# Service difficulty reports: N322UP

A list on [N322UP](https://openairdocs.org/aircraft/N322UP.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 · 144 reports

- [SDR IPXA2026102133469](https://openairdocs.org/sdr/IPXA2026102133469.md): Floor Panel · damaged · Oct 20, 2026 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE,
- [SDR IPXA2026102108780](https://openairdocs.org/sdr/IPXA2026102108780.md): Floor Panel · damaged · Oct 18, 2026 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.149 REMOVED MAIN DECK CARGO HANDLING AND G.V.I CHECK NORMAL.IAW AMM 53-01-06-000-801 REV.149, REMOVED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2026102268685](https://openairdocs.org/sdr/IPXA2026102268685.md): Skin · damaged · Oct 9, 2026 · N322UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > MAJOR REPAIR, PANEL AFT OF 321D RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 7.5€? FROM BOTTOM & 12€? FROM LEADING EDGE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, IAW NDT MANUAL PART 1 51-01-
- [SDR IPXA2026102268850](https://openairdocs.org/sdr/IPXA2026102268850.md): Skin · damaged · Oct 9, 2026 · N322UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > MAJOR REPAIR, PANEL AFT OF 321C RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 43€? FROM TOP & 14€? FROM TRAILING EDGE. SEE ATTACHED PICTURE. PERFORMED NDT/UT FOR THE BONDED REPAIR & 8 INCHES FROM WHERE THE EDGES OF THE HEAT BLANKET, I.A.W. 767
- [SDR IPXA2026092264312](https://openairdocs.org/sdr/IPXA2026092264312.md): Warning Message · false activation · Sep 22, 2026 · N322UP · Boeing 76734AF · Leading Edge Slat Position Indicating System
  > EMERGENCY DECLARED ON APPROACH TO LANDING. FLAPS 25 SELECTED AND LE-SLAT DISAGREE EICAS CAME ON. TROUBLESHOT IAW FIM 27-51 FT 808, NO FAULTS NOTED. EXTENDED AND RETRACTED SLATS/FLAPS IAW AMM 27-81-00. OPS CHECKED GOOD.
- [SDR IPXA2026091329466](https://openairdocs.org/sdr/IPXA2026091329466.md): Pump · faulted · Sep 13, 2026 · N322UP · Boeing 76734AF · Hydraulic Pump (Electric/Engine), Main
  > RECEIVED A CHYD PUMP1 OVERHEAT. RAN QRH PROCEDURE, RAN QRH PROCEDURE, DECLARED EMERGENCY FOR PRIORITY HANDLING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CTR HYS SYS ACMP NO.1 REF AMM 29-11-02/401 UP TO AND INCLUDING AMM TASK 29-11-02-404-018 PARA 3.F.(2
- [SDR IPXA2026062555305](https://openairdocs.org/sdr/IPXA2026062555305.md): Swivel Fitting · corroded · Jun 7, 2026 · N322UP · Boeing 76734AF · Main Landing Gear Strut/Axle/Truck
  > AFTER REMOVAL RT MLG STRUT SWIVEL FITTING FOUND OUTER SHAFT OF INBOARD CRANK AND DRIVE ARMS WITH CORROSION IN THE TEETH, FLL-023, ATA 57. NEW SHAFT ASSEMBLY PROCURED AND ACCOMPLISHED INSTALLATION ON TASK CARD "T3F18E008YJ8T" LINE # 50. NO FURHTER ACTION IS R
- [SDR IPXA2026062532624](https://openairdocs.org/sdr/IPXA2026062532624.md): Swivel · corroded · May 23, 2026 · N322UP · Boeing 76734AF · Main Landing Gear Attach Section
  > RT MLG, SIDE STRUT SWIVEL (PART OF THE MLG SUPPORT BEAM ASSEMBLY) HAS CORROSION AROUND AND UNDERNEATH THE O/B BUSHING, FLL-005, REMOVE CORROSION OF RH MLG, SIDE STRUT SWIVEL INSIDE LUG BORE, CHANFER AND AROUND AREA OUTSIDE OF SPOTFACE IAW B767-300F SRM 51-10-
- [SDR IPXA2025081104151](https://openairdocs.org/sdr/IPXA2025081104151.md): Sensor · out of adjust · Aug 11, 2025 · N322UP · Boeing 76734AF · Door Warning System
  > BTD DUE TO FWD ENTRY DOOR EICAS L FWD ENTRY DOOR ON PUSH BACK. ADJUSTED SENSOR AND TESTED SATIS PER AMM TASK 52-12-00-715-119 REV 137.
