# Service difficulty reports: Douglas DC-8-62

A list on [Douglas DC-8-62](https://openairdocs.org/model/douglas-dc-8-62.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 56 · 2,778 reports

- [SDR IXXA201308180280](https://openairdocs.org/sdr/IXXA201308180280.md): Bleed Valve · malfunctioned · Aug 18, 2013 · N41CX · Doug DC862 · Compressor Bleed Valve
  > COMPRESSOR STALL AT APPROX 75 KNOTS. SUSPECT NR 1 AND 2 ENGINES. RAN NR 1 AND 2 ENGINES IAW ENGINE RUN HANDBOOK 70.01. FOUND NR 1 ENGINE PRESSURE RATIO BLEED CONTROL VALVE WILL NOT CLOSE ABOVE 64 PERCENT N1. R & R PRESSURE RATIO BLEED CONTROL VALVE IAW MM 75
- [SDR IXXA20130202002O](https://openairdocs.org/sdr/IXXA20130202002O.md): Link · inoperative · Feb 2, 2013 · N41CX · Doug DC862 · Landing Gear Retraction/Extension System
  > ON CLIMBOUT, AFTER A GOOD UPLATCH CHECK, HEARD A LOUD NOISE IN NOSE GEAR AREA. (SOUNDED LIKE A NOSE GEAR DOOR POPPED OPEN). R & R RT NLG DOOR FORWARD LINK ASSY IAW MM 32-22-1. OPS CHECKS GOOD ON NOSE GEAR SWING.
- [SDR IXXA2013020700006](https://openairdocs.org/sdr/IXXA2013020700006.md): Skin · cracked · Dec 5, 2012 · N41CX · Doug DC862 · Wing, Plate/Skin
  > RT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED DOUBLER 0.190", FILLER 0.200" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED FABRICATED PARTS AND
- [SDR IXXA2013020700005](https://openairdocs.org/sdr/IXXA2013020700005.md): Panel · damaged · Nov 23, 2012 · N41CX · Doug DC862 · Trailing Edge Flaps
  > RT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PANEL IAW SRM 51-3-0. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21. FABRICATED NEW PANEL PLATING 0
- [SDR IXXA2013020700004](https://openairdocs.org/sdr/IXXA2013020700004.md): Fitting · corroded · Nov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach Fittings
  > AFTER CARGO COMPARTMENT - INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000, L-32R (AFTER PART). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, NOV 15, 2012, DWG ED-5546 NOV 15, 2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING (
- [SDR IXXA2013020700003](https://openairdocs.org/sdr/IXXA2013020700003.md): Fitting · corroded · Nov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach Fittings
  > AFTER ACCESSORY COMPARTMENT INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000 L-34R (AFTER PART). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DWG NR ED-5546 NOV 15,2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING AL 7075T651 IAW DW
- [SDR IXXA2013020700002](https://openairdocs.org/sdr/IXXA2013020700002.md): Skin · corroded · Nov 9, 2012 · N41CX · Doug DC862 · Rudder, Plate/Skin
  > RUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21, SRM 55-1-0. FABRICATED NEW PANEL PLATING 0.016" AND BONDED DOUBLER 0.016" BOTH FROM AL 2
- [SDR IXXA121109SMN026S](https://openairdocs.org/sdr/IXXA121109SMN026S.md): Longeron · cracked · Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 24R, HORIZONTAL LEG CRACKED 2 INCHES AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5 TR 53-123. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-20D.
- [SDR IXXA121109SMN025S](https://openairdocs.org/sdr/IXXA121109SMN025S.md): Longeron · cracked · Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 24L, HORIZONTAL LEG CRACKED 1 INCH AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5, TR 53-123.
