# Service difficulty reports: N451UP

A list on [N451UP](https://openairdocs.org/aircraft/N451UP.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 6 · 283 reports

- [SDR IPXA2026061121630](https://openairdocs.org/sdr/IPXA2026061121630.md): Strap · corroded · Jun 11, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 24.75.
- [SDR IPXA2026061122255](https://openairdocs.org/sdr/IPXA2026061122255.md): Strap · corroded · Jun 11, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 45.50 C/W SDR
- [SDR IPXA2026040115702](https://openairdocs.org/sdr/IPXA2026040115702.md): Floor Support · corroded · Mar 17, 2026 · N451UP · Boeing 75724APF · Fuselage Floor Panel
  > AFTER REMOVAL OF FLOOR TAPE FOUND AFT CARGO COMP FLOOR CENTER STRINGER STA 1475 RBL 2 EXFOLIATED INSTALLED 10 EA NUT PLATES ON NEW FLOOR SUPPORT STRINGER AND INSTALLED FLOOR SUPPORT STRINGER AT AFT CARGO STA 1443.6 TO 1495 RBL 2 IAW B757-200 SRM51-40-02-0G-
- [SDR IPXA2026031834297](https://openairdocs.org/sdr/IPXA2026031834297.md): Strap · corroded · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 45.50, ID STICKER NUM. (085-073). ATA 53-20 INSTALLED CEILING STABILIZATION STRAP, REPLACEMENT SECTION AND 2EA REPAIR SPLICES IN AFT CARGO COMPARTMENT BETWEEN STA
- [SDR IPXA2026030934060](https://openairdocs.org/sdr/IPXA2026030934060.md): Strap · corroded · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 24.75, ID STICKER NUM. (085-078). ATA 53-20 INSTALLED NEW STABILIZATION STRAP P/N STESAA7003349028-2 FOR AFT CARGO CEILING COMP BETWEEN STA 1360 AND STA 1440 IAW B7
- [SDR IPXA2026040633932](https://openairdocs.org/sdr/IPXA2026040633932.md): Frame · dented · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > MAJOR REPAIR. AFT CARGO BAY FRAME UPPER ANGLE DENTED, APPROX AT BS 1220, BTW STGR 26L AND STGR 27 L, REPAIR WAS ACCOMPLISHED IAW EO-96988-REQ1 AND VT-SAA EA 757-5360-01-B0699 REV IR PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2026040233747](https://openairdocs.org/sdr/IPXA2026040233747.md): Frame · dented · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > MAJOR REPAIR, AFT CARGO COMP. FRAME UPPER CHORD HAS 3 EA DENT, APPROX AT BS 1360, BTW STGR 25R AND STGR 27 R, ID STICKER NUM. (085-068). ATA 53-10. REMOVED (3EA) SOLID RIVETS FROM DISCREPANT AREAS AT FS 1360 INBD OF STR 26R FOR ACCESS IAW B757-200PF SRM 51-40-
- [SDR IPXA2026040133784](https://openairdocs.org/sdr/IPXA2026040133784.md): Intercostal · dented · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. INTERCOSTAL HAS A DEFORMATION APPROX BTW BS 1360 AND BS 1380, BTW STGR 24R AND STGR 25 R, ID STICKER NUM. (085-069). ATA 53-10 INSTALLED 1EA. SHIM AND NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026033134415](https://openairdocs.org/sdr/IPXA2026033134415.md): Floorbeam · corroded · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1400, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-074). ATA 53-10. REMOVED CORROSION AT MAIN CARGO COMP. FLOOR BEAM LWR CHORD APPROX. AT BS 1400, BTW RBL 24.75 AND RBL
- [SDR IPXA2026033134469](https://openairdocs.org/sdr/IPXA2026033134469.md): Floorbeam · corroded · Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1420, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-075). ATA 53-10. REMOVED 5EA ANGLES FROM AFT CARGO COMP. FRAME UPPER CHORD APPROX AT BS 1360, BTW STGR 25R AND STGR 27
