N481US

Part: LENS — DISLODGED (SEAT 9) · airframe 29,889 hrs · 36,885 cycles

BOI - THE EMERGENCY LIGHT LENS ON SEAT 9A FELL OFF. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — MALFUNCTIONED (CABIN) · airframe 28,999 hrs · 35,991 cycles

GEG- FORWARD EMERGENCY EXIT SIGN AT ROW 8 INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 28,958 hrs · 35,949 cycles

GEG- 28V LAMPS IN EXIT SIGN OVER COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED FORWARD EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLADE — FAILED (2ND STAGE LPT) · airframe 28,745 hrs · 35,741 cycles

BOI - CLIMBING THROUGH 28,500 FEET, THE NR 1 ENGINE BEGAN VIBRATING ALONG WITH THE ASSOCIATED FUEL LEVER. NR 1 TGT ROSE TO APPROXIMATLY 540 DEG. ENGINE WAS SHUT DOWN, FLIGHT LANDED WITHOUT INCIDENT. UPON INSPECTION FOUND SECOND STAGE LOW PRESSUR TURBINE DAMAGED. REMOVED AND REPLACED #1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE VENDOR CONFIRMED LP 2 COMPRESSOR BLADE FAILURE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 28,718 hrs · 35,715 cycles

GEG - AFT EMERGENCY EXIT SIGN HAS LAMPS OUT. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (ROW 9)

SEA - FORWARD EXIT SIGN AT ROW 9 INOPERATIVE. REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

SEA - EXIT SIGN ABOVE FLIGHT DECK INOP. REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN)

SEA - EXIT SIGN ABOVE GALLEY IN ARM POSITION, ONE LAMP WORKING. REPLACED SIGN ASSEMBLY OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (ROW 9)

GEG - EMERGENCY EXIT SIGN OVER ROW 9 WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT ASSY — BROKEN (ROW 8)

PDX- SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 8AB BROKEN. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (COCKPIT)

BOI- OVERHEAD EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (LTEMER EXIT)

PDX - LEFT AFT OVERWING EMERGENCY EXIT TOP AFT CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5.

Part: SKIN — CHAFED (LT EMER EXIT)

PDX - LEFT AFT OVERWING EMERGENCY EXIT BOTTOM FORWARD CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 3, FIGURE 1.

Part: SKIN — CHAFED (LT EMER EXIT)

PDX - LEFT OVERWING EMERGENCY EXIT BOTTOM AFT CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 3, FIGURE 1 AND SRM 52-01-01, PAGE 9.

Part: SKIN — CRACKED (LT EMER EXIT)

PDX - LEFT AFT OVERWING EMERGENCY EXIT TOP FORWARD CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-02-03, PAGE 5.

Part: SKIN — DENTED (FRAME 16660)

PDX- A .75 INCH LONG DENT IN LEFT FUSELAGE SKIN, FORWARD OF REAR PRESSURE BULKHEAD 4 AFT OF FRAME 16660, 1 ABOVE STRINGER 6. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 5A AND SRM 51-10-04, PAGE 9, PARAGRAPH 4BC.

Part: SKIN — CRACKED (BS 104.33)

PDX - TWO CRACKS LOCATED THROUGH THE RIGHT SIDE SKIN AT STATION 104.330 APPROXIMATELY WL 30.00. REPAIRED IAW HORIZON AIR EA 4-53-886.

Part: FRAME — CRACKED (BS 2650)

PDX - FORWARD FRAME AT STATION 2650 IN NOSEWHEEL BAY HAD BOTH LEFT AND RIGHT LOWER LIPS CRACKED OFF AT THE NUT PLATE SUPPORT BLOCKS. REPAIRED IAW HORIZON AIR EA 4-53-886.

Part: EXHAUST — CRACKED (RT ACM)

PDX - RIGHT ACM EXHAUST HAS A SUSPECTED SMALL CRACK AT THE LOWER FORWARD CORNER. REPAIRED IAW FOKKER SRM 51-31-01.

Part: STRINGER — CORRODED (FRAME 3450-4150)

PDX - FORWARD CARGO COMPARTMENT STRINGER 65 HAD SURFACE CORROSION BETWEEN FRAMES 3450 AND 4150. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1F.

Part: SKIN — CHAFED (FRAME15205-15635)

PDX - RIGHT FUSELAGE SKIN LAP JOINT AT STRINGER 66 BETWEEN FRAMES 15205 AND 15635 HAD CHAFE DAMAGE FROM PANEL 92BD, LOOSE AND MISSING PAINT AND SURFACE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGES 2-6.

