N349PH
Registered owner: BAM LEASING LLC, MD (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
220 reports on file, 1998-03-21 – 2008-10-30.
Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 25,358 hrs · 36,682 cycles
PDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3/4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN. REPLACED CRACKED NOSE GEAR DOWN LINE, CHECK GOOD. PERFORMED EDP HYD FLUID LOSS INSP IAW MM 05-50-33-280-801, NO DEFECTS. CLEANED AIRCRAFT AND INSTALLED NEW SEAT COVERS, OVERHEAD BINS, PSU'S, AND OTHER INTERIOR EQUIPMENT AS REQUIRED. RETURNED TO SERVICE.
Part: PRESSURE SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 25,358 hrs · 36,682 cycles
PDX- NR 2 ENG HYD PUMP CAUTION ILLUMINATED. CAUTION REMAINED ILLUMINATED THROUGHOUT LANDING. TAXI AND PARKING. NO LOSS OF HYD PRESS OR QTY. PERFORMED ALTERNATE GEAR EXTENTION. UNEVENTFUL LANDING. REMOVED AND REPLACED NR 2 HYD PRESSURE SWITCH, GROUND RAN NR 2 ENGINE. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.
Part: SWITCH — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 24,683 hrs · 35,662 cycles
PDX - FLIGHT 2193, AUTOFEATHER ARM LIGHT FLICKERING AND SHOWING AS "ARM" WITHOUT THE BUTTON BEING SELECTED. DURING CLIMB AND CRUISE. MAINTENANCE REPLACED THE AUTOFEATHER SELECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SERVO — INOPERATIVE (NR 1 ENGINE) · airframe 24,187 hrs · 34,879 cycles
PDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND NR 1 ENGINE IBV SERVO INOPERATIVE, REMOVED AND REPLACE IBV SERVO COMPLETED GROUND RUNS, ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FLAP TRACK — DAMAGED (TE FLAPS) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD FLAP AREA NR 5 FLAP TRACK. THERE ARE TWO ROLLER CHAFE AREAS ON THE UPPER SURFACE. MAINTENANCE BLENDED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X330. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (BS 447-457) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK NR 5 X447 TO X457 IS GOUGED. MAINTENANCE BLENDED OUT GOUGE ON SEAT TRACK, INSPECTED AND REMAINED WITHIN LIMITS, NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (BS 520-522) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SUSPECT CORROSION AROUND 2 SKIN RIVETS X520 TO X522 BELOW SEAT TRACK NR 2. MAINTENANCE REMOVED RIVETS, BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - NUTPLATE AND MOUNTING SURFACE AT STA X599.00 Y21.00 LT IS CORRODED. MAINTENANCE REMOVED NUTPLATE AND REMOVED CORROSION. INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER, AND PAINT. INSTALLED NEW NUTPLATE.
Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK LOWER SIDE THERE ARE TWO AREAS OF ROLLER CHAFE DAMAGE WITH PITTING CORROSION IN BETWEEN. MAINTENANCE BLENDED OUT CHAFE AND PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.
Part: SEAT TRACK — GOUGED (BS 476-486) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X476 TO X 486. MAINTENANCE BLENDED OUT GOUGE. INSPECTED, REMAINED WITHIN LIMITS AND NO CRACK NOTED. RESTORED FINISH TO REPAIR AREA.
Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SUPPORT ANGLE AT APPROX STA X600.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE.
Part: SKIN — CORRODED (FUSLEAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - LAV SERVICE DOOR APERATURE AFT LOWER CORNER CORRODED AROUND FASTENER. MAINTENANCE REMOVED LAV SERVICE DOOR CUT OUT DAMAGED AREA, FABRICATED REPAIR PACKER AND BACKING PLATE AND INSTALLED PACKER AND BACKING PLATE.
Part: SEAT TRACK — CORRODED (BS 468) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK NR 5 AT X468 HAS 2 CORROSION PITS ON INNER FLOORBOARD FLANGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: SKIN — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - X534 AND STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION AT CLIP, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. INSTALLED NEW RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (BS 310) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - NR 4 SEAT TRACK HAS CORROSION AT CAMLOCK RECEPTACLE UNDER DRIP TRAY AT STA X240. MAINTENANCE REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK.
Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK INBOARD SIDE LOWER SURFACE OF UPPER FLANGE. THERE IS PITTING CORROSION AT ROLLER CONTACT AREA. MAINTENANCE BLENDED OUT THE PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.
Part: SEAT TRACK — CORRODED (BS 496) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK NR 11 AT X496 HAS A CORROSION PIT ON TOP ANGLE. MAINTENANCE BLENDED OUT THE CORROSION, INSPECTED, REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Part: BRACKET — CRACKED (LT WING) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - LT WING INBOARD LEADING EDGE LOWER OUTBOARD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACE LEADING EDGE BRACKET.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - NR 2 SEAT TRACK HAS VERY LIGHT PITTING IN THE CHANNEL AT APPROXIMATELY X488. MAINTENANCE BLENDED THE PITTED AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - X468 AND STRINGER 31R SUSPECT CORROSION AT CLIP EDGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Part: SKIN — DENTED (RUDDER) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - FORE RUDDER HAS A 1/4 BY 1/2 DENT ON RIGHT SIDE 13 INCHES FROM TOP EDGE 4 INCHES FROM TRAILING EDGE. MAINTENANCE CUT OUT SKIN DAMAGE, INSPECTED FOR CRACKS, NO CRACKS NOTED. REPAIRED IAW RD 8-55-1905 AND DHC8 200 SRM.
Part: SHEAR TIE — CORRODED (BS 545 S31R) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - X545 STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION FROM CLIP, BLEND REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - CORROSION ON AVIONICS RACK INTERCOSTAL AT FS X202 TO FS 198.300 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SET TRACK NR 10 HAS SMALL AREA OF CORROSION AT APPROX X346. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X364. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO BLENDED AREA.
Part: SKIN — DENTED (BS 106) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SCRATCH AND SMALL DENT AT APPROXIMATELY STA X106.00 AND APPROXIMATELY 4 INCHES ABOVE PANEL 112BR RIGHT EXTERNAL FUSELAGE. MAINTENANCE BLENDED AREA OF SCRATCH TO REMOVE DAMAGE, STILL WITHIN LIMITS AND INSPECTED NO CRACKS NOTED. RESTORED FINISH.
Part: SEAT TRACK — CORRODED (BS 545) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK 36 AT X545 HAS PIT OF CORROSION THAT IS OUT OF LIMITS AT .028 DEEP. MAINTENANCE REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK.
Part: SKIN — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SPOT OF CORROSION ON THE INNER SKIN AROUND RIVET HOLE FORWARD OF FRAME STA 201 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED MINOR CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT INBOARD SEAT TRACK NR 7 HAS APPROX .060 GOUGE ON THE OUTBOARD FLANGE AT APPROX X256. MAINTENANCE REMOVED TRACK AND INSTALL NEW TRACK.
Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - MAIN CABIN DOOR THRESHOLD HAS LIGHT CORROSION AT 5 EA NUTPLATES. MAINTENANCE REMOVED MCD THRESHOLD AND NUTPLATES. REMOVED LIGHT SURFACE CORROSION FROM LOWER SILL PLATE AND INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. INSTALLED NEW NUTPLATES.
Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 23,973 hrs · 34,562 cycles
PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X594.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION. INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATES.
