N497US

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,030 hrs · 44,778 cycles

PDX- MID CABIN EXIT CEILING LIGHT HAS NUMEROUS BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 34,983 hrs · 44,734 cycles

PDX - FLIGHT 2430 - MAIN CABIN DOOR DIFFICULT TO OPERATE IN BOTH DIRECTIONS. OPEN BUTTON DOES NOT RESPOND UNLESS THE DOOR HANDLE IS CYCLED SEVERAL TIMES. MAINTENANCE INSPECTED THE DOOR AND LUBRICATED THE LATCHING AND LOCKING MECHANISM. THE MAIN CABIN DOOR SEAL WAS LUBRICATED ALSO. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT CARD — DEFECTIVE (CABIN) · airframe 34,561 hrs · 44,384 cycles

PDX-EMERGENCY EXIT SIGN OVER COCKPIT ENTRY WAY HAS BULBS BURNT OUT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FASTENER — LOOSE (LT WING) · airframe 34,348 hrs · 44,204 cycles

PDX- CLASS THREE FUEL SEEP FROM LEFT HAND NR 5 LIFT DUMPER BELLCRANK FITTING, LOWER SIDE UPPER OUTBOARD HI-LOK. REPAIRED IAW F-28 SRM 28-11-0-5 AND 27-50-5.

Part: CONTROL UNIT — BURNED (ZONE 200) · airframe 34,165 hrs · 44,043 cycles

BOI-SMOKE IN COCKPIT-ELECTRICAL SMELL. FOUND STRONG BURNT SMELL FROM GENERATOR POWER CONTROL UNIT. NO OTHER DEFECTS NOTED. GROUND RAN ENGINES AND PERFORMED AC GENERATOR SYSTEM WITH NO DEFECTS NOTED. REPLACED EXTERNAL POWER CONTROL UNIT AND EXTERNAL POWER CONTACTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 34,111 hrs · 43,997 cycles

PDX-ONE COCKPIT EMERGENCY LIGHT UNDER GLARESHIELD ON F/O'S SIDE FAILS TO ILLUMINATE WHEN SELECTED ON. REPLACED 3RD FROM RIGHT EMERGENCY LIGHT ASSEMBLY UNDER GLARESHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (ZONE 100) · airframe 34,065 hrs · 43,961 cycles

SEA-REAR FACING PORTION OF EXIT SIGN IS INOPERATIVE AT EMERGENCY EXIT ROE. REMOVED AND REPLACED EXIT SIGN AT EMERGENCY EXIT ROW. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (CABIN) · airframe 33,982 hrs · 43,895 cycles

PDX- MID CABIN CEILING EMERGENCY EXIT SIGN HAS BULBS BURNED OUT. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,915 hrs · 43,839 cycles

PDX- LIGHT OUT ON EXIT SIGN OVER ROW 8. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 33,907 hrs · 43,828 cycles

PDX- THERE IS A SCRATCH IN THE FUSELAGE SKIN ABOVE THE RIGHT HAND STUBWING. REPAIRED IAW F-28 SRM 53-01-01 PAGE 3.

Part: STRUCTURE — CHAFED (SERVICE DOOR) · airframe 33,907 hrs · 43,828 cycles

PDX- SERVICE EMERGENCY DOOR TOP FORWARD CORNER IS CHAFED. REPAIRED IAW F-28 SRM 51-31-01 AND SRM 51-10-05.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 33,907 hrs · 43,828 cycles

PDX- CORROSION ON FORWARD ENGINE MOUNT BEAM NR 2 SIDE. REPAIRED IAW FOKKER 20-20-05 AND 54-40-03, PG 201.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,810 hrs · 43,745 cycles

SEA- EXIT SIGN ABOVE COCKPIT DOOR HAS BULBS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,483 hrs · 43,458 cycles

BOI- EXIT LOCATING SIGN AT GALLEY ENTRANCE HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,472 hrs · 43,452 cycles

BOI - EMERGENCY EXIT SIGN IS INOPERABLE AT FORWARD ROW. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PIN — DAMAGED (CABIN) · airframe 33,450 hrs · 43,434 cycles

PDX - ESCAPE PATH LIGHTS ON ROWS 1 THROUGH 4 WILL NOT RESET. REMOVED AND REPLACED CONNECTOR PIN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPLICE — BROKEN (CABIN) · airframe 33,450 hrs · 43,434 cycles

PDX - ROWS 1, 2, AND 3 EVACUATION LIGHTS STAY ON WITH BATTERY SHUTDOWN. REPAIRED BROKEN SPLICE ON THE ARM WIRE FOR THE FORWARD BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 33,316 hrs · 43,319 cycles

PDX - EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR IN GALLEY AREA HAS MULTIPLE LAMPS BUNED OUT. REPLACED CURCUIT BOARD IN EMERGENCY EXIT SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,223 hrs · 43,236 cycles

PDX - NUMBER 3 EMERGENCY EXIT LIGHT IS BURNED OUT. REMOVED AND REPLACED EXIT LIGHT PANEL IAW F-28 MAINTENANCE MANUAL CHAPTER 33-24-00 PAGE 205-206, SECTION 6, PARAGRAPH A AND B. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 32,892 hrs · 42,960 cycles

PDX- EXIT SIGN AT CABIN ENTRY DIM. MAINTENANCE REPLACED SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — STUCK (HORIZONTAL STAB) · airframe 32,833 hrs · 42,905 cycles

LAX - DURING CLIMB, FLIGHT CREW NOTED HORIZONTAL STABILIZER CHANNEL WARNING LIGHTS ILLUMINATED. FOUND SPRING BOX STICKING SWITCH OUT OF ADJUSTMENT. MADE PROPER ADJUSTMENTS, NO PARTS REPLACED. FUNCTIONALLY CHECKED STABILIZER MOVEMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SELECTOR VALVE — LEAKING (NLG) · airframe 32,139 hrs · 42,291 cycles

BOI - FLIGHT CREW REPORTED UNSAFE GEAR INDICAION DURING EXTENTION CYCLE UPON APPROACH. CYCLED GEAR, NO CHANGE IN INDICATION. CREW USED ALTERNATE GEAR EXTENTION METHOD. GEAR EXTENDED AND INDICATED DOWN AND LOCKED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR SELECTOR VALVE SHAFT LEAKING. REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE. OPERATIONAL GEAR SWINGS CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROD — CRACKED (T/E FLAP) · airframe 32,110 hrs · 42,262 cycles

YYC-LEFT HAND WING STATION 7306 TRAILING EDGE STRUT ROD CRACKED. REPAIRED IAW FOKKER SRM 51-31-05, PAGE 8, 9 AND HORIZON AIR EA 4-57-540.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-GOUGED SKIN AT FORWARD LOWER REAR CARGO DOOR APERTURE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 7 AND SRM 51-10-04.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 32,110 hrs · 42,262 cycles

YYC-LEFT HAND AILERON TRAILING EDGE HAS 5 DISBONDS FROM OUTBOARD END AT EXITING DOUBLER ON TOP SKIN. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 13 AND SRM 57-50-41, PAGE 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 22293 AT STRINGER 21A. REPAIRED IAW HORIZON AIR EA 4-53-1458.

