N422UP

Service difficulty reports · 271

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 = 'N422UP' 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 IPXA2026040685799Support Strap · corrodedCORROISION FOUND ON FWD CARGO CEILING GILL LINER SUPPORT STRAP UNDER NUT PLATE STA 820 LBL 45. FOUND WHILE WORKING EO.89712-REQ007 DECOMPRESSION PANEL.ATA 25. INSTALLED STRAP P/N STESAA7003345555-7 AT FWD CARGO CEILING SUPPORT STA 760 TO STA 840 LBL 45.5 PEMar 15, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031475944Web · corrodedCORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN.Mar 14, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031425145Floorbeam · corrodedMAJOR REPAIR, AGING A/C INSP DOT AA024 STR ATA 53-00 MAIN CABIN FLOORBEAM CORRODED STA 1420 RH OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR INSTALLED FABRICATED -1 REPAIR ANGLE, FABRICATED -2 FILLER AND FABRICATED RADIUS FILLER REPAIR PARTS PER B757-200PF SRM Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026032324391Splice Strap · corrodedWORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510. SPLICE STRAP P/N 453N1611-23 TO BE INSTALLED. AUDITEDFeb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026032324635Splice Strap · corrodedWORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP BS 1470. FABRICATED 01 EA SPLICE STRAP P/N 453N1611-25 IAW DWG 453N1611 SHT 1 REV. A AND IAW SRM 51-40-05-0G-0.Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031424391Splice Strap · corrodedWORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510 ATA 53-60 PRODUCTION AUDIT C/WFeb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031424635Splice Strap · corrodedWORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1470 PRODUCTION AUDDIT C/WFeb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022825145Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED BS 1420 RT OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR VERIFIED STEP 17. FORMED TWO REPAIR ANGLES IAW SRM 53-00-51-2R-6.Feb 26, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026022845547Floor Skin · corrodedCORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN. REMOVED CORROSION FROM 2EA. FLOOR WEB PANELS IAW B757-200PF SRM 51-10-02-0G-0. INSTALLED 2EA. FLOOR WEB PANELS, 1EA. STRAP, AND 2EA. FILLERS IAW B757-200PF SRM51-40-02-0G-0, AND SEALED IAW B757-200PF AMM 5Feb 22, 2026 · N422UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026031635090Floorbeam · corrodedMAJOR REPAIR. UPON REMOVAL OF DAMAGED ON DECK PLATE, FOUND FLOORBEAM UPER FLANGE EXFOLIATED BS 1681, LBL 28 - 33. REMOVED THE DAMAGE. CUT OUT THE FLOORBEAM UPPER TEE AND CUT AWAY ANY DAMAGE ON FLOORBEAM VERTICAL WEB AS REQUIRED IAW E.A. 757-5310-01-B0703Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026032038490Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, ID STICKER NUM. (085-002). REMOVED 2 EA NUTPLATES AND REMOVED CORROSION AT STA 1470 AFT CARGO COMP FLOOR STRUCFeb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026030838490Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, INSTALLED 4 EA NUTPLATES AT AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER BTW STA 1440 AND STA 1480 LBL 16.10 IFeb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031138732Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 7.55, ID STICKER NUM. (085-004). ATA 53-10 VERIFIED STEP 24, C/W B757-200PF AMM 51-24-09-377-001.Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031810473Floor Panel · gougedAPPROX. 1 INCH LINE GOUGE, DIRT/ DEBRIS ON AFT CARGO FLOOR PANEL TAGGED, FROM BS 1460 - 1500. BLENDED DAMAGE. ORIGINAL MATERIAL THICKNESS IS .071, MATERIAL REMOVED IS .021. FABRICATED, LOCATED, DRILLED AND COUNTERSUNK NEW FLOOR PANEL 161AF IAW SRM 51-40-05-Feb 20, 2026 · N422UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026031499164Floorbeam · corrodedMAJOR REPAIR, MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOOR BEAM UNDERNEATH SURFACE REF SRM 51-10-02-0G-0 REPAIRED PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAIFeb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026032299492Stringer Splice · corrodedAFT CARGO COMP FLOOR STGR AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. INSTALLED 1 EA NEW FLOOR STRINGER AT AFT CARGO COMPARTMENT STA. 1460, RBL 15 IAW B757-200PF SRM 51-40-02-0G-0 PAR 4 AND PAR 7.