N423QX

Part: CONTROLLER — MALFUNCTIONED (NR 2) · airframe 27,195 hrs · 29,043 cycles

INTERMITTANT #2 PEC CAUTION, REMOVED FROM SERVICE. NO CODES FOUND IN CDS. REMOVED AND REPLACED #2 PEC IAW AMM TASKS 61-20-36-000-801 AND 400-801. CALIBRATION AND POST RUNS ALL GOOD. CAUTION DOES NOT ILLUMINATE. NO FAULTS POSTED. RETURNED TO SERVICE.

Part: APU — ODOR · airframe 26,928 hrs · 28,737 cycles

ACRID ODOR EMANATING FROM THE AIR VENTS IN THE CABIN. APPEARS TO BE ASSOCIATED WITH APU BLEED AIR. ODOR DISSIPATED WITH APU BLEED AIR OFF. VERIFIED TO BE APU, MEL. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,852 hrs · 28,645 cycles

FA ADVISED OF BURNING OIL SMELL FROM BLEED SYSTEM DURING DESCENT. REMOVED FROM SERVICE. CREW STATED SMELL WAS BRIEF DURING DESCENT. C/W FIM MCN 62172-01 ISSUE 2 STEP 2. FORM M-744 COMPLETED BY FLIGHT CREW. C/W FAULT ISOLATION PROCEDURE PER FIM TASK 71-00-00-810-817. PERFORMED GVI OF THE ENGINES, NO EVIDENCE OF OIL LEAK NOTED. CHECK ENGINES OIL LEVEL, CHECKED GOOD. RAN ENGINES AT DIFFERENT POWER SETTINGS WITH DIFFERENT BLEED SCENARIOS, NO BURNING SMELL NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE SYS — UNKNOWN (MLG) · airframe 26,657 hrs · 28,425 cycles

BRAKES INEFFECTIVE, TOOK FAR MORE PRESSURE THAN NORMAL TO GET BRAKE RESPONSE. REMOVED FROM SERVICE. GVI OF BRAKES, NO DEFECTS, PERFORMED FUNCTIONAL TEST OF ANTI-SKID CONTROL SYSTEM (BUILT IN TEST), FUNCTIONAL TEST OF ANTI-SKID SYSTEM, NO DEFECTS, VISUAL INSPECT OF ALL FOUR WHEEL SPEED XDUCERS, NO DEFECTS, FUNCTIONAL TEST OF MAIN LANDING GEAR BRAKE SYSTEM, ALL FUNCTIONAL TESTS GOOD. BLED ALL BRAKES, PERFORMED GROUND TAXI OPS (20 KNOTS), BRAKES SEEM TO WORK NORMALLY WITH ANTI-SKID ON AND OFF. RETURNED TO SERVICE.

Part: DISCHARGE TUBE — KINKED (NR 1 NAC EXTING) · airframe 26,474 hrs · 28,233 cycles

NR 1 ENGINE FIRE DISCHARGE TUBE WAS KINKED ON THE OUTBOARD SIDE OF THE NACELLE. 2 INCHES FORWARD OF THE MID FRAME AND ABOVE THE FORWARD LOWER STRUT. REPLACED DISCHARGE TUBE.

Part: SCREW — LOOSE (DOOR FRAME) · airframe 26,048 hrs · 27,756 cycles

FLIGHT DECK DOOR DIFFICULT TO OPEN DUE TO UPPER CORNER CATCHING ON LAV DOOR TRIM. REMOVED FROM SERVICE. FOUND LAV DOOR HINGE SCREWS LOOSE. RETIGHTENED SCREWS LAV DOOR AND COCKPIT DOOR HAVE PROPER FREEDOM OF MOVEMENT. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROL PANEL — MALFUNCTIONED (NR 1 PROPELLER) · airframe 25,858 hrs · 27,546 cycles

NR 1 PROPELLER DOES NOT FEATHER USING ALT FEATHER SWITCH AND LIGHT DOES NOT ILLUMINATE. REPLACED THE ENGINE FUEL, PROPELLER CONTROL PANEL IAW AMM 31-10-01-000-801, AND 31-10-01-400-801. OPS TESTED.

Part: SOCKET — BURNED (NLG INDICATOR) · airframe 24,905 hrs · 26,545 cycles

GREEN NOSE GEAR DOWN AND LOCKED LIGHT DIM. REMOVED FROM SERVICE. FOUND LEFT BULB TERMINAL BURNED. R & R LANDING GEAR CONTROL PANEL IAW AMM 32-31-01-000-801. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (RT MLG INDICATOR) · airframe 24,905 hrs · 26,545 cycles

SELECTED GEAR DOWN, ON FINAL, NO RIGHT MAIN GEAR DOWN AND LOCKED INDICATION. RAN E/A CHECKLIST. ALTERNATE GEAR LOCKED DOWN INDICATOR WAS NORMAL, 3 GREEN. RIGHT MAIN GEAR DOWN AND LOCKED LIGHT DOES NOT ILLUMINATE WITH ADVSY LIGHTS TEST. ALL OTHER LIGHTS TEST NORMALLY. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACED THE LAMP IN THE RT MLG INDICATOR LIGHT IAW AMM TASK 32-31-01-960-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BUMPER — OUT OF ADJUST (CABIN DOOR) · airframe 24,350 hrs · 25,969 cycles

RAMP REPORTS UNABLE TO OPEN MAIN CABIN DOOR FROM THE OUTSIDE HANDLE SEEMS MISALIGNED. REPLACED THE RUBBER STOP OF THE MCD HANDLE IAW TASK 52-11-00-820-801 STEPS 4B(3)(A)-(E). HANDLE STILL UNDERFLUSH APPROX 0.25". ADJUSTED THE MCD OUTER HANDLE BUMPER STOP REF AMM TASK52-11-00-820-801 STEPS 4.B.(3) (A) TRU (E). CHECKS GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 24,146 hrs · 25,747 cycles

EMERGENCY EXIT LIGHT AT THE LOWER CORNER OF THE RIGHT EMERGENCY EXIT IS CRACKED AND HAS A BROKEN BASE PLATE. REPLACED DAMAGED ASSEMBLY IAW CMM 25-23-29. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-801. CHECKS GOOD. RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (CAPTAIN'S) · airframe 24,143 hrs · 25,742 cycles

CAPTAIN'S OPEN SPEED BUG STUCK AT 171, WILL NOT CHANGE. DIVERTED, LANDING UNEVENTFUL. REPLACED NR 1 INDEX CONTROL PANEL, PERFORMED OPERATIONAL TEST IAW TC 6316103, ALL CHECKED GOOD. RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,642 hrs · 25,231 cycles

AT ROTATION SPEED MASTER WARNING DOOR LIGHT CAME ON. ABORTED TAKE OFF AT 123 KNOTS. INTERROGATED PSU FOUND NO FAULT CODES. PERFORMED OPERATIONAL TEST OF THE AFT PASSENGER DOOR WARNING SYSTEM IAW AMM REF TASK 52-12-00-710-802 3B. (1)-(9). OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. NO PARTS REPLACED.

Part: LIGHT — LOOSE (ROW 2D) · airframe 22,677 hrs · 24,208 cycles

EMERGENCY LIGHT STRIP IN FRONT OF ROW 2D IS LOOSE. SECURED THE LIGHT STRIP. RETURNED TO SERVICE.

Part: SHIM — MISSING (PAX DOOR) · airframe 22,583 hrs · 24,099 cycles

RAMP COULD NOT OPEN THE MAIN CABIN DOOR FROM THE OUTSIDE. . INSTALLED MISSING SHIMS AT THE EXTERIOR HANDLE BUMPER IAW AMM TASK 52-11-00-820-801. RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

FRAME STA X401.0 TO STA X428.5, STR 24 EVIDENCE OF CORROSION. CORROSION REMOVAL FROM STR 24P IAW STRUCTURAL ID-02, PAR 2A BETWEEN FSX 401.0 TO FSX 428.5 HAS OVER HALF OF STR MATERIAL LOSS WITH CORROSION STILL PRESENT. REMOVED REMAINING CORROSION FROM STR 24P BETWEEN FSX 423.50 TO FSX 416.50 CORROSION REMOVAL WAS FROM VERTICAL LEG INSIDE LOWER RADIUS AND LOWER HORIZONTAL LEG OF STR 24P IAW SRM 51-21-00, STRUCTURAL ID-02, PAR 4A, ITEM 5A THRU 5D. USING DEPTH GAGE TUC-4745 AT DEEPEST POINT OF CORROSION REMOVAL ON STR 24P AT 125. X 421.50, .065 MATERIAL LOSS ORIGINAL MATERIAL THICKNESS AT STR 24P, VERTICAL LEG .080 LOWER HORIZONTAL LEG .110 IAW DWG: 85360021, REV H, SHT 19. REMOVE CORROSION FOUND BETWEEN FS X428.50 TO 423.50 AT STR 24P. BLENDED OUT CORROSION AT STR 24P FROM FSX 425.50-FSX 422.00 IAW SRM 51-21-00-00-02, BLENDED INTO RADIUS, HORIZONTAL AND VERTICAL LEG. C/W INSP, REF NDTM 51-00-06 + 51-00-04, NO DEFECTS NOTED MIN THICK=.046" ON LOWER HORIZONTAL SURFACE + .067" ON VERTICAL SURFACE. TREATED, PRIMED AND PAINTED REWORKED AREA, REF SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-15-02-01.

Part: HOUSING — WORN (CARGO DOOR) · airframe 22,224 hrs · 23,703 cycles

AFT CARGO DOOR FLUSH HANDLE ASSY HAS EXCESSIVE PLAY. REMOVED BRACKET HANDLE ASSY FROM HSG ASSY, PN 85237500-109-901, REF AMM 52-31-01-000-802 PARA 4A, 2. INSTALLED BRACKET AND HANDLE ASSY ON HOUSING ASSY, PN 85237500-109-901 IAW AMM 52-31-01-400-802 STEP 4D, 18. REMOVED FASTENERS THAT SECURE HOUSING ASSY TO CARGO DOOR SKIN REF AMM 52-31-01-000-802. INSTALLED FASTENERS COMNMON TO HOUSING ASSY TO CARGO DOOR SKIN REF AMM 52-31-01-400-802. REMOVED BRACKET WHICH HOLDS DOOR SEAL CONTROL VALVE REF AMM 52-31-01-000-802, PARA 4D, 6. LOCATED AND DRILLED BRACKET WHICH HOLDS DOOR SEAL CONTROL VALVE, PN 85237852-107 FOR NEW FASTENERS, HS 10, AG5, REF AMM 52-31-01-300-802, PARA 4E. REMOVED HOUSING ASSY FROM DOOR STRUCTURE REF AMM 52-31-01-000-802 PARA 4 D, 9. INSTALLED HOUSING ASSY TO DOOR STRUCTURE REF AMM 52-31-01-400-802, STEP 4D, 1-12. INSTALLED AFT BAGGAGE DOOR PROXIMITY SENSOR TARGET ON NEW HANDLE IAW HS NR 52-0024. REMOVED AFT BAGGAGE DOOR PANEL, PN 951291-501 IAW AMM 25-52-16-400-801. INSTALLED AFT BAGGAGE DOOR PANEL, PN 951291-501 IAW AMM 25-52-16-400-801.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 7 REQUIRES REPLACEMENT. REMOVED SEAT TRACK NR 7, PN 85361510-103, REF SRM 51-42-05, REPAIR -01, SRM 51-40-00-00-01, AND 51-40-15 REPAIR -01. SEAT TRACK NR 7 INSTALLED REF SRM 51-42-05, DWG 85361501, REV E, DWG 85307071, REV A. REMOVED FORWARD SPLICE ASSY COMMON TO SEAT TRACK NR 6 AND 7, PN 85338216-101 AND PN 85338215-101, REF SRM 51-40-15 REPAIR -01 AND SRM 51-42-05 REPAIR -01. INSTALLED FORWARD SPLICE REF SRM 51-42-05, 54-40-15 DWG 85307071 REV A. REMOVED AFT SPLICE ASSY COMMON TO SEAT TRACK, NR 7 AND NR 8, PN 85338216-101 AND 85338215-101, REF SRM 51-40-15, REPAIR -01 AND 51-42-05, REPAIR -01. INSTALLATION OF AFT SPLICE ASSY COMMON TO SEAT TRACKS NR 7 AND NR 8 PN 85338216-101 AND PN 85338215-101 ACCOMPLISHED ON ITEM 10. LOCATED AND DRILLED NEW SEAT TRACK NR 7 AT FWD AND AFT SPLICE LOCATIONS AND 5 EA STANDOFFS AND 1 EA BONDING BRACKET REF SRM 51-40-07 REPAIR -01. DRIP ANGLES, 2EA, ALSO LOCATED AND DRILLED. DRILLED BOLT HOLES & HOLES COMMON TO WEB REF SRM 51-40-07, DWG 85361501, REV E. DEBURRED SEAT TRACK NR 7 REF SRM 51-40-07-02-01. INSTALLED FASTENERS AT X 571.0 JOINT REF SRM 51-42-05-00-01, 51-40-15-02-01. INSTALLED FASTENERS COMMON TO WEB AND BOLTS REF SRM 51-42-05 51-41-00, DWG 85361501, REV E. REPLACED 6 RIVETS REF SRM 51-42-05-00-01. PERFORMED BONDING CHECK ON SEAT TRACK 7 TP9 REF AMM 51-80-00-760-830, BONDING CHECKS GOOD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

CORROSION ON GUSSET AT FS X281.0 AT STR 24P. REMOVED STRINGER-TO-FRAME CLEAT, PN 85328131-179 AT FS X 281, STR 24P, REF SRM 5142-05-02-01. INSTALLED REPLACEMENT CLEAT AT FS 281.00, STR 24P, PN 85328131, PO TX-5452, REF SRM 51-42-05-02-01, PARA 1-4, A-D DWG-85328131. LOCATED AND DRILLED REPLACEMENT CLEAT, GUSSET, PN 85328131-179, REF SRM 51-40-07-02-01, REPAIR-01.

Part: BEAM — CORRODED (EMERGENCY EXIT) · airframe 22,224 hrs · 23,703 cycles

FOUND CORROSION ON BEAM, PN 85329514-101 AND UNDER NUT PLATES AT EMERGENCY EXIT DOOR SURROUND. REMOVED FLOOR RETAINER, PN 85329515 REF SRM 51-41-00-00-01. INSTALLED FLOOR RETAINER, PN 853259515, REF SRM 51-41-00-00-01 AND DWG 85329511. REMOVED LOWER FORWARD EMERGENCY DOOR AT FS X 71.2- X 94.8 REF AMM 52-23-00-000-801. INSTALLED LOWER FORWARD EMERGENCY EXIT DOOR REF AMM 52-23-00-400-801. REMOVED 2 LOWER EMERGENCY DOOR STOP FITTINGS, PN 85329283-001 AT FS X88.2, FS X 77.38, Y40, REF SRM 51-41-00-00-01. INSTALLED 2 LOWER EMERGENCY DOOR STOP FITTINGS, PN 85329283-001 REF SRM 51-41-00-00-01. REMOVED CORRODED EDGE BEAM, PN 85329514-101, REF SRM 51-42-05-02-01. INSTALLED NEW EDGE BEAM, PN 85329514-101, REF SRM 51-42-05-02-01 AND DWG 85329511, REV D. LOCATED & DRILLED FASTENER HOLES FOR NEW REPLACEMENT EDGE BEAM, PN 85329514-101, REF SRM 51-40-07-02-01. PERFORMED FUNCTIONAL TEST OF THE LOWER FORWARD EMERGENCY DOOR REF AMM 52-23-00-720-801, FUNCTION TEST GOOD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 6, PN 85328210-111, REQUIRES REPLACEMENT. LOCATED AND DRILLED SPLICE ANGLE, PN 85338215-110 AND PN 85338216-11 AT FS X102.50 NR 5 AND NR 6 SEAT TRACK IAW SRM 51-40-07-02-01, 51-40-15-02-01 AND 51-42-05-02-01, DWG: 85338216, REV, DWG: 85338215, REV. LOCATED AND DRILLED NR 6 SEAT TRACK, PN 85328210-111 IAW SRM 51-40-15-02-01, 51-41-05-00-01, 51-42-05-02-01, 51-40-07-02-01 AND DWG: 8532821, REV E. REMOVED NR 6, SEAT TRACK, PN 85328210-111. INSTALLED SEAT TRACK NR 12, PN 85328210-111, REF SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-00-00-01 AND DWG 85328201, REV E. LOCATED AND DRILLED AFT SPLICE ANGLES COMMON TO SEAT TRACK NR 6 AND NR 7, INBD AND OTBD AT FS X 229.50, REF SRM 51-40-07-02-01 AND DWG 85328201, REV E. REMOVED 11 TOTAL, STANDOFFS COMMON TO NR 6 SEAT TRACK IAW SRM 51-42-05-02-01. INSTALLED, 11 TOTAL, STANDOFFS COMMON TO NR 6 SEAT TRACK IAW SRM 51-42-05-02-01. LOCATED AND DRILLED DRIP ANGLE COMMON TO SEAT TRACKS NR 6 AND NR 7, REF SRM 51-40-07-02-01. FINISH RESTORED TO FASTENERS, REF SRM 51-25-10.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

