Boeing 757-236

Service difficulty reports · 2,544

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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 = '757236'
  ORDER BY difficulty_date DESC"

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SDR FDEA200902140517Floorbeam · corrodedSTA 345 FLOORBEAM HAS CORROSION BL 0-24L, ON EXISTING REPAIR. REMOVED AND REPLACED TCAP REPAIR IAW SRM 53-00- 51. FABRICATED ANGLES AND STRAPS IAW SRM 53-00-51.Feb 14, 2009 · N910FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200902100501Web · corrodedCORREDED LOWER SURFACE OF SUPPORT WEB ALONG RT EMERGENCY EXIT DOOR LOWER SILL AREA. REMOVED CORROSION IAW SRM 51-10-02 ON RT EMER EXIT DOOR LWR SILL, BLENDED AREA L=10.0" X W= 3.0" X D=0.020".ORIG MAT IS 0.063" MAT LOSS 0.048" AREA OUT OF LIMIT IAW SRM 5Feb 10, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902090494Web · corrodedCORRODED SUPPORT WEB AT STA 1560-STA 1580 ALONG STR 17R, CABIN AREA. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA FOUND TO BE OUT OF LIMIT, L=12.0', W=5.0" D=.038" AS PER SRM 53-60-13 FIG 101 DET II. INSTALLED REPAIR WEB STA 1560-1580 IAW SRM 51-40-02. Feb 9, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902090493Crease Beam · corrodedCABIN FLOOR SUPPORT ANGLE AT STA 790-755 RBL 64 HAS SPOTS OF SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA L=3" BY W=1.2" D=.O20". ORIGINAL MAT .063 INCH, REMAINING .040 INCH, OUT OF LIMITS AS PER SRM 53-30-13, FIG 101, DET II. REPLACFeb 9, 2009 · N910FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200902090492Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED AT BS 345-365, LBL 60, L1 DOOR SILL. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02 AT BS 345-365, LBL 60. REMOVED FLOOR SUPPORT IAW SRM 41-40-02. BLENDED AREA IS L=18.0", W=2.0", D=.015", OUT OF LIMITS PER SRM 53-00-51Feb 9, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902090491Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED AT BS 333.45-345, LBL 64, L1 DOOR SILL. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02, AT BS 333.45-345, LBL 64. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. BLENDED AREA IS L=3.0", W=2.0", D=.012", OUT OF LIMITS PER SRM 53Feb 9, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902050464Bracket · corrodedCORROSION AT STA 310.5 LBL 25 INTERCOSTAL BRACKET REMOVED CORROSION BY BLEND ON AN AREA IAW SRM 53-00-51. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL 3. REMOVED, LOCATED, DRILLED AND INSTALLED NEW REPAIR SUPPORT FROM BATCH NR 0001586153 ATFeb 5, 2009 · N910FD · Boeing 757236 · Fuselage Main, Attach FittingsSDR FDEA200902030441Frame · damaged3 HOLES AT STA 1300 BETWEEN STRINGER 5R AND 4R ARE OUT OF LIMIT. REMOVED DAMAGED AREA IAW 757 SF SRM 53-00-07 REPAIR NR3 FIG 201. FABRICATED REPAIR CHANNELS -1 AND -2. INSTALLED REPAIR CHANNELS IAW SRM 53-00-07 REPAIR NR 3 FIG 201. THIS REPAIR IS A CATEGOFeb 3, 2009 · N912FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA200902030440Support Angle · corrodedCABIN FLOOR SUPPORT ANGLE, AT BS 700-720, RBL 64 HAVE SPOTS OF CORROSION. REMOVED CORROSION FROM SUPPORT ANGLE PER SRM 51-10-02. OUT OF LIMITS PER SRM 53-00-51, FIG 101, DETAIL 3. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 53-00-51, 51-40-02. THIS RFeb 3, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902030439Floor Support · corrodedMAIN DECK FLOOR INTERCOSTALS, CORRODED ALONG L1 DOOR LOWER SILL, FROM BS 333-377, . REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02. FLOOR SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. FABRICATED FLOOR SUPPORT. LOCATED, DRILLED, TREFeb 3, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200902030438Floorbeam · corrodedSTA 2681 FLOORBEAM TOP AND BOTTOM SURFACE ALONG ANCHOR NUTS AREA HAVE CORROSION. REPAIRED FLOORBEAM AT STA 1681 RBL-31 BOTTOM SURFACE IAW SRM 53-00-51 REPAIR NR 2. THIS IS MAJOR 'A' REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Feb 3, 2009 · N910FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200901300406Sill · corrodedLT EMERGENCY DOOR, LOWER SILL, AT BS 1340, LOWER SURFACE IS CORRODED, AFT OF FLOORBEAM. REMOVED CORROSION ON LT EMERGENCY DOOR LOWER SILL WEB, BS 1340, LBL 60, PER SRM 51-10-02. CORROSION OUT OF LIMITS PER SRM 53-60-15, FIG 101, DETAIL 4. L=6.0", W=3.0", DJan 30, 2009 · N910FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA200901290395Crease Beam · corrodedCABIN FLOOR CREASE BEAM WEB SKIN CORRODED AT STA 740. REMOVED AND REPLACED CREASE BEAM WEB IAW SRM 53-30-15 AND 51-40-02. THIS IS A MAJOR 'A' REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Jan 29, 2009 · N910FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200901290394Crease Beam · corrodedCORRODED TOP SURFACE OF ANGULAR SUPPORT FROM STA 1260-1280 RT SIDE FLOOR LEVEL. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-05 FROM FSTA 1180-1290 RT RBL 65. THIS IS A MAJOR 'A' WITH NO FOLLOW-UP REQUIRED.Jan 29, 2009 · N910FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200901240315Crease Beam · corrodedCABIN FLOOR SUPPORT ANGLE AT BS 755-780 LBL64 CORRODED. CORROSION FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-13 FIG 101 DETAIL VIII. REPLACED CREASE BEAM IAW SRM 51-40-02 AND SRM 53-50-13, CATEGORY "A" MAJOR REPAIR.Jan 24, 2009 · N910FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200901240314Frame Splice · corrodedFWD CARGO COMPT, RT FRAME SPLICE CORRODED AT FS 720, STR 26R. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS, ORIG MAT .071, REWORK .060, L=3.5, W=1.5, D=.011, OUT OF LIMITS IAW SRM 53--00-07 PAGE 103 FIG 101 DETAIL 2. FABRICATED ON MAE SPLICE PLATE TRAVJan 24, 2009 · N910FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA200901210297Floorbeam · corrodedSTA 377 FLOORBEAM HAS CORROSION, REMOVED CORROSION IAW SRM 53-00-51. FABRICATED NEW UPPER CHORD AND SPLICE ANGLES ON MAE TRAV NR T9/445482, AND T9/445483. INSTALLED REPAIR PARTS IAW SRM 53-00-51, STA 377, RBL 36- LBL 70, MAJOR REPAIR NR 3. CATEGORY B.Jan 21, 2009 · N910FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200901210294Doubler · dentedLOWER FUSE AT STA 710 RT HAS A DENT, L= 1.75, W= 1.0, D = 0.047. FABRICATED REPAIR DOUBLER IAW SRM 53-00-013. INSTALLED REPAIR DOUBLER IAW SRM 53-00-013. CATEGORY B MAJOR REPAIR NR 3 REPAIR..Jan 21, 2009 · N910FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA200901210293Frame Splice · corrodedFWD CARGO COMPT, LT FRAME SPLICE