N81536

Part: ELEVATOR — OUT OF RIG · airframe 34,194 hrs · 42,134 cycles

ON TAKEOFF, WITH FLIGHT TRIM SET, 1.5 HAD TO FIGHT ELEVATOR TO KEEP FROM PITCHING UP IN LEVEL CRUISE, FORWARD TRIM AT 2. COMPLIED WITH ELEVATOR CONTROL SYSTEM RIGGING AND ELEVATOR TRIM TAB CONTROL RIGGING.

Part: TRIM PANEL — OUT OF POSITION (PAX DOOR) · airframe 33,330 hrs · 40,870 cycles

CABIN DOOR NOT LOCKING. FOUND TRIM INTERFERING WITH DOOR HANDLE, ADJUSTED TRIM PANEL AS REQUIRED, OPS CHECK GOOD.

Part: MOUNT — CRACKED (ENGINE) · airframe 31,399 hrs · 37,687 cycles

DURING MAGNETIC PARTICLE INSPECTION, DISCOVERED ENGINE TRUSS MOUNT WELD AREA CRACKED AND TRUSS TUBE CHAFED. PERFORMED WELD REPAIR TO ENGINE MOUNT ATTACH POINTS WELD AREAS AND ENGINE TRUSS TUBE IN ACCORDANCE WITH FAA APPROVED DATA.

Part: ACTUATOR — BYPASSING (MLG) · airframe 31,138 hrs · 37,268 cycles

FLIGHT:3536 SDY/BIL DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY PERFORMED MANUAL GEAR EXTENSION. REPLACED NUMBER ONE AND NUMBER TWO MAIN LANDING GEAR ACTUATORS OPERATIONAL CHECK GOOD.

Part: OIL COOLER — DEFECTIVE (LT ENGINE) · airframe 31,131 hrs · 37,258 cycles

FLIGHT: 3564 BIL/BIL AIR RETURN DUE TO HIGH OIL TEMPERATURE ON LEFT ENGINE, LEFT ENGINE WAS SHUT DOWN AS A PRECAUTION IN FLIGHT. REPLACED NUMBER ONE OIL COOLER LEAK CHECK AND OPERATIONAL CHECK GOOD.

Part: VALVE — INOPERATIVE (MLG) · airframe 30,635 hrs · 36,422 cycles

LANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED MANUAL GEAR EXTENSION AND MADE NORMAL LANDING. R & R LANDING GEAR SERVICE VALVE.

Part: SWITCH — FAILED (MLG) · airframe 30,617 hrs · 36,392 cycles

DURING APPROACH, LANDING GEAR WOULD NOT EXTEND ON APPROACH. NO GEAR UNSAFE GREEN LIGHTS WARNING HORN, DIVERTED, NORMAL LANDING WITH MANUAL EXTENSION. REPLACED LANDING GEAR SWITCH. OPS CHECKED GOOD.

Part: ROD — LACK OF LUBE (EMERGENCY EXIT) · airframe 30,560 hrs · 36,301 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT WILL NOT OPEN. LUBRICATED DOOR SLIDING ROD. OPS CHECK GOOD.

Part: BRAKE — WORN (MLG) · airframe 30,474 hrs · 36,159 cycles

PILOT REPORTED CHECK RT BRAKES NO BRAKING ACTION. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES.

Part: RELAY — SHORTED (MLG) · airframe 30,407 hrs · 36,046 cycles

WHEN LANDING GEAR WAS SELECTED DOWN NO DOWN ANNUNCIATORS ILLUMINATED. RAN QRH AND EXTENDED LANDING GEAR MANUALLY. ALL GREEN ANNUNCIATORS ILLUMINATED EXCUTED SAFE LANDING. R & R LANDING GEAR RELAY.

Part: BULKHEAD — CRACKED (BS 84) · airframe 30,396 hrs · 36,041 cycles

DURING SCHEDULED ROUTINE OXYGEN INSP DISCOVERED A CRACK ON INBD LT PRESSURE BULKHEAD AT FS 84.00. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER AT LT PRESSURE BULKHEAD F/A 84.00.