- [SDR IXXA2013020700001](https://openairdocs.org/sdr/IXXA2013020700001.md): Skin · damaged · Nov 6, 2012 · N41CX · Doug DC862 · Wing, Plate/Skin
  > RT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. TRIMMED OUT DAMAGED AREA IAW DWG ED-5545 NOV 14, 2012. FABRICATED DOUBLER 0.071" FILLER 0.063" BO
- [SDR IXXA20120706017O](https://openairdocs.org/sdr/IXXA20120706017O.md): Lock · lack of lube · Jul 6, 2012 · N799AL · Doug DC862 · Landing Gear Position and Warning
  > HAD A DOOR NOT LATCH LAMP ON DURING UPLATCH CHECK. UNSATISFACTORY UP LATCH, BOTH ALTERNATE DOOR LIGHTS DID NOT COME ON AFTER RECYCLE OF THE LANDING GEAR. JACKED ACFT IAW MM 7-11-0. PERFORMED OPS CHECK OF MLG IAW MM 32-30-0 FOUND RT MAIN GEAR DOOR LOCK MECHA
- [SDR RRXA001532](https://openairdocs.org/sdr/RRXA001532.md): Frame · damaged · Jan 21, 2008 · N994CF · Doug DC862 · Fuselage Main, Frame
  > DURING A MAINT VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT. FS 1340 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO
- [SDR IXXA08SMN013S](https://openairdocs.org/sdr/IXXA08SMN013S.md): Frame · cracked · Jan 15, 2008 · N41CX · Doug DC862 · Fuselage Main, Frame
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT CRACK ON FRAME FLANGE AT STATION 240.000 LONGERON 21RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME. FABRICATED FRAME AND SPLICE AND ANGLE PERFORMED HEAT TREATMENT.
- [SDR IXXA08SMN012S](https://openairdocs.org/sdr/IXXA08SMN012S.md): Door · delaminated · Jan 15, 2008 · N41CX · Doug DC862 · Landing Gear Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED DAMAGED DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MAINTENANCE MANUAL 32-12-1 PAGE 401, DC8 27-10-0, 27-20-0, 27-40-0
- [SDR IXXA08SMN011S](https://openairdocs.org/sdr/IXXA08SMN011S.md): Skin · delaminated · Jan 15, 2008 · N41CX · Doug DC862 · Landing Gear Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) MIDDLE DOOR DELAMINATED SKIN. REMOVED DELAMINATED DOOR. INSTALLED NEW MID DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MM 27-10-0, 27-20-0, 27-40-0, 27
- [SDR IXXA08SMN010S](https://openairdocs.org/sdr/IXXA08SMN010S.md): Door · delaminated · Jan 15, 2008 · N41CX · Doug DC862 · Landing Gear Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MAINTENANCE MAN
- [SDR IXXA08SMN009S](https://openairdocs.org/sdr/IXXA08SMN009S.md): Skin · delaminated · Jan 15, 2008 · N41CX · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) MIDDLE DOOR, DELAMINATED SKIN. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN CENTER DOOR ON RIGHT MAIN LANDING GEAR FUSELAGE. PERFORMED OPERATIONAL CHECK FOR HYD SYSTEM LEAKS, GOOD IAW DC8 MINATE
- [SDR IXXA08SMN008S](https://openairdocs.org/sdr/IXXA08SMN008S.md): Skin · delaminated · Jan 15, 2008 · N41CX · Doug DC862 · Spoilers
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER DELAMINATED. REMOVED DAMAGED SPOILER. INSTALLED NEW RIGHT SPOILER IAW DC8 MAINTENANCE MANUAL 27-60-1 PAGES 201-207. PERFORMED OPERATIONAL CHECK TO ALL FLIGHT CONTROLS, GOOD IAW DC8 MAINTEN
- [SDR IXXA08SMN004S](https://openairdocs.org/sdr/IXXA08SMN004S.md): Panel · delaminated · Jan 14, 2008 · N41CX · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER PANEL DELAMINATED AT STATION XF 219 TO XF 339.000. REMOVED DAMAGED PANEL. INSTALLED NEW PANEL IAW DC8 SRM 51-3-0, 51-3-1.
