Boeing 757-24APF

Service difficulty reports · 16,054

Newest first. General aviation reporting is voluntary.

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 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 IPXA2025071153206Indicator · inoperativeAIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP REMOVED AND REPLACED ON R/H WING TANK: FUEL PROBES: #1, #2, #3, #4, #5, #7, #8, #9, #10, #11 AND 12, AND PERFORMED LEAK CHECK ON THOSE FUEL ACCESS PANEL, WHERE FUEL PROBES INSTALLED BY A UPS VENDOR. ACCOJul 3, 2025 · N469UP · Boeing 75724APF · Fuel Quantity IndicatorSDR IPXA2025070753206Indicator · inoperativeAIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP ACCOMPLISHED DRY CAPACITANCE TEST PER AMM 28-41-00-735-080-002.<BR>RM TU 10 AND 11 CAPACITANCES WITHIN LIMITS.Jul 3, 2025 · N469UP · Boeing 75724APF · Fuel Indicating SystemSDR IPXA2025071890990Strap · corrodedAPU INLET DOOR AFT STRAP AT STA 1825.00 HAS CORROSION.REMOVE AND REPLACE 1 EACH S-3R SUPPORT ANGLE (P/N: 148N3152-2) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS. INSTALLED ANGLE. IAW B757-200 SRM 51-40-05. RIVET P/N: BACR15FT5Jun 30, 2025 · N472UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071890598Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS A CORROSION. FABRICATED REPAIR PARTS IAW B757-200PF SRM 53-80-15-2R-1 TABLE 201 DETAIL I.++INSTALLED ALL REPAIR PARTS (2EA STRAPS AND 2EA FILLERS) IAW B757-200PF SRM 51-40-02-0G-0 FOR ACCOMPLIJun 30, 2025 · N472UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071467822Angle · corrodedAPU INLET DOOR BETWEEN STA 1787.45 TO STA 1825 S-6R, LOWER ANGLE HAS CORROSION.Jun 28, 2025 · N472UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025062605725Proximity Sensor · dirtyON TAKE OFF WE GOT A MOMENTARY LEFT ENTRY DOOR EICAS. ON LANDING LEFT ENTRY DOOR EICAS CAME BACK ON AND REMAINED ON UNTIL PARKING. CHECKED AND INSPECTED LEFT ENTRY DOOR IAW AMM 52-12-00. CLEANED DEBRIS FROM PROX SENSOR AND TARGET. NO MESSAGE DISPLAYED ON EICASJun 25, 2025 · N455UP · Boeing 75724APF · Door Warning SystemSDR IPXA2025071090624Strap · corrodedUPON REMOVAL OF FWD UPPER AND LOWER NUT PLATE STRAPS APU INLET FOUND AFT INNER AND OUTER NUTPLATE STRAPS CORRODED ATA 53-80. FABRICATED REPAIR STRAP -2 AND REPAIR FILLER-4 TREATED AND PRIMED REF. B 757-200 SRM 53-80-15-2R-1 REPAIR 1 REQUEST OK TO INSTALL.Jun 24, 2025 · N464UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070993897Frame · dentedWORKING FRAME REPAIR BS 600 T3F18E006XCWS FOUND DENT ON FRAME BS 580. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE & REPAIR ANGLE), ONE CLIP AT FRAME BS 580 RT STGR 16, 1 EA WEB CLIP AND 1 EA FILLER AT RT FRAME BS 580 STR 17 IAW B757-200PF SRM 53-3Jun 24, 2025 · N464UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025070993879Frame · dentedWORKING FRAME STA. 520 T3F18E006XCUX FOUND DENT ON FRAME STA. 540 ATA 53-10. INSTALLED 3 EA REPAIR PARTS (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE), 1 EA CLIP AT FRAME STA 540 RH STGR 16, 1 EA WEB CLIP P/N 143N5269-2 AND 1 EA FILLER P/N: 143N5520-14 AT R/H Jun 24, 2025 · N464UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025062483756Door · bindingCREW ENTRY DOOR DIFFICUILT TO UNLOCK PERFORMED ADJUSTMENT OF CREW ENTRY DOOR IAW AMM 52-12-00, OPS CHECK GOOD AT THIS TIME.Jun 24, 2025 · N458UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025070973491Frame · dentedUPON REMOVAL OF ISOLATOR STA.600 R/H LWR. DATO PANEL T3F18E006W161 FOUND DENT ON FRAME ATA 53-10. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE), 1 EA CLIP AT FRAME STA 600 RH STGR 16, 1 EA WEB CLIP P/N 143N5269-1 AND 1 EA FILLER P/N:Jun 23, 2025 · N464UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025070973399Frame · dentedUPON REMOVAL OF ISOLATOR STA. 520 LWR. DATO PANEL T3F18E006W14Y FOUND DENT ON FRAME. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE) AND 1 EA CLIP AT FRAME STA 520 RH STGR 16 IAW B757-200PF SRM 53-30-07-2R-1 REP. 1 DETAIL VI PAR.4 STEJun 23, 2025 · N464UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025071027826Support Angle · corrodedAPU INLET INTERNAL ACCESED FROM 311 SHOWS SIGNS OF ADVANCED CORROSION AND DELAMINATION AROUND NUTPLATES AND AREA WHERE DUCT ATTACHES TO FUSLAGE ON ALL SIDE. REMOVED UPPER AND LOWER NUT PLATE SUPPORT ANGLE AT APU INLET INTERNAL IAW SRM 51-40-02-G-0. FABBRICATJun 20, 2025 · N464UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070416637Angle · corrodedSTR / AFT CARGO COMPARTMENT ANGLE UNDER R/H TRANSITION PANEL IS CORRODED BETWEEN STA 1440 AND STA 1460, RBL 25. 031-013. ATA-53-00.REMOVED CORRODED ANGLE FROM LOWER SIDE OF R/H TRANSITION PANEL STA 1440 TO STA 1460 TO F.O.M.IAW B757-200PF SRM 51-40-02-OG-0.REMJun 19, 2025 · N464UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070316837Angle · corrodedSTR / AFT CARGO COMPARTMENT FRAME STA 1440 LOWER FLANGE HAS CORROSION BETWEEN STGR 27RH AND STGR 28RH. 031-015. ATA-53-00.REMOVED CORRODED ANGLE AT AFT CARGO COMPARTMENT FRAME STA 1440 BETWEEN STGR 27RH AND STGR 28R REF B 757 SRM 51-40-02-OG-O.CLEANED AREA ON Jun 19, 2025 · N464UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025063081666Frame · dentedFAULT Z-100 STR: AFT CARGO COMPARTMENT FRAME AT STA 1480 AT STR 25 AND STR 26 L/H HAS A DENTS. INSTALLED FRAME REPAIR AND STRINGER CLIP APPLIED CIC ON AFT CARGO COMPARTMENT FRAME AT STA 1480 AT STR 25 TO STR 26 L/H IAW B757-200 SRM 53-00-07-2R-5. AND AMM 51-0Jun 12, 2025 · N450UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025062552431Attach Bracket · debondedF/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE. REPLACED F/O'S EMERGENCY ESCAPE ROPE DOOR REFERENCE IPC 25-14-01-02, ITEM 850 & 705.Jun 11, 2025 · N458UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR 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 IPXA2025061258372Evas Unit · abnormal**SUPPLEMENTAL SDR** CAPTAINS EVAS TEST TOOL MISSING. INSTALLED EVAS TOOL FOR CAPTAIN'S EVAS IAW AMM 25-69-00. OPS CHECK GOOD. REMOVED FROM NEF.Jun 11, 2025 · N428UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2025061152431Attach Bracket · debondedF/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE DEFERRED F/OS ESCAPE ROPE DOOR PANEL IAW SREO-84962-REQ001 ACOMPLISHED STEPS TO REMOVE AND STOW PANEL AND INSPECT AREA AND ROPE FOR SECURITY IAW SREO-84962-REQ001Jun 11, 2025 · N458UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025061158372Evas Unit · abnormalCAPTAINS EVAS TEST TOOL MISSINGJun 11, 2025 · N428UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2025063045954Structure · corrodedL/H ELEVATOR BETWEEN CONDUCTIVE FRAME AND TIP, SPLICE PLATE IS CORRODED UPPER AND LOWER AREAS. LOCATED AND DRILLED NEW KIT, ELEVATOR TIP FITTING ASSY P/N: 654N0244-139 S/N: TAG 453024 IAW B757-200PF SRM 51-40-02-0G-0. LOCATED AND DRILLED 2EA NEW FRAMES CONDUCJun 10, 2025 · N450UP · Boeing 75724APF · Elevator StructureSDR IPXA2025061648182Skin · dentedHORIZONTAL STABILIZER LH UPPER SKIN RIB 12 HAS A DENT.REMOVED DAMAGE APPROX. 1.90" X 2.95", WITH CORE REMOVAL. LOCATED FROM CENTER OF CUTOUT, 6.250" AFT OF FWD EOP, 18.250" FWD OF AFT EOP, 83.250" O/B OF I/B EOP, 71" I/B OF O/B EOP. IAW B757 SRM 51-70-10-2R-0 Jun 10, 2025 · N475UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA2025062648679Angle · corrodedFAULT-STR-Z600-RH WING UPPER SURFACE IN THE ROOTWING NUTPLATES BRACKET THAT ATTACH ACCESS PANEL 192CR WITH CORROSION.REMOVED CORROSION ON BRACKETS PNS 149N7210-128 AND 149N7210-190 IAW B757-200 SRM 51-10-02.EMOVED 2 EA. BRACKETS IAW B757-200 SRM 51-40-02.TREJun 10, 2025 · N450UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA2025061646315Splice Plate · corrodedR/H ELEVATOR BETWEEN CONDUCTIVE FRAME AND TIP, SPLICE PLATE IS CORRODED UPPER AND LOWER AREAS. INSTALLED 2 SPLICES PLATES + 2 SHIMS AND RESTORED TO NORMAL CONFIGURATION IAW B757-200-SRM-51-40-02.Jun 10, 2025 · N450UP · Boeing 75724APF · Elevator StructureSDR IPXA2025061608397Skin · damagedFAULT-STR-ZONE 200. UPPER FUSELAGE (CROWN), STA 1200-1220 AT S-L3 PREVIOUS BLEND OUT AROUND FASTENER NOT LISTED ON MAPPING.REMOVED PAINT ON PREVIOUS BLEND OUT AREA WITH PAINT STRIPPERS IAW 757-200PF AMM 51-21-01-157-111.ACCOMPLISHED STEP 1 OF PRELIMINARY 1, E.Jun 8, 2025 · N475UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025061608628Skin · damagedUPPER FUSELAGE (CROWN), STA 1300-1320 BETWEEN S-4L AND S-3L PREVIOUS BLEND OUT AROUND FASTENER NOT LISTED ON MAPPING.REMOVED PAINT ON PREVIOUS BLEND OUT IAW 757-200PF AMM 51-21-01-157-111.REMOVED THE NECESSARY FASTENERS (30EA) ON THE REPAIR AREA IAW 757-200PF Jun 8, 2025 · N475UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025062712469Structure · damagedFAULT Z100 STR: REFERANCE EO-92743-REQ2 #2 ENGINE PYLON OB NACELLE STRUT INTERNAL UPPER STRUCTURE AT PPS 162.76 HAS HEAT DAMAGE.VERIFIED ACCOMPLISHMENT OF STEP 1, PRELIMINARY 2, PER E.A. # 757-5450-27-A4006.WIPED AREA USING ALCOHOL P/N 02-003-414 BATCH #439286Jun 8, 2025 · N475UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2025062112617Stop Fitting · corrodedACCESS PANEL 313AL RIGHT DOOR STOP BRACKETS (2EA) CORRODED.REMOVED 02EA BRACKETS FROM ACCESS DOOR 313AL LATCH STOPS FOR EVALUATION