACED FA EMERGENCY LIGHT SWITCH IAW AMM TASKS 33-51-05-000-801 AND 400-801. DEFECT FIXED. ALL OPS TESTS GOOD FOR EMERGENCY LIGHTS AND PAX INFO WARNING LIGHTS. RETURNED TO SERVICE.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 27,391 hrs · 29,011 cycles

AFT SERVICE DOOR NR 2 BEAM CRACKED AT VENT DOOR BRACKET LOCATION. NR 2 BEAM REPLACED IAW SRM 51-40-45,51-47-05,51-42-45.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

CORROSION FOUND ON STRINGER 24L AT FS X 230. CUT OUT CORRODED SECTION ON STRINGER 24L AT FS X230 IAW RD84-53-8916. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. REPAIRED STRINGER 24 LT AT FS X230 IAW RD84-53-8916.

Part: SKIN — CRACKED (RT WING) · airframe 27,391 hrs · 29,011 cycles

RT WING TRAILING EDGE SKIN OB OF AILERON NR 2 HINGE, IS CRACKED 3.5 INCHES IN LENGTH VERTICALLY. DAMAGE ON RT WING TRAILING EDGE SHROUD AT AILERON NR 2 HINGE MEASURED, MAPPED AND THD CONTACTED FOR REPAIR REQUEST IAW SRM 51-15-05-00-01. DAMAGE ON RT WING SHROUD REPAIRED IAW RD84-57-4123. NDT CARRIED OUT IAW NDTM 1, 51-00-06-910-801.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

CORROSION FOUND ON STR'S 16, 17 & 18, FS X248 TO 714 LT AND RT SIDE. REPAIRED CORROSION ON STR'S 16,17 AND 18 FS 248 TO 714 LT AND RT SIDE IAW RD 84-53-8390 REFERENCE TASK CARD WO 241470 TASK CARD RD84-53-830-84-53-8917 FOR WORK ACCOMPLISHED. NDT CARRIED OUT IAW RD84-53-8917, ISSUE 1 & RD84-53-8930, ISSUE 1. REPROTECTED STR'S 16,17 AND 18 FS 248 TO 714 LT AND RT SIDE IAW SRM 51-25-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

LT OB SEAT RAIL NR 2 FROM X229.50 TO X 571.5 LBL -40.950 CORRODED IN VARIOUS LOCATIONS. LT OB SEAT RAIL NR 2 FROM X229.50 TO X571.5 LBL -50.950 REPLACED IAW SRM 51-40-15, 51-42-05, 51-42-15 AND 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

SEAT RAIL NR 10 FROM FSX -39.00 -X10.50 IS CORRODED BEYOND LIMITS. SEAT RAIL NR 10 FROM FSX -39.00-X10.50, REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: SHEAR WEB — CORRODED (AFT CARGO) · airframe 27,391 hrs · 29,011 cycles

AFT CARGO AFT SHEAR WEB WAS CORRODED BEYOND LIMITS. REMOVED AND REPLCED THE SHEAR WEB IAW SRM 51-42-05, 51-40-15, AND 51-42-75.

Part: THRESHOLD — CORRODED (FWD PAX DOOR) · airframe 27,391 hrs · 29,011 cycles

FWD PASSENGER DOOR SURROUND, THRESHOLD AND ATTACH ANGLE CORRODED BEYOND LIMITS. REPLACED THE THRESHOLD AND ATTACH ANGLE IAW SRM 51-42-05-02-01, 51-42-15, & 51-23-00.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 27,391 hrs · 29 cycles

FWD BAGGAGE DOOR BEAM NR 2 CRACKED AT VENT DOOR BRACKET LOCATION. BEAM REPLACED ON FWD BAGGAGE DOOR IAW SRM 51-42-05, 51-42-45, 51-40-15, 54-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

LT IB SEAT TRACK NR 9 CORRODED BEYOND LIMITS. REMOVED LT IB SEAT TRACK NR 9 IAW SRM 51-42-05, 51-40-15, 51-41-05. REPLACED LT IB SEAT TRACK NR 9 IAW SRM 51-42-05, 51-40-15, 51-41-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,391 hrs · 29,011 cycles

SEAT RAIL 11 FROM FS 10.50 -X102.50 IS CORRODED BEYOND LIMITS. SEAT RAIL 11 REPLACED IAW SRM 51-42-05, 51-40-15 AND AMM 20-10-01.

Part: SHEAR WEB — CORRODED (NOT REPORTED) · airframe 27,391 hrs · 29,011 cycles

FORWARD SHEAR WEB CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR WEB IAW 51-42-05, 51-40-15, AND 51-42-45.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,188 hrs · 28,802 cycles

EMERGENCY LIGHTS DISARMED CAUTION LIGHT NOT ILLUMINATED WITH FLIGHT DECK SWITCH IN OFF. EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO ON, IN THE FLIGHT DECK. EMERGENCY LIGHTS OPERATE NORMALLY FROM F/AS SWITCH. REMOVED AND REPLACED THE F/A EMERGENCY LIGHTS SWITCH IAW AMM 33-51-05-000-801, AND 33-51-05-400-801, OPS TESTED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,081 hrs · 28,880 cycles

EMRGENCY LIGHTS WILL NOT TURN OFF. R & R THE ADVISORY SIGN/PASSENGER WARNING PANEL ASSEMBLY IAW 31-51-10-400-801, AND 31-51-10-000-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,033 hrs · 28,629 cycles

WHILE SHUTTING DOWN POWER TO THE ACFT, WITH BOTH EMERGENCY LIGHT SWITCHES IN THE OFF POSITION, EMERGENCY LIGHTS STAYED ON. REMOVED FROM SERVICE. REMOVED THE CONNECTOR FROM THE ADVISORY SIGNS AND PASSENGER WARNING PANEL, PERFORMED GVI, NO DEFECTS NOTED. CONNECTED THE CONNECTOR, EMERGENCY LIGHTS STARTED WORKING WITHOUT DEFECT. DUE TO RECENT HISTORY, REMOVED AND REPLACED THE EMERGENCY LIGHT RELAYS 3351-K1, AND 3351-K2 AS A PRECAUTION. WORK PERFORMED IAW AMM 31-51-10-000/400-801, 25-24-03-000-400-803 AND WDM 33-51-00 AND AMM 20-30-16-960-801. OPS TESTED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (NR 1 PITCH) · airframe 26,885 hrs · 28,453 cycles

NR 1 ENGINE SLOW TO COME OUT OF FEATHER. NR 1 PROPELLER GREASE LEVEL IS NORMAL, NO SIGNS OF LEAKAGE AT THE NR 1 PCU AND OSG. PROPELLER WILL NOT UNFEATHER ALL THE WAY IN MANUAL MODE, ONLY MOVES A FEW DEGREES. PROP TIME TO UNFEATHER TEST WITH ENGINES RUNNING TAKES APPROX 30-40 SECONDS AND IS ALSO SLOW TO FEATHER. REPLACED THE PROPELLER PISTON SEAL IAW 61-10-00-960-801. SERVICED THE PROPELLER GREASE LEVEL IAW 61-10-00-640-801. FUNCTIONAL TEST OF PROPELLER TIME TO UNFEATHER FAILED. PROPELLER WILL NOT UNFEATHER MANUALLY. ON NR 1 ENGINE START WITH CONDITION LEVER IN START - FEATHER & POWER LEVER AT DISC, THE NR 1 PROPELLER RPM COMES OUT OF FEATHER AND PROPELLER RPM STABILIZES AT 420 RPM. REMOVED THE THR NR 1 BETA TUBE IAW MTC 6610001. REMOVED AND REPLACED THE NR 1 PITCH CONTROL UNIT IAW AMM 61-20-11-000-400-801. REINSTALLED THE NR 1 BETA TUBE IAW MTC 6610002 AND MTC 6710006. NO LEAKS NOTED. NR 1 FEATHER WITHIN TIME FRAME AND UNFEATHERS PROPERLY.

Part: LIGHT — UNKNOWN · airframe 26,882 hrs · 28,451 cycles

FORWARD CABIN EMERGENCY LIGHTS ILLUMINATED AFTER AIRCRAFT POWERED DOWN. REMOVED FROM SERVICE. APPLIED EXTERNAL POWER TO ACFT TO TURN OFF EMERGENCY LIGHTS. EMERGENCY LIGHTS OPS TESTED GOOD IAW AMM 33-51-00-710-803. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ACCESS PANEL — MISSING (LT NACELLE) · airframe 26,821 hrs · 28,379 cycles

HYDRAULIC SERVICE PANEL, ON LEFT SIDE OF THE LEFT NACELLE WAS FOUND MISSING. REMOVED FROM SERVICE. INSTALLED A NEW DOOR AND RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 26,675 hrs · 28,234 cycles

NR 2 BLEED HOT CAUTION ON TAKEOFF. AIRCRAFT DID NOT PRESSURIZE. LIGHT EXTINGUISHED AFTER BLEED SWITCH CYCLED, AIRCRAFT STILL DID NOT PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. INTERROGATED CDS NOTED FAULT 3001 - PACK FCV REMOVED AND REPLACED PACK FLOW CONTROL VALVE IAW 21-52-01-000/400-801. PRESSURIZATION CKS GD GRD RAN NR 2 ENG NO BLEED HOT CAUTION NOTED OK FOR CONTINUED SERVICE.

Part: SENSOR — MALFUNCTIONED (AC BAY) · airframe 26,051 hrs · 27,593 cycles

AT FL230 SLOW DECREASE IN PRESSURIZATION CAUSING A CABIN PRESS WARNING WITH A DESCENT TO 10,000 CONDUCTED CABIN PRESS WARNING CHECKLIST, PRESSURIZATION FAIL CHECKLIST AND UNPRESSURIZED FLIGHT CHECKLIST. REMOVED FROM SERVICE. IN CDS FOUND ECS FAULT CODE 3101- PACK 1LT MISCMP MULTIPLE TIMES. REPLACEMENT OF PACK INLET TEMP SENSOR. COMPLIED WITH OPS CHECK OF PRESSURIZATION CONTROL IAW AMM TASK 21-31-00-710-801 ALTERNATE PROCEDURE 4B AND PARA 5. NO DEFECTS. RETURNED TO SERVICE.

Part: SEAL — OUT OF POSITION (SERVICE DOOR) · airframe 25,969 hrs · 27,519 cycles

AFT GALLEY SERVICE DOOR IS TOUGH TO OPEN. BOTH INSIDE AND OUTSIDE DIFFICULT. REMOVED FROM SERVICE. R & R THE AFT SERVICE DOOR SEAL. DOOR RIG OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 25,657 hrs · 27,194 cycles

AUTOFEATHER TEST DURING DAILY SYSTEMS CHECK SHOWS ABORT ON THE LEFT SIDE AND FAILED ON THE RIGHT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND POWER LEVERS OUT OF POSITION . POSITION POWER LEVERS BACK AND PERFORMED AUTOFEATHER TEST. AUTOFEATHER TESTED GOOD NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 25,624 hrs · 27,153 cycles

AUTOFEATHER TEST FAILED FOR NR 1 AND 2 ENGINES. NR 1 AUTOFEATHER SAYS ABORT. NR 2 AUTOFEATHER SAYS FAILED. THREE ATTEMPTS AT TEST. THIRD ATTEMPT WAS AFTER COMPLETE ELECTRONIC SHUTDOWN AND RESTART. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND FAULT CODES FOR NR 1 ENGINE 72A & 771A AS WELL AS NR 2 ENGINE 292A. CLEARED FAULT CODES IN CDS AND THEN RAN OPS TEST IAW AMM 61-20-00-710-801 WITHOUT AND WITH ENGINE RUNS. OPS CHECKED GOOD BOTH TIMES & NO NEW FAULT CODES APPEARED. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (AFT CARGO DOOR) · airframe 25,534 hrs · 27,062 cycles

ON CLIMB OUT AT AROUND 14,000 FT, RECEIVED A FUSELAGE DOORS WARNING. THE WARNING WAS INTERMITTENT UP TO FL 210. CONDUCTED PROCEDURE IAW E&A CHECKLIST. THE DOOR WAS IDENTIFIED AS AFT CARGO DOOR. THE WARNING BECAME INTERMITTENT FROM FL 210 TO 6000 FT DURING DESCENT. REMOVED FROM SERVICE. RIGGED THE PROXIMITY SENSOR TO 8.77 MILLIHENRYS IAW AMM TASK 52-71-01-830-806 AND 32-61-00-280-801. COMPLIED WITH OPERATIONAL TEST OF THE CLOSED SENSOR IAW TASK 31-62-00-710-801. CHECKED GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 25,106 hrs · 26,601 cycles

SEVERAL AREAS OF EMERGENCY LIGHT STRIPS ARE LOOSE IN THE MCD ENTRANCE AREA. REPAIRED AS REQUIRED.

