# Service difficulty reports: N806DH, cancelled Sep 26, 2017

A list on [N806DH, cancelled Sep 26, 2017](https://openairdocs.org/deregistered/N806DH-2017-09-26.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 15 · 746 reports

- [SDR DHLA201200005](https://openairdocs.org/sdr/DHLA201200005.md): Warning Light · false activation · Apr 5, 2012 · N806DH · Doug DC873F · Engine Thrust Reverser
  > ON CLIMB OUT, NR 4 THRUST REVERSER LIGHT ILLUMINATED. RAN THRUST REVERSER EMERGENCY STOW CHECKLIST. LIGHT REMAINED ILLUMINATED. RAN ABNORMAL IN FLIGHT ENGINE SHUTDOWN AND SHUTDOWN ENGINE. WINDMILLED OIL PRESSURE JUST ABOVE 0 PSI AND SHUTDOWN FOR APROX 10 M
- [SDR DHLA201203140004](https://openairdocs.org/sdr/DHLA201203140004.md): Cap · loose · Mar 14, 2012 · N806DH · Doug DC873F · Turbine Engine Oil System
  > NR 4 ENGINE SHUTDOWN DURING FLIGHT WITH OIL QTY AT 2 QUARTS. ACFT WAS GROUNDED. INSPECTED ENGINE FOUND OIL CAP TO BE LOOSE INSTALLED NEW CAP ASSY IAW MM 79-11-10 OIL IAW MM 12-10-00 INSPECTED CHIP DETECTOR IAW MM 79-00-00 NO DEFECTES NOTED RAN NR 4 ENGINE IA
- [SDR DHLA20120106002](https://openairdocs.org/sdr/DHLA20120106002.md): Battery Pack · inoperative · Jan 6, 2012 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY LIGHTS BATTERY PACK IAW MM 33-50-0 WORKING NORMAL.
- [SDR DHLA201100538](https://openairdocs.org/sdr/DHLA201100538.md): Battery Pack · inoperative · Oct 6, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHTS ARMED-NO POWER ON ACFT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY RACK ASSY IAW MMS 33-50-00. OPS CK-NORMAL.
- [SDR DHLA201100534](https://openairdocs.org/sdr/DHLA201100534.md): Engine · failed · Jul 28, 2011 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > DURING DESCENT NR3 ENGINE AT IDLE, STARTED RUMBLING ENGINE N1 & N2 SPOOLED DOWN NO- OIL PRESSURE. ACFT WAS GROUNDED. REPLACED NR 3 ENGINE ASSY.
- [SDR DHLA201100533](https://openairdocs.org/sdr/DHLA201100533.md): Line · leaking · Jul 26, 2011 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > AT FL 380 ENGINE NR 1 FAILED. COMPLETED ENGINE FAILURE CHECK LIST. TRIED RESTART AT 340 NO GOOD. AT FL 220 RESTART SUCCESSFUL. ALL PARAMETERS NORMAL. ACFT WAS GROUNDED UPON ARRIVAL AT CVG. PERFORMED MM TS CHART 71-00-00FAULT 51. CHECKED SPECIFIC GRAVITY WAS.
- [SDR DHLA201100525](https://openairdocs.org/sdr/DHLA201100525.md): Battery · inoperative · Jul 11, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ONLY STAY ON FOR A FEW SECONDS. ACFT WAS GROUNDED. REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY AND SYS. OPS CK GOOD IAW MM 33-50-1.
- [SDR DHLA201100515](https://openairdocs.org/sdr/DHLA201100515.md): Amplifier · inoperative · Jun 7, 2011 · N806DH · Doug DC873F · Smoke Detection
  > AMBER CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT, LIGHT EXTINGUISHED ON SHORT FINAL APPROACH TO LANDING, NO SMOKE OR FIRE WAS NOTICED TO CREW. EMERGENCY WAS DECLARED. ACFT WAS GROUNDED
- [SDR DHLA201100049](https://openairdocs.org/sdr/DHLA201100049.md): Battery Pack · discharged · May 4, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > ALL 3 EMERGENCY EVAC LIGHTS DO NOT ILLUMINATE OR ARE VERY DIM WHEN PERFORMING A BATTERY CHECK. ACFT WAS GROUNDED. R & R EMERGENCY LIGHTS BATTERY RACK ASSY IAW DC8 33-50-1, OPS CK OK.
