N499US
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.
464 reports on file, 1995-01-25 – 2002-11-28.
Part: SIGN — INOPERATIVE (CABIN) · airframe 42,815 hrs · 52,594 cycles
PDX- CABIN ENTRANCE EXIT LOCATING SIGN HAS SEVERAL LIGHT BULBS BURNT OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PRESSURE PANEL — DENTED (FUSELAGE) · airframe 42,615 hrs · 52,433 cycles
PDX-DENT IN FORWARD WALL OF NOSE WHEEL WELL IN SECOND CHANNEL AREA 6 INCHES FROM TOP. REPAIRED IAW FSRM 51-31-01 AND 53-02-01.
Part: RELAY — FAILED (FIRE WARNING) · airframe 42,204 hrs · 52,114 cycles
PDX- ENGINE FIRE BELL DOES NOT SOUND, ALL LIGHTS ILLUMINATED. REMOVED AND REPLACED FIRE WARNING BELL RESET RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CABLE — BROKEN (EMERGENCY EXIT) · airframe 42,048 hrs · 51,981 cycles
SEA - FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY DOOR HANDLE FOR THE GALLEY EMERGENCY EXIT IS STUCK. MAINTENANCE INSPECTED AND FOUND THE FORWARD TENSION CABLE BROKEN. THE DOOR WAS REMOVED, CABLE WAS REPLACED, THE DOOR WAS REINSTALLED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WHEEL — DEFECTIVE (ZONE 700) · airframe 42,031 hrs · 51,966 cycles
SEA-DURING ROTATION MODERATE TO SEVERE VIBRATION FELT FROM NOSE WHEEL AREA. VIBRATION WAS EVIDENT IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO SEA, LANDED AIRCRAFT WITHOUT INCIDENT. FIRE AND RESCUE MET AIRCRAFT ON LANDING. REPLACED #1 AND #2 NOSE WHEEL ASSY. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 41,948 hrs · 51,894 cycles
BOI- AFT MID CABIN CEILING EXIT SIGN HAS SEVERAL LAMPS INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 41,861 hrs · 51,820 cycles
BOI- EMERGENCY EXIT SIGN ABOVE CENTER AISLE ROW 8 HAS SEVERAL LIGHTS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 41,861 hrs · 51,820 cycles
BOI- EMERGENCY EXIT SIGN LIGHT ABOVE PASSENGER CABIN ENTRANCE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONTROL BOX — MALFUNCTIONED (APU) · airframe 41,772 hrs · 51,750 cycles
BOI- TOWER REPORTED PUFF OF SMOKE AND SMALL AMOUNT OF FLAME FROM AREA OF NR 2 ENGINE FOLLOWING TOUCHDOWN. NO ABNORMAL INDICATIONS ON ENGINE INSTRUMENTS OR APU. REMOVED AND REPLACED START AND OVERSPEED CONTROL BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: VALVE — INOPERATIVE (CABIN) · airframe 41,756 hrs · 51,737 cycles
BOI- CLIMBING THROUGH 25,000 FEET CABIN PRESSURIZATION WAS CLIMBING 8,000 FEET. LEVELED OFF AT 26,000 FEET, CABIN PRESSURE CONTINUED TO CLIMB TO 10,000. (AIRFOIL ANTI-ICE WAS ON AND WING TEMPERATURE WAS IN YELLOWAND BACK-UP VALVE WAS CLOSED).AIRCRAFT RETURNED TO FEILD WITH OUT INCIDENT.ON DECENT TO BOI TURNED AIRFOIL OFF, BACK-UP VALVE OPENED AND PRESSURE RETURNED TO 55 PSI.REMOVED AND REPLACED #1 BACK-UP VALVE AND #2 MAIN VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FIRE — DETECTED (NR 2 ENGINE) · airframe 41,735 hrs · 51,735 cycles
BOI- BOI TOWER REPORTED FLAMES AND SMOKE COMING FROM NR 2 ENGINE AT TOUCHDOWN, NO ABNORMAL INDICATIONS ON ENGINE GAUGES. SHUTDOWN NR 2 ENGINE ON ROLL OUT. PERFORMED VISUAL INSPECTION OF TAILPIPE/EXHAUST AND INTAKE, NO DEFECTS NOTED. PERFORMED GROUND RUN AT NUMEROUS POWER SETTINGS WITH THROTTLE IDLE, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 41,548 hrs · 51,562 cycles
PDX - AIRCRAFT RETURNED TO FIELD WHEN LAVATORY SMOKE DETECTOR SOUNDED. AIRCRAFT DOWN FOR MAINTENANCE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 41,548 hrs · 51,561 cycles
PDX- RIGHT ARROW OF FORWARD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TURNED ON. REMOVED AND REPLACED FORWARD EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: APU — LEAKING (APU BAY) · airframe 41,472 hrs · 51,497 cycles
YEG - AIRCRAFT RETURNED TO FIELD WHEN THE LAVATORY SMOKE DETECTOR SOUNDED. DURING INSPECTION OF APU AN EXTERNAL OIL LEAK WAS NOTED. MAINTENANCE INSPECTED THE ACM PACK CONDENSER SOCKS FOR OIL CONTAMINATION. NONE WAS NOTED. PRESSURIZED AND RAN AIRCRAFT WITH PACKS AT FULL HOT FOR 20 MINUTES. NO SMOKE WAS NOTED AND SMOKE DETECTOR DID NOT SOUND. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 1995–2001 · 450 reports
2001
Part: BATTERY — DISCHARGED (CABIN) · airframe 41,135 hrs · 51,230 cycles
SEA- CABIN FORWARD EXIT SIGN IS DIM. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 41,048 hrs · 51,157 cycles
PDX- BOTH FORWARD EXTERIOR EVACUATION LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 40,962 hrs · 51,089 cycles
PDX - EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR HAS NUMEROUS LIGHTS OUT. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 40,907 hrs · 51,040 cycles
PDX - EMERGENCY EXIT SIGN FACING AFT AT THE MIDDLE CABIN POSITION HAS BULB SEGMENTS THAT ARE INOPERATIVE. REMOVED AND REPLACED THE EXIT SIGN ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 40,907 hrs · 51,040 cycles
PDX - EMERGENCY EXIT SIGN FACING FORWARD AT THE MIDDLE CABIN POSITION IS INOPERATIVE IN THE ARMED MODE. REPLACED THE EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RELAY — FAILED (COCKPIT) · airframe 40,846 hrs · 50,988 cycles
PDX- COCKPIT EMERGENCY LIGHTS ILLUMINATED WHEN EXTERNAL POWER IS ON. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHTS RELAY LV3-164. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - INTERCOSTAL AT FRAME 6305 AND STRINGER 18 HAS A 3/8 INCH CRACK EMITTING FROM RIVET HOLE. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FUSELAGE SKIN EXTERIOR HAS A DENT THAT MEASURES 3 INCHES X 1.2 X .025 DEEP. LOCATED 6 INCHES AFT OF FRAME 6805 AND 8 INCHES BELOW SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31-01.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - DENT IN SIDE OF FUSELAGE APT APPROXIMATELY 40 INCHES AFT OF MAIN CABIN DOOR WL 22.047 AND FS 238.779. REPAIRED IAW HORIZON AIR EA 4-53-1513 AND FOKKER SRM 51-31-01.
Part: SKIN — DAMAGED (FUSEAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FUSELAGE SKIN EXTERIOR HAS A VERTICAL CREASE MARK THAT MEASURES 2 INCHES X .100 X .021 DEEP. LOCATED 8 INCHES AFT OF FRAME 6805 AND 6 INCHES BELOW SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FUSELAGE EXTERIOR SKIN HAS A DENT MEASURING .500 X .200 X 0.11 DEEP. LOCATED 1.5 INCHES AFT OF FRAME 6805 AND 1.5 INCHES BELOW SKIN LAP JOINT AT 560WL. REPAIRED IAW FOKKER SRM 53-02-07 AND SRM 51-31-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FUSELAGE EXTERIOR SKIN HAS A DENT MEASURING 3 INCHE X 2 X .029 DEEP. LOCATED 3 INCHES AFT OF FRAME 6805 AND 2 INCHES BELOW SKIN LAP JOINT AT -560WL.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FORWARD FUSELAGE SKIN EXTERIOR HAS A DENT THAT MEASURES 1.2 INCHES X .400 X 0.37 DEEP. LOCATED 1.2 INCHES FORWARD OF FRAME 3050 AND 10 INCHES ABOVE SKIN LAP JOINT AT -560WL. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, FIGURE 1.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,382 hrs · 50,601 cycles
PDX - LEFT-HAND SIDE FORWARD FUSELAGE SKIN EXTERIOR HAS A SHARP DENT THAT MEASURES 1.4" X 1.0" X .035" DEEP. LOCATED 1.5" ABOVE SKIN LAP JOINT AT -560WL AND 8.5" AFT OF FRAME 3050. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3, FIGURE 1.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 40,071 hrs · 50,324 cycles
PDX - AFT EXTERIOR EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 39,991 hrs · 50,248 cycles
PDX- UPON INSPECTION, FOUND DAMAGE TO CARGO DOOR FRAME. REPAIRED IN ACCORDANCE WITH FOKKER STRUCTURAL REPAIR MANUAL. REQUIRED INSPECTION COMPLIED WITH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 39,981 hrs · 50,241 cycles
SEA- EMERGENCY LIGHT EXIT SIGN INOP AT MID CABIN FORWARD POSITION. REMOVED AND REPLACED FORWARD FACING MID CABIN EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAULTY (CABIN) · airframe 39,989 hrs · 50,158 cycles
PDX - UPON INSPECTION, FOUND EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR AND CENTER AISLE TO HAVE INOPERATIVE LAMPS. REMOVED AND REPLACED CIRCUIT CARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 39,401 hrs · 49,689 cycles
GEG- ROW 8 AFT EXIT SIGN HAS INOPERATIVE BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 39,392 hrs · 49,679 cycles
PDX-DURING OVERNIGHT CHECK FOUND CEILING AND RIGHT HAND FORWARD AND AFT EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT RIGHT HAND AFT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (GALLEY) · airframe 39,190 hrs · 45,490 cycles
SEA- EXIT LIGHT GALLEY OVERHEAD INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
2000
Part: POWER SUPPLY — FAILED (CABIN) · airframe 38,353 hrs · 48,715 cycles
SEA - SEVERAL EMERGENCY EXIT LIGHTS ILLUMINATED WITH POWER TO SYSTEM OFF. REMOVED AND REPLACED POWER SUPPLY AT FORWARD OVERHEAD LOCATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND HORIZONTAL STABILIZER AT RIB 1886 HAS A 2 INCH CRACK AT OLD REPAIR WITH MANY POPPED CHERRY RIVETS. REPAIRED IAW HORIZON AIR EA 4-55-256.
Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND AIR CYCLE MACHINE TO NOSE BAY SIDE WALL HAS DAMAGE AROUND FASTENERS. REMOVED ATTACHING PIN STORAGE BOX. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2 AND 53-01-01 PAGE 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 5805 HAS A CRACKED CASTELLATION BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-12 FIGURE 1 AND HORIZON AIR EA 4-53-1360.
Part: FRAME — DAMAGED (NLG WW) · airframe 38,317 hrs · 48,678 cycles
PDX- INSIDE NOSE WHEEL BAY RIGHT HAND SIDE, BETWEEN PIN STORAGE BOX AND FRAMES 2240 AND 2650 IS A DAMAGED WEB PLATE. REPAIRED IAW HORIZON AIR EA 4-53-1361.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,317 hrs · 48,678 cycles
PDX- DELAMINATION AT TRAILING EDGE OF INBOARD FLAP, RIGHT HAND WING LOWER SIDE 38 INCHES FROM INBOARD EDGE. REPAIRED IAW FOKKER SRM 51-70-0 PAGE 17.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 CASTELLATION BETWEEN STRINGERS 28 AND 29 HAVE SIX CRACKED DIMPLED HOLES. REPAIRED IAW FOKKER SRM 51-10-05, 51-10-06 AND HORIZON AIR EA 4-53-1358.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- INSIDE NOSE WHEEL BAY RIGHT HAND SIDE, FRAME 2650 DAMAGED NEXT TO THE PIN STORAGE BOX. REPAIRED IAW HORIZON AIR EA 4-53-1361.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- INSIDE NOSE WHEEL BAY RIGHT HAND SIDE, FRAME 2240 DAMAGED NEXT TO THE PIN STORAGE BOX. REPAIRED IAW HORIZON AIR EA 4-53-1361.
Part: STRAP — DELAMINATED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING LOWER SKIN STRAP AT STATION 8200 AND FRONT SPAR STRAP LAMINATIONS ARE DEBONDING. REPAIRED IAW HORIZON AIR EA 4-57-477.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 4610 IS CRACKED AT STRINGER AND SKIN CONNECTION, FORWARD CARGO PIT BETWEEN STRINGERS 8 AND 8A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND HORIZON AIR EA 4-53-1359.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- PITTING CORROSION ON FUSELAGE SKIN UNDER WHERE UPPER NAV/COMM ANTENNA IS ATTACHED. REPAIRED IAW FOKKER SRM 53-02-04 FIGURE 2, 53-01-01 PAGE 5 AND 6 AND HORIZON AIR EA 4-53-1346.
Part: RIVET — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- RIVET HEAD DAMAGED IN TOP BOX BEAM OF LEFT HAND AFT OVERWING EMERGENCY EXIT. REPAIRED IAW FOKKER SRM 51-31-05 AND HORIZON AIR EA 4-53-1357.
Part: FRAME — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON FRAME 5305 UNDER NUT PLATE ABOVE STRINGER 2. REPAIRED IAW HORIZON AIR EA 4-53-1352.
Part: FAIRING — CRACKED (LT STUBWING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND STUBWING AFT LOWER FAIRING SKIN HAS A 3 INCH LONG CRACK EXTENDING FROM EXISTING REPAIR. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-05 AND 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660, CASTELLATION CRACKED BELOW STRINGER 56. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-11.
Part: BOLT — CORRODED (FLAP ROLLER FRM) · airframe 38,317 hrs · 48,678 cycles
PDX- FLAP ROLLER A FRAME BOLT AT RIGHT HAND STATION 1700 HAS LIGHT CORROSION. REPAIRED IAW HORIZON AIR EA 4-57-476.
Part: FRAME — BUCKLED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- BETWEEN STRINGER 46 AND 50, FRAME 16660 IS BUCKLED. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1353.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTER SKIN ON FRAME 16660 HAS A CRACK COMING OUT OF A RIVET HOLE BETWEEN STRINGERS 56 AND 57. REPAIRED IAW FOKKER SRM 53-02-11 AND 51-31-01.
Part: BEAM — CRACKED (BULKHEAD) · airframe 38,317 hrs · 48,678 cycles
PDX- BEAM TWO UPPER SURFACE OF REAR PRESSURE BULKHEAD HAS A .25 INCH CRACK IN THE RIGHT HAND OUTBOARD EDGE OF THE BEAM RADIUS. REPAIRED IAW FOKKER SRM 53-02-18 PAGE 35, 51-10-04, 51-31-01 PAGE 13, AND HORIZON AIR EA 4-53-1354.
Part: BULKHEAD — CRACKED (ACM BAY) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND AIR CYCLE MACHINE BULKHEAD WALL APPEARS TO BE CRACKED AT LOWER EDGE, SEEN THROUGH PANEL 24A. REPAIRED IAW FOKKER SRM 51-31-05, 51-31-01, 53-02-18 PAGE 29 AND 51-10-04.
Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 38,317 hrs · 48,678 cycles
PDX- FLOOR SURFACE BENEATH CO-PILOTS SEAT TRACKS HAVE LOOSE AND MISSING PAINT WITH SOME SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PARA 4.
Part: FASTENER — MISINSTALLED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STEMS PROTRUDING FROM THREE BLIND RIVETS AT RIGHT HAND STATION 8200 UPPER RIB FROM PANEL 74E. REPAIRED IAW HORIZON AIR EA 4-57-474.
Part: CLAMP — CHAFED (HYDRAULIC LINE) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND STUBWING, NR 1 HYDRAULIC SUCTION LINE ATTACHING CLAMP, JUST AFT OF DOOR O2J IS CHAFING AGAINST ENGINE THRUST ROD. REPAIRED IAW FOKKER SRM 29-10-01.
Part: STRUCTURE — CRACKED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- ONE CRACK COMING FROM THE AFT BUSHED HOLE AT THE 6 O''CLOCK POSITION APPROXIMATELY .5 INCH LONG. REPAIRED IAW HORIZON AIR EA 4-57-471.
Part: RIB — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION AT END RIB 1825, 28 INCHES AFT OF FORWARD SPAR ACCESS THRU 72A. REPAIRED IAW FOKKER SRM 51-30-02 AND 28-11-0.
Part: ANGLE — GOUGED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 BETWEEN STRINGERS 39 AND 40, FRAME TO SKIN ATTACH ANGLE GOUGED THROUGH ANGLE. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- .135 DEEP, 4 WIDE, 5.5 INCHES LONG CONCAVE DENT IN EXISTING REPAIRED PATCH, JUST BELOW STRINGER 58, 4 INCHES FORWARD OF FRAME 17065. REPAIRED IAW FOKKER SRM 53-02-05 FIGURE 3, 53-02-02 FIGURE 1, 51-10-4 AND HORIZON AIR EA 4-53-1348.
Part: BULKHEAD — CRACKED (ACM BAY) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGH HAND AIR CYCLE MACHINE BULKHEAD APPEARS TO BE CRACKED AT LOWER EDGE BETWEEN NOSE BAY AND AIR CYCLE MACHINE COMPARTMENT. REPAIRED IAW FOKKER SRM 53-02-18 PAGE 29.
Part: LATCH — CORRODED (CARGO DOOR) · airframe 38,317 hrs · 48,678 cycles
PDX- GAIN ACCESS TO AFT CARGO BAY DOOR LATCH FITTING TORSION BOX INTERIOR FOR CORROSION REMOVAL. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND HORIZON AIR EA 4-53-1343.
Part: BEAM — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- BEAM BL1562R HAS SEVERAL CRACKS PROPAGATING FROM RIVET HEADS BETWEEN STRINGERS 2.08 AND 2.04. REPAIRED IAW FOKKER SRM 53-02-17 PAGE 10, 51-31-01, 51-10-04.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX-CORROSION ON BOTTOM OF FLOOR SUPPORT FLANGE 2 INCHES FORWARD OF RIGHT HAND INBOARD SEAT TRACK FORWARD END. CORROSION APPEARS TO EXTEND UNDER MATING AREA WITH SUPPORT ANGLE ATTACHED AT FRAME 4610 AND FLOORBEAM 10. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-10-04 PAGE 9.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- INSIDE AT FRAME 24-2 STRINGER 31 AT TOP THERE IS A CRACK THAT CONTINUES BEYOND THE STOP DRILL. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 7 AND HORIZON AIR EA 4-53-1349.
Part: PANEL — DAMAGED (RT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND FORWARD WING PANEL 92J LOWER AFT BOLT AT STATION 1700 HAS CREATED A HOLE IN THE LOWER WING ATTACH PLATE. REPAIRED IAW HORIZON AIR 4-57-473.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- INSIDE AT FRAME 17565 AND STRINGER 23 ONE FRAME AFT OF BULKHEAD THERE IS A CRACKED CLIP RUNNING BETWEEN TWO RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: RIVET — MISINSTALLED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- ABOVE STRINGER 33 BETWEEN FRAMES 16060 AND 16660 AT PREVIOUS REPAIR SPLICE, ONE RIVET HAS NO EDGE DISTANCE AND ONE RIVET HOLE DRILLED INTO EDGE OF REPAIR SPLICE. REPAIRED IAW HORIZON AIR EA 4-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK HAS CORROSION PITS ON OUTBOARD FLANGE AT FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-01, PAGE 201-206. HORIZON AIR EA 4-53-1347.