Part: SKIN — CORRODED (BS 408.25) · airframe 30,396 hrs · 36,041 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED FUSELAGE SKIN SHOWS SIGNS OF CORROSION AT FS 408.25 BL 0.00. REMOVED DAMAGED SECTION OF STRINGER AND SKIN AND INSTALLED STRINGER SPLICE REPAIR AND AN EXTERNAL DOUBLER REPAIR.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 30,396 hrs · 36,041 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT WILL NOT OPEN FROM INSIDE HANDLE. LUBRICATED RT AFT EMERGENCY EXIT DOOR. ACFT DOWN FOR MAJOR REPAIR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,234 hrs · 35,861 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED FWD RT PRESSURE BULKHEAD BEHIND STIFFENER CRACKED. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR.

Part: HANDLE — STIFF (EMERGENCY LIGHT) · airframe 30,099 hrs · 35,701 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT OUTER HANDLE STIFF TO OPERATE. LUBRICATED LATCH MECHANISM ON RT AFT EMERGENCY EXIT OPS CHECK NORMAL.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 29,521 hrs · 35,035 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT EMERGENCY FWD EXIT DOOR IS HARD TO OPEN. ADJUSTED RT FWD EMERGENCY EXIT DOOR UPHOLSTRY.

Part: SPAR — DAMAGED · airframe 29,146 hrs · 34,610 cycles

SPAR DAMAGED, ACFT REQUIRES D+ INSP ACFT COMPANY KIT 118-4014-0003. COMPLIED WITH D+ INSP COMPANY KIT 118-4014-0003.

Part: STRUCTURE — CORRODED (LT WING) · airframe 29,097 hrs · 34,551 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON TOP LT WING T/E BY NR (1) FLAP. REMOVED CORRODED SECTION OF SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: TURBINE BLADES — DAMAGED (POWER SECTION) · airframe 28,932 hrs · 34,376 cycles

DURING CLIMBOUT LT PROPELLER KEPT ON INCREASING TO 1700 RPM EVEN AFTER CLIMB POWER SET. ALL ENGINE PARAMETERS WERE NORMAL. DURING POST FLIGHT OBSERVED HOLES IN BOTH EXHAUST STACKS AND LT PROPELLER FAILED TO ROTATE. REPLACED LT ENGINE POWER SECTION, OPS CHECKS NORMAL.

Part: SKIN — CORRODED (BS 393.25) · airframe 28,932 hrs · 34,375 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE SKIN EXFOLIATED AT FS 393.25 AND FS 408.25. REMOVED CORRODED SECTION OF SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 28,932 hrs · 34,375 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED INBD RT WING UPPER T/E HAS SURFACE CORROSION BETWEEN WS 140.36 TO WS 196.06. REMOVED DAMAGE AND INSTALLED AND EXTERNAL REPAIR DOUBLER.

Part: CABLE — BROKEN (PAX DOOR) · airframe 28,392 hrs · 33,799 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED PAX DOOR TOP FWD CABLE BROKEN NEEDS TO BE REPLACED. REPLACED PAX DOOR TOP FWD CABLE.

Part: DOOR — CORRODED (PAX DOOR) · airframe 28,392 hrs · 33,799 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR LOWER FWD SKIN EXFOLIATED AND CRACKED AND LOWER AFT AREA DEBONDED. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED INNER SKIN FILLER AND EXTERNAL DOUBLER REPAIR. OPEN

Part: ANGLE — CRACKED (PAX DOOR) · airframe 28,392 hrs · 33,799 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED CRACKS ON AIRSTAIR DOOR FRAME INTERIOR ANGLE AT FS 150.50 BETWEEN STINGERS 9L TO 10L. REPAIRED AIRSTAIR DOOR FRAME ANGLE. INSTALLED FRAME ANGLE AND JOINT ANGLES.

Part: CAMLOCK — STUCK (PAX DOOR) · airframe 28,195 hrs · 33,577 cycles

PILOT REPORTED UNABLE TO CLOSE CABIN DOOR APPEARS CAMLOCKS ON AFT SIDE OF DOOR ARE NOT ROTATING. REPLACED AFT UPPER AND LOWER CABIN DOOR CABLES. OPS CHECK NORMAL.

