# Service difficulty reports: N326UP

A list on [N326UP](https://openairdocs.org/aircraft/N326UP.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 · 146 reports

- [SDR IPXA2026072007978](https://openairdocs.org/sdr/IPXA2026072007978.md): Window · cracked · Jul 17, 2026 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM! REPLACED LT SLIDING FLIGHT DECK WINDOW IAW AMM 56-11-02. PRESSURIZED AIRCRAFT WITH NO LEAKS NOTED. WINDOW HEAT OPS TEST SUCCESSFUL. CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM
- [SDR IPXA2026071707978](https://openairdocs.org/sdr/IPXA2026071707978.md): Window · cracked · Jul 17, 2026 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM!
- [SDR IPXA2026060105255](https://openairdocs.org/sdr/IPXA2026060105255.md): Window · cracked · May 29, 2026 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > L SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH. PERFORMED RII INSPECTION PER GMM 04-02 AND AMM 56-11-10 VERIFIED PROPER INSTALL AND TORQUE OF ELECTRICAL CONNECTORS R+R LH NO. 3 WINDOW PER AMM 56-11-10/401. WINDOW HEAT CHECK OPS TES
- [SDR IPXA2026052900055](https://openairdocs.org/sdr/IPXA2026052900055.md): Window · cracked · May 29, 2026 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > LEFT SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH.
- [SDR IPXA2026052906642](https://openairdocs.org/sdr/IPXA2026052906642.md): Window · failed · May 29, 2026 · N326UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > L3 WINDOW BURNED AT TEMP CONTROL SENSORS. CREW REPORTED BURNING SMELL PRIOR TO WINDOW CRACKING. REF BARCODE [T3F18E008X3R6] FOR WINDOW REPLACEMENT. R+R RIGHT FORWARD AND LEFT SIDE WINDOW HEAT CONTROL UNIT, WHCU M192 PER AMM 30-41-02/401. OPS CHECK GOOD.
- [SDR IPXA2026021059426](https://openairdocs.org/sdr/IPXA2026021059426.md): Skin Panel · corroded · Jan 31, 2026 · N326UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, CORROSION FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. (REPAIR. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-01 REPAIR 29 REV. 94 AND EGAT EI NO.F2026A53M-286 REV.1 AND UPS EO-96454-REQ1 REV1.
- [SDR IPXA2026020707464](https://openairdocs.org/sdr/IPXA2026020707464.md): Skin Panel · cracked · Jan 28, 2026 · N326UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER SKIN. ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 94 AND EGAT WORK SHEET NO: 60075 AND UPS EO-87307-REQ7 REV2.
- [SDR IPXA2026020977464](https://openairdocs.org/sdr/IPXA2026020977464.md): Skin · cracked · Jan 28, 2026 · N326UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. FOUND A CRACK ON THE NR1 FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED ENTRY DOOR SCUFF PLATE IAW AMM 53-13-01-424-005, REV 147. INSTALLED ENTRY DOOR DOORWAY LINING IAW AMM 52-12-02-404-025, REV 147.
- [SDR IPXA2025063074896](https://openairdocs.org/sdr/IPXA2025063074896.md): Light · inoperative · Jun 29, 2025 · N326UP · Boeing 76734AF · Emergency Lighting
  > COCKPIT EMERGANCY LIGHT EXIT INOP REMOVED AND REPLACED EMERGANCY BATTERY CHARGER ASSY PER MM 33-51-07. OPS CK GOOD
- [SDR IPXA2024102127737](https://openairdocs.org/sdr/IPXA2024102127737.md): Cover · detached · Oct 19, 2024 · N326UP · Boeing 76734AF · Emergency Lighting
  > EXIT LIGHT COVER FOR LIGHT OVER CREW DOOR HANDLE FELL OFF WILL NOT STAY ATTACHED. C/W EO-91789-REQ1
- [SDR IPXA2024101927838](https://openairdocs.org/sdr/IPXA2024101927838.md): Charger · inoperative · Oct 19, 2024 · N326UP · Boeing 76734AF · Emergency Lighting
  > MAIN ENTRY DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE AFTER ATTACHING COVER REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY IAW AMM 33-51-07. OPS CHECK GOOD.
