Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA00387Intercostal · crackedMAIN CARGO DOOR INTERCOSTAL IS CRACKED AT DOME NUT FOR UPPER BOLT TO FORWARD UPPER HOIST ATTACH POINT. INSTALLED NEW INTERCOSTAL REF SRM 51-30-2 PAGE 2 ITEM 4B. CLASSIFIED AS A MAJOR REPAIR.Feb 8, 2007 · N284FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA00386Angle · crackedLT AFT W/W EMERGENCY EXIT HATCH SEAL ANGLE FLANGE HAS 2 CRACKED OUT FASTENERS HOLES ONE LOCATED UPPER SEAL ANGLE, ANOTHER LOCATED LOWER AFT SEAL ANGLE. REMOVED AND REPLACED 1 ANGLE. REMOVED FABRICATED, HEAT TREATED, TREATED AND PRIMED 1 ANGLE REF SRM 51-30Feb 8, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00385Angle · crackedRT FWD O/W EMERGENCY EXIT HATCH SEAL ANGLE UPPER FORWARD CORNER 3 EACH HOLES ARE CRACKED OUT. REMOVED AND REPLACED 1 ANGLE. REMOVED, FABRICATED, HEAT TREATED AND PRIMED 1 ANGLE. REF SRM 51-30-2 PGS 1-7. REPAIR CLASSIFIED AS MAJOR. REF SRM 51-10-2 PAGE 2Feb 8, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00384Angle · crackedRT AFT WO EMERGENCY EXIT HATCH SEAL ANGLE HAS 5 EACH HOLES THAT ARE CRACKED OUT ALONG FWD EDGE OF HATCH. FABRICATED NEW SEAL ANGLE REF DWG 50-7978. TREATED AND PRIMED ANGLE REF SRM 51-10-2 AND MM 51-20-031-7 AND INSTALLED ANGLE REF SRM 51-30-2.Feb 8, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00383Angle · corrodedRT FORWARD O/W EMERGENCY EXIT HATCH, 5 EACH SEAL ANGLES ARE CORRODED. VERIFIED ORIGINAL MATERIAL ON ALL 5 ANGLES TO BE .040". THE FOLLOWING ANGLES WERE OUT OF LIMITS: P/N'S 50-7978-65 AT .031", 50-7978-67 AT .029", 50-7978-72 AT .029". ANGLE P/N'S 50-7978Feb 8, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00382Angle · corrodedLT AFT OW EMERGENCY EXIT HATCH 5 EACH SEAL ANGLES ARE CORRODED BLENDED 4 EACH SEAL ANGLES AND FOUND WITHIN LIMITS AND TREATED AND PRIMED. REMOVED AND REPLACED 1 EACH SEAL ANGLE REF SRM 51-10-6 PAGE 2, SRM 51-30-2 PAGE 2 AND SRM 51-10-1 PAGE 7.Feb 8, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00381Web · damagedMAIN ENTRY DOOR L1, INTERNAL SKIN WEB DAMAGED LOCATED AFT EDGE JUST ABOVE 8TH STOP PIN FROM THE TOP. REMOVED DAMAGE, FABRICATED REPAIR PIECES, TREAT, AND PRIMED AND INSTALLED REPAIR PARTS REF SRM 51-40-2. CLASSIFIED AS A MAJOR REPAIR.Feb 8, 2007 · N284FE · Boeing 727233 · Passenger/Crew DoorsSDR 07FDEA00365Unknown · unknownON DEP AT 200'AGL (APPROX) RED WINDSHEAR WARNING LIGHT AND AURAL WARNING. PERFORMED ESCAPE MANV. FIREWALL POWER SET FOR ABOUT 3-5 SECONDS. WINDSHEAR WARN STOPPED AND LIGHT WENT OUT. RETURNED TO MEM. NO ENG PARAMETERS APPEARED TO BE EXCEEDED. AIRSPEED WAFeb 7, 2007 · N267FE · Boeing 727233 · Standard Practices/StructuresSDR 07FDEA00363Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK I/B FLANGE IS CORRODED BS 380-400, LBL 44, WL208 BLENDED CORROSION, ACCOMPLISHED HFEC NO DEFECTS NOTED. FLAP PEENED ALL BLENDED AREAS. ALODINED AND PRIMED, AS NEEDED REF EA NR 7-5310-108847 A.Feb 7, 2007 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00362Skin · delaminatedLT IB FOREFLAP