Boeing 757-24APF

Service difficulty reports · 16,054

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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 = '75724APF'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2025050888488Skin · crackedRIGHT WING BEHIND SLAT # 9, FIXED LEADING EDGE HAS A CRACK.REMOVED FIXED LEADING EDGE SKIN AT RIGHT WING BEHIND SLAT # 8 AND #9 FOR REPAIR FROM OSS 562 TO OSS 696 PER SRM 51-40-02. REMOVED DAMAGE AND PREPARED AREA IAW B757-200PF SRM 51-70-17-0G-0 PAR. 4.BONDEDApr 22, 2025 · N447UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2025042390147Web · corrodedFAULT STR Z300: REMOVED THE 148N8201-8 FWD WEB ON JOB CARD T3F18E006CLWR. INSTALL FWD WEB (148N8201-8) AFTER SKIN REPAIR IS COMPLETED.148N8201-8 WEB (LONGERON 17) WAS REMOVED ON JOB CARD T3F18E006CLWR STEP #25.LOCATED AND DRILLED IAW B757-200, SRM 51-40-05.REApr 22, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042577738Flap System · warning messageON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT.REMOVED & REINSTALLED #1 FWD TE FLAP TRACK FAIRING. IAW AMM 27-51-31-422-068.(FWD AND AFT FAIRING) COMPLETE, REPAIR COMPLETE. OPS CHECK NORMAL PER AMM 27-51-00-715-00Apr 22, 2025 · N405UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2025042377738Transmission · trippedEMERGENCY DECLARED, ON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT. FLAPS TO 25 T/S REF FIM 27-51 FAULT TREE 808, FOUND LH WING FLAP TRANSMISSIONS #1 & #4 OVERLOAD INDICATORS POPPED. SEE BARCODES T3F18E006J294 & T3Apr 22, 2025 · N405UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2025050761389Plate · bulgedFAULT: STR-100-AFT CARGO COMP THRESHOLD PLATE HAS A BULGE IN IT. 33-027.RECIVED NEW PLATE #2 CARGO DOOR SILL.LOCATED AND DRILLED NEW PLATE #2 CARGO COOR SILL IAW B757-200 SRM 51-40-05.INSTALLED NEW PLATE #2 CARGO DOOR SILL IAW B757-200 SRM 51-40-02-0G-0.Apr 21, 2025 · N447UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025050152017Strap · corrodedFAULT: STR-300-APU AIR INTAKE DOOR ENTRANCE HAS CORROSION. 33-025.REMOVED FWD STRAP SND UPER ANGLE ON APU AIR INTAKE DOOR IAW B757-200 SRM 51-40-02-0G.REMOVE AND REPLACE 1 EACH APU INLET FORWARD STRAP AT STA 1787.45 (P/N: 148N3138-20) PER PRODUCTION DRAWING REApr 20, 2025 · N447UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025050948569Skin · dented*** MAJOR REPAIR *** 3EA DENTS ON LH HORIZONTAL STAB UPPER SKIN AT APROXIMATELY FS STA 90. DOT 21-18. REPAIR IAW: 757-200PF SRM REV 122 CHAPTER 51-70-10-2R-2, 250 DEG. F CURE PER SRM DETAIL III PER SRM 55-10-01-1A-1. UPPER SKIN OF LH HORIZONTAL STABILIZER UPPEApr 19, 2025 · N447UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA2025050645522Floorboard · deteriorated*** MAJOR REPAIR *** TAIL COMPARTMENT, FLOORBOARD IS DETERIORATED CENTER AFT EDGE, BELOW THS HYD MOTORS. INSTALLED TAIL COMPARTMENT FLOOR PANEL IAW AMM 53-01-01/401.Apr 19, 2025 · N447UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025050234228Frame · dented*** MAJOR REPAIR *** DENT ON FRAME STA 760 S23L AT FWD CARGO COMPARTMENT. DOT 21-03. PERFORMED TRIM OUT TO REMOVED DAMAGED IAW B757-200-SRM-51-10-02 