Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR FDEA201002120416Support Angle · crackedAFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE HAS CRACK INDICATION AND WORKING FASTENERS. BS 1263, FWD SIDE. REMOVED RT TORQUE BOX WEB DOUBLER FROM BS1243 TO 1283 IAW SRM, REV 102, 51-30-2. CUT WEB AT BS 1263 IAW SRM 51-10-1. REMOVED RT LOWER TORQUE BOX AFeb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002120415Support Angle · crackedAFT AIRSTAIR LT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT RIVET, BS 1250. REMOVED SUPPORT ANGLE FROM AFT AIRSTAIR LT LOWER TORQUE BOX AT BS 1250 IAW SRM, REV 102, 51-30-2. FABRICATED SUPPORT ANGLE IAW DWG NR 65-17516 AND BAC 1517-1457. INSTALLED SUPPORT AFeb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002110397Skin · gougedEVALUATE EXTERNAL SKIN REPAIR BS 360, STR 17L, DIM: 25 1/2 X 20 IAW EO 7-5100-7-5005, PT1. REMOVED PREVIOUS REPAIR DOUBLER, HFEC AND AND UT INSP IAW NDTM 51-00-00 AND FOUND SKIN GOUGED, CUT OUT DAMAGED AREA IAW SRM 51-10-1, HFEC INSPECTED. CUTOUT AND HOLES WFeb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201002110396Stringer · corrodedAFT CARGO STA 1030, STR 26R CORRODED. REMOVED 2" SECTION OF DAMAGED STRINGER AND FABRICATED FILLER AND STRINGER REPAIR SPLICE IAW SRM 53-10-2 FIGURE 9 AND 53-10-3 FIGURE 1 DETAIL 1. INSTALLED SPLICE AND FILLER IAW SRM 51-30-2, REV. 102.Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201002110411Attach Bracket · crackedLT WING L/E CAVITY, BOTH INBD AND OTBD NR 1 SLAT ACTUATOR ATTACH BRACKETS HAVE INSIDE PLATES CRACKED. REMOVED INBOARD AND OUTBOARD ATTACH BRACKETS IAW SRM, REV 102, 51-30- 2. FABRICATED 2 ATTACH BRACKETS FOR NR 1 SLAT ACTUATOR, IAW SRM 51-20-1 FIGURE 7 AND 5Feb 11, 2010 · N482FE · Boeing 727227 · Wing, Attach FittingsSDR FDEA201002110395Stringer · corrodedAFT CARGO ATA 1170, STR 26R CORRODED. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-10-1, REV. 102. FABRICATED STRINGER AND SPLICE IAW SRM 53-10-3 FIG. 1 DETAIL 1. INSTALLED STRINGER SECTIONS AND SPLICE IAW SRM 53-10-3 FIG. 1, DETAIL 1 AND 51-30-2.Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201002110412Web · damagedAFT AIRSTAIRS RT LOWER TORQUE BOX WEB, LIGHTING HOLE ROUTE OUT IS GREATER THAN .100 INCH, BS 1230. FABRICATED NEW DOUBLER IAW SRM 53-10-2, FIG 6 AND 51-40-2 FIG 1. INSTALLED NEW DOUBLER IAW SRM 51-30-2 AND 51-40- 2 FIG 1, REV 102.Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201002110403Sill · damagedDOUBLE DRILLED HOLES FOUND MCD UPPER FWD INBD SILL BS 520 STR 2L. R & R MAIN CARGO DOOR FWD IB SILL AT BS 442055 TO BS 570.5 IAW DWG NR 53FX1475, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2.Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002100436Floorbeam · corrodedCORROSION FLOORBEAM MAIN CABIN BS 1110, RBL12. CUTOUT DAMAGED FLOORBEAM DIM: 1.9" X 2" IAW SRM 53-10-8, FIG 3 FABRICATED FLOORBEAM REPAIR, SUPPORT ANGLE, AND STRAP IAW SRM 53-10-3 FIG 3. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTSFeb 10, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002100421Hinge Fitting · crackedCRACK & GOUGED LOBE MCD HINGE SUPPORT FUSELAGE SIDE FWD NR 1. REMOVED DAMAGED HINGE SECTIONS, FABRICATED NEW HINGE SECTIONS USING 5212791. PO NR 29146119 DIMS 45.75" AND 20.1250" AND INSTALLED IAW DWG 52FX1433 REV E.Feb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Door HingeSDR FDEA201002100420Hinge Bracket · wornEXCESSIVE PLAY 6 EA HINGE SUPPORT ASSY MCD FUSELAGE ATTACHMENT TOP AFT NR 7. REMOVED DAMAGED HINGE SECTION UPPER AND LOWER, FABRICATED NEW HINGE SECTIONS. UPPER AND LOWER, INSTALLED NEW HINGE SECTIONS AT MAIN CARGO DOOR AFT SIDE. UPPER AND LOWER IAW MM 51-3Feb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Door HingeSDR FDEA201002100387Seat Track · corrodedCORROSION SEAT TRACK BS 690-530 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5 FIG 1 FABRICATED 2 SEAT TRACK SPLICES IAW SRM 53-10-5 FIG 1 LOCATED AND DRILLED SEAT TRACK IAW SRM 51-30-5. INSTALLED SEAT TRACK AND SPLICES IAW Feb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002100386Seat Track · corrodedCORROSION SEAT TRACK BS 600-BS 720 BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK IAW SRM 51-30-2.Feb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002100385Seat Track · crackedCRACK SEAT TRACK MAIN CABIN BS 950D BL 0. REMOVED SECTION SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SECTION SEAT TRACK, & STRAPS IAW SRM 53-10-5, FIG 1. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2 AND INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2.Feb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002100384Seat Track · crackedCRACKED SEAT TRACK MAIN CABIN BS 950D RBL 25. REMOVED SEAT TRACK AND SPLICE, FABRICATED SEAT TRACK REPAIR AND SPLICE REPAIR. INSTALLED IAW SRM 53-10-2, FIG 7A AND SRM 53-10-5 FIG 1, 51-30-5, 51-30-2. TREATED AND PRIMED REPAIR PARTS PRIOR TO INSTALLATION IFeb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002100383Seat Track · corrodedCORROSION AND CRACKED SEAT TRACK MAIN CABIN FLOOR BS 950 PLUS 10" IN - BS 950D. REMOVED SECTION SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK, STRAP AND 2 ANGLES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW REPAIR PARTS IAW SRM 51-10-2 AND INSTALLED RFeb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002100382Seat Track · corrodedCORROSION AND CRACKED SEAT TRACK MAIN CABIN BS 510-690 LBL 25. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SPLICE REPAIR AND DRILLED AND LOCATED SEAT TRACK, INSTALLED SEAT TRACK, INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 51-30-2, 51-30-5, 53-10-5 FFeb 10, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002090540Skin · gougedRT WING NR 7 SLAT T/E BOTTOM SIDE GOUGED INBD OF SLAT HOOK WS 639. BLENDED OUT GOUGE AT NR 7 SLAT T/E WS 639, FOUND BLEND OUT OF LIMITS, FABRICATED REPAIR DOUBLER & INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, SRM 57-50-1 FIG 2, SRM 57-50-3 FIG 10 & SRM 51-1Feb 9, 2010 · N482FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201002090404Sill · crackedMAIN CARGO DOOR UPPER SILL, STA 490, BETWEEN STR 3L AND 4L. CRACKS ORIGINATING FROM 