N456UP

Service difficulty reports · 269

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N456UP' AND registry_match = 'registration'
  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 IPXA2026081830212Actuator · faultedATB, GEAR DISAGREE EICAS AND GEAR LIGHT. RAN CHECKLIST RETURN TO CAE & CAUTION LIGHT TOO. REVERSED DMP 32-30-1. REPLACED PROX SWITCH 065 REF FIM 32-09 FAULT TREE 821. ADJUSTED PROX SWITCHES 065 AND 078 AS REQUIRED TO 5.5 MILIHENRI NEAR BOTH LOCKED AND UNLOCKEDAug 18, 2026 · N456UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2026073088683Landing Gear · warning messageAIR TURN BACK, AFTER TK-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK TO SLC. R&R NOSE LANDING GEAR RETRACT ACTUATOR PER AMM 32-34-01 UP TO AND INCLUDING STEP F.(13)(C)Jul 28, 2026 · N456UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2026072888683Warning Light · false activationAIR TURN BACK, AFTER TAKE-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK TO SLC. PERFORMED NOSE GEAR SWING IAW AMM 32-34-00. OPS CHECKED GOOD AND GEAR SWING TIMES ARE WITHJul 28, 2026 · N456UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2026070256697Warning Message · illuminatedAIR TURN BACK, GEAR DISAGREE EICAS MSG AND GEAR LIGHT PRESENT AFTER T/O. ATB AS DIRECTED BY FLIGHT CONTROL. GEAR OPERATED NORMALLY DURING EXTENSION. FOUND FAULT S10065 AND S10078 ON PSEU. C/W OPS OF PSEU IAW AMM 32-61-03. OPS CHECK GOOD. LUBRICATED NLG LOCK AJul 1, 2026 · N456UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2025112157102Strap · corrodedWORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05.FABRICATED STRAP P/N 143N5553-1SAAU FOR LWR FWD FLOOR BEAM, IAW DWG 143N5553. WORK ACCOMPLISHED ON TRAVELER #7003269899Oct 31, 2025 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025110357102Floor Support · corrodedWORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05 INSP VERIFIED STEP 16 OUT OF SEQUENCE INSTALLED REPLACEMENT RADIUS FILLER P/N 143N5553-1 PER BOEING DWG. 143N5255 REQUIREMENT AND B757-200PF SRM 51-40-02-0G -0.Oct 31, 2025 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025111264443Strut · crackedFOUND DURING DVI NR 1 PYLON OTBD SIDE HAS A CRACKED PANEL LANDING UNDER PANEL P/N 311N5049-139. INSTALL REPAIR DOUBLER, FILLERS 2 EACH /ALL REPAIR PARTS AT # 1 PYLON O/B SIDE IAW EA # 757-5450-01-B0589 STEP 17. ACCOMPLISH REPAIR PER VT-SAA EA 757-5450-01-B05Oct 14, 2025 · N456UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2025111897577Seat Track · corrodedMAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95706-REQ1 AND VT-SAA EA 757-5300-01-B0624 REV IR PRIOR TO FURTHER FLIGHT.Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025110597614Retainer · corrodedSTR, MAIN DECK CABIN FLOOR STRUCTURE STRAP HAS CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 61, ID STICKER NUM. (061-002). ATA 53-05. INSTALLED NEW RETAINER P/N 146N5064-2SAAU AND NEW FILLER ON MAIN DECK CABIN FLOOR AT APPROX FROM BS 1660 TO BS 1681, RBL Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025110593368Floorbeam · corrodedMAIN DECK CARGO COMPARTMENT BELOW ACCESS PANNEL FLOOR 231XSF HAS CORROSION. ACCOMPLISHED REPAIR PER EO-95804-REQ1 AND VT-SAA EA 757-5310-01-B0586, REV. IR, PRIOR TO FURTHER FLIGHT.Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025110593910Floorbeam · corrodedMAIN DECK CARGO COMPARTMENT STA 620 RBL-45.5 TO RBL-54.9 BELOW ACCESS PANNEL FLOOR 232XPF HAS CORROSION ON FLOORBEAM LOWER AREA, INSTALLED REPAIR PARTS AND TWO ANGLES ON FLOORBEAM UPPER CHORD APPROX. STA 620 BETWEEN RBL 45.5 AND RBL 62 IAW SRM 53-00-51-2R-6 ROct 10, 2025 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025110597577Seat Track · corrodedMAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50.Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025110598112Floorbeam · corrodedMAIN DECK CABIN FLOORBEAM UPPER CHORD HAS CORROSION AT APPROX BS 1600, LBL 45.50 THRU LBL 62.22, ACCOMPLISHED REPAIR PER VT-SAA EA 757-5300-01-B0603, REV IR.Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025110598146Floorbeam · corrodedMAIN DECK CABIN FLOORBEAM LOWER CHORD HAS CORROSION ONTO SEVERAL AREAS AT APPROX BS 1360, BL 0 THRU LBL 45.50, ACCOMPLISH REPAIR PER EO-95790-REQ1 AND VT-SAA EA 757-5310-01-B0588, REV. IR, PRIOR TO FURTHER FLIGHT.Oct 10, 2025 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025110581619Support Fitting · corrodedMAIN DECK CARGO COMPARTMENT BELOW FLOOR ACCESS PANEL 222XAF HAS CORROSION. REMOVED AND REPLACED FITTING P/N 141N5131-35 PER BOEING DRAWINGS 141N5131 AND 141N5250 AND B757-200PF SRM B757-200PF-SRM-51-40-02-0G-0.Oct 9, 2025 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025110540630Strap · corrodedRT ELEV TIP HAS CORROSION ON UPPER AND LOWER STRAPS, FLL-003, INSTALL CONDUCTIVE FRAME AT R/H ELEVATOR TIP UPPER SURFACE REF. B-757-200 SRM 51-40-02-OG-0. INSTALLED CONDUCTIVE FRAME, 2EA. STRAPS 1EA. SHIMS, 1EA. FITTING, AT R/H ELEVATOR TIP UPPER SURFACE REOct 7, 2025 · N456UP · Boeing 75724APF · Elevator StructureSDR IPXA2025111315848Support · corrodedRT APU DOOR SUPPORT LONGERON HAS MULTIPLE AREAS OF CORROSION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0582, REV IR.Oct 6, 2025 · N456UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025111395107Skin · corrodedSECTION 48 CORRODED FUSELAGE SKIN BET. STA.1885.20 TO 1918.90 LH SIDE JUST ABOVE THE APU LH DOOR FWD HINGE AS MARKED (059-07). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95725-REQ1 AND VT-SAA EA 757-5330-01-B0581 REV IR. REVIEWEDOct 5, 2025 · N456UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025061164148Plate · missingATB GEAR DOORS EICAS MESSAGE. CYCLED FROM OFF TO UP PER QRH.MESSAGE CLEARED. UPON TROUBLESHOOTING FOUND LFT MAIN GEAR DOOR PROXIMITY SWITCH S10242 DAMAGED. R & R€™D S10242 IAW MM 32-61-02-201, SYS OPS CK€™S NORMAL.Jun 11, 2025 · N456UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2024111362738Heater · faultedR WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW R/R #3 RT SIDE WINDOW IAW AMM 56-11-10-424-015. WINDOW HEAT OPS CHECK AND LEAK CHECK CW. NO FAULTS NOTED. THIS CLEARS THIS DEFERRAL. DMP REVERSED, PLAC REMOVED.Nov 8, 2024 · N456UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2024110862738Heater · faulted*** SDR FILED OPEN *** R WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW DEFERRED RT #3 SIDE WINDOW HEAT IAW MEL 30-41-1-3. C/W DMP.Nov 8, 2024 · N456UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2023112705282Tee Angle · corrodedFAULT: R/H WTB T-CHORDS STA 1240 FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 TO RBL 63. INSTALLED NEW T-CHORD AND 4 E/A PLATES I.A.W SRM 51-40-02-0G.