Part: SPRING — FAILED (STOWAGE BOX) · airframe 24,659 hrs · 26,140 cycles

EMERGENCY FLASHLIGHT AND FORWARD F/A LIFE VEST COMPARTMENT DOOR DOES NOT SPRING CLOSED. REPLACED THE DOOR HINGE SPRING. DOOR NOW OPERATES CORRECTLY. RETURNED TO SERVICE.

Part: LATCH — STUCK (COCKPIT DOOR) · airframe 23,855 hrs · 25,272 cycles

FLIGHT DECK DOOR IS STUCK IN THE CLOSED POSITION. REPLACED LATCH ASSEMBLY. RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (AFT PAX DOOR) · airframe 23,664 hrs · 25,067 cycles

DURING TAKE OFF ROLL, AT ABOUT 85 KTS THE MASTER WARNING LIGHT AND FUSELAGE DOORS WARNINGS ILLUMINATED. ABORTED THE TAKE OFF AND RETURNED TO THE GATE. INSPECTED THE AFT PAX DOOR. FOUND THE LOCK HANDLE NOT FULLY STOWED. PERFORMED GVI OF DOOR ASSEMBLY AND APERTURE, NO DEFECTS NOTED. OPS TEST OF AFT PASSENGER DOOR IAW MM 52-12-00-710-802. OPS CHECKED GOOD. NO HISTORY DURING PREVIOUS MONTHS. RETURNED TO SERVICE.

Part: LANDING GEAR — SMOKE (LEFT) · airframe 23,550 hrs · 24,952 cycles

ON POST FLIGHT, BOTH TIRES ON LEFT MAIN LANDING GEAR WERE SMOKING. MODERATE BRAKING USED ON LANDING. PERFORMED A GVI OF THE GEAR IAW AMM TASK 32-41-00-210-801. FOUND NO DEFECTS OR FLUID LEAKS. RETURNED TO SERVICE.

Part: HANDLE — OBSTRUCTED (EMERGENCY EXIT) · airframe 22,133 hrs · 23,457 cycles

WHILE OPENING RT FWD EMERGENCY DOOR, TO AIR OUT FWD CABIN, DUE TO SEALANT APPLICATION, "DITCHING DAM" HANDLE ON LOWER DOOR, WILL NOT MOVE TO "WATER" POSTION. PERFORMED GVI OF RT FWD EMERGANCY DOOR, FOUND WORN STOPPER BRACKET, IPC 53-20-00, FIG 10, ITEM 340, TP 98253 2/2/16. R & R STOPPER BRACKET IAW SRM 51-42-05. NO ADJUSTMENTS MADE, "DITCHING DAM" HANDLE MOVES WITHOUT DEFECT. COMPLIED WITH OPS TEST OF RT FWD EMERGENCY DOOR, REF AMM TASK 52-23-00-710-801, OPS CHECKS GOOD. ACFT OK FOR CONTINUE SERVICE. NOTE: AFT LOWER LATCH STOP FITTING, WAS REMOVED AND REINSTALLED TO R & R THE WORN STOPPER, REF AMM TASKS 53-20-17-000/400-801. NO ADJUSTMENTS MADE.

Part: SIGN — WRONG PART (EMERGENCY LIGHTS) · airframe 22,035 hrs · 23,360 cycles

FORWARD EMERGENCY EXIT LOWER LT EXIT SIGN ARROW POINTS THE WRONG WAY. REPLACED THE SIGN. RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (PROP DE ICE) · airframe 21,952 hrs · 23,264 cycles

ENROUTE, NR 2 PROPELLER DE-ICE CAUTION ILLUMINATED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INTEROGATED CDS FOUND FAULT TMCU 14 ON NR 2 TMCU CLEARED FAULT AND PERFORMED FUNCTIONAL TEST IAW AMM 30-61-00-720-801 PROP DEICE DID ILLUMINATE. R & R TMCU AS PRECAUTIONARY MEASURE IAW AMM TASK 30-61-06-000/400-801 FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: HINGE — BROKEN (CABIN) · airframe 21,875 hrs · 23,187 cycles

FLIGHT LIGHT PANEL UNDER AFT F/A JUMPSEAT WILL NOT RETRACT OUT OF THE WAY. FOUND SPRINGS DETENSIONED AND HINGE BAD. REPLACED SPRINGS AND HINGE. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (ZONE 800) · airframe 21,837 hrs · 23,150 cycles

EMERGENCY EXIT DOOR LIGHT COVER FELL OFF. RESECURED LIGHT COVER AT EMERGENCY EXIT AT ROW 2E. RETURNED TO SERVICE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 21,759 hrs · 23,065 cycles

EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH IN ARM. REPLACED SWITCH.

Part: MOUNT — CRACKED (CARGO DOOR) · airframe 21,638 hrs · 22,939 cycles

MACHINED FITTING MOUNT FOR AFT CARGO DOOR FWD COUNTER BALANCE BELL CRANK IS CRACKED. C/W ET INSP ON MACHINED FITTING MOUNT FOR AFT CARGO DOOR, FWD COUNTER BALANCE BELL CRANK REF NDTM PT 1 51-00-06. DEFECT, CRACK, NOTED AND MARKED. RECEIVED NEW UPPER MAIN SILL FROM STOCK. MACHINED SUPPORT PLATE, PN 85237815 REMOVED REF SRM 51-40-15 X 744.00 COMMON TO CARGO DOOR UPPER SILL. INSTALLED SUPPORT PLATE, PN 85237815 REF SRM 51-40-15. REMOVED FRAME WEB, PN 85339583, REF SRM 51-42-05. INSTALLED FRAME WEB DOUBLER RD-1, DOUBLER RD-2, PACKER RD-3 AND PACKER PD-4 REF RD 8/4-53-7141, ISSUE 1. REMOVED DAMAGE AREA, REF GGAR-15-31549298. REMOVED DAMAGED AREA ON AFT CARGO DOOR FWD COUNTER BALANCE BELL CRANK FITTING MOUNT REF GGAR-15-31549298. C/W ET INSP ON CUT LINES. REWORKED AREA ON MACHINED FITTING MOUNT FOR AFT CARGO DOOR, FWD COUNTER BALANCE BELL CRANK AS MARKED REF NDTM PT.1 51-00-06. ET INSP REF NDTM 51-00-06, PT 1, UT THICK TEST REF NDTM PT.1, MIN THICKNESS MEASURES .135" IN BLENDED AREAS. ET INSP REF NDTM PT 1 51-00-06, NO DEFECTS NOTED IN 2 EA FABRICATED ANGLES. FABRICATED REPAIR ANGLES RD-1 AND RD-2 REF RD 8/4-53-7141, ISSUE 1, PO:TX-0595 7075-T3.063". FABRICATED REPAIR PACKERS RD-3 AND RD-4 REF RD8/4-53-71-41, ISSUE 1, PO T21964-2024TC, 0.080". COMPLIED WITH RD 8/4-53-7141, ISSUE 1, STEPS 1-11. WEB PN 85339583, COMMON TO ACFT SKIN INSTALLED REF SRM 51-42-05.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK NR 13 REQUIRES REPLACEMENT, PN 85361510-104. REMOVED FWD SPLICE MEMBERS COMMON TO SEAT RAIL NR 12 AND NR 13 AT FS 229.5, Y9.250 REF SRM 51-40-15. REMOVED AFT SPLICE MEMBERS COMMON TO SEAT RAIL NR 13 AND NR 14 AT FS 571.5, Y9.250, REF SRM 51-40-15. INSTALLED AFT SPLICE MEMBERS COMMON TO SEAT TRACK NR 13 & 14 AT X571.5, X9.250 REF SRM 51-40-15 AND 51-42-05. REMOVED GROUND WIRE FROM SEAT RAIL BRACKET AT FS 290.5, Y-9.250 REF WM 20-12-10. INSTALLED GROUND WIRES 2421-GS18 AND 2421-GS19 ON SEAT TRACK RAIL BRACKET AT FS 290.5, Y9.250, REF SRM 51-41-00-00-01. DETACHED CABLES FROM LOWER WEB OF SEAT TRACK AT LOCATIONS Y9.250, FS 253.5, FS 286.5 AND FS 293.5, REF WM 20-12-10. REATTACHED CABLES AT LOWER WEB OF SEAT TRACK AT LOCATIONS Y9.250, FS253.5, FS286.5 AND FS X293.5 REF REF WM 20-12-10. INSTALLED 12 RIVETS ON FWD SPLICE MEMBERS COMMON TO SEAT RAIL NR 12 AND NR 13 AT FS 229.5, Y9.250, REF SRM 51-42-05. REMOVED SEAT TRACK PN 85361510-104, SEAT TRACK NR 13 REF SRM 51-42-05 AND 51-41-00 AND 51-40-15. INSTALLED BOLTS COMMON TO SEAT TRACK 13 AND FRAMES FROM BS X236.00 TO X564.500 INSTALLED RIVETS ON WEB FROM BS X439.500 TO X469.5, REF SRM 51-41-00 AND SRM 51-42-05-02-01, STEP 4D, 3-10. FITTED AND DRILLED .2500" BOLT HOLES, FS 230 TO FS 401 AND .1250" WEB ATTACH HOLES FRAME SEAT TRACK NR 13 LOCATED AND DRILLED REF SRM 51-40-07. COMPLETED INSTALLATION OF SEAT TRACK 13, PN 85361510-104, REF DWG 85361501, REV E, AND SRM 51-42-05. COMPLETED INSTALLATION OF FWD SPLICE MEMBERS COMMON TO SEAT TRACK NR 12 AND NR 13 REF SRM 51-40-15.