Part: SUPPORT BRACKET — CHAFED (LT MLG) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND MAIN LANDING GEAR SIDE TRAY UPPER MEMBER CHAFING ON SUPPORT ANGLE IN OVERHEAD STRUT BAY. REPAIRED IAW FOKKER SRM 51-00-00 PAGE 2 AND HORIZON AIR EA 4-32-201.
Part: RIVET — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 33 BETWEEN FRAMES 16060 AND 16660 HAS THREE TOENAILED RIVETS IN STRINGER SPLICE. REPAIRED IAW FOKKER SRM 4-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE, 4 AREAS BETWEEN FRAMES 11905 AND 13345. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON TOP FLANGE OF FLOORBEAM LOCATED AT BL 620R 12 INCHES AFT OF FRAME 3870. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, 55-01-00.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION ON BOTH FLANGES FROM FRAME 9305 TO 9805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGES 201-206.
Part: STRINGER — DENTED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 40 IS DENTED BETWEEN 3 AND 8 INCHES AFT OF FRAME 16660. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-01 PAGE 8.
Part: PANEL — CRACKED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- SEVEN CRACKS AT FIVE FASTENER HOLES ON PANEL 72A APERTURE. REPAIRED IAW HORIZON AIR EA 4-57-470.
Part: RIVET — MISINSTALLED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- BELOW STRINGER 33 REPAIR SPLICE BETWEEN FRAMES 16060 AND 16660, ONE RIVET HAS NO EDGE DISTANCE AND ONE RIVET HOLE WAS DRILLED INTO EDGE OF SPLICE. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND HORIZON AIR EA 4-53-1342.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD CABIN SEAT TRACK HAS CORROSION PITS ON INBOARD FLANGE AT FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-01, PAGE 201-206, AND HORIZON AIR EA 4-53-1347.
Part: FITTING — CRACKED (MLG DOOR ACT) · airframe 38,317 hrs · 48,678 cycles
PDX- BATH TUB FITTING CRACKED AT BL225 INBOARD AT AFT MAIN LANDING GEAR DOOR ACTUATOR ATTACH POINT. REPAIRED IAW FOKKER SRM 51-30-02 AND HORIZON AIR EA 4-53-1350.
Part: SEAT TRACK — GOUGED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 10 INCH LONG GOUGES STARTING 4 INCH AFT OF STATION 6805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND HORIZON AIR EA 4-53-1347.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE BETWEEN FRAMES 13345 AND 15635. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9, 53-40-01 AND HORIZON AIR EA 4-53-1347.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON TOP FLANGE OF FLOORBEAM LOCATED BL 1140R BETWEEN FRAMES 4610 AND 3870. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-01-00.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 WHERE STRINGER 51 REPAIR PASSES THROUGH FRAME IS CHAFING REPAIR STRINGER. REPAIRED IAW FOKKER SRM 53-01-01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- AFT CARGO DOOR FORWARD APERTURE HAS IMPACT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-31-05.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- MEASURED THICKNESS OF SKIN DUE TO METAL REMOVED UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 53-02-10, FIG 1, 53-00-00 AND HORIZON AIR EA 4-53-1345.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 WHERE STRINGER 50 REPAIR PASSES THROUGH FRAME IS CHAFING REPAIR STRINGER. REPAIRED IAW FOKKER SRM 53-01-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND FUSELAGE SKIN IS DENTED BETWEEN FRAMES 6305 AND 6805 AT APPROXIMITLY WL-0-, DENT MEASURES APPROXIMATELY 9 INCHES BY 4 INCHES BY .095 DEEP. STRINGER 16 IS BENT DIRECTLY BEHIND SKIN DENT. REPAIRED IAW HORIZON AIR EA 4-53-1337 AND FOKKER SRM 53-02-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CASTELLATION CRACKED IN UPPER CORNER AT FRAME 6805, JUST BELOW STRINGER 16. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 1 AND 53-16-04 PAGE 12.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 WHERE STRINGER 48 REPAIR PASSES THROUGH FRAME IS CHAFING REPAIR STRINGER. REPAIRED IAW FOKKER SRM 53-01-01.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305A AND STRINGER 45. CLIP REPAIR DOUBLER HAS GOUGES AND SHEET METAL TOOL DAMAGE. REPAIRED IAW FOKKER SRM 51-10-04, 53-02-13 PAGE 4 AND 51-31-01.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 WHERE STRINGER 49 REPAIR PASSES THROUGH FRAME IS CHAFING REPAIR STRINGER. REPAIRED IAW FOKKER SRM 53-01-01.
Part: STRINGER — CORRODED (BULKHEAD) · airframe 38,317 hrs · 48,678 cycles
PDX- FAKE BULKHEAD SUPPORT STRINGER IS CORRODED AT STATION 15635 AND STRINGER 21 AT BULKHEAD ATTACHMENT POINTS. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-02-01 PAGE 7.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FUSELAGE SKIN IS DENTED AT FRAME 16660 BETWEEN STRINGERS 51 AND 52. REPAIRED IAW HORIZON AIR EA 4-53-1341.
Part: SEAT TRACK — CRACKED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK VERTICAL SUPPORT ANGLE IS CRACKED AT TIE IN POINT OF INBOARD FLANGE AT STATION 9305B. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9, 53-15-05 PAGE 5 AND 51-31-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 10 INCH LONG GOUGE MARKS WITH SOME PITTING CORROSION BETWEEN FRAMES 8305 AND 8805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 AT STRINGER 36, CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 6305 AND STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8805 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8305 AND STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 10 INCHES LONG GOUGE MARKS WITH SOME PITTING CORROSION AT FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: FRAME — TOOL DAMAGE (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- COCKPIT FRAME 1890 LEFT HAND LBL 40, W34 STRUCTURAL BRACKET HAS TOOL MARKS. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND 51-00-00 PAGE 2.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS A 5 INCH LONG AREA WITH CORROSION PITS LOCATED 6 INCHES AFT OF FRAME 9305A. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: RIVET — CRACKED (FUSELAGE FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- COCKPIT FRAME 1890 LEFT HAND FORWARD SIDE OF FRAME ANGLE HAS TWO CRACKED RIVETS. REPAIRED IAW FOKKER SRM 53-13-11 PAGE 10 AND 11.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 15 INCH LONG GOUGE MARKS WITH PITTING CORROSION BETWEEN FRAMES 9305A AND 9305B. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: CLIP — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CLIP REPAIR ON FRAME 9305A AT STRINGER 40, BUCK TAILS NAILED OVER AND REPAIR CLIP TORN. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BEAM — CRACKED (BULKHEAD) · airframe 38,317 hrs · 48,678 cycles
PDX- BEAM THREE LOWER SURFACE OF REAR PRESSURE BULKHEAD HAS A .25 INCH CRACK ALONG THE LOWER SURFACE OF THE BEAM RADIUS RIGHT HAND SIDE BEHIND THE LAV DRAIN PIPE. REPAIRED IAW FOKKER SRM 53-02-18 PAGE 38 AND 51-31-01.
Part: STRUCTURE — CRACKED (MLG WW) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACK INDICATION AT RIVET ROW ABOVE LANDING GEAR PIN STORAGE BOX, STATION 2250. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1338.
Part: SEAT TRACK — GOUGED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK, INSIDE CHANNEL HAS 2 GOUGES WITH SOME PITTING CORROSION BETWEEN FRAME 9305C - 9805. REPAIRED IAW FOKKER 51-10-4, PAGE 9 AND SRM 53-40-01, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD CABIN SEAT TRACK, INSIDE CHANNEL HAS A CORROSION PIT MARKED AT FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-01, PAGE 201-206.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FORWARD FACE OF FRAME 15635 AND ATTACH BRACKETS ARE CHAFED AND SHOW FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01 PAGE 201-206.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16060 HAS A CRACK IN CASTELLATION RADIUS IMMEDIATELY ABOVE STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 13 INCH LONG GOUGE MARKS WITH SOME PITTING CORROSION BETWEEN FRAMES 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16060 HAS A CASTELLATION CRACKED AT STRINGER 36 AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS A CORROSION PIT 9 INCHES FORWARD OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK INBOARD FLANGE HAS FRETTING CORROSION AT FRAME 9305C-10346. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-01, PAGE 201-206.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16060, CASTELLATION CRACKED ABOVE STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05, PAGE 601.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660, CASTELLATION CRACKED BELOW STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND FUSELAGE SKIN IS DENTED BETWEEN FRAME 6305 AND 6805 AT WL 560 AND STRINGER 17. REPAIRED IAW HORIZON AIR EA 4-53-1335.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 12 INCH LONG GOUGE MARKS WITH SOME PITTING CORROSION AT FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660, CASTELLATION CRACKED ABOVE STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8805 AND STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 6305 AND STRINGER 40. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-15 PAGE 4 AND 51-10-04.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 AT AIRCRAFT CENTER LINE SPLICE, BETWEEN STRINGERS 37 AND 38, FRAME SPLICE ANGLE IS GOUGED. REPAIRED IAW FOKKER SRM 51-31-01, 53-24-04 PAGE 19 AND 51-10-05.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 AT STRINGER 35, CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 34. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305B AND STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305B AND STRINGER 39. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8305 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: RIVET — LOOSE (TE FLAP) · airframe 38,317 hrs · 48,678 cycles
PDX- ROW OF LOOSE RIVETS AT INBOARD EDGE OF INBOARD RIGHT HAND FLAP. REPAIRED IAW HORIZON AIR EA 4-57-464.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16060 HAS A CASTELLATION CRACKED AT STRINGER 35 AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 35. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 6805 AND STRINGER 16. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 8805 AND STRINGER 31. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305B AND STRINGER 36. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS SCRATCHES AND CORROSION PITS INSIDE CHANNEL BETWEEN FRAME 11905 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- THERE IS A CRACK IN CONNECTION ANGLE BETWEEN THE AFT PRESSURE BULKHEAD AND LAV FLOORBEAM AT APPROXIMATELY AT BL 300 LT. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-30-02.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK, INSIDE CHANNEL HAS GOUGES WITH SURFACE CORROSION BETWEEN FRAME 11905 TO 12405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGES AND PITTING CORROSION BETWEEN FRAME 10346 AND 10790. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS 2 SPOTS OF CORROSION LOCATED 6 INCHES FORWARD OF STATION 5805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION AT FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS CORROSION INBOARD CORNER OF CHANNEL AFT SIDE OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK HAS A GOUGE WITH CORROSION ON TOP SURFACE OF CHANNEL AT FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-01, PAGE 201-206.
