N482US
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
433 reports on file, 1995-05-16 – 2001-11-29.
Part: RIVET — MISSING (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - TWO RIVET HEADS MISSING ON FUSELAGE SKIN AT FRAME 16060 NEAR STRINGER 55. REPAIRED IAW FOKKER SRM 51-31-01.
Part: RIVET — LOOSE (VERTICAL STAB) · airframe 33,478 hrs · 40,605 cycles
PDX - VERTICAL STABILIZER SMOKING RIVETS LT SIDE JUST BELOW RIB 5 ON 50 PERCENT SPAR. REPAIRED IAW HORIZON AIR EA 4-55-299.
Part: RIVET — LOOSE (VERTICAL STAB) · airframe 33,478 hrs · 40,605 cycles
PDX - VERTICAL STABILIZER SMOKING RIVET JUST BELOW RIB 5 ON 50 PERCENT SPAR RT SIDE. REPAIRED IAW HORIZON AIR EA 4-55-299.
Part: ANGLE — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - REMOVE DAMAGED LOWER THRESHOLD COAMING AND REPLACE WITH A34918-007. REPAIRED IAW HORIZON AIR EA 4-53-904A AND FOKKER MM 51-30-00, PAGE 701-706.
Part: SHIM — DAMAGED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING FUEL ACCESS APERTURE 71A, SHIM HAS BEEN BLENDED COMPLETELY THROUGH AT SEVERAL SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-568.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FLOORBEAM CRACKED 9 INCHES AFT OF FRAME 3450 AND APPROXIMATELY 30 INCHES FROM SERVICE/EMERGENCY DOOR. REPAIRED IAW HORIZON AIR EA 4-53-1525 AND FOKKER SRM 53-02-14.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACK AT VERTICAL FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - ANGLED FRAME 15810 TIE IN CLIP TO FUSELAGE BELLY SKIN HAS CORROSION ON TOP SURFACE BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE INTERIOR BELLY SKIN HAS CORROSION AROUND (8) RIVETS BETWEEN FRAMES 15635 AND 15810, FROM STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9 AND SRM 51-31-01.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE INTERIOR BELLY SKIN AT AFT SIDE OF FRAME 16060 BETWEEN STRINGER 1 AND 2 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - ANGLED FRAME 15810 HAS CORROSION ON FORWARD AND AFT SIDES AT CUTOUTS AROUND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE BELLY STRINGER 1 HAS CORROSION AT TIE IN CLIP AREA AFT SIDE OF FRAME 16060. REPAIRED IAW FOKKER SRM 51-10-01, 4B, C, PAGE 9.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE FRAME 15635 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND RIVETS BETWEEN STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE INTERIOR BELLY SKIN DOUBLER HAS CORROSION AROUND (3) RIVETS AT AFT SIDE OF ANGLED FRAME 15810 BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 6.
Part: STRUCTURE — CHAFED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - STRUCTURE IS CHAFED AT LOWER ATTACH POINT FOR LT WING ROOT FAIRING 91J. REPAIRED IAW HORIZON AIR EA 4-57-569.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE ROUND RIVETS BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 22293 CRACKED APPROXIMATELY 1.5 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-1524.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 22293 CRACKED APPROXIMATELY .5 INCH IN OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-1524.
Part: DOUBLER — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 11905 RT COLD SLEEVE REPAIR PLATE HAS 10/32 SCREW CHAFE DAMAGE AT .023 DEEP. REPAIRED IAW HORIZON AIR EA 4-53-1523.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 340-404. REPAIRED IAW HORIZON AIR EA 4-53-1527.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK IS PITTED ON INBOARD FLANGE AT APPROXIMATELY STATION 676 - 685. REPAIRED IAW HORIZON AIR EA 4-53-1527.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 306 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1527.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 22293 CRACKED APPROXIMATELY 1.25 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 21A. REPAIRED IAW HORIZON AIR EA 4-53-1524.
Part: STRINGER — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CLIP ON CASTELLATION, FRONT SIDE OF FRAME 50-2 IS CHAFING INTO STRINGER 27. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, PARAGRAPH 3E AND SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS THREE PITS ON OUTBOARD FLANGE AT APPROXIMATELY STATION 232 - 234. REPAIRED IAW HORIZON AIR EA 4-53-1528.
Part: CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CLIP CONNECTING LOWER WING TO FUSELAGE FAIRING SUPPORT AT FRAME 13815A AND CENTER RIB IS CRACKED. REPAIRED IAW FOKKER SRM 53-53-04, FIGURE 5, ITEM 190, SRM 51-30-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FLOORBEAM REPAIR BL 0 JUST FORWARD OF FRAME 4900 TOP TIE PLATE HAS LIGHT CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-1526.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 349 - 357. REPAIRED IAW HORIZON AIR EA 4-53-1528.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 325 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1528.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 180.5 TO 191. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-11-4, AND SRM 51-30-02.
Part: SUPPORT — BENT (FAIRING) · airframe 33,478 hrs · 40,605 cycles
PDX - BENT FAIRING SUPPORT STRUCTURE IS BENT. REPAIRED IAW FOKKER SRM 53-53-11, PAGE 35, ITEM 265, SRM 51-10-4, PARAGRAPH 4 B AND C.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, SRM 51-31-01 AND SRM 53-10-05.
Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 33,478 hrs · 40,605 cycles
PDX - DENT 1.8 INCH LONG, 1.2 INCH WIDE, APPROXIMATELY .10 INCH DEEP ON TOP EDGE OF CENTER CARGO DOOR, 15INCHES AFT OF LEADING EDGE OF DOOR. REPAIRED IAW MM 51-00-00, PAGE 1 AND MM 51-30-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 14755 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 70 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: STRAP — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - THREE RIVETS PULLED THROUGH STRAP ON BELLY SKIN JUST AFT OF RT MAIN LANDING GEAR DOOR. REPAIRED IAW FOKKER SRM 51-31-05.
Part: STRAP — CRACKED (SPEEDBRAKE) · airframe 33,478 hrs · 40,605 cycles
PDX - SPEEDBRAKE ACCUMULATOR FORWARD MOUNT ASSEMBLY TOP FINGER STRAP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 5 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 6 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: VANE — CHAFED (T/E FLAP) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING INBOARD, TRAILING EDGE FLAP, VANE, LEADING EDGE IS CHAFED AT OUTBOARD END. REPAIRED IAW FOKKER SRM 51-10-4, SRM 57-01-01, PAGE 3 AND FOKKER MM 51-30-00.
Part: CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 16660 CLIP CRACKED AT INBOARD END IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CORROSION ON FUSELAGE SKIN CUTOUT NEXT TO RIVETS AND NUT PLATES WHERE AFT BLANKING PLATE ATTACHES FOR RADIO ALTIMETER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-1521.
Part: RIB — CRACKED (HORIZ STAB) · airframe 33,478 hrs · 40,605 cycles
PDX - HORIZONTAL STABILIZER LEADING EDGE 51B THIRD RIB FROM INBOARD END CRACK TOP FORWARD. REPAIRED IAW FOKKER SRM 51-10-4, SRM 51-31-01, PAGE 13, PARAGRAPH 7B.
Part: DOUBLER — TORN (CARGO DOOR) · airframe 33,478 hrs · 40,605 cycles
PDX - BOTTOM TRAILING CORNER OF REPAIR DOUBLER TORN, CENTER CARGO DOOR INNER SKIN, 10 INCHES FORWARD OF TRAILING EDGE OF CENTER CARGO DOOR, ALONG BOTTOM OF DOOR. REPAIRED IAW HORIZON AIR EA 4-52-462 AND FOKKER MM 51-30-00 AND FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION AT TOP OF OBLIQUE FRAME 41-2 AT STRINGER 43 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 6, PAGE 8, SRM 51-10-4 AND 53-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED IN RADIUS ON FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 48. REPAIRED IAW FOKKER SRM 51-10-0, SRM 53-02-18, PAGE 5 AND SRM 53-10-05, PAGE 601.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT VHF LOWER COMM ANTENNA LOCATION HAS SURFACE CORROSION ON FUSELAGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 A AND B, SRM 51-31-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 14755 CORROSION TOP SURFACE AND UNDERSIDE OF TOP FLANGE AT STRINGER 72. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY ANTENNA BOX STRUCTURE AND AIRCRAFT INTERIOR BELLY SKIN FORWARD OF AND INSIDE BOX IS CORRODED BETWEEN STRINGER 1 AND 74 AT AFT SIDE OF FRAME 15205. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.
Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 33,478 hrs · 40,605 cycles
PDX - DENT IN CENTER CARGO DOOR, FORWARD, LOWER CORNER, 2.5 INCHES LONG, 1.2 INCHES WIDE, APPROXIMATELY .150 INCH DEEP. REPAIRED IAW FOKKER SRM 51-10-4 AMD SRM 51-31-01.