2 FASTENER HOLES. R & R UPPER OTBD SILL AT BS 442.65 TO BS 570.5 AND REPAIRED ADDITIONAL OPEN HOLES IN SKIN IAW EA 7-5310-135527 AND SRM 51-10-1, 51-30-2, 51-30-5 AND 51-10-2Feb 9, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002080410Shear Tie · corrodedFWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED SECTION OF SHEAR TIE 1"X5 7/8" IAW SRM 51-10-1. FABRICATED SHEAR TIE FROM 7075-T6, .063" X 2 1/4"X 5 7/8" IAW B727 SRM 53-10-4 FIG 15 AND 53-10-2 FIG 3. IFeb 8, 2010 · N482FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201002080409Shear Tie · corrodedFWD PIT - CORROSION ON SHEAR TIE AT BS 540, BETWEEN STRINGERS 28L AND 28R. REMOVED CORROSION IAW SRM, REV 102, 51-10-6. UT INSPECTED AREA IAW NDTM 51-00-00, FIGURE 3, PART 4. ORIGINAL THICKNESS OF .046", MATERIAL LOSS OF .001", MATERIAL REMAINING .045". AREFeb 8, 2010 · N482FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201002060408Structure · crackedRT WING NR 5 SLAT T/E CRACKED, WS 400. ROUTED OUT DAMAGED EDGE AT RT WING NR 5 SLAT T/E IAW SRM 51-10-1, COMPLIED WITH HFEC INSP IAW NDTM 51-00-00 WITH NO CRACK NOTED, AREA FOUND TO BE WITHIN LIMITS IAW DWG SR27-57-046 AND SRM 57-50-1.Feb 6, 2010 · N482FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201002060407Skin · crackedRT WING NR 8 SLAT OTBD STOP PAD INBD SIDE SKIN CRACKED IN RADIUS OF SLAT SKIN, SLAT STA 760. REMOVED LOWER CHORD FROM NR 8 SLAT IAW SRM, REV 102, 51-30-2. FABRICATED NEW LOWER CHORD IAW SRM 57-50-2 FIG. 2, AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2Feb 6, 2010 · N482FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201002050339Angle · crackedCRACKED CHORD ANGLE, RT WING FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. REMOVED DAMAGE BY CUTTING OUT WEB AND CHORD IAW FED EX B727 DRAWING NUMBER SR27-57-038 REV C. FABRICATED 2 REPAIR ANGLES, LOWER CHORD, DOUBLER , STRAP, WEB, & 2 RADIUS FILLERSFeb 5, 2010 · N482FE · Boeing 727227 · Wing Main, Frame StructureSDR ABXR201002010001Skin · tornWHILE ACCOMPLISHING ROUTINE SCHEDULED MX, THE LT WING-TIP WAS FOUND TO HAVE A TEAR OUT IN THE AREA OF THE AFT LOWER MOUNTING FASTENER HOLE. CUT DAMAGED AREA OUT AND PERFORMED HFEC TO ENSURE DAMAGE WAS REMOVED IAW NDT MANUAL PART 6 51-00-00 FIG. 23. REPAIR INFeb 1, 2010 · N308AS · Boeing 727227 · Wing, Plate/SkinSDR FDEA201001290291Floorbeam · corrodedFLOORBEAM CORRODED AT BS 1130 RBL 30 TO RBL 46. CUT OUT DAMAGED AREA, FABRICATED 2 FLOORBEAM REPAIRS, 1 STRAP, 1 FILLER, 2 ANGLES, 1 STRAP AND 1 FILLER . HEAT TREATED PARTS TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A AND INSTALLED PARTS IAW 53-10-8 Jan 29, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201001290290Floorbeam · corrodedFLOORBEAM CORRODED STA 1070, RBL 5 TO RBL 10. CUT OUT DAMAGED AREA, FABRICATED 2 FILLERS, 2 REPAIR ANGLES AND INSTALLED IAW SRM 53-10-8, 51-10-2 AND 51-30-2.Jan 29, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor BeamSDR CA100201003Switch · damaged(CAN) UPON FLAP RETRACTION AFTER DEPARTURE, THE NR 6 KRUGER FLAP IN TRANSIT LIGHT REMAINED ILLUMINATED. ACFT RETURNED TO