Boeing 757-2B7

Service difficulty reports · 3,730

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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 = '7572B7'
  ORDER BY difficulty_date DESC"

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SDR FDEA200912034345Stringer · crackedWHILE REMOVING FLOORBEAM AT STA 1661 A CRACK WAS FOUND AT STA 1661 STR 18L. REMOVED CRACKED STRINGER 18L, STA 1645 - 1670 IAW SRM 51-40-02. LOCATED, DRILLED, AND TRIMMED STRINGER AND HAT CHANNEL . IAW SRM 51-40-05. INSTALLED STRINGER AND HAT CHANNEL STA 1645Dec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Longeron/StringerSDR FDEA200912034344Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 324-365 B/L 0 CORRODED. REMOVED IAW SRM 51-10-02. BLENDED AREA & FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. REMOVED SUPPORT IAW SRM 51-40-02. RECEIVED NEW PART. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRDec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200912034342Strap · corrodedAPU AIR INTAKE DOOR HSG FWD SUPPORT STRAP HAS CORROSION UNDER NUTPLATES. REMOVED CORROSION ON FORWARD APU SUPPORT STRAP IAW SRM 51-10-02, BLENDED AREA ORIG MAT 0.095. MAT LOSS L=.5 W=0.025, D= 0.025 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL I.Dec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200912034341Support Angle · corrodedAPU AIR INTAKE DOOR HSG RT SIDE SUPPORT ANGLE HAS CORROSION UNDER NUTPLATES. REMOVED CORROSION ON RT SUPPORT ANGLE AT BS 1787-1825, S6R, IAW SRM 51-10-02. BLENDED AREA; ORIGINAL MATERIAL WAS .063" THICK/AFTER REWORK WAS .044" / HAD .019" MATERIAL LOSS. FODec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200912034340Support Angle · corrodedAPU AIR INTAKE CUTOUT BET. STA 1787-1825 S3R, SUPPORT ANGLE CORRODED AROUND FASTENER HOLES. REMOVED CORROSION ON SUPPORT ANGLE AT BS 1787-1825, AT S3R, IAW SRM 51-10-02. BLENDED AREA WAS; L= 3.0", W=1.0", D= .020". FOUND TO BE OUT OF LIMITS IAW SRM 53-80-03Dec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200912034339Skin Splice · corrodedAFT PIT BILGE STA 1400 SKIN SPLICE STRAP BET S 29L AND S30 HAS CORROSION. REMOVED CORROSION ON SKIN SPLICE IAW SRM 51-10-02. BLENDED AREA L=3.0 W=1.0 D=0.029. ORIG MATERIAL 0.071 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED SPLICE Dec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA20091203BB158Battery · dischargedMCO - F/A EMERGENCY FLASHLIGHT AT POSITION 3R DOOR HAS A LOW BATTERY. MAINTENANCE REPLACED FLASHLIGHT.Nov 30, 2009 · N941UW · Boeing 7572B7 · Emergency EquipmentSDR FDEA200911304254Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM STA 377.7 AT LBL 25 BOTH FWD AND AFT FASTNER HOLES AT LOWER SURFACE HAVE CORROSION. REMOVED CORROSION FROM UPPER TEE, MAT. REMOVED .016 FROM 0125. FOUND TEE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL 4, REMOVED PREVIOUS REPAIR Nov 30, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200911304253Skin · crackedRT WING NR 10 SLAT INNER COVE PANEL INBD OF OTBD TRACK IS CRACKED AT FASTNER HOLE REMOVED COVE PANEL IAW SRM 51-40-02. FABRICATED NEW COVE PANEL PN 7075-T6, 0.050C, P/N 0001375870 IAW SRM 57-43-01 FIG 1 SHEET 3. LOCATED AND DRILLED IAW SRM 51-40-02. INSTALLENov 30, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR USAA20091130BB156Battery · dischargedPHL - THE FLASHLIGHT AT L1 DOOR NEEDS A NEW BATTERY. REMOVED AND REPLACED FLASHLIGHT L1 