RADOME BULKHEAD, PN 85310146 REQUIRES REPLACEMENT. REMOVED RADOME BULKHEAD, REF SRM 51-42-05-00-01. INSTALLED NEW BULKHEAD SKIN PN 85310146 AT FS X66.00 IAW SRM 51-42-05, SRM 51-42-45 AND DWG:85310011, REV AN. REMOVED ALL STIFFENERS FWD OF RADOME BULKHEAD REF SRM 51-42-05-00-01. INSTALLED ALL STIFFENER COMMON TO BULKHEAD SKIN AT X66.00 MINUS STIFFENER, PN:85311478 IAW SRM 51-42-05 AND DWG:85310011, REV AN. LOCATED AND DRILLED NEW RADOME BULKHEAD REF SRM 51-40-07-02-01. REMOVED FITTING, PN 85312192-003 COMMON TO BULKHEAD X66.00 AND FITTING, PN 85312193-009 IAW SRM 51-42-05. INSTALLED FITTING, PN 85312192-003, COMMON TO BULKHEAD X66.0 AND FITTING, PN 8532193-009, REF SRM 51-42-005-02-01 AND DWG:85310011, REV AN. REMOVED 2 EA CLEAT, PN 85311101-101 COMMON TO FITTING, PN 85312193-003 AND STIFFENER, PN 85311302 IAW SRM 51-42-05. INSTALLED 2EA CLEATS, PN 85311101-101 COMMON TO FITTING, PN 85312193-003 AND STIFFENER, PN 85311302, REF SRM 51-42-05-2-01, 51-42-45-02-01 AND DWG:85310011 REV AN. RESTORED FINISH ON BULKHEAD INSIDE AND OUTSIDE FACE REF SRM 51-25-10-02-01 AND 51-25-25-02-01. INSTALLED STIFFENER, PN 85311478-103 ON FWD BULKHEAD ST X-66.00, REF SRM 51-42-05-02-01. REMOVED AND REINSTALLED BRACKET, PN 85311312-001 IAW SRM 51-42-05. CLARIFICATION STATEMENT FOR ABOVE MAINTENANCE ACTIONS AND CORRECTIVE ACTIONS. RADOME BULKHEAD, PN 85310146 WAS INSTALLED AT FRAME STA X -155.00, NOT X66.00 AS INDICATED ON DWG 85310011, REV AN.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 14 REQUIRES REPLACEMENT, PN 85338210-113. REMOVED FWD SPLICE MEMBERS COMMON TO SEAT TRACK NR 14 REF SRM 51-40-15-02-01. INSTALLED FWD SPLICE MEMBERS COMMON TO SEAT TRACK NR 13 AND NR 14 REF SRM 51-42-05-02-01 AND 51-40-15-02-01. REMOVED AFT SPLICE MEMEBERS COMMON TO SEAT TRACK NR 14, REF SRM 51-40-15-02-01. INSTALLED AFT SPLICE ANGLES INBD AND OTBD ON SEAT TRACK NR 14 AND 15 REF SRM 51-42-05-02-01, 51-40-15-02-01 AND DWG:85338201, REV F. REMOVED 4 BOLTS WHICH FASTEN SEAT TRACK NR 14 TO SUPPORTS AT FS 584.5 AND FS 604.5, Y 9.250, REF SRM 51-40-00-00-01. INSTALLED 4EA BOLTS ON SEAT TRACK NR 14, FS 584.5 AND AT FS 604.5, Y9.250, REF SRM 51-40-00-00-01 AND DWG:85338201, REV F, LOCATED AND DRILLED NEW SEAT TRACK NR 14, PN 85338210-113 REF SRM 51-40-07-02-01. REMOVED SEAT TRACK NR 14 REF SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. INSTALLED SEAT TRACK NR 14 PN 85338210-113, REF SRM 51-42-05-02-01, 51-40-15-02-01, 51-41-00-00-01 AND DWG 85338201, REV F RESTORED FINISH ON SEAT TRACK NR 14 REF SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 13 REQUIRES REPLACEMENT. REMOVED SEAT TRACK, NR 13, REF SRM 51-42-050-02-01 AND 51-41-00-00-01. INSTALLED 36 BOLTS TO SEAT TRACK NR 13, REF SRM 51-41-00-00-01. DISPLACED GROUND CONNECTION 2421-GS18 AND 2421-G519 FROM FS X290.5 AND Y9.250 REF SRM 51-41-00-00-01. CONNECTED GROUND CONNECTION 2421-GS18 AND 2421-GS19 ON FS X290.5 AND Y9.250 REF SRM 51-41-00-00-01. DRILLED HOLES ON NEW SEAT TRACK NR 13 BETWEEN STA X236.0-X301.0 AND X469.50-X564.500 REF SRM 51-40-07-02-01. ATTACHED BUNDLE WIRES TO STAND OFFS 5E ON NEW SEAT TRACK NR 13, REF WM 20-12-10, FIG 201. LOCATED AND DRILLED NEW SEAT TRACK NR 13, PN 85361510-104, REF SRM 51-40-07. LOCATED AND DRILLED DRIP ANGLE COMMON TO SEAT TRACK NR 12 AND NR 13 ONTO NEW SEAT TRACK NR 13. REF SRM 51-42-05, FS 234.40, FS 301. INSTALLED RIVETS COMMON TO WEB AND SEAT RAIL REF SRM 51-42-05, DWG:85361501, REV E. BONDING CHECK GOOD ON GROUND CONNECTION 2421, GS1B REF AMM 51-80-00-760-830 TABLE 7, FIG 299.17. FINISH RESTORED TO FASTENER HEADS AND BUCK TAILS REF SRM 51-25-10.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

LOWER TCAS ANTENNA EXTERIOR DOUBLER IS CORRODED. REMOVED LOWER TCAS ANTENNA EXTERIOR DOUBLER, PN 85314193-103, REF SRM 51-42-05-02-01. INSTALLED NEW LOWER TCAS ANTENNA EXTERIOR DOUBLER, PN QX85314193-103, REF SRM 51-42-05-02-01 AND DWG:85310015, REV I. NO PITTING IS ALLOWED IAW SRM 51-21-00 AND NO REPAIRS ALLOWED IAW SRM 53-10-31, EXTERIOR DOUBLER IS OUT OF LIMITS, REPLACE, PN 85314193-103. LOCATED AND DRILLED LOWER TCAS ANTENNA EXTERIOR DOUBLER REF SRM 51-40-07-02-01 AND DWG: 85310015, REV J. FILLET SEALED PERIPHERY OF EXTERIOR DOUBLER REF DWG:85310015, REV J. APPLIED TOP COAT TO LOWER TCAS ANTENNA EXTERIOR DOUBLER REF SRM 51-25-05, PG 206-207, ITEM F1-F4.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 5, PN 85328210-109 REQUIRES REPLACEMENT. REMOVED CABLE TIES FROM WIRE HARNESS ATTACH TO TRACK NR 5 AT THE FOLLOWING LOCATION; 1 AT FS 9, 4 AT FS 35-39, 2 AT FS 75, 4 AT FS 81-84, REF WM 20-12-10-21. INSTALLED CABLE TIES TO SECURE WIRE HARNESSES TO TRACK NR 5 AT THE FOLLOWING LOCATIONS: 1 AT FS 9, 4 AT FS 35-39, 2 AT FS 75, 4 AT FS 81-84, REF WM 20-12-10-201. REMOVED 2 FASTENERS COMMON TO TRACK NR 5 AND SUPPORT BRACKET AT FS 61, Y-9.250, REF SRM 51-42-05-02-01. INSTALLED 2 FASTENERS COMMON TO NEW TRACK, NR 5 AND SUPPORT BRACKET AT FS 61, Y-9.250 REF SRM 51-42-05-002-01. REMOVED AFT SPLICE MEMBERS COMMON TO TRACK NR 5 AND NR 6, REF SRM 51-42-05-002-01, 51-40-15-02-01. INSTALLED AFT SPLICE MEMBERS COMMON TO SEAT TRACKS NR 5 AND NR 6, REF SRM 51-42-05-2-001 AND 51-40-15-02-01. REMOVED WIRE HARNESS SUPPORT ANGLE COMMON TO SEAT TRACK NR 5 AND 6 FS, 97 TO 108, Y-9.250, 5 FASTENERS, REF SRM 51-42-05-2-01. INSTALLED WIRE SUPPORT ANGLE COMMON TO SEAT TRACK NR 5 AND NR 6, FS X97.0 Y-9.250 5 EA FASTENERS REF SRM 51-42-05-02-10. REMOVED 11 CABLE TIE MOUNTS FROM TRACK NR 5 AT LOCATIONS STATED IN ITEM 4, REF SRM 51-42-05-02-01. INSTALLED 11 CABLE TIE MOUNTS TO NEW TRACK NR 5 AT LOCATIONS STATED IN ITEM 4, REF SRM 51-42-05-02-01. LOCATED AND DRILLED NEW SEAT TRACK NR 5, PN 85328210-109, REF SRM 51-40-07-02-01. COMPLETED, LOCATION AND DRILL OF NEW TRACK NR 5 AT Y-9.250 AND FS-39 VERTICAL STIFFENER, REF SRM 51-40-07-02-01. PERFORMED BONDING CHECK ON NR 5 SEAT TRACK, CHECK FOUND GOOD IAW AMM 51-80-00-760-831.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

DRIP ANGLE COMMON TO SEAT TRACK NR 5 AND NR 6 REQUIRE REPLACEMENT, PN 85307495-111, FS 49.5-FS 156, Y-9.250. REMOVED DAMAGED DRIP ANGLE COMMON TO SEAT TRACK NR 5 AND NR 6 REF SRM 51-42-05-02-01. INSTALLED NEW DRIP ANGLE, PN 85307445-111 AT FS X 49.5 TO FS X 156.0 -4 -9,250, REF SRM 51-42-05-02-01. LOCATED AND DRILLED DRIP ANGLE, PN 85307495-111 AT SEAT TRACK NR 5 AND NR 6 IAW SRM 51-40-07-02-01 AND DWG 85307401, REV C, SRM 51-40-07-02-1 AND DWG: 85307401, REV C, SRM 51-42-05-02-01, 51-40-15-02-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 12, PN 85328210-112 REQUIRES REPLACEMENT. REMOVED SPLICE MEMBERS COMMON TO SEAT TRACKS 11 & 12, REF SRM 51-42-05, 51-40-15. INSTALLED SPLICE MEMBERS COMMON TO SEAT TRACKS NR 11 AND NR 12, REF SRM 51-42-05, 51-40-15 AND DWG 85328201, REV D. LOCATED AND DRILLED INBD AND OTBD SPLICES COMMON TO SEAT TRACK NR 11 AND NR 12 ONLY ON SEAT TRACK NR 11 SIDE REF SRM 51-40-07-2-01. DRILLED AND DEBURRED COMPLETE INBD AND OTBD NEW SPLICES COMMON TO SEAT TRACK NR 11 AND NR 12, REF SRM 51-40-07-02-01. REMOVED DRIP ANGLE, DRIP SILL, FROM SEAT TRACK NR 12 FS 162-290, REF SRM 51-42-05, 51-40-15 COMMON TO SEAT TRACK 12 & 13. LOCATED AND DRILLED, COUNTERSUNK AS WELL, DRIP ANGLE, DRIP SILL, REMAINING HOLES ON TO SEAT TRACK NR 12, REF SRM 51-40-07, 51-42-05 COUNTERSINKING, JOB 5415331, OPS NR 242 FOR DRIP ANGLE INSTALLATION, PN 85307495-114. DISPLACED ANVC ACCELEROMETER AT STA X204.00, REF AMM 23-35-51-000-801. INSTALLED DISPLACED ANVC ACCELEROMETER BACK ONTO SEAT TRACK NR 12 AT STA X 204.000 REF AMM 23-35-51-400-801. REMOVED SEAT TRACK NR 12, REF SRM 51-41-00-00-01. INSTALLED SEAT TRACK NR 12 REF SRM 51-41-00, 51-42-05, 51-40-15 AND DWG 85328201, REV D. LOCATED, DRILLED AND DEBURRED NEW SEAT TRACK NR 12, PN 85328210-112, PO TX 00004770, REF SRM 51-40-07-02-01.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

STIFFENER, PN 85311302-109 HAS BLOWN OUT HOLES. REMOVED STIFFENER, REF SRM 51-42-05-00-01. INSTALLED NEW STIFFENER BULKHEAD, PN 85311302-109 IAW SRM 51-42-05 AND DWG 85310011, REV-AN. LOCATED AND DRILLED NEW STIFFENER REF SRM 51-40-07-02-01.

Part: PLATE — CORRODED (TCAS) · airframe 22,224 hrs · 23,703 cycles

LOWER TCAS ANTENNA ADAPTER PLATE CORRODED, MARKED. REMOVED LOWER TCAS ANTENNA, BOTTOM PLATFORM, PN 85335262-105, REF SRM 51-42-05-02-01. INSTALLED LOWER TCAS ANTENNA BOTTOM PLATFORM, PN 85335262-105, REF SRM 51-42-05-02-01 AND DWG 85310015, REV J, DATED JULY 2ND, 2015. REMOVED MOISTURE DAM, PN 85334915-001, REF SRM 51-42-05-02-01. INSTALLED MOISTURE DAM, PN 85334915-001, REF SRM 51-42-05-02-01 AND DWG 85310015, REV J, DATED JULY 2ND, 2015. NO PITTING IS ALLOWED IAW SRM 51-21-00 AND NO REPAIRS ALLOWED IAW SRM 53-10-31. BOTTOM PLATFORM, PN 85335262-105 IS OUT OF LIMITS, REPLACE. COMPLIED WITH FORM M-184. LOCATED AND DRILLED BOTTOM PLATFORM, PN 85335262-105, REF SRM 51-40-07-02-01 AND DWG 85310015, REV J, DATED JULY 2ND, 2015. APPLIED FILLET SEAL OUTSIDE PERIPHERY OF BOTTOM PLATFORM, INSIDE CUT OUT EDGE AND INSIDE/OUTSIDE PERIPHERY OF MOISTURE DAM REF DWG 85310015, REV J, DATED JULY 2ND, 2015.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 8 REQUIRES REPLACEMENT, PN 85338210-109. REMOVED SPLICE COMMON TO SEAT TRACK NR 8 AND NR 9, REF SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED SPLICE INBD AND OTBD COMMON TO SEAT TRACK NR 8 AND NR 9, REF SRM 51-42-05-02-01, STEP 4D, 3-10, AND SRM 51-40-15-002-01, STEP 6H2. REMOVED SEAT TRACK NR 8, REF SRM 51-41-00-00-01 AND 51-42-05-02-01. INSTALLED NEW SEAT TRACK NR 8, REF SRM 51-41-00-00-01A AND 51-42-05-02-01, STEP 4D,3-10. LOCATED, DRILLED AND DEBURRED NEW SEAT TRACK NR 8, PN 85338210-109, PO:TX-4965, REF SRM 51-40-07-02-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 15 REQUIRES REPLACEMENT. REMOVED SPLICE MEMBERS COMMON TO SEAT TRACKS NR 14 AND NR 15. REMOVED SPLICE MEMBERS COMMON TO SEAT TRACKS NR 15 AND NR 16. INSTALLED SPLICE MEMBERS COMMON TO, NEW, SEAT TRACK NR 15 AND SEAT TRACK NR 16 REF SRM 51-40-15-02-01, AND DWG 85338201. REMOVED 29 RIVETS COMMON TO SEAT TRACK NR 15 AND VERTICAL WEB BETWEEN FS 644 AND FS667, Y9.250. INSTALLED 29 FASTENERS COMMON TO NEW SEAT TRACK NR 15 AND VERTICAL WEB BETWEEN FS 644 AND FS 677, Y9.250, REF SRM 51-42-05-02-01. REMOVED 6 BOLTS, NAS 6204-3 WHICH FASTEN SEAT TRACK NR 15 TO SUPPORTS AT FS 624, FS 644, AND FS 664, Y9.250. INSTALLED 6 BOLTS WHICH FASTEN SEAT TRACK NR 15 TO SUPPORTS AT FS 624, FS 644 AND FS664, Y9.250, REF SRM 51-41-00-00-01. LOCATED AND DRILLED FASTENER HOLES FOR SPLICE MEMBERS COMMON TO SEAT TRACK NR 15 AT FS 612, Y9.250 REF SRM 51-40-07-02-01. LOCATED AND DRILLED FASTENER HOLES FOR SPLICE MEMBERS COMMON TO SEAT TRACK NR 15 AT FS 670, Y9.250, REF SRM 51-40-07-02-01. LOCATED AND DRILLED 6 X0.250" DIA FASTENER HOLES COMMON TO SEAT TRACK NR 15 AT FS624, FS644, AND FS664 REF SRM 51-40-07-02-01. LOCATED AND DRILLED 29 RIVET HOLES COMMON TO SEAT TRACK NR 15 AND VERTICAL WEB BETWEEN FS 644 AND 667, Y9.250 REF SRM 51-40-07-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

REPLACE SEAT TRACK NR 10. REMOVED SPLICE ANGLES, PN: 85338215-101 AND PN: 85338216-101 AT FS X 10.5 SEAT RAIL NR 10 IAW SRM 51-40-15 AND 51-42-05. INSTALLED SPLICE ANGLES INBD AND OTBD AT FS X 1.5 REF SRM 51-42-05-02-01, STEP 4D, 3-10 AND SRM 51-40-15-02-01, STEP 6, NR 2. REMOVED SEAT TRACK NR 10 IAW SRM 51-40-15, 51-41-05 AND 51-42-05. INSTALLED 4 EA BOLTS ON SEAT TRACK NR 10 REF SRM 51-41-00-00-01. REMOVED WIRE BUNDLES BRACKET AT FS X 10.5 COMMON TO TRACK NR 10, PN: 85307835-015 IAW SRM 51-42-05. INSTALLED WRIE BUNDLE BRACKET BACK ONTO ACFT AT FS X 10.5 COMMON TO SEAT TRACK NR 10 PN: 85307835-05 REF SRM 51-42-05. LOCATED AND DRILLED NR 10 SEAT TRACK REF SRM 51-40-07. ZIP TIED WIRE BUNDLES, 5 PLACES, BACK ONTO WIRE BUNDLE STAND OFFS ON SEAT TRACK NR 10 REF SRM 20-12-10. INSTALLED SEAT TRACK NR 10 COMPLETELY. BONDING CHECK WAS GOOD REF AMM 51-80-00, TABLE 8, PG 299-308, SRM 51-42-05, 51-23-00, 51-40-15 AND DWG: 85328201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

SEAT TRACK NR 11 REQUIRES REPLACEMENT. REMOVED DRIP TRAY, PN:82570105-102 COMMON TO SEAT TRACK NR 11-13 IAW SRM 51-41-05. JOB 5415331, OPS 242 FOR THE COMPLETION OF THIS TASK. REMOVED SEAT TRACK SILL, PN:85307495-112, COMMON TO SEAT TRACK NR 11 AND NR 12 IAW SRM 51-2-05. REMOVED 7 WIRE BUNDLE ZIPTIES COMMON TO SEAT TRACK NR 11, REF SRM 51-41-00, 20-12-10. INSTALLED 7 WIRE BUNDLE ZIPTIES BACK ONTO ACFT COMMON TO SEAT TRACK NR 11 REF SRM 20-12-10. REMOVED SEAT TRACK NR 11 REF SRM 51-42-05, 51-41-00, 51-40-15. INSTALLED 10 EA BOLTS ON SEAT TRACK NR 11 REF SRM 51-41-00-00-01. LOCATED AND DRILLED NEW SEAT TRACK PN: 85328210-115, PO:TX-5244 REF SRM 51-40-07-02-01. INSTALLED SEAT TRACK NR 11 REF SRM 51-2-05, 20-12-10 AND DWG: 85328210 REV E, LOCATED AND DRILLED EXISTING DRIP ANGLE "DRIP SILL" TO NEW NR 11 SEAT TRACK REF SRM 51-40-07. CLARIFICATION STATEMENT: CAPTURE C/A FOR M/A ITEM NR 2. INSTALLED SEAT TRACK DRIP ANGLE, DRIP SILL, PN:85307495-112 COMMON TO SEAT TRACK NR 11 AND NR 12 REF SRM 51-42-05.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

FOUND CORROSION ON THRESHOLD PLATE, PN 85329539-001 AT FWD PAX DOOR. LOCATED AND TRANSFERRED HOLES TO NEW PART THRESHOLD PLATE, PN 85329539-001 IAW SRM 51-42-05-02-01 AND DWG 85329539, REV 96/05/21. INSTALLED RUBBING PAD, PN 85329538 NEW PART AT THRESHOLD PLATE IAW SRM 51-42-05-02-01 AND DWG 85329532, REV 96/05/21. OP 132 FOR INSTALLATION. COMPLIED WITH FORM M-184.