- [SDR IPXA2025022030552](https://openairdocs.org/sdr/IPXA2025022030552.md): Sensor · faulted · Feb 19, 2025 · N322UP · Boeing 76734AF · Landing Gear Position and Warning
  > IN FLIGHT, AIR/GND DISAGREEE€? STATUS MESSAGE PERFORMED PSEU BITE TEST. R GEAR TILT SENSOR S268 FAULTED. REMOVED AND REPLACED RH TILT SENSOR PER AMM 32-09-07. OPS CHECKS GOOD.
- [SDR IPXA2024101654112](https://openairdocs.org/sdr/IPXA2024101654112.md): Cargo Track · broken · Oct 10, 2024 · N322UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN DECK CARGO TRACK ASSY BROKEN AT: STA 1510 LBL 33.00 (REPAIR) ATTACHEMENTS ARE UPLOADED. OPEN
- [SDR IPXA2024101697157](https://openairdocs.org/sdr/IPXA2024101697157.md): Bear Strap · cracked · Oct 7, 2024 · N322UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FAULT - FOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR) REVIEWED
- [SDR IPXA2024100894916](https://openairdocs.org/sdr/IPXA2024100894916.md): Floor Panel · damaged · Oct 7, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > *** MAJOR REPAIR *** FAULT - DAMAGE - FLOOR PNL, AT MAIN DECK, PANEL P/N: 145T5876-64 PNL NO.242CFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N: 145T5876-64
- [SDR IPXA2024100895541](https://openairdocs.org/sdr/IPXA2024100895541.md): Floor Panel · cracked · Oct 7, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR *** FAULT - CRACK - FLOOR PNL, AT MAIN DECK STA 1043~ STA 1109, PANEL P/N: 145T5876-44, PNL NO.242WFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N: 145T5876-44
- [SDR IPXA2024101684508](https://openairdocs.org/sdr/IPXA2024101684508.md): Rib · cracked · Oct 6, 2024 · N322UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > CRACK - FITTING, RIGHT WING NO.10 SPOILER HINGE INBD SIDE (REPLACE) 1.OK TO INSTALL CHECK SATISFIED. 2.I.A.W AMM 20-10-03-404-037 REV.143 RECONNECT RH OUTBOARD AILERON A4A AND A4B CONTROL CABLE. 3.I.A.W AMM 27-61-02-424-023 REV.143 RECONNECT NO.11 AND NO.12 SP
- [SDR IPXA2024100876218](https://openairdocs.org/sdr/IPXA2024100876218.md): Floor Panel · broken · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > *** MAJOR REPAIR *** FAULT - BROKEN - FLOOR PNL, AT MAIN DECK, PANEL P/N: 145T5876-63, PNL NO.241DFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N: 145T5876-63
- [SDR IPXA2024100876234](https://openairdocs.org/sdr/IPXA2024100876234.md): Floor Panel · damaged · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > *** MAJOR REPAIR *** FAULT - DAMAGE - FLOOR PNL, AT MAIN DECK, PANEL P/N: 145T5876-60 PNL NO.241FFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N: 145T5876-60
- [SDR IPXA2024100871727](https://openairdocs.org/sdr/IPXA2024100871727.md): Floor Panel · damaged · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE PANEL NO.251UFF P/N: 146T5869-79 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024100872662](https://openairdocs.org/sdr/IPXA2024100872662.md): Floor Panel · dented · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE 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 25-57-02-404-016 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024100876223](https://openairdocs.org/sdr/IPXA2024100876223.md): Floor Panel · damaged · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR *** FAULT - CRACK - FLOOR PNL, M/D STA 977~STA 1043, PANEL P/N: 145T5876-71, PNL NO.241YFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N: 145T5876-71
- [SDR IPXA2024100871732](https://openairdocs.org/sdr/IPXA2024100871732.md): Floor Panel · damaged · Oct 5, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE PANEL NO.231RFF P/N: 143T5876-58 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024102287628](https://openairdocs.org/sdr/IPXA2024102287628.md): None · none · Oct 1, 2024 · N322UP · Boeing 76734AF · Standard Practices/Structures
  > (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)
- [SDR IPXA2024102291536](https://openairdocs.org/sdr/IPXA2024102291536.md): Lens · cracked · Oct 1, 2024 · N322UP · Boeing 76734AF · Emergency Lighting
  > FOUND ENTRY DOOR FWD SIDE DOORWAY SIGN ASSY LENS CRACK. (REPLACE) 1. I.A.W AMM 33-51-01-022-029, 33-51-01-402-030 REV 143 REPLACED EXIT SIGN, AND CONDITION CHECK NORMAL. I.A.W AMM 33-51-01-402-030 REV 143 PERFORMED EXIT SIGN LAMP TEST, RESULT WAS SATISFACTORY.