Part: RIVET — CHAFED (CARGO DOOR) · airframe 33,478 hrs · 40,605 cycles
PDX - RIVET HEAD CHAFED THROUGH, NEAR LATCHING MECHANISM ON CENTER CARGO DOOR SUPPORT ROD. REMOVED AND REPLACED RIVET WITH CR3223 5-2 RIVET.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 11405 LT SIDE TO CENTER WING TIE BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1520.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SURFACE AND UNDER SIDE OF TOP FLANGE AT STRINGER 3. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED BEYOND 1ST STOP DRILL AND PROGRESSING UP WEB OF CASTELLATION ON FRAME 17565, ABOVE STRINGER 10. REPAIRED IAW FOKKER SRM 53-02-13.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 1 AND 74 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACKS ON VERTICAL WEB. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SIDE OF UPPER FLANGE FROM STRINGER 2 TO 72. REPAIRED IAW FOKKER SRM 51-10-04.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN AT STRINGER 74 HAS CORROSION ON TOP SURFACE AROUND RIVET HOLE. REPAIRED IAW FOKKER SRM 53-02-13, SRM 51-10-04 AND SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15635 DRAIN HOLE AND 90 DEGREE FLANGE AREA TOP SURFACE IS CORRODED BETWEEN STRINGER 1 AND 74 AT FORWARD SIDE OF FRAME 15635. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.
Part: FLANGE — CRACKED (CARGO DOOR) · airframe 33,478 hrs · 40,605 cycles
PDX - CENTER CARGO DOOR LOWER FORWARD CORNER FLANGE ABOVE SEAL MATING SURFACE CRACKED. REPAIRED IAW FOKKER SRM 52-02-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, PAGE 5.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A 1.2 INCH LONG BY .150 INCH WIDE CHAFE MARK 3 INCHES FORWARD OF FRAME 1890, CHAFE IS THROUGH CLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH D, AREA B AND SRM 51-01-4, AMM 51-30-00, PAGE 701-706.
Part: DUCT — CRACKED (ACM EXHAUST) · airframe 33,478 hrs · 40,605 cycles
PDX - RT ACM EXHAUST DUCT HAS A 2.5 INCH CRACK ALONG A WELD AT BOTTOM EDGE OF PANEL. REPAIRED IAW FOKKER MM 21-50-8, PAGE 401, PARAGRAPH 2 AND AMM 51-30-00, PAGE 701-706.
Part: SUPPORT — CHAFED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING SKIN LOWER SURFACE SUPPORT STRUCTURE CHAFED. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-30-00, PAGE 701-706.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION WORKING POSSIBLY CRACKED WITH LOOSE RIVETS ON FRAME 17565 BETWEEN STRINGERS 9 AND 10. REPAIRED IAW FOKKER SRM 53-02-13.
Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 33,478 hrs · 40,605 cycles
PDX - RT FORWARD EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05.
Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 33,478 hrs · 40,605 cycles
PDX - RT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED BEYOND 1ST STOP DRILL ON FRAME 17565 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13.
Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 33,478 hrs · 40,605 cycles
PDX - LT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED ADJACENT TO DIMPLE AT LOWER RIVET IN FRAME 17565 ABOVE STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, PAGE 5 AND SRM 51-31-01.
Part: STRINGER — BROKEN (RUDDER) · airframe 33,478 hrs · 40,605 cycles
PDX - RUDDER, RT STRINGER BROKEN AT RIB 6, BEHIND PANEL 57Y. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A .75 INCH LONG X .100 INCH WIDE CHAFE MARK, 5 INCH FORWARD OF FRAME 1890, CHAFE IS THROUGH ALCLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AREA B.
Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 33,478 hrs · 40,605 cycles
PDX - RT AFT EMERGENCY EXIT DOOR IS CRACKED IN RADUIS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3,
Part: SKIN — DENTED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - DENT IN FUSELAGE SKIN APPROXIMATELY .040 INCH DEEP, 1 INCH WIDE, 1 INCH LONG, LOCATED 9.375 INCH FORWARD OF CUT OUT FOR THE RT SERVICE EMERGENCY DOOR JUST BELOW STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-02.
Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 33,478 hrs · 40,605 cycles
PDX - LT FORWARD EMERGENCY EXIT DOOR IS CRACKED IN RADIUS ON OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND SRM 51-31-05.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT TOP RIVET ON FRAME 17565 BELOW STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED ADJACENT TO LOWER RIVET ON FRAME 17565 ABOVE STRINGER 55. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8-9 AND SRM 53-02-13.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT SIDE COCKPIT EXTERNAL SKIN HAS A .25 INCH LONG X .100 INCH WIDE CHAFE MARK, 10 INCHES FORWARD OF FRAME 1890, CHAFE IS THROUGH ALCLAD LAYER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, AREA B AND AMM 51-30-00, PAGE 701-706.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815B AND STRINGER 47 CLIP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815A AND STRINGER 41 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET HOLE ON FRAME 32-2 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01.
Part: SKIN — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - EMPENNAGE SKIN GOUGED FROM INSIDE, FORWARD OF OBLIQUE FRAME 58.5-2, ABOVE STRINGER 9, APPROXIMATELY .2 INCHES LONG, .050 INCH WIDE, .040 INCH DEEP. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED PAST PREVIOUS STOP DRILL ON AFT SIDE OF FRAME 16-2, ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND FOKKER MM 51-31-01.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 14285 AND STRINGER 47 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815A AND STRINGER 31 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 41-2 ABOVE STRINGER 61. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 14(E) AND SRM 53-10-05, PAGE 601-601A.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET OF FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 14. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY ANGLED FRAME THAT TIES INTO FORWARD END OF DOOR LOWER TORSION BOX AT FRAME 15810 HAS CORROSION AT FORWARD AND AFT SIDE OF STRINGER 1 AND 74 CUTOUTS. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 11405 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 50-2 ABOVE STRINGER 61. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A, SRM 51-31-01, PAGE 14(E).
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815A AND STRINGER 46 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED IN RADIUS AT JOGGLE ON AFT SIDE OF FRAME 32-2 ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13345 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 15205 AND STRINGER 21 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 9 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 15205 AND STRINGER 53 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 9 AND SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY BELLY SKIN HAS AREAS MARKED WITH CORROSION AT AFT EDGE OF LOWER CONNECTION ANGLE OF FRAME 15635 TO 8 INCHES AFT OF FRAME BETWEEN STRINGER 2 AND 73. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15635 HAS CORROSION ON AFT SIDE BOTTOM CONNECTION FLANGE TO SKIN BETWEEN STRINGER 3 AND 73. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 15205 AND STRINGER 52 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12875 AND STRINGER 42 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - POSSIBLE CRACK IN CASTELLATION ADJACENT TO DIMPLE AT LOWER RIVET IN FRAME 17565, ABOVE STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01.
Part: CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME CLIP CRACKED AT STRINGER 47 AND FRAME 16060. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED ADJACENT TO LOWER RIVET ON OBLIQUE FRAME 16-2 ABOVE STRINGER 12. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - DENT IN FORWARD CARGO DOOR APERTURE, FRAME 5805, WL 50.0. REPAIRED IAW FOKKER SRM 53-02-16, PAGE 3, FIGURE 1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FLOORBEAM BL600L FROM FRAME 3820 TO 4900 TOP TIE PLATE HAS LARGE BUBBLES OF PAINT AND CORROSION. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 51-31-01.
Part: RIVET — MISSING (ATTACH ANGLE) · airframe 33,478 hrs · 40,605 cycles
PDX - ATTACH ANGLES MISSING RIVETS ABOVE RT FIXED WINDOW, FRAME STATION 4050 AND STRINGER 45. REPAIRED IAW FOKKER MM 51-31-01.
Part: STOP FITTING — WORN (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT AFT OVERWING EMERGENCY EXIT APERTURE STOP PLATES TWO EACH ARE STEP WORN. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED IN RADIUS UPPER AND AFT SIDE OF FRAME 50-2 BELOW STRINGER 24. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601-601A AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13345 AND STRINGER 28 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT JOGGLE FOR LOWER RIVET ON FRAME 17565 ABOVE STRINGER 50. REPAIRED IAW FOKKER SRM 53-10-05, PP 601A AND SRM 53-02-13, PAGE 5.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED AT LOWER RIVET ON FORWARD SIDE OF FRAME 50-2, ABOVE STRINGER 25. REPAIRED IAW FOKKER SRM 51-10-4, SRM 53-02-13, PAGE 5 AND SRM 53-10-05.
Part: RIVET — LOOSE (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE SKIN TO FRAME 13815A RIVET IS LOOSE AND DOES NOT FILL THE COUNTERSINK. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN HAS CORROSION ON TOP SURFACE AT STRINGER 3. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - CASTELLATION CRACKED IN RADIUS LOWER END OF FRAME 32-2, FORWARD SIDE ABOVE STRINGER 23. REPAIRED IAW FOKKER MM 53-10-05, PAGE 610-601A.
Part: CLIP — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 16660 CLIP CORRODED AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 16060 HAS CORROSION ON TOP SURFACE OF LOWER FLANGE ON FORWARD SIDE BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-01 AND SRM 51-10-04.
Part: RUDDER — DAMAGED (TAIL) · airframe 33,478 hrs · 40,605 cycles
PDX - REMOVE RUDDER FOR SHEET METAL REPAIR. REPAIRED IAW FOKKER MM 27-20-01, PAGE 404, PARAGRAPH 3D AND MM 27-20-02, PAGE 201.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 248-249. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SKIN — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING FUEL ACCESS PANEL 73A, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGES 703 AND 704, PARAGRAPH 3-C, STEPS 1 THRU 10.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS SEVERAL GOUGES IN TOP OF RAIL THE DEEPEST APPROXIMATELY .003 INCH AT APPROXIMATELY STATION 510-512. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION AT APPROXIMATELY STATION 331-333 ON INBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 1B(2).
