N560SW
Registered owner: JAHN 560SW LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Ameriflight, LLC (JIKA) | Certificate holder | — | Matched by certificate designator |
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.
73 reports on file, 1999-02-09 – 2014-07-21.
Part: LIGHT — BROKEN (CABIN) · airframe 33,438 hrs · 46,989 cycles
FLOOR EMERGENCY LIGHT NEAR FWD GALLEY BROKEN. R & R FORWARD MOST FLOOR EMERGENCY LIGHT IAW AMM.
Part: LAMP — INOPERATIVE (CABIN LIGHT) · airframe 33,410 hrs · 46,954 cycles
FWD GALLEY AREA LIGHT IS INOPERATIVE. C-CHECK, R & R LAMP IN FWD GALLEY LIGHT IAW AMM.
Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 33,184 hrs · 46,652 cycles
FLOOR LEVEL EMERGENCY EXIT SIGN NEAR THE PAX DOOR IS DAMAGED. R & R FLOOR LEVEL EMERGENCY EXIT LIGHT FIXTURE NEAR THE PAX DOOR IAW AMM.
Earlier reports · 1999–2013 · 70 reports
2013
Part: CONNECTOR — LOOSE (RT MLG) · airframe 32,639 hrs · 45,979 cycles
RT MAIN GEAR WOULD NOT RETRACT. FLT 7390 TIGHTENED RT MLG DOWN LOCK UPPER PROX SENSOR CANNON PLUG & ADJUSTED UPLOCK PROX SENSOR. SWUNG GEAR MULTIPLE TIMES WITH NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (LT WING) · airframe 31,477 hrs · 44,413 cycles
LEFT OTBD WING STRINGER 10 IS CRACKED AT RIB 15. (C-CHECK) CUT OUT THE DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER ON LT OTBD WING STRINGER 10 AT RIB 15 IAW SRM AND AMM.
2012
Part: FIXTURE — DEFECTIVE (CABIN) · airframe 30,445 hrs · 43,125 cycles
ELECTRICAL SMELL COMING FROM AFT CABIN. SMELL SLOWLY DISSIPATED ONCE CABIN LIGHTS WERE TURNED OFF. (FLT 7799) REPLACED SIDEWALL LIGHT FIXTURE AT SEAT 7D IN REFERENCE TO EMB 120 AMM. P/N: BC1-0047-005 S/N OFF: N/A.
Part: ALTIMETER — FAILED (COCKPIT) · airframe 29,359 hrs · 41,867 cycles
ON TAKEOFF CAPTAINS ALTIMETER WAS STUCK TILL 4500 FT THEN WOULD MOVE IN SEGMENTS OF 50 TO 100 FEET EVERY SECOND. (FLT 7760) REPLACED CAPTAIN'S ALTIMETER IN REFERENCE TO AMM. P/N: 1190AMI S/N OFF: AG299
Part: BUSHING — FROZEN (CABIN DOOR) · airframe 29,230 hrs · 41,719 cycles
MAIN CABIN DOOR IS HARD TO OPEN OR CLOSE. (FLT 7763) FOUND INTERCONNECT TORQUE TUBE BUSHING FROZE. REPLACED FORWARD AND AFT BEARING ASSEMBLIES.
2011
Part: WIRE — BROKEN (CABIN) · airframe 28,597 hrs · 40,952 cycles
TWO FORWARD FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 5314) REPAIRED BROKEN WIRE ON 2 FORWARD EMERGENCY LIGHTS.
Part: WIRE — DAMAGED (CABIN) · airframe 28,441 hrs · 40,746 cycles
FORWARD FLOOR LEVEL EMERGENCY LIGHT IS OUT. (FLT 7784) REPAIRED WIRE AT FORWARD FLOOR LEVEL EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,441 hrs · 40,746 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5309) RELAMPED EMERGENCY LIGHT.
