# Service difficulty reports: N661AV, cancelled Sep 16, 2013

A list on [N661AV, cancelled Sep 16, 2013](https://openairdocs.org/deregistered/N661AV-2013-09-16.md).

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

Page 1 of 5 · 222 reports

- [SDR ARWA20080707](https://openairdocs.org/sdr/ARWA20080707.md): Fuel Control · malfunctioned · Jul 31, 2008 · N661AV · Doug DC863F · Fuel Control/Turbine Engines
  > ENG 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)
- [SDR ARWA20080705](https://openairdocs.org/sdr/ARWA20080705.md): Gyro · malfunctioned · Jul 24, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating System
  > NR 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)
- [SDR ARWA20080304](https://openairdocs.org/sdr/ARWA20080304.md): Compass · inoperative · Mar 23, 2008 · N661AV · Doug DC863F · Directional Gyro and Indicating System
  > FIRST 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 A
- [SDR ARWA20070703](https://openairdocs.org/sdr/ARWA20070703.md): Bleed Valve · malfunctioned · Jul 10, 2007 · N661AV · Doug DC863F · Compressor Bleed Valve
  > ABORTED 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. OPERATION
- [SDR ARWA20070607](https://openairdocs.org/sdr/ARWA20070607.md): Control Unit · unknown · Jun 17, 2007 · N661AV · Doug DC863F · Brake Anti-Skid Section
  > L/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.
- [SDR ARWA20070611](https://openairdocs.org/sdr/ARWA20070611.md): Access Door · cracked · Jun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING "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 01-12
- [SDR ARWA20070610](https://openairdocs.org/sdr/ARWA20070610.md): Access Door · cracked · Jun 15, 2007 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING "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, SH
- [SDR ARWA20070609](https://openairdocs.org/sdr/ARWA20070609.md): Skin · corroded · Jun 15, 2007 · N661AV · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "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, SHE
- [SDR ARWA20070608](https://openairdocs.org/sdr/ARWA20070608.md): Skin · dented · Jun 15, 2007 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/Skin
  > DURING "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 1
- [SDR ARWA20060705](https://openairdocs.org/sdr/ARWA20060705.md): Hinge Fitting · cracked · Jul 18, 2006 · N661AV · Doug DC863F · Trailing Edge Flaps
  > DURING 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-
- [SDR ARWA20060401](https://openairdocs.org/sdr/ARWA20060401.md): Wire · broken · Apr 12, 2006 · N661AV · Doug DC863F · Flight Control System Wiring
  > DURING 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.
- [SDR ARWA20051102](https://openairdocs.org/sdr/ARWA20051102.md): Blades · damaged · Nov 17, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor Section
  > UPON 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.
- [SDR ARWA20051101](https://openairdocs.org/sdr/ARWA20051101.md): Control Cable · damaged · Nov 11, 2005 · N661AV · Doug DC863F · Rudder Control System
  > DURING 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 C
- [SDR ARWA20051004](https://openairdocs.org/sdr/ARWA20051004.md): Compressor · stalled · Oct 22, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor Section
  > LOG 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. NOT
- [SDR ARWA20051005](https://openairdocs.org/sdr/ARWA20051005.md): Brake Assy · damaged · Oct 20, 2005 · N661AV · Doug DC863F · Brake
  > LOG 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.
- [SDR ARWA20050909](https://openairdocs.org/sdr/ARWA20050909.md): Bleed Valve · failed · Sep 10, 2005 · N661AV · Doug DC863F · Compressor Bleed Valve
  > DURING 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 NR