- [SDR IXXA070043O](https://openairdocs.org/sdr/IXXA070043O.md): B-Nut · loose · Aug 23, 2007 · N41CX · Doug DC862 · Turbine Engine Oil System
  > DURING CRUISE FROM KBWI NUMBER THREE ENGINE OIL QUANITY SLOWLY DECREASED UNTIL INDICATING ZERO. PRESSURE AND TEMPERATURE REMAINED NORMAL UNTIL THE OIL PRESSURE BEGAN TO FLUCTUATE APPROXIMATELY 15 PSI WITH NR 3 OIL PRESSURE LIGHT COMING ON AND OFF. THE CREW SH
- [SDR IXXA070036O](https://openairdocs.org/sdr/IXXA070036O.md): Fuel Control · malfunctioned · Aug 1, 2007 · N799AL · Doug DC862 · Fuel Controlling System
  > DURING CRUISE FROM WSAP TO RJTY NR 1 ENGINE LOST POWER EPR REDUCED 1.2 AND FUEL FLOW DECREASED 1000 POUNDS PER HOUR. THE CREW PERFORMED THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE ENGINE, THE AIRCRAFT LANDED AT RJTY WITHOUT INCIDENT. MAINTENANCE INSPECTED
- [SDR IXXA07SMN106S](https://openairdocs.org/sdr/IXXA07SMN106S.md): Door Frame · cracked · Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "A" DOOR AFT LOWER JAMB CORNER CRACKED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND, AFTER TRIM OUT. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER. CLEANED, TREATED
- [SDR IXXA07SMN105S](https://openairdocs.org/sdr/IXXA07SMN105S.md): Vane · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STATION XS 515.720 AND XS 520.168. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROS
- [SDR IXXA07SMN104S](https://openairdocs.org/sdr/IXXA07SMN104S.md): Vane · damaged · Feb 8, 2007 · N71CX · Doug DC862 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HOLES ELONGATED, BETWEEN STATION XOLDI 6.225 AND XS 435.789. REMOVED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND.
- [SDR IXXA07SMN103S](https://openairdocs.org/sdr/IXXA07SMN103S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETWEEN STATION XFS 710.000 AND XFS 716.250. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK
- [SDR IXXA07SMN102S](https://openairdocs.org/sdr/IXXA07SMN102S.md): Skin · broken · Feb 8, 2007 · N71CX · Doug DC862 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP, UPPER SKIN BROKEN AT STATION XCW 64.000. REMOVED DAMAGED PANEL PLATING. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND PANEL
- [SDR IXXA07SMN101S](https://openairdocs.org/sdr/IXXA07SMN101S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR, AT STATION XW 115.000. REMOVED PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND PLATIN
- [SDR IXXA07SMN100S](https://openairdocs.org/sdr/IXXA07SMN100S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING, OUTBORD FLAP UPPER SKIN NON STANDARD REPAIR, AT STATION XF 210.000. REMOVED PANEL PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. C
- [SDR IXXA07SMN099S](https://openairdocs.org/sdr/IXXA07SMN099S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA.. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FA
- [SDR IXXA07SMN098S](https://openairdocs.org/sdr/IXXA07SMN098S.md): Fitting · cracked · Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME, CRACKED AT STATION 759.000, LONGERON 18 LEFT. REMOVED FASTENERS. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSION FOUND. FABRICATE
- [SDR IXXA07SMN097S](https://openairdocs.org/sdr/IXXA07SMN097S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XOLDI 6.225. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND.
- [SDR IXXA07SMN096S](https://openairdocs.org/sdr/IXXA07SMN096S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XS 520.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND.