Part: SPLICE — BROKEN (CABIN) · airframe 28,336 hrs · 40,616 cycles
FORWARD EMERGENCY FLOOR LIGHT BY MAIN CABIN DOOR IS OUT. (FLT 5405) REPLACED BROKEN SPLICES AT FORWARD FLOOR EMERGENCY LIGHT.
Part: WIRE — DAMAGED (CABIN) · airframe 28,248 hrs · 40,520 cycles
TWO FORWARD RED EMERGENCY LIGHTS AT MAIN CABIN DOOR ARE OUT. (FLT 7766) REPAIRED WIRE AT FLOOR LEVEL EMERGENCY LIGHTS.
Part: WIRE — BROKEN (CABIN) · airframe 27,800 hrs · 39,950 cycles
EMERGENCY FLOOR LIGHT OUT NEAR MAIN CABIN DOOR. (FLT 6909) REPAIRED BROKEN WIRE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,732 hrs · 39,867 cycles
OVERHEAD CABIN EMERGENCY LIGHT, AT ROW 7 IS OUT. (FLT 1300) RELAMPED EMERGENCY LIGHT.
Part: FRAME — CRACKED (LT NACELLE) · airframe 27,800 hrs · 39,950 cycles
LEFT OUTBOARD NACELLE FRAME CRACKED ABOVE AFT GEAR DOOR. (C-CHECK) REPAIRED LEFT NACELLE OUTBOARD AFT NACELLE FRAME SUPPORT BRACKET PER SRM.
Part: STRINGER — CRACKED (LT WING) · airframe 27,800 hrs · 39,950 cycles
LEFT WING LOWER STRINGER FORWARD SIDE OF DRYBAY IS CRACKED. (C-CHECK) REPAIRED INBOARD SECTION OF LEFT NR 10 WING STRINGER BETWEEN RIBS 5 & 6 PER SRM.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,696 hrs · 38,556 cycles
FORWARD EMERGENCY LIGHT OUT. (FLT 6869) RELAMPED EMERGENCY LIGHT.
Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 26,119 hrs · 37,832 cycles
EMERGENCY LIGHT ABOVE ROW 9 INOP. (FLT 6315) RESEATED WIRES.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,239 hrs · 36,710 cycles
FORWARD OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.
2009
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,698 hrs · 36,078 cycles
FLOOR SEAT TRACKS CORRODED. (C CHECK) REPLACED TRACKS PER AMM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,698 hrs · 36,078 cycles
FLOORBEAM AT FRAME 16L CORRODED. (C CHECK) REPLACED FLOORBEAM SUPPORT BRACKET PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,698 hrs · 36,078 cycles
STRINGERS 18L AND 19L CORRODED. (C CHECK) REPLACED STRINGERS PER SRM.
Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 24,698 hrs · 36,078 cycles
FUSELAGE CABIN GALLEY TRACK CORRODED. (C CHECK) REPLACED TRACK PER SRM.
Part: LANDING GEAR — OUT OF RIG (RIGHT MAIN) · airframe 24,268 hrs · 35,511 cycles
FLT 7769 - RIGHT MAIN GEAR DID NOT RETRACT. RIGGED GEAR RETRACT SYSTEM.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,920 hrs · 35,093 cycles
FLT 5871 - EMERGENCY LIGHTS IN AFT THIRD OF CABIN INOP. REPLACED AFT EMERGENCY LIGHT BATTERY PACK.
2008
Part: WIRE — BURNED (C/B PANEL) · airframe 23,250 hrs · 34,243 cycles
SVC CHECK, FOUND WIRE W138-0001-2 BURNED ABOVE OVERHEAD CB PANEL. REPLACED FULL LENGTH OF WIRE W138-0001-2.
Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 23,120 hrs · 34,045 cycles
FLT 7811 - EMERGENCY LIGHTS CAME ON JUST BEFORE THE LANDING CHECK AND STAYED ON UNTIL TURNING OFF RUNWAY. REPLACED RELAY K0201.
