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 FDEA201003100745Seat Track · gougedBS 418-440, RBL 45.5, SEAT TRACK GOUGED, OUT OF LIMITS.Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003100744Seat Track · gougedBS 418-440, RBL 24.75, SEAT TRACK GOUGED OUT OF LIMITS.Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003100743Support · corrodedBS 365-418, RBL 45.5, SEAT TRACK SUPPORT IS CORRODED. REMOVED CORROSION; .020" MATERIAL REMOVED, ORIGINAL MATERIAL .070", FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 7. REMOVED SUPPORT 2 BS 365-418, RBL 45 IAW SRM 51-40-02. RECEIVED NEW SUPPORT IAW Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201003100742Support · corrodedSTA 365-418 RBL 45.5 SEAT TRACK SUPPORT CORRODED FWD OUTBD CORNER. REMOVED CORROSION ; .020" MATERIAL REMOVED, ORIGINAL MATERIAL .070" , FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SUPPORT 2 BS 365-418, RBL 45, IAW SRM 51-40-02. Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201003100741Seat Track · gougedSTA 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED .018" FROM .070" ORIGINAL MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT TRACK FROM BS 418-440, RBL 45.5, SRM 51-40-02. FABRICATED NEW SEAT TRACK FROM MATERIAL PN BAC 1520Mar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003100740Seat Track · gougedSTA 418-440 RBL 24.5 SEAT TRACK GOUGED. REMOVED .019" FROM .070" ORIGINAL MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 2. REMOVED SEAT TRACK AT BS 418-440, RBL 24.75, IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK FROM MATERIAL PN BACMar 10, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010031090556Panel · crackedCLT - C1 - MAJOR REPAIR - CRACKS EMANATING FROM RIGHT WING NR 9 SLAT COVE PANEL ATTACH HOLES. REPAIRED RIGHT WING NR 9 SLAT COVE PANEL IAW EA 101742.Feb 25, 2010 · N937UW · Boeing 7572B7 · Leading Edge DevicesSDR USAA2010022690457Frame · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON FUSELAGE FRAME AT BS 729 BETWEEN S16L TO S18L. REPAIRED FUSELAGE FRAME AT BS 729 BETWEEN S16L TO S18L IAW EA 101761.Feb 25, 2010 · N937UW · Boeing 7572B7 · Fuselage Main, FrameSDR USAA2010022690456Crease Beam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON CREASE BEAM Z-ANGLE AT BS 680 & BS 740. REPLACED CREASE BEAM Z-ANGLE AT BS 680 & BS 740 IAW B757 SRM 51-40-01.Feb 24, 2010 · N937UW · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201002220490Seat Track · damagedMAIN CABIN SEAT TRACK BETWEEN STA 860-880 RBL 25 HAS DAMAGED LUG. R & R SEAT TRACK, FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL II , III AND SRM 51-40-02. FABRICATED SEAT TRACK. CLASSIFIED CATEGORY "A" MAJOR REPAIR.Feb 22, 2010 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002180452Skin · dentedDENT IN ACFT SKIN AT STA 557 BETWEEN S-24L AND S-25L SKIN REPAIRED IAW SR 53-00-01 FIG. 201 REPAIR 7, THIS IS A CAT. "B" REPAIR WITH INSPECTIONS THRESHOLD OF 24,000 F.C. AND REPEAT EVERY 12,000 FLT CYCLES. USING HFEC INSP IAW NDTM 51-00-01 PT. 6 THIS IS MAJOFeb 18, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA2010022690454Floorbeam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON FLOORBEAM