- [SDR IPXA2026032721947](https://openairdocs.org/sdr/IPXA2026032721947.md): Floor Panel · corroded · Mar 4, 2026 · N451UP · Boeing 75724APF · Fuselage Floor Panel
  > EXFOLIATION FLOOR PANEL RT SIDE AFT CARGO BS 1600-1560, STR 27 AND 28R. REMOVED CORROSION FROM FLOOR PANEL RT SIDE AFT CARGO. MAT LOSS MORE THAN 50%. MAX ALLOWABLE IS 10%. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 101. INSTALLED REPAIR DOUBLER IN
- [SDR IPXA2026032803895](https://openairdocs.org/sdr/IPXA2026032803895.md): Splice Angle · corroded · Mar 3, 2026 · N451UP · Boeing 75724APF · APU Cowling/Containment
  > BS 1992 AT THE 6 O`CLOCK POSITION HAD CORROSION BETWEEN FRAME AND SPLICE ANGLE TO INCLUDE SURROUNDING EXTERNAL SURFACES. VERIFIED STEP 10 IAW GMM. INSTALLED REPLACED SPLICE, REINSTALLED DOUBLER AT STA. 1992, 6:0 O'CLOCK PER B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026032854460](https://openairdocs.org/sdr/IPXA2026032854460.md): Skin · corroded · Feb 28, 2026 · N451UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > APU, RIGHT DOOR 316 EXTERNAL SKIN EDGE HAS EVIDENCE OF CORROSION AT APPROX BS 1963.8, VERIFIED EO NO DEFERRALS REQUIRED EA 757-5240-01-B0698, REV P1, STEP 16. ACCOMPLISHED REPAIR PER EO-96910-REQ1 AND VT-SAA EA 757-5240-01-B0698, REV IR
- [SDR IPXA2026032033198](https://openairdocs.org/sdr/IPXA2026032033198.md): Bracket · corroded · Feb 27, 2026 · N451UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORZ STAB OTBD HINGE REAR SPAR TO ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS HAVE HEAVY CORROSION ALSO BONDING STRAPS CORRODED AND FRAYED. RL032 INSTALLED NEW BRACKET P/N 183N1341- 2SAAU AT R/H HORIZONTAL STAB. O/B HINGE REAR SPAR TO ELEVATOR IAW
- [SDR IPXA2026032433764](https://openairdocs.org/sdr/IPXA2026032433764.md): Bracket · corroded · Feb 27, 2026 · N451UP · Boeing 75724APF · Horizontal Stabilizer Structure
  > LEFT HORZ STAB OTBD HINGE REAR SPAR TO ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS HAVE HEAVY CORROSION LARGE SECTION OF BRACKET AND BONDING STRAPS MISSING. RL039. INSTALLED REPLACEMENT NEW BRACKET, 1EA WEB AND 1EA BONDING STRAP P/N BACJ40E20-20 BATCH 0
- [SDR IPXA2026031433198](https://openairdocs.org/sdr/IPXA2026031433198.md): Attach Bracket · corroded · Feb 27, 2026 · N451UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORZ STAB OTBD HINGE REAR SPAR TO ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS HAVE HEAVY CORROSION ALSO BONDING STRAPS CORRODED AND FRAYED. RL032 VERIFIED STEP 22
- [SDR IPXA2026031433764](https://openairdocs.org/sdr/IPXA2026031433764.md): Attach Bracket · corroded · Feb 27, 2026 · N451UP · Boeing 75724APF · Horizontal Stabilizer Structure
  > L/H HORZ STAB OTBD HINGE REAR SPAR TO ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS HAVE HEAVY CORROSION LARGE SECTION OF BRACKET AND BONDING STRAPS MISSING. RL039 VERIFIED STEP 20
- [SDR IPXA2025052811205](https://openairdocs.org/sdr/IPXA2025052811205.md): Sign · inoperative · May 28, 2025 · N451UP · Boeing 75724APF · Emergency Lighting
  > FLIGHT DECK EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW B757 AMM 33-51-07. OPS CHECK GOOD.
