Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  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 IXXA080006OFire Loop · looseDURING CRUISE FROM KPHL TO KTOL, NUMBER FOUR ENGINE SHORT LIGHT CAME ON WITH NO FIRE TEST INDICATION, THE CREW ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT DOWN NUMBER FOUR ENGINE. THE CREW LANDED AT KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHTFeb 19, 2008 · N828BX · Doug DC871F · Fire DetectionSDR UPS08851691Slide · out of positionINSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REMOVED EVACUATION SLIDE AND CONTAINER PER MM 25-60-01-2. REPOSITIONED SLIDE IN CONTAINER AND INSTALLED PER MM 25-60-01-2.Feb 18, 2008 · N708UP · Doug DC871F · Escape SlideSDR IXXA08SMN081SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 857.000 LONGERON 1. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED LIQUID PENETRANT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREAFeb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN088SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LOWER FORWARD PANEL PLATING DENTED AT STATION XW 2.000 - STA XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN087SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER INNER SKIN INBOARD SPLICE CRACKED AT STATION XFS 341.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN085SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN DENTED AT STATION XE 246.875. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED ANFeb 15, 2008 · N822BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA08SMN084SSkin · misrepairedDURING ROUTINE C CHECK, FOUND AT EXTERNAL DOUBLER AFT LOWER FUSELAGE BELLY TAIL SKID FAIRING HAS IMPROPER REPAIR AT STATION FS 1745 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED SKIN. FABRICATEDFeb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN082SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FRAME FITTING CRACKED AT STATION 879.000 LONGERON 18 RIGHT TO LONGERON-19 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FITTING. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOUFeb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN089SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING CENTER LEADING EDGE OUTER SKIN LOWER SHOWS IMPROPER REPAIR AT STATION XFS 385.200. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPEFeb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN086SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE TAIL SECTION PLATING CRACKED AT STATION FS 1766.000 TO STATION 1781.000 LONGERON10 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN080SSupport Fitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SKID SUPPORT FITTING CRACKED AT STATION 1734.000 LONGERON36. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B.Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN079SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD AFT LOWER FLAP SKIN SHOWS DENTS AT STATION XE 2.000 TO STA XE 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WIFeb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN078SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS DENT AND NO STANDARD REPAIR AT STATION XA 580.000 TO XA 610.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTFeb 15, 2008 · N822BX · Doug DC871F · AileronsSDR IXXA08SMN077SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME LOWER FLANGE CRACKED AT STATION 480.000 LONGERON 34 RIGHT. REMOVED DAMAGED AREA. FABRICATED NEW FRAME SEGMENT, SPLICES, ANGLES. HEAT TREATED EXTRUSION FRAME SEGMENT. CLEANED, TREATED,Feb 14, 2008 · N822BX · Doug DC871F · Fuselage Main, FrameSDR IXXA08SMN076SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND ELEVATOR LEFT UPPER SKIN SHOWS DENTS AND CORROSION AT DIFFERENT POINTS AT STATION XE 146.000 AND XE 270.000. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGFeb 14, 2008 · N822BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA08SMN075SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XOLDI 6.2246. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Feb 14, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN074SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRAFeb 14, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN072SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN SHOWS SCRATCHES AT STATION XE 273.000 TO STATION XE 283.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED Feb 14, 2008 · N822BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA08SMN073SFlap · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBD FLAP UPPER PART SHOWS DENTS AT STATION XF 375.000 TO STA XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. Feb 14, 2008 · N822BX · Doug DC871F · Trailing Edge FlapsSDR IXXA08SMN070SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO INTERCOSTAL END CLIP CRACKED AT STATION 857.000 LONGERON 18 RIGHT. REMOVED CRACKED INTERCOSTAL END CLIP. FABRICATED INTERCOSTAL END CLIP. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND INTFeb 14, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN047SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1690.000 LONGERON 28 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-3-1, SRM 51-1-20D, AND SRM 51-Feb 14, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN071SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER AFT SKIN HAS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, Feb 14, 2008 · N822BX · Doug DC871F · Trailing Edge FlapsSDR UPS08851661Slide · out of positionINSPECTION TYPE:N/A CREW REPORTED THAT THE MAIN ENTRY DOOR SLIDE GIRT BAR WILL NOT LOCK IN TO FLOOR WITH DOOR CLOSED. REPACKED MAIN ENTRY DOOR SLIDE IAW MM 25-60, OPS CHECK GOOD.Feb 12, 2008 · N708UP · Doug DC871F · Escape SlideSDR UPS08851653Bracket · brokenEVAC SLIDE PSI AND EXPIRATION ILLEGIBLE FROM INSPECTION WINDOW. EVAC SLIDE COVER LATCH BRACKET IS BROKEN. SLIDE COVER REMOVED AND ROUTED FOR REPAIR INSTALLED LATCH AS REQUIRED PER SRM 