N334UP

Service difficulty reports · 126

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 = 'N334UP' 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 IPXA2026062204155Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 7:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 27" FROM OUTBD EDGE, AT 7 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). BOND THE SPACER WITH FILJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062204145Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 21" FROM FWD EDGE, 18" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062204122Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 11:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 18.5" FROM AFT EDGE, 24" FROM UPPER EDGE, AT 11 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062204106Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL BARREL NEAR 4:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 20" FROM FWD EDGE, 4" FROM LOWER EDGE, AT 4 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203995Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 4.75" FROM AFT EDGE, 33" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CUREJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203992Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 10.5" FROM AFT EDGE AND 45" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BOND THE SPACER WITH FILM ADHESIJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203971Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM AFT EDGE AND 24" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203947Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 5:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 19.5" FROM UPPER EDGE AND 11.5" FROM AFT EDGE, AT 5 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BONDED THE SPACER WITH FILM AJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203822Nose Cowl · dentedDENT - SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 4:00 POS. (REPAIR) CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0 REV. 95.Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203799Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE , 29" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH AJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062203788Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 50.5" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESJun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062102849Skin · crackedCRACKED SKIN, LT WING T/E NR 3 FLAP AFT FAIRING INBD. (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND.Jun 17, 2026 · N334UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026061903308Bracket · chafedCHAFED BRACKET, NR 2 ENG RT T/R CLOSURE DOOR T/E AREA. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96 C/W REVIEWJun 17, 2026 · N334UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA2026061903879Support Angle · crackedCRACKED SUPPORT ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061903908Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.Jun 17, 2026 · N334UP · Boeing 76734AF · Wing StructureSDR IPXA2026061903869Support Angle · crackedCRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061904932Bracket · crackedCRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.Jun 17, 2026 · N334UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA2026062585393Torque Box · dentedMANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX UPPER PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: B, SH 2 REV: A, 114T2800 SH 5 REV: G AND SREO-62436-REQ001 REV2Jun 16, 2026 · N334UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026062485353Longeron Fitting · crackedLEFT UNDERWING LONGERON FITTING HAS CRACK DURING PERFORMED J/C: EO-48156-JIC001. ACCOMPLISHED JOB I.A.W UPS EO-48156-JIC003 REV2 AND UPS EO-97843-REQ1 REV1 (EGAT EI NO.F2026A57M-1306 REV.0) AND BOEING DWG NO. 111T4022 SH 1 REV: CJun 16, 2026 · N334UP · Boeing 76734AF · Wing, Longeron/StringerSDR IPXA2026061989107Adapter · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061989218Seal · crackedCRACKED SEAL, NR 2 ENG RT CORE COWL FLIPPER DOOR. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV.95. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.95, & CMM IPL 71-13-24 REV. 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026061990900Adapter · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061989175Adapter · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061988855Adapter · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24 REV. 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026062287436Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 3:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE AND 25.5" FROM LOWER EDGE, AT 3 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH AJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062287408Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 8:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 7.5" FROM AFT EDGE AND 16.5" FROM OUTBD EDGE, AT 8 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH ADJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062287404Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 5:30 POSITION. (REPAIR). CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.75" FROM AFT EDGE AND 50" FROM INBD EDGE, AT 5:30 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPAJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062286352Skin · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 6:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.25" FROM FWD EDGE AND 38.5" FROM INBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPACER WITH FIJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR IPXA2026061989062Bracket · chafedCHAFED BRACKET, NR 1 ENG RT T/R FWD LWR CLOSURE DOOR T/E AREA. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96. C/W REVIEWJun 16, 2026 · N334UP · Boeing 76734AF · Engine Thrust ReverserSDR IPXA2026062572828Torque Box · debondedMANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX LWR PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: B, SH 2 REV: A, 114T1305 SH 1 REV: L, 112T2001 SH 2 REV: H AND UPS SREO-62416-REQ001 REV2Jun 15, 2026 · N334UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026062173665Skin · crackedCRACKED SKIN, LT WING T/E OTBD FLAP INBD END CAP (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND. I.A.W CMM 57Jun 15, 2026 · N334UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2026062158828Antenna · erodedFOUND VST HF ANTENNA (321E) ERODED. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. NO DEFECT FOUND. I.A.W AMM 55-35-01-404-006 REV.148 INSTALL V.S.Jun 14, 2026 · N334UP · Boeing 76734AF · Communications SystemSDR IPXA2026061860062Flap Track · crackedCRACK - SKIN, R/H WING NO.6 FLAP TRACK MID FAIRING INBD SIDE T/E SKIN. (REPAIR) I.A.W. B767 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. NO DEFECT FOJun 14, 2026 · N334UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026062542487Seal Depressor · damagedROUND CREW REPORTED DAMAGE ON AFT MCD DOOR CUTOUT .INSTALLED MAIN DECK CARGO DOOR DEPRESSOR SEAL AT AFT SIDE I.A.W AMM 20-11-00-910-802 REV.148 AND TORQUE BOLTS TO 35 IN-LB.Jun 6, 2026 · N334UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2024070337674Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. EO-82173-JIC001 WAS ACCOMPLISHED.Jul 3, 2024 · N334UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2024062856854Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 251AGF, P/N : 146T5869-91 (REPAIR) I.A.W AMM 25-57-02-404-016, AMM 25-58-01-404-005, AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR REPAIRJun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062856740Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL 251AFF DENTED. OPENJun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062856846Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 222BFF, P/N : 141T5856-49 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL MAJOR REPAIR.Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062858148Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 251LFF, P/N : 146T5869-78 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR.Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062856784Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 231LFF, P/N : 143T5876-87 I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-57-02-404-016 AND AMM 25-58-03-404-004 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR REPAIR.Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062856822Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL 252BFF DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 252BFF, P/N : 146T5869-62 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECJun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062857620Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 232NFF, P/N : 143T5876-20 (REPAIR) I.A.W AMM 25-58-04-404-015, AMM 25-57-05-404-006, AMM 25-57-02-404-016 AND AMM 25-58-01-404-005 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR REPAIRJun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024062857602Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 231FFF, P/N : 143T5876-49 (REPAIR) I.A.W AMM 25-57-03-404-005, AMM 25-58-03-404-017, AMM 25-57-02-404-016 AND AMM 25-58-03-404-004 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL. MAJOR REPAIRJun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024070906655Fitting · brokenFOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1175 BL00.0 AND STA 1197 BL00.0 TTL : 2EA (REPLACE). INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 457T4000 SH. 11 REV. B. JOB COMPLETED.Jun 25, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024070876655Fitting · broken**SDR FILED OPEN**FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1175 BL00.0 AND STA 1197 BL00.0 TTL : 2EA (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89.<BR>2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND Jun 25, 2024 · N334UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024070791131Angle · crackedFOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SHEET 5 REV.C. JOB COMPLETED.Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024070791142Angle · crackedFOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD (REPLACE). INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SHEET 5 REV.C. JOB COMPLETED. REVIEW COMPLETEJun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024071179048Angle · crackedFOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SHEET 5 REV.C. JOB COMPLETED. REVIEW COMPLETEJun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024070871131Angle · crackedOPEN, FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 (REPLACE) ATTACHEMENTS ARE UPLOADED.Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2024070871142Angle · crackedOPEN, FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD.Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
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