# Service difficulty reports: N906R, cancelled Dec 27, 2016

A list on [N906R, cancelled Dec 27, 2016](https://openairdocs.org/deregistered/N906R-2016-12-27.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 2 · 53 reports

- [SDR ARWA20060704](https://openairdocs.org/sdr/ARWA20060704.md): Hinge Fitting · cracked · Jul 8, 2006 · N906R · Doug DC863F · Trailing Edge Flaps
  > DURING DAILY CHECK INSPECTION THE FOLLOWING WAS FOUND; LT OUTBOARD WING FLAP STATION XW 219, LT HINGE BASE FITTING CRACK. REMOVED LEFT O/B WING FLAP ASSEMBLY IN ACCORDANCE WITH M/M 27-51-2. INSTALLED LT OUTBOARD WING FLAP ASSY IN ACCORDANCE WITH M/M 27-51-2.
- [SDR ARWA20060203](https://openairdocs.org/sdr/ARWA20060203.md): Connector · dirty · Feb 15, 2006 · N906R · Doug DC863F · Hydraulic Power System Wiring
  > BLOCK TURNBACK PRIOR TO TAKEOFF DUE TO HYDRAULIC QUANTITY LOSS. CHECKED HYDRAULIC RESERVOIR, FOUND FULL; CLEANED CONNECTOR AT HYDRAULIC QUANTITY TRANSMITTER IN ACCORDANCE WITH M/M 20-50-1; CHECKED HYDRAULIC QUANTITY, FOUND NORMAL READING.
- [SDR ARWA20050606](https://openairdocs.org/sdr/ARWA20050606.md): Seal · open · Jun 16, 2005 · N906R · Doug DC863F · Passenger/Crew Doors
  > UNABLE TO CONTROL PRESSURIZATION DURING CLIMB. PERFORMED AIR TURNBACK - OVERWEIGHT LANDING INTO KMIA WITHOUT ANY FURTHER INCIDENTS. PRESSURIZED AIRCRAFT AND FOUND CABIN ENTRANCE DOOR ANGLE-SEAL UPPER AND LOWER RETAINER PARTIALLY OPEN, LUBE CABIN SEAL IN ACC
- [SDR ARWA20050605](https://openairdocs.org/sdr/ARWA20050605.md): Control Cable · broken · Jun 15, 2005 · N906R · Doug DC863F · Rudder Control System
  > ON PRE-FLIGHT RUDDER CONTROL LIGHT OFF WITH AUXILIARY HYDRAULIC PUMP ON AND RUDDER POWER LEVER OFF POSITION. FOUND RUDDER HYDRAULIC SHUT-OFF CABLE BROKEN. REMOVED AND REPLACED CONTROL CABLE IN ACCORDANCE WITH M/M 20-17-0 AND 91-10-0; OPERATIONAL CHECK NORMAL
- [SDR ARWA20050403](https://openairdocs.org/sdr/ARWA20050403.md): Control Panel · failed · Apr 12, 2005 · N906R · Doug DC863F · AC Generator-Alternator
  > ON TAXI OUT, NR 4 GENERATOR TRIPPED OFF. REMOVED AND REPLACED GCU IN ACCORDANCE WITH M/M 24-20-5. REMOVED AND REPLACE BUSS PROTECTION PROTECTION PANEL IN ACCORDANCE WITH 24-20-7. REMOVED AND REPLACED FREQUENCY LOAD CONTROLLER IN ACCORDANCE WITH M/M 24-10-16.
- [SDR ARWA20050503](https://openairdocs.org/sdr/ARWA20050503.md): Generator · tripped · Apr 12, 2005 · N906R · Doug DC863F · AC Generator-Alternator
  > ON TAXI OUT, NR 4 GENERATOR TRIPPED OFF.
