Boeing 727-227

Service difficulty reports · 5,082

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727227'
  ORDER BY difficulty_date DESC"

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SDR CA090109009Blades · damaged(CAN) ON TAKEOFF, A JUMP IN EPR AND WAS OBSERVED AS WELL AS A MOMENTARY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT ON THE NR 3 ENGINE. THE ENGINE WAS SHUTDOWN AFTER THE TOWER REPORTED SEEING SPARKS. ON EXAMINATION DAMAGE WAS FOUND TO THE C1 AND C2 BLADES AND SJan 1, 2009 · Boeing 727227 · Turbine Engine Compressor SectionSDR FDEA200812105120Skin · corrodedLWR FUSELAGE SKIN BETWEEN STA 950B AND 950C AT BL0 IS BULDGING WITH 2 EACH RIVET HEADS POPPED. COMPLIED WITH EA 7-5330-124049 PART 1 BY MANUFACTURING FILLER, DOUBLER AND TRIPLER OUT OF2024T3 180/90/100C. REMOVED DAMAGE AND INSTALLED PARTS ALL IAW EA 7- 5330Dec 10, 2008 · N493FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA200812095112Seat Track · corrodedUPPER CARGO COMPARTMENT STA 770 BL24L SEAT TRACK LOBE CORRODED REMOVED PANEL TO GAIN ACCESS IAW 51-30-2 AND REMOVED CORRODED SEAT TRACK AT STA 760-848; BL 24L IAW SRM 53-10-5. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5. TREATED AND PRIMED IAW SRM 51-10-2, ADec 9, 2008 · N493FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812075102Skin · corrodedBS 1183 TO 1148 AT STR 26L HAS SURFACE CORROSION ON INNER SKIN REMOVED CORROSION AND FOUND OUT OF LIMITS REPAIRED SKIN IAW EA 7-5330-126867.Dec 7, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA200812045084Accessory Unit · illuminatedLANDING GEAR HANDLE FAILED TO RETRACT ABOVE OFF POSITION AFTER TAKEOFF, ACCOMPANIED BY ILLUMINATION OF ALL LIGHTS ON GEAR ANNUNCIATOR LIGHT PANEL UP FRONT AND RT MAIN GEAR DOOR LIGHT ON S/O PANEL. RAN QRH BUT FAILED 1ST TEST STEP. RECONFIGURED FOR LANDING WIDec 4, 2008 · N489FE · Boeing 727227 · Landing Gear Retraction/Extension SystemSDR FDEA200812035061Skin · damagedNUMEROUS FASTENERS WITH IMPROPER ED AND SPACING STA 440 STR'S 8L TO 10L. REPAIRED THE AFFECTED AREA IAW FEDEX EA NR 7-5330-126864, FUSELAGE SKIN AD 98-11-03R1. MCD CUTOUT REINFORCEMENT DOUBLER AND FUSELAGE SKIN LAP JOINT REPAIR AT STA 440, S10L.Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA200812035063Spar · corrodedCORROSION IN NLG LT STRUT DOOR SPAR BOX, APPX FUSELAGE STA 290. REMOVED WEB IAW SRM 51-30-2 AND REMOVED CORROSION IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED 2ND WEB LT AREA FOR ACCESS IAW SRM 51-30-2 AND REMOVED NLG SPAR IAW SRM 51Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA200812035062Skin · corrodedBS 1183 - 1148 OB AND STR 26L HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2 AND 53-30-2 FIG 2. REPAIRED SKIN IAW EA NR 7-5330-126867 FUSELAGE SKIN AD 98-11-03 R1, STA 1152 STA 1175 STR 26L 65-54583 LAP JOINT UPPDec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA200812035060Failsafe · corrodedAFT CARGO COMP BS 950 AT STR 29R OTBD SIDE HAS LEVELING COMPOUND CRACKED, BELOW FAILSAFE. CORROSION ON FAILSAFE BS 950 STR 29R TO STR 28R. REMOVED LEVELING COMPOUND AND FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW SRM 51-10-1Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA200812015024Skin · dentedE&E DOOR DENTED & HAS GOUGE MARKS AT LH EDGE OF DOOR EXTERIOR