- REVIEWEDNov 22, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112605348Tee Angle · corrodedFAULT: R/H WTB T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. INSTALLED NEW PART P/N UP536071D1-1 IAW B757 SRM 51-40-02-0G. REVIEWEDNov 22, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112605270Tee Angle · corrodedFAULT: R/H WTB T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD AT RBL 63 BETWEEN FS 1180 TO FS 1240 IAW SRM 51-40-02-0G. REF, STEP 14 WORK VERIFIED. INSTALLED T-CHORD AT RBL 63 BETWEEN FS 1180 TO FS 1240 .INSPECTED.Nov 22, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112413955Skin · corroded*MAJOR REPAIR* FAULT: #1 ENGINE PYLON O/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154. NO DOT. VERIFIED COMPLIED WITH FINAL EA 757-5450-27-A3447 REV -. AND UPS EO 88763-REQ1Nov 16, 2023 · N456UP · Boeing 75724APF · Nacelle/Pylon StructureSDR IPXA2023120195921Tee Angle · corroded*SUPPLEMENTAL SDR* FAULT: R/H WTB T-CHORD, RBL 67, FOUND EXFOLIATED CORROSION, BET STA 1037 TO 1060. INSTALLED T- CHORD RBL 67 STA 1037 TO 1060 IAW SRM 51-40-02-OG. REVIEWEDNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112750267Tee Angle · corrodedFAULT: WTB STRUCTURE - FRAME WTB STRUCTURE STA. 1240 BETWEEN RBL 57 AND RBL 63 IS EXFOLIATED. INSTALLED CHANNEL STA.1240 RBL 63 I.A.W. SRM 51-40-02-0G STEP. 4,7,8 AND SRM 51-70-11-0G-0. REVIEWEDNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112750323Frame · corrodedFAULT: WTB STRUCTURE - FRAME WTB STRUCTURE BETWEEN STA. 1180 AND 1240. RBL 63 IS EXFOLIATED. INSTALLED WEB STA.1180 TO 1240 RH, 6 EA STIFFENERS BETWEEN STA.1187 TO 1235, ANGLES 1180 RBL 63 AND STA 1200 RBL 63 AND FRAME STA 1220 RBL 63 I.A.W SRM 51-40-02-0G.- VNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2023112637854Fairing · corrodedFAULT-FUS BELLY FAIRING AFT W/W CUTOUT SUPPORT FITTING WITH CORROSION SEVERAL PLACES. INSTALLED T-CHORD AT LBL 5750 BETWEEN STA 1180 TO 1240 IAW SRM 51-40-02-0G. WORK VERIFIED, NUTPLATES INSTALLED NUTPLATES P/N; BACN11P3A5C, BATCH #0004204060. RIVETS P/N: MS20Nov 10, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023112919701Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112915514Floor Support · corroded*** SUPPLEMENTAL SDR *** FAULT: MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) . DOT 07608-026 INSTALLED SUPPORT BEAM IAW SRM 51-40-02-0G. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023120119733Tee Angle · corrodedWTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65. INSTALLED NEW T-CHORD STA 1060 IAW SRM 51-40-02, STEP 4. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112819755Tee Angle · corrodedFAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 20 TO LBL 30. INSTALLED T-CHORD SECTION I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2023111315514Unknown · unknownMAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) .Nov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2023111319733Unknown · unknown*** SDR FILED OPEN *** FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65 EVALUATED T-CHORD AT STA 1060 BETWEEN LBL 50 TO LBL 65, EXFOLIATED CORROSION NOTED, AFTER FUTHER INVESTIGATION FOUND TO BE OUT LIMITS I.A.W SRM 53-00-71-1A-1 FINov 9, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023111319701Unknown · unknownWTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REF. STEP 3 , WORK VERIFIED. REMOVED T-CHORD STA 1037.67 BETWEEN LBL 20 TO LBL 65 INSPECTED.Nov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2023112984644Angle · corroded*** SUPPLEMENTAL SDR *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 INSTALLED T-CHORD I.A.W SRM 51-40-02-0G INSTALLED HINGE ASSY (4EA) AND GAUSSET ASSY 5(EA) I.A.W SRM 51-40-02-0G. REVIEWEDNov 7, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112984377Angle · corroded*** SUPPLEMENTAL SDR *** FAULT LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 INSTALLED T-CHORD STA 1037,67 TO 1060 LH SIDE IAW SRM 51-40-02, STEP 4. REVIEWEDNov 7, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112486155Skin · corroded*MAJOR REPAIR* FAULT: #1 ENGINE PYLON I/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154 . DOT 07308-005 (PLACED AT EXTERNAL SKIN) VERIFIED COMPLIED WITH EO 88741-REQ1 AND EA 757-5450-27-A3437 REV. -. JOB COMPLETENov 7, 2023 · N456UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2023111384377Unknown · unknownLEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 REMOVED T-CHORD FROM STA 1037.67 TO 1060 LH SIDE LBL 67 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA 1037.67 TO 1060 LH SIDE REMOVED.Nov 7, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023111384644Unknown · unknown*** SDR FILED OPEN *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 REMOVED T-CHORD AT AREA INTERIOR DOOR RAT I.A.W SRM 51-40-02-0G.- VERIFIED REMOVAL OF T-CHORD INTERIOR RAT DOOR AREA.Nov 7, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023112956677Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 INSTALLED WEB AT STA 900 I.A.W. SRM 51-40-02-0G. INSTALLED SECTION T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED INTERCOSTAL AT STA 900 I.A.W. SRNov 6, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023111360602Unknown · unknown*** SDR FILED OPEN *** FAULT: RH RAM AIR INLET STRUCTURE AT APROX STA 880 HAS 2 ANGLES WITH CORROSION. DOT 07608-006 REMOVED RAM AIR INLET ASSY P/N: 149N7160-31 IAW AMM 21-53-01-004-001 AND LIP P/N: 149N7160-24 AND 2 CHANNELS WITH CORROSION P/N: 149N7160-8 & 1Nov 6, 2023 · N456UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2023111356677Unknown · unknownWTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 REMOVED WEB ON FRAME STA 900 L/H IAW B757 SRM 51-40-02. VERIFIED WEB ON FRAME STA. 900 LH REMOVED.Nov 6, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023110759388Unknown · unknownWTB STRUCTURE - T-CHORD STA 900 HAS CORROSION AT APROX LBL 16 - DOT 07608-005 PERFORMED CUT OUT DAMGED T-CHORD L= 75.5" STA 900 IAW SRM 51-10-02.Nov 6, 2023 · N456UP · Boeing 75724APF · Fuselage Structure (General)SDR IPXA2023112532382Shear Tie · dentedFAULT: AFT CARGO PIT - FRAME STA. 1460 RH SIDE BETWEEM STR. 25R AND 26R HAS A DENT AT UPPER FLANGE. DOT 07308-001. INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G.- SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118.00 SRM CHAPTER 53-00-07-2R-5, TABLE #3, FOR ZNov 4, 2023 · N456UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2023100410733Engine · surgesATB ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BACK. (OR FLUCTUATIONS) REF.LINE ITEMS 9 AND 13. TECH RECOMMENDS R&R OF RT ENG BLEED VALVES AND SOLENOSep 29, 2023 · N456UP · Boeing 75724APF · Powerplant SystemSDR IPXA2023093000733Unknown · unknownATB, ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BACK. (OR FLUCTUATIONS). OPENSep 29, 2023 · N456UP · Boeing 75724APF · Powerplant SystemSDR IPXA2023092126666Control Unit · unknown**ATB**RIGHT ENG EGT REMOVED AND REPLACED RT BVCU PER AMM 75-32-01-404-023 OPS CHK OKSep 21, 2023 · N456UP · Boeing 75724APF · Compressor Bleed ValveSDR IPXA2022101787184Skin · dentedINSPECTION TYPE:N/AREF D779518 FUSELAGE TAILCONE UPPER SURFACE DENTREPAIRED PER EO B757-5330-83549-COct 17, 2022 · N456UP · Boeing 75724APF · Aerodynamic Fairings
Back to N456UP