- [SDR ARWA20050303](https://openairdocs.org/sdr/ARWA20050303.md): Resistor · failed · Mar 22, 2005 · N906R · Doug DC863F · Cabin Pressure Control System
  > ON TOP OF CLIMB, A BURNING ODOR & SMOKE APPEARED IN COCKPIT, REPEATEDLY PERFORMED APPROPRIATE CHECKLIST; PERFORMED FUEL DUMPING PER ABNORMAL CHECKLIST; PULLED CUR. C/B PER EMERGENCY CHECKLIST. SMOKE SOURCE IDENTIFIED AT LOW BLOW FAN RESISTOR "COCKPIT CLIMAT
- [SDR ARWA20050302](https://openairdocs.org/sdr/ARWA20050302.md): Wire · damaged · Mar 18, 2005 · N906R · Doug DC863F · Flight Control System Wiring
  > WING SLOT LIGHT DID NOT COME ON. REPAIR WIRES 2F MAIN CONNECTOR P1-10 IN ACCORDANCE WITH M/M 20-50-1. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 27-52-3.
- [SDR ARWA20050205](https://openairdocs.org/sdr/ARWA20050205.md): Line · leaking · Feb 13, 2005 · N906R · Doug DC863F · Hydraulic System, Main
  > AFTER LANDING LOST HYDRAULIC PRESSURE; QUANTITY DOWN TO AUX LEVEL. REMOVED AND REPLACED BOGIE TRIM CYLINDER (BTC) HYDRAULIC LINE AS PER MM 32-33-1. LEAK CHECK OK, NO LEAKS NOTED.
- [SDR ARWA20050203](https://openairdocs.org/sdr/ARWA20050203.md): Pressure Switch · failed · Feb 10, 2005 · N906R · Doug DC863F · Engine Oil Pressure
  > ON CLIMBOUT FROM MIAMI, NR 1 ENGINE OIL LIGHT ILLUMINATED, PERFORMED ABNORMAL OIL PRESSURE LIGHT ILLUMINATED CHECKLIST. LIGHT REMAINED ON. SHUTDOWN ENGINE NR 1. ALL OTHER INDICATIONS WERE NORMAL. RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR
- [SDR ARWA20050201](https://openairdocs.org/sdr/ARWA20050201.md): Fuel Control · failed · Feb 2, 2005 · N906R · Doug DC863F · Fuel Control/Turbine Engines
  > ON TAKEOFF, LOSS ENGINE OIL PRESSURE PRIOR TO V-1 ABORTED TAKEOFF; ALSO NOTICED COMPRESSOR STALLED. TROUBLESHOOTING FOUND NR 4 ENGINE FUEL CONTROL UNIT (FCU) LEAKING. REMOVED AND REPLACED FUEL CONTROL UNIT IN ACCORDANCE WITH MM 73-20-1. OPERATIONAL CHECK FO
- [SDR ARWA20040907](https://openairdocs.org/sdr/ARWA20040907.md): Skin · corroded · Sep 28, 2004 · N906R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; DISCREPANCY: FORWARD LOWER CARGO COMPARTMENT STA 230 BETWEEN LONG. 36 AND LONG 35R, SKIN WITH CORROSION.
- [SDR ARWA20040906](https://openairdocs.org/sdr/ARWA20040906.md): Skin · cracked · Sep 28, 2004 · N906R · Doug DC863F · Wing, Plate/Skin
  > DURING A "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND, RT WING INBOARD L/E LOWER SECTION STA XCW 69 OUTER PLATING AND INNER DOUBLER WITH 3 INCH CRACK.