- [SDR ARWA20050705](https://openairdocs.org/sdr/ARWA20050705.md): Wire · damaged · Jul 30, 2005 · N661AV · Doug DC863F · Fire Detection
  > AFTER 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.
- [SDR ARWA20050704](https://openairdocs.org/sdr/ARWA20050704.md): Fire Loop · chafed · Jul 27, 2005 · N661AV · Doug DC863F · Fire Detection
  > NR 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 CO
- [SDR ARWA20050603](https://openairdocs.org/sdr/ARWA20050603.md): Transmitter · malfunctioned · Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil Pressure
  > AT 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 79-32-0
- [SDR ARWA20050602](https://openairdocs.org/sdr/ARWA20050602.md): Indicator · defective · Jun 7, 2005 · N661AV · Doug DC863F · Engine Oil Pressure
  > PRIOR 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.
- [SDR ARWA20050601](https://openairdocs.org/sdr/ARWA20050601.md): Cable · broken · Jun 2, 2005 · N661AV · Doug DC863F · Gust Lock Damper System
  > GUST 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.
- [SDR ARWA20050502](https://openairdocs.org/sdr/ARWA20050502.md): Switch · malfunctioned · May 5, 2005 · N661AV · Doug DC863F · Landing Gear Door Retract Section
  > DOORS 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 CHE
- [SDR ARWA20050305](https://openairdocs.org/sdr/ARWA20050305.md): Link · damaged · Mar 31, 2005 · N661AV · Doug DC863F · Trailing Edge Flap Control System
  > WHEN 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.
- [SDR ARWA20050304](https://openairdocs.org/sdr/ARWA20050304.md): Compressor · stalled · Mar 2, 2005 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)
  > NR 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 COMPR
- [SDR ARWA20050206](https://openairdocs.org/sdr/ARWA20050206.md): Smoke Detector · faulty · Feb 20, 2005 · N661AV · Doug DC863F · Smoke Detection
  > IN 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;
- [SDR ARWA20050101](https://openairdocs.org/sdr/ARWA20050101.md): Crank Assy · broken · Jan 11, 2005 · N661AV · Doug DC863F · Elevator Tab Control System
  > DURING 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
- [SDR ARWA20041201](https://openairdocs.org/sdr/ARWA20041201.md): Pump · inoperative · Dec 2, 2004 · N661AV · Doug DC863F · Rudder Control System
  > PRIOR TO TAKEOFF STANDBY RUDDER PUMP INOPERATIVE. FOUND CURRENT LIMITER FUSE BLOWOUT. REPLACED IN ACCORDANCE WITH MM 27-24-2.
- [SDR ARWA20041006](https://openairdocs.org/sdr/ARWA20041006.md): Engine · hung up · Oct 26, 2004 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)
  > ON 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 ENGINE
- [SDR ARWA20041003](https://openairdocs.org/sdr/ARWA20041003.md): Fuel Control · malfunctioned · Oct 13, 2004 · N661AV · Doug DC863F · Fuel Control/Turbine Engines
  > NR 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. NO
- [SDR ARWA20040905](https://openairdocs.org/sdr/ARWA20040905.md): Wire · broken · Sep 30, 2004 · N661AV · Doug DC863F · Fire Protection System Wiring
  > NR 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.
- [SDR ARWA20040903](https://openairdocs.org/sdr/ARWA20040903.md): Engine · vibration · Sep 27, 2004 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)
  > NR 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.
- [SDR ARWA20040704](https://openairdocs.org/sdr/ARWA20040704.md): Skin Panel · cracked · Jul 19, 2004 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES.
- [SDR ARWA20040603](https://openairdocs.org/sdr/ARWA20040603.md): Amplifier · failed · Jun 21, 2004 · N661AV · Doug DC863F · Attitude and Direction Data System
  > LOG 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.
- [SDR ARWA20031103](https://openairdocs.org/sdr/ARWA20031103.md): Axle · damaged · Nov 15, 2003 · N661AV · Doug DC863F · Main Landing Gear Strut/Axle/Truck
