N794CP

Part: DITCHING DAM — STIFF (ZONE 200) · airframe 31,887 hrs · 32,553 cycles

DITCHING DAM AT FORWARD PASSENGER DOOR IS DIFFICULT TO DEPLOY. AFT EDGE OF DAM CATCHES ON OVERHEAD BIN. ADJUSTED END CAP OF OVERHEAD BIN BEHIND DITCHING DAM TO CREATE MORE CLEARANCE FOR OPERATION OF DAM. OPS CHECKS GOOD.

Part: WIRE HARNESS — MISROUTED (ZONE 100) · airframe 31,631 hrs · 32,401 cycles

PILOT WAS UNABLE TO MAKE LEFT RUDDER INPUT DURING TAXI FOR DEPARTURE. AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE PERFORMED INSPECTION OF THE PILOT AND COPILOT'S RUDDER CONTROL CABLES/HARDWARE. FOUND COPILOTS LH RUDDER PEDAL PUSH RODS AND BELL CRANK WAS CATCHING ON WIRE HARNESS FOR COCKPIT TEMPERATURE SENSOR. REPAIRED AND ADJUSTED WIRE HARNESS TO BE CLEAR OF ALL RUDDER CONTROLS, COMPLETED RUDDER CONTROL SYSTEM FUNCTION TEST AND NO DEFECTS NOTED.

Part: UNKNOWN — CRACKED (ZONE 200) · airframe 31,438 hrs · 32,296 cycles

CRACK DAMAGE TO UPPER CHANNEL OF RH WING TO FUSELAGE (ARMPIT) FAIRING SUPPORT STRUCTURE AT STA X400 AND Z173.0.

Part: SELECTOR VALVE — STUCK (MLG) · airframe 30,579 hrs · 31,818 cycles

MANUAL GEAR EXTENSION DOOR WILL NOT FULLY OPEN. CLEANED AND LUBRICATED EXPOSED SURFACE OF THE SELECTOR VALVE. OPS CHECKS GOOD. NOTE THE OAT WHEN THIS HAPPED WAS 6 DEGREES FAHRENHEIT, SO COULD ALSO BE COLD RELATED SINCE THE AIRCRAFT WAS MOVED INTO A HEATED HANGAR FOR TROUBLESHOOTING.

Part: NONE — CHAFED (ZONE 600) · airframe 30,535 hrs · 31,796 cycles

CHAFING DAMAGE ON RH INBOARD FLAP, OUTBOARD WING TANK CAN (P/N 85714630-004. DAMAGE IS BEYOND MANUFACTURES LIMITS; PART REQUIRES REPLACEMENT.

Part: STRINGER FITTING — CORRODED · airframe 30,535 hrs · 31,796 cycles

STRINGER FITTING WITH CORROSION DAMAGE AND HOLE ELONGATION BEYOND MANUFACTURES PUBLISHED LIMITS.

Part: NONE — CRACKED · airframe 30,535 hrs · 31,796 cycles

LH NACELLE EXHAUST SHROUD SPRING CLIPS CRACKED AT 2 LOCATIONS (P/N 8Z9029-103). CRACKS ARE OUTSIDE OF MANUFACTURES LIMITS REQUIRING PART REPLACEMENT.

Part: INTERCOSTAL — CORRODED (BS 100-116 S24R) · airframe 30,535 hrs · 31,796 cycles

CORROSION DAMAGE ON STRINGER INTERCOSTAL AT STATION X100.800 - X116.00 STRINGER 24S. DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS.

Part: FRAME — CORRODED (ZONE 100) · airframe 30,535 hrs · 31,796 cycles

CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. DAMAGE IS BEYOND MANUFACTURES PUBLISHED LIMITS. DAMAGE AT STA. X32.400 STRINGERS 30P AND 30S. PART NUMBERS ARE 85329152-103 (LH) / 85329256-101 (RH)

Part: DOOR FRAME — DAMAGED (FWD CARGO) · airframe 30,535 hrs · 31,796 cycles

SCORING DAMAGE O THE FORWARD BAGGAGE DOOR AFT FRAME THAT IS BEYOND MANUFACTURES LIMITATIONS.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 30,535 hrs · 31,796 cycles

CORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. CORROSION ON FORWARD WARDROBE SUPPORT STRUCTURE. 11.4" AFT OF STA. -18.250 AND 2.85" FORWARD OF STA. 1.0.

