N308GB

Part: CONTROLLER — MALFUNCTIONED (A/C BAY) · airframe 61,756 hrs · 27,246 cycles

NR 1 PACK OVERHEAT, SMELLED SMOKE IN COCKPIT. RETURNED TO RAMP. RESET TEMPERATURE CONTROLLER NR 1 PACK, OPS CHECK NORMAL IAW MM 21-62-01. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN.

Part: INDICATOR · airframe 61,517 hrs · 27,125 cycles

LOG PAGE 21540. DISCREPANCY: #1 ENGINE STARTER ACCELERATES N3 TO 46% VERY RAPIDILY THEN CUTS OUT BEFORE FULL ENGINE LIGHT UP. CORRECTIVE ACTION: REMOVED AND REPLACED N3 INDICATOR IAW MM 77-12-03 OPS CK NORMAL IAW MM 71-00. AIRCRAFT RETURN TO SERVICE.

Part: SENSOR — FAILED (RT MLG) · airframe 61,410 hrs · 27,069 cycles

LANDING GEAR LEVER COULD NOT BE RAISED, HAD TO DEPRESS BUTTON TO RAISE SELECTOR. TROUBLESHOOT SYSTEM, REMOVED AND REPLACED RT MLG AIR/GROUND SENSOR IAW MM 32-63-01, OPS CHECKED SYSTEM NORMAL IAW MM 32-63-0. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — MALFUNCTIONED (L/E SLAT) · airframe 61,390 hrs · 27,061 cycles

DURING FLAP EXTENSION NO SLAT INDICATION ON FLIGHT ENGINEER PANEL. AIRCRAFT RETURNED TO BLOCKS. RESET L/E SLAT ASYMMETRY BRAKES AND ACCOMPLISHED ALL REQUIRED TEST. L/E SLAT TESTED GOOD PER MM 27-81-00. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — DEFECTIVE (LANDING GEAR) · airframe 61,294 hrs · 27,018 cycles

COULD NOT EXTEND LANDING GEAR NORMALLY AT MIA; EXTENDED GEAR BY ABNORMAL ALTERNATE EXTENSION PROCEDURES. REMOVED AND REPLACED LANDING GEAR CONTROL (MODULE) & 4 WAY SOLENOID VALVE IAW MM 32-31-14 & 32-31-02. PERFORMED LANDING GEAR RETRACTION AND EXTENSION TEST AND WAS NORMAL IAW MM 32-20-00.

Part: ENGINE — MAKING METAL (NR 3) · airframe 61,274 hrs · 27,009 cycles

AT CRUISE 33,000; NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI - MOVED THROTTLE TO IDLE, OIL PRESSURE REDUCED TO 20 PSI; COMPLETED ENGINE SHUTDOWN PROCEDURE AT 23:45 ZULU. OIL QUANTITY IS OK. INSPECTION REVEALED METAL IN OIL SYSTEM. ACCOMPLISHED NR 3 ENGINE CHANGE IAW ARROW AIR RB 211 MAINTENANCE FORM L-1011-7104A & ENGINE OPERATIONAL CHECK IAW ARROW AIR RB 211 MAINTENANCE FORM L-1011-7102B ENGINE OPS CHECKED NORMAL. ACCOMPLISHED ADJUSTMENT AND TEST ALT ALERT, OPS NORMAL IAW MM 22-17-00 PG 512.

Part: COMPRESSOR — VIBRATION (NR 3 ENGINE) · airframe 61,169 hrs · 26,972 cycles

AIRFRAME VIBRATION FELT FOLLOWED BY INCREASED VIBRATION ON NR 3 ENGINE. ENGINE SHUTDOWN PER CHECKLIST, REPORTED TIME 16:50Z. REMOVED AND REPLACED LP FAN BLADES IAW MM 72-31-05, REMOVED 3 HOLE BALANCE WEIGHT FROM THRUST RING. RAN ENGINE NR 3, PERFORMED TEST NR 16 IAW MM 71-00-00. VIBRATION SURVEY WITHIN LIMITS. ENGINE OK FOR SERVICE.