Part: ACTUATOR — FAILED (MLG) · airframe 22,898 hrs · 33,791 cycles
ON CLIMB-OUT, LEFT MAIN GEAR WOULD NOT RETRACT. REPLACED LEFT GEAR ACTUATOR, PN 19595-000-07.
Part: ALTIMETER — INACCURATE (COCKPIT) · airframe 21,806 hrs · 32,343 cycles
FLT 5574 - CAPTAINS ALTIMETER INDICATES BELOW FIELD ELEVATION. REPLACED ALTIMETER. OPS CHECK GOOD, PN 28704-E2101, SN/OFF 1248.
2007
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,281 hrs · 31,647 cycles
FLT 3785 - CAPTAINS WINDSHIELD IS CRACKED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-01, P/N: NP-151311-1, S/N OFF: 06138H8653.
Part: WINDOW — CRACKED (COCKPIT) · airframe 21,281 hrs · 31,647 cycles
FLT 3735 - CAPTAINS DV SIDE WINDOW IS CRACKED. REPLACED CAPTAINS DV WINDOW IAW EMB MM 56-11-01. LEAK CHECK GOOD.
Part: DOOR — LOOSE (EMERGENCY EXIT) · airframe 20,965 hrs · 31,265 cycles
FLT 3704 - AIRCRAFT WOULD NOT PRESSURIZE ON DEPARTURE. INSPECTED AND RE-INSTALLED LEFT OVERWING EXIT DOOR. NO ABNORMAL DISCREPANCIES NOTED.
Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 20,833 hrs · 31,084 cycles
FLT 5504 - FORWARD FLOOR LEVEL EMERGENCY EXIT SIGN IS BROKEN. INSTALLED SERVICEABLE EMERGENCY EXIT LENS.
Part: ELEMENT — INOPERATIVE (WINDSHIELD HEAT) · airframe 20,706 hrs · 30,908 cycles
FLT 3733 - CAPTAIN'S WINDSHIELD HEATING ELEMENT IS INOP. REPLACED WINDSHIELD ASSEMBLY IAW MM 56-10-01.
2006
Part: A/C PACK — FAILED (RIGHT) · airframe 18,257 hrs · 27,575 cycles
RIGHT PACK FAIL DURING TAXI IN AND FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. PERFORMED OPERATIONAL CHECKS OF RIGHT PACK OFF APU BLEED AND ENGINE BLEED. OPERATIONAL CHECKS GOOD. UNABLE TO DUPLICATE SQUAWK.
Part: LIGHT — BROKEN (FA JUMPSEAT) · airframe 17,590 hrs · 26,661 cycles
FOUND LOWER EXIT LIGHT LOCATED INSIDE AND FWD BY FA JUMPSEAT IS BROKEN. REPLACED LOWER FWD EXIT LIGHT ASSY BY FA JUMPSEAT IAW 33-51-02. OPERATIONAL CHECK GOOD.
2005
Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 16,963 hrs · 25,761 cycles
A/P FAILED INFLIGHT WHILE SELECTED TO EITHER SIDE. REPLACED A/P ELEVATOR SERVO, OPERATIONAL CHECK GOOD IAW MM 22-10-00.
Part: LINKAGE — OBSTRUCTED (LT AILERONS) · airframe 16,902 hrs · 25,683 cycles
WHEN CHECKING FLIGHT CONTROLS, YOKE HANGS UP HALF WAY TO THE RIGHT. REPLACED LT AILERON RIVET TO QUADRANT LINKAGE IAW MM 31-30-11. OPERATIONAL CHECK GOOD.
Part: ACTUATOR — INOPERATIVE (RT RUDDER) · airframe 15,742 hrs · 23,865 cycles
UNABLE TO PRESS RIGHT RUDDER FAST 2" OF CENTER. REPLACED BLUE RUDDER ACTUATOR IAW 27-22-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 15,306 hrs · 23,186 cycles
EMERGENCY LIGHTS INOPERATIVE. INSTALLED SERVICEABLE BATTERIES FOR EMERGENCY LIGHTS. OPERATIONALCHECK GOOD. P/N D366-04-001; S/N OFF 1120, P/N D366-04-001; S/N OFF 1238, P/N D366-04-001; S/N OFF 312.
