N493US

Part: SIGN — INOPERATIVE (CABIN) · airframe 45,447 hrs · 55,184 cycles

SEA ON FLIGHT 2423- EMERGENCY LIGHT NEXT TO LAVATORY SIGN HAS SOME BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,447 hrs · 55,184 cycles

SEA-ON FLT NR 2423, EMERGENCY LIGHT NEXT TO LAVATORY SIGN HAS SOME BURNED OUT BULBS. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 45,324 hrs · 55,091 cycles

PDX- MID CABIN OVERHEAD EMERGENCY EXIT SIGN FORWARD SIDE HAS NUMEROUS LIGHTS THAT DO NOT ILLUMINATE WHEN SELECTED ON. REPLACED MID CABIN EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (ZONE 700) · airframe 45,161 hrs · 54,970 cycles

BIL - ON APPROACH, THE GEAR WAS SELECTED DOWN. THE LEFT MAIN RED LIGHT REMAINED ILLUMINATED WITH NO GREEN ILLUMINATION. A GO-AROUND WAS INITIATED AND THE ABNORMAL CHECKLIST WAS PERFORMED. RESULTS WERE THE SAME. AFTER 3 MINUTES THE GEAR INDICATED GREEN AND AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT DOWNLOCK ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 45,001 hrs · 54,832 cycles

PDX- CRACK AT FASTENER ON RT SIDE OF VERTICAL STABILIZER ATTACH ANGLE. SECOND FROM THE AFT FASTENER ON THE UPPER FLANGE OF THE ATTACH ANGLE. REPAIRED IAW FOKKER SRM 51-10-4 AND 55-31-00

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 45,001 hrs · 54,838 cycles

PDX- CRACK IN RADIUS OF VERTICAL STABILIZER ATTACH ANGLE AT 32 PERCENT OF VERTICAL STABILIZER SPAR ON THE LT SIDE. REPAIRED IAW FOKKER SRM 55-31-00.

Part: RIVET — LOOSE (VERTICAL STAB) · airframe 45,001 hrs · 54,838 cycles

PDX- ON THE LT SIDE VERTICAL STABILIZER ATTACH ANGLE THE MOST AFT RIVET ON THE LOWER FLANGE OF THE ATTACH ANGLE IS LOOSE. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SIGN — INOPERATIVE (CABIN) · airframe 44,804 hrs · 54,669 cycles

PDX- EXIT SIGN ABOVE GALLEY HAS SEGMENTS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ABOVE GALLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SOCKET — DEFECTIVE (COCKPIT) · airframe 44,770 hrs · 54,636 cycles

PDX- BURNT SMELL IN COCKPIT. REMOVED AND REPLACED PILOT'S CENTER PEDESTAL. INBOARD SIDE RED LAMP SOCKET. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 44,573 hrs · 54,468 cycles

BOI-BOTH MID CABIN EXIT SIGNS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BOTH EMERGENCY EXIT SIGNS IN MID CABIN. OPERATIONAL CHECK GOOD. AORCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (ZONE 100) · airframe 44,508 hrs · 54,413 cycles

PDX-LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE.REMOVED AND REPLACED BATTERY SUPPLY PACK IN OVERHEAD BIN AT ROW 9AB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 44,199 hrs · 54,159 cycles

PDX- EXIT SIGN ABOVE COCKPIT ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (ZONE 400) · airframe 44,199 hrs · 54,158 cycles

SEA - DURING FLIGHT THE FLIGHT CONTROL HYDRAULIC QUANTITY DROPPED TO ZERO. LANDING AT SEA WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE FLIGHT CONTROL HYDRAULIC SYSTEM TO FULL. THE SYSTEM WAS PRESSURIZED FOR 45 MINUTES WITH NO LEAKS OR MIGRATION NOTED. THE # 1 HYDRAULIC SYSTEM ACCUMULATOR WAS ALSO SERVICED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 43,848 hrs · 53,864 cycles

SEA-EXIT SIGN BULB INOPERATIVE. LOCATED ON FORWARD FACING PANEL BETWEEN ROW 8 AND 9. REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 43,663 hrs · 53,707 cycles

PDX-TWO EMERGENCY LIGHTS IN CABIN CEILING REMAIN ILLUMINATED WITH POWER SELECTED OFF. REMOVED AND REPLACED LEFT HAND AFT OVERHEAD BIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,646 hrs · 53,686 cycles

SEA- AFT OVERWING EXIT SIGN HAS SEVERAL BURNED OUT BULBS. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,355 hrs · 53,438 cycles

PDX-EMERGENCY EGRESS LIGHTS AT ROW 11-14 INOP. REMOVED AND REPLACED THE CARTRIDGE BATTERY AS NEEDED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CARGO BAY) · airframe 43,351 hrs · 53,434 cycles

PDX-BOTH AFT EXTERIOR EVACUATION LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT CARGO PIT EVACUATION LIGHTS BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,328 hrs · 53,415 cycles

PDX - EXIT SIGN AT PASSENGER ENTRANCE IS INOPERATIVE. REPLACED EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — BURNED OUT (CABIN) · airframe 43,270 hrs · 53,360 cycles

PDX- CABIN FORWARD EMERGENCY EXIT SIGN HAS NUMEROUS LAMPS BURNED OUT. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CARGO BAY) · airframe 43,091 hrs · 53,211 cycles

PDX - AFT EXTERIOR FAIRING EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED AFT CARGO BATTERY POWER SUPPLY UNIT FOR EVACUATION LIGHTS. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,020 hrs · 53,140 cycles

SEA - EXIT SIGN ABOVE COCKPIT DOOR HAS SEVERAL LIGHTS INOPERABLE. REMOVED AND REPLACED SIGN ABOVE COCKPIT DOOR. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

airframe 42,479 hrs · 52,688 cycles

SEA - CREW REPORTED AND ELECTRICAL BURNING SMELL, FOLLOWED BY THE #2 GENERATOR CAUTION LIGHT ILLUMINATING. REMOVED AND REPLACED GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

airframe 42,464 hrs · 52,682 cycles

SEA - EXIT SIGN ATTACHED TO SEAT 8B REPORTED DAMAGED. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 42,240 hrs · 52,476 cycles

PDX - LIGHT BULB FOUND BURNT OUT ON NR 3 EXIT SIGN. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 42,235 hrs · 52,470 cycles

PDX - EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — CRACKED (RUDDER) · airframe 41,992 hrs · 52,219 cycles

YYC- RIB 4 THROUGH 2 HAS SMALL CRACKS AT TRAILING EDGE RUDDER. REPAIRED IAW FOKKER SRM 55-02-01 PAGE 4, 55-02-07 PAGE 3 AND 51-31-01 PAGES 13 AND 14.

Part: SUPPORT BRACKET — CRACKED (SPEEDBRAKE) · airframe 41,992 hrs · 52,219 cycles

YYC- SPEEDBRAKE UPPER HINGE SUPPORT BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1476.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- SUPPORT STRUCTURE AND FRAME 14755 CORRODED AND HAS BROKEN ANCHOR NUTS. REPAIRED IAW HORIZON AIR EA 4-53-1469.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815B AND STRINGER 72 AND 73. REPAIRED IAW FOKKER SRM 53-22-04 AND 51-31-01.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACK AT STATION 1550 AND STRINGER 72. REPAIRED IAW HORIZON AIR EA 4-53-1466.

Part: DUCT — ERODED (ACM) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND AIR CYCLE MACHINE INLET ERRODED. REPAIRED IAW FOKKER SRM 51-10-05, 51-31-01 AND 51-31-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FRAME 13815A HAS MINOR CORROSION BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-22-04.

Part: ANGLE — CORRODED (ENTRY STAIRS) · airframe 41,992 hrs · 52,219 cycles

YYC- MAIN CABIN DOOR ENTRANCE WAY SECOND STEP BOTTOM INBOARD ANGLE CORRODED. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: HINGE — WORN (SPOILER) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND NUMBER 5 LIFTDUMPER INBOARD ATTACHMENT HINGE BRACKET BOLT ANTI SPIN BASES WORN. REPAIRED IAW FOKKER SRM 27-63-01 AND HORIZON AIR EA 4-57-552.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815A AND STRINGER 73 AND 72. REPAIRED IAW FOKKER SRM 53-02-13, 53-22-04 AND 51-31-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION IN REAR CARGO PIT AT FRAME 13815B AND STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-22-04 AND 51-31-01.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51B HAS CRACKS AT OUTBOARD AND FLANGE CORNERS. REPAIRED IAW HORIZON AIR EA 4-55-287.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51C HAS CRACKS AT INBOARD AND FLANGE CORNER. REPAIRED IAW HORIZON AIR EA 4-55-287.

Part: SKIN — TORN (CARGO DOOR) · airframe 41,992 hrs · 52,219 cycles

YYC- REAR CARGO DOOR INSIDE SKIN TORN BY BOTTOM MID SECTION ALONG RIVET LINE. REPAIRED IAW FOKKER SRM 52-30-00, 52-02-05 PAGE 3 AND 51-31-05 PAGES 8 AND 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION FOUND UNDER LOWER TRANSPONDER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: BRACKET — DAMAGED (SPOILER) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND NR 2 LIFTDUMPER SPIGOT MOUNTING BRACKET REQUIRES REAMING FOR OVERSIZE BOLTS. REPAIRED IAW HORIZON AIR EA 4-57-551.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND WING INBOARD TRAILING EDGE UPPER ATTACH ANGLE TO 5280 BEAM IS CRACKED. REPAIRED IAW FOKKER SRM 51-32-01, 51-32-01 AND 51-35-02.

Part: BEAM — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- 18MM LONG CRACK LOWER RADIUS OF BEAM 3 AT BUTT LINE 55R FRONT SIDE OF REAR PRESSURE BULKHEAD. REPAIRED IAW HORIZON AIR EA 4-53-1227.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- AFT CARGO PIT CRACKED CASTELLATION AT FRAME 13815A AND STRINGER 1-2. REPAIRED IAW FOKKER SRM 53-02-13, 53-22-04 AND 51-31-01.

Part: BRACKET — DAMAGED (SPOILER) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND NUMBER 1 LIFTDUMPER BRACKET MOUNTING HOLES REQUIRE REAMING FOR OVERSIZED BOLT. REPAIRED IAW HORIZON AIR EA 4-57-551.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED ANGLE ON VERTICAL STAB ABOVE RIB 3 AND 2 BELOW RUDDER. REPAIRED IAW FOKKER SRM 55-31-04 AND 51-31-01.

