N883EA

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 63,228 hrs · 74,123 cycles

LANDING GEAR FAILED TO EXTEND, HAD TO EXTEND MANUALLY. CREW DECLARED AN EMERGENCY. REPLACED LANDING GEAR SELECTOR VALVE.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 63,224 hrs · 74,121 cycles

CREW ATTEMPTED TO LOWER THE LANDING GEAR, RED IN TRANSIT LIGHTS CAME ON BUT NONE OF THE GEAR LOWERED. MANUAL GEAR EXTENSION PERFORMED.

Part: NONE — NONE · corrosion level 3 · airframe 62,263 hrs · 73,087 cycles

L/H SEAT TRACK ON CARGO AREA FOUND CORRODED.

Part: NONE — NONE · corrosion level 3 · airframe 62,263 hrs · 73,087 cycles

SEVERAL CORROSION SPOTS ON SKIN BTW STA X 487-510 BTW STR 31S-31P (INTERNAL).

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,606 hrs · 71,629 cycles

EMERGENCY LIGHTS ON IN ARM POSITION

Part: SKIN — DENTED (LT SPOILER) · airframe 58,757 hrs · 69,886 cycles

DENTS ON BOTTOM SKIN LT OUTBOARD GROUND SPOILER.

Part: PLATE — CRACKED (RT WING) · airframe 58,757 hrs · 69,886 cycles

CRACK ON RT WING LADDER PLATE AT YW 137.0 JUST FORWARD OF STRINGER 6. P/N: 85711069.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 55,546 hrs · 66,424 cycles

AFTER START UP A SMOKE LIGHT ILLUMINATED AND WOULD NOT GO OUT. FOUND THE NR 2 CARGO SMOKE DETECTOR STAYS IN TEST MODE. OPEN

Part: O-RING — SPLIT (HYD MANIFOLD) · airframe 54,984 hrs · 65,693 cycles

NR 1 HYDRAULIC ISOLATION VALVE LIGHT ON. FLAPS STOPPED DURING RETRACTION AT 4 DEGREES, REMOVED AND REPLACED THE 1 HYD PRESSURE MANIFOLD ASSY IAW MM 29-10-31, BLEED SYSTEM COMPLIED WITH. PERFORMED AN OPS CHECK OF THE NR1 HYD SYSTEM, OPS CHECKED GOOD. FOUND THE NR 1 SPU O-RING AT THE MANIFOLD SPLIT.

Part: STRINGER — CORRODED (BS 222) · corrosion level 2 · airframe 54,862 hrs · 65,560 cycles

CORROSION ON STRINGER 31L, BS 222.

Part: SKIN — CORRODED (BS 123-136) · airframe 54,862 hrs · 65,560 cycles

CORROSION UNDER BELLY ANTENNA.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,862 hrs · 65,650 cycles

CORRODED STRINGER.

Part: STRINGER — CORRODED (BS 167-182) · airframe 54,862 hrs · 65,560 cycles

CORROSION DAMAGE TO STRINGER 31. BLENDED AND REPAIR IAW RD8-53-15145 AND ECO008.53-17.16

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 54,862 hrs · 65,560 cycles

REPAIR FOR DENT, SCRATCH DAMAGE TO EXTERIOR LOWER FUSELAGE SKIN. REPAIRED IAW RD8-53-15090, RD8-53-15104, RD8-53-15115 AND ECO008.53-17.11

Part: SKIN — DENTED (BS 167-182) · airframe 54,862 hrs · 65,560 cycles

DENTS ON SKIN BETWEEN BS 167 - 182, ABOVE AND BELOW STRINGER 24L. REPAIRED IAW RD8-53-15109 AND ECO008.53-17.13

Part: FRAME — CHAFED (FUSELAGE) · airframe 54,862 hrs · 65,560 cycles

CHAFE DAMAGE TO LT MACHINED FRAME (P/N 85320575) AT X253.4 AND BETWEEN STR 23P & 24P. REPAIRED IAW RD 8-53-15102 AND ECO008.53-17.12.