Part: STRUCTURE — CORRODED (PAX DOORWAY) · airframe 21,400 hrs · 22,676 cycles

AFT PAX DOOR INNER EDGE PN 85339512-101 IS CORRODED. REMOVED INNER EDGE BEAM, PN: 85339512-101, REF SRM 51-42-05-02-01 AND SRM 51-42-45-02-01. LOCATED AND DRILLED NEW INNER EDGE BEAM, PN: 85339512-101, REF SRM 51-40-07-02-01 AND DWG. 85339541, REV B, 02/11/26. INSTALLED NEW NUTPLATES ON NEW INNER EDGE BEAM, PN: 85339512-101 IAW ITEMS OF TASK CARD 6-53-1160-AFT PAX DOOR. FLT JOB 5414935, OP 5458 AND DWG 85339541, REV B 02/11/26. COMPLIED WITH FORM M-184. OK TO CLOSE. INSTALLED INNER EDGE BEAM, PN: 85339512-101 REF DWG 85339541, REV B, 02/11/26 AND TASK CARD 6-53-1160. AFT PAX DOOR, FLT JOB 5414935, OP 5458 ITEM 5. APPLIED AV-DEC TO INNER SUFACE AND UNDER INNER EDGE BEAM FS 697.600 TO 669.300 PCS T/C 6-53-1160-AFT PAX DOOR, FLT ITEM 5 AND FIGURE 1.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK NR 7, PN 85361510-103, CORRODED. REMOVED MID SUPPORT WEB FROM SEAT TRACK NR 7 BS 321.0 TO 469.5 REF SRM 51-42-05. INSTALLED MID WEB SUPPORTS FROM BS 321.0 TO 469.5, REF SRM 51-42-05 AND DWG 85361501, REV E. DETACHED SEAT TRACK SUPPORT FRAME FROM 547.0 TO 564.5 REF SRM 51-41-00. INSTALLED SUPPORT FRAME FROM BS 547-0 TO BS 564.5 & REF SRM 51-41-05, AMD DWG 85361501, REV E. COMPLETE REMOVAL OF SEAT TRACK NR 7 BY DETACHING SUPPORT STRAPS FROM BS 234.0 TO 529.5. INSTALLED SUPPORT STRAPS REMAINING SEAT TRACK BS 7 FROM BS 234.0 TO 529.5, REF SRM 51-41-05 AND DWG 85361501, REV E. LOCATED AND DRILLED NR 7 SEAT TRACK, PN 85361510-103 REF SRM 51-40-07. LOCATED AND DRILLED SEAT TRACK SPLICE COMMON TO SEAT TRACK NR 6 + NR 7. REF SRM 51-40-07-02-01, REF SRM 51-40-07-02-01. LOCATED AND DRILLED SEAT TRACK 7, PN 8536-1510-103, FWD AND AFT SPLICES, REF SRM 51-40-07-02-01. INSTALLED BOLTS AT FRAMES BS 234.0 TO BS 341.0 AND 6 EA HILIGHTS IN AFT SPLICE COMMON TO SEAT TRACK 7 & NR 8, REF SRM 51-41-00-00-01 AND SRM 51-40-15-02-01. COMPLETED INSTALLATION OF SEAT TRACK, NR 7, PN 85361510-103, REF 51-42-05, SRM 51-41-05 + 51-40-15 DWG 85361501, REV 15. INSTALLED DRIP ANGLE FROM FS 301-FS 401 IAW SRM 51-42-05. INSTALLED GROUNDING STUD AND WIRES REF SRM 51-42-05-02-01 AND AMM 51-80-00-400-801. BOND CHECK GOOD REF AMM 51-80-00-760-801. INSTALLED DRIP ANGLE FROM FS 172.0-FS 301.0 ADJACENT TO SEAT TRACK NR 7, REF SRM 51-42-05. RESTORED FINISH TO SEAT TRACK NR 7, REF SRM 51-25-01.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK NR 19 REQUIRES REPLACEMENT PN 85361561-104. REMOVED SEAT TRACK NR 19 REF SRM 51-42-05-02-01. COMPLETED LOCATING AND INSTALLING SEAT TRACK NR 19 FROM FS 281.440.94 TO FS 571.5.440.94 REF SRM 51-40-07-03-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 21,638 hrs · 22,939 cycles

LEFT INBD SEAT TRACK NR 6, PN 85528210-111, CORRODED. REMOVED SEAT TRACK NR 6 IAW SRM 51-41-00. INSTALLED SEAT TRACK, NR 6 REF SRM 51-41-00. LOCATED, DRILLED AND INSTALLED 2 WIRE HARDNESS STAND OFFS ON SEAT TRACK NR 6 REF SRM 51-42-05 AND 51-40-07. LOCATED AND DRILLED 12EA SEAT TRACK NR 6 SUPPORT STRAPS, REF SRM 51-40-07. DRILLED AND LOCATED HOLES COMMON TO SEAT TRACK 6 AND SPLICE MEMBERS AT FS 102.5, Y-9.250, REF SRM 51-40-07. DRILLED AND LOCATED HOLES COMMON TO SEAT TRACK NR 6 AND SPLICE MEMBERS AT FS 571.5, Y-9.250, REF SRM 51-40-07. LOCATED AND DRILLED HOLES COMMON TO SEAT TRACK NR 6 DRIP ANGLE FROM FS 91.0 TO FS 231.5, REF SRM 51-40-07. INSTALLED DRIP ANGLE COMMON TO SEAT TRACK NR 5 AND NR 6 REF SRM 51-42-05.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 24,100 hrs · 22,676 cycles

AFT SERVICE DOOR INNER BEAM, PN:85339543-101 HAS EVIDENCE OF CORROSION. REMOVED AFT SERVICE DOOR BEAM, PN: 85339543-101, REF SRM 51-42-05-00-01. OK TO CLOSE. INSTALLED AFT SERVICE DOOR INNER BEAM, PN: 85339543-101, REF SRM 42-45-02-01, STEP 6G, 1-7. LOCATED AND DRILLED AFT SERVICE DOOR INNER BEAM, NEW, PN: 85339543-101, 51-40-07 SRM. INSTALLED ANCHOR NUT'S ON NEW INNER BEAM, PN: 85339543-101 AND APPLIED AVDEC TO UNDER SIDE OF INNER BEAM. REF SRM 51-42-75, 51-42-05 AND TASK CARD 6-53-1160 SERVICE DOOR FLT, PUT AVDEC ON BEFORE A NUT INSTALL. COMPLIED WITH FORM M-184.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,400 hrs · 22,676 cycles

SEAT TRACK NR 10, PN: 85328210-121, REQUIRES REPLACEMENT. REMOVED WEB, PN-85311097-001 FROM FS-39.00 TO GAIN ACCESS TO SEAT TRACK FASTENERS REF SRM INSTALLED WEB, PN-85311097-001, FS-39.00, REF SRM 51-42-45. REMOVED BONDING CABLES 2, FROM SEAT TRACK NR 10 PN-85328210-113 AT FS-36.00. REINSTALLED BONDING CABLES TO SEAT TRACK NR 10 AT FS-36, Y9.250, REF SRM 51-41-00. REMOVED ZIPTIES, 5 FROM WIRE HARNESS BUNDLE STANDOFFS BETWEEN FS-18.250 AND FS 1.000. INSTALLED ZIPTIES, 5, FOR WIRE HARNESSES TO STANDOFFS BETWEEN FS-18.250 AND FS 1.000 IAW WM 20-12-10, PARA 5, SECTION C. REMOVED CROSS MEMEBER "X", SUPPORT BOLTS, 4 PLACES, BETWEEN FS 18.250 AND FS 1.000. INSTALLED CROSSMEMBER SUPPORT BOLTS, 4 EA, BETWEEN FS-18.250 AND FS 1.000, REF SRM 51-41-00. REMOVED, 4 ZIPTIES FROM WIRE HARNESS BUNDLE STANDOFFS BETWEEN FS 1.000 AND FS 19.40. INSTALLED, 4, ZIPTIES TO WIRE HARNESS BUNDLE STANDOFFS BETWEEN FS 1.000 AND FS 19.40 REF WM 20-12-10. REMOVED SPLICE MEMBERS PN-85338216-101, 85338215-101 AND 85307835-167 REF: SRM 51-42-05. INSTALLED SPLICE MEMBERS PN 85338216-101, 85338215-101 AND 85307835-167 REF: SRM 51-42-05 AND DWG 85328201, REV E, DATED 97/12/10. REMOVED SEAT TRACK, PN-85328210-121, REF SRM 51-42-05. INSTALLED NEW SEAT TRACK, PN 85328210-121, REF: SRM 51-42-05 AND DWG NR 85328201, REV E DATED 97/12/10. LOCATED AND DRILLED SEAT TRACK, PN 85328210-121 IAW SRM 51-40-07. RESTORED FINISH ON SEAT TRACK NR 10, REF SRM 51-25-20. PERFORMED BONDING CHECK ON SEAT RAIL NR 10, REF SRM 51-80-00-760-830. BONDING CHECK GOOD. BONDING POST AT FS-36, Y9.250 AFTER BONDING CHECK COMPLETED, REF SRM 51-23-00.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK, NR 18, PN 85328261-105, REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 18, PN 85328261-105, REF SRM 51-42-05. INSTALLED SEAT TRACK NR 18, PN 85328261-105, REF SRM 51-42-05-02-01,51-40-15-02-01 AND DWG 85328251, REV A. REMOVED 8 EA RADIUS BLACKS COMMON TO SEAT TRACK NR 18 REF SRM 51-42-05. INSTALLED 8 EA RADIUS BLOCKS, PACKERS, COMMON TO SEAT TRACK 18, REF SRM 51-42-05-02-01 AND DWG 85328251, REV A. REMOVED 8 EA DADO BRACKETS COMMON TO SEAT TRACK NR 18, REF SRM 51-42-05. INSTALLED 8 EA DADO BRACKETS COMMON TO SEAT TRACK NR 18 REF SRM 51-42-05-02-01 AND 51-40-15-02-01. REMOVED AFT DOUBLER STRAP COMMON TO SEAT TRACK NR 18 AND SEAT TRACK NR 19 SPLICE REF SRM 51-42-05. INSTALLED AFT DOUBLER STRAP COMMON TO SEAT TRACK NR 18 AND NR 19 REF SRM 51-42-05-02-01, 51-40-15-02-01 AND DWG 85328251, REV A. REMOVED DADO ANGLES COMMON TO SEAT TRACK NR 18, REF SRM 51-42-05. INSTALLED DADO ANGLES COMMON TO SEAT TRACK NR 18 REF SRM 51-42-05-02-01 AND 51-42-45-02-01. LOCATED AND DRILLED NR 18 SEAT TRACK, PN 85328261-105 AFT SPLICE COMMON TO WEB BS 2016 TO 229 AND NR 30 HOLES COMMON TO WEB BS 94.8 TO 105.0, REF SRM 51-40-07, SWG 85328251, REV A. WHILE LOCATING SEAT TRACK NR 18, PN 85328261-105 MIS-DRILLED 1 HOLE ABOVE WEB FORWARD OF FS 216, REF SRM 51-40-07. LOCATED AND DRILLED REPLACEMENT NR 18 SEAT TRACK 85328261-105 FROM BS 95.0 TO 216, REF SRM 51-40-07 AND DWG 85328251, REV A. COMPLETED LOCATING AND DRILLING SEAT TRACK NR 18 FROM FS X216.00 TO FS X228.0, PN 85328261-105 REF SRM 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,400 hrs · 22,676 cycles

SEAT TRACK NR 5, PN 85328210-109, REQUIRES REPLACEMENT. DISPLACED 1 EA GROUND WIRE, 2931-G519, AT BS X-18.250. INSTALLED GROUND WIRES, 2431-G519, AT BS X-18.25, REF SRM 51-40-05. CABLE TIED WIRE BUNDLES AT BS 1.0 TO 19.4 QTY 1, BS 32.4 TO 47.9 QTY 4 AND BS 71.2 TO 94.8, QTY 6 REF WM 20-12-10. REMOVED NR 5 SEAT TRACK, PN 85328210-119, REF SRM 51-40-05-02-01. INSTALLED SEAT TRACK NR 5, PN 85328210-109, REF SRM 51-42-05-02-01, AND SRM 51-41-00-00-01. RECEIVED NEW SEAT TRACK, PN 85328210-109, LOCATED AND DRILLED FROM BS X -5.4 TO BS 94.8 FRAMES AND WEB REF SRM 51-40-07-02-01. COMPLETED LOCATING AND DRILLING OF SEAT TRACK NR 5, PN 8532810-109, REF SRM 51-40-07-02-01. BOND CHECK CARRIED ON GROUND WIRES, 2431-G519, AT BS X 18.25, 0.36 MILLI OHMS MEASURED. ACCEPTABLE REF AMM 51-80-00.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK NR 11, PN 85328210-115 REQUIRE REPLACEMENT. REMOVED DRIP ANGLE, PN 85307495-112 FROM FS 712.00 TO FS 216.00. REF SRM 51-42-05, REPAIR 01. DRIP ANGLE DRILLED AND LOCATED AND COUNTERSINK TO NEW SEAT TRACK REF SRM 51-40-07, REF ITEM 7. REMOVED SEAT TRACK NR 12 TO SEAT TRACK NR 11 SPLICE REF SRM 51-40-15, REPAIR 01. SPLICE HOLES COMMON TO STEAT TRACK NR 11 LOCATED DRILLED AND C-SINK, REF SRM 51-40-07, REF ITEM 8. REMOVED FASTENERS FROM SPLICE ADJACENT TO SEAT TRACK NR 10 AND SEAT TRACK NR 11 REF SRM 51-40-15. FASTENERS COMMON TO SEAT TRACK NR 10 AND NR 11 SPLICE INSTALLED REF SRM 51-42-05, 51-40-15, DWG 85328201, REV E. REMOVED 10EA BOLTS FROM "X" SUPPORT BRACKETS ADJUST TO SEAT TRACK NR 11, REF SRM 51-41-00. 10EA BOLTS INSTALLED NEW SEAT TRACK NR 11 SRM 51-41-00, DWG 85328201, REV E. REMOVED SEAT TRACK NR 11, PN 85328210-115, REF SRM 51-40-15, REPAIR 01. SEAT TRACK NR 11, PN 85328210-115 INSTALLED REF DWG 85328201-115, REV E. NEW SEAT TRACK 11, PN 85328210-115, LOCATED AND DRILLED REF SRM 51-40-07. DRIP ANGLE F, PN 85307495-112, INSTALLED REF SRM 51-42-05. SPLICE COMMON TO SEAT TRACK NR 11 AND NR 12 INSTALLED REF SRM 51-42-05,51-40-15, DWG 85328201, REV E. 7 EA WIRE BUNDLES INSTALLED TO NEW SEAT TRACK NR 11, REF WM 20-12-10.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 21,638 hrs · 22,939 cycles

