N355PH
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.
223 reports on file, 1997-12-24 – 2008-06-28.
Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 24,058 hrs · 34,904 cycles
PDX - CREW REPORTS OIL ODOR IN CABIN. FOUND ENGINE OIL FOR NR 1 OVER SERVICED. ADJUSTED LEVEL. GROUND RUN CHECKS OK. RETURNED TO SERVICE. NO PARTS REPLACED. (A)
Part: STRUT — CHAFED (RT MLG) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING MID ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP IAW -8/200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. PERFORMED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IAW -8/200 CMM 32-10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A. PRIMED PAINTED IAW
Part: INTERCOSTAL — CORRODED (BS 190-201 S31L)
C4-CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL AT BELLY SKIN, JUST OB OF STRINGER 31P FROM STA X190 TO X201. REPAIRED IAW SRM. (K)
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y546 AND Y35.5L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .003 MATERIAL FROM .045 ORIGINAL THICKNESS, .042 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED PAINTED IAW -8 200 SRM 51-20-16, 51-20-36 PG 6 PARA F(1) AND 51-20-26 PG 8 PARA B(1-6).
Part: SEAT TRACK — CORRODED (BS 333) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK FUSELAGE INTERIOR WEB THAT TIES INTO LT O/B SEAT TRACK HAS AN OVERSIZED HOLE LOCATED 2" AFT OF FRAME 333.300. REMOVED WEB BETWEEN FRAMES 333.30 AND 354.25 NEXT TO LH O/B SEAT TRACK. FABRICATED NEW WEB IAW T/C 2-53-836. INSTALLED WEB IAW -8 200 SRM 51-40-11.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK SUSPECT CORROSION AT I/B BOTTOM OF VERTICAL KEELBEAM AT STA X370 AND STR 31P. REMOVED CORROSION AT BOTTOM OF VERTICAL KEEL BEAM STA 370.8. REF CPM CHAP 4 PG 4-25 PARA 9. ORIGINAL THICKNESS .050" REMAINING THICKNESS .046". MAX MATERIAL REMOVED .004 WITHIN LIMITS REF -8 200 SRM 51-20-11 PARA 3. HFEC INSP. IAW -8 200 NDTM PT6, 51-00-01 NO CRACKS NOTED. ETCHED ALODINE PRIME REF -8 CPM CHAP 5, PARA 2C.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK SUPPORT BRACKET UNDER MCD SILL IS CRACKED. R&R SUPPORT BRACKET WITH NEW FROM STOCK REF -8 200 SRM 51-40-11 FOR RIVETING.
Part: STRUCTURE — CORRODED (CABIN) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK ZONE 144 SUBFLOOR TOP SURFACE IS CORRODED AT Y580-X581 AND Y24L-Y26L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .002 MATERIAL FROM ORIGINAL THICKNESS. .043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. C/W CPM CHAP 5 FOR SURFACE TREATMENT. PRIMED AND PAINTED IAW SRM 51-20-26 PARA 5A.
Part: FRAME — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK SUSPECT CORROSION OF FRA X201 AT STR 31S. REMOVED CORROSION IAW CPM CHAP 4 PARA 9A-B(1-6(A)). UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI .032 LOW .029. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED IAW -8 200 SRM 51-20-16, 51-20-36.
Part: FLAP — CHAFED (RT WING) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK RT O/B FLAP HAS A CHAFFED AREA AT THE O/B END APPROX 10" FROM THE TRAILING END. BLENDED ARE OF CHAFE, FOUND OUT OF LIMITS IAW -8 200 SRM 57-50-16. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI .025, LO .017. MAPPED FOR ENG. FOUND WITHIN LIMITS PER RD8-57-3923. UT DISBONDING CHECK IAW -8 200 NDTM PT 1, 51-00-04, NO DISBOND NOTED. ALODINE PRIMED, PAINTED IAW -8 200 RD8-57-3923 NOTES 5 AND 6.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. SURFACE CORROSION ON SEAT TRACK NR 7 BETWEEN STA X220 AND X226. REMOVED NR 7 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102.
Part: STRUT — CHAFED (RT MLG STRUT) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING UPPER ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFORMED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IAW -8/200 CMM 32-10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A PRIMED PAINTED IAW
Part: SUPPORT BRACKET — DAMAGED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK LT O/B SEAT TRACK SUPPORT BRACKET ON FWD SIDE OF FRAME AT STA X333.3 HAS DAMAGED HOLE, 2ND HOLE AFT TOP. REMOVED LT O/B SEAT TRACK SUPPORT BRACKET FWD SIDE FRAME AT STA X3333.3. INSTALLED NEW BRACKET FROM STOCK AT LT O/B SEAT TRACK ON FWD SIDE OF FRAME AT STA 333.3 IAW -8 200 SRM 51-40-11.
Part: DOOR — GOUGED (CARGO BAY) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CARGO DOOR HAS SEVERAL GOUGES ON CENTER FWD LOWER SIDE. REMOVED DAMAGE IAW -8 200 51-20-11. HFEC INSP IAW -8 200 NDTM PT6, 51-00-01 NO CRACKS NOTED. WITHIN LIMITS PER -8 200 52-00-16. ALODINED PRIMED IAW SRM 51-20-36.
Part: FITTING — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK FITTING CORRODED JUST AFT OF CARGO DOOR FUSELAGE CUTOUT, LOWER AFT CORNER. REMOVED CORRODED FITTING AT AFT LOWER CORNER IAW -8 200 SRM 51-40-11. INSTALLED NEW FITTING IAW -8 200 SRM 51-40-11 AND RD8-51-102.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y29.5R. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI .083 LOW .077. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. REMOVED .006" MATERIAL FOUND WITHIN LIMITS PER -8 200 SRM 51-20-11 STEP 3. PREP PRIMED, PAINTED IAW 51-20-16, 51-20-36 PARA F,1 AND 51-20-26 PG 8, PARA B(1-6).
Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CORROSION ON STR 23S (X387 TO X392) AND CONNECTING CLIP TO FRONT SPAR MAIN FRAME ON AFT SIDE AT X387.35. REMOVED LIGHT SURFACE FROM STRINGER AND CONNECTING CLIP USING SCOTCH BRITE PAD. ALODINED EXPOSED ALUM. IAW -8 200 CPM CHAP 4 AND 5. NEGLIGIBLE MATERIAL REMOVED. PRIMED IAW 51-20-36PG 6 PARA F1.
Part: STOP FITTING — WORN (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. MCD SURROUND STOP FITTINGS ALL HAVE SIGNS OF WEAR. BLENDED FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 1.2. WITHIN LIMITS. INSPECTED AS PER RD8-53-3933 NO CRACKS NOTED. COLD GALV. PRIMED STOP FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 4-7.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CORROSION ON RT O/B SEAT TRACK AT APPROX X488.5. BLENDED OUT CORROSION IAW RD8-53-10103. ALODINE PRIMED IAW -8 200 SRM 51-20-16, 51-20-36.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK BRACKET FOR NR 1 SEAT TRACK WEB AFT OF FRAME 354 IS DAMAGED. REMOVED BRACKET IAW -8 200 SRM 51-40-11. INSTALLED NEW BRACKET IAW -8 200 SRM 51-40-00, 51-40-11.
Part: STRUCTURE — CORRODED (CABIN) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y565 AND Y25L-Y27L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .002 MATERIAL FROM ORIGINAL THICKNESS, .043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED PAINTED IAW -8 200 SRM 51-20-16, 51-20-36 PG 6 PARA F(1) AND 51-20-26 PG 8 PARA B(1-6).