IAW 757-200PF SRM 51-40-02.FABRICATED BRACKETS (GUSSET) R/H AND L/H IAW B757-200PF, DWG 148N8402.INSTALLED NEW BRACKETS 2 EA ON AJun 8, 2025 · N475UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025062512268Angle · crackedFWD CARGO COMPT, STA 560 ANGLE HAS A CRACK AT PANEL 122AZ SUPPORT STRUCTURE. INSTALLED NEW PART AT THE FWD CARGO COMP STA 560 ANGLE. I.A.W SRM 51-40-02-0G.Jun 8, 2025 · N475UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025062197411Support Angle · crackedRIGHT W/W FWD SEAL RETAINER/ DOOR SENSOR, 2ND FROM OUTBD SUPPORT CLIP IS CRACKED IN LOWER CORNER. DOT 8-002.IDENTIFIED, CLIP CRACKED AT W/W FWD SEAL RETAINER/ DOOR SENSOR, 2ND FROM OUTBD SUPPORT.REMOVED CRACKED SUPPORT CLIP (BRACKET) IAW 757-200PF SRM 51-40-02Jun 7, 2025 · N475UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025062100870Gusset · crackedFAULT-100-STR- LEFT WHEEL WELL FWD SEAL RETAINER/DOOR SENSOR SUPPORT CLIP, SECOND FROM OUTB IS CRACKED. DOT 8-010. IDENTIFIED AND REMOVED CRACKED SUPPORT CLIP (BRACKET) IAW 757-200PF SRM 51-40-02.LOCATED AND DRILLED NEW SUPPORT CLIP ON LEFT WHEEL WELL FWD SEAJun 7, 2025 · N475UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025060801104Blower · inoperativeF/O€™S EVAS FAILS BLOWER TEST. BLOWER DOES NOT COME ON. R&R RH (1ST OFFICER) EVAS UNIT IAW MM 25-69-00. OPS CK OKJun 7, 2025 · N461UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2025060974825Fuel Sys · out of balance**SUPPLEMENTAL SDR** FUEL STARTED L13.0 USED 7.2 = 5.8. LEFT GAUGE READS 5.4. FUEL STARTED R13.2 USED 7.7 = 5.5. RT GAUGE READS 6.2. FUEL IMBALANCE DID NOT AGREE WITH FUEL FLOWS IN CRUISE. PERFORMED OPS CHECK OF LH DEFUEL VALVE PER AMM 28-26-01. OPS CHECK GOODJun 6, 2025 · N454UP · Boeing 75724APF · Aircraft Fuel Distribution SystemSDR IPXA2025060674825Fuel Sys · out of balance*** SDR FILED OPEN *** FUEL STARTED L13.0 USED 7.2 = 5.8. LEFT GAUGE READS 5.4. FUEL STARTED R13.2 USED 7.7 = 5.5. RT GAUGE READS 6.2. FUEL IMBALANCE DID NOT AGREE WITH FUEL FLOWS IN CRUISE. DEFERRING FUEL IMBALANCE WITH REF TO AMM 28-21-00-702-001.PAR. B.(5).Jun 6, 2025 · N454UP · Boeing 75724APF · Aircraft Fuel Distribution SystemSDR IPXA2025060656280Window · arcedL FWD WINDOW EICAS ARCING NOTED ACCOMPLISHED WINDOW DAMAGE CHECK LIST. WINDOW SWITCH HEAT REMAINED OFF REST OF FLIGHT WINDOW LATER CRACKED. VERIFIED WINDOW TERMINALS TORQUED PROPERLY PER AMM 56-11-01-424-015Jun 5, 2025 · N454UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025060293029Controller · faultedCABIN ALT R&R'D ACTUATOR REF AMM 21-31-04-404-009, PERFORMED OPERATINAL CHECK OF AUTO 1, AUTO 2, AND MAN, OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF AUTO 1, AUTO 2, AND MANUAL, OPS GOOD, REF AMM 21-31-04-404-009, VERIFIED WORK PERFORMED, MSG CLEARED AIRCRAJun 1, 2025 · N419UP · Boeing 75724APF · Cabin Pressure ControllerSDR IPXA2025053025425A/C Pack · odorDURING DESCENT THROUGH 15000€™ CREW NOTICED BURNING SMELL AND STRONG ODOR, DONNED OXYGEN MASKS, CABIN ATMOSPHERE WARM AND HUMID, TURNED RIGHT PACK OFF AND CONDITIONS ABATED