Part: CABLE — FRAYED (PAX DOOR) · airframe 28,195 hrs · 33,578 cycles

PILOT REPORTED CABIN DOOR CABLES APPEAR TO BE BINDING AND VERY DIFFICULT TO CLOSE AND LOCK CABIN DOOR. REPLACED CABIN DOOR FWD BOTTOM CABLE ASSY.

Part: GAS GENERATOR — LOW PRESSURE (RT ENGINE) · airframe 28,085 hrs · 33,462 cycles

WHILE ENROUTE, THE RT ENG OIL PRESSURE DROPPED TO THE YELLOW ARC AND FLUCTUATED BETWEEN 60-70 PSI. THE RT LOW OIL PRESSURE ANNUNCIATOR STARTED FLASHING, SECURED THE RT ENGINE. PERFORMED EMERGENCY CHECKLIST, DECLARED AN EMERGENCY WITH ATC AND RETURNED TO DEPARTURE. ACFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RT GAS GENERATOR MODULE.

Part: SWITCH — OUT OF ADJUST (NLG) · airframe 27,896 hrs · 33,262 cycles

FLIGHT: 9166, AFTER TAKEOFF THE LANDING GEAR UNSAFE HANDLE LIGHT REMAINED ON AFTER GEAR RETRACTION. CONTINUED TO DESTINATION. LANDED WITHOUT INCIDENT. ADJUSTED NOSE LANDING GEAR UP POSITION INDICATOR SWITCH. LANDING GEAR OPERATIONAL CHECK OK.

Part: DOWNLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 27,877 hrs · 32,240 cycles

FLIGHT: 9236, AFTER TAKEOFF WHEN LANDING GEAR RETRACTED THE GEAR HANDLE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. ADJUSTED RT DOWNLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK OK.

Part: LANDING GEAR — FAILED · airframe 27,570 hrs · 32,942 cycles

ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT WITHOUT MOVING THE "J" HOOK. TROUBLESHOT LANDING GEAR SYS, SAFETY SWITCH COULD NOT DUPLICATE. OPS CHECK SATISFACTORY.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 27,193 hrs · 32,547 cycles

PILOT REPORTED FUEL LEAK FROM PANEL UNDER RT WING OTBD SIDE OF THE ENGINE. REPAIRED LOWER WING SKIN AROUND FUEL ACCESS PANELS 631DB AND 631CB.

Part: GAS GENERATOR — FOD (NR 1 ENGINE) · airframe 27,187 hrs · 35,542 cycles

DURING CLIMBOUT, SPARKS COMING OUT OF THE NR 1 ENGINE. ALL INSTRUMENT INDICATIONS READING NORMAL AND NO ANNUNCIATOR ILLUMINATED. FOUND NR ONE ENGINE GAS GENERATOR FIRST STAGE COMPRESSOR BLADE DAMAGE DUE TO FOREIGN OBJECT DEBRIS, REPLACED GAS GENERATOR.

Part: SWITCH — OUT OF ADJUST (MLG WARNING HORN) · airframe 27,029 hrs · 32,376 cycles

FLIGHT:5202 FLL/FLL - DURING TEST FLIGHT LANDING GEAR WARNING HORN ACTIVATE AT 81 PERCENT N1. ADJUSTED LANDING GEAR WARNING HORN SWITCHES TEST FLIGHT SATISFACTORY.

Part: PUMP — LEAKING (ENG DRIVEN FUEL) · airframe 27,029 hrs · 32,376 cycles

FLIGHT: 5202 FLL/FLL - DURING TEST FLIGHT, CABIN SMELLS LIKE FUEL. REPLACED LEFT ENGINE DRIVEN FUEL PUMP.

Part: SPAR — CORRODED (LT WING) · airframe 27,028 hrs · 32,375 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED POSSIBLE AREAS OF CORROSION IN LT WING FUEL COLLECTOR TANK ON MAIN SPAR. REMOVED CORROSION ON LEFT MAIN SPAR LOWER CAP AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS.