ASSEMBLY.Nov 30, 2009 · N942UW · Boeing 7572B7 · Emergency EquipmentSDR FDEA200911274206Bushing · corrodedLT WING PYLON DIAGONAL BRACE FITTING " WING SIDE" HAS MIGRATING BUSHINGS. REMOVED 2 EA BUSHINGS IAW SOPM 20-50-03 FOUND CORROSIONS IN LUG BORE, REAMED LUG TO A FINAL DIAMETER OF 1.640 IN. AND HFEC FOUND NO DAMAGE OR DEFECTS IAW NTM 51-00-00 PT6 FIG 11 COMPLIEDNov 27, 2009 · N907FD · Boeing 7572B7 · Wing, Attach FittingsSDR FDEA200911274205Skin · crackedRT WING NR 10 SLAT AT OTBD TRACK ATTACHMENT SKIN CRACKED AROUND ATTACH RIVETS. REMOVED COVE PANEL IAW SRM 51-40-02. FABRICATED NEW COVE PANEL PN 7075-T6 0.050C B/T NR 0001375870 IAW SRM 57-43-01 LOCATED AND DRILLED IAW SRM 51-40-02. INSTALLED NEW COVER PANELNov 27, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200911274204Seat Track · crackedDURING SURVEILLENCE FOUND SEAT TRACK FLANGE CRACKED AT APROX STA 490, RBL 415.5. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIG 1, REPAIR 1, THIS IS A CATEGORY A REPAIR NO FOLLOW-UP INSPECTIONS REQUIRED.Nov 27, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911254169Crease Beam · corrodedMCD FLOOR BOARD SUPPORT CREASE IS CORRODED APPROX BETWEEN STA 1260-1270 AT RBL 65. REMOVED CORROSION IAW 51-10-02 MAT THICKNESS 0.080. AFTER REWORK 0.040 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101. VARIFIED MATERIAL AS BAC 1515-5537075T6 IAW SRM 53-Nov 25, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200911254171Seat Track · gougedSEAT TRACK STA 418-440 RBL 24 GOUGED. BLENDED AREA ORIG- MAT .125, AFTER REWORK .098, OUT OF LIMITS, 1 IN X 1 IN AREA, IAW SRM 51-10-02, 53-00-52, DETAIL VII. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 53-10-52, FIG I, TRENov 25, 2009 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911254170Seat Track · gougedSEAT TRACK STA 418-440 RBL 45 IS GOUGED. REMOVED SEAT TRACK STA 418-440, RBL 45, IAW SRM 51-40-02. BLENDED AREA IAW SRM 51-10- 02, ORIG-MAT .125 AFTER REWORK .098 OUT OF LIMITS, I IN BY 1.5 IN AREA, IAW SRM 53-00-52, DETAIL VII. FABRICATED NEW SEAT TRACK IAWNov 25, 2009 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911254168Crease Beam · corrodedFS 1270 L CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIG MATERIAL 0.071 MAT. LOSS 0.010 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101 DETAIL III . REMOVED CREASE BEAM STA 1180-1285, LBL 68 IAW SRM 51-40-02. FAB CREASE BEAM IAW SRM 53-60-Nov 25, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200911234129Attach Angle · bentLT HORZ STAB PANEL 332CL NUTPLATE ATTACH ANGLE BENT CUT OUT DAMAGE, FABRICATED FILLER, RADIUS FILLERS AND REPAIR ANGLES. IAW EA F-5510-131542. INSTALLED REPAIR PARTS IAW EA F-5510-131542. COMPLIED WITH EA F-5510-131542 DATED 11/23/2009.Nov 23, 2009 · N908FD · Boeing 7572B7 · Horizontal Stabilizer StructureSDR FDEA200911234128Skin · dentedDENT ON FUSELAGE SKIN, BS 1704, S20L, IN THE LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL 3, DUE TO PROXIMITY TO SKIN SPLICE. ACCOMPLISHED SKIN DOUBLER REPAIR IAW EA F-5330-131129, REV DATE 10/21/09; "FUSELAGE - PLANov 23, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200911204104Crease Beam · crackedRT SIDE CREASE BEAM WEB STA 740-760 CRACKED AT INBD CREASE BEAM CHORD SPLICE POINT. REMOVED ANGLE SPLICE SHIM FOR ACCESS, IAW SRM 51-40-02. REMOVED CREASE BEAM WEB THAT WAS FOUND TO BE OUT LIMITS IAW SRM 53-60-15 AT BS 740-760, RBL 65, INBD CREASE BEAM SPLICENov 20, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200911204096Door Frame · corrodedL2 DOOR CUTOUT FWD FRAME, LWR, BS 690 INBD SIDE, HAS AN APPROX 4 INCH SECTION OF CORROSION, DIRECTLY ABOVE FLOOR LEVEL. ACCOMPLISHED L2 DOOR SURROUND WEB CORROSION REPAIR IAW EA F-5310-131540, DATED 10/07/09, REV-. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJORNov 20, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200911204094Frame · damagedMAIN DECK BS 820, S2L, AFTER REMOVAL OF TV MONITOR, DOUBLERS FOUND DOUBLE DRILLED HOLES. CUTOUT DAMAGED FRAME AT BS 820, S5L-S5R IAW SRM 53-00-07, FIG. 201, REPAIR NR 1. REMOVED 2 EA ACFT BRACKETS, LAV BRACKET, ELEV BRACKET FOR FOM IAW SRM 51-40-02. FABRNov 20, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA200911194047Skin · crackedNR 1 SLAT 2ND INBD COVE PANEL CRACKED AT FASTNER HOLES. FABRICATED NEW COVE PANEL IAW SRM 57-43-01 FIG 1. LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED NEW COVE PANEL IAW SRM 51-40-02. MAJOR REPAIR.Nov 19, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200911194046Slat Track · crackedFASTNER HOLE CRACKS AT LT NR1 SLAT INBD TRACK FWD WEB SURFACE. REMOVED COVE PANEL ON NR 1 SLAT WS 711.5-WS 806.5 IAW SRM 51-40-02. FABRICATED NEW COVE PANEL PN 7075-T6 0.050C, BN 1610155 IAW SRM 57-43-01 FIG 1. LOCATED AND DRILLED IAW SRM 51-40-05. INSTANov 19, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200911184013Frame · damagedMAIN DECK STA 800 L/BL8 (APPROX) AFTER REMOVAL OF TV MONITOR DOUBLERS FOUND WITH DOUBLE DRILLED HOLES. CUT OUT DAMAGED FRAME AT STA 800 STR 5L TO 5R IAW SRM 53-00-07 FIG 2014 R1,REMOVED 2 EA. ACFT BRACKET 1 EA LAV BRACKET 1 EA ELEV BRACKET FOR FOM IAW SRM 51-Nov 18, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA200911184012Floor Support · misalignedEXISTING FLOORBEAM REPAIR AT STA 700, LBL 55, TO LBL 65, WILL INTERFERE WITH INSTALLATION OF SECTION 43, SEAT TRACK 657N3332-3, AT LBL-58, STA 660, TO STA 884. REPAIR AT STA 700, LBL 55, TO LBL 65, WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONNov 18, 2009 · N908FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200911184011Skin · crackedRT WING NR 9 SLAT AT OTBD TRACK ATTACHMENT SKIN CRACKED AROUND ATTACH POINTS. REMOVED PANEL 624GB ,OTBD RIB, SEAL RETAINER, SEAL, AND CRACKED COVE PANEL FROM OTBD NR 9 SLAT AT WS 565-WS 681. IAW SRM 51-40-02. FABRICATED NEW COVE PANEL IAW SRM 57-43-05 FIG 1 ANov 18, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200911133953Web · corrodedMAIN CABIN DECK AFT FLOOR WEB CORRODED STA 1700 TO 1720 BL O, TO LBL 53, REMOVED CORR, REMOVED ANGLE IAW SRM 51-40-02. RECEIVED NEW ANGLE ON MAE TRAV NR T9/808947, P/N 7075-0.071B, FABRICATED NEW DOUBLER REPAIR MAT PN 2024-T3.063C, INSTALLED NEW ANGLE AND REPNov 13, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200911133952Bracket · misalignedACFT HAS INCOMING MISSING STRUCTURE THAT IS NEEDED TO ASSEMBLE THE E-7 RACK. DUE TO THE DISCREPANCY AFFECTING THE PTF MOD , NEW BRACKETS WERE FAB, AND INSTALLED ON MAE EA NR 3002772/ 757-5362-16-F2323, AND MAE W/C 118550428ACSR01, THIS NR IS FOR TRACKING PURPNov 13, 2009 · N907FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200911133951Floor Support · corrodedMAIN DECK STA 660-680 S-17L FLOOR PANEL SUPPORT EXFOLIATED. REMOVED FLOOR SUPPORT AT STA 680-750 LBL 63. RECEIVED INNER CHORD PN 143N8328-53. LOCATED AND