Part: DOOR FRAME — CRACKED (APU INLET) · airframe 41,992 hrs · 52,219 cycles

YYC- TWO CRACKS AT APU AIR INLET DOOR SURROUND TOP AND BOTTOM AFT CORNERS. REPAIRED IAW FOKKER SRM 53-02-07 PAGE 7, 53-26-01 PAGE 8, 51-31-01 PAGES 13 AND 14 AND 51-31-05 PAGES 8-10.

Part: CLIP — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CLIP AT FRAME 8305 AND STRINGER 70. REPAIRED IAW FOKKER SRM 53-02-01, 53-02-13, 54-31-01 AND 51-30-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- SHARP DENT IN FUSELAGE SKIN AT RIGHT HAND AIR CYCLE MACHINE INLET FORWARD END IN UNPRESSURIZED AREA. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 AND 51-31-01 PAGES 13 AND 14.

Part: DUCT — ERODED (ACM) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND AIR CYCLE MACHINE INLET ERRODED. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14 AND 51-31-04.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- VERTICAL STAB RIB 8 IS CRACKED ON THE RIGHT HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-55-284.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- REAR PRESSURE BULKHEAD FLOORBEAM SUPPORT ANGLE IS CRACKED AT STATION 19275 BL425R. REPAIRED IAW FOKKER SRM 53-24-05, 51-31-01 AND 51-32-01.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACK ON REAR PRESSURE BULKHEAD AT BEAM 2 BL425R - BL1050R. REPAIRED IAW HORIZON AIR EA''S 4-92-21 A&B AND 4-53-1473.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- REAR PRESSURE BULKHEAD PULLEY REINFORCEMENT BRACKET FORWARD SIDE CRACKED. REPAIRED IAW FOKKER SRM 53-24-04 AND 51-31-01.

Part: SKIN — DENTED (RT FLAP VANE) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD FLAP VANE DENT IN LEADING EDGE OUTBOARD END. REPAIRED IAW FOKKER SRM 51-11-4 PAGE 2 AND 51-31-04 PAGES 10 AND 11.

Part: WINDOW POST — DAMAGED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- REMOVED WINDOW POST NR 2 REPAIR FOR INSPECTION AND NDT. REPAIRED IAW HORIZON AIR EA 4-53-1474.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- 10 MM LONG CRACK IN RADIUS OF UPPER CONSOLE AT BEAM 2 BUTT LINE 425R, FRONT SIDE OF REAR PRESSURE BULKHEAD. REPAIRED IAW FOKKER SRM 51-31-02 PAGE 9 AND 10 AND 51-31-01 PAGES 13 AND 14.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- DENT AND SCRATCH BETWEEN FRAME 15635 AND 16060 BETWEEN STRINGER 68 AND 67, FORWARD OF REAR CARGO DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-02-04, 51-31-01 AND HORIZON AIR EA 4-53-1471.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACK ON FRAME 2650 AT STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.

Part: SKIN — DELAMINATED (RUDDER) · airframe 41,992 hrs · 52,219 cycles

YYC- RUDDER TRAILING EDGE TO BE REPLACED DUE TO EXCESSIVE DELAMINATION. REPAIRED IAW FOKKER SRM 51-10-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CORROSION ON FORWARD SIDE OF FRAME 11905 LT BETWEEN STRINGERS 28-31. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- EXFOLIATING CORROSION ON FRAME SPLICE AT STATION 13353 AND STRINGER 31, FORWARD AND AFT OF FRAME. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14.

Part: SKIN — CRACKED (LT WING) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND UPPER AFT SKIN PANEL REBATE IS CRACKED BETWEEN WS 2635-3100 AT FALSE SPAR. REPAIRED IAW HORIZON AIR EA 4-57-548.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- CORROSION FOUND ON LEFT HAND HORIZONTAL STAB BOTTOM SKIN FORWARD OF PANEL 52E. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: CABLE — DAMAGED (SERVICE DOOR) · airframe 41,992 hrs · 52,219 cycles

YYC- SERVICE EMERGENCY DOOR RELEASE CABLES DAMAGED. REPAIRED IAW FOKKER SRM 52-40-01.

Part: STRINGER — DAMAGED (RUDDER) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND RUDDER STRINGER AT ACCESS PANEL 57Y DAMAGED. REPAIRED IAW FOKKER SRM 55-40-04, 55-02-07, 51-31-01 AND 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND AT FRAME 5805 AND STRINGER 19 HAS CRACKED CASTELLATION. REPAIRED IAW HORIZON AIR EA 4-53-1461.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 7305 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 7305 AND STATION 19. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 6805 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 5805 AND STRINGER 16 AND 17 (LEFT HAND FUSELAGE SKIN). REPAIRED IAW HORIZON AIR EA 4-53-1461.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- EXFOLIATING CORROSION ON FRAME SPLICE AT STATION 13353 AND STRINGER 45, FORWARD AND AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- DAMAGE TO LEFT HAND FUSELAGE SKIN BETWEEN 5305 AND 7305 BETWEEN STRINGERS 14 AND 18. REPAIRED IAW HORIZON AIR EA 4-53-1460.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND AT FRAME 5805 AND STRINGER 18 HAS CRACKED CASTELLATION. REPAIRED IAW HORIZON AIR EA 4-53-1461.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FUSELAGE FRAME ATTACH ANGLES CRACKED AT FRAME 5305 AND STRINGERS 16 AND 17. REPAIRED IAW FOKKER SRM 53-02-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC-MINOR CORROSION FOUND UNDER UPPER NAV/COM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND 53-01-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION FOUND UNDER AFT DME ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 1. REPAIRED IAW FOKKER SRM 55-02-02.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CORROSION ON FRAME SPLICE ANGLES AT FRAME 11905 AND STRINGER 45 FORWARD AND AFT RIGHT HAND SIDES. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FRAME 8305 AT STRINGER 3 TOP FLANGE OF FRAME IS DENTED. REPAIRED IAW HORIZON AIR EA 4-53-1462.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION FOUND UNDER LOWER COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SKIN PANEL — DAMAGED (WING) · airframe 41,992 hrs · 52,219 cycles

YYC- REBATE ON ACCESS PANEL 73B NEEDS INVESTIGATION ON PREVIOUS REPAIR. REPAIRED IAW HORIZON AIR EA 4-57-550.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 5. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: BRACKET — CRACKED (RUDDER) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED RIB FAIRING BRACKET BELOW RIB 12 ON RUDDER. REPAIRED IAW FOKKER SRM 55-40-04 AND 51-31-01 PAGES 13 AND 14.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FRONT PRESSURE BULKHEAD REAR SIDE BELOW FLOOR RIGHT OF CENTER AT BEAM 2 HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FRONT PRESSURE BULKHEAD REAR SIDE BELOW FLOOR, RIGHT OF CENTER AT BEAM 3 HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51B HAS A CRACK ON RIB 6. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FRAME 9305 AT STRINGER 3 HAS MINOR SURFACE CORROSION ON TOP SURFACE OF UPPER FLANGE. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION ON FUSELAGE SKIN UNDER LOWER VHF COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FORGED STRINGER 2 AT FRAME 9305C HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FORWARD DOOR AFT LOWER CORNER OF APERTURE HAS MINOR SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FRAME 8305 AT STRINGER 73 BOTTOM SIDE OF UPPER FLANGE HAS SURFACE CORROSION AROUND ANCHOR NUT. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION ON FUSELAGE SKIN UNDER FORWARD RADIO ALTIMETER ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT AFT DOOR AFT LOWER CORNER OF APERTURE HAS MINOR SURFACE CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-11.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FORWARD DOOR FORWARD LOWER CORNER OF APERTURE HAS MINOR SURFACE CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FORWARD CARGO PIT FORGED STRINGER 73 AT FRAME 9305C HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A IS CRACKED ON RIB 4. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATION 8805 AND 10753. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 6. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 8805 AND 9305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 5. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND AT FRAME 6305 AND STRINGER 19 HAS CRACKED CASTELLATION. REPAIRED IAW FOKKER SRM 53-02-12.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 10966 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 10346 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK AT NUMBER 1 RIB. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 2. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FUSELAGE SKIN DENTED ON RIGHT HAND SIDE ON THE ROOF OF STATION 20285 THROUGH 20785 AND STRINGERS 37 AND 38 BY DORSAL FIN. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13.

Part: WASHER — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED RIVET WASHER IN CABIN AT FRAME 14755 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATION 10753 AND 11253. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 7305 AND 8065. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 15205 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- DENT IN FUSELAGE SKIN LEFT HAND SIDE, AFT OF FIRE BOTTLE DISCHARGE AT STATION 19775 AND STRINGERS 12 AND 13 FOUND BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATIONS 8065 AND 8565. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: RIB — CRACKED (HORIZ STAB) · airframe 41,992 hrs · 52,219 cycles

YYC- HORIZONTAL STAB LEADING EDGE 51A HAS A CRACK ON RIB 8. REPAIRED IAW HORIZON AIR EA 4-55-286.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- LEFT HAND INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 9805 AND 10253. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 12405 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND INBOARD SEAT TRACK CORRODED BETWEEN STATIONS 6565 AND 7305. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 53-40-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 58A. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CLIP AT FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13.

Part: WASHER — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED RIVET WASHER IN CABIN AT FRAME 15205 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CLIP AT FORWARD CARGO PIT FRAME 9305 AND STRINGER 66. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MINOR CORROSION UNDER MARKER BEACON ANTENNA ON FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: CLIP — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CRACKED CLIP IN FORWARD CARGO PIT FRAME 9305 AND STRINGER 66. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14.

Part: TRACK — DENTED (SERVICE DOOR) · airframe 41,992 hrs · 52,219 cycles

YYC- SERVICE EMERGENCY DOOR FORWARD LOWER TRACK DENTED. REPAIRED IAW HORIZON AIR EA 4-52-444.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- NOSE LANDING GEAR BAY TOP COVER IS CRACKED ON LEFT HAND SIDE OF STATIONS 2996 - 3050L. REPAIRED IAW HORIZON AIR EA 4-53-1459.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FUSELAGE SKIN TO FRAME IS CRACKED AT FORWARD CARGO PIT FRAME 7305 AND STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13 AND 51-31-01 PAGES 13 AND 14.

