N313UP

Service difficulty reports · 177

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 = 'N313UP' 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 IPXA2026041371289Fitting · noneNR 2 WING STRUT SUPPORT CLEVIS FITTING FREEZE PLUG - PERMANENT REPAIR. CONDITION CHECK NORMAL. PAPER FINAL CHECK OK.Apr 13, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041575356Bushing · migratedMIGRATED BUSHING, RT WING T/E NR 8 SPOILER MID LWR. IAW CMM:57-70-11, REV 42, REPAIR 2-1, PAGE 601 - 602 STEP 3, COMPLETED THE REPLACEMENT OF BUSHING.Apr 7, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041070344Seal · crackedNR 1 ENG FAIRING PANEL 436CR SPRING SEAL CRACKED. INSTALL NEW STRIP SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 1 REV.NApr 7, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041669415Depressor · deformedDEFORMED DEPRESSOR SILL, FORWARD CARGO DOOR CUTOUT AREA AFTER SIDE. INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:143T8540 SH1 REV.B AND BOEING DWG NO:143T8540 SH2 REV.B.Apr 7, 2026 · N313UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2026041172897Skin · bulgedSKIN, R/H WING T/E OUTBD FLAP INBD LWR. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA IAW NDT MANUAL PART 1 51-01-01 REV 143.Apr 7, 2026 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026040958846Seal · brokenNO.2 PYLON, RT FAIRING PANEL 446CR SEAL BROKEN INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 311T2570 SH. 1 REV. N.Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041159269Hinge · wornNR 2 PYLON L/H PRSOV ACCESS DWR. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV. 94, BOEING DWG NO. 311T1064 SH. 1 REV. G AND BOEING DWG NO. 311T1064 SH. 2 REV. E.Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041658143Floorbeam · crackedCRACK, ANGLE FLOORBEAM BS 246, RBL 38. ACCOMPLISHED REPAIR I.A.W UPS EO-97146-REQ1 REV1.Apr 6, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA2026041458575Strut · crackedCRACKED STRUT, RT WING L/E PANEL NR 621SB, OTBD, OSS 694.  INSTALLED NEW STRUT I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T2214 SH 1 REV. B, 112T2000 SH 13 REV. B.Apr 6, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041259154Bracket · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041259005Bracket · chafedCHAFED BRACKET, NR 1 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041159001Stiffener · crackedCRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT STIFFENER NEAR 2:00 POS. INSTALL A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-60, REV 141.Apr 6, 2026 · N313UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA2026041158718Stiffener · crackedCRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER. FWD TORQUE BOX SUPPORT STIFFENER NEAR 1:00 POS. INSTALLED A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94 & AIPC 78-31-00-60, REV 141.Apr 6, 2026 · N313UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA2026041058741Channel · crackedCRACKED CHANNEL, NR 2 ENG AFT FAIRING PANEL 447DB INNER AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G REV.94, & DWG 313T3360, SH 42, REV E.Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041059158Floor Panel · delaminatedFLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94. CHECKED SATISFACTORY.Apr 6, 2026 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026041346666Rub Strip · crackedNR 2 ENG LT CORE COWL INNER T/E UPPER RUB STRIP. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV. 94 AND CMM IPL 71-13-23 REV. 47.Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041447390Structure · crackedCRACKED CHORD, RT WING L/E PNL 621HB MID AREA OSS 531. INSTALLED NEW CHORD I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO: 114T2206 SH 1REV. B.Apr 5, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041047733Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94.Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026041047753Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0 REV. 94.Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026041047769Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW SRM 53-00-50-2R-0, REV 94, PERFORMED A BOND THE REPAIR OF PLIES WITH RESIN CURED AT 170°F FOR 2 HRS WITH A MINIMUM VACUUM OF 20 IN/HG.Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026041047239Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94.Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026040746687Bracket · crackedL/H WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET CRACKED. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND DWG 114T1240, SHT 2, REV E.Apr 5, 2026 · N313UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA2026040746494Angle · crackedCRACKED CLIP, NR 2 PYLON AFT LWR FAIRING INNER NUT FRAME OUTBD SIDE SUPPORT CLIP. INSTALLED NEW CLIP IAW SRM 51-40-02-0G, REV 94 AND DWG 313T3380, SHT 3, REV F.Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026040746727Clamp · crackedCRACKED CLAMP, NR 2 ENG AFT FAIRING DOOR SUPPORT ROD STOW AREA. INSTALLED NEW CLAMP IAW SRM 51-40-02-0G REV. 94 AND DWG 313T3349, SH. 2 REV. B.Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041535922Tee Fitting · crackedCRACKED TEE FITTING, NR 1 PYLON AFT FAIRING INNER OUTBD LWR TEE CRACK. INSTALLED NEW TEE IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2380, SHT 7, REV H, AND EO NO:EO-97048-REQ1, REV.1 & SB 767-54-0109, REV 1.Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026041536044Seal · crackedCRACKED ZEE, NR 2 PYLON RT FAIRING DOOR AFT LWR CUTOUT AREA. INSTALLED NEW ZEE IAW SRM 51-40-02-0G, REV.94, AND DWG 313T2380, SHT 10, REV K AND DWG 313T2380, SHT 9, REV G AND SB 767-54-0109 REV.1Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041635932Rub Strip · brokenBROKEN STRIP, NR 1 ENG NOSE COWL T/E RT UPPER WEAR STRIP. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV. 94 AND GOODRICH CMM IPL 71-11-16 REV. 54. AND AMM INTRODUCTION SIP REV.147.Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041637268Floorbeam · corrodedCORROSION DAMAGE ON UPPER CHORD OF FLOOR BEAM AT STA 246 NEAR RBL 30 (EVALUATE) REVIEWED PER GMM-MTX 09.05.01.09. ACCOMPLISHED REPAIR I.A.W EO-97113-REQ1 REV1 AND EGAT EI F2026A53M-685 REV.2. MAJOR REPAIRApr 4, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA2026041435847Plate · crackedTHE FORWARD CARGO SIDE GUIDE RAIL TIE PLATE AT LT BS 566 IS CRACKED. REPLACED. INSTALLED FABRICATE TIE PLATE IAW SRM 51-40-02-0G, REV 94, AND DWG 452T2003, SHT 24, REV D.Apr 4, 2026 · N313UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA2026041235947Bracket · crackedCRACKED, NR 2 PYLON AFT LWR FAIRING INNER DRAIN TUBE SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 272T0333, SHT 8, REV -.Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041035897Channel · crackedCRACKED, NR 1 PYLON AFT FAIRING PNL NR 437DB INNER CHANNEL AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E.Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026041035962Bulkhead · crackedCRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL NR.437DB INNER NEW AREA. INSTALL NEW BULKHEAD IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E.Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Bulkhead/FirewallSDR IPXA2026041518128Winglet · damagedR/H WING OUTBD AREA WINGLET. (REPAIR) REPAIR LIGHTNING STRIKE DAMAGE ON FASTENER HOLE OF RH WINGLET LOWER SKIN I.A.W. UPS EO-97110-REQ1 REV.1 AND EGAT EI NO. F2026A57M-668 REV.0Apr 3, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026041517950Handle · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148,Apr 3, 2026 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2026041317026Floorbeam · corrodedFOUND MAIN DECK FLOOR BEAM FITTING CORROSION. INSTALLED FABRICATED FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 146T5650, SHEET 5, REV C.Apr 3, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA2026040317950Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)Apr 3, 2026 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2026041091568Seat Track · wornFOUND SEAT TRACK ASSY INBOARD FWD OF CAPTAIN SEAT WORN. REPLACED THE SEAT TRACK ASSY IAW AMM 25-11-01-822-095-001, REV 147.Apr 2, 2026 · N313UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026030586411Sensor · false indicationL1 DOOR EICAS MESSAGE CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. REPLACED DOOR CLOSED SENSOR IAW AMM 52-71-01-964-211. DMP REVERSED. DEFERRAL CLEARED. GOOD TO CLOSEJan 27, 2026 · N313UP · Boeing 76734AF · Door Warning SystemSDR IPXA2026012786411Warning Message · illuminatedLEFT FWD ENTRY DOOR EICAS MSG CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. DEFERRED PER MEL 52-71-1-1AJan 27, 2026 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2025092645526Latch · faultedCOVER FOR YELLOW ENTRY DOOR LATCH PROTRUDES OUT AND WILL NOT CLOSE. DEFERRED MAIN ENTRY/SERVICE DOOR ARMING LEVER HINGED COVERS IAW MEL 52-11-2.Sep 25, 2025 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024070994662Handle · detachedCREW DOOR HANDLE FELL OFF. R&R DOOR HANDLE ESCUTCHEON DOOR ACCESS AND FWD ENTRY DOOR HINGE ASSY REF AMM 52-12-02/401. THIS CLEARS MEL 52-11-2. PLACARDS REMOVED. OKAY FOR SERVICE.Jun 30, 2024 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024063094662Handle · detachedCREW DOOR HANDLE FELL OFF. DEFERRING PER MEL 52-11-2 PLACARD INSTALLED. OPENJun 30, 2024 · N313UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024032147565Skin · corrodedFAULT - CORROSION ON FUSELAGE SKIN BETWEEN STA 1395-STA 1417, S-38R-S-39R. (REPAIR). PERFORMED FPI INSPECTION AT TRIM AREA PER SOPM 20-20-02 TO CONFIRM CORROSION FREE CONDITION,RESULT:NO CORROSION WAS FOUND REVIEW COMPLETEMar 19, 2024 · N313UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2024030138141Floor Panel · broken*MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231AFF P/N: 143T5876-78 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2. CONDITION CHECK IS SATISFACTORY. REVIEWEDMar 1, 2024 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024030138116Floor Panel · broken*MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231FFF, P/N: 143T5876-85 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2. CONDITION CHECK IS SATISFACTORY.Mar 1, 2024 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024031397889Strap · crackedFOUND CRACK AT STA 1725.5 STR-7R BULKHEAD OUTER CHORD STRAP. ACCOMPLISHED REPAIR I.A.W EO-24301-REQ002 REV.5 AND EO-24301-JIC003 REV.3 AND EO-89771-REQ1 REV.1 AND EGAT EI NO.F2024A53M-612 REV.1 AND EGAT WORK SHEET NO.40222Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024031197280Access Panel · crackedFOUND RH WING LOWER OUTBOARD MAIN FUEL PUMP ACCESS CRACK (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV.141 REPLACED THE ACCESS PANEL. COND CHECK NORMAL. ATTACHMENT ARE UPLOADEDFeb 28, 2024 · N313UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2024030700729Angle · leakingANGLE CRACKED BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60 (REPLACE) ACCOMPLISHED MAIN DECK CARGO ACCESS DADO PANEL AND FLOOR PANEL OK TO INSTALL CHECK,AND ACCESS FLOOR PANEL SEALANT REMOVE CHECK NORMAL.Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Structure (General)SDR IPXA2024030700671Angle · crackedCRACKED ANGLE STA 246, LBL 49. FABRICATE P/N(141T5146-16) PER BOEING DWG NO.:141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 6B REQUIREMENT INSTALLED FABRICATED PARTS I.A.W SRM 51-40-02-0G REV.88 AND BOFeb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024030500756Angle · crackedCRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 (REPAIR) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88 2. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88 AND BOEING DWG NO: 146T5650 SH 5 REV.C. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous Structure
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