AND SRM 53-00-07-2R-5 DETAIL I. LOCATED AND DRILLE NEW FRAME IN STA 760 S23L AT GWD CARGO IAW B757-200PF SRM Apr 18, 2025 · N447UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025050634634Skin · corrodedPYLON #2 INTERNAL AREA BETWEEN ACCESS PANEL 443CR AND 443BR HAVE CORROSION DOT 07-008 PERFORMED TRIM OUT CORROSION DAMAGE PER EA E.A# 757-5450-27-A3911 STEP 2 A, B, C, D. AND SRM 51-10-02. WORK ACCOMPLISHED PER UPS EO: EO-93643-REQ 1 AND VTMAE EA 757-5450-27-AApr 18, 2025 · N447UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025050324761Doubler · corrodedNR 1 ENG I/B PYLON PPS. 1.8317 AFT LOWER INSIDE PANEL 433HR HAS CORROSION. BLUE DOT TRIMMED OUT CORROSION DAMAGE FOR ACCOMPLISH STEP 2 OF E.A.# 757-5450-27-A3910 PRELIMINARY 1. COMPLETED THE REPAIR FOR ACCOMPLISH STEP 27 OF E.A.# 757-5450-27-A3910 PRELIMINARY Apr 18, 2025 · N447UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025042635619Tee Angle · corrodedEVIDENCE OF CORROSION ON TCHORD LOWER FUSELAGE SECTION STA900. DOT 21-06 TREATED AND PRIMED 1 E/A T-CHORD AND 8 E/A PLATES STA 900 IAW SRM 51-20-01 P/N ALODINE1132 BTCH 0004350419, PRIMER P/N 10-P4-2/2TU BTCH 0004341754. INSTALLED T CHORD REPAIR PARTS PER SRM Apr 18, 2025 · N447UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025050534270Frame · dentedDENT ON FRAME STA 840 S24R AT FWD CARGO COMPARTMENT. DOT 21-02.PERFORMED TRIM OUT AT DAMAGE AREA IAW SRM-51-10-02 AND B757-200 SRM 53-00-07-2R-5.REMOVED FASTENERS COMMON WITH THE REPAIR IAW SRM-51-40-02 AND B757-200 SRM 53-00-07-2R-5.PERFORMED HFEC ON TRIM OUTApr 18, 2025 · N447UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025042533339Structure · dentedFAULT-STR-Z800- FWD CARGO DOOR, LEFT LOWER INTERNAL CORNER WITH A DENT. DOT 21-01. INSTALLED NEW PART AT FWD CARGO DOOR P/N: 143N6618-5, BTCH: 0004388038 IAW B757 SRM 51-40-02-0G. RIVETS P/N: NAS1097KE6-5 BTCH: 0004233585. REVIEWED.Apr 18, 2025 · N447UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025050222871Floorbeam · corrodedMDC, STA 1100, BETWEEN RBL 45 AND RBL 60, BEHIND FLOOR PANEL 242XJF, FLOOR BEAM HAS 2EA SPOTS WITH CORROSION. NO DOT. REMOVED RH SIDE RAIL FROM STA 1100-1200 TO FOM I.A.W AMM 25-56-12-004-001.REMOVED 1EA CARGO LOCK AT STA 1140 TO FOM I.A.W AMM 25-56-05-024-022Apr 15, 2025 · N470UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025041625107Channel · debondedFOUR EACH EMER DESCENT REELS ATTTACH CABLE RETAINING CHANNELS BECOMING DISBONDED FROM CEILING PANEL. *<BR>CHANNELS SECURED AND IN-TACT, DEFERRED PER EO-93451-REQ1, PARTS ORDERED FOR REPAIR.<BR><BR>DEFERED PER EO-93451-REQ1, REPAIR WITHIN 90 DAYS, ACP REPEAT Apr 15, 2025 · N430UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2025041403757Floor Panel · damagedFAULT- MCD FLOOR PANEL 242XCF HAS GOUGES AND EDGE DAMAGE.FABRICATED MCD FLOOR PANEL 242XCF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XCF. AUDIT COMPLETE.Apr 14, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025042381265Support Angle · corrodedAFT BULKHEAD UPPER CEILING HORIZONTAL SUPPORT HAS CORROSION BETWEEN STA 1701 - 1720. ATA 53-60. INSTALLED 1EA ANGLE SUPPORT P/N: 146N5240U7 BATCH NO: 0004386450 AT AFT BULKHEAD UPPER CEILING BTW STA 1701-1720 IN REF B757 SRM 51-40-02-0G-0. REPLACE 1 EACH ANGApr 12, 2025 · N468UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042283146Stop Fitting · crackedEXTERNAL-LWR-HALF-FUSELAGE-DOOR-STOPS/CUTOUTS; AT AFT-CARGO-COMPT.