N825PH
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.
93 reports on file, 1995-08-15 – 2006-04-03.
Part: WARNING HORN — INTERMITTENT (TE FLAPS)
ABORTED TAKEOFF, DURING TAKEOFF ROLL, TAKEOFF CONFIGURATION HORN CAME ON. FLAP CYCLED. SYSTEM FUNCTIONED SATISFACTORY, HORN NO LONGER EVIDENT ON TAKEOFF REF MM. (K)
Earlier reports · 1995–2001 · 92 reports
2001
Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 28,593 hrs · 39,842 cycles
PDX - BAGGAGE DOOR INNER STRUCTURE DENTED WITH CRACK ON VERTICAL MEMBER ABOVE FORWARD COUNTERBALANCE ASSEMBLY. REPAIRED DAMAGE IAW E.A. 9-52-123.
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 28,593 hrs · 39,842 cycles
PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING.REPAIRED IAW HORIZON AIR EA 9-52-122.
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 28,593 hrs · 39,842 cycles
PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING. REPAIRED IAW HORIZON AIR EA 9-52-122.
Part: INVERTER — DEFECTIVE · airframe 28,578 hrs · 39,817 cycles
GEG-ELECTRICAL SMELL NOTICED IN FLIGHT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROLLER — WILL NOT TEST (AUTOFEATHER SYS) · airframe 27,251 hrs · 38,010 cycles
LWS - AUTOFEATHER WILL NOT TEST. CYCLED POWER LEVERS AND CONDITION LEVERS FULL TRAVEL NUMEROUS TIMES. TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,188 hrs · 37,927 cycles
PDX - FOUND LEFT HAND SIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
2000
Part: ACM — MALFUNCTIONED (ACM BAY) · airframe 26,479 hrs · 36,987 cycles
SEA- FLIGHT ATTENDANT REPORTED SMELL OF SMOKE ON SHORT AND FINAL APPROACH JUST AFTER BLEED AIR TURNED OFF FOR LANDING. REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — MALFUNCTIONED (CABIN) · airframe 25,674 hrs · 35,856 cycles
PDX- FORWARD ENTRY DOOR LOWER EMERGENCY EGRESS EXIT SIGN BROKEN. REPLACED ENTRY DOOR LOWER EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: INVERTER — MALFUNCTIONED (COCKPIT) · airframe 25,346 hrs · 35,402 cycles
SEA- DURING FLIGHT AIRCRAFT COCKPIT/CABIN BEGAN TO SMELL OF SMOKE. AUXILIARY INVERTER MASTER CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
1999
Part: SKIN — DENTED (BS 507)
PDX - 4 DENT ON OUTER SKIN AT STATION 507, WL100, BL40RH. REPAIRED IAW HORIZON AIR EA 9-53-531.
Part: WEB — CORRODED (RT NACELLE)
PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN286.0. REPAIRED IAW DHC-8 SRM 51-40-4.
Part: WEB — CORRODED (RT NACELLE)
PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN280.00. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.
Part: SKIN — CRACKED (RT NACELLE)
PDX - RIGHT NACELLE EXTERIOR OUTBOARD SKIN HAS .250 CRACK FROM RIVET HOLE TO SKIN PANEL EDGE AT STATION XN122.00 AND YW171.200, ALSO HAS LOOSE WORKING RIVET IN SAME AREA JUST AFT OF PANEL 426AR. REPAIRED IAW HORIZON AIR EA 9-54-239.
Part: STRINGER — GOUGED (BS 550)
PDX - SMALL GOUGE IN LEFT-HAND STRINGER 31 AT APPROXIMATELY STATION 550. REPAIRED IAW HORIZON AIR EA 9-53-532.
Part: GUARD — WORN (NACELLE)
PDX - INBOARD MIDDLE GRAVEL GUARD ATTACH POINT WORN EXCESSIVELY THIN. REPAIRED IAW RD8-54-41.