- [SDR DHLA201100041](https://openairdocs.org/sdr/DHLA201100041.md): Skin · corroded · May 1, 2011 · N806DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGING AND CRACKED AT FS 26.0, BETWEEN LONGERONS 35L AND 36. ACCOMPLISHED SKIN EXTERNAL DOUBLER REPAIR IAW EVA D853-0041 REV A, DWG D85300441-001-D, REV D, AND SRM 53-2-1, FIG 8. REF NR 10081-10 UNDER W/O 10081. REPAIR LOCATIONS LISTED BELOW.
- [SDR DHLA201100001](https://openairdocs.org/sdr/DHLA201100001.md): Battery Pack · inoperative · Jan 12, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARE VERY DIM. ACFT WAS GROUNDED. R & R EMER EXIT LIGHTS POWER SUPPLY, OPS CHECK GOOD IAW AMM 33-50-1. EMERGENCY LIGHT CB WILL NOT RESET. R & R EMERGENCY LIGHT BATTERY PACK. SYS OPS CHECK GOOD IAW 33-50-00.
- [SDR 2011F00016](https://openairdocs.org/sdr/2011F00016.md): Power Supply · discharged · Jan 12, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > UPON CHECKING THE EMERGENCY LIGHTS FOUND THE LIGHTS TO BE VERY DIM. THE LIGHT POWER SUPPLY WAS REPLACED. OPS CHECKED SERVICABLE
- [SDR 2011F00015](https://openairdocs.org/sdr/2011F00015.md): Power Supply · discharged · Jan 12, 2011 · N806DH · Doug DC873F · Emergency Lighting
  > UPON CHECKING THE EMERGENCY LIGHTS FOUND THE LIGHTS TO BE VERY DIM. THE LIGHT POWER SUPPLY WAS REPLACED. OPS CHECKED SERVICABLE.
- [SDR DHLA201000142](https://openairdocs.org/sdr/DHLA201000142.md): Skin · corroded · Dec 4, 2010 · N806DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00386 REV IR, DWG NR D85300386-001-D, REV IR, AND SRM CHAPTERS 51 & 53. HFEC OF REPAIR PARTS
- [SDR DHLA201000140](https://openairdocs.org/sdr/DHLA201000140.md): Skin · bulged · Dec 1, 2010 · N806DH · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACFT WAS GROUNDED COMPLIED WITH EVA D853-00386 DWG D85300386-001-D AND NR 9855-2.
- [SDR DHLA201000091](https://openairdocs.org/sdr/DHLA201000091.md): Lamp · burned out · Sep 16, 2010 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS DISARM LIGHT FAILS TO ILLUMINATE WITH SWITCH IN DISARM. ACFT WAS GROUNDED. R & R EMERGENCY LIGHTS DISARM LIGHT BULB, OPS CHECK OK IAW MMS 33-50-00. PN 313.
- [SDR DHLA201000089](https://openairdocs.org/sdr/DHLA201000089.md): Bulb · inoperative · Aug 28, 2010 · N806DH · Doug DC873F · Emergency Lighting
  > COCKPIT LIGHTING HAS ONE EMERGENCY EXIT LIGHT BULB INOP IN CEILING. ACFT WAS GROUNDED. R & R BULB ON COCKPIT CEILING LIGHTING IAW MM 33-22-0. OPS CK OK.