Part: KEELBEAM — CORRODED (BS 201 S31P)
C4-CHECK- SUSPECT CORROSION ON BOTTOM OF VERT KEEL BEAM AT STR 31P AND STA X201. REPAIRED IAW SRM. (K)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. CORROSION ON SEAT TRACK NR 1 AT APPROX. STA X360. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-00. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CORROSION ON FORE AND AFT LOWER CORNER COMBING PIECES, I/B FLANGE, ON PAX DOOR APERTURE LOWER EDGE. REMOVED NUTPLATE FROM CASTING AND REMOVED CORROSION. REMOVED .002" MATERIAL REF CPM SECT 4. WITH IN LIMITS PER -8 200 SRM 51-20-11. REINSTALLED NUT PLATE ON CASTING.
Part: HINGE FITTING — CORRODED (CARGO DOOR) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK - MCD LAY SHAFT, AFT HINGE FITTING HAS PITTING AROUND BOLT HOLES. REMOVED MCD LAY SHAFT. SEPARATED LAYSHAFT AND DRILLED OUT AFT HINGE FITTING. DRILLED UP AND INSTALL NEW HINGE FITTING REF SRM 51-40-00. INSTALLED MCD LAY SHAFT.
Part: FLOOR SKIN — CORRODED (CARGO BAY) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CORROSION AT CARGO PIT DECK SKIN I/B AND BELOW CORNER FITTING STA X597.5, Y40.95. REMOVED CORROSION USING SCOTCH BRITE PAD IAW -8 200 SRM 51-40-11 AND CPM CHAP 4 PG25-26. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04, HI.063 AND LOW .058. WITHIN LIMITS IAW -8 200 SRM 51-20-11. ALODINED PRIMED IAW -8 200 SRM 51-20-16 AND 51-20-36.
Part: FLOOR SKIN — CORRODED (CARGO BAY) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK CARGO PIT LOWER FLOOR DECK SKIN HAS CORROSION ALONG RIVET ROW AT STA X600 BETWEEN Y10L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI.040 LO.038. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. BLEND WITHIN LIMITS IAW -8 200 SRM 51-20-11 C.3 F. ALODINED AND PRIMED IAW SRM -8 200 51-20-16.
Part: STRUT — CHAFED (RT MLG) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE AT LOWER O/B SURFACE WHERE O/B WOW HARNESS CONDUIT HAS CONTACTED. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFORMED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IAW -8/200 CMM 32-10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A.
Part: CASTING — CORRODED (CARGO DOOR) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. FWD CORNER CASTING ON MCD HAS CORROSION AROUND NUTPLATE, TOP AND BOTTOM. REMOVED FWD CORNER MCD CASTINGS AND INSTALL NEW CASTING REF -8 200 SRM 51-40-00 AND 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. CORROSION ON SEAT TRACK NR 4 CAMLOCK RECEP. STA X222. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y20L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI .083 LOW .061. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. REMOVED .022" MATERIAL FOUND OUT OF LIMITS PER -8 200 SRM 51-20-11 STEP 3. DRILLED AFFECTED FLOOR SUPPORT ANGLE OFF AND INSTALL NEW ANGLE IAW -8 200 SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. LT SEAT TRACK NR 2 HAS CORROSION AT APPROX STA 438 STA 466.5, STA 485, AND STA 498. REMOVED SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11.
Part: FITTING — CORRODED (FUSELAGE) · airframe 23,775 hrs · 34,452 cycles
PDX C4 CHECK. TENSION FITTING LOCATED AT FRAME X201 STR 31S HAS CORROSION. REMOVED TENSION FITTING AND INSTALLED NEW FITTING IAW 8 200 SRM 51-40-11, 51-20-36.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 23,775 hrs · 34,452 cycles
SEA - LAVATORY SMOKE DETECTOR WENT OFF. NO EVIDENCE OF SMOKE, OR FIRE. MAINTENANCE COMPLIED WITH A OPERATIONAL CHECKS OF THE SYSTEM AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: UNKNOWN — ODOR (CABIN) · airframe 23,775 hrs · 34,452 cycles
SEA - LAVATORY SMOKE DETECTOR WENT OFF FOR THE SECOND TIME. NO SMOKE OR FIRE NOTED. ON THE FLIGHT DECK THOUGH NOTICED A ODOR IN THE AIR AND BOTH PILOTS SENSED A SCRATCHING IN THEIR THROATS. MAINTENANCE FOUND ENGINE OIL IN THE NR 1 LP FOR THE ENGINE. AIRCRAFT FERRIED TO PDX FOR REPAIRS.
Part: DOOR — OPEN · airframe 23,765 hrs · 34,436 cycles
SEA - AFTER TAKEOFF, TRIED TO RAISE THE GEAR AND THE GEAR DOOR LIGHTS WERE STILL ILLUMINATED ALONG WITH THE LEFT AND RIGHT UNSAFE LIGHTS. A LOUD FLAPPING SOUND WAS HEARD. VISUAL INSPECTION SHOWED THE GEAR TO STILL BE DOWN. CYCLED THE GEAR AND PROBLEM REMAINED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. TRASH BAGS AROUND THE ALTERNATE EXTENSION RELEASE DOOR CAUSED INTERFERENCE. ENSURED THAT THE ALTERNATE EXTENSION DOOR WAS COMPLETELY CLOSED. OPERATIONAL CHECKS GOOD NO PARTS REPLACED.
Part: CONNECTOR — DAMAGED (SMOKE DETECTOR) · airframe 23,699 hrs · 34,334 cycles
SEA - FLIGHT 2101 - LAVATORY SMOKE DETECTOR GOES OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE PLACED ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 3/31 BY CONNECTING THE PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 23,626 hrs · 34,227 cycles
PDX - FLIGHT 2193, ON APPROACH THE LAVATORY SMOKE DETECTOR WENT OFF TWICE. BOTH TIMES THE FLIGHT ATTENDANT REPORTED NO INDICATIONS OF SMOKE. AIR WAS SMOOTH AND THE BLEEDS WERE ON MAX. MAINTENANCE REPLACED THE AIR CYCLE MACHINE, CONDENSER/MIXER AND HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 23,597 hrs · 34,183 cycles
YKM - FLIGHT 2002 - LAVATORY SMOKE DETECTOR WENT OFF WITH NO SMOKE DETECTED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. CLEARED BY REPLACING THE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: INDICATOR — SMOKE (RADAR) · airframe 23,576 hrs · 34,085 cycles
PDX - FLIGHT 2058 - WHEN APPLYING ELECTRICAL POWER TO THE IRU AND FMS. SMOKE NOTICED FROM THE AREA BETWEEN THOSE UNITS AND THE RADAR INDICATOR. MAINTENANCE POWERED UP EACH UNIT ON IT'S OWN. THE RADAR DISPLAY (INDICATOR) STARTED TO SMOKE. REPLACED THE RADAR INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ALTIMETER — MALFUNCTIONED (NR 1) · airframe 23,488 hrs · 34,007 cycles
SEA - FLIGHT 2027, RETURNED TO THE FIELD FOR THE CAPTAIN'S ALTIMETER FLAGGING AT 420 FEET. MAINTENANCE REPLACED THE NR 1 ALTIMETER. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SERVO — JAMMED (AILERONS) · airframe 23,448 hrs · 33,947 cycles
PDX - FLIGHT 2193 (OTH-PDX) ON APPROACH WITH THE AUTOPILOT ON, EXPERIENCED A UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WAS TURNED OFF AND THE WHEEL APPEARED TO BE JAMMED (NO MOVEMENT POSSIBLE). CONTROL THEN BECAME UN-JAMMED AND OPERATED NORMALLY AFTER A FEW SECONDS. LANDED WITH SPOILER CONTROL ONLY. EMERGENCY DECLARED WITH ATC. LANDING UNEVENTFUL. MAINTENANCE REPLACED THE AUTOPILOT AILERON SERVO. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 1997–2007 · 181 reports
2007
Part: DRAIN MAST — FROZEN (NR 1 ENGINE) · airframe 23,171 hrs · 33,535 cycles
RDM - FLIGHT 2191 - ON SHUTDOWN AT THE GATE, RAMP NOTICED SMOKE FROM THE TOP OF NR 1 ENGINE. MAINTENANCE CHECKED NACELLE AND ENGINE AREA AND FOUND NO SOURCE FOR THE SMOKE. FOUND SOME ICE IN THE COWL DRAIN MAST AND THAWED OUT. PERFORMED ENGINE RUNS AT TEMPERATURE AND SHUT DOWN WITH NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: LAMP — INOPERATIVE (HEATER) · airframe 23,040 hrs · 33,344 cycles
PDX - FLIGHT 2011 - HEATER LIGHT ON LEFT ENGINE INTAKE BYPASS DOOR DOES NOT TEST. RETURNED TO THE GATE. MAINTENANCE REPLACED THE LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BLADE — MALFUNCTIONED (NR 2 PROPELLER) · airframe 22,459 hrs · 32,463 cycles
BOI FLIGHT NR 2115, SPARKS OBSERVICED FROM NR 2 PROP ON CLIMB-OUT. REPLACED BLADES NR 1 AND NR 4 ON NR 2 PROP PER TC 9611003. S/N 9801028-23, TSN 89.53, CSN 134. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RELAY — MALFUNCTIONED (AUTOFEATHER) · airframe 21,874 hrs · 31,597 cycles
SEA FLIGHT NR 2019 ON TAKEOFF, AUTOFEATHER FAILED TO ARM. REPLACED NR 1 POWER LEVER LIMIT SWITCH 6121-S7, ADJUSTED SWITCH. REPLACED RELAY 6121-K15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: AUTOFEATHER SYS — NONE · airframe 21,740 hrs · 31,402 cycles
SEA FLIGHT NR 2110 ON TAKEOFF, AUTOFEATHER SWITCH LIGHT DAR. TAKEOFF ABORTED AT 60KTS. MAINTENANCE PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM TEST IAW -8200 ENGINE RIG MANUAL 6-8, PAGE 3-65, STEPS B1-13. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (GALLEY) · airframe 21,543 hrs · 31,112 cycles
SEA FLIGHT NR 2017, BURNING RUBBER ODOR FROM MAPCO, GALLEY EQUIPMENT INOP. MAINTENANCE PLACED MAPCO ON MEL.