SKIN. DENTS FOUND TO BE OUT OF LIMITS BY MECHANICAL MEANS IAW SRM 52-100-2. CUT OUT DAMAGE (DIMS: 2 1/8 X 1 1/8) IAW SRM 52-00-3 FIG 1. FABRICATED DOUBLER AND FILLER REPAIR IAW SRM 52-00-3 FIG ADec 1, 2008 · N495FE · Boeing 727227 · Service DoorsSDR FDEA200812015028Shear Tie · corrodedNLG W/W WEB AT STA 312 UPPER SECTION OF SHEAR TIE WEB IS CORRODED AT LBL 22. CUT OUT DAMAGE AREA DIM: 5 1/2 BY 4 AND REPAIRED NLG W/W WEB AT STA 312 SHEAR TIE LBL 22 IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 1.Dec 1, 2008 · N495FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA200812015027Shear Tie · crackedNLG W/W SHEAR TIE AT STA 312 BETWEEN STR 24R - 25R IS CRACKED AT BOTTOM HOLE. REMOVED FASTENERS A ND CUT OUT SHEAR TIE IAW B727 SRM 51-30-2 AND 53-10-4 FIG 15. REPAIRED NLG W/W SHEAR TIE AT BS 312 BETWEEN STR 24R AND STR 25R IAW B727 SRM 53-10-4 FIG 15. TREDec 1, 2008 · N495FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA200812015036Pressure Switch · malfunctionedNR 1 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW PRESSURE/FILTER BYPASS LIGHT. COMPLIED WITH QRH ENGINE WINDMILLED 2 MIN PRIOR TO SHUT DOWN. OIL PRESSURE AT APPROX 40 PSI. FOUND FAULTY LOW OIL PRESS SWITCH, REMOVED AND REPLACED SWITCH IAW MM 79-34-001-4, ALSO CDec 1, 2008 · N492FE · Boeing 727227 · Engine Oil PressureSDR CA081121011Accessory Unit · failed(CAN) JUST AFTER TAKEOFF, THE CREW ATTEMPTED TO SELECT GEAR UP, THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. ACFT RETURNED TO WHERE MAINT REPLACED THE LANDING GEAR ACCY UNIT. A/C RETURNED TO SERVICE.Nov 20, 2008 · Boeing 727227 · Landing Gear Retraction/Extension SystemSDR 08FDEA04942Skin · erodedNR 1 NOSE COWL L/E SKIN AT BOTTOM HAS AREAS OF EROSION AND 3 CRACKS. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, CUT OUT DAMAGE DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3. FAB DOUBLER MAT 2024T3 .050 PO NR 9007861 DIMS 19 3/8 BY 3 1/2 AND FILLER MATERIAL 2Nov 20, 2008 · N495FE · Boeing 727227 · Nacelle/Pylon, Plate/SkinSDR 08FDEA04941Skin · corrodedAFT CARGO COMP BS 950F - 970 OUTBD OF STR 28L HAS SURFACE CORROSION RUNNING AFT BEHIND INTERCOSTAL. REMOVED FLOOR SUPPORT AND INTERCOSTAL FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE AREA. FABBED DOUBLER REPAIR AND 2 FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FNov 20, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04939Skin · crackedRT WING L/E SLAT NR 6 LOWER SURFACE SKIN IS CRACKED AROUND RIVET HOLE. REMOVED RT NR 6 SLAT COVE PNL FOR ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLE IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-3 FIG 1, REINov 20, 2008 · N495FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA04937Skin · canningEVIDENCE OF SKIN OIL CANNING AT BS 1347.65 BETWEEN STR 6 R AND STR 7R. CUT OUT DAMAGE AREA IAW SRM 53-30-5 FIG 26. FAB REPAIR PART IAW SRM 53-30-3 FIG 26 AND 54-30-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2.Nov 20, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04936Frame · corrodedCORROSION ON THE FWD CARGO BILGE AREA AT ST 480 BETWEEN STR 27R AND STR 26R. CUT OUT DAMAGE AREA SHEAR TIE IAW SRM 53-10-4 FIG 15. FAB SHEAR TIE IAW SRM 53-10-2 FIG 3. HEAT TREAT PART IAW ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED IAW SRM Nov 20, 