- [SDR ARWA20040807](https://openairdocs.org/sdr/ARWA20040807.md): Buss Cable · broken · Aug 31, 2004 · N906R · Doug DC863F · Flight Control System Wiring
  > UPON INSPECTION, FOUND LT (LT) AILERON BUS CABLE BROKEN. ALSO FOUND LT AILERON BUS CABLE CRANK PULLEYS WORN. REMOVED DAMAGE CABLE AS REQUIRE IAW MM 27-10-0. FABRICATED NEW CABLE IAW SAMPLE IAW MM 91-10-12. INSTALLED NEW CABLE, ADJUSTMENT AND TEST FOUND NORM
- [SDR ARWA20040602](https://openairdocs.org/sdr/ARWA20040602.md): Indicator · erratic · Jun 19, 2004 · N906R · Doug DC863F · Engine Pressure Ratio (EPR)
  > LOG PAGE NR 107344, AFTER ALL ENGINES SPOOLED AND TAKEOFF STARTED NR 1 EPR (ENGINE PRESSURE RATIO) ERRATIC; DISCONTINUED TAKEOFF AND TAXIED BACK TO RAMP. TRANSFERRED TO DMI NR 18568 IAW MM. AIRCRAFT RELEASED IAW MEL NR 77-1-2 CAT (A). REMOVED AND REPLACED NR
- [SDR ARWA20040601](https://openairdocs.org/sdr/ARWA20040601.md): Amplifier · malfunctioned · Jun 9, 2004 · N906R · Doug DC863F · Fire Detection
  > DURING TAXI, NR 2 ENGINE FIRE WARNING INTERMITENTLY ILLUMINATED FIRE WARNING TEST INOPERATIVE, SHUT DOWN ENGINE; RETURNED TO RAMP. NO FIRE NOTED. CHECK FIRE WARNING SYSTEM AT RUNUP CONDITION. CHECK WIRING FOR CONDITION, ELEMENTS FOR CONDITION AT NR 2 ENGIN
- [SDR ARWA20040509](https://openairdocs.org/sdr/ARWA20040509.md): Structure · corroded · May 19, 2004 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STA -12.000 SUBFLOOR WITH CORROSION, RBL 50. CLEANED UP CORROSION, TREATED AND PRIMED AREA IN ACCORDANCE WITH DC8 SRM 51-1-8. REPAIR COCKPIT BETWEEN STA 12 & RBL 49 SUBFLOOR WAS ACCOMPLISHED IAW A
- [SDR ARWA20040508](https://openairdocs.org/sdr/ARWA20040508.md): Pressure Panel · corroded · May 19, 2004 · N906R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STATION 12.000 AND STA 8.000 SUBFLOOR WAS FOUND WITH CORROSION, RBL 60. REPAIRED FUSELAGE NOSE FLOOR PRESSURE PANEL BETWEEN -12 TO FS 8 AND L22L IAW ELEVEN INC DRAWING AS11566 SHEET 1 THRU 4, DATED
- [SDR ARWA20040505](https://openairdocs.org/sdr/ARWA20040505.md): Blade · damaged · May 13, 2004 · N906R · Doug DC863F · Turbine Section
  > NR 2 ENGINE EGT (EXHAUST GAS TEMPERATURE) IS 40 DEGREES HIGHER THAN OTHER ENGINES IN CRUISE. ALL OTHER PARAMETERS NORMAL. ON POST-FLIGHT INSPECTION, NR 2 ENGINE APPEARS TO HAVE T4 BLADES DAMAGED. UPON INSPECTION, NR 2 ENGINE TURBINE 1ST STAGE (T-1) VANE BLA
- [SDR ARWA20040401](https://openairdocs.org/sdr/ARWA20040401.md): Bleed Valve · surges · Apr 17, 2004 · N906R · Doug DC863F · Compressor Bleed Valve
  > ON TAKEOFF ROLL NR 3 ENGINE EPR INDICATOR SUDDENLY INCREASED TO 2.02 UNITS AFTER ALL ENGINES HAD BEEN SPOOLED AND STABLE AND ALL POWER LEVERS ALIGNED. EGT ALSO INCREASED TO MAX TAKEOFF LIMITS. ABORTED TAKEOFF AT 80 KIAS AND REJECTED TAKEOFF CHECKLIST WAS ACCO
- [SDR ARWA20040102](https://openairdocs.org/sdr/ARWA20040102.md): Door Frame · cracked · Jan 13, 2004 · N906R · Doug DC863F · Fuselage Main, Structure
  > DURING AN A-CHECK INSPECTION, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB TOP FORWARD CORNER WITH CRACK STA 1440.000. TRIMMED OUT CRACK & FABRICATED FILLER, DOUBLER AND TRIPLER IAW DC8SRM 53-2-0, TR 53-188 AND SRM 51-1-21, 51-1-20D & 51-1-11.