Part: SEAT TRACK — GOUGED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK HAS GOUGES INSIDE CHANNEL THAT HAVE CORROSION BETWEEN FRAME 10966 TO 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK, INBOARD FLANGE HAS FRETTING CORROSION BETWEEN FRAMES 6305 AND 8305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION FROM FRAME 9305C TO SPLICE JUST FORWARD OF 9805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE AFT OF FRAME 8805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS 2 INCH LONG GOUGE MARKS WITH PITTING CORROSION BETWEEN FRAME 5805 AND 6305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE AT FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16060 HAS A CASTELLATION CRACKED AT STRINGER 32 AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 10346 AND STRINGER 32. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305B AND STRINGER 56. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS CORROSION AT INBOARD CORNER OF CHANNEL BETWEEN 8805 AND 9305 FRAME. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: STRINGER — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 29 IS CHAFING AGAINST FRAME 16660, HERE IT PASSES THROUGH THE FRAME. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK OUTBOARD FLANGE HAS FRETTING CORROSION 8 INCHES LONG, STARTING AT THE AFT SIDE OF FRAME 5805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND CABIN SEAT TRACK INSIDE CHANNEL HAS CORROSION PITS JUST FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK INSIDE CHANNEL HAS 4 SPOTS OF CORROSION 3 INCHES TO 6 INCHES FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK HAS GOUGES WITH CORROSION AT FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE BETWEEN FRAME 9805 AND 10346. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305C AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13 PAGE 4 AND 51-10-4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE AT FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION FORWARD OF FRAME 10346. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: BEAM — CRACKED (BULKHEAD) · airframe 38,317 hrs · 48,678 cycles
PDX- REAR PRESSURE BULKHEAD BEAM THREE HAS TWO .5 INCH CRACKS ON THE LOWER FLANGE IN THE BEAM RADIUS AT APPROXIMATELY BL 0. REPAIRED IAW FOKKER SRM 53-02-18 PAGE 33 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 CASTELLATION BETWEEN STRINGERS 29 AND 30 HAS FOUR CRACKED DIMPLED HOLES. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-05 AND 51-10-06.
Part: ANGLE — CRACKED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- THERE IS A CRACK IN A CONNECTION ANGLE BETWEEN THE AFT PRESSURE BULKHEAD AND LAV FLOORBEAM AT APPROXIMATELY BL 300 RT. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 51-11-01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FUSELAGE SKIN UNDER VHF COMM LOWER FORWARD ANTENNA GROOVED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6 AND 53-01-01 PAGE 3.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 33 BETWEEN FRAME 16660 AND 17065 HAS SIX RIVETS PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BRACKET — CORRODED (MLG) · airframe 38,317 hrs · 48,678 cycles
PDX- PITTING CORROSION ON RIGHT HAND MAIN LANDING GEAR SIDE STAY BRACKET. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 57-01-01 PAGE 3.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 7805 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305A AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: WASHER — MISSING (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660, BUCKTAIL WASHERS ARE MISSING AT MOST FRAME TO STRINGER ATTACH RIVET LOCATIONS. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-10-05.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 7805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON FUSELAGE SKIN UNDER LOWER ATC ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04 AND 53-01-01 PAGE 6.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS PITTING CORROSION AT FRAME 12405. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FUSELAGE SKIN UNDER VHF COMM FORWARD LOWER ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 & 6 AND 51-10-4 PAGE 9.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- AT STRINGER 33 AND FRAME 16660 CASTELLATION APPEARS TO BE CRACKED AND IS MISSING A WASHER. REPAIRED IAW FOKKER SRM 53-02-13.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305A AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 AND 51-31-01 PAGE 13.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE AT FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK HAS FRETTING CORROSION ON BOTH FLANGE BETWEEN FRAME 11405 TO 12405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 32 AND FRAME 16660 CASTELLATION IS CRACKED AT STRINGER. REPAIRED IAW FOKKER SRM 53-02-13.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 9305 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 7805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-31-01 PAGE 13 AND 51-10-04.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 26 BETWEEN FRAMES 16060 AND 16660 HAS TEN RIVETS TOENAILED OR PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BRACKET — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 AT STRINGER 32 CAMLOCK RECEPTICAL BRACKET IS CHAFED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 6 AND 51-10-04.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73E FASTENER HOLES AT INBOARD AND OUTBOARD ENDS HAVE FRETTING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73G FASTENER HOLES AT INBOARD AND OUTBOARD ENDS HAVE FRETTING. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 57-63-02 FIGURE 1.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK , INSIDE CHANNEL HAS GOUGES WITH PITTING CORROSION FROM FRAME 9305C TO 9805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 AND STRINGER 27, FRAME INBOARD SURFACE CHAFED LBL 47. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION AT FRAME 7805 AND FORWARD OF 7805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 29 BETWEEN FRAMES 16060 AND 16660 HAS 1 RIVIT PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 25 BETWEEN FRAMES 16060 AND 16660 HAS FIFTEEN RIVETS TOENAILED OR PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SHIM — MISINSTALLED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- TAPERED SHIM OVERLAPS REPAIR STRAP ON INSIDE OF FUSELAGE SKIN UNDER STRINGER 29 BETWEEN FRAMES 16060 AND 16660. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-10-05.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS PITTING CORROSION 5 INCHES AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 27 BETWEEN FRAME 16060 AND 16660, ONE RIVET HAS INSUFFICIENT BUCKTAIL AND ONE RIVET PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73A, MOST OF FASTENER HOLES HAVE VARYING DEGREES OF FRETTING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 58 BETWEEN FRAME 16060 AND 16660 HAS FIVE TOENAILED BUCKTAILS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION ON BOTH FLANGES FROM FRAME 10346 TO 12405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS TWO LONG GOUGE MARKS WITH PITTING CORROSION FROM STATION 5805 - 6305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-40-01.
Part: ACCESS PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- FUEL PANEL 73A APERTURE HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.
Part: STRUCTURE — CORRODED (COCKPIT FLOOR) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON FLOOR STRUCTURE BENEATH PILOTS INBOARD SEAT. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 BETWEEN STRINGERS 32 AND 39 INBOARD SURFACE OF FRAME CHAFED. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, AND SRM 51-10-4.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73D, MAJORITY OF FASTENER HOLES HAVE FRETTING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — GOUGED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS TWO 10 INCH LONG GOUGES AT STATION 7805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND FUEL PANEL 73C SEVERAL HOLES ON INBOARD AND OUTBOARD ENDS HAVE FRETTING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION AROUND A CAMLOCK RECEPTICLE ON THE INBOARD FLANGE AT STATION 12531. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73B SEVERAL HOLES HAVE EVIDENCE OF FRETTING AROUND ALL SIDES OF PANEL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: FRAME — CHAFED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FRAME 16660 BETWEEN STRINGERS 28 AND 29 CAMLOCK RECEPTICAL BRACKET CHAFED. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, AND SRM 51-10-04.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 31 BETWEEN FRAMES 16060 AND 16660 HAS RIVETS PANCAKED AND 1 RIVET TOENAILED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FASTENER — DAMAGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- BETWEEN STRINGER 26 AND 27, AND BETWEEN FRAMES 16060 AND 16660, SIX RIVETS PANCAKED AND ONE RIVET UNDERSHOT. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS AREAS WITH BARE/EXPOSED METAL WITH SURFACE CORROSION INSIDE CHANNEL AND FLANGE BETWEEN FRAME 11905 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON FLOOR STRUCTURE BENEATH PILOTS OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 73H, FEW OF FASTENER HOLES HAVE FRETTING AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD CABIN SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE BETWEEN FRAME 12405 AND 14755. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: PANEL — CORRODED (LT WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND WING FUEL PANEL 71A, FEW FASTENER HOLES AT INBOARD AND OUTBOARD ENDS FRETTING AROUND HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: FASTENER — DAMAGED (STRINGER) · airframe 38,317 hrs · 48,678 cycles
PDX- STRINGER 30 BETWEEN FRAMES 16060 AND 16660 HAS RIVETS PANCAKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74C APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74F APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD CABIN SEAT TRACK, INSIDE CHANNEL HAS PITTING CORROSION AFT OF FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGES WITH PITTING CORROSION FROM FRAME 9305A TO 9305B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 72A APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74E APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: FLANGE — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- FLANGE ON AUXILIARY STRUCTURE/BEAM IS CRACKED AT AFT FLANGE LOCATED AT FRAME 5305 AND STRINGER 18. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-11-04.
Part: CLIP — CRACKED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- AFT CARGO PIT AT FRAME 13815B AT STRINGER NR 2 FRAME CLIP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74G APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGES WITH PITTING CORROSION AT FRAME 9305A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK INSIDE CHANNEL HAS A 2 INCH AREA WITH SPOTS OF CORROSION LOCATED 6 INCHES AFT OF STATION 9305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74D APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: SKIN — WORN (EMERGENCY DOOR) · airframe 38,317 hrs · 48,678 cycles
PDX- EMERGENCY DOOR HAS SEVERAL SCRATCHES THAT ARE THRU THE PAINT AND INTO THE METAL ON OUTER SKIN. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 52-01-01, PAGE 6.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74A APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- RUST UNDER NUT PLATE LOCATED AT FRAME 6805 BETWEEN STRINGERS 35 AND 36. REPAIRED IAW FOKKER SRM 51-31-01.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74H APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK HAS AREAS OF BARE/EXPOSED METAL WITH SURFACE CORROSION INSIDE CHANNEL AND ON FLANGES BETWEEN FRAME 13815 AND 15205. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74B APERTURE. REPAIRED IAW FOKKER SRM 51-10-4, AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK HAS FRETTING CORROSION ON BOTH FLANGES BETWEEN FRAME 7305 AND 8305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: BEAM — GOUGED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- GOUGE IN TOP BOX BEAM OF LEFT HAND AFT OVERWING EMERGENCY EXIT LOCATED 7.5 INCHES AFT OF FORWARD EDGE OF BEAM. REPAIRED IAW FOKKER SRM 51-10-04 AND 53-01-01.