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 193-200. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 327 TO 330. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 376-425. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION IN BOTTOM OF CHANNEL AT APPROXIMATELY STATION 559-562. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 347-357. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING FUEL ACCESS PLATE 73B, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGES 703-704, PARAGRAPH 3-C STEPS 1 -10.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS A CHAFE ON OUTBOARD FLANGE AT APPROXIMATELY STATION 583. REPAIRED IAW FOKKER SRM 53-40-01, FIGURE 204.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT OUTBOARD SEAT TRACK HAS SEVERAL GOUGES ON TOP OF RAIL AT APPROXIMATELY STATION 677 TO 683. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PITTING CORROSION ON INBOARD AND OUTBOARD FLANGES AT APPROXIMATELY STATION 202-256. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION AT APPROXIMATELY STATION 228 TO 242, BOTTOM OF CHANNEL. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 388-405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT OUTBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 331 TO 335. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON INBOARD FLANGE AT APPROXIMATELY STATION 561-563. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS A GOUGE ON THE TOP RAIL AT APPROXIMATELY STATION 337-338. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — SCRATCHED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT OUTBOARD SEAT TRACK HAS A SCRATCH ON TOP OF RAIL AT APPROXIMATELY STATION 491. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION BOTTOM OF CHANNEL AT APPROXIMATELY STATION 223 TO 225. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 387-398. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS GOUGE ON TOP RAIL AT APPROXIMATELY STATION 434. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 684-695. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 520-531. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION IN BOTTOM OF CHANNEL AT APPROXIMATELY STATION 357-359. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 475-478. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS A WORN SPOT ON TOP RAIL AT APPROXIMATELY STATION 593. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP OF RAIL AT APPROXIMATELY STATION 180.5 TO 187. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS A GOUGE IN INBOARD FLANGE AT APPROXIMATELY STATION 503. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS HOLE EDGE DAMAGE ON TOP OF RAIL AT APPROXIMATELY STATION 653. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS WEAR ON TOP OF RAIL AT APPROXIMATELY STATION 195-196. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS SLIGHT DAMAGE TO HOLE EDGE AT APPROXIMATELY STATION 370-371. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 510-520. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 204 AND SRM 51-10-4, PARAGRAPH 4B(2).
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING FUEL ACCESS PANEL 73C MATING FLANGE ON WING SHOWS LIGHT FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGES 703-704, PARAGRAPH 3-C, STEPS 1-10.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 256-272. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 656-567. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT OUTBOARD SEAT TRACK HAS A GOUGE ON TOP OF TRACK AT APPROXIMATELY STATION 673.5. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS LIGHT PITTING CORROSION INBOARD FLANGE AT APPROXIMATELY STATION 306. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT OUTBOARD SEAT TRACK HAS WORN AREA AT BOTTOM OF GROOVE APPROXIMATELY STATION 192. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - LT INBOARD SEAT TRACK HAS WORN AREA FRONT TOP EDGE OF RAIL AT APPROXIMATELY STATION 254. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4B(2).
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12405 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE BELLY FAIRING FRAME CLIP IS CRACKED AT FRAME 13815B AT THE 6 O'CLOCK POSITION. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815B CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1, PAGE 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 10346 AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: PAINT — MISSING (SEAT TRACK) · airframe 33,478 hrs · 40,605 cycles
PDX - RT INBOARD SEAT TRACK HAS PAINT MISSING IN BOTTOM CHANNEL AT APPROXIMATELY STATION 623-638. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9-B2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12875 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12405 AND STRINGER 39 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12405 AND STRINGER 36 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 11405 AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 10966 AND STRINGER 44 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 10966 AND STRINGER 43 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815B CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER NR 2. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1, PAGE 2.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815B AND STRINGER 40 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815B AND STRINGER 41 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815B AND STRINGER 45 CLIP CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12405 AND STRINGER 42 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 13815B AND STRINGER 32 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FRAME 12405 AND STRINGER 40 CLIP IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4.
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 71A FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4 AND SRM 51-10-4.
Part: BOLT — STRIPPED (WING) · airframe 33,478 hrs · 40,605 cycles
PDX - INSIDE FUEL PANEL 72A, 5TH VENT STRUT FROM FORWARD SPAR TOP AND BOTTOM OUTBOARD MOUNTING BOLTS WILL NOT TIGHTEN UP. REPAIRED IAW FOKKER SRM 51-31-01.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - DOUBLER FORWARD OF FRAME 16660 BETWEEN STRINGER 1 AND 74 CORRODED. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 6 AND SRM 51-10-4.
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73C FLANGE. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4.
Part: PANEL — CORRODED (WING) · airframe 33,478 hrs · 40,605 cycles
PDX - FRETTING CORROSION AROUND SCREW HOLES ON PANEL 74C. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4.
Part: PANEL — CORRODED (RT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - RIGHT WING FUEL PANEL 72A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4.
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73B FLANGE. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4.
Part: SKIN — CRACKED (RUDDER) · airframe 33,478 hrs · 40,605 cycles
PDX - RUDDER APERTURE FOR PANEL 574 IS CRACKED AT NUT PLATE HOLES. REPAIRED IAW FOKKER SRM 51-31-01.
Part: PANEL — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - FRETTING CORROSION PRESENT ON LT WING FUEL PANEL 73A FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 4 AND SRM 51-10-4.
Part: SKIN — CORRODED (LT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - LT WING FUEL ACCESS PANEL 71A, MATING FLANGE ON WING SHOWS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-30-03, PAGE 703, PARAGRAPH 3 A-C.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13015 CASTELLATION TIE IN TO BELLY SKIN OUTBOARD OF STRINGER 1 HAS CORROSION ON TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13015 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 74 HAS CORROSION ON TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 AND SRM 53-01-01, PAGE 6.
Part: SPOILER — DENTED (RT WING) · airframe 33,478 hrs · 40,605 cycles
PDX - DENT ON RT NR 5 LIFE DUMPER PANEL 82G. REPAIRED IAW FOKKER SRM 51-70-0, PAGE 13, FIGURE 7, PARAGRAPH C.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY INTERIOR BELLY SKIN HAS CORROSION 1 INCH INBOARD OF STRINGER 73 EXTENDING UNDER FRAME 13815A CASTELLATION TIE-IN AT AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PAGE 4.
Part: RIB — CRACKED (RUDDER) · airframe 33,478 hrs · 40,605 cycles
PDX - RUDDER STRUCTURE RIB NR 5 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815A HAS CORROSION ON TOP OF FRAME UNDER FLOOR SUPPORT 4 WAY TIE-IN AT STRINGER 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 73 AND 74 HAS CORROSION ON TOP SIDE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PAGE 4.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, PAGE 9.
Part: RIB — CRACKED (RUDDER) · airframe 33,478 hrs · 40,605 cycles
PDX - FOUND NR 6 RIB CRACKED BEHIND PANEL 573. REMOVED AND REPLACED RIB PER FOKKER SRM 51-31-01.
Part: RIB — CRACKED (RUDDER) · airframe 33,478 hrs · 40,605 cycles
PDX - RUDDER STRUCTURE RIB NR 4 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FITTING — CORRODED (NR 2 NACELLE) · airframe 33,478 hrs · 40,605 cycles
PDX - NR 2 NACELLE AFT MOUNT BEAM AT ENGINE CHATTER PROOF BOLT END HAS SURFACE CORROSION ON FORWARD LUG. REPAIRED IAW FOKKER SRM 51-01-04.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE BELLY SKIN CHAFED FROM PANEL 92BD, RT FUSELAGE BETWEEN FRAMES 15205 AND 15635 AND STRINGER 66 AND 65. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5F, SRM 53-23-01, PAGE 9, ITEM 51, SRM 51-10-4, PAGE 94B AND SRM 51-10-4, PAGE 8-3C.
Part: SUPPORT — CORRODED (RT ENGINE) · airframe 33,478 hrs · 40,605 cycles
PDX - FORWARD ENGINE SUPPORT BEAM SHACKLES HAVE SURFACE CORROSION AT RT STUBWING. REPAIRED IAW IPC 71-20-01, FIGURE 1, ITEM 15 AND 4313-1B, CHAPTER 6, PARAGRAPH 165.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE-IN TO BELLY SKIN IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - AFT CARGO BAY FRAME 13815A CASTELLATION TIE IN TO BELLY SKIN IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: BOLT — CORRODED (ENGINE MOUNT) · airframe 33,478 hrs · 40,605 cycles
PDX - FORWARD ENGINE MOUNT BEAR ATTACH BOLTS AND NUTS HAVE SURFACE CORROSION ON RT STUB WING. REPAIRED IAW REF:43-13-1B, CHAPTER 6, PARAGRAPH 165.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE BELLY SKIN CHAFED BETWEEN FRAMES 15205 AND 15635, STRINGERS 8 AND 9. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - BELLY SKIN CHAFED FROM CONTACT WITH PANEL 91BD ALONG FUSELAGE BETWEEN FRAMES 14755 AND 15205 AND STRINGER 67 AND 68. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 9, ITEM 60, SRM 51-10-4, PAGE 9 4B AND SRM 51-10-9, PAGE 8 3C.