Part: SKIN — DAMAGED (BS 277) · airframe 54,862 hrs · 65,560 cycles

DENT AND SCRATCH DAMAGE TO RT FUSELAGE SKIN, AFT AND BELOW ICE SHIELD. REPAIRED IAW RD 8-53-15089 AND ECO008.53-17-11.

Part: SKIN PANEL — DAMAGED (ELEVATOR) · airframe 54,862 hrs · 65,560 cycles

LOOSE FASTENERS AT UPPER ELEVATOR HORN TOP SKIN REPAIRED IAW RD8-553035 AND ECO008.55-17.02.

Part: DOUBLER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 54,862 hrs · 65,560 cycles

CORROSION DAMAGE TO AFT CARGO DOOR SKIN DOUBLER. REPAIRED IAW RD8-53-15082 AND ECO008.53-17.06.

Part: SKIN PANEL — DENTED (CARGO DOOR) · airframe 54,862 hrs · 65,560 cycles

DENT DAMAGE REPAIRED TO AFT CARGO DOOR IAW RD8-52-1509 AND ECO008.52-17-01

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 54,862 hrs · 65,560 cycles

DENT DAMAGE TO LT FUSELAGE SKIN. REPAIRED IAW RD8-53-15088 AND ECO 008.53-17.10.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 54,862 hrs · 65,560 cycles

DENT DAMAGE TO THE LT SIDE FUSELAGE SKIN REPAIRED IAW RD 8-53-15085 AND ECO008.53-17.09.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 54,862 hrs · 65,560 cycles

DENT DAMAGE TO FUSELAGE SKIN PANEL 85310533 STA X123 STR 24S AND 25S. REPAIRED IAW ECO 008.53-17-05.

Part: SKIN — DENTED (BS 291-312) · airframe 54,862 hrs · 65,560 cycles

DENT DAMAGE TO THE FUSELAGE SKIN PANEL BETWEEN BS 291.4 AND 312.35, STRINGER 1-2R. REPAIRED IAW RD 8-53-15073 WC 53-123.

Part: THRESHOLD — CORRODED (BS 222-253.4) · corrosion level 2 · airframe 50,173 hrs · 60,764 cycles

CORROSION AT PAX DOOR THRESHOLD. BEYOND LIMITS PART REPLACED WC 1050

Part: PANEL — CORRODED (ZONE 500) · airframe 50,173 hrs · 60,764 cycles

LEFT STRESS PANEL 521AT 9EA COUNTERSINKS CORRODED. REPAIRED IAW RD 8-57-4240.

Part: WEB — CORRODED (BS 531-600) · corrosion level 2 · airframe 50,173 hrs · 60,764 cycles

BAGGAGE FLOOR WEB CORRODED AT SEVERAL PLACES, DOUBLER WEB INSTALLED SRM REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,173 hrs · 60,764 cycles

CORROSION ON STRINGER 31P AT BS 354. SPLICED STRINGER IAW RD 8-53-2499.

Part: BOLT — CORRODED (ZONE 200) · airframe 50,173 hrs · 60,764 cycles

LT AND RT REAR SPAR WING/FUSELAGE JOINT BOLTS CORRODED. REPLACED THE BOLTS IAW AMM .

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 50,173 hrs · 60,764 cycles

RT INBD CARGO TRACK CORRODED, REWORKED THE CARGO TRACK IAW RD 8-53-784 AND 8-53-4936.

Part: FRAME SPLICE — CORRODED (BS 123-182) · corrosion level 2 · airframe 50,173 hrs · 60,764 cycles

CORROSION SPOTS UNDER COCKPIT AREA ZONE 121-122. REPAIRED CORROSION; REPLACED HORIZONTAL STIFFNER, REPLACED FRAME, REPLACED 4 FRAME LEGS.