- [SDR DHLA201000067](https://openairdocs.org/sdr/DHLA201000067.md): Pump · malfunctioned · Aug 10, 2010 · N806DH · Doug DC873F · Fuel Boost Pump
  > ON LEVEL OFF AT 370, NR 3 ENG FAILED. NORMAL OIL PRESSURE, TEMP & FUEL PRESSURE, ENG N1 & N2 REMAINED ROTATING. PERFORMED ENG FAIL CHECKLIST & INFLT ENG START. ENG OPS RESTORED. R & R NASH PUMP IAW MM 73-10-6, GROUND CHECKS GOOD. ALSO MM 71-00 TROUBLESHOOTI
- [SDR DHLA201000059](https://openairdocs.org/sdr/DHLA201000059.md): Skin · corroded · May 12, 2010 · N806DH · Doug DC873F · Rudder, Plate/Skin
  > RT RUDDER SKIN CORRODED STA ZR159.094-168.656. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 5
- [SDR DHLA201000035](https://openairdocs.org/sdr/DHLA201000035.md): Seat Track · worn · May 7, 2010 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT NR 2 TRACK LUGS WORN STA 1590.000-1615.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0, PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT (PN S2772660) IAW S
- [SDR DHLA201000036](https://openairdocs.org/sdr/DHLA201000036.md): Seat Track · worn · May 7, 2010 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO COMPT. NR 2 TRACK LUGS WORN STA, 1550.000-1595.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 14, SHEET 1-2, PG 49-50-51. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT (PN S4889185)
- [SDR DHLA201000063](https://openairdocs.org/sdr/DHLA201000063.md): Skin · corroded · May 6, 2010 · N806DH · Doug DC873F · Wing, Plate/Skin
  > RT WING UPPER PLATING CORRODED STA XRS 76.869 S-9R. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 17. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 FIG. 7. CUT OUT DAMAGED AREA IAW SRM 57-2-1 FIG. 17. FABRICATED EXT DOUBLER (AL7075
- [SDR DHLA201000060](https://openairdocs.org/sdr/DHLA201000060.md): Longeron · corroded · May 6, 2010 · N806DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FWD ACCY COMPT L-36 CORRODED STA 35.000. RESOLUTION: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-3 FIG. 2 SHEET 1 ITEM "A". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED LONGERON IAW SRM 53-1-0
- [SDR DHLA201000058](https://openairdocs.org/sdr/DHLA201000058.md): Frame · cracked · May 5, 2010 · N806DH · Doug DC873F · Fuselage Main, Frame
  > MAIN CARGO COMPT. FRAME CRACKED 1" BS 220.000 L20-21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2 SHEET 2,6. REMOVED FRAME SEGMENT, ANGLE & SPLICE (EXISTING) IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT IAW SRM 53-2-0 FIG 2, SHEET 2, SRM 53-2-0 FIG 2 SHEET
- [SDR DHLA201000061](https://openairdocs.org/sdr/DHLA201000061.md): Skin · delaminated · May 4, 2010 · N806DH · Doug DC873F · Spoilers
  > NR 1 LT SPOILER PANEL DELAMINATED. R & R NR 1 LT SPOILER PANEL (REPAIRED CONDITION) IAW MM 27-61-1 PG 201-207. ADJUSTED GROUND SPOILER IAW MM 27-60-0, PG 509-510. REFER TO NR 218133 FOR OPS CHECK.
- [SDR DHLA201000064](https://openairdocs.org/sdr/DHLA201000064.md): Angle · cracked · May 3, 2010 · N806DH · Doug DC873F · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG PYLON LT UPPER ANGLE CRACKED.7500" STA YN 202.6. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 06-10-10, EVA D854-00335 REV IR DATED 05-13-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA IAW SMN DWG ED-5130 REV 01 DATED 05-07
- [SDR DHLA201000062](https://openairdocs.org/sdr/DHLA201000062.md): Frame · worn · May 3, 2010 · N806DH · Doug DC873F · Engine Thrust Reverser
  > NR3 ENGINE T/R FIXED STRUCTURE FRAME WORN. STA YN 203.000 AT 7 O'COCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 06-10-10, EVA D878-00332 REV IR DATED 05-12-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED AREA IAW SMN DWG ED-5129 REV
- [SDR DHLA201000056](https://openairdocs.org/sdr/DHLA201000056.md): Longeron · cracked · May 3, 2010 · N806DH · Doug DC873F · Fuselage Main, Longeron/Stringer
  > LT MLG W/W L-24L CRACKED 3" STA 902.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG. 5 SHEET 1,1,3,14,15,16,17,25,26,27 TR NR 53-123 DATED 05-15-01. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP HOLE AND DETAILED VISUAL INSP OF CRACKED END. NO CRACK FOUND.