BASE. THE SWITCH WAS REPLACED AND THE ACFT RETURNED TO SERVICE. (TC 20100201003)Jan 28, 2010 · Boeing 727227 · Trailing Flap Position Indicating SystemSDR FDEA201001270285Floorbeam · damagedDOUBLE DRILLED HOLES IN FLOORBEAM STA 1130 LBL 47. CUT OUT DAMAGE IN FLOORBEAM DIMS 1" X 1", FABRICATED NEW ANGLE, HEAT TREATED PART TO T6 CONDITION IAW FAS ENG REPORT 2-37153-801 REV A, FABRICATED STRAP, FILLERS AND INSTALLED IAW SRM 51-30-2, 53-10-8, AND 51-Jan 27, 2010 · N489FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201001270270Compressor · stalledCLIMBING THROUGH 16,000 FT VERY LOUD "THUMP" WITH ASSOCIATED AIRFRAME SHUDDER. COMPLIED WITH QRH ENGINE COMPRESSOR STALL/LIMIT/SURGE AND RETURNED TO DEPARTURE. DID A WALK AROUND OF AFT. NO AIRFRAME DAMAGED NOTED. ALL CONTROL SURFACES ACCOUNTED FOR. R & Jan 27, 2010 · N482FE · Boeing 727227 · Turbine Engine Accessory DriveSDR FDEA201001260269Skin · bentMAIN CARGO DOOR AFT EDGE AT STR 10 LT IS BENT OUT. TRIMMED OUT DAMAGED AREA, HFEC INSPECTED CUTOUT WITH NO DEFECTS NOTED IAW NDTM 51-00-00, HFEC INSPECTED HOLES WITH NO DEFECTS NOTED NDTM 51-00-00, FABRICATED DOUBLER, TRIPLER, FILLER AND INSTALLED IAW EA 7-Jan 26, 2010 · N489FE · Boeing 727227 · Cargo/Baggage DoorsSDR FDEA201001230268Skin · corrodedSURFACE CORROSION UNDER BASE OF NR 2 STATIC WICK ON RT HORIZ STAB OTBD T/E. REMOVED CORROSION AND FOUND OUT OF LIMITS AND CRACKED. TRIMMED OUT DAMAGE, FABRICATED DOUBLER PLATE, TWO FILLERS AND INSTALLED IAW SRM 51-30-2, 51-10-6, 55-20-3 AND 51-80-7.Jan 23, 2010 · N489FE · Boeing 727227 · Horizontal Stabilizer, Plate/SkinSDR FDEA201001230281Beam · damagedAFTER REMOVING MAIN CARGO DOOR FWD UPPER SILL, FOUND EXISTING OPEN HOLES WITH SHORT SPACING AT STA'S 480, 490, 500 AND 520. DAMAGE REPAIR DOCUMENTED.Jan 23, 2010 · N489FE · Boeing 727227 · Fuselage Main, StructureSDR 2010FA0000070Skin · corrodedCORROSION ON FUSELAGE SKIN AFT OF BS 540, INBD OF STRINGER 27RJan 23, 2010 · N422BN · Boeing 727227 · Fuselage Main, Plate/SkinSDR 2010FA0000069Structure · corrodedCORROSION FOUND AROUND FASTENERS ON RT WING L/E WING STATION 277.Jan 23, 2010 · N422BN · Boeing 727227 · Wing Main, Frame StructureSDR 2010FA0000068Skin · corrodedCORROSION FOUND AROUND FASTENERS ON RT WING, L/E AT WING STA 320.Jan 23, 2010 · N422BN · Boeing 727227 · Wing, Plate/SkinSDR 2010FA0000067Skin · bulgedFUSELAGE SKIN, EXTERNAL, HAS A BULGE AND PULLING FASTENERS AT STA 1148, BETWEEN STRINGER 24R AND 27R.Jan 23, 2010 · N422BN · Boeing 727227 · Fuselage Main, FrameSDR FDEA201001220253Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 620 TO 640 STR 4L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201001220252Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 640 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201001220251Skin · gougedMAIN CARGO DOOR INNER SURROUND DOUBLER GOUGED AT STA 480 STR 8L. EVALUATED AREA AND FOUND OUT OF LIMITS. REMOVED INNER SKIN DOUBLER SECTION, FABRICATED NEW SKIN AND INSTALLED IAW SRM 53-10-1, 51-30-2, 51-30-5 AND 51-10-2.