Part: SKIN — CHAFED (BS 242.20)
PDX - CHAFE DAMAGE AT STATION 242.20 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT. IT IS APPROXIMATELY .035 DEEP. REPAIRED IAW HORIZON AIR EA 9-53-535.
Part: FRAME — CORRODED (FUSELAGE) · airframe 24,597 hrs · 34,363 cycles
PDX - CORROSION ON UNDER SIDE OF HORIZONTAL STIFFENING RIB ON AFT FLANGE OF FRAME 253.400, BETWEEN STRINGERS 24 LT AND 25 LT. REPAIRED IAW HORIZON AIR EA 9-53-534.
Part: BRACKET — CORRODED (BS 600)
PDX - CORROSION IN ANGLE BRACKET AT FRAME X600.0 AND STRINGER 21S. REPAIRED IAW HORIZON AIR EA 9-53-536.
Part: STRINGER — CRACKED (NACELLE)
PDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11.
Part: STRINGER — CORRODED (BS 488)
PDX - CORROSION INBOARD SIDE OF RIGHT-HAND STRINGER 32 AT FRAME STATION 488. INSTALLED NEW STRINGER SPLICE IAW DHC-8 SRM 51-40-11.
Part: STRINGER — DAMAGED (NACELLE)
PDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2.
Part: SKIN — CRACKED (RT NACELLE)
PDX - RIGHT NACELLE EXTERIOR INBOARD SKIN HAS 1.5 CRACK AT STATION XN127.5 AND YW139.200, JUST AFT OF PANEL 425AL TOP EDGE. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: WEB — PUNCTURED (NACELLE)
PDX - AFT NACELLE TOP DECK HAS A PUNCTURE HOLE AT APPROXIMATELY STATION X236.00 AND YW139.900. REPAIRED IAW HORIZON AIR EA 9-54-237.
Part: FLOOR PANEL — CORRODED (CABIN)
PDX - MAIN ENTRY THRESHOLD WHERE FLOOR PANEL ATTACHES HAD NUMEROUS SPOTS OF CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SPLICE — CORRODED (BS 488.5)
PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5, STRINGER 29RH. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SPLICE — CORRODED (BS 488.5)
PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5 AND STRINGER 30RH. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: THRESHOLD — CORRODED (PAX DOOR)
PDX - MINOR SURFACE CORROSION AROUND NUT PLATES UNDER MAIN CABIN DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 6, PARAGRAPH 2C.
Part: ICE SHIELD — SCRATCHED (FUSELAGE)
PDX - TWO DEEP SCRATCHES FOUND ABOVE RIGHT ICE SHIELD. REPAIRED IAW HORIZON AIR EA 9-53-530.
Part: CLIP — CORRODED (BS 445)
PDX - CLIP CORROSION BETWEEN LEFT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
Part: FITTING — CORRODED (MLG ACTUATOR)
PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER MOUNTING PADS. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233A.
Part: SPLICE — CORRODED (BS 531)
PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 30 RT. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-40-11 AND SRM 51-20-36.
Part: FITTING — CORRODED (MLG ACTUATOR)
PDX - LEFT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233A.
Part: CLIP — CORRODED (BS 445)
PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
Part: SEAT TRACK — CHAFED (BS 282)
PDX - RIGHT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT APPROXIMATELY STATION 282. REPAIRED IAW DHC-8 SRM 51-40-00.
Part: FRAME — GOUGED (BS 618)
PDX - GOUGE AT FRAME X618.0, BETWEEN STRINGERS 21S AND 20S. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SILL — DAMAGED (CARGO DOOR)
PDX - NICKS BELOW CARGO DOOR SILL. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2.
Part: CONNECTOR — CORRODED (DEICE SYSTEM)
PDX - INSPECT DEICE DISTRIBUTOR CANNON PLUGS AND PRESSURE SWITCHES FOR CORROSION AND SERVICEABILITY. REMOVED AND REPLACED PRESSURE SWITCHES. (S/N 6503, 3509, 7020 AND 6951).