- [SDR DHLA2009806001](https://openairdocs.org/sdr/DHLA2009806001.md): Skin · corroded · Dec 5, 2009 · N806DH · Doug DC873F · Fuselage Main, Plate/Skin
  > INTERGRANULAR CORROSION DISCOVERED ON FUSE. EXTERIOR SKIN, FS 59.0, LONG 34L TO 35L. ACCOMPLISHED EXTERNAL DOUBLER REPAIR, FS 53.5 TO 70.0, LONG 34L TO 34R, IAW D857-00297 REV IR DATED 12/4/09, DWG NR D85300297-001-D REV IR DATED 12/4/09, AND SRM CHPT'S 51 &
- [SDR DHLA200900054](https://openairdocs.org/sdr/DHLA200900054.md): Spoiler Sys · malfunctioned · Nov 23, 2009 · N806DH · Doug DC873 · Drag Control System
  > REJECTED TAKEOFF DUE TO SPOILERS DEPLOYING ON TAKEOFF ROLL AT APPROX 60 KNOTS MAX SPEED ATTAINED 70 KNOTS 252,000 LBS TOW 22C 4880 PA NORMAL BRAKE ENERGY CHART. IAW MM PERFORMED SPOILER OPERATION CK INSPECTED RIGGING AND LINKAGE PERFORM SPOILER ELECTRICAL OPS
- [SDR DHLA20090049](https://openairdocs.org/sdr/DHLA20090049.md): Unknown · unknown · Sep 10, 2009 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > NUMBER 3 AND 4 ENG SLOW TO SPOOL UPON A ROLLING T/O. REJECTED T/O DUE TO DIRECTIONAL CONTROL. PERF ENG NR 3 AND 4 T/S IAW MM 71-00-00 ALL ENG INSPECTIONS AND PARAMETERS NORMAL. OK FOR SERVICE. ACFT GROUNDED. AT POWER UP AIRCRAFT PULLED OFF THE RUNWAY, S
- [SDR DHLA200900046](https://openairdocs.org/sdr/DHLA200900046.md): Engine · slow · Aug 21, 2009 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)
  > RTO ON RNWY 34R SLC DUE TO ENGINES SPOOLING UP UNEVENLY. SPEED 70 KTS, LIGHT BRAKING, PRESSURE ALTITUDE 4127 FT, FULL REVERSE, A/C WEIGHT 225,000 LBS. NR 3 & NR 4 SLOW TO SPOOL UP. INFO NOTED BY MX.
