# Service difficulty reports: N334UP

A list on [N334UP](https://openairdocs.org/aircraft/N334UP.md).

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

Page 1 of 3 · 126 reports

- [SDR IPXA2026062204155](https://openairdocs.org/sdr/IPXA2026062204155.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 FIL
- [SDR IPXA2026062204145](https://openairdocs.org/sdr/IPXA2026062204145.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 ADHES
- [SDR IPXA2026062204122](https://openairdocs.org/sdr/IPXA2026062204122.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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
- [SDR IPXA2026062204106](https://openairdocs.org/sdr/IPXA2026062204106.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 CU
- [SDR IPXA2026062203995](https://openairdocs.org/sdr/IPXA2026062203995.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 CURE
- [SDR IPXA2026062203992](https://openairdocs.org/sdr/IPXA2026062203992.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 ADHESI
- [SDR IPXA2026062203971](https://openairdocs.org/sdr/IPXA2026062203971.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 CUR
- [SDR IPXA2026062203947](https://openairdocs.org/sdr/IPXA2026062203947.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 A
- [SDR IPXA2026062203822](https://openairdocs.org/sdr/IPXA2026062203822.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENT - 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.
- [SDR IPXA2026062203799](https://openairdocs.org/sdr/IPXA2026062203799.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 A
- [SDR IPXA2026062203788](https://openairdocs.org/sdr/IPXA2026062203788.md): Nose Cowl · dented · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 ADHES
- [SDR IPXA2026062102849](https://openairdocs.org/sdr/IPXA2026062102849.md): Skin · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF · Trailing Edge Flaps
  > CRACKED 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.
- [SDR IPXA2026061903308](https://openairdocs.org/sdr/IPXA2026061903308.md): Bracket · chafed · Jun 17, 2026 · N334UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED 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 REVIEW
- [SDR IPXA2026061903879](https://openairdocs.org/sdr/IPXA2026061903879.md): Support Angle · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED 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: -
- [SDR IPXA2026061903908](https://openairdocs.org/sdr/IPXA2026061903908.md): Bracket · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF · Wing Structure
  > CRACKED 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.
- [SDR IPXA2026061903869](https://openairdocs.org/sdr/IPXA2026061903869.md): Support Angle · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED 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: -
- [SDR IPXA2026061904932](https://openairdocs.org/sdr/IPXA2026061904932.md): Bracket · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED 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.
- [SDR IPXA2026062585393](https://openairdocs.org/sdr/IPXA2026062585393.md): Torque Box · dented · Jun 16, 2026 · N334UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous Structure
  > MANY 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 REV2
- [SDR IPXA2026062485353](https://openairdocs.org/sdr/IPXA2026062485353.md): Longeron Fitting · cracked · Jun 16, 2026 · N334UP · Boeing 76734AF · Wing, Longeron/Stringer
  > LEFT 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: C
- [SDR IPXA2026061989107](https://openairdocs.org/sdr/IPXA2026061989107.md): Adapter · chafed · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED 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.
- [SDR IPXA2026061989218](https://openairdocs.org/sdr/IPXA2026061989218.md): Seal · cracked · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED 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.
- [SDR IPXA2026061990900](https://openairdocs.org/sdr/IPXA2026061990900.md): Adapter · chafed · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED 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.
- [SDR IPXA2026061989175](https://openairdocs.org/sdr/IPXA2026061989175.md): Adapter · chafed · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED 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.
- [SDR IPXA2026061988855](https://openairdocs.org/sdr/IPXA2026061988855.md): Adapter · chafed · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED 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.
- [SDR IPXA2026062287436](https://openairdocs.org/sdr/IPXA2026062287436.md): Nose Cowl · dented · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 A
- [SDR IPXA2026062287408](https://openairdocs.org/sdr/IPXA2026062287408.md): Nose Cowl · dented · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 AD
- [SDR IPXA2026062287404](https://openairdocs.org/sdr/IPXA2026062287404.md): Nose Cowl · dented · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED 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 SPA