- [SDR ARWA20040101](https://openairdocs.org/sdr/ARWA20040101.md): Skin · damaged · Jan 12, 2004 · N906R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND, FUSELAGE EXTERIOR STA 1690 BETWEEN L-35R AND L-36 SKIN BROKEN, NEAR BUTT JOINT. PERFORMED REPAIR OF THE SKIN NEAR BUTT JOINT AT STA 1690, BTW LONGERON 35R & 36R IAW DC8SRM 53-2-1, FIG8, SHEET 1,2, PAGES 123/
- [SDR ARWA20031206](https://openairdocs.org/sdr/ARWA20031206.md): Connector · damaged · Dec 18, 2003 · N906R · Doug DC863F · Fire Detection
  > MASTER FIRE WARNING ILLUMINATED NR 2 FIRE SHUTOFF LEVER LIGHT ON, DISCHARGED BOTH FIRE BOTTLES. THREE ENGINE APPROACH AND LANDING WAS COMPLETED. DURING TROUBLESHOOTING FOUND NR 2 ENGINE FIRE WARNING CONNECTION P1-136 DAMAGE. REMOVED AND REPAIR CONNECTION IA
- [SDR ARWA20030502](https://openairdocs.org/sdr/ARWA20030502.md): Pressure Switch · failed · May 12, 2003 · N906R · Doug DC863F · Engine Oil Indicating System
  > NR 1 ENGINE LOST OIL QTUANTITY. ENGINE WAS SHUT DOWN. AIRCRAFT LANDED IN KMIA WITHOUT INCIDENTS. FOUND NR 1 ENGINE OIL PRESS DIFFERENTIAL SWITCH LEAKING. REMOVED AND REPLACED SWITCH IAW DC8 MM 79-31-06. PERFORMED ENGINE RUN UP AND OPS CK IAW DC8 MM 71-00 FOU
- [SDR ARWA20021107](https://openairdocs.org/sdr/ARWA20021107.md): Accumulator · Nov 18, 2002 · N906R · Doug DC863F · Hydraulic Power Accumulator, Main
  > LOG PAGE # 502922. DISCREPANCY: ON CLIMB OUT OF MIA AT 8.0, OBSERVED QUANTITY DROPPED TO STAND PIPE WITH RESERVE LOW AND AILERON AND RUDDER REVERSION LITES ON; EMERGENCY CHECK LIST ACCOMPLISHED, FUEL DUMPED TO MAX LANDING WEIGHT PER ABN CHECK LIST. CORREC
- [SDR ARWA20021008](https://openairdocs.org/sdr/ARWA20021008.md): Fuse · melted · Oct 23, 2002 · N906R · Doug DC863F · Landing Gear Brake System
  > DURING POST FLIGHT INSPECTION THE FOLLOWING WAS FOUND: NR 3, 4 & 8 MWA THERMAL FUSE MELTED; NR 7 MWA DUE CHANGE FROM STRESS BEYOND LIMITS. FOUND CRACK AT NR 3 & 4 BRAKE ASSY. DURING MWA; FOUND NR 8 BRAKE ASSY. SEVERLY OVERHEATED AT MWA. FOUND NR 7 & 6 BRA
- [SDR ARWA20021003](https://openairdocs.org/sdr/ARWA20021003.md): Indicator · sticking · Oct 8, 2002 · N906R · Doug DC863F · Airspeed/Mach Indicator
  > ON TAKEOFF ROLL OUT OF MIAMI, FIRST OFFICERS AIRSPEED INDICATOR STUCK AT 70 KNOTS. CAPTAINS INDICATOR 95 KNOTS. ABORTED TAKEOFF, RETURNED TO RAMP FOR CORRECTIVE ACTION. REMOVED & REPLACE WITH NEW PART, FIRST OFFICERS AIRSPEED INDICATOR. ALL WORK ACCOMPLISH
- [SDR IXXA0000030](https://openairdocs.org/sdr/IXXA0000030.md): Pin · sheared · Aug 17, 2000 · N906R · Doug DC863F · Landing Gear Retraction/Extension System
  > DURING POST FLIGHT INSPECTION IN OMA, THE FLIGHT ENGINEER FOUND THAT THE RIGHT MAIN LANDING GEAR RETRACT PIN SHEARED. THE AIRCRAFT WAS FERRIED FOR REPAIRS IN ACCORDANCE WITH COMPANY PROCEDURES. MAINTENANCE REPLACED THE RETRACT PIN IN ACCORDANCE WITH MAINTENA
- [SDR IXXA0000014](https://openairdocs.org/sdr/IXXA0000014.md): Fan · defective · Apr 10, 2000 · N906R · Doug DC863F · Air Distribution Fan
  > EN ROUTE FROM DWI TO NSY, WHEN THE FLIGHT CREW OPERATED THE CENTER RECIRCULATION FAN, AN ODOR WAS SENSED IN THE COCKPIT. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO NSY FOR AN UNEVENTFUL LANDING. A COMPANY REPERSENTATIVE I
- [SDR IAAX0000002](https://openairdocs.org/sdr/IAAX0000002.md): Actuator · malfunctioned · Jan 19, 2000 · N906R · Doug DC863F · Landing Gear Actuator
  > RMS - FLT DQ1 - EN ROUTE FROM CAI TO RMS, THE GEAR DOOR WARNING LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK.. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUES TO RMS FOR AN UNEVENTFUL LAND