- [SDR IPXA2024100287628](https://openairdocs.org/sdr/IPXA2024100287628.md): None · none · Oct 1, 2024 · N322UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OK TO WORK
- [SDR IPXA2024100191536](https://openairdocs.org/sdr/IPXA2024100191536.md): Lens · cracked · Oct 1, 2024 · N322UP · Boeing 76734AF · Emergency Lighting
  > *SDR FILED OPEN* FAULT - FOUND ENTRY DOOR FWD SIDE DOORWAY SIGN ASSY LENS CRACK. (REPLACE)
- [SDR IPXA2024101674413](https://openairdocs.org/sdr/IPXA2024101674413.md): Angle · cracked · Sep 30, 2024 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD. (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 90. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETED.
- [SDR IPXA2024101674438](https://openairdocs.org/sdr/IPXA2024101674438.md): Angle · cracked · Sep 30, 2024 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.143 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024090764443](https://openairdocs.org/sdr/IPXA2024090764443.md): Floor Panel · damaged · Sep 6, 2024 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND DAMAGE ON PREVIOUS REPAIR OF REMOVED FLOORBOARD FROM POS 9/10 CENTER. ROUTED FLOOR PANEL TO SHEET METAL FOR EVAL INSTALLED MAIN CARGO DECK FLOOR PANEL IAW AMM 53-01-06-400-801. C/W EO 9693
- [SDR IPXA2024032136997](https://openairdocs.org/sdr/IPXA2024032136997.md): Skin · corroded · Mar 13, 2024 · N322UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FUSELAGE DRAIN VALVE ASSY AT BELLY ZONE 155/156,APPROXIMATE FUSELAGE STA. 1373 HAS PULLED THROUGH SKIN AND HAS EXTENSIVE CORROSION AROUND HOLE CREATED,ON OUTER AND INNER SKIN AREA.SKIN IS DEFOLIATING REVIEWED. CUT OUT DAMAGE AREA AT FUSELAGE DRAIN VALVE ASSY
- [SDR IPXA2024031436997](https://openairdocs.org/sdr/IPXA2024031436997.md): Drain Valve · corroded · Mar 13, 2024 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FUSELAGE DRAIN VALVE ASSY AT BELLY ZONE 155/156,APPROXIMATE FUSELAGE STA. 1373 HAS PULLED THROUGH SKIN AND HAS EXTENSIVE CORROSION AROUND HOLE CREATED,ON OUTER AND INNER SKIN AREA.SKIN IS DEFOLIATING REMOVED AFT CARGO COMPARTMENT FLOORBOARDS AND DRAIN VALVE A
- [SDR IPXA2024012052414](https://openairdocs.org/sdr/IPXA2024012052414.md): Cabin Pressure · faulted · Jan 20, 2024 · N322UP · Boeing 76734AF · Cabin Pressure Control System
  > *ETOPS FILED OPEN* STATUS MSG CABIN ALT AUTO 2 APPEARED ENROUTE AT CRUISE ALTITUDE WHILE SWITCH WAS IN AUTO 2 DEFERRED CABIN ALT AUTO 2 INOP PER MEL 21-31-1A. PLACARD INST.