-I/B-DOOR SURROUND-CUT-OUT STA.1400.00, UPPR-FWD (DOOR-STOP)-FITTING HAS CRACK'S ON EACH SIDE AS MRKD. #034-39.- ATA-53-00. INSTALLED SPLICE PLATE AT AFT CARGO DOOR CUTOUT O/B OF UPPER FWD DOORApr 12, 2025 · N468UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025041482306Angle · corrodedFAULT: STR Z-300 APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 HAS CORROSION ( T3F18E006CECF) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA SUPPORT ANGLE + 1 PLATE IAW B757-200-SRM-51-40-02-OG. REVIEWEDApr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025041482337Angle · corrodedFAULT: STR Z-300 APU INLET DOOR FWD UPPER CORNER ANGLE STA 1787.45 HAS CORROSION (T3F18E006CEBJ) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA CORNER ANGLE B757-200-SRM-51-40-02-OG. REVIEWEDApr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025041482229Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 (T3F18E006CEAL) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA UPPER ANGLE IAW B757-200-SRM-51-40-02-OG. REVIEWEDApr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025041017701Floor Panel · damagedMCD FLOOR PANEL 241XEF DAMAGED AT CORNER. FABRICATED MCD FLOOR PANEL 241XEF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF PANEL 241XEF.Apr 9, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025042701425Floor Support · corrodedFAULT-STR-100-AFT CARGO COMP ON 3RD RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-152. INSTALLED THE SUPPORT PANEL 3RD RH SIDE AT THE AFT CARGO PIT I.A.W SRM 51-40-02. REVIEWED.Apr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042401310Floor Support · corrodedFAULT-STR-100-AFT CARGO COMP ON FIRST RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-150. INSTALLED THE FIRST RH SIDE FLOOR PANEL IAW 757 SRM 51-40-02-0G.Apr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042401530Floor Support · corrodedAFT CARGO COMP ON 4TH LH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPORT, IAW 757-200PF SRM 51-40-05. INSTALLED 4TH LH SIDE FLOOR PANEL SUPPORT IAW SRM 51-40-02.Apr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042501411Floor Support · corrodedAFT CARGO COMP ON 2ND RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-151. LOCALED AND DRILLED NEW STRINGER, IAW B757-200 SRM 51-40-05. INSTALLED 2ND RH SIDE FLOOR SUPPORT IAW SRM 51-40-02.Apr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042701512Floor Support · corrodedAFT CARGO COMP ON 2ND LH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. LOCATED AND DRILLED FLOOR STRINGER SUPPORT T AT THE STA 1460 AND 1480. I.A.W SRM 51-40-05. INSTALLED FLOOR STRINGER SUPPORT AT THE AFTApr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025042701464Floor Support · corrodedAFT CARGO COMP ON 4TH RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-153. INSTALLED 