- [SDR IXXA9900029](https://openairdocs.org/sdr/IXXA9900029.md): Switch · corroded · Oct 28, 1999 · N906R · Doug DC863F · Landing Gear Position and Warning
  > DURING APPROACH INTO TOL, AFTER THE LANDING GEAR WAS EXTENDED THE LEFT MAIN GEAR DOWN AND LOCK INDICATION LIGHT FAILED TO ILLUMINATE. THE FLIGHT CREW CYCLED THE LANDING GEAR SEVERAL TIMES BEFORE THE DOWN AND LOCK LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE LA
- [SDR IXXA9900027](https://openairdocs.org/sdr/IXXA9900027.md): Striker · loose · Oct 23, 1999 · N906R · Doug DC863F · Landing Gear Position and Warning
  > EN ROUTE FROM TOL TO CLT, AFTER GEAR RETRACTION, THE GEAR NOT LATCH LIGHT ILLUMINATED ACCOMPANIED BY AN ALTERNATE RIGHT MAIN GEAR DOOR WARNING LIGHT. THE FLIGHT CREW CYCLED THE GEAR, THE GEAR NOT LATCH LIGHT REMAINED ILLUMINATED AND THE ALTERNATE GEAR DOOR
- [SDR IXXA9800059](https://openairdocs.org/sdr/IXXA9800059.md): Wire · chafed · Jun 24, 1998 · N906R · Doug DC863F · Landing Gear System Wiring
  > EN ROUTE MGUM TO KFLL, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO KFLL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED T
- [SDR IXXA9700087](https://openairdocs.org/sdr/IXXA9700087.md): Plating · cracked · May 21, 1997 · N906R · Doug DC863F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, A TWO INCH CRACK WAS FOUND ON THE RIGHT WING LEADING EDGE PLATING AT STATION XFS376.000. REPAIR ACCOMPLISHED STOP DRILLING ENDS OF THE CRACK, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRA
- [SDR IXXA9700096](https://openairdocs.org/sdr/IXXA9700096.md): Bracket · cracked · May 14, 1997 · N906R · Doug DC863F · Wing Miscellaneous Structure
  > DURING ROUTING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD CANOE FITTING HANGER BRACKET CRACKED. REPAIR ACCOMPLISHED REMOVAL OF BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 51-1-21, 51-1-0 AND
- [SDR IXXA9700100](https://openairdocs.org/sdr/IXXA9700100.md): Bulkhead Bracket · cracked · May 13, 1997 · N906R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING ROUTINE C-CHECK INSPECTION, THE TOP AFT PRESSURE BULKHEAD SUPPORT BRACKET WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 51-1-21, 51-1-0 AND
- [SDR IXXA9700098](https://openairdocs.org/sdr/IXXA9700098.md): Bulkhead Bracket · cracked · May 13, 1997 · N906R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD RIGHT SUPPORT BRACKET CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY
- [SDR IXXA9700097](https://openairdocs.org/sdr/IXXA9700097.md): Bulkhead Fitting · cracked · May 13, 1997 · N906R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT SUPPORT FITTING CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY
- [SDR IXXA9700093](https://openairdocs.org/sdr/IXXA9700093.md): Cap Clip · cracked · May 7, 1997 · N906R · Doug DC863F · Wing Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, THE LEFT WING LOWER OUTBOARD FILLET CAP CLIP WAS FOUND CRACKED AT STATION 69.5. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW CAP CLIP IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 5
- [SDR IXXA9700090](https://openairdocs.org/sdr/IXXA9700090.md): Bracket · corroded · Apr 19, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FOUND MID SHIP ACCESSORY COMPARTMENT KEEL BEAM BRACKET WITH STRESS CORROSION CRACK AT FUSELAGE STATION 640. REPAIR ACCOMPLISHED REMOVAL OF THE BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS A