- [SDR IPXA2024013124637](https://openairdocs.org/sdr/IPXA2024013124637.md): Trim Panel · broken · Jan 13, 2024 · N322UP · Boeing 76734AF · Passenger/Crew Doors
  > **SUPPLEMENTAL SDR**TRIM BROKEN L1 DOOR SIDE WALL PANEL INSTALLED NEW SPLINE TRIM PIECE I/A/W INDUSTRY STANDARD PRACTICES AND IPC 52-11-02-10A. NO DEFECTS NOTED AT THIS TIME.
- [SDR IPXA2024011424637](https://openairdocs.org/sdr/IPXA2024011424637.md): Unknown · unknown · Jan 13, 2024 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > RIM BROKEN L1 DOOR SIDE WALL PANEL ASSIGNED EO-89173-REQ1 TO FAULT.
- [SDR IPXA2024020776726](https://openairdocs.org/sdr/IPXA2024020776726.md): Cover · broken · Sep 16, 2023 · N322UP · Boeing 76734AF · Passenger/Crew Doors
  > PLASTIC DOOR HANDLE COVER ON MAIN ENTRY DOOR BROKE OFF. INSTALLED HINGE AND ACCESS DOOR IAW SRM 51-40-02. C/W REINSTALLED ACCEST PANEL
- [SDR IPXA2023091676726](https://openairdocs.org/sdr/IPXA2023091676726.md): Unknown · unknown · Sep 16, 2023 · N322UP · Boeing 76734AF · Passenger/Crew Doors
  > **SDR FILED OPEN**PLASTIC DOOR HANDLE COVER ON MAIN ENTRY DOOR BROKE OFF.***REQ 465504***SM4/LMX4*** DEFERRED PER MEL 52-11-2
- [SDR IPXA2023050846048](https://openairdocs.org/sdr/IPXA2023050846048.md): Escape Reel · damaged · May 6, 2023 · N322UP · Boeing 76734AF · Emergency Equipment
  > 3RD (FROM FWD) EMERGENCY DESCENT DEVICE DAMAGED WILL NOT STOW PROPERLY R&R'D EMERGENCY DESCENT DEVICE ( POS 3) IAW AMM 25-61-03-201
- [SDR IPXA2023050847127](https://openairdocs.org/sdr/IPXA2023050847127.md): Escape Reel · partial deploy · May 6, 2023 · N322UP · Boeing 76734AF · Emergency Equipment
  > EMERGENCY DESCENT DEVICE (4TH FROM FWD) PARTIALLY DEPLOYED R&R'D EMERGENCY DESCENT DEVICE #4 IAW AMM 25-61-03-201
- [SDR IPXA2023051393098](https://openairdocs.org/sdr/IPXA2023051393098.md): Floorboard · damaged · Feb 22, 2023 · N322UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR (SREO) 27379. REF EO-27379 * PARTS REQ 438130 *)***SM13/LMX8*** ALL STEPS COMPLIED WITH, REF SREO-9693-REQ001 T3F18E001DJ6X CLEARING DMI
- [SDR IPXA2022110287740](https://openairdocs.org/sdr/IPXA2022110287740.md): Skin · corroded · Oct 28, 2022 · N322UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C13, CORROSION WAS FOUND ON SKIN (P/N:114T4103-4) OF NO.10 SLAT BETWEEN OSS 684 AND 693.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAGE 1 REV 84.01
- [SDR IPXA2022110387788](https://openairdocs.org/sdr/IPXA2022110387788.md): Skin · cracked · Oct 25, 2022 · N322UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C13, CRACK DAMAGE WAS FOUND ON NR 1 PYLON OUTBD SKIN ASSEMBLY (P/N:311T2450-25) NEAR NAC STA 237.5. PERFORM REPAIR I.A.W UPS EO B767-5430-85116-A
- [SDR IPXA2022110287741](https://openairdocs.org/sdr/IPXA2022110287741.md): Skin · corroded · Oct 25, 2022 · N322UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C13CORROSION WAS FOUND ON SKIN(P/N:114T4104-4) OF NO.9 SLAT BETWEEN OSS 670 AND 682.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAMGE 1 REV 84.01
- [SDR IPXA2021022466057](https://openairdocs.org/sdr/IPXA2021022466057.md): Shutoff Valve · malfunctioned · Feb 23, 2021 · N322UP · Boeing 76734AF · Pneumatic Distribution System
  > INSPECTION TYPE: ETOP** ETOPS FILED OPEN ** ON TAKEOFF @70 KTS, RECEIVED A L ENG HPSOV VALVE EICAS CAUTION LIGHT. RESULTED IN A RTO. DEFERRED LEFT ENG HPSOV PER MEL 36-11-2-2. ACCOMPLISHED DMP 36-11-2-2. PLACARD INSTALLED.