Part: ACTUATOR — LEAKING (TE FLAP) · airframe 15,199 hrs · 23,039 cycles
ON LANDING BLUE SIDE HYDRAULICS FAILED WITH FLAPS 15 DEGREES. REPLACED LEFT INBOARD FLAP ACTUATOR IAW AMM 27-50-00. OPERATIONAL CHECK GOOD.
Part: WIRE — DAMAGED (EMEGENCY LIGHT) · airframe 14,966 hrs · 22,691 cycles
FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE (FIRST 4 LIGHTS). REPAIRED MAIN POWER WIRE. REPLACED FUSE. OPERATIONAL CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,966 hrs · 22,691 cycles
EMERGENCY FLOOR LIGHT INOPERATIVE (1ST BULB). RELAMPED FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,898 hrs · 22,591 cycles
FLOOR EMERGENCY LIGHT OUT. RELAMPED WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,875 hrs · 22,545 cycles
FLOOR LEVEL EMERGENCY LIGHT (1ST LIGHT BULB) INOPERATIVE. RESECURED LOOSE CONNECTION ON FORWARD WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
2004
Part: SMOKE — DETECTED (A/C PACK) · airframe 14,721 hrs · 22,291 cycles
ON GROUND WITH APU, RIGHT PACK PRODUCES ON HIGH OR NORM, BURNING SMELL AND FAINT SMOKE IN COCKPIT. OPERATED RIGHT PACK IN HIGH AND NORMAL FOR 1/2 HOURS, INSPECTED GROUND COOLING FAN AND TURBINE FOUND NO DEFECTS, OPERATIONAL CHECK GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,291 hrs · 21,611 cycles
EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AT AFT EMERGENCY EXIT. OPERATIONAL CHECK GOOD.
Part: SPRING — WORN (ELEVATOR) · airframe 14,045 hrs · 21,239 cycles
ON PREFLIGHT, NOTICED UNUSUALLY LIGHT ELEVATOR BACK PRESSURE. REPLACED ELEVATOR RETURN SPRING ON CAPTAIN'S SIDE. OPERATIONAL CHECK GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,792 hrs · 20,838 cycles
SOME LIGHTS INOP ON FLOOR LEVEL EMERGENCY LIGHTS IN CABIN. REMOVED AND REPLACED 1ST WHITE EMERGENCY LIGHT AS NEEDED ON EMERGENCY STRIP. OPS CHECK GOOD.
Part: SEQUENCE VALVE — OUT OF ADJUST (MLG) · airframe 13,748 hrs · 20,773 cycles
AFTER TAKEOFF LEFT MAIN GEAR WOULD NOT RETRACT. RE-ADJUSTED BOTH MAIN GEAR DOOR SEQUENCE VALVES PER MM 32-32-04 PG 503. OPERATIONAL CHECK OK.
Part: PANEL — CRACKED (LT NACELLE FLAP) · airframe 13,283 hrs · 20,051 cycles
LEFT NACELLE FLAP HAS A CRACK ON THE OUTBOARD SIDE PANEL. DISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH A SERVICEABLE UNIT IAW MM 27-50-02. OPS CHECKS GOOD.
2003
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,711 hrs · 19,215 cycles
EMERGENCY LIGHTS - FLOOR LIGHTING INOP (IN FRONT OF GALLEY). RELAMPED AND SECURED FLOOR LIGHTING EMERGENCY IN FRONT OF GALLEY. OPS TEST GOOD.
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 12,216 hrs · 18,467 cycles
THREE EMERGENCY EXIT SIGN LIGHTS INOP - 2C, F/A JUMPSEAT AND MAIN CABIN DOOR. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. S/N OFF: 1270/08-96.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 11,705 hrs · 17,708 cycles
FLOOR LEVEL EMERGENCY LIGHT BULBS DO NOT ILLUMINATE AT ROWS 3, 4, 5. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY.
Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 11,267 hrs · 17,024 cycles
EMERGENCY LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW EMB 120 MM 33-50-1.
2002
Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 10,487 hrs · 15,812 cycles
GALLEY, FORWARD INBOARD LOWER ATTACH POINT TRACK ON FLOOR, HAS CORROSION. FOUND DURING C CHECK INSPECTION. REPLACED FLOOR TRACK THAT SERVES AS FORWARD LOWER INBOARD ATTACHMENT POINT FOR GALLEY.
Part: BUTT STRAP — CORRODED (FUSELAGE) · airframe 10,487 hrs · 15,812 cycles
FORWARD CENTER BUTT STRAP IS CORRODED IN CABIN (IN FRONT OF GALLEY). FOUND DURING C CHECK INSPECTION. REPLACED BUTT STRAP IAW 120 SRM 51-10-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,487 hrs · 15,812 cycles
FORWARD LEFT FLOOR SEAT TRACK FOUND CORRODED. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD SEAT TRACK.
2001
Part: FUSE — MISINSTALLED (AHARS COMPUTER) · airframe 8,715 hrs · 13,124 cycles
CAPTAIN AHRS FAILED INFLIGHT (RED HDG/ATT FLAGS) AND F/O'S RMI FAILED AS WELL. FAILED AGAIN INFLIGHT. REPLACED AHRS COMPUTER. OPS CHECK GOOD. FOUND AHRS FUSE F0029 NOT PROPERLY INSTALLED. RESECURED FUSE CAP. OPS CHECK GOOD.
Part: ACTUATOR — FAILED (T/E FLAP) · airframe 8,276 hrs · 12,585 cycles
LOST BLUE HYDRAULIC SYSTEM ON FINAL APPROACH INTO SAN. REPLACED LT NACELLE FLAP ACTUATOR IAW EMB120 MM CHAPTER 27-50-00. OPS AND LEAK CHECK GOOD.
Part: PROXIMITY SENSOR — DEFECTIVE (RT MLG) · airframe 3,873 hrs · 5,604 cycles
LANDING GEAR LEVER WOULD NOT RELEASE FROM DOWN POSITION ON TAKEOFF. PERFORMED ALTERNATE GEAR RETRACTION PROCEDURE PER THE QRH. REMOVED AND REPLACED RIGHT STRUT GROUND PROXIMITY SENSOR. CYCLED LANDING GEAR SEVERAL TIMES. OPS AND LEAK CHECKS GOOD IAW EMB120 MM 32-01-01. P/N: 20505-001-01.
Part: ROLLER — DAMAGED (COCKPIT WINDOW) · airframe 6,781 hrs · 10,316 cycles
RIGHT DIRECT VISION WINDOW AFT ROLLER ASSEMBLY (ON BOTTOM) FELL APART. REPLACED SNAP RING ON AFT LOWER RIGHT DIRECT VISION WINDOW ROLLER. OPS CHECK GOOD.
Part: PRESSURE SWITCH — FAILED (DEICE SYSTEM) · airframe 6,731 hrs · 10,230 cycles
MIDDLE LEFT DEICE INOP INFLIGHT. DIVERTED TO FAT FROM VIS. REPLACED LEFT MIDDLE DEICE BOOT PRESSURE SWITCH AND PATCHED SMALL HOLE IN BOOT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N ON: N735, S/N OFF: 088D10021A.
Part: BULB — BURNED OUT (CABIN) · airframe 6,665 hrs · 10,119 cycles
CEILING EMERGENCY LIGHT OVER ROW TWO INOP. INSTALLED NEW BULB AND RESPECTIVE FUSE LAMP. CHECKS GOOD.
