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"

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SDR IPXA2025012042868Floorbeam · corrodedFLOOR BEAM STA 560 BTWN BL-0 AND LBL 24.75 IS CORRODED. DOT 142-326. EVALUATED DAMAGE IN FLOOR BEAM STA 560 BTWN BL-0 AND LBL24.75.:P1)ORIGINAL THICKNISS 0.220'' MATERIAL LOSS 0.010'' MAXIMUN ALLOWABLE 0.022'' MATERIAL REMANING 0.210''.P2) ORIGINAL THICKNISS Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025012041655Shear Web · corrodedMAIN CABIN DECKING STA 620 TO 660 BTWN LBL 64 AND LBL 45.5 HAS NUMEROUS AREAS OF CORROSION. CIRCLED IN RED. DOT 142-322. ORIGINAL MATERIAL 0.063" AFTER REWORK 0.059", MATERIAL REMOVED 0.004" FOUND TO BE IN LIMITS PER SRM 53-30-15-1A-3 DETAIL II. TOOL T17449.Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025020444461Bracket · crackedFS 900 LBL12 BRACKET THAT ATTACHES TO INTERCOSTAL TO 900 T-CHORD IS CRACKED INSTALLED NEW BRACKET ON STR FS 900 LBL12 IAW SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025020444699Tee Angle · corrodedFS 1037-1060 RBL 65 T-CHORD IS EXFOLIATED ON NUTPLATE EDGE. INSTALLED T-CHORD IAW B757-200, SRM 51-40-02 ON STR FS 1037-1060 RBL 65. PERFORMED CPCP STEPSJan 11, 2025 · N401UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025020443836Tee Angle · corroded.LH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 30 HAS LIGHT CORROSION. DOT 28-08. INSTALLED 8 NUTPLATE AND T-CHORD AT STA 1020-1040, LBL 30 IAW B757-200, SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025020443736Attach Bracket · crackedFS1180 LBL 13 ON BOTTOM OF FUSELAGE SKIN WTB STR ATTACH BRACKET HAS CRACK IB SIDE OF RADIUS. INSTALLED BRACKET AT FS 1180 LBL 13 OUTER FUSELAGE SKIN TO WTB STR IAW B757-200, SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025020444064Tee Fitting · corrodedFAULT-STR-ZONE 100. RH WING TO BODY STRUCTURE, T-CHORD AT STA 900-920, RBL 60 HAS CORROSION. DOT 28-10. INSTALLED T-CHORD AT STA 900-920 RBL 60 IAW B757 SRM51-40-02 HL P/N BACB30NX6K2 BACH #4244109 COLLAR P/N BACC30BL6 BACH # 4207142. REVIEWEDJan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025020443668Tee Fitting · corrodedLH WING TO BODY STRUCTURE, T-CHORD AT STA 1040-1060, LBL 57 HAS LIGHT CORROSION . DOT 28-04. INSTALLED T-CHORD AT STA 1040-1060, LBL 57 LH WING TO BODY STRUCTURE, IAW B757-200, SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025013043970Tee Fitting · corrodedLH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 50 HAS 10 NUTPLATES CORRODED. DOT 28-09. INSTALLED T-CHORD AT STA 1020-1040, LBL 50 IAW B757-200, SRM 51-40-02. OSD: 1/31/2025Jan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025020443088Bracket · crackedFS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR BRACKET HAS CRACK ON IB RADIUS. INSTALLED BRACKET AT FS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR IAW B757-200, SRM 51-40-02.Jan 11, 2025 · N401UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025020343798Tee Fitting · corrodedLOWER FUSELAGE STRUCTURE, T-CHORD AT STA 1020-1040, LBL 0, HAS CORROSION. VERIFIED INSTALLATION OF NEW T-CHORD AT STA 1020-1040 RBL 0. P/N BACB30NX8K12, BATCH 0004260079, QUANTITY 1EA. COLLAR P/N HL79-8, BATCH 0004088263, QUANTITY 1EA. RIVETS P/N MS20470AD6-6Jan 11, 2025 · N401UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025012042718Seat Track · corrodedSEAT TRACK AT STA 600 RBL 64 IS CORRODED ON INSIDE OF TRACK. DOT 142-324. RESTORED SURFACE PROTECTION IAW.SRM 51-20-01 AMM 51-21-15. MATERIAL USED ALODINE P/N ALODINE1132 BATCH 0004336881. PRIMER P/N 02-013-8 BATCH 4263196, WHITE P/N PG6-W2K4Q BATCH 4340857 ANJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012042799Floorbeam · corrodedFLOOR BEAM STA 560 BTWN RBL 45.5 AND RBL 24.75 IS CORRODED. DOT 142-325. VERIFIED EVALUATED DAMAGE IN FLOOR BEAM STA 560 BTWN RBL 45.5 AND 24.75 FOUND TO BE WITHIN LIMITS. GIVEN OK TO RESTORE SURFACE PROTECTION. RESTORED SURFACE PROTECTION IAW.SRM 51-20-01 ANJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025012041370Seat Track · corrodedFLOOR STRUCTURE AT STA 440 LBL 24.75 UNDER FLOOR PANEL 231XBF HAS AREA OF CORROSION. DOT 142-314. RESTORED SURFACE PROTECTION IAW SRM 51-20-01 AND TOP COAT IAW AMM 51-21-15. MATERIALS USED.Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012041456Seat Track · corrodedSEAT TRACK AT STA 500 LBL 45.5 IS CORRODED. DOT 142-316. CLEANED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS OF SEAT TRACK CROWN IS, 0.130". A MATERIAL LOSS OF 0.006" WAS NOTED USING ULTRA SONIC, T93968. MAX LOSS ALLOWED IS 0.020". REMAINING THICKNESS IJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012041468Floor Panel · corrodedMAIN CABIN FLOOR DECKING UNDER FLOOR PANEL 231XFF HAS AREAS OF CORROSION ON DECKING. DOT 142-317. CLEANED MULTIPLE AREAS IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS FOR ALL AREAS IS 0.100". ALL FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2.Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025012041407Web · corrodedMAIN CABIN FLOOR DECKING STA 440 TO 460 BTWN LBL 24.75 TO LBL 65 HAS NUMEROUS AREAS OF CORROSION. (UNDER FLOOR PANEL 221XCF) (CIRCLED IN RED) DOT 142-315. CLEANED MULTIPLE AREAS IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS FOR ALL AREAS IS 0.100". ALL FOUND TJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025020431025Skin · dentedR/H WING, #8 SLAT, UPPER SKIN WITH 8 DENTS (RED CIRCLE). DOT 73-004. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.Jan 10, 2025 · N401UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA2025012012393Skin · damagedFUSELAJE ZONE 200 HAS EVIDENCE LIGHTNING STRIKE BETWEEN STA. 1320 TO 1440 (S11-S26). ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-00-01-2R, REPAIR 28 PER SRM 53-60-01-2R-0.Jan 9, 2025 · N401UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025012404769Deck Plate · corrodedCORROSION FOUND BOTTOM OF THE FRAME AT STA 1681.80 APPROX 5" LEFT OF RBL 24.75. AREA MARKED IN RED. INSTALLED 1 EA PLATE + 2 FASTENERS PN BACB30NW6K5X BTCH 000349754. IAW SRM 51-40-02-OG.Jan 9, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012404348Deck Plate · corrodedCORROSION FOUND BOTTOM OF THE FRAME AT STA 1681.80 APPROX 13" LEFT OF RBL 24.75. AREA MARKED IN RED. INSTALLED 1 EA PLATE + 2 FASTENERS PN BACB30NW6K5X BTCH 000349754. IAW SRM 51-40-02-OG.Jan 9, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012004883Deck Plate · corrodedFAULT: CORROSION FOUND ON SURFACE OF THE DECK PLATE AROUND A FASTENER HOLE AT STA 1681.80 APPROX 5.75" LEFT OF LBL 24.75. AREA MARKED IN RED. INSTALLED 1 PLATE + 2 EA FASTENERS REMOVED FOR FOM IAW SRM 51-40-02 OG. FASTENER PN BACB30NW6K5 BTCH 0004349754.Jan 9, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012005151Deck Plate · corrodedCORROSION FOUND AROUND 3EA FASTENERS ON THE TOP OF THE DECK PLATE AT STA 1701, RBL 24.75. AREA MARKED IN RED. INSTALLED 3 FASTENERES IAW SRM 51-40-02-OG. PN BACB30NW6K8X BTCH 0004346844. REQUET OK TO RESTORE SUFACE PROTECTION.Jan 9, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012005950Seat Track · corrodedCORROSION FOUND ON TOP OF THE SEAT TRACK FLANGE AROUND 2EA ATTACHING FASTENERS AT STA 1681.80 RBL 45.50. AREA MARKED IN RED. INSTALLED 2 FASTENERES IAW SRM 51-40-02-OG. PN