Part: POST — IMPROPER (AFT GALLEY) · airframe 32,110 hrs · 42,262 cycles

YYC-AFT GALLEY CENTER FREIGHT POST LOWER ATTACHMENT TO FLOOR STRUCTURE IN NON CONFORMANCE, ALSO LOWER END OF FREIGHT POST IS IN CONTACT WITH GUSTLOCK CABLE RUN. REPAIRED IAW HORIZON AIR EA 4-53-1457.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 32,110 hrs · 42,262 cycles

YYC-LEFT HAND AILERON TRAILING EDGE HAS DELAMINATION FROM OUTBOARD END AT EXITING DOUBLER. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 14 AND SRM 57-50-41, PAGE 1.

Part: FRAME — CHAFED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FRAME 41-2 CHAFING ON STRINGER 54. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 7 AND SRM 53-02-01, PAGE 7, AND SRM 51-31-01, PAGE 13, 14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN AFT OF FRAME 32-2 BETWEEN STRINGER 5 & 7 DAMAGED. REPAIRED IAW FOKKER SRM 53-02-02 AND SRM 53-00-00, PAGE 2.

Part: DOUBLER — MISINSTALLED (RUDDER) · airframe 32,110 hrs · 42,262 cycles

YYC-RUDDER ACCESS PANEL 57V DOUBLER PLATE WAS INCORRECTLY INSTALLED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 20075 AT STRINGER 40. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, AND SRM 53-10-05, PAGE 601, AND SRM 51-30-02, PAGE 9, 10.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-DENTS FOUND ON LEFT HAND SIDE OF ZONE 400 AT FRAME 18075. REPAIRED IAW FOKKER SRM 53-02-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 5. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-26-04.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-RIGHT HAND FUSELAGE HAS SHARP DENT LOCATED 5 INCHES DOWN AND 4 INCHES IN FROM TRAILING EDGE OF RIGHT HAND STUBWING. REPAIRED IAW FOKKER SRM 53-02-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN AROUND ACCESS PANEL 41B DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-1453.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 24-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05, PAGE 601 AND SRM 51-30-02, PAGE 9, 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 68. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: FLANGE — CRACKED (SERVICE DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK ON SERVICE EMERGENCY DOOR INNER FLANGE UPPER AFT CORNER. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 66. REPAIRED IAW FOKKER SRM 53-26-01 AND SRM 53-02-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 16-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 41-2 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-01, PAGE 13, 14, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 20075 AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13, SRM 53-10-05, PAGE 601, AND SRM 51-30-02, PAGE 9, 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 9. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 41-2 AND STRINGER 64. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 58.5 AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, SRM 53-10-05, PAGE 601, AND SRM 51-30-02, PAGE 9, 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-SLIGHT CORROSION FOUND UNDER LOWER VHF COMM ANTENNA FORWARD POSITION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND HORIZON AIR EA 4-53-1454.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 24-2 AT STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 53-10-05, PAGE 601, AND SRM 51-30-02, PAGE 9, 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 58.5 AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, SRM 53-10-05, PAGE 601, AND SRM 51-30-02, PAGE 9, 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AND STRINGER 9. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: FRAME — CHAFED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CHAFING FOUND ON FRAME 18075 BETWEEN STRINGER 19 AND 20. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 53-25-04.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND AT FRAME 32-2 AND STRINGER 11. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-LEFT HAND FUSELAGE HAS A SHARP DENT BETWEEN FRAME 50-2 AND STRINGER 6-8 APPROXIMATELY WL 220. REPAIRED IAW FOKKER SRM 53-02-06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AND STRINGER 7. REPAIRED IAW FOKKER SRM 53-26-04 AND SRM 53-02-13.

Part: BUSHING — WORN (SPEED BRAKE) · airframe 32,110 hrs · 42,262 cycles

YYC-SPEED BRAKE ACTUATOR TO TOWER SUPPORT BUSHINGS WORN. REPAIRED IAW HORIZON AIR EA 4-53-1456.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-30-02, AND SRM 53-10-05.

Part: PRESSURE PANEL — DENTED (NLG WW) · airframe 32,110 hrs · 42,262 cycles

YYC-NOSE LANDING GEAR BAY RIGHT HAND SIDEWALL HAS DENTS IN SKIN AT UPPER FORWARD AND AFT ACM ATTACH AREAS. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 29 AND HORIZON AIR EA 4-53-1452.

Part: FITTING — LOOSE (RT SPOILER) · airframe 32,110 hrs · 42,262 cycles

YYC-RIGHT HAND NR 2 LIFT DUMPER SPIGOT LOOSE IN SPAR BRACKET. REPAIRED IAW FOKKER SRM 27-63-00, PAGE 402 AND HORIZON AIR EA 4-57-546.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN AROUND ACCESS PANEL 41C DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-1453.

Part: DOUBLER — CRACKED (RUDDER) · airframe 32,110 hrs · 42,262 cycles

YYC-RUDDER ACCESS PANEL 57V DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-UPPER FLUTTER DAMPER BOLT TOO LONG AND HAS WORN SUPPORT STRUCTURE ABOVE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14, AND HORIZON AIR EA 4-35-282.

Part: RIB — CRACKED (RUDDER) · airframe 32,110 hrs · 42,262 cycles

YYC-RUDDER RIBS 3, 4, 5 CRACKED AND OR BROKEN. REPAIRED IAW FOKKER SRM 55-40-04, SRM 51-31-01, AND SRM 51-31-02.

Part: DOUBLER — CRACKED (RUDDER) · airframe 32,110 hrs · 42,262 cycles

YYC-RUDDER ACCESS PANEL 57Y RIGHT HAND DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-31-01, AND SRM 53-10-05, PAGE 601.

Part: STRUCTURE — PUNCTURED (CARGO DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-PUNCTURE AT AFT LOWER RADIUS OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14, AND SRM 51-31-03, PAGE 10, 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, AND SRM 51-31-01 PAGE 13, 14, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 17. REPAIRED IAW FOKER SRM 53-02-13, PAGE 5, SRM 51-31-01, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 51-31-01, PAGE 13, 14, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 32-2 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-31-01, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, SRM 51-31-01, PAGE 13, 14 AND SRM 53-10-05, PAGE 601.

Part: ANGLE — BROKEN (CARGO DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-BROKEN REINFORCEMENT ANGLE AT AFT LOWER CORNER OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 51-31-03, PAGE 10, 11 AND SRM 52-30-00.

Part: PRESSURE PANEL — MISALIGNED (NLG WW) · airframe 32,110 hrs · 42,262 cycles

YYC-NOSE LANDING GEAR BAY LEFT HAND SIDEWALL STATION 2650 LOWER CONNECTION ATTACH IS SITTING HIGH ON LOWER AFT CORNER AND HI-LOK HOLES. REPAIRED IAW FOKKER SRM 53-11-00 AND SRM 51-31-01, PAGE 13 & 14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 11. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 9. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601.

