N816PH
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.
80 reports on file, 1995-10-27 – 2001-12-20.
Part: FIREWALL — CRACKED (NR 2 NACELLE) · airframe 37,817 hrs · 52,221 cycles
PDX - NR 2 ENGINE AFT FIREWALL IS CRACKED AT ABOUT 10:00 AT Z-BRACKET. REPAIRED IAW RD 8-54-611.
Part: STRUT — GOUGED (NR 2 NACELLE) · airframe 37,817 hrs · 52,221 cycles
PDX - TWO GOUGES ON NR 2 ENGINE OUTBOARD LOWER TORQUE STRUT AT BOTTOM END. REPAIRED IAW RD 8-54-036.
Part: DOOR — OUT OF TOLERANCE (CARGO BAY) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGGED MCD, DOOR IS NOT WITHIN CLEARANCE LIMITS OF STOP 4. REPAIRED IAW HORIZON AIR EA 9-52-116.
Part: DOOR — OUT OF TOLERANCE (CARGO BAY) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGGED MCD, DOOR IS NOT WITHIN CLEARANCE LIMITS OF STOP 2. REPAIRED IAW HORIZON AIR EA 9-52-116.
Part: RIVET — LOOSE (RT NACELLE) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT NACELLE HAS FOUR LOOSE RIVETS BOTTOM OUTBOARD OF OIL COOLER. REPAIRED IAW HORIZON AIR EA 9-54-290A AND DHC-8 RD-8-54-057.
Part: STOP — WORN (EMERGENCY EXIT) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT HAND FORWARD EMERGENCY EXIT DOOR STOPS HAVE STEP WEAR. REPAIRED IAW DHC-8 RD-8-52-349.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,265 hrs · 50,105 cycles
PDX-CORROSION ON SUPPORT STRUCURE FOR FLOOR PANEL 131C8 ON THE MOST OUTBOARD SECTION OF SUPPORT STRUCTURE, AROUND THE NUT PLATE HOLE. REPAIRED IAW DHC-8 RD8-53-832 AND HORIZON AIR EA 9-53-613.
Part: SKIN — TORN (NACELLE) · airframe 36,265 hrs · 50,105 cycles
PDX-LEFT HAND NACELLE OUTBOARD LOWER CORNER S/M TORN WHERE MAIN LANDING GEAR FORWARD HINGE ATTACH POINT. REPAIRED IAW DHC-8 RD-8-54-729.
Part: VORTEX GEN — UNAPPROVED PART (HORIZ STAB) · airframe 36,265 hrs · 50,105 cycles
PDX-INBOARD VORTEX GENERATOR ON RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN IS NOT APPROVED PART FOR THIS AIRCRAFT. REPAIRED IAW HORIZON AIR EA 9-55-144.
Part: FRAME — CHAFED (CARGO DOOR) · airframe 36,265 hrs · 50,105 cycles
PDX-CHAFE DAMAGE TO FRAME FOR SEAL RETAINER ON BAGGAGE DOOR AT X597.0 AFT SIDE OF DOOR. REPAIRED IAW DHC-8 SRM 51-20-31 AND HORIZON AIR EA 9-52-115.
Part: RIB — CHAFED (RT NACELLE) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED AT XN137.35 AND ZN17.0. REPAIRED IAW HORIZON AIR EA 9-54-288 AND DHC-8 SRM 51-20-11.
Part: SKIN — DENTED (SERVICE DOOR) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT HAND FORWARD SERVICE EMERGENCY DOOR DENTED AT STATION Z143.00 AND X262.00, AFT OF DOOR WINDOW. REPAIRED IAW HORIZON AIR EA 9-52-114.
Part: RIB — CHAFED (RT NACELLE) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED IN TWO AREAS XN141.95 AND ZN18.0. REPAIRED IAW HORIZON AIR EA 9-54-287 AND DHC-8 SRM 53-00-16, PAGE 4.
Part: DOOR — DELAMINATED (NLG) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT HAND FORWARD NOSE LANDING GEAR DOOR COMPOSITE IS DELAMINATED ON FORWARD EDGE OF DOOR. REPAIRED IAW DHC-8 SRM 32-20-21, PAGE 211 AND SRM 32-30-00, PAGE 204.