Part: SEAT TRACK — CORRODED (BS 312) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - NR 1 SEAT TRACK WEB TO FRAME ANGLE CLIP IS CRACKED FORWARD SIDE OF FRAME 312. MAINTENANCE REMOVED AND INSTALLED NEW CLIP.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX -C1 CHECK - SEAT TRACK NR 3 HAS A CORROSION PIT IN THE CHANNEL AT X544. MAINTENANCE BLENDED THE AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - FLOORBOARD SUPPORT ANGLE CORRODED AT APPROX STA X599.00, Y26.00 RT TO Y31.00 RT, Y 0.00 TO Y 8.00 RT, Y 0.00 TO Y 6.00 LT. MAINTENANCE REMOVED CORROSION INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKED NOTED. ALODINED, PRIMED AND PAINTED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 IS CORRODED ON THE FRONT OUTBOARD CORNER AT APPROX X262. MAINTENANCE BLENDED OUT CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: SUPPORT ANGLE — CORRODED (BS 600 S28L) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - CORROSION UNDER AFT CARGO DOOR THRESHOLD SUPPORT ANGLE APPROXIMATELY STA X600 STRINGER 28L. MAINTENANCE REMOVED RIVETS BLENDED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SUSPECT LIGHT CORROSION FORMING ON WEB TIE RIVET HEADS BELOW FLOOR AND SEAT TRACK. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIVET HEADS ABOVE INNER SKIN ON WEB X528 TO X534 ON THE RIGHT SIDE BELOW SEAT TRACK 8/9 SUSPECT LIGHT CORROSION. MAINTENANCE REMOVED RIVETS AND BLENDED CORROSION FROM WEB, REMAINED WITHIN LIMITS AND INSPECTED NO CRACKS NOTED. INSTALLED NEW RIVETS AND RESTORED FINISH TO REPAIR AREA.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 23,976 hrs · 34,562 cycles
PDX - C1 CHECK - TOP OF RIGHT OUTBOARD SEAT TRACK NR 10 IS CHAFED AT APPROX X362. MAINTENANCE BLENDED CHAFED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMED AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE BLENDED OUT CORROSION, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA.
Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 23,973 hrs · 34,562 cycles
PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X553.00 AT DOOR THRESHOLD HAS CORROSSION ON NUTPLATES AND MOUNTING SURFACE. REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND WITHIN LIMITS NO CRACKS FOUND. ALODINED PRIMED AND PAINTED INSTALLED NUTPLATES.
Part: SEAT TRACK — CORRODED (BS 370) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SUSPECT CORROSION AROUND RIVET ON VERTICAL FRAME SUPPORT FOR NR 4 SEAT TRACK AT STA X370.00 INBOARD OF STRINGER 31L BOTTOM MOST INBOARD RIVET. MAINTENANCE REMOVED RIVET BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVET AND RESTORED FINISH TO REPAIR AREA.
Part: STRINGER CLIP — CORRODED (BS 466 S31R) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - X466 AND STRINGER 31R SUSPECT CORROSION AT CLIP RADIUS. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED REPAIR AREA. RESTORED FINISH.
Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 23,973 hrs · 34,562 cycles
PDX - C CHECK - SUPPORT ANGLE AT APPROX X586.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATES.
Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 23,973 hrs · 34,562 cycles
PDX - C CHECK - SUPPORT ANGLE AT APPROX STA X569.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS NO CRACKS NOTED. ALODINED, PRIMED AND PAINTED. INSTALLED NUTPLATES.
Part: SEAT TRACK — GOUGED (BS 510-520) · airframe 23,973 hrs · 34,562 cycles
PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X510 TO 520. MAINTENANCE BLENDED OUT GOUGE ON TRACK, INSPECTED REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA.
Earlier reports · 1998–2007 · 172 reports
2007
Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 23,909 hrs · 34,471 cycles
MFR - FLIGHT 2150 - SHORTLY AFTER TAKEOFF, THE LAV SMOKE DETECTOR WENT OFF. THE FLIGHT ATTENDANT CHECKED AND SAW NO SMOKE, BUT DID SMELL A HOT DUSTY SMELL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, MAINTENANCE REPLACED THE NR 2 ENGINE AFTER FINDING OIL ON THE HP IMPELLER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 23,909 hrs · 34,471 cycles
MFR - ON TAXI THE LAV SMOKE DETECTOR WENT OFF. RETURNED TO THE GATE AND RESET THE DETECTOR. MAINTENANCE COULD NOT DUPLICATE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: TRIM PANEL — FAILED (COCKPIT) · airframe 23,814 hrs · 34,335 cycles
LWS - FLIGHT 2027 - WHILE BOARDING PASSENGERS WITH GROUND POWER ON, SMOKE STARTED TO COME FROM THE TRIM INDICATOR PANEL IN THE COCKPIT. POWER TURNED OFF AND BATTERIES TURNED OFF. SMOKE STOPPED. NO INDICATION OF FIRE. FOUND CIRCUIT BREAKER POPPED. MAINTENANCE REPLACED THE RUDDER TRIM PANEL. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: TSCU — FAILED (AUTOFEATHER SYS) · airframe 23,574 hrs · 33,986 cycles
PDX - ON FLIGHT 2048, NR 2 PROPELLER FAILED AUTOFEATHER TEST. FEATHER LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AUTOFEATHER CONTROL RELAYS 6121-K6, 6121-K8. COMPLIED WITH AUTOFEATHER TEST BUT FEATHER STILL FAILED TO ILLUMINATE. REPLACED NR 2 TSCU IAW PWC EMM 72-01-10 PG 420 PARA 7A-B. C/W TC 9720019. OPERATIONS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN · airframe 23,385 hrs · 33,715 cycles
PDX FLIGHT NR 2156 - MULTIPLE NO AIII WARNINGS ON CAT III APPROACH. PERFORMED INDEX COMPENSATION ADJUSTMENT FOR NR 1 AND NR 2 FLUX VALVES, PERFORMED OPERATIONAL TEST IAW -8 200 TC 9340021, ALL CHECKS GOOD. PERFORMED OPERATIONAL TEST OF HGS RETURN TO SERVICE CAT III, ALL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — LOOSE (OUTFLOW VALVE) · airframe 23,166 hrs · 33,373 cycles
PDX FLIGHT NR 2093, AFTER TAKEOFF AIRCRAFT BEGAN PRESSURIZATION AT HIGH RATE, CABIN DIFF OF 5.75 REACHED BY 4000 FEET MSL. SWITCHED TO MAIN MODE, NO CONTROL. ATTEMPTED TO DUMP CABIN WOULDN'T DUMP. FINALLY DUMPED CABIN PRESSURE FOR LANDING BY OPENING FORWARD OUTFLOW VALVE. RE-SECURED CONNECTOR ON CABIN PRESSURE CONTROLLER. PRESSURIZED AIRCRAFT ON GROUND IN DUMP, AUTO AND MANUAL IAW DHC-8-200 AMM 21-30-00. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: CONTACTOR — DAMAGED (NR 1 AC) · airframe 23,061 hrs · 33,207 cycles
SEA FLIGHT NR 2070 WITH NR 1 FEATHERED AND NR 2 UNFEATHERED THE LEFT TRU CAUTION ILLUMINATED. WITH NR 2 FEATHERED AND NR 1 UNFEATHERED THE LIGHT WAS NOT ILLUMINATED. FOUND NO AC POWER ON LEFT BUSS WHILE NR 1 AC GENERATOR OFF LINE AND NR 2 GENERATOR ON LINE. REMOVED AND REPLACED NR 1 AC CROSS TIE CONTACTOR 24-21-K1. PERFORMED FUNCTION TEST OF THE AC GENERATOR SYSTEM IAW -8 Q200 AMM 24-21-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — MISALIGNED (AUTOFEATHER SYS) · airframe 22,960 hrs · 33,049 cycles
SEA FLIGHT NR 2104 - DURING TAKEOFF ROLL AUTO FEATHER FAILED TO ARM THROUGH 80 PERCENT. TORQUE ON BOTH NR 1 AND NR 2. FOUND CONNECTOR 6121-P9 TO BE ASKEW. RESEATED CONNECTOR 6121-P9. FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: LIMIT SWITCH — OUT OF ADJUST (AUTOFEATHER SYS) · airframe 23,599 hrs · 33,623 cycles
SEA FLIGHT NR 2104 AUTOFEATHER DID NOT ARM. MAINTENANCE ADJUSTED THE NR 1 POWER LEVER LIMIT SWITCH. OPERATIONAL CHECK GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE.
Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 22,799 hrs · 32,810 cycles
YVR FLIGHT NR 2025 - AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL WITH POWER SET ABORTED TAKEOFF, AUTOFEATHER SYSTEM INOP. MAINTENANCE PERFORMED AUTO FEATHER SYSTEM ADJUSTMENT AND TEST IAW DHC-8-200 ENGINE RIGGING MANUAL. RT ER 10, PARAGRAPH 5-1-A 1 38. PERFORMED FUNCTIONAL TEST OF THE AUTOFEATHER SYSTEM OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: TSCU — MALFUNCTIONED (AUTOFEATHER) · airframe 22,363 hrs · 32,172 cycles
PDX AUTO FEATHER ARM SWITCH LIGHT DOES NOT EXTINGUISH, LIGHT FLICKERS ON AND OFF EN ROUTE AND EXTINGUISHES IN DESCENT. REPLACED 6121-K5 RELAY AND NR 1 AND NR 2 TSCU UNITS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POTENTIOMETER — OUT OF ADJUST (STEERING TILLER) · airframe 22,193 hrs · 31,920 cycles
SEA FLIGHT NR 2243 WHEN NOSE WHEEL STEERING SELECTED ON, WITH TILLER CENTERED, NOSE WHEEL TURNS FULL LEFT, NOSE WHEEL STEERING INOP. MAINTENANCE RESECURED LINKAGE BETWEEN TILLER HANDLE AND RVDT ADJUSTED POT NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
2006
Part: AHRS — MALFUNCTIONED (COCKPIT) · airframe 21,584 hrs · 31,045 cycles
SEA FLIGHT NR 2084 ADI ROLL MISMATCH ON ADVISORY DISPLAY. FIRST OFFICER ADI SHOWS 5 DEGREE ROLL TO LEFT. MAINTENANCE REPLACED NR 2 AHRS AS PER T/C 9340019. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SWITCH — MALFUNCTIONED (DE-ICE SYSTEM) · airframe 21,435 hrs · 30,832 cycles
SEA FLIGHT NR 2203 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED 65 PSI SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 2) · airframe 21,216 hrs · 30,515 cycles
PDX FLIGHT 2228 NR 2 AUXILARY POWER CAUTION. MAINTENANCE REPLACED NR 2 SPU IAW DHC-8 AMM 29-*11-17-00-062 AND 29-11-17-00-802. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — INOPERATIVE (INSTRUMENT PANEL) · airframe 21,015 hrs · 30,216 cycles
SEA FLIGHT NR 2053 NR 2 AUXILLARY PUMP LIGHT INOP. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: COWL DOOR — OPEN · airframe 200,917 hrs · 30,072 cycles
PDX FLIGHT 2149 COWL DOOR OPEN. MAINTENANCE CLOSED THE COWL DOOR. OPERATION CHECK GOOD, NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 20,225 hrs · 29,039 cycles
SEA - FORWARD CENTER CEILING EMERGENCY LIGHTS INOP AND NR 1 EMERGENCY EXIT EGRESS LIGHTS AT STATION X 324.1 INOP. MAINTENANCE REPLACED EMERGENCY BATTERY PACK PS3 IAW DASH 8 200 AMM 33-51-00, OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FRAME — CORRODED (BS 424 S23R) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FUSELAGE FRAME X424 TO STRINGER 23R TIE CLIP IS CORRODED ON TOP SURFACE, LOWER EDGE AND MOUNTING RIVETS. REPAIRED IAW SRM 51-40-11 AND SRM 51-20-36.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, LEFT HAND AFT FUSELAGE SKIN AND STRINGER DENTED BETWEEN RPB AND FRAME NR 1, STRINGER 13P - 15P. REPAIRED IAW RD 8-55-1651 AND EA 2-55-111.
Part: FRAME — CORRODED (BS 424-436) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, FUSELAGE FRAME WEB HAS SPOTS OF CORROSION ON TOP SURFACE AND AROUND 4 RIVETS AT AFT END OF WEB, LOCATED BETWEEN FS X424 AND X436, WEB IS ON TOP OF STRINGER 23R AT FLOOR LEVEL. REPAIRED IAW SRM 51-20-11 AND SRM 51-40-11
Part: INTERCOSTAL — BENT (BS 424 S23R) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, OUTBOARD INTERCOSTAL IS BENT AND BROKEN AT FS X424 AND STRINGER 23R. REPAIRED IAW SRM 51-40-11.
Part: FRAME — CORRODED (BS 425 S23R) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, FUSELAGE FRAME WEB HAS SPOTS OF CORROSION ON TOP SURFACE AND AROUND 4 RIVETS AT AFT END OF WEB, LOCATED BETWEEN FS X425 AND X436, WEB IS ON TOP OF STRINGER 23R AT FLOOR LEVEL Z100.032. REPAIRED IAW SRM 51-40-11.
Part: PANEL — CORRODED (WING ROOT) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, ROOT FAIRING PANEL 262PT HAS CORRODED FASTENERS. REPAIRED IAW SRM 53-50-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK HAS CORROSION/CHAFE MARKS AT X409, X375 - 379, X313 - 316, AND X281 - 284. REPAIRED IAW RD 8-53-1339 AND SRM 51-40-00, SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX C4 CHECK, LEFT HAND INBOARD SEAT TRACK NR 4 HAS PITTING CORROSION INSIDE TRACK AT STATION X266, X280 AND X298. REPAIRED IAW RD 8-53-1339 AND RD 8-51-1102.
Part: SEAT TRACK — CORRODED (BS 281-405) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK. CONTINUATION CARD RIGHT HAND INBOARD SEAT TRACK HAS CORROSION/CHAFE MARKS AT THESE LOCATIONS X405, X375 - X379, X313 - X316, AND X281 - 284. REPAIRED IAW RD 8-53-4473.
Part: SKIN — CHAFED (TE FLAP) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT OUTBOARD FLAP HAS A 4" CHAFE ON TOP EXTERIOR SKIN AT WS YW236.000 AND FORWARD OF TRAILING EDGE. REPAIRED IAW RD 8-57-1022 AND SRM 51-20-36, SRM 51-20-16, AND SRM 51-20-26.
