# Service difficulty reports: Douglas DC-8-71F

A list on [Douglas DC-8-71F](https://openairdocs.org/model/douglas-dc-8-71f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 179 · 8,938 reports

- [SDR IXXA1100520](https://openairdocs.org/sdr/IXXA1100520.md): Wire Harness · damaged · Aug 9, 2011 · N821BX · Doug DC871F · Fuel System Wiring
  > DURING CLIMBOUT, NR 3 MAIN TANK BOOST PUMP C/B`S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MA
- [SDR IXXA110052O](https://openairdocs.org/sdr/IXXA110052O.md): Wire Harness · damaged · Aug 9, 2011 · N821BX · Doug DC871F · Fuel System Wiring
  > DURING CLIMB OUT, NR 3 MAIN TANK BOOST PUMP C/B'S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTUE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MA
- [SDR IXXA11SMN094S](https://openairdocs.org/sdr/IXXA11SMN094S.md): Skin · dented · Jun 14, 2011 · N830BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR LOWER SKIN PANEL DENTED AT SEVERAL POINTS AT STA XE 246.000 - XH 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PE
- [SDR IXXA11SMN093S](https://openairdocs.org/sdr/IXXA11SMN093S.md): Skin · corroded · Jun 10, 2011 · N830BX · Doug DC871F · Landing Gear Doors
  > DURING ROUTINE C-CHECK INSP FOUND RT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 52-2-0, SRM
- [SDR IXXA11SMN092S](https://openairdocs.org/sdr/IXXA11SMN092S.md): Skin · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR UPPER SKIN DENTED AND CRACKED AT STATION XE 246.000 - 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED RT
- [SDR IXXA11SMN091S](https://openairdocs.org/sdr/IXXA11SMN091S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER T/E UPPER SKIN CORRODED AT STA XE 29.000 - 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INNER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED
- [SDR IXXA11SMN090S](https://openairdocs.org/sdr/IXXA11SMN090S.md): Web · worn · Jun 8, 2011 · N830BX · Doug DC871F · Engine Thrust Reverser
  > DURING ROUTINE C-CHECK INSP FOUND NR 3 ENGINE THRUST REVERSER RT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR
- [SDR IXXA11SMN089S](https://openairdocs.org/sdr/IXXA11SMN089S.md): Web · worn · Jun 8, 2011 · N830BX · Doug DC871F · Engine Thrust Reverser
  > DURING ROUTINE C-CHECK INSP, FOUND NR 3 ENGINE THRUST REVERSER LT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAI
- [SDR IXXA11SMN088S](https://openairdocs.org/sdr/IXXA11SMN088S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING UPPER SKIN CORRODED AT STA XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0,
- [SDR IXXA11SMN086S](https://openairdocs.org/sdr/IXXA11SMN086S.md): Skin · corroded · Jun 8, 2011 · N830BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND LT WING T/E PANEL CORRODED AT STATION XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0, SRM 51-3-0, SRM 51-1-8B, SRM
- [SDR IXXA11SMN085S](https://openairdocs.org/sdr/IXXA11SMN085S.md): Fitting · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD BATHTUB FITTING CRACKED AT STA 680.000, LONGERON 9 RT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D
- [SDR IXXA11SMN084S](https://openairdocs.org/sdr/IXXA11SMN084S.md): Fitting · cracked · Jun 8, 2011 · N830BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 798.000, LONGERON 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING SRM 51-1-20D, SRM 51-1-0, SRM 51-1-8B, SRM 51-1-20D,
- [SDR IXXA11SMN087S](https://openairdocs.org/sdr/IXXA11SMN087S.md): Skin · dented · Jun 7, 2011 · N830BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER EXTERNAL SKIN DENTED AT SEVERAL POINTS AT STA XF 415.000 - 440.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLE
- [SDR IXXA11SMN083S](https://openairdocs.org/sdr/IXXA11SMN083S.md): Support Fitting · cracked · Jun 7, 2011 · N830BX · Doug DC871F · Wing, Control Surface Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING FLAP LINK SUPPORT LT SIDE CRACKED AT STA XF 409.000. REMOVED HINGE CRACKED SUPPORT FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW HINGE SUPPORT FITTING IAW S/B 27-249, REV 1, SRM 51-3-0, SRM 51-1-21, SRM
- [SDR IXXA11SMN082S](https://openairdocs.org/sdr/IXXA11SMN082S.md): Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 879.375. REMOVED CRACKED FRAME FITTING. FABRICATED NEW FITTING, SPLICERS, SHIMS AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING, DOUBLER, SPLI
- [SDR IXXA11SMN081S](https://openairdocs.org/sdr/IXXA11SMN081S.md): Skin · misrepaired · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND, IMPROPER REPAIR AT FWD BASKET DOOR OPENING FWD CTR LIP AT STATION FS 290, LONGERON 34.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR
- [SDR IXXA11SMN080S](https://openairdocs.org/sdr/IXXA11SMN080S.md): Strap · corroded · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FOUND NLG WHEEL WELL LT TUNNEL COMPARTMENT STRAP CORRODED AT STA 8.000. REMOVED CORROSION. REMOVED DAMAGED STRAP SEGEMENT. FABRICATED STRAP SEGMENT AND SPLICE. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED N
- [SDR IXXA11SMN079S](https://openairdocs.org/sdr/IXXA11SMN079S.md): Support Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP FOUND NR 1 ALT TANK NR 6 FUEL PROBE FITTING SUPPORT CRACKED. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.