SEAT TRACK NR 8, PN 85338210-109, REQUIRES REPLACEMENT. REMOVED SEAT TRACK 8, PN 85338210-109, REF SRM 51-42-05, 51-41-00. INSTALLED SEAT TRACK NR 8 PN 85338210-109 REF SRM 51-42-05 AND 51-41-05, REF DWG 85538201, REV E. REMOVED SPLICE MEMBERS COMMON TO SEAT TRACK 8+9, REF SRM 51-42-05, 51-40-15. INSTALLED SPLICE MEMBER COMMON TO SEAT TRACK 8 AND 9, REF SRM 51-42-05 AND 51-40-15, REF DWG 85338201, REV E. DRILL 4 EA .2500" BOLT HOLES 1 AT EACH FOLLOWING LOCATIONS 664, 644, 624, AND 604. DRILLED, 4 EA .2500" BOLT HOLES 1 AT EACH FOLLOWING LOCATIONS, FS 664, 644, 624, AND 604 REF SRM 51-40-07. LOCATED, DRILLED AND COUNTERSUNK SEAT TRACK NR 8 REF SRM 51-40-07 AT FWD & AFT SPLICES AND WEB LOCATIONS. LOCATED AND DRILLED FWD & AFT SPLICES COMMON TO SEAT TRACKS NR 8 AND 9, 8 AND 7 REF SRM 51-40-07.

Part: SEAT TRACK — CORRODED · airframe 21,400 hrs · 22,676 cycles

SEAT TRACK NR 14, PN 85328210-113, REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 14, PN: 85328210-113, REF SRM 51-41-00-00-01. INSTALLED NEW SEAT TRACK NR 14, PN: 85338210-113, REF SRM 51-42-05, 51-41-00, 51-40-15. ALSO, DWG 85338201, REV C, 02-04-09. LOCATED AND DRILLED NEW SEAT TRACK, PN: 85338210-113, REF SRM 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (NOT RESPORTED) · airframe 21,400 hrs · 22,676 cycles

SEAT TRACK NR 15, PN 85338210-115, REPLACEMENT REQUIRED. REMOVED FWD SPLICE, PN: 85338215-101 AND PN: 85338216-101 COMMON TO SEAT TRACK NR 14 AND 15, REF SRM 51-42-05-02-01 AND 51-40-15, REPAIR-01. INSTALLED FWD SPLICE, PN: 85338215-101 AND PN: 85338216-101 COMMON TO SEAT TRACK NR 14 AND NR 15, PN: 85338210-115 AND 85338210-113, REF SRM 51-40-15 AND 51-42-05. REMOVED AFT SPLICE, PN: 85338215215-101, REF SRM 51-42-05-02-01 AND 51-40-15, REPAIR-01. INSTALLED AFT SPLICE INBD AND OTBD, PN: 85338215-101 AND PN: 85338216-101 COMMON TO SEAT TRACK NR 15 AND NR 16 REF SRM 51-42-05-02-01, 51-40-15-02-01 AND DWG: 85338201, REV C DATED 02/04/09. REMOVED SEAT TRACK NR 15, PN: 85338210-115, REF SRM 51-41-00 STRUCT IDENT-01. INSTALLED SEAT TRACK NR 15 PN: 85338210-115, REF SRM 51-42-05-02-01, 51-41-00 STRUCT IDENT-01 AND DWG 85338201, REV C, DATED 02/04/09. LOCATED AND DRILLED NEW SEAT TRACK, PN: 853382101-115, REF SRM 51-41-00-02-01. RESTORED FINISH REF SRM 51-25-00.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 21,638 hrs · 22,939 cycles

AFT OTBD SPLICE, PN 85338215-101, COMMON TO SEAT RAIL NR 15 AND NR 16 HAS ELONGATED HOLES. LOCATED AND DRILLED NEW AFT OTBD SPLICE, PN 85338215-101, REF SRM 51-40-07-02-01.

Part: ANGLE — CORRODED (INTERCOSTAL) · airframe 21,638 hrs · 22,939 cycles

TWO ANGLES AT BS 6.7 AND BS 26.700 ON MACHINED INTERCOSTAL FOUND CORRODED. PN 85329333-103, COMPLIED WITH FORM M-184. LOCATED AND DRILED NEW ANGLES, PN 85329333-103, REF SRM 51-40-07-02-01. REMOVAL AND INSTALLATION OF OLD AND NEW ANGLES, PN 85329333-103 IS ACCOMPLISHED ON JOB 5414935, OP 5464, TASK CARD 6-53-1160-FWD PASSENGER DOOR ITEM 15, ITEM 25.

Part: ANGLE — CORRODED · airframe 21,400 hrs · 22,676 cycles

MACHINED INTERCOSTAL ANGLE AT BS 26-700 CORRODED, PN:85329576-104. COMPLIED WITH FORM M-184. LOCATED AND DRILLED NEW ANGLE, PN: 85329576-104, REF SRM 51-40-07-02-01. REMOVAL AND INSTALLATION OF OLD AND NEW ANGLE, PN: 85329576-104 IS ACCOMPLISHED ON JOB 5414935, OP 5464, TASK CARD 6-53-1160 FWD PASSENGER DOOR ITEM 15, ITEM 25.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 21,400 hrs · 22,676 cycles

MILLED WEB SKIN ATTACH ANGLE CORRODED AT BS 6.7, PN:85329542-107. COMPLIED WITH FORM M1-84. LOCATED AND DRILLED NEW ANGLE, PN 85329542-107, REF SRM 51-40-07-02-01. REMOVAL AND INSTALLATION OF OLD AND NEW ANGLE, PN 85329542-107 IS ACCOMPLISHED ON JOB 5414935, OP 5464 , TASK CARD, 6-53-1160-FWD PASSENGER DOOR ITEM 14, ITEM 26.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 21,638 hrs · 22,939 cycles

MACHINED INTERCOSTAL ANGLE AT BS 6.7 CORRODED, PN 85329576-103, COMPLIED WITH FORM M-184. LOCATED AND DRILLED NEW ANGLE, REF SRM 51-40-07-02-01. REMOVAL AND INSTALLATION OF OLD AND NEW ANGLE, PN 85329576-103 IS ACCOMPLISHED ON JOB 5414935, OP 5464, TASK CARD, 6-53-1160-FWD PASSENGER DOOR ITEM 15, ITEM 25.

Part: ATTACH ANGLE — CORRODED · airframe 21,638 hrs · 22,939 cycles

MILLED WEB SKIN ATTACH ANGLE CORRODED AT BS 26.700, PN 85329542-108, COMPLIED WITH FORM M-184. LOCATED AND DRILLED NEW ATTACHMENT ANGLE, PN 85329542-108, REF SRM 51-40-07-02-01. REMOVAL AND INSTALLATION OF OLD AND NEW ANGLE, PN 85329542-108 IS ACCOMPLISHED ON JOB 5414935, OP 5464, TASK CARD, 6-53-1160 FWD PASSENGER DOOR ITEM 14, ITEM 27.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 21,400 hrs · 22,676 cycles

SEAT TRACK NR 25, 85337843-103, REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 4 PN 85337843-103 IAW SRM 51-42-05 AND 51-42-45. INSTALLED NEW SEAT TRACK, PN 85337843-103, REF SRM 51-42-05-02-01 AND 51-42-45-02-01 AND DWG 85338806, REV P, DATED 98/05/08. LOCATED AND DRILLED SEAT TRACK NR 4, PN 85337843-103 IAW SRM 51-40-07. RESTORED FINISH REF SRM 51-25-05-02-01.

Part: BOLT — BROKEN (DOOR HANDRAIL) · airframe 21,594 hrs · 22,890 cycles

FORWARD HANDRAIL ATTACH BOLT FOR THE MAIN CABIN DOOR BROKEN. REPLACED BOLT. DOOR OPERATES NOTMALLY. RETURNED TO SERVICE.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 21,492 hrs · 22,783 cycles

EMERGENCY LIGHTS ILLUMINATED WHEN THE SWITCH WAS PLACED INTO "ARM". FOUND SWITCH MAKING INTERMITTENT CONTACT. REPLACED SWITCH BODY MODULE. OPS TESTS GOOD. REF AMM 33-51-05-000-801 AND 33-51-05-400-801. RETURNED TO SERVICE.

Part: PROPELLER — UNKNOWN · airframe 20,976 hrs · 22,224 cycles

NR 1 PROP SLOW TO COME OUT OF FEATHER WHEN CONDITION LEVER SET TO MAX. C/W FIM TASK 61-20-00-810-801, STEPS 1-5A, 10 AND, 6. NO FAULTS NOTED IN CDS FOR EMU. NO EXTERNAL PROPELLER LEAKS NOTED. PROP UNFEATHER NORMALLY WITH FEATHER PUMP. R & R NR 1 OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801, 61-20-26-400-801, OPERATIONAL TESTED GOOD IAW 61-20-00-710-803. LEAK CHECKED GOOD IAW 71-00-00-790-801. NO FAULTS IN CDS PROPELLER FEATHERS, UNFEATHERS NORMAL. RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 20,526 hrs · 21,708 cycles

ENROUTE, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED FOR 15-20 SECONDS. ON APPROACH TO LAND GEAR CAME DOWN NORMALLY. R & R NLG LOCK ACTUATOR. REF MM TASK 32-31-51-000-801 AND 32-31-51-400-801. PERFORMED A FUNCTIONAL CHECK OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYS. IAW MM 32-31-00-720-801. OPS CHECKED GOOD, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (OVERSPEED) · airframe 20,287 hrs · 21,457 cycles

DURING CLIMB, THE NR 2 ENGINE PROPELLER NP ROLLED BACK TO APPROXIMATELY 970-980 RPM. ALSO NOTED A TORQ SPLIT BETWEEN NR 1 AND NR 2 ENGINE WITH NR 2 ENGINE APPROXIMATELY 2-3 PERCENT HIGHER. AFTER REDUCING PROP RPM TO 900 ALL INDICATIONS WERE NORMAL. USED 1020 RPM FOR LANDING AND ALL INDICATIONS WERE NORMAL. IAW MAINTENANCE REQUEST C/W ENGINE TREND DOWNLOAD IAW MAINTENANCE 6773101. DUE TO ACFT HISTORY AND MAINTENANCE REQUEST, R & R NR 2 OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801 AND 61-20-26-400-801. OPS CHECKS GOOD. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: ENGINE — SURGES (NR 2) · airframe 20,258 hrs · 21,431 cycles

ABORTED TAKEOFF AT 85 KNOTS DUE TO NR 2 ENGINE TORQUE SURGE. ACFT CURRENTLY DOWN FOR REPAIRS.

Part: AUTOFEATHER SYS — NO TEST · airframe 19,755 hrs · 20,886 cycles

AUTOFEATHER SYSTEM TEST FAILED. PERFORMED OPS TEST OF THE SYS IAW AMM 61-20-00-710-801. TEST PASSED. COULD NOT DUPLICATE. RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,035 hrs · 20,125 cycles

EMERGENCY LIGHTS AT RT AND LT AFT PASSENGER DOORS ARE INOPERATIVE. REPLACED BATTERY PACKS AT NR 4 POWER SUPPLY IAW AMM 33-51-00-820-801. CHECKS GOOD.