Part: PANEL — CORRODED (ZONE 600) · airframe 50,173 hrs · 60,764 cycles

RIGHT STRESS PANEL 624AT ONE COUNTERSINK CORRODED, REPAIRED WITH A BUSHING IAW RD 8-57-2673.

Part: CARGO TRACK — CORRODED (BS 531-600) · corrosion level 2 · airframe 50,173 hrs · 60,764 cycles

LT INBD CARGO TRACK CORRODED. REPLACED THE CARGO TRACK IAW WC 1062 RD 8-53-4472

Part: GENERATOR — DEFECTIVE (NR 1) · airframe 49,700 hrs · 60,297 cycles

NUMBER 1 AC GEN CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF EJECTED. R & R NR 1 AC GENERATOR IAW DHC-8 PPBM 71-00-02. OPERATIONS & LEAK CHECKED GOOD. OK FOR SERVICE.

Part: INVERTER — FAILED (ZONE 100) · airframe 49,277 hrs · 59,867 cycles

DURING PREFLIGHT WITH ENGS COLD 1ST OFFICER NOTED ELEC SMOKE ON THE FLIGHT DECK & HEARD 115 VOLT BUSS TIE CB POP. FOUND SECONDARY INVERTER BURNT UP. REPLACED INVERTER & GND TESTED GOOD.

Part: ACTUATOR — CRACKED (SPOILER) · airframe 49,155 hrs · 59,753 cycles

NUMBER 1 HYD ISO VLV, ROLL SPOILER INBD, FLAP POWER CAUTION LIGHTS WITH LESS THAN MIN NR 1 HYD FLUID. FLAPS REMAINED AT 5 DEGREES. FOUND RT INBD ROLL SPOILER ACTUATOR HOUSING CRACKED. R & R INBD ROLL SPOILER ACTUATOR IAW MM 27--14-05. RIGGING NOT AFFECTED, OK FOR SERVICE.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 48,958 hrs · 59,556 cycles

HYDRAULIC FLUID LEAKING FROM DRAIN HOLES ON WING FLAP FAIRINGS WITH NR 2 ENG RUNNING. R & R LT OTBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. RIGGED IAW 27-14-00. LEAK & OPS CHECKED GOOD.

Part: WIRE — DAMAGED (RT WING) · airframe 48,942 hrs · 59,543 cycles

SPOILER 2 PUSH OFF SWITCH LIGHT CAME ON IN FLIGHT. VERIFIED PROBLEM ON RT WING BY DISCONNECTING 2700-P4 & THEN 9811-J172, IT WENT AWAY. RAN NEW WIRE FROM 9811-J172 TO 2762-S6 TO E2 REPLACED. GND TEST GOOD IAW MM 27-19-00.

Part: AHRS — INACCURATE (NR 1) · airframe 48,336 hrs · 58,900 cycles

NR 1 ADI SHOWING INCORRECT PITCH & ROLL INFORMATION. ADI PITCH & ROLL MISMATCH MESSAGES DISPLAYED ON 802 DISPLAY. R & R NR 1 AHRU IAW 34-20-06, OPERATIONS NORMAL.

Part: ROD END — OUT OF ADJUST (MLG DOOR ACT) · airframe 47,302 hrs · 57,907 cycles

LEFT GEAR DOOR INTERMITTENTLY STAYS OPEN ON GEAR RETRACTION. ADJUSTED LEFT FWD GEAR DOOR ACTUATOR ROD END IAW MM 32-10-36. GEAR SWING C/W IAW MM 32-30-00. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,300 hrs · 57,897 cycles

F/A REPORTED ODOR OF "HOT OIL" ON DECENT. INSPECTED IAW FAULT ISOLATION 72-00-02. ENGINE OIL LEVELS CHECKED GOOD, NO STANDING OIL NOTED. ACM LEVELS CHECK OK. RAN UP NR 1 AND NR 2 ENGINE BLEEDS ON. NO DEFECTS NOTED, COULD NOT DUPLICATE. OK FOR SERVICE AT THIS TIME.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 47,196 hrs · 57,797 cycles