Part: ANGLE — BROKEN (CARGO DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-BROKEN REINFORCEMENT ANGLE AT FORWARD LOWER CORNER OF REAR CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00 AND SRM 51-31-03, PAGE 10, 11.

Part: DOOR — CORRODED (A/C SERVICE DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-CORROSION FOUND IN HOLES AROUND PANEL 25C (GROUND SUPPLY AIR CONDITIONING SERVICE DOOR). REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 8. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 15 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 21. REPAIRED IAW FOKKER SRM 51-30-02, PAGE 9,10 AND SRM 51-31-01, PAGE 13,14, SRM 53-10-05, PAGE 601, AND SRM 53-25-04, PAGE 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 52. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20 AND SRM 51-31-01, PAGE 13, 14, AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-25-04, PAGE 5, AND SRM 51-31-01, SRM 53-10-05, 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 24. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20 AND SRM 51-31-01, PAGE 13, 14 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 7. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 50. REPAIRED IAW FOKKER SRM 53-26-04, PAGE 20, AND SRM 51-31-01, PAGE 13, 14 AND SRM 53-10-05, PAGE 601.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-10-05, PAGE 601, AND SRM 51-31-01, PAGE 13, 14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 17565 AT STRINGER 53A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 53-25-04, PAGE 5, AND SRM 53-10-05, PAGE 601 AND SRM 51-31-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK FOUND ON FRAME 50-2 AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-26-04, SRM 51-31-01, SRM 53-10-05, PAGE 601.

Part: WEB — MISREPAIRED (NLG WW) · airframe 32,110 hrs · 42,262 cycles

YYC-NOSE LANDING GEAR BAY RIGHT HAND SIDE NON STANDARD REPAIR SIDE BOX WEBPLATE. REPAIRED IAW FOKKER SRM 53-11-00 AND SRM 53-11-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-SKIN UNDER AFT DME ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND SRM 53-01-01, PAGE 3, SRM 51-10-04, PAGE 7.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,110 hrs · 42,262 cycles

YYC-CABIN SEAT RAIL LEFT HAND HAS MINOR CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 7 AND SRM 51-10-04, PAGE 9.

Part: STRINGER — CRACKED (RUDDER) · airframe 32,110 hrs · 42,262 cycles

YYC-RUDDER STRINGER 10 CRACKED AT RIB 4. REPAIRED IAW FOKKER SRM 55-02-07, PAGE 3.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACK ON HORIZONTAL STIFFENER ON AFT SIDE OF FRAME 3870 ABOVE LEFT HAND BLEED AIR DUCT ACCESS THROUGH FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 53-03-01, PAGE 7 AND SRM 51-31-01, PAGE 14.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 32,110 hrs · 42,262 cycles

YYC-SKIN CRACKED AT CENTER CARGO DOOR HANDLE TORSION BOX. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN UNDER FORWARD RADIO ALTIMETER ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 53-01-01, PAGE 3, SRM 51-10-04, PAGE 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN UNDER AFT RADIO ALTIMETER ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3 AND SRM 51-10-04, PAGE 7, SRM 53-15-01.

Part: SKIN — CHAFED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FUSELAGE SKIN CHAFED AT LOWER EDGE OF FUSELAGE FAIRING 91BD. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AND SRM 51-10-04, PAGE 7.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-DENT FOUND BETWEEN STRINGER 60 AND 61 FRAME 7305 AND FRAME 7805 ON RIGHT HAND SIDE OF FUSELAGE. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, AND SRM 53-17-03, PAGE 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-SKIN UNDER LOWER ATC ANTENNA HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 53-15-01, AND SRM 51-10-04, PAGE 7.

Part: PAN — CORRODED (LAVATORY) · airframe 32,110 hrs · 42,262 cycles

YYC-CORROSION ON BOTTOM OF LAV DRAIN TUB INSIDE AFT CARGO PIT. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-01, PAGE 6, AND SRM 51-10-04, PAGE 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CORROSION FOUND UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, AND SRM 51-01-01, PAGE 3, SRM 53-15-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 32,110 hrs · 42,262 cycles

YYC-CABIN SEAT RAIL RIGHT HAND INBOARD HAS MINOR CORROSION. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 7.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-FORWARD RADIO ALTIMETER BLANKING PLATE SKIN CUTOUT HAS MINOR SURFACE CORROSION STATION 386.023, BLI, WL-64.960. REPAIRED IAW FOKKER SRM 53-01-01, AND SRM 51-10-04, PAGE 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 9305 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 5805 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 9305C AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 20.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CASTELLATION CLIP ON FRAME 13815 AT STRINGER 42 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CASTELLATION CLIP ON FRAME 13815 AT STRINGER 43 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 8305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 7805 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CASTELLATION CLIP ON FRAME 12405 AT STRINGER 31 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 53-21-01, PAGE 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CASTELLATION CLIP ON FRAME 12405 AT STRINGER 33 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-21-04, PAGE 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 9305C AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 53-16-04, PAGE 20.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 9305A AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 9305B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-16-04, PAGE 20 AND SRM 53-02-13, PAGE 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-CRACKED CASTELLATION AT FRAME 8805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 13 AND SRM 53-16-04, PAGE 16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-LONGITUDINAL BUTT JOINT CRACKED BETWEEN FRAME 3850 - 3960 AND STRINGER 61, FOUND CRACK AT STATION 4460. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-30-03.

Part: SPAR — CORRODED (LT WING) · airframe 32,110 hrs · 42,262 cycles

YYC-LEFT HAND WING FRONT SPAR CAPS (UPPER AND LOWER) HAVE LIGHT FRETTING BETWEEN STATION 1825 AND 6440. REPAIRED IAW FOKKER SRM 57-01-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,110 hrs · 42,262 cycles

YYC-DENT FOUND TO BE BEYOND LIMITS, NON FLUSH REPAIR. REPAIRED IAW FOKKER SRM 53-02-02, AND SRM 53-01-01, PAGE 8.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 31,608 hrs · 41,790 cycles

PDX-ROW 2 AND 4 CABIN CEILING EMERGENCY EVACUATION LIGHTS DIM. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,548 hrs · 41,733 cycles

SEA - 4 CENTER ISLE EXIT SIGNS FOUND TO HAVE MULTIPLE BURNT OUT LAMPS. REMOVED AND REPLACED ALL 4 EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 31,486 hrs · 41,675 cycles

PDX-SEAT 6AB EMERGENCY PATH LIGHT BROKEN OUT OF SEAT TRIM. REMOVED AND REPLACED SEAT TRIM ASSY WITH EMERGENCY PATH LIGHT. LIGHT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PIN — INOPERATIVE (PAX DOOR) · airframe 31,407 hrs · 41,599 cycles