Part: STRINGER — CORRODED (LT WING) · airframe 27,028 hrs · 32,375 cycles

DURING SCHEDULED INSP DISCOVERED POSSIBLE AREAS OF CORROSION IN LT WING FUEL COLLECTOR TANK FWD BONDED STRINGER. FABRICATED AND INSTALLED REPAIR STRINGER AND FORWARD AND AFT REPAIR DOUBLERS.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 26,379 hrs · 31,694 cycles

FLIGHT 9181 PNS/TPA - PILOT REPORTED CABIN DOOR EXTREMELY DIFFICULT TO CLOSE FROM INSIDE CABIN. CLOSED DOOR PROPERLY MULTIPLE TIMES. OPERATIONAL CHECK NORMAL.

Part: UNKNOWN — NOISY (NLG) · airframe 26,360 hrs · 31,676 cycles

FLIGHT 5403 MIA/FLL - AFTER TAKEOFF RETRACTING LANDING GEAR A "CLUNK AND THUD" IS HEARD FROM NOSE WHEEL, GEAR FUNCTIONS NORMALLY AND VISUAL INSPECTION DOES NOT LOOK ABNORMAL. PERFORMED LANDING GEAR OPERATIONAL CHECK. NO DEFECTS NOTED.

Part: KEEL — CHAFED (LT NACELLE) · airframe 26,305 hrs · 31,623 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED LT NACELLE KEEL CHAFING AT THE INBD SIDE FENDER ATTACHMENT FLANGE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND CAP REPAIR DOUBLER.

Part: ACTUATOR — CRACKED (NLG) · airframe 25,705 hrs · 30,911 cycles

FLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT INSPECTION FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR.

Part: ACTUATOR — CRACKED (NLG) · airframe 26,256 hrs · 31,567 cycles

FLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR.

Part: SOCKET — DIRTY (COCKPIT) · airframe 26,232 hrs · 31,538 cycles

FLIGHT 9166 - NAS/FLL - PILOT REPORTED LANDING GEAR ANNUNCIATOR GREEN "L" DOESN'T ILLUMINATE WITH GEAR DOWN. CLEANED ANNUNCIATOR LIGHT SOCKET.

Part: SKIN — CORRODED (FUSELAGE) · airframe 26,200 hrs · 31,507 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LOWER FUSELAGE SKIN AT FS 438.250 STRINGER 16. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: UNKNOWN — LEAKING

DURING FLIGHT, STRONG FUEL ODOR IN CABIN, MADE PASSENGER SICK. REMOVED AND CLEANED OLD SEALANT AT SUSPECTED FUEL LEAK AREA AND RESEALED. NO LEAKS NOTED. (K)

Part: FUEL SYS — LEAKING · airframe 26,108 hrs · 31,399 cycles

DURING ROUTINE MX, CUT OUT A SMALL ACCESS SECTION OF LT FUSELAGE BETWEEN FS 288 AND FS 318 FOR FUEL LEAK REPAIR. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER.

Part: UNKNOWN — ODOR (FUEL SYSTEM)

DURING FLIGHT STRONG SMELL OF FUEL IN CABIN, PASSENGERS COMPLAINED. AUX TANKS SHOW ZERO FUEL ON GUAGES. INSPECTED AUX TANKS FOUND NO FUEL PRESENT. INSPECTED CABIN CLEANED RESIDUAL FUEL FROM CABIN FLOOR. (K)

Part: FUEL — ODOR (CABIN)

DURING FLIGHT, STRONG ODOR OF FUEL IN CABIN, PASSENGERS COMPLAINED. AUX TANKS SHOW ZERO FUEL ON GUAGES. INSPECTED AUX TANKS FOUND NO FUEL PRESENT, INSPECTED CABIN CLEANED RESIDUAL FUEL CABIN FLOOR. (K)

Part: UNKNOWN — ODOR (FUEL SYSTEM)

DURING FLIGHT, STRONG SMELL OF FUEL VAPORS IN CABIN. DRAINED RT AUX TANK. TEST RAN AIRCRAFT FOR 40 MINUTES. NO FUEL SMELL NOTED. (K)

Part: TANK — LEAKING (FUEL SYSTEM)

DURING FLIGHT, STRONG FUEL ODOR PRESENT IN CABIN. LT AUX TANK SUSPECT, LEAK AREA, REMOVED OLD SEALANT AND APPLIED NEW SEALANT. SEALANT CURE TIME ACCOMPLISHED. PERFORMED LEAK CHECK, NO FUEL NOTED. (K)

Part: CHECK VALVE — ODOR (FUEL SYSTEM)