- [SDR IPXA2026062286352](https://openairdocs.org/sdr/IPXA2026062286352.md): Skin · dented · Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > DENTED 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 FI
- [SDR IPXA2026061989062](https://openairdocs.org/sdr/IPXA2026061989062.md): Bracket · chafed · Jun 16, 2026 · N334UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED 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 REVIEW
- [SDR IPXA2026062572828](https://openairdocs.org/sdr/IPXA2026062572828.md): Torque Box · debonded · Jun 15, 2026 · N334UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous Structure
  > MANY 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 REV2
- [SDR IPXA2026062173665](https://openairdocs.org/sdr/IPXA2026062173665.md): Skin · cracked · Jun 15, 2026 · N334UP · Boeing 76734AF · Wing, Plate/Skin
  > CRACKED 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 57
- [SDR IPXA2026062158828](https://openairdocs.org/sdr/IPXA2026062158828.md): Antenna · eroded · Jun 14, 2026 · N334UP · Boeing 76734AF · Communications System
  > FOUND 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.
- [SDR IPXA2026061860062](https://openairdocs.org/sdr/IPXA2026061860062.md): Flap Track · cracked · Jun 14, 2026 · N334UP · Boeing 76734AF · Trailing Edge Flaps
  > CRACK - 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 FO
- [SDR IPXA2026062542487](https://openairdocs.org/sdr/IPXA2026062542487.md): Seal Depressor · damaged · Jun 6, 2026 · N334UP · Boeing 76734AF · Cargo/Baggage Doors
  > ROUND 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.
- [SDR IPXA2024070337674](https://openairdocs.org/sdr/IPXA2024070337674.md): Drain · none · Jul 3, 2024 · N334UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. EO-82173-JIC001 WAS ACCOMPLISHED.
- [SDR IPXA2024062856854](https://openairdocs.org/sdr/IPXA2024062856854.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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 REPAIR
- [SDR IPXA2024062856740](https://openairdocs.org/sdr/IPXA2024062856740.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL 251AFF DENTED. OPEN
- [SDR IPXA2024062856846](https://openairdocs.org/sdr/IPXA2024062856846.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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.
- [SDR IPXA2024062858148](https://openairdocs.org/sdr/IPXA2024062858148.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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.
- [SDR IPXA2024062856784](https://openairdocs.org/sdr/IPXA2024062856784.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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.
- [SDR IPXA2024062856822](https://openairdocs.org/sdr/IPXA2024062856822.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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 CHEC
- [SDR IPXA2024062857620](https://openairdocs.org/sdr/IPXA2024062857620.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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 REPAIR
- [SDR IPXA2024062857602](https://openairdocs.org/sdr/IPXA2024062857602.md): Floor Panel · dented · Jun 28, 2024 · N334UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND 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 REPAIR
- [SDR IPXA2024070906655](https://openairdocs.org/sdr/IPXA2024070906655.md): Fitting · broken · Jun 25, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR IPXA2024070876655](https://openairdocs.org/sdr/IPXA2024070876655.md): Fitting · broken · Jun 25, 2024 · N334UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > **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
- [SDR IPXA2024070791131](https://openairdocs.org/sdr/IPXA2024070791131.md): Angle · cracked · Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR IPXA2024070791142](https://openairdocs.org/sdr/IPXA2024070791142.md): Angle · cracked · Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND 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 COMPLETE
- [SDR IPXA2024071179048](https://openairdocs.org/sdr/IPXA2024071179048.md): Angle · cracked · Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND 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 COMPLETE
- [SDR IPXA2024070871131](https://openairdocs.org/sdr/IPXA2024070871131.md): Angle · cracked · Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > OPEN, FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 (REPLACE) ATTACHEMENTS ARE UPLOADED.
- [SDR IPXA2024070871142](https://openairdocs.org/sdr/IPXA2024070871142.md): Angle · cracked · Jun 24, 2024 · N334UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > OPEN, FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD.

Next page: https://openairdocs.org/aircraft/N334UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N334UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.