N661AV, cancelled Sep 16, 2013

Service difficulty reports · 222

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N661AV' AND deregistration_id = 'N661AV-2013-09-16'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ARWA20080707Fuel Control · malfunctionedENG NR 1 FAILED TO ACCELERATE BEYOND GROUND IDLE. REMOVED AND REPLACED FUEL CONTROL UNIT AT NR 1 ENG IAW DC8 MM 73-20-1. PERFORMED ENG RUN UP IAW DC8 MM 77-00. FOUND NORMAL. (S)Jul 31, 2008 · N661AV · Doug DC863F · Fuel Control/Turbine EnginesSDR ARWA20080705Gyro · malfunctionedNR 2 COMPASS PROCESSES 10 DEGREES. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO IN ACCORDANCE WITH DC8 M/M 34-21-1; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 M/M 34-21-0. (A)Jul 24, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating SystemSDR ARWA20080304Compass · inoperativeFIRST OFFICER'S COMPASS INOPERATIVE. REMOVED AND REPLACED DIRECTIONAL GYRO NR 2 (DG-2) IN ACCORDANCE WITH M/M 34-21-1 AND RADIO DIRECTION INDICATOR NR 2 (RDI NR 2) IN ACCORDANCE WITH 31-00. COMPASS GROUND TEST NORMAL IN ACCORDANCE WITH M/M 34-21-0; 34-54-0 AMar 23, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating SystemSDR ARWA20070703Bleed Valve · malfunctionedABORTED TAKE-OFF AT 118 KTS, UNABLE TO MAINTAIN TAKEOFF POWER WITHOUT EXCEEDING NR 3 ENGINE EGT LIMIT. REMOVED NR 3 ENGINE SURGE VALVE IN ACCORDANCE WITH M/M 75-30-3. INSTALLED NEW COMPRESSOR BLEED VALVE AND CONTROL IN ACCORDANCE WITH M/M 75-30-3. OPERATIONJul 10, 2007 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA20070607Control Unit · unknownL/F I/B ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH M/M 32-43-1; CHECK GOOD IN ACCORDANCE WITH M/M 32-43-0.Jun 17, 2007 · N661AV · Doug DC863F · Brake Anti-Skid SectionSDR ARWA20070611Access Door · crackedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505C WT OUT WITH 02 CRACKS. REPAIR ACC DOOR NR 505C OF RT WING UPPER SURFACE MAIN FUEL TANK IN ACCORDANCE WITH DRAWING NR AIPSAC - N661AV-02/07, DATED 01-12Jun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA20070610Access Door · crackedDURING "C" CHECK INSPECTIONS, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACCESS DOOR NR 505E CUT OUT WITH CRACK. REPAIRED RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505E CUT OUT IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-02/07 RD, SHJun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA20070609Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 260 L-21L SKIN WITH CORROSION. REPAIRED FUSELAGE EXTERIOR SKIN ATW FS 200 AND FS 350 AND BETWEEN L-18L AND L-24L IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-01/06, REVISION 0, SHEJun 15, 2007 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA20070608Skin · dentedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND LT HORIZONTAL STABILIZER XH 285.00 L/E LOWER SURFACE WITH DENT. REPAIRED L/E PLATING OF LT HORIZONTAL STABILIZER BETWEEN XFS 263 AND XH 285 IN ACCORDANCE WITH AIPSAC DRAWING NR AIPSAC-N661AVE-03/07, SHEET 1Jun 15, 2007 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR ARWA20060705Hinge Fitting · crackedDURING SERVICE CHECK INSPECTION FOUND LEFT WING OUTBOARD FLAP HINGE BASE FITTING AT STATION 219 