- [SDR IXXA07SMN094S](https://openairdocs.org/sdr/IXXA07SMN094S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND CORROSION AT STATION XFS 178.750. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE
- [SDR IXXA07SMN095S](https://openairdocs.org/sdr/IXXA07SMN095S.md): Fitting · cracked · Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER FITTING ANGLE CRACKED AT STATION XFS 60.000. REMOVED DAMAGED FITTING ANGLE. CLEANED, TREATED AND PRIMED. INSTALLED NEW FITTING ANGLE IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM
- [SDR IXXA07SMN093S](https://openairdocs.org/sdr/IXXA07SMN093S.md): Skin · corroded · Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR, AND REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INS
- [SDR IXXA07SMN092S](https://openairdocs.org/sdr/IXXA07SMN092S.md): Skin · corroded · Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FOUND. FABRICATED NEW
- [SDR IXXA07SMN091S](https://openairdocs.org/sdr/IXXA07SMN091S.md): Panel · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Spoilers
  > DURING ROUTINE C CHECK INSPECTION, LEFT WING OUTBORD AILERON LOWER PANEL NON STANDARD REPAIR, BETWEEN STATION XA 650.000 AND XA 693.000. REMOVED SKIN WITH EXISTING NON STANDAR REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYS
- [SDR IXXA07SMN090S](https://openairdocs.org/sdr/IXXA07SMN090S.md): Skin · misrepaired · Feb 8, 2007 · N71CX · Doug DC862 · Standard Practices/Structures
  > DURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED SKIN WITH EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA A
- [SDR IXXA07SMN089S](https://openairdocs.org/sdr/IXXA07SMN089S.md): Skin · corroded · Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT UPPER SKIN CORRODED AT STATION 1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA
- [SDR IXXA07SMN088S](https://openairdocs.org/sdr/IXXA07SMN088S.md): Skin · corroded · Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SKIN CORRODED AT STATION XFS1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AR
- [SDR IXXA070004O](https://openairdocs.org/sdr/IXXA070004O.md): Fiber Optic Gyro · precesses · Jan 26, 2007 · N799AL · Doug DC862 · Directional Gyro and Indicating System
  > APPROXIMATELY 1.5 HOURS AFTER TAKEOFF FROM WSAP THE NR 2 COMPASS STARTED PROCESSING AT THE RATE OF 60° TO 70° PER HOUR, DG MODE PROCESSING AT THE RATE OF 25° PER HOUR. THE CREW ELECTED TO RETURN TO WASP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AND CLE
- [SDR IXXA06SMN418S](https://openairdocs.org/sdr/IXXA06SMN418S.md): Fitting · corroded · Nov 17, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 530.000 RBL 45. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING FROM 7075-T651 TO 7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TR
- [SDR IXXA06SMN373S](https://openairdocs.org/sdr/IXXA06SMN373S.md): Skin · corroded · Nov 10, 2006 · N799AL · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CORRODED AT STATION XE127.960. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREA
- [SDR IXXA06SMN355S](https://openairdocs.org/sdr/IXXA06SMN355S.md): Skin · corroded · Nov 10, 2006 · N799AL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD STUB WING UPPER SKIN CORRODED AT STATION XFS246.000 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER FILLERS AND STRAP. TREATED REPAIR AREA AND REPA
- [SDR IXXA06SMN350S](https://openairdocs.org/sdr/IXXA06SMN350S.md): Skin · damaged · Nov 4, 2006 · N799AL · Doug DC862 · Ailerons
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER FASTENERS INSTALLED ON THE LEFT OUTBOARD AILERON EXTERNAL LOWER SKIN FROM STATION XA542.000 TO STATION XA566.000. REMOVED IMPROPER FASTENERS AND FOUND SKIN DAMAGED. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AN
- [SDR IXXA06SMN347S](https://openairdocs.org/sdr/IXXA06SMN347S.md): Fitting · cracked · Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION FOUND FITTING CRACKED AT STATION 742.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING FROM 7075-T651 TO 7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED,
- [SDR IXXA06SMN346S](https://openairdocs.org/sdr/IXXA06SMN346S.md): Fitting · cracked · Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 857.000, LONGERON 19 RIGHT. REMOVED CRACK FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B.
- [SDR IXXA06SMN339S](https://openairdocs.org/sdr/IXXA06SMN339S.md): Skin · corroded · Nov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORROSION AT STATION XF803.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS,
- [SDR IXXA06SMN352S](https://openairdocs.org/sdr/IXXA06SMN352S.md): Skin · corroded · Nov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS341.500. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO
- [SDR IXXA06SMN351S](https://openairdocs.org/sdr/IXXA06SMN351S.md): Skin · dented · Nov 4, 2006 · N799AL · Doug DC862 · Ailerons
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN DENTED AT STATION XA558.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFAC

Next page: https://openairdocs.org/model/douglas-dc-8-62/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 = 'DC862'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-62/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.