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,535 hrs · 31,796 cycles

CORROSION DAMAGE BEYOND MANUFACTURER’S PUBLISHED LIMITS. CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. PN: 85329152-103(LH) AND 85329256-101(RH).

Part: NONE — CORRODED (ZONE 100) · airframe 30,535 hrs · 31,796 cycles

GOUGE DAMAGE PAST MANUFACTURER LIMITS ON LOWER RH FUSELAGE SKIN PN 85337133-109.

Part: NONE — CORRODED (ZONE 100) · airframe 30,535 hrs · 31,796 cycles

CORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. RH LOWER FRAME AND SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 10.5-39) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

REFERENCE KF AERO WO. 1000072826. FLOOR RAIL AT STA. X-39.00 TO 10.5 STR. 23 RBL 8 CORRODED BEYOND LIMITS. FLOOR RAIL WAS REPLACED WITH NEW PURCHASED PART IAW Q400 SRM 53-20-49 REV. 19. FLOOR RAIL P/N 85328210-121.

Part: STRINGER SPLICE — CORRODED (FRAMES 32-47) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

REFERENCE KF AERO WO. 1000074504. STRINGER SPLICE AT STA. X32 – X47 LH STR. 31 IS CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW STRINGER SPLICE IAW DHC-8-400 SRM 51-42-05 REV. 19.

Part: STRUCTURE — CORRODED (FRAME 32) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

CORROSION ON Z SECTION AT STA. X32 LBL 38 UNDER FLOOR US BEYOND LIMITS. Z SECTION REPLACED WITH MANUFACTURED PART IAW DHC-8-400 SRM 53-20-43, ITEM 211, AND 51-24-35 REV. 19. INSTALLED Z SECTION FOLLOWING SRM REV. 19 SECTION 51-42-05.

Part: FUEL LINE — OUT OF POSITION · airframe 28,477 hrs · 30,583 cycles

FUEL PIPE TOO CLOSE TO STRUCTURE AT 2 PLACES, LT YW 8.68 AND 25.265 IAW AMM PART 2, PSM 1-84-2 SECTION, 28-10-00-280-811, SUBTASK 28-10-00-210-019 (B). FUEL LINE ADJUSTED CLAMPS TO ALLOW FOR PROPER CLEARANCE IAW Q400 AMM 28-11-06 REV. 67.

Part: BRACKET — CRACKED (LEFT NACELLE) · airframe 28,477 hrs · 30,583 cycles

REPLACE BROKEN AND CRACKED LT PYLON BRACKET FWD OF O/B LUG FITTING YW STA. 155.20. REPLACED WITH NEW IAW DRAWING NO. 85404001 REV. A AND SRM 51-42-05 REV. 19.

Part: BRACKET — CORRODED (L1 DOOR STEP) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

REFERENCE WO. 1000076529. CORRODED MOUNT BRACKET REQUIRES REPLACEMENT AT FORWARD SIDE OF STAIRS L1 DOOR. BRACKET PN: 85217097-101 REPLACED IAW DHC-8-400 SRM 51-10-00 PARAGRAPH 2 SECTION 3 REV. 19 AND SRM 51-41-05.

Part: MOUNT FITTING — CRACKED (L1 DOOR) · airframe 28,477 hrs · 30,583 cycles

CRACKED DOOR SHELL MOUNT FITTING ON L1 DOOR STAIRS. FITTING REPLACED WITH NEW IAW SRM 51-10-00, PARAGRAPH 2, SECTION 3, REV 19, AND SRM 51-41-05.