CRACKED; O/B FITTING. REMOVED LEFT OUTBOARD FLAP ASSEMBLY IAW M/M 27-51-2 FOR REPAIR. PERFORMED WING FLAP SYSTEM ADJUSTMENT AND TEST IN ACCORDANCE DC-8 M/M 27-50-Jul 18, 2006 · N661AV · Doug DC863F · Trailing Edge FlapsSDR ARWA20060401Wire · brokenDURING TAKEOFF ROLL, WARNING HORN SOUNDED. REPAIRED BROKEN WIRE AT SPOILER SWITCH IN ACCORDANCE WITH DC-8 M/M 20-50-0. OPERATIONAL CHECK TAKEOFF WARNING SYSTEM NORMAL IN ACCORDANCE WITH DC-8 M/M 27-63-0.Apr 12, 2006 · N661AV · Doug DC863F · Flight Control System WiringSDR ARWA20051102Blades · damagedUPON ENGINE SPOOL UP FOR TAKEOFF, NR 4 ENGINE COMPRESSOR STALLED. PERFORMED BOROSCOPE TO NR 4 ENGINE; FOUND BLADES DAMAGED, SECURED NR 4 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH ARROW GMM 6-3-4/5.Nov 17, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ARWA20051101Control Cable · damagedDURING PRE-FLIGHT, FOUND RUDDER POWER LEVER STIFF; "RUDDER CONTROL MANUAL" LIGHT REMAINS ILLUMINATED WITH LEVER IN "ON" POSITION. REMOVED AND REPLACED RUDDER SHUT-OFF VALVE CONTROL CABLE RUN NR 67-C IN ACCORDANCE WITH DC8 M/M 27-22-1; RIGGED AND OPERATIONAL CNov 11, 2005 · N661AV · Doug DC863F · Rudder Control SystemSDR ARWA20051004Compressor · stalledLOG PAGE NR 117333, DURING TAKEOFF, NR 2 ENGINE COMPRESSOR STALLED. PERFORM NR 2 ENGINE INLET AND EXHAUST SECTION INSPECTION FOR DAMAGE IAW M/M 71-00 AND PERFORMED OPERATIONAL RUN IAW M/M 71-00; FOUND ALL PARAMETERS IN LIMITS, COULD NOT DUPLICATE FAILURE. NOTOct 22, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ARWA20051005Brake Assy · damagedLOG PAGE NR 117327. NR 2 MAIN WHEEL TIRE BLOWN; NR 2 BRAKE DAMAGED. REMOVED AND REPLACED NR 2 MAIN WHEEL IAW M/M 32-40-1; REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-42-1, NO LEAKS NOTICE.Oct 20, 2005 · N661AV · Doug DC863F · BrakeSDR ARWA20050909Bleed Valve · failedDURING TAKEOFF AT MAX POWER 1.87 GPR BETWEEN 60 AND 80 KNOTS, HAD A LOUD BANG ON NR 2 ENGINE COMPRESSOR N2 INDICATOR SWUNG VIOLENTLY. ABORTED TAKEOFF AND SECURED NR 2 ENGINE WITH APPROPRIATE CHECKLIST. REMOVED AND REPLACED NR 2 SURGE BLEED VALVE ON ENGINE NRSep 10, 2005 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA20050705Wire · damagedAFTER LANDING, FIRE WARNING CAME ON; ENGINE NR 4. COMPLETED APPROPIATE CHECKLIST. REPAIRED WIRING ON NR 4 FIRE WARNING LOOP CONNECTOR (AFT) IN ACCORDANCE WITH M/M 20-50-1. CHECK GOOD IN ACCORDANCE WITH M/M 26-10-0 AND M/M 71-00.Jul 30, 2005 · N661AV · Doug DC863F · Fire DetectionSDR ARWA20050704Fire Loop · chafedNR 4 ENGINE FIRE WARNING ON CLIMB-OUT, MROL SECURED ENGINE IN ACCORDANCE WITH ARROW PROCEDURES "NOTED HIGH OIL TEMPERATURE AFTER SHUTDOWN, OIL PRESSURE 20 PSI IN-CRUISE, 10 PSI ON APPROACH. INSPECTED NR 4 ENGINE; FOUND NR 4 FIRE LOOP CHAFING AGAINST ENGINE COJul 27, 2005 · N661AV · Doug DC863F · Fire DetectionSDR ARWA20050603Transmitter · malfunctionedAT 1845Z NR 1 ENGINE OIL PRESSURE WENT -0- PSI, PERFORMED ABNORMAL CHECKLIST AND ENGINE INFLIGHT SHUTDOWN AT 1848Z. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IN ACCORDANCE WITH M/M 79-32-1; OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 79-32-0Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil PressureSDR ARWA20050602Indicator · defectivePRIOR TO TAKEOFF SPOOLED ALL FOUR ENGINES; NR 1 ENGINE -0- OIL PRESSURE FOLLOWED BY ABNORMAL CHECKLIST. REMOVED AND REPLACED NR 1 OIL PRESSURE INDICATOR IN ACCORDANCE WITH M/M 79-32-0; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 7100 FOUND NORMAL.Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil PressureSDR ARWA20050601Cable · brokenGUST LOCK HARD TO ENGAGE SUSPECT CABLE BROKEN. R & R GUST LOCK CABLE RUNNING NR 79A IN ACCORDANCE WITH DC8 M/M 27-70-0. RIGGED AND OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC8 M/M 27-70-0.Jun 2, 2005 · N661AV · Doug DC863F · Gust Lock Damper SystemSDR ARWA20050502Switch · malfunctionedDOORS NOT LATCHED LIGHT REMAINS ON AFTER GEAR RETRACTED AND UPLATCH CHECK. PERFORMED T/S FOUND RT DOOR LATCHED SW INOP. REMOVED AND REPLACE RT DOOR LATCHED SW IN ACCORDANCE WITH M/M DC8 32-60-0. PERFORMED LANDING GEAR DOOR SWITCH TEST SYSTEM OPERATIONAL CHEMay 5, 2005 · N661AV · Doug DC863F · Landing Gear Door Retract SectionSDR ARWA20050305Link · damagedWHEN FLAPS SELECTED, 10 SPLIT WITH NO CONTROL PROBLEMS. REPLACE FLAP LINK FITTING AT STA 98. OPERATIONAL CHECK SATISFACTORY IN ACCORDANCE WITH DC8 M/M 37-51-41.Mar 31, 2005 · N661AV · Doug DC863F · Trailing Edge Flap Control SystemSDR ARWA20050304Compressor · stalledNR 2 ENGINE COMPRESSOR STALL ON TAKEOFF ABORT AT 30 KNOTS. INSPECTED INLET AND EXHAUST AREA OF ENGINE NR 2; FOUND -PAPER FOD-. REMOVED SMALL RESIDUE IN ACCORDANCE WITH PRATT & WHITNEY 72-00; OPERATIONAL CHECK ON RUN-UP IN ACCORDANCE WITH M/M 71-00. NO COMPRMar 2, 2005 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20050206Smoke Detector · faultyIN FLIGHT MAIN CARGO LIGHT CAME ON. FALSE ALERT; FOUND NR 1 SMOKE DETECTOR AND NR 4 SMOKE DETECTOR LIGHTS REMAINED ILLUMINATED WHILE TESTING. ENTERED ON DMI 19008 AS PER MEL 26-6 CAT-C. RELAMP NR 1 AND NR 4 BEACON LIGHT BULB AT NR 1 AND NR 4 SMOKE DETECTOR;Feb 20, 2005 · N661AV · Doug DC863F · Smoke DetectionSDR ARWA20050101Crank Assy · brokenDURING FLIGHT CONDITION CHECK ON THE ELEVATOR CHECK EPI WILL NOT SATISFACTORY RESPOND TO ELEVATOR INPUTS. RETURN TO BLOCK. ON PARKING CHECK UNABLE TO SET GUST LOCK ON. FOUND RT ELEVATOR GEARED TAB INBOARD DRIVE MECHANISM CRANK ASSEMBLY BROKEN. REMOVED AND Jan 11, 2005 · N661AV · Doug DC863F · Elevator Tab Control SystemSDR ARWA20041201Pump · inoperativePRIOR TO TAKEOFF STANDBY RUDDER PUMP INOPERATIVE. FOUND CURRENT LIMITER FUSE BLOWOUT. REPLACED IN ACCORDANCE WITH MM 27-24-2.Dec 2, 2004 · N661AV · Doug DC863F · Rudder Control SystemSDR ARWA20041006Engine · hung upON APPROACH, NR 4 ENGINE HUNG IN-FLIGHT; PERFORMED EMERGENCY ENGINE HUNG IN FLIGHT CHECKLIST. ENGINE ACCELERATED NORMAL. AFTER LANDING, NR 4 ENGINE SPOOLED DOWN TO 40 PERCENT N2 AND STAYED HUNG. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL. SECURED NR 4 ENGINEOct 26, 2004 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20041003Fuel Control · malfunctionedNR 4 ENGINE SLOW TO SPOOL AT MHLM AND DURING APPROACH ENGINE WOULD NOT ACCELERATE PAST IDLE. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT IN ACCORDANCE WITH MM 73-20-1 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN UP IN ACCORDANCE WITH MM 71-00. NOOct 13, 2004 · N661AV · Doug DC863F · Fuel Control/Turbine EnginesSDR ARWA20040905Wire · brokenNR 2 ENGINE FIRE DETECTION TEST FIRE SHUTOFF LEVER LIGHTS VERY DIM AND C/B POPPED OUT. REPAIRED WIRES OF FIREWALL DISC. BOX ENGINE NR 2 IAW MM 20-50-1. PERFORMED OPERATIONAL CHECK TEST DETECTION SYSTEM IAW M/M 26-10-0, FOUND NORMAL.Sep 30, 2004 · N661AV · Doug DC863F · Fire Protection System WiringSDR ARWA20040903Engine · vibrationNR 2 ENGINE VIBRATES AT 1.2 EPR ON THE GROUND AND IN FLIGHT. REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD DC-8 UN-003. OPERATIONAL CHECK SATISFACTORY.Sep 27, 2004 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20040704Skin Panel · crackedDURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES.Jul 19, 2004 · N661AV · Doug DC863F · Wing, Plate/SkinSDR ARWA20040603Amplifier · failedLOG PAGE NR 107128. CAPTAIN'S HEADING FLAG DISPLAYED INTERMITTENTLY; RETURNED TO RAMP. REMOVED AND REPLACED INSTRUMENT AMP IAW M/M 34-21-0; HORIZON SYSTEM OPERATIONAL NORMAL IAW M/M 34-25-0.Jun 21, 2004 · N661AV · Doug DC863F · Attitude and Direction Data SystemSDR ARWA20031103Axle · damagedRED DOOR NOT LATCHED, LIGHT WOULD NOT GO OUT AFTER MLG RETRACTION. RECYCLED PER ABNORMAL CHECKLIST, NO HELP. RED GEAR NOT LATCHED. LIGHT WOULD NOT GO OUT AFTER GEAR RETRACTION. RECYCLED PER ABNORMAL CHECK LIST, NO HELP. UPON INSPECTION OF MLG FOUND NR 7 WHNov 15, 2003 · N661AV · Doug DC863F · Main Landing Gear Strut/Axle/TruckSDR ARWA20030910Structure · brokenDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON EDGE BROKEN, AFT OF LT FORWARD MOUNT.Sep 15, 2003 · N661AV · Doug DC863F · Nacelle/Pylon, Main FrameSDR ARWA20030909Structure · crackedDURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON WITH CRACK, AFT OF RT FORWARD MOUNT.Sep 15, 2003 · N661AV · Doug DC863F · Nacelle/Pylon, Main FrameSDR ARWA20030709Cylinder · inoperativeAFTER LANDING, LOST ALL HYDRAULIC FLUIDS. FOUND RT BOGIE TRIM CYLINDER IAW MM 32-33-1 ALTERNATE METHOD. OPERATIONAL CHECK NORMAL.Jul 31, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ARWA20030606Pin · damagedON WALK-AROUND FOUND LT MAIN LANDING GEAR EYEBOLT ACTUATOR WITH EXCESSIVE GAP AT PIN BOSS ATTACHMENT. REMOVED LT MAIN LANDING GEAR ROUTED TO SHOP FOR ACTUATOR PIN REPLACEMENT, REINSTALLED SERVICIABLE MAIN LANDING GEAR IAW MM 32-11-0, OPERATIONAL LEAK CHECK OKJun 25, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ARWA20030404Fuel Control · malfunctionedNR 4 ENGINE HUNG START IN SKGO, SLOW TO SPOOL ON GROUND AND SLOW TO SPOOL IN FLIGHT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT (FCU) IAW DC-8 MM 73-20-1. LEAK CHECK OK. OPERATIONAL CHECK PERFORMED IAW MM 71-00 ON RUN UP FOUND NORMAL.Apr 13, 2003 · N661AV · Doug DC863F · Fuel Control/Reciprocating EnginesSDR ARWA20020913Line · loosePRECAUTIONARY SHUTDOWN NR 1 ENGINE. OIL QUANTITY DECREASING, OIL PRESSURE FLUCTUATING, OIL TEMPERATURE RISING AT 1215Z WINDMILL OIL PRESSURE 15 PSI. REMOVED AND REPLACED NR 1 ENGINE MAIN OIL FILTER ELEMENT IAW P&W MM 72-0 PG 424A.B FIGURE 40B. INSPECTED REMSep 12, 2002 · N661AV · Doug DC863F · Engine Oil Distribution (Airframe Furnished)SDR ARWA20020811Bleed Valve · malfunctionedWHILE SPOOLING ENGINES FOR TAKEOFF, NR 3 ENGINE MADE A LOUD NOISE