Part: SKIN — DENTED (RT WING) · airframe 41,992 hrs · 52,219 cycles

YYC- DENT ON RIGHT HAND LEADING EDGE 62D BEYOND LIMITS. REPAIRED IAW FOKKER SRM 57-02-03.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- CHANNEL CRACKED FORWARD OF STATION 3820-3450, RIGHT HAND SIDE UNDER GALLEY FLOOR. REPAIRED IAW FOKKER SRM 53-11-05, 53-02-14 AND 51-31-01 PAGES 13 AND 14.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- RIGHT HAND FUSELAGE SKIN DENTED AFT OF MID CARGO DOOR STATION 8805-9305 AND STRINGERS 64 AND 65. REPAIRED IAW FOKKER SRM 53-02-02 PAGE 2 AND 51-31-01 PAGES 13 AND 14.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- ATTACH ANGLE CRACKED FORWARD OF STATION 4900 AT CHANNEL 6 INBOARD FROM SERVICE EMERGENCY DOOR UNDER FORWARD GALLEY. REPAIRED IAW FOKKER SRM 53-11-05 AND 51-32-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- SHARP DENT IN FUSELAGE SKIN AT STATION 5805, 3INCHES FORWARD OF FORWARD CARGO DOOR. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 AND 51-31-01 PAGES 13 AND 14.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- MID CARGO DOOR COMING FORWARD IS GOUGED AND BLENDED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- SHARP DENT IN FUSELAGE SKIN 5 INCHES ABOVE ACCESS PANEL 24B AND 4 INCHES AFT OF STATION 2750 IS BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-01 PAGE 3 AND 51-31-01 PAGES 13 AND 14.

Part: DOOR — CRACKED (HYD SERVICE DR) · airframe 41,992 hrs · 52,219 cycles

YYC- HYDRAULIC SERVICE PANEL DOOR REBATE CRACKED AT FORWARD END CENTER AND UPPER CORNER AND BENT LOWER FORWARD CORNER. REPAIRED IAW HORIZON AIR EA 4-52-442.

Part: SKIN — CANNING (FUSELAGE) · airframe 41,992 hrs · 52,219 cycles

YYC- FUSELAGE SKIN OIL CANNED FORWARD OF DORSAL FIN AT STATION 17845-18270 AND STRINGER 34 AND 33 ON ROOF. REPAIRED IAW FOKKER SRM 53-02-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,991 hrs · 52,218 cycles

PDX-CRACK IN AFT PRESSURE BULKHEAD TO THE RIGHT OF APU. COMPLIED WITH PROVISIONS FOR FERRY FLIGHT TO MTX FACILITY.

Part: SIGN — BURNED OUT (CABIN) · airframe 41,772 hrs · 52,021 cycles

PDX- THE FORWARD, MIDDLE AND AFT EMERGENCY EXIT SIGNS HAVE SEVERAL BURNED OUT BULBS. REMOVED AND REPLACED SIGNS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — BURNED OUT (CABIN) · airframe 41,648 hrs · 51,909 cycles

PDX- EMERGENCY EXIT SIGN AFT LIGHTS AT MID CABIN OUT. INSTALLED NEW EXIT SIGN AT MID CABIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 41,640 hrs · 51,899 cycles

BOI-ALL FOUR EMERGENCY DOOR/OVERWING EXITS EVACUATION GREEN EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — MALFUNCTIONED (GALLEY) · airframe 41,640 hrs · 51,899 cycles

SEA-ELECTRICAL BURNING SMELL COMING FROM COFFEE URN LOCATION TOP AND BOTTOM. REMOVED AND REPLACED BOTH UPPER AND LOWER COFFEE JUG ELECTRICAL RECEPTICALS. OPERATIONAL WARM-UP CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — BURNED OUT (CABIN) · airframe 41,287 hrs · 51,584 cycles

PDX-FORWARD CABIN EXIT SIGN PARTIALLY INOPERATIVE. REMOVED AND INSTALLED NEW EMERGENCY EXIT SIGN.OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 41,232 hrs · 51,531 cycles

SEA- EXIT SIGN ABOVE COCKPIT DOOR HAS SOME LIGHTS OUT. REPLACED FORWARD OVERHEAD EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSFORMER — FAILED (CABIN) · airframe 41,153 hrs · 51,454 cycles

SEA - CREW REPORTED STRONG SMELL IN FLIGHT COMPARTMENT. REMOVED AND REPLACED DEFECTIVE TRANSFORMER BALLAST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 41,050 hrs · 51,362 cycles

GEG - MID CABIN EXIT SIGN FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARDS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 40,829 hrs · 51,152 cycles

SEA - EXIT LIGHT ABOVE FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 12) · airframe 40,711 hrs · 51,055 cycles

SEA - EMERGENCY EXIT LIGHT ON SEAT 12B INOP. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — MALFUNCTIONED (CABIN) · airframe 39,699 hrs · 50,053 cycles

PDX - MID CABIN OVERHEAD EXIT SIGNS FOUND DIM. REMOVED AND REPLACED CIRCUIT BOARDS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 39,252 hrs · 49,627 cycles

BOI - EMERGENCY TRACK LIGHTING ILLUMINATED WITH SWITCH IN ARM MODE. INSPECTION REVEALED BROKEN WIRE UNDER CARPET. REPAIRED WIRING AS REQUIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

BOI - EXIT SIGN AT RIGHT HAND OVERWING STATION WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN POWER SUPPLY, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 5 & 6)

GEG - DURING INSPECTION, FOUND ROWS 5 AND 6 EVACUATION LIGHTS INOPERATIVE. REPAIRED CHAFED WIRE WITH SERVICABLE CONNECTOR. OPERATIONAL CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN)

PDX - MID CABIN FORWARD FACING EXIT SIGN WAS REPORTED AS INOPERATIVE. THE AFFECTED SIGN WAS REMOVED AND REPLACED, OPERATIONAL CHECK GOOD.

Part: BALLAST — OVERHEATED (COCKPIT)

SEA - ELECTRICAL SMELL ON FIRST OFFICERS SIDE FLOOD LIGHTING. MAINTENANCE INSPECTED AND FOUND SOURCE OF SMELL TO BE FROM LIGHTING BALLAST. REMOVED AND REPLACED BALLAST, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (COCKPIT)

PDX - PILOT REPORTS LEFT RED FLOOD BALLAST SMELLS HOT OR BURNING. MAINTENANCE INSPECTED COCKPIT LIGHTING. CHANGED TWO DETERIOATED BULBS. RAN LIGHTS FOR TWO HOURS, NO SMELLS NOTED, OPERATIONAL CHECKS WERE GOOD.

Part: CLIP — CRACKED (FRAME 19976)

PDX - AFT FUSELAGE FRAME 19976 HAS CRACKED CLIP BETWEEN STRINGER 39-40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 4.

Part: STRINGER — MISINSTALLED (FRAME 4900)

PDX - STRINGER 50, A SECTION FROM FRAME 4900 TO SPLICE BETWEEN FRAMES 5805 AND 6305 IS INCORRECT THICKNESS FOR THIS LOCATION. REPLACED STRINGER IAW HORIZON AIR EA 4-53-824.

Part: CLIP — CRACKED (FRAME 19976)

PDX - AFT FUSELAGE FRAME 19976 CRACKED CLIP NEXT TO STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3.

Part: SKIN — CRACKED (FRAME 19976)

PDX - AFT FUSELAGE BETWEEN FRAMES 19976 AND 20075, ALONG STRINGER 39 SUSPECT CRACK. REPAIRED IAW HORIZON AIR EA 4-53-823.

Part: SKIN — CRACKED (WING)

PDX - SKIN CRACKED ACROSS RIVET ON UPPER WING SKIN, INSIDE PANEL 81X. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.

Part: MOUNT — LOOSE (LT WING)

PDX - LEFT WING CANOE 81CE FORWARD MOUNT IS LOOSE. REPAIRED IAW HORIZON AIR EA 4-57-278.

Part: PANEL — WORN (PANEL)

PDX - PANEL 82CE NEEDS TO BE REMOVED TO DETERMINE THE WEAR TOLERANCES ON ATTACHING HOLES. REPAIRED IAW HORIZON AIR EA 4-57-279.

Part: SKIN — CHAFED (FUSELAGE)

PDX - THERE IS A FUSELAGE SKIN CHAFE 18 LONG WHERE PANEL 92BD WAS MARKED. REPAIRED IAW HORIZON AIR EA 4-53-805.

Part: SKIN — CHAFED (FRAME 14285)

PDX - AIRFRAME SKIN CHAFED FROM FRAME 14285 TO 14755 WHERE PANEL 91BC WAS INSTALLED, AFT EDGE ENTIRE LENGTH. REPAIRED IAW HORIZON AIR EA 4-53-805.

Part: BRACKET — LOOSE (FUSELAGE)

PDX - OUTBOARD REAR ATTACH BRACKET, PANEL 81CE, HAS WORKING RIVETS AND LOOSE BRACKET. REPAIRED IAW HORIZON AIR EA 4-57-278.

Part: FRAME — CORRODED (FRAME 8305)

PDX - CORROSION ON OUTBOARD FLANGE OF C-CHANNEL OF FRAME 8305 BETWEEN STRINGER 30 AND 36. REPAIRED IAW FOKKER SRM 51-10-4.

Part: STRINGER — CRACKED (RT MLG WW)

PDX - THERE IS A CRACKED STRINGER AT TOP STRUCTURE IN RIGHT-HAND MAIN LANDING GEAR STRUT BAY, DIRECTLY ABOVE THE GEAR STRUT AFT LUG. REPAIRED IAW FOKKER SRM 51-31-1 AND SRM 51-30-02.

Part: SKIN — DAMAGED (FUSELAGE)

PDX - UPPER NAV/COMM ANTENNA HAS MULTIPLE PITS ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-821.

Part: FRAME — CORRODED (FRAME 8305)

PDX - LEFT-HAND CABIN FRAME 8305 IS CORRODED ON AFT SIDE AT SPLICE NEAR STRINGER 18. REPAIRED IAW HORIZON AIR EA 4-53-822.

Part: SKIN — DENTED (RT TE FLAP)

PDX - RIGHT INBOARD FLAP HAS A DENT IN UPPER SURFACE OF TRAILING EDGE, 30 OUTBOARD OF STATION 1700. REPAIRED IAW FOKKER SRM 51-70-0, PARAGRAPH 7E.

Part: FRAME — CORRODED (FRAME 12853)

PDX - THERE IS CORROSION ON FRAME 12853 FROM STRINGER 41 TO STRINGER 45. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01-01.

Part: CLIP — CRACKED (FRAME 16-2)

PDX - AFT FUSELAGE OBLIQUE FRAME 16-2 HAS CRACKED CLIP BETWEEN STRINGERS 69-70. REPAIRED IAW MM 20-30-07, PAGE 203.

Part: PANEL — CORRODED (WING)

PDX - FRETTING CORROSION AROUND BOLT HOLES AT PANEL 24B ON INSIDE OF PANEL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: SEAT TRACK — GOUGED (FRAME 6805)

PDX - LEFT OUTBOARD SEAT TRACK HAS A .5 INCH LONG GOUGE 7 FORWARD OF FRAME 6805 ON INBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-813.