Part: SEAT TRACK — GOUGED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND CABIN SEAT TRACK, INSIDE CHANNEL HAS GOUGES WITH CORROSION BETWEEN FRAME 13345 - 13815B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS CORROSION BETWEEN FRAME 8305 AND 8805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5305 AND STRINGER 16. REPAIRED IAW FOKKER SRM 51-31-01, 51-31-05, AND 51-11-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND OUTBOARD SEAT TRACK HAS TWO GOUGES WITH PITTING CORROSION 6 INCHES FORWARD OF STATION 8805. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-01.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5805 AND STRINGER 35. REPAIRED IAW FOKKER SRM 51-10-4, 51-51-01 AND 53-02-13 PAGE 4.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74D. REPAIRED IAW FOKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74F. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74E. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5805 AND STRINGER 34. REPAIRED IAW FOKKER SRM 51-10-04, 51-31-01 AND 53-02-13 PAGE 4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGE WITH CORROSION BETWEEN FRAME 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-10, PAGE 201-206.
Part: STRUT — CORRODED (ENGINE MOUNT) · airframe 38,317 hrs · 48,678 cycles
PDX- ENGINE STRUT HAS AREAS OF EXPOSED BARE METAL THAT ARE STARTING TO RUST. REPAIRED IAW FOKKER SRM 51-10-04.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74H. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74C. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74G. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,317 hrs · 48,678 cycles
PDX- CORROSION ON FUSELAGE SKIN UNDER REAR RADIO ALTIMETER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- LEFT HAND INBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGES WITH CORROSION FROM FRAME 14285 TO 15205. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 53-40-10, PAGE 201-206.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 72A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-10-4, 51-31-01 AND 53-02-13 FIG 4.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,317 hrs · 48,678 cycles
PDX- RIGHT HAND OUTBOARD SEAT TRACK, INSIDE CHANNEL HAS GOUGE WITH PITTING CORROSION BETWEEN FRAME 5805 AND 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-40-1, PAGE 205.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5805 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-10-04, 51-31-01 AND 53-02-13 FIG 2.
Part: CLIP — CRACKED (FRAME) · airframe 38,317 hrs · 48,678 cycles
PDX- CRACKED CLIP AT FRAME 5805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 51-10-04, 51-31-01 AND 53-02-13 PAGE 4.
Part: PANEL — CORRODED (WING) · airframe 38,317 hrs · 48,678 cycles
PDX- LIGHT CORROSION AT FASTENER HOLES ON PANEL 74A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SRM 57-01-01, PAGE 5.
Part: STRINGER CLIP — CRACKED (CARGO BAY) · airframe 38,317 hrs · 48,678 cycles
PDX- AFT CARGO PIT AT FRAME 13815B AND STRINGER 2 HAS A CRACKED CLIP. REPAIRED IAW FOKKER SRM 51-31-05 PAGE 8 AND 51-31-01 PAGE 13.
Part: SIGN — INOPERATIVE (CABIN) · airframe 38,277 hrs · 48,635 cycles
SEA- EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INTERMITTANT. REPLACED EXIT SIGN, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 38,241 hrs · 48,580 cycles
PDX- OVERHEAD EXIT LIGHT ROW 8 IS OUT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CIRCUIT BOARD AT ROW 8. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 37,921 hrs · 48,294 cycles
GEG - EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED CIRCIUT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: COFFEEMAKER — INOPERATIVE (GALLEY) · airframe 37,533 hrs · 47,916 cycles
BOI- NR 1 COFFEE WARMER CIRCUIT BREAKER POPPED. FLIGHT ATTENDANT REPORTED SEEING SPARKS BEHIND HOT WATER-MAPCO. REPLACED MAPCO WATER HEATER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — MALFUNCTIONED (CABIN) · airframe 37,467 hrs · 47,862 cycles
GEG- ROW 8 EMERGENCY SIGN HAS INOPERATIVE BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RECEPTACLE — FAILED (GALLEY) · airframe 37,073 hrs · 47,468 cycles
GEG- UPPER MAPCO SMELLS LIKE AMONNIA WHEN TURNED ON. REMOVED AND REPLACED COFFEE WARMER RECEPTICLE THAT WAS BURNT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LENS — MISSING (ROW 9)
GEG - THE EXIT LIGHT 2 SEAT 9, ROW B WAS REPORTED TO HAVE MISSING LENSE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — LOOSE (SEAT 8)
SEA- PLASTIC EXIT SIGN CAME OFF AT SEAT 8A. REPLACED EXIT SIGN, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN)
GEG - FORWARD AND AFT FACING OVERHEAD EXIT SIGNS FOUND TO HAVE INOPERATIVE LIGHTING. REMOVED AND REPLACED BOTH CIRCUIT BOARDS. OPERATIONAL CHECKS GOOD.
Part: UNKNOWN — ODOR (COCKPIT)
SEA - ELECTRICAL ODOR IN FLIGHT COMPARTMENT. FOUND UPON DEACTIVATION OF RADAR UNIT, ODOR DISSIPATED. DEFERED SYSTEM, SAFTIED CURCUIT BREAKERS. AIRCRAFT RETURNED TO SERVICE.
1999
Part: CIRCUIT BOARD — FAILED (SIGN)
BOI- FORWARD OVERHEAD EMERGENCY SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOP (ROW 8)
GEG - ROW 8 AISLE EMERGENCY SIGN, SOME LIGHTS INOPERATIVE. REPLACED LAMP BOARD. CHECKS GOOD ALL MODES. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — MISSING (RT EMER EXIT)
PDX- EMERGENCY EXIT SIGN MISSING BETWEEN RIGHT HAND OVERWING EXITS. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD.
Part: SIGN — INOPERATIVE (CABIN)
GEG- EXIT SIGN AT CABIN ENTRANCE INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK OF EMERGENCY LIGHTS ARE NORMAL.
Part: RIVET — FAILED (BS 1600)
PDX - RIVET HEAD PARTIALLY MISSING ON FORWARD LEFT-HAND FUSELAGE SKIN AT FRAME/STATION 1600, STRINGERS 16 AND 17. REPAIRED IAW FOKKER SRM 51-31-01.
Part: PANEL — TORN (LT ELEVATOR)
PDX - LEFT-HAND ELEVATOR HINGE PANEL 53K HAS BEEN TORN AT 2 PLACES DUE TO PANEL 53AB CONTACTING IT WHEN ROTATING ELEVATOR THOUGH TRAVEL RANGE. REPAIRED IAW HORIZON AIR EA 4-27-72.
Part: FRAME — CORRODED (FRAME 14755)
PDX - AFT CARGO PIT CORROSION UNDER 6 NUT PLATES ON FRAME 14755 BETWEEN STRINGERS 3 AND 74. REPAIRED IAW FOKKER SRM 53-02-12, PARAGRAPH 2, PAGE 7.
Part: CASTELLATION — CRACKED (FRAME 50-2)
PDX - REAR FUSELAGE FRAME 50-2 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-10-05 PAGE 601, SRM 51-31-01 PAGE 17 AND SRM 51-30-02.
Part: FRAME — CORRODED (FRAME 9305)
PDX - FORWARD CARGO PIT FRAME 9305 BETWEEN STRINGERS 74-1-2 HAS EXFOLIATION UNDER TOP FLANGE AROUND NUT PLATES. REPAIRED IAW FOKKER 53-02-12 PAGE 9, FIGURE 3.
Part: CASTELLATION — CRACKED (FRAME 198.32)
PDX - REAR FUSELAGE UPPER SHORT FRAME 198.32 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-669.
Part: CASTELLATION — CRACKED (FRAME 19976)
PDX - REAR FUSELAGE UPPER SHORT FRAME19976 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKKER SRM 53-10-2, PAGE 601.
Part: CASTELLATION — CRACKED (FRAME 32-2)
PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION HAS BEEN STOP DRILLED THREE TIMES AND EXCEEDS LIMITATIONS AT STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 4.
Part: SKIN — CRACKED (NACELLE)
PDX - INSIDE PANEL 02C, AT THE OUTBOARD SIDE THE 7TH STAGE BLEED AIR NACELLE FLANGE AREA IS CRACKED FROM SEVERAL RIVET HEADS ALONG THE FORWARD EDGE. REPAIRED IAW FOKKER SRM 54-14-01, PAGE 405 AND SRM 54-02-01, PAGE 4, FIGURE 3.
Part: CASTELLATION — CRACKED (FRAME 32-2)
PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6, FIGURE 4 AND MM 53-10-05 PAGE 601A.
Part: CASTELLATION — CRACKED (FRAME 20075)
PDX - REAR FUSELAGE UPPER SHORT FRAME 20075 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05, PAGE 601.
Part: CASTELLATION — CRACKED (FRAME 32-2)
PDX - REAR FUSELAGE FRAME 32-2 FORWARD SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 7. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5 FIGURE 3.
Part: CHANNEL — CRACKED (BS 1700)
PDX - PANEL 92L UPPER MOUNTING Z CHANNEL HAS 5 CRACKS THROUGHOUT LENGTH OF CHANNEL, STATION 1700 RT BETWEEN FRAMES 9805 AND 11905. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01.
Part: CASTELLATION — CRACKED (FRAME 32-2)
PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 4.
Part: CASTELLATION — CRACKED (FRAME 17565)
PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 13. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601.
Part: BULKHEAD BEAM — MISREPAIRED (AFT PRESS BLKHD)
PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XI BETWEEN BL1050R AND BL425R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 51-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677.
Part: BULKHEAD BEAM — MISREPAIRED (AFT PRESS BLKHD)
PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XI BL425L DOES NOT CONFORM TO SRM REPAIR SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677.