Part: THRESHOLD — NOT REPORTED (FUSELAGE) · airframe 22,224 hrs · 23,703 cycles

COMPLY WITH HORIZON TASK CARD 6-53-1160, AFT PASSENGER DOOR FLT, REMOVED STAINLESS SILL, THRESHOLD PLATE, INNER REF SRM 51-40-00, PN 85-339540-103. INSTALLED STAINLESS SILL, THRESHOLD PLATE AT AFT PASSENGER DOOR. REF SRM 51-41-00 THRESHOLD PLATE, PN 85339540-103. REMOVED SCUFF/THRESHOLD PLATE STAINLESS, OUTER, REF SRM 51-40-00, PN 85339549-101. INSTALLED SCUFF PLATE, PN 85339549-101 AT PASSENGER DOOR LOWER SURROUND REF SRM 51-41-00. REMOVED INNER EDGE BEAM/CHANNEL REF SRM 51-42-90, 51-40-15, 51-42-05, PN 85339512-101. INSTALLED INNER EDGE BEAM CHANNEL, PN 85339512-101 REF SRM 51-42-90, SRM 51-42-15, 51-42-05, AND DWG 85339541, RELEASE PREV B DATED 02/11/26. INSTALLED NEW EDGE BEAM. REMOVED OUTER EDGE BEAM/CHANNEL REF SRM 51-42-05, PN 85339542-101. INSTALLED OUTER EDGE BEAM CHANNEL, PN 85339542-101 AT AFT PASSENGER DOOR LOWER SURROUND REF SRM 51-42-05 AND DWG 85339541, RELEASE PREV B DATED 2/11/26. OK TO CLOSE INNER EDGE CHANNEL, PN 85339512-101 AFTER APPLICATION OF SELF-LEVELING GREEN COMPOUND BETWEEN X697.600 AND X669.300, STRINGER 23P TO 24P IAW NR IS 4Q5100004, REV B, DATED 25TH MARCH 2011.

Part: BEAM — CORRODED (PAX DOOR) · airframe 22,224 hrs · 23,703 cycles

INNER EDGE BEAM CORRODED PN 85339512-101, NEEDS REPLACEMENT. LOCATED AND DRILLED NEW INNER EDGE BEAM, PN 85339512-101, REF SRM 51-40-07-02-01. APPLIED ALUMINIZE TOP COAT TO INNER EDGE BEAM, REF SRM 51-25-02-01. INSTALLED 12 EA NUTPLATES WET, HT3326-5FR ON NEW INNER EDGE BEAM REF SRM 51-42-05-02-01 AND TASK CARD 6-53-1160-AFT PASSENGER DOOR, FLT ITEM NR 5 COMPLIED WITH FORM M-184.

Part: SPAR — GOUGED (RUDDER) · airframe 21,566 hrs · 23,028 cycles

TRAILING RUDDER FRONT SPAR AT LOWER MAIN HINGE HAS GOUGED. REPAIRED IAW RD 8/4-55-1221, ISSUE 2. NO DEFECTS NOTED.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS) · airframe 21,382 hrs · 22,828 cycles

EMERGENCY LIGHT BATTERY POSITION 2 INTERMITTENT. REPLACED BATTERY PACKS IAW AMM 33-51-00-820-801. CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 BLEED) · airframe 21,333 hrs · 22,782 cycles

NR 1 BLEED HOT ILLUMINATED IN FLIGHT, DIVERTED, UNEVENTFUL LANDING. ACCOMPLISHED FSM BLEED HOT RESET PROCUDURE RESET SUCCESSFULL BLEED HOT CAUTION DID NOT ILLUMINATE. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 21,228 hrs · 22,664 cycles

FLOOR PATH LIGHTING STRIP AT ROW 1 LOOSE. RE-INSTALLED FLOOR PATH STRIP IAW AMM TASK 33-51-16-400-801. RETURNED TO SERVICE.

Part: CONNECTOR — ARCED · airframe 21,138 hrs · 22,547 cycles

FOUND CONNECTOR PLUG 2421-P5 AT RACCB WIRES AND PLUG HAVE ARCING DAMAGE. ALL WIRES PINS A THRU F ARE DAMAGED. REMOVED DAMAGED WIRES BY RETERMINATING PIN A THRU F. REPLACED CONNECTOR PLUG 2421-P5 IAW WM 20-17-19-401. CONTINUITY CHECKS GOOD IAW WD 24-21-00 AND 30-61-00, T/E 3542 12/17/15. CW OPS TEST OF AC GEN SYS 24-21-00-710-801,WINDSHIELD AND SIDE WINDOW HEAT 30-41-00-710-802, ICE DETECT 30-80-00-710-801, PITOT HEAT 30-30-00-710-801, ENGINE LIP HEAT 30-21-00-710-801, DRAIN MAST 38-32-00-710-801, PROP DEICE 30-61-00-720-801, SPU 29-11-36-710-801. MAPCO'S AND AOA VANES ARE HOT WITH AC ON. ALL OPS TEST GOOD. INCLUDED ABOVE FUEL AUXILIARY PUMPS OPS CK GOOD IAW AMM 28-27-31-710-801.

Part: BULB — WRONG PART (LIGHT) · airframe 20,953 hrs · 22,345 cycles

ELECTRICAL ODOR IN THE AFT CARGO COMPARTMENT ON THE GROUND. FOUND LIGHT IN COMPARTMENT TO HAVE HIGH WATTAGE NR 1683 BULB INSTALLED. REPLACED WITH LOW WATTAGE NR 305. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 20,825 hrs · 22,211 cycles

FORWARD EMERGENCY LIGHT STRIP AT ROW 1 CAME OFF. SECURED FLOOR STRIP. RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 20,820 hrs · 22,206 cycles

FLOOR PATH STRIP AT ROW 1 IS LOOSE. REPLACED FLOOR PATH STRIP. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (BRAKE SYSTEM) · airframe 20,587 hrs · 21,962 cycles

ON LANDING, BRAKES INEFFECTIVE. INTERROGATED CDS ANTI-SKID SYS, NO CURRENT FAULTS. IN HISTORY, FOUND ASC PAST FAULTS RT INBD WST LEG 0, RT INBD WST LEG 14. REPLACED RT INBD WST NR 3. REMOVED IAW AMM TASK 32-46-11-000-801. INSTALLED IAW TASK 32-46-11-400, PAR 1-5A, B, & D. PERFORMED FUNCTIONAL TEST OF MLG BRAKE SYS, FUNCTIONAL TEST GOOD. RETURNED TO SERVICE.

Part: LIGHT — DETACHED (ROW 1) · airframe 19,925 hrs · 21,268 cycles

EMERGENCY LIGHTING STRIP IS LOOSE AT ROW 1. ATTACHED LIGHT STRIP. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,643 hrs · 20,966 cycles

F/A EMERGENCY LIGHT SWITCH IS INOPERATIVE FOR THE "NORMAL" POSITION. RELAMPED AS REQUIRED. OPS CHECKS GOOD.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHT) · airframe 19,072 hrs · 20,367 cycles

EMERGENCY LIGHT BATTERY PACK 3 INTERMITTENT. REPLACED BATTERY PACK IAW AMM TASKS 33-51-01-000-801 & 33-51-01-400-801. CHECKS GOOD.

Part: LATCH — INOPERATIVE (ZONE 200) · airframe 18,666 hrs · 19,948 cycles

FWD F/A EMERGENCY COMPARTMENT, BELOW FA JUMP SEAT, WILL NOT OPEN WITH ONLY 1 LATCH. R & R FWD EMERGENCY COMPARTMENT DOOR LATCH ASSY. NO OTHER DEFECTS NOTED. OPS TEST GOOD. RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (AUTO LAND) · airframe 17,991 hrs · 19,218 cycles

LANDING MODE FAILED TO ARM FOR 2 LOW VISIBILITY APPROACHES. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING.

Part: LIGHT — DELAMINATED (CABIN) · airframe 17,342 hrs · 18,530 cycles

EMERGENCY LIGHT ASSY AT ROW 2AB DELAMINATED. REPLACED LIGHT IAW AMM 33-51-16-400-801.

Part: CONTROLLER — NO TEST (ZONE 400) · airframe 17,153 hrs · 18,342 cycles

AUTOFEATHER TEST FAILED FOR NR 2 ENGINE. COMPLIED WITH FIM TASK TASK 61-20-00-810-805. FOUND FAULTS 398, 404, 280, 282, 398 AND 70 ON NR 2 PEC. R & R NR 2 PEC IAW AMM 61-20-36-000-801/-400-801. C/W MAINTENANCE 671008. ALL OPS CHECKS GOOD. C/W OPS TEST OF AUTOFEATHER AND UPTRIM IAW AMM 61-20-00-710-801 AND MCN 661292-001. CHECKS GOOD. NO FAULTS IN CDS. NO FURTHER DEFECTS NOTED.

Part: AUTOFEATHER SYS — NO TEST · airframe 17,146 hrs · 18,336 cycles

AUTOFEATHER TEST FAILED. CDS FAULT CODE IS NR 1 ENG 398. COMPLIED WITH FIM 61-20-08-810-818. R & R NR 1 PEC IAW AMM 61-20-36-000-801, 61-20-36-400-801.

Part: HOSE — CHAFED (ZONE 200) · airframe 16,962 hrs · 18,113 cycles

DURING CRUISE, AT FL 230 NOTICED A/S SPLIT BETWEEN STANDBY ATT INDICATOR AIRSPEED AND PILOT'S & CO-PILOT'S AIRSPEED. BOTH PFD'S SHOWED 240 KNOTS, STANDBY SHOWED 271 KNOTS. SPLIT DECREASED WITH ALTITUDE, ALL INDICATIONS MATCHED AT 8000'. ON FINAL APPROACH, PFD 1 & 2 SHOWED AIRSPEEDS APROXIMATELY 5-6 KNOTS FASTER THAN STANDBY AIRSPEED. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED ISI, INSPECTED TUBING. FOUND PITOT FLEX LINE CHAFED BETWEEN BEHIND INSTRUMENT. R & R PITOT LINE, COMPLIED WITH NITROGEN PURGE OF ALL PITOT AND STATIC LINES AND COMPLIED WITH PITOT STATIC LEAK CHECK IAW MM 34-12-16-000-801, 34-12-16-400-801, & 34-11-00-170-801. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,796 hrs · 17,933 cycles

FORWARD F/A EMERGENCY LIGHTS SWITCH BACKLIGHT INOPERATIVE, REPLACED LAMP. CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: THRESHOLD — OUT OF TOLERANCE (PAX DOORWAY) · airframe 16,454 hrs · 17,580 cycles

MAIN CABIN DOOR HANDLE MAKING UNUSUAL POPPING SOUND WHEN OPENING. FOUND BOTTOM OF DOOR CATCHING ON AIRSTAIR DOOR, SURROUND THRESHOLD AND TEFLON RUB PAD. TRIMMED THRESHOLD AND RUB PAD TO FIT ACFT KEEPING WITHIN LIMITS OF SRM 51-42-00-00-01. APPLIED ALODINE TO TRIMMED AREA IAW AMM 51-25-01-390-801 AND PRIMED IAW AMM 51-25-01-390-801. OPS TEST OF FWD PASSENGER DOOR IAW AMM 52-11-00-710-802. CHECKED GOOD. POPPING NOISE NO LONGER NOTED. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 16,385 hrs · 17,513 cycles

LOWER SILL PLATE IN FORWARD CARGO DOOR CUTOUT CORRODED. INSTALLED FABRICATED SILL IAW SRM 51-42-05, STEP 4,D.

Part: PLATE — CORRODED (PAX DOOR) · airframe 16,385 hrs · 17,513 cycles

CORROSION FOUND ON BOTH FWD AND AFT BACKING PLATES OF THE AIRSTAIR DOOR. R & R FWD AND AFT BACKING PLATES IAW AMM 20-10-01-430-801 & 51-23-00390-801. RESTORED FINISH TO FWD AND AFT BACKING PLATES, IAW SRM 51-25-05.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 16,385 hrs · 17,513 cycles

FWD PAX DOOR INTERCOSTAL, HAS CORROSION ON AFT SIDE APPROX .5 FROM FRAME. DRILLED A .159" HOLE TO REMOVE CORROSION PIT IAW SRM 51-40-07. INTERCOSTAL TO BE REPLACED IAW TASK CARD 6-53-1160 FWD PAX DRINSVR ITEM 9. REMOVED INTERCOSTAL, PN 85329342-105 IAW SRM 51-42-05 & SRM 51-40-15. INSTALLED INTERCOSTAL, PN 85329342-105 RIVETS AND HI LITE FASTENERS IAW SRM 51-42-05 & SRM 51-40-15. FIT AND DRILLED NEW INTERCOSTAL, PN 85329342-105 IAW SRM 51-40-07. COMPLIED WITH FORM M-184. COMPLETED INSTALLATION OF INTERCOSTAL IAW AMM TASK 20-10-01-430-801, PAR 6E, TABLE 1 & TABLE 3.

Part: CHANNEL — CORRODED (THRESHOLD) · airframe 16,385 hrs · 17,513 cycles

FWD PAX DOOR THRESHOLD CHANNEL CORRODED. REMOVED AND REPLACED CHANNEL IAW SRM 51-42-05.

Part: BEAM — CORRODED (EMEGENCY EXIT) · airframe 16,385 hrs · 17,513 cycles

EMERGENCY EXIT DOOR THRESHOLD HAS SEVERE CORROSION ON EDGE BEAM. REMOVED CORRODED EDGE BEAM IAW SRM'S 51-42-05, STEP 4.E, 51-42-45 STEP 6H. CORROSION BEYOND ALLOWABLE LIMITS IAW TASK 6-53-1160. INSTALLED NEW EDGE BEAM IAW SRM 51-42-05 PROCEDURE 4-D (3-10) AND SRM 51-42-45 STEPS 1-6 A-G.

Part: PIVOT — GOUGED (SERVICE DOOR) · airframe 16,385 hrs · 17,513 cycles

AFT SERVICE DOOR PIVOT ASSY STUD GOUGED. REMOVED PIVOT ASSY STUD IAW AMM 52-41-01-000-801. INSTALLED NEW PIVOT ASSY STUD AMM 52-41-06-400-801, STEP 4 B.

Part: SEAT TRACK — CORRODED (NR 11) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK, NR 11, CORROSION WAS FOUND BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-10/ 51-42-05. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, STEP 4 D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 16,385 hrs · 17,513 cycles

FWD PAX DOOR RIB TO LONGERON ATTACH ANGLES ARE CORRODED. REMOVE ATTACH ANGLES IAW SRM 51-42-05. INSTALLED NEW ATTACH ANGLES IAW SRM 51-42-05 AND SRM 51-40-15.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

ACCESS PANEL 621BT CORRODED IN COUNTER SINKS. REMOVED CORROSION IAW SRM 57-10-35. FOUND WITHIN LIMITS . NDT IAW NDTM 51-00-06. NO DEFECTS.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

ACCESS PANEL 623AT CORRODED ON COUNTER SINKS. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 57-10-35, REPAIR 3, FIG 201. INSTALLED NEW ACCESS PANEL.

Part: SKIN — CORRODED (LT WING) · airframe 16,385 hrs · 17,513 cycles

LEFT WING FUEL PANEL 524AT ACCESS HOLE MATING SURFACE LANDING HAS CORROSION ON INBD AND OTBD ENDS. REMOVED CORROSION IAW SRM 57-20-35, STEP 7A(1)-(3). FOUND WITHIN LIMITS IAW SRM 57-20-35 FIG 201 & DWG NR 85714201.