Part: SEAT TRACK — CRACKED (FRAME 4610)

PDX - RIGHT-HAND INBOARD PASSENGER SEAT TRACK HAS 2 SUPPORT RISERS AT THE INBOARD AND OUTBOARD FLANGES AT FRAME 4610 TIE IN TABS CRACKED, UNDERSIDE OF FLANGES. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - LEFT INBOARD SEAT TRACK HAS CORROSION 5 FORWARD OF FRAME 7805 ON THE OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: SEAT TRACK — CORRODED (FRAME 10966)

PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL AREA OF FRETTING CORROSION ADJACENT TO FRAME 10966 ON INBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-813.

Part: SEAT TRACK — CORRODED (BS 9550-9700)

PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE BETWEEN STATION 9550 AND 9700. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4,A,1 AND HORIZON AIR EA 4-53-813.

Part: SEAT TRACK — CORRODED (FRAME 11905)

PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION AROUND CAMLOC RECEPTACLE 2 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 4 BAND HORIZON AIR EA 4-53-813

Part: SKIN — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER NAV/COMM 1 ANTENNA PLATE. REPAIRED IAW HORIZON AIR EA 4-53-811.

Part: STRINGER — CORRODED (FRAME 4900)

PDX - STRINGER 41 FORWARD END, 2.5 INCHES AFT OF FRAME 4900 HAS EXFOLIATION CORROSION. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1E.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 34 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: STRINGER — CRACKED (FRAME 7305)

PDX - CRACK AT INSULATION ATTACH HOLE ON STRINGER 46, FORWARD OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: STRINGER — CORRODED (FRAME 8305)

PDX - STRINGER 30 CORROSION AT CRACKED INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 46 HAS CORROSION/CRACK AT HOLE, 10 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 46 HAS CORROSION/CRACK AT HOLE, 2.8 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: SKIN — MISREPAIRED (RT TE FLAP)

PDX - QUESTIONABLE REPAIR TO UPPER SURFACE OF RIGHT INBOARD FLAP JUST ABOVE PANEL 81AD. REPAIRED IAW FOKKER SRM 51-70, PARAGRAPH 3E, STEP 3.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 46 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.

Part: STRINGER — CRACKED (FRAME 7805)

PDX - LEFT-HAND FORWARD CABIN STRINGER 34 HAS TWO CRACKS AT INSULATION HOLES, 1.7 FORWARD OF FRAME 7805 AND 3.9 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 34 CRACKED A INSULATION FASTENER HOLE, 8.8 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: CASTELLATION — CRACKED (FRAME 16060)

PDX - FRAME 16060 CASTELLATION CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.

Part: FRAME — CHAFED (FRAME 16660)

PDX - FRAME 16660 CHAFED AT STRINGER 27 INBOARD FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH E1.

Part: DOUBLER — CRACKED (CARGO DOOR)

PDX - AFT CARGO DOOR HAS A CRACK IN REPAIR DOUBLER AT NUT PLATE HOLE FOR STAY FITTING. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01.

Part: FRAME — CORRODED (FRAME 11253)

PDX - FRAME 9805 AT STATION 11253 HAS CORROSION AT DOUBLER BELOW STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.

Part: LINK — CHAFED (LT SPEED BRAKE)

PDX - SUPPORT LINK ASSEMBLY FOR LEFT SPEEDBRAKE HAS CHAFE DAMAGE NEAR LOWER ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-55-139.

Part: SKIN — CORRODED (FRAME 6805-7305)

PDX - FORWARD CARGO BAY BELLY SKIN HAS SURFACE CORROSION INSIDE BETWEEN FRAMES 6805 AND 7305 BETWEEN STRINGER 1 AND ANTENNA DOUBLER. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B.

Part: FRAME — CRACKED (FRAME 9305)

PDX - FRAME 9305 HAS CRACKED CLIP AT STRINGER 28 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: FRAME — CORRODED (FRAME 12853)

PDX - THERE IS CORROSION ON FRAME 12853 AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 3.

Part: SKIN — CORRODED (FRAME 9305)

PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION AT EDGE OF SKIN CUTOUT AND AROUND RIVETS 6 AFT OF FRAME 9305A, BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-4 PARAGRAPH 3A, STEPS 1-3.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AND IN CHANNEL AT FRAME 9305C AND EXTENDS 6 AFT OF FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: SEAT TRACK — CORRODED (FRAME 10966)

PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION 2 INCHES AFT OF FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SKIN — CORRODED (FRAME 7805-8305)

PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION IN AREA BETWEEN FRAMES 7805 AND 8305 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-04, PAGE9, PARAGRAPH 4.

Part: SHEAR TIE — CORRODED (FRAME 7305)

PDX - FRAME 7305 SHEAR TIE TOP SURFACE HAS CORROSION BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C.

Part: DUCT — CRACKED (ACM EXHAUST)

PDX - RIGHT-HAND ACM EXHAUST DUCT IS CRACKED AT TOP AFT CORNER. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — DAMAGED (LT MLG WW)

PDX - LEFT-HAND MAIN LANDING GEAR DOOR WHEEL BAY OUTER SKIN HAS A OPENING IN THE SKIN. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 1 AND SRM 51-31-05.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT FRAME 9305C AND EXTENDS 3 FORWARD OF FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B.

Part: STRINGER — DAMAGED (FRAME 5805)

PDX - CASTELLATION FLANGE REMOVED TO FACILITATE STRINGER REPAIRED AT STRINGER 34 AND FRAME 5805. FABRICATED REPAIR ANGLE IAW FOKKER SRM 53-02-12, FIGURE 1.

Part: CLIP — CRACKED (FRAME 12414)

PDX - FRAME CLIP ON FRAME 12414 IS CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — CORRODED (BS 7800-8000)

PDX - RIGHT INBOARD SEAT TRACK HAS 3 SMALL AREAS OF FRETTING CORROSION BETWEEN STATION 7800 AND 8000 ON INBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-813 AND FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: STRINGER — CORRODED (BS 10753)

PDX - DOME NUT PLATE 4 AFT OF FRAME 9305C AT STATION 10753 ON STRINGER 37 HAS SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C, SRM 51-31-01 PAGE 13, PARAGRAPH B.

Part: FRAME — CORRODED (FRAME 6805)

PDX - FRAME 6805 AT STRINGER 74 HAS CORROSION UNDERSIDE OF TOP FLANGE OF FRAME AROUND NUT PLATES FOR THE 4 WAY TIE-IN. REPAIRED IAW HORIZON AIR EA 4-53-799.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE 4 FORWARD OF FRAME 9305A. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B AND HORIZON AIR EA 4-53-813.

Part: SEAT TRACK — CORRODED (FRAME 4850)

PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT FRAME 4850. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C AND 4B.

Part: STRINGER — CORRODED (FRAME 9305)

PDX - STRINGER 74 HAS CORROSION ON TOP SIDE WHERE IT PASSES THROUGH FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: SKIN — CORRODED (FRAME 8305)

PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION AROUND BELLY DRAIN, AFT SIDE OF FRAME 8305 BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: FRAME — CORRODED (FRAME 7305)

PDX - FRAME 7305 AT STRINGER 74 HAS CORROSION AROUND NUT PLATE FOR THE 4 WAY TIE-IN, UNDERSIDE OF TOP FLANGE OF FRAME. REPAIRED IAW HORIZON AIR EA 4-53-808.

Part: FRAME — CORRODED (FRAME 8805)

PDX - FRAME 8805 AT STRINGER 74 HAS CORROSION AT UNDERSIDE OF TOP FLANGE AROUND NUT PLATES AT 4 WAY TIE-IN. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: STRINGER — CORRODED (FRAME 9305)

PDX - STRINGER 74 HAS TOP SURFACE CORROSION BETWEEN FRAMES 9305A AND 9305B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: SKIN — CORRODED (FRAME 7305-7805)

PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION BETWEEN FRAME 7305, 7805 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: STRINGER — CORRODED (FRAME 11405)

PDX - MID CABIN, STRINGER 38 HAS CORROSION AROUND HOLE, 5.5 AFT OF FRAME 11405 AT STATION 12853. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: JAMB — DAMAGED (CARGO DOORWAY)

PDX - CENTER CARGO DOOR APERTURE DOES NOT ALLOW FOR USE OF STANDARD HARDWARE. REPAIRED IAW FOKKER SRM 51-31-05.

Part: SHEAR TIE — CORRODED (FRAME 9305)

PDX - FRAME 9305 SHEAR TIE CLIP HAS CORROSION ON FORWARD SIDE OF FRAME WHERE CUTOUT IS FOR STRINGER 74 PASS THROUGH. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: FRAME — CORRODED (FRAME 7305)

PDX - FRAME 7305 AT STRINGER 1 HAS EXFOLIATION CORROSION AROUND NUT PLATE HOLE UNDERSIDE OF TOP FLANGE OF FRAME. REPAIRED IAW HORIZON AIR EA 4-53-798 AND EA 4-53-808.

Part: FRAME — DAMAGED (FRAME 12414)

PDX - FRAME 12414 HAS PIT/DIVOT 4 AFT OF STRINGER 41. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 5B, STEP 3 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3C, STEPS 1-2-3-4.

Part: FRAME — CORRODED (FRAME 7805)

PDX - RIGHT-HAND CABIN FRAME 7805 HAS CORROSION ON TOP FLANGE BELOW STRINGER 31 THROUGH 33. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH A-B, STEPS 1 AND 2.

Part: STRINGER — CORRODED (FRAME 4900)

PDX - STRINGER 34 FORWARD END, 2.5 INCHES AFT OF FRAME 4900 HAS EXFOLIATION CORROSION. REPAIRED IAW FOKKER SRM 53-02-06.

Part: STRINGER — CRACKED (FRAME 7305-7805)

PDX - LEFT-HAND FORWARD CABIN STRINGER 35 HAS 2 CRACKS BETWEEN FRAMES 7305 AND 7805. ONE AT THE INSULATION FASTENER HOLE AND ONE 1.3 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.

Part: SKIN — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 6, FIGURE 4 AND SRM 53-00-00, PAGE 2.

Part: STRINGER — CRACKED (FRAME 7805)

PDX - LEFT-HAND FORWARD CABIN STRINGER 36 HAS ONE CRACK AT INSULATION FASTENER HOLE, 1.7 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.

Part: FRAME — CORRODED (FRAME 7805)

PDX - SURFACE CORROSION ON FRAME 7805 ON TOP FLANGE BELOW STRINGER 41 THROUGH 43, 44 AND 45. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9 AND PARAGRAPHS 4B AND 3C.

Part: STRINGER — CRACKED (FRAME 8805)

PDX - STRINGER 35 CRACKED AT INSULATION FASTENER HOLE, 6.6 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.

Part: STRINGER — CORRODED (FRAME 12414)

PDX - THERE IS CORROSION ON STRINGER 43 APPROXIMATELY 3 INCHES AFT OF FRAME 12414. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 9, PARAGRAPH 4B AND SRM 53-10-4 PAGE 8, PARAGRAPH 3C.