Part: FLOOR — DAMAGED (CABIN)
PDX - FLOOR PANEL 94AK HAD CORE DAMAGE ALONG EDGES AND SKIN PUNCTURE. FABRICATED A NEW PANEL IAW HORIZON AIR EA 4-53-666.
Part: FLOOR — DAMAGED (CABIN)
PDX - FLOOR PANEL 94AJ CORNER DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-672.
Part: BULKHEAD BEAM — MISREPAIRED (AFT PRESS BLKHD)
PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM X AT BL1050R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 3 AND HORIZON AIR EA 4-53-677.
Part: BEARING — LOOSE (SPEED BRAKES)
PDX - SPEED BRAKE AIRFRAME CONNECTION LINK PIVOT POINT, UPPER AND LOWER BEARINGS ON LEFT-HAND AND RIGHT-HAND SIDES ARE LOOSE IN HOUSINGS. REPAIRED IAW HORIZON AIR EA 4-53-652.
Part: BULKHEAD SUPPORT — MISREPAIRED (FWD PRESS BLKHD)
PDX - REPAIR LOCATED BETWEEN SUPPORTS III AND IV AT THE FORWARD PRESSURE BULKHEAD RIGHT SIDE DOES NOT CONFORM TO SRM 53-02-18 PAGE 41-46. REPAIRED IAW HORIZON AIR EA 4-53-673.
Part: BEAM — CHAFED (FRAME 17565)
PDX - RIGHT-HAND APU ENCLOSURE HAD BEEN CHAFING ON LATERAL BEAM AT FRAME 17565. REPAIRED IAW HORIZON AIR EA 4-53-676.
Part: SKIN — CORRODED (FUSELAGE)
PDX - LOWER ATC ANTENNA/FUSELAGE MOUNT AREA HAS SURFACE CORROSION AND LIGHT PITTING ON FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-01, PAGE 8 FIGURE 6.
Part: BULKHEAD BEAM — MISREPAIRED (AFT PRESS BLKHD)
PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XII OUTBOARD OF BL425R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677.
Part: FLOOR — DAMAGED (CABIN)
PDX - FLOOR PANEL 94AM CORE DAMAGED ALONG EDGES, LOWER SKIN PUNCTURE. REPAIRED IAW HORIZON AIR EA 4-53-666.
Part: SKIN — CHAFED (TE FLAP VANE)
PDX - OUTBOARD FLAP VANE UPPER SURFACE SKIN INBOARD END DENTED AT ROLLER CHAFE PAD. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN LOWER FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21E.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - RIGHT-HAND AFT OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21E.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - LEFT-HAND AFT OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21E.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN TOP AFT CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON EO 4-52-21E.
Part: CASTELLATION — CRACKED (FRAME 17565)
PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 3, FIGURE 3 AND MM 53-10-05, PAGE 601.
Part: SKIN — DENTED (EMER EXIT DOOR)
PDX - RIGHT-HAND FORWARD EMERGENCY DOOR EXIT HAS A DENT 6 INCHES BELOW WINDOW PANEL IN OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE RADIUS. REPAIRED IAW HORIZON AIR EA 4-52-21 E.
Part: BULKHEAD WEB — CRACKED (FWD PRESS BLKHD)
PDX - FRONT PRESSURE BULKHEAD WEB HAS CRACK AT THE VII BEAM AT BL100L. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 14.
Part: FRAME — CRACKED (EMER EXIT DOOR)
PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN LOWER AFT CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21 E.
Part: CASTELLATION — CRACKED (FRAME 41-2)
PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 FIGURE 4 AND MM 53-10-05, PAGE 601.
Part: SEAT TRACK — GOUGED (FRAME 14285)
PDX - THERE IS A GOUGE IN THE LEFT INBOARD SEAT TRACK JUST FORWARD OF FRAME 14285. REPAIRED IAW HORIZON AIR EA 4-53-564.
Part: SEAT TRACK — WORN (FRAME 10790)
PDX - THERE IS A CIRCULAR GROOVE WORN INTO INBOARD FLOOR SUPPORT FLANGE OF THE LEFT INBOARD SEAT TRACK, JUST FORWARD OF FRAME 10790. REPAIRED IAW HORIZON AIR EA 4-53-675.
Part: CASTELLATION — CRACKED (FRAME 17565)
PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION HAS A PIECE MISSING AND A CRACK AT STRINGER 10. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601.
Part: RAIL — CORRODED (PEDESTAL)
PDX - LEFT-HAND AND RIGHT-HAND SIDES OF PEDESTAL HAVE CORROSION ON THE BOTTOM SIDE OF THE LOWER RAILS AND AT THE MOUNT BOLT HOLES FROM THE CENTER MOUNT BOLTS AFT. REPAIRED IAW HORIZON AIR EA 4-53-649.
Part: SUPPORT — CORRODED (FRAME 14755)
PDX - THERE IS A AREA OF LIGHT FRETTING CORROSION ALONG THE INBOARD EDGE OF FLOOR SUPPORT FLANGE ON THE LEFT-HAND INBOARD SEAT TRACK, JUST AFT OF FRAME 14755. REPAIRED IAW HORIZON AIR EA 4-53-658.
Part: CASTELLATION — CRACKED (FRAME 41-2)
PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT RIVET NEAR STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6 FIGURE 4 AND MM 53-10-05 PAGE 601.
Part: SKIN — DAMAGED (EMER EXIT DRWAY)
PDX - SERVICE EMERGENCY DOOR APERTURE LOWER FORWARD CORNER REQUIRES DOUBLER MOD. COMPLIED WITH HORIZON AIR EA 4-53-593.
Part: SKIN — CRACKED (FUSELAGE)
PDX - .25 INCH CRACK AT BELLY CENTER TUNNEL LEFT-HAND WALL CUTOUT FOR Z STRINGER 2.02 AT BL 225 LT. REPAIRED IAW HORIZON AIR EA 4-53-638, STEPS 3 THROUGH 6.
Part: CASTELLATION — CRACKED (FRAME 17565)
PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601.
Part: CASTELLATION — MISREPAIRED (FRAME 50-2)
PDX - REAR FUSELAGE FRAME 50-2 FORWARD SIDE FRAME CASTELLATION STOP DRILL REPAIR IS DRILLED INTO STRINGER AT STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6 FIGURE 4 AND MM 53-10-05, PAGE 601.
Part: CASTELLATION — CRACKED (FRAME 41-2)
PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED AND STOP DRILLED BEYOND LIMITATIONS AT STRINGER 30. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7.
Part: SEAT TRACK — CORRODED (FRAME 6805-7305)
PDX - THERE ARE TWO AREAS OF LIGHT TO MODERATE CORROSION IN CHANNEL OF RIGHT-HAND INBOARD SEAT TRACK BETWEEN FRAME 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C.
Part: SUPPORT LINK — WORN (RT SPEED BRAKE)
PDX - RIGHT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD HAS APPROXIMATELY .050 RADIAL PLAY AT SUPPORT LINK. REPAIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108.
Part: BEARING — WORN (LT SPEED BRAKE)
PDX - LEFT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD AFT BEARING HAS APPROXIMATELY .030 RADIAL PLAY. REPAIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108.
Part: SEAT TRACK — CORRODED (FRAME 7305-8305)
PDX - THERE ARE THREE AREAS OF LIGHT TO MODERATE CORROSION IN CHANNEL OF RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 7305 AND 8305. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6.
Part: SUPPORT — CRACKED (FUSELAGE FAIRING)
PDX - 91J FAIRING SUPPORT ON FUSELAGE HAS APPROXIMATELY 10 INCH CRACK AT FORWARD CURVED SECTION JUST FORWARD OF NUT PLATES. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-03.
Part: SEAT TRACK — CORRODED (FRAME 9305)
PDX - THERE IS A SMALL AREA WITH PITTING CORROSION IN RIGHT INBOARD SEAT TRACK, JUST AFT OF FRAME 9305A. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6.
Part: CASTELLATION — CRACKED (FRAME 50-2)
PDX - REAR FUSELAGE FRAME 50-2 AFT SIDE FRAME CASTELLATION IS CRACKED BEYOND LIMITATION AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, REPAIR SCHEME 2.
Part: SEAT TRACK — CORRODED (FRAME 8305-9305)
PDX - THERE ARE THREE AREAS WITH LIGHT PITTING CORROSION INSIDE CHANNEL OF RIGHT INBOARD SEAT TRACK BETWEEN FRAME 8305 AND 9305. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6.
Part: SKIN — CRACKED (FUSELAGE)
PDX - .5 INCH CRACK AT BELLY CENTER TUNNEL LEFT-HAND WALL CUTOUT FOR Z STRINGER 2.01 AT BL 225 LT. REPAIRED IAW HORIZON AIR EA 4-53-638.
Part: CLIP — CRACKED (FRAME 13815)
PDX - FRAME CLIP IN AFT PIT FRAME 13815B AND STRINGER 2 IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BRACKET — LOOSE (CARGO DOOR)
PDX - FORWARD PIT AFT DOOR SUPPORT ROD FUSELAGE BRACKET LOOSE AND PREVIOUS REPAIR UNDER BRACKET APPEARS BENT AND BUCKLED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.
Part: FRAME — CORRODED (FRAME 13815)
PDX - AFT CARGO PIT FRAME 13815B AT STRINGER 74 UNDER TOP LIP OF CHANNEL FRAME HAS EXFOLIATION CORROSION UNDER NUT PLATE. REPAIRED IAW HORIZON AIR EA 4-53-644.
Part: CLIP — CRACKED (FRAME 13815)
PDX - AFT CARGO PIT CRACKED CLIP ON FRAME 13815A AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1 AND SRM 53-02-13, FIGURE 3.
Part: CLIP — CRACKED (FRAME 13815)
PDX - AFT CARGO PIT CRACKED CLIP ON FRAME 13815A AT STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4.
Part: RIB — CRACKED (WING)
PDX - RIB NR 6 HAS A CRACK APPROXIMATELY .25 INCH LENGTH. REPAIRED IAW FOKKER SRM 51-31-05.