- [SDR DHLA200900044](https://openairdocs.org/sdr/DHLA200900044.md): Connector · broken · Aug 8, 2009 · N806DH · Doug DC873F · Fire Protection System Wiring
  > DURING CRUISE FLT, NR 2 FIRE WARNING ILLUMINATED INTERMITTENTLY. B-LOOP DID NOT TEST. CHANGED TO LOOP "A". NORMAL OPS. TRANSFER NR 2 ENG B-SYS FIRE DET TO DMI 35399, PER MEL 26-2-3, CAT B. PLACARD INSTALLED. REPLACED BROKEN CONNECTOR AT LOWER RT HOT SECT
- [SDR DHLA200900042](https://openairdocs.org/sdr/DHLA200900042.md): Ground Wire · loose · Aug 5, 2009 · N806DH · Doug DC873F · Fire Protection System Wiring
  > NR 4 ENG FIRE WARNING INTERMITTENT AFTER ENG FIRE CHECKLIST COMPLETE. LIGHT AND BELL INTERMITTENT, TRIED BOTH LOOPS. FOUND LOOSE GROUND WIRE ON NR 4 FIRE HANDLE. RE-SECURED GROUND WIRE ON NR 4 FIRE HANDLE, SYS GROUND OPS CHECK NORMAL IAW M/M 26-10-0. AIRCR
- [SDR DHLA200900041](https://openairdocs.org/sdr/DHLA200900041.md): Fire Detector · failed · Aug 1, 2009 · N806DH · Doug DC873F · Fire Detection
  > DEFECT DESCRIPTION: (ACFT LANDED INTO SDF NOT CODED FOR TRAX) DESCENDING INTO CVG AT ABOUT FL 210 NR 4 MASTER FIRE T-HANDLE MASTER FIRE LIGHT ILLUMINATED. EMERGENCY PROC COMPLETED PER AOM. DURING FIRE EMERGENCY PROC, UNABLE TO FIRE SECOND BOTTLE. INSPECTED
- [SDR DHLA200900040](https://openairdocs.org/sdr/DHLA200900040.md): Tube · blocked · Jul 21, 2009 · N806DH · Doug DC873F · Fuel Controlling System
  > NR 2 ENGINE FLAMED OUT AT FL 380, ALL ENGINE PARAMETERS NORMAL. SUCCESSFUL RESTART AT 18,000 FT ALL ENGINE PARAMETERS NORMAL. IN-FLIGHT ENGINE RESTART ABNORMAL PROCEDURE COMPLIED. PERFORMED NR 2 ENG INSP IAW CFM 71-00-00, FOUND CDP TUBE BLOCKED. CLEARED, S
- [SDR DHLA200900029](https://openairdocs.org/sdr/DHLA200900029.md): Battery Pack · discharged · May 16, 2009 · N806DH · Doug DC873 · Emergency Lighting
  > EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PACK ASSY EMERGENCY BATTERY, CHECKED OPS GOOD PER MM 33 50 0.
- [SDR DHLA200900028](https://openairdocs.org/sdr/DHLA200900028.md): Battery Pack · failed · May 7, 2009 · N806DH · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT DISARM RESOLUTION DESCRIPTION, REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY/RELAY PACK. OPS CHK GOOD IAW MM 33-50-1.
- [SDR DHLA200900027](https://openairdocs.org/sdr/DHLA200900027.md): Battery Pack · inoperative · May 2, 2009 · N806DH · Doug DC873F · Emergency Lighting
  > AMBER DISARM LIGHT DID NOT ILLUMINATE WHEN DISARM WAS SELECTED. RESECURED EMERGENCY BATTERY IN RACK AND ITS CONNECTOR. OPS OK PER DC8MMS 33-50-00. NO OTHER DEFECTS NOTED.
- [SDR DHLA200900026](https://openairdocs.org/sdr/DHLA200900026.md): Battery Pack · discharged · Apr 24, 2009 · N806DH · Doug DC873 · Emergency Lighting
  > DURING PREFLIGHT CHECK EMERGENCY LIGHTS DID NOT COME ON DURING BITE CHECK. RECHARGED BATTERY PACK IAW MM 33-50-21, CHECKED OPERATION OK.
- [SDR DHLA200800010A](https://openairdocs.org/sdr/DHLA200800010A.md): Pump · failed · Feb 5, 2009 · N806DH · Doug DC873 · Fuel Boost Pump
  > PASSING THROUGH 39600 FL ENG NR 4 FAILED AIRSPEED.79M DESCENDED TO 30FL AND RESTARTED WITH NORMAL OPERATION AFTER RESOLUTION. FOUND VSV OUT OF RIG. RIGGED NR 4 ENG VSV AND VBV PER MM 73-21-10. REMOVED AND REPLACED ENGINE DRIVEN FUEL BOOST PUMP (NASH) PER MM
- [SDR DHLA200800128](https://openairdocs.org/sdr/DHLA200800128.md): Fan · burned · Nov 18, 2008 · N806DH · Doug DC873 · Air Distribution Fan
  > SMOKE IN CABIN AFT OF CABIN AFTER LANDING. REMOVED AND REPLACED CABIN AIR RECIRC FAN INSTALLED CABIN FAN TRANSFERED TO DMI LOG PER MEL21-16, PLACARD INSTALLED. A/C WAS GROUNDED.