EMEGENCY LIGHTS INOPERATIVE AT SIDE KICK PANELS AT ALL EMERGENCY EXITS. R & R NR 3 POWER SUPPLY UNIT AS REQUIRED WITH AN INSPECTED UNIT. OPS CHECKED GOOD. WORK DONE IAW MM SECTION 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,186 hrs · 57,787 cycles

EMERGENCY LIGHTS NOT ILLUMINATED. R & R BATTERY PACK AT STA X500. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF RIG (LT MLG DOOR) · airframe 47,156 hrs · 57,760 cycles

LT MAIN GEAR DOOR CAUTION LIGHT STAYED ON WITH GEAR RETRACTION. VISUALLY CHECKED GEAR DOOR WAS OPEN. COMPLIED WITH TROUBLESHOOTING IAW MM SECTION 32-00-00. RIGGED UPLOCK PROXIMITY SENSOR IAW SECTION 32-30-26. OPS CHECK ON GROUND FOUND GOOD. OPS CHECK FLIGHT PERFORMED GEAR DOOR FLIGHT CHECKS GOOD.

Part: BRACKET — CRACKED (NLG) · airframe 46,703 hrs · 57,329 cycles

NLG UPLOCK ACTUATOR ATTACH BRACKET CRACKED. REMOVED FITTING, REINSTALLED BRACKET IAW RD 8-53-3805. OK FOR SERVICE.

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 46,689 hrs · 57,315 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. R & R BATTERY 3351P2 IAW MM 33-52-00. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 42,738 hrs · 55,290 cycles

LEFT FWD EXTERIOR EGRESS EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR DISCONECTED AND WIRE DISCONNECTED FROM CONNECTOR SOCKET. INSTALLED NEW SOCKET, CONNECTED CONNECTORS IAW MM 20-45-09 CHECKED NORMAL. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,717 hrs · 56,379 cycles

NUMEROUS EMERGENCY EXIT LIGHTS INOP AT ALL EXITS (LOWER LIGHT ASSEMBLY). REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHTS. OPS CHECK OK. REFERENCE DASH 8 MM 33-52-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

CORROSION FOUND ON RIGHT INBOARD SEAT TRACKS BETWEEN SAT X182 AND X 262. REPLACED TRACK REF BOMBARDIER RD 8-53-3074.

Part: RIB — WORN (LT ELEVATOR) · airframe 45,706 hrs · 36,380 cycles

SMOKING RIVETS FOUND ON UPPER SURFACE OF LEFT ELEVATOR HORN. TOP SKIN AND RIB REPLACED REF BOMBARDIER SRM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,706 hrs · 36,380 cycles

CORROSION FOUND ON LEFT FLOOR STRUCTURE AT X597.5. MAIN FITTING, STIFFENER ANGLE THREE BRACKETS REPLACED REF BOMBARDER SRM. PNS 85331059-101, 85331060-101, 85331060-101, 85331064-101, 85331063-107, 85331150-103, 85334438-101.

Part: FLOOR SUPPORT — CORRODED (BS 597.5) · corrosion level 2 · airframe 45,706 hrs · 36,380 cycles

CORROSION FOUND ON LEFT FLOOR STRUCTURE AT BS 597.5. MAIN FITTING, STIFFENER, ANGLE LOWER SILL THREE BRACKETS LOWER MAIN SILL REPLACED IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

2 WEB FOUND CRACKED ON RIGHT AFT CARGO AREA BETWEEN X600 AND X 618 AND BETWEEN X 618 AND X 636. REPLACED WEB STRUCTURE REF BOMBARDIER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