PILOT DISCREPANCY: PILOT REPORTED DURING FLIGHT FUEL ODOR IN CABIN. REPLACED RT FUEL TRANSFER LINE CHECK VALVE. (K)

Part: CHECK VALVE — LEAKING (FUEL SYSTEM)

FLIGHT 9186, DURING FLIGHT, STRONG ODOR OF FUEL IN CABIN. REPLACED LT AUX TANK TRANSFER LINE CHECK VALVE. (A)

Part: UNKNOWN — ODOR (CABIN) · airframe 25,891 hrs · 31,123 cycles

FLIGHT: 5200, DURING FLIGHT CABIN SMELLS LIKE JET FUEL FUEL. INSPECTED UNDER CABIN FLOORBOARD NO LEAK NOTED CLEANED UNDER FLOOR AS NEEDED.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 25,891 hrs · 31,122 cycles

FLIGHT: 9184, DURING FLIGHT, CABIN AND COCKPIT SMELLS OF FUEL ON THE GROUND AND IN FLIGHT, SMELL OF FUEL OUT OF VENTS AS WELL. INSPECTED FOR FUEL AROUND ACM AND INLET NO FUEL NOTED ALSO INSPECTED VENT BLOWERS AND AIR VENTS NO FUEL NOTED.

Part: INLET — CONTAMINATED (ACM) · airframe 25,887 hrs · 31,118 cycles

FLIGHT: 9254, DURING APPROACH, AIRCRAFT CABIN SMELLS OF FUEL. CLEANED RESIDUAL FUEL AT ACM AIR INLET. RAN ENGINES NO FUEL SMELL NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,884 hrs · 31,115 cycles

FLIGHT: 9150, DURING FLIGHT, FUEL SMELL IN THE CABIN. INSPECTED FOR FUEL AROUND ACM NO FUEL FOUND, RAN ENGINES NO FUEL SMELL NOTED.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 25,881 hrs · 31,109 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED RT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT CTR ELEVATOR HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 25,881 hrs · 31,109 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET.

Part: SPAR CAP — CORRODED (HORIZ STAB) · airframe 25,881 hrs · 31,109 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED RT HORIZONTAL STABILIZER UPPER SPAR CAP EXFOLIATED. REPLACED RT HORIZONTAL STABILIZER UPPER SPAR CAP.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 25,881 hrs · 31,109 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 25,881 hrs · 31,109 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT CENTER ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT CTR ELEVATOR HINGE BRACKET.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,826 hrs · 31,046 cycles

DURING FLIGHT, STRONG FUEL SMELL IN THE CABIN WITH BLOWERS ON HIGH. RAN BOTH ENGINES COULD NOT DETECT ODOR TREATED CARPET AS NEEDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,777 hrs · 30,993 cycles

FLIGHT 9174, DURING FLIGHT, STRONG SMELL OF FUEL. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. INSPECTED AC FUEL SYS, LT AND RT WING FUEL PANELS, LT AND RT ENGINE FOR LEAKS, NO LEAKS NOTED. PERFORMED ENGINE RUN FOR(15) MINUTES WITH BLEEDS ON AND OFF, NO STRONG FUEL SMELL NOTED.

Part: SKIN — CORRODED (BS 290-326) · airframe 24,597 hrs · 29,603 cycles

AT SCHEDULED INSPECTION DISCOVERED SEVERAL SPOTS OF SURFACE CORROSION ON AIRCRAFT BELLY SKIN BETWEEN LBL 29.06 AND RBL 29.06 FS 290.50 AND 326.00. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED NEW SKIN PANEL FROM IAW FAA APPROVED DATA CONTAINED IN FIELD REPAIR FR-CO-01592, REV 1.

Part: PCB — SHORTED (MLG) · airframe 24,415 hrs · 29,393 cycles

FLIGHT: 9162 FLL/FPO DURING APPROACH NO GREEN LANDING GEAR INDICATION WHEN GEAR HANDLE DOWN. RETURNED, LANDED WITHOUT INCIDENT. REPLACED ANNUNCIATOR PCB A125 LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: WIRE — LOOSE (FIRE BOTTLE) · airframe 24,131 hrs · 29,063 cycles

FLIGHT: 9170 FLL/TCB, AFTER TAKEOFF THE NR (1) FIRE DISCHARGE ANNUNCIATOR FLICKERED ON AND OFF. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE ON THE NR (1) FIRE BOTTLE.