Part: FRAME — CRACKED (BS 253) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, FRAME CRACKED APPROX STATION X253.4, BLR 24R Z100.8. REPAIRED IAW EA 2-53-690.
Part: SKIN — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, JACK PAD (NOSE) IS CORRODED, AS SEEN FROM INSIDE AIRCRAFT. REPAIRED IAW SRM 51-40-11.
Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, GALLEY OUTBOARD MOUNT FLANGE IN AIRCRAFT IS CORRODED ON AFT END. REPAIRED IAW SRM 51-20-11 AND SRM 51-20-16, RD 8-53-8936.
Part: BULKHEAD — CHAFED (RT NACELLE) · airframe 19,954 hrs · 28,627 cycles
PDX C4 CHECK, RIGHT HAND NACELLE WHEEL WELL AFT BULKHEAD HAS CHAFED BETWEEN GRAVEL GUARD AND RECEPTACLES. REPAIRED IAW SRM 51-20-11, RD 8-54-2139 AND EA 2-54-253.
Part: STRINGER — CORRODED (BS 167 S31R) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, STRINGER 31R IS CORRODED BETWEEN PILOTS BULKHEAD AND FRAME AT X167. REPAIRED IAW EA 2-53-689, SRM 51-20-16 AND SRM 51-40-11.
Part: STRINGER — CORRODED (BS 151-167) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, CORROSION ON STRINGER 31R TOP SURFACE OF LOWER FLANGE BETWEEN FSX151 AND X167. REPAIRED IAW EA 2-53-689 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 167) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 31R AND 32R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.
Part: SEAT TRACK — CORRODED (BS 597-580) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, RIGHT INBOARD SEAT TRACK INBOARD FLANGE HAS SCREW HOLES CORRODED AT X597, X580. REPAIRED IAW RD 8-53-4936.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT X437 - X439, AND X501 - 505. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.
Part: FRAME — CORRODED (BS 167 S29L) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, FRAME X167 HAS SMALL AREA OF CORROSION ON FORWARD SIDE JUST OUTBOARD OF STRINGER 29L. REPAIRED IAW SRM 51-20-16, SRM 51-00-04, SRM 51-20-36 AND SRM 51-20-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, RIGHT HAND OUTBOARD SEAT TRACK CORRODED ON LUGS AND IN BOTTOM OF CHANNEL AT X266 - X269, X279, X299, AND X330. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.
Part: FRAME — CORRODED (BS 167 S30-31R) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 30R AND 31R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.
Part: FRAME — CORRODED (BS 151 S31-32R) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME X151 IS CORRODED AT CASTELLATION BETWEEN STRINGER 31R AND 32R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK AFT MOST SEGMENT CORRODED ON TOP AND INSIDE LUGS AT X597. REPAIRED IAW RD 8-53-4936.
Part: STRINGER — CORRODED (BS 152-202) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, STRINGER 33 UPPER AND LOWER FLANGES CORRODED BETWEEN X152 - X202. REPAIRED IAW SRM 51-20-11.
Part: FRAME — CORRODED (BS 167 S28-29L) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 28L AND 29L. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CHANNEL AT X530 - X542. REPAIRED IAW RD 8-53-4936 AND SRM 51-20-16.
Part: FRAME — CORRODED (BS 151 S31-32L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME AT X151 HAS CORRODED CASTELATION BETWEEN STRINGER 31L - 32L. REPAIRED IAW SRM 51-20-11, SRM 51-20-26, SRM 51-20-36 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 167 S31-32L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME AT X167 HAS CORRODED CASTELATION BETWEEN STRINGER 31L - 32L. REPAIRED IAW SRM 51-20-11, SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 167 S32-33L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 32L AND 33L. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX C4 CHECK, RIGHT OUTBOARD SEAT TRACK HAS CHAFE DAMAGE ON TOP OF LUGS AT X470. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.
Part: FLAP TRACK — CORRODED (NR 3) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, RIGHT HAND NR 3 FLAP TRACK HAS PITTING CORROSION ALONG THE LENGTH OF THE TRACKS, ALONG THE PATHS OF THE ROLLERS. REPAIRED IAW RD 8-57-987.
Part: SKIN — CORRODED (LT WING LE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, LOWER FLANGE ON LEFT INBOARD WING LEDING EDGE 511AL HAS FRETTING DAMAGE AT INBOARD 9" ON WING FACE. REPAIRED IAW SRM 51-20-16 AND RD 8-57-811.
Part: ATTACH FITTING — CRACKED (EMPENNAGE) · airframe 19,954 hrs · 28,627 cycles
PDX C4 CHECK, EMPENNAGE HALF OBLIQUE FRAME NR 4 HAS CRACKED ATTACH CLIP AT AFT SIDE OF FRAME AND STRINGER NR 4 RIGHT HAND. REPAIRED IAW RD 8-55-199 AMD SRM 51-10-21.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, RIGHT HAND OUTBOARD SEAT TRACK HAS CHAFE DAMAGE ON TOP OF RIGHT HAND LUGS AT X519, AND CORROSION ON TOP LUGS AT X526 - 530. REPAIRED IAW RD 8-53-3644.
Part: SPAR CAP — CHAFED (RT WING) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, RIGHT HAND WING FRONT SPAR, LOWER CAP IS CHAFED AT INBOARD ATTACH POINT FOR 611AR. REPAIRED IAW SRM 51-20-16, SRM 51-40-00 AND RD 8-57-811.
Part: SILL — GOUGED (CARGO DOORWAY) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, TWO GOUGES ON UPPER CARGO DOOR SILL, LOCATED BETWEEN TWO UPPER CARGO STEP PADS. REPAIRED IAW RD 8-53-7447.
Part: PANEL — CHAFED (RT NACELLE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, RIGHT ENGINE NACELLE APERTURE FOR PANEL 422CT IS CHAFED. REPAIRED IAW SRM 54-00-11, SRM 51-00-16 AND SRM 51-20-11.
Part: SILL — MISINSTALLED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FORWARD INBOARD RIVETS DOESN'T FILL HOLE PROPERLY, UNDER MAIN CABIN DOOR LOWER SILL. REPAIRED IAW SRM 51-40-11.
Part: SILL — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, CORROSION AROUND ALL 5 BOLT HOLES ON TOP OF MAIN CABIN DOOR LOWER SILL. REPAIRED IAW SRM 51-40-11.
Part: ACCESS PANEL — CHAFED (WING ROOT) · airframe 19,954 hrs · 28,627 cycles
PDX- C4 CHECK, ROOT FAIRING ACCESS PANEL 262LT CHAFED RIGHT AFT CORNER. REPAIRED IAW RD 8-53-3366.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, MAIN CABIN DOOR THRESHOLD MEMBER HAS CORROSION AROUND RIVET HEAD. REPAIRED IAW SRM 51-20-11.
Part: FRAME — CORRODED (BS 167 S29-30L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME AT X167 HAS CORRODED CASTELATION BETWEEN STRINGER 29L - 30L. REPAIRED IAW SRM 51-20-11, SRM 51-20-26, SRM 51-20-36 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 151 S29-30L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME AT X151 HAS CORRODED CASTELATION BETWEEN STRINGER 29L - 30L. REPAIRED IAW SRM 51-20-11, SRM 51-20-26, SRM 51-20-36 AND SRM 51-40-11.