Part: FRAME — CORRODED (FUSELAGE)

PDX - FRAME HAS SURFACE CORROSION ON TOP/OUTBOARD FLANGE FROM STRINGER 43 TO 44. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 8-9, PARAGRAPHS EC AND 4B.

Part: STRINGER — CRACKED (FRAME 5305)

PDX - STRINGER 34 CRACK/CORROSION AT HOLE, 2.6 INCHES AFT OF FRAME 5305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.

Part: STRINGER — CRACKED (FRAME 5805)

PDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 2.7 INCHES FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 44 AT RIVET. REPAIRED IAW FOKKER SRM 51-02-13, FIGURE 2.

Part: STRINGER — CRACKED (FRAME 6805-7305)

PDX - RIGHT-HAND FORWARD CABIN STRINGER 44 HAS TWO CRACKS BETWEEN FRAMES 6805 AND 7305. ONE CRACK AT EACH INSULATION FASTENER HOLE. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3.

Part: STRINGER — CORRODED (FRAME 9305)

PDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 2.6 FORWARD FRAME 9305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: STRINGER — CORRODED (FRAME 6805)

PDX - RIGHT-HAND CABIN STRINGER 41 HAS CORROSION DAMAGE LOCATED JUST ABOVE FRAME 6805 AND 2.9 FORWARD OF EXISTING REPAIR. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION A-A, FIGURE 1.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 8.8 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: SKIN — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER NAV/COMM 1 ANTENNA BLANKING PLATE. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 6 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: STRINGER — CRACKED (FRAME 8305)

PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: MOUNT — CORRODED (CORRODED)

PDX - LIGHT SURFACE CORROSION ON LOWER NR 1 DME FUSELAGE MOUNTING BASE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B 112 C.

Part: STRINGER — CORRODED (FRAME 8805)

PDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: STRINGER — CRACKED (FRAME 5805)

PDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 9.7 FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE.

Part: STRINGER — CRACKED (FRAME 6805)

PDX - STRINGER 47 CORROSION/CRACK AT HOLES, 2 CRACKS ONE AT EACH HOLE 6.3 AFT OF FRAME 6805 AND 6.4 FORWARD OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06.

Part: FRAME — LOOSE (FRAME 8305)

PDX - OVERHEAD BIN OUTBOARD ATTACH AT FRAME 8305 BETWEEN STRINGER 47 AND 48 IS LOOSE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1, 2, 3, 5.

Part: STRINGER — CRACKED (FRAME 8805)

PDX - LEFT-HAND CABIN STRINGER 30 HAS CRACK WITH CORROSION AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.

Part: ANGLE — CORRODED (FRAME 7805-8305)

PDX - FLOOR SUPPORT ANGLE BETWEEN FRAMES 7805 AND 8305 ABOVE STRINGER 3 HAS CORROSION AROUND NUT PLATES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4BC.

Part: STRINGER — CRACKED (FRAME 8805)

PDX - LEFT-HAND CABIN STRINGER 31 HAS CRACK WITH CORROSION AT HOLE, 6.3 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: FRAME — CORRODED (FRAME 12875)

PDX - THERE IS CORROSION ON FRAME 12875 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4B.

Part: FRAME — CORRODED (FRAME 9305)

PDX - FRAME 9305 AT STRINGER 73, 4 WAY TIE-IN FOR FLOOR SUPPORT HAS CORROSION ON TOP SIDE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B AND C.

Part: STRINGER — CRACKED (FRAME 8805)

PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.8 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: SHEAR TIE — CORRODED (FRAME 8805)

PDX - FRAME 8805 SHEAR TIE CLIP HAS CORROSION, ALSO RIVET BUCK TAILS HAVE CORROSION BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C.

Part: FRAME — CORRODED (FRAME 7805)

PDX - LIGHT SURFACE CORROSION ON FRAME 7805 BOTTOM FLANGE JUST BELOW STRINGER 37. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4.

Part: CLIP — CRACKED (FRAME 9305)

PDX - FRAME 9305 HAS CRACKED CLIP AT STRINGER 32 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: FRAME — CORRODED (FRAME 8305)

PDX - FRAME 8305 AT STRINGER 74 HAS CORROSION ON UNDERSIDE OF TOP FLANGE AROUND NUT PLATE HOLES AT 4 WAY TIE-IN. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C, SRM 51-31-01.

Part: STRINGER — CRACKED (FRAME 8805)

PDX - STRINGER 31 CRACKED AT INSULATION FASTENER HOLE, 6.3 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: STRINGER — CRACKED (FRAME 7305-7805)

PDX - STRINGER 30 IS CRACKED AT INSULATION FASTENER HOLE MID WAY BETWEEN FRAME 7305 AND 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB.

Part: SEAT TRACK — CORRODED (FRAME 7305)

PDX - LEFT OUTBOARD SEAT TRACK HAS CORROSION 4 AFT OF FRAME 7305 ON INBOARD AND OUTBOARD FLANGES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C4.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL AREA OF FRETTING CORROSION ON INBOARD FLANGE 8 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: STRINGER — CRACKED (FRAME 7305)

PDX - STRINGER 28 CORRODED AT CRACK 8.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B.

Part: STRINGER — CRACKED (FRAME 7305-7805)

PDX - STRINGER 28 HAS CORROSION WITH CRACKS AT TWO INSULATION FASTENER HOLES BETWEEN FRAMES 7305 AND 7805. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B, FIGURE 1EE.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION IN 3 SMALL AREAS JUST FORWARD OF FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: FRAME — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ON THE AFT SIDE OF FRAME 15635 AND BOTH SIDE OF STRINGER 34. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH 3C AND 4B.

Part: STRINGER — CRACKED (FRAME 7305)

PDX - STRINGER 28 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B.

Part: SEAT TRACK — CORRODED (FRAME 8305)

PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE 2 FORWARD AND 2 AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: FRAME — CORRODED (FRAME 5805)

PDX - FRAME 5805 CORRODED OUTBOARD FLANGE FORWARD SIDE FROM STRINGER 27 TO 29. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8-9, PARAGRAPHS 3C AND 4B.

Part: STRINGER — CRACKED (FRAME 7805)

PDX - STRINGER 28 IS CRACKED AT INSULATION FASTENER HOLE, 2.7 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: FRAME — LOOSE (FRAME 6305)

PDX - 90 DEGREE FLOOR SUPPORT BRACKET AT FRAME 6305 AND STRINGER 3 HAS LOOSE ATTACH RIVETS FORWARD SIDE OF FRAME. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT OUTBOARD SEAT TRACK HAS FRETTING CORROSION ADJACENT TO FRAME 9305B ON INBOARD FLANGE AND AROUND CAMLOC RECEPTACLE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT FRAME 9305B AND EXTENDING 6 FORWARD OF 9305B. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 18 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: SEAT TRACK — DAMAGED (FRAME 6305)

PDX - RIGHT INBOARD SEAT TRACK HAS TOOLING DAMAGE 4 FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: FRAME — CORRODED (FRAME 5305)

PDX - FORWARD CARGO BAY FRAME 5305 HAS CORROSION AROUND 2 NUT PLATES ON UNDERSIDE OF TOP FLANGE OF C-CHANNEL AT STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-800.

Part: SEAT TRACK — CORRODED (FRAME 11905)

PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL TOOLING DAMAGE 4 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: STRINGER — CORRODED (FRAME 8305)

PDX - STRINGER 28 IS CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.5 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: SEAT TRACK — CORRODED (FRAME 6305)

PDX - LEFT OUTBOARD SEAT TRACK HAS FRETTING CORROSION 3 AFT OF FRAME 6305, ON OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4.

Part: STRINGER — CORRODED (FRAME 8805, 9305)

PDX - LEFT-HAND CABIN STRINGER 28 CORRODED BETWEEN FRAMES 8805 AND 9305. REPAIRED IAW FOKKER SRM 53-02-0, FIGURE 1EE.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION ON OUTBOARD FLANGE EXTENDING 3 AFT TO 8 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: FRAME — CORRODED (FRAME 8805)

PDX - LEFT-HAND CABIN FRAME 8805 HAS CORROSION ON TOP/OUTBOARD FLANGE AFT SIDE FROM STRINGER 30 TO 34. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4.

Part: STRINGER — CORRODED (FRAME 8805)

PDX - STRINGER 28 CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.8 FORWARD FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE.

Part: SEAT TRACK — CORRODED (FRAME 9805)

PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION 9 AFT OF FRAME 9805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: FRAME — CORRODED (FRAME 6805)

PDX - FRAME 6805 AT STRINGER 1 HAS CORROSION UNDERSIDE OF TOP FLANGE OF FRAME AROUND NUT PLATES FOR THE 4 WAY TIE-IN. REPAIRED IAW HORIZON AIR EA 4-53-799.

Part: SKIN — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER ATC ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4.

Part: MOUNTS — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON BOTH RAD ALT FUSELAGE MOUNTING BASES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: MOUNTS — CORRODED (FUSELAGE)

PDX - LIGHT SURFACE CORROSION ON FUSELAGE MOUNTS FOR BLANKING PLATES BY RAD ALT ANTENNAS. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: SEAT TRACK — CORRODED (FRAME 11905)

PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION AROUND CAMLOC RECEPTACLE 2 FORWARD OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ALONG LENGTH OF STRINGER 31 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 3C AND 4B.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE ADJACENT TO FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — DAMAGED (FRAME 10346)

PDX - LEFT OUTBOARD SEAT TRACK HAS A GOUGE 9 FORWARD OF FRAME 10346. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C4.

Part: SEAT TRACK — DAMAGED (FRAME 14755)

PDX - LEFT OUTBOARD SEAT TRACK HAS 3 SMALL NICKS AND GOUGES BETWEEN FRAMES 14755 AND 15205. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION 2 FORWARD OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: SEAT TRACK — DAMAGED (FRAME 11905)

PDX - LEFT INBOARD SEAT TRACK HAS SMALL NICKS AND LIGHT CHAFE DAMAGE 4 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ALONG STRINGER 45 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-31-0, PAGES 1-10 AND SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: RIVETS — MISSING (FRAME 5805)

PDX - FRAME 5805 HAS 90 DEGREE BRACKET AT AFT SIDE BETWEEN STRINGERS 4 AND 5 WITH 2 MISSING RIVETS. REPAIRED IAW FOKKER SRM 51-30-02.

Part: CLIP — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY AT FRAME 13815 CLIP IS CRACKED BETWEEN STRINGER 73 AND 72. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ON STRINGER 29 AT FORWARD END BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8-9 PARAGRAPH 3C AND 4B.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ALONG STRINGER 32 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-4, PAGES 8-9, PARAGRAPH 3C AND 4B.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ALONG STRINGER 33 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-4, PAGES 8-9, PARAGRAPH 3C AND 4B.