Part: SPACER — MISSING (NLG) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT HAND FORWARD NOSE LANDING GEAR DOOR SPRING HAS SPACERS MISSING AT DOOR BRACKET ATTACH POINT. REPAIRED IAW DHC-8 SRM 32-20-21, PAGE 205 AND SRM 32-30-00, PAGE 204.
Part: SEAT TRACK — DAMAGED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-NR 7 SEAT TRACK RIGHT HAND INBOARD STATION 182-424 REQUIRES REMOVAL DUE TO MULTIPLE WRITE-UPS. REPAIRED IAW HORIZON AIR EA 9-53-612 AND DHC-8 SRM 51-40-00.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,265 hrs · 50,105 cycles
PDX-CORROSION ON ANGLE AT STATION 600, WL 100. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: WINDOW FRAME — CHAFED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-CHAFING AT LOWER APERTURE OF LEFT HAND MAIN CABIN WINDOW AT STATION 501. REPAIRED IAW DHC-8 RD-8-53-655 AND SRM 51-20-11, PAGE 3.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-SEAT TRACK REQUIRES REPLACEMENT DUE TO CORROSION BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-00 AND RD-8-53-3403.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-RIGHT OUTBOARD FORWARD SEAT TRACK REQUIRES REPLACEMENT DUE TO CORROSION REMOVAL BLENDING BEYOND LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD-8-53-1102.
Part: SKIN — CORRODED (FLOORBOARD) · airframe 36,265 hrs · 50,105 cycles
PDX-CORROSION ON TOP AND BOTTOM OF FLOORBOARD SKIN AT 2 NUT PLATES, STATION 599, WL100. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-00.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-CORROSION .024 INCH REMOVED FROM BOTTOM OF SEAT TRACK AFT OF STATION 467. RIGHT HAND OUTBOARD SEAT TRACK CORROSION OUT OF LIMITS. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD-8-53-1102.
Part: SEAT TRACK — DAMAGED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-DUE TO THE MULTIPLE WRITE-UPS ON SEAT TRACK NR 4 REQUIRES REPLACEMENT. REPAIRED IAW DHC-8 SRM 51-40-00, SRM 51-40-11, AND RD-8-53-3403.
Part: CONTROL CABLE — BROKEN (NR 1 ENGINE) · airframe 36,265 hrs · 50,105 cycles
PDX- NR 1 ENGINE POWER CONTROL CABLE HAS A BROKEN STRAND JUST FORWARD OF PULLEY. REPAIRED IAW DHC-8 SRM 76-10-14, PAGE 211.
Part: BRACKET — CHAFED (RT MLG) · airframe 36,265 hrs · 50,105 cycles
PDX-NACELLE WHEEL WELL RIGHT HAND AT STATION 240.76 AFT DOOR ACTUATOR BRACKET IS CHAFED AND HAS RTV HANGING OFF. REPAIRED IAW HORIZON AIR EA 9-54-283.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-PITTING CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 370. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD-8-53-1102.
Part: ACTUATOR — CORRODED (LT MLG) · airframe 36,265 hrs · 50,105 cycles
PDX-LEFT HAND LANDING GEAR RETRACTION ACTUATOR FRETTING MOUNTING PADS HAVE PITTING. REPAIRED IAW HORIZON AIR EA 9-54-279, SRM 32-30-11, PAGE 202 AND SRM 51-20-16, PAGE 4.
Part: SKIN — DENTED (FUSELAGE) · airframe 36,265 hrs · 50,105 cycles
PDX-DENT PROTRUDING IN LOWER EMPENNAGE SKIN LEFT OF TAIL SKID BUMPER, 12 INCHES FORWARD OF COMPOSITE TAIL CONE. REPAIRED IAW DHC-8 SRM 53-30-24, PAGE 1.
Part: SEAT TRACK — GROOVED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-12 INCH GROOVE ON RIGHT HAND INBOARD SEAT TRACK STATION 510. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339.
Part: SEAT TRACK — GROOVED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-12 INCH GROOVE WORN ON RIGHT HAND INBOARD SEAT TRACK STATION 450. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339.