AT 1.1 EPR 80 PERCENT N2 BLEEDS OFF. REMOVED AND REPLACED PRESSURE RATIO BLEED CONTROL IAW DC-8 MM 75-30-0. CHECKED ENGINE RUN UP NORMAL IAW 71-00.Aug 31, 2002 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA20020808Cylinder · crackedDURING DAILY INSPECTION FOUND RIGHT HAND CYLINDER CRACKED AT LOWER OUTBOARD SIDE. REMOVED AND REPLACED RT MLG STRUT ASSEMBLY. OPERATIONAL CHECK NORMAL.Aug 27, 2002 · N661AV · Doug DC863F · Main Landing Gear Strut/Axle/TruckSDR ARWA20020806Spar · crackedDURING C-CHECK, LEFT WING FRONT LOWER SPAR WITH CRACKS, STA XFS 526.7 (0.125 INCH) AND STA XFS 518 (1.25 INCH). ACCOMPLISHED REPAIR OF LEFT WING FRONT SPAR LOWER OUTBOARD CAP IAW RED SKETCH 02-07-11-001 SHEET 1 TO 6. BOEING MESSAGE ARW-MIA-02-00016H. THIS RJul 5, 2002 · N661AV · Doug DC863F · Wing SparSDR ARWA20020805Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD UPPER LEFT SIDE WITH 0.125 INCH, 0.050 INCH, 0.375 INCH, & 0.580 INCH CRACKS, STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, DOUBLER AND FINGER DOUBLER IAW DRAWING SRO8530007; INSTALLED PARTS IAW DRAWING SRO8530007.Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, BulkheadSDR ARWA20020804Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD UPPER RIGHT SIDE WITH 1.5 INCH CRACK STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, FINGER DOUBLER AND DOUBLER IAW DRAWING SR08530007; INSTALLED PARTS IAW DRAWING SR08530007.Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, BulkheadSDR ARWA20020509Mount · brokenDURING A-CHECK AT MIA THE FOLLOWING WAS FOUND, NR 4 ENGINE AFT MOUNT BROKEN. REPLACED FORWARD LT, FORWARD RT AND AFT ENGINE MOUNT ASSEMBLY IAW MM 71-20-2. AFT MOUNT SENT OUT FOR ANALYSIS.May 29, 2002 · N661AV · Doug DC863F · Engine Mount SectionSDR ARWA20020401Cylinder · leakingAFTER LANDING, LOSS OF HYD PRESSURE WITH LOW PRESSURE LIGHT, AILERON & RUDDER POWER LIGHTS ON, QUANTITY NORMAL. ACFT WAS STOPPED ON THE TAXIWAY & TOWED TO THE RAMP. REMOVED AND REPLACED RIGHT HAND MLG BOGIE TRIM CYLINDER ASSY IAW MM 32-33-1. LEAK CHECK ACCOApr 2, 2002 · N661AV · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ARWA20020113SensorLOG PAGE 107160. DISCREPANCY: #4 ENGINE OIL TEMP @ 150 @ 15 MINUTES ENGINE SHUT DOWN AS PER AOM. AIRCRAFT RETURNED TO KMIA AND LANDED OVERWEIGHT UNEVENTFUL. CORRECTIVE ACTION: TROUBLESHOOTING INDICATED OPENED RESISTANCE AT TEMP BULB. REMOVED AND REPLACED #4 ENJan 20, 2002 · N661AV · Doug DC863F · Engine Oil TemperatureSDR ARWA20020112Wire · damagedDURING CLIMB NR 2 ENGINE OIL TEMP INDICATION READ 150. SWAPPED GAUGES FOR TROUBLESHOOTING, NO HELP. AFTER RETARDING NR 2 POWER LEVER, OIL TEMPERATURE DECREASED, ADVANCE POWER LEVER, TEMPERATURE INCREASED. NEVER EXCEEDED THE 15 MINUTES LIMIT. AIRCRAFT RETURJan 18, 2002 · N661AV · Doug DC863F · Engine Oil System WiringSDR ARWA20011206Engine · failedAPPROX 200 MILES OUT OF BAHRAIN AT FL 330 NR 4 ENGINE COMPRESSOR STALLED IN CLEAR WEATHER, FOLLOWED BY DROP IN EPR FROM 1.65 TO 1.15. ALL OTHER PARAMETERS NORMAL, ABOVE 85 PERCENT N2 ENGINE SURGES. AIRCRAFT LANDED WITHOUT INCIDENTS. POST FLIGHT INSPECTION RDec 12, 2001 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)
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