Part: SEAT TRACK — CORRODED (FRAME 7805)

PDX - RIGHT INBOARD SEAT TRACK JUST FORWARD OF FRAME 7805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-895.

Part: FRAME — CRACKED (FRAME 20075)

PDX - CRACK IN FRAME 20075, STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 51-30-02.

Part: BULKHEAD — CRACKED (FWD PRESS BLKHD)

PDX - FRONT PRESSURE BULKHEAD BEAM VI AT CENTERLINE HAD A CRACK ON PREVIOUS REPAIR AT TOP FLANGE IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-18.

Part: BULKHEAD — CRACKED (FWD PRESS BLKHD)

PDX - FRONT PRESSURE BULKHEAD BEAM VI AT CENTER LINE HAD A CRACK IN PREVIOUS REPAIR AT BOTTOM FLANGE IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-18.

Part: FRAME — CRACKED (FRAME 20075)

PDX - CRACK IN FRAME 20075, STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5.

Part: SEAT TRACK — SCRATCHED (FRAME 13815)

PDX - LEFT INBOARD SEAT TRACK AT FRAME 13815 CENTER FLANGE HAD LIGHT SCRATCHES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: FRAME — CORRODED (FRAME 9305)

PDX - FORWARD CARGO COMPARTMENT FRAME 9305 HAS CORROSION AROUND NUTPLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW HORIZON AIR EA 4-53-891.

Part: FAIRING — CHAFED (LT WING/FUS)

PDX - FUSELAGE HAS CHAFE DAMAGE FROM PANEL 92BD AFT LEFT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: FRAME — CRACKED (FRAME 17565)

PDX - CRACK IN FRAME 17565, STRINGER 57. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601A.

Part: FAIRING — CHAFED (RT WING/ FUS)

PDX - FUSELAGE HAD CHAFE DAMAGE FROM PANEL 91BD AFT RIGHT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGRAPH 3C.

Part: FRAME — CRACKED (FRAME 17565)

PDX - CRACK IN FRAME 17565, STRINGER 56. REPAIRED IAW FOKKER SRM 5302-13, PAGE 5, FIGURE 3.

Part: SEAT TRACK — GOUGED (FRAME 10546)

PDX - LEFT OUTBOARD SEAT TRACK HAD TWO SMALL GOUGES ON TOP FLANGE JUST AFT OF FRAME 10546. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — GOUGED (FRAME 6305)

PDX - LEFT OUTBOARD SEAT TRACK HAD A GOUGE ON TOP INBOARD FLANGE APPROXIMATELY 3 FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, C AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — SCRATCHED (FRAME 10346)

PDX - LEFT OUTBOARD SEAT TRACK HAD LIGHT SCRATCHES AT CENTER FLANGE JUST AFT OF FRAME 10346. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — GOUGED (FRAME 11405)

PDX - LEFT OUTBOARD SEAT TRACK HAD TWO GOUGES TOP OUTBOARD FLANGE APPROXIMATELY 3 FORWARD OF FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — GOUGED (FRAME 6305)

PDX - RIGHT OUTBOARD SEAT TRACK, 3 INCHES FORWARD OF FRAME 6305 HAD TWO GOUGES ON CENTER FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — SCRATCHED (FRAME12875-13345)

PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SURFACE CORROSION AND LIGHT SCRATCHES BETWEEN FRAME 12875 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - RIGHT INBOARD SEAT TRACK APPROXIMATELY 10 AFT OF FRAME 6805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — CORRODED (FRAME 6805)

PDX - RIGHT INBOARD SEAT TRACK JUST FORWARD OF FRAME 6805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — SCRATCHED (FRAME 5805-6805)

PDX - LEFT OUTBOARD SEAT TRACK HAD LIGHT SCRATCHES IN CENTER FLANGE BETWEEN FRAME 5805 AND 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, C AND SRM 51-10-7, PAGE 8, PARAGRAPH 3, C, 4.

Part: CLIP — CRACKED (FRAME 12875)

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

Part: FRAME — CRACKED (FRAME 17565)

PDX - CRACK IN FRAME 17565, STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — CORRODED (FRAME 13345)

PDX - LEFT INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CENTER FLANGE APPROXIMATELY 12 AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SEAT TRACK — SCRATCHED (FRAME 6805)

PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SCRATCHES IN CENTER FLANGE AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: SEAT TRACK — SCRATCHED (FRAME 11905)

PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SCRATCHES AT CENTER FLANGE APPROXIMATELY 6 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4.

Part: CLIP — MISREPAIRED (FRAME 13815)

PDX - AFT CARGO PIT CRACK IN PREVIOUS REPAIR TO FRAME CLIP ON FRAME 13815A AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.