BACB30NY6K8X BTCH 0004346844. REQUET OK TO RESTORE SUFACE PROTECTION.Jan 9, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012089351Seat Track · corrodedTHE SEAT TRACK FLANGE AT BL-0 STA 1681.80, HAS PITTING CORROSION AROUND THE ATTACHING FASTENERS. ALL DAMAGE MARKED IN RED. INSTALLED 2 FASTENERES IAW SRM 51-40-02-OG. PN BACB30NY6K8X BTCH 0004346844. REQUET OK TO RESTORE SUFACE PROTECTION.Jan 8, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012959818Angle · corrodedFOUND AN ANGLE CORRODED UNDER DECK PLATE AT STA 1720 RBL 24. INSTALLED 1 NEW ANGLE IAW SRM B757-200 SRM 51-40-02-OG. OSD: 1/30/2025Jan 7, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025013059623Skin · dentedFUSELAGE BETWEEN STA.1896.20 AND STA 1918.9 LEFT UPPER SIDE SKIN HAS DENT (NOT MAPPED). DOT 62-06. EA-62.ACCOMPLISH PERMANENT REPAIR PER 757-200PF SRM REV 121 CHAPTER 51-70-10-2R-4 FIGURE 201 SHEET 1 (REPAIRS TO LARGE DAMAGE) PER SRM 53-80-01-2R. OSD: 2/4/202Jan 7, 2025 · N401UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025020765831Cam · gouged*SUPPLEMENTAL SDR* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. VERIFIED SREO-14721-REQ001 REV1 WAS ACCOMPLISHED. REVIEWEDJan 7, 2025 · N401UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025012959971Angle · corrodedCORRODED ANGLE FOUND UNDER THE DECK PLATE AT STA 1720 LBL 5. INSTALLED 1 NEW ANGLE IAW SRM B757-200 SRM 51-40-02-OG. PN BACR15GF6D7 BTCH 0003812153. 0.20 LB.. OSD: 1/30/2025Jan 7, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025020465996Angle · crackedNR 2 ENG STRAP AT NAC STA. 149.5 HAS CRACK AT HI-LOCK.DOT 69-003. EL-69. INSTALLED FRAME ANGLE IAW SRM 51-40-02-0G. AUDIT COMPLETE.Jan 7, 2025 · N401UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025020465427Bracket · crackedFAULT:STR-Z400 #1 ENG PYLON HYD LINE BRACKET DAMAGED AT STRAP.NAC STA 149.5. DOT 69-001. EL-69. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.Jan 7, 2025 · N401UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025013165597Angle · damagedCORRODED ANGLE FOUND UNDER THE DECK PLATE AT STA 1720 RBL 30.Jan 7, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025011359796Angle · faultedFAULT: REFERANCE FRAME REPAIR T3F18E005ERCC, CORRECTIVE ACTION 6 & 7 SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1500 IN AFT PIT REQUIRES RII AUTHERIZATION. ACCOMPLISH REPAIR PER EA 757-5360-27-A3758, REV- PRIOR TO FURTHER FLIGHT. VERIFIED RECEIVING OF FINAL EJan 7, 2025 · N406UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025010865831Cam · gouged*SDR FILED OPEN* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. APPROVED.Jan 7, 2025 · N401UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025012948449Beam · dentedFWD CARGO DOOR, AFT LOWER CORNER EDGE BEAM HAS A DENT AND GOUGES. INSTALLED CORNER BRACKET PER SRM 51-40-02. OSD: 1/30/2025Jan 6, 2025 · N420UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025011351200Panel · crackedRT WING #8 SLAT OUTBD TRACK GAP PANEL IS CRACKED. DOT 8-010. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.Jan 6, 2025 · N401UP · Boeing 75724APF · Wing Main, Frame StructureSDR IPXA2025011349181Frame · damagedFAULT: Z100 STR OPEN UP FLOOR PANELS, MBA SYSTEM, SIDEWALLS, AND TRANSITION PANEL TO F.O.M FS 1500 FRAME REPAIR AT STR 26R. INSTALLED SIDEWALL PANELS 162BW, 154JW IAW B757-200 SRM 51-40-02 AND INSTALLED LOWER AFT MBA SYSTEM AFT/AFT #8 AND #9, IAW B757-200 AMMJan 6, 2025 · N406UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025020332269Deck Plate · corrodedMAIN CARGO COMPARTMENT DECK PLATE STA 1720 FROM LBL 22 TO RBL 22 HAS CORROSION. ACCOMPLISH REPAIR PER 757-200PF SRM REV 121 CHAPTER 53-60-51-2R-5, ALTERNATIVE 1 - CUTOUT REPAIR.Jan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025020332464Angle · corrodedMAIN CARGO COMPT. STA 1715 LBL 12 UNDER THE DECK PLATE SUPPORT ANGLE HAS CORROSION. INSTALLED 1 NEW ANGLE IAW SRM B757-200 SRM 51-40-02-OG. PN BACR15GF6D7 BTCH 0003812153. 