Part: NOZZLE — CRACKED (ENGINE EXHAUST)
PDX - THE PROPELLING NOZZLE AT SUPPORT HAS A CRACK ON THE OUTBOARD LEG. REPAIRED IAW HORIZON AIR EA 4-78-011.
Part: HINGE — CORRODED (LT MLG DOOR)
PDX - LEFT-HAND MAIN LANDING GEAR DOOR HINGE ATTACH AREA ALONG LEFT-HAND KEEL BEAM HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-650.
Part: HINGE — CORRODED (LT MLG DOOR)
PDX - LEFT-HAND MAIN LANDING GEAR DOOR HINGE ATTACH AREA ALONG LEFT-HAND KEEL BEAM HAS PITTING CORROSION AT FORWARD CORNER. REPAIRED IAW HORIZON AIR EA 4-53-650.
Part: SKIN — CRACKED (WING)
PDX - WING REPAIR FOR ACCESS PANEL 72A HAS A CRACK RADIATING FROM A SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-203.
Part: KEEL BEAM — CORRODED (RT MLG WW)
PDX - MINOR PITTING CORROSION ON KEEL BEAM LOCATED ON FORWARD AND AFT END OF MAIN LANDING GEAR DOOR HINGE ATTACH POINT, RIGHT-HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-53-647.
Part: NOZZLE — CRACKED (RT ENG EXHAUST)
PDX - THE RIGHT ENGINE EXHAUST PROPELLING NOZZLE HAS A CRACK AT INBOARD AND UPPER CENTER LOBE SUPPORT. REPAIRED IAW HORIZON AIR EA 4-78-010.
Part: FITTING — DAMAGED (RT WING/FUS)
PDX - RIGHT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (2) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RADIUS OF CASTING. REPAIRED IAW FOKKER SRM 51-10-4.
Part: STRINGER — CRACKED (FRAME 3870-4175)
PDX - A 3 TO 4 INCH CRACK BETWEEN RIVETS ON STRINGER 69 BETWEEN FRAMES 3870 AND 4175. REPAIRED IAW FOKKER SRM 53-02-02 AND SRM 51-31-01.
Part: SUPPORT — CORRODED (FRAME 6305)
PDX - THERE IS A FRETTING CORROSION ON INBOARD FLOOR SUPPORT FLANGE ON LEFT-HAND INBOARD SEAT TRACK AT FRAME 6305. REPAIRED IAW HORIZON AIR EA 4-53-657.
Part: STRINGER — CRACKED (BS 3820-4150)
PDX - STRINGER 68A CRACKED BETWEEN STATION 3820 AND 4150. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 3 AND SRM 51-31-01.
Part: SKIN — DAMAGED (PAX DOORWAY)
PDX - PASSENGER DOOR APERTURE DENTED AND CHAFED IN AREA ADJACENT TO THE CURVED LEVER AND FRICTION DISC ASSEMBLY WHEN THE DOOR IS IN THE OPEN POSITION. REPAIRED IAW HORIZON AIR EA 4-53-656.
Part: FLANGE — MISDRILLED (EMER EXIT DOOR)
PDX - RIGHT-HAND AFT OVERWING EMERGENCY EXIT UPPER TORSION BOX TOP FLANGE HAS DOUBLE DRILLED RIVET HOLE. REPAIRED IAW HORIZON AIR EA 4-53-655.
Part: SEAT TRACK — CORRODED (FRAME12875-13345)
PDX - THERE IS LIGHT PITTING CORROSION ON THE INBOARD FLOOR SUPPORT FLANGE OF THE LEFT-HAND INBOARD SEAT TRACK BETWEEN FRAMES 12875 AND 13345. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.
Part: FITTING — DAMAGED (LT WING/FUS)
PDX - LEFT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (3) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RADIUS OF CASING. REPAIRED IAW FOKKER SRM 51-10-4.
Part: CLIP — CORRODED (FRAME 7805)
PDX - FORWARD PIT FRAME 7805 CLIPS BETWEEN STRINGERS 74 AND 72 HAS LIGHT SURFACE CORROSION, PAINT MISSING OR BUBBLY. REPAIRED IAW FOKKER SRM 51-10-04.
Part: CLIP — CORRODED (FRAME 8305)
PDX - FORWARD PIT FRAME 8305 CLIP BETWEEN STRINGERS 2 AND 72 HAVE LIGHT CORROSION AND MISSING PAINT. REPAIRED IAW FOKKER SRM 51-10-04.
Part: LEVER — WORN (RUDDER)
PDX - TOP AND MID RUDDER DAMPER LEVER ASSEMBLIES WORN. REMOVED AND REPLACED TOP AND MID RUDDER DAMPER LEVER ASSEMBLIES.
Part: CLIP — CORRODED (FRAME 8805)
PDX - FORWARD CARGO PIT FRAME 8805 CLIPS BETWEEN STRINGERS 1 AND 72 HAVE MISSING PAINT AND LIGHT CORROSION. REPAIRED IAW FOKKER SRM 51-10-04.
Part: RUDDER PEDAL — CORRODED (LT & RT COCKPIT)
PDX - CORROSION AT THE BASE OF PILOTS AND CO-PILOTS RUDDER PEDAL ASSEMBLY. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8, PARAGRAPH 3A.
Part: RIVETS — MISINSTALLED (FRAME 12875)
PDX - FRAME 12875 CLIP REPAIR AT STRINGER R29 HAS 2 RIVETS THAT DO NOT FILL THE HOLES AT CLIP TO CASTILLATION. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-30-02.
Part: SKIN — DAMAGED (LT SPEED BRAKE)
PDX - LEFT-HAND SPEED BRAKE HAS SEVERAL RIVETS PULLING THROUGH SKIN ON BACK MIDDLE FRAME. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 53-02-01, PAGE 11 FIGURE 9.
Part: SKIN — DAMAGED (COCKPIT)
PDX - COCKPIT ROOF FORWARD SKIN PANEL ABOVE PILOT AND CO-PILOT WINDSHIELDS HAS SIGNIFICANT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01.
Part: RIVET — LOOSE (RT SPEED BRAKE)
PDX - RIGHT-HAND SPEED BRAKE HAS THREE LOOSE RIVETS JUST BELOW SKID PLATE. REPAIRED IAW FOKKER SRM 51-31-05.
Part: RIVETS — MISINSTALLED (FRAME 12875)
PDX - FRAME 12875 CLIP REPAIRED AT STRINGER 28 HAS 2 RIVETS WITH IMPROPER BUCKED TAILS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 29A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.
Part: SEAT TRACK — GOUGED (FRAME 12875)
PDX - THERE ARE THREE AREAS WITH LIGHT GOUGES IN CHANNEL LIP ON THE LEFT OUTBOARD SEAT TRACK, BETWEEN FRAME 12875 AND 13815. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH B AND C.
Part: SUPPORT — CORRODED (FRAME 10966)
PDX - THERE ARE TWO AREAS WITH LIGHT CORROSION ON OUTBOARD FLOOR SUPPORT FLANGE, ON LEFT-HAND OUTBOARD SEAT TRACK, JUST AFT OF FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C.
Part: SEAT TRACK — CORRODED (FRAME 10966)
PDX - THERE ARE TWO AREAS OF PITTING CORROSION ON INBOARD FLOOR SUPPORT FLANGE OF THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 10966 AND 11905. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6.
Part: CLIP — CRACKED (FRAME 16060)
PDX - CRACKED CLIP AT FRAME 16060 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-10, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CLIP — CRACKED (FRAME 16060)
PDX - CRACKED CLIP AT FRAME 16060 AND STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13, FIGURE 2.
Part: SUPPORT — CORRODED (FRAME 5805)
PDX - THERE IS LIGHT TO MODERATE PITTING CORROSION ON THE INBOARD FLOOR SUPPORT FLANGE OF THE RIGHT-HAND OUTBOARD SEAT TRACK AT FRAME 5805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH B AND C.
Part: SEAT TRACK — CORRODED (FRAME 10966)
PDX - THERE ARE THREE AREAS WITH PITTING CORROSION INSIDE CHANNEL OF RIGHT OUTBOARD SEAT TRACK, BETWEEN FRAMES 10966 AND 12875. REPAIRED IAW SRM 51-10-4, PAGES 8 AND 9, PARAGRAPH B AND C.
Part: CASTELLATION — CRACKED (FRAME 14755)
PDX - FRAME 14755 CASTELLATION CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01, FIGURE 2.
Part: CLIP — CRACKED (FRAME 13815)
PDX - AFT CARGO PIT CRACKED CLIP AT FRAME 13815B BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-12M PAGE 4.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTILLATION CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — DAMAGED (EMER EXIT DRWAY)
PDX - CRACK APPROXIMATELY 1.2 LONG ON LEFT SIDE FORWARD OVERWING EMERGENCY DOOR APERTURE AT FORWARD LOWER CORNER. REPAIRED IAW HORIZON AIR EA 4-53-633.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.
Part: BRACKET — CORRODED (AILERON PULLEY)
PDX - AILERON PULLEY CLUSTER BRACKET HAS CORROSION STARTING AT PULLEY ATTACH BOLT. REPAIRED IAW FOKKER MM 27-11-00, PAGE 602, PARAGRAPH 3C (1).
1998
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.
Part: CASTELLATION — CRACKED (FRAME 13345)
PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5 AND SRM 51-30-02.
Part: PLATE — CORRODED (FUSELAGE)
PDX - LOWER VHF COMM ANTENNA BASE PLATE HAS MINOR LIGHT SURFACE CORROSION AROUND FEED THROUGH HOLE. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: FRAME — DENTED (CARGO DOORWAY)
PDX - FORWARD CARGO DOOR APERTURE FRAME DENTED AND SLIGHTLY PROTRUDING INTO APERTURE. REPAIRED IAW FOKKER SRM 53-02-16, FIGURE 1.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12875)
PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: SKIN — CORRODED (FUSELAGE)
PDX - LIGHT SURFACE CORROSION AROUND SEVERAL NUT PLATE RIVETS OF REAR RAD ALT ANTENNA MOUNT, FORWARD BLANKING FUSELAGE SKIN CUTOUT HAS MINOR PITTING CORROSION AROUND MOUNT FLANGE. REPAIRED IAW FOKKER SRM 53-01-01.