Part: FIREWALL — CRACKED (LT NACELLE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, LEFT HAND NACELLE FIREWALL IS CRACKED AT STATION XN125, ZN0.0 AND YW166, VIEWED THROUGH PANEL 415AL. REPAIRED IAW RD 8-54-806.
Part: FRAME — CORRODED (BS 151 S30-31L) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, FRAME AT X151 HAS CORRODED CASTELATION BETWEEN STRINGER 30L - 31L. REPAIRED IAW SRM 51-20-11, SRM 51-20-26, SRM 51-20-36 AND SRM 51-40-11.
Part: BULKHEAD — CHAFED (LT NACELLE) · airframe 19,954 hrs · 28,627 cycles
PDX-C4 CHECK, LEFT HAND NACELLE AFT BULKHEAD HAS CHAFE MARKS FROM GRAVEL GAURD LOCATED 6" UP FROM BOTTOM OF NACELLE. REPAIRED IAW SRM 51-20-11, SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-41.
Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 19,954 hrs · 28,627 cycles
PDX - C4 CHECK, MAIN CABIN DOOR LOWER THRESHOLD HAS CORROSION AROUND NUTPLATES AND MANY NUTPLATES ARE CORRODED. REPAIRED IAW SRM 51-20-11.
Part: ATTENUATOR — INOPERATIVE (NR 27) · airframe 19,769 hrs · 28,337 cycles
PSC - ON FLIGHT 2279, RETURNED TO GATE, FA REPORTS KNOCKING AND SLAPPING SOUND COMING FROM OUTSIDE MAIN CABIN DOOR. MAINTENANCE INSPECTED MAIN CABIN DOOR AND SURROUND, TIGHTENED LOOSE SCREW ON AFT HANDRAIL. NO OTHER DEFECTS NOTED. GROUND RAN AND CYCLED PROPS IN AND OUT OF FEATHER (ANVS C/B'S PULLED) SOUND HAPPENED A COUPLE OF TIMES AND STOPPED OCCURRING. RESET C/B'S. SOUND DID NOT COME BACK. AT NEXT STOP, SOUND RETURNED, MAINTENANCE REMOVED AND REPLACED NR 27 ATTENUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2005
Part: GENERATOR — MALFUNCTIONED (DC SYS) · airframe 19,652 hrs · 28,173 cycles
FLIGHT NR 2093, NR 1 DC GENERATOR ILLUMINATED DURING CLIMB-OUT, RAN CHECKLIST AND RESET GENERATOR, CAUTION LIGHT REMAINED OUT FOR REMAINDER OF FLIGHT. MAINTENANCE REPLACED NR 1 DC STARTER/GENERATOR IAW MTC 98010-001. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: GENERATOR — MALFUNCTIONED (AC SYSTEM) · airframe 19,411 hrs · 27,836 cycles
BOI FLIGHT NR 2192, NR 1 AC GENERATOR CAUTION ILLUMINATED ON CLIMB. MAINTENANCE REPLACED NR 1 AC GENERATOR AND COMPLIED WITH FUNCTIONAL TEST IAW AMM 24-21-00, PAGES 401-403. OPERATIONAL CHECK AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 19,120 hrs · 27,416 cycles
PDX - EMERGENCY LIGHT INOP AT CABIN AFT OVERHEAD AND OUTSIDE RIGHT AFT, AND CABIN CENTER EMERGENCY OVERHEAD. MAINTENANCE REPLACED NR 4 EMERGENCY BATTERY PACK AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS SYSTEM, IAW DASH 9 AMM 33-51-01-710-801, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 18,820 hrs · 26,963 cycles
SEA - LEFT AND RIGHT EMERGENCY EGRESS LIGHTS, CENTER AND AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES AND BATTERY PACKS BEHIND CEILING PANEL 235BZ. REMOVED AND REPLACED BATTERY PACK PS4 BEHIND CEILING PANEL 245BZ. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ELEMENT — MALFUNCTIONED (FUEL TEMP) · airframe 18,125 hrs · 25,903 cycles
SEA - FLIGHT NR 2046, NR 2 FUEL TEMP AT 57 DEGREES ON CLIMB AND CRUISE, RAN CHECKLIST, TEMP REMAINED HIGH. ABOUT 25 DEGREES WARMER THAN NR 1. MAINTENANCE REPLACED FUEL TEMP BULB, NR 2 FUEL HEATER THERMAL ELEMENT IAW MTC 9730002. FUEL TEMP INDICATION CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 18,100 hrs · 25,866 cycles
AFTER ENGINE START, DC BUSS CAUTION LIGHT ILLUMINATED. RESET BUSS OK. NR 2 GENERATOR WOULD NOT RESET. MX STARTED NR 1 AND 2 ENGINES, DESELECTED EXTERNAL POWER SWITCH. TURNED NR 2 GENERATOR OFF, CAUTION LIGHT ILLUMINATED. TURNED NR 2 GENERATOR ON, LIGHT WENT OUT. NO DEFECTS NOTED, ALL VOLTAGES NORMAL. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: ODOR — DETECTED (COCKPIT) · airframe 18,076 hrs · 25,823 cycles
ACRID ELECTRICAL ODOR IN ACFT STRONGEST IN COCKPIT. FOUND ICE PROTECTION LEFT IN "ON" POSITION. ODOR DIMINISHED THROUGHOUT FLIGHT. MX INVESTIGATED ACFT INTERIOR FOR ANY ODOR. NONE NOTED. ATTRIBUTE ODOR TO SEVERAL ICE PROTECTION SWITCHES IE VALVE HEAT AND PITOT HEAT IN "ON" POSITION WITH ACFT ON GROUND IN RDM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: DISPLAY — INACCURATE (ZONE 200) · airframe 18,019 hrs · 25,742 cycles
HEADING MISMATCH INTERMITTENTLY DISPLAYED IN ADVISORY DISPLAY. COMPLIED WITH CHECKLIST PROCEDURE, MESSAGE RETURNED SEVERAL TIMES. COMPLIED WITH IAW CHECKS AND NO HEADER ON MISMATCH MESSAGE OCCURRED, COMPLIED WITH AMM TASK 34-21-00-40-801. OPS CHECKS GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.
Part: CONNECTOR — DIRTY (HYD PUMP) · airframe 18,020 hrs · 25,742 cycles
AFTER TAKEOFF, NR 2 STANDBY PUMP HOT LIGHT BEGAN CYCLING AND THEN CAME ON STEADY. PERFORMED NR 2 STANDBY PUMP HOT CHECKLIST AND LIGHT EXTINGUISHED APPROX A MINUTE. OPERATED NORMALLY FOR REMAINDER OF FLIGHT. MX CLEANED CONNECTOR ON NR 2 STANDBY PUMP. GROUND RAN ACFT AND CYCLED APPLICABLE HYDRAULIC SYSTEM USING NR 2 STANDBY PUMP. LIGHT REMAINED EXTINGUISHED. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.
Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 17,661 hrs · 25,200 cycles
SEA - LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. DID CHECKLIST, LIGHT EXTINGUISHED. OAT -1 NO ICE, PRECIPITATION. MAINTENANCE REPLACED THE PILOTS WINDSHIELD CONTROLLER IAW AMM 31-41-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2004
Part: NUT PLATE — STRIPPED (FUSELAGE) · airframe 17,410 hrs · 24,828 cycles
PDX - FUSELAGE PANEL HAS FOUR STRIPPED OUT NUTPLATES. REPLACED OLD NUTPLATES WITH NEW NUTPLATES.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,305 hrs · 24,674 cycles
EMERGENCY LIGHTS FAIL OPERATIONAL CHECK. LIGHTS POWERED BY BATTERY PACK 3351 PS2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PS2. OPERATIONAL TEST OF EMERGENCY LIGHTS SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — CRACKED (ZONE 200) · airframe 15,960 hrs · 22,671 cycles
PDX - EMERGENCY FLOOR TRACK LIGHTING AT STATION 270.50 IS CRACKED AND HAS EXPOSED WIRES. REMOVED AND REPLACED TRACK LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2003
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
PDX- NR 9 SEAT TRACK REQUIRES REPLACEMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD'S 8-53-784 AND 8-53-4472.
Part: STRUT — CHAFED (NR 2 NACELLE) · airframe 14,822 hrs · 20,975 cycles
PDX- UPPER OUTBOARD ENGINE STRUT IS CHAFED AT TWO LOCATIONS AT INBOARD AFT END OF NR 2 NACELLE. REPAIRED IAW DHC-8 RD 8-54-036.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
PDX- AIRCRAFT SKIN UNDER LOWER VHF ANTENNA IS CORRODED. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16, 51-00-06, 51-00-04, RD 8-53-7635 AND HORIZON AIR EA 2-53-505.
Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
PDX- FLOOR NUTPLATE HAS CORROSION AT STATION X223.00, LEFT OF YL29.00. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-11 AND RD 8-53-7637.
Part: SKIN — DAMAGED (RT AILERON) · airframe 14,822 hrs · 20,975 cycles
PDX- RIGHT HAND AILERON TOP SKIN HAS A BURN HOLE AT RIVET ON TRAILING EDGE. REPAIRED IAW DHC-8 RD 8-57-2702 AND HORIZON AIR EA 2-57-241.
Part: SKIN — DAMAGED (ZONE 300) · airframe 14,822 hrs · 20,975 cycles
LEFT HAND AILERON OUTBOARD TIP HAS HOLE IN FIBER. REPAIRED IAW DHC-8 SRM 51-20-61, 51-30-70, 51-20-26 AND 57-60-71.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
PDX- NR 11 SEAT TRACK REQUIRES REPLACEMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-00, 51-40-11 AND RD 8-51-102.
Part: SKIN — DENTED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
PDX- FIVE INVERTED DENTS FROM STATIONS X409.75 TO X417.75 BETWEEN STRINGERS 29 AND 31. REPAIRED IAW DHC-8 SRM 51-00-06, 51-00-05 RD 8-53-7629 AND HORIZON AIR EA 2-53-502.
Part: SEAT TRACK — CHAFED (ZONE 100) · airframe 14,822 hrs · 20,975 cycles
NR 5 SEAT TRACK HAS A CHAFE ON THE INBOARD FACE OF RIGHT HAND LUG 12 INCHES FORWARD OF FRAME X467. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36, RD 8-53-2636 AND HORIZON AIR EA 2-53-507.
Part: RIVET — BROKEN (ZONE 300) · airframe 14,822 hrs · 20,975 cycles
PDX- BROKEN RIVET ON LEFT HAND SIDE OF VERTICAL STABILIZER ALONG TOP EDGE, MID POINT OF STABILIZER. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: RIVET — LOOSE (RUDDER) · airframe 14,822 hrs · 20,975 cycles
PDX- FORE RUDDER LOWER CLOSING RIB HAS LOOSE RIVET AT FORWARD RIGHT HAND SIDE. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — CHAFED (ZONE 100) · airframe 14,822 hrs · 20,975 cycles
NR 5 SEAT TRACK HAS A CHAFE ON THE INBOARD FACE OF THE RIGHT HAND LUG .5 INCH AFT OF FORWARD END OF TRACK. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-53-507.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,822 hrs · 20,975 cycles
NR 5 SEAT TRACK HAS CORROSION ON THE INBOARD FACE OF THE RIGHT HAND LUG 2 INCHES AFT OF X467. REPAIRED IAW DHC-8 SRM 51-00-06, 51-20-36, RD 8-53-7636 AND HORIZON AIR EA 2-53-507.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 14,822 hrs · 20,975 cycles
NR 10 SEAT TRACK REQUIRES REPLACMENT DUE TO DAMAGE THAT IS OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-51-102.
Part: SWITCH — CONTAMINATED (CABIN) · airframe 14,804 hrs · 20,943 cycles
SEA- ON FLIGHT 2163 EXIT FLOOR TRACK EMERGENCY LIGHTS FLICKER ON AND OFF IN FLIGHT. FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH IS DAMP. CLEANED AND DRIED SWITCH. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (ZONE 200) · airframe 14,600 hrs · 20,644 cycles
ON FLIGHT 2052 SMOKE WARNING LIGHT CAME ON IN FLIGHT THREE TIMES FOR 45 SENCONDS, THEN WENT OUT. NO OTHER INDICATIONS OF SMOKE IN COCKPIT OR CABIN. REMOVED AND REPLACED NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCARFT RETURNED TO SERVICE.
Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 14,180 hrs · 20,006 cycles
EAT- ON FLIGHT 2134 ENROUTE SEA TO EAT MASTER WARNING AND CHECK FIRE DETECTION ILLUMINATED. DURING EMERGENCY CHECKLIST SELECTED LOOP A ONLY BECAUSE LOOP B WAS ILLUMINATED. MASTER WARNING AND CHECK FIRE DETECTION WENT OUT. REMOVED AND REPLACED SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,082 hrs · 19,857 cycles
PDX- AFT INTERIOR CEILING EMERGENCY LIGHT INOPERATIVE AND AFT RIGHT HAND EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR — OPEN (MLG) · airframe 12,977 hrs · 18,250 cycles
SEA-ON FLIGHT NUMBER 2396, RETURNED TO FIELD FOR GEAR DID NOT RETRACT DUE TO ALT RELEASE HANDLE DOOR BEING OPEN. CLOSED MAIN LANDING GEAR ALT DOOR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
2002
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 12,102 hrs · 16,991 cycles
PDX- SMOOTH DEFORMATION DAMAGE TO STRINGER 165 AT STATION X-151. THIS IS THE POINT OF GREATEST DEFORMATION WITH 9 INCH TAPER TO ZERO DAMAGE FORWARD AND AFT STRINGER APPEARS TO BE PUSHED IN APPROXIMATELY .25 INCH AT GREATEST POINT. REPAIRED IAW HORIZON AIR EA 2-53-415.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 12,102 hrs · 16,991 cycles
PDX- DEFORMATION DAMAGE TO STRINGER 165 AT STATION X-151. REPAIRED IAW HORIZON AIR EA 2-53-415.
Part: WIRE — BROKEN (CABIN) · airframe 11,927 hrs · 16,747 cycles
SEA- EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 7. INSPECTED AND FOUND BROKEN WIRE AT PLUG 3352-P9. REPAIRED WIRE WITH SEAL SPLICE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
2001
Part: SKIN — BUCKLED (RT NACELLE) · airframe 10,235 hrs · 14,284 cycles
PDX - RIGHT NACELLE IS BENT AND BUCKLED JUST AFT OF THE LOWER COWL. REPAIRED IAW RD 8-54-063.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,049 hrs · 14,012 cycles
SEA - FORWARD RED PROXIMITY EMERGENCY ESCAPE PATH LIGHTS DO NOT ILLUMINATE. REPLACED SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - RIGHT NACELLE FINGNAIL ATTACHMENT TAP CRACKED AT NUPLATE RIVET, INBOARD OF STATION XN236.20. REPAIRED IAW DHC-8 RD 8-54-163.