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2026031493675Support Angle · corrodedAPU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION. LOWER SUPPORT ANGLE APU INLET P/N 148N3152-2 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N LINE # 614Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031699642Strap · corrodedAFT CARGO COMP LH SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN BS 1560 & 1580 IS CORRODED. INSTALLED NEW CEILING DECOMPRESSION PANEL STABILIZATION STRAP, AND 1EA. REPAIR SPLICE AT STA. 1610 L/H  IAW B757-200PF SRM 51-40-02-0G-0.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031393618Strap · corrodedAPU INLET SUPPORT STRUCTURE AFT STRAP IS CORRODED ATA 53-80 INSTALLED, 1EA REPAIR STRAP, 2EA REPAIR FILLER, 1EA STRAP AND 1EA EXISTING STRAP AT APU INLET SUPPORT STRUCTURE AFT IAW 757-200PF-SRM 53-80-15-2R-1 REPAIR 1.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031499075Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1681 LBL 31 METAL PLATE PANEL SURFACE BULGING SIGN OF CORROSION. ACCOMPLISHED REPAIR PER SRM 53-60-51-2R-6 REPAIR 6.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026031499159Retainer · corrodedMAIN DECK FLOOR AREA STA 1620-1640 LBL 62 ANGLE BAR SURFACE BULGING AND FASTENER HEAD FULL THROUGH SIGN OF CORROSION. INSTALLED NEW ANGLE BAR FASTENER RETAINER AT MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 IAW SRM 51-40-02-0G-0.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026031499642Strap · corrodedAFT CARGO COMP LT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1560 AND 1580 IS CORRODED. 83-015. ATA 53-00 QC AUDIT C/WFeb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031499696Strap · corrodedAFT CARGO COMP RT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1400 AND 1420 HAS CORROSION. 83-018. INSTALLED DECOMPRESSION PANEL LANDING ON AFT CARGO COMP RH SIDE CEILING DECOMPRESSION PANEL STRAP IAW B757-200PF SRM 51-41-02-0G-0.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031499056Seat Track · corrodedMAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORROSION. INSTALLED FABRICATED FILLER AT MAIN DECK RBL45 SEAT TRACK P/N 146N5337-1SAAU IAW B757 SRM 51-40-02-0G-0 AND DWG 146N5337.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031693647Support Angle · corrodedAPU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031693675Support Angle · corrodedAPU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION ATA 53-80 PRODUCTION AUDIT C/WFeb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031493686Support Angle · corrodedAPU INLET SUPPORT STRUCTURE FWD SIDE SMALL UPPER SUPPORT ANGLE HAS CORROSION. FABRICATED LOWEER SUPPORT ANGLE APU INLET IAW DWG 148N3141/ SAMPLE, WORK ACCOMPLISHED ON TRAVELER 7003344123. LOWER SUPPORT ANGLE APU INLET WILL BE INSTALLED ON JOB CARD T3F18E008ALFeb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031498924Support Angle · corrodedAPU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION ATA 53-80 UPPER SUPPORT ANGLE APU INLET P/N 148N3152-1 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022399164Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026022899492Floor Support · corrodedAFT CARGO COMP FLOOR SUPPORT AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. 83-010. VERIFIED REMOVAL OF FLOOR SUPPORT ON STEP 7.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022399056Seat Track · corrodedMAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORRODED. 7VERIFIED STEP 6 HAS BEEN ACCOMPLISHED.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031355302Support Strap · corrodedAPU INTAKE SUPPORT STRUCTURE FWD STRAP CORRODED FWD O/B SIDE. 61-016 ATA 53-80 INSTALLED 1EA UPPER SUPPORT ANGLE P/N: 148N3152-2, 1EA LOWER SUPPORT ANGLE P/N: 148N3152-1 APU INTAKE SUPPORT STRUCTURE BETWEEN STA 1787.45 AND STA 1825.00 STR 3R AND STR 6R IAW 757Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026022355337Nut Plate · corrodedCORROSION AROUND NUT PLATE 5 INCHES FWD OF STATION 1720 BTWN 24.75LB AND 0 LB AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1715 BTWN 24.75BL TO 0 BL IAW SRM 51-40-02-0G-0. OK TO REINSTALL PAN.