Part: WIRE HARNESS — SHORTED (PROP DEICE) · airframe 18,578 hrs · 19,626 cycles

NR 1 PROPELLER DEICE CAUTION LIGHT ILLUMINATED INTERMITTENTLY. DIVERTED, LANDING UNEVENTFUL. CDS REPORTS NR 1 PROP, BLADE 3, PHASE C OPEN. R & R NR 1 PROPELLER BLADE 3 DEICER HARNESS IAW AMM TASK 61-10-16-00-802/400-802. FUNTIONAL TEST AND CALIBRATION OF DEICEING SYSTEM FOR NR 1 PROP OPS CKS NORMAL. ACFT OK FOR CONTINUED SERVICE. FUNCTIONAL TEST AND CALI PERFORMED IAW AMM TASK 30-61-00-720-802. RETURNED TO SERVICE.

Part: HANDLE — DISLODGED (CARGO DOOR) · airframe 18,500 hrs · 19,547 cycles

FUSELAGE DOOR WARNING LIGHT ILLUMINATED IMMEDIATELY AFTER GETTING AIRBORNE. ACFT WAS NOT PRESSURIZING. RETURNED TO DEPARTURE, AND LANDED UNEVENTFULLY. DURING TAXI IN, AGENTS NOTICED THAT THE MAIN BAGGAGE DOOR HANDLE WAS PROTRUDING ABOUT 1.5 INCHES, DOOR WAS SECURE PRIOR TO LEAVING GATE. NO DOOR LIGHTS ON FLIGHT DECK UNTIL BECOMING AIRBORNE. INSPECTED THE AFT BAGGAGE DOOR AFTER LANDING, FOUND HANDLE TO BE NOT LATCHED. INSPECTED THE AFT BAGGAGE DOOR HANDLE LOCK MECHANISM IAW AMM HS52-0028, NO DEFECTS NOTED. PERFORMED THE OPS TEST OF THE AFT BAGGAGE DOOR IAW AMM TASK 52-31-00-710-801, OPS CHECK GOOD. PRESSURIZED THE ACFT IAW AMM TASK 21-00-00-863-801, 21-00-00-863-802, AND RIL 84-21-012. ALL DOOR INDICATIONS NORMAL AND AFT BAGGAGE DOOR REMAINED CLOSED AND LOCKED DURING PRESSURIZATION CHECK WITH NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (CARGO DOOR) · airframe 17,761 hrs · 18,737 cycles

AFT CARGO DOOR MASTER WARNING AFTER TAKEOFF. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED AFT CARGO DOOR CLOSED SENSOR. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 17,528 hrs · 18,495 cycles

EMERGENCY LIGHT AT MAIN CABIN DOOR ENTRANCE IS LOOSE. SECURED EMERGENCY LIGHT. NO FURTHER DEFECTS NOTED.

Part: RECEIVER — MALFUNCTIONED (VHF) · airframe 17,194 hrs · 18,154 cycles

NO AIII MESSAGE ON HEADINGS DURING APPROACH. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INTERROGATED HEADINGS FAULT HISTORY NR 1 VHF NAV SHOWS INVALID FAULTS. R & R THE NR 1 VHF RECEIVER AS A PRECAUTIONARY MEASURE IAW MAINTENANCE 6345101. OPS CHECKS GOOD. ACFT IS CATEGORY III QUALIFIED COCKPIT PLACARD READS CAT III. DEFERRAL PLACARDS REMOVED. RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 17,036 hrs · 17,991 cycles

EMERGENCY EXIT SIGN IN FRONT OF ROW 2DE IS BROKEN. REPLACED THE SIGN LENS. OPS TEST FAILS. FERRIED ACFT FOR REPAIRS. INSPECTED AND FOUND AT EMERGENCY LIGHTS POWER SUPPLY "EPS2: CONNECTOR P4 THE WIRING WITHIN 3" OF THE BACKSHELL IS DAMAGED, REPAIRED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,030 hrs · 17,894 cycles

ALL EMERGENCY LIGHTS ASSOCIATED WITH NR 2 POWER SUPPLY ARE INOPERATIVE. INSPECTED AND FOUND AT EMERGENCY LIGHTS POWER SUPPLY "EPS2", CONNECTOR P4 THE WIRING WITHIN 3" OF THE BACKSHELL IS DAMAGED. FERRIED ACFT FOR REPAIRS. REPAIRED AND REPLACED DAMAGED WIRES AT POWER SUPPLY 2 AND REPLACED POWER SUPPLY 2. EMERGENCY LIGHTS, OPS CHECKED GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 17,000 hrs · 17,950 cycles

MAIN CABIN DOOR INOPERATIVE. MECHANICAL RESISTANCE ON DOOR HANDLE LAST PART OF OPENING AND PUSHING HANDLE. INSPECTED AND VERIFIED MAIN CABIN DOOR IS NOT BINDING ON THE FWD DRAFT BULKHEAD. PERFORMED OPS TEST OF THE DOOR WARNING SYSTEM IAW AMM TASK 52-11-00-710-802, STEPS 3.B.(1)THRU3.B(10). OPS TESTED GOOD. PERFORMED FUNCTIONAL TEST OF THE MAIN CABIN DOOR IAW AMM TASK 52-11-00-720-802. FUNCTIONAL TEST FAILED, MCD REQUIRED 70 LBS OF FORCE TO OPEN AND STILL FELT MECHANICAL RESISTANCE FELT ON BOTH THE INTERNAL AND EXTERNAL DOOR HANDLE. FERRIED ACFT FOR REPAIRS. ADJJUSTED MCD DOWN LIMIT STOP, REF. MM, TASK 52-11-00-820-801, PARA. 4A (9)(J) AND PARA. 4B (5). ADJ MCD INTERNAL HANDLE STOP BOLT REF. MM TASK 52-11-00-820-801, PARA.4B (7). ADJ MCD UP LIMIT STOP. REF. TASK 52-11-00-820-801, PARA 4B (9). PERFORMED FUNCTION TEST IAW MM TASK 52-11-00-720-801, PARA. 1 THRU 3A (11) AND 5. PARA. 3A (12) NOT REQUIRED AS DOOR SEAL NOT DISTURBED. FUNCTION TEST GOOD. PERFORMED FUNCTION TEST OF MCD HANDLE FORCES IAW MM TASK 52-11-720-802. FUNCTION TEST GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,785 hrs · 16,712 cycles

F/A EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP . LIGHT FUNCTIONS NORMAL. RETURNED TO SERVICE.

Part: GLOWSTRIP — LOOSE (ZONE 200) · airframe 15,719 hrs · 16,646 cycles

PHOTO ILLUMINESCENT STRIP CAME LOOSE. R & R GLOW STRIP (ROW 3A-5A) IAC AMM TASK 33-51-16-00-801 & TASK 33-51-16-400-801. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. RETURNED TO SERVICE.

Part: SEAT TRACK — GOUGED (BS 707-714) · airframe 15,683 hrs · 16,609 cycles

GOUGING ON RT SEAT TRACK AT FS Y9.250 BETWEEN FS X707.0 AND X714.0, SEAT TRACK NR 16. BLENDED SEAT TRACK, FOUND OUT OF LIMITS. REMOVED SEAT TRACK NR 16 IAW SRM 51-42-05-02-01 AND 51-41-00-00-01. DRILLED NEW SEAT TRACK IAW SRM 51-40-07-02-01. INSTALLED NEW TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. PRIMED IAW SRM 51-25-10-02-01. APPLIED AVDEC SELF LEVELING GREEN IAW SRM 51-21-10-02-01. APPLIED TOP COAT AND CPC IAW AMM 51-25-01-390-801 AND SRM 51-25-15-02-01.

Part: PANEL — CORRODED · airframe 15,683 hrs · 16,609 cycles

SEVERAL AREAS OF SUSPECTED CORROSION ON PANEL 144JZ. REMOVED OLD PANEL IAW SRM 51-41-00-00-01. TRANSFERRED HOLES FROM OLD PANEL TO NEW PANEL IAW SRM 51-40-07-02-01. COUNTERBORED ALL HOLES ON NEW PANEL USING A MICRO STOP AND COUNTERSINK. TREATED BARE METAL IN COUNTERSINKS IAW SRM 51-21-10-02-01. PRIMED PANEL IAW SRM 51-25-10-02-01. INSTALLED PANEL 144JZ IAW SRM 51-41-05-00-01.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 15,683 hrs · 16,609 cycles

DURING REMOVAL OF FWD PAX DOOR FOUND THRESHOLD TO BE CORRODED. DRILLED OFF CORRODED THRESHOLD IAW SRM 51-42-05-02-01. LOCATED FASTENER HOLES ON NEW THRESHOLD, PN 85329539-105. DRILLED FASTENER HOLES ON NEW THRESHOLD, COUNTER SUNK AND DEBURRED ALL HOLES AS REQUIRED IAW SRM 51-40-07-02-01 AND 51-42-05-02-01. REF STEP NR 1 DRILLED OFF 8 EA CHERRY MAX FASTENERS IAW SRM 51-42-90-02-01. INSTALLED THRESHOLD IAW SRM 51-42-05-02-01 AND SRM 51-42-45-02-01.

Part: LIGHT — UNSECURE (CABIN) · airframe 15,255 hrs · 16,171 cycles

EMERGENCY FLOOR PATCH LIGHT STRIP NOT SECURED. RESECURED FLOOR EMERGENCY LIGHT STRIP IN FRONT. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: LIGHT — LOOSE (CABIN) · airframe 14,936 hrs · 15,818 cycles

EMERGENCY FLOOR PATH LIGHTING STRIP AT THE MAIN CABIN DOOR IS LOOSE. SECURED THE STRIP AT THE MAIN CABIN DOOR AREA. OPS CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: STRUCTURE — MALFUNCTIONED (JUMP SEAT) · airframe 14,907 hrs · 15,783 cycles

F/A REPORTS THAT THE DOOR TO THE COMPARTMENT UNDER THE AFT F/A JUMPSEAT DOES NOT CLOSE PROPERLY. R & R AFT JUMPSEAT OTBD LOWER BASE/SEAT ASSY IAW AMM TASK 25-22-00-000-803, STEP 1-4A, PARA (6) AND 25-22-00-400-803, STEPS 1-4 A PARA (1) AND STEP 5. OPS CHECK GOOD ATTACH SEAT BELTS IAW MX SUPPLEMENT 25-0046. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 14,575 hrs · 15,458 cycles

FLOOR PATH PHOTO LUMINCENT STRIP AT ROW 1 A/B HAS COME OFF. SECURED FLOOR PATH STRIP. RETURNED TO SERVICE.

Part: ISOLATION MOUNT — BROKEN (EMERGENCY EXIT) · airframe 14,512 hrs · 15,390 cycles

SCREW SPINNING ON FORWARD UPPER EMERGENCY DOOR SUPPORT HANDLE SHOCK MOUNT BRACKET. REPLACED ISOLATOR MOUNT IAW SRM 51-42-45.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 14,480 hrs · 15,357 cycles

CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE FROM STATIONS X340.25 TO X683.45. REPLACED EP53 POWER SUPPLY AND BATTERY PACKS IAW AMM 33-51-01-000-400-801. OPS CHECK GOOD.

Part: SEAL — LOOSE (CARGO DOOR) · airframe 14,435 hrs · 15,316 cycles

DITCHING DAM MCD FELL, UNABLE TO REINSTALL. INSPECTED AND FOUND DITCHING DAM DOOR SEAL LOOSE. REINSTALLED SEAL IAW CMM 25-70-01, PAGE 7001, PARA 2.A(1), PERFORMED OPS CK OF DITCHING DAM IAW AMM TASK 25-62-01-710-801, NO DEFECT NOTED. RETURNED TO SERVICE.