CRACK FOUND ON FRAME AT SAT X136 NEAR OF STR 15A ON THE RT SIDE. REMOVED AND REPLACED FRAME REF BOMBARDIER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,706 hrs · 36,380 cycles

CORROSION ON LT INBD SEAT TRACKS BETWEEN STATION X182 AND X262.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

CRACK FOUND ON FRAME STA X136 NEAR STR 15A ON THE LT SIDE. REPLACED FRAME REF BOMBARDIER SRM.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 45,706 hrs · 36,380 cycles

PAX DOOR SHELL LOWER ATTACHMENT CHAFED. LOWER ATTACH BRACKET REPAIRED REF BOMBARDIER RD 8-52-647.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

DENT FOUND ON LEFT FUSELAGE SKIN AT SAT X690 BTW STR 2P - 3P. REPAIRED SKIN AND FRAME REF BOMBARDIER RD 8-55-2493.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 45,706 hrs · 36,380 cycles

CORROSION FOUND ON FUEL PANEL 524AT AND BT. REMOVED CORROSION REF BOMBARDIER RD 8-57-320.

Part: SKIN PANEL — WORN (PAX DOOR) · airframe 45,706 hrs · 36,380 cycles

PAX DOOR SHELL LIP WORN AT LOWER SECTION FWD AND AFT. BLENDED DAMAGE REF BOMBARDIER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,706 hrs · 36,380 cycles

CORROSION AT FUSELAGE STRINGER 29P BETWEEN X291 AND X312. REMOVED CORROSION AND REPAIRED REF BOMBARDIER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,703 hrs · 56,374 cycles

CRACK FOUND ON LEFT WEB OF WING TO FUSELAGE FAIRING AT STA.X370.8. REPAIRED IAW BOMBARDIER REPAIR DRAWING RD8-53-12831 ISS. 2

Part: RIVET — LOOSE (FUSELAGE) · airframe 45,706 hrs · 36,380 cycles

RIVETS FOUND LOOSE ON FUSELAGE TOP SKIN AT STATION X240, X 253 AND X312 BETWEEN 3P AND 3S REV BOMBARDIER SRM.

Part: ANGLE — CORRODED (AIRSTAIR DOOR) · airframe 45,706 hrs · 36,380 cycles

AIRSTAIR DOOR LOWER INTERNAL ANGLES, FWD AND AFT CORRODED. ANGLES REPLACED REF AMM. LT AND RT ANGLES REPLACED P/N 85210301-101 AND 85210301-102.

Part: SKIN PANEL — DENTED (LT WING) · airframe 45,706 hrs · 36,380 cycles

LEFT WING LOWER SKIN DENT FOUND AT SAT YW290. HFEC AND UT INSP NO DISBONDS OR CRACKS. DENT ALLOWABLE WITHIN LIMITS REF BOMBARDIER RD 8-57-5779. LOCATION UW290 - YW297 BETWEEN STR 15 - 16.

Part: PUMP — CORRODED (LT WING) · airframe 45,706 hrs · 36,380 cycles

EXTERNAL SURFACE OF BOTH FUEL PUMPS HAVE SURFACE CORROSION. REPAIRED BY BLENDING OUT CORROSION REF BOMBARDIER RD 8-57-1907.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · airframe 45,706 hrs · 36,380 cycles

PAX DOOR LOWER INTERNAL ANGLES, FWD AND AFT CORRODED. ANGLES REPLACED REF AMM. LT AND RT ANGLES REPLACED 85210301-101 85210301-102.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,868 hrs · 55,575 cycles

WHILE PERFORMING TASK CARD 5310/08A(1) FUSELAGE OUTER FRAME AT STATION 333.30 6L AND 6R WERE FOUND TO HAVE A CRACK EMINATING FROM THE LAST OUTBOARD RIVET. THE REPAIR WAS ACCOMPLISHED IAW RD8-53-4811 A GENERIC LOOSE ANGLE REPAIR FOR THE FUSELAGE FRAMES.