Part: SKIN — CHAFED (FUSELAGE) · airframe 33,478 hrs · 40,605 cycles
PDX - FUSELAGE BELLY SKIN CHAFED FROM LOWER EDGE OF PANEL 92BD ON RT FUSELAGE BETWEEN FRAMES 14755 AND 15205 AND STRINGER 67 AND 68. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-23-01, PAGE 9, ITEM 51, SRM 51-10-4, PAGE 9 AND SRM 51-10-4, PAGE 8-3C.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,201 hrs · 40,362 cycles
PDX - EVACUATION LIGHTS AT SEAT 8AB IS MISSING LENS COVER AND IS INOPERABLE. INSTALLED LENS COVER AND AND RECONNECTED WIRE AS REQUIRED. OPERATIONAL CHECK IS GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 32,953 hrs · 40,126 cycles
PDX - THE NR 1 GALLEY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 42,499 hrs · 52,706 cycles
BOI - MID CABIN EXIT SIGN REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 32,882 hrs · 40,064 cycles
GEG - MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT CARD. OPERATIIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 32,473 hrs · 39,680 cycles
FCA - AFTER GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. GEAR WAS CYCLED AS PER CHECK LIST, AT SUCH TIME THE NR 1 HYDRAULIC QUANTITY INDICATED ZERO. AFTER COMPLETING HYDRAULIC FAILURE CHECK LISTS, EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH EXTENDED ROLL OUT, BUT WITH OUT FURTHER COMPLICATIONS. AIRCRAFT GROUNDED.
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 32,474 hrs · 39,680 cycles
PDX- AFT SMOKE DETECTOR IN AFT BAG COMPARTMENT HAS RED LIGHT SHOWING. REMOVED AND REPLACED AFT SMOKE DETECTORS IN AFT CARGO PIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,467 hrs · 39,672 cycles
BIL- EMERGENCY EXIT ROW 9 SEAT A LIGHT INOPERATIVE.
Part: CABLE — INOPERATIVE (DOOR) · airframe 32,324 hrs · 39,548 cycles
PDX-WITH AIRSTAIR DOOR HANDLE IN ALTERNATE POSITION, CAN''''T PUSH OPEN AIRSTAIR DOOR. REMOVED AND REPLACED PASSENGER DOOR ACTUATOR MECHANICAL RELEASE CABLE FROM INBOARD HANDLE TO CABLE TENSION BALANCE LINK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LANDING GEAR — FAILED (NLG) · airframe 32,232 hrs · 39,460 cycles
YEG - ON GEAR EXTENTION, NOSE LANDING GEAR INDICATED NOT DOWN AND LOCKED. CYCLED GEAR, ALL INDICATION NORMAL. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,296 hrs · 39,429 cycles
PDX-LAST 4 ROWS OF ESCAPE PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT SEAT 14A FOR REAR 4 ESCAPE PATH LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,007 hrs · 39,246 cycles
BOI- CENTER AND AFT AISLE EXIT PLACARDS HAVE BULBS INOPERATIVE. REPLACED BOTH LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,941 hrs · 39,183 cycles
PDX- ROWS 10 - 17 SEAT EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED ROW 14 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 1995–2000 · 216 reports
2000
Part: SMOKE — DETECTED (COCKPIT) · airframe 31,671 hrs · 38,922 cycles
GEG - REPORT OF SMOKE IN CABIN AREA. UPON INSPECTION, FOUND NO EVIDENCE OF SMOKE. GROUND RAN ENGINES AND APU. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,428 hrs · 38,686 cycles
SEA- EXIT LIGHT OVER ROW 9 INOPERATIVE. REMOVED AND REPLACED FORWARD AND AFT AISLE EXIT LIGHT ASSY. PERFORMED EMERGENCY EXIT LIGHT CHECK, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,920 hrs · 38,212 cycles
SEA- FORWARD EMERGENCY LIGHT OVER FLIGHT DECK DOOR HAS BULB INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (GALLEY) · airframe 30,920 hrs · 38,212 cycles
SEA- EMERGENCY EXIT LIGHT OVER GALLEY HAS BULBS OUT. REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 30,784 hrs · 38,073 cycles
FEA - THE EMERGENCY EXIT SIGN, IN THE FORWARD CABIN AREA WAS FOUND INOPERATIVE. AIRCRAFT WAS FERRIED TO SEA MAINTENANCE FACILITY AND THE SIGN ASSEMBLY WAS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,670 hrs · 37,952 cycles
PDX- LEFT HAND FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD BELLY CARGO COMPARTMENT POWER SUPPLY UNIT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DRAIN LINE — DIRTY (ACM) · airframe 30,595 hrs · 37,876 cycles
SEA - OIL SMELL REPORTED IN CABIN BEFORE TAKEOFF. OIL SMELL DISSIPATED AFTER TAKEOFF. CLEANED DRAIN LINES IN AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 30,366 hrs · 37,649 cycles
GEG- CENTER AISLE EXIT SIGN FORWARD SIDE AT ROW 8 IS INOPERATIVE. REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (ROW 8) · airframe 30,358 hrs · 37,643 cycles
SEA- EXIT SIGN ROW 8 INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 30,292 hrs · 37,578 cycles
GEG - OVERHEAD EXIT SIGN AT ROW 8 FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,235 hrs · 37,530 cycles
PDX - THE EMERGENCY ESCAPE PATH LIGHTING AT ROWS 11 - 14 WERE FOUND INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: RECEPTACLE — INOPERATIVE (GALLEY) · airframe 30,100 hrs · 37,392 cycles
GTF- FLIGHT ATTENDANT REPORTED ODOR OF SMOKE FROM COFFEE WARMER AREA. TURNED OFF BOTH COFFEE WARMERS, ODOR DISAPPEARED. INSTALLED NEW POWER RECIPTICAL ON LOWER COFFEE WARMER POSITION. TURNED ON WARMER UNTIL COFFEE WAS HOT, NO ODOR NOTED.
Part: TRANSFORMER — FAILED (E/E BAY) · airframe 30,100 hrs · 37,392 cycles
SEA- FLIGHT ATTENDANT REPORTED ELECTRIC SMELL. SELECT DC ESSENTIAL TRANSFORMER RECTIFIER UNIT AND FOUND DC VOLTS OFF SCALE, INDICATOR SHORT. PULLED ESSENTIAL TRANSFORMER RECTIFIER UNIT CIRCUIT BREAKER. NO MORE ELECTRIC SMELL TILL SHORT FINAL, MORE SMELL. INSPECTED TRANSFORMER RECTIFIER UNIT 1, TRANSFORMER RECTIFIER 2 AND ESSENTIAL TRANSFORMER RECTIFIER. NO DEFECTS OR SIGNS OF SMOKING NOTED. PERFORMED TRANSFORMER RECTIFIER UNIT TEST. ALL TRANSFORMER RECTIFIER UNITS OPERATIONAL CHECK GOOD. NO PARTS REPLACED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,030 hrs · 37,320 cycles
GEG - OVERHEAD EXIT SIGNS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT ROW 13AB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 29,879 hrs · 37,166 cycles
SEA - AFTER START, FLIGHT ATTENDANT ADVISED FLIGHT US OF A HEAVY TOXIC ODOR IN CABIN. CHECKED SERVICE LEVEL OF ACM OILS, COCKPIT SLIGHTLY OVERSERVICED, ADJUSTED LEVEL. CHECKED ACM COOLINR INLET & OUTETS. NO DISCREPANCIES NOTED. GROUND RAN ENGINE AND BOTH PACKS. NO ABNORMAL ODORS. COULD NOT DUPLICATED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
Part: CSD — MALFUNCTIONED (ENGINE)
PDX - DURING DESCENT, NR 2 CONSTANT SPEED DRIVE WARNING LIGHT ILLUMINATED. DISCONNECTED NR 2 CONSTANT SPEED DRIVE AS PER EMERGENCY CHECK LIST. NR 2 DRIVE TEMP DECREASED BUT REMAINED ABOVE RED LINE. CHECKED CONSTANT SPEED DRIVE OIL LEVEL. DEFERED SYSTEM. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN)
SEA - OVERHEAD MIDCABIN EXIT SIGN WAS REPORTED AS HAVING INOPERATIVE LIGHTS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
1999
Part: FRAME — MISDRILLED (FRAME 8805)
PDX - THERE ARE TWO DRILLED HOLES IN FRAME 8805 ABOVE STRINGER 67IN THE FORWARD CARGO BAY. REPAIRED IAW HORIZON AIR EA 4-53-921.
Part: BULKHEAD — CHAFED (FUSELAGE)
PDX - ANGLE AND BULKHEAD CHAFFED IN RIGHT WHEELWELL WHERE AFT OUTBOARD EDGE OF GEAR DOOR CONTACTS. REPAIRED IAW HORIZON AIR EA 4-57-328.
Part: POST — CRACKED (COCKPIT WINDOW)
PDX - TYPE A CRACK ON RIGHT SIDE NR 3 WINDOW POST. REPAIRED IAW HORIZON AIR EA 4-53-56B.
Part: FRAME — CRACKED (FRAME 50)
PDX - THERE IS A CRACK ON THE CORNER CUTOUT FOR STRINGER 27 ON FRAME 50-2. REPAIRED IAW HORIZON AIR EA 4-53-934.
Part: FRAME — CRACKED (FUSELAGE)
PDX - FRAME 32-2 AND STRINGER 25 HAS THREE CRACKS AROUND BOTTOM RIVET OF CLIP. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND FOKKER MM 53-10-05, PAGE 601.