Part: ISIS — MALFUNCTIONED (ZONE 200) · airframe 14,417 hrs · 15,302 cycles

DURING CLIMBOUT, NOTICED STANDBY ISI WAS BLANK ,CIRCUIT BREAKER WAS IN APPROX 15 MIN LATER ISI CAME BACK ON, OPERATED NORMALLY FOR REMAINDER OF FLT. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. R & R ISI IAW AMM TASKS 34-12-16-000-801/400-801 & HS 34-0026 DUE TO ISI UNIT HAVING HISTORY OF PR. C/W PITOT/STATIC SYS LEAK CHECK IAW TC 6341102. LEAK CHECK PASSED. ISI OP CHECKS GOOD IAW AMM TASK 34-12-16-710-801. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (BRAKES) · airframe 13,609 hrs · 14,487 cycles

BRAKES FELT WEAK. INBD BRAKES FELT HOTTER THEN THE OTBD BRAKES. BRAKE TEMP SPLIT 100 DEGREES INBD TO OTBD. PLACED ANTI SKID SYS ON MEL 32-40-2. CLEARED ON 7/17 BY: PERFORMED FUNCTIONAL TEST OF THE ANTI-SKID SYSTEM IAW AMM 32-46-00-720-802. BRAKE PRESSURES FOUND TO BE WITHIN LIMITS. INSPECTED & FOUND RT OTBD WHEEL SPEED TRANSDUCER BINDING & STIFF TO ROTATE BY HAND. R & R RT OTBD TRANSDUCER IAW AMM 32-46-11-000-801 & 32-46-11-400-801. TAXIED A/C WITH ANTI-SKID ON & OFF. NO DISCREPANCIES NOTED. OP'S CHECKS ARE GOOD. RETURNED TO SERVICE.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 13,573 hrs · 14,451 cycles

FOUND DAMAGE AT THE SHORT SECTION OF LUMINESCENT TRACK LIGHTING IN THE COCKPIT ENTRY WAY AND THE SECTION THAT RUNS ON THE RT SIDE OF THE AISLE IN FRONT OF THE FWD GALLEY. R & R THE COCKPIT ENTRANCE & RT SIDE IN FRONT OF GALLEY IAW AMM 33-51-16-000/400-801. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED · airframe 13,285 hrs · 14,163 cycles

DURING TAXI IN, THE NR 2 AC GEN AND NR 2 PEC CAUTION ILLUMINATED. COMPLIED WITH THE EC FOR THE NR 2 AC GEN CAUTION. COMPLIED WITH EC AND SHUT NR 2 ENGINE DOWN. ALSO THERE IS A POWERPLANT MESSAGE ON THE ED. INTERROGATED CDS AND FOUND THE FOLLOWING FAULTS: ENG2 CHA 12, 130, 134 CHB 122,130,134. SINCE FIM TASKS 61-20-03-810-815, 61-20-03-810-818, AND 61-20-03-810-822 INDICATE A FAULTED BETA FEEDBACK TRANSDUCER R & R THE NR 2 BETA FEEDBACK TRANSDUCER IAW AMM TASKS 61-20-11-000-803 AND 61-20-11-400-803. C/W MX 6710005 AND 6710006. C/W OPS TEST OF THE AC GEN SYS IAW AMM TASK 24-21-00-710-801. OPS TEST GOOD. NO FAULTS, CODES, CAUTIONS OR MESSAGES RETURNED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: STARTER GEN — FAILED (APU) · airframe 12,826 hrs · 13,682 cycles

APU STARTER GENERATOR FAILED AFTER APU START, RESULTING IN WHITE SMOKE. REPLACED THE STARTER GENERATOR IAW AMM 24-33-01-000-801. RETURNED TO SERVICE.

Part: WHEEL — SMOKE (MLG) · airframe 10,853 hrs · 11,655 cycles

DURING PREFLIGHT INSP FOUND NR 1 GEAR WHEEL ASSY, NR 2 WHEEL WAS SMOKING. OFF GOING CREW REPORTED NORMAL BRAKING APPLICATION DURING LANDING. INSPECTED NR 1 AND 2 BRAKE ASSY FOR SIGNS OF DAMAGE, OVERHEAT AND LEAKAGE, NONE NOTED. C/W VISUAL INSP OF BRAKE WEAR PINS IAW AMM 32-40-00-210-803. NO OTHER DEFECTS NOTED. OK FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: WIRE HARNESS — BURNED · airframe 10,459 hrs · 11,232 cycles

UNDER FLOOR AREA AFT OF THE COCKPIT FOUND WIRE BUNDLE W10 HAS 11 BURNED WIRES AND WIRE BUMDLE W17 HAS 2 BURNED WIRES. REPAIRED WIRES BY SPLICING OUT BURNED SECTIONS IAW WIRING DIAGRAM 20-16-10 AND 20-16-20. WIRES AFFECTED WERE : 2800-T11A-20-1, 2800-T14A-20-1, 3041-4B23-1, 3071-B512-1, 3041-LB12-1, 3000-98A20-1, 3000-95C20-1, 3000-97A20-1, 3000-40A16-1, 3000-10A16-1, 3000-93A-20, 3434-W83A-24.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,322 hrs · 11,089 cycles

CORROSION FOUND ON AFT SERVICE DOOR SILL. REMOVED CORROSION IAW SRM 51-21-00-00-02. PERFORMED LPI OF AREA, NO CORROSION OR CRACKS FOUND IAW NDTM SEC 8. REMOVED AFT SERVICE DOOR SILL AND FABRICATED NEW DOOR SILL REF EXISTING PATTERN AND SRM 51-40-07-02-01 AND TC 6-53-984. APPLIED ALODINE TREATMENT IAW SRM 51-21-10-02-01. INSTALLED NEW SILL IAW SRM 51-42-45-02-01.

Part: ANTI-SKID SYS — INTERMITTENT (MLG) · airframe 10,160 hrs · 10,921 cycles

BRAKES AND ANTI-SKID APPEARS SOFT & INTERMITTENT AT 80 KTS & LOWER. CHECKED CDS, NO CURRENT FAULTS. INSPECTED BRAKES TIRES, ALL LOOK NORMAL, NO LEAKS PERFORMED 3 HIGH SPEED TAXI & BRAKES CKS WITH CAPTAIN AT CONTROLS WITH ANTI-SKID ON & OFF. NO DEFECTS NOTED. ACFT OK FOR CONT SERVICE. NO PARTS REPLACED.

Part: UPLOCK SENSOR — OUT OF RIG (RT MLG) · airframe 10,043 hrs · 10,789 cycles

AFTER SELECTING MLG UP, RT MLG UNSAFE LIGHT STAYED ON. MLG HANDLE STAYED LIT. UNSAFE LIGHT WENT OUT BUT THE "RT DOOR" LIGHT CAME ON. THEN "RT DOOR' LIGHT WENT OUT & RT MLG UNSAFE LIGHT CAME ON & MLG HANDLE LIGHT CAME ON. THIS SEQUENCE CYCLED 3 TIMES & FINALLY SHOWED NORMAL INDICATIONS. COMPLIED WITH THE E /C & COMPLETED ALTERNATE MLG EXTENSION. LANDING UNEVENTFUL. FERRIED FOR REPAIRS. FOUND RT MLG UPLOCK SENSOR AT MAX LIMITS. RIGGED RT MLG UPLOCK SENSOR IAW AMM 32-61-06-830-801. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CONTROL BOX — MALFUNCTIONED (BRAKES) · airframe 9,986 hrs · 10,728 cycles

BRAKE APPLICATION SEEM NORMAL EARLY IN LANDING ROLL (HIGHER SPEEDS) BUT AS THE ACFT SLOWS TO MAKE A TURN OFF AND BRAKE APPLICATION IS A BIT HARDER, ANTI SKID SEEMS TO CYCLE, GRABBING THE BRAKES THEN RELEASING, THEN SEVERAL CYCLES MAKING TURN OFF'S DIFFICULT. PLACED THE ANTI-SKID SYS ON MEL 32-40-2. CLEARED 2/11 BY: C/W GVI OF MLG HUB CAPS & WHEEL SPEED GEN'S WITH NO DEFECTS NOTED. C/W GVI OF BRAKES WITH NO DEFECTS NOTED REPLACED ANTI-SKID CONTROL BOX IAW 32-46-01 FOR PRECAUTIONARY MEASURES. CHECKS GOOD. RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKES) · airframe 9,965 hrs · 10,704 cycles

AFTER LANDING, BRAKES WERE INEFFECTIVE AT TAXI SPEEDS. TOOK FULL FORCE ON BRAKE PEDALS FOR BRAKES TO WORK, THEN BRAKES WOULD IMMEDIATELY GRAB. DUE TO PREVIOUS HISTORY OF BRAKE CHANGE, R & R MAIN BRAKE CONTROL VALVE IAW AMM TASKS 32-42-06-000-801 AND 32-42-06-400-801. COMPLIED WITH TAXI CHECK OF ACFT AND BRAKING SYS. ACFT STOPS WITH NORMAL PRESSURE ON BRAKE PEDALS. ALL CHECKS ARE GOOD. NO LEAKS NOTED. RETURNED TO SERVICE.

Part: BRAKE — WORN (MLG) · airframe 9,958 hrs · 10,696 cycles

BRAKES VERY INEFFECTIVE WHEN SLOWING TO TURN DURING TAXI. FOUND NR 1 BRAKE WEAR INDICATORS TO BE RECESSED. REPLACED BRAKE ASSY AND ALSO TIRE IAW MX 6324101. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 9,905 hrs · 10,642 cycles

RT AMBER & RED GEAR DOOR LIGHTS AND GEAR HANDLE LIGHT CYCLED 3 OR 4 TIMES AFTER GEAR RETRACTION. IAW CHECKLIST WE PERFORMED A MANUAL GEAR EXTENSION. RETURNED TO THE FIELD, DUE TO HLN BRAKING ACTION. LANDED NORMAL. TOWED OFF RUNWAY. FERRIED FOR REPAIRS. PERFORMED GEAR SWINGS, COULD NOT DUPLICATE. INTERROGATED PSEU, FOUND RGDRCL SENSOR TO BE TOO FAR. RIGGED PROX SENSOR IAW MM TASK 32-61-06-830-801. PERFORMED GEAR SWINGS. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SKIN — CORRODED (LT WING) · airframe 22,657 hrs · 23,429 cycles

C5 CHECK - LT WING SKIN CUTOUT FOR PANEL 524BT HAS FRETTING. REMOVED FRETTING CORROSION IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. TREATED AND PRIMED AREA IAW RD 8/4-57-442.

Part: FRAME — CORRODED (FUSELAGE) · airframe 22,657 hrs · 23,429 cycles

C5 CHECK - FUSELAGE FRAME X71-200 LOWER FLANGE HAS CORROSION BETWEEN STR 31S AND 32S. REMOVED LIGHT SURFACE CORROSION IAW RD 8/4-53-2344. FLANGE IS WITHIN LIMITS IAW RD 8/4-53-2344. APPLIED ALODINE, PRIMER, TOPCOAT AND IAW RD 8/4-53-2344.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - RT WING OTBD FLAP HAS WEAR MARKS ON UPPER SURFACE FROM WING T/E PANEL AT STA YW 191.200 TO YW 270.000. BLENDED AREA IAW SRM 57-52-30-02-01. BLENDING WITHIN LIMITS OF RD 8/4-57-1489. COMPLIED WITH THE HORIZON TASK CARK RD 8/4-57-1489. COMPLETED REPAIR IAW RD 8/4-57-016.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - LT WING OTBD FLAP UPPER SURFACE HAS WEAR MARKS FROM WING T/E PANELS. DAMAGE TO PAINT ONLY. PREPARED AND PAINTED SURFACE IAW SRM 51-25-05-02-01.

Part: RIB — CRACKED (WING) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FOUND BOTH OTBD RIBS CRACKED ON LT L/E PANEL 511AL. REMOVED CRACKED FLANGES IAW SRM 51-42-05-02-01. VERIFIED AREA AS CRACK FREE IAW NDTM 8.1.0-1. FABRICATED REPAIR ANGLE AND MATCH DRILLED IAW RD 8/4-57-105. TREATED, PRIMED AND INSTALLED REPAIR ANGLES IAW RD 8/4-57-105.