Part: TRANSDUCER — MALFUNCTIONED (STALL WARNING) · airframe 21,276 hrs · 30,718 cycles
PDX FLIGHT NR 2200, IMMEDIATELY AFTER TAKEOFF, NR 1 STALL WARNING CAUTION LIGHT ILLUMINATED STALL WARNING INOP. MAINTENANCE REPLACED THE NR 1 STALL WARNING TRANSDUCER. COMPLIED WITH FUNCTION TEST OF STALL WARNING SYSTEM IAW AMM 27-330-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2006
Part: LATCH — UNSECURE (ENGINE COWL) · airframe 21,009 hrs · 30,336 cycles
SEA - ON FLIGHT 2224, RETURNED TO GATE. ENGINE COWL NR 2 LATCH OPEN. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: PITOT SYSTEM — ODOR (COCKPIT) · airframe 20,973 hrs · 30,290 cycles
SEA FLIGHT NR 2244, FUNNY ODOR IN COCKPIT. MAINTENANCE INVESTIGATED SMELL, FOUND PITOT HEAT SWITCHES IN "ON" POSITION. DETERMINED ODOR COMING FROM PITOT SOURCE. TURNED SWITCHES OFF. ODOR DISSIPATED. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE.
Part: GENERATOR — MALFUNCTIONED (AC SYSTEM) · airframe 20,587 hrs · 29,754 cycles
PDX FLIGHT NR 2147 ON TAXI OUT F/O NOTED AC LOAD OF .35 ON PHASE A WITH NR 2 PROP OUT OF FEATHER AND NR 1 PROP IN FEATHER. TURNED WINDSHIELD HEAT OFF AND NOTED AC LOAD ON PHASE A DROPPED TO .33, BUT PHASE C LOAD WAS AT .36. MAINTENANCE REPLACED THE NR 1 AC GENERATOR IAW AMM TASK 24-21-00-000-801 AND 24-21-00-400-801. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.
Part: YAW DAMPER — INOPERATIVE · airframe 20,087 hrs · 29,022 cycles
YKM FLIGHT 2003 RIGHT YAW DAMPER INOP. MAINTENANCE PERFORMED AFCS OPERATION GROUND POWER UP TEST. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: CAUTION MESSAGE — ILLUMINATED (AUX INVERTER) · airframe 19,877 hrs · 28,709 cycles
SEA FLIGHT 2285 AUXILIARY INVERTER CAUTION. MAINTENANCE PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE.
Part: PRESSURE SWITCH — DIRTY (RUDDER PRESSURE) · airframe 19,816 hrs · 28,614 cycles
PDX FLIGHT NR 2163, RUDDER PRESSURE CAUTION ILLUMINATED BELOW 140 KTS. MAINTENANCE CLEANED CONTAMINATION FROM DUAL PRESSURE REGULATOR PRESSURE SWITCHES. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: VALVE — LEAKING (RT ENGINE) · airframe 19,710 hrs · 28,448 cycles
PDX FLIGHT NR 2268 NR 2 NACELLE FLUID LEAK. MAINTENANCE RESEATED SPR ADAPTER POPPET VALVE. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC- C4 FUSELAGE INTERIOR WEB ATTACH ANGLE IS CORRODED ON THE FORWARD SIDE OF FRAME AT STATION X 424, LEFT HAND STRINGER 23. REPAIRED IAW SRM 51-40-00 AND SRM 53-00-16.
Part: SHOCK ABSORBER — CHAFED (RT MLG) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT HAND NACELLE, MAIN LANDING GEAR AREA, SHOCK STRUT HAS CHAFING DAMAGE AT LOWER/FORWARD END OF CYLINDER. CHAFING IS CAUSED BY WEIGHT ON WHEEL WIRING CONDUIT CONTACT. REPAIRED IAW RD8-32-1575 AND EA 2-32-108.
Part: FITTING — CHAFED (AIR STAIR DOOR) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 AIR STAIR DOOR SHELL FORWARD UPPER AND LOWER STEP BOLT FITTINGS CHAFED, AFT LOWER FITTING CHAFED. REPAIRED IAW RD8-52-828 AND EA 2-52-224.
Part: STOP — WORN (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT EMERGENCY EXIT OPENING. FORWARD AND AFT DOOR STOPS WORN WITH PITTING. REPAIRED IAW RD8-52-126.
Part: STOP FITTING — WORN (RT EMER DOOR) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 CENTER FUSELAGE RIGHT EMERGENCY DOOR CUTOUT, AFT UPPER AND LOWER STOP FITTINGS HAVE WEAR DAMAGE. REPAIRED IAW RD8-53-126.
Part: STOP — WORN (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT FORWARD TYPE II EMERGENCY EXIT. FORWARD AND AFT DOOR STOPS WORN WITH PITTING. REPAIRED IAW RD8-52-349.
Part: SKIN — CHAFED (RT FLAP) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT FLAP UPPER SKIN OUTBOARD END HAS CHAF MARK FROM TRAILING EDGE. REPAIRED IAW RD8-57-3376 AND EA 2-57-365.
Part: SKIN — CHAFED (RT OB FLAP) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT OUTBOARD FLAP UPPER SKIN HAS CHAF MARK FROM TRAILING EDGE. REPAIRED IAW RD8-57-3376 AND EA 2-57-365.
Part: SKIN — DENTED (TAILCONE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE EXTERIOR, TAIL CONE LEFT HAND SIDE SKIN AT STATION X 718 AND Z 155 IS DENTED. REPAIRED IAW RD8-55-1689 AND EA 2-55-123.
Part: DRAG STRUT — CHAFED (RT NACELLE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT HAND NACELLE, MAIN LANDING GEAR AREA, DRAG STRUT ASSY HAS CHAFING DAMAGE FROM CONTACT WITH WEIGHT ON WHEEL WIRING RIGID CONDUIT NEAR LOWER ATTACH POINT. REPAIRED IAW RD8-32-1566 AND EA 2-32-107.
Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT NACELLE FINGER NAIL UPPER RIGHT SIDE AT STATION XN 270 CRACKED AT FASTENERS. REPAIRED IAW RD8-54-2184 AND EA 2-54-279.
Part: ATTACH BRACKET — CORRODED (LT WING) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT HAND WING FRONT SPAR ATTACH BRACKET AT YW 58.0 IS CORRODED, BRACKET IS BLEED AIR DUCT ATTACHMENT SUPPORT. REPAIRED IAW EA 2-57-366, SRM 51-40-11.
Part: WEB — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR WEB IS CORRODED ON THE AFT SIDE OF FRAME AT STATION X 424, LEFT HAND STRINGER 23. REPAIRED IAW SRM 51-40-00 AND SRM 53-00-16.
Part: COWL DOOR — CHAFED (RT NACELLE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT NACELLE OUTBOARD COWL DOOR 424AR HAS CHAFING DAMAGE THROUGH THE BOTTOM EDGE CHANNEL. REPAIRED IAW RD8-71-0507 AND EA 2-71-302.
Part: HINGE — WORN (VERTICAL STAB) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 VERTICAL STAB TOP SAFETY HINGE FOR THE FORE RUDDER ATTACHMENT HAS DEEP WEAR MARK ON TOP SURFACE. REPAIRED IAW RD8-57-752.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT, LOWER DOOR SILL ATTACH ANGLE ON THE FORWARD SIDE OF FRAME AT STATION X 600 AND LBL 30 IS CORRODED. REPAIRED IAW SRM 51-40-11.
Part: STRUCTURE — CORRODED (RT WING) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT HAND WING UPPER ACCESS 622AT, COUNTERSINK HOLES HAVE FRETTING CORROSION. REPAIRED IAW RD8-57-1715.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT SEAT TRACK LEFT HAND INBOARD AT STATION X 598 AND Y 9.25 HAS NICKS AND CORROSION INSIDE AND ON TOP OD CLAW PORTION. REPAIRED IAW RD8-53-4936 SRM 51-20-16 AND SRM 51-20-36.
Part: SKIN — NICKED (EMERGENCY EXIT) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT HAND CENTER EMERGENCY EXIT EXTERIOR SKIN HAS SMALL NICK. REPAIRED IAW RD8-53-5384.
Part: SEAT TRACK — CORRODED (BAGGAGE COMP) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT SEAT TRACK RIGHT HAND INBOARD AT STATION X 598 AND Y 9.25 HAS NICKS AND CORROSION INSIDE AND ON TOP OD CLAW PORTION. REPAIRED IAW RD8-53-4936 SRM 51-20-16 AND SRM 51-20-36.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 CABIN ROOF, CARGO DOOR FORWARD TRACK SUPPORT STRUT, ATTACH ANGLE IS CRACKED AT STATION X 565.0 AND LEFT HAND STRINGER 5. REPAIRED IAW SRM 51-40-00 AND SRM 51-40-11.
Part: SKIN — DENTED (LT AILERON) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT HAND AILERON, TOP SKIN DENTED, MID AREA AT STATION YW 457. REPAIRED IAW SRM 57-60-21 AND SRM 57-60-71.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR FS 222.7 RIGHT HAND INBOARD SEAT TRACK AT Y 9.25 HAS COROSION ON UPPER SURFACE. REPAIRED IAW RD8-53-4478 AND RD8-53-3403.
Part: FITTING — WORN (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR LEFT HAND STATION X 252, STRINGER 11 DOOR SURROUND STOP UPPER FITTING WORN. REPAIRED IAW RD8-53-3933.
Part: SKIN — CHAFED (RT FLAP) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT HAND INBOARD FLAP TOP SKIN HAS CHAFED MARK FROM TRAILING EDGE. REPAIRED IAW SRM 51-20-11, SRM 57-50-16, AND SRM 51-20-51.
Part: PLATE — DAMAGED (WING) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT HAND CENTER WING, LADDER PLATE UNDER PANEL 522AT HAS FRETTING DAMAGE BETWEEN YW 62 - YW 77. REPAIRED IAW RD8-57-1471 AND SRM 51-20-36.
Part: RIVET — LOOSE (LT NACELLE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT NACELLE, INBOARD SIDE, STATION XN122, BELOW WING LEADING EDGE, SEVERAL RIVETS ARE LOOSE. REPAIRED IAW RD8-54-1193.
Part: STRUCTURE — GOUGED (WING) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT HAND, TOP REBATE AT STATION YW 260.0 IS GOUGED. REPAIRED IAW RD8-57-1675 AND SRM 51-20-36.
Part: FRAME — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR UNDERFLOOR FRAME FLANGES BETWEEN STRINGERS 32P - 32S HAVE CORROSION AROUND RIVETS AT STATION X 405. REPAIRED IAW SRM 51-40-1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR UNDERFLOOR, FLOOR SUPPORT FITTING AT FS 240.0 Y24.0 LEFT HAND HAS CORROSION ON TOP SURFACE. REPAIRED IAW SRM 51-40-11 AND EA 2-53-743.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FORWARD FUSELAGE EXTERIOR LEFT SIDE. SKIN PANEL HAS 1 SHARP OUTWARD DENT AT FSX260.0 BETWEEN STRINGER 30L AND 31L. REPAIRED IAW RD8-53-2181.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FORWARD FUSELAGE EXTERIOR LEFT HAND SIDE. SKIN PANEL HAS 1 SHARP OUTWARD DENT AT FSX 380.0 BETWEEN STRINGER 30L AND 31L. REPAIRED IAW RD8-53-2181.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR FORWARD RIGHT HAND EMERGENCY EXIT OPENING, FORWARD FRAME STATION X 240, FLOOR LEVEL TRIM SUPPORT ANGLE HAS CORROSION AT A-NUT LOCATION. REPAIRED IAW SRM 51-40-00, AND SRM 51-20-11.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 RIGHT FORWARD EMERGENCY EXIT OPENING, AFT FRAME STATION X264 LOWER ATTACH ANGLE ON FRAME AND SEATRAIL HAS CORROSION. REPAIRED IAW SRM 51-40-00, SRM 51-20-11.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FORWARD FUSELAGE EXTERIOR RIGHT SIDE. SKIN PANEL HAS 1 SHARP OUTWARD DENT AT FSX252.0 BETWEEN STRINGER 28R AND 29R. REPAIRED IAW RD8-53-2181.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT HORIZONTAL FLOORBOARD ANGLE ON THE FORWARD SIDE OF FRAME AT STATION X 600 AND RBL 28 IS CORRODED. REPAIRED IAW PSM 1 - GENERAL 5 PART CHAPTER 4, PARAGRAPH 9.
Part: STIFFENER — CRACKED (LT NACELLE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 LEFT HAND NACELLE, OUTBOARD COWLING DOOR PANEL 413AL, INTERNAL STIFFENER FOR BLOWOUT DOOR IS CRACKED. REPAIRED IAW RD8-71-213.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FUSELAGE INTERIOR BAGGAGE COMPARTMENT, FLOOR SKIN DIRECTLY UNDER FLOOR PANEL 144AZ HAS AREAS OF CORROSION ON TOP FROM STATION X 600 TO X 564 AND LBL 10 TO LRL 26, AND UNDER 3 A-NUTS AT STATION X 580 AND LBL 16. REPAIRED IAW SRM 51-40-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 AFT FUSELAGE EXTERIOR LEFT HAND SIDE. SKIN PANEL HAS 1 SHARP OUTWARD DENT AT FSX521.0 BETWEEN STRINGER 27L AND 28L. REPAIRED IAW RD8-53-2181.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,627 hrs · 28,328 cycles
YYC - C4 FORWARD FUSELAGE EXTERIOR LEFT SIDE. SKIN PANEL HAS 1 SHARP OUTWARD DENT AT FSX205.0 BETWEEN STRINGER 30L AND 31L. REPAIRED IAW RD8-53-2181.