Part: CLIP — CRACKED (FRAME 13815A)
PDX - AFT CARGO PIT CRACKED FRAME CLIP AT FRAME 13815A AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: STRINGER — CRACKED (WS 4700)
PDX - Z STRINGERS 2.13 AND 2.10 ARE CRACKED ON LEFT WING AT APPROXIMATELY STATION 4700. REPAIRED IAW HORIZON AIR EA 4-57-327.
Part: MOUNT — CORRODED (DME ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR DME 2 ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4.
Part: BEAM — DAMAGED (BS 19775)
PDX - THERE IS SEVERE CHAFFING DAMAGE INTO VERTICAL BEAM TENSION MEMBER WEBBING, AT BL425R, JUST AFT OF STATION 19775, REPAIRED IAW HORIZON AIR EA 4-53-932.
Part: FRAME — CORRODED (BS 9305)
PDX - FORWARD CARGO BAY CORROSION ON UNDERSIDE OF UPPER FLANGE OF FRAME 9305 ABOVE STRINGER 2, UNDER AND AROUND NUT PLATE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7.
Part: SKIN — CHAFED (FUSELAGE)
PDX - FUSELAGE SKIN UNDER AFT EDGE OF PANEL 91BC IS CHAFFED. REPAIRED IAW HORIZON AIR EA 4-53-931.
Part: SEAT TRACK — CORRODED (BS 10253 - 10753)
PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT PITTING CORROSION BETWEEN STATION AF4910253 AND 10753. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: SEAT TRACK — CORRODED (COCKPIT)
PDX - CORROSION UNDER PILOTS LEFT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (BS 4900 - 5805)
PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAD PITTING CORROSION BETWEEN FRAMES 4900-5805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: SEAT TRACK — CORRODED (COCKPIT)
PDX - CORROSION UNDER PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (BS 13551 - 13853)
PDX - LEFT-HAND INBOARD SEAT TRACK HAD LIGHT CORROSION PITTING BETWEEN STATION 13551 AND 13853. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: SEAT TRACK — DAMAGED (BS 1305 & 9805)
PDX - LEFT-HAND INBOARD SEAT TRACK HAD GROOVES WORN IN TRACK BETWEEN STATION 1305 AND 9805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND UPPER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB DRIVE FITTING LEFT-HAND UPPER AFT LUG CORRODED. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: SEAT TRACK — CORRODED (COCKPIT)
PDX - CORROSION UNDER CO-PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: SEAT TRACK — CORRODED (BS 8305 - 9305)
PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT PITTING CORROSION AT STATION 8305-9305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB DRIVE FITTING AFT LEFT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: SEAT TRACK — GOUGED (BS 4850)
PDX - LEFT-HAND INBOARD SEAT TRACK AT STATION 4850 WAS CHAFED AND GOUGED. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.
Part: SEAT TRACK — CORRODED (BS 14793 - 15263)
PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAD PITTING CORROSION AT STATION 14793 TO 15263. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: FLOOR PANEL — CORRODED (COCKPIT)
PDX - BL33.0 WL22.047 CORROSION IN SEVERAL PLACES, NEAR AFT WALL 3 OUTBOARD OF CO-PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (BS 9805 - 10253)
PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT PITTING CORROSION BETWEEN STATION 9805 AND 10253. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: SEAT TRACK — CORRODED (COCKPIT)
PDX - CORROSION UNDER CO-PILOTS LEFT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (BS 6805 - 8305)
PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT CORROSION PITTING BETWEEN STATION 6805-8305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB JUNCTION FITTING LOWER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: FLOOR PANEL — CORRODED (COCKPIT)
PDX - CORROSION ON CO-PILOTS FLOOR, 11 FORWARD OD COCKPIT AFT WALL, JUST OUTBOARD OF CO-PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CHAFED (BS 4850)
PDX - LEFT-HAND OUTBOARD CABIN SEAT TRACK WAS CHAFED AT STATION 4850. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB JUNCTION FITTING LOWER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB JUNCTION FITTING UPPER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: FITTING — CORRODED (HORIZONTAL STAB)
PDX - HORIZONTAL STAB JUNCTION FITTING UPPER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.
Part: CLIP — CRACKED (FRAME 13815B)
PDX - AFT CARGO PIT CRACKED FRAME CLIP AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: SKIN — CORRODED (FUSELAGE)
PDX - PANEL 74D ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5.
Part: SKIN — CORRODED (FUSELAGE)
PDX - PANEL APERTURE AND PANEL 72A HAVE PITTING/FRETTING CORROSION AROUND HOLES FOR FASTENERS. REPAIRED IAW 57-01-01, PAGE 5.
Part: SKIN — CORRODED (FUSELAGE)
PDX - SEVERAL RIVET HEADS AND NUT PLATE SURROUNDS ON FUSELAGE SKIN UNDER APU HEAT SHIELD, HAVE LIGHT SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04.
Part: SKIN — CORRODED (FUSELAGE)
PDX - PANEL 74B AND ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND THE FASTENERS. REPAIRED IAW 57-01-01, PAGE 5.
Part: CLIP — CRACKED (FRAME 19976)
PDX - THERE IS A CRACKED CLIP AT FRAME 19976 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIGURE 4 AND FOKKER MM 53-10-05, PAGE 601.
Part: HINGE — WORN (PAX DOOR)
PDX - PASSENGER DOOR HINGE IS WORN TO LIMITS. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.
Part: SKIN — CORRODED (FUSELAGE)
PDX - PANEL 74C AND ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5.
Part: CLIP — CRACKED (FRAME 50)
PDX - THERE IS A CRACKED CLIP AT AFT SIDE OF FRAME 50-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3.
Part: SKIN — CORRODED (FUSELAGE)
PDX - PANEL APERTURE AND PANEL 74A HAS CORROSION AROUND THE FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5.
Part: CLIP — CRACKED (FRAME 20075)
PDX - THERE IS A CRACKED CLIP AT FRAME 20075 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIGURE 4, REPAIR SCHEME 1.
Part: CLIP — CRACKED (FRAME 58.5)
PDX - CRACK IN CLIP AT AFT SIDE OF FRAME 58.5-2, ABOVE STRINGER 46. REPAIRED IAW FOKKER MM 53-10-05.
Part: SKIN — DAMAGED (FUSELAGE)
PDX - TOP LAYER OF FUSELAGE SKIN, IMMEDIATELY AFT OF RADOME IS ROLLED BACK OVER AND AREA OF .375 BY 5 WIDE. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2.
Part: BRACKET — CRACKED (FUSELAGE)
PDX - THERE IS A CRACK IN THE ANGLE/BRACKET WHICH ATTACHES THE SHORT FLOORBEAM TO THE AFT PRESSURE BULKHEAD, AT BL330 RH. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A.
Part: CLIP — CRACKED (FRAME 50)
PDX - THERE IS A CRACKED CLIP AT FRAME 50-2 AND STRINGER 24. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-30-02 AND SRM 53-10-05.
Part: SKIN — DENTED (BS 17565)
PDX - FUSELAGE SKIN IS DENTED IN FOUR AREAS JUST FORWARD OF FRAME 17565, BETWEEN STRINGERS 55-59. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1.
Part: FRAME — CORRODED (BS 9305B)
PDX - FORWARD CARGO BAY CORROSION UNDER TWO NUT PLATES ON FRAME 9305B ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8 FIGURE 3.
Part: BRACKET — CRACKED (FUSELAGE)
PDX - THERE IS A CRACK IN THE ANGLE/BRACKET WHICH ATTACHES THE SHORT FLOORBEAM TO THE AFT PRESSURE BULKHEAD AT BL320LH. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A.
Part: LINK — CHAFED (SPEED BRAKE)
PDX - THERE IS A GROOVE CHAFFED INTO LUG, IN SUPPORT STRUCTURE, DIRECTLY UNDER LEFT SPEED BRAKE PANEL SUPPORT LINK, LOWER ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-53-936.
Part: BULKHEAD — GOUGED (BS 2650)
PDX - LEFT-HAND ACM BAY INNER WALL HAD 4 GOUGE MARKS APPROXIMATELY .25 INCH LONG AND RANGE FROM APPROXIMATELY .003 - .005 DEEP AT FUSELAGE STATION 2650, 13 INCHES FROM BOTTOM OF WALL. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: BULKHEAD — DENTED (FUSELAGE)
PDX - RIGHT-HAND ACM BAY INNER WALL HAD 2 DENTS JUST FORWARD OF LOWER/AFT ACM MOUNT. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: MOUNT — CORRODED (M/B ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR MARKER BEACON ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: MOUNT — CORRODED (DME ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR DME 1 ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B.
Part: MOUNT — CORRODED (ATC ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR LOWER ATC ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C.
Part: FRAME — CORRODED (BS 9305A)
PDX - FORWARD CARGO BAY CORROSION UNDER NUT PLATES AND ON FLANGE OF FRAME 9305A BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3.
Part: FLOORBEAM — CORRODED (BS 3820 - 4610)
PDX - MINOR PITTING CORROSION ON TOP OF FLOORBEAM 600L BETWEEN FRAME 3820 AND 4610. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.
Part: FRAME — DAMAGED (FRAME 8305)
PDX - TOOLING DAMAGE TO PLATE ON TOP OF FRAME 8305 AT CENTER CARGO DOOR LOWER TORSION BOX. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, SRM 51-31-05 AND SRM 51-30-02.