2000
Part: PUMP — FAILED (LT ENGINE) · airframe 6,460 hrs · 9,823 cycles
LEFT MAIN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATES IN FLIGHT. REFERRED TO QRH. RETURNED TO LAX FOR LANDING. REPLACED LEFT ENGINE HYDRAULIC PUMP WITH SERVICEABLE UNIT, CHECKED GOOD. NO LEAKS. SN OFF MA575897 SNON: MX521768. ALSO REMOVED INSPECTED AND REPLACED GREEN SYSTEM HYDRAULIC PUMP FILTER, ALL FOUND GOOD. NO LEAKS AFTER REPLACEMENT.
Part: INDICATOR — MALFUNCTIONED (PROPELLER) · airframe 6,282 hrs · 9,564 cycles
RIGHT NP LOW - APPROXIMATELY 97 PERCENT - AT ROTATION/INCREASED TO 98 PERCENT AS AIRSPEED INCREASED. RETURNED TO SEA. INSPECTED CONDITION AND SECURITY OF PCU CONTROL ROD INSTALLATION. CHECKED CONDITION LEVER FREEDOM OF MOVEMENT AND LUBRICATED TELESCOPIC INPUT RODS. PERFORMED ENGINE RUN. FOUND RIGHT NP TO OPERATE AT 100 PERCENT WITHIN OPERATING LIMITS OF TABLE 203 EMB MM 71-00-00.
Part: RELAY — INTERMITTENT (WARNING LIGHT) · airframe 5,610 hrs · 8,551 cycles
ELECTRIC LIGHT ON MAP AND EMERGENCY 115V AC LIGHT ON OVERHEAD PANEL ILLUMINATES INTERMITTENTLY INFLIGHT. RETURNED TO SEA. REPLACED RELAY K0006 IAW WM 24-20-00, OPS CHECKS GOOD.
Part: SELECTOR KNOB — FAILED (TE FLAP CONTROL) · airframe 5,393 hrs · 8,238 cycles
WHEN FLAPS ARE SELECTED TO 45 DEGREES GET A CONTROL FAULT. RETURNED TO SEA. REPLACED FLAP SELECTOR HANDLE, OPS CHECKS GOOD IAW MM 275001. P/N ON: 12042642507, S/N: 405403, S/N OFF: 120040.
Part: ANNUNCIATOR — FAILED (TE FLAPS) · airframe 5,345 hrs · 8,171 cycles
DURING CLIMBOUT, THE FLAPS WOULD NOT RETRACT. THE MAP SHOWED FLAP AND ADVANCE STALL WARNING, THE FLAP OVERHEAD PANEL HAD CONTROL FAULT. REPLACED FLAP ANNUNCIATOR IAW MM 275005, OPS CHECKS GOOD ON GROUND. S/N: 0228, S/N OFF: 0216.
Part: FUEL FILTER — FAILED (NR 1)
CLIMBING THROUGH FL 180, NUMBER ONE FUEL FILTER LIGHT ILLUMINATED. RETURNED TO SFO. REPLACED HIGH AND LOW PRESSURE FUEL FILTERS, OPS CHECKS GOOD.
1999
Part: AURAL WARNING — ACTIVATED (COCKPIT)
AT V' RECEIVED TRIPLE CHIME AND HIGH SPEED WARNING. CONSULTED QRH, UNABLE TO SILENCE WARNING AND AURAL WARNING. FINALLY SILENCED AT 150 KTS AIRSPEED AND FLAPS 25'. RETURNED TO SAN. REPLACED FO'S AIRSPEED INDICATOR. PERFORMED CHECK OF HIGH SPEED AURAL WARNING SYSTEM. OPS CHECK GOOD.
Part: BOOT — FAILED (LT HORIZ STAB)
LEFT INBOARD STABILIZER BOOT FAILS INFLIGHT AT ALL CONFIGURATIONS OF TIMERS AND SETTINGS. RETURNED TO PDX. REPLACED RIGHT PRESSURE REGULATOR DUE TO LOW OUTPUT (18 PSI) AND PATCHED BOOT, OPS CHECKS GOOD.