- [SDR DHLA200800009](https://openairdocs.org/sdr/DHLA200800009.md): Fire Detector · malfunctioned · Jan 25, 2008 · N806DH · Doug DC873F · Fire Detection
  > FLT 160, DURING START OF DESCENT, NR 1 ENG FIRE WARNING LIGHT ILLUMINATED AND WARNING BELL ACTIVATED INTERMITTENTLY FOR 5 SECS IN DESENT "A LOOP' PER MEL 26-2-3 CAT C MDDR NR 31535 PLACARD INSTALLED, S/P COMPLIED WITH M/M 26-10-0. R7R FIRE DETECTOR CONTROL BO
- [SDR DHLA200800031](https://openairdocs.org/sdr/DHLA200800031.md): Fire Detector · malfunctioned · Jan 23, 2008 · N806DH · Doug DC873F · Fire Detection
  > FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND RE
- [SDR DHLA200800032](https://openairdocs.org/sdr/DHLA200800032.md): Fire Detector · malfunctioned · Jan 22, 2008 · N806DH · Doug DC873F · Fire Detection
  > FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485, PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND
- [SDR DHLA200800030](https://openairdocs.org/sdr/DHLA200800030.md): Fire Detector · malfunctioned · Jan 22, 2008 · N806DH · Doug DC873F · Fire Detection
  > FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND RE
- [SDR DHLA200800008](https://openairdocs.org/sdr/DHLA200800008.md): Fire Warning · malfunctioned · Jan 22, 2008 · N806DH · Doug DC873F · Fire Detection
  > FLT 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP, OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10-0. REMOVED AND REP
- [SDR DHLA200800006](https://openairdocs.org/sdr/DHLA200800006.md): Connector · loose · Jan 20, 2008 · N806DH · Doug DC873 · Fire Protection System Wiring
  > FLT 631, NR 1 ENGINE FIRE WARN COMES ON INTERMITTENTLY AT CRUISE FLIGHT FL 350 3 TIMES AND BOTH FIRE LOOPS CHECKED OK AND IN DESCENT FIRE LIGHT CAME ON STEADY. COMPLETED ENG FIRE CHECKLIST (CONT) LIGHT REMAINED ON, BOTH BOTTLES DISCHARGED IN A LOOP. FOUND L
- [SDR DHL2007806591](https://openairdocs.org/sdr/DHL2007806591.md): Angle · cracked · Apr 20, 2007 · N806DH · Doug DC873F · Wing Miscellaneous Structure
  > RT INBD FLAP LWR "T" ANGLE CRACKED 1 1/2" STA XW 91.000. REMOVED CRACKED "T" ANGLE IAW SRM 51-1-21. FABRICATED NEW "T' ANGLE (EXTRUSION S2701008) IAW SRM 57-7-1 PG 4. CLEANED, TREATED AND PRIMED AREA AND "T" ANGLE IAW SRM 51-1-8B. INSTALLED "T" ANGLE IAW S
- [SDR DHL2007806599](https://openairdocs.org/sdr/DHL2007806599.md): Channel · worn · Apr 20, 2007 · N806DH · Doug DC873F · Landing Gear Doors
  > LT MLG LT DOOR ZEE CHANNEL EDGE WORN (MAJOR REPAIR) STA 865.000 RBL 45. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00002 DATED 03-17-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SE

Next page: https://openairdocs.org/deregistered/N806DH-2017-09-26/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 = 'N806DH' AND deregistration_id = 'N806DH-2017-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N806DH-2017-09-26/reports

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