Part: SKIN — DAMAGED (FRAME 15205)

PDX - TOOLING MARK ON FUSELAGE SKIN AT FRAME 15205 NEAR STRINGER 20. REPAIRED IAW FOKKER SRM 53-10-01, PARAGRAPH 3D, FIGURE 1.

Part: SKIN — DAMAGED (BS 6900)

PDX - LEFT-HAND FUSELAGE SKIN HAS TWO SCRAPES THROUGH PAINT AT STATION 6900 AND WL-400. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 3B, AREA B, FIGURE 1.

Part: CLIP — CRACKED (FRAME 15205)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 15205 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 11405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 11405 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 43. ALSO, FRAME IS DENTED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B-C.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 7805 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13185)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9035)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SKIN — DENTED (BS 6565)

PDX - DENT IN LEFT-HAND FUSELAGE SKIN AT STATION 6565 AND WL-420, 1.5 WIDE .080 DEEP. REPAIRED IAW FOKKER SRM 53-02-07, PAGE 5, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305B AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305C AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 14755)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 14755 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 10346)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12405)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9035)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9035)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 10346)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 10346)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9035)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 6305)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 9035)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: FLOORBEAM — CORRODED (FRAME 4175-4610)

PDX - CORROSION ON TOP OF LONGITUDINAL FLOORBEAM THAT EXTENDS FORWARD FROM RIGHT-HAND OUTBOARD SEAT TRACK BETWEEN FRAME 4175 AND 4610. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.

Part: CLIP — CRACKED (FRAME 10346)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 12875)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 14755)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 14755 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 5805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 7805)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 7805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CLIP — CRACKED (FRAME 10966)

PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10966 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: SKIN — DENTED (CARGO DOOR)

PDX - CENTER CARGO DOOR INNER SKIN HAS SEVERAL DENTS AND ONE AREA ALL CANNING IN TOP 15 INCHES. REPAIRED IAW HORIZON AIR EA 4-52-271.

Part: CLIP — CRACKED (FRAME 13815)

PDX - AFT CARGO PIT CRACK COMING OUT FROM UNDER WASHER ON PREVIOUSLY REPAIRED FRAME CLIP AT FRAME 13815A AND STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.

Part: CLIP — CRACKED (FRAME 13815)

PDX - CLIP CRACKED ON RIGHT-HAND SIDE AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.

Part: CIRCUIT BOARD — FAILED (CABIN)

GEG- CENTER AISLE ROW 8 EXIT SIGN HAS INOPERATIVE LIGHTS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD.

Part: SIGN — INOP (COCKPIT DOOR)

BOI- EXIT SIGN OVER COCKPIT DOOR IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLEY. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOP (CABIN)

SEA- NUMEROUS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AT ENTRANCE WAY. OPERATIONAL CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN)

PDX - EMERGENCY EXIT LIGHT OVER COCKPIT DOOR PARTIALLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN. OPERATIONAL TEST PERFORMED, OK FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PDX- OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN WERE INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECK GOOD.

Part: TURBINE BLADE — FAILED (RT ENGINE)

MWH - A/C EN ROUTE FROM SEA TO BIL, WHILE CLIMBING THROUGH 26,000 FT HEARD A BANG AND RIGHT ENGINE BEGAN TO VIBRATE, TGT ON RISE. SHUT DOWN ENGINE AND DIVERTED TO MWH. MAINTENANCE REPLACED THE ENGINE. A TURBIN BLADE ON THE NR 2 DISK OF THE LP HAD EXITED THE ENGINE. THE RESULT OF THAT TEARDOWN WAS THE ENGINE HAD FAILED DUE TO A BLADE IN THE SECOND STAGE OF THE LPT BREAKING OFF JUST ABOVE THE FIR TREE AREA OF THE BLADE. ROLLS-ROYCE HAD AN ENGINEERING PERSON ON SIGHT TO CONDUCT THE DISASSEMBLY.

Part: AIR DIST — ODOR (CABIN)

BOI - DURING TAKEOFF ROLL, THERE WAS SMOKE SMELL IN CABIN. NO PRESSURE ABOVE 3 PSI, DUCT PRESSURE 10 PSI WITH ANTI-ICE ON. MAINTENANCE GROUND RUN AIRCRAFT, ENGINE 1 AND 2 SAME ACCELERATION RATE. RAN BOTH AT HIGH POWER, NO SMOKE SMELL IN CABIN. AIRCRAFT PRESSURE TO 4.0 PSI, AFT PRESSURE DROP. CHECK OK, NO PARTS REPLACED.