- [SDR IPXA2025051950196](https://openairdocs.org/sdr/IPXA2025051950196.md): Latch · stiff · May 18, 2025 · N451UP · Boeing 75724APF · Flight Compartment Windows
  > CAPTAINS SIDE WINDOW LATCH SLIGHTLY STIFF TO OPEN,SEEMS TO NEED A LITTLE LUBRICATION ADJUSTED CAPT #2 SLIDING WINDOW INBD/OTBD LINK ARM ROD END REF AMM TASK 56-11-02-825-001. OPERATED SLIDING WINDOW, NO OBSTRUCTION NOTED. CAPT SLIDING WINDOW OPERATION CHECK GO
- [SDR IPXA2024101482944](https://openairdocs.org/sdr/IPXA2024101482944.md): Battery Pack · inoperative · Oct 11, 2024 · N451UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHTS INOP REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSY IAW B757 AMM 33-51-07-902-001, 33-51-07-862-054 AND 33-51-07-612-048 OPS CHECK GOOD
- [SDR IPXA2024080808548](https://openairdocs.org/sdr/IPXA2024080808548.md): Sign · inoperative · Aug 5, 2024 · N451UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY EXIT SIGN LIGHTS INOP RELAMPED IAW MM 33-51-01. OPS CKS GOOD. THIS CLEARS 2820838. PLACARDS REMOVED.
- [SDR IPXA2024080508548](https://openairdocs.org/sdr/IPXA2024080508548.md): Light · inoperative · Aug 5, 2024 · N451UP · Boeing 75724APF · Emergency Lighting
  > *SDR FILED OPEN* EMERGENCY EXIT SIGN LIGHTS INOP DEFERRED PER MEL 33-51-1-1. NO DMP REQUIRED. PLACARD INSTALLED.
- [SDR IPXA2024080129069](https://openairdocs.org/sdr/IPXA2024080129069.md): Door · binding · Aug 1, 2024 · N451UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR HARD TO OPEN, DAMPNER SEAL GETTING STUCK IN DOOR JAMB. FOUND LOOSE HARDWARE AT BOTTOM OF DOOR LINER CAUSING DAMPER SEAL TO RUB BOTTOM DOOR FRAME. SECURED HARDWARE AND DAMPER SEAL IAW AMM 20-11-00 AND AMM 52-12-01. OPS CHECK GOOD.
- [SDR IPXA2024080284845](https://openairdocs.org/sdr/IPXA2024080284845.md): Seal · sticking · Jul 30, 2024 · N451UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN ENTRANCE DOOR STICKING (HARD TO OPEN) UPON INSP FOUND MAIN ENTRY CREW DOOR LOWER SEAL GETTING STUCK UNDER LINER. SECURED LINER SCREWS IAW MM LINER INSTALLATION SYS OPS CK€™S NORMAL REF MM 52-12-01-401.
- [SDR IPXA2024073084845](https://openairdocs.org/sdr/IPXA2024073084845.md): Seal · binding · Jul 30, 2024 · N451UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN ENTRANCE DOOR STICKING (HARD TO OPEN) UPON INSP FOUND MAIN ENTRY CREW DOOR LOWER SEAL GETTING STUCK UNDER LINER. SECURED LINER SCREWS IAW MM LINER INSTALLATION SYS OPS CK€™S NORMAL REF MM 52-12-01-401. OPEN
- [SDR IPXA2024041736479](https://openairdocs.org/sdr/IPXA2024041736479.md): Control Panel · malfunctioned · Apr 17, 2024 · N451UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHTS UNARMED LIGHT DOES NOT EXTINGUISH WHEN ARMED REMOVED AND REPLACED EMERGENCY LIGHT PANEL PER AMM 33-51-08 OPS CHECK GOOD.
