# Service difficulty reports: N324UP

A list on [N324UP](https://openairdocs.org/aircraft/N324UP.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 4 · 155 reports

- [SDR IPXA2026092364703](https://openairdocs.org/sdr/IPXA2026092364703.md): Unknown · odor · Sep 22, 2026 · N324UP · Boeing 76734AF · Air Distribution System
  > VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180 REF AMM 71-00-00-795-034-H03 TEST NO. 3 - GROUND TEST - IDLE LEAK TEST. RAN ENGINES FOR 15 MINUTES WITH NO NOXIOUS ODOR NOTED AT THIS TIME WHILE ENGINE 2 SOLE SOURCE OF BLE
- [SDR IPXA2026092264703](https://openairdocs.org/sdr/IPXA2026092264703.md): Unknown · odor · Sep 22, 2026 · N324UP · Boeing 76734AF · Air Distribution System
  > VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180. PERFORMED GVI IN BOTH PACK BAYS WITH NO OBVIOUS FAULTS NOTED. DURING RIGHT ENGINE RUN, EXHAUST FUMES WERE DETECTED IN THE FLIGHT DECK. SWAPPING BETWEEN PACK 1 AND PACK 2
- [SDR IPXA2025082044859](https://openairdocs.org/sdr/IPXA2025082044859.md): Structure · delaminated · Aug 19, 2025 · N324UP · Boeing 76734AF · Vertical Stabilizer Miscellaneous Structure
  > DELAMINATE- COMPOSITE, VERICAL STABILIZER AUXILIARY SPA AFT FSS 18.037 AREA. (RAPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR.
- [SDR IPXA2025082301209](https://openairdocs.org/sdr/IPXA2025082301209.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 93. INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 93 AND DWG 146T5650 SH 5, REV C.
- [SDR IPXA2025082301719](https://openairdocs.org/sdr/IPXA2025082301719.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. REMOVED FLOOR PANEL 252YFF I.A.W AMM 53-01-06-000-801 REV. 145, G.V.I AND CONDITION CHECK NORMAL. REMOVED FLOOR PANEL SEALANT I.A.W AMM 53-01-06-000-801 REV. 145, COMPLET
- [SDR IPXA2025082301758](https://openairdocs.org/sdr/IPXA2025082301758.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED FLOOR PANEL NO. 251CGF IAW AMM 53-01-06-000-801 REV. 145, GVI AND CONDITION CHECK NORMAL. REMOVED FLOOR PANEL SEALANT IAW AMM 53-01-06-000-801 REV. 145, COMPLETED AN
- [SDR IPXA2025090801808](https://openairdocs.org/sdr/IPXA2025090801808.md): Hinge · damaged · Aug 16, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE. REPLACED HINGE ASSY. I.A.W AMM 20-11-00-910-802 REV.146. INSTALLED PLACARD I.A.W AMM 20-10-13-964-001 REV.146. INSTALLED DOORWAY LINING OF THE ENTRY DOOR. I.A.W AMM 52-12-02-404-025 REV.1
- [SDR IPXA202508261209](https://openairdocs.org/sdr/IPXA202508261209.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) ATTACHMENT ARE UPLOADED.
- [SDR IPXA202508261758](https://openairdocs.org/sdr/IPXA202508261758.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) PAPER CHECK OK.
- [SDR IPXA202508261719](https://openairdocs.org/sdr/IPXA202508261719.md): Angle · cracked · Aug 16, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE) PAPER CHECK OK.
- [SDR IPXA2025082501844](https://openairdocs.org/sdr/IPXA2025082501844.md): Bumper · missing · Aug 16, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING. INSTALLED THE BUMPER IAW DWG 411T2036, SHEET 1, REV H & PSDL 411T2240, SHEET DL, REV A.
- [SDR IPXA2025081800044](https://openairdocs.org/sdr/IPXA2025081800044.md): Bumper · missing · Aug 16, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING.
- [SDR IPXA2025081800008](https://openairdocs.org/sdr/IPXA2025081800008.md): Hinge · deformed · Aug 16, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE.
- [SDR IPXA2025090884241](https://openairdocs.org/sdr/IPXA2025090884241.md): Pawl · damaged · Aug 15, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE. REMOVED THE PAWL IAW AMM 52-11-26-004-001, REV 145. INSTALLED A NEW PAWL IAW AMM 52-11-26-404-003, REV 145.