Part: CIRCUIT BOARD — FAILED (CABIN)

CENTER CABIN EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CIRCUIT BOARD, OPERATIONAL CHECK NORMAL.

Part: POWER SUPPLY — INOP (CABIN)

SEVERAL CEILING EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED 3 BATTERY POWER SUPPLIES. OPERATIONAL CHECKED NORMAL PER FOKKER F-28 MAINTENANCE MANUAL, CHAPTER 33-50-00.

Part: BULB — FAILED (EMERGENCY EXIT)

LIGHT INSIDE LEFT FORWARD EMERGENCY EXIT HANDLE COVER INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL.

Part: AIR DISTR — ODOR (CABIN)

DURING FLIGHT NOTICED AN EXHAUST SMELL IN THE COCKPIT AND CABIN FROM ROW 6. VISUALLY INSPECTED COCKPIT, CABIN, APU AREA AND CARGO AREAS. GROUND RAN BOTH ENGINES. ON DEFECTS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT WING EVACUATION LIGHTS INOP. INSTALLED BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

EXIT SIGN ABOVE NR 2 GALLEY WILL NOT ILLUMINATE. RELAMPED, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIONS (CARGO COMPT)

FORWARD EXTERIOR UNDERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY IN FORWARD CARGO PIT. OPERATIONALLY TESTED IN ACCORDANCE WITH 33-50-01. NO DEFECTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (CARGO COMPT)

AFT EXTERIOR UNDERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY IN AFT CARGO PIT. OPERATIONALLY TESTED IN ACCORDANCE WITH 33-50-01. NO DEFECTS NOTED.

Part: SIGN — INOPERATIVE (CABIN)

AFT FACING EXIT SIGN AT MID CABIN HAS SEVERAL BULBS OUT. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL TESTS WERE PERFORMED, RESULTS NORMAL.

Part: BULB — FAILED (CABIN)

SEA - RIGHT AFT OVERWING EXIT HAS A BURNT OUT BULB. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

GEG - EMERGENCY EXIT LIGHT IN FORWARD CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AND OPERATIONALLY TESTED, TEST SHOWS NORMAL OPERATION.

Part: BULB — FAILED (CABIN)

PDX - FORWARD GALLEY EXIT LIGHT HAS A BURNT OUT BULB. MAINTENANCE REMOVED AND REPLACED BULB, OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

PDX - FORWARD EXIT LIGHT HAS BURNT OUT BULBS. MAINTENANCE REMOVED AND REPLACED BULBS, OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

BOI - CEILING EMERGENCY LIGHT INOPERATIVE AT ROWS 1 AND 8. MAINTENANCE RELAMPED AND OPERATIONAL TESTED, CHECKS GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT ROW 10 IS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (CABIN)

CEILING EMERGENCY LIGHT OUT AT ROW 13. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT IN CENTER AISLE HAS SEVERAL BURNT OUT BULBS. MAINTENANCE RELAMPED, TESTS GOOD.

Part: BULB — FAILED (CABIN)

FORWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

SEVERAL OVERHEAD EMERGENCY LIGHTS OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTED GOOD.

Part: BULB — FAILED (CABIN)

LEFT FORWARD WINDOW EXIT EVACUATION LIGHT INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EXIT LIGHT INOPERATIVE OVER EXIT HATCH 8A. MAINTENANCE RELAMPED, TESTS NORMAL.

Part: SIGN — INOPERATIVE (INOPERATIVE)

SEAT FLOOR PROXIMITY EXIT SIGN MISSING AT ROW 8. MAINTENANCE INSTALLED NEW FLOOR PROXIMITY SEAT SIGN AT ROW 8, FUNCTION TESTED NORMAL.

Part: BULB — FAILED (CABIN)

EXIT LIGHT OUT AT 9A. REPLACED BULB, OPERATIONAL TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT COVER ON SEAT 8B MISSING. THE LIGHT ASSEMBLY WAS REPLACED, CHECKS GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT SIGN IN THE CENTER OF THE CABIN HAS INOP BULBS. REPLACED BULBS, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (LT EMER EXIT)

GEG - LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

EXIT SIGN ABOVE COCKPIT DOOR HAS ALL LIGHTS INOP. MAINTENANCE RELAMPED WITH 28 VOLT BULBS, OPERATIONAL CHECK GOOD.