FORWARD LOWER SURFACE AT BS 377.7 BETWEEN LBL 9.25 TO LBL 35.75. REPAIRED FLOORBEAM AT BS 377.7 BETWEEN LBL 9.25 TO LBL 35.75 IAW B757 SRM 53-00-51.Feb 18, 2010 · N937UW · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201002180453Bracket · missingACFT IS MISSING SUPPORT BRACKET FOR FAN DUCT ASSY. A REPAIR WAS ACCOMPLISHED AT BS 1681, S28L; ON MAE MOD W/C 118550428ACSR01, MAE EA NR 757-5362-16-F2487 REV -.Feb 18, 2010 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201002160435Frame · damagedMAIN DECK STA 395 FRAME BETWEEN STR S-1 AND S-2R HAS EXISITING HOLES WITH LESS THAN SRM PITCH AT BS 395 S-2L TO S-2R FRAME REPAIR WAS ACCOMPLISHED ON MAE W/C 43188560001 AND MAE EA 757-5332-16-F2538, REV -DATED 02/10/2010. CLASSIFIED CATEGORY "A" MAJOR REPAIFeb 16, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, FrameSDR USAA20100219BB009Power Unit · inoperativePHL - FLASHLIGHT, FWD FLIGHT ATTENDANT STATION WAS INOPERATIVE. REPLACED POWER UNIT AT FWD F/A SEAT FLASHLIGHT.Feb 15, 2010 · N936UW · Boeing 7572B7 · Emergency EquipmentSDR FDEA201002150427Shim · migratedSTRUT NR 1 INBD WING FITTING HAS A SHIM MIGRATION ON OTBD SIDE ABOUT .5". COMPLIED WITH EA F-5740-131555 WINGS LT INBD SIDE LOAD FITTING EXPOSED SHIM PART 1. TRACKING IS REQUIRED IAW PART 2, AND PART 3 OF EA. A/C FLIGHT CYCLES (21,726), AND FLIGHT HOURS (52,Feb 15, 2010 · N909FD · Boeing 7572B7 · Wing Main, Frame StructureSDR USAA2010030490496Slat · debondedCLT - C2 - MAJOR REPAIR - NR 6 SLAT HAS DISBOND ON THE OUTBOARD END OF WEDGE. REPLACED NR 6 SLAT IAW JOB CARD 19L51027001.Feb 12, 2010 · N937UW · Boeing 7572B7 · Leading Edge DevicesSDR FDEA201002120405Gate · corrodedL-1 DOOR LOWER EDGE SECTION HAS CORROSION. REMOVED AND REPLACED L-1 DOOR LOWER GATE IAW MM 52-11-38 AND SRM 51-40-02, ADJUSTED AND PRESSURE CHECK IAW MM 52-11-00, THIS IS A MAJOR REPAIR.Feb 12, 2010 · N909FD · Boeing 7572B7 · Passenger/Crew DoorsSDR FDEA201002110390Gate · corrodedNR 2 PAS RT DOOR LOWER GATE CORRODED AND PITTED ON OUTER SEAL RETAINER. R & R R2 DOOR LOWER GATE ASSY. FOUND OUT OF LIMITS IAW AMM 52-11-38 AND SRM 52-10-02 FIG 101 DETAIL III. ADJUSTED R2 DOOR IAW AMM 52-11-00-5. CLASSIFIED CATEGORY "A" MAJOR REPAIR.Feb 11, 2010 · N909FD · Boeing 7572B7 · Passenger/Crew DoorsSDR FDEA201002020303Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CAP CORRODED AT STA 740 BETWEEN LBL 54.9 TO APPROX LBL 72 DUE TO DISCREPANCY EFFECTING THE PTF MOD A FLOORBEAM REPAIR WAS ACCOMPLISHED AT STA 740 LBL 36-65 ON MAE W/C NR 11835002B22R02 AND MAE EA NR 757-5335-16-F2407 REV- DATED 11/1Feb 2, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201002020299Connector · dirtyON DEPARTURE GOT EICAS TE FLAP DISAGREE WITH FLAPS SHOWING BETWEEN 1 AND 5 DEGREES. EXTENDED FLAPS BY ALT METHOD AND LANDED UNEVENTFULLY PREFORMED FIM 27-51-00 BIT TEST OF FSEU SHOWED LT WING ASYM INSPECTED IAW FIM LT WING TORQUE TUBES, NO DAMAGE. INSPECTED Feb 2, 2010 · N901FD · Boeing 7572B7 · Flight Control System WiringSDR FDEA201001270278Slide · looseTEST FLIGHT - L-1 DOOR SLIDE ASSY LOOSE FROM DOOR AND COVER. REINSTALLED ESCAPE SLIDE AND SLIDE COVER - OPS CHECK, OPS CHECK GOOD IAW MM 25-66-01-4. PN D30654-122, SN 0618.Jan 27, 