IMMEDIATELY. SMELL DISSAPATED AT APPROX 5000' NO SMOKE. STARTED CONDITION INSPECTION FMay 29, 2025 · N449UP · Boeing 75724APF · Cabin Cooling SystemSDR IPXA2025052925425Unknown · odorDURING DESCENT THROUGH 15000€™ CREW NOTICED BURNING SMELL AND STRONG ODOR, DONNED OXYGEN MASKS, CABIN ATMOSPHERE WARM AND HUMID, TURNED RIGHT PACK OFF AND CONDITIONS ABATED IMMEDIATELY. SMELL DISSAPATED AT APPROX 5000' NO SMOKE STARTED CONDITION INSPECTION FOMay 29, 2025 · N449UP · Boeing 75724APF · Air Distribution SystemSDR IPXA2025052810387Hydraulic System · warning message**ATB** ON TAKE OFF AFTER- 80 KTS , LEFT HYD QTY IN FLIGHT PROGRESSED TO (L) HYD SYS PRESS, ALT GEAR EXTEND, AND ALT FLAP EXTEND. FOUND FLAP/SLAT DEPRESSURIZATION MODULE PRESSURE SWITCH LEAKING. REPLACED REF AMM 27-51-29-422-026. OPS AND LEAK CHECKS GOOD.May 28, 2025 · N465UP · Boeing 75724APF · Hydraulic System, MainSDR IPXA2025052811205Sign · inoperativeFLIGHT DECK EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW B757 AMM 33-51-07. OPS CHECK GOOD.May 28, 2025 · N451UP · Boeing 75724APF · Emergency LightingSDR IPXA2025060694490Floor Panel · damagedMAIN DECK FLOOR PANEL 242XBF IS DAMAGED. FABRICATED MCD FLOOR PANEL 242XBF, IAW UPS SREO: B757-9692-REQ 001.May 27, 2025 · N448UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025052787473Tee Angle · corrodedFS 1037 RBL 45 T CHORD HAS CORROSION INSTALLED T-CHORD AT STA 1037 RBL 45 IAW B757-200PF, SRM 51-40-02-0G-0.May 26, 2025 · N432UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025061662819Skin · chafedRT WING O/B FLAP UPPER SURFACE L/E SKIN IS CHAFED ON O/B END. # 3513 REVIEWEDMay 24, 2025 · N448UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA2025061664053Stringer · corrodedAFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI ATA 53-05 ACCOMPLISHED REPAIR PER EO-94038-REQ1 AND VT-SAA EA 757-5360-01-B0497, REV I/RMay 24, 2025 · N403UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2025061264053Stringer · corrodedAFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI.May 24, 2025 · N403UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2025061164954Splice · dentedFWD PIT STA 680 L/H SIDE BETWEEN S-26L AND S-25L DENT ON FRAME MARKED IN RED. REPAIR DETAILED CONTAINS SUPPLEMENTAL REINSPECT INFORMATION AND MUST HAVE ASSOCIATED DEFERRALMay 24, 2025 · N448UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025061165015Frame · dentedFWD PIT STA 680 L/H SIDE BETWEEN S-24L AND S-23L DENT ON FRAME.May 24, 2025 · N448UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025060662822Floor Panel · damagedMDC, FLOOR PANEL 241XEF HAS AN INSERT AND COMPOSIT DAMAGED. FABRICATED MCD FLOOR PANEL 241XEF, IAW .UPS SREO: B757-9692-REQ 001. FLOOR PANEL 241XEF INSTALLATION.May 24, 2025 · N448UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025060364625Tee Angle · corrodedT-CHORD 1060 LBL 15 WITH EVIDENCE OF CORROSION NO DOT NSTALLED T-CHORD AT STA 1060 LBL 15 IAW B757-200PF, SRM 51-40-02-0G-0.May 24, 2025 · N432UP · Boeing 75724APF · Fuselage Main, Structure
Back to Boeing 757-24APF