2005
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,823 hrs · 27,180 cycles
PDX FLIGHT NR 2132 FLIGHT LEVEL 220, FIRST OFFICERS WINDSHIELD SHATTERED. EMERGENCY DECLARED. LANDED WITHOUT INCIDENCE. MAINTENANCE REPLACED CO-PILOTS WINDSHIELD IAW Q200 AMM TASKS 56-10-11-000-801 AND 56-10-11-400-801. OPERATIONAL TEST OF WINDSHIELD HEAT GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BRUSH BLOCK — BURNED · airframe 18,811 hrs · 27,165 cycles
SEA FLIGHT NR 2285 LT TRU CAUTION LIGHT AND ASSOCIATED CIRCUIT BREAKERS POPPED. LT PROP HEAT LIGHTS NOT ILLUMINATING. MAINTENANCE FOUND NR2 BRUSH BLOCK BURNED, REPLACED BRUSH BLOCK IAW Q200 AMM 61-10-11 AND 61-10-11-820-801. ALSO FOUND AC FUSE POPPED. REPLACED FUSE AS REQUIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 18,382 hrs · 26,550 cycles
PDX - EMERGENCY LIGHTS AT CABIN CENTER OVERHEAD, AFT OVERHEAD AND OUTSIDE RIGHTHAND AFT ARE INOP. REPLACED NR 4 EMERGENCY BATTERY PACK AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: TIRE — BLOWN (ZONE 700) · airframe 18,128 hrs · 26,168 cycles
BOI - ON FLIGHT 2204, NR 1 MAIN LANDING GEAR WHEEL BLOWN ON TAKEOFF. TIRE BLEW BEFORE RETRACTING GEAR. BELOW MAX LANDING WEIGHT. VERIFIED WITH CREW AIRCRAFT WAS BELOW MAX LANDING WEIGHT. C/W INSPECTION OF TIRE AND NACELLE/ENGINE AREA, FOUND LEFT OUTBOARD AFT DRAG STRUT FAIRING DAMAGED, NO OTHER DAMAGE NOTED. ALSO, INSPECTED PROPS AND ENGINE INLET AREA WITH NO DEFECTS NOTED. REMOVED AND REPLACED BOTH NR 1 AND NR 2 MAIN TIRES. INSPECTED BRAKES AND HYDRAULIC LINES WHILE TIRES REMOVED WITH NO DAMAGE NOTED.
Part: RELAY — INOPERATIVE (PROP FEATHER) · airframe 17,695 hrs · 25,498 cycles
RETURNED TO GATE, FAILURE OF AUTOFEATHER TO ARM ON TAKEOFF. AIRSPEED 60 KTS. TRQ APPROX 85 PERCENT. REMOVED AND REPLACED 6121 K-5 RELAY. ALL CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 17,649 hrs · 25,431 cycles
PDX-AFT TWO RED LIGHTS ON FLOOR TRACK LIGHTING AT ROW 1DE INOPERATIVE. REMOVED AND REPLACED PS6 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LINE — CRACKED (HYDRAULIC SYS) · airframe 17,025 hrs · 24,491 cycles
BLI - FLIGHT 2136 - UPON GEAR DOWN SELECTION, THE NR 2 ENGINE HYDRAULIC FLUID QUANTITY AND PRESSURE WAS TOTALLY LOST. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWN HYDRAULIC LINE CRACKED. THE LINE WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 17,003 hrs · 24,457 cycles
SEA - FLIGHT 2006 - THE CREW REPORTS THE SMOKE DETECTOR LIGHT ILLUMINATING INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR AND RELAMPED THE AFT SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: DETECTOR — DIRTY (CARGO BAY) · airframe 16,777 hrs · 14,090 cycles
PDX - FLIGHT 2287 - ON FINAL APPROACH, AT 2000 FEET, THE MASTER WARNING/SMOKE ALARM SOUNDED. NO FUMES OR ODORS WERE DETECTED. MAINTENANCE INSPECTED BOTH BAG BAY SMOKE DETECTORS FOR LOOSE CONNECTORS, CHAFED WIRES AND ANY OBVIOUS DEFECTS, NONE WERE NOTED. BOTH DETECTORS WERE CLEANED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BRUSH BLOCK — INOPERATIVE (ZONE 100) · airframe 16,699 hrs · 23,993 cycles
RT TRU CAUTION LIGHT AND R STALL WARNING CAUTION LIGHT CAME ON, RETURNED TO GATE. MAINTENANCE FOUND NR 2 PROP BRUSH BLOCK SHORTED AND FUSE FOR PHASE "B" OF NR 2 AC ELECTRIC SYSTEM BLOWN. REMOVED AND REPLACED NR 2 BRUSH BLOCK AND REPLACED NR 2 PHASE "B" FUSE AC CONTACTOR BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2004
Part: SWITCH — FAILED (RUDDER) · airframe 16,578 hrs · 23,797 cycles
THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDDER PRESS CATUION LIGHT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 1 PRESSURE REGULATOR SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: GCU — INOPERATIVE (ZONE 100) · airframe 16,501 hrs · 23,693 cycles
NR 1 DC CAUTION LIGHT ILLUMINATED, WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC GCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: GENERATOR — INOPERATIVE (ZONE 100) · airframe 16,501 hrs · 23,693 cycles
NR 1 DC GENERATOR FAILED AND WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC STARTER GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,487 hrs · 23,675 cycles
THE TAKEOFF WAS ABORTED WHEN AFTER REACHING 102KTS, THE AIRCRAFT DID NOT ROTATE WHEN THE CONTROL YOKE WAS PULLED BACK. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE BEGAN WORKING ON THE AIRCRAFT TO DETERMINE THE CAUSE. THE AIRCRAFT IS DOWN FOR MAINTENANCE AND THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING FURTHER INFORMATION. CAUSE WAS DETERMINED TO BE AN EXCESSIVE AMOUNT OF TYPE 4 DE-ICE FLUID ON THE FLIGHT CONTROLS.
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 16,445 hrs · 23,606 cycles
THE CREW REPORTED THE SMOKE WARNING LIGHT CAME ON INTERMITTENTLY DURING CLIMB AND STAYED ON FOR APPROXIMATELY 5 MINUTES DURING CRUISE. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETECTORS, AND NOTED NO DEFECTS. THE DETECTORS WERE CLEANED AS A PRECAUTIONARY MEASURE AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CONNECTOR — DISCONNECTED (RUDDER) · airframe 16,238 hrs · 23,289 cycles
PDX - FLIGHT 2201 - FLIGHT RETURNED TO GATE AFTER THE CREW NOTICED NO INDICATION ON THE RUDDER AND AILERON TRIM INDICATORS. MAINTENANCE RECONNECTED THE CANNON PLUG ON THE AILERON AND RUDDER TRIM PANEL. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND THE CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 15,917 hrs · 22,809 cycles
THE CREW OBSERVED AN INTERMITTENT SMOKE WARNING WHILE IN FLIGHT. THE SYSTEM TESTS NORMALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: CONNECTOR — DIRTY (SMOKE DETECTOR) · airframe 15,839 hrs · 22,699 cycles
PDX - FLIGHT 2082 - DURING CRUISE FLIGHT, THE CREW REPORTED AN INTERMITTENT BAGGAGE SMOKE WARNING. NO SMOKE WAS NOTED. MAINTENANCE INSPECTED THE SYSTEM AND AIRCRAFT, THEN CLEANED AND RE-SEATED THE CONNECTORS ON BOTH BAGGAGE BAY SMOKE DETECTORS. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (SMOKE DETECTOR) · airframe 15,802 hrs · 22,644 cycles
THE SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY DURING THE APPROACH AND THEN AGAIN ON FLARE. MAINTENANCE INSPECTED THE AIRCRAFT AND SMOKE DETECTORS AND COULD NOT DUPLICATE THE WRITE-UP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WIRE — EXPOSED (ZONE 100) · airframe 15,581 hrs · 22,295 cycles
PDX - FLIGHT 2151 - EMERGENCY FLOOR LIGHTING AT ROW 1 HAS EXPOSED WIRES. REMOVED AND REPLACED FORWARD SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — BROKEN (ZONE 100) · airframe 15,325 hrs · 21,908 cycles
PDX - EMERGENCY TRACK LIGHTING FORWARD SIX INCH RED SECTION IS BROKEN. REMOVED AND REPLACED EMERGENCY TRACK LIGHTING.
