Douglas DC-8-62F

Service difficulty reports · 1,163

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'DC862F'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IXXA06SMN398SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING REPAIR OUTBOARD LEADING EDGE UPPER SKIN HAS A NON STANDARD REPAIR AT STATION XFS566.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND ANov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN388SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LEADING EDGE INTERNAL FORWARD FITTING CRACKED AT STATION XW92.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, AND DC8 SRM 51-1-8B.Nov 17, 2006 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA06SMN384SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD LEADING EDGE UPPER SKIN DOUBLER CORRODED AT STATION XFS195.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED PANEL WITH EXISTING DOUBLER. FABRICATED NEW PANEL. CLEANED, TREATED AND PRIMNov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN375SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND WING CENTER SECTION FITTING CRACKED AT STATION 759.000 RBL-24. REMOVED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, AND DC8 SRM 51-3-1.Nov 17, 2006 · N799AL · Doug DC862F · Wing, Center BoxSDR IXXA06SMN402SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE TAIL CONE LEFT SIDE EXTERIOR SKIN CRACKED AT STATION 1756.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREANov 17, 2006 · N799AL · Doug DC862F · Aerodynamic FairingsSDR IXXA06SMN401SLongeron · crackedDURING ROUTINE C CHECK INSPECTION FOUND LONGERON 17 RIGHT CRACKED AT STATION 1610.000. REMOVED CRACK LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON. IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-Nov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA06SMN397SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING HAS A NON STANDARD REPAIR ON THE LOWER SKIN AT STATION XFS566.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FNov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN396SRepair · improperDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR LOWER SKIN HAS A NON STANDARD REPAIR AT STATION XE272.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRNov 17, 2006 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA06SMN395SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AT STATION XFS47.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND RNov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN394SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED AT STATION XE198.0039. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. ANov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN393SBeam · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND WHEEL WELL PRESSURE PANEL BEAM LOWER FLANGE CORRODED AT STATION 902.000, LBL62” TO LBL69. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED 02 EACH EXISTING SPLICE ANGLES AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTNov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, StructureSDR IXXA06SMN392SBeam · crackedDURING ROUTINE C CHECK INSPECTION, FOUND WHEEL WELL PRESSURE PANEL BEAM LOWER FLANGE CORRODED AT STATION 902.000 FROM RBL62” TO RBL69”. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED 02 EACH EXISTING SPLICE ANGLES AND REMOVED DAMAGE. PERFORMED NDT INSPECTNov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, StructureSDR IXXA06SMN379SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LEADING EDGE UPPER SKIN HAS A NON-STANDARD REPAIR AT STATION XF227.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. AFTER Nov 17, 2006 · N799AL · Doug DC862F · AileronsSDR IXXA06SMN391SHinge Fitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP RIGHT INBOARD HINGE FITTING CRACKED AT STATION XW94.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, DC8 SRM 51-1-8B, AND DC8 SRM 51-3-1.Nov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN390SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN DENTED AT STATION XA665.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. APPLIED SEALNov 17, 2006 · N799AL · Doug DC862F · AileronsSDR IXXA06SMN389SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE272.000 TO STATION XE301.656. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRINov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN387SSkin · nickedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LOWER SKIN NICKED AT STATION XW32.000. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. BONDED PARTS AS REQUIRED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTNov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN383SPressure Panel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR WHEEL WELL PRESSURE WALL SKIN CORRODED AT STATION 902.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. Nov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, BulkheadSDR IXXA06SMN382SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR WHEEL WELL PRESSURE WALL SKIN CORRODED AT STATION 902.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE RENov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN381SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING LOWER SKIN DRAIN HOLE CRACKED AT STATION XFS597.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMANov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN380SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER SKIN HAS A NON-STANDARD REPAIR AT STATION XF210.000. REMOVED SKIN WITH NON STANDARD REPAIR FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND INTERNAL SURFACE OF NEW SKNov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN378SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER SKIN HAS A NON-STANDARD REPAIR AT STATION XW90.000. REMOVED DAMAGED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND INTERNAL SURFACENov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN377SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER SKIN HAS A NON-STANDARD REPAIR AT STATION XW105.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED Nov 17, 2006 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA06SMN376SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP TRAILING EDGE PANEL UPPER SKIN HAS A NON-STANDARD REPAIR AT STATION XW83.