Part: BRACKET — CRACKED (FUSELAGE)
PDX - VERTICAL STIFFENER/BRACKET ON LEFT-HAND FORWARD SIDE OF REAR PRESSURE BULKHEAD WAS CRACKED AND HAD TWO POPPED RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16060)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16060)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (FRAME 19976)
PDX - THERE IS A CRACKED CLIP AT FRAME 19976 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 4, SCHEME 1 AND SRM 51-31-01.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: SKIN — CRACKED (FUSELAGE)
PDX - CRACKS IN RADIUS OF FUSELAGE SKIN TO REAR PRESSURE BULKHEAD STIFFENER/ANGLE, BETWEEN STRINGER 48 AND 49. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4 B&C.
Part: CLIP — CRACKED (BS 16060)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16660)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (BS 16060)
PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: FRAME — CHAFED (BS 16660)
PDX - THERE WAS CHAFING DAMAGE TO FRAME 16660 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9, VIEW C-C.
Part: MOUNT — CORRODED (ALT ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR AFT RAD ALT ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.
Part: MOUNT — CORRODED (ALT ANTENNA)
PDX - AIR FRAME MOUNTING SURFACE FOR FORWARD RAD ALT ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.
Part: DUCT — CRACKED (APU)
PDX - APU FUSELAGE INTAKE DUCT IS CRACKED AT AFT LOWER CORNER. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05.
Part: SIGN — INOP (CABIN)
SEA - LIGHTING DIM IN EXIT SIGN ABOUT COCKPIT DOOR. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOP (CABIN)
GEG - FORWARD GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD.
Part: LIGHT — INOP (CABIN)
PDX - LEFT FORWARD EVACUATION LIGHT INOP. SECURED LAMP HOLDER ASSEMBLY IN NR 1 FORWARD EMERGENCY LIGHT ASSEMBLY. OPERATIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: POWER SUPPLY — INOPERATIVE (COCKPIT)
SEA - EXIT SIGN OVER COCKPIT DOOR WAS DIM THEN WENT OUT. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, TESTED NORMAL.
Part: SIGN — INOPERATIVE (ROW 8-9)
BOI- OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 8 TO 9 INOP. REPLACED LIGHT PANEL, OPERATIONAL CHECK GOOD.
1998
Part: CIRCUIT BOARD — FAILED (COCKPIT)
PDX- EXIT SIGN AT ENTRANCE TO COCKPIT WILL NOT LIGHT. REPLACED COCKPIT ENTRANCE EMERGENCY EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN)
LIGHTS DIM IN EXIT LIGHT ON CEILING NEXT TO CLOSET. MAINTENANCE REPLACED THE FORWARD CABIN EXIT CIRCUIT BOARD, OPERATIONAL TESTED NORMAL.
Part: BULB — FAILED (CABIN)
PDX - EXIT SIGN OVER COCKPIT DOOR HAS SOME BULBS OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LAMP ASSEMBLY, OPERATIONAL TESTS NORMAL.
Part: BULB — FAILED (CABIN)
AFT SIDE OF CENTER EXIT LIGHT HAS A LAMP OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL.
Part: BULB — FAILED (CABIN)
GEG - OVERHEAD EXIT LIGHT ABOVE COCKPIT DOOR HAS LAMPS OUT. MAINTENANCE RELAMPED. OPERATIONAL TESTS ARE NORMAL.
Part: BULB — FAILED (CABIN)
LIGHT IN OVERWING EXIT SIGN AT ROW 9E IS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL CHECK GOOD.
Part: SIGN — INOPERATIVE (CABIN)
FORWARD FACING EMERGENCY EXIT SIGN IS OUT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY, OPERATONAL TEST NORMAL.
Part: BULB — FAILED (CABIN)
SEA - EXIT LIGHT AT SEAT 9A IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.
Part: BULB — FAILED (CABIN)
ROW 8 FORWARD 28V EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TEST RESULTS NORMAL.
Part: BULB — FAILED (CABIN)
CEILING EMERGENCY EXIT SIGN LIGHTS DIM NEXT TO COAT CLOSET. MAINTENANCE RELAMPED AND OPERATIONALY TESTED, TESTS NORMAL.
Part: CIRCUIT BOARD — FAILED (CABIN)
SEA - LIGHTS OUT IN EXIT SIGN. MAINTENANCE REPLACED EXIT SIGN CIRCUIT BOARD, OPERATIONAL TESTS ARE NORMAL.
Part: COALESCER DUCT — FAILED (FWD PACK)
SEA - BURNING SMELL AND LOUD SQUEAL COMING FROM COCKPIT PACK. STOPPED WHEN COCKPIT PACK WAS TURNED OFF. MAINTENANCE INSPECTED AND PLACED ON MEL. LATER THAT DAY AT GEG MAINTENANCE FOUND THE INLET DUCT TO WATER SEPARATOR COLLAPSED. THE WATER SOCK WAS INSPECTED AND LOOKED GOOD, MAINTENANCE THEN INSTALLED WATER SEPARATOR AND DUCT, PERFORMED A GROUND RUN, OPERATIONAL CHECKS WERE NORMAL. CLEARED THE MEL. AIRCRAFT WAS RETURNED TO SERVICE.
Part: DRAIN — PLUGGED (COALESCER BAG)
GEG - AIRCRAFT RETURNED TO FIELD DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND THE WATER SOCK DRAIN PLUGGED FOR THE CABIN PACK. THE DRAIN WAS UNPLUGGED AND THE WATER SOCK WAS CLEANED, IT WAS FULL OF WATER MIXED WITH OIL. SYSTEM WAS OPERATIONALLY TESTED AND A TEST FLIGHT ACCOMPLISHED, TESTS NORMAL. THE APU WAS SUSPECTED OF PUTTING THE OIL IN THE BLEED AIR SYSTEM AND IS CURRENTLY ON MEL.
Part: PACK — SMOKING (CABIN)
FLIGHT ATTENDANT REPORTED SMOKE AND HAZY CONDITIONS IN CABIN AND LAV SMOKE DETECTOR ACTIVATED. TURNED BOTH PACKS OFF AND RETURNED TO GEG. MAINTENANCE ISOLATED PROBLEM TO CABIN PACK. DEFERRED PER MEL 21-1. AIRCRAFT RELEASED FOR TEST FLIGHT, TEST FLIGHT SATISFACTORY. ON 980416 CLEARED MEL BY REMOVING AND REPLACING THE CABIN REFRIGERATION UNIT. GROUND RAN AIRCRAFT AT HIGH POWER, CABIN PACK FULL HOT THEN FULL COLD, 10 MINUTS ON EACH SETTING. NO SMOKE NOTED.
Part: PACK — SMOKE (CABIN)
GEG - FLIGHT ATTENDANT REPORTED SMOKE AND HAZY CONDITIONS IN CABIN AND LAV SMOKE DETECTOR ACTIVATED. TURNED BOTH PACKS OFF AND RETURNED TO GEG. MAINTANENCE ISOLATED PROBLEM TO CABIN PACK. DEFERRED PER MEL 21-1. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLIGHT SATISFACTORY.
Part: BULB — FAILED (CABIN)
AFT LEFT AND RIGHT EXIT EVACUATION LIGHTS INOP. MAINTENANCE TIGHTENED LT AND RT EVACUATION LIGHT SOCKETS, CLEANED GROUND CONNECTIONS, AND REMOVED AND REPLACED LAMPS. EVACUATION LIGHTS CHECKED GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY LIGHTS AT ROW 8 ARE INOP. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY LIGHTS OVER THE COCKPIT DOOR ARE BURNT OUT. REPLACED LAMPS, OPERATIONAL CHECKS GOOD.
Part: HOOK LATCHES — LACK OF LUBE (PAX DOOR)
PDX - MAIN CABIN DOOR IS HARD TO OPEN AND LOCK. CLEANED THE CABIN DOOR HOOK LATCHES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: CIRCUIT BOARD — MALFUNCTION (CABIN)
FORWARD OVERWING EXIT SIGN LIGHTS INOP. MAINTENANCE REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD.
Part: STRINGER — CHAFED (FUSELAGE)
FRAME 18075 AT STRINGER 58 IS CHAFED MORE THAN 50 PERCENT. BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 4-53-339.
Part: SKIN — DENTED (BS 11000)
DENT 3.2 X .75 WITH A SHARP CREASE IN THE BOTTOM AT STATION 11000 AND BETWEEN BL 1147L AND BK1002L DENT IS .103 DEEP. REPAIRED DENT IAW FOKKER SRM 53-02-12 FIGURE 1, PAGE 3 AND SRM 51-31-01.
Part: FAIRING — DENTED (FUSELAGE)
DENT 2.5 BY 2.0 AND .092 DEEP ADJACENT TO FRAME 10775 AND RIB BL13456 ON LOWER FAIRING DENT HAS CREASE IN THE BOTTOM. FABRICATED AND INSTALLED REPAIR IAW FOKKER SRM 53-02-17 FIGURE 1, PAGE 3.
Part: FASTENER — MISINSTALLED (FUSELAGE)
CASTELLATION AT STRINGER 47 FRAME 15205 HAS TWO HI-LOKS INSTALLED WHERE ACCESS IS ACCESSABLE. HI- LOKS CORRECTLY INSTALLED IAW FOKKER SRM 51-30-02 AND MM 53-10-05, PAGE 601.