- [SDR IPXA202508154241](https://openairdocs.org/sdr/IPXA202508154241.md): Pawl · worn · Aug 15, 2025 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE OK TO WORK
- [SDR IPXA2025043032293](https://openairdocs.org/sdr/IPXA2025043032293.md): Skin Panel · damaged · Apr 24, 2025 · N324UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > DAMAGE SKIN PANEL FROM STA. 1405 TO STA. 1540, STRINGER 38L TO 38R DUE TO TAIL STRIKE. ALL WORK COMPLETED ON ATTACHED BOEING WORK DOCUMENTS.
- [SDR IPXA2025050588602](https://openairdocs.org/sdr/IPXA2025050588602.md): Floor Support · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > REMOVED 5 FLOOR STRINGERS AT STA 1417- 1540 FOR FOM AREA RESTORED ON BOEING DOC REM 1 AND 2 ATTACHED. ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO LINE ITEM 103 OF THIS WORK PACKAGE.
- [SDR IPXA2025050588728](https://openairdocs.org/sdr/IPXA2025050588728.md): Stiffener · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > REMOVED 4 VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1502 AREA RESTORED ON BOEING DOC REM-10 & 11 (SEE ATTACHED). ENTIRE REPAIR DOCUMENTED ON LINE 103.
- [SDR IPXA2025050588609](https://openairdocs.org/sdr/IPXA2025050588609.md): Shear Tie · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Internal Mounting Structure
  > REMOVED 4 STRINGER SHEAR TIES AND 3 SHEAR CLIPS FROM FRAME AT STA 1439 AREA RESTORED ON REM 12, 13 & 14 (SEE ATTACHED). ENTIRE BOEING REPAIR PACKAGE ATTACHED TO LINE 103 OF THIS WORK PACKAGE.
- [SDR IPXA2025050588685](https://openairdocs.org/sdr/IPXA2025050588685.md): Shear Tie · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Internal Mounting Structure
  > REMOVED 4 SHEAR TIES AND 3 STRINGER TIES FROM FRAME STA 1461 AREA RESTORED ON BOEING DOC REM-15 & 16 (ATTACHED). ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO LINE ITEM 103 OF THIS WORK PACKAGE. (PLEASE SEE BARCODE T3F18E005W6PJ - NLL 0782896)
- [SDR IPXA2025050588569](https://openairdocs.org/sdr/IPXA2025050588569.md): Stiffener · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > REMOVE 4 DAMAGED VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1439 4 VERTICAL STIFFENERS REPLACED ON BOEING DOCUMENT REM 8 & 13
- [SDR IPXA2025050588712](https://openairdocs.org/sdr/IPXA2025050588712.md): Stiffener · not reported · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > REMOVED 2 VERTICAL L SHAPED SATIN EARS FROM FRAME AT STA 1480 AREA RESTORED ON REM-12
- [SDR IPXA2025050588745](https://openairdocs.org/sdr/IPXA2025050588745.md): Failsafe · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Main, Structure
  > CUT OUT DAMAGED SECTION OF LOWER TEE CHORD ON FRAME AT STA 1439 PART REPLACED ON REM-13.
- [SDR IPXA2025050588761](https://openairdocs.org/sdr/IPXA2025050588761.md): Failsafe · damaged · Jan 14, 2025 · N324UP · Boeing 76734AF · Fuselage Main, Structure
  > CUT OU DAMAGED SECTION OF TEE CHORD FROM FRAME AT STA 1461 PART REPLACED ON BOEING REPAIR DOC REM-14 (ATTACHED). ENTIRE BOEING WORK PACKAGE ATTACHED TO LINE ITEM 103. (PLEASE SEE BARCODE T3F18E005W6PJ - NLL 0782896)
- [SDR IPXA2025011317523](https://openairdocs.org/sdr/IPXA2025011317523.md): Skin · pilot error · Jan 10, 2025 · N324UP · Boeing 76734AF · Standard Practices/Structures
  > *SDR FILED OPEN* TAIL STRIKE IDENTIFIED ON WALK AROUND INSPECTION
- [SDR IPXA2024013038949](https://openairdocs.org/sdr/IPXA2024013038949.md): Support · broken · Jan 26, 2024 · N324UP · Boeing 76734AF · Wing Main, Frame Structure
  > FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY) REMOVED THE BROKEN INBD LE SUPPORT LINK DOORS AND REPLACED NEW INBD LESUPPORT LINK DOORS PER AMM 57-41-59-401 AND OPS CHK OK
- [SDR IPXA2024012638949](https://openairdocs.org/sdr/IPXA2024012638949.md): Support · broken · Jan 26, 2024 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY)
- [SDR IPXA2023082131089](https://openairdocs.org/sdr/IPXA2023082131089.md): Skin · chafed · Aug 9, 2023 · N324UP · Boeing 76734AF · Doors
  > *** SUPPLEMENTAL SDR *** FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) REVIEWED
- [SDR IPXA20230816089](https://openairdocs.org/sdr/IPXA20230816089.md): Unknown · unknown · Aug 9, 2023 · N324UP · Boeing 76734AF · Tail Cone Doors
  > FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) PAPER OK
- [SDR IPXA2023081296740](https://openairdocs.org/sdr/IPXA2023081296740.md): Stiffener · cracked · Aug 5, 2023 · N324UP · Boeing 76734AF · Fuselage Structure (General)
  > FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4.O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5202 SH.2 REV.- AND BOEING D
- [SDR IPXA2023081296743](https://openairdocs.org/sdr/IPXA2023081296743.md): Stiffener · cracked · Aug 5, 2023 · N324UP · Boeing 76734AF · Fuselage Structure (General)
  > FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 RBL 11 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4. O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5201 SH.2 REV.A AND BOEING
- [SDR IPXA2022081985422](https://openairdocs.org/sdr/IPXA2022081985422.md): None · inoperative · Aug 19, 2022 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/AENTRY DOOR GASKET NOT IN TRACKACCOMPLISHED EO B767-5210-84538-A
- [SDR IPXA2022063083650](https://openairdocs.org/sdr/IPXA2022063083650.md): Fan · odor · Jun 29, 2022 · N324UP · Boeing 76734AF · Air Distribution Fan
  > STRONG ODOR ON FINAL FWD EQIP COOLING EXH FAN STATUS AFTER LANDING. DEF FWD EQPT COOLING EXH FAN PER MEL 21-58-4-2-1 C/W DMP ACCESS FWD EQPT EXH FAN VERIFIED FAN NOISE AND SMELL PULLED P6H21/P11 P22 NO FURTHER SMELL NOTEDR/R FWD EQUIP COOLING EXHIT FAN IAW AMM
- [SDR IPXA2021081372700](https://openairdocs.org/sdr/IPXA2021081372700.md): Floor Support · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-8)ON MAIN DECK FLOOR NEAR STA 1602.64, RBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV"A"; SH 5, REV"C" AND 767-300F SRM 51-40-02 REV 80.03.
- [SDR IPXA2021081372699](https://openairdocs.org/sdr/IPXA2021081372699.md): Angle · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON ANGLE (P/N:146T5628-22) ON MAIN DECK FLOOR BETWEEN STA 1581.845 AND STA 1597.940, RBL 33.INSTALL NEW PART I.A.W. BOEING DWG 146T5650 SH 2, REV "A", AND 767-300F SRM 51-40-02 REV 80.03
- [SDR IPXA2021081372698](https://openairdocs.org/sdr/IPXA2021081372698.md): Intercostal · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-3) ON MAIN DECK FLOOR NEAR STA 1597.04, BETWEEN RBL 11 AND RBL 33.INSTALL NEW I.A.W BOEING DWG 146T5650 SH 2, REV"A" AND 767-300F SRM 51-40-02 REV 80.03.
- [SDR IPXA2021081372697](https://openairdocs.org/sdr/IPXA2021081372697.md): Filler · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER (P/N:146T5609-67) ON MAIN DECK FLOOR NEAR STA 1601,LBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5, REV "C" AND 767-300F SRM 51-40-02 REV 80.03.
- [SDR IPXA2021081372696](https://openairdocs.org/sdr/IPXA2021081372696.md): Angle · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON CLIP(P/N:146T5619-357) ON MAIN DECK FLOOR NEAR STA 1586.51, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV"A" AND 767-300F SRM 51-40-02 REV 80.03
- [SDR IPXA2021081372695](https://openairdocs.org/sdr/IPXA2021081372695.md): Intercostal · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL (P/N;146T5649-7) ON MAIN DECK FLOOR NEAR STA 1602.64, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV "A";SH 5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
- [SDR IPXA2021081372694](https://openairdocs.org/sdr/IPXA2021081372694.md): Filler · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Main, Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER(P/N:146T5649-67) ON MAIN DECK FLOOR NEAR STA 1601, RBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
- [SDR IPXA2021081372693](https://openairdocs.org/sdr/IPXA2021081372693.md): Channel · corroded · Aug 5, 2021 · N324UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON MOPSILL(P/N:146T5651-15) ON MAIN DECK CARGO FLOOR STRUCTURE AT STA 1605, LBL54.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
- [SDR IPXA2021081072606](https://openairdocs.org/sdr/IPXA2021081072606.md): Stiffener · cracked · Aug 4, 2021 · N324UP · Boeing 76734AF · Fuel Storage
  > INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7)ON STA 785.9,LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.03 AND UPS EO B767-5740-58151-C AND B767-5720-76672-A.