Part: PANEL — CHAFED (NR 1 NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - NR 1 NACELLE PANEL 414AR IS CHAFED APPROXIMATELY .014 INCH DEEP. REPAIRED IAW HORIZON AIR EA 2-71-157.
Part: FLAP TRACK — CORRODED (WING) · airframe 9,844 hrs · 13,711 cycles
PDX - PITTING ON THE TOPSIDE OF THE LOWER TRACK ON THE RIGHT-HAND NR 3 FLAP TRACK. REPAIRED IAW DHC-8 RD 8-57-987.
Part: SKIN — DENTED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - DENT .067 INCH DEEP X 1.70 INCH HIGH X 1.60 INCH WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD. REPAIRED IAW HORIZON AIR EA 2-53-322.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - DENT 0.37 INCH DEEP X 1.350: HIGH X 1.050 WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD AT STATION X298.4, Z163 AND EDGE OF STRINGER 10L. REPAIRED IAW HORIZON AIR EA 2-53-322.
Part: SKIN — DENTED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - DENT .043 INCH DEEP X 1.00 INCH HIGH X 1.15 INCH WIDE IN LEFT-HAND OUTER FUSELAGE SKIN UNDER LEFT-HAND ICE SHIELD AT STATION X305.5, Z176.5 AND EDGE OF STRINGER 6L. REPAIRED IAW HORIZON AIR EA 2-53-322.
Part: FRAME — CHAFED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - TOP CAP OF FRAME IS CHAFED AT STATION X222.000 WHERE LAVATORY SITS. REPAIRED IAW HORIZON AIR EA 2-53-321.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-93, DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95 AND DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: SKIN — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - AIRCRAFT SURFACE UNDER BOTTOM TCAS ANTENNA NEEDS TO BLEANED DUE TO CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-320, DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: SKIN — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-AIRCRAFT SURFACE UNDER BOTTOM TCAS ANTENNA NEEDS TO BE CLEANED DUE TO CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 2-53-320.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN272.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: FLAP TRACK — CHAFED (LT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-LEFT HAND WING TOP INBOARD FLAP TRACK NEXT TO FUSELAGE HAS EDGE CHAFING. REPAIRED IAW HORIZON AIR EA 2-57-128.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN258.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-94, DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: SKIN — TOOL DAMAGE (WING) · airframe 9,844 hrs · 13,711 cycles
PDX-TOOL MARKS AROUND FASTENER HOLE ON TRAILING EDGE OF PANEL 624AT 14 INCHES FROM INBOARD AFT CORNER. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36, SRM 51-20-26, AND HORIZON AIR EA 2-57-129.
Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK IS CRACKED AT STATION XN249.00. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - RIGHT HAND INBOARD SEAT TRACK TOP FLANGE HAS NICKS WITH RAISED METAL AT STATION 352 Y9.25 RIGHT. REPAIRED IAW DHC-8 SRM 51-40-11, RD 8-53-3403 AND HORIZON AIR EA 2-53-314.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-CORROSION IN AND AROUND NUTPLATES ON LEFT HAND INBOARD SEAT TRACK AT STATION X182.0-X190.9. REPAIRED IAW DHC-8 SRM 51-00-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - CORROSION IN AND AROUND NUT PLATES ON LEFT-HAND INBOARD SEAT TRACK AT STATION X182.0 TO X190.9. REPAIRED IAW DHC-8 CPM 5-2 THROUGH 5-7 AND CPM 5-47.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW288. REPAIRED IAW DHC-8 RD8-57-1675, SRM 51-20-36, AND SRM 51-20-16.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACEOF RIGHT WING LEADING EDGE FLANGE AT YW297. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE FROM YW321 TO YW326. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACE OF LEADING EDGE FLANGE AT RIGHT WING STATION YW376. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.
Part: STRINGER — CRACKED (LT NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK STRINGER CRACKED IN TWO PLACES AT STATION XN264.5. REPAIRED IAW HORIZON AIR EA 2-54-95.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACE RIGHT WING LEADING EDGE FLANGE AT YW315. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.
Part: SKIN — SCRATCHED (PAX DOOR) · airframe 9,844 hrs · 13,711 cycles
PDX - MAIN CABIN DOOR SHELL FORWARD EDGE KNICKED, 18" FROM OUTBORD END. REPAIRED IAW DHC-8 SRM 51-20-11 AND SRM 51-20-51.
Part: FLANGE — SCRATCHED (RT WING SKIN) · airframe 9,844 hrs · 13,711 cycles
PDX - SCRATCHES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW230. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-26 AND RD 8-57-1675.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW195. REPAIRED IAW DHC-8 RD8-57-1675, RM 51-20-16, AND SRM 51-20-36.
Part: FLANGE — GOUGED (RT WING) · airframe 9,844 hrs · 13,711 cycles
PDX-GOUGES ON TOP SURFACES OF RIGHT WING LEADING EDGE FLANGE AT YW202. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-16 AND SRM 51-20-36.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-CORROSION UNDER AND ON NUTPLATES JUST ABOVE CABIN DOOR. REPAIRED IAW DHC-8 51-20-16 AND SRM 51-20-36.
Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 9,844 hrs · 13,711 cycles
PDX - NR 1 NACELLE PANEL 413AL , OIL SERVICE DOOR, CENTER STIFFENER CRACKED. REPAIRED IAW DHC-8 RD 8-71-213.
Part: FLANGE — CORRODED (WING) · airframe 9,844 hrs · 13,711 cycles
PDX-CORROSION AROUND FASTENER HOLES ON FLANGE FOR PANEL 624BT FORWARD INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-00-06, RD8-57-529, AND RD8-57-633.
Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 9,844 hrs · 13,711 cycles
PDX - LIGHT CORROSION BELOW VERTICAL STABILIZER LEADING EDGE, RIGHT-HAND FASTENER HOL AT X813.823, Z335.5. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 9,844 hrs · 13,711 cycles
PDX - CORROSION ON AND UNDER NUT PLATE ON BOTTOM PERIPHERY OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 CPM CHAPTER 4, PAGE 4-25 AND SRM 51-40-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-PITTING CORROSION IN CENTER OF SEAT TRACK LEFT HAND INBOARD FORWARD OF STATION X545.0. REPAIRED IAW DHC-8 RD8-53-1339, SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - PITTING CORROSION IN CENTER OF LEFT-HAND SEAT TRACK FORWARD OF STATION X545.0., REPAIRED IAW DHC-8 SRM 51-20-16, SECTION C 1-9 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND RAISED METAL AT STATION X265-268. REPAIRED IAW DHC-8 RD8-53-1342, SRM 51-20-16 AND SRM 51-20-26.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND RAISED METAL AT STATION 265 TO 268. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-20-16 AND SRM 51-20-26.
Part: COWLING — CHAFED (NR 1 ENGINE) · airframe 9,844 hrs · 13,711 cycles
PDX- NR 1 ENGINE LOWER COWL, FORWARD OUTBOARD LATCH BUTTPLATE IS CHAFED. REPAIRED IAW DHC-8 RD8-71-18 AND HORIZON AIR EA 2-71-155.
Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX-DOPPLER ABOVE CARGO DOOR INCLOSURE IS CHAFED IN TWO SPOTS. REPAIRED IAW DHC-8 RD8-53-5461, SRM 51-00-06.
Part: WEB — CHAFED (LT MLG WW) · airframe 9,844 hrs · 13,711 cycles
PDX - LEFT-HAND NACELLE DECK INBOARD WHEEL PAN CHAFED THROUGH IN TWO PLACED. REMOVED AND REPLACED DAMAGED PAN IAW DHC-8 SRM 51-40-11.
Part: STRUCTURE — CHAFED (CARGO DOORWAY) · airframe 9,844 hrs · 13,711 cycles
PDX-DOPPLER ABOVE CARGO DOOR INCLOSURE IS CHAFED IN 2 SPOTS. REPAIRED IAW DHC-8 RD8-53-5461.
Part: ATTACH FITTING — CORRODED (MLG ACTUATOR) · airframe 9,844 hrs · 13,711 cycles
PDX-LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING HAS MINOR CORROSION JUST OUTBOARD OF BUSHING. REPAIRED IAW DHC-8 RD8-54-1178.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - RIGHT-HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AND SOME RAISED METAL AT STATION 541 TO 548. REPAIRED IAW RD 8-53-784 , DHC-8 SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,844 hrs · 13,711 cycles
PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AND SOME RAISED METAL AT STATION 542 TO 545. REPAIRED IAW DHC-8 RD 8-53-3644, SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26.
Part: UNKNOWN — ODOR (CABIN) · airframe 9,430 hrs · 13,116 cycles
SEA - AFTER ENGINE START, A OIL LIKE ODOR WAS NOTED COMING FROM THE BLEED AIR SYSTEM. ODOR DISSIPATED AFTER TAKEOFF. ENGINE WAS INSPECTED FOR LEAKS, NONE NOTED. RAN ENGINE THROUGH NUMEROUS POWER SETTINGS, NO ODOR NOTED. COULD NOT DUPLICATE DISCREPENCY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUT — CHAFED (NACELLE) · airframe 9,066 hrs · 12,614 cycles
PDX - DURING INSPECTION, FOUND TWO CHAFED AREA''S IN LOWER INBOARD ENGINE NACELLE SUPPORT STRUT. REPAIRED IN ACCORDANCE WITH ENGINEERING APPROVED REPAIR DRAWING RII COMPLIED WITH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (COCKPIT) · airframe 9,048 hrs · 12,590 cycles
PDX - FLIGHT COMPARTMENT EMERGENCY EXIT SIGN REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 8,781 hrs · 12,224 cycles
SEA- MAIN CABIN DOOR VERY STIFF TO OPEN. CLEANED AND LUBED DOOR LINKAGE AND STOPS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
2000
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,085 hrs · 11,303 cycles
PDX- OVERHEAD COCKPIT EMERGENCY PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED OVERHEAD EMERGENCY PORTABLE LIGHT.
Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 6,473 hrs · 9,103 cycles
SEA- FORWARD SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PS-5. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
1999
Part: JAMB — DAMAGED (CARGO DOORWAY)
PDX - CARGO DOOR UPPER APERTURE JUST BEFORE BOTH TOP PRESSURE PADS HAVE DAMAGE FROM DOOR STOPS. REPAIRED IAW HORIZON AIR EA 2-53-79.
Part: ANGLE — DAMAGED (FUSELAGE)
PDX - LEFT-HAND FORWARD INBOARD CONNECTION ANGLE AT AFT END HAS DAMAGE ATTACHMENT HOLES. REPAIRED IAW HORIZON AIR EA 2-53-78.
Part: SEAT TRACK — CORRODED (BS 202-222)
PDX - LEFT-HAND INBOARD SEAT TRACK FROM STA 202.750 TO 222.700 HAS MINOR SURFACE CORROSION AND LIGHT PITTING. REPAIRED IAW SHC-8 SRM 51-40-11 AND SRM 51-40-00.
Part: SKIN — DENTED (FUSELAGE)
PDX - SMALL DENT/SCRATCH IN FUSELAGE SKIN 6 INCHES ABOVE AND 1 INCH AFT OF RIGHT-HAND PITOT TUBE. REPAIRED IAW HORIZON AIR EA 2-53-76.
Part: SKIN — CHAFED (CARGO DOOR)
PDX - CARGO DOOR SKIN SMALL CHAFED AREA NEAR AFT UPPER CORNER. REPAIRED IAW HORIZON AIR EA 2-52-28.
Part: SKIN — CHAFED (LT WING)
PDX - LIGHT FRETTING CORROSION AROUND SEVERAL SCREW HOLES AND LIGHT CHAFING DAMAGE ON LOWER LEADING EDGE ATTACH FLANGE OF THE LEFT-HAND WING, FORWARD SPAR. REPAIRED IAW DHC-8 PSM 1-8-3, CHAPTER 51-20-26.
Part: SEAT TRACK — CORRODED (CARGO COMPT)
PDX - RIGHT-HAND INBOARD SEAT TRACK HAS MINOR CORROSION WHERE CARGO TIE DOWN MOUNTS. REPAIRED IAW HORIZON AIR EA 2-53-73.
Part: SKIN — CHAFED (LT TE FLAP)
PDX - LEFT-HAND WING OUTBOARD FLAP TOP SKIN SURFACE HAS HEAVY CHAFING DAMAGE FROM MAKING CONTACT WITH WING. REPAIRED IAW HORIZON AIR EA 2-57-26.
Part: PADS — WORN (CARGO DOOR)
PDX - BOTH BOTTOM PRESSURE PADS FOR LOWER DOOR STOPS GROOVES WORN IN THEM. REPAIRED IAW 51-20-16 AND RD 8-53-104 AND HORIZON AIR EA 2-53-70.
Part: SKIN — CHAFED (FUSELAGE)
PDX - LEFT-HAND SIDE FUSELAGE AREA FOR PANEL 261DT HAS CHAFE DAMAGE. REPAIRED IAW DHC MM 20-32-02, PAGE 202 PARAGRAPH D1-6.
Part: SKIN — DENTED (FUSELAGE)
PDX - RIGHT-HAND SIDE FUSELAGE AREA FOR PANEL 261NT HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 MM 20-32-02, PAGE 202, PARAGRAPH D1-6.
Part: SKIN — DENTED (FUSELAGE)
PDX - DENT IN REAR FUSELAGE RIGHT-HAND SIDE BETWEEN FRAME 2 AND 3 AND STRINGERS 20 AND 21. REPAIRED IAW DHC-8 SRM 53-30-24, PAGE 2, FIGURE 1 SHEET 1.
1998
Part: WIRE — BROKEN (CARGO SMOKE DET)
EAT- BAGGAGE SMOKE DETECTOR LIGHT REMAINS ON. MAINTENANCE PLACED ON MEL. MEL CLEARED ON 12/4/98 BY REPAIRING WIRES THAT GOT CAUGHT IN DOOR ROLLERS. WRAPPED WIRES TO PREVENT REOCCURRANCE. OPERATIONAL CHECKS GOOD, NO PARTS REPLACED.
Part: BATTERY — DISCHARGED (CABIN)
FORWARD LEFT EXTERNAL EMERGENCY LIGHT IS INOP. REPLACED PS1 BATTERY PACK, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
FORWARD LEFT EMERGENCY AIRSTAIR LIGHT INOP. RELAMPED, OPERATIONAL CHECKS GOOD.