Part: SKIN — CORRODED (RT WING) · airframe 16,385 hrs · 17,513 cycles

RIGHT WING FUEL PANEL 624AT ACCESS HOLE MATING SURFACE LANDING HAS CORROSION ON INBD AND OTBD ENDS. REMOVED CORROSION IAW SRM 57-20-35, STEP 7A 1-3. ET INSP REF NDTM, PT 1, 51-00-06. NO DEFECTS NOTED IN BLENDED AREAS. SKIN WITHIN LIMITS IAW SRM 57-20-35, FIG 201 & DWG 85714201.

Part: SEAT TRACK — CORRODED · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 10 CORRODED. REMOVED SEAT TRACK IAW SRM 51-42-05, STEP 4E AND INSTALLED NEW IAW SRM 51-42-05, SRM 51-40-15 AND SRM 51-41-00.

Part: SILL — CORRODED (AFT PAX DOORWAY) · airframe 16,385 hrs · 17,513 cycles

AFT PAX DOOR LOWER SILL IN FUSELAGE DOOR CUTOUT HAS CORROSION.

Part: CHANNEL — CORRODED (DOOR FRAME) · airframe 16,385 hrs · 17,513 cycles

AFT PAX DOOR CUTOUT EDGE CHANNEL, FOUND CORRODED. REMOVED AND REPLACED EDGE CHANNEL, IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 71-94) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 5 IS CORRODED. BLENDED SEAT TRACK AT BS 71.2-94.8 IAW SRM 53-20-49, FIG.201. FOUND OUT OF LIMITS IAW SRM 53-20-49. SEAT TRACK NR 5 REPLACED.

Part: BEAM — CORRODED · airframe 16,385 hrs · 17,513 cycles

EVIDENCE OF CORROSION FOUND ON INNER EDGE BEAM. REMOVED INNER EDGE BEAM IAW SRM 51-42-05, STEP 4E AND 51-42-90. INSTALLED EDGE IAW SRM 51-40-07, STPE 5 AND SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 606-612) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 14 HAS AREA OF PITTING. BLENDED SEAT TRACK 14, FS 606-612 CENTER RT SRM 53-20-49, FIG 1. EVALUATED BLEND AT SEAT TRACK 14 RT CENTER, FS 606-612 RT CENTER , MATERIAL REMOVED TOP PORTION IS .010", ORIGINAL THICKNESS IS .460" MATERIAL REMOVE INSIDE CLAW PORTION IS .015", ORIGINAL MATERIAL IS .200" FOUND WITHIN IN LIMITS, REF SRM 53-20-49. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH, REF SRM 51-21-10.

Part: LENS — DAMAGED (EXTERIOR LIGHT) · airframe 16,385 hrs · 17,513 cycles

LEADING EDGE LIGHT LENS HARDWARE IS CORRODED. REPLACED FLARE LIGHT RETAINER ASSY HARDWARE ON L/E IAW AMM 33-41-01-400-802, STEPS 4.A, 13 & 14. REPLACED APPROACH LIGHT RETAINER ASSY HARDWARE IAW AMM 33-41-01-400-801, STEPS 4.A 13-14.

Part: SEAT TRACK — CORRODED (BS 612-620) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK, NR 15 IS PITTED. BLENDED SEAT TRACK 15, FS 612-620, RT CENTER REF SRM 53-20-49 FIG 1. EVALUATED BLEND AT SEAT TRACK 15 RT CENTER MATERIAL REMOVED ON TOP PORTION OF CLAW IS .009". ORIGINAL THICKNESS .460" FOUND WITHIN LIMITS REF SRM 53-20-49. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH, SRM 51-21-10.

Part: BEAM — CORRODED · airframe 16,385 hrs · 17,513 cycles

OUTER EDGE BEAM CORRODED. REMOVED AND REPLACED OUTER EDGE BEAM ON AFT SERVICE DOOR CUTOUT IAW SRM 51-42-05, STEP 4E.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

FUEL PANEL 524AT HAS CORROSION ON MATING SURFACE. REMOVED DAMAGE AT MARKED AREA ON PANEL 524AT MATING SURFACE, REF SRM 57-20-35. PERFORMED E/T AND U/T INSP ON PANEL 524AT BLEND OUTS IAW NDTM 51-00-04 AND 51-00-06 THICKNESS IS .118-.128. NO DEFECTS NOTED. RESTORED FINISH ON FUEL PANEL 524AT IAW SRM 57-20-35, STEP 7A, ITEMS 5 & 7. REMAINING MATERIAL THICKNESS OF FUEL PANEL 524AT AT BLEND AREAS IS .118-.128 IAW NDT REPORT, MINIMUM ALLOWABLE IS .105 IAW SRM 57-20-35. PANEL 524AT WITHIN ALLOWABLE LIMITS.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

FUEL PANEL 521AT HAS CORROSION AND PITTING ON COUNTERSINKS. REMOVED DAMAGE ON PANEL 521AT COUNTERSINKS, ALL HOLES WITHIN LIMITS, REF SRM 57-10-35. COUNTERSINKS AT .643 ALLOWED .650". PERFORMED E/T INSP ON PANEL 521AT COUNTERSINK BLENDOUTS IAW NDTM 51-00-06, NO DEFECTS NOTED. RESTORED FINISH ON FUEL PANEL 521AT IAW SRM 57-10-35, STEP 6A, ITEMS 4 & 5.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

FUEL PANEL 522CT HAS CORROSION AND PITTING ON COUNTER SINKS. REMOVED DAMAGED ON PANEL 522CT COUNTERSINKS ALL HOLES WITHIN LIMITS, REF SRM 57-10-35, PG 202. COUNTERSINKS AT .626 ALLOWED .656. PERFORMED E/T INSP ON PANEL 522CT COUNTERSINK BLENDOUTS IAW NDTM 51-00-06 NO DEFECTS NOTED. RESTORED FINISH ON FUEL PANEL 522CT IAW SRM 57-10-35, STEP 6A, ITEMS 4 & 5.

Part: ACCESS PANEL — CORRODED (WING) · airframe 16,385 hrs · 17,513 cycles

FUEL PANEL 521AT HAS CORROSION AND PITTING ON COUNTER SINKS. REMOVED DAMAGE ON PANEL 521BT COUNTERSINKS, ALL HOLES WITHIN LIMITS REF SRM 57-10-35, PG 202. COUNTERSINKS AT .632" ALLOWED .650". PERFORMED E/T INSP. ON PANEL 521BT COUNTERSINK BLENDOUTS IAW NDTM 51-00-06. NO DEFECTS NOTED NDT REPORT ATTACHED. RETORED FINISH ON FUEL PANEL 521BT IAW SRM 57-10-35, STEP 6A, ITEMS 4 & 5.

Part: SKIN — CORRODED (BS 321-337) · airframe 16,385 hrs · 17,513 cycles

LT FUSELAGE SKIN, BS 321 - 337, LOCATED 18 CORRODED RIVETS ON STR 24P. REMOVED 18 RIVETS FROM LT FUSELAGE SKIN, FSX321 TO X337 STR24P IAW SRM 51-42-05. INSTALLED 18 RIVETS INTO LT FUSELAGE SKIN FSX321 TO X337, STR 24P IAW SRM 51-42-05. RESTORED FINISH IAW SRM 51-25-10.

Part: FITTING — CORRODED (BULKHEAD) · airframe 16,385 hrs · 17,513 cycles

CORROSION ON BULKHEAD BOTTOM FITTING. R & R CORRODED FITTING IAW SRM 51-22-35, STEPS 1 THRU 6, PAGES 201 THRU 203.

Part: SEAT TRACK — CORRODED (BS 229-571) · airframe 16,385 hrs · 17,513 cycles

NR 2 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05 REPAIR-01, P.205, STEP 4E. INSTALLED NEW SEAT TRACK BS 229.5 - 571.5 IAW SRM 51-40-07, STEP 5B, 51-42-05 STEPS 4A-4D, 51-40-15, STEPS 6H-6J.

Part: SEAT TRACK — CORRODED · airframe 16,385 hrs · 17,513 cycles

NR 1 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED CORRODED SEAT TRACK IAW SRM 51-42-05-020-01, STEP 4, E 1 THRU (8) AND 51-40-15-02-01 STEP 6, M, 1 THRU 3. INSTALLED NEW SEAT TRACK NR 1, AT X32.40 TO X234. LT SIDE, REF SRM 51-42-05, STEP 4-D, 3-10 & SRM 51-40-15, STEP 6-G TO PN 85328261-107. LOCATED AND DRILLED HOLES IN NEW SEAT TRACK, PN 85328261-107 UP TO 50 PERCENT SRM 51-40-07-02-01, STEP 5,B, 1 THRU 6. LOCATED AND DRILLED HOLES IN NEW SEAT TRACK PN 85328261-107, 100 PERCENT IAW SRM 51-40-07-02-01, STEP 5, B, 1 THRU 6. INSTALLED RIVETS AT INTERCOASTAL ON LT SEAT TRACK NR 1 FROM X71.200 TO X136.00 IAW SRM 51-42-05, STEP 4, D, 3 THRU 10. INSTALLED SPLICES AND DADO PANEL BRACKET BETWEEN STA X216.000-234.475 TO COMPLETE SEAT TRACK NR 1 REPLACEMENT IAW SRM 51-40-15-02-01, STEP 6, F TO J 1-7. RESTORED FINISH TO NEW SEAT TRACK SRM 51-25-10-02-01, STEP 5, G 2.

Part: FRAME — CORRODED · airframe 16,385 hrs · 17,513 cycles

FRAME 19.4 HAS CORRODED. REMOVED CORROSION MANUALLY IAW SRM 51-21-00.

Part: STRINGER — CORRODED (BS 604-624) · airframe 16,385 hrs · 17,513 cycles

STRINGER 31RT HAS CORROSION ON AND AROUND FOUR RIVETS BETWEEN FRAMES BS 604.5 - 624.5. REMOVED CORROSION IAW SRM 51-21-00.

Part: FRAME — CORRODED · airframe 16,385 hrs · 17,513 cycles

FRAME X32.4 HAS CORROSION AROUND GROUND STUDS. REMOVED CORROSION IAW SRM 51-21-00.

Part: STRINGER — CORRODED (BS 254) · airframe 16,385 hrs · 17,513 cycles

STRINGER 31 LEFT HAS CORROSION ON AND AROUND 4 RIVETS AT STA X254. C/W CORROSION REPORT M-184. 2-M/A. REMOVED CORROSION IAW SRM 51-21-00.

Part: FRAME — CORRODED (BS 301) · airframe 16,385 hrs · 17,513 cycles

FRAME BS 301 HAS CORROSION STRINGER 31RT. REMOVED LIGHT CORROSION ON CLIP ATTACHED TO STR 31RT AT FS X301.00, REF SRM 51-21-00, PROCEDURE A 1-2, NO MATERIAL LOSS NOTED. RESTORED FINISH TO ATTACHING CLIP ON STR 31 RT AT FS X301.00 REF SRM 51-20-00, PG 19, FIG 1 AND PG 23, FIG 5.

Part: SEAT TRACK — CORRODED (BS 612-620) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 15 HAS BE GOUGED. BLENDED SEAT TRACK NR 15, FS 612-620 RT CENTER REF SRM 53-20-49, FIG 1. EVALUATED BLEND AT SEAT TRACK 15 RT CENTER F9612-620 , MATERIAL REMOVED INSIDE CLAW PORTION IS .015". ORIGINAL MATERIAL IS .200" FOUND WITHIN LIMITS REF SRM 53-20-49. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH REF SRM 51-21-10.

Part: SEAT TRACK — CORRODED (BS 650-656) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 20 HAS 1 PITTING AREA. BLENDED SEAT TRACK NR 20 RT FS 650-656. REF SRM 53-20-49. EVALUATED BLEND ON SEAT TRACK NR 20 MATERIAL, REMOVED ON TOP PORTION OF CLAW IS .005" ORIGINAL MATERIAL .460" FOUND WITHIN LIMITS REF SRM 53-20-49, FIG 1. C/W ET INSP ON REWORKED AREAS REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH IAW SRM 51-21-10.

Part: STRINGER — CORRODED (BS 256) · airframe 16,385 hrs · 17,513 cycles

STRINGER 31 RT HAS CORROSION ON AND AROUND 2 RIVETS AT STA X256. REMOVED CORROSION AT STR 31RT ST X256 WITH SCOTCH BRITE PAD IAW SRM 51-21-00, STRUCTURAL ID -02 PG.2, STEP 4.A 2. NO MATERIAL LOSS. RESTORED FINISH IAW SRM 51-20-00, STRUCTURAL ID -01.

Part: SEAT TRACK — CORRODED · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 18 HAS 5 AREAS THAT ARE PITTING. BLENDED SEAT TRACK IAW SRM 53-20-49, FIG 201. FOUND WITHIN LIMIT IAW SRM 53-20-49. ALL BLENDED AREA ON SEAT TRACK 18 REPROTECTED IAW SRM 51-21-10. C/W ET INSP ON REWORKED AREAS REF NDTM PT1 51-00-06. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 621-620) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 15 IS PITTED. BLENDED SEAT TRACK NR 15, BS 612-620 RT CENTER IAW SRM 53-20-49, FIG 1. EVALUATED BLEND AT SEAT TRACK NR 15 RT CENTER MATERIAL REMOVED ON TOP PORTION OF CLAW IS .009". ORIGINAL THICKNESS .460" FOUND WITHIN LIMITS REF SRM 53-20-49. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH REF SRM 51-21-10.

Part: SEAT TRACK — CORRODED (BS 71.2) · airframe 16,385 hrs · 17,513 cycles

RIGHT OTBD SEAT TRACK NR 17 HAS CORROSION AT STA X71.200 ON TOP OF RAIL AND AT BOTTOM OF CLEAT. SEAT TRACK NR 17 AT X 71.200 BLENDED IAW SRM 53-20-49. EVALUATED BLEND X71.200 MATERIAL REMOVED ON TOP IS .012" ORIGINAL THICKNESS: .420" MATERIAL REMOVED INSIDE CLAW PORTION IS 0.015" ORIGINAL THICKNESS IS .160". FOUND WITHIN LIMIT IAW SRM 53-20-49. BLENDED AREA ON SEAT TRACK NR 17 REPROTECTED IAW SRM 51-21-10. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 301) · airframe 16,385 hrs · 17,513 cycles

FRAME BS 301 HAS CORROSION ON FUSELAGE SKIN CLIP BETWEEN STRS 31 AND 32 LT. REMOVED LIGHT CORROSION ON FUSELAGE SKIN CLIP BETWEEN STR 31 & 32LT AT FS X301.00, REF SRM 51-21-00, PROCEDURE A 1 AND 2 NO MATERIAL LOSS NOTED. RESTORED FINISH ON FUSELAGE SKIN CLIP BETWEEN STR 31 & 32 LT AT FS X301.00, REF SRM 51-20-00.

Part: SEAT TRACK — CORRODED (BS 606-612) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 14 HAS 1 AREA OF PITTING. BLENDED SEAT TRACK NR 14, FS 606-612 CENTER RT REF SRM 53-20-49, FIG 1. EVALUATED BLEND AT SEAT TRACK NR 14 RT CENTER FS 606-612 RT CENTER, MATERIAL REMOVED TOP PORTION IS .010", ORIGINAL THICKNESS IS .460" MATERIAL REMOVE INSIDE CLAW PORTION IS .015", ORIGINAL MATERIAL IS .200" FOUND WITHIN IN LIMITS REF SRM 53-20-49. C/W ET INSP ON REWORKED AREA REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH REF SRM 51-21-10.

Part: SEAT TRACK — CORRODED (BS 575) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 20 CORRODED IN 2 AREAS. BLENDED SEAT TRACK 20 RT FS 575.5, REF SRM 53-20-49, FIG 1. EVALUATED BLEND ON SEAT TRACK 20, FS 575.5, MATERIAL REMOVED ON TOP PORTION OF CLAW IS .008" ORIGINAL MATERIAL: .460" FOUND WITHIN LIMITS REF SRM 53-20-49, FIG 1. ET INSP ON REWORKED AREAS REF NDTM PT1 51-00-06. NO DEFECTS NOTED. RESTORED FINISH IAW SRM 51-21-10.

Part: SEAT TRACK — CORRODED (NR 1) · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 2 IS CORRODED. REMOVED DISCREPANCIES ON SEAT TRACK NR 2 REF SRM 53-20-49, REPAIR-02. BLENDED AREA EXCEEDS MAX MAT REMOVAL .017 MAT LOSS OUT OF LIMITS REF SRM 53-20-49. REPAIR-02, PG 204, FIG 201. SEAT TRACK REPLACEMENT COMPLIED WITH ON JOB 5415311, OP 114.

Part: SEAT TRACK — CORRODED · airframe 16,385 hrs · 17,513 cycles

SEAT TRACK NR 3 HAS 2 AREAS OF PITTING. REMOVED PITTING ON NR 3 SEAT TRACK REF SRM 53-20-49, REPAIR -02 6A.B. BLENDED AREA EXEEDS MAX MATERIAL REMOVAL .019 MAT LOSS, OUT OF LIMITS, REF SRM 53-20-49, REPAIR 02, PGS 204, FIG 201.

Part: VALVE — MALFUNCTIONED (ZONE 300) · airframe 16,099 hrs · 17,220 cycles

ON APPROACH, DEICE PRESSURE CAUTION, IN SEVERE ICING. RETURNED TO FIELD AND ACCOMPLISHED UNEVENTFUL LANDING. CDS FAULT LOW PRESSURE 5A FAIL STATUS. COMPLIED WITH GVI/PHYSICAL INSPECTION OF ALL DEICE BOOTS. NO DEFECTS NOTED. R & R NR 5 DDV IAW MM 30-11-16-000-801 AND 30-11-16-400-801. FUNCTIONAL CHECKED GOOD. FAULT DID NOT RETURN. RETURNED TO SERVICE.