4TH RH SIDE FLOOR PANEL SUPPORT P/N UP-146N5447-4R-5, IAW 757-200PF SRM 51-40-02.Apr 8, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025040873394Floor Panel · damagedFAULT MCD FLOOR PANEL 242XGF HAS SURFACE /EDGE DAMAGE DOT 103-17. FABRICATED / INSTALLED MCD FLOOR PANEL 242XGF, IAW / UPS SREO: B757-9692-REQ 001. REVIEWEDApr 7, 2025 · N443UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025040747037Carabiner · missingONE ESCAPE HARNESS IS MISSING A CARABINER. INSTALLED CARABINER AND STOWED ESCAPE HARNESS IN BAG PER AMM 25-61-02Apr 5, 2025 · N442UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2025042837359Frame · corrodedAFT CARGO DOOR: AFT CARGO DOOR INTERNAL LWR FRAME NO.3 (FROM FWD) HAS CORROSION. DOT NO. 17-10. INSTALLED NEW LOWER FRAME ON AFT CARGO DOOR. P/N MS20470AD6-6, B/N 0004377267, QTY 15. P/N BACB30NX6K3, B/N 0004325741, QTY 2. P/N BACN10ZV3, B/N 0000281333, QTApr 4, 2025 · N470UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025042838583Support Bracket · corrodedAFT CARGO DOOR: AFT CARGO DOOR INTERNAL LIGHT L391 ATTACHMENT PLATE IS CORRODED. INSTALLED NEW LIGHT SUPPORT OF L391 (01EA) ON AFT CARGO DOOR IAW SRM 51-40-02.Apr 4, 2025 · N470UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025041029360Floor Panel · damagedMDC, ABOVE CENTER BOX, FLOOR PANEL 242XGF EXTERNAL/INNER SURFACE AND EDGE IS DAMAGED. DOT 103-46.FABRICATED MCD FLOOR PANEL 242XGF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED MCD FLOOR PANEL 242XGF FABRICATED. AUDIT COMPLETEApr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025041029238Floor Panel · dentedMDC, ABOVE CENTER BOX, FLOOR PANEL 242XHF, EXERNAL AND INNER SURFACE HAS DENTS AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XHF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XHF.Apr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025041029564Floor Panel · dentedFAULT - Z200, COMP, MDC, ABOVE CENTER BOX, FLOOR PANEL 242XEF INNER SURFACE AND EDGE IS DAMAGED. DOT 103-51. FABRICATED MCD FLOOR PANEL 242XEF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XEF. AUDIT COMPLETE.Apr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025040929634Floor Panel · damagedMDC, ABOVE CENTER BOX, FLOOR PANEL 242XDF HAS INNER SURFACE AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XDF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XDF.Apr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025041029490Floor Panel · puncturedMDC, ABOVE CENTER BOX, FLOOR PANEL 242XBF INNER SURFACE HAS PUCTURES AND DENTS. FABRICATED MCD FLOOR PANEL 242XBF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XBF.Apr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025041029722Floor Panel · damagedMDC, ABOVE CENTER BOX, FLOOR PANEL 242XAF HAS EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XAF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PANEL 242XAF.Apr 4, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025040833949Unknown · fumesAT CRUISE LEVEL 300 SMELLED FUMES IN THE COCKPIT PERFORMED CHECKLIST CLEARED EMERGENCY AND LANDED IN IND. ACCCOMPLISHED CONDITIONAL