Part: AHRS — DEFECTIVE (NR 2) · airframe 44,539 hrs · 55,226 cycles

YD KICKED OFF FOLLOWED BY ADI PITCH MISMATCH FOLLOWED BY HEADING MISMATCH ALL ON NR 2 SIDE. REMOVED AND REPLACED NR 2 AHRS, OPS TEST GOOD IAW DHC-8 MM 34-20-06.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 44,236 hrs · 54,865 cycles

NR 2 TORQUEMETER INOP, ABORTED TAKEOFF DUE TO ERRONEOUS TORQUE READING. REMOVED AND REPLACED NR 2 ENGINE TORQUE INDICATOR. OPS CHECK GOOD. REFERENCE AMM 77-10-00.

Part: ACTUATOR — DEFECTIVE (LT MLG DOOR) · airframe 43,486 hrs · 54,073 cycles

LEFT GEAR DOOR LIGHT STAYED ON AFTER GEAR SELECTED UP/ RECYCLED AND LIGHT STAYED ON. REMOVED AND REPLACED LT MLG FWD DOOR ACTUATOR IAW DASH 8 PSM 1-8-2 CH 32-101-36 LEAK AND OP CHECKED GOOD AT GEAR SWING. AIRCRAFT RELEASED FOR PROVISIONAL FLIGHT CHECK OF LANDING GEAR RETRACTION SYSTEM. GEAR CYCLED 4 TIMES NO DEFECTS NOTED.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 43,208 hrs · 53,764 cycles

LEFT STALL WARNING ILLUMINATED IN FLIGHT MOMENTARILY. PULLED AND RESET STALL WARNING CIRCUIT BREAKERS VERIFIED STALL WARNING CAUTION LIGHT NOT ILLUMINATED ON GROUND. SEE FLIGHT LOG 259108 FOR OPERATIONAL CHECK FLIGHT AS DIRECTED BY MAINTENANCE. FLIGHT LOG 259108 OPERATIONAL CHECK FLIGHT-STALL WARNING SYSTEM FLIGHT CHECKS GOOD.

Part: TRANSDUCER — INTERMITTENT (STALL WARNING) · airframe 43,143 hrs · 53,701 cycles

LEFT STALL WARNING CAUTION LIGHT ILLUMINATED ON ROTATION. REPLACED LEFT LIFT TRANSDUCER AND CALIBRATED/OPS CHECKED IAW MAINTENENCE MANUAL 27-33-00.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 40,900 hrs · 51,243 cycles

(V0XR) WEAR AROUND EDGES OF AFT HOLE IN CO-PILOTS RT SEAT TRACK EXCEEDS 0.028 INCHES. ACCOMPLISHED RD 8-53-11684.

Part: DIAPHRAGM — CRACKED (RT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) DIAPHRAGM AND CHANNEL ON RT THUMBNAIL REQUIRES REPLACEMENT DUE TO CRACKS. REPLACED DIAPHRAGM P/N A23837-1 AND CHANNEL P/N A23840-1 ON RT THUMBNAIL IAW DHC8-100 SRM 51-10-00, 51-40-11.

Part: STIFFENER — CRACKED (LT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) STIFFENER AT O/B YN 3.75 AND XN 169-244 HAS CRACKED OUT HOLES. FABRICATED STIFFENER AND INSTALLED AT YN 3.75 AND XN 169-244, LT NACELLE IAW DHC8-100 SRM 51-40-205, 51-40-07, 51-20-36 AND DRAWING 85410739.

Part: ANGLE — CRACKED (RT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) RT THUMBNAIL O/B FWD RT ANGLE CRACKED. REPLACED O/B FWD RT ANGLE ON RT THUMBNAIL IAW DASH8-100 SRM 51-40-11 AND 51-10-00.