Part: ENGINE — VIBRATION (NR 3) · airframe 61,164 hrs · 26,970 cycles

EXPERIENCED SUDDEN INCREASE IN VIBRATION ON NR 3 ENGINE FROM 1.2 TO 2.4. RETURNED TO MIAMI FOR AN UNEVENTFUL LANDING. LUBED CLAPPERS, CHECKED CHIP DETECTORS ACCOMPLISHED TEST NR 11 VIBRATION SURVEY IAW L1011 FORM 7102B VIBRATION WITHIN LIMITS.

Part: ENGINE — VIBRATION (NR 3) · airframe 61,167 hrs · 26,971 cycles

ON TAKEOFF ROLL C&W PANEL ENGINE VIBRATION FILTER PRESS LIGHT ON NR 3 ENGINE INDICATING 2.6 UNITS FAN POSITION. ABORTED TAKEOFF AT 80 KNOTS POWER SETTING .427 EPR. CHECKED CHIP DETECTORS AND MAIN OIL SCREEN, ALL OK. LUBED BLADES IAW MM 72-31-05, PERFORMED TEST 11 VIBRATION SURVEY WITHIN LIMITS IAW MM 71-91-00. BOROSCOPE DEFERRED FOR 25 HRS IAW 71-00-00.

Part: ENGINE — VIBRATION (NR 3)

ENGINE NR 3 SHUTDOWN AT 0535Z DUE TO VIBRATION A & B LOW POSITION 2.5 WARNING LIGHT ON OTHER PARAMETERS NORMAL.

Part: ENGINE · airframe 61,083 hrs · 26,939 cycles

LOG PAGE 21133. DISCREPANCY: IN CRUISE FL 330 #1 ENGINE VIBRATION SPIKED TO 4.5 BOTH CHANNELS ON VIBRATION MONITOR WITH NOTICEABLE INCREASE IN AIRFRAME VIBRATION. AS PER EMERGENCY CHECKLIST ENGINE WAS SHUT DOWN AT 12:40Z ALL OTHER ENGINE INDICATIONS APPEARED NORMAL. AIRCRAFT RETURN TO KMIA AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION:

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 60,991 hrs · 26,900 cycles

F/O'S RIGHT PITOT HEAT LIGHT ON WITH SWITCH IN. F/O AIRSPEED INDICATION FAILED 5' LATER, THEN NR 2 MACH FEEL CHANNEL AND NR 2 MACH TRIM FAILED, RUDDER HYDRAULIC LIMITER LIGHT ON PILOT'S C&W PANEL ON 34-14-61-02. REMOVED AND REPLACED AIR DATA SENSOR HEAT PANEL IAW MM 30-31-00, OPS CK NORMAL.

Part: ENGINE — VIBRATION (NR 1) · airframe 60,835 hrs · 26,832 cycles

AT TOP OF CLIMB NR 1 ENGINE VIBRATION SPIKED AT 3.0 BOTH CHANNELS IN-FLIGHT SHUT DOWN AND RETURN TO KMIA. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE - PER MM L1011 FORM 7104A, OPS CHECK OK IAW MM L1011 - 7102B; RUN UP IAW MM 71-00-00.

Part: ENGINE — VIBRATION (NR 1) · airframe 60,799 hrs · 26,814 cycles

ENGINE NR 1 SUDDEN INCREASE IN VIBRATION FROM 1.8 TO 3.0 UNITS WITH A OR B SELECTED ON NORMAL OR LOW. WARNING LIGHT WAS ON. AIRCRAFT LANDED WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE INSPECTION, NO DEFECTS NOTED. INSPECTED CHIPS AND REMOVED AND REPLACED OIL FILTERS, ALL CHECKED CLEAN, NO INDICATION OF FAILURE. INSPECTED INLET AND EXHAUST AREAS, NO DEFECTS NOTED. FAN BLADES REMOVED AND CLEANED, ALSO CLEANED DAMPNERS. ALL ABOVE ACCOMPLISHED IAW MM FAULT ISOLATION MANUAL 71-91-00 PAGE 106 THRU 108. ACCOMPLISHED TEST NR 11 VIBRATION WITHIN MM LIMITS IAW MM 71-00-00 PAGE 217. MAX AVM AT 1.63 T/O EPR WAS .09.