Part: SKIN — CHAFED (BS 262.400)
PDX - CHAFE DAMAGE AT STATION 262.400 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT, IT IS APPROXIMATELY .003 DEEP. REMOVAL WAS .001. FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM PAGE 4, TABLE 2.
Part: SEAT TRACK — GOUGED (BS 377)
PDX - SMALL GOUGE IN BOTTOM OF LEFT INBOARD SEAT TRACK, APPROXIMATELY STATION 377. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 300)
PDX - LEFT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT STATION 300. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 242)
PDX - LEFT OUTBOARD SEAT TRACK HAS CHAFING PITS ON INBOARD LIP APPROXIMATELY STATION 242. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 330)
PDX - LEFT INBOARD SEAT TRACK CHAFFED IN BOTTOM OF TRACK APPROXIMATELY AT STATION 330. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 387 - 405)
PDX - LIGHT SURFACE CORROSION ON RIVET HEADS AND WEB PLATE FROM RIGHT-HAND OUTBOARD SEAT TRACK TO STRINGER 23, BETWEEN FRAMES 387.350 AND 405.737. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: STRINGER — CORRODED (BS 488)
PDX - CORROSION AROUND RIVET LEFT-HAND SIDE OF STRINGER 33 AT FRAME STATION 488. REPAIRED IAW DHC-8 SRM 51-40-11.
Part: SPLICE — CORRODED (BS 531)
PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 29 RT. REPAIRED IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, PARAGRAPH 8D AND DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.
Part: FRAME — CORRODED (BS 510)
PDX - CORROSION ON FRAME FLANGE AT STATION 510 BETWEEN STRINGERS 30 AND 31 RT. REPAIRED IAW 20-32-02, PAGE 2, PARAGRAPH A, B AND C.
Part: FRAME — CORRODED (BS 653.349)
PDX - CORROSION NUMEROUS PLACED AROUND RIVETS ON TOP OF FRAME X653.349, BETWEEN STRINGER 23S AND 23P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2, SRM 51-20-11, PAGE 6, PARAGRAPH 2C AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 531)
PDX - CORROSION ON FRAME FLANGE AT STATION 531 BETWEEN STRINGERS 30 AND 31 RT. REMOVED LIGHT CORROSION IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, PARAGRAPH 8D. FOUND WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.
Part: CLIP — CORRODED (BS 531)
PDX - CLIP HAS CORROSION BETWEEN RIGHT-HAND STRINGER 31 AND 32 AT FRAME STATION 531. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2 AND SRM 51-20-11, PAGE 6, PARAGRAPH 2C.
Part: SPLICE — CORRODED (BS 531)
PDX - MINOR CORROSION ON TOP FLANGE OF STRINGER SPLICE AT STATION 531 AND STRINGER 28 RT. ACID ETCHED, ALODINED, AND PRIMED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.
Part: SEAT TRACK — CHAFED (BS 456)
PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED AND NICKED AT APPROXIMATELY STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 531)
PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 531. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 540 - 543)
PDX - PITTING CORROSION AND NICKS ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 540-543. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: ANGLE — CRACKED (FUSELAGE)
PDX - LEFT-HAND FORWARD CONNECTION ANGLE WAS CRACKED THROUGH THE OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 9-53-348A.
Part: SEAT TRACK — CHAFED (BS 436)
PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED IN BOTTOM OF TRACK APPROXIMATELY 10 FROM STATION 436. REPAIRED IAW DHC08 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 471)
PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 471. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 456)
PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 456)
PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED AND NICKED AT APPROXIMATELY STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (FUSELAGE)
PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL BETWEEN STRINGER 467.000 AND 445.500, LESS THAN 1 INCH LONG. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: BRACKET — CORRODED (BS 618)
PDX - CORROSION IN AND AROUND NUT PLATE AND BRACKET AT FRAME X618.0, STRINGER 21S. REMOVED SURFACE CORROSION AROUND BRACKET AND IN NUT PLATE. FOUND TO BE WITHIN LIMITS OF DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.