0.20 LB.Jan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025013031348Stop · gougedRIGHT WINSHIELD WIPER STOP IS GOUGED. ALL WORK ACCOMPLISHED PER IAW EO: EO-92507-REQ 1 AND VT MAE EA 757-3042-27-A3762 REV -.Jan 4, 2025 · N420UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2025012932464Angle · corrodedMAIN CARGO COMPT. STA 1715 LBL 12 UNDER THE DECK PLATE SUPPORT ANGLE HAS CORROSION. OPENJan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025012032339Deck Plate · corrodedMAIN CARGO COMPT. STA 1690 TO STA 1704 BL 0 DECK PLATE HAS CORROSION. VERIFIED INSTALLED FASTENERS IAW SRM 51-40-02-OG. RESTORED SURFACE PROTECTION IAW SRM 51-20-01 AND TOP COAT IAW AMM 51-21-15. MATERIALS USED.Jan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012032269Floor Support · corrodedSTR MAIN CARGO COMPARTMENT DECK PLATE STA 1720 FROM LBL 22 TO RBL 22 HAS CORROSION REQUEST OK TO REINSTALL 1 SUPPORT ANGLE REMOVED FOR FOM ON STEP 2.Jan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025012032379Deck Plate · corrodedMAIN CARGO COMPT. STA 1681.8 BETWEEN BL 0 TO LBL 22 DECK PALTE HAS CORROSION. VERIFIED: PERFORMED OPEN-HOLE HFEC INSP ON ALL FASTENER HOLES IN THE BLENDED REPAIR AREA AT STA 1681.80 BETWEEN BL-0 TO LBL 22. ALL FASTENER HOLES IN THE REPAIR AREA ARE CRACK / DEFEJan 4, 2025 · N420UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025010731065Buss Bar · arced*SUPPLEMENTAL SDR* R1 WINDOW: LOWER BUSS BAR HAS SIGNS OF ARCING WITH MOISTURE INGRESS ALONG OUTBOARD AREA REMOVED AND REPLACED R1 WINDOW, OPS CHECK GOOD. AMM 56-11-01Jan 4, 2025 · N409UP · Boeing 75724APF · Window System WiringSDR IPXA2025010631065Buss Bar · arcedR1 WINDOW: LOWER BUSBAR HAS SIGNS OF ARCING WITH MOISTURE INGRESS ALONG OUTBOARD AREA ACCOMPLISHED STEPS UP TO 2.D.(6) OF R1 WINDOW REMOVAL IN REF TO AMM 56-11-01.Jan 4, 2025 · N409UP · Boeing 75724APF · Window System WiringSDR IPXA2025010522565Frame · not reported*SDR FILED OPEN* REF FRAME REPAIR T3F18E005ERBT, CORRECTIVE ACTION 7. - SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1460 RH SIDE IN AFT PIT REQUIRES RII AUTHORIZATION ACCOMPLISH REPAIR PER EA 757-5360-27-A3756, REV- PRIOR TO FURTHER FLIGHT.Jan 4, 2025 · N406UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025011305368Window · faultedL SIDE WINDOW *EICAS. LH NO.2 SLINGING WINDOW REPLACED BY SERVICEABLE. I.A.W AMM 56-11-02/401 REV 135, CONFIRM THE WINDOW IS CORRECT ELECTRICAL CONNECTED IAW GMM MTX 04.02.01 REV.9. OPERATIONAL CHECK AND ADJUST C/O O.K WINDOW AND SYSTEM CONSIDERED FULLY SEJan 3, 2025 · N427UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025010305368Controller · malfunctioned*SDR FILED OPEN* L SIDE WINDOW *EICAS( ACCOMPLISHED TROUBLESHOOTING PER WDM 30-41-12-1 REV 97. SWAPPED WINDOW HEAT CONTROLLER LEFT WITH RIGHT. SAME FAULT. SWAPPED BACK TO ORIGINAL POSITION PER AMM 30-41-01 PB 401 REV 135. MEASURED RESISTANCE ON WINDOW CONTROL Jan 3, 2025 · N427UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2025010289404Lamp · inoperativeDURING PS1 CHECK FOUND MULTIPLE LIGHTS OUT IN INTERIOR EMERGENCY EXIT SIGN. RELAMPED ALL INOPERATIVE LIGHTS IN THE INTERIOR EMERGENCY EXIT LIGHTED SIGN IAW AMM 33-51-01. OPS CHECK GOOD.Jan 2, 2025 · N453UP · Boeing 75724APF · Emergency Lighting
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