Part: LIGHT — FAILED (CABIN) · airframe 14,902 hrs · 21,262 cycles
PDX - EMERGENCY EXIT FAILS BETA LIGHT TEST. REMOVED AND REPLACED BETA LIGHTS.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 14,734 hrs · 21,023 cycles
PDX - MAINTENANCE FOUND THE ENGINE DISCHARGE BLOW OUT DISK TUBE BRACKET CRACKED AT THE FUSELAGE. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-42-11.
Part: GUIDE — LACK OF LUBE (CABIN DOOR) · airframe 14,607 hrs · 20,835 cycles
SEA - FLIGHT 2062 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBED THE DOOR GUIDES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: HAND RAIL — LACK OF LUBE (MAIN CABIN DOOR) · airframe 14,607 hrs · 20,835 cycles
SEA - FLIGHT 2054 - THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE RESEATED THE AFT HANDRAIL SUPPORT NUT; LUBED ALL MOVING POINTS; PRESSURIZED THE AIRCRAFT TO ENSURE THE DOOR SEAL WAS DEFLATING. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 14,576 hrs · 20,792 cycles
PDX - FLIGHT 2820 - CLIMBING OUT OF 10,00 FT, CABIN PRESS AND MASTER WARNING ILLUMINATED. THE APPROPRIATE CHECKS WERE RUN. MAINTENANCE INSPECTED THE AIRCRAFT AND THE PRESSURE CONTROL SYS. THE SYSTEM OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED.
Part: RIVET — LOOSE (ZONE 200) · airframe 14,574 hrs · 20,790 cycles
PDX - LOOSE RIVET IN RIGHT HAND WING ROOT FAIRING, LOWER EDGE X426 BELOW WING REAR SPAR. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: SKIN — CORRODED (ZONE 100) · airframe 14,574 hrs · 20,790 cycles
PDX - FUSELAGE SKIN AT TCAS ANTENNA MOUNT HAS CORROSION/PITTING AT STATION X501 AND Z35. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,574 hrs · 20,790 cycles
PDX - NR 10 SEAT TRACK HAS CORROSION PITS IN BOTTOM OF CHANNEL, BELOW RIGHT HAND LUG. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 14,574 hrs · 20,790 cycles
PDX - NR 7 SEAT TRACK LEFT HAND FLOOR SUPPORT FLANGE HOLE IS CORRODED, 4 INCHES AFT OF X222. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-30-26.
Part: BRACKET — CRACKED (ZONE 500) · airframe 14,574 hrs · 20,790 cycles
PDX - S-BRACKET CRACKED BOTH FLANGES AT TOP END. LEFT HAND WING FORWARD SPAR AT STATION YW55.0. REPAIRED IAW DHC-8-200 SRM 51-40-11.
Part: BRACKET — CRACKED (ZONE 600) · airframe 14,574 hrs · 20,790 cycles
PDX - FRONT SPAR BLEED AIR ATTACH BRACKET CRACKED AT TOP, 2 RIVETS AT WS YW45.00 RIGHT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-11.
2002
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 11,646 hrs · 16,450 cycles
SEA- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. REMOVED AND REPLACED BOTH TORQUE INDICATORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RELAY — INOPERATIVE (AUTOFEATHER SYS) · airframe 11,288 hrs · 15,924 cycles
PDX- ABORTED TAKEOFF, DURING TAKEOFF ROLL AT 70 KIAS ON TAKEOFF POWER SET, NOTED THAT AUTO-FEATHER ARM LIGHT WAS NOT ON. LIGHT TESTED GOOD. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED 6121-K5 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SWITCH — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 11,280 hrs · 15,914 cycles
LWS- ABORTED TAKEOFF DUE TO NR 1 AUTOFEATHER DOES NOT TEST. REMOVED AND REPLACED ALT FEATHER MICRO SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SWITCH — DIRTY (COCKPIT) · airframe 11,279 hrs · 15,913 cycles
LWS- ABORTED TAKEOFF DUE TO AUTOFEATHER FAILED TO ARM. BULB CHECKED OKAY. CLEANED POWER LEVER SWITCHES. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 10,762 hrs · 15,141 cycles
SEA- SMOKE WARNING, MASTER WARNING LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 SMOKE DETECTOR IN CARGO BAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: TSCU — FAULTY (ENGINE) · airframe 10,543 hrs · 14,807 cycles
SEA - ABORTED TAKEOFF, AUTO FEATHER FAILED TO ARM. REPLACED BOTH ENGINE TSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROLLER — FAULTY (AUTOFEATHER SYS) · airframe 10,539 hrs · 14,801 cycles
PDX - ABORTED TAKEOFF, AUTO FEATHER DID NOT ARM. REPLACED AUTO FEATHER CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — LOOSE (AUTOFEATHER SYS) · airframe 8,355 hrs · 11,713 cycles
PDX - ABORTED TAKEOFF. DURING TAKEOFF ROLL WITH POWER LEVERS SET, NO AUTO FEATHER ARM LIGHT ILLUMINATED. FOUND CONNECTOR AT AUTO FEATHER CONTROLLER LOOSE. REMOVED CONNECTOR AND CHECKED NR 1 AND 2 POWER LEVER A, F POTENTIOMETERS. RIGS CHECKED NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: PRESSURE SWITCH — FAILED · airframe 10,064 hrs · 14,102 cycles
PDX - ROLL SPOILER INBOARD CAUTION LIGHT ILLUMINATED IN FLIGHT. EMERGENCY CHECKLIST WAS COMPLIED WITH. LIGHT REMAINED ILLUMINATED. REPLACED #1 HYDRAULIC ROLL SPOILER PRESSURE SWITCH. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WEB — DAMAGED (NACELLE) · airframe 10,006 hrs · 14,020 cycles
PDX - WEB RIVET HOLES FOR SPR BOX INBOARD BRACKET HOLES ARE ELONGATED. REPAIRED IAW HORIZON AIR EA 4-54-214.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X296 TO X298 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X360 TO X362 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.
Part: STOP FITTING — WORN (EMERGENCY EXIT) · airframe 10,006 hrs · 14,020 cycles
PDX - EMERGENCY DOOR STOPS HAVE APPROXIMATELY .10 WEAR (FRETTING). REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 4 AND SRM 51-20-26, PAGE 7, PARAGRAPH 5A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X403 TO X408 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X390 AND X392 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT SEAT TRACK VENT CRACKED 42 INCHES FROM AFT END. REPAIRED IAW HORIZON AIR EA 2-53-360, DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X309 TO X313 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1352, SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X328 TO X330 HAS CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 651-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X339 TO X344 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1352, SRM 51-40-00 AND SRM 51-40-11.
Part: FRAME — SCRATCHED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - AFT SIDE OF WEB FRAME AT X66 HAS NUMEROUS SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: ANGLE — CRACKED (NACELLE) · airframe 10,006 hrs · 14,020 cycles
PDX - TWO CRACKS NOTED IN VERTICAL ANGLE ADJACENT TO FORWARD SPAR AND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X454 HAS CORROSION ON THE TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X392 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-4473.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT INBOARD SEAT TRACK X437 HAS A CORROSION PIT IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-4473 AND SRM 51-40-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X434 TO X439 HAS CORROSION PITS IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC8 RD 8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X465 TO X470 HAS CORROSION IN THE CHANNEL AND ON TOP FLANGE. REPAIRED IAW RD 8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X451 TO X455 HAS CORROSION PITS IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X482 TO X487 HAS CORROSION IN THE CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1342.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X497 TO 504.5 HAS CORROSION IN CHANNEL AND ON TOP FLANGE. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-40-11 AND SRM 51-40-00.