HLN- FLIGHT ATTENDANT UNABLE TO OPEN MAIN CABIN DOOR ON ARRIVAL. BY EXERTING SIGNIFICANT FORCE ON DOOR HANDLE TO CONTACT MICROSWITCH, WERE ABLE TO OPEN IT ELECTRONICALLY. REMOVED AND REPLACED SLIDING BACK-UP PIN ON MAIN CABIN DOOR. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,295 hrs · 41,493 cycles

SEA - MULTIPLE EMERGENCY EXIT LIGHTS DIM IN CABIN. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 30,883 hrs · 41,095 cycles

PDX- F/A REPORTED EXIT SIGN IN CEILING ABOVE GALLEY INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 30,874 hrs · 41,085 cycles

GEG - ON CLIMBOUT THROUGH 10,000 FEET, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. SILENCED ALARM, SHUT DOWN ENGINE PER EMERGENCY CHECKLIST, BOTTLES NR 1 AND 2. BOTH FIRE LIGHTS REMAINED ILLUMINATED. MADE SINGLE ENGINE EMERGENCY LANDING IN GEG WITH OUT INCIDENT. NO FIRE DAMAGE WAS FOUND UPON INSPECTION. CLEANED FIRE LOOP CONNECTORS. REPLACED EXTENDABLE SQUIB CARTIRAGE AND EXTINGISHING BOTTLES. COMPLIED WITH HIGH POWER ENGINE RUNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 30,732 hrs · 40,943 cycles

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

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 30,732 hrs · 40,943 cycles

SEA- EXIT SIGN ABOVE COCKPIT HAS INOPERATIVE BULBS. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (GALLEY) · airframe 30,467 hrs · 40,673 cycles

EXIT SIGN IN CEILING NEXT TO GALLEY INOPERATIVE. REPLACED LIGHTING PANEL, LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 30,367 hrs · 40,574 cycles

GEG - AFT PORTION OF THE EMERGENCY EXIT SIGN ABOVE ROW 8 WAS FOUND INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,320 hrs · 40,531 cycles

GEG - FORWARD HALF OF OVERHEAD ROW 8 EXIT SIGN FOUND INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,320 hrs · 40,531 cycles

GEG- EMERGENCY EXIT SIGN FORWARD OF ROW 8 INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 30,173 hrs · 40,382 cycles

SEA- EXIT SIGN ABOVE COCKPIT DOOR IS INOPERATIVE. REPLACED EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (EXIT SIGN) · airframe 29,664 hrs · 39,912 cycles

GEG - OVERHEAD EMERGENCY EXIT SIGN AT MID CABIN HAS BURNED OUT LIGHTS. REPLACED FORWARD FACING LIGHT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 29,655 hrs · 39,913 cycles

BOI - 28V EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (ROW 9)

GEG - EXIT LIGHT AT CHAIR 9B WAS REPORTED LOOSE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK GOOD.. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (LAVATORY)

BOI- FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR COMING FROM THE LAVATORY. FUEL BOOST PUMP CIRCUIT BREAKER OPENED AT THE SAME TIME. DID NOT RESET BREAKER. UPON LANDING, MAINTENANCE INSPECTION DID NOT REVEAL ANY ABNORMALITIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — MALFUNCTIONED (CABIN)

GEG - EMERGENCY EXIT SIGN, FACING AFT HAD 4 INOPERATIVE BULBS AT ROW 8. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN)

PDX - FORWARD CABIN EXIT SIGN WAS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAILED (FUEL CROSSFEED)

PDX- DURING FLIGHT, RIGHT HAND FUEL CROSSFEED VALVE WOULD NOT OPEN. REMOVED AND REPLACED CROSSFEED VALVE, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN)

BOI- EXIT SIGNS IN GALLEY AND CABIN ARE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN POWER SUPPLIES, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOP (ROW 9E)

BOI- EMERGENCY LIGHT AT ROW 9E INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — INOP (CABIN)

LEFT HAND OVERWING EXIT SIGN HAS INOPERATIVE LIGHTS. REMOVED AND REPLACED NR 5 POWER SUPPLY, OPERATIONAL CHECK GOOD.

Part: CIRCUIT BOARD — FAILED (COCKPIT DOOR)

PDX- EXIT LIGHT OVER COCKPIT DOOR HAS LIGHT INOPERATIVE. REPLACED CIRCUIT BOARD, OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RECEPTICAL — FAILED (GALLEY)

PDX - STRONG OR BURNING ODOR COMING FROM AREA OF LOWER COFFEE JUG. MX PULLED AND COLLARED CIRCUIT BREAKER FOR LOWER COFFEE JUG AND PLACED ON MEL. MEL CLEARED ON 7/2/99 BY REPLACING THE PLUG-IN RECEPTICLE FOR THE LOWER COFFEE JUG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (EXTERIOR)

PDX- RIGHT HAND AFT WING/BELLY FAIRING EVACUATION LIGHT INOPERATIVE. CLEANED CONTACTS FOR RIGHT HAND AFT WING/BELLY FAIRING LAMP SOCKET. NO PARTS REPLACED, OPERATIONAL CHECK GOOD.

Part: COALESCER — DIRTY (CABIN)

PDX- OIL SMELL IN COCKPIT WITH APU AIR OFF. REMOVED AND REPLACED ACM WATER SEPARATOR SOCKS. VERIFIED PROPER ACM OIL SERVICE. GROUND RUN CHECK GOOD AT VARIOUS SETTINGS.

Part: LIGHT — INOPERATIVE (CABIN)

PDX- EMERGENCY LIGHTS IN CABIN OVERHEAD WILL NOT TEST. AIRCRAFT IN C-CHECK.

Part: SKIN — CORRODED (FRAME 18075)

PDX - CORROSION BETWEEN FRAME 18075 AND 17565 AT STRINGER 58. REMOVED SURFACE CORROSION, ALODINED AND PRIMED.

Part: SEAT TRACK — CORRODED (FRAME 9805-14285)

PDX - RIGHT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 114285 HAS LIGHT FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: SEAT TRACK — DAMAGED (CABIN)

PDX - LEFT INBOARD PASSENGER SEAT TRACK SECTIONS FROM FRAME 5305 TO 9805, FRAME 9802 TO 14285 AND FRAME 14285 AND 15635 REQUIRE REPLACEMENT. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SEAT TRACK — SCRATCHED (FRAME 14755)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT SCRATCHES INSIDE IN A 2 INCH AREA ADJACENT TO FRAME 14755. REPAIRED IAW FOKKER SRM 53-01-01.

Part: SEAT TRACK — CORRODED (FRAME 5305-9805)

PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN FRAME 5305 AND 9805 HAS PITTING AND FRETTING CORROSION ON FLANGES ALONG ENTIRE LENGTH. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SILL — CHAFED (PAX DOORWAY)

PDX - MAIN CABIN DOOR SILL FORWARD LOWER CORNER IS CHAFED. REPAIRED IAW FOKKER SRM 53-01-01.