Part: ENGINE — VIBRATION (NR 3 ENGINE) · airframe 60,527 hrs · 26,696 cycles

NR3 ENGINE VIBRATION UNITS WENT ABOVE 2.5 SHORTLY AFTER LEVEL OFF IN CRUISE. 04:50Z SHUTDOWN ENGINE IN ACCORDANCE WITH ABNORMAL VIBRATION CHECKLIST. HIGH VIBRATION READING WAS ONLY IN THE LOW SELECTION ALL OTHER READINGS WERE NORMAL.CORRECTIVE ACTION: PERFORMED BOROSCOPE INSPECTION IAW L1011 MM VOLUME I FORM PAGE 3-9-1 THRU 3-9-5 NO DISCREPANCIES FOUND. CLEANED FIR TREE AND LUBED MID-SPANS PER MM 72-31-05, PERFORMED TEST NR11 VIBRATION SURVEY. VIBRATION WITHIN LIMITS.

Part: SENSOR — OUT OF ADJ (LT MLG) · airframe 60,460 hrs · 26,666 cycles

TRUCK LIGHT REMAINS ON AFTER TAKEOFF. GEAR WOULD NOT RETRACT. AIR TURNBACK. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUSTED TRUCK SENSOR LEFT MLG, COMPLETED LANDING GEAR RETRACTION AND ALL SYSTEMS CHECK OK IAW MM 32-30-00.

Part: ENGINE — VIBRATION (NR 1 ENGINE)

NR 1 ENGINE SHUTDOWN IN FLIGHT AND RETURNED TO MIAMI DUE TO 2.5 SPIKE ON VIBRATION, BOTH CHANNELS IN THE LOW RANGE. REMOVED AND INSPECTED MASTER INTERNAL GEARBOX CHIP DETECTORS IAW 72-01-00, NO EVIDENCE OF INTERNAL FAILURE FOUND. VISUALLY INSPECTED AIR INLET LOW PRESS COMPRESSOR AND EXHAUST, NO EVIDENCE OF FOD. CLEANED AND LUBRICATE CLAPPERS IAW MM 72-31-05. PERFORMED VIBRATION SURVEY TEST NR 11 IAW 71-00-00 VIBRATION WITHIN LIMITS CHECK OK.

Part: ENGINE — MALFUNCTIONED (NR 2)

MIA - FLT 308 - NR 2 ENGINE FILTER PRESSURE LIGHT ON IN STEADY RUNNING CONDITION (OIL) IN CRUISE NR 2 ENGINE SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR JOB CARD L1011 M131. OPS NORMAL, AIRCRAFT RETURN TO SERVICE. (M)

Part: COMPARATOR — FAILED (TE FLAPS)

MIA - FLT 558 - FLAPS NOT EXTENDED FOR LANDING, LE SLATS OK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FLAP BRAKES LOCKED OUT. RESET FLAPS. OPS NORMAL IAW MM 27-51-60. REMOVED AND REPLACED FLAP ASSY COMPARATOR. OPS CHECK NORMAL IAW MM 27-51-49. (M)

Part: VALVE — FAILED (NR 1 PACK)

MIA - FLT 508 - CABIN SMOKE ALARM, VERY ACRID SMELL. FOUND NR 1 PACK, OIL IN SYSTEM. NR 1 PACK ON DMI NR 9904 PER MEL 21-51-07. NR 1 PACK VALVE LOCKED IN CLOSE POSITION. (M)

Part: CONTROL — OUT OF ADJUST (HORIZ STAB)

STAB C/D PF CS LIGHTS ON. ON CONTROL CHECK, WITH PULL PITCH DISC LIGHT, PERFORMED STAB POS SYSTEM FAULT ISOLATION PER MM 27-43-00, NO FAULTS DETECTED. PERFORMED STAB CONTROL SYSTEM ADJUSTMENT AND TESTED PER MM 27-41-0. OPS NORMAL, NO FAULTS DETECTED.

Part: WIRE — FAILED (CARGO DOOR)

CABIN CARGO DOOR LIGHT ON F/E PANEL ILLUMINATED WHEN DOOR IS CLOSED REPAIRING WIRING AT 5272TBY2 PER MARSHALL WIRING DIAGRAM. OPS NORMAL IAW 52-72-01.