Part: SKIN PANEL — GOUGED (RT WING) · airframe 10,006 hrs · 14,020 cycles
PDX - GOUGE IN UPPER WING SKIN PANEL ON RT WING AT AFT EDGE OF PANEL AT STATION 155.2. REPAIRED IAW DHC-8 51-20-11, PAGE 7, PARAGRAPH 3E-F (1).
Part: ANGLE — TORN (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT FORWARD OUTBOARD SEAT TRACK MOUNTING ANGLE AT STATION X354.150 TORN. REPAIRED IAW HORIZON AIR EA 2-53-359, DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: FRAME — CRACKED (TAIL CONE) · airframe 10,006 hrs · 14,020 cycles
PDX - REAR TAIL SECTION INTERNAL FRAME 4 STRINGER 4 HAS CRACK NEAR STATION 700.409. REPAIRED IAW DHC-8 RD 8-55-199.
Part: INTERCOSTAL — BOWED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - INTERCOSTAL WEB IS BOWED WHERE IT ATTACHES TO LEFT HAND INBOARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: FRAME — CRACKED (TAIL CONE) · airframe 10,006 hrs · 14,020 cycles
PDX - REAR FUSELAGE TAIL CONE INTERNAL TOP STRUCTURE FRAME FOUR CASTELLATION IS CRACKED AT STRINGER 4R. REPAIRED IAW DHC-8 RD 8-55-199.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT INBOARD SEAT TRACK IS CORRODED BETWEEN FUSELAGE STATIONS X182.0 AND X222.0. REPAIRED IAW DHC-8 RD 8-53-4693, RD 8-53-4473, RD 8-53-2295 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT INBOARD SEAT TRACK HAS CORROSION BETWEEN X504 AND X517. REPAIRED IAW RD 8-53-1102, RD 8-53-4473 AND DHC-8 SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X340 AND X343. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00.
Part: FIREWALL — CRACKED (NACELLE) · airframe 10,006 hrs · 14,020 cycles
PDX - AFT FIRE WALL OUTBOARD SIDE HAS CRACK AT Z100, YN12-0. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X262 AND X270. REPAIRED IAW DHC-8 RD 8-53-1342, SRM 51-40-00 AND SRM 51-40-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X434 AND X438. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-20-26.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X541 THERE IS A GOUGE IN THE CHANNEL. REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X514 AND X523. REPAIRED IAW DHC-8 RD 8-53-3644, PAGE 1-2 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X467 AND X471. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN STATIONS X452 AND X456. REPAIRED IAW RD 8-53-1342 AND DHC-8 SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X483 AND X505. REPAIRED IAW DHC-8 RD 8-53-1342 AND SRM 51-20-16.
Part: SKIN — CHAFED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - THERE IS CHAFE DAMAGE AT TWO LOCATIONS ON UPPER CARGO DOOR APERTURE. REPAIRED IAW RD 8-53-5461.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X530 AND X532. REPAIRED IAW DHC-8 SRM 8-53-3644, PAGE 1-3 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - RT OUTBOARD SEAT TRACK X514 TO 517 HAS PITTING CORROSION ON TOP FLANGE AND IN CHANNEL. REPAIRED IAW DHC-8 RD 8-53-3644 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT OUTBOARD CABIN SEAT TRACK HAS CORROSION BETWEEN STATIONS X541 AND X544. REPAIRED IAW DHC-8 RD 8-53-3644, PAGES 1-2, STEPS 1-2 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT INBOARD SEAT TRACK HAS CORROSION AT X540 TO X544. REPAIRED IAW RD 8-53-4963 AND DHC-8 SRM 51-20-16.
Part: SKIN — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - X600, Y21L, Z100 UNDERSIDE SKIN AT NUT PLATE HAS CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, PAGE 3, TABLE 1.
Part: STOP FITTING — CHAFED (EMERGENCY EXIT) · airframe 10,006 hrs · 14,020 cycles
PDX - RT FORWARD EMERGENCY EXIT ALL EIGHT DOOR STOPS CHAFED ON BEARING SURFACES. REPAIRED IAW RD 8-52-349.
Part: FITTING — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - X594, Y30L, Z100 WEB TIE SKIN UNDER NUT PLATE HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11.
Part: ARM — GOUGED (NLG) · airframe 10,006 hrs · 14,020 cycles
PDX - NOSE LANDING GEAR LOWER TRAILING ARM IS GOUGED. REPAIRED IAW RD 8-32-289.
Part: SKIN — CHAFED (CARGO DOOR) · airframe 10,006 hrs · 14,020 cycles
PDX - CARGO DOOR SKIN CHAFED 3 INCHES FROM BOTTOM. REPAIRED IAW RD 8-52-230, RD 8-52-230, DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: FIREWALL — CRACKED (NR 1 NACELLE) · airframe 10,006 hrs · 14,020 cycles
PDX - NR 1 ENGINE FIREWALL CRACKED .25 INCH ABOVE FIRE LOOP SUPPORT BRACKET. REPAIRED IAW DHC-8 RD 8-54-611.
Part: DOUBLER — CHAFED (CARGO DOOR) · airframe 10,006 hrs · 14,020 cycles
PDX - CARGO DOOR SKIN UPPER REPAIR DOUBLER CHAFED. REPAIRED IAW DHC-8 SRM 52-00-16, PAGE 2.
Part: BRACKET — CRACKED (WING) · airframe 10,006 hrs · 14,020 cycles
PDX - OUTBOARD BRACKET FOR LEADING EDGE 611AR AT NACELLE END, LOWER SIDE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: ANGLE — CHAFED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - X220 TO X240, BL45R, Z103 LAV HAS CHAFED SPOTS ON WEB ANGLE. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 7, STEP 3 (1).
Part: STRUT — CHAFED (ENGINE MOUNT) · airframe 10,006 hrs · 14,020 cycles
PDX - NR 2 ENGINE MOUNT LOWER OUTBOARD STRUT HAS TWO CHAFED SPOTS ON INBOARD SIDE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
2001
Part: SKIN — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LOWER FORWARD ATC ANTENNA AIRCRAFT SURFACE IS CORRODED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3 AND SRM 51-20-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LT INBOARD SEAT TRACK X593 THERE IS CORROSION UNDER A NUT PLATE. REPAIRED IAW DHC-8 SRM 51-20-36 AND SRM 51-40-11.
Part: SKIN — CORRODED (FUSELAGE) · airframe 10,006 hrs · 14,020 cycles
PDX - LOWER TCAS ANTENNA HAS CORROSION AT MOUNT HOLES. REPAIRED IAW DHC-8 SRM 51-20-11, SRM 53-00-16 AND SRM 51-20-16.
Part: SEAT — BROKEN · airframe 9,982 hrs · 13,984 cycles
PDX - FIRST OFFICERS SEAT BACK BROKE. AIRCRAFT RETURNED TO FIELD. REPLACED FIRST OFFICERS SEAT. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 9,704 hrs · 13,616 cycles
PDX- GOUGE ON UPPER AFT CARGO DOOR. REPAIRED IAW DHC-8 RD 8-52-029 AND SRM 52-00-16.