  > RED 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 WH
- [SDR ARWA20030910](https://openairdocs.org/sdr/ARWA20030910.md): Structure · broken · Sep 15, 2003 · N661AV · Doug DC863F · Nacelle/Pylon, Main Frame
  > DURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON EDGE BROKEN, AFT OF LT FORWARD MOUNT.
- [SDR ARWA20030909](https://openairdocs.org/sdr/ARWA20030909.md): Structure · cracked · Sep 15, 2003 · N661AV · Doug DC863F · Nacelle/Pylon, Main Frame
  > DURING AN A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 1 PYLON WITH CRACK, AFT OF RT FORWARD MOUNT.
- [SDR ARWA20030709](https://openairdocs.org/sdr/ARWA20030709.md): Cylinder · inoperative · Jul 31, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension System
  > AFTER LANDING, LOST ALL HYDRAULIC FLUIDS. FOUND RT BOGIE TRIM CYLINDER IAW MM 32-33-1 ALTERNATE METHOD. OPERATIONAL CHECK NORMAL.
- [SDR ARWA20030606](https://openairdocs.org/sdr/ARWA20030606.md): Pin · damaged · Jun 25, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension System
  > ON 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 OK
- [SDR ARWA20030404](https://openairdocs.org/sdr/ARWA20030404.md): Fuel Control · malfunctioned · Apr 13, 2003 · N661AV · Doug DC863F · Fuel Control/Reciprocating Engines
  > NR 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.
- [SDR ARWA20020913](https://openairdocs.org/sdr/ARWA20020913.md): Line · loose · Sep 12, 2002 · N661AV · Doug DC863F · Engine Oil Distribution (Airframe Furnished)
  > PRECAUTIONARY 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 REM
- [SDR ARWA20020811](https://openairdocs.org/sdr/ARWA20020811.md): Bleed Valve · malfunctioned · Aug 31, 2002 · N661AV · Doug DC863F · Compressor Bleed Valve
  > WHILE 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.
- [SDR ARWA20020808](https://openairdocs.org/sdr/ARWA20020808.md): Cylinder · cracked · Aug 27, 2002 · N661AV · Doug DC863F · Main Landing Gear Strut/Axle/Truck
  > DURING DAILY INSPECTION FOUND RIGHT HAND CYLINDER CRACKED AT LOWER OUTBOARD SIDE. REMOVED AND REPLACED RT MLG STRUT ASSEMBLY. OPERATIONAL CHECK NORMAL.
- [SDR ARWA20020806](https://openairdocs.org/sdr/ARWA20020806.md): Spar · cracked · Jul 5, 2002 · N661AV · Doug DC863F · Wing Spar
  > DURING 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 R
- [SDR ARWA20020805](https://openairdocs.org/sdr/ARWA20020805.md): Bulkhead · cracked · Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR ARWA20020804](https://openairdocs.org/sdr/ARWA20020804.md): Bulkhead · cracked · Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR ARWA20020509](https://openairdocs.org/sdr/ARWA20020509.md): Mount · broken · May 29, 2002 · N661AV · Doug DC863F · Engine Mount Section
  > DURING 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.
- [SDR ARWA20020401](https://openairdocs.org/sdr/ARWA20020401.md): Cylinder · leaking · Apr 2, 2002 · N661AV · Doug DC863F · Landing Gear Retraction/Extension System
  > AFTER 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 ACCO
- [SDR ARWA20020113](https://openairdocs.org/sdr/ARWA20020113.md): Sensor · Jan 20, 2002 · N661AV · Doug DC863F · Engine Oil Temperature
  > LOG 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 EN
- [SDR ARWA20020112](https://openairdocs.org/sdr/ARWA20020112.md): Wire · damaged · Jan 18, 2002 · N661AV · Doug DC863F · Engine Oil System Wiring
  > DURING 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 RETUR
- [SDR ARWA20011206](https://openairdocs.org/sdr/ARWA20011206.md): Engine · failed · Dec 12, 2001 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)
  > APPROX 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 R

Next page: https://openairdocs.org/deregistered/N661AV-2013-09-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N661AV-2013-09-16/reports

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