Part: STRINGER — CORRODED (FRAME 15635)

PDX - THERE IS CORROSION ALONG LENGTH OF STRINGER 30 BETWEEN FRAME 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8 AND 9, PARAGRAPHS 3C AND 4B.

Part: CLIP — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY AT FRAME 13815 CLIP IS CRACKED BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1.

Part: DOUBLER — CORRODED (FRAME 4610)

PDX - TCAS ANTENNA DOUBLER INSIDE FORWARD CARGO BAY HAS CORROSION, 3 FORWARD OF FRAME 4610 BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4 A, B, C.

Part: FRAME — CORRODED (FRAME 5305)

PDX - RIGHT-HAND DIAGONAL C-CHANNEL PORTION OF FRAME 5305 ABOVE STRINGER 65 HAS CORROSION AROUND LOWER NUT PLATE AND THE AFT FACE OF FRAME. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B AND C, SRM 51-31-02 AND SRM 51-31-05.

Part: FRAME — CORRODED (FRAME 5305)

PDX - FRAME 5305 CORRODED ON AFT SIDE OF INBOARD AND OUTBOARD FLANGE FROM STRINGER 32 TO 35. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8-9 AND PARAGRAPHS 3C AND 4B.

Part: SKIN — DAMAGED (RT MLG DOOR)

PDX - RIGHT-HAND INBOARD MAIN LANDING GEAR DOOR HAS IMPACT DAMAGE 6 FROM UNLOCK BRACKET. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

PDX - FRAME 7805 HAS CRACKED CLIP AT STRINGER 43 AT RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 43 AT RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 47 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 8805)

PDX - FRAME 8805 CRACKED CLIP AT STRINGER 45 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

PDX - FRAME 7805 CLIP CRACKED AT STRINGER 44 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: POWER SUPPLY — DISCHARGED (RT EMER EXIT)

SEA - RIGHT HAND SIDE OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, TESTED NORMAL.

Part: BULB — FAILED (CABIN)

PDX - PILOT REPORTS LIGHT BULBS IN THE EMERGENCY EXIT SIGN OVER THE COCKPIT DOOR ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN. AN OPERATIONAL TEST WAS PERFORMED, RESULTS WERE NORMAL.

Part: BULB — FAILED (SEAT 8E)

EMERGENCY OVERWING EXIT LIGHT AT SEAT 8E IS VERY DIM. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.

Part: WIRE — BROKEN (SEAT 4B)

EMERGENCY EXIT LIGHT AT SEAT 4B BASE IS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT BASE OF SEAT. OPERATIONAL CHECK IS NORMAL.

Part: BULB — FAILED (CABIN)

GEG - SECOND FORWARD FACING OVERHEAD EMERGENCY EXIT SIGN HAS ALL 28 VOLT BULBS BURNT OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (ROW 9A)

EXIT SIGN AT ROW 9A INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL.

Part: BULB — FAILED (CABIN)

PDX - LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

OVERHEAD EMERGENCY EXIT LIGHT AT ROW 13 AND 14 INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT AT ROW 9 IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE BULBS. OPERATIONAL TESTS WERE PERFORMED, RESULTS NORMAL.

Part: BULB — FAILED (CABIN)

LIGHT IN OVERWING EXIT SIGN ON LEFT SIDE, ROW 8 IS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL CHECK GOOD.

Part: CURCUIT BOARD — INOPERATIVE (CABIN)

LIGHTS ARE DIM IN EXIT SIGN ON PASSENGER CABIN CEILING AT ROWS 8 AND 9. MAINTENANCE REPLACED CIRCUIT BOARD FOR CEILING EXIT SIGN AT ROWS 8 AND 9, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

BOI - AISLE EVACUATION LIGHT AT 4B OUT. MAINTENANCE REPAIRED A BROKEN WIRE, RESECURED BUNDLE, AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

SEA - EMERGENCY EXIT LIGHT AT ROW 9 IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (CABIN)

BOI - THE AISLE EMERGENCY EXIT LIGHTS ARE INOPERATIVE AT ROWS 1 AND 13. MAINTENANCE REMOVED AND REPLACED BULBS, OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

PDX - EMERGENCY LIGHT AT SEAT 9A INOPERATIVE. MAINTENANCE RELAMPED, TESTS GOOD.

Part: BULB — FAILED (CABIN)

EXIT SIGN AT FORWARD CABIN IS INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL.

Part: BULB — FAILED (CABIN)

THE EMERGENCY LIGHT AT ROW 9A WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED AND FUNCTION CHECKED WORK, CHECKED GOOD.

Part: BULB — FAILED (CABIN)

SEA - EMERGENCY LIGHT AT ROW 9E IS BURNT OUT. RELAMPED, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

BOI - EMERGENCY LIGHT ON RIGHT SIDE ROW 8 IS INOP. MAINTENANCE REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

THE 28V EVACUATION LIGHTS AT EXIT 9E AND OVERHEAD ROW 2 INOP. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

BOI- EMERGENCY EXIT LIGHT ON GALLEY SERVICE DOOR IS INOP (LOWER RIGHT CORNER). RELAMPED EMERGENCY LIGHT, OPERATIONAL CHECKS GOOD.

Part: CIRCUIT CARD — FAILED (CABIN)

LIGHT BULB BURNT IN THE OVERHEAD EMERGENCY EXIT LIGHT ON THE LEFT SIDE. REPLACED LAMP CIRCUIT CARD, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG- DURING INSPECTION, SEVERAL OVERHEAD EVACUATION LIGHTS WERE NOTICED TO BE INOP. RELAMPED EFFECTED LIGHTS, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

BOI - CABIN EXIT SIGN HAS LAMPS INOP. REPLACED LAMPS, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

PDX - NR 2 EVACUATION BATTERY PACK DEAD. REPLACED SAME, OPERATIONAL CHECK GOOD.

Part: BALLAST — MALFUNCTION (COCKPIT)

FIRST OFFICERS RED/WHITE INSTRUMENT LIGHT PANEL OUT WITH A STRONG ELECTRICAL SMELL. PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY REPLACING LG17 BALLAST AND INSTRUMENT PANEL LIGHTS, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOI- ENTRANCE COMPARTMENT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, OPERATIONAL CHECKS GOOD.

Part: ENGINE — SMOKING (LEFT)

PDX- TOWER REPORTED SMOKE FROM AIRCRAFT DURING FIRST 300 TO 400 FEET OF TAKEOFF. GROUND RAN ENGINE AT HIGH POWER FOR SEVERAL MINUTES, NO EXCESSIVE SMOKE NOTED. OIL SERVICED CORRECTLY, OPERATIONAL CHECK GOOD.

Part: LAMP — FAILED (CABIN)

SEA - EMERGENCY EXIT LIGHT INOP AT 9A. REPLACED LIGHT BULB, OPERATIONAL CHECK GOOD.

Part: SWITCH — LACK OF LUBE (PASSENGER DOOR)

SEA - THREE INTERMITTANT PASSENGER DOOR WARNINGS IN FLIGHT. EMERGENCY CHECKLIST COMPLIED WITH. LUBED DOOR SWITCH, OPERATIONAL CHECK GOOD.

Part: LAMP — FAILED (CABIN)

GEG - SEAT 9E EMERGENCY EXIT SIGN INOP. RELAMPED LIGHT AT EMERGENCY EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

SEA - OVERWING EXIT SIGN ABOVE SEAT 9A IS INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

SEA- MID LEVEL OVERWING EMERGENCY EXIT LIGHTS ARE VERY DIM. REPLACED BATTERY POWER SUPPLY UNIT, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — MALFUNCTION (CABIN)

SEA - FORWARD EMERGENCY EXIT LIGHTING INOP. REPLACED BATTERY POWER SUPPLY IN FORWARD GALLEY CEILING. OPERATIONAL CHECK GOOD.

Part: LAMP — FAILED (CABIN)

THE 28V EVACUATION SIGN AT ROW 9 OVERWING EXIT AFT GALLEY INOP. RELAMPED, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

OVERWING EXIT LIGHT DIM. REPLACED BATTERY POWER SUPPLY FOR OVERWING EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

ROW 8E WINDOW EXIT LIGHT INOP. REPLACED BULBS AT 8E WINDOW EXIT, OPERATIONAL CHECK GOOD.

Part: BULBS — FAILED (CABIN)

SEA - OVERHEAD EMERGENCY EXIT SIGN BY OVERWING EXITS HAVE UNILLUMINATED AREAS. RELAMPED OVERHEAD EMERGENCY EXIT SIGNS AS REQUIRED. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY PATH LIGHTS INOP. REPAIRED BROKEN WIRE AT BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: SKIN — PUNCTURED (FUSELAGE)

FUSELAGE SKIN HAS A SMALL PUNCTURE BETWEEN OBLIQUE FRAMES 50 AND 58.5 INBOARD OF STRINGER 1. INSTALLED FLUSH PATCH AND DOUBLER PER FOKKER SRM 53-02-02 PAGE 2.

Part: ANGLE — DENTED (CARGO COMPT)

PDX - AFT CARGO APERATURE AT FORWARD LOWER INTERIOR ANGLE IS DENTED, GOUGED, AND BUCKLED. FABRICATED REPAIR ANGLE AND INSTALLED PER FOKKER SRM 53-02-16 PAGE 4 SECTION C-C.

Part: BULKHEAD BEAM — CRACKED (PRESS BLKHD)

PDX - CRACK IN LEFT SIDE OF BEAM NR V IN RADIUS BETWEEN LAST 3 RIVETS ON FORWARD SIDE OF FRONT PRESSURE BULKHEAD. REPAIRED LEFT HAND HORIZIONTAL BEAM NR V AS PER E.A. 4-53-183.

Part: FRAME — CORRODED (FUSELAGE)

PDX - FORWARD CARGO BAY FRAME 9305 CASTELLATION HAS CORROSION AROUND THE NUT PLATES ON THE UNDERSIDE OF THE FRAME, FROM STRINGERS 3 TO 73. IDENTIFIED AS LEVEL 2 CORROSION. CUT OUT CORRODDED TOP AREA OF FRAME AND FABRICATED NEW FRAME PIECE, AND INSTALLED PER E.A. 4-53-179.

Part: PANEL — CORRODED (FUSELAGE)

PANEL 73C HAS MANY AREAS OF FRETTING CORROSION AROUND THE SCREW HOLES. REMOVED FRETTING CORROSION PER EA 4-57-49.