Part: LAMP — FAILED (CABIN)

SEA - UPPER EMERGENCY LIGHT LEFT OF FORWARD SERVICE DOOR INOP. MAINTENANCE RELAMPED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — BROKEN (CARGO DOOR)

CLT-CAE - FLT 751 - DURING TAKEOFF ROLL, CARGO DOOR WARNING LIGHT ILLUMINATED. CAPTAIN REJECTED TAKEOFF. SPEED AT TIME OF REJECTION WAS 90 KTS. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND CENTER CARGO DOOR WARNING SWITCH OUT OF ADJUSTEMENT. THEY ADJUSTED THE SWITCH. OPERATION CHECK NORMAL. (M)

Part: SEAL — LEAKING (LOW PRESS VLV)

CLT - FL 425 - AFTER TAKEOFF, THE RIGHT BAY OVERHEAT LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED WHEN THE RIGHT BLEED SYSTEM WAS SECURED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LOWER PRESSURE VALVE SEALS. (M)

Part: DOWNLOCK ACT — FAILED (RT MLG)

CLT - FLT 1147 - AFTER LANDING GEAR EXTENSION, CREW HAD ONE RED LIGHT AND NO GREEN LIGHT ON THE RIGHT MAIN LANDING GEAR. CREW RECYCLED THE GEAR AND NOTED SAME INDICATIONS. TOWER FLYBY WAS CONDUCTED. GEAR WAS MANUALLY EXTENDED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE RIGHT GEAR DOWNLOCK ACTUATOR DUE TO INCOMPLETE EXTENSION. (M)

Part: EXIT SIGN — INOPERATIVE (CABIN)

FORWARD CABIN EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN. (M)

Part: CONTROLLER — FAILED (CABIN)

CLT - FLT 2309 - AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. THE CAPTAIN LEVELED OFF AT 9,000 FEET AND RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. (X)

Part: EEL LEGEND PLATE — FAILED (CABIN)

PIT - FLIGHT 464 - PIREP READS, CHECK BULBS IN CABIN OVERHEAD EMERGENCY EXIT LIGHTS. REPLACED LIGHT PLATE ASSEMBLYS IN FORWARD CABIN AND MID CABIN EMERGENCY EXIT SIGNS. OPS CHECKED. (M)

Part: ACTUATOR — INOPERATIVE (LT MLG DOOR)

CMH - FL 1101, AFTER TAKEOFF FROM FWA AND GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ABNORMAL PROCEDURES COMPLIED WITH, INDICATIONS SHOWED AND UNLOCKED DOOR. GEAR WAS SELECTED DOWN AND FLIGHT DIVERTED TO CMH. AFTER LANDING AND ENGINE SHUTDOWN, LEFT MAIN GEAR DOOR OPENED AND RESTED ON THE GROUND. MAINTENANCE REPLACED THE LEFT MAIN GEAR DOOR ACTUATOR. (M)

Part: COMPRESSOR — STALLED (ENGINE)

CLT - FLT 0456 - WHILE CLIMBING OUT OF CLT, FLIGHT ENCOUNTERED A COMPERSSOR STALL. THE CAPTAIN POWERED BACK TO IDLE THEN UP AGAIN AND GOT ANOTHER COMPRESSOR STALL. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. REPLACED ENGINE ASSEMBLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

CLE - MAIN ENTRANCE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPS CHECKS GOOD. (X)

Part: EEL BATTERY PACK — DISCHARGED (MAIN DOOR)

CLE - THE MAIN ENTRANCE DOOR OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (M)

Part: CONNECTOR — FAILED (WHEELWELL)

CLT - FLT 0052 - FLIGHT RETURNED TO CLT DUE TO A FUEL IMBALANCE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED A CONNECTOR IN THE WHEELWELL AND SEVERAL FLAG TERMINALS ON THE PROBES. (X)

Part: ANGLE — CRACKED (RT VERT STAB)

PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 55-30-01 AND FOUND 2 .5 INCH CRACKS IN RT SIDE CONNECTION ANGLE AT VERTICAL STABILIZER TO FUSELAGE AT 50 PERCENT SPAR. CUT OUT CRACK SECTION OF ANGLE AND ACCOMPLISHED SPLICE REPAIR PER SRM 55-31-00. (Z)

Part: CLIP — CRACKED (FRAME 3450)

PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 53-10-09 AND FOUND ONE .5 INCH CRACK RT AISLE OF MAIN FRAME CLIP 3450 40 INCHES ABOVE FLOOR LEVEL. REMOVED AND REPLACED CLIP PER SRM 53-02-12 FIG 6 AND USAIR EO 5391L681. (Z)

Part: SEQUENCING VLV — FAILED (NLG)

SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07. LEAK AND OPERATION CHECKS NORMAL. REF USAA950011.

Part: SELECTOR VLV — FAILED (NLG)

SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07. LEAK AND OPERATION CHECKS NORMAL. REF 95ZZZW83.