Part: BUSHING — MISSING (RT AILERON) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FOUND MISSING BUSHING IN FWD LVDT BRACKET OF RT AILERON CAUSING EXCESSIVE WEAR IN BRACKET. REMOVED FWD LVDT BRACKET IAW SRM 51-42-05-02-01. DRILLED UP NEW FITTING IAW SRM 51-40-07 AND INSTALL NEW LVDT FWD FITTING IAW SRM 51-42-05-02-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FWD PAX DOOR TRESHOLD HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. R & R THRESHOLD IAW MFG RD 8/4-53-1660.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,801 hrs · 10,526 cycles

EXTERIOR FUSELAGE SKIN HAS IMPACT DAMAGE FROM BOTH LATCHES OF THE TOILET SERVICE DOOR. REMOVED DAMAGE IAW RD 8/4-53-2037. HFEC INSP SHOWED NO DEFECTS. PRIMED AND TREATED AREA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FLOOR SUPPORT WEB AT STA X32.400 JUST AFT OF FWD PAX DOOR ENTRY HAS AREAS OF CORROSION. REMOVED FLOOR SUPPORT WEB TO FOM IAW SRM 51-42-45. FOUND TO BE OUT OF LIMITS IAW SRM 51-14-00. FABRICATED FLOOR SUPPORT WEB IAW TC 6-53-967 USING .050 2024T3. INSTALLED FLOOR SUPPORT WEB IAW SRM 51-42-45.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - RT INBD SEAT RAIL NR10 HAS AREAS OF CORROSION TOP AND BOTTOM SURFACES AT STA X16.000 XO AND X1.000-X7.000. FOUND SEAT RAIL TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED NR10 SEAT RAIL IAW SRM 51-42-05 AND 51-40-15. PREPARED AND INSTALLED NEW SEAT TRACK IAW 51-42-05 AND 51-40-15.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - LT WING FUEL ACCESS PANEL, 524AT HAS AREAS OF FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-442.

Part: FRAME — CORRODED (FUSELAGE) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FRAME X71.200 LOWER FLANGE HAS CORROSION BETWEEN STR 32S AND 33. REMOVED CORROSION IAW RD 8/4-53-2344. FOUND FLANGE TO BE WITHIN LIMITS. COMPLIED WITH RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 116) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - FRAME X116.000 LOWER FLANGE HAS CORROSION BETWEEN STR 31P AND 32P. REMOVED CORROSION IAW RD 8/4-53-2344. FOUND FLANGE TO BE WITHIN LIMITS. COMPLIED WITH RD 8/4-53-2344.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - LT WING FUEL ACCESS MOUNT FLANGE HAS AREAS OF FRETTING. REMOVED DAMAGE FROM MOUNT FLANGE IAW RD 8/4-57-445. FOUND FLANGE TO BE WITHIN LIMITS. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - LT WING FUEL ACCESS PANEL 524BT MOUNT FLANGE HAS AREAS OF CORROSION AND MINOR FRETTING. REMOVED DAMAGE FROM ACCESS PANEL 524BT IAW RD 8/4-57-445. FOUND DAMAGE TO BE WITHIN LIMITS. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - LT WING FUEL ACCESS PANEL 524BT HAS AREAS OF CORROSION AND MINOR FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-442.

Part: CARGO TRACK — CORRODED · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - AFT BAGGAGE COMPARTMENT SEAT TRACK NR16 HAS CORROSION. REMOVED CORROSION IAW RD 8/4-53-884. FOUND TO BE WITHIN LIMITS IAW SRM 51-14-00-02-03. COMPLIED WITH STEPS IAW RD 8/4-53-884.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - AFT BAGGAGE COMPARTMENT SEAT TRACK, NR 9 MID AND AFT AREA HAVE CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884 AND RD 8/4-53-2362. COMPLIED WITH STEP IAW RD 8/4-53-884 AND RD 8/4-53-2362.

Part: FRAME — CORRODED (BS 783) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - CORROSION ON LOWER FLANGE OF AFT BAGGAGE COMPARTMENT STEPUP STA X783.10 LT SIDE. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW SRM 51-14-00-02-03. APPLIED ALODINE, PRIMER AND PAINT IAW SRM 51-21-10-02-01 AND 51-25-10-02-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - AFT BAGGAGE COMPARTMENT SEAT TRACK NR 25 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. COMPLIED WITH STEP IAW RD 8/4-53-884.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 9,801 hrs · 10,526 cycles

C2 CHECK - RT INBD SEAT RAIL NR11 HAS SURFACE CORROSION AT STA 15.000. REMOVED MINOR CORROSION FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. APPLIED ALODINE, PRIMER AND PAINT IAW SRM 51-21-10, 51-25-10 AND 51-25-15-02-01.

Part: ENGINE — FAILED (APU) · airframe 9,149 hrs · 9,813 cycles

APU FAILED ON START, RAMP REPORTED SMOKE FROM APU EXHAUST, APU L3 SOV C/B POPPED. PLACED APU ON MEL 49-00-1. RETURNED TO SERVICE.

Part: ANTENNA — FAILED (WX RADAR SYSTEM) · airframe 8,747 hrs · 9,371 cycles

WX FAIL ON BOTH MFD'S. RETURNED TO THE FIELD, LANDING UNEVENTFUL. R & R WEATHER RADAR ANTENNA IAW AMM TASKS 34-41-06-000-801 AND 34-41-06-400-801 , PERFORMED OPS CHECK IAW AMM TASKS 34-41-00-710-801 AND 34-41-00-710-802 , OPS CHECK GOOD NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (DE ICE SYS) · airframe 8,237 hrs · 8,777 cycles

"DEICE PRESS" CAUTION LIGHT ILLUMINATED DURING BOOT SEQUENCE WITH INBD TAIL. A BEAM RDM AT THE TIME. DIVERTED, LANDING UNEVENTFUL. INTERROGATED CDS FOUND FAULT LOW PRESSURE 6B. INSPECTED LT INBD HORIZ L/E FOR LEAKS. NONE FOUND R & R NR 6 DDV IAW AMM TASKS 30-11-16-000/400-801. FUNCTIONAL TEST GOOD IAW AMM TASK 30-11-720-801. RETURNED TO SERVICE.

Part: SKIN — NONE (FUSELAGE) · airframe 8,028 hrs · 8,547 cycles

LIGHTNING STRIKE IN CRUISE FLIGHT. ACFT WAS IN A "CLEAN" CONFIGURATION. PASSENGERS REPORT STRIKE ON RT SIDE OF ACFT. RETURNED TO DEPARTURE FOR A UNEVENTFUL LANDING. MX PERFORMED A PRELIMINARY LIGHTNING STRIKE INSP IAW FORM M-160. NO DAMAGE WAS FOUND OR EVIDENT. ACFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: INDICATOR — ILLUMINATED (MLG) · airframe 7,983 hrs · 8,500 cycles

ON GEAR RETRACTION, GEAR HANDLE REMAINED ILLUMIATED, 3 GREEN LIGHTS, & 3 RED LIGHTS WERE ILLUMINATED. STARTED THE "GEAR HANDLE LIGHT" CHECKLIST WHICH DROVE TO THE ALT EXTENSION CK LIST UPON WHICH WE DISCOVERED THE LANDING GEAR ALTERNATE RELEASE " DOOR WAS PARTIALLY OPEN. CONTACTED MX WHEN WE CLOSED THE DOOR ALL THE WAY AND GEAR RETRACTION, TOLD TO RETURN- CONTINUED WITH REMAINDER OF CHECK LIST. RETURNED TO THE FIELD. LANDING UNEVENTFUL. INSPECTED THE LANDING GEAR ALTERNATE RELEASE DOOR, NO DEFECTS NOTED. JACKED THE ACFT IAW MX NR 6071001, PERFORMED OPS TEST OF THE PRIMARY EXTENSION & RETRACTION SYS IAW AMM 32-31-00-710-801 & ALTERNATE EXT. SYS IAW AMM 32-34-00-710-801. ALL OPS TESTS GOOD NO DEFECTS NOTED. THE ALTERNATE EXT DOOR MOVES FREELY & NO ABNORMAL CONDITIONS EXIST, NO BINDING EITHER. NO FAULT FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WIRE — BURNED (WINDSHIELD) · airframe 7,562 hrs · 8,002 cycles

OUT OF 14,000 FT DEPARTING PDX SMOKE (ODOR, REDUCED VIS, NO FLAMES) IN COCKPIT CA'S SIDE. CREW RAN SMOKE CHECKLIST. ALSO TURNED OFF W/S HEAT SMOKE DECREASED ON APPROACH TO AIRPORT, F/A'S DID NOT DETECT SMOKE IN CABIN. RETURNED TO FIELD. LANDING UNEVENTFUL. INSP OF FLIGHTDECK FOUND BURNED WIRE AND EVIDENCE OF ARCING AT COPILOTS WINDSHIELD HEAT TERMINAL. WIRING REPAIRED AND COPILOTS WINDSHIELD REPLACED. CHECKS GOOD. ACFT RETURNED TO SERVICE.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (RT MLG DOOR) · airframe 7,220 hrs · 7,599 cycles

RT MAIN GEAR DOOR REMAINED OPEN AFTRE GEAR EXTENSION. FERRIED FOR REPAIRS. REMOVED AND REPLACED RT DOWNLOCK NR 2 (RGDLK2) SENSOR IAW AMM 32-61-06-000-801 AND 32-61-06-400-801. PERFORMED LG PRIMARY SYS OPS CHECK IAW 32-31-00-710-801 OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (DISTRIBUTOR) · airframe 7,066 hrs · 7,414 cycles

GEG- DEICE CAUTION LIGHT ILLUMINATED, DEICE LIGHT ILLUMINATED WHEN NR 2 INTAKE LIGHT DIMLY ILLUMINATED. DEICE PRESSURE WAS NORMAL. DEICE LIGHT IS ALL TESTED NORMAL. REPLACED NR 4 DDV IAW AMM 30-11-16, PGS 401-708. FUNCT. CK'S GOOD. VISUAL INSP OF NR 2 INTAKE BOOT- NDN. A/C OK FOR SERVICE.

Part: DOOR — STIFF (MAIN PAX) · airframe 6,840 hrs · 7,156 cycles

PDX- LEFT REAR PASSENGER DOOR HARD TO OPEN AND CLOSE AS REPORTED BY FLIGHT ATTENDANT. INSPECTED DOOR NO DEFECTS NOTED CLEANED AND LUBED DOOR SEAL DOOR OPERATION NORMAL AT THIS TIME. COULD NOT DUPLICATE. NO PARTS REPLACED.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 6,833 hrs · 7,146 cycles

FA AND RAMP AGENTS BOTH REPORT LT REAR PAX DOOR EXTREMELY DIFFUCULT TO OPERATE. CYCLED AFT PAX DOOR THROUGH SEVERAL CYCLES FOUND NO OBVIOUS DEFECTS VISUALLY AND FUNTIONALLY. CLEANED AND LUBED AFT PAX DOOR SEAL CYCLED DOOR SEVERAL MORE TIMES NO FURTHER DEFECTS NOTED, ACFT OK'D FOR CONTINUED SERVICE. NO PARTS REPLACED.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 5,771 hrs · 5,920 cycles

SEA - AFTER SELECTING THE GEAR UP, THE LEFT MAIN GEAR RED UNSAFE LIGHT STAYED ILLUMINATED. DID ALTERNATE GEAR EXTENSION. GEAR CAME DOWN AND LOCKED AS NORMAL. LANDING UNEVENTFUL. DIVERT FROM HLN. FERRY TO PDX. PSEU SHOWED NO FAULTS LIGHTLY TAPING ON LEFT GEAR INDICATOR LIGHT WITH FINGER TURNED RED UNSAFE LIGHT ON AND OFF. REPLACED LANDING GEAR CONTROL PANEL PER Q400 32-31-01-000-801 AND 32-31-01-400-801 TESTS GOOD. RETURNED TO SERVICE.

Part: DIODE — FAILED (POWERPLANT) · airframe 5,399 hrs · 5,498 cycles

PDX - POWERPLANT MESSAGES ON CLIMB-OUT ALL INDICATIONS NORMAL. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REPLACED DIODE 3442-CR4, REF WM 32-61-01 SHEET 11. PERFORMED POWER ASSURANCE CHECK ON BOTH ENGINES PER MTC NR 670005, ALL CHECKS GOOD, NO " POWERPLANT" MESSAGES AFTER RUNS. RETURNED TO SERVICE.