Part: SEAT TRACK — GROOVED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-15 INCH GROOVE ON RIGHT HAND INBOARD SEAT TRACK BETWEEN STATION 467 - 488. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1339.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-FRETTING CORROSION ON LEFT HAND INBOARD SEAT TRACK STATION 545. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-3644.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-CORROSION ON OUTBOARD FLANGE OF RIGHT HAND INBOARD SEAT TRACK, STATION 580-600 (CARGO PIT). REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36, AND RD-8-53-784.
Part: RIVET — MISSING (STRINGER) · airframe 36,265 hrs · 50,105 cycles
PDX-2 RIVETS MISSING AT RIGHT HAND STRINGER 32 AND FRAME CLIP STATION 426. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 501. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-LIGHT CORROSION ON LEFT HAND SEAT TRACK STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 465. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342.
Part: SEAT TRACK — GROOVED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-LIGHT CORROSION ON LEFT HAND OUTBOARD SEAT TRACK STATION 436. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,265 hrs · 50,105 cycles
PDX-LIGHT CORROSION ON RIGHT HAND OUTBOARD SEAT TRACK STATION 440. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36, AND RD-8-53-1242.
Part: LANDING GEAR — GOUGED (NLG) · airframe 36,265 hrs · 50,105 cycles
PDX-NOSE LANDING GEAR LOWER MEMBER FORWARD FACE IS GOUGED AT Z70.00. REPAIRED IAW DHC-8 RD8-32-289.
Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 36,081 hrs · 49,849 cycles
SEA- COCKPIT EMERGENCY LIGHT INOPERATIVE WHEN CONTROL SWITCH IS ON POSITION. INTERMITTENTLY ILLUMINATED ON WHEN SWITCH IN ARM OR OFF POSITION. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 1995–2000 · 39 reports
2000
Part: HAND RAIL — LOOSE (PAX DOOR) · airframe 35,323 hrs · 48,819 cycles
PDX- UNABLE TO OPEN THE MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. REPLACED LOOSE HARDWARE ON MAIN CABIN DOOR HANDRAIL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: HANDLE — OUT OF ADJ (PAX DOOR) · airframe 35,228 hrs · 48,683 cycles
YVR- UNABLE TO OPEN MAIN CABIN DOOR, OPENING LATCHES STUCK. ADJUSTED EXTERNAL HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: INVERTER — MALFUNCTIONED (COCKPIT) · airframe 34,949 hrs · 48,294 cycles
ALW- DETECTED ELECTRICAL SCENT IN COCKPIT. DETERMINED TO BE BAD SECONDARY INVERTER. REPLACED INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LENS — BROKEN (CABIN) · airframe 34,380 hrs · 47,492 cycles
PDX- EXIT LIGHT LENS AT MAIN CABIN DOOR LOWER ENTRANCE IS BROKEN. REPLACED EXIT LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 2,295 hrs · 3,209 cycles
SEA- FORWARD TWO LIGHTS INOPERATIVE ON FLOOR PROXIMITY LIGHTS. REMOVED AND REPLACED BATTERY AND POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 34,125 hrs · 47,122 cycles
PSC- PORTABLE EMERGENCY LIGHT ABOVE OBSERVERS SEAT INOPERATIVE DURING TEST OF EMERGENCY LIGHT SYSTEM. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: GAS STRUT — INOPERATIVE (PAX DOOR)
SEA- REPORTED BY FLIGHT ATTENDANT, MAIN CABIN DOOR IS GETTING PROGRESSIVELY HARDER TO OPEN. REPLACED DOOR LIFT SPRING STRUT, OPERATIONAL CHECKS GOOD.
1999
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
SEA - MAIN CABIN DOOR EXCEEDINGLY HARD TO OPEN. INSPECTED DOOR AND FOUND NO DISCREPANCIES. LUBED STOPS. CYCLED DOOR SEVERAL TIMES. OPERATIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE REPLACED.
Part: MECHANISM — DIRTY (PAX DOOR)
SEA- MAIN CABIN DOOR HARD TO OPEN FROM INSIDE. CLEANED MAIN CABIN DOOR SEAL AND DOOR LOCKING/UNLOCKING LEVERS. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: MECHANISM — LACK OF LUBE (PASSENGER DOOR)
GEG - THE MAIN CABIN DOOR OPERATION HANDLE IS HARD TO MOVE, HANGS UP DURING OPERATION. MAINTENANCE CLEANED AND LUBRICATED THE DOOR STOPS AND PIVOT POINTS. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.