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201001220226Bulkhead · crackedRT W/W FWD BULKHEAD IS CRACKED BELOW APU LOAD CONTROL VALVE AT BS 870 RBL 18. REPAIRED RT WHEEL WELL BULKHEAD APU LOAD CONTROL VALVE AREA BS 870 RBL18 IAW SRM 53-10-9 FIG 5, REV 102.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage Main, BulkheadSDR FDEA201001220225Hinge · wornMAIN CARGO DOOR AFT HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTION USING 5212791 PO NR 79014501 DIMS 48 1/2" LONG FOR UPPER SECTION AND 20 1/4" LONG FOR LOWER SECTION AND INSTALLED IAW DWG B27-53-070 REV B.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage, Door HingeSDR FDEA201001220224Hinge · wornMAIN CARGO DOOR FWD HINGE SEGMENT HAS EXCESSIVE PLAY. REMOVED HINGE SECTION, FABRICATED NEW HINGE SECTIONS AND INSTALLED IAW DWG B27-53-070 REV B.Jan 22, 2010 · N489FE · Boeing 727227 · Fuselage, Door HingeSDR FDEA201001210213Skin · damagedL-1 DOOR UPPER AND LOWER HINGE CUTOUT DOUBLERS HAVE COUNTERSUNK FASTENERS INSTALLED. REMOVED DOUBLERS, FABRICATED 2 NEW DOUBLERS, CADMIUM PLATED DOUBLERS IAW SOPM 20-40-01 AND INSTALLED IAW EO 7-5330-7-2345 PT 2 AND SRM 51-30-2.Jan 21, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201001210208Skin · crackedLT INBD AILERON LOWER SURFACE SKIN IS CRACKED AT FWD EDGE. SKIN CRACK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 4 1/2" X 5 1/8", FABRICATED DOUBLER, FILLER AND INSTALLED IAW SRM 57-50-1, 57-50-5, 51-10-1, AND 51-30-2.Jan 21, 2010 · N489FE · Boeing 727227 · AileronsSDR FDEA201001200264Seat Track · corrodedSEAT TRACK CORRODED STA 970-990 RBL 24. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 144" AND SPLICE ANGLES USING BAC1503-100122 7178-T6511 PO NR 2912649 DIMS 1Jan 20, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR C8GA201000002Duct · crackedDURING CLIMB OPERATION THE LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT. CREW PERFORMED APPROPRIATE CHECKLIST AND DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 3 ENGINE ANTI-ICE DUCT WAS CRACKED. REMOVED AND REPAIRED DAMAGJan 20, 2010 · N89427 · Boeing 727227 · Engine Anti-Icing SystemSDR FDEA201001190190Seat Track · corrodedCABIN SEAT TRACK BS 950 - 950, 10" LBL 24 OB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 PO NR 9006020 DIMS 91" AND INSTALLED IAW SRM 51-10-Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001190189Stringer · crackedAFT PIT STR 27L HAS CORROSION WITH EXFOLIATION AROUND FASTENERS BTWN BS 950D-950F. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED 3 EACH STRINGER SECTIONS, FABRICATED 3 FILLERS AND 4 EACH SPLICES. INSTALLED IAW SRM 51-10-6, 53-10-2, 53-10-3, AND 51-30-2.Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201001190187Skin · corrodedFWD PIT - CORROSION ON SKIN AT BS 660 (AFT SIDE) BETWEEN STRINGERS 28R AND 29L. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 102. FABRICATED REPAIR DOUBLER, FABRICATED FILLER, INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2. FABRICATION IAW SRM 53-30-3, FIG.Jan 19, 2010 · N489FE · Boeing 727227 · Fuselage Main, Plate/Skin
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