- [SDR IPXA2021020465312](https://openairdocs.org/sdr/IPXA2021020465312.md): Battery · no test · Feb 4, 2021 · N322UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:NAEMER. LIGHT TEST INOP.R&R BATTERY IAW AMM 33-51-01 EMER. LIGHT TEST OK.
- [SDR IPXA2021020265212](https://openairdocs.org/sdr/IPXA2021020265212.md): Battery Pack · inoperative · Feb 1, 2021 · N322UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:NAEMERGENCY LIGHT'S WOULD NOT ILLUMINATE WITH SWITCH IN ON POSITION.R&R BATTERY PACK I/A/W AMM 33-51-07-422-012, OP'S CK'ED OK. REF 33-51-07-32-020Q
- [SDR IPXA2021011864558](https://openairdocs.org/sdr/IPXA2021011864558.md): Control Panel · intermittent · Jan 16, 2021 · N322UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE: NA EMERGENCY LIGHTS COME ON FOR 1-2 SECONDS, THEN GO OUT. RESET SWITCHES SEVERAL TIMES, PROBLEM CONTINUES. R & R THE EMERGENCY LIGHT CONTROL PANEL ASSEMBLY, IAW AMM IPC: 33-51-08-01A.
- [SDR IPXA2020101261186](https://openairdocs.org/sdr/IPXA2020101261186.md): Stiffener · cracked · Oct 2, 2020 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C12 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-6) ON STA 785, RBL 55. REPAIR IAW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 78.00 AND UPS EO B767-5740-78055-A.
- [SDR IPXA2020101261185](https://openairdocs.org/sdr/IPXA2020101261185.md): Stiffener · cracked · Oct 2, 2020 · N322UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C12 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785, RBL 33. REPAIR IAW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 78.00, AND UPS EO B767-5740-78055-A.
- [SDR IPXA2019112749468](https://openairdocs.org/sdr/IPXA2019112749468.md): Window · cracked · Nov 26, 2019 · N322UP · Boeing 76734AF · Flight Compartment Windows
  > CAPTAIN FWD WINDOW IS CRACKED, PRESSURE HOLDING, NO AIR LEAK NOTED. R & R THE LEFT FWD AND RT SIDE WINDOW HEAT CONTROL UNIT IAW AMM 30-40-01. OPS CHECKED GOOD. R & R WINDOW IAW AMM 56-11-01. OPS CHECKED NORMAL.
- [SDR IPXA2019112544328](https://openairdocs.org/sdr/IPXA2019112544328.md): Skin · punctured · Nov 24, 2019 · N322UP · Boeing 76734AF · Elevator, Plate/Skin
  > INSPECTION TYPE:N/ALEFT ELEVATOR UPPER SKIN HAS SMALL PUNCTUREREPAIRED PER EO B767-5520-74726-A
- [SDR IPXA2018120236483](https://openairdocs.org/sdr/IPXA2018120236483.md): O-Ring · leaking · Dec 1, 2018 · N322UP · Boeing 76734AF · Turbine Engine Oil System
  > NR 2 ENGINE, NR 1 BEARING MANIFOLD WAS LEAKING. R & R THE BEARING MANIFOLD O-RING IAW 72-31-03-401.

Next page: https://openairdocs.org/aircraft/N322UP/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 = 'N322UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N322UP/reports

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