Part: SKIN — DAMAGED (NR 2 NACELLE)
YXX - NR 2 NACELLE HAS RIVETS PULLED THROUGH SKIN AT NACELLE STATION 134.68 AT LOWER LONGERON OUTBOARD SIDE. REPAIRED IAW SRM 51-20-16.
Part: SKIN — CHAFED (LT TE FLAP)
YXX - CHAFE MARK ON UPPER SKIN OF LEFT-HAND INBOARD FLAP STATION YW 74.35, 1 AFT OF FLAP FRONT SPAR. REPAIRED IAW DASH 8 RD 8-57-1361.
Part: COWL — CRACKED (NR 2 ENGINE)
YXX - NR 2 ENGINE PANEL 432AL CRACKING AROUND RIVET ON GUSSET AND CHANNEL AT COOLING DUCT ATTACH FLANGE. REPAIRED IAW CONAIR EO 2251 AND HORIZON AIR EA 9-71-105.
Part: HOUSING — CHAFED (NR 1 NACELLE)
YXX - NR 1 HORSE COLLAR INBOARD FORWARD LATCH HOUSING CHAFED BADLY AND CRACKED. REPAIRED IAW DASH 8 RD 8-71-154, CONAIR EA 2240 AND HORIZON AIR EA 9-71-103.
Part: FIREWALL — CRACKED (NR 1 NACELLE)
YXX - CRACK IN NR 1 FIREWALL, INBOARD SIDE JUST ABOVE CUT OUT FOR ATTACHMENT HARDWARE OF MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING. REPAIRED IAW DASH 8 RD 8-54-10147, CONAIR EO 2254 AND HORIZON AIR EA 9-54-193.
Part: SHROUD — DENTED (VERT STAB)
YXX - VERTICAL STABILIZER RIGHT-HAND TRAILING EDGE SHROUD BETWEEN RIB 8 AND RIB 9 DENTED. REPAIRED IAW DASH 8 RD 8-555-718.
Part: SKIN — DENTED (BS 148)
YXX - FORWARD LEFT-HAND SIDE AT STATION X148.000 DENT FOUND OUT OF SRM LIMITS, CHAPTER 53-00-16, PAGE 4. REPAIRED IAW DASH 8 RD 8-53-4107.
Part: SKIN — DENTED (WS 279)
YXX - LEFT-HAND WING HAS DENT ON LOWER SKIN SURFACE STATION YW 279.00. REPAIRED IAW DASH 8 RD 8-57-1359.
Part: PLATE — CORRODED (WS 171.2-261)
YXX - LEFT-HAND WING LADDER PLATE HAS CORROSION ON UPPER SURFACE LADDER PLATE STATION YW 171.2 TO YW 261.0. REPAIRED IAW DASH-8 RD 51-20-16.
Part: STRAP — CHAFED (CABIN)
YXX - CHAFE FOUND ON LEFT-HAND MID CABIN EXIT CAP STRAP AT FORWARD UPPER CORNER. REPAIRED IAW HORIZON AIR EA 9-53-77C.
Part: STRUT — MALFUNCTION (CABIN DOOR)
YVR- MAIN CABIN DOOR WILL NOT OPEN. MAINTENANCE FERRIED FROM YVR TO PDX FOR REPAIRS. IN PDX, REPLACED FORWARD HANDRAIL STRUT. OPERATIONAL CHECKS GOOD.
1998
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
SEA - PASSENGER DOOR DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE THRESHOLD STRIP ON THE BOTTOM OF THE DOOR AND LUBRICATED THE DOOR PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: AIR DIST — ODOR (CABIN)
SMELL OF JET FUEL IN THE CABIN AND COCKPIT AFTER TURNING ON NR 2 BLEED. TURNING OFF NR 2 BLEED GETS RID OF THE SMELL. MAINTENANCE PERFORMED AN INSPECTION OF THE BLEED AIR SYSTEM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: SCREW — LOOSE (PAX DOOR)
SEA- MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM THE INSIDE. IT TAKES A LARGE AMOUNT OF FORCE TO MOVE THE INTERIOR HANDLE INTO THE UP POSITION. INSPECTED THE MAIN CABIN DOOR AND FOUND A SCREW BACKING OUT OF THE AFT DOOR SUPPORT ROD. TIGHTENED LOOSE SCREW.