Part: FRAME — CRACKED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME 6305 CASTELLATION HAS A .25 INCH CRACK FROM RIVET HOLE TO EDGE OF MATERIAL AT STRINGERS 73 TO 74. FABRICATED AND INSTALLED FRAME CASTELLATION PER FOKKER SRM 53-02-13 PAGE 4.

Part: PANEL — GOUGED (FUSELAGE)

PANEL 73C HAS ONE COUNTERSUNK SCREW HOLE THAT HAS DEEP GOUGES IN IT. COMPLIED WITH EA 4-57-49.

Part: BULKHEAD WEB — CRACKED (AFT PRESS BLKHD)

PDX - REAR PRESSURE BULKHEAD BELOW CABIN FLOOR IN CARGO BAY, HAS A CRACK IN THE BULKHEAD WEB UNDER LOWER FLOOR OF HORIZIONTAL BEAM III 6 OUTBOARD OF BL 425R. LENGTH OF CRACK APPROX 1.75 . REPAIRED CRACK ON REAR PRESSURE BULKHEAD ON BEAM III PER FOKKER SRM 53-02-18 PAGES 38 AND 39.

Part: COVER — CRACKED (BS 2475)

PDX - NOSE LANDING GEAR BAY TOP COVER AT STATION 2475 HAS 8 CRACKS BETWEEN 5 TO 23 INCHES LONG, FROM RIGHT HAND EDGE OF NOSE BAY TOP COVER. FABRICATED REPAIR DOUBLER AND INSTALLED PER FOKKER SRM 53-02-18 PAGE 14.

Part: FRAME — CRACKED (FRAME 11405)

FRAME 11405 IS CRACKED AT RADIUS AT END OF FRAME ON RIGHT SIDE OUTBOARD ON BL 560. FABRICATED AND INSTALLED REPAIR PER EA 4-53-162.

Part: BULKHEAD BEAM — CRACKED (AFT PRESS BLKHD)

PDX - REAR PRESSURE BULKHEAD BEAM II RIGHT END IS CRACKED IN RADIUS OF UPPER ATTACH FLANGE. REPAIRED HORIZONTAL BEAM II PER FOKKER SRM 53-02-18 FIGURE 13 SECTION B-B.

Part: CLIP — CRACKED (FRAME 32-2)

CLIP ON FRAME 32-2 STRINGER 27 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 50-2 AT STRINGERS 53, 50 AND 49 ARE CRACKED. FABRICATED AND INSTALLED NEW CLIPS PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: WINDOW POST — CRACKED (NR 3 WINDOW)

PDX - TOP OF NR 3 WINDOW POST AFT SIDE HAS A CRACK FROM FIRST HI-LOK UP FROM SUPPORT BRACKET. REPLACED WINDOW POST IAW E.A. 4-53-56.

Part: CLIP — CRACKED (FRAME 17565)

CLIP ON FRAME 17565 AT STRINGER 21 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 67-2 LEFT TOP ATTACHMENT, IS CRACKED BEYOND STOP DRILL. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: DOUBLER — CRACKED (FRAME)

REPAIR DOUBLER ON FRAME 42-2 ON STRINGER 190 IS CRACKED. FABRICATED NEW DOUBLER AND INSTALLED PER FOKKER SRM 53-30-02.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 32-2 AT STRINGER 29 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME 17565)

CLIP ON FRAME 17565 LEFT SIDE AT STRINGER 19 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: FRAME — CRACKED (FUSELAGE)

PDX - CRACK FROM RIVET TAIL AT FRAME 1890 AND STRINGER NR 18. REPAIRED FRAME CASTELLATION AT FRAME 1890, STRINGER NR 18 AS PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 32-2 AT STRINGER 190 IS CRACKED BEYOND STOP DRILL. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: FRAME — CRACKED (FRAME 16-2)

REPAIR ON OBLIQUE FRAME 16-2 ON LEFT TOP, AT STRINGER 34 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 4.

Part: CLIP — CRACKED (FRAME)

CLIPS ON FRAME 16-2 AT STRINGERS 41 AND 43 ARE CRACKED. FABRICATED AND INSTALLED NEW CLIPS PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME)

CLIPS ON FRAME 32-2 AT STRINGER 46 AND 54 ARE CRACKED. FABRICATED AND INSTALLED NEW CLIPS PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME 20075)

CLIP ON FRAME 20075 STRINGER 35 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13, PAGES 5-6.

Part: CLIP — CRACKED (FRAME)

CLIPS ON FRAME 67-2 RIGHT TOP ATTACHMENT, IS CRACKED BEYOND STOP DRILL. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME 20075)

CLIP ON FRAME 20075 AT STRINGER 39 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: CLIP — CRACKED (FRAME 50-2)

CLIPS ON FRAME 50-2 STRINGERS 48 AND 49 IS CRACKED BEYOND STOP DRILL. FABRICATED AND INSTALLED NEW CLIPS PER FOKKER SRM 51-31-01.

Part: DOUBLER — CRACKED (FRAME 24-2)

REPAIR DOUBLER ON FRAME 24-2 AT TOP LEFT SIDE OF CLIP ATTACHMENT AREA IS CRACKED. FABRICATED AND INSTALLED NEW DOUBLER PER FOKKER SRM 53-02-13 PAGES 7-8.

Part: CLIP — CRACKED (FRAME 17565)

CLIP ON FRAME 17565 AT STRINGER 15 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: DOUBLER — CRACKED (FRAME)

REPAIR DOUBLER ON FRAME 24-2 IS CRACKED. FABRICATED NEW DOUBLER AND INSTALLED PER FOKKER SRM 53-02-13 FIGURE 5.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 50-2 AT STRINGER 27 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: FAIRING — CHAFED (FUSELAGE)

AFT FUSELAGE BELLY FAIRING PANEL 91BC HAS CHAFED INTO THE FUSELAGE SKIN ALONG ITS TRAILING EDGE. REMOVED PAINT AROUND AREA, BLENDED AREA AS REQUIRED. NDT INSPECTION SHOWED NO CRACKS. WORK PERFORMED PER EA 4-53-181.

Part: PANEL — CRACKED (RUDDER)

RIGHT HAND RUDDER PANEL 57Y HAS A DOUBLER CUTOUT CRACKED. INSTALLED NEW DOUBLER PER FOKKER SRM 51-101-04.

Part: CLIP — CRACKED (FRAME)

CLIP ON FRAME 67-2 ON TOP OF LEFT AND RIGHT SKIN ATTACHMENTS, HAVE CRACKS PAST THE STOP DRILLS. FABRICATED AND INSTALLED NEW CLIPS PER FOKKER SRM 53-02-13 PAGES 5-6.

Part: PANEL — CRACKED (VERT STAB)

LEFT SIDE VERTICAL STABLIZER PANEL 57V DOUBLER CUTOUT IS CRACKED. INSTALLED NEW DOUBLER PER FOKKER SRM 51-10-04.

Part: BULKHEAD BEAM — CRACKED (FWD PRESS BLKHD)

PDX - AFT SIDE OF FORWARD PRESSURE BULKHEAD IS CRACKED AT HORIZONTAL BEAM VIII BL325L. STOP DRILLED CRACK, DRILLED UP REPAIR AND INSTALLED AD RIVETS IN NEW HOLES AND INSTALLED NEW DOUBLER PER SRM 53-02-18.

Part: WINDOW POST — CRACKED (NR 2 WINDOW)

PDX - LEFT NR 2 WINDOW POST FORWARD LOWER SILL TO WINDOW POST BRACKET IS CRACKED. INSTALLED NEW WINDOW POST BRACKET.

Part: FRAME — CRACKED (BS 3820)

PDX - RIGHT FRAME STRIP AT STATION 3820 AFT OF NOSE GEAR WHEEL BAY, HAS CRACKED. INNER FRAME STRIP HAS A CRACK TYPE 2 AT STRINGER 73. REPAIRED CRACK PER E.A. 4-53-33 A.

Part: ANGLE — CRACKED (LT MLG WW)

THE LEFT SIDE MAIN LANDING GEAR BRACKET REPAIR ANGLE IN THE BACK-UP STRUCTURE HAS A CRACK RADIATING UP FROM THE UPPER BOLT OF THE LOWER BRACKET, LOCATED INSIDE PANEL 81X. PERFORMED NDT INSPECTION AND CONFIRMED 1 CRACK COMING OUT OF THE TOP OF THE BOLT HOLE APPROX .5 INCH LONG. REWORKED THE MLG BRACKET AND ALL FASTENERS PER FOKKER SRM 52-02-09 PAGE 5.

Part: FRAME — CRACKED (BS 3820)

PDX - LEFT FRAME STRIP AT STATION 3820 AFT OF NOSE LANGING GEAR WHEEL BAY, IS CRACKED. FINGER HAS A CRACK TYPE 1. REPAIRED CRACK PER E.A. 4-53-33A.

Part: WINDOW POST — CRACKED (NR 2 WINDOW)

PDX - RIGHT NR 2 WINDOW POST FORWARD LOWER SILL TO WINDOW POST BRACKET, HAS A CRACK. INSTALLED NEW WINDOW POST BRACKET.

Part: SKIN — DAMAGED (CARGO DOOR)

PDX - FORWARD CARGO DOOR OUTER SKIN HAS A DENT APPROX .5 INCH IN DIAMETER AND APPROX .025 DEEP. FABRICATED REPAIR AND INSTALLED PER FOKKER SRM 52-20-01.

Part: FRAME — CORRODED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME 9305A HAS CORROSION ABOVE STRINGER 74. IDENTIFIED AS LEVEL 1 AND 2 CORROSION. MECHANICALLY REMOVED CORROSION PER E.A. 4-53-15.

Part: FRAME — CORRODED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME 8305 HAS EXFOLIATION TYPE CORROSION BETWEEN STRINGERS 1 AND 74. IDENTIFIED AS LEVEL 2 CORROSION. REPAIRED PER E.A. 4-53-156.

Part: FRAME — CORRODED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME 8805 HAS EXFOLIATION TYPE CORROSION UNDER TOP FRAME ANGLE BETWEEN STRINGERS 2 AND 14. IDENTIFIED AS LEVEL 2 CORROSION. SPLICED IN NEW FRAME ANGLE PER E.A. 4-53-157.

Part: FRAME — CORRODED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME 8805 HAS CORROSION UNDER TOP FRAME ANGLE AT STRINGER 73. IDENTIFIED AS CORROSION LEVEL 2. SPLICED IN NEW FRAME PER FOKKER SRM 51-30-02.

Part: FRAME — CRACKED (CARGO COMPT)

PDX - FORWARD CARGO BAY FRAME CASTELLATION ON FRAME 5805 AND BETWEEN STRINGERS 1 AND 2 IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED PER FOKKER SRM 53-02-13.