Part: SHROUD — DAMAGED (TE FLAP) · airframe 15,724 hrs · 16,817 cycles

LT AND RT INBD T/E FLAP SHROUD HAS BROKEN AND SHEARED RIVETS. REPLACED THE RIVETS IN THE AREA IAW SRM 51-42-05.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 15,061 hrs · 16,118 cycles

FORWARD GALLEY FLOOR STRIP PHOTO-LUMINECENT IS LOOSE. RESECURED FWD GALLEY PHOTO-LUMINESCENT STRIP. RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 15,056 hrs · 16,110 cycles

AFTER TAKEOFF, GEAR RETRACTION WAS SLOW TO INDICATE AND FINALLY RESULTED IN A NOSE GEAR DOOR AMBER LIGHT AND RED LIGHT. NOSE WHEEL STEERING CAUTION LIGHT ILLUMINATED. ALTERNATE GEAR EXTENSION ACCOMPLISHED WITH DESIRED RESULTS. RETURNED TO FIELD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 15,032 hrs · 16,087 cycles

ALTERNATE GEAR EXTENSION DOOR IS HARD TO OPEN AND CLOSE BECAUSE OF STICKY VALVE. R & R THE SECONDARY MLG SELECTOR VALVE IAW AMM TASK 29-21-06-000-801 AND 29-21-06-400-801, DOOR OPERATES NORMAL AND NO DEFECTS, NO LEAKS. RETURNED TO SERVICE.

Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 14,939 hrs · 15,994 cycles

NR 2 HYD ISOLATION VALVE ILLUMINATED ON CLIMBOUT. NR 2 HYD QTY INDICATES 10 PERCENT. RETURNED TO FIELD, LANDING UNEVENTFUL. CHAFED THROUGH HYD LINE IN LT WHEEL WELL WAS REPAIRED ON WO 152803. HYD QTY SERVICED FULL AND LEAK CKS C/W AFTER REPAIR. RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (WHEEL SPEED) · airframe 14,460 hrs · 15,478 cycles

ON LANDING, BRAKING VERY POOR. POST FLIGHT FOUND NR 3 BRAKE COLD. CDS HISTORY SHOWS "RT INBRD WST". REPLACED RT INBD WHEEL SPEED TRANSDUCER IAW AMM TASKS 23-46-11-000-801 AND 23-46-11-400-801. OPS CHECK - GOOD. RETURNED TO SERVICE.

Part: FLAP TRACK — DAMAGED (RT WING) · airframe 13,885 hrs · 14,885 cycles

RT WING NR 4 FLAP TRACK INBD WEB HAS 2 AREAS SHOWING WEAR. BLENDED DAMAGE IAW RD 8/4-57-1238. HFEC SHOWS CRACK FREE. REMAINING MATERIAL WITHIN LIMITS. VERIFIED RIG OF THE FLAPS IAW AMM 27-54-06-400-801.

Part: TORQUE TUBE — DAMAGED (ESCAPE HATCH) · airframe 13,885 hrs · 14,885 cycles

COCKPIT ESCAPE HATCH TORQUE TUBE RT HINGE FITTING HAS SHARP DAMAGE IN THE RADIUS TO THE FLANGE. BLENDED DAMAGE IAW SRM 51-14-00-02-04. HFEC CRACK FREE. REMOVED MATERIAL WITHIN LIMITS OF RD 8/4-52-885. PRIMED AND TREATED AREAS.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 13,885 hrs · 14,885 cycles

AFT PASSENGER ENTRY DOOR HAS ONE CORRODED NUTPLATE AND BRACKET 4" BELOW NR 3 DOOR STOP FITTING. REMOVED BRACKET AND NUTPLATES IAW SRM 51-42-05-02-01. REPLACED THE NUTPLATE IAW SRM 51-42-05-02-01. FABRICATED NEW BRACKET DUE TO CORROSION OUTSIDE OF LIMITS. INSTALLED BRACKET, APPLIED CPC COMPOUND.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 13,885 hrs · 14,885 cycles

AFT SERVICE DOOR HAS FOUR AREAS OF CORROSION ON THE AFT FACE OF THE AFT FRAME. REMOVED CORROSION FROM FRAME IAW SRM 51-21-00-00-02. VERIFIED CRACK FREE. REMOVED AREA IS IN LIMITS OF RD 8/4-52-887. TREATED AND PRIMED AREAS.

Part: FLAP TRACK — WORN (RT WING TE FLAP) · airframe 13,885 hrs · 14,885 cycles

RIGHT WING NR 3 LOWER FLAP TRACK AFT SURFACE IS WORN. REMOVED TRACK IAW RD 8/4-52-1511. BLENDED AREA. HFEC CRACK FREE. REPAIR WITHIN LIMITS. INSTALLED, VERIFY RIGGING OF FLAPS, REINSTALLED REMOVED PANELS.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 13,885 hrs · 14,885 cycles

AFT PASSENGER DOOR HAS SIX AREAS OF CORROSION ON THE AFT FACE OF THE AFT FRAME. REMOVED CORROSION IAW SRM 51-21-00-00-02. NO CRACKS DETECTED. BLENDED AREAS WITHIN LIMITS OF RD 8/4-52-884. TREATED AND PRIMED AREAS.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 13,885 hrs · 14,885 cycles

AFT SERVICE DOOR HAS TWO AREAS OF CORROSION ON THE FORWARD FACE OF THE FORWARD FRAME. REMOVED THE CORROSION IAW SRM 51-21-00-00-02. HFEC SHOWS CRACK FREE. BLENDING IS WITHIN LIMITS IAW DWG 85247121. APPLIED ALODINE AND PRIMERS TO AREAS.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 13,885 hrs · 14,885 cycles

AFT PASSENGER DOOR HAS SEVEN AREAS OF CORROSION ON THE FORWARD FACE OF THE FORWARD FRAME. REMOVED CORROSION IAW SRM 51-21-00-00-02. HFEC SHOWS NO CRACKS. BLENDED AREAS WITHIN LIMITS OF RD 8/4-52-884. PRIMED AND PAINTED AREA.

Part: CONTROL VALVE — MALFUNCTIONED (PAX DOOR SEAL) · airframe 13,563 hrs · 14,553 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. R & R SEAL CONTROL VALVE IAW AMM TASK 52-11-36-000-801 AND 52-11-36-400-801. DOOR SEAL OPERATES NORMALLY. C/W FUNCTIONAL TEST OF THE MCD IAW AMM TASK 52-11-00-720-801. DOOR OPENS FULLY IN APPROX 8 SECS, HANDLE FORCES ARE WITHIN LIMITS. FUNCTIONAL CHECKS GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: HINGE — CONTAMINATED (PAX DOOR) · airframe 13,568 hrs · 14,556 cycles

MAIN CABIN DOOR HANDLE HARD TO OPEN. FOUND EXCESSIVE WATER IN DOOR HINGE DRAINS. OPS TEST PERFORMED IAW AMM TASK 52-11-00-710-802. OPS TEST NORMAL, FLIGHT CREW MUST WAIT 2 SECONDS FOR DOOR SEAL TO DEFLATE BEFORE ATTEMPTING TO OPEN DOOR PAST 1ST OVER CENTER POSITION. RETURNED TO SERVICE.

Part: COVER — DISLODGED (EMERGENCY LIGHTS) · airframe 13,361 hrs · 14,346 cycles

FORWARD RT EMERGENCY EXIT DOOR SIGN COVER FELL OFF. SECURED FORWARD RT EMERGENCY EXIT DOOR SIGN COVER. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: CONTROL SWITCH — MALFUNCTIONED (AUTOFEATHER) · airframe 13,326 hrs · 14,302 cycles

AUTOFEATHER WOULD NOT ARM ON TAKEOFF ROLL. SELECT LIGHT WAS ILLUMINATED. ABORTED T/O AT APPROX 50 KNOTS. INTEROGATED CDS AND FOUND FAULT CODE 70A ON NR 1 PROPELLER, FOUND AUTOFEATHER SWITCH STICKING AND NOT LATCHING PROPERLY. REMOVED FUEL/ ENGINE/ PROPELLER CONTROL PANEL IAW AMM TASK 31-10-01-000-801. REPLACED AUTOFEATHER SWITCH WITH NEW FROM STOCK IAW AMM TASK 31-10-01-000-802 STEPS 1-3 AND 4E. AND 31-10-01-400-802 STEPS 1-3 AND 4E AND STEP 5. REINSTALLED FUEL/ ENGINE/ PROPELLER CONTROL PANEL IAW AMM TASK 31-10-01-400-801. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,283 hrs · 14,263 cycles

F/A REPORTED ON PREFLIGHT, EMERGENCY LIGHTING SWITCH DOES NOT SHOW THE NORMAL INDICATION ILLUMINATION SCREEN. R & R BURNED OUT LIGHT BULBS. OPS TESTED GOOD, NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: CONNECTOR — FAILED (MLG) · airframe 13,026 hrs · 13,997 cycles

AFTER TAKEOFF, THREE RED GEAR UNSAFE INDICATION LIGHTS. ACCOMPLISHED EMERGENCY GEAR EXTENSION IAW CHECKLIST, RETURNED TO FIELD AND LANDED UNEVENTFUL. DURING FUNCTIONAL TEST, NOSE WHEEL DID NOT CENTER FOR STEPS 4.A. (11)(5)- (U0, AMM 32-51-00-720-801. TOOK VOLT READINGS AT SCU TEST POINTS FOUND SOV SHUTOFF AFTER 5 SECONDS BUT SERVO MOTOR GETS CENTERING SIGNAL AFTER 5 SECOND DELAY INSTEAD OF IMMEDIATELY AS EXPECTED. DURING WIRING CHECK, FOUND WIRE 121B-22-4 MEGGERED BAD, REPLACED CONNECTOR 9811-J181. RETURNED TO SERVICE.

Part: LIGHT — DIRTY (ZONE 200) · airframe 12,829 hrs · 13,782 cycles

ALL EMERGENCY FLOOR PATH LIGHTING STRIPS ARE DIRTY. CLEANED AND OR REPLACED AS REQUIRED.

Part: SEAL — LEAKING (ZONE 400) · airframe 12,504 hrs · 13,440 cycles

AFTER TAKEOFF, NR 2 ENGINE OIL PRESSURE DECREASED TO 50 PSI VARING TO 60 PSI. PROP WAS FEATHERED AND RETURN TO FIELD. ALL OTHER ENGINE INDICATORS REMAINED NORMAL. LANDING UNEVENTFUL. FOUND EVIDENCE OF OIL LEAK IN DRAIN LINE FROM VARIABLE DELIVERS HYD PUMP. R & R HYD PUMP DRIVE OIL SEAL IAW AMM TASK 79-22-77-000-801 AND 79-22-77-400-801. PERFORMED ENGINE RUNS/LEAK CHECK IAW AMM TASK 71-00-00-790-801. NO LEAKS NOTED. OIL PRESSURE REMAINED IN NORMAL RANGES AND HELD STEADY. NO FURTHER DEFECTS. RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,201 hrs · 13,109 cycles

PASSENGERS COMPLAIN ABOUT MOLDY OLD SOCK ODOR, MOST NOTICEABLE IN CLIMB & DESCENT. COULD NOT DETECT ANY FOUL ODORS IN CABIN OR FLIGHT COMPARTMENT. RAN BOTH ENGINES SEPARATELY FOR 10 MINS AND DID NOT NOTICE ANY ODORS. ALSO RAN APU FOR 10 MINUTES AND, NO ODOR NOTICED. RAN BLEEDS AT FULL HOT AND FULL COLD WITH NO OBVIOUS CHANGES IN ODORS. COULD NOT DUPLICATE ODOR. NO DEFECTS NOTED.

Part: DOOR — BINDING (MAIN PAX) · airframe 12,134 hrs · 13,042 cycles

F/A REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN. OPS TESTED GOOD IAW AMM 52-11-00-710-802, CHECKED FUNCTION OF DOOR, AND APPLIED FORCE GAUGE, FOUND TO BE IN LIMITS FOR OPENING DOOR HANDLE INTERNAL IAW AMM 52-11-00-720-802 1-3A(1)(A-E) A/C FOR OK FOR CONT SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 12,037 hrs · 12,940 cycles

F/A REPORTS MAIN CABIN DOOR IS DIFICULT TO OPEN. CLEANED AND LUBED DOOR MECHANISM. PERFORMED OPS CHECK OF MCD IAW AMM TASK 52-11-00-710-802. OPS CHECKED GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FILTER — DIRTY (ZONE 200) · airframe 11,924 hrs · 12,829 cycles

BLEED AIR INTO CABIN SMELLS LIKE DIRTY SOCKS. R & R RECURCULATION AIR FILTER, OP'S TESTED NORMAL. RETURNED TO SERVICE.

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG) · airframe 11,179 hrs · 12,057 cycles

NOSE GEAR DOOR AND GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION DID ALT GEAR EXTENSION IAW CHECKLIST NO DEFECTS NOTED. DIVERTED, LANDING WT 62800 DESCENT RATE 200' IAW MIN LANDING UNEVENTFUL. REPLACED NLG SELONIOD SEQUENCE VALVE. CHECKS GOOD. ALSO PERFORMED OVERWEIGHT LANDING INSP WITH NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FWD LT PAX DOOR THRESHOLD BEAM HAS AREAS OF CORROSION FROM STA X7.000 TO X28.000. REMOVED CORROSION IAW RD 8/4-53-1600. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW GENERIC RD 8/4-53-1600. REMOVED THRESHOLD MEMBER IAW SRM 51-42-05-02-01. MATCH DRILLED REPLACEMENT THRESHOLD MEMBER IAW SRM 51-42-05-02-01. TREATED, PRIMED FWD PAX DOOR THRESHOLD BEAM IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW THRESHOLD MEMBER AND ASSOCIATED PARTS IAW SRM 51-42-05-02-01.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FOUND PAX DOOR THRESHOLD SUPPORT CHANNEL CORRODED. BLENDED CORROSION IAW RD 8/4-53-1660. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-1660. REMOVED THRESHOLD SUPPORT CHANNEL IAW SRM 51-42-05-02-01. MATCH DRILLED REPLACEMENT THRESHOLD SUPPORT CHANNEL IAW SRM 51-42-05-02-01. TREATED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED THRESHOLD SUPPORT CHANNEL IAW SRM 51-42-05-02-01.

Part: PLATE — CORRODED (PAX DOOR) · airframe 10,464 hrs · 11,347 cycles

FWD PAX DOOR BOTTOM STEP REINFORCEMENT PLATE FOUND CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00-00-02. FABRICATED REPLACEMENT LOWER STEP IAW DWG NR 85217076, AND SRM 51-40-07-02-01. TREATED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED INSTALLED STEP PLATES IAW SRM 51-41-05-00-01 AND AMM 25-25-01-400-801.

Part: STRINGER — CORRODED (BS 116 S25R) · airframe 10,464 hrs · 11,347 cycles

STRINGER 25S AND RIVETS HAVE CORROSION 6 IN AFT OF FRAME 116.000. REMOVED 4 RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION TO BE LIMITED TO RIVETS. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. PAINTED IAW SRM 51-25-15.

Part: FRAME — CORRODED (BS 156 S30-33L) · airframe 10,464 hrs · 11,347 cycles

FRAME X156.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 33. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .045", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. FLANGES FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND PAINTED REF AMM 51-25-31-370-801 AND RD 8/4-53-2344.

Part: STRINGER — CORRODED (BS 116 S24R) · airframe 10,464 hrs · 11,347 cycles

STRINGER 24S HAS CORROSION JUST FWD OF STA X116.000. REMOVED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .048" FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3812. TREATED, PRIMED,PAINTED AND APPLIED CPC IAW RD 8/4-53-3812.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

LT WING ACCESS PANEL 524CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS. CONFIRMED CRACK FREE AREA REF RD 8/4-53-442. TREATED AND PRIMED PANEL IAW RD 8/4-57-442.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X1.000 LOWER FLANGE HAS CORROSION BETWEEN STRINGERS 31P AND 32P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .048", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED, PRIMED AND PAINTED REF RD 8/4-53-2344.

Part: FLAP TRACK — DAMAGED (RT WING) · airframe 10,464 hrs · 11,347 cycles

RT WING NR 4 FLAP TRACK VERTICAL LEG INBD SIDE OF TRACK HAS CHIPPED CARBIDE COATING. BLENDED DAMAGED AREA IAW RD 8/4-57-1238. MINIMUM REMAINING THICKNESS .150" IS WITHIN LIMITS IAW RD 8/4-57-1238. COMPLETED REPAIR IAW RD 8/4-57-1238.

Part: FLOOR PANEL — CORRODED (BS 835) · airframe 10,464 hrs · 11,347 cycles

AFT CARGO FLOOR WEB AT STA 835 RT Y 21 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. REMAINING THICKNESS .081" REF NTM 51-00-01-250-801, FOUND WITHIN LIMITS. TREATED AND PRIMED AREA IAW SRM 51-21-10-02-01 AND 51-25-45-02-01.

Part: SKIN — CORRODED (BS 547-564.5) · airframe 10,464 hrs · 11,347 cycles

SKIN LAP HAS AREA OF CORROSION BETWEEN STA 547 - 564.5 AND LT STR 31-32. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3814. RESTORED SURFACE PROTECTION IAW SRM 51-25-15-02-01, 51-21-10-02-01, 51-25-16-02-01 AND RD 8/4-53-3814.

Part: ATTACH FITTING — MISSING (AILERON) · airframe 10,464 hrs · 11,347 cycles

LT WING INTERNAL T/E AILERON ATTACH FITTING CENTER RIVET ON SPAR BRACKET IS MISSING. INSTALLED HI-LITE AND COMPLIED WITH IAW RD 8/4-57-1609.

Part: FLAP TRACK — DAMAGED (LT WING) · airframe 10,464 hrs · 11,347 cycles

LT WING NR4 FLAP TRACK VERTICAL LEG ON INBD SIDE OF TRACK HAS CHIPPED CARBIDE COATING. BLENDED DAMAGED AREA IAW RD 8/4-57-1238. MINIMUM REMAINING THICKNESS .150" AND CRACK FREE REF RD 8/4-57-1238. BLENDED AREA IS WITHIN LIMITS IAW RD 8/4-57-1238.