- [SDR IPXA2024030705540](https://openairdocs.org/sdr/IPXA2024030705540.md): Window · leaking · Mar 5, 2024 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > R2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. PERFORMED R2 WINDOW ADJUSTMENT PER AMM 56-11-02-825-122, STEP 2.J(1)(H). APPLIED FILLET SEALANT TO LOWER AFT CORNER OF R2 SEAL PER AMM 56-11-11-404-006.G(
- [SDR IPXA2024030605540](https://openairdocs.org/sdr/IPXA2024030605540.md): Window · leaking · Mar 5, 2024 · N326UP · Boeing 76734AF · Flight Compartment Windows
  > *** SDR FILED OPEN *** R2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. C/W RII
- [SDR IPXA2024012302696](https://openairdocs.org/sdr/IPXA2024012302696.md): Angle · broken · Jan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 141T8310 SH. 4 REV. H. REVIEWED
- [SDR IPXA2024012301393](https://openairdocs.org/sdr/IPXA2024012301393.md): Scuff Plate · cracked · Jan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE). 1.I.A.W AMM 53-13-01-424-005 REV.141 INSTALLED THE SCUFF PLATE. 2.ACCOMPLISHED THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST I.A.W AMM 05-51-24-782-001 REV.141, NO LEAKAGE WAS FOUND. 3.JOB
- [SDR IPXA2024011202696](https://openairdocs.org/sdr/IPXA2024011202696.md): Unknown · unknown · Jan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE)
- [SDR IPXA2024011201393](https://openairdocs.org/sdr/IPXA2024011201393.md): Unknown · unknown · Jan 12, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE) OK TO WORK
- [SDR IPXA2024012382386](https://openairdocs.org/sdr/IPXA2024012382386.md): Pawl · worn · Jan 11, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > FAULT - FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.141 AND AMM 52-11-26-404-003 REV.141 REPLACED PAWL, OPERATION CHECK NORMAL. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWED
- [SDR IPXA2024012382163](https://openairdocs.org/sdr/IPXA2024012382163.md): Cap · cracked · Jan 11, 2024 · N326UP · Boeing 76734AF · Trailing Edge Flaps
  > FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR). REMOVE THE DAMAGE AREA (L:0.2", W:0.1, 5" FROM AFTER EDGE AT LOWER EDGE) AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURE AT 200°F FOR 220 MINUTES KEEP A MINIMUM VACUUM OF 22 IN/HG I.A.W. UPS
- [SDR IPXA2024012382059](https://openairdocs.org/sdr/IPXA2024012382059.md): Web · cracked · Jan 11, 2024 · N326UP · Boeing 76734AF · Wing Main, Frame Structure
  > *SUPPLEMENTAL SDR* FAULT - CRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-89236-REQ1 REV.1. JOB COMPLETED. C/W REVIEW
- [SDR IPXA2024012282141](https://openairdocs.org/sdr/IPXA2024012282141.md): Spar · broken · Jan 11, 2024 · N326UP · Boeing 76734AF · Wing Spar
  > FAULT - BROKEN PLATE, LH WING T/E REAR SPAR LOWER SURFACE NEAR WS 698 (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 113T1663 SH. 2 REV. D. 3. JOB COMPLETED. REVIEWED
- [SDR IPXA2024011182059](https://openairdocs.org/sdr/IPXA2024011182059.md): Unknown · unknown · Jan 11, 2024 · N326UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR) OK TO WORK
- [SDR IPXA2024011182386](https://openairdocs.org/sdr/IPXA2024011182386.md): Unknown · unknown · Jan 11, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE) OK TO WORK
- [SDR IPXA2024011182163](https://openairdocs.org/sdr/IPXA2024011182163.md): Unknown · unknown · Jan 11, 2024 · N326UP · Boeing 76734AF · Trailing Edge Flaps
  > *** SDR FILED OPEN *** FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR) OK TO WORK
- [SDR IPXA2024012360713](https://openairdocs.org/sdr/IPXA2024012360713.md): Skin · damaged · Jan 10, 2024 · N326UP · Boeing 76734AF · Wing, Plate/Skin
  > FAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE). 1.REMOVED DAMAGE PARTS I.A.W. SRM 51-40-02-0G REV.88 2.INSTALLED NEW PARTS I.A.W. SRM 51-40-02-0G REV.88 AND BOEING DWG NO 114T2800 SH.5 REV.G 3.JOB COMPLETED. REVIEWED
- [SDR IPXA2024012355631](https://openairdocs.org/sdr/IPXA2024012355631.md): Skin · eroded · Jan 10, 2024 · N326UP · Boeing 76734AF · Leading Edge Devices
  > *SUPPLEMENTAL SDR* FAULT - EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA(LENGTH:0.5", WIDTH:0.3",DEPTH:1 PLY, 0.7" FROM TRAILING EDGE, 1" FROM OUTBOARD EDGE).BOND THE REPAIR PLIES WITH FI
- [SDR IPXA2024011060713](https://openairdocs.org/sdr/IPXA2024011060713.md): Unknown · unknown · Jan 10, 2024 · N326UP · Boeing 76734AF · Wing Main, Frame Structure
  > *** SDR FILED OPEN *** FAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE)
- [SDR IPXA2024011055631](https://openairdocs.org/sdr/IPXA2024011055631.md): Unknown · unknown · Jan 10, 2024 · N326UP · Boeing 76734AF · Wing Structure
  > EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR) OK TO WORK
- [SDR IPXA2024011635744](https://openairdocs.org/sdr/IPXA2024011635744.md): Angle · cracked · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETE
- [SDR IPXA2024012337994](https://openairdocs.org/sdr/IPXA2024012337994.md): Bumper · deformed · Jan 9, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE). I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141 REPLACED BUMPER. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWED
- [SDR IPXA2024012335573](https://openairdocs.org/sdr/IPXA2024012335573.md): Seal · broken · Jan 9, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > FAULT - FOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE). I.A.W AMM 52-09-01-024-018 REV. 141 AND AMM 52-09-01-424-019 REV.141 REPLACED DOORWAY LINING SEAL. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWED
- [SDR IPXA2024011735666](https://openairdocs.org/sdr/IPXA2024011735666.md): Angle · cracked · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK - ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL 49.3.(REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-05 REV. 88. PERFORMED THE HEAT TREATMENT FROM 7075-O-063 CLAD TO T62 CONDITION. I.A.W. WORK SHEET NO.:40034 WORK INSTRUCTIONS STEP 3 A
- [SDR IPXA2024011635775](https://openairdocs.org/sdr/IPXA2024011635775.md): Angle · cracked · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Structure (General)
  > *SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV.