DRILLED HOLES IAW SRM 51-40-05. INSTALLED FLOOR SUPPORT IAW SRM 51-40-02 CATEGORY "A" MAJOR REPAIR.Nov 13, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA200911133949Skin · corrodedFUSELAGE EXTERNAL SKIN LT SIDE, APPROX STA 925 AND STR 13, HAS A BULGE WITH BROKEN RIVETS. REMOVED WINDOW DOUBLER, STRINGER CLIPS, SPLICE, AND SHEAR TIES IAW SRM 51-40-02. CUTOUT DAMAGE IAW SRM 51-10-02. HFEC INSP INDICATED NO CRACKS AROUND CUTOUT OR FASTNERNov 13, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200911123935Mount · corrodedNR1 ENG PYLON FWD ENG MOUNT PAD CORRODED. REMOVED CORROSION AT NR 1 ENG PYLON FWD LWR WEB (MOUNT) IAW SRM 54-50-01. ORIG MAT THICKNESS AT FWD BLENDOUT AREA .263, AFTER REWORKED .261, AND AT MIDDLE BLENDOUT AREA ORIG MAT THICKNESS .264, AFTER REWORKED .261, ANNov 12, 2009 · N907FD · Boeing 7572B7 · Engine Mount SectionSDR FDEA200911113927Floorbeam · corrodedMCD FLOORBEAM AT STA 345 BETWEEN LBL 20 TO RBL 3 HAS CORROSION. (FLOORBEAM TEE). REMOVED CORROSION ORIG- MAT .125 REMOVED .025, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51- FIG 101, DETAIL III, FABRICATED UPPER TEE IAW SRM 53-00-51, FIG 201, INSTALLED TEE.Nov 11, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200911113928Floorbeam · corrodedMCD FLOORBEAM IS CORRODED AT STA 365 BETWEEN BL 0 TO RBL 24.75. REMOVED CORROSION. REMOVED 0.020 FROM .125 ORIGINAL. OUT OF LIMITS IAW SRM 53-00-51. REMOVED PREVIOUS REPAIR FROM LBL 14-RBL 68 IAW SRM 51-40-02. FABRICATED -1 CHORD FROM PN BAC1505-100617/20 BNov 11, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200911103922Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CAP CORRODED AT FS 740 BETWEEN LBL 54.9 TO APPROX LBL 72.0. FLOORBEAM REPAIR WAS ACCOMPLISHED ON NR N00002, W/O NR 0046071. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. THIS N/R IS FOR TIME TRACNov 10, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200911063881Seat Track · corrodedMAIN DECK, BS 700-740, LBL 45.5, SEAT TRACK ASSY HAS CORROSION IN SEVERAL AREAS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. ORIGINAL MAT THICKNESS .071" / REMOVED .016". FABRICATED NEW SEAT TRACK MAT. 60-6549/24, BATCH NR 1544829 IAW SRNov 6, 2009 · N907FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200911053854Skin · dentedFUSELAGE SKIN PROTRUDING DENT STA 1440 STR 24L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-00-01, REMOVED LINER AND INSULATION FOR ACCESS IAW MM 25-52-003 AND 25-50-007-4. CUT OUT DAMAGED AREA DIM 7/8" IAW SRM 53-00-01 FIG 201, FABRICATED DOUBLER ANDNov 5, 2009 · N901FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200911043849Skin · delaminatedLT WING, NR5 L/E SLAT, T/E WEDGE, OTBD END, IS DELAMINATED. REPAIRED LT WING, NR 5 L/E SLAT, IAW SRM 57-43-02; BONDED DOUBLER REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.Nov 4, 2009 · N908FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200911043843Skin · damagedFUSELAGE SKIN, BS 715, BETWEEN S24L/ 25L, SKIN HAS AN OUTWARD PUNCTURE, APPROX 12" AFT OF ANOTHER DOUBLER REPAIR. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. FABRICATED REPAIR PARTS (DOUBLER AND FILLER) IAW SRM 53-00-01, FIG 201 AND SRM 53-30-01, FIGNov 4, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200911023790Crease Beam · corrodedMAIN DECK FLOOR, BS 664-753, LBL 64, IS CORRODED IN SEVERAL AREAS. REMOVED CORROSION IAW SRM 51-10-02. BLENDED ORIGINAL THICKNESS, .080", AFTER REWORK, LOST .028" THICKNESS. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13. -REMOVED CREASE BEAM IAW SRM 51-40-02Nov 2, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, StructureSDR USAA20091103BB149Battery · dischargedLAS - FLASHLIGHT BATTERY DEAD AT F/A SEAT ROW L2. REPLACED FLASHLIGHT BATTERY.Oct 31, 2009 · N937UW · Boeing 7572B7 · Emergency EquipmentSDR FDEA200910313748Shear Tie · corrodedAFT CARGO COMPT - SHEAR TIE CORRODED AT FRAME 1320, BTW S-28L TO S-29L, WL138.5. REMOVED SHEAR TIE FROM STA 1320 S28L TO 29L. FABRICATED NEW SHEAR TIE IAW MAE TR NR T9/806073. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-70-16. TREATED AND PRIMED IAW SRM 51Oct 31, 2009 · N907FD · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR FDEA200910303738Floorbeam · damagedFLOOR BEAM AT BS 1640 REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED FLOORBEAM AT BS 1640, LBL 63 TO RBL 63, IAW SRM 51-40-02. ANODIZED NEW FLOORBEAM IAW BAC 5019, REV. U, P.O. NR MSC0012758. FABBED NEW FLOOR BEAM FROM BAC1518-338, BATCH NR 000169230Oct 30, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910283719Floorbeam · damagedFLOORBEAM AT STA 1661, REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED FLOORBEAM IAW SRM 51-40-02, FABED NEW FLOORBEAM BAC1518-338, IAW SRM 51-40-05. INSTALLED NEW FLOORBEAM STA 1661, RBL TO LBL 63, IAW SRM 51-40-02. CATEGORY "A" , MAJOR REPAIR.Oct 28, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910273690Skin · dentedFUSELAGE, LHS, BS 690, BETWEEN S24L/25L, SKIN HAS DENTS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG. 101, DETAIL 3. CUT OUT DAMAGED AREA PER SRM 53-00-01, FIG. 201, REPAIR NR 3. FABRICATED REPAIR DOUBLER PER DWG 143N3691. LOCATED, DRILLED, TREATED REPAIROct 27, 2009 · N907FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200910273689Floorbeam · damaged2EA EXISTING HOLES IN THE FLOORBEAM UPPER CHORD AT STA 780 RBL 58 ARE ELONGATED AT BS 780 RBL 58 FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE W/C 118350441BZ2R03 AND MAE EA# 757-5335-16-F2306 REV - DATED SEPT 30, 2009.Oct 27, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910273688Floorbeam · failed2 EA EXISTING HOLES IN THE FLOORBEAM UPPER CHORD AT STA 680 RBL 58 ARE ELONGATED AT BS 680 RBL 58 FLOORBEAM REPAIR WAS ACCOMPLISHED ON MAE MOD W/C 118350441BZ2R03 AND MAE EA# 757-5335-16-F2306.Oct 27, 2009 · N908FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA200910273686Skin · misrepairedPREVIUSLY INSTALLED FLASH REPAIR AT NR 7 L/E SLAT, EXTERNAL SKIN, NOT INSTALLED PER SRM. CUT AND REMOVED EXISTING REPAIR ON NR 7 L/E SLAT EXTERNAL SKIN IAW SRM 57-43-01 FIG 201 REPAIR 1 , FABRICATED REPAIR PLATE ON TRAV. T9/ 806985AND DOUBLER IN TRAV T9/ 8Oct 27, 2009 · N907FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200910263675Web · wornNUMBER 2 PYLON 311N5040-6 UPPER AFT WEB IS WORN AT APPROX. PPS 162 - 172. BLENDED WORN AREA AT APPROX PPS 170.90. ORIGINAL MATERIAL THICKNESS .063", AFTER REWORK .054"; D=.009", L=1.0", W=.700". FOUND TO BE OUT OF LIMITS PER SRM 54-50-01, NOTE "B", DETAIL 3.Oct 26, 2009 · N907FD · Boeing 7572B7 · Nacelle/Pylon Miscellaneous StructureSDR USAA20091027BB148Flashlight · inoperativePHL - L1 DOOR FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY.Oct 25, 2009 · N201UU · Boeing 7572B7 · Emergency Equipment
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