Part: STRINGER — CORRODED (24 RIGHT) · airframe 10,464 hrs · 11,347 cycles

STRINGER 24S AND FASTENERS HAVE CORROSION BETWEEN STA X196.000 AND 216.000. REMOVED AFFECTED RIVETS IAW SRM 51-42-05-02-01. REMOVED CORROSION FROM AFFECTED AREA IAW SRM 51-21-00-00-01. FOUND TO BE WITHIN LIMITS RD 8/4-53-3812. TREATED AND PRIMED IAW RD 8/4-53-3812. INSTALLED RIVETS REF SRM 51-42-05-02-01. APPLIED TOP COAT IAW RD 8/4-53-3812. APPLIED CPC IAW RD 8/4-53-3812.

Part: FLAP TRACK — CHAFED (LT WING) · airframe 10,464 hrs · 11,347 cycles

LT WING UPPER FLAP TRACK HAS CHAFING ON VERTICAL LEG. BLENDED CHAFING IAW RD 8/4-57-1352. MINIMUM REMAINING THICKNESS IN BLEND AREA .184". CONFIRMED CRACK FREE REF RD 8/4-57-1352. ALODINED, PRIMED AND PAINTED BLEND AREA IAW RD 8/4-57-1611.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X8.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD PAX DOOR THRESHOLD. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .043" FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-2344. REMOVED CORRODED ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED REPLACEMENT ANGLE IAW SRM 51-42-05-02-01. TREATED AND PRIMED ANGLE IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED ANGLE IAW SRM 51-42-05-02-01. ALODINED, PRIMED, AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01, AND 51-25-05-02-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

STRINGER 30S CORRODED AROUND RIVET AFT OF FRAME X32.400. REMOVED 1 RIVET IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-01. APPLIED TOP COAT AND CPC IAW RD 8/4-53-3825.

Part: FRAME — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

FRAME X28.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD LT PAX DOOR THRESHOLD. REMOVED CORROSION IAW Q400 51-21-00-00-01. MINIMUM REMAINING THICKNESS .037" FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-2344. REMOVED CORRODED ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED REPLACEMENT ANGLE IAW SRM 51-42-05-02-01. TREATED AND PRIMED ANGLE IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED ANGLE IAW SRM 51-42-05-02-01. ALODINED, 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 10,464 hrs · 11,347 cycles

FRAME X176.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 31P AND 32P. BLENDED CORROSION IAW RD 8/4-53-2344. BLEND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, AND PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 156) · airframe 10,464 hrs · 11,347 cycles

FRAME X156.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .045". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: SHEAR TIE — CORRODED · airframe 10,464 hrs · 11,347 cycles

STRINGER 31P, FRAME TIE IN DOUBLER AT AFT SIDE OF FRAME X18.250 HAS CORROSION AND CORRODED HARDWARE. REMOVED CORRODED HARDWARE REF SRM 51-41-00-00-01. REMOVED STR 31P FRAME TIE IN DOUBLER REF SRM 51-40-15-02-01 AND SRM 51-42-05-02-01. FOUND OUT OF LIMITS REF SRM 53-20-03-00-01. RECEIVED NEW PART AND MATCH DRILLED REF SRM 51-40-07-02-01. TREATED AND INSTALLED REF SRM 51-21-10-02-01, 51-40-15-02-01 AND 51-42-05-02-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X216.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW SRM 53-23-44. MINIMUM REMAINING THICKNESS MEASURED .045". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 53-23-44.

Part: FRAME — CORRODED (BS 489.5 S31) · airframe 10,464 hrs · 11,347 cycles

FRAME FLANGE AT STA 489.5 RT STR 31 HAS CORROSION. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .055". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 196) · airframe 10,464 hrs · 11,347 cycles

FRAME X196.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 341) · airframe 10,464 hrs · 11,347 cycles

FRAME X341.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 31P. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .056". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 216) · airframe 10,464 hrs · 11,347 cycles

FRAME X216.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .046". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 156 S30-32R) · airframe 10,464 hrs · 11,347 cycles

FRAME X156.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS IS .046". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 176) · airframe 10,464 hrs · 11,347 cycles

FRAME X176.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

SEAT TRACK NR 23 HAS CORROSION. BLENDED CORROSION REF RD 8/4-53-884. REMOVED MEASURED .027. MAX ALLOWED .050" FOUND WITHIN LIMITS REF RD 8/4-53-884. RESTORED SURFACE PROTECTION IAW RD 8/4-53-884.

Part: FRAME — CORRODED (BS 401) · airframe 10,464 hrs · 11,347 cycles

FRAME X401.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 31S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .064". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X94.800 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS MEASURED .039". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X94.800 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .041". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X94.800 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. BLENDED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS MEASURED .039". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 401 S30-32L) · airframe 10,464 hrs · 11,347 cycles

FRAME X401.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .063". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, AND COMPLETED REPAIR IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 216 S30-32R) · airframe 10,464 hrs · 11,347 cycles

FRAME X216.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS MEASURED .046". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X281.000 LOWER FLANGE HAS CORROSION BETWEEN STRINGERS 31S AND 32S. REMOVED CORROSION IAW SRM 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .045". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 94 S30-32L) · airframe 10,464 hrs · 11,347 cycles

FRAME X94.800 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. BLENDED CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS MEASURED .041". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 116 S30-32R)

FRAME X116.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS .044. CONFIRMED CRACK FREE CONDITION. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 136) · airframe 10,464 hrs · 11,347 cycles

FRAME X136.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLEND IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITING COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 196) · airframe 10,464 hrs · 11,347 cycles

FRAME X196.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS MEASURED .046". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 116) · airframe 10,464 hrs · 11,347 cycles

FRAME X116.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .047". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 136) · airframe 10,464 hrs · 11,347 cycles

FRAME X136.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X19.400 LOWER FLANGES HAVE CORROSION BETWEEN STRINGER 30S AND 32S. REMOVED CORROSION FROM AFFECTED AREA IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. MINIMUM REMAINING THICKNESS .037" FOUND TO BE IN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-45-02-01 AND 51-25-15-02-01. APPLIED CPC IAW AMM 51-25-01-390-801.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X413.000 LOWER FLANGE HAS CORROSION BETWEEN STRINGERS 30S AND 31S. REMOVED CORROSION IAW 51-21-00-00-02. MINIMUM REMAINING THICKNESS MEASURED .060". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 765) · airframe 10,464 hrs · 11,347 cycles

FRAME SECTION UNDER LOWER CARGO DOOR SEAL AT STA 765 HAS LIGHT CORROSION AROUND FASTENER HOLE. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AFFECTED AREAS CRACK FREE CONDITION REF NTM 51-00-02-250-801. UT REMAINING THICKNESS MEASURED .063" REF NTM 51-00-02-250-801. FOUND AFFECTED AREA TO BE WITHIN LIMITS OF RD 8/4-53-3800. ALODINED IAW SRM 51-21-10-02-01, COMPLETED REPAIR IAW RD 8/4-53-3800.

Part: FRAME — CORRODED (BS 258) · airframe 10,464 hrs · 11,347 cycles

FRAME X258.500 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 31S AND 32S. REMOVED CORROSION IAW SRM 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 32.4) · airframe 10,464 hrs · 11,347 cycles

FRAME X32.400 LOWER FLANGE HAVE CORROSION BETWEEN STRINGERS 28S AND 29S. BLENDED CORROSION IAW Q400 RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .038". CONFIRMED CRACK FREE CONDITION REF Q400 NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF BOMBARDIER RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND PER RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X49.500 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW SRM 51-21-00-00-01. FOUND FLANGES TO BE WITHIN LIMITS PER RD 8/4-53-2344. TREATED,PRIMED AND PAINTED PER RD 8/4-53-2344.

Part: WEB — CORRODED (BS 714.6-783.1) · airframe 10,464 hrs · 11,347 cycles

AFT CARGO, LT FLOOR WEB STA 714.6 - 783.1 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. HFEC CONFIRMED CRACK FREE REF NTM, 51-00-02-250-801 UT REMAINING THICKNESS MEASURED .047" IN REF NTM 51-42-05-02-01. COMPLETED REPAIR IAW TASK CARD RD 8/4-53-3802.

Part: WEB — CORRODED (BS 687.6-714.6) · airframe 10,464 hrs · 11,347 cycles

LT CARGO, LT FLOOR WEB STA 687.6-714.6 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. HFEC CONFIRMED CRACK FREE REF NTM, 51-00-02-250-801 UT REMAINING THICKNESS MEASURED .049" IN REF NTM 51-00-02-250-801. COMPLETED REPAIR IAW TASK CARD RD 8/4-53-3802.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X49.500 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S AND 32S. REMOVED CORROSION IAW SRM 51-21-00-00-01. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. TREATED,PRIMED AND PAINTED IAW RD 8/4-53-2344

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X281.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW SRM 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .043". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. TREATED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 32.4) · airframe 10,464 hrs · 11,347 cycles

FRAME X32.400 LOWER FLANGE HAVE CORROSION BETWEEN STRINGERS 29S AND 32S. BLENDED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .040". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X1.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 28S AND 29S. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .044". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 32.4) · airframe 10,464 hrs · 11,347 cycles

FRAME X32.400 LOWER FLANGE HAVE CORROSION BETWEEN STRINGERS 29P AND 31P. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS MEASURED .039". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 136) · airframe 10,464 hrs · 11,347 cycles

FRAME X136.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. REMOVED CORROSION IAW RD 8/4-53-2344. MINIMUM REMAINING THICKNESS MEASURED .045". CONFIRMED CRACK FREE CONDITION REF NTM 51-00-02-250-801 AND 51-00-01-250-801. BLENDED AREA IS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CORROSION PREVENTATIVE COMPOUND IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 71.2) · airframe 10,464 hrs · 11,347 cycles

FRAME X71.200 LOWER FLANGE HAVE CORROSION BETWEEN STRINGER 29S & 32S. BLENDED CORROSION IAW RD 8/4-53-2344. HFEC CONFIRMED CRACK FREE REF NTM, 51-00-02-250-801 UT REMAINING THICKNESS MEASURED .040" IN REF NTM 51-00-01-250-801. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. ALODINE, PRIMED AND PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X71.200 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 29S AND 32S. BLENDED CORROSION REF RD 8/4-53-2344. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED,PRIMED AND PAINTED IAW RD 8/4-53-2344.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 10,464 hrs · 11,347 cycles

RT OTBD FLAP UPPER SKIN IS CHAFED BETWEEN STA YW-191.200 & YW-281.019. BLENDED AWAY ALL DAMAGE IAW BOMBARDIER RD 8/4-57-1594. MINIMUM REMAINING THICKNESS .025" REF NTM 51-00-02-250-801 AND DISBOND CRACK FREE REF RD 8/4-57-1594. NOMINAL THICKNESS .032" FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1594. RESTORED SURFACE FINISH IAW RD 8/4-57-1594.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X19.400 LOWER FLANGE HAS CORROSION BETWEEN STRINGER 28S AND 29S. REMOVED CORROSION FROM AFFECTED AREAS IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X71.200 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. BLENDED CORROSION REF RD 8/4-53-2344. CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND PAINTED PER RD 8/4-53-2344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

FRAME X19.400 LOWER FLANGE HAS CORROSION BETWEEN STRINGER 30P AND 32P. REMOVED CORROSION FROM AFFECTED AREAS IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED IAW RD 8/4-53-2344.

Part: FRAME — CORRODED (BS 116) · airframe 10,464 hrs · 11,347 cycles

FRAME X116.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30P AND 32P. BLENDED CORROSION REF RD 8/4-53-2344. CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED,PRIMED AND PAINTED IAW RD 8/4-53-2344.

Part: SEAT TRACK — CORRODED (BS 664) · airframe 10,501 hrs · 11,466 cycles

C2 - CORROSION FOUND ON LT INBD SEAT TRACK 2 X664.50. BLENDED CORROSION IAW SRM 51-21-00 AND FOUND TO BE WITHIN MAX LIMIT IAW SRM 53-20-49. TREATED AFFECTED AREA WITH ALODINE IAW SRM 51-21-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

SEAT RAIL NR 11 HAS AREAS OF CORROSION. BLENDED CORROSION IAW RD 8/4-53-2358 AND RD 8/4-53-884. FOUND TO BE OUT OF LIMITS, REMOVED SEAT RAIL NR 11 IAW SRM 51-40-15-02-01, 51-41-00-00-01 AND 51-42-05-02-01. RECEIVED NEW SEAT TRACK AND MATCH DRILLED TO STRUCTURE IAW SRM 51-40-07-02-01. INSTALLED NEW SEAT RAIL, IAW SRM 51-42-05-02-01, 51-41-00-00-01 AND 51-40-15.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524AT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS PANEL 525AT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

COE - C2 - LT WING ACCESS LANDING FOR PANEL 525AT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: FRAME — CORRODED (BS 301 S30-33R) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME X301.000 LOWER FLANGES HAVE CORROSION BETWEEN STRINGERS 30S &33.. BLENDED OUT CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT RAIL NR 5 HAS CORROSION AND SCRATCHES BETWEEN STA X32.500 AND X102.000. BLENDED CORROSION IAW RD 8/4-53-884. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10, AND RD 8/4-53-884.

Part: FRAME — CORRODED (BS 301) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME X301.000 LOWER FLANGE HAS CORROSION BETWEEN STRINGERS 31P AND 32P. BLENDED CORROSION IAW RD 8/4-53-2344. FOUND TO BE WITHIN LIMITS RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: FRAME — CORRODED (BS 584.5 S32-33R) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME FLANGE AT STA 584.5 RT STR 32 - 33 HAS CORROSION. BLENDED OUT CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524BT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524FT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS PANEL 524FT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

C2 - FLOORBOARD SUPPORT PLATE AFT OF FWD LT PAX DOOR OPENING AT STA X32.400 HAS AREAS OF CORROSION. REMOVED CORROSION REF SRM 51-21-00-00-02. REMOVED SUPPORT PLATE REF SRM 51-42-45-02-01. FABRICATED NEW SUPPORT PLATE IAW TC 6-53-996. ALODINED AND PRIMED PART IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW SUPPORT PLATE IAW SRM 51-42-05-02-01.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

LT WING ACCESS PANEL 524BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION ON LT WING ACCESS PANEL 524BT PAD MATING SURFACE IAW RD 8/4-57-442. REMAINING MATERIAL THICKNESS .117" WITH IN LIMITS IAW RD 8/4-57-442. CONFIRMED CRACK FREE REF RD 8/4-57-4420. TREATED, PRIMED PANEL IAW RD 8/4-57-442.

Part: FRAME — CORRODED (BS 509.5 S32-33R) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME FLANGE AT STA 509.5 RT STR 32 -33 HAS CORROSION. BLENDED OUT CORROSION IAW BOMBARDIER RD 8/4-53-2344. REMAINING THICKNESS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: FRAME — CORRODED (BS 509.5 S31-32L) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME FLANGE AT STA 509.5 LT STR 31-32 HAS CORROSION. BLENDED OUT CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: SKIN — CORRODED (BS 830) · airframe 10,464 hrs · 11,347 cycles

SKIN HAS AREA OF CORROSION AT STA 830 JUST ABOVE STR 25. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS .038 REF NTM 51-00-02-250-801. CONFIRMED AREA CRACK FREE REF NTM 51-00-01-250-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3802. ALODINED, PRIMED AND PAINTED IAW RD 8/4-53-3807. COMPLIED WITH RD 8/4-53-3807.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524DT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS PANEL 524ET HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.

Part: FRAME — CORRODED (BS 509.5) · airframe 10,464 hrs · 11,347 cycles

FRAME FLANGE AT STA 509.5 RT STR 31-32 HAS CORROSION. BLENDED OUT CORROSION IAW RD 8/4-53-2344. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: FITTING — CORRODED (PAX DOOR) · airframe 10,464 hrs · 11,347 cycles

C2 - FWD PAX DOOR FWD AND AFT SHOCK FITTINGS SHOW SIGNS OF CORROSION. REPLACED FITTINGS AND BUSHINGS IAW AMM 52-11-21-000-801. REMOVED BUSHINGS IAW AMM 52-11-23-000-801. INSTALLED BUSHINGS AND FITTINGS IAW AMM 52-11-23-400-801, 52-11-01-400-801 AND 52-11-21-400-801.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LT WING ACCESS LANDING FOR PANEL 524ET HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: FRAME — CORRODED (BS 584.5 S31-32R) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME FLANGE AT STA 584.5 RT STR 31-32 HAS CORROSION. BLENDED OUT CORROSION IAW MFG RD 8/4-53-2344. REMAINING THICKNESS WITHIN LIMITS OF RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-21-10-02-01, 51-25-10-02-01, 51-25-05-02-01 AND 51-25-01-390-801.

Part: FRAME — CORRODED (BS 156) · airframe 10,464 hrs · 11,347 cycles

C2 - FRAME X156.000 STRINGER CLIP AT STRINGER 24S HAS CORROSION. REMOVED CORROSION REF SRM 51-21-00-00-01. NO REPAIRS ALLOWED IAW SRM 53-20-15-00-01. REMOVED CLIP AND FABRICATED NEW CLIP IAW SRM 51-42-05-02-01 AND TASK CARD 6-53-998. ALODINED, PRIMED IAW SRM 51-21-10-02-01 AND IAW SRM 51-25-10-02-01. INSTALLED CLIP IAW SRM 51-42-05-02-01. APPLIED TOP COAT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - LEFT WING ACCESS PANEL 524BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 11 HAS AREAS OF CORROSION. BLENDED CORROSION IAW RD 8/4-53-2358, RD 8/4-53-884. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK NR 11 IAW SRM 51-40-15-02-01, 51-42-05-02-01 AND 51-41-00-00-01. INSTALLED NEW SEAT TRACK IAW SRM 51-40-07-02-01, 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01.