Part: LATCH — DIRTY (EMERGENCY DOOR) · airframe 23,952 hrs · 28,869 cycles

AT SCHEDULED FLEET CAMPAIGN INSPECTION: EMERGENCY DOOR AT SEAT 6A UNABLE TO OPEN FROM INSIDE AIRCRAFT. CLEANED AND LUBED DOOR LATCH ASSEMBLY.

Part: TRUSS — CHAFED (ZONE 400)

AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE MFG AIRLINER SERIES STRUCTURAL REPAIR MANUAL, CHAPTER 71-91-05.

Part: WARNING LIGHT — INTERMITTENT (LT ENGINE)

DURING FLIGHT, LT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. CHECKED SYSTEM AND PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE. OPS CHECK NORMAL. (K)

Part: CONNECTOR — CORRODED (DISPLAY)

FLT 9225 - MIA/NAS - DURING FLIGHT, PILOTS DISPLAY PROCESSOR CIRCUIT BREAKER POPPED ACCOMPANIED BY SMELL OF SMOKE MOMENTARILY. MAINTENANCE FERRY TO FLL. FOUND BULKHEAD CONNECTOR J368 PINS SHORTED. REMOVED AND REPLACED J368 CONNECTOR AND RECEPTACLE P/N MS3476W2241S. OPERATIONAL CHECK NORMAL. (M)

Part: BRACKET — CORRODED (RT STAB ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET.

Part: BRACKET — CORRODED (ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.

Part: TURBINE BLADES — FAILED (LT ENGINE)

FLT 9236 - EYQ/TPA - AFTER CLEARANCE FOR TAKEOFF, LEFT ENGINE FAILED. ENGIEN IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POEWR SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CONFIRMED 2ND STAGE POWER TURBINE BLADE FAILURE. SUBSTANTIAL DAMAGE OCCURRED. ONLY 'STUBS' REMAIN. FULL OVERHAUL OF POWER SECTION REQUIRED. (M)

Part: TURBINE BLADES — FAILED (LT ENGINE)

AFTER CLEARANCE FOR TAKEOFF, LT ENGINE FAILED. ENGINE IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAD MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODUEL AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. (M)

Part: BOLT — LOOSE (VERTICAL STAB)

AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.

Part: FIRE LOOP — FAULTY (LT ENGINE)

FLT 9428 - MCO-MIA - DURING FLIGHT, LEFT FIRE LOOP AMBER ANNUNCIATOR CAME ON. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP. OPERATIONAL TEST NORMAL. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

FLT 9501 - EYW/TPA - DURING FLIGHT, NR 1 ENGINE HAS A RAPID INCREASE IN ITT AND FUEL FLOW. PRECAUTIONARY SHUTDOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: CONNECTOR — LOOSE (LT ENGINE)

FLT 9122 - NAS/FLL - DURING FLIGHT, LEFT FIRE BOTTLE DISCHARGE LIGHT COMES ON INTERMITTENTLY. SECURED LOOSE CONNECTION AT LEFT ENGINE FIRE BOTTLE SQUIB. SYSTEM OPS CHECK NORMAL. (M)

Part: WIRE — LOOSE (FIRE BOTTLE)

FLT 9453 - NAS-MIA - DURING FLIGHT, LEFT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. SECURED WIRE AT LEFT ENGINE FIRE BOTTLE. (M)

Part: BRACKET — BROKEN (PASSENGER DOOR)

CREW REPORTED AFTER TAKEOFF FROM CLEVELAND THEY RECEIVED WARNING LIGHT FOR PASSENGER DOOR. A/C RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED/REPLACED PASSENGER DOOR MICROSWITCH BRACKET WHICH WAS FOUND TO BE BROKEN. PERFORMED OPERATIONAL CHECKS FOR THE PASSENGER DOOR WARNING SYSTEM IAW BEECHCRAFT MM 52-70-00. A/C WAS RELEASED FOR SERVICE.