Part: STRINGER CLIP — CORRODED (BS 47) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

STRINGER CLIP AT BS 47 STRINGER 30L BELOW FLOOR WAS CORRODED. THE STRINGER CLIP WAS REPLACED IAW SRM 51-10-00-00-01, SECTION 2, SUB SECTION 3, RE. 19.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 28,477 hrs · 30,583 cycles

REFERENCE WO. 1000078407. REPLACED BROKEN/CRACKED RH PYLON BRACKET FORWARD OF O/B LUG FITTING IN ACCORDANCE WITH DHC-8-400 SRM 51-10-00 PARAGRAPH 2 SECTION 3 REV. 19 AND SRM 51-42-05-02-01 REV. 19 PART REPLACED WITH NEW BRACKET PART NUMBER 82454318-102.

Part: FITTING — CORRODED (LAVATORY FLOOR) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

EXFOLIATION CORROSION ON FWD LAV FLOOR AT DOOR ENTRYWAY (SILL PLATE FLOOR FITTING). REPLACED EXTRUSION ON FLOOR AT DOOR ENTRYWAY. PART NUMBER 9701029-5. WORK ACCOMPLISHED IAW Q400 SRM 51-41-00 REV. 19.

Part: SCUFF PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

FWD BAGGAGE DOOR HAS CORROSION IN SILL AREA THAT IS BEYOND MANUFACTURES LIMITS. FABRICATED AND INSTALLED REPLACEMENT PART AT STA. 32 - 41 RH SIDE FOLLOWING BOMBARDIER DRAWING #85329381 REV. C.

Part: SCUFF PLATE — CORRODED (BS 697.6) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

CORROSION UNDER DOOR SCUFF PLATE L2 DOOR STA. 697.600 STR. 23. REMOVED CORROSION AND REMAINING THISCKNESS IS BEYOND LIMITS IN SRM. SCUFF PLATE REPALACED WITH NEW MANUFACTURED PN: 85339540.

Part: SUPPORT — CORRODED (BS 783) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

CORROSION BEYOND ALLOWABLE LIMITS ON AFT CARGO SILL PIECE CONNTECTED TO AFT 1 FRAME STA. X783.102 STR. 24. FABRICATED AND INSTALLED REPLACMENT PART FOLLOWING Q400 SRM 51-15-00 PARA B. REV. 19

Part: SUPPORT — CORRODED (BS 783) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

CORROSION FOUND ON FLOOR STRUCTURE BS 783, LBL 20, IN THE AFT CARGO BAY, WAS FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM. INSTALLED NEW PARTS IAW SRM REV. 19 51-41-00-00-01 AND 51-42-02-01.

Part: SEAT TRACK — CORRODED (BS 216-584) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

SEAT TRACK IN THE MAIN CABIN BS 216 +10 - 584.5 +10, LBL 9.25 WAS FOUND CORRODED OUT OF SRM LIMITS. REPAIRED IAW SRM 51-40-10, 51-40-15, AND 51-42-05, REV. 19.

Part: STIFFENER — CRACKED (ACCESS PANEL) · airframe 28,477 hrs · 30,583 cycles

CRACKS ON STIFFENERS (X3) ON BODY ACCESS PANEL #262AT. REPLACED WITH NEW FABRICATED PARTS IAW Q400 SRM 51-42-05 AND 51-24-35 REV. 19 AND DHC DWG. # 85357339 REV. A.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

LIGHT CORROSION ON SEAT TRACK RAIL (FLOOR RAIL) FS 10.5 TO FS 102.5 RBL 9.25. FOUND CORROSION BEYOND LIMITS IAW Q400 SRM. REPLACED FLOOR RAIL WITH NEW PART.

Part: SCUFF PLATE — CORRODED (BS 697) · corrosion level 2 · airframe 284,777 hrs · 30,583 cycles

CORROSION UNDER DOOR SCUFF PLATE L2 DOOR STA. 697.600 STR. 23 ON MULTIPLE FASTENENR HOLES. CORROSION BEYOND SRM LIMITS, REPLACEMENT REQUIRED.

Part: ANGLE — CORRODED (BS 783) · corrosion level 2 · airframe 28,477 hrs · 30,583 cycles

CORROSION ON FLOOR STRUCTURE STA 783 LBL 20 AFT CARGO PIT. PART REPLACEMENT REQUIRED.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 28,477 hrs · 30,583 cycles

CRACKS ON STIFFENERS EXTENDING FROM END FASTENERS ON FUSELAGE TO BODY ACESS PANEL 262HT.