- [SDR IPXA2020012751443](https://openairdocs.org/sdr/IPXA2020012751443.md): Unknown · odor · Jan 25, 2020 · N324UP · Boeing 76734AF · Air Distribution System
  > ON DESCENT INTO ONT PASSING THROUGH 17,000, STRONG ODOR OF BURNING RUBBER FILLED THE COCKPIT LASTED FOR APPROXIMATELY 3 MINUTES. THEN DISSIPATEDA/C POWERED FOR 24 HOURS. RAN BOTH PACKS 1 HOUR. NO ODOR DETECTED. OK PER AMM 05-51-56.
- [SDR IPXA2020011550914](https://openairdocs.org/sdr/IPXA2020011550914.md): Pitot Tube · obstructed · Jan 13, 2020 · N324UP · Boeing 76734AF · Pitot/Static System
  > INSPECTION TYPE:N/A**AIR TURN BACK** AIRSPEED UNRELIABLE, SINGLE AIR DATA, RUDDER RATIO, L ENG EEC, R ENG EEC, AILERON LOCKOUT.FLUSHED PITOT STATIC SYS AS PER AMM 34-11-00 FOUND DEBRIS IN FO PITOT TUBE. ACCOMPLISHED AIR DATA SYS TEST AS PER AMM 34-12-00 OPS CH
- [SDR IPXA2019091346699](https://openairdocs.org/sdr/IPXA2019091346699.md): Skin · cracked · Sep 4, 2019 · N324UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN (P/N: 148T3121-2) ON STA 1725.5, NEAR S-7R. REPAIR IAW EO B767-5330-24301 APPX C AND 5330-73933-A, SR:4-4555838821, AND SRM 53-80-01 REPAIR 5, REV 75.00.
- [SDR IPXA2019091146598](https://openairdocs.org/sdr/IPXA2019091146598.md): Stiffener · cracked · Sep 2, 2019 · N324UP · Boeing 76734AF · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C11 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25. REPAIR IAW EO B767-5310-20118-F AND SRM 51-70-12 GENERAL, FIGURE 1, REV 75.00.
- [SDR IPXA2019082876060](https://openairdocs.org/sdr/IPXA2019082876060.md): Switch · failed · Aug 26, 2019 · N324UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHT SWITCH INOP. R&R'D CONT PNL PER AMM 33 51 08. OS CHK GOOD. IPC 32 51 08 01A, 010
- [SDR IPXA201906143225](https://openairdocs.org/sdr/IPXA201906143225.md): Seal · out of position · Jun 12, 2019 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN ENTRY DOOR IS DIFFICULT TO LIFT AFTER FLIGHT.FOUND AFT DOOR LINER SEAL OUT OF RETAINER. REINSTALLED SEAL AND CLEANED. DOOR OPS NORMAL PER AMM 52-12-00
- [SDR IPXA2019050341714](https://openairdocs.org/sdr/IPXA2019050341714.md): Door Seal · unsecure · May 3, 2019 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/A CREW ENTRY DOOR SEAL (INNER) IS COMING OFF. REINSTALLED CREW ENTRY DOOR FWD INNER TRIM SEAL REF AMM 52 09 01 OPERATED DOOR SEVERAL TIMES REF AMM 52 12 00 SEAL REMAINS SECURED.
- [SDR IPXA2019031340010](https://openairdocs.org/sdr/IPXA2019031340010.md): Door Seal · not seated · Mar 12, 2019 · N324UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/A CREW ENTRY DOOR RUBBER SEAL WILL NOT STAY STRAIGHT WHEN CLOSING THE CREW ENTRY DOOR. RESEATED SEAL ON TRACK RE AMM 52-09-01.

Next page: https://openairdocs.org/aircraft/N324UP/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 = 'N324UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N324UP/reports

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