- [SDR IXXA11SMN078S](https://openairdocs.org/sdr/IXXA11SMN078S.md): Angle · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Nacelle/Pylon Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON INTERNAL ANGLE CRACKED AT STATION YN 321.397 AND STA XRS 495.665. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR ANGLE, STRAP DOUB
- [SDR IXXA11SMN077](https://openairdocs.org/sdr/IXXA11SMN077.md): Fitting · cracked · Jun 6, 2011 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND RT MLG WHEEL WELL DOG HOUSE FITTING CRACKED AT STA 855.000, RT BOTTOM LINE 46. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-0, SRM 51-3-0 AND SRM
- [SDR IXXA11SMN076S](https://openairdocs.org/sdr/IXXA11SMN076S.md): Skin · corroded · Jun 6, 2011 · N830BX · Doug DC871F · Landing Gear Doors
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW
- [SDR IXXA110044O](https://openairdocs.org/sdr/IXXA110044O.md): Striker · bent · Jun 4, 2011 · N822BX · Doug DC871F · Landing Gear Position and Warning
  > DURING CRUISE, THE MLG DOOR LIGHT REMAINED ON. THE CREW CYCLED THE MAIN LANDING GEAR AND LIGHT REMAINED ON. WHEN AIRSPEED INCREASED TO 210 IAS LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND THE RT GEAR DOOR STRIKER BENT. TH
- [SDR IXXA11SMN075S](https://openairdocs.org/sdr/IXXA11SMN075S.md): Structure · misrepaired · Jun 3, 2011 · N830BX · Doug DC871F · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT SMALL DRAIN DOUBLER FWD LOWER CENTER FUSELAGE FORWARD OF CENTER EQUIP DOOR AT STA FS 615 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED REPAIR EXISTING REPAIR. FABRICATED REPAIR DOUB
- [SDR IXXA11SMN072S](https://openairdocs.org/sdr/IXXA11SMN072S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Emergency Exits
  > DURING ROUTINE C-CHECK INSP FOUND IMPROPER DOUBLER REPAIR AT LT FWD FUSELAGE EMERGENCY EXIT DOOR AT STA FS 404 LONGERON 15.5 LT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR DOUBLER. INSTALLED NEW FASTENERS AND
- [SDR IXXA11SMN071S](https://openairdocs.org/sdr/IXXA11SMN071S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTUIN FOUND IMPROPER DOUBLER REPAIR AT RT FWD FUSELAGE EMERGENCY EXIT DOOR AT STATION FS 392, LONGERON 16.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED,
- [SDR IXXA11SMN070S](https://openairdocs.org/sdr/IXXA11SMN070S.md): Skin · misrepaired · Jun 2, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER DOUBLER REPAIR, RT FWD FUSELAGE, 2 WINDOWS FWD OF EMERGENCY EXIT DOOR AT STATION FS 300 LONGERON 16 RT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLE
- [SDR IXXA110035O](https://openairdocs.org/sdr/IXXA110035O.md): Control Cable · out of rig · Apr 28, 2011 · N830BX · Doug DC871F · Turbine Engine Compressor Section