2008 · N495FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA04935Skin · wornLT WING NR 2 SLAT UPPER T/E LIP DAMAGED AT INBD UP STOP HOOK. TRIMMED OUT DAMAGE AREA IAW SRM 57-50-1, REMOVED SLAT HOOK IAW SRM 51-30-2, FAB REPAIR PLATE IAW SRM 57-50-3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHERS IAW SRM 51-30-8 FINov 19, 2008 · N495FE · Boeing 727227 · Leading Edge DevicesSDR 08FDEA04934Support Beam · damagedFASTENERS LOOSE LWR SIDE OF NR 7 SPOILER FITTING. UPON FURTHER EVALUATION FOUND IMPROPER REPAIR IAW DRAWING SR27-57-038. REPAIRED LT WING INBD SPOILER SUPPORT BEAM IAW DRAWING SR 27-57-038 REV C, SEE WO NR 00042909, N/R N00197, JPF FOR DETAILS.Nov 19, 2008 · N495FE · Boeing 727227 · Wing Main, Frame StructureSDR 08FDEA04858Skin · gougedRT INBD FOREFLAP L/E O/B CORNER IS GOUGED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PART, MAT USED 2024T3 .063 PO NR 9007835, DIMENSION 4 INCH BY 3 3/4 INCH IAW B727 57-50-4 FIG 1. TREATED AND PRIMED AREA ANDNov 11, 2008 · N495FE · Boeing 727227 · Trailing Edge FlapsSDR 08FDEA04782Switch · failed"NOSE GEAR DOWN AND LOCKED LIGHT" AND NOSE GEAR UNSAFE LIGHT" ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO OFF POSITION FOLLOWING GEAR RETRACTION. BOTH LIGHTS THEN REMAINED ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO "UP" POSITION. JACKED ACFT IANov 7, 2008 · N494FE · Boeing 727227 · Landing Gear Position and WarningSDR 08FDEA04791Support · corrodedAPU EXHAUST DUCT MOUNT FLANGE AT UPPER WING PANEL, AFT Z ANGLE SUPPORT CORRODED. REPLACED FLANGE SUPPORT/STIFFENER REF SRM 51-30-02 PG 2 AND 5. THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 7, 2008 · N487FE · Boeing 727227 · Wing Miscellaneous StructureSDR 08FDEA04646Linkage · looseNUMBER 4 LE FLAP ON RIGHT SIDE DID NOT RETRACT AFTER TAKEOFF DURING FLAP/SLAT RETRACTION. RAN QRH. EXTENDED NORMALLY AND DID NOT RETRACT SECOND TIME. FOUND LOOSE LINKAGE ON NR 4 LE FLAP SWITCH. SECURED LINKAGE, OPERATED FLAPS AND OPS CHECKED GOOD IAW MM 2Oct 30, 2008 · N490FE · Boeing 727227 · Leading Edge Slat Control SystemSDR 08FDEA04637Shear Tie · corrodedCORROSION AT SHEAR TIE STR 30R AND STA 970 REMOVED DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 15. FAB NEW SHEAR TIE IAW SRM 53-10-4 FIG 15 AND 53-10-2 FIG 5. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREAT AND PRIMED IAW SRM 51-10-2. Oct 30, 2008 · N491FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA04636Shear Tie · crackedAFT CARGO COMPT SHEAR TIE AT BS 950F BETWEEN STR 28L AND 29L IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-30-2. FAB NEW SHEAR TIE FROM 7075-O 0.080 INCH IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPORT NR 2-37153-807 REVOct 30, 2008 · N491FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA04574Skin · dentedDENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPT CUT-OUT. REMOVED FASTENER AT STA 180 LWR NOSE IAW SRM 51-30-2, FOUND AREA TO HAVE OIL CAN CONDITION AND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA, DIM 1 INCH BY 1 INCH IAW SRM 53-30-3 FIG 13. Oct 27, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04558Frame · crackedE/E COMPT DOOR CRACKED AT AFT FRAME. REMOVED INNER SKIN AND CRACKED FRAME, FABRICATED NEW FRAME. INSTALLED NEW FRAME AND SKIN IAW SRM 51-20-1, 52-40-1 FIG 