- [SDR IPXA2024040618602](https://openairdocs.org/sdr/IPXA2024040618602.md): Floorbeam · corroded · Mar 28, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR - STA 1720 BETWEEN BL 0 AND RBL 45, 3 NUTPLATES STRAPS WITH CORROSION INSTALLED (3EA) ANGLES AND (3EA) NUTPLATES STRAP I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2024040618589](https://openairdocs.org/sdr/IPXA2024040618589.md): Floorbeam · corroded · Mar 28, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR - STA 1720 BETWEEN BL 0 AND LBL 45, 4 NUTPLATES STRAPS WITH CORROSION INSTALLED (2EA) NEW ANGLES, (4EA) NUTPLATES STRAP AND (2EA) EXISTING ANGLES I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2024041599046](https://openairdocs.org/sdr/IPXA2024041599046.md): Tee Fitting · corroded · Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Structure
  > *** SUPPLEMENTAL SDR *** FAULT: THE CROSS-FLOOR SUPPORT TIE AT STA 1060 LBL ZERO HAS INITAIL SIGNS OF CORROSION. DOT 39-03 INSTALLED SUPPORT FLOOR P/N 144N5005-5 I.A.W. SRM 51-40-02 FASTENRES USED:MS20426AD3-12 BTCH: 0004238822, BACN10JZ3A2U BATCH:004200335.
- [SDR IPXA2024041594591](https://openairdocs.org/sdr/IPXA2024041594591.md): Tee Fitting · corroded · Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Structure
  > *** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1220 LH HAS CORROSION APPLIED TOPCOAT NEW T-CHORD I.A.W AMM51-21-15 PAINT CUP. #: 02-012-176.
- [SDR IPXA2024040999046](https://openairdocs.org/sdr/IPXA2024040999046.md): Floorbeam · corroded · Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAJOR REPAIR. THE CROSS-FLOOR SUPPORT TIE AT STA 1060 LBL ZERO HAS INITAIL SIGNS OF CORROSION. DOT 39-03 AUDIT COMPLETE
- [SDR IPXA2024032894591](https://openairdocs.org/sdr/IPXA2024032894591.md): Tee Fitting · corroded · Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > WTB STRUCTURE - T-CHORD STA 1220 LH HAS CORROSION VERIFIED EVALUATED T-CHORD AT STA 1200 LH, 100% MATERIAL LOST, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71-1A-1 DETAIL V. AND REMOVED T-CHORD DAMAGED I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2024041084031](https://openairdocs.org/sdr/IPXA2024041084031.md): Frame · dented · Mar 26, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > *** SUPPLEMENTAL SDR *** FAULT: AFT CARGO PIT - FRAME RH SIDE STA 1220 HAS A DENT IN UPPER FLANGE AT STR23R INSTALLED REPAIR SPLICE AT FRAME 1220 RH IAW SRM 51-40-02-0G AND 53-00-07-2R-6.
- [SDR IPXA2024032784031](https://openairdocs.org/sdr/IPXA2024032784031.md): Frame · dented · Mar 26, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO PIT - FRAME RH SIDE STA 1220 HAS A DENT IN UPPER FLANGE AT STR23R FRAME STA1220 RH THE DAMAGE FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-07-1A-9.
- [SDR IPXA2024041560472](https://openairdocs.org/sdr/IPXA2024041560472.md): Tee Angle · corroded · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Structure
  > WTB STRUCTURE - T-CHORD STA 1200 -1240 LH HAS CORROSION INSTALLED NEW T-CHORD I.A.W SRM 51-40-02-0G.
- [SDR IPXA2024041060688](https://openairdocs.org/sdr/IPXA2024041060688.md): Frame · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT - FRAME STA 820 LH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 24L AND 25L. DOT 101-5 INSP COMPLETE JOB COMPLETE.
- [SDR IPXA2024040860472](https://openairdocs.org/sdr/IPXA2024040860472.md): Tee Fitting · corroded · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > WTB STRUCTURE - T-CHORD STA 1200 -1240 LH HAS CORROSION VERIFIED CIC.
- [SDR IPXA2024040260754](https://openairdocs.org/sdr/IPXA2024040260754.md): Transition Panel · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO PIT - TRANSITION PANEL BETWEEN FS580 TO 600 LH SIDE HAS A DENT. DOT 101-6 VERIFIED: AFTER FURTHER EVALUATION, DENT FOUND TO BE WITHIN LIMITS I.A.W. B757 SRM 53-00-53-1A-1, FIGURE 101, DETAIL VI. VERIFIED JOB COMPLETE. REVIEWED.