Part: SKIN — FAILED (FUSELAGE)

DURING A 1ST 200 HOUR INSPECTION, A 3 INCH CRACK WAS FOUND ON THE RIGHT SIDE EXTERIOR SKIN OF AIRCRAFT MIDSECTION INBOARD OF PANEL 611AB NEAR THE MAIN SPAR. MAINTENANCE REMOVED THE INTERIOR FOR INSPECTION OF THE SPAR AND SURROUNDING AREAS AND FOUND NO OTHER DAMAGE. THE SKIN WAS REPAIRED AT SF 288 WITH A DOUBLER PATCH IAW FAA/DER APPROVED DRAWING NR DA006-35S DATED 6/23/00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SWITCH — DIRTY (RT MLG)

AZO-CLE - FLT 3032 - THE CREW REPORTED THE LANDING GEAR LIGHTS ON THE RIGHT SIDE DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GEAR SWINGS AND FOUND THE RT DOWNLOCK INDICATOR TO BE VERY DIM, THE CLEANED THE UP AND DOWN LOCK SWITCHES AND OPS CHECKED THE SYSTEM GOOD IAW B1900D MM 32-30-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: TRUSS — CHAFED (RT ENGINE)

CLE - THE ORIGINAL SDR FILED ON 3/3/99, REPORTED THAT THE RIGHT ENGINE TRUSS ASSEMBLY ATTACHMENT BOLT WAS MISSING, CAUSING CHAFED DAMAGE TO THE TRUSS TO WING ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD UPPER KEEL IAW B1900 SRM 51-40-02 AND 51-40-04. THE TRUSS ASSEMBLY WAS REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES IAW B1900 MM 71-20-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BOLT — MISSING (RT ENGINE)

CLE - DURING A SCHEDULED INSPECTION THE RIGHT ENGINE AND TRUSS ASSEMBLE WAS FOUND TO HAVE EXCESSIVE MOVEMENT. THE ASSEMBLE WAS INSPECTED FURTHER AND WAS FOUND TO HAVE THE INBOARD UPPER TRUSS ATTACHMENT BOLT MISSING. THE REPAIR OF ASSOCIATED CHAFE DAMAGE IS PENDING EVALUATION BY THE MANUFACTURE AND CONTINENTAL EXPRESS ENGINEERING DEPT. (M)

Part: SWITCH — INOPERATIVE (NLG)

IAH - FLT 3462 - THE CREW REPORTED THAT AFTER THE GEAR WAS RETRACTED THE RED INTRANSIT LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK SWITCH IAW B1900 MM 32-60-01. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)

Part: TURBINE — DAMAGED (RT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT ENGINE WAS FOUND TO HAVE A BLADE TIP MISSING ON THE 2ND STAGE POWER TURBINE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 4272003. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FIRE LOOP — CHAFED (LT ENGINE)

CLE - FLT 3160 - CREW REPORTED THE LEFT FIRE WARNING SYSTEM ACTIVATED IN FLIGHT, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE FIRE LOOP IAW B1900 MM 26-10-00, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SWITCH — FAULTY (EMPENNAGE)

CLE - FLT 3107 - CREW REPORTED THAT THE TAIL DE-ICE LIGHT WOULD NOT EXTINGUISH IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE TAIL DE-ICE PRESSURE SWITCH IAW B1900 MM 30-10-00. OPERATIONAL CHECK WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TRANSMITTER — FAILED (LT ENGINE)

CLE - FLT 3237 - CREW REPORTED DURING CRUISE FLIGHT, THE LEFT HAND ENGINE OIL PRESSURE ROSE TO 140 PSI. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE OIL PRESSURE TRANSMITTER IAW B1900 MM 79-30-00. OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT 3,234.5 HOURS. ACFT TC 4,053. (X)

Part: COMPRESSOR — DAMAGED (LT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, LEFT HAND ENGINE COMPRESSOR BLADES WERE FOUND DAMAGED BY UNKNOWN FOREIGN OBJECTS. THE COMPRESSOR BLADES WERE FOUND DAMAGED BEYOND LIMITS, MAINTENANCE REMOVED AND REPLACED THE LEFT HAND ENGINE IAW B1900 MM 71-00-00. OPERATIONAL CHECKS SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. ACFT TT 3,195.2 HOURS. ACFT TC 4,003. (X)