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 IXXA07SMN139SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 445, LONGERON 27.5 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER AND INTERNAL DOUBLER, CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SUApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA070029SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN,Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN135SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 LEFT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN141SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION 1.600 LONGERON 28 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, INTERNAL DOUBApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN146SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP CRACKED ON UPPER PART EXTERNAL COATING AT STATION XW 104.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANTApr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/SkinSDR IXXA07SMN150SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE WITH A CRACK AT STATION 1580.000 LONGERON 21LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT. PERFORMED HEAT TREATMApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, FrameSDR IXXA07SMN158SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FRAME WITH A CRACK AT STATION 1260.000 LONGERON 34 RIGHT TO LONGERON 35 LEFT. REMOVED CRACKED FITTING. FABRICATED FRAME FITTING, SPLICES, AND DOUBLER. PERFORMED HEAT TREATMENT. PERFORMED NDT INApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, FrameSDR IXXA07SMN144SHook · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE AT NOSE SECTION FORWARD PAX DOOR HOLD OPEN HOOK, WAS CRACKED AT STATION 15.000 LONGERON 16 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT INApr 21, 2007 · N828BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA07SMN136SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL JOINT FITTING WITH CORROSION AT STATION 940.000 LONGERON 24 RIGHT. REMOVED CORROSION. FOUNDED OUT OF LIMITS REMOVED CORRODED FITTING. FABRICATED FRAME FITTING, SPLICES AND DOUBLER. Apr 21, 2007 · N828BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA07SMN145SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BATH TUB FITTING CORRODED, BETWEEN STATION 70.000 AND STATION 80.000 LONGERON 35 RIGHT. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN147SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR. UPPER SKIN DENT WITH CRACK AT STATION XE 156.468 AND STATION XE 161.375. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL REPAIR PARTS. BONDED PARTApr 21, 2007 · N828BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA07SMN148SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 RIGHT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGUREApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN149SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 LEFT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGUREApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN152SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAD CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 LEFT BOTTOM LINE 40”. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN151SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, IN MAIN CARGO COMPARTMENT, FOUND CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 RIGHT BOTTOM LINE 40". REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN157SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAD A NON STANDARD REPAIR AT STATION XFS 426.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER NDT TEST. Apr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/SkinSDR UPS07849666A/C Pack · odorINSPECTION TYPE:N/A STALE ODOR IN FLIGHT APPEARS TO COME FROM RIGHT PACK. NO SMELL NOTED WHEN LEFT PACK RAN. TRANSFERRED RIGHT PACK INOP PER MEL 21-38-1. DEFERRAL M348809. PERFORMED ADJ/TEST OF RT PACK W/NO DEFECTS NOTED PER MM 21-55-00-5. DEFERRAL CLEAREDApr 21, 2007 · N718UP · Doug DC871F · Cabin Cooling SystemSDR UPS07849665Slide · out of positionINSPECTION TYPE:N/A CREW DOOR ESCAPE SLIDE PRESSURE INDICATOR IS BELOW VIEWING WINDOW. REPOSITIONED SLIDE SO THAT PRESSURE INDICATOR IS BETTER VISIBLE.Apr 21, 2007 · N729UP · Doug DC871F · Escape SlideSDR UPS07849616Slide · out of positionINSPECTION TYPE:N/A DOOR SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED AT SDF. GIRT BAR WAS CORRECTLY