Part: SEAT TRACK — CORRODED (FRAME 9805-14285)

PDX - LEFT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 14285 HAS PITTING AND FRETTING CORROSION ALONG ENTIRE LENGTH ON FLANGES. REPAIRED IAW FOKKER SRM 51-31-01.

Part: JAMB — CHAFED (FRAME 4610)

PDX - TWO CHAFES AT SERVICE EMERGENCY DOOR APERTURE IN FRAME 4610 OUTBOARD OF MAIN GUIDE TRACK. REPAIRED IAW HORIZON AIR EA 4-53-752.

Part: BULKHEAD WEB — CRACKED (AFT PRESS BLKHD)

PDX - REAR PRESSURE BULKHEAD WEB IS CRACKED IN TWO PLACES ABOVE HORIZONTAL BEAM I AT BL 575R AND BL 765R. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 39 AND 40.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL ACCESS PANEL 73C HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL PANEL 73D HAS SURFACE CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PARAGRAPH 3A, STEPS 1-10.

Part: RIB — CRACKED (HORIZ STAB)

PDX - THERE IS A CRACK AT THE LOWER, AFT EDGE, OF RIB NR 4, ON THE HORIZONTAL STAB LEADING EDGE PANEL NR 51E. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-130.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFTWING FUEL ACCESS PANEL 73A HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PARAGRAPH 3A, STEPS 1-10.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL PANEL 71A HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PARAGRAPH 3A, STEPS 1-10.

Part: JAMB — CHAFED (CARGO DOORWAY)

PDX - THE CENTER CARGO DOOR AFT APERTURE HAS CHAFE DAMAGE 10 INCHES LONG AT THE OUTBOARD EDGE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-04.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PDX - RIGHT OUTBOARD PASSENGER SEAT TRACKS FROM SECTION 4875 TO 5305, FRAME 5305 TO FRAME 9805 AND FRAME 14285 TO FRAME 16535 REQUIRED REPLACEMENT. REPLACED IAW FOKKER SRM 51-31-01 AND 51-10-5.

Part: FLOORBEAM — DAMAGED (FRAME 16660)

PDX - MAIN CABIN FLOORBEAM STRUCTURE IS DISTORTED BETWEEN FRAME 16660 AND 16060. REPAIRED IAW HORIZON AIR EA 4-53-713.

Part: STRAP — GOUGED (WING)

PDX - SCREW GOUGE IN LOWER WING BUTT STRAP AT FORWARD END. REPAIRED IAW HORIZON AIR EA 4-57-226, STEP 2.

Part: BEAM — WORN (FRAME 12075)

PDX - LEFT-HAND MAIN LANDING GEAR HINGE MOUNTING BEAM ON AIRCRAFT HAS STEP WEAR AND CORROSION AT FORWARD AND AFT ENDS. ALSO, ON BEAM BOTTOM BETWEEN FRAMES 12075 AND 13109. REPAIRED IAW HORIZON AIR EA 4-53-733.

Part: SKIN — DAMAGED (HORIZ STAB)

PDX - INTERNAL SKIN OF HORIZONTAL STAB LEADING EDGE PANEL 51C IS PEELING BACK AT RIB 1 AND BETWEEN RIBS 3 AND 4. REPAIRED IAW HORIZON AIR EA 4-55-124.

Part: RIB — CRACKED (LT HORIZ STAB)

PDX - THERE IS A CRACK IN THE LOWER, FORWARD EDGE OF THE LEFT HORIZONTAL STAB, INBOARD MOST RIB AT STATION 215. REPAIRED IAW HORIZON AIR EA 4-57-250.

Part: BRACKET — WORN (ELEVATOR)

PDX - 3 HOLES IN ATTACHMENT BRACKET FOR THE ELEVATOR BOOSTER UNIT ARE WORN SO THAT THE BUSHINGS ARE LOOSE. REPAIRED IAW HORIZON AIR EA 4-55-126.

Part: RIB — CRACKED (LT HORIZ STAB)

PDX - THERE IS A CRACK IN THE TOP, FORWARD EDGE OF THE LEFT, HORIZONTAL STAB, INBOARD MOST RIB AT STATION 215. REPAIRED IAW HORIZON AIR EA 4-57-250.

Part: INTERCOSTAL — CUT (FUSELAGE)

PDX - INTERCOSTAL CUT ON FLANGE ADJACENT TO INNER SKIN. REPAIRED IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 14755)

PDX - CABIN FRAME 14755 CLIP CRACKED AT TOP SIDE OF STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 14755)

PDX - CABIN FRAME 14755 CLIP CRACKED AT TOP SIDE OF STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CASTELLATION — CRACKED (FRAME 15205)

PDX - FRAME 15205 ENTIRE CASTELLATION FLANGE BETWEEN STRINGERS 5 AND 6 HAS BEEN CUT OUT TO REMOVE CRACK. FABRICATED PATCH ALDOINED, PRIMED, INSTALLED IAW FOKKER SRM 53-02-12, PAGE 5.

Part: DRAIN — CORRODED (FRAME 14755)

PDX - AFT CARGO BAY, THE DRAIN PLATE HAS CORROSION AT NUT PLATES, LOCATED BETWEEN FRAMES 14755 AND 14285 AND STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A.

Part: WASHER — CORRODED (FRAME 14755)

PDX - AFT CARGO BAY, THE CASTELLATION WASHER AT FRAME 14755 AND STRINGER 74 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A.

Part: SKIN — CRACKED (EMER EXIT DRWAY)

PDX - UPPER FORWARD CORNER OF SERVICE EMERGENCY DOOR CUTOUT HAS ON CRACK APPROXIMATELY 1.5 INCHES LONG. REPAIRED IAW HORIZON AIR EA 4-53-703.

Part: CASTELLATION — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY, FRAME 13815A BETWEEN STRINGER 2 AND 3 THE CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4.

Part: CASTELLATION — CRACKED (FRAME 16060)

PDX - AFT CARGO BAY FRAME 16060 THE CASTELLATION AT STRINGER 74 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: CASTELLATION — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGERS 73 AND 72 HAS A CRACK IN THE CASTELLATION. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 3.

Part: CASTELLATION — CRACKED (FRAME 16660)

PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CASTELLATION — CRACKED (FRAME 13815)

PDX - FRAME 13815B ENTIRE CASTELLATION FLANGE BETWEEN STRINGERS 72 AND 73 HAS BEEN CUT OUT TO REMOVE TWO CRACKS. FABRICATED PATCH, ALDOINED, PRIMED AND INSTALLED IAW FOKKER SRM 53-02-11, PAGE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CRACKED CLIP AT FRAME 9305A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SKIN — MISMANUFACTURED (FUSELAGE)

PDX - RIGHT DIMPLED LAP JOINT REPAIR DOES NOT CONFORM TO FOKKER DRAWING. REPAIRED IAW HORIZON AIR EA 4-53-738.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CASTELLATION — CORRODED (FRAME 14755)

PDX - FRAME 14755 CASTELLATION FLANGE BETWEEN STRINGERS 1 AND 2 IS MISSING RIVETS. REMOVED LIGHT CORROSION, ALDOINED, PRIMED AND INSTALLED RIVETS IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 10340)

PDX - CABIN FRAME 10340 CLIP CRACKED AT TOPSIDE OF STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SKIN — DENTED (BS 19275-19525)

PDX - DENT IN FUSELAGE BELLY SKIN AT STATION 19275 TO 19525. REPAIRED IAW HORIZON AIR EA 4-53-683A.