CORROSION, STA 740, STR 26L. REMOVED AND REPLACED SPLICE PLATE STA 740, STR 26L IAW SRM 51- 40- 02. SPLICE FABRICATED ON MAE TRAV NR T9/ 777465 IAW SRM 51-40-05. CATEGORY A MAJOR REPAIR.Jan 21, 2009 · N910FD · Boeing 757236 · Fuselage Main, FrameSDR CA081212001Switch · malfunctioned(CAN) COCKPIT MAIN CARGO DOOR WARNING LIGHT ILLUMINATED AT FL340 AND THE AMBER CAUTION LIGHT ON THE CARGO DOOR CONTROL PANEL ALSO ILLUMINATED. AIRCRAFT BEGAN TO RETURN TO BASE AND WHILE DESCENDING THROUGH 13,000 FEET THE LIGHTS EXTINGUISHED. THE AIRCRAFT RETDec 10, 2008 · Boeing 757236 · Door Warning SystemSDR ANCF200800030Wheel · damagedDURING TAXI OUT RT MAIN GEAR GOT STUCK INTO THE PAVED AREA UNABLE TO CONTINUE TAXI. IAW AIRPLANE RECOVERY DOCUMENT 4-10-3 AIRPLANE WAS TOWING OUT OF SOFT GND IAW AMM 32-00-10 PG 601. LANDING GEAR INNER CYLINDER CHROME INSPECTION CHECK ACCOMPLISHED AND FOUND Dec 10, 2008 · N522NA · Boeing 757236 · Wheel/Ski/FloatSDR 08FDEA04969Door Frame · corrodedL-1 DOOR, AFT -SIDE, FRAME EXFOLIATED BELOW DOOR ASSIST HANDLE. REPAIRED DAMAGED FRAME, L-1 DOOR, AFT-SIDE, BELOW DOOR ASSIST HANDLE, IAW SRM 51- 70-11. ALL PARTS REMOVED FOR ACCESS WERE RE-INSTALLED IAW SRM 51-40-02. ALL REPAIR PARTS INSTALLED IAW SRM 51Nov 24, 2008 · N915FD · Boeing 757236 · Passenger/Crew DoorsSDR 08FDEA04904Skin · damagedWHILE DRILLING THE NR 1 PYLON INBD FWD 311N5193-2 SKIN PANEL NUMEROUS FASTENER HOLES WERE OVERSIZED AND ELONGATED. THE NUMEROUS FASTENER HOLES THAT WERE OVERSIZED AND ELONGATED WERE REPAIRED AND A NEW 311N5193-2 SKIN PANEL INSTALLED PER MAE EA NR 757-5452-1Nov 17, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Attach FittingsSDR FDEA200811064775Stringer · gougedINTERNAL STRUCTURE S 8L BS 1000-1020 STR HAVE SEVERAL NICKS. REPAIRED STR 8 L BS-1000-1020 IAW SRM 53-00-03 REPAIR NR 1 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Longeron/StringerSDR FDEA200811064774Stringer · gougedINTERNAL STRUCTURE , STR 5L HAVE SEVERAL SCRATCHES BS 750-BS770. REPAIRED IAW SRM 53-00-03, REPAIR NR 1, ENTIRE STR SECTION REPLACED BS 730-780 AT S-5L CAT "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Longeron/StringerSDR FDEA200811064777Floorbeam · corrodedFLOORBEAM CORRODED AT STA 1681 RBL 13. REPAIRED CORRODED FLOORBEAM AT STA 1681, RBL 13 IAW SRM 53-00-51 REPAIR NR 2 , "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED ( TRANSFERRED FRON N00582 )Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200811064776Web · corrodedDECK PLATE WEB AT STA 1681, RBL 13 CORRODED. REPAIRED CORRODED DECK PLATE WEB AT STA 1681 RBL 13 IAW SRM 53-60-51 REPAIR NR 2 "A" MAJOR REPAIR NO FOLOW-UP INSP REQUIRED (TRANSFERED FROM N00582 ).Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR 08FDEA04777Floorbeam · corrodedFLOORBEAM CORRODED AT STA 1681 RBL 13. REPAIRED CORRODED FLOORBEAM AT STA 1681 RBL 13 IAW SRM 53-00-51. REPAIR NR 2, "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED .Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA04776Web · corrodedDECK PLATE WEB AT STA 1681 RBL 13 CORRODED. REPAIRED CORRODED DECK PLATE WEB AT STA 1681 RBL 13 IAW SRM 53-60-51 REPAIR NR 2 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED (TRANSFERED FROM N00582 ).Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR 08FDEA04775Stringer · damagedINTERNAL STRUCTURE S 8L BS 1000-1020 STRINGER HAS SEVERAL NICKS. REPAIRED STRINGER 8 L BS-1000-1020 IAW SRM 53-00-03 REPAIR NR 1 "A" MAJOR REPAIR, NO FOLLOW-UP INSP REQUIRED.Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Longeron/StringerSDR 08FDEA04774Stringer · damagedINTERNAL STRUCTURE, STRINGER 5L HAVE SEVERAL SCRATCHES BS 750-BS 770. REPAIRED IAW SRM 53-00-03, REPAIR NR 1, ENTIRE STRINGER SECTION REPLACED BS 730-780 AT S-5L CAT "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.Nov 6, 2008 · N915FD · Boeing 757236 · Fuselage Main, Longeron/StringerSDR 08FDEA04710Frame · gougedMAIN CABIN AT STA 1620 STR 5L HAS TOOLMARK. REPAIRED FRAME BS 1620 S5L IAW SRM 53-00-07 REPAIR NR 1. REMOVED AND REINSTALLED SHEAR TIES FOR ACCESS. CATEGORY A REPAIR, NO FOLLOW-UP REQUIRED.Nov 4, 2008 · N915FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA200811034690Seat Track · corrodedMAIN CABIN FLOOR BS 640 RBL 45 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR NR 1. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.Nov 3, 2008 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04690Seat Track · corrodedMAIN CABIN FLOOR STA 640 RBL 45 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR NR 1. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.Nov 3, 2008 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04668Floorbeam · corrodedMAIN CABIN STA 345 LBL14 FLOOR SUPPORT HAS AREA OF CORROSION AROUND FASTENER HOLES. REMOVED THE DAMAGED AND FABRICATED PARTS ON MAE TRAVELERS NR T8/755777, T8/755776, T8/748077, T8/748078. INSTALLED REPAIR PARTS AND UPPER T-CHORD ON STA 345 LBL 52 TO RBL18 INov 1, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200810304638Frame · dentedFWD CARGO COMPT., BS 760, S-24L, FRAME UPPER J-ANGLE IS DENTED. REPAIRED FRAME, BS 760, S-24L, FWD CARGO COMPT, IAW SRM 53-00-07, REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 51-40-02. THIS REPAIR I CLASSIFIED AS A CATEGORY 'B" MAJOR REPAIR WITH THE FOLLOWING FOLLOct 30, 2008 · N918FD · Boeing 757236 · Fuselage Main, FrameSDR 08FDEA04618Skin · corrodedNR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. FOUND SKIN ASSY CORRODED OUT OF LIMITS IAW SRM 54-50-01 (L= 1.5 INCH, W= 2.0 INCH, D= .028 INCH). ROUTED SKIN PANEL ASSY FOR REPAIR ON AMII WORK ORDER NR 7434, DATED 07/14/08 AGAOct 29, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA200810144348Floorbeam · gougedFLOORBEAM BS 1280 UPPER SURFACE LBL 60 TO RBL 60 HAS GOUGES. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED DAMAGED AREA OF FLOORBEAM UPPER CHORD, FABRICATED NEW CHORD, LOCATED AND DRILLED ANGLES AND STRAPS IAW SRMOct 14, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA04348Floorbeam · gougedFLOORBEAM STA 1280 UPPER SURFACE LBL 60 TO RBL 60 HAS GOUGES. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. REMOVED DAMAGED AREA OF FLOORBEAM UPPER CHORD, FABRICATED NEW CHORD, LOCATED AND DRILLED ANGLES AND STRAPS IAW SRM Oct 14, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA200810064248Crease Beam · corrodedCREASE BEAM ANGLE FITTING ATTACHMENT AND CHORD HAS CORROSION AT S-17R, BS 520-540. REMOVED AND REPLACED CREASE BEAM ANGLES, 2EA, ANGLE SPLICES, 4EA, AND O/B CHORD IAW MAE TRAVELERS T8/760009, T8/760007, T8/760010 AND EA F-5310-110929, REV-, DATED 10/03/08.Oct 6, 2008 · N920FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA04250Skin · corrodedNR 2 PYLON O/B FWD. 311N5193-3 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED HINGE TO GAIN ACCESS TO REMOVED SKIN PER SRM 51-40-02, INSTALLED AFT T/R HINGE PER SRM 51-401-02. REMOVED FWD SKIN P/N 311N5193-2 PER SRM 51-40-02, REMOVED CORROSION PER SRM 54-Oct 6, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR 08FDEA04234Skin Panel · corrodedNR 2 PYLON I/B FWD SKIN PANEL ASSY, HAS CORROSION ON INNER AND OUTER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B FWD SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIEDOct 6, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR 08FDEA04233Skin Panel · corrodedNR 2 PYLON I/B AFT SKIN PANEL, 311N5046-33, HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B AFT SKIN PANEL IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AOct 6, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR 08FDEA04232Skin Panel · corrodedNR 1 PYLON LT SKIN, INNERWALL IS CORRODED JUST FWD OF PRE-COOLER. REMOVED AND REPLACED LT SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002 AND EA F-5450-121408. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS Oct 6, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA200809234009Bulkhead · damagedNR 1 PYLON MID BULKHEAD LT SIDE HAS 1EA NUT PLATE WITH DOUBLE DRILLED FASTENER HOLES. REPAIR COMPLIED WITH EA F 5452-110907 AND MAE EA 757- 54521-16-A1802, MAJOR REPAIR.Sep 23, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Bulkhead/FirewallSDR 08FDEA04009Bulkhead · damagedNR 1 PYLON MID BULKHEAD LT SIDE HAS 1 NUT PLATE WITH DOUBLE DRILLED FASTENER HOLES. REPAIR COMPLIED WITH EA F 5452- 110907 AND MAE EA 757- 54521-16-A1802, REV, MAJOR REPAIR.Sep 23, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Bulkhead/FirewallSDR 08FDEA03991Skin · misrepairedEXISTING RT FUSELAGE SKIN EXTERNAL DOUBLER REPAIR AT BS 670, S-20R-S-21R, COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. DURING EVALUATION OF ABOVE NOTED REPAIR PER ATTACHMENT "B" OF EO F-5100-7-5001, PART 1, IT WAS DISCOVERED THAT PREVIOUS REPAIR WASep 22, 2008 · N915FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA200809173911Crease Beam · corrodedAFT PIT, CREASE BEAM WEB, LWR SURFACE BS 1360 BS 1340 RBL 67 INCHES HAS CORROSION REMOVED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FABED NEW WEB ON TRAVELER T8/753327, INSTALLED NEW WEB IAW SRM 51-40-02 AND REINSTALLED CREASE BEAM IAW SRM 51-4Sep 17, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA03911Crease Beam · corrodedAFT PIT, CREASE BEAM WEB, LOWER SURFACE BS 1360 BS 1340 RBL 67 INCH HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. FABRICATED NEW WEB ON TRAVELER T8/753327. INSTALLED NEW WEB IAW SRM 51-40-02 AND REINSTALLED CREASE BEAM IAW SRM Sep 17, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR RYN2008F00018Slide · unwanted deployF/O ACCIDENTALLY BLEW L1 DOOR SLIDE. C/A IN WORK. (K)Sep 11, 2008 · N526NA · Boeing 757236 · Escape Slide
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