STOWED. REINSTALLED SLIDE PER AMM 25-60-01-2.Apr 13, 2007 · N718UP · Doug DC871F · Escape SlideSDR IXXA07SMN159SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON33 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED TREATED AND PRIMEDApr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN160SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED NDT. NO CRACK OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPApr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS07849607Unknown · odorINSPECTION TYPE:N/A THERE IS AN EXTREMELY FOUL -DIRTY SOCK- ODOR IN THE COCKPIT WITH PACKS ON. ACCOMPLISHED ADJ/TEST OF BOTH PACK SYSTEMS DURING ENGINE RUN. REF MM 21-50-00-5. ALL SYSTEMS CHECK NORMAL. NO ODORS NOTED. NO HISTORY.Apr 8, 2007 · N718UP · Doug DC871F · Air Distribution SystemSDR UPS07849557Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP, OP PRE-DEP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OP CHECKS GOOD PER MM 33-50-01-2.Mar 26, 2007 · N700UP · Doug DC871F · Emergency LightingSDR IXXA070018SSkin · crackedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 9. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRMar 22, 2007 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA070017SSkin · crackedDURING ROUTINE CPCP INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74 STRINGER 16. REMOVED DAMAGE AREA, NO CRACK'S OR CORROSION FOUND AFTER DAMAGE REMOVED. MANUFACTURED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIMar 22, 2007 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA070016OProximity Sensor · defectiveDURING CLIMB OUT OF KTOL AFTER GEAR WAS RETRACTED THE DOOR LIGHT REMAINED ON AFTER UPLATCH CHECK. THE CREW DID ALL NECESSARY PROCEDURES AND RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PROXIMITY CONTROL SWITCH FAILED BITE TEST. MAINTENANCMar 17, 2007 · N820BX · Doug DC871F · Landing Gear Position and WarningSDR UPS07849499Indicator · dislodgedDOOR SLIDE PRESS INDICATOR SLIDE OUT OF SIGHT. CANNOT READ. REPACKED/REPOSITIONED SLIDE INDICATOR, NOW IN VIEW.Mar 14, 2007 · N705UP · Doug DC871F · Escape SlideSDR UPS07849428Light · inoperativeON CREW PREFLIGHT, FOUND EMERGENCY LIGHTS INOP AWAITING CLOSING LP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-50-01-2. CHECKS GOOD.Mar 14, 2007 · N750UP · Doug DC871F · Emergency LightingSDR IXXA070013OUnknown · malfunctionedDURING CLIMB-OUT OF KTOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER A SATISFACTORY GEAR UP-LATCH CHECK. THE CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN LANDING GEAR DOOR SYSTEM AND REPLACED THE DOOR ACTUATORS, CONTROL VALVESMar 8, 2007 · N829BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR UPS07849334Girt Bar · malfunctionedINSPECTION TYPE:N/A GIRT BAR WILL NOT LATCH IN PLACE TO ARM THE SLIDE CHUTE WHEN DOOR IS CLOSED. REPOSITIONED SLIDE ON DOOR PER MM 25-60-00. OPS CHECK OK.Mar 6, 2007 · N772UP · Doug DC871F · Escape SlideSDR UPS07849327Battery · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW MM 33-50-01.Mar 5, 2007 · N708UP · Doug DC871F · Emergency LightingSDR IXXA07SMN132SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER HAS ELONGATED HOLES AT LEADING EDGE STATION XFS 285.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER Mar 3, 2007 · N820BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA070010SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 14. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVEFeb 23, 2007 · N820BX · Doug DC871F · Wing, Plate/SkinSDR IXXA070009SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 12. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVEFeb 23, 2007 · N820BX · Doug DC871F · Wing, Plate/SkinSDR UPS07849226O-Ring · leakingINSPECTION TYPE:N/A EMERGENCY DECLARED - AT TOP OF DESCENT FLUID DROPPED TO AUX POSITION PERFORMED LOSS OF FLUID ON PRESSURE CHECKLIST. AS PER QRH LANDING & TAXI IN NORMAL. FLUID INDICATION NEVER DROPPED BELOW AUX POSITION. FOUND LEFT MLG BOGIE SWIVEL UNLOCFeb 21, 2007 · N703UP · Doug DC871F · Landing Gear Retraction/Extension SystemSDR UPS07849343Attach Fitting · crackedINSPECTION TYPE:C3 1ST CLIP FROM FWD C/S IS CRACKED NR 4 PYLON O/B SKATE ANGLE. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-1-20D, DWG 5804007.Feb 20, 2007 · N701UP · Doug DC871F · Nacelle/Pylon, Main FrameSDR UPS07849288Skin · crackedINSPECTION TYPE:C3 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE R-2 DOOR FWD UPPER CORNER APPROX .50 INCH IN LENGTH. CUT OUT DAMAGED AREA OF THE R-2 DOOR FWD UPPER CORNER IAW SRM 53-02-00 FIG 16, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SFeb 20, 2007 · N701UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS07849243Web · crackedINSPECTION TYPE:C3 NR 2 MAIN TANK THRU PNL 506C WEB IS CRACKED FWD OF CTR/SPAR XRS -6. STOP DRILLED CRACK AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-Feb 20, 2007 · N701UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS07849370Floorbeam · corrodedINSPECTION TYPE:C3 HEAVY CORROSION & EXFOLIATION ON AFT SIDE OF FLOORBEAM, C-PIT TUNNEL LT SIDE STA 1260 LBL 59. REPAIRED FLOORBEAM AT STA 1260 LBL 59 IAW SAA EA 008-5310-01-A0693 UPS RAA DC8-53-20612, AND FAA FORM 8100-9.Feb 17, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07849289Floorbeam · corrodedINSPECTION TYPE:C3 HEAVY CORROSION ON TOP OF FLOORBEAM AFT ACCY COMPT STA 1580 RBL 50-60, FWD SIDE. CUT OUT CORRODED AREA ON FLOORBEAM AT STA 1580 RBL 50-60 IAW SRM TR 51-2-1. FABRICATED AND INSTALLED REPAIR FILLER, REPAIR ANGLES AND SPLICE ANGLES IAW SRM TRFeb 17, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07849266Frame · corrodedINSPECTION TYPE:C3 C-PIT STA 1040 FRAME FROM L35L-L35R HAS EXFOLIATION CORROSION. REMOVED DAMAGED AREA OF FRAME CAP AT STA 1040 IAW SRM 51-1-21, AND DWG 53A-011-A. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP AT STA 1040 FROM L35L-L35R IAW DWG 2537716, DWFeb 16, 2007 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS07849372Floorbeam · crackedINSPECTION TYPE:C3 CRACKED END FITTING ON FLOORBEAM AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER REMOVED FLOORBEAM END FITTING AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER IAW SRM 51-1-20D. FABRICATED AND INSTALLED FLOORBEAM END FITTING AT STA 2Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07849280Support Angle · missingINSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX SUB FLOOR FRAME FITTING SUPPORT ANGLE MISSING AT STA 740 L22R. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 51-3-2, 51-1-20D AND DWG 2892086.Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Main, StructureSDR UPS07849240Support Channel · crackedINSPECTION TYPE:C3 SUPPORT CHANNEL CRACKED AT STA 1730 RBL 20. REMOVED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-3-0, AND DWG 5755032.Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA070008OLimit Switch · damagedDURING CLIMB-OUT OF KTOL, AFTER SATISFACTORY UPLATCH CHECK, THE MAIN LANDING DOOR LIGHT REMAINED ILLUMINATED. THE CREW COMPLIED WITH THE ABNORMAL PROCEDURES AND CONTINUED THE FLIGHT TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED WIRING OF THE RIGFeb 15, 2007 · N829BX · Doug DC871F · Landing Gear Door Retract SectionSDR UPS07849249Web · crackedINSPECTION TYPE:C3 CABIN STA 3.0 RBL 45 SUBFLOOR WEB IS CRACKED. STOP DRILLED CRACK ON WEB AT STA 3.0 RBL 45 IAW SRM 53-2-00 FIG 001B. FABRICATED AND INSTALLED REPAIR DOUBLER AT SUBFLOOR STA 3.0 RBL 45 IAW SRM 53-02-00-0 FIG 001D, AND SRM 51-1-20D.Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849245Beam · crackedINSPECTION TYPE:C3 CRACK IN RADIUS OF NR 3 J-BEAM, 60 COMPT RBL 2. STOP DRILLED CRACK IN RADIUS OF NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05. FABRICATED AND INSTALLED REPAIR DOUBLER, AND ANGLE IN RADIUS OF THE NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05-Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849232Floor Support · crackedINSPECTION TYPE:C3 CABIN SUBFLOOR STA 25-48 RBL 10 FLOOR SUPPORT ANGLE IS BROKEN. REMOVED FLOOR SUPPORT ANGLE AT CABIN SUBFLOOR AT STA 25-48 RBL 10, REPAIRED FLOOR SUPPORT ANGLE AT STA 25-48 RBL10 IAW SRM 51-01-19, AND SRM 51-3-2.Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849413Frame · crackedINSPECTION TYPE:C3 CRACK IN DRILL START IN FRAME ON OUTBOARD LWR SIDE OF NR 3 ENG STUB WING. STOP DRILLED CRACK IN FRAME AT RIGHT STUB WING STA 252.351 IAW SRM 54-2-0, AND SRM TR 54-38. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER AT RIGHT STUB WING STAFeb 13, 2007 · N701UP · Doug DC871F · Wing SparSDR UPS07849371Boss · corrodedINSPECTION TYPE:C3 LEFT MLG RETRACT PIN BOSS HAS PITTING AND TOOLING MARKS. REMOVED AND REPLACED LEFT MLG SHOCK STRUT ASSY IAW 32-11-00, RETRACT AND EXTENSION CHECKS GOOD IAW 32-11-00.Feb 13, 2007 · N701UP · Doug DC871F · Fuselage, Landing Gear Attach Fittings
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