2010 · N907FD · Boeing 7572B7 · Escape SlideSDR FDEA201001210211Skin · chafedFUSELAGE SKIN, REPAIR DOUBLER AT BS 745, S19L/20L, HAS A RIDING CONDITION AT LAP SEAM. INTERNAL CUTOUT HAS EXCESSIVE EM/NOT IAW SRM. REMOVED DOUBLER IAW SRM 51-40-02. REMOVED DAMAGE ON SKIN IAW SRM 53-00-01. PERFORMED HFEC ON INTERNAL AND EXTERNAL DOUBLER SJan 21, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA201001180173Skin · chafedRT WING INBD UPPER FLAP L/E STRUCTURE HAS CHAFINGS. REMOVED CHAFE FROM RT WING INBD FLAP IAW SRM 57-53-01, FIG 101 DETAIL VI. FOUND TO BE OUT OF LIMITS. ORIG MATERIAL 0.055 AFTER REWORK 0.049. CUT OUT DAMAGE AREA IAW SRM 57-53-01 FIG 201 REPAIR 2. REMOVED PAJan 18, 2010 · N909FD · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA201001170165Bushing · misalignedSTRUT NR 1 DIAG BRACE WING FITTING OTBD BUSHING HAS MIGRATED. REMOVED BUSHINGS IAW SOPM 20-50-03. RECEIVED REPAIR BUSHINGS ON TRAV NR T9/811726. INSTALLED 2EA REPAIR BUSHINGS IAW EA F-5740-131560. CATEGORY "A". MAJOR REPAIR.Jan 17, 2010 · N909FD · Boeing 7572B7 · Nacelle/Pylon, Main FrameSDR FDEA201001140138Skin · dentedSTA 1401, 1" BELOW S-25L. FUSELAGE SKIN IS DENTED. MEASURED DENT AT STA 1401 S-25L, A=1.0, Y=.050 . A/Y= 20, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED SHEAR TIE BETWEEN S-25L TO S-26L. CUT OUT DAMAGED SKIN 3"X4" IAW SRM 53-00-01 FIG 2Jan 14, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA201001140144Floorbeam · corrodedFLOORBEAM UPPER CAP CORRODED AT STA 740 BETWEEN RBL 54.9 AND APPROX RBL 72.0. (INTERFERS WITH MAE P TO F CONVERSION) AT BS 740 RBL 54-9-RBL 72.0. FLOOR BEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C 118350441BZ2R04Jan 14, 2010 · N909FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201001140136Shear Tie · damagedAFT CARGO PIT STA 1400 S-25L TO S-26L SHEAR TIE HAS ELONGATED HOLES REMOVED SHEAR TIE STA 1400 S-25L TO S-26L IAW SRM 51-40-02. FABRICATED SHEAR TIE ON MAE TRAVELER T10/814745. IAW SRM 51-10-01. LOCATED HOLES AND TRIMMED IAW SRM 51-40- 05. TREATED AND PRIJan 14, 2010 · N909FD · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR USAA2011011390197Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL AT FIN STA 116 APPROX 12 INCHES AFT OF LEADING EDGE. REPLACED RIGHT VERTICAL STABILIZER PANEL IAW B757 SRM 55-30-01.Jan 13, 2010 · N939UW · Boeing 7572B7 · Vertical Stabilizer, Plate/SkinSDR FDEA201001120087Spar · corrodedRT WING REAR SPAR WEB CORRODED AT RT WING FUEL SHUTOFF VALVE AT VALVE MATING SURFACE AREA. ACCOMPLISHED EA NR F-5710-131557, WING RT REAR SPAR CORROSION AT FUEL SHUTOFF VALVE. MAJOR REPAIR.Jan 12, 2010 · N907FD · Boeing 7572B7 · Wing SparSDR USAA20091231BB168Cylinder · out of limitsFLL - L1 EMERGENCY POWER SPRING CYLINDER BELOW LIMITS. REMOVED AND REPLACED POWER SPRING CYLINDER.Dec 30, 2009 · N200UU · Boeing 7572B7 · Passenger/Crew DoorsSDR FDEA200912304569Skin · dentedLT FUSELAGE STA 720, 4 INCHES BELOW LWR LAP SEAM SKIN IS DENTED. MEASURED DENT WITH AN A=.620, Y=.024, A/Y=26, AT BS 720, 4" BELOW LOWER LAP SEAM. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL 3. CUT OUT DAMAGED SKIN IAW SRM 53-00-01, REPAIDec 30, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA200912214491Skin · dentedRTWING NR 10 SLAT T/E WEDGE UPPER SURFACE, HAS A DENT 34" FROM OTBD EDGE. EVALUATED DENTS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG. 101, SHEET 4, NOTE K. DENT "A"- L=.500", W=.400", D=.003", A/Y=133. DENT "B"- L=.700", W=.670", D=.005", A/Y=134. BOTDec 21, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200912214490Skin · dentedRT WING NR 8 SLAT T/E WEDGE UPPER SURFACE HAS 3EA. DENTS, 54" FROM INBD EDGE. EVALUATED DENTS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, SHEET 4, NOTE K. DENT "A" - L=.900", W=.850", D=.010", A/Y=85 / DENT "B" - BOTH ARE L=1.40", W=1.10", D=Dec 21, 2009 · N909FD · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200912184486Spar · corrodedRT WING REAR SPAR WEB CORRODED AT RT FUEL SHUTOFF VALVE AT VALVE MATING SURFACE AREA. REPAIR IAW EA F-5710-131557. ACCOMPLISHED EA NR F-5710-131557 WING-RT REAR SPAR WEB CORROSION AT FUEL SHUTOFF VALVE, THIS IS A MAJOR REPAIR WITH NO FOLOW=UP INSPECTION REDec 18, 2009 · N907FD · Boeing 7572B7 · Wing SparSDR FDEA200912184484Skin · corrodedNR 2 PYLON INBD SIDE SKIN HAS CORROSION AT STA 174.30 INSIDE FWD OF FWD BULKHEAD. BLENDED CORROSION ON NR 2 PLYON SKIN LOCATED AT PP STA 174.30 IAW SRM 54-50-01DETAIL II, III, AND IV. ORIGINAL SKIN THICKNESS 0.090. DIMENSION OF BLEND OUT IS .5 X .5 X .014. RDec 18, 2009 · N909FD · Boeing 7572B7 · Nacelle/Pylon, Plate/SkinSDR USAA2010012990221Flap · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT WING INBOARD MAIN FLAP TRAILING EDGE AT OUTBOARD END. REPAIRED RIGHT WING INBOARD MAIN FLAP TRAILING EDGE AT OUTBOARD END IAW B757 SRM 57-53-01 & 51-70-10.Dec 16, 2009 · N936UW · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA200912164476Seat Track · corrodedSEAT TRACK LBL 45.5 FS 440 TO 680 PITTED, SCRATCHED, AND GOUGED AROUND SCALLOPS. REMOVED CORROSION AND GOUGES I.A.W SRM 51-10-02 BLENDED AREA L=10.0"XW=.50 X D=.06 EXCEEDS THE .02 DEPT GIVEN IN SRM 53-00-52 FIG 101 DET 1 VERIFIED MAT. AS BAC1520- 792 IAW SDec 16, 2009 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA20091217BB164Actuator · unwanted extendMCO FLT 1729 EN ROUTE CLT TO MCO. SPOILER LIGHT ILLUMINATED. EICAS MESSAGE SPOILERS DISPLAYED. WITH SPOILERS SELECTED DOWN. UNCOMMANDED ROLL TO RIGHT. RIGHT OUTBOARD SPOILER PANEL FULLY EXTENDED, WOULD NOT STOW/RETRACT. THE FLIGHT LANDED IN MCO WITHOUT Dec 16, 2009 · N942UW · Boeing 7572B7 · Drag Control ActuatorSDR FDEA200912164475Skin · crackedLWR AFT CARGO DOOR INNER SKIN CRACKED AT EDGE OF CUTOUT BELOW FWD VENT DOOR. REMOVED AFT CARGO DOOR INNER SKIN IAW SRM 51-40-02. RECEIVED NEW CARGO DOOR INNER SKIN. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. TOP COATED IAW SDec 16, 2009 · N909FD · Boeing 7572B7 · Cargo/Baggage DoorsSDR USAA20091216BB163Transformer · faultyCLT FLT 1728 EN ROUTE MCO TO CLT. DURING APPROACH, TRAILING EDGE AND LEADING EDGE FLAPS FAILED TO EXTEND NORMALLY. LEADING EDGE EXTENDED BY ALTERNATE. TRAILING EDGE FLAPS NEVER INDICATED MOVEMENT, EVEN AT ALTERNATE 15 FLAP GAUGE NEVER MOVED. TRAILING EDGEDec 15, 2009 · N202UW · Boeing 7572B7 · Trailing Edge Flap Control SystemSDR FDEA200912154473Frame · damagedFWD ACCY COMT-AREA FWD OF NLG W/W - FRAME 231.25 AT BL0 (FRAME, FRAME REPAIR, INTERCOSTAL UPPER PLATE AND DOORLOCK FITTING) DAMAGED "CHAFED AND GOUGED". BLENDED GOUGE IN REPAIR DOUBLER IAW SEM 51-10-02. L=.100",W=.250",D=.023", FOUND OUT OF LIMITS IAW SRM 53-Dec 15, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA200912104405Support · corrodedSEAT TRACK SUPPORT STA 365-418 RBL 24 CORRODED REMOVED CORRISION ON SEAT TRACK SUPPORT STA 365-418 RBL 24 IAW SRM 53-00-52 FIG 101 DETAIL VIII. ORIG MATERIAL 0.080 AFTER REWORK 0.061 FOUND TO BE OUT OF LIMITS. REMOVED SUPPORT IAW SRM 51-40-02. RECEIVED NEW SUDec 10, 2009 · N909FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA2009121193328Skin · delaminatedPHX - B1 - MAJOR REPAIR - NR 5 SLAT T/E WEDGE SURFACE HAS 2 AREAS OF DELAMINATION FROM ISS104 TO ISS150. REPAIRED NR 5 SLAT T/E UPPER SURFACE IN BEND FROM ISS104 TO ISS150 IAW B757 SRM 51-70-10.Dec 10, 2009 · N202UW · Boeing 7572B7 · Leading Edge DevicesSDR FDEA200912104404Skin · delaminatedPREVIOUSLY INSTALLED REPAIR REQUIRES REPLACEMENT. REPAIR IDENTIFIED AT RT WING, OTBD AFT FLAP, LWR SURFACE, 103" FROM INBD EDGE. REPAIRED AREA IAW SRM 51-70-05. REMOVED DAMAGE, CLEANED AND PREPPED AREA FOR REPAIR. FABRICATED REPAIR PLIES, BONDED REPAIR PLIEDec 10, 2009 · N908FD · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA200912104403Skin · damagedPREVIOUS REPAIR INSTALLED REPAIR REQUIRES REPLACEMENT, REPAIR INDENTIFIED AT RT WING OB AFT FLAP LWR SURFACE 40" FROM IB EDGE REMOVED DAMAGE ON RT WING OB AFT FLAP LWR SURFACE AT WS 397-459. CLEANED AND PREPED AREA, FABRICATED REPAIR PN 04-009-0022 BATCH NR 0Dec 10, 2009 · N908FD · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA200912094392Shear Tie · corrodedAFT PIT BILGE FRAME SHEAR TIE, STA 1500 BETWEEN S-29L TO S-30 HAS CORRSION. REMOVED CORROSION FROM SHEAR TIE STA 1500 S-29L - S30L. ORIG. MAT 0.050 AFTER REWORK 0.020 FOUND TO BE OUT OF LIMITS. IAW SRM 53-00-04 FIG 101 DETAIL V. FABRICATED NEW SHEAR TIE. LODec 9, 2009 · N909FD · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR FDEA200912094390Strap · corrodedCORROSION AROUND FASTENER HOLES AT APU AIR INTAKE CUTOUT STA 1825 BET S 3R-6R. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=15.0 W=1.0 D=0.025 ORIG MATERIAL 0.100. FOUND OUT OF LIMITS IAW SRM 53-80-01 DET III. REMOVED ANGLE IAW SRM 51-40-02. REMOVED FADec 9, 2009 · N909FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA200912074365Seat Track · corrodedSEAT TRACK STA 365-418 RBL 45 CORRODED. REMOVED CORROSION ORIG MATERIAL 0.080 REMOVED 0.018. FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL VIII. REMOVED SEAT TRACK IAW SRM 51-40-02. INSTALLED NEW SEAT TRACK SUPPORT AT STA 365-418, RBL 45 IAW SRM 5Dec 7, 2009 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912034346Seat Track · gougedMCD SEAT TRACK HAS NUMEROUS GOUGES APPROX BETWEEN STA 1180 TO STA 1280 AT RBL 25. BLENDED GOUGES IN SEAT TRACK IAW SRM 53-00-52. ORIGINAL MATERIAL THICKNESS; .250" /AFTER REWORK; .017"/ MATERIAL LOSS; .080". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PAGE 10Dec 3, 2009 · N909FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach Fittings
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