Part: SKIN — CRACKED (FUSELAGE)
PDX - FUSELAGE SKIN CRACKED AT LOWER FORWARD CORNER OF PILOTS SLIDING WINDOW APERTURE AT NR 2 WINDOW POST. REPAIRED IAW HORIZON AIR EA 4-53-632.
Part: SKIN — CORRODED (FUSELAGE)
PDX - VHF COMM AFT LOWER ANTENNA/FUSELAGE SKIN MOUNT AREA HAS SMALL AREA OF LIGHT SURFACE CORROSION AT AFT EDGE. REPAIRED IAW FOKKER SRM 51-10-04.
Part: SKIN — CORRODED (FUSELAGE)
PDX - NR 2 DME ANTENNA/FUSELAGE SKIN MOUNT HAS PITTING CORROSION AROUND SCREW HOLES ON SKIN. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8.
Part: SUPPORT — CRACKED (FRAME 3450-3820)
PDX - CRACKED FLOOR SUPPORT AT BL1390 RT BETWEEN FRAMES 3450 AND 3820. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7B.
Part: CASTELLATION — CRACKED (FRAME 13345)
PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 29A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.
Part: STRIP — CHAFED (WING)
PDX - .25 INCH CHAFE MARK ON FORWARD END OF LOWER CENTER TO OUTER WING JOINT STRIP. REPAIRED IAW HORIZON AIR EA 4-57-202.
Part: CASTELLATION — CRACKED (FRAME 13345)
PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13345)
PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: SKIN — MISDRILLED (WING)
PDX - HOLE DRILLED THROUGH OUTER WING TO CENTER WING BOX JOINT SPAR FORWARD END. REPAIRED IAW HORIZON AIR EA 4-57-201.
Part: FRAME — CORRODED (FRAME 6805)
PDX - EXFOLIATION CORROSION AROUND NUT PLATES ON FRAME 6805 ABOVE STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SKIN — CORRODED (FUSELAGE)
PDX - UPPER FUSELAGE UPPER NAV/COMM ANTENNA BASE PLATE ON FUSELAGE SKIN HAS PITTING CORROSION AROUND FEED THROUGH HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH B AND C.
Part: SUPPORT — LOOSE (LT WING/FUS)
PDX - LEFT-HAND WING ROOT FAIRING SUPPORT FOR 91G LOWER AFT END HAS 15 LOOSE RIVETS AND CHANNEL IS CHAFED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-02.
Part: SKIN — CORRODED (FUSELAGE)
PDX - UPPER FUSELAGE UPPER TCAS ANTENNA, FUSELAGE SKIN BASE PLATE HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH B AND C.
Part: CASTELLATION — CRACKED (FRAME 13345)
PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 49A. REPAIRED IAW FOKKER SRM 51-31-01.
Part: CASTELLATION — CRACKED (FRAME 12405)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12405)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12045)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12405)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: FRAME — CORRODED (FRAME 7305)
PDX - FORWARD CARGO COMPARTMENT FRAME 7305 IS CORRODED AT INTERSECTION WITH STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9, FIGURE 3, SRM 51-31-01 AND 51-31-05.
Part: CASTELLATION — CRACKED (FRAME 12405)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 12405)
PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1-5 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 29. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1-5 AND SRM 53-02-13, FIGURE 2.
Part: CASTALLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1-5 AND SRM 53-02-13 FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 10966)
PDX - FRAME 10966 CASTELLATION CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1-5 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 10966)
PDX - FRAME 10966 CASTELLATION IS CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 10966)
PDX - FRAME 10966 CASTELLATION IS CRACKED AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 15205)
PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 23. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: SKIN — DENTED (CARGO DOOR)
PDX - AFT CARGO DOOR HAS A SMALL DENT ON THE FORWARD EDGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 7.
Part: CASTALLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 51-31-10 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 13815)
PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 15205)
PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 15205)
PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 15205)
PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 10346)
PDX - FRAME 10346 CASTELLATION IS CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: CASTELLATION — CRACKED (FRAME 10346)
PDX - FRAME 10346 CASTELLATION IS CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: SKIN — MISSING (CARGO DOOR)
PDX - AFT CARGO DOOR OUTER SKIN, OUTER LAYER IS CRACKED/BROKEN AND MISSING 1.5 X .375 NEXT TO HINGE ON LEFT-HAND SIDE. REPAIRED IAW FOKKER SRM 52-02-01 PAGE 2, FIGURE 2 AND MM 53-00-00 PAGE 2.
Part: BULB — FAILED (ROW 8)
EMERGENCY EXIT SIGN AT ROW 8 IS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.
Part: BULB — FAILED (CABIN)
LEFT FORWARD EMERGENCY EXIT 28 VOLT LIGHT IS BURNT OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.
Part: BATTERY — DISCHARGED (CABIN)
MOST AFT (3 EACH) EVACUATION LIGHTS INOPERATIVE IN CABIN OVERHEAD. MAINTENANCE REMOVED AND REPLACED LEFT HAND EMERGENCY BATTERY PACK IN AFT LEFT HAND OVERHEAD BIN, OPERATIONAL TESTS NORMAL.
Part: BATTERY — DISCHARGED (CABIN)
EXTERIOR WING ROUTE TRAILING EDGE EMERGENCY LIGHTS INOP. REPLACED NR 8 POSITION BATTERY PACK, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT SIGN AT ROW 8 HAS SEVERAL 28V BULBS OUT. MAINTENANCE RELAMPED SIGN, OPERATIONAL TESTS NORMAL.
Part: BULB — FAILED (CABIN)
GEG - FOUND CABIN EMERGENCY EXIT LIGHTS OUT. MAINTENANCE RELAMPED. OPERATION CHECKS GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (NR 2 ENGINE)
GEG - CREW REPORTED NR 2 ENGINE FIRE WARNING IN FLIGHT. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO INDICATION OF FIRE OR OVERHEAT. FIRE WARNING FOUND TO BE AN INDICATION PROBLEM. TROUBLE SHOT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. FOUND INBOARD PIGTAIL AND OUTBOARD AFT PIGTAIL OF FIRE LOOP TO HAVE CORRODED CONNECTIONS. REMOVED AND REPLACED FIRE WARNING LOOP AND CONTROL UNIT. SYSTEM OPERATIONALLY TESTS NORMAL.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT IN ROW 9E OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.
Part: BULB — FAILED (CABIN)
CABIN EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR IS DIM. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL.
Part: CIRCUIT BOARD — FAILED (CABIN)
GEG - FORWARD AND AFT ROW 8 OVERHEAD EXIT ANNUNCIATORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOARDS AND OPERATIONALLY TESTED. TESTS NORMAL.
Part: BATTERY — DISCHARGED (CABIN)
THE EMERGENCY EVACUATION LIGHTS ON THE RIGHT ESCAPE HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK LOCATED ABOVE SEAT ROW 7. SYSTEM WAS TESTED AND OPERATED NORMAL.
Part: WIRE — FAILED (CABIN)
THE EMERGENCY EVACUATION LIGHT AT SEAT 4B WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKED WIRE AT THE LIGHT. SYSTEM TESTED NORMAL.
Part: SIGN — INOPERATIVE (CABIN)
THE FORWARD CABIN EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE SIGN AND TESTED, OPERATIONAL TESTS NORMAL.
Part: BULB — FAILED (CABIN)
OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 10. MAINTENANCE REPLACED SAME, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
OVERHEAD EMERGENCY LIGHT AT ROW 10 HAS AN INOP 28 VOLT BULB. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: CIRCUIT — MALFUNCTION (CABIN)
FORWARD EXIT SIGN ABOVE THE COCKPIT DOOR HAS INOP BULBS. REPLACED CIRCUIT CARD, OPERATIONAL CHECKS GOOD.
Part: SLIDE — MALFUNCTION (CABIN)
ESCAPE SLIDE HAS UNLASHED CORDS AND THE LANYARD IS NOT ATTACHED TO THE AIRCRAFT STRUCTURE. REPLACED SLIDE.
Part: BULB — FAILED (ROW 9A)
BOI - EMERGENCY EXIT LIGHT ON ROW 9A INOP. MAINTENANCE RELAMPED LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOOR — DAMAGED (RT EMER EXIT)
PDX - RIGHT OVERWING AFT EMERGENCY EXIT GOUGED AT UPPER TORSION BOX. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7 AND SRM 51-31-05, PAGE 9, PARAGRAPH 7.
Part: SEAT TRACK — CORRODED (FRAME 10966)
PDX - THERE ARE TWO AREAS OF LIGHT PITTING CORROSION ON THE OUTBOARD FLOOR SUPPORT FLANGE OF THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 10966 AND 11905. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9 AND PARAGRAPH B AND C.
1996
Part: SWITCH — MALFUNCTIONED (NLG)
AIR TURN BACK, NOSE GEAR GREEN DOWN LIGHT WOULD NOT GO OUT. JACKED AIRCRAFT AND CLEANED DOWNLOCK SWITCH, GEAR SWING OPS CHECKED OK. ON ARRIVAL AT PSP PM, SAME DAY SWITCH STUCK AGAIN. CAPTAIN REQUESTED TOWER CHECK AND OK. MANUAL INDICATION OK. AIRCRAFT FERRIED TO FAT. SWITCH REPLACED AND GEAR SWING CHECK OK. (M)
1995
Part: SKIN — CRACKED (STA 2422-2650)
PIT - DURING SCHEDULED STRUCTURES VISIT FOUND MULTIPLE SMALL CRACKS TOTALING 3 INCHES IN THE NOSE GEAR BAY TOP COVER STATION 2422 TO 2650. REF SIP 53-10-10 (EDDY CURRENT). STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-02-18. (Z)
Part: BULKHEAD — CRACKED (FWD PRESS)
PIT - DURING SCHEDULED STRUCTURES VISIT, FOUND 7.5 INCH CRACK IN AFT SIDE OF FORWARD PRESSURE BULKHEAD BETWEEN STA 72 AND STA 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PLATE PER SRM 53-11-00, PAGE 2. (X)