Part: CLAMP — LOOSE (AFT FUSELAGE)

RETURNED TO BLOCKS DUE PNEUMATIC LEAK, AFTER ENGINE START NR 8R CABIN SMOKE DETECTOR ILLUMINATED. UPON VISUAL INSPECTION HOT AIR WAS FOUND COMING THROUGH A HOLE IN THE AFT CABIN. FOUND LOOSE CLAMP AT AFT FUSELAGE DUCT COUPLING, RETORQUED CLAMP, OPS NORMAL, NO LEAKS NOTED AS PER M/M 20-20-00 PG 64-08.

Part: PROX SWITCH — BROKEN (RT MLG DOOR)

ON LANDING GEAR EXTENSION GOT 3 GREEN, RED DOOR AND IN TRANS, LIGHT ALSO GOT RT GEAR DOOR LIGHT ON F/E ANUNCIATOR. FOUND RT GEAR DOOR PROX SWITCH BROKEN. REMOVED AND REPLACED PROX SWITCH AND CONDUIT IAW 32-6-1, OPS CHECK NORMAL.

Part: ANNUNCIATOR — MALFUNCTIONED (COCKPIT)

SJU - FLT 504 - GROUND TURN-BACK. FLIGHT CONTROL LIGHT ON PILOT'S ANNUNCIATOR PANEL NR 1 YAW SAS. RE-SEATED IA34 CARD IN ICCB BOARD. OPS CHECK NORMAL IAW MM 33-17-00. (X)

Part: COMPARATOR — FAILED (FLAP ASYMMETRY)

MIA - FLT 617 - SLAT ASYMMETRY DETECTION FAULT, LIGHT ON AFTER EXTENDING FLAPS. PERFORMED ABNORMAL PROCEDURES. LIGHT REMAINED ON. RETURNED TO BLOCK. REMOVED AND REPLACED SLAT ASYMMETRY COMPARATOR. OPS CHECK NORMAL IAW MM 27-81-01. (X)

Part: TR COWL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE TRANSLATING COWL EXTERIOR SKIN AT 6 O'CLOCK POSITION CRACKED. REPAIRED DAMAGED SKIN AS PER EO NR 2112543001. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3, L/P 12689, ITEM 3M.

Part: ADC — MALFUNCTIONED (E/E BAY)

BDL - FLT 505 - ON TAKEOFF ROLL, CAPTAIN'S AIRSPEED FAILED WITH NR 1 MACH FEEL, NR 1 ATS, NR 1 MASK TRIM FAIL WITH NUMEROUS FLAGS. REMOVED AND REPLACED A.D.C., GROUND CHECKED, AND OPERATIONAL NORMAL IAW MM 34-14-00. (X)

Part: ADC — MALFUNCTIONED (E/E BAY)

BDL - FLT 505 - ON TAKEOFF, CAPTAIN'S AEROSPEED FAILED WITH NR 1 MACH FEEL, NR 1 ATS, NR 1 MACH TRIM FAIL WITH NUMEROUS FLAGS. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER GROUND CHECKED AND OPERATIONAL CHECKED NORMAL IAW MM 34-14-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — DIRTY (AIR DATA COMP)

ON TAKEOFF, CAPTAINS AIRSPEED INOPERATIVE WITH NUMBER ONE (1) MACH FEEL, NUMBER ONE (1) ATS, NUMBER ONE MAIN TRIM FAIL, THEN CAPTAINS AIRSPEED FAIL WITH NUMEROUS FLAGS, TAKEOFF REJECTED. CLEANED PINS NUMBER, ADC RACK AND ADC CONNECTORS, RERACKED, CHECKED FOR OPERATION PER M/M 34-14-01, ALL CHECKED NORMAL, NO FLAGS.

Part: ENGINE — FAILED (NR 3)

AIR TURNBACK DURING CLIMBOUT, GOT HIGH AVM READING IN EXCESS OF 3.0. BOTH 'A' AND 'B' WITH VIBRATION NOTICED IN FLT CONTROLS. PERFORMED NR 3 ENGINE FAILURE IN FLT SHUTDOWN AT 0705Z. RETURNED TO MIA WITHOUT FURTHER INCIDENT. ENGINE CHANGE IN PROGRESS. CAUSE OF FAILURE TO BE DETERMINED AT SHOP TEARDOWN.