Part: FRAME — CORRODED (FRAME 8805)

PDX - CORROSION ON FRAME 8805 AND STRINGER 1 TO 74, UNDER NUT PLATES. REPAIRED IAW HORIZON AIR EA 4-53-720.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME 12875 CLIP CRACKED AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: WASHER — CORRODED (FRAME 15025)

PDX - AFT CARGO BAY, AT FRAME 15205 AND STRINGER 94 THE WASHER ON THE CASTELLATION IS CORRODED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-1.

Part: CASTELLATION — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY, THE CASTELLATION AT FRAME 13815B HAS A CRACK AT STRINGER 2. REPAIRED IAW FOKKER SRM 52-02-13, PAGE 4 AND SRM 51-31-01, PAGE 13.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME 12875 CLIP CRACKED AT TOP SIDE OF STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: FRAME — CORRODED (FRAME 7805)

PDX - CORROSION AT FRAME 7805 AND STRINGER 74 UNDER NUT PLATES. REPAIRED IAW HORIZON AIR EA 4-53-723.

Part: PANEL — DETERIORATED (FUSELAGE)

PDX - PANEL 29AH DETERIORATED. FABRICATED NEW PANEL 29AH FROM 090 GILNER STOCK. INSTALLED USING PANEL CARD PC29A.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 52. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.

Part: CASTELLATION — MISINSTALLED (FRAME 15205)

PDX - FRAME 15205 CASTELLATION FLANGE BETWEEN STRINGERS 1 AND 2 IS MISSING FOUR RIVETS. REMOVED LIGHT CORROSION ALDOINED, PRIMED AND INSTALLED RIVETS IAW FOKKER SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME 13815A CLIP CRACKED AT TOP SIDE OF STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CASTELLATION — CRACKED (FRAME 16660)

PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13.

Part: CASTELLATION — CRACKED (FRAME 16060)

PDX - AFT CARGO BAY FRAME 16060, THE CASTELLATION OUTBOARD OF STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.

Part: RIB — CRACKED (ELEVATOR)

PDX - FALSE RIB ASSEMBLY FOR LEADING EDGE 51E HAS .5 CRACK UNDER CORNER OF FLANGE. REPAIRED IAW HORIZON AIR EA 4-55-121.

Part: FRAME — CRACKED (FRAME 50-2)

PDX - FUSELAGE TAIL SECTION FRAME 50-2 AT STRINGER 44 IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2B, STEPS 1 AND 2.

Part: FRAME — CORRODED (FRAME 9305)

PDX - CORROSION ON FRAME 9305 BETWEEN STRINGER 2 AND 72. REPAIRED IAW HORIZON AIR EA 4-53-721.

Part: CASTELLATION — CRACKED (FRAME 13815)

PDX - AFT CARGO BAY, FRAME 13815B AND BETWEEN STRINGERS 74 AND 73 IS CRACKED AT THE CASTELLATION. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-1.

Part: CASTELLATION — CRACKED (FRAME 16660)

PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.

Part: FRAME — CORRODED (FRAME 7305)

PDX - CORROSION ON FRAME 7305 BETWEEN STRINGERS 2 AND 73. REPAIRED IAW HORIZON AIR EA 4-53-722.

Part: FRAME — CRACKED (FRAME 50-2)

PDX - FUSELAGE TAIL SECTION FRAME 50-2 AT STRINGER 48 IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2B, STEPS 1 AND 2.

Part: SKIN — DENTED (VERT STAB)

PDX - DENT ON LEFT SIDE OF VERTICAL STAB AFT OF LEADING EDGE. REPAIRED IAW HORIZON AIR EA 4-55-122.

Part: CASTELLATION — CORRODED (FRAME 15205)

PDX - AFT CARGO BAY, FRAME 15205 THERE IS CORROSION ON THE CASTELLATION BETWEEN STRINGERS 5 AND 6. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4.

Part: HOUSING — CRACKED (ELEVATOR)

PDX - ELEVATOR GUSTLOCK HOUSING HAS POSSIBLE CRACK AT ATTACH LEGS. REPAIRED SB F28-27-182.

Part: SEAT TRACK — CORRODED (FRAME 4875-5305)

PDX - LEFT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 4875 AND 5305 HAS ONE AREA OF PITTING CORROSION ON INBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: CLIP — CRACKED (FRAME 11405)

PDX - CABIN FRAME 11405 CLIP CRACKED AT TOP SIDE OF STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 15205)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 14285 AND 15635 HAS FRETTING AND PITTING CORROSION IN FLANGES FORWARD OF FRAME 15205. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205.

Part: CLIP — CRACKED (FRAME 50-2)

PDX - FUSELAGE TAIL SECTION AT FRAME 50-2 BETWEEN STRINGERS 23 AND 24 CLIP IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2B, STEPS 1 AND 2.

Part: CLIP — CRACKED (FRAME 50-2)

PDX - FRAME CLIP REPAIR CRACKED ON FRAME 50-2 BETWEEN STRINGERS 46 AND 48. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 14285)

PDX - LEFT INBOARD SEAT TRACK SECTION BETWEEN SPLICES FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ON FLANGES ALONG ENTIRE LENGTH WITH ON PITTED AREA ON RIGHT FRAME. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FRAME 11703)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE BETWEEN FRAME 11703 AND 13345. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206, FIGURE 205.

Part: CLIP — CRACKED (FRAME 14285)

PDX - CABIN FRAME 14285 CLIP CRACKED FROM STRINGER 32 TO 33. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 5, FIGURE 1, SHEET 2 OF 2.

Part: FRAME — CORRODED (FRAME 6805)

PDX - CORROSION ON FRAME 6805 BETWEEN STRINGERS 2 AND 73, UNDER NUT PLATES AND LOWER SURFACE. REPAIRED IAW FOKKER SRM 53-01-01.

Part: CLIP — CRACKED (FRAME 14285)

PDX - CABIN FRAME 14285 CLIP HAS 3 INCH CRACK BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 5, FIGURE 1, SHEET 2 OF 2.

Part: CLIP — CRACKED (FRAME 32-2)

PDX - FRAME CLIP CRACKED ON FRAME 32-2 BETWEEN STRINGERS 29 AND 31. REPAIRED IAW FOKKER SRM 53-10-5, PAGE 601, PARAGRAPH 2B, STEP 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 9805-14285)

PDX - RIGHT-HAND SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 14285 HAS PITTING AND FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGES. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205.