Part: FAIRING — CHAFED (FUSELAGE) · airframe 4,815 hrs · 4,852 cycles

PDX - C1 - FUSELAGE FAIRING PANEL 261CT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING SURFACE. BLENDED DAMAGED AREA MAX MATERIAL REMOVED .003" , IAW RD 8/4-53-521 STEP 1-2. HFEC AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED REPAIR AREAS IAW RD 8/4-53-521 STEP 4-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,815 hrs · 4,852 cycles

PDX - C1 - LT INBOARD SEAT TRACK HAS CORROSION BETWEEN STA X664 AND X 666. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS REF RD 8/4-53-884. REMOVED NR 8 SEAT TRACK IAW Q400 SRM 51-40-07. MATCH DRILLED NEW SEAT TRACK AND INSTALLED SEAT TRACK IAW -8 Q400 SRM 51-40-07, 51-40-15 AND 51-42-05.

Part: FAIRING — CHAFED (FUSELAGE) · airframe 4,815 hrs · 4,852 cycles

PDX - C1 - FUSELAGE FAIRING PANEL 261FT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING EDGE. BLENDED OUT DAMAGE MAX MATERIAL REMOVED .003" IAW RD 8/4-53-521 STEP 1-2. HFEC INSPECTED AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINED AND PRIMED AREA IAW RD 8/4-53-521 STEPS 4-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,815 hrs · 4,852 cycles

PDX - C1 - RT INBOARD SEAT TRACK HAS CORROSION BETWEEN STA X665 AND STA X668. BLENDED OUT CORROSION, MAX MATERIAL REMOVED .026", FOUND TO BE OUT OF LIMITS PER RD 8/4-53-884. REMOVED SEAT TRACK REF Q400 SRM 51-40-15 AND 51-42-05. INSTALLED NEW SEAT TRACK REF Q400 SRM 51-40-15 AND 51-42-05.

Part: EXCITER — FAILED (APU)

FLIGHT 2215. APU FAILED TO START, FLAME CAME OUT OF THE TAIL ON START ATTEMPT. PLACED THE APU ON MEL 49-00-1. CLEARED ON 9/28 BY REPLACING THE APU EXCITER AND IGNITER "B". OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (K)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 2,570 hrs · 2,482 cycles

PDX - FLIGHT 2239 - PUSHER SYSTEM FAIL CAUTION ILLUMINATED ON LANDING. AFTER CHECKLIST, LIGHT STILL ON. MAINTENANCE COMPLIED WITH SERVICE LETTER SL-31-005. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: VALVE — FAILED (DE ICE SYS) · airframe 2,461 hrs · 2,358 cycles

DURING CRUISE RECEIVED A DE-ICE PRESSURE CAUTION LIGHT. RAN THE CHECKLIST AND THE LIGHT WENT OUT. 15 MINUTES LATER IT RETURNED. THE ADVISORY LIGHT FOR THE RT BOOT SEGMENT FLICKERED. DE-ICE PRESSURE WAS OK. MAINTENANCE REPLACED THE NR4 DDV VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (AOA) · airframe 2,343 hrs · 2,243 cycles

PDX- FLIGHT 2466 - ON PUSHBACK WITH THE PROPS COMING OUT OF FEATHER, THE STALL PUSHER SYSTEM LIGHT ILLUMINATED. RETURNED TO THE GATE. MAINTENANCE REPLACED THE AOA TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (STICK PUSHER) · airframe 1,961 hrs · 1,847 cycles

PDX - ON FLIGHT 2239, AFTER LANDING AND CLEARING RUNWAY, PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED. RAN EMERGENCY CHECKLIST DIRECTED STALL WARNING TEST WITH NO CHANGE. MAINTENANCE COMPLIED WITH OPERATOR ACTION CYCLED SPM NR 1 AND SPM NR 2 CIRCUIT BREAKERS. LIGHT CLEARED. NO MAINTENANCE ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: NONE — NONE (NONE) · airframe 1,953 hrs · 1,835 cycles

SEA FLIGHT NR 2229, ON TAXI OUT, ADC1 MESSAGE ON BOTH PFD'S. ALSO FO'S IVSI SHOWS 10 FPM CLIMB INTERMITTENTLY. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE FOUND ADC SOURCE SWITCH TO BE IN ADC1 POSITION. PLACED SWITCH TO NORMAL POSITION AND PFD DISPLAYED CORRECTLY, ADC1 STATUS MESSAGE WENT AWAY. REMOVED AND REPLACED ADU2 IAW MTC 6341101. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 1,728 hrs · 1,619 cycles

SEA FLIGHT NR 2316: EMERGENCY LIGHTS REMAIN ON IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTS, NORMAL/ON SWITCH ON FWD BULKHEAD ASSY. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM IAW Q400 AMM TASK 33-51-00-710-801. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 1,637 hrs · 1,538 cycles

SEA FLIGHT NR 2332: EMERGENCY LIGHTS COME ON IN THE ARMED POSITION. MAINTENANCE CYCLED AIRCRAFT POWER OFF THEN ON. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 1,507 hrs · 1,393 cycles

BOI FLIGHT NR 2360: DURING TAXI OUT FA REPORTS THE EMERGENCY LIGHTS REMAIN ON WHEN THE COCKPIT EM SWITCH IS IN THE ARM POSITION. FA EMERGENCY SWITCH IS WHERE IT IS SUPPOSED TO BE, THE COCKPIT EM SWITCH IS PUT IN THE OFF POSITION, THE LIGHTS GO OFF. MAINTENANCE REMOVED AND REPLACED 3351-K2 RELAY IWA FIM 33-50-00. ALL OPS AND INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 1,507 hrs · 1,393 cycles

BOI FLIGHT NR 2360: DURING TAXI OUT, FA REPORTS THE EMERGENCY LIGHTS REMAIN ON WHEN THE COCKPIT EM SWITCH IS IN THE ARM POSITION. FA'S EM SWITCH IS WHERE IT IS SUPPOSED TO BE. THE COCKPIT EM SWITCH IS PUT IN THE OFF POSITION. THE LIGHT GOES OUT. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE REMOVED AND REPLACED 3351-K2 RELAY IAW FIM 33-50-00. ALL OPS AND INDICATIONS ARE NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 1,426 hrs · 1,324 cycles

PDX FLIGHT NR 2359: DURING BOARDING, EMERGENCY LIGHTS ACTIVATED AND REMAINED ON AFTER SWITCH WAS CYCLED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW TASK 33-51-00-710-801. OPS CHECK NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 1,359 hrs · 1,262 cycles

SEA FLIGHT NR 2287: AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. REJECTED TAKEOFF AT 65 KIAS. PERFORMED REJECTED T/O CHECKLIST. MAINTENANCE INTERROGATED CDS. NO FAULTS POSTED. PERFORMED OPS TEST OF AUTOFEATHER SYSTEM. BOTH ENGINES STARTED AND RUNNING IAW AMM TASK 61-20-00-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — INOPERATIVE (FUEL) · airframe 1,270 hrs · 1,183 cycles

SEA - ON FLIGHT 2288 RETURNED TO GATE, NR 2 TANK AUXILIARY PUMP SWITCH LIGHT INOPERABLE. REMOVED AND REPLACED NR 2 AUXILIARY PUMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (PEC) · airframe 514 hrs · 444 cycles

SEA FLIGHT NR 2418: POWER PLANT MESSAGE AFTER ENGINES STARTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODES 130B ON 32 PROP AND 274 ON NR 1 PROP. CLEARED FAULTS PER Q400 AMM TASK 61-20-36-070-801. CLEANED ALL ELECTRICAL CONNECTORS ON NR 1 AND NR 2 PEC AND PCU. PERFORMED GROUND IDLE ENGINE RUN PER AMM TASK 71-00-00-868-811. POWER PLANT MESSAGE AND FAULT CODES DID NOT REOCCUR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 400 hrs · 338 cycles

PDX - ON FLIGHT 2362, RETURNED TO GATE. CREW REPORTS CABIN EMERGENCY LIGHTS WILL NOT TURN OFF WHILE ARMED. MAINTENANCE REPLACED 3351 K2 RELAY. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 354 hrs · 301 cycles

POWER PLANT MESSAGE OCCURRED DURING TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND PEC FAULT CODE 130B ON NR 2 PEC. CLEARED FAULT IAW Q400 AMM TASK 61-20-36-070-801. C/W OPS CHECK OF AUTO FEATHER (FAULT OCCURRED DURING A/F TEST WHILE TAXING) IAW Q400 AMM TASK 61-20-00-710-805. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (RT BLEED SYS) · airframe 258 hrs · 215 cycles

OAK/SUN FLIGHT NR 2409: DURING LEVEL CRUISE FLIGHT AT 25,000 FT, NR 2 BLEED HOT CAUTION ILLUMINATED AND REMAINED ILLUMINATED WITH NR 2 BLEED SWITCH OFF FOR DURATION. FLIGHT DIVERTED TO BOI. MAINTENANCE FOUND CDS MESSAGE B BLD ANA OT. REMOVED AND REPLACED RIGHT BLEED OVER TEMP SWITCH AND RIGHT PRECOOLER TEMP SWITCH (P/N 820907-5). REF Q400 FIM 36-11-16-810-802 PARA 1 THROUGH 4A, STEPS (1) AND (2) AND PARA 5. NO CDS FAULTS. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 247 hrs · 206 cycles

SEA - ON FLIGHT 2476, EMERGENCY LIGHT ILLUMINATED WHEN POSITIONED TO ARM RECYCLED SWITCH. NO GOOD. MAINTENANCE REMOVED AND REPLACED FA'S EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 176 hrs · 140 cycles

SEA FLIGHT NR 2378: FOUND MAIN CABIN DOOR EXTERIOR OPEN HANDLE RECESSES TOO DEEP, CANNOT OPEN DOOR FROM OUTSIDE. MAINTENANCE SHIMMED EXTERIOR DOOR HANDLE STOP BUMPER AS REQUIRED FOR FLUSH FIT OF HANDLE. DOOR OPERATES NORMALLY OPENING AND CLOSING. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — UNKNOWN (NR 2) · airframe 135 hrs · 106 cycles

LAX FLIGHT NR 2343: AS THE AIRCRAFT TAXIED ONTO THE RUNWAY, THE POWER PLANT MESSAGE APPEARED ON THE ED. AIRCRAFT RETURNED TO GATE. MAINTENANCE UPON INTERROGATION OF CDS FOR ENGINE FAULTS, FOUND NR 2 ENGINE LANE B FAULT 130. C/W FIM TASK 61-20-03-810-815. AFTER FAULT CODE WAS CLEARED, RAN NR 2 ENGINE TWICE IN BETA RANGE. FAULT DID NOT RETURN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 135 hrs · 106 cycles

SEA FLIGHT NR 2334: AS THE AIRCRAFT ONTO THE RUNWAY, THE POWER PLANT MESSAGE APPEARED ON THE ED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE UPON INTERROGATION OF THE CDS FOR ENGINE FAULTS FOUND NR 2 ENGINE LANE B FAULT 130. C/W FIM TASK 61-20-03-810-815. AFTER FAULT CODE CLEARED, RAN NR 2 ENGINE TWICE IN BETA RANGE. FAULT DID NOT RETURN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (DOOR WARNING) · airframe 94 hrs · 69 cycles

SEA FLIGHT NR 2379: FUSELAGE DOOR WARNING ON APPROACH AND ON TAXI. LEFT REAR BAGGAGE DOOR. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO FAULTS ON THE PROX SENSOR COMPUTER. PROX SENSOR COMPUTER SHOWS ALL AFT BAGGAGE SENSORS GOOD WHEN DOOR CLOSED AND LOCKED. NO VISUAL DISCREPANCIES WITH DOOR OR DOOR HANDLE. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS) · airframe 49 hrs · 33 cycles

SEA FLIGHT NR 2328: FLAP POWER CAUTION LIGHT ILLUMINATED DURING PUSH BACK. RESET C/B PER EA CHECKLIST. LIGHT WAS STILL ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE PERFORMED Q400 FIM TASK 27-50-00-810-802 AND OPS TEST OF THE WING FLAPS IAW Q400 AMM TASK 27-50-00-710-801. OPERATIONAL TEST IS GOOD WITH NO DISCREPANCIES AND NO REOCCURRENCE OF FLAP POWER CAUTION LIGHT. NO PARTS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.