Part: STRINGER CLIP — CORRODED (BS 216 S32L) · airframe 10,464 hrs · 11,347 cycles

C2 - STRINGER CLIP AT FRAME X216.000 AND STRINGER 32P HAS CORROSION. REMOVED 5 CORRODED RIVETS FROM STRINGER AND CLIP. FOUND DEFECTS TO BE IN TOP COAT OF PAINT. NO CORROSION NOTED. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. RESTORED PROTECTIVE FINISH IAW SRM 51-25-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 9 HAS CORROSION IN SEVERAL PLACES. SEAT TRACK NR 9 FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK REF SRM 51-40-15-02-01, 51-42-05-02-01 AND 51-41-00-00-01. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. RESTORED FINISH IAW SRM 51-25-15.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT RAIL NR 10 HAS AREA OF CORROSION. REMOVED DAMAGE IAW RD 8/4-53-2358, FOUND SEAT RAIL TO BE OUT OF LIMITS IAW RD 8/4-53-2358. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01.

Part: SEAT TRACK — CORRODED · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR24 HAS CORROSION. BLENDED CORROSION REF RD 8/4-53-884. REMOVED MATERIAL .002" FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. RESTORED PROTECTIVE FINISH IAW SRM 51-25-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT RAIL NR13 HAS CORROSION AT STA X404.000. REMOVED CORROSION ON SEAT RAIL NR13 IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. ALODINED AFFECTED AREA IAW SRM 51-21-10.

Part: SEAT TRACK — CORRODED (BS 600-668) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 8 HAS SEVERAL SPOTS OF CORROSION FROM STA 600- 668. BLENDED CORROSION IAW RD 8/4-53-884. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK REF SRM 51-42-05-02-01 AND 51-41-00-00-01. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND 51-41-00-00-01. STORED FINISH IAW SRM 51-25-15.

Part: SEAT TRACK — NICKED (BS 331) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT RAIL NR 7 IS NICKED AT STA X331.000 AND HAS CORROSION AT STA X367.000. REMOVED NICK IAW Q400 SRM 51-14-00-02-01 AND CORROSION IAW BOMBARDIER RD 8/4-53-884. MATERIAL LOSS .002 WITH A NOMINAL THICKNESS OF .454 AND .015 ALLOWED. CONFIRMED CRACK FREE REF RD 8/4-53-884. APPLIED ALODINE IAW Q400 SRM 51-21-10.

Part: SEAT TRACK — CORRODED (BS 612-668) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 15 HAS SEVERAL SPOTS OF CORROSION FROM STA 612- 668. BLENDED CORROSION IAW RD 8/4-53-884. FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK REF SRM 51-40-15-02-01 AND 51-42-05-02-01. PREPPED AND INSTALLED NEW SEAT TRACK NR15 IAW SRM 51-25-10-02-01, 51-42-05-02-01, 51-40-15-02-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 16 HAS CORROSION. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED NR 16 SEAT TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-07-02-01, 51-21-10-02-01, 51-25-10-02-01, 51-40-15-02-01 AND 51-42-05-02-01.

Part: ATTACH ANGLE — CORRODED (BS 783.1) · airframe 10,464 hrs · 11,347 cycles

C2 - AFT CARGO AREA AT STA 783.1 ATTACH ANGLE FOR FLOOR WEB TO VERTICAL WEB HAS BARE METAL AND CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-00-01. ALODINED, PRIMED AND APPLIED CORROSION PREVENTATIVE IAW 51-21-10-02-01, 51-25-10-02-01 AND 51-25-01-390-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,464 hrs · 11,347 cycles

C2 - SEAT TRACK NR 25 HAS CORROSION. BLENDED CORROSION RQ400 RD 8/4-53-884. FOUND TRACK TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01, 51-42-45-02-01. INSTALLED NEW NR25 TRACK REF 51-40-07-02-01, 51-42-05-02-01 AND 51-42-45-02-01.

Part: STRINGER — CORRODED (BS 321 S31R) · airframe 10,464 hrs · 11,347 cycles

C2 - STRINGER 31S AND FASTENERS HAVE CORROSION FWD OF STATION X321.000. REMOVED 1 RIVET FROM STRINGER 31S IAW SRM 51-42-05-02-01. NO CORROSION FOUND ON STRINGER. INSTALLED NEW RIVET IAW SRM 51-42-05-02-01. ALODINED AND PRIMED IAW SRM 51-21-10-02-01. PAINTED IAW SRM 51-20-00-00-01.

Part: STRINGER — CORRODED (BS 281 S31R) · airframe 10,464 hrs · 11,347 cycles

C2 - STRINGER 31S HAS CORROSION AFT OF STA X281.000. REMOVED 5 RIVETS FROM STRINGER 31S AND FOUND NO CORROSION ON STRINGER. RIVETS REMOVED IAW SRM 51-42-05-02-01. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. PAINTED IAW SRM 51-20-00-00-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 10,464 hrs · 11,347 cycles

C2 - INTERNAL BELLY LAP BETWEEN STA X156.000 AND X176.000 HAS AREAS OF CORROSION BETWEEN STRINGERS 31P AND 32P. REMOVED PAINT AND PRIMER IAW SRM 51-21-00-00-01. CORROSION WAS CONFINED TO PAINT AND PRIMER. ALODINED PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-40-02-01 AND 51-20-00-00-01.

Part: STRINGER — CORRODED (BS 469.5-489.5) · airframe 10,464 hrs · 11,347 cycles

C2 - RT STR 31 BETWEEN STA 469.5 TO 489.5 HAS CORROSION AROUND FASTENERS COMMON TO STRINGER. REMOVED 5 RIVETS FROM RT STRINGER IAW SRM 51-42-05-02-01. NO CORROSION FOUND ON STRINGER. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-20-00-00-01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 10,464 hrs · 11,347 cycles

C2 - STRINGER 31S & RIVETS HAVE CORROSION BETWEEN STA X49.500 AND X71.200. REMOVED 14 RIVETS IAW SRM 51-42-05-02-01. CORROSION CONFINED TO RIVETS. INSTALLED NEW RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-20-00-00-01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 10,464 hrs · 11,347 cycles

C2 - RT STR BETWEEN STA 469 TO 489 HAS CORROSION AROUND FASTENERS. REMOVED AFFECTED RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION TO BE LIMITED TO RIVETS ONLY. INSTALLED RIVETS IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-20-00-00-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,646 hrs · 11,347 cycles

C2 - RIGHT WING FUEL PANEL 625AT HAS FRETTING CORROSION. BLENDED CORROSION, REMAINING MATERIAL FOUND WITH IN LIMITS AND COMPLETED REPAIRS REF RD 8/4-57-442.

Part: STRINGER — CORRODED (BS 489-509 S24L) · airframe 10,464 hrs · 11,347 cycles

C2 - LT STR 24 BETWEEN STA 489 - 509 HAS CORROSION AROUND FASTENERS. REMOVED RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION LIMITED TO FASTENERS ONLY. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: STRINGER — CORRODED (BS 547-564) · airframe 10,646 hrs · 11,347 cycles

C2 - LT STR 24 BETWEEN STA 547 - 564 HAS CORROSION. AFTER FUTHER REVIEW NO CORROSION FOUND IN AREA OF QUESTION, FOUND BUBBLED BENEATH HI LIGHT COLLAR. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTALLED NEW FASTENER IAW SRM 51-40-15-02-01, PAINTED IAW SRM 51-25-15-02-01.

Part: STRINGER — CORRODED (BS 529-547) · airframe 10,464 hrs · 11,347 cycles

C2 - LT STR 24 BETWEEN STA 529 - 547 HAS CORROSION ON STRINGER AND AROUND FASTENERS. REMOVED RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION LIMITED TO FASTENERS ONLY. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED RIVETS IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: STRINGER — CORRODED (BS 469-489) · airframe 10,464 hrs · 11,347 cycles

C2 - LT STR 24 BETWEEN STA 469 - 489 HAS CORROSION AROUND FASTENERS. REMOVED RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION LIMITED TO FASTENERS ONLY NO DAMAGE FOUND ON STRINGER. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 -RT WING FUEL PANEL 624AT HAS CORROSION. TURNED PANEL OVER TO MFG ENGINEERING. NEW PANEL RECEIVED, TOP COATING IAW SRM 51-25-05-02-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RT WING FUEL LANDING FOR PANEL 624FT HAS CORROSION. BLENDED CORROSION IAW RD 8/4-57-445. REMAINING THICKNESS .079 REF NTM 51-00-02-250-801. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-445. TREATED AND PRIMED IAW RD 8/4-57-445.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RT FUEL PANEL 624FT HAS CORROSION. BLENDED CORROSION IAW RD 8/4-57-442, .115" REMAINING MATERIAL, ALLOWED .105", WITHIN LIMITS REF Q400 RD 8/4-57-442. TREATED AND PRIMED IAW RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RIGHT WING FUEL LANDING FOR PANEL 625AT HAS CORROSION. BLENDED CORROSION, REMAINING MATERIAL THICKNESS .081", FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: STRINGER — CORRODED (BS 509-529) · airframe 10,464 hrs · 11,347 cycles

C2 - LT STR 24 BETWEEN STA 509 - 529 HAS CORROSION AROUND FASTENERS. REMOVED RIVETS IAW SRM 51-42-05-02-01. FOUND CORROSION LIMITED TO FASTENERS ONLY. INSTALLED RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED IAW SRM 51-25-10-02-01 AND 51-25-15-02-01.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,646 hrs · 11,347 cycles

C2 - RT WING FUEL PANEL 624BT HAS CORROSION. BLENDED CORROSION, FOUND TO BE WITHIN LIMITS AND COMPLETED REPAIRS REF RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,646 hrs · 11,347 cycles

C2 - RT WING PANEL 624DT HAS CORROSION. BLENDED CORROSION, FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW BOMBARDIER RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RIGHT WING FUEL PANEL 624ET HAS CORROSION. REMOVED CORROSION REMAINING THICKNESS FOUND WITHIN LIMITS AND COMPLETED REPAIRS REF RD 8/4-57-442.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RT WING FUEL LANDING FOR PANEL 625AT HAS CORROSION. BLENDED CORROSION, MATERIAL THICKNESS REMAINING .081", FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: SKIN — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 - RT WING FUEL LANDING FOR PANEL 624ET HAS CORROSION. BLENDED CORROSION FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: SKIN — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 -RT WING FUEL LANDING FOR PANEL 624DT HAS CORROSION. REMOVED DAMAGE REMAINING MATERIAL THICKNESS .073", FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: SKIN — CORRODED (RT WING) · airframe 10,464 hrs · 11,347 cycles

C2 -RT WING FUEL LANDING FOR PANEL 624AT HAS CORROSION. REMOVED DAMAGE FOUND WITHIN LIMITS AND COMPLETED REPAIRS IAW RD 8/4-57-445.

Part: BOOT — FAILED (LEFT) · airframe 9,831 hrs · 10,714 cycles

DE-ICE PRESSURE CAUTION LIGHT WHILE BOOTS CYCLING. LT INBD TAIL INDICATOR LIGHT FLICKERED OFF AND ON AND DE-ICE PRESSURE DROPPED TO 16 PSI. FOLLOWED CHECK LIST, RETURNED TO DEPARTURE. LANDING UNEVENTFUL. INSPECTED LT INBD L/E 331AL FOUND TORN AND EMBEDDED WITH WATER. R & R L/E 331AL IAW AMM TASK 55-13-00-000/400-801. OPS TEST GOOD. AT MX CONTROL REQUEST R & R DDB NR6 IAW AMM TASK 30-11-16-000/400-801. C/W FUNCTION TEST OF DEICE SYS. INSPECTED ALL L/E BOOTS AND DRAIN AIR HOSE OF L/E 331AL FOR ANY RESIDUAL WATER. NO FUTHER DEFECTS NOTED. RETURNED TO SERVICE.

Part: BRAKE SYS — WEAK (MLG) · airframe 9,411 hrs · 10,229 cycles

BRAKES INEFFECTIVE DURING THE LANDING ROLL. PERFORMED FUNCTIONAL TEST OF MAIN GEAR BRAKING SYS IAW AMM TASK 32-42-00-720-801, OPS TEST GOOD. PERFORMED FUNCTIONAL TEST OF ANTI-SKID SYS IAW AMM TASK 32-46-00-720-802, OPS TEST GOOD. TAXIED ACFT AT VARIOUS SPEEDS, BRAKES PERFORMED NORMAL WITH ANTI-SKID SWITCH ON AND OFF. CHECKED CDS FOR FAULT CODES, NO HISTORIC OR CURRENT FAULTS IN ANTI-SKID SYS. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DISPLAY — FAILED (ZONE 200) · airframe 9,189 hrs · 9,994 cycles

"PFD 1 MON FAIL" MESSAGE ON ED. C/A FD HAS MULTIPLE FAILURES OF ALL INSTRUMENTS (RED X'S, ATT FAIL, IAS FAIL, ALT FAIL, HDG FAIL). RETURNED TO FIELD, LANDING UNEVENTFUL. INSPECTED GROUNDS FOR NR1 PFD AND NR1 ICP. ALL GROUNDS WERE SECURE. REPLACED NR1 PFD IAW TC 6316104, ALL CHECKS GOOD. ACFT CONTINUES CAT III, PLACARD READS CAT III. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (NR 1 PROPELLER) · airframe 9,133 hrs · 9,939 cycles

NR1 PROP WILL NOT UNFEATHER WITH BLEED AIR ON, UNFEATHERS WHEN BLEED SELECTED OFF. REPLACED NR1 OVERSPEED GOVERNOR IAW MM TASK 61-20-26-000-801/400-801. OPS AND LEAK CHECKS GOOD. UNFEATHER TIME SAME BLEEDS ON OR OFF. RETURNED TO SERVICE.

Part: GOVERNOR — MALFUNCTIONED (PROPELLER) · airframe 8,776 hrs · 9,548 cycles

AFTER START, WHEN CONDITION LEVERS ADVANCED TO 1020, PROP NR2 DID NOT ADVANCE OR COME OUT OF START AND FEATHER. AFTER 90 SECONDS,PLACED THE NR2 CONDITION LEVER TO START & FEATHER FOR 1 MIN. THEN ADVANCED TO 1020, THE PROP TOOK APPROX 45 SECONDS. 2ND ATTEMPT PROP TOOK APPROX 45 SECONDS TO UNFEATHER. RETURNED CONDITION LEVER TO START & FEATHER FOR 1 MINUTE. ON 3RD ATTEMPT, PROP UNFEATHERED IN APPROX 30 SECONDS. INTERROGATED CDS & FOUND NO FAULT CODES. R & R OVERSPEED GOVERNOR IAW AMM 61-20-26 PGS 401-411. LEAK CK & OPS CK GOOD. C/W H/S 61-0038. NR2 ENG UNFEATHERS IN 15 SECONDS. RETURNED TO SERVICE.

Part: PROPELLER — MALFUNCTIONED (FEATHERING) · airframe 8,764 hrs · 9,539 cycles

NR2 ENGINE TOOK LONGER THAN 30 SECONDS TO START AND FEATHER POSTION TO MIN 850 RPM. INTERROGATED CDS, FOUND NO FAULTS. PERFORMED FUNCTIONAL CHECK OF PROP TIME TO UNFEATHER ON NR2 ENG. IAW AMM TASK 61-20-00-720-801, NR2 PROP UNFEATHERED WITH IN TIME LIMITS, NO OTHER DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BRUSH BLOCK — MALFUNCTIONED (PROP DE ICE) · airframe 8,751 hrs · 9,522 cycles

"PROP DEICE" CAUTION ILLUMINATED DURING CLIMBOUT -4C LIGHT ILLUMINATES WHEN NR2 PROP DEICE COMES ON. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED CDS, FOUND FAULT CODE TMCU(14) IN TMCU2. C/W CONTINUATY CHECK OF THE PROPELLER DEICING HEATER ELEMENT IAW AMM TASK 30-61-00-760-801, FOUND DEICE WIRE HARNESS ON NR2 PROP BLADE NR1 OPEN. R & R IAW AMM 61-10-06-000-805 AND 61-10-06-400-805. DID NOT FIX PROBLEM, PERFORMED GVI OF BUS BARS, NO DEFECTS NOTED. FOUND MIDDLE SLIP RING ROUGH. IAW PROPELLER MM TASK 61-10-46 STEP1 LETTER G SUB NR (4), POLISHED MIDDLE SLIP RING AS REQUIRED. IAW MX CONTROL REQUEST R & R BRUSH BLOCK ON NR2 PROP IAW AMM 30-61-00-000-801 AND 30-61-00-400-801. ALL CHECKS GOOD. NO FURTHER CAUTIONS OR FAULTS NOTED. RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (DEFOGGER) · airframe 8,006 hrs · 8,711 cycles

AFTER ABOUT 20 MINUTES IN CRUISE FO WINDSHIELD FOGGED OVER, THEN FROZE. THERE WAS NO ASSOCIATED CAUTION LIGHT. RETURNED TO THE FIELD. LANDING UNEVENTFUL. PERFORMED ELECTRICAL RESISTANCE CHECK OF F/O WINDSHIELD IAW AMM TASK 30-41-00-760-801, CHECKS GOOD. R & R ANTI-ICE RELAYS 3041 K3 AND 3041 K4 IAW AMM TASK 30-41-01-000-802 & 30-41-01-400-802. AS A PRECAUTIONARY MESSURE R & R THE F/O'S ANTI-ICE CONTROLLER IAW AMM TASK 30-41-01-000-801 & 30-41-01-400-801. PERFORMED OPERATION TEST OF WINDSHIELD ANTI-ICING SYS IAW AMM TASK 30-41-00-710-801, OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: DOOR — STIFF (MAIN PAX) · airframe 7,155 hrs · 7,684 cycles

F/A ADVISED THAT FWD MAIN CABIN DOOR WAS DIFFICULT TO OPEN. OPERATED MAIN PAX DOOR 10 TIMES. DOOR OPERATED SMOOTHLY AND CORRECTLY. NO DEFECT NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HANDLE — STUCK (CARGO DOOR) · airframe 6,519 hrs · 6,944 cycles

F/A REPORTS MCD HANDLE DIFFICULT TO UNLATCH DOOR. OPERATED MAIN CABIN DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PIVOT — LACK OF LUBE (CABIN DOOR) · airframe 5,891 hrs · 6,215 cycles

SEA - MAIN CABIN DOOR IS STIFF TO GO DOWN. HANGS UP AT ABOUT THE HALF WAY POINT. PERFORMED GVI OF MCD FOUND NO EVIDENCE OF BINDING OR MECHANICAL PROBLEMS, LUBED ALL PIVOT POINTS ON DOOR & CHECKED OPERATION OF MECH DAMPENERS IN WARDROBE. PERFORMED OPS CHECK OF MCD IAW Q-400 AMM TASK 52-11-00-710-802. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: HYDRAULIC SYSTEM — LOW (NR 2) · airframe 5,607 hrs · 5,878 cycles

SEA - AFTER DEPARTURE NR 2 HYDRAULIC QUANTITY DEPLETED. PERFORMED ALTERNATE LANDING GEAR EXTENSION AND RETURNED TO THE FIELD. LANDING UNEVENTFUL. AIRCRAFT TOWED TO THE GATE.