Part: BULB — FAILED (CABIN)
PDX - EMERGENCY FLOOR PROXIMITY LIGHTING RED BULB INOP (4TH BULB FROM FORWARD). RELAMPED PROXIMITY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (COCKPIT)
PDX - OVERHEAD EMERGENCY LIGHT IN COCKPIT ABOVE OBSERVER SEAT WILL NOT HOLD A CHARGE. REPLACED LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
PSC- EMERGENCY OVERHEAD LIGHT AT ROW NR 6 HAS A LIGHT BULB THAT IS INOP. REPLACED LAMP, OPERATIONAL CHECKS GOOD.
Part: SCREW — LOOSE (PAX DOOR)
MAIN CABIN DOOR IS DIFFICULT TO OPEN. INSPECTED AND FOUND A LOOSE SCREW AT THE FORWARD HANDRAIL WHICH WAS BLOCKING THE DOOR FROM EXTENDING FULLY. TIGHTENED SCREW, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.
Part: HANDRAIL — MALFUNCTION (PAX DOOR)
PDX- MAIN CABIN IS DIFFICULT TO OPEN. REPLACED BOTH THE FORWARD AND AFT MAIN CABIN DOOR HANDRAILS, OPERATIONAL CHECKS GOOD.
1997
Part: CABLE — INOPERATIVE (PAX DOOR)
PDX- MAIN CABIN DOOR WON'T OPEN. REPLACED CABLE AND ASSIST STRUTS, OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN)
SEA - AFT CEILING EMERGENCY LIGHT AND AFT LEFT HAND EXTERIOR LIGHT INOP. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - LEFT AFT EMERGENCY LIGHT INOP. REPLACED LAMP, MATRIX BLOCK AND BATTERY PACK. OPERATIONAL CHECK GOOD.
Part: OIL COOLER — MALFUNCTION (NR 2 ENGINE)
AFTER TAKEOFF, NR 2 ENGINE OIL TEMPERATURE STARTED UP INTO THE YELLOW AND NR 2 FUEL FLOW WAS IN THE YELLOW. PULLED TO FLIGHT IDLE AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. REPLACED NR 2 OIL TEMPERATURE INDICATOR, OIL TMPERATURE BULB, OIL COOLER AND VERNATHERM. GROUND RAN/FLIGHT TESTED GOOD.
Part: HMU — MALFUNCTION (NR 1 ENGINE)
AT LEVEL OFF AT FLIGHT LEVEL 19,000, NOTICED A GRADUAL POWER LOSS ON NR 1 ENGINE (19 PERCENT IN 2 MINUTES). RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. REPLACED NR 1 HYDROMECHANICAL UNIT, OPERATIONAL CHECKS GOOD.
1996
Part: UPLOCK ACTUATOR — INOPERATIVE (LT MLG)
ALTERNATE GEAR EXTENSION PERFORMED BECAUSE LEFT MAIN GEAR REMAINED IN THE WHEEL WELL DURING NORMAL GEAR EXTENSION. LEFT MAIN GEAR EXTENDED USING ALTERNATE METHOD. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEMS. LEFT HAND UPLOCK ACTUATOR REPLACED IAW MAINTENANCE MANUAL, UPLOCK ROLLER LUBED AND GEAR OPS CHECKED GOOD ON GEAR SWING.
Part: O-RING — SPLIT (SPOILER ACT FTG)
NUMBER 2 HYDRAULIC SYSTEM CAUTION LIGHT ILLUMINATED, LOST ALL HYD FLUID IN THE NUMBER 2 SYSTEM. ALTERNATE GEAR EXTENSION PERFORMED FOR LANDING AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. REPLACED SPLIT O-RING AT GROUND SPOILER FITTING, RETURN FITTING. SERVICED NUMBER 2 HYDRAULIC SYSTEM AND SYSTEM OPS CHECKED GOOD.
Part: BULB — FAILED (CABIN)
SEA - AFT OVERHEAD AISLE EMERGENCY LIGHT IS INOPERATIVE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN)
FORWARD EMERGENCY FLASHLIGHT BATTERY PACK IS WEAK. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD.
1995
Part: BULB — FAILED (CABIN)
SEA - OVERHEAD EMERGENCY LIGHT INOP. BULB REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.