  > DURING LEVEL OFF, NR 3 ENGINE COMPRESSOR STALLED WHEN THROTTLES WERE RETARDED,(N1-93 PERCENT, N2-91 PERCENT, F/F-3100, OAT-44 DEGREES AND M-.80/300KIAS). THE CREW DIVERTED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED TROUBLESHOOTING TREE NR 41, RERIGGED VSV AND
- [SDR IXXAIXXA110031O](https://openairdocs.org/sdr/IXXAIXXA110031O.md): Engine · power loss · Mar 30, 2011 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FL 380 IN CALM AIR, NR 2 ENG N1 RPM AND NR 2 RPM ROLLED BACKED TO 50 PERCENT N1 AND 85 PERCENT N2. EGT WAS 530°C FUEL FLOW DECREASED TO APPROX 700 LBS. OIL TEMP DECREASED TO ZERO AND OIL PRESS WAS AT 35 PSI FUEL PRESS FLUCTUATING BETWEEN 30
- [SDR IXXA11SMN028S](https://openairdocs.org/sdr/IXXA11SMN028S.md): Skin · dented · Mar 4, 2011 · N821BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP LOWER SKIN SCRATCH AND DENTS XF AT STA 174.000 TO XF 219.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 57-7-1,
- [SDR IXXA110023O](https://openairdocs.org/sdr/IXXA110023O.md): Wire Harness · defective · Feb 18, 2011 · N822BX · Doug DC871F · Engine Indicating System Wiring
  > DURING CLIMBOUT FROM KTOL NR ONE EGT ANALOG AND DIGITAL READ OUTS DROPPED FROM 700 DEGREE TO 420 DEGREE WITH FLUCTUATION PLUS/ MINUS 5 DEGREE, N1 AND N2 SIMILAR TO THE OTHER 3 ENG. ALL 4 THROTTLES WERE ALIGNED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER
- [SDR IXXA110022S](https://openairdocs.org/sdr/IXXA110022S.md): Skin · dented · Feb 14, 2011 · N830BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING PREFLIGHT FOUND LT SIDE BELLY SKIN TO BE (DENTED AND CRACKED) AT STA 55 BETWEEN 15" TO 19.2500" FROM CTR LINE. OPEN
- [SDR IXXA11SMN048S](https://openairdocs.org/sdr/IXXA11SMN048S.md): Spar Cap · cracked · Feb 11, 2011 · N821BX · Doug DC871F · Wing Spar
  > DURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP, NO DISCREPANCY FOUND. FABRICATED SPLICE ANGLES, EXTERNAL DOUBLER, STRAP. CLEANED, TREATED, PRIM
- [SDR U2RA449SPIM003](https://openairdocs.org/sdr/U2RA449SPIM003.md): Skin · corroded · Feb 11, 2011 · N872SJ · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZ STAB BETWEEN XE 75.672 AND XE 147.906 T/E UPPER PANEL SKIN WITH CORROSION AROUND FASTENERS.
- [SDR IXXA110019O](https://openairdocs.org/sdr/IXXA110019O.md): Connector · dirty · Feb 10, 2011 · N823BX · Doug DC871F · Engine Oil System Wiring
  > DURING TAKEOFF, NR 1 ENG OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL TEMP AND PRESSURE GOOD ON FLIGHT ENGINEER PANEL. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX CLEANED THE CONNECTOR PLUG ON DIFFERENTIAL PRESSURE WITH. O
- [SDR IXXA11SMN047S](https://openairdocs.org/sdr/IXXA11SMN047S.md): Fitting · cracked · Feb 8, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND RT MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 6, RT. REMOVED CRACKED FITTING. CLEANED AND APPLIED PRIMER TO AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.