Part: CLIP — CORRODED (BS 467)
PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 467. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
Part: SEAT TRACK — CORRODED (BS 405.737)
PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL AT STATION 405.737. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CORRODED (BS 467)
PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL 4 AFT OF STATION 467.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: BRACKET — CHAFED (BS 636)
PDX - A .25 INCH CHAFE MARK ON TIE IN BRACKET AT FRAME X636.0 AND STRINGER 22S. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.
Part: SEAT TRACK — CORRODED (BS 488.5)
PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL AT STATION 488.500. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 488)
PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT STATION 488 AND LUG LIP WORN. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: CLIP — CORRODED (BS 531)
PDX - CLIP HAS CORROSION OUTBOARD END BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 531. REPAIRED IAW PSMI-GEN-5, CHAPTER 4, PART 2, PARAGRAPH 3, 1, PAGE 4-4.
Part: SEAT TRACK — CHAFED (BS 500 - 520)
PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED FROM APPROXIMATELY STATION 500 TO 520. REPAIRED IAW DHC-8 SRM 51-20-36 AND SRM 51-20-16.
Part: SEAT TRACK — CHAFED (BS 500 - 545)
PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT APPROXIMATELY STATION 500 TO 520 AND 545. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
Part: SEAT TRACK — CHAFED (BS 445 - 470)
PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT APPROXIMATELY STATION 445, 456 AND 470. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-21-36.
Part: FRAME — CORRODED (BS 636)
PDX - CORROSION ON FRAME X636.0 AT STRINGER 22P. REPAIRED IAW DHC-8 SRM 51-20-26.
Part: BRACKET — CORRODED (BS 636)
PDX - CORROSION ON UPPER AND LOWER ANGLE BRACKETS, FRAME X636.0, STRINGER 22P. REPAIRED IAW DHC-8 SRM 51-20-41, SRM 51-20-16 AND SRM 51-20-26.
Part: AXLE — DAMAGED (NLG)
PDX- NOSE GEAR TRAILING ARM HAS SEVERAL GOUGES. MAINTENANCE REPLACED TRAILING ARM ASSEMBLY. GEAR SWINGS AND OPERATIONAL CHECKS GOOD.
Part: TRAILING ARM — GOUGED (NLG)
SEA- NOSE WHEEL SWIVEL GOUGED APPROX .035 DEEP. AIRCRAFT FERRIED FROM SEA TO PDX FOR REPAIRS. IN PDX, MAINTENANCE REMOVED THE DAMAGED TRAILING ARM, AND THE UNDAMAGED AXLE AS A UNIT. REPLACED WORN CONNECTION LINK PIN. INSTALLED OVERHAULED TRAILING ARM, AND NEW AXLE IAW CMM 32-20-01, OPERATIONAL CHECKS GOOD.
Part: LIGHT — INOP (COCKPIT)
COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE OVERHEAD LIGHT, OPERATIONAL CHECKS GOOD.
1998
Part: LIGHT — INOP (ROW 3E)
SEA - ESCAPE PATH LIGHTING AT ROW 3E INOP. MAINTENANCE PLACED ON MEL 33-13. AIRCRAFT RETURNED TO SERVICE.