2 AND 51-30-2.Oct 26, 2008 · N491FE · Boeing 727227 · Service DoorsSDR 08FDEA04556Frame · chafedFRAME AT STA 344 AND STR 5L CONTACTING 9G BULKHEAD. TRIMMED OUT FRAME AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. FABRICATED REPAIR IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR AT FRAME STA 344 STR Oct 26, 2008 · N491FE · Boeing 727227 · Fuselage Main, FrameSDR 08FDEA04555Skin · dentedDENT STA 324 STR 23L EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIMS 7/8 INCH BY 7/8 INCH. FABRICATED FILLER USING 2024-T3 .040 DIMS 7/8" BY 7/8" AND DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 13 AND 51-30-Oct 26, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04382Skin · damagedFUSELAGE LT/RT, FWD WING TO BODY ATTACHMENT AREAS, SCRIBE MARKS IN SKIN STA 700, 72D STR 19L TO STR 19R. BLEND OUT DAMAGE IAW SRM 51-10-1 AND UT AREA IAW NDTM 51-00-00. FOUND SKIN OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AREA LT SIDE & FABRICATED 1 DOUOct 16, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04344Skin · crackedFWD CARGO HAS CRACK AROUND RIVETS BACK TAIL AT STR 28R, STA 640. CUT OUT DAMAGED AREA AND REMOVED PREVIOUS SPLICE AS REQUIRED, FABRICATED REPAIR HAT SECTION AND ONE SPLICE AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53 10-2, 51-10-2 AND 51-30-2.Oct 14, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04343Skin · dentedDENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPARTMENT CUTOUT.Oct 14, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04342Stringer · corrodedCORROSION INSIDE OF STR 27L, STA 950F TO STA 1110. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED STRINGER SECTION FOR ACCESS AND REMOVED DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION, FABRICATED REPAIR SPLICE. INSTALLED REPAIR PARTS AND STRIOct 14, 2008 · N491FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA04341Skin · dentedFUSELAGE SURFACE HAS DENT AT STA 682 S24L. COMPLIED WITH HFEC ON DENT IAW NDTM PT.6 51-00-00, CRACK INDICATED. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED REPAIR DOUBLER AND FILLER ACCOMPLISED IAW SRM 53-30-3 & 53-30-2. TREATED AND PRIMED AREA IAW SRM 5Oct 14, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR R5KB10132Light · dischargedL2 DOOR EMERGENCY EXIT LIGHT INOP.Oct 13, 2008 · N422BN · Boeing 727227 · Emergency LightingSDR R5KB10131Light · looseEMERGENCY PATH LIGHTING INOP FROM ROW 14 TO ROW 23.Oct 13, 2008 · N422BN · Boeing 727227 · Emergency LightingSDR 08FDEA04305Shear Tie · crackedLEFT AFT AIR STAIR AREA, BS 1262 SHEAR TIE CRACKED BETWEEN S11-12L REMOVED CRACKED SHEAR TIE, FABRICATED, TREATED AND PRIMED AND INSTALLED SHEAR TIE REPAIR. REF SRM 51-10-2, SRM 51-30-2 PG 1-4, SRM 53-10-04, NDT HOLES AND COUNTERSINKS, NO DEFECTS NOTED, REOct 10, 2008 · N485FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA04299Stringer · corrodedAFT CARGO COMPARTMENT, S29L HAS CORROSION AND PEELING PROTECTIVE FINISH BS 950C TO 950E. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, REMOVED FRAMES, INTERCOASTALS, FLOOR SUPPORTS, AND FAIRINGS FOR ACCESS IAW SRM 51-30-2 REMOVED AND REPLACED STROct 10, 2008 · N491FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 08FDEA04295Seat Track · misalignedSTA 720F LBL 45 HAS HOLE FOR FLOORBOARD DRILLED ON EXISTING SEAT TRACK SPLICE ON A FASTENER. REMOVED SEAT TRACK AND SPLICE BS 720F - 750 LBL 45 IAW SRM 51-30-2. LOCATED, DRILLED, DEBURRED NEW SEAT TRACK SECTION IAW SRM 53-10-5. FABRICATED SPLICE ANGLE IAW SROct 9, 2008 · N468FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04289Casting · corrodedL/H FWD EMERGENCY DOOR CASTING AROUND HANDLE HOUSING IS CORROSION REPLACED CASTING AROUND HANDLE HOUSING REF SRM 51-30-02 PG 1-5. OPS CHECK OF DOOR OK THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 9, 2008 · N485FE · Boeing 727227 · Emergency ExitsSDR 08FDEA04287Shear Tie · shearedCABIN LEFT SIDE BS 660 FRAME, FWD SIDE SHEAR TIE BETWEEN STR 14L & 15L, 1 EA FASTENER BUCKTAIL SHEARED OFF BLEND OUT TRIPLER, PREFORMED HFEC, NO DEFECTS NOTED. INSTALLED RIVET, FILLED GAP WITH SEALENT, PAINT TO MATCH, ALL IN REF TO EA 7-5330-113102. THIS IOct 9, 2008 · N485FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 08FDEA04276Panel · crackedFWD LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND SCUFF PLATE CRACKED IN SEVERAL AREAS REMOVED THRESHOLD REF SRM 51-30-2, WELDED CRACKS REF DWG SR27-53-025 REV.C ON N/R N00383. INSTALLED THRESHOLD REF SRM 51-30-2 PG 2-14 THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 8, 2008 · N485FE · Boeing 727227 · Cargo/Baggage DoorsSDR 08FDEA04275Support Beam · crackedLEFT WING NR 7 SPOILER FALSE SPAR LWR PANEL HAS LOOSE FASTENERS. EVALUATED AND FOUND SUPPORT BEAM CRACKED AT WS 251. REPAIRED IAW DRAWING SR27-57-038 REV C.Oct 8, 2008 · N491FE · Boeing 727227 · SpoilersSDR 08FDEA04274Seat Track · corrodedMAIN CARGO COMPARTMENT, SEAT TRACK CORRODED AT STA 880 TO STA 920 , BL 0. REMOVED FLOOR BOARD IAW SRM 51-30-2, REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2; FABRICAETD NEW SEAT TRACK SECTION, LOCATED AND DRILLED. IAW SRM 53-10-5. DRAWING 53 FX 1497 REV TOct 8, 2008 · N491FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04273Skin · dentedFUSELAGE LT SIDE, PROTRUDING DENT AT STA 392 ,STR 20L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1, CUT OUT DAMAGED AREA. FABRICATED DOUBLER REPAIR INTERNAL FILLER AND EXTERNAL FILLER IAW SRM 53-30-3 AND SRM 53-30-2 AND INSTALLED REPAIR PARTS IAWOct 8, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04272Skin · dentedFUSELAGE LH SIDE, DENT ON LAP SEAM AT STA 338, STR 24R. DENT LOCATED ON LAP SEAM & FOUND OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE IAW SRM 53-30-3. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR WASHER IAW SRM 51-30-8, TREATED AND PRIMEOct 8, 2008 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 08FDEA04269Gusset · corrodedLOWER FWD CARGO DOOR S/N 822, INTERNAL LOWER FRAME, 2 GUSSETS ARE CORRODED AT LWR END. 1 AT 28" AFT, 2ND AT 39" AFT. REMOVED AND REPLACED GUSSETS REF SRM 51-30-02 P 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.Oct 8, 2008 · N485FE · Boeing 727227 · Fuselage Main, StructureSDR 08FDEA04268Door Frame · crackedMAIN ENTRY DOOR 1L CUTOUT, AFT FRAME, BS 344, STR 15L JUST BELOW 2ND STOP FITTING FROM BOTTOM, FRAME CRACKED FABRICATED REPAIR PARTS PER DWG 65-17685-24, -9, -7. REPLACED LWR AFT FRAME REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 8, 2008 · N485FE · Boeing 727227 · Fuselage Main, Structure
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