AT IB END UPPER SURFACE IS WORN AND DELAMINATED REPAIRED LT IB FOREFLAP REF SRM 51-40-20 PGS 1-63 AND REBONDED RUBSTRIP REF SRM 51-20-4 PGS 1 AND 2. TAP CHECKS GOOD. CLASSIFIED AS A MAJOR REPAIR.Feb 7, 2007 · N284FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA00354Frame · damagedAFT PIT FRAME AT STA 1148, LOWER CHORD HAS MISDRILLED HOLE JUST BELOW STR 23L REMOVED DAMAGE NDT. NO DEFECTS NOTED, FABBED AND INSTALLED SHEAR TIE ANGLE REPAIR REF SRM 51-30-2 PG 1-12, SRM 51-40-3 PG 2 FIG 1, SRM 53-10-4 PG 46-49 AND BOEING DWG 65-16348. CLAFeb 6, 2007 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA00351Floor Panel · crackedLWR AFT CARGO COMPT NR 4 FLOOR PANEL HAS SEVERAL DEEP GOUGES AND IS CRACKED THROUGH AT BS 1035 BL ''0'' CUT SHEETMATAL TO FORM OF OLD FLOOR PNL. JOGGLED EDGED, TRANSFERED FASTENER HOLES FOR PANEL, PRIMED BACK (UNDERSIDE) OF PNL. INSTALLED FASTENERS SECURING Feb 6, 2007 · N284FE · Boeing 727233 · Fuselage Floor PanelSDR 07FDEA00350Structure · failedRT WING INBD T/E WAFFLE BOARD HAS PANEL FASTENERS PULLED THROUGH AT LWR SPAR FLANGE JUST FWD OF MLG MAIN ACTUATOR REMOVED DAMAGE WAFFLE BOARD AND INSTALLED NEW SEAL AND WAFFLE BOARD IN AREA, REF SRM 51-30-2 PG 2-5.Feb 6, 2007 · N284FE · Boeing 727233 · Wing Main, Frame StructureSDR 07FDEA00349Rib · gougedNR 3 ENGINE UPPER COWL 2ND FROM FWD END RIB IS GOUGED ACCOMPLISHED TYPICAL FORMED REPAIR ON NR 3 ENG UPPER COWL REB REF SRM 51-43-3, PG 1-3 FIG 1. REINSTALLED NR 3 ENG UPPER COWL REF MM 71-10-011-4.Feb 6, 2007 · N284FE · Boeing 727233 · Nacelle/Pylon, Frame/Spar/RibSDR 07FDEA00348Stiffener · crackedLT MLG WHEEL WELL KEEL BEAM STIFFENER IS CRACKED AT BL 0, STA 930, WL 198. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED NEW STIFFENER REF SRM 51-30-2 PG 2. CLASSIFIED AS MAJOR REPAIR.Feb 6, 2007 · N284FE · Boeing 727233 · Fuselage Main, KeelSDR 07FDEA00347Panel · gougedRT WING INBD TE LWR SURFACE PANEL JUST OB OF MLG FWD TRUNNION, DELAMINATED ON UPPER SURFACE FWD EDGE. OIL SOAKED REMOVED DAMAGED PANEL ASSY. TRIED TO REMOVE DAMAGE REF SRM 51-40-9 PG 4 AND DAMAGE WAS MORE THEN 25% OF PANEL, BEYOND REPAIRABLE LIMITS REF SRM Feb 6, 2007 · N284FE · Boeing 727233 · Wing, Plate/SkinSDR 07FDEA00338Structure · damagedNR 1 PYLON HOLE ''E'' IS CONICAL IN SHAPE AND ITS MAXIMUM HOLE DIAMETER IS OUT OF LIMITS. NDT HOLE, REAMED, FABRICATED CONICAL WASHER AND INSTALLED WASHER AND FASTENER REF WRI NR 54508487 AND EA NR 7-5450-106973.Feb 5, 2007 · N284FE · Boeing 727233 · Nacelle/Pylon, Main FrameSDR 07FDEA00337Floorbeam · corrodedFLT DECK FLOORBEAM AT BS 277 HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND LBL 13. REMOVED CORROSION REF SRM 51-10-1 PG 5, MAT LOSS =.007'' HFEC, ROTO PEENED, TREATED, PRIMED, REF EA NR 7-5310-107610 AND AAR EA NR I070063.Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00336Floorbeam · gougedFLT DECK FLOORBEAM AT BS 277 UPPER SURFACE OF UPPER CHORD GOUGED AT LBL 14.5 BLEND DAMAGE, ORIGINAL THICKNESS .090'' AMOUNT REMAINING 0.075'' HFEC IAW EA# I070063, ROTO PEENED, TREATED, PRIMED, REF FED EX EA NR 7-5310-107610.Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00332Floor Support · corrodedFLT DECK FLOOR SUPPORT UPPER SURFACE CORRODED BETWEEN BS 277-266.75 AT RBL 13 REMOVED CORROSION REF SRM 51-10-1 PG 5. MAT LOSS IS .007''. HFEC IAW AAR EA I070063 REF FED EX EA NR 7-5310-107610/ WO#35039.Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00331Skin · dentedEXTERNAL FUSELAGE, STA 1422 LT SIDE. SKIN DENTED 4.0'' BELOW VERTICAL FIN Y=.080'' A=1.25'' A/Y = 15, REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, REF SRM 51-40-2, PG 1-6.Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA00322Handle · damagedFUSELAGE LOWER LOBE, NR 1 CARGO DOOR EXT HANDLE HAS EXCESSIVE PLAY AT CONTROL ROD FWD END REPLACED DOOR REF MM 52-35-011-4, PG 3 B. OPS CHECKED GOOD.Feb 5, 2007 · N284FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA00316Pan · gougedFUSELAGE LOWER LOBE NR 1 CARGO DOOR EXT HANDLE PAN LOWER SIDE IS GOUGED FROM CONTACT WITH CONTROL ROD FWD EYE BOLT AT BS 569 REF N01095. REPLACED DOOR REF MM 52-35-011-4, OPS CHECKED GOOD.Feb 5, 2007 · N284FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA00299Skin · misrepairedLT WING NR 4 SLAT REPAIR AT O/B TRACK SKIN DOES NOT CONFORM TO FEDX DWG SR 27-57-034 REMOVED AND REPLACED LT NR 4 SLAT REF MM 27-81-011.Feb 3, 2007 · N284FE · Boeing 727233 · Leading Edge DevicesSDR 07FDEA00298Floorbeam · corrodedFOUND MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 620 LBL 4-20, WL 208. INSTALLED REPAIR ON MAIN DECK FLOORBEAM UPPER CHORD AT STA 620, LBL 4 THRU 20, WL 208 REF B727 SRM 53-10-8 PG 18-23 AND DWG 53FX1547. CLASSIFIED AS A MAJOR REPAIR.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00297Frame · tool damageMAIN CABIN BS 620 BETWEEN STR S-3L AND S-4L UPPER SILL TO FRAME SPLICE AREA HAS 2. MISDRILLED HOLES AND 1 OVER CHAMFERED HOLE (VIEW FROM AFT SIDE) COMPLIED WITH EA NR 7-5310-106977 (WRI53108462) AND AAR WO NR 11701/2400/0004 PART 1, ITEM 1 THRU 10 ACCOMPLISHFeb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA00296Intercostal · tool damageINTERCOSTAL AT BS 1086, JUST ABOVE STRINGER 23R HAS A HOLE DRILLED IN RADIUS. HOLE LOCATED BELOW NUT PLATE ATTACH RIVET. DAMAGED INTERCOSTAL REMOVED NEW PART FABRICATED AND INSTALLED REF BAC DWG 65-56131, SRM 51-30-2, SRM 51-10-2 PG 7. CLASSIFIED AS A MAJORFeb 3, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00295Web · gougedFOUND MAIN DECK FLOOR WEB UPPER SURFACE IS GOUGED BS 617-620, LBL 57-60, SL 208. FABRICATED NEW WEB REF DWG 53FX1565 AND SRM 51-30-2 P3 1-12.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00294Stringer Clip · gougedFOUND STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 660 STRINGER 8L. REPLACED STRINGER CLIP, REF SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00293Stringer Clip · crackedFOUND STRINGER CLIP CRACKED IN CUT OUT RADIUS AT BS 680 STR 7L. REMOVED AND REPLACED STR CLIP AT STA 680 STR 7L REF SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00292Stringer Clip · gougedSTRINGER CLIP HAS BEEN GROUND AT THE RADIUS CUT OUT BS 440 STR 3L REMOVED STR CLIP STA 440 STR 3L. RECEIVED CLEARANCE AND INSTALLED STR CLIP REF SRM 51-30-2 PG 1. CLASSIFIED AS MAJOR REPAIR.