Part: DOOR — STIFF (MAIN PAX) · airframe 5,555 hrs · 5,810 cycles

PDX - MAIN PASSENGER DOOR L1 (FWD) IS HARD TO OPEN. LUBED ALL HINGE POINTS ON MAIN CABIN DOOR. NO FURTHER DEFECTS FOUND. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 5,357 hrs · 5,576 cycles

COMPLY WITH PERMANENT REPAIR FOR DAMAGE TO AFT PASSENGER DOOR IAW R/D 8/4-52-452 ISSUE 1 DATED 24-MAR-09. REMOVED LOWER AND AFT LOWER CORNER SEAL RETAINERS FOR ACCESS FOR REPAIR. CUT OUT DAMAGED AREA REF TC RD8/4-52-452. HFEC IAW -8 400 NDTM PART 6, 51-00-01 AT CUTOUT. NO CRACKS NOTED. FABRICATED PACKER AND REPAIR DOUBLER, DRILLER UP, DEBURRED, COUNTERSUNK, ETCHED ALODINED AND PRIMED. INSTALLED COUNTERSINK FILLERS PER RD 8/4-52-452. INSTALLED PACKER AND DOUBLER REF RD 8/4-52-452, PRIMED AND PAINTED AND APPLIED CORROSION INHIBITING COMPOUNDS REF RD 8/4-52-452. REINSTALLED SEAL AND RETAINERS.

Part: COMPUTER — FAILED (AHRS) · airframe 4,998 hrs · 5,150 cycles

BOI - CRUISING 23000 FEET MASTER CAUTION AND "ELEVATOR FEEL" CAUTION LIGHT. AUTOPILOT DISCONNECTED ATT FAIL HDG FAIL ON FO'S PFD AND HDG FAIL ON FO'S MFD. FMS INFORMATION ON FO'S MFD DISAPPEARED. MSG ON FO'S FMS SAYING SOMETHING ABOUT AHRS 2. DIVERTED TO BOI. LANDING UNEVENTFUL. REMOVED AND REPLACED AHRU NR 2 COMPUTER, OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (PITOT TUBE) · airframe 4,965 hrs · 5,113 cycles

PDX- AFTER PUSH BACK AND AFTER PITOT HEAT ON, WE NOTICED LIGHT SMOKE BELOW AND OUTSIDE OF FLIGHT DECK WINDOWS. RETURNED TO THE GATE. APPLIED AC EXTERNAL POWER TO ACFT, INSPECTED PITOT TUBES FOR SIGNS OF DAMAGE, NONE NOTED. OPERATED PITOT HEAT FOR APPROX. 5 MINUTES, NO ABNORMALITIES NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - RT INBD CABIN SEAT TRACK IS CORRODED ON TOP SURFACE OF SEAT MOUNT LUG AT STA X36.0 BLENDED OUT CORROSION FROM TOP SURFACE OF TRACK AT AFFECTED AREA AND FOUND REMAINING THICKNESS WITHIN LIMITS PER RD 8/4-53-2358 (MAX MATERIAL REMOVED .041") GENERAL NOTES STEPS 1 AND 3. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. ALODINED AND FILLED BLEND AREA AS REQUIRED TO ORIGINAL CONTOUR IAW RD 8/4-53-2358. (STEPS 5 AND 6). CHECKED ATTACHMENTS TO SEAT RAIL REF RD 8/4-53-2358 NOTE 7, FOUND TO BE TIGHT AND SECURE WITH NO POSSIBILITY OF MOVEMENT IN ANY DIRECTION.

Part: PANEL — CORRODED (CENTER WING) · airframe 4,940 hrs · 5,081 cycles

PDX -C1- CENTER WING AFT PANELS 262AT, 262HT, 262FT MATING SURFACE ON FWD SIDE HAS FRETTING CORROSION. HFEC INSPECTED BLENDS FOR CRACKS IAW Q400 NDT6M PART 6, 51-00-000-250-801 AND STEP 3 GENERAL NOTES OF RD 8/4-53-521. NO CRACKS NOTED. PERFORMED REPAIR ON PANELS IAW RD 8/4-53-521 STEPS 1,2,4-8. THE REMAINING THICKNESS OF THE MATERIAL IS .1 INCH. PANEL FOUND TO BE WITHIN LIMITS REF RD 8/4-53-521, PG 2 AND NOTE 2 ON PAGE 4. VERIFIED CAMLOCK GRIP LENGTH, LANDING STRIP FOUND TO BE GREATER THAN .090 INCH STANDARD CAMLOCK STUD GRIP LENGTH IS ACCEPTABLE IAW RD 8/4-53-521 GENERAL NOTES 9 AND 10. INSTALLED TEFLON TAPE IN LIEU OF WET SEALANT IAW RD 8/4-53-451 GENERAL NOTES 7.

Part: SPAR — CORRODED (WING) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - FWD SPAR ATTACH FLANGE FOR PANELS 261CT AND 261LT HAS FRETTING ON OTBD ENDS. BLENDED FRETTING AT FWD SPAR ATTACH FLANGE FOR PANELS 261CT AND 261LT. REF RD 8/4-53-451 GENERAL NOTES STEP 1. HFEC INSP BLENDS FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. UT THICKNESS INSP OF BLENDS IAW Q400 NDTM PART 1, 51-00-04. PANEL 261LT HIGH .100 INCH LOW .097 INCH, PANEL 261CT HIGH .097 INCH, LOW .075 INCH. COMPLETED GENERAL NOTES 3 THRU 7 OF RD 8/4-53-451. GENERAL NOTE 8 TO BE COMPLETED ON PANEL CARD. BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-451 DETAIL L.

Part: SPAR — CORRODED (WING) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - TURTLE BACK PNL AFT SPAR ATTACH FLANGE HAS FRETTING ALONG ITS ENTIRE LENGTH. REPAIRED AFT TURTLEBACK PANEL, AFT SPAR ATTACH FLANGE ALONG ENTIRE LENGTH BY BLENDING IAW RD 8/4-53-451. MEASURED THICKNESS AND FOUND LOWEST POINT TO BE .90, FOUND FLANGE TO BE WITHIN LIMITS IAW RD 8/4-53-451. HFEC INSPECTED BLENDED AREAS FOR CRACKS IAW NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. APPLIED ALODINE AND PRIMER IAW RD 8/4-53-451. INSTALLED TEFLON TAPE IN LIEU OF FAY SEAL ALONG AFT SPAR ATTACH FLANGE IAW RD 8/4-53-451 NR 7.

Part: PANEL — CORRODED (CENTER WING) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - CENTER WING FWD PANELS 261CT, 261LT, 261HT MATING SURFACE ON AFT SIDE HAS FRETTING CORROSION. HFEC INSPECTION BLENDED AREAS FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. THIS COMPLETES STEP 3, GENERAL NOTES RD 8/4-53-521. PERFORMED REPAIR ON PANELS IAW RD 8/4-53-521 STEPS 1-8 (N/A STEP 3, PREVIOUSLY COMPLIED WITH). THE REMAINING THICKNESS OF THE MATERIAL IS 0.1 INCH. PANEL FOUND TO BE WITHIN LIMITS, REF RD 8/4-53-521, PAGE 2 AND NOTE 2 ON PAGE 4. COMPLETED STEPS 9 AND 10, RD 8/4-53-521.

Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - UPPER TCAS ANTENNA BOTH AFT NUTPLATES ARE BROKEN. REMOVED AND REPLACED TO NUTPLATES IAW DASH 8-400 SRM 51-42-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - THERE IS LIGHT CORROSION IN THE LT NR 16 SEAT TRACK BETWEEN X721 AND X743. BLENDED CORROSION ON NR 16 SEAT TRACK AT STA X721 TO X743. MAX MATERIAL REMOVED IS .0202 INCH. BLEND IS WITHIN LIMITS, REF 8/4-53-884. ALODINED BLENDED AREA ON LT NR 16 SEAT TRACK IAW Q400 RD 8/4-53-884 PG 6 NR 6. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - THERE IS LIGHT CORROSION IN RT NR 9 SEAT TRACK BETWEEN X721 AND X743. BLENDED CORROSION ON NR 9 SEAT TRACK AT STA X721 TO X743. MAX MATERIAL REMOVED IS .013 INCH. BLEND IS WITHIN LIMITS, REF RD8/4-530884. ALODINED BLEND AREA ON RT NR 9 SEAT TRACK IAW Q400 R/D 8/4-53-884 PG 6 NR 6. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - THERE IS LIGHT CORROSION IN THE RT NR 9 SEAT TRACK BETWEEN X701 AND X708. BLENDED CORROSION ON NR 9 SEAT TRACK AT STA X701 TO X708. MAX MATERIAL REMOVED IS .015 INCH. BLEND IS WITHIN LIMITS, REF RD 8/4-53-884. ALODINED BLEND AREA AT RT NR 9 SEAT TRACK IAW Q-400 RD 8/4-53-884 PG 6 NR 6. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-25-801, NO CRACKS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 4,940 hrs · 5,081 cycles

PDX - C1 - THERE IS LIGHT CORROSION IN THE LT NR 16 SEAT TRACK BETWEEN X701 AND X708. BLENDED CORROSION ON SEAT TRACK NR 16 AT STA X701 TO X 708. MAX MATERIAL REMOVED IS .020". BLEND IS WITHIN LIMITS, REF RD 8/4-53-884. ALODINED BLENDED AREA ON LT NR 16 SEAT TRACK IAW Q400 RD 8/4-53-884 PG 6 NR 6. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801, NO CRACKS NOTED.

Part: SEAL — FAILED (CARGO DOOR) · airframe 2,829 hrs · 2,804 cycles

SEA - FLIGHT 2232 (PDX-YVR) - LOSS OF PRESSURE AND CABIN PRESSURE WARNING AT 17,000 FEET. COMPLIED WITH A QUICK DESCENT AND LANDING AT SEA. FOUND A 2 INCH AREA OF SEAL MISSING FROM THE AFT CARGO DOOR. REPLACED SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,824 hrs · 2,799 cycles

PSC- FLIGHT 2222 - FLIGHT ATTENDANT AT "B" STATION REPORTED THE POSSIBLE SMELL OF SMOKE. NO VISUAL INDICATION OF ANY SMOKE. MAINTENANCE INSPECTED THE GALLEY AREA FOR SIGNS FOR SIGNS OF OVERHEATING, NONE FOUND. INSPECTED CIRCUIT BREAKERS, NONE TRIPPED AND NO SMOKE OR ELECTRICAL SMELLS NOTED. ALL GALLEY EQUIPMENT FUNCTIONS NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (ELEVATORS) · airframe 1,797 hrs · 1,723 cycles

ELEVATOR ASSYMMETRY CAUTION LIGHT ILLUMINATED IN A TURN WITH THE AUTOPILOT ENGAGED. NO ASYMMETRY OBSERVED ON PFCS INDICATOR. COMPLIED WITH CHECKLIST. ON LANDING ROLLOUT, THE LIGHT WENT OUT. MAINTENANCE COMPLIED WITH SL DH8-400-SL-27-001R1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (NR 1 GENERATOR) · airframe 1,797 hrs · 1,723 cycles

FLIGHT 2461, NR1 DC GENERATOR CAUTION LIGHT ILLUMINATED. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-30-6. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (HYD TEMP) · airframe 1,514 hrs · 1,442 cycles

SEA FLIGHT NR 2490: NR 1 HYD PUMP FAILED AND CAUTION LIGHT DURING CLIMB-OUT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE FOUND GOOD QUANTITY LEVEL IN NR 1 HYD SYSTEM. FOUND ALL 3 DPI'S AND IN AND ON THE NR 1 HYD SYSTEM. UNABLE TO DUPLICATE PROBLEM. SUSPECT NR 1 HYD RESERVOIR LOW LIMIT SWITCH. REPLACED THE NR 1 HYD RESERVOIR AND THE RESERVOIR 225 DEG F TEMP SWITCHES IAW D8-400 MM 29-11-16-000-801 AND 29-11-16-400-801 AND 29-11-00-710-807. OPS CHECK GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 1 HYD SYSTEM) · airframe 1,462 hrs · 1,390 cycles

RNO FLIGHT NR 2447: NR 1 ENGINE HYD PUMP ILLUMINATED ON CLIMB AFTER TAKEOFF. ALL HYD QTY/PRESSURE INDICATES NORMAL AFTER RUNNING CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 ENG HYD WARNING PRESSURE SWITCH IAW AMM 29-30-16-400-801. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 1,446 hrs · 1,373 cycles

SEA FLIGHT NR 2244: ON APPROACH, NR 1 ENGINE HYD PUMP CAUTION ILLUMINATED WITH A DROP OF NR 1 HYD PRESSURE TO 0. PRESSURE RETURNED TO 3000 PSI WITH SELECTION OF STANDBY HYD PUMP. CAUTION EXTINGUISHED MOMENTARILY, BUT ILLUMINATED WHEN FLAPS WERE SELECTED. MAINTENANCE REMOVED AND REPLACED NR 1 HYD SYSTEM EDP AND NR 1 ENGINE HYD NACELLE SHUTOFF VALVE. FLUSHED NR 1 HYD SYSTEM IAW Q400 AMM 29-10-00 PAGES 319-321. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 1,351 hrs · 1,270 cycles

EUG FLIGHT NR 2280: FLAP POWER CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET FLAP NUM AND PULLED C/B L7. RAN FLAPS DOWN AND UP. NO DEFECTS NOTED PER SL DH8-400-SL-27-00-2A. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 1,310 hrs · 1,234 cycles

SMF FLIGHT NR 2302: LOUD HUM WITH PTU AND STANDBY PUMP ACTIVATED. ALL PRESSURE GOOD. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE C/W Q400 AMM TASK 29-11-36-710-801 AND TASK 29-11-61-710-801. ALL TESTS NORMAL WITH NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 532 hrs · 496 cycles

SEA FLIGHT NR 2292: CABIN AUTO PRESSURIZATION CONTROL INOP. FAULT LIGHT ILLUMINATED IN AUTO MODE. FAULT LIGHT EXTINGUISHED IN MANUAL MODE PER A/C EMERGENCY CHECKLIST. ABLE TO CONTROL PRESSURIZATION MANUALLY. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURIZATION CONTROLLER IAW AMM Q400 TASK 21-31-06-000-801 AND 21-31-06-400-801. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. PLACARD REMOVED FROM LOG BOOK AND CABIN PRESSURE CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (PROPELLER) · airframe 372 hrs · 351 cycles

GEG FLIGHT NR 2393: ON START, NR 2 NH HUNG AT 16-17 PERCENT FOR SEVERAL SECONDS. THEN WAS SLOW TO ACCELERATE WHEN BROUGHT OUT OF FEATHER. 'RDC TOP' WOULD NOT ADJUST PRIOR TO RESET. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS AND FOUND FAULT CODE 968. C/W FIM TASK 73-20-00-810-821. PERFORMED FUNCTIONAL TEST OF THE PROPELLER TIME TO UNFEATHER IAW AMM 61-20-00, PG 515-516. SYSTEMS OPERATE NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (ENGINE HEAT) · airframe 117 hrs · 108 cycles

SEA - ON FLIGHT 2332, ENGINE ADAPTER HEAT 2 CAUTION LIGHT ILLUMINATED AFTER PUSHBACK. MAINTENANCE REMOVED AND REPLACED CONNECTOR. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (COMPRESSOR) · airframe 105 hrs · 94 cycles

PDX FLIGHT NR 2541: CABIN PACK HOT LIGHT ILLUMINATED WITH APU BLEED ON. PACK HOT LIGHT EXTINGUISHES WITH PACK SELECTED OFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE, AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED RT COMPRESSOR OUTLET TEMP SENSOR IAW Q400 AMM TASK 21-51-91-000-801 AND 21-51-91-400. RAN APU FOR 10 MINUTES. SELECTED APU BLEED ON. CHECKED CDS FOR FAULTS. NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (INTAKE HEAT) · airframe 101 hrs · 91 cycles

RNO FLIGHT NR 2444: ENG ADAPT HEAT 2 CAUTION LIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE AIR INTAKE WIRE HARNESS FROM WHERE THE HARNESS CONNECTS TO THE INTAKE LIP HEATER TO THE FIREWALL CONNECTOR PLUG 9811-2601. C/W OPS CHECK OF THE ENGINE AIR INTAKE ANTI-ICING SYSTEM PER Q400 AMM 30-21-00-710-801. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AUX FUEL PUMP) · airframe 30 hrs · 13 cycles

BOI FLIGHT NR 2423: AFTER ENGINE START, CREW NOTICED FUEL AUX PUMP CIRCUIT BREAKERS POPPED. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET CIRCUIT BREAKERS PER GMM 5-18-0. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.