INSPECTION PER MM 05-51-56-202. PERFORMED TROUBLESHOOTING PER FIM 21-00-01/801. INITIALLY FOUND OIL SMELL IN COCKPIT WHEN LEFT EApr 4, 2025 · N463UP · Boeing 75724APF · Air Distribution SystemSDR IPXA2025040433949Unknown · odorEMERGENCY DECLARED. AT CRUISE LEVEL 300 SMELLED FUMES IN THE COCKPIT PERFORMED CHECKLIST CLEARED EMERGENCY AND LANDED IN IND.Apr 4, 2025 · N463UP · Boeing 75724APF · Air Distribution SystemSDR IPXA2025040322399Transition Panel · corrodedAFT CARGO TRANSITION PANEL R/H SIDE BETWEEN STA 1440-1460 HAS CORROSION UNDER NUTPLATE DOT#21-5. INSTALLED FLOOR PANEL SUPPORT IAW B757 SRM 51-40-02.Apr 3, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025040323286Tee Angle · corrodedFAULT, STR, ZONE 100,T-CHORD AT FS 1220 RBL 15 UNDER WING TO BODY PANEL 198 MR HAS CORROSION DOT#21-10. REMOVED FRAME AT 1220 RBL 15 UNDER WTB PANEL 198MR IAW B757 SRM 51-40-02. RECIEVED NEW T-CHORD FROM MACHINE SHOP ON TRAVLER # T25/1809365.LOCATED AND DRILLEApr 3, 2025 · N470UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025042122221Frame · dentedFAULT: STR, ZONE 100, AFT CARGO FRAME AT STA 1460 HAS A DENT BETWEEN SR26 AND SR27 DOT#21-4.STRIPPED PROTECTIVE FINISHES ON TRANSITION PANEL ANCHOR-PLATE AT RHS TRANSITION PANEL STA 1620, IAW SOPM 20-30-02 TO INVESTIGATE THE AREA FOR CORROSION, NO CORROSION FOApr 3, 2025 · N470UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025041011799Insert · missingMAIN DECK FLOORBOARD PANEL 241XFF MISSING INSERT FWD EDGE. DOT 140-010. REPLACED MISSING FLOORBOARD PANEL 241XFF IAW SREO B757-5320-9692-KApr 3, 2025 · N470UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025040419949Guard · inoperativeEMER LIGHT ARM SWITCH COVER INOP REPLACED SWITCH GUARD PER AMM 33-51-04.Apr 3, 2025 · N419UP · Boeing 75724APF · Emergency LightingSDR IPXA2025042807149Tee Angle · corrodedCORROSION ON T CHORD STA 1150-1200 BL 70. INSTALLED (14EA NUT PLATES AND 3EA FASTENERS) AT AREA I.A.W B757-200 RM 51-40-02-OG.Apr 2, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025040207006Tee Angle · corrodedCORROSION ON T CHORD AT STA 1180-1220 BL 57.50. INSTALLED NEW T-CHORD FROM STA 1180 TO 1220 LBL 57. NUTPLATES-BACN11P3B6CG, BATCH 0004386857, QTY 17. RIVETS-MS20426AD3-6, BATCH 0004370829, QTY 34. MS20470AD6-6, BATCH 0004377267, QTY 52. HI-LOKS-BACB30MY6K5X,Apr 2, 2025 · N470UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025040206822Floorbeam · corrodedCORROSION ON L/H SIDE T CHORD AT STA 1200.REMOVED T-CHORD ON L/H, STA 1200, IAW SRM 51-40-02. RECIVED THE NEW PART P/N: UP-536071011-3.TRAVELER #: T25/1809242.INSTALLED T-CHORD L/H SIDE AT STA 1200. I.A.W SRM 51-40-02-0GApr 2, 2025 · N470UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025040206878Floorbeam · corrodedCORROSION ON L/H SIDE T CHORD AT STA 1220 BL 30.75- BL 57.50 REMOVED T-CHORD ON L/H SIDE AT STA 1220 BL 30.75 BL 57.50 FOR DELAMINATION OUT OF LIMITS IAW 53-00-71-1A-1 MATERAIL LOST 90% ALLOWABLE DAMAGE 10%. DETAIL XII.RECEIVED NEW T-CHORD FROM MACHINE SHOP ONApr 2, 2025 · N470UP · Boeing 75724APF · Fuselage Main, Floor Beam
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