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026030956993Drain Mast · corrodedRIGHT AFT FUSELAGE RT APU EXHAUST CONE DRAIN MAST BASE EXFOLIATED. REMOVED CORROSION AT RT AFT FUSELAGE AT APU EXHAUST DRAIN MAST BASE IAW SRM 51-10-02-0G-0. INSTALLED DRAIN MAST FROM RT AFT FUSELAGE RH APU EXHAUST CONE IAW IAW AMM 28-25-05-404-162.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026030855388Nut Plate · corrodedCORROSION AROUND NUT PLATE 6 INCHES AFT OF STA 1701 BTWN LBL 45.5 AND 62. AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1707 BTWN LBL 45.5 AND LBL 62 IAW SRM 51-40-02-0G-0.Feb 17, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025121057370Brake · inoperativeUPON BLOCK IN AT DF THE PARKING BRAKE WAS SET THE BRAKES WERE RELEASED AND I FELT THE A\C MOVING . LOOKED UP AND QUICKLY SET THE FOOT BRAKES. ATTEMPTED TO SET THE PARKING BRAKE BUT IT WOULD NOT HOLD TESTED BRAKE IAH FIM 32-44. NORMAL OPERATIONDec 10, 2025 · N422UP · Boeing 75724APF · Landing Gear Brake SystemSDR IPXA2025071881182Sign · inoperativeEMERGENCY EXIT SIGN HAS 7 EACH LIGHTS INOP. ++REPLACED 7 EACH BULBS IN EMERGENCY EXIT SIGN IAW AMM 33-51-01 OPS CHECK GOODJul 17, 2025 · N422UP · Boeing 75724APF · Emergency LightingSDR IPXA2025012126292None · noneREF HEAVY CHECK REPAIR T3F18E004J5QK, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3771, REV- COMPLETED.COMPLIED WITH EO-92554. REVIEWED.Jan 16, 2025 · N422UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025012222873Window · scratched**SUPPLEMENTAL SDR**FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. <BR>INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-0Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025011622873Window · scratchedFIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-02.Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2024102987439Windshield · crackedLEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING. COMPLETED #1 WINDSHIELD INSTALL IAW AMM 56-11-01. WITNESSED TERMINAL HARDWARE TORQUE OF THE #1 WINDSHIELD. C/W AS REQUIRED PER GMM 04-02 AND TORQUES WERE DONE PER AMM 56-11-01.Oct 27, 2024 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2024102887439Windshield · crackedLEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING REMOVED AND REPLACED #1 WINDSHIELD REF AMM 56-11-01 UP TO STEP 13 (A) FIRST TORQUE. INITIAL TORQUE HAS BEEN ACCOMPLISHED @0330L ON 10/28/2024.Oct 27, 2024 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2024061824985Floor Support · corrodedR/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION. VERIFIED INSTALLED NUT PLATE IN T-CHORD STA 1040 -1060 RBL 0-68 IAW SRM 51-40-02. REVIEWEDMay 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024061428155Floor Support · corrodedFAULT FLIGHT DECK ENTRANCE STA 297 SECTION 41 LOWER FLOOR BRACKET CORROSION DOT 44-44 INSTALLED ANGLE FROMFLIGHT DECK ENTRANCE STA 297, SECC 41, I.A.W. SRM 51-40-02-0G REVIEWEDMay 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024061425327Tee Angle · corrodedL/H T-CHORD FROM STA 1040-1060 LBL 0-37 HAS EXFOLIATED CORROSION (NEXT TO RAM EXHAUST) INSTALLED NEW LH T-CHORD ON STA 1040-1060 LBL0-37IAW B757 SRM 51-40-02 REVIEWEDMay 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024061225283Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) INSTALLED NEW T-CHORD AT STA 1045 L/H. FASTENER P/N NAS603-16P, BATCH # 0004207085. IAW SRM 51-40-02-0G.May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024060924985Tee Angle · corroded*SDR FILED OPEN* FAULT: R/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION JOP COMPLETE.May 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024060725283Tee Angle · corroded**SDR FILED OPEN**FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) VERIFIED INSTALLMay 23, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024061899986Floor Support · corroded**SUPPLEMENTAL SDR** FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION.INSTALLED NEW T-CHORD IAW SRM 51-40-02. INSTALLED NUT PLATES IAW SRM 51-40-02. REVIEWEDMay 22, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024060899986Tee Angle · corroded*SDR FILED OPEN* FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION VERIFIED INSTALL.May 22, 2024 · N422UP · Boeing 75724APF · Fuselage Miscellaneous Structure
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