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00291Stringer Clip · gougedSTRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 440 STR 1 BLENDED RADIUS ON STR CLIP REF SRM 53-10-4 PG 3. DAMAGE OUT OF LIMITS, REMOVED STR CLIP REF SRM 51-30-2 PG 2. VERIFY MATERIAL FOR FABRICATION OF NEW STR CLIP 7075-T6- .032 (A02779) REF BOEING DWFeb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00290Stringer Clip · damagedSTRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 380 STRINGER 2L REMOVED AND REPLACED STRINGER CLIP AT 380 STR 2L REF SRM 53-10-4 PG 3 CLASSIFIED AS MAJOR REPAIR.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00289Attach Angle · crackedRT WING LOWER T/E WING PANEL BELOW NR 12 SPOILER, OTBD ATTACH, LOWER INBD ATTACH ANGLE IS CRACKED AT ROD ATTACH AREA. REMOVED CRACKED ANGLE, VERIFIED NEW ANGLE TO BE INSTALLED AS P/N 65-21658Y29. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED NEW ANFeb 3, 2007 · N284FE · Boeing 727233 · Wing, Attach FittingsSDR 07FDEA00288Channel · corrodedAFT PIT STR 29R CORRODED IN U-CHANNEL AT SPLICE BETWEEN STA 990-1010. REMOVED CORROSION, HFEC BLEND AREA, FLAP PEENED, ALODINED AND PRIMED, INSTALLED FASTENERS WET W/ SEALANT, APPLIED CIC TO AREA, REF EA NR 7-5310-107615 AND AAR EA NR I070076.Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00287Angle · corrodedLT FWD O/W EMERG EXIT HATCH LOWER SEAL ANGLE FLANGE IS CORRODED ALONG MATERIAL SURFACE AND 3 FASTENER HOLES HAVE NO ED. REPLACED LOWER SEAL ANGLE REF SRM 51-30-2 PG 1.Feb 3, 2007 · N284FE · Boeing 727233 · Emergency ExitsSDR 07FDEA00250Indication Sys · malfunctionedAFTER LANDING LEVER PLACED DOWN, FRONT GEAR INDICATION PANEL HAD ALL 8 LIGHTS ON. PER CHECK LIST, RECYCLED LANDING GEAR, INDICATIONS NORMAL. PER CREW ACTIONS AND RESULTING NORMAL INDICATIONS, SUSPECT INDICATION ANOMALY. NO FAULTS NOTED. NO PRIOR HISTORY. Feb 2, 2007 · N285FE · Boeing 727233 · Landing Gear Position and WarningSDR 07FDEA00247Skin · delaminatedREPAIR FOUND ON THE RT OB AFT FLAP LOWER SURFACE SKIN 17" FROM IB END REQUIRED EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO BE OUT OF LIMITS. REPLACED AFT FLAP. NEW AFT FLAP INSTALLED ON SNFeb 2, 2007 · N284FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA00239Stringer · corrodedAFT PIT STR 29L CORRODED STA 999 OUTBD SIDE. REMOVED CORROSION, CHECKED MATERIAL LOSS, ORIG MATERIAL = .156". REMOVED .036", ROTO PEENED, TREATED, PRIMED, PAINTED. INSTALLED FASTENERS (2EA) REF AAR EA NR I070060.Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA00238Skin · gougedRT HORIZ STAB OUTBD BALANCE BAY PANEL UPPER SKIN, PANEL IS GOUGED ON INNER SURFACE OUTBD SIDE. REMOVED EXISTING DOUBLER, VERIFY NO DAMAGE NOTED. FABRICATED, TREATED AND PRIMED, AND REINSTALLED REPAIR. REF SRM 55-20-3 FIG 7 SHEET 1, PG 4.Feb 1, 2007 · N284FE · Boeing 727233 · Horizontal Stabilizer, Plate/SkinSDR 07FDEA00236Support Angle · crackedLT WING LOWER T/E PANEL SUPPORT ANGLE I/B OF NR 3 SPOILER ACTUATOR, I/B ANGLE IS CRACKED IN RADIUS AND AROUND ATTACH HOLE. REMOVED CRACKED SUPPORT ANGLE AND REPLACED WITH NEW SUPPORT ANGLE REF SRM 51-30-2.Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA00235Stringer Clip · crackedSTRINGER CLIP CRACKED IN RADIUS CUTOUT BS 680 STRINGER L9. REMOVED DAMAGED STRINGER CLIP, TRANSFERED FASTENER HOLES FOR NEW CLIP. INSTALLED NEW CLIP, REF SRM 51-30-2 PG 2 AND 5, SRM 51-30-5 PG 1.Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00234Stringer Clip · crackedSTRINGER CLIP CRACKED IN RADIUS CUTOUT BS 680, STR L9. REMOVED CLIP, REMOVED DAMAGE FROM CLIP, HFEC CLIP, NO DEFECTS NOTED, ALODINED AND PRIMED, INSTALLED CLIP, REF SRM 51-30-2, 53-10-4.Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00233Attach Fitting · corrodedRT MLG UPLOCK ASSY MOUNTING LUGS ON FUSELAGE BOLT HOLES CORRODED AT STA 910, WL 188 RBL 63-66. REMOVED MLG UP LOCK ASSY MOUNTING LUG, VERIFIED PART AND DRILLED PART. INSTALLED FITTING, PAINTED FITTING, REF SRM 51-30-2, 51-10-2, WO NR 11701-7000-0001.Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA00232Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK IS CORRODED AT BS 360-380, RBL 23, WL 208 REMOVED CORROSION REF SRM 51-10-6 AND EA 7-5310-108847. HFEC IAW EA 7-5310-108847. FLAP PEEN AREA REF SOPM 20-10-3 AND EA 7-5310-108847. TREAT AND PRIME AREA REF SRM 51-10-2 PG 7 AND 24. Feb 1, 2007 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00228Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 380, RBL 35, WL208. REMOVED, BLENDED CORROSION, FROM BS380, RBL 35. ROTO PEENED AREA, TREATED AND PRIMED AREA. REF EA NR 5310-106966 AND EA NR-7-5310-106966 REV A.Jan 31, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00227Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED, BS 380, RBL 48-55, WL208. BLENDED CORROSION AREA, ROTO PEENED, TREATED AND PRIMED. REF EA NR 7-5310-106966, AND 7-5310-106966 REV A.Jan 31, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00226Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 380, LBL 28-31 WL208 BLENDED CORROSION AT STA 380 LBL 28-31. ROTO PEENED, TREATED AND PRIMED AREA. REF EA NR 7-5310-106966, AND EA NR 7-5310-106966 REV A.Jan 31, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00220Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 400, RBL 33, WL 208. BLENDED CORRODED AREA, WITHIN LIMITS REF SRM 53-10-1, PG 22. ROTO PEENED AREA, TREATED AND PRIMED AREA, REFERENCE WRI NR 53108449, EA NR 7-5310-106967 CLASSIFIED AS MAJOR.Jan 31, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA00219Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 360, LBL 8, WL 208. BLENDED CORROSION AT STA 360, LBL 8. ROTO PEENED, TREATED AND PRIMED AREA. REF WRI NR 53108448, EA 7-7310-106965. CLASSIFIED AS MAJOR REPAIR.Jan 31, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor Beam
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