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED REPAIR PARTS. BONDED NEW PARTS AS NEEDED WITH HYSOL. CLNov 17, 2006 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA06SMN364SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 902.000 LONGERON 5 LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED FROM 7075-T6-51 TO 7075-T6 PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. INSTALLED NEW FITTINov 10, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN371SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CRACKED AT STATION XE87.000. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACNov 10, 2006 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA06SMN370SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN DELAMINATED AT STATION XE50.000. REMOVED DELAMINATED SKIN. FABRICATED REPAIR PARTS. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYINNov 10, 2006 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA06SMN366SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 780.000 LBL-22. REMOVE CRACKED FITTING CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.Nov 10, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN363SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 902.000 LONGERON 7 LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED FROM AL7075-T651 TO 7075-T6. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. INSTALLED NEW FINov 10, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN362SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 857.000 LONGERON 2 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING FROM 7075-T6 51 TO 7075-T6. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. INSNov 10, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN361SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 857.000 LONGERON 3 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. HEAT TREATED FROM AL 7075-T6 51 TO AL7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. INSTALLED NEWNov 10, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN359SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED FROM STATION XE52.822 TO STATION XE75.672. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYINNov 10, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN372SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR TRAILING EDGE UPPER SKIN CORRODED BETWEEN STATION XE71.250 AND XE198.039. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURNov 10, 2006 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA06SMN374SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND ELEVATOR UPPER SKIN CORRODED AT STATION XE28.843. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMEDNov 10, 2006 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA06SMN369SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR SKIN CRACKED AT STATION 1586.000 BETWEEN LONGERON 20 LEFT TO LONGERON 21 LEFT. REMOVED FASTENERS AS NEEDED TO ACCOMPLISH REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLNov 10, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN368SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION , FOUND RIGHT WING OUTBOARD AILERON AT STATION XA656.000 HAS A NON STANDARD REPAIR. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED ANDNov 10, 2006 · N799AL · Doug DC862F · AileronsSDR IXXA06SMN367SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR AT STATION XF304.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. APPLIED SEALANT TO FANov 10, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN365SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A FITTING SPLICE CRACKED AT STATION 690.000, LONGERON 1. REMOVED DAMAGED SPLICE FITTING. FABRICATED NEW SPLICE FITTING. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND NEW SPLICE FITTING. INSTALLED NNov 10, 2006 · N799AL · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA06SMN360SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING DOUBLER CORRODED, LOWER CENTER WING AREA AT STATION XCW10.000, STRINGER 62. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, FABRICATED Nov 10, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN358SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE29.812 TO STATION 763.844. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRIMENov 10, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN357SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE75.000 TO STATION XE147.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRIMENov 10, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN354SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND RIGHT WING INTERNAL LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS157.000 TO STATION XFS163.750. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERNov 10, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN353SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORRODED STATION XF195.500 UPPER SIDE. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED NEW SKIN Nov 10, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN342SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 680.000, LONGERON 11 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.Nov 4, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN210SSkin · dentedDURING ROUTINE C CHECK INSPECTION, RT WING.- OTBD AILERON UPPER SKIN DENTED , XA 737.000 - XA 755.000.Jun 30, 2006 · N41CX · Doug DC862F · AileronsSDR IXXA06SMN198SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E UPPER SKIN CORRODED BETWEEN XW 257.000 AND XW 261.000.Jun 30, 2006 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN197SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING.- INBD L/E UPPER SKIN CORRODED BETWEEN XFS 207.000 AND XFS 211.000.Jun 30, 2006 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN196SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT WING.- INBD L/E UPPER SKIN CRACKED 2" APPROX BETWEEN XFS 204.000 AND XFS 207.000.Jun 30, 2006 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN213SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD AILERON UPPER SKIN DENTED, XA 662.000.Jun 30, 2006 · N41CX · Doug DC862F · AileronsSDR IXXA06SMN212SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING.- OTBD AILERON UPPER SKIN DENTED, XA 669.000.Jun 30, 2006 · N41CX · Doug DC862F · Ailerons
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