Part: SEAT TRACK — CORRODED (FRAME 13345)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS AN AREA OF CORROSION 8 INCHES AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-4.

Part: CLIP — CRACKED (FRAME 50-2)

PDX - FRAME CLIP REPAIR IS CRACKED ON FRAME 50-2 BETWEEN STRINGER 24 AND 25. REPAIRED IAW FOKKER SRM 53-10-5, PARAGRAPH 2B, STEP 1 AND 2, PAGE 601 AND SRM 53-10-5.

Part: SEAT TRACK — CORRODED (FRAME 13815)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS AN AREA OF CORROSION 3 INCHES AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-40-01, PAGE 206, FIGURE 205.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: WEB — CRACKED (CARGO DOOR)

PDX - AFT CARGO PIT DOOR FORWARD LOWER WEB IS CRACKED AT NUT PLATE. REPAIRED IAW FOKKER SRM 51-10-04 AND 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME 13815 CLIP CRACKED AT TOP SIDE OF STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SKIN — DENTED (CARGO DOOR)

PDX - AFT CARGO DOOR, FORWARD FACE OF CARGO DOOR IS DENTED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: FRAME — CORRODED (FRAME 8305)

PDX - FRAME 8305 HAS CORROSION AT STRINGER 74 AT RIVET BY LIGHTENING HOLE UNDER NUT PLATE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: SKIN — CORRODED (FRAME 5805-6065)

PDX - CORROSION ON INSIDE SKIN OF ANTENNA MOUNTING AREA BETWEEN FRAMES 5805, 6065 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - CRACKED CLIP AT STRINGER AND FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: JAMB — DAMAGED (SERVICE DOORWAY)

PDX - UPPER AFT CORNER OF SERVICE EMERGENCY DOOR APERTURE REQUIRES EXTERNAL DOUBLER INSTALLATION. REPAIRED IAW HORIZON AIR EA 4-53-703.

Part: CLIP — CRACKED (FRAME 7805)

PDX - CRACKED CLIP AT FRAME 7805 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — GOUGED (FRAME 14755)

PDX - RIGHT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGE AND TWO GOUGES IN LEFT-HAND FLANGE AT FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4.

Part: STRINGER — CORRODED (FRAME 6305-6565)

PDX - CORROSION ON STRINGER 1 BETWEEN FRAMES 6305 AND 6565. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: CLIP — CRACKED (FRAME 8805)

PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: FRAME — CORRODED (FRAME 9305)

PDX - CORROSION ON FRAME 9305A AT STRINGER 11, TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 4, PARAGRAPH 4.

Part: CLIP — CRACKED (FRAME 8805)

PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: STRINGER — CORRODED (FRAME 6305-6565)

PDX - CORROSION ON STRINGER 74 BETWEEN FRAMES 6305 AND 6565. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: SKIN — CORRODED (FRAME 6305-6565)

PDX - CORROSION ON INSIDE OF SKIN AT ANTENNA MOUNTING AREA BETWEEN FRAME 6565 AND 6305 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: SEAT TRACK — CORRODED (FRAME 14285)

PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN SPLICES FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGE OF FLANGES AND TWO GOUGES IN LEFT FLANGE AT FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4,

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 1 AND 74 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY, CORROSION ON THE CASTELLATION ABOVE STRINGER 74 AT FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, PARAGRAPH 4 B-C.

Part: SKIN — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE SKIN HAS CORROSION AT FRAME 13815 AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, STRINGER 4 B-C.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 2 AND 1 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SKIN — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY FRAME 13815A AT STRINGER 2 THE SKIN HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL ACCESS APERTURE 73B HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PARAGRAPH 4, FIGURE 2 AND SRM 51-31-01.

Part: SKIN — DENTED (FRAME 7305)

PDX - DENT IN FUSELAGE AT FRAME 7305 AND STRINGER 67. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8 AND 9.

Part: DOUBLER — CORRODED (FRAME 15635)

PDX - AFT CARGO BAY, THERE IS CORROSION ON AND IN THE NR 3 VHF COMM DOUBLER AND STIFFENER, LOCATED BETWEEN FRAMES 15635, 15205 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGER 1 AND 2 THE CASTELLATION HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815A, 13815 AND STRINGER 2 THE SKIN IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: STRUCTURE — CRACKED (FRAME 8305)

PDX - CRACK AT FRAME 8305 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL PANEL 73A APERTURE HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGERS 74 AND 73 THE CASTELLATION HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SUPPORT — CORRODED (FRAME 16060)

PDX - AFT CARGO BAY FRAME 16060 LEFT OUTBOARD CABIN FLOOR SUPPORT HAS CORROSION AT LOWER NUT PLATE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.

Part: CLIP — CRACKED (FRAME 8805)

PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CRACKED CLIP AT FRAME 9305 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 74 AND 72 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CASTELLATION — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE CASTELLATION HAS CORROSION AT FRAME 13815 AND STRINGER 71. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CLIP — CRACKED (FRAME 8805)

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

Part: SPLICE — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY AT FRAME 13815A BETWEEN STRINGERS 1 AND 74 THERE IS CORROSION ON THE OUTER SPLICE PIECES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: PANEL — CORRODED (WS 2230)

PDX - LEFT WING FUEL PANEL 71A AT STATION 2230 HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW 51-10-4, PAGE 9, PARAGRAPH 4B.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP AND BOTTOM SIDE OF STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13, PARAGRAPH 4, FIGURE 2 AND SRM 51-31-01.

Part: SEAT TRACK — CORRODED (FRAME 4875-5305)

PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN FRAME 4875 AND 5305 HAS DEEP CORROSION ON FLANGES ALONG ENTIRE LENGTH. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SKIN — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE SKIN IS CORRODED UNDER CASTELLATION AT FRAME 13815 AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SEAT TRACK — WORN (FRAME 7805)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK THAT EXTENDS FROM FRAME 7805 TO 9 INCHES AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 11703)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FRAME 11703 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 21 THROUGH TWO RIVET HOLES. REPAIRED IAW FOKKER SRM 53-02-11 AND SRM 51-31-01.