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED MAIN CABIN DOOR STOPS AND LINKAGE, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: POWER SUPPLY — INOP (CABIN)
EMERGENCY LIGHT AT ROW 4 INOPERATIVE. ONE OUTSIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY PACK AND CHARGING UNIT. OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
ROW 5 CENTER EMERGENCY LIGHT INOP. RELAMPED OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
PDX - RIGHT FORE FUSELAGE EMERGENCY LIGHT INOP, RIGHT EXIT SIGN WITH THRESHOLD LIGHTS INOP, AND FRONT CABIN EXIT LOCATOR LIGHTS INOP. REPLACED PS2 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
1997
Part: SEAT TRACK — CORRODED (BS 302-400)
PDX - CORROSION AT LEFT OUTBOARD SEAT TRACK AT STA 302.400 (MARKED AT TOP SECTION) REPAIRED IAW EA 9-53-353.
Part: Z MEMBER — CRACKED (NLG WW)
PDX - Z-MEMBER ON LHEFT HAND SIDE OF NLG SIDEWALL AT K97.0 AND APPROX Z109 HAS A CRACK RUNNING BETWEEN 2 RIVETS THROUGH THE RADIUS OF THE BEND. REPAIRED IAW 9-53-352.
Part: SKIN — GOUGED (FUSELAGE)
PDX - GOUGE LOCATED ON LOWER RIGHT FUSELAGE SKIN. REPAIRED IAW EA9-53-184.
Part: SKIN — DAMAGED (CARGO DOOR)
PDX - CARGO DOOR TOP AFT ADJUSTABLE STOP HAS BEEN STRIKING THE DOOR APATURE AND THE INNER SKIN HAS MATERIAL LOSS .400 DEEP FROM ORIGINAL. REPAIRED IAW EA 9-53-349.
Part: BRACKET — CORRODED (LT MLG ACT)
PDX - LEFT MAIN LANDING GEAR ACTUATOR UPPER ATTACH BRACKET MOUNTING FACE ON AIRFRAME SIDE HAS LIGHT CORROSION AROUND UPPER ATTACH BOLD HOLE. REPAIRED IAW EA 9-54-146.
Part: LIGHT — BROKEN (CABIN)
SEA- EMERGENCY EXIT LIGHT BY SEAT 1E IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ON SIDE WALL, OPERATIONAL CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
SEA- AFT OVERHEAD AND LEFT AFT OUTBOARD EMERGENCY EXIT LIGHTS ARE OUT. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
AFT OVERHEAD AND AFT LEFT HAND EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY BOX P-3. ORIGINAL BATTERY IN AIRCRAFT EMERGENCY LIGHTS CHECKED GOOD, OPERATIONAL CHECK GOOD.
1996
Part: BULB — FAILED (FWD EXIT)
PDX - ONE FLOOR PROXIMITY LIGHT IS INOPERATIVE AT THE FORWARD EXIT, 3RD BULB BACK. BULB WAS REPLACED AND BULB OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SENSOR — INTERMITTENT (NLG)
SEA - NOSE GEAR RED UNSAFE ADVISORY LIGHT AND GEAR HANDLE LIGHT CYCLED ON AND OFF FOR VARYING LENGTHS OF TIME IN CRUISE. AIRCRAFT LANDED IN SEA WITHOUT FURTHER PROBLEM. AIRCRAFT INSPECTED AND FERRIED TO PDX. NLG DRAG STRUT PROX SENSOR FAILED AIR/GRO TEST. DRAG STRUT PROX SENSOR REPLACED AND CHECKED GOOD IAW MAINT MANUAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE.
1995
Part: SENSOR — OUT OF ADJUST (NLG)
BOI - NOSE GEAR INTRANSIT LIGHT ILLUMINATES IN-FLIGHT. AIRCRAFT LANDED IN BOI WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. NOSE GEAR DRAG LINK PROXIMITY SENSOR ADJUSTED I/A/W MAINT MANUAL. PSEU TARGET/SENSOR TEST PERFORMED, CHECK GOOD. SENSOR CANNON PLUG CLEANED. NOSE GEAR INIDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE.
Part: EEL CONTROL BOX — MALFUNCTIONED (COCKPIT)
PDX - EMERGENCY LIGHTING REMAINS ON WITH EMERGENCY LIGHTING SWITCH OFF. LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.