- [SDR IXXA11SMN044S](https://openairdocs.org/sdr/IXXA11SMN044S.md): Floorbeam · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Floor Beam
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CRACKED AT STA 960.000 LT BOTTOM LINE 56. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW EXTRUSION ANGLE AND FILLER. CLEANED TREATED, PRIMED AREA AND R
- [SDR IXXA11SMN043S](https://openairdocs.org/sdr/IXXA11SMN043S.md): Fitting · corroded · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STA 879.000, LONGERON-19 RT TO LONGERON-22 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE FITTING. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FR
- [SDR IXXA11SMN041S](https://openairdocs.org/sdr/IXXA11SMN041S.md): Rib · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD FLAP RIB CRACKED AT STA XF 129.000. REMOVED DAMAGED RIB. FABRICATED NEW RIB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIME AREA AND REPAIR PARTS. INSTALLED NEW RIB IAW SRM CHAP 57-7-1 FIGURE 2, SHEET 4, SRM
- [SDR IXXA11SMN038S](https://openairdocs.org/sdr/IXXA11SMN038S.md): Skin · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND SKIN CRACKED AT STA 55.000, 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLER AND F
- [SDR IXXA11SMN046S](https://openairdocs.org/sdr/IXXA11SMN046S.md): Fitting · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE NR 60 ACCESS RT FITTING CRACKED AT STA 1766.000, LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.
- [SDR IXXA11SMN045S](https://openairdocs.org/sdr/IXXA11SMN045S.md): Fitting · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND EMPENNAGE NR 60 ACCESS LT FITTING CRACKED AT STA 1766.000 LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.
- [SDR IXXA11SMN042S](https://openairdocs.org/sdr/IXXA11SMN042S.md): Fitting · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 702.000 LONGERON 19 RT. REMOVED CRACKED FITTING.INSTALLED NEW FITTING IAW SRM 51-1-21D AND SRM 51-3-1.
- [SDR IXXA11SMN040S](https://openairdocs.org/sdr/IXXA11SMN040S.md): Angle · corroded · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND FWD LOWER CARGO FWD DOOR AND JAMB INTERIOR CORRODED AT STA 335.000, LONGERON 36 TO LONGERON 35 RT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR ANGLE, FILLER AND REPAIR STRAP. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INST
- [SDR IXXA11SMN037S](https://openairdocs.org/sdr/IXXA11SMN037S.md): Fitting · cracked · Feb 7, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STA 1160.000. R & R AFT CARGO COMPARTMENT FITTING IAW SRM 51-1-20D.
- [SDR U2RA449SPIM004](https://openairdocs.org/sdr/U2RA449SPIM004.md): Drive Assy · cracked · Feb 7, 2011 · N872SJ · Doug DC871F · Rudder Tab Control System
  > RUDDER TAB DRIVE SECTOR BROKEN.
- [SDR IXXA11SMN039S](https://openairdocs.org/sdr/IXXA11SMN039S.md): Skin · dented · Feb 6, 2011 · N821BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPÈR SKIN SHOWS DENTS AT DIFFERENT LOCATIONS AT STATION XW 3.000 - XW 92.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND REPAIR DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND R
- [SDR IXXA11SMN030S](https://openairdocs.org/sdr/IXXA11SMN030S.md): Door Frame · cracked · Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSP FOUND LOWER FWD CARGO COMPARTMENT FRAME CRACKED AT STA 200.000 BETWEEN LONGERON-32 RT AND LONGERON -33 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. R & R EXTRUSION FRAME SEGMENT. FABRICATED SPLICE AND A
- [SDR IXXA11SMN036S](https://openairdocs.org/sdr/IXXA11SMN036S.md): Cargo Track · broken · Feb 5, 2011 · N821BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 TRACK LUGS BROKEN AT STA 1580.000 - STA 1600.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREATED, PRIMED AND PAINTED AREA. INSTALLED NEW TRACK SEGMENT IAW SRM 51-1-21, 53-2-3 FIG 8A, SRM 51-1-8B,
- [SDR IXXA11SMN035S](https://openairdocs.org/sdr/IXXA11SMN035S.md): Cargo Track · broken · Feb 5, 2011 · N821BX · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT NR 4 TRACK LUGS BROKEN AT STA 320.000 - STA 340.000. REMOVED DAMAGED TRACK SEGMENT. CLEANED, TREATED, PRIMED AND PAINTED AREA. INSTALLED NEW TRACK SEGMENT IAW SRM 51-1-21, 53-2-3, SRM 51-1-8B, SR
- [SDR IXXA11SMN034S](https://openairdocs.org/sdr/IXXA11SMN034S.md): Fitting · cracked · Feb 5, 2011 · N821BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 1690.000, LONGERON 21 LT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-18B, SRM 51-1-20D AND SRM 51-3-1.

Next page: https://openairdocs.org/model/douglas-dc-8-71f/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 aircraft_model_key = 'DC871F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-71f/reports

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