Part: SEAT TRACK — CHAFED (FRAME 11405)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF CHAFE DAMAGE 2 INCHES FORWARD OF FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 10966)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION BETWEEN FRAME 10966 AND 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — GOUGED (FRAME 12875)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS SMALL GOUGES 5 INCHES FORWARD OF FRAME 12875. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION AND WEAR INSIDE TRACK BETWEEN FRAME 9305 AND 9305A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: ANGLE — CORRODED (FRAME 13345)

PDX - AFT CARGO BAY THERE IS CORROSION ON ATTACH ANGLE TO FRAME 13345 BETWEEN STRINGERS 2 AND 1. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SKIN — CORRODED (FRAME 13865)

PDX - AFT CARGO BAY THERE IS CORROSION ON THE SKIN AT STRINGER 2 BETWEEN FRAME 13865 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SEAT TRACK — CORRODED (BS 9305)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 9305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — WORN (FRAME 8805)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK THAT EXTENDS FROM 3 INCHES AFT TO 12 INCHES FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 51-10-9 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (BS 6305)

PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 11405)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF CORROSION 2 INCHES FORWARD OF FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 14323)

PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 14323. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SKIN — CORRODED (FRAME 13815)

PDX - AFT CARGO BAY THE SKIN IS CORRODED UNDER CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SEAT TRACK — CORRODED (FRAME 10346)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION EXTENDING 5 INCHES FORWARD AND AFT OF FRAME 10346. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT BOTTOM SIDE OF STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 7805)

PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 7805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 9305-9805)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION AND WEAR INSIDE TRACK BETWEEN FRAMES 9305C AND 9805. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 201, PARAGRAPH 4(B) AND SRM 51-10-04, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK EXTENDING 6 INCHES FORWARD AND AFT OF FRAME 9305B. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SKIN — CORRODED (FRAME 15635)

PDX - AFT CARGO BAY, THERE ARE FIVE SPOTS OF CORROSION ON SKIN SURFACE LOCATED BETWEEN FRAMES 15635, 15205 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP AND BOTTOM SIDE OF STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SEAT TRACK — CORRODED (BS 13353)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION IN TWO AREAS INSIDE TRACK AT STATION 13353. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SECTION 4, PARAGRAPH B1 AND 2.

Part: SKIN — CORRODED (FRAME 15635)

PDX - AFT CARGO BAY, 40MM FORWARD OF FRAME 15635 AND BETWEEN STRINGERS 1 AND 2 CORRODED. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.

Part: SEAT TRACK — CORRODED (FRAME 15205)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK IN 4 INCH AREA ADJACENT TO FRAME 15205. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B1 AND 2.

Part: SEAT TRACK — GOUGED (FRAME 11703)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS TWO GOUGES IN CIRCUMFERENCE OF SEAT TRACK HOLE 2 INCHES AFT OF FRAME 11703. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (FRAME 10966)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK BETWEEN FRAMES 10966 AND 11405. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201-202, STEPS 2-6.

Part: SEAT TRACK — CORRODED (BS 11794)

PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 11794. REPAIRED IAW FOKKER SRM 51-10-14, SECTION 4 PARAGRAPH B, STEPS 1 AND 2.

Part: SEAT TRACK — CORRODED (BS 8805)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS SCORING 8 INCHES LONG WITH CORROSION AT STATION 8805. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FRAME 5805)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK 2 INCHES FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-01.

Part: SEAT TRACK — WORN (FRAME 5805-6305)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK BETWEEN FRAMES 5805 AND 6305. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205.

Part: SEAT TRACK — CORRODED (FRAME 13815)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS PITTING CORROSION BETWEEN FRAMES 13815A AND 13815B. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-01, PAGE 206, FIGURE 205.

Part: SEAT TRACK — CORRODED (FRAME 4805-5305)

PDX - LEFT INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF TRACK BETWEEN FRAME 4805 AND 5305. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FRAME 5305-9805)

PDX - LEFT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 5305 AND 9805 HAS PITTING AND FRETTING CORROSION ON FLANGES ALONG LENGTH AFT OF STATION 5700. REPAIRED IAW FOKKER SRM 53-40-01, FIGURE 204.

Part: SEAT TRACK — CORRODED (BS 16745)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 16745. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: SEAT TRACK — WORN (FRAME 5805-6305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS WEAR INSIDE THE TRACK BETWEEN FRAME 5805 AND 6305. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT FRAME 6805 AND EXTENDS 10 INCHES FORWARD. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FRAME 9305C AND 9805. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 201, PARAGRAPH 4(B).

Part: SEAT TRACK — GOUGED (FRAME 9305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS 2 SMALL GOUGES AROUND SEAT TRACK HOLES BETWEEN FRAMES 9305 AND 9305A. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — GOUGED (FRAME 6805)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGES AROUND SEAT TRACK HOLE AT FRAME 6805. REPAIRED IAW FOKKER SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 14323)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 14323. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (FRAME 7805-8305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A 3 INCH AREA OF CORROSION BETWEEN FRAME 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-40-1, PAGE 201, PARAGRAPH 4 (B).

Part: SEAT TRACK — WORN (FRAME 6305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS WEAR ON TOP OF THE TRACK 3 INCHES LONG AND IS LOCATED 3 INCHES FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — SCRATCHED (FRAME 12875)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SCRATCH 6 INCHES AFT OF FRAME 12875. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205.

Part: SEAT TRACK — CORRODED (BS 16203)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 16203. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 9305)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 9305. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205.

Part: SEAT TRACK — GOUGED (FRAME 7305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGES AROUND 4 SEAT TRACK HOLES, 6 INCHES FORWARD OF FRAME 7305. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-1 PAGE 201, PARAGRAPH 4 (B).

Part: SEAT TRACK — CORRODED (BS 10203)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION IN TWO AREAS INSIDE TRACK AT STATION 10203. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-04.

Part: SEAT TRACK — GOUGED (FRAME 8305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL GOUGE, 5 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION AROUND SEAT TRACK HOLE, 6 INCHES FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-1 PAGE 201, PARAGRAPH 4 (B).

Part: SEAT TRACK — CORRODED (FRAME 6305)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK 3 INCHES FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 206, FIGURE 205.

Part: SKIN — DENTED (CARGO DOOR)

PDX - FORWARD CARGO DOOR INNER SKIN HAS 3 DENTS JUST BELOW HINGE. REPAIRED IAW FOKKER SRM 52-02-01 PAGE 3, FIGURE 2.

Part: SEAT TRACK — CORRODED (BS 11253)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 11253. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: SEAT TRACK — GOUGED (FRAME 13345)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS 2 SMALL GOUGES BETWEEN FRAMES 13345 AND 13815. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5.

Part: SEAT TRACK — CORRODED (FRAME 13815)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF SURFACE CORROSION ADJACENT TO FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FRAME 9305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION EXTENDING 5 INCHES FORWARD AND AFT OF FRAME 9305B. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 201, PARAGRAPH 4(B).

Part: SEAT TRACK — GOUGED (FRAME 9305)

PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGE 2 INCHES AFT OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 7805)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION 7805. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 15733)

PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 15733. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4.

Part: ANGLE — DAMAGED (CARGO DOOR)

PDX - FOUND LARGE OUT OF ROUND HOLES IN ANGLES FOR FORWARD CARGO DOOR. REPAIRED IAW FOKKER SRM 51-11-04, 51-31-01 AND 51-10-05.

Part: PANEL — CORRODED (LEFT WING)

PDX - LEFT WING FUEL PANEL 73G HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.

Part: SEAT TRACK — WORN (FRAME 6805-7305)

PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK FROM FRAME 6805 TO 7305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2.

Part: CLIP — DAMAGED (FUSELAGE)

PDX - INNER SKIN REINFORCE CLIP CUT AT FLANGE ADJACENT TO INNER SKIN. REPAIRED IAW FOKKER SRM 51-31-01.