Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS06848192Longeron Splice · corrodedINSPECTION TYPE:C3 L36 AFT FITTING AND LONGERON AT STA 1690 HAVE CORROSION. FOUND CORROSION OUT OF LIMITS AT STA 1690 L36 SPLICE FITTING IAW SRM 51-20-00. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1690 L36 IAW SRM 51-1-20D, AND SRM 53-02-02-00.Sep 22, 2006 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN317SLongeron · corrodedDURING ROUTINE C-CHECK, INSPECTION FOUND LONGERON 32 LT CORRODED AT STA 610.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN316SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 34 RIGHT CORRODED BETWEEN STATION 1566.000 AND STATION 1766.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIMSep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN315SFrame · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING FRAME REPAIR CORRODED AT STA 600 BETWEEN LONGERON 36 AND LONGERON 35 RT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR DOUBLER. INTERNAL FINGER DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPASep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06SMN313SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON NUMBER 2 PYLON AT STATION XAR0.000. REMOVED EXISTING NON STANDARD REPAIR FROM STATION XAR0.000 TO STATION XE60.000. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED PARTS WITH HYSOL. Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR IXXA06SMN314SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION 405.000, LONGERON 12 RIGHT. CORRECTIVE ACTION: REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED ASep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06848287Rib · crackedINSPECTION TYPE:C3 RT WING OB LE UPPER RIB CRACKED AT XFS 824. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-21, 51-01-20D.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR IXXA06SMN312SClamp · improperDURING ROUTINE C CHECK INSPECTION, FOUND ON NUMBER 2 PYLON ACCESS DOOR NUMBER 297, GENERATOR FEEDER CABLES ATTACH CLAMP IMPROPER. REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, (AL 2024 T3 0.016). BONDED BOTH PARTS WITH HYSOL. CLEANED, Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Attach FittingsSDR UPS06848094Doubler · crackedINSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 597. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21,51-1-20D AND DWG 5769600.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Plate/SkinSDR UPS06848058Doubler · crackedINSPECTION TYPE:C3 RT WING OB LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS566. REMOVED, FABRICATED AND INSTALLED INNER DOUBLER AND FILLER IAW DWG 5769600, SRM 51-1-21 AND 51-1-20D.Sep 21, 2006 · N708UP · Doug DC871F · Wing Main, Frame StructureSDR UPS06848047Rib · crackedINSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS 653. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848046Rib · crackedINSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS659. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848045Rib · crackedINSPECTION TYPE:C3 RT WING OB LE LWR RIB CRACKED AT XFS772. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848044Rib · crackedRT WING OB LE LWR RIB CRACKED AT XFS 734. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 51-1-20D,51-1-21.Sep 21, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848022Slide · inoperativeMAIN CABIN EXIT SLIDE/SLIDE INOP, LOW PRESSURE. REMOVED AND REPLACED SLIDE ASSY PER 25-60-01-2. CLEARED, PLACARD REMOVED AND BOTH COURIER SEATS REACTIVATED.Sep 21, 2006 · N706UP · Doug DC871F · Escape SlideSDR UPS06848289Rib · crackedINSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848288Rib · crackedINSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002, 51-01-21, AND 51-01-20D.Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848286Rib · crackedINSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS 379. CRACK TERMINATES AT FASTENER HOLE. FABRICATED REPAIR ANGLES AND INSTALLED IAW DC-8 SRM 57-02-00-0 AND 51-01-20D.Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848285Rib · crackedINSPECTION TYPE:3C RT WING CENTER LE UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848284Rib · crackedINSPECTION TYPE:C3 RT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED IAW DC-8 SRM 57-02-00-0 FIG 002 AND 51-01-20D.Sep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848242Skin · corrodedINSPECTION TYPE:C3 AFTER REMOVAL OF CORROSION AT LWR D-PIT DOOR, SKIN, FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED D-PIT SKIN FROM 1350-1490 L31L-L31R IAW SRM 51-1-21 AND 51-1-20D.Sep 20, 2006 · N708UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS06848033Rib · crackedINSPECTION TYPE-C3 RT CENTER L/E UPPER RIB CRACKED AT XFS 366. STOPDRILLED CRACK AT RT L/E CENTER UPPER RIB AT XFS 366 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT RT L/E CENTER UPPER RIB AT STA XFS 366 IAW SRM 57-02-00 FIG 002 AND SRMSep 20, 2006 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06848290Fitting · crackedINSPECTION TYPE:C3 AT STA 742.2 FRAME FITTING IS CRACKED ON AFT UPPER SIDE OF CUSP. REMOVED AND REPLACED FRAME FITTING IAW DC-8 SRM 51-01-20D AND 51-01-21.Sep 19, 2006 · N708UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06848218Cusp Web · corrodedINSPECTION TYPE:C3 UPPER CUSP FROM STA 1260 TO 1290 EXFOLIATED CORROSION ON UPPER CUSP AND CRACKED LT SIDE. REMOVED DAMAGED CUSP AT STA 1260-1290 IAW SRM 51-3-0 AND SRM 51-1-8. REPAIRED DAMAGED CUSP AT STA 1250-1290 IAW SAA EA NR 008-5300-01-A0455 REV B, UPSSep 19, 2006 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06848059Skin · crackedINSPECTION TYPE:C3 NR 1 PYLON INBD SIDE FOUND CRACK AT APPROX STA YN 321. STOP DRILLED CRACK. CRACK TERMINATES AT STOP DRILL EO DC8-5740-0716.Sep 19, 2006 · N708UP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR UPS06848011Window · stuckF/O SLIDING WINDOW WILL NOT OPEN. PERFORMED ADJ/TEST OF F/O SLIDING WINDOW IAW MM 56-10-03-5. NO DEFECTS NOTED. OPS CHECK GOOD.Sep 19, 2006 · N715UP · Doug DC871F · Flight Compartment WindowsSDR IXXA06SMN308SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND FITTING CRACKED STA 1220.000 BETWEEN LONGERON 27 RT AND LONGERON 29 RT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION, NO CRACKS FOUND. CLEANED, TREATED AND PRISep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN310SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR LEFT TRAPEZOIDAL FITTING WEB CRACKED AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND REINSTALLED INBOARD AND OUTSep 18, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA06SMN309SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FRAME FITTING CRACKED AT STATION FS 1160.000 LONGERON 27 RIGHT RBL 44. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TRSep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN307SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA, AND FITTING. INSTALLED FITTING. IAW Sep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN311SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND NON STANDARD REPAIR ON THE LEFT HAND SIDE OF THE RUDDER FROM STATION ZR 178.000 TO STATION ZR 188.781. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040). CLEANED, TREATED, AND PRIMED AREA, Sep 18, 2006 · N825BX · Doug DC871F · Rudder, Plate/SkinSDR UPS06848062Fitting · crackedINSPECTION TYPE:C3 BATHTUB FITTING CRACKED AT STA 280 BETWEEN L35L-L36. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 53-02-00-0 FIG 002D AND 51-1-20D.Sep 18, 2006 · N729UP · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN306SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR RIGHT HAND TRAPEZOIDAL FITTING OUTBOARD FLANGE CRACKED, AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND OUTBOARSep 15, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA06SMN300SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION -12 LONGERON 27 LEFT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN305SFitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 240.000 LONGERON 36. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA, AND FITTING.Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN304SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 75.000, LONGERON 29 LEFT. REMOVED CORROSION. FOUND OUT ALLOWABLE LIMITS. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21, DC-8 SRM 5Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA06SMN301SFrame · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND FRAME WITH NON STANDARD REPAIR AT STATION 1580.000 BETWEEN LONGERON 20 LT AND LONGERON 21 LT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRICSep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06SMN303SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACKED LONGERON AT STATION 1770.000 LONGERON 17 LEFT. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA, AND NEW LONGERON. INSTALLED LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-1-0, DC-8 SRM 51-1-20D, Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN302SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED LONGERON AT STATION 1776.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA, AND NEW LONGERON. INSTALLED NEW LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-5-1 FIG 7 SHEET 1 Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA06SMN293SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION FS 29 LONGERON 9.75 LT, DOES NOT MEET CURRENT SRM CRITERIA. REMOVED EXISTING REPAIR. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMEDSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN299SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN CRACKED AT STATION XFS360.000. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. APPLIED SEALANSep 12, 2006 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN286SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 370 LONGERON 30.5 RIGHT DOES NOT MEET DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN292SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND PASSENGER DOOR UPPER AFT CORNER. REPAIR FALLS INTO GROUP 2 PER SERVICE BULLETIN DC 8 53.075, AND AD 2000-20-08 GROUP 2. WITHIN 2,000 LANDINGS OR 3 YEARS AFTER THE EFFECTIVE DATE ACCOMPLISH THE PREVENTATIVE MODIFICATIONSep 12, 2006 · N825BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA06SMN296SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP EXISTING UPPER SKIN DOUBLER IMPROPER AT STATION, XW38.000. REMOVED EXISTING SKIN WITH EXISTING IMPROPER REPAIR. FABRICATED NEW SKIN WITH AL 2024 T3 0.025” AND BONDED DOUBLER AL 2024 T3 0.020”. BONDSep 12, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN295SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING IB FLAP EXISTING LOWER. SKIN DOUBLER IMPROPER FROM STATION XW2.000 TO XW91.000. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED ARESep 12, 2006 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN289SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 1430 LONGERON 36 IN CLOSE PROXIMITY TO ANOTHER EXISTING REPAIR AT THE LOWER SIDE OF (D) PIT DOOR. INCORPORATED BOTH REPAIRS INTO ONE REPAIR. (D) PIT DOOR CORNER REPAIR. REMOVED EXISTING RESep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN287SSkin · misrepairedDURING ROUTINE, C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 1384 LONGERON 35.5 RT DOES NOT MEET THE DTA REQUIREMENTS OF MDC 91K0262. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TOSep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN285SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER EXISTING REPAIR AT STATION 370 LONGERON 25.5 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMESep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN284SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 248, LONGERON 26 RIGHT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN282SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 8 LONGERON 28.5 RIGHT DOES NOT MEET THE DTA REQUIREMENTS OD MDC 91K0262. REMOVED EXISTING REPAIR DOUBLER. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEASep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
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