Part: SKIN PANEL — CORRODED (RT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) SKIN LOCATED BELOW RIGHT FINGERNAIL FOUND TO BE CORRODED BEYOND LIMITS. REPLACED SKIN PER DASH8-100 SRM 51-10-00, 51-40-00, 51-40-11. FABRICATED PARTS FROM DASH8-100 DRAWINGS FOR STIFFNER RIBS.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) STRINGER IN LT NACELLE HAS A CRACK AT AFT END I/B STA YN6, XN 169.9 TO XN 206.0. REPLACED STRINGER IN LT NACELLE I/B AT YN6 FROM XN 169.9 TO XN 206 IAW DHC8-100 SRM 51-10-00, 51-40-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) PAX DOOR SILL IS CORRODED. REMOVED AND REPLACED PAX DOOR SILL IAW DHC-8/100 SRM 51-42-05, 51-40-11, 51-20-00, 51-10-00, 51-40-07.

Part: SKIN PANEL — CORRODED (LT NACELLE) · airframe 40,900 hrs · 51,243 cycles

(V0XR) SKIN LOCATED BELOW LEFT FINGERNAIL FOUND TO BE CORRODED BEYOND LIMITS. REPLACED CORRODED SKIN (HEAT SHIELD) WITH NEW PART IAW DASH 8-100 SRM 51-42-05, 51-40-11, 51-10-00, 51-40-07, 51-20-16, 51-20-36. W/C 4177

Part: SOLENOID VALVE — SEPARATED (MLG DOOR) · airframe 37,437 hrs · 47,111 cycles

ADQ - COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM FLUID QUANTITY. PERFORMED ABNORMAL PROCEDURES CHECKLIST AND RETURNED TO ADQ. MAINTENANCE ARRIVED ADQ REMOVED AND REPLACED NR 1 MAIN GEAR DOOR SOLENOID SEQUENCE VALVE IAW DASH 8 MAINTENANCE MANUAL 32-10-51. CLEANED NR 1 MAIN LANDING GEAR OF HYDRAULIC FLUID. REMOVED UNIT HAD TWO OF FOUR BOLTS THAT HOLD THE SOLENOID AND VALVE TOGETHER SHEAR, ALLOWING THE SOLENOID TO SEPARATE FROM THE VALVE.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 35,864 hrs · 45,043 cycles

CORROSION ON KEELBEAM, STR 31P, FS 222.7 AND 222.7. CORROSION ON KEEL BEAM ,STR 31P, FS 222.7 AND 252.7, BLENDED IAW RD 8-53-10403. FOUND TO BE WITHIN LIMITS OF RD 8-53-10403.

Part: ACTUATOR — CRACKED (MLG) · airframe 33,932 hrs · 42,340 cycles

NR 2 HYD SYSTEM PRSR DROPPED TO ALMOST ZERO UPON GEAR EXTENSION. LOUD BANG & NR 2 HYD ISO VALVE CAUTION LIGHT AND OUTBOARD ROLL SPOILER LIGHT ILLUMINATED. LEFT MLG RETRACT ACTUATOR HOUSING CRACKED. REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR.

Part: PCU — INOPERATIVE (RT ENGINE)

NR 2 PROPELLER SURGED ON FINAL TO FAIL TWICE, THEN DROPPED TO 1000 RPM FROM 1180 ON ROLLOUT. FEATHERED MOMENTARILY TO 300 RPM THEN BACK TO 900 RPM. REVIEWED DFDR DATA FOR OVER-TORQUE PARAMETERS. REPLACED NR 2 PCU SN 921069. NR 2 PROPELLER HYDRAULIC PUMP, SN2246874, AND NR2 OVERSPEED GOVERNOR SN 2246442. ENGINE GROUND OPERATIONAL CHECK GOOD. FERRIED AIRCRAFT, NR 2 PROPELLER CHANGED FOR OVERHAUL INSPECTION DUE TO OVER-TOUQUE. (K)