1997
Part: SKIN — CHAFED (RT SPEED BRAKE)
RIGHT HAND SPEED BRAKE INNER SKIN HAS DEEP CHAFE 24 INCHES FROM THE TRAILING EDGE AND 1.25 INCH DOWN FROM THE TOP EDGE. REPAIR DOESN'T MATCH UPPER ROW, RIVETS NOT FLUSH. GAP BETWEEN REPAIR AND SPEED BRAKE SKIN APPROX .015. REPAIRED IAW EA 4-53-323.
Part: FRAME — CRACKED (FUSELAGE)
CRACKED CASTELLATION ON FRAME 50-2 AT STRINGER 27. INSTALLED HI-LOKS THROUGH FRAME IAW FOKKER SRM 51-30-03. ALODINED AND PRIMED IAW FOKKER SRM 51-16-4, PAGE 9.
Part: FRAME — CRACKED (FUSELAGE)
CRACKED FRAME CASTELLATION ON THE BACKSIDE OF FRAME 50-2 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND MM 53-10-05.
Part: FRAME — CRACKED (FUSELAGE)
CRACKED CASTELLATION ON FRAME 16-2 JUST OUTBOARD OF THE LEFT HAND CUTOUT FOR THE VERTICAL STAB SPAR. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND MM 53-10-5, SUPP, PAGE 601.
Part: FRAME — MISREPAIRED (FUSELAGE)
CASTELLATION END RIVET HOLE ON FRAME 17565 AND STRINGER 59 IS DISTORTED FROM PREVIOUS REPAIR ATTEMPT. INSTALLED CLIP REPAIR IAW FOKKER SRM 53-02-13 AND MM 53-10-05, PAGE 601.
Part: ANGLE — CORRODED (CARGO COMPT)
AFT CARGO BAY FLOOR SUPPORT ANGLE ON FRAME 16060 CORRODED BETWEEN STRINGERS 74, 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.
Part: CLIP — CRACKED (CARGO COMPT)
AT CARGO BAY CRACKED FRAME CLIP ON FRAME 13815B BY STRINGER 2. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME CLIP — CRACKED (FUSELAGE)
CRACKED FRAME CLIP ON FRAME 13815B BY STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: ANGLE — BENT (CARGO COMPT)
AFT CARGO BAY FLOOR SUPPORT ANGLE ON FRAME 15205 BENT/TORN BETWEEN STRINGER 1 TO 3 AND 71 TO 74. REPAIRED IAW FOKKER SRM 53-02-17, FIGURE 2 AND 51-31-01.
Part: RIVET — MISINSTALLED (FUSELAGE)
CABIN FUSELAGE CLIP REPAIR AT FRAME 15205 STRINGER 47 HAS IMPROPERLY INSTALLED RIVETS AT FRAME ATTACH POINT. INSTALLED TWO HI-LOKS AFTER REMOVED DAMAGED RIVETS IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 51-30-02.
Part: FLOOR PANEL — BENT (CARGO COMPT)
AFT CARGO BAY PANEL BETWEEN FLOORBEAMS FRAMES 1666 AND 16060, IS BENT. DIRECTLY ABOVE AFT CARGO DOOR BOTTOM DOOR SILL. REPAIRED PANEL IAW HORIZON EA 4-53-335 AND REINSTALLED TO FLOORBEAM PER FOKKER SRM 51-31-01.
Part: SKIN — MISDRILLED (SPEED BRAKE)
ROW OF 12 NR 5 CHERRY MAX RIVETS WHICH ARE LOOSE AND HAVE INSUFFICIENT EDGE DISTANCE ON THE INNER SKIN OF THE RIGHT HAND SPEED BRAKE 35 FROM THE TRAILING EDGE NEAR THE TOP. REPAIRED SPEED BRAKE SKIN AS PER HORIZON EA 4-53-325.
Part: SKIN — CHAFED (SPEED BRAKE)
RIGHT HAND SPEED BRAKE INNER SKIN HAS A DEEP CHAFE 24 DOWN FROM THE TRAILING EDGE AND 1.25 DOWN FROM THE TOP EDGE. REPAIRED IAW EA 4-53-323.
Part: BULKHEAD BEAM — CRACKED (AFT PRESS BLKHD)
FORWARD PRESSURE BULKHEAD BEAM NR 5 UPPER FLANGE IS CRACKED AT A PREVIOUS REPAIR AT THE CENTER OF THE BEAM. REPAIRED IAW FOKKER SRM 51-10-4, 51-31-01 AND 51-30-02.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: STRINGER — CRACKED (LT WING)
LEFT HAND WING 2 STRINGER FLANGE THAT HOLDS BELLY SKIN TO FUSELAGE SEVERAL RIVETS WITH CRACKS COMING FROM AROUND THEM. INSTALLED REPAIR ANGLES AS REQUIRED PER FOKKER SRM 53-02-17 PAGE 11 FIGURE 6.
Part: ANGLE — CRACKED (RT WING)
RIGHT HAND WING 2 STRINGER AT 2.19, 2.18, 2.17 HAVE SMALL 2 ANGLE THAT ARE CRACKED. INSTALLED NEW 2 STRINGER CONNECTION ANGLE PER FOKKER SRM 51-31-01.
Part: NUT PLATE STRIP — CRACKED (WING FAIRING)
RIGHT HAND WING NUT PLATE STRIP FOR FUSELAGE TO WING FAIRING CRACKED JUST IN FRONT OF FORWARD LANDING GEAR LUG FITTING PANEL 92L. INSTALLED PREVIOUSLY FABRICATED DOUBLER IAW FOKKER SRM 51-31-01 AND VERTICAL FASTENER AS PER MM 20-30-5.
Part: PANEL — CRACKED (FUSELAGE)
LEFT HAND SIDE BELLY PANEL 91BC SECONDARY RIB CRACKED AT CENTER SECTION. INSTALLED REPAIR DOUBLER IAW FOKKER SRM 51-31-01.
Part: SKIN — DENTED (PAX DOOR)
THREE DENTS ON MAIN CABIN DOOR SKIN. TWO LOCATED BY EXTERNAL ASSIST HANDLE AND ONE LOCATED ON FORWARD EDGE APPROXIMATELY MID SPAN LOCATION. REPAIRED IAW FOKKER SRM 52-01-01 AND SRM 51-31-01.
Part: ANGLE — CRACKED (FUSELAGE)
LEFT HAND SIDE BELLY FAIRING CONNECT ANGLE UNDER PANEL 986 NEAR CENTER SECTION CRACKED. FABRICATED NEW BRACKET IAW FOKKER SRM 51-11-4 AND INSTALLED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7 A, B AND D1.
Part: PANEL — CRACKED (FUSELAGE)
RIGHT HAND SIDE BELLY PANEL 91BC CENTER SECTION SECONDARY RIB CRACK. REPAIRED IAW FOKKER SRM 53-02-05 FIGURE 1, SECTION D-D.
Part: SUPPORT — DAMAGED (CABIN)
FORWARD GALLEY UNDERFLOOR SUPPORT AT BL 1000 ALONG FRAME 3820 AND 510 MM AFT OF FRAME 3450, (LOCATION MARKED). REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 A, B, C.
Part: FAIRING — DENTED (FUSELAGE)
DENT 2.5 X 2.0 AND .092 DEEP ADJACENT TO FRAME 10775 AND RIB BL13452 ON LOWER FAIRING DENT HAS CREASE IN THE BOTTOM. CUT OUT DENTED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER FOKKER SRM 53-02-17, FIGURE 1.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 48. REPAIRED IAW FOKKER 53-02-13, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 10346 CASTELLATION IS CRACKED AT STRINGER 44. REPAIRED CRACK IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: STRINGER — CORRODED (FUSELAGE)
STRINGER 65 IS CORRODED BETWEEN FRAMES 4150 AND 4610. REPAIRED IAW FOKKER SRM 53-02-05 AND SRM 51-30-02.
Part: FRAME — CHAFED (CABIN)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 45. INSTALLED REPLACEMENT CLIP PER FOKKER SRM 53-02-13 FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 33. COMPLIED WITH INSTALLATION OF CLIP PER FOKKER SRM 51-31-01.