Part: SKIN — CHAFED (CARGO DOOR) · airframe 9,704 hrs · 13,616 cycles
PDX- CHAFE ON CARGO DOOR SKIN AT FORWARD LOWER CORNER. REPAIRED IAW DHC-8 RD 8-52-230 AND SRM 51-40-11 AND 51-40-00.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 9,236 hrs · 12,948 cycles
PDX-TWO INCH DENT AT STATION 700.409 LEFT HAND SIDE, TAIL. FABRICATED AND INSTALLED DOUBLER REPAIR IAW THE DASH 8 STRUCTURAL REPAIR MANUAL 53-30-24, FIGURE 1, SHEET 2.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 8,186 hrs · 11,485 cycles
SEA - A PORTION OF THE FLOOR ESCAPE PATH LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: ELEMENT — CONTAMINATED (STATIC SYS) · airframe 8,186 hrs · 11,466 cycles
SEA - FLIGHT CREW REPORTED AN UNIDENTIFIED FUME (SMELL) IN THE FLIGHT COMPARTMENT. MAINTENANCE FOUND SEALANT ON STATIC HEATER ELEMENT. REMOVED AND REPLACED STATIC PORT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 7,919 hrs · 11,108 cycles
SEA- EMERGENCY FLOOR PATH LIGHTS, FORWARD RED SECTION INOPERATIVE. REPLACED FORWARD RED SECTION OF FLOOR PATH LIGHTS (82520999-001), POWER SUPPLY (60-3844-1) AND BATTERY PACK. EMERGENCY LIGHTS TEST NORMAL. AIRCRAFT RETURNED TO SERVICE.
2000
Part: INVERTER — MALFUNCTIONED (COCKPIT) · airframe 7,368 hrs · 10,327 cycles
PDX- STRONG SMELL IN COCKPIT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — MALFUNCTIONED (COCKPIT) · airframe 7,214 hrs · 10,117 cycles
SEA- FLIGHT COMPARTMENT EMERGENCY LIGHT NOT CHARGING. REPLACED EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 6,855 hrs · 9,628 cycles
SEA- FLIGHT ATTENDANT REPORTS DIFFICULTY OPENING MAIN CABIN DOOR. MECHANISM CATCHES. REPLACED FORWARD MAIN CABIN DOOR HAND RAIL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INTERMITTENT (COCKPIT) · airframe 5,871 hrs · 8,281 cycles
PDX- COCKPIT EMERGENCY LIGHT ILLUMINATES INTERMITTANTLY. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPERATIONAL CHECKS OK. AIRCRAFT RETURNED TO SERVICE.
Part: FIRE DETECTOR — MALFUNCTIONED (NR 1 ENGINE)
BOI- FIRE DETECTION LOOP B FAULT LIGHT ILLUMINATED ON NUMBER 1 ENGINE IN FLIGHT. REMOVED AND REPLACED B LOOP AND FIRE PROTECTION PANEL. OPERATIONAL CHECKS GOOD.
1999
Part: SKIN — DAMAGED (LT NACELLE)
YXX - LEFT FORWARD LOWER NACELLE STRUCTURE ADJACENT TO LOWER COWL HINGE POINTS DAMAGED. REPAIRED IAW RD8-54-063.
Part: SEAT TRACK — CORRODED (BS 598)
YXX - CORROSION FOUND ON LEFT INBOARD SEAT TRACK AT X598.0 AT TIE DOWN IN BAGGAGE AREA. REPAIRED IAW RD8-53-4697 AND HORIZON AIR EA 2-53-122.
Part: SEAT TRACK — CORRODED (BS 598)
YXX - CORROSION FOUND ON RIGHT INBOARD SEAT TRACK AT X598.0 AT TIE DOWN IN BAGGAGE AREA. REPAIRED IAW RD8-53-4697.
Part: STOP — DAMAGED (CARGO DOOR)
YXX - DRESS OUT CONTACT AREA OF UPPER AND LOWER BAGGAGE DOOR STOPS AT LOCATIONS 7, 8, 9 AND 10. REPAIRED IAW RD8-53-104, MM PSM 1-8-2, CHAPTER 52-30-00, PAGE 210.
Part: STRAP — DAMAGED (CARGO DOOR)
YXX - BAGGAGE DOOR UPPER SILL STRAPS AND FORWARD PRESSURIZATION STOP DAMAGED BY CONTACT WITH DOOR FITTINGS DURING CLOSING. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SKIN — CHAFED (TE FLAP)
YXX - RIGHT OUTBOARD FLAP TOP SURFACE AT YW232-242 AND 20 FORWARD OF TRAILING EDGE IS CHAFFED FROM SHROUD. REPAIRED IAW RD8-57-1022 AND RD8-57-1241.
Part: HEAT SHIELD — CHAFED (LT NACELLE)
YXX - LEFT NACELLE DISHED HEAT SHIELDS HAVE CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND RD8-54-1442.
Part: LINE — CRACKED (BLEED AIR)
YXX - LEFT CENTER WING BLEED PIPE MOUNT FLANGE CRACKED. REPAIRED IAW DHC-8 RD8-21-028.
Part: SKIN — CHAFED (TE FLAP)
YXX - RIGHT OUTBOARD FLAP TOP SURFACE AT YW176 AND 18 FORWARD OF THE TRAILING EDGE IS CHAFFED. REPAIRED IAW DHC-8 SRM 57-50-16, TABLE 1 AND SRM 51-20-36.
Part: HEAT SHEILD — CRACKED (LT NACELLE)
YXX - LEFT HEATSHIELD TO FINGERNAIL ATTACH TABS AT XN280 IS CRACKED ON OUTBOARD TAB. REPAIRED IAW RD8-54-163 AND DHC-8 SRM 51-40-11.
Part: SCREW — STRIPPED (WING PANEL)
YXX - STRESS PANEL 622AT, UPON REMOVAL OF PANEL ONE SCREW WAS FOUND STRIPPED HEAD AND SEIZED. REPAIRED IAW RD8-57-1420.
Part: HEAT SHIELD — CHAFED (RT NACELLE)
YXX - RIGHTHEATSHIELD HAS CHAFE DAMAGE AT XN245.0. REPAIRED IAW DHC-8 RD8-54-866.
Part: HEAT SHILED — CHAFED (RT NACELLE)
YXX - RIGHT OUTBOARD DISHED HEAT PANEL HAS CHAFE DAMAGE ON INBOARD SIDE AT XN223. REPAIRED IAW RD8-54-194.
Part: SKIN — CRACKED (TAIL CONE)
YXX - COMPOSITE TAIL CONE LOWER SKIN CRACKED JUST AFT OF INSPECTION PANEL OPENING, RIGHT OF CENTER. REPAIRED IAW DHC-8 SRM 51-70-00, PAGES 11-19 AND 601.
1998
Part: VALVE — MALFUNCTION (ENG P2.5/P3)
PDX - STRONG ACRID SMELL NOTICED FROM THE VENTILATION SYSTEM. REPLACED THE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — MISSING (CABIN)
EXIT SIGN AT THE LEFT UNDERWING EXIT MISSING. REPLACED SIGN, OPERATIONAL CHECKS GOOD.
Part: SWITCH — FAILED (POWER LEVER)
PDX - AUTOFEATHER SYSTEM WILL NOT TEST. MAINTENANCE REPLACED POWER LEVER SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: AUTOFEATHER — MALFUNCTIONED (PROP SYST)
PUW - AUTOFEATHER WOULD NOT TEST. MAINTENANCE CONTROL HAD CREW CYCLE ECU'S, POWER LEVERS AND CONDITION LEVERS STATICALLY, THEN STARTED ENGINES AND TESTED SYSTEM. OPERATIONAL CHECK GOOD, NO PARTS REPLACED.
Part: AUTOFEATHER — FAILED TEST (PROP SYST)
MFR - AIRCRAFT AUTO FEATHER TEST INOP. MAINTENANCE CYCLED POWER LEVERS SEVERAL TIMES, OPERATIONAL CHECK GOOD.
1997
Part: RELAY — MALFUNCTION (E/E COMPT)
PDX- AUTO FEATHER TEST INOP. AUTO FEATHER ARMS NORMALLY. REPLACED RELAYS 6121-K3 AND 6121-K4. ACCOMPLISHED AUTO FEATHER SYSTEM AND POWER UPTRIM TEST, SYSTEM TESTS GOOD.