- [SDR IPXA2024011635793](https://openairdocs.org/sdr/IPXA2024011635793.md): Angle · cracked · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETE
- [SDR IPXA2024011635810](https://openairdocs.org/sdr/IPXA2024011635810.md): Angle · cracked · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV
- [SDR IPXA2024011037994](https://openairdocs.org/sdr/IPXA2024011037994.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > *** SDR FILED OPEN *** FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE) OK TO WORK
- [SDR IPXA2024011035573](https://openairdocs.org/sdr/IPXA2024011035573.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE) OK TO WORK
- [SDR IPXA2024010935666](https://openairdocs.org/sdr/IPXA2024010935666.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL (REPLACE) OK TO WORK
- [SDR IPXA2024010935810](https://openairdocs.org/sdr/IPXA2024010935810.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935744](https://openairdocs.org/sdr/IPXA2024010935744.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935793](https://openairdocs.org/sdr/IPXA2024010935793.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935775](https://openairdocs.org/sdr/IPXA2024010935775.md): Unknown · unknown · Jan 9, 2024 · N326UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *** SDR FILED OPEN *** FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024012322914](https://openairdocs.org/sdr/IPXA2024012322914.md): Beam · cracked · Jan 8, 2024 · N326UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV. 88. AND BOEING SERVICE BULLETIN 767-54-0
- [SDR IPXA2024012322940](https://openairdocs.org/sdr/IPXA2024012322940.md): Beam · cracked · Jan 8, 2024 · N326UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV. 88. AND BOEING SERVICE BULLETIN 767-54-0
- [SDR IPXA2024010822914](https://openairdocs.org/sdr/IPXA2024010822914.md): Unknown · unknown · Jan 8, 2024 · N326UP · Boeing 76734AF · Nacelle/Pylon Structure
  > *** SDR FILED OPEN *** FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)
- [SDR IPXA2024010822940](https://openairdocs.org/sdr/IPXA2024010822940.md): Unknown · unknown · Jan 8, 2024 · N326UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)
- [SDR IPXA2022110787881](https://openairdocs.org/sdr/IPXA2022110787881.md): Lock · inoperative · Nov 6, 2022 · N326UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:NACREW ENTRY DOOR SECURE LOCK STICKING.LUBED EXTERIOR APPR LATCH IN MECHANISM. DOOR OPERATES AS ADVERTISED.Ï¿½52-12-00-715-119
- [SDR IPXA2022082785667](https://openairdocs.org/sdr/IPXA2022082785667.md): None · none · Aug 27, 2022 · N326UP · Boeing 767 · Pitot/Static Anti-Ice System
  > INSPECTION TYPE:NA**ATB**AT APPROXIMIMATELY 3000FT, ON DEPARTURE "TAT PROBE" EICAS MESSAGE AND FAILURE.REPLACED TAT PROBE PER AMM 34-12-02-404-008, BUT SAME CONDITION. REPLACED CURRENT SENSING RELAY PER WDM 30-33-11 SHEET1, TAT PROBE HEAT SYSTEM OPERATION TEST
- [SDR IPXA2022080985047](https://openairdocs.org/sdr/IPXA2022080985047.md): Light · inoperative · Aug 8, 2022 · N326UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/ADURING PDC FOUND EMG LIGHTS INOP.R/R EMG BATT PACK IAW AMM 33-51-07. OPS CHECK SAT.
- [SDR IPXA2022072584563](https://openairdocs.org/sdr/IPXA2022072584563.md): Eicas · fault message · Jul 24, 2022 · N326UP · Boeing 76734AF · Air Conditioning System
  > INSPECTION TYPE:ETOP** ETOPS FILED OPEN**GOT A "R PACK TEMP" EICAS MSG ON SHORT FINAL. RAN QRH AND INOP LIGHT EXTINGUISHED. DEFERRED R PACK TEMP CONTROL AUTO MODE IAW MEL 21-51-3-1 - PLACARD INSTALLED; PARTS ON REQ 406077. SUGGEST REPLACING C/P AND SENSORD - 2

Next page: https://openairdocs.org/aircraft/N326UP/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 = 'N326UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N326UP/reports

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