- [SDR IPXA2024032660576](https://openairdocs.org/sdr/IPXA2024032660576.md): Frame · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT - FRAME STA 780 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-3 APPROVED.
- [SDR IPXA2024032660754](https://openairdocs.org/sdr/IPXA2024032660754.md): Transition Panel · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO PIT - TRANSITION PANEL BETWEEN FS580 TO 600 LH SIDE HAS A DENT. DOT 101-6 VERIFIED: AFTER FURTHER EVALUATION, DENT FOUND TO BE WITHIN LIMITS I.A.W. B757 SRM 53-00-53-1A-1, FIGURE 101, DETAIL VI. VERIFIED JOB COMPLETE. OPEN
- [SDR IPXA2024032660672](https://openairdocs.org/sdr/IPXA2024032660672.md): Frame · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT: FWD CARGO PIT - FRAME STA 820 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-4 FRAME STA 820RH, DENT IN UPPER FLANGE IS NOT ALLOWED I.A.W. B757-200 S.R.M. 53-00-07-1A-1 FIG 101. OPEN
- [SDR IPXA2024032660588](https://openairdocs.org/sdr/IPXA2024032660588.md): Frame · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT - FRAME STA 720 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-1 VERIFIED: TRIMMED OUT DAMAGED AREA I.A.W. B757-200 S.R.M. 51-10-02.<BR>DIMENSIONS CUT OUT L=1.800" W=.900". OPEN
- [SDR IPXA2024032660625](https://openairdocs.org/sdr/IPXA2024032660625.md): Frame · dented · Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > FWD CARGO PIT - FRAME STA 760 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 22R AND 23R.DOT 101-2 REQUEST NDT. OPEN
- [SDR IPXA2024041540206](https://openairdocs.org/sdr/IPXA2024041540206.md): Transition Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1200 TO STA 1310 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1220,1240,1260,1280,1300) DOT 07308-009 INSTALLED DOUBLER AND SIDE PANEL I.A.W B757 SRM 51-40-02-0G.
- [SDR IPXA2024041540194](https://openairdocs.org/sdr/IPXA2024041540194.md): Transition Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Cargo Compartments
  > *** SUPPLEMENTAL SDR *** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1310 TO STA 1380 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1320,1340,1360,1380) DOT 07308-007 INSTALLED NEW TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.
- [SDR IPXA2024041540134](https://openairdocs.org/sdr/IPXA2024041540134.md): Transition Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1440 TO STA 1530 HAS CORROSION AROUND TIE DOWN FITTINGS ( STA 1460,1480,1500,1520) DOT 07308-002 INSTALLED TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.
- [SDR IPXA2024041140134](https://openairdocs.org/sdr/IPXA2024041140134.md): Transition Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1440 TO STA 1530 HAS CORROSION AROUND TIE DOWN FITTINGS ( STA 1460,1480,1500,1520) DOT 07308-002 VERIFIED: INSTALLED TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.
- [SDR IPXA2024041040212](https://openairdocs.org/sdr/IPXA2024041040212.md): Frame · dented · Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Frame
  > *MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - FRAME RH SIDE STA 1240 HAS A DENT IN UPPER FLANGE AT STR26R VERIFIED NDT FINDINGS FOR STEP #6 AND STEP #11, NO DEFECTS NOTED AT THIS TIME.
- [SDR IPXA2024041040206](https://openairdocs.org/sdr/IPXA2024041040206.md): Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Cargo Compartments
  > *MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1200 TO STA 1310 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1220,1240,1260,1280,1300) DOT 07308-009 REVIEWED.
- [SDR IPXA2024041040194](https://openairdocs.org/sdr/IPXA2024041040194.md): Panel · corroded · Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1310 TO STA 1380 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1320,1340,1360,1380) DOT 07308-007 REF STEP 16. INSPECTED AND VERIFED TRANSITION PANEL IS INSTALLED. INSP

Next page: https://openairdocs.org/aircraft/N451UP/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 = 'N451UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N451UP/reports

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