51-01-21A. REINSTALLED SLIDE INSIDE COVER AND ON TO AIRCRAFT, REF MM 25-6Feb 11, 2008 · N708UP · Doug DC871F · Escape SlideSDR UPS08851654Skin · gougedRIGHT INBOARD T/E FLAP LOWER SURFACE DENT AT INBOARD LOCATION. MEASURE DENT AT 1 1/4 BY 1 3/4 .063 DEEP. FOUND .015 GOUGE IN DENT AND BLENDED TO .019 DEEP. REMOVED DAMAGE PER SRM 57-02-05. VERIFIED DAMAGED REMOVED. OK TO INSTALL DOUBLER. INSTALLED DOUBLEFeb 10, 2008 · N708UP · Doug DC871F · Trailing Edge FlapsSDR IXXA08SMN065SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN FORWARD SHOWS DENTS BETWEEN STATION XF 160.000 - XF 213.000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK NO CORROSION FOUND. PERFORMED MEASUREMENT DIA 2.00 BY 0.008" DEPTH WITHIN PERMFeb 8, 2008 · N822BX · Doug DC871F · Trailing Edge FlapsSDR IXXA08SMN067SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 847.000 LONGERON1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8-B, DC8 SRM 51-1-2Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN63SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN SHOWS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED TREAFeb 8, 2008 · N822BX · Doug DC871F · Trailing Edge FlapsSDR IXXA08SMN062SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 SRM 51-1-21, AND DC8 SRM 51-Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN061SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 TO STATION 980.000 LEFT BUTTOCKS LINE 45. REMOVED CORRODED FITING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN066SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 690.000 LONGERON 1. REMOVED CRACKED 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.Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN064SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN DENTS AT STATION XF 169.000 - XF 213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANFeb 8, 2008 · N822BX · Doug DC871F · Wing, Plate/SkinSDR IXXA08SMN054SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN SCRATCHED BETWEEN STATION XA 737.000 AND XA 763.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH Feb 7, 2008 · N822BX · Doug DC871F · AileronsSDR IXXA08SMN053SSupport Angle · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FORMER CRACKED AT STATION 1766.000 LONGERON1. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE ON END CRACK. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT CLEANED, TREATED AND PRIMEFeb 7, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN052SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 20 RT. REMOVE CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-1, SRM 51-1-20D, AND SRM 51-1-8B.Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA08SMN058SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RUDDER RIGHT SKIN SIDE DENTED AT STATION ZR 276.531 TO ZR 267.218. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLFeb 7, 2008 · N822BX · Doug DC871F · Rudder, Plate/SkinSDR IXXA08SMN051SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN SHOWS IMPROPER REPAIR AT STATION XE 50.000 TO XE 132.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEFeb 7, 2008 · N822BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA08SMN060SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 1. REMOVED CRACKED 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. Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Internal StairsSDR IXXA08SMN057SFitting · crackedDURING ROUTINE C CHECK, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALL NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN056SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 960.000 LONGERON19 LEFT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSFeb 7, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN055SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 759.000 LONGERON 11 RIGHT. REMOVED (CRACKED) FITTING. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA08SMN059SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE LONGERON 17 RIGHT CRACKED AT STATION 1766.00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FASTENERS AND LONGERON SEGMENT Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA08SMN050SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED XFS 60.000. REMOVED CRACKED FITTING. PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-14, AND 51-3-1.Feb 7, 2008 · N822BX · Doug DC871F · Horizontal Stabilizer, Attach FittingsSDR IXXA08SMN049SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 51-1-8B, AND Feb 7, 2008 · N822BX · Doug DC871F · Horizontal Stabilizer, Attach FittingsSDR UPS08851655Battery Pack · dischargedFOUND EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2.Feb 7, 2008 · N798UP · Doug DC871F · Emergency LightingSDR IXXA08SMN041SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL DOUBLER AFT LOWER FUSELAGE AFT OF L-2 DOOR WITH IMPROPER REPAIR AT STATION FS 1733 LONGERON 26 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFeb 1, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN035SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR SIDE SKIN LAP JOINT FORWARD OF AFT PRESSURE BULKHEAD AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NOFeb 1, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN034SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Feb 1, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN036SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AFT LOWER FUSELAGE BELLY AFT OF OUTFLOW VALVE "SUGAR SCOOP" AT STATION FS 1682 LONGERON 35.6 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREAFeb 1, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA08SMN048SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LT ELEVATOR UPPER SKIN SHOWS DENTS AND CORROSION AT SEVERAL POINTS BETWEEN STATION XE 50.000 AND STA XE 132.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGEDFeb 1, 2008 · N822BX · Doug DC871F · Elevator, Plate/Skin
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