Part: SKIN — CRACKED (RT WING)

RIGHT WING SHROUD DOOR SPRING BOX BELLCRANK FOR PANEL 82M HAS A 1 INCH CRACK IN THE SKIN UNDER THE BELLCRANK OUTBOARD MOUNT. FABRICATED AND INSTALLED NEW DOUBLER PLATE PER EA 4-57-48.

Part: FRAME — CRACKED (FRAME 15205)

CRACK IN DIP BELOW STRINGER 26 ON FRAME 15205. FABRICATED AND INSTALLED REPAIR PER FOKKER SRM 51-31-01.

Part: SKIN — CRACKED (FUSELAGE)

AFT OF FRAME 10346 AT STRINGER 42 THERE IS A CRACK UNDER A RIVET. FABRICATED AND INSTALLED REPAIR PER FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: FRAME — CRACKED (FRAME 10346)

AFT SIDE OF FRAME 10346 AT STRINGER 33 IS CRACKED. FABRICATED AND INSTALLED REPAIR PER FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 AFT LEFT SIDE, AT STRINGER 34 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 AFT LEFT SIDE, ON STRINGER 33 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 4 PAGE 2.

Part: SEAT TRACK — CORRODED (CABIN)

RIGHT OUTBOARD SEAT TRACK HAS PITTING CORROSION IN THE BOTTOM OF THE CHANNEL BETWEEN FRAMES 13815B AND 14285. IDENTIFIED AS LEVEL 1 (LOCAL) AND LEVEL 2 TYPE CORROSION. REMOVED CORROSION PER FOKKER SRM 51-10-04 AND EA 4-53-173.

Part: RIVET — LOOSE (FRAME 13345)

AT FRAME 13345 ON THE LEFT SIDE FORWARD, AT FLOOR LEVEL. THERE ARE 2 RIVETS THAT ARE IMPROPERLY INSTALLED (UNDER BUCKED TAILS). REMOVED AND REPLACED RIVETS PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 BELOW UPPER NACELLE STUBWING LONGERON, BELOW STRINGER 24 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP IN FRAME 15205 BELOW LOWER NACELLE STUB WING LONGERON, ABOVE STRINGER 21A IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 21A IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

CLIP ON FRAME 15205 AT STRINGER 18 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-12 PAGE 4 FIGURE 1.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 21 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 48 IS CRACKED. FABRICATED NEW CLIP AND INSTALLED PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 BELOW STRINGER 49 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 14775 AT STRINGER 49 IS CRACKED. FABRICATED AND INSTALLED A DOUBLER PER FOKKER SRM 53-02-12 PAGE 4 FIGURE 1.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 AFT LEFT SIDE, AT STRINGER 31 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME 12875)

AT FRAME 12875 ON THE RIGHT SIDE AT STRINGER 44 THERE IS A CLIP THAT IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME 12875)

CLIP ON FRAME 12875 ON LOWER SIDE OF STRINGER 44 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: SKIN — CRACKED (EMER EXIT DOOR)

THE UPPER FORWARD CORNER OF THE RIGHT FORWARD OVERWING EXIT IS CRACKED. PERFORMED NDT OF AREA AND IDENTIFIED CRACK AS .5 INCH LONG. FABRICATED AND INSTALLED REPAIR PER FOKKER SRM 52-02-03 FIGURE 6.

Part: CLIP — CRACKED (FRAME 10966)

CLIP ON FRAME 10966 AT STRINGER 43 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 14755 AT STRINGER 19 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 10966)

CLIP ON FRAME 10966 ON LEFT SIDE AT STRINGER 31 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

CLIP ON FRAME 15205 AT STRINGER 28 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 ABOVE LOWER STUB WING LONGERON ABOVE STRINGER 53A. FABRICATED NEW CLIP AND INSTALLED PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FRAME 10966)

CLIP ON FRAME 10966 AT STRINGER 32 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAM 15205 AT STRINGER 55 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: SKIN — DENTED (CARGO DOOR)

PDX - AFT CARGO DOOR EXTERIOR SKIN DENT ABOVE WEB, MEASURES .035 BY .900 OUT OF SRM LIMITS. FABRICATED AND INSTALLED REPAIR PER E.A. 4-52-65.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 50 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 54 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 ABOVE UPPER NACELLE STUB WING LONGERON, BELOW STRINGER 24 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 AFT LEFT SIDE, AT STRINGER 35 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 19 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 14755 AT STRINGER 26 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 2.

Part: SKIN — DENTED (CARGO DOOR)

PDX - AFT CARGO DOOR EXTERIOR SKIN DENT BELOW WEB, MEASURES .038 BY .700 OUT OF SRM LIMITS. FABRICATED AND INSTALLED REPAIR PER E.A. 4-53-65.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 ABOVE STRINGER 49 IS CRACKED. FABRICATEED NEW CLIP AND INSTALLED PER FOKKER SRM 51-31-01.

Part: SKIN — CRACKED (EMER EXIT DRWAY)

LEFT FORWARD OVERWING EMERGENCY EXIT APERTURE HAS A CRACK IN THE EXTERNAL SKIN AT THE LOWER FORWARD CORNER. FABRICATED REPAIR AND INSTALLED PER EA 4-53-160.

Part: CLIP — CRACKED (FRAME 10966)

CLIP ON FRAME 10966 AT STRINGER 33 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 AFT LEFT SIDE AT STRINGER 32 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-03-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

CLIP ON FRAME 12405 LEFT SIDE AFT, ON STRINGER 29 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: ANGLE — CRACKED (FRAME 13345)

AT FRAME 13345 CRACK FOUND EXTENDING FROM RIVET TO CORNER EDGE OF ANGLE. REPAIRED ANGLE PER EA 4-53-171.

Part: CLIP — CRACKED (FRAME 15205)

CLIP ON FRAME 15205 ABOVE STRINGER 26 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 58A IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 20 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 14755 AT STRINGER 18 IS CRACKED. FABRICATED NEW CLIP AND INSTALLED PER FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 14755 AT STRINGER 27 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 2.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 AT STRINGER 56 IS CRACKED. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13.

Part: CLIP — CRACKED (FUSELAGE)

PDX - CLIP ON FRAME 15205 BELOW UPPER STUB WING LONGERON, BELOW STRINGER 51 IS CRACKED. FABRICATED NEW CLIP AND INSTALLED PER FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

CRACK IN CLIP AT FRAME 15205 ABOVE LOWER STUB WING LONGERON ABOVE STRINGER 53A. FABRICATED AND INSTALLED NEW CLIP PER FOKKER SRM 53-02-13 FIGURE 2.

Part: STRINGER — CRACKED (FUSELAGE)

PDX - LEFT SIDE BOX STRINGER NR 3 HAS A 1.50 CRACK AT FRONT PRESSURE BULKHEAD, JUST ABOVE CONNECTING ANGLE. REPAIRED CRACK AS PER E.A. 4-53-180.

Part: BULB — FAILED (CABIN)

GALLEY 28 VOLT EMERGENCY EVACUATION LIGHT IS INOP. RELAMPED, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

LEFT HAND EMERGENCY EXIT LIGHT INOP, 3 VOLT BULB. RELAMPED, OPERATIONAL CHECKS GOOD.

Part: BULB — BURNED (CABIN)

OVERHEAD EMERGENCY EVACUATION LIGHTS AT ROW NUMBERS 13 AND 14 ARE INOP. REPLACED BURNED BULBS, OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

SEA- TWO AFT UNDER WING EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: CABLE — LACK OF LUBE (PAX DOOR)

MAIN CABIN DOOR FAILED TO OPEN ELECTRICALLY. DE-CLUTCHED CABLE AT DOOR ACTUATOR. FOUND CABLE TO BE STUCK. FREED CABLE AND LUBRICATED, OPERATIONAL CHECK OF DOOR GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONING (AFT LAVATORY)

SEA - LAV SMOKE DETECTOR SOUNDED IN-FLIGHT. NO VISABLE SMOKE NOTED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. SMOKE DETECTOR REPLACED AND UNIT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — SMOKING (TAIL)

PDX - FLIGHT CREW NOTED SMOKE COMING FROM AIR CONDITIONING VENTS. AIRCRAFT WAS AT THE GATE FOR 45 MINUTES WITH NO PROBLEM, THEN WHEN BOARDING, FLIGHT CREW NOTICED SMOKE BEGAN SLOWLY (COCKPIT OFF CABIN ON). APU REPLACED I/A/W MAINTENANCE MANUAL AND APU OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

GEG - SEVERAL OVERHEAD EMERGENCY LIGHTS IN THE CABIN ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN)

FORWARD EMERGENCY EXIT SIGN IN GALLEY HAS SEVERAL LIGHTS INOP. CIRCUIT BOARD WAS REPLACED AND SIGN OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT AT ROW 8 STARBOARD SIDE IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

FLOOR PROXIMITY LIGHT AT SEAT 6A IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

LOWER EXIT LIGHT BY RIGHT HAND FORWARD EXIT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

THREE EMERGENCY LIGHT IN THE CABIN OVERHEAD ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EVAC LIGHT AT ROW 2 AND 4 ARE INOP. NR 4 BATTERY PACK REPLACED AND LIGHTS OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

EXIT LIGHT ABOVE SEAT 8C ISN'T ILLUMINATED WHEN THE EMERGENCY LIGHTS ARE ARMED. BULB WAS REPLACED, LIGHT OPS CHECKED GOOD.

Part: BULBS — FAILED (CABIN)

SEA - SEVERAL EMERGENCY BULBS ARE INOPERATIVE IN AISLE EXIT SIGN AT ROW 8. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PDX - FORWARD HALF OF CABIN EVACUATION LIGHTS INOPERATIVE. POWER SUPPLY NRS 2 AND 3 REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (CABIN)

CLT - MX FOUND THE AFT EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE AFT EXTERIOR POWER SUPPLY UNIT. (M)

Part: ANGLE — CRACKED (VERT STAB)

PIT - DURING FC-2 CHECK INSPECTION, FOUND 5 .125 INCH LONG CRACKS, 3 IN VERTICAL STAB CONNECTION ANGLE INTERMEDIATE SPAR II AND 2 IN INTERMEDIATE SPAR I CONNECTION ANGLE RT. CONFIRMED VISUAL BY EDDY CURRENT. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-31-00 PG 2. (W)

Part: ANGLE — CRACKED (FWD PRES BLKD)

PIT - DURING FC- CHECK INSPECTION, FOUND 4 INCH CRACK BETWEEN STRINGER 72 AND 74 AFT SIDE OF FORWARD PRESSURE BULKHEAD CONNECTION ANGLE. SIP INSPECTION REF 53-10-06. STOP DRILLED CRACK FABRICATED AND INSTALLED NEW CONNECTION ANGLE DOUBLER PER SRM 53-11-08 PG 2. (W)