- [SDR IXXA9700089](https://openairdocs.org/sdr/IXXA9700089.md): Fitting · corroded · Apr 19, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON A SUPPORT FITTING AT FUSELAGE STATION 1200, LONGERON 32 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF THE FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8
- [SDR IXXA9700088](https://openairdocs.org/sdr/IXXA9700088.md): Fitting · cracked · Apr 19, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTING C-CHECK INSPECTION, FOUND A CRACKED SUPPORT FITTING AT FUSELAGE STATION 1180, LONGERON 27 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 5
- [SDR IXXA9700095](https://openairdocs.org/sdr/IXXA9700095.md): Plating · cracked · Apr 13, 1997 · N906R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE FUSELAGE PLATING AT FUSELAGE STATION 1900, LONGERON 9 LEFT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND EXTERNAL REPAIR DOUBLER IN ACCORDAN
- [SDR IXXA9700103](https://openairdocs.org/sdr/IXXA9700103.md): Fitting · cracked · Apr 12, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, A LONGERON ATTACH FITTING WAS FOUND CRACKED AT FUSELAGE STATION 1260, LONGERON 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY
- [SDR IXXA9700092](https://openairdocs.org/sdr/IXXA9700092.md): Web · cracked · Apr 12, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, THE CENTER WING FUEL TANK OUTER SURFACE WEB WAS FOUND CRACKED ON THE LEFT SIDE OF KEEL BEAM AT FUSELAGE STATION 810. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT CO
- [SDR IXXA9700091](https://openairdocs.org/sdr/IXXA9700091.md): Angle · cracked · Apr 12, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FOUND CENTER WING FUEL TANK SUPPORT ANGLE CRACKED AT FUSELAGE STATION 781, LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW ANGLE IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM
- [SDR IXXA9700102](https://openairdocs.org/sdr/IXXA9700102.md): Fitting · cracked · Apr 11, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, A LONGERON ATTACH FITTING WAS FOUND CRACKED AT FUSELAGE STATION 360, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY S
- [SDR IXXA9700101](https://openairdocs.org/sdr/IXXA9700101.md): Fitting · cracked · Apr 11, 1997 · N906R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, THE LEFT FLOORBEAM SUPPORT FITTINGS WERE FOUND CRACKED BETWEEN FUSELAGE STATION 180 AND 240. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTINGS, FABRICATION AND INSTALLATION OF NEW FITTINGS IN ACCORDANCE WITH DOUGLAS AIRCRAFT C
- [SDR IXXA9700094](https://openairdocs.org/sdr/IXXA9700094.md): Bulkhead Angle · cracked · Apr 11, 1997 · N906R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING ROUTING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND ON THE AFT PRESSURE BULKHEAD CIRCUMFERENTIAL MOUNT ANGLE AT FUSELAGE STATION 1766, STIFFENER 3 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW MOUNT ANGLE
- [SDR IXXA9609](https://openairdocs.org/sdr/IXXA9609.md): Dnlock Switch · failed · Feb 2, 1996 · N906R · Doug DC863F · Landing Gear Position and Warning
  > IN PREPARATION FOR LANDING AT DAY, THE LANDING GEAR WAS EXTENDED, BUT NO SAFE INDICATION WAS PRESENT FOR THE RIGHT MLG. THE AIRCRAFT ACCOMPLISHED A FLY-BY OF THE CONTROL TOWER AND OBTAINED VISUAL VERIFICATION THAT THE RIGHT MLG WAS EXTENDED. A NORMAL LANDING

Next page: https://openairdocs.org/deregistered/N906R-2016-12-27/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 = 'N906R' AND deregistration_id = 'N906R-2016-12-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N906R-2016-12-27/reports

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