Part: SKIN — CHAFED (EMER EXIT DRWAY)
LEFT HAND OVERWING EMERGENCY EXIT APATURE TOP FRAME BOX HAS TWO CHAFED RIVETS. EMERGENCY DOOR HAS BEEN HITTING THESE. REMOVED DAMAGED AREA AND REPAIRED IAW HORIZON EA 4-53-324. INSTALLED NEW RIVET IAW FOKKER SRM 51-31-05.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 14285 CASTELLATION IS CRACKED AT STRINGER 36. COMPLETED INSTALLATION OF CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13345 CASTELLATION IS CRACKED AT STRINGER 33. INSTALLED REPAIR CLIP PER FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815 CASTELLATION IS CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 33. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305A BETWEEN STRINGERS 36 AND 37 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 8805 BETWEEN STRINGER 27 AND 28 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 93050 BETWEEN STRINGER 35 AND 36 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305A BETWEEN STRINGER 27 AND 28 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CHAFED (EMEREXIT DRWAY)
RIGHT HAND AFT OVERWING EMERGENCY EXIT APATURE TOP FRAME BOX SKIN HAS A CHAFE IN SKIN AND A CHAFED RIVET. EMERGENCY DOOR HAS BEEN HITTING THESE. REPAIRED IAW HORIZON EA 4-53-324 STEPS 1-4.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305A BETWEEN STRINGER 29 AND 30 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305A BETWEEN STRINGER 25 AND 26 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 5305A BETWEEN STRINGER 46 AND 47 IS CRACKED. REPAIRED IAW FOKKER SRM 43-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815 CASTELLATION IS CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 31. INSTALLED DOUBLER PER FOKKER SRM 53-02-13M FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 15205 CASTELLATIONS CRACKED AT STRINGER 49. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 6805 BETWEEN STRINGERS 18 AND 19 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CHAFED (CABIN)
INBOARD FACE OF CABIN FRAME 11905 HAS TWO CHAFED AREA'S AT APPROXIMATELY STRINGER 54. REPAIRED IAW HORIZON EO 4-53-03 FOR REPLACEMENT OF AFFECTED PORTION OF FRAME 11905.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815 CASTELLATION IS CRACKED AT STRINGER 42. FABRICATED REPAIR CLIP, ETCHED, ALODINED, INSTALLED PER FOKKER SRM 53-02-13 FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 46. RE-CHECKED FRAME 13815A CASTELLATION AT STRINGER 46, NO CRACK FOUND AT LOCATION NOTED.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305A BETWEEN STRINGER 28 AND 29 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 8805 BETWEEN STRINGERS 28 AND 29. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: SKIN — CHAFED (EMER EXIT DRWAY)
LEFT HAND AFT OVERWING EMERGENCY EXIT APATURE TOP FRAME BOX SKIN HAS A CHAFE IN SKIN AND A CHAFED RIVET. EMERGENCY DOOR HAS BEEN HITTING THERE. REPAIRED CHAFE IAW HORIZON EA 4-53-324, FIGURE 1 AND 2.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 46. INSTALLED REPLACEMENT CLIP PER FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 34. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 46. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 33. COMPLETED INSTALLATION OF CLIP AS PER FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 8805 BETWEEN STRINGER 44 AND 45 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 30. REPAIRED FRAME CASTELLATION CLIP PER FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION CRACKED AT STRINGER 32. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CABIN FUSELAGE FRAME 13815 CASTELLATION IS CRACKED AT STRINGER 35. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 33. INSTALLED REPAIR DOUBLER PER FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 29. INSTALLED REPAIR CLIP PER FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 29. INSTALLED REPAIR CLIP PER FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 46. INSTALLED REPLACEMENT CLIP PER FOKKER SRM 53-02-13 FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE)
FRAME 9305 CASTELLATION BETWEEN STRINGER 48 AND 49 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 8305 BETWEEN STRINGER 36 AND 37 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 44. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 45. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (FUSELAGE)
CASTELLATION ON FRAME 9305 BETWEEN STRINGER 75 AND 76 IS CRACKED. REPAIRED IAW FOKKR SRM 53-02-13 PAGE 4 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 41. REPAIRED FRAME CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12875 CASTELLATION IS CRACKED AT STRINGER 29. REPAIRED CLIP IAW FOKKER SRM 53-02-13 FIGURE 2.
Part: FRAME — CRACKED (CABIN)
CABIN FUSELAGE FRAME 12405 CASTELLATION IS CRACKED AT STRINGER 29. INSTALLED REPAIR DOUBLER PER FOKKER SRM 53-02-13 FIGURE 2.
Part: WEB — CRACKED (LT MLG WW)
A .25 INCH CRACK FROM RIVET HEAD. LOCATED APPROXIMATELY 3 FORWARD OF BULKHEAD FRAME 13345 AND IN LEFT WHEEL BAY AFT, TOP OUTBOARD CORNER. INSTALLED NEW DOUBLER IAW HORIZON EA 4-53-318.
Part: DRAIN — BLOCKED (LT WATER BAY)
DRAIN PATH BLOCKED. LOCATED ON FORWARD SIDE OF BULKHEAD FRAME 13345 AND NEAR THE UPPER OUTBOARD SIDE OF LEFT WHEEL BAY. CLEANED AND UNBLOCKED DRAIN ON UPPER OUTBOARD SIDE OF LEFT WATER BAY.
Part: BULKHEAD FRAME — CRACKED (RT MLG WW)
THREE CRACKS EXTENDING FROM RIVET HEADS. LOCATED IN RIGHT WHEEL BAY APPROXIMATELY 3 FORWARD OF BULKHEAD FRAME 13345 AND IN THE TOP, AFT, OUTBOARD CORNER. INSTALLED NEW DOUBLER IAW EA 4-53-317.
1996
Part: POWER SUPPLY — FAILED (CABIN)
MAINTENANCE CHECK REVEALED AFT CABIN EMERGENCY LIGHTING INOP. MAINTENANCE REPLACED AFT RIGHT EMERGENCY LIGHTING POWER SUPPLY. (M)
Part: POWER SUPPLY — FAILED (CABIN)
ROA - AFT CABIN EMERGENCY LIGHTING INOPERATIVE. REPLACED AFT RIGHT EMERGENCY LIGHTING POWER SUPPLY. (M)
Part: LAMP — BLOWN (CABIN)
FOUND FLOOR LEVEL EMERGENCY LIGHTING FIXTURE 8C BROKEN. MAINTENANCE RELAMPED LIGHTING FIXTURE. (M)
Part: PANEL — INOPERATIVE (CABIN)
PIT - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD, MID AND AFT EMERGENCY PANELS. (X)
Part: SKIN — CRACKED (BS 600-623)
PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN, LEFT SIDE 23 INCHES LONG AT STATION 600-623 AT STRINGER 17. INSTALLED DOUBLER PER EO 5393L023 AND EA 33032. (M)
Part: SKIN — CRACKED (BS 600-619)
PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN RIGHT SIDE 19 INCHES LONG AT STATION 600-619 STRINGER 58. INSTALLED DOUBLER PER EO 5393L023 AND EA 33032. (M)
Part: FRAME — CRACKED (FUSELAGE)
PIT - DURING SIP INSPECTION, FOUND .25 INCH CRACK IN THE LOWER AFT APERTURE FRAME CORNER SIP REF 53-10-20 EDDY CURRENT. REMOVED DAMAGED AREA AND INSTALLED FILLER PLUG AND 2 DOUBLERS PER SRM 53-02-16. (M)
Part: FRAME — CRACKED (FUSELAGE)
PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, .25 INCH FWD AND .25 INCH AFT SED UPPER APERTURE FRAME CORNERS, SIP REF 53-10-20 EDDY CURRENT. REMOVED DAMAGED AREAS AND INSTALLED DOUBLER REPAIR AND FILLER PLUGS PER USAIR TYPICAL REPAIR 53-10-04. (M)
Part: BLKHD ANGLE — CRACKED (FWD PRESS BLKHD)
PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, 3 INCHES AND 1.5 INCHES A REPAIR DOUBLER AT THE FORWARD PRESSURE BULKHEAD FS 1550 AFT SIDE OF LOWER CONNECTION ANGLE SIP REF 53-10-06 VISUAL/EDDY CURRENT. REMOVED DOUBLERS, STOP DRILLED CRACKS AND INSTALLED NEW DOUBLERS PER SRM 53-02-18. (M)
1995
Part: EEL BATT CHARGER — FAILED (CABIN)
CLT - FLT NR 947 - EMERGENCY EXIT LIGHTS FORWARD CABIN STAY ON WITH SWITCH IN ARMED OR OFF POSITION. REPLACED BATTERY CHARGER. EMERGENCY LIGHTS CHECK OK. (M)
Part: ACTUATOR — OUT OF ADJUST (RT MLG DOOR)
SDF - FLT NR 846 - AFTER TAKEOFF, RIGHT MAIN RED GEAR LIGHT REMAINED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE 1-312-5 OF PHB AND RECYCLED GEAR. AFTER RECYCLE ALL RED AND AMBER LIGHTS STAYED ON ALONG WITH GREEN LIGHTS. THEN FOLLOWED ABNORMAL PROCEDURE 1-312-4 AF PHB AND CYCLED GEAR DOWN AND UP. RED RIGHT GEAR STAYED ON. FOLLOWED PROCEDURE 1-312-5 AGAIN, NO HELP. RETURNED TO SDF, LANDING NORM. FOUND RIGHT MLG DOOR NOT CLOSING PROPERLY. ADJUSTED DOOR ACTUATOR. AFT AND LANDING GEAR OPERATED NORMAL. ALL INDICATIONS NORMAL PER M/M. AIRCRAFT OK FOR SERVICE. (M)
Part: CONNECTOR — BENT PIN (LT MLG WW)
CLT - FLT NR 0578 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. USED OVERIDE BUTTON TO RETRACT LANDING GEAR. FOUND PIN IN CONNECTOR CM62 BENT. STRAIGHTENED PIN AND RECONNECTED CONNECTOR, SYSTEM TEST NORMAL PER CHAP 32 AND CHAP 27 IN MM. (M)
Part: WINDOW POST — CRACKED (RT NR 2 WINDOW)
PIT - DURING AN FC-6 CHECK INSPECTION, FOUND .75 INCH CRACK IN RIGHT NR 2 WINDOW POST (TYPE 3) REF SIP 53-10-08. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-10-01 REV A. (M)
Part: DOOR FRAME — DENTED (CARGO COMPT)
PIT - DURING AN FC-6 CHECK INSPECTION, FOUND 2 DENTS IN THE FORWARD SIDE OF THE AFT CARGO COMPARTMENT DOOR FRAME IN AREA OF HOLD OPEN ROD SUPPORT. INSTALLED DOUBLER REPAIR PER SRM 53-02-16 PG 4. (M)