# Service difficulty reports: N323UP

A list on [N323UP](https://openairdocs.org/aircraft/N323UP.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 · 161 reports

- [SDR IPXA2026101442976](https://openairdocs.org/sdr/IPXA2026101442976.md): Flap System · faulted · Oct 14, 2026 · N323UP · Boeing 76734AF · Trailing Edge Flaps
  > AIR TURN BACK, EMERGENCY DECLARED. AFTER TAKEOFF ON FLAP RETRACTION EICAS MESSAGE LE SLAT ASYMMETRY. FOLLOWED QRH PROCEDURE COULD NOT RETRACT SLAT. RETURNED SDF.
- [SDR IPXA2026092495235](https://openairdocs.org/sdr/IPXA2026092495235.md): Pawl · not seated · Sep 23, 2026 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > L FWD ENT DOOR SECURE HANDLE WILL NOT SEAT FOUND DEEP GOUGES IN ENTRY DOOR INTERLOCK PAWL. REPLACED INTERLOCK PAWL IAW AMM 52-11-26-404-003. OPS CHECK GOOD IAW AMM 52-11-26-710-801.
- [SDR IPXA2026072263413](https://openairdocs.org/sdr/IPXA2026072263413.md): Elevator · damaged · Jul 21, 2026 · N323UP · Boeing 76734AF · Elevator Structure
  > ***SUPPLEMENTAL SDR*** LINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LH INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESSED OPS CHECKS PER GMM 04-02. INSTALLED LEFT INBD ELEVATOR. REF MM 27-31-01-401.ALL BOLTS TORQUED
- [SDR IPXA2026072163413](https://openairdocs.org/sdr/IPXA2026072163413.md): Elevator · damaged · Jul 21, 2026 · N323UP · Boeing 76734AF · Elevator Structure
  > LINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LT INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESSED OPS CHECKS PER GMM 04-02.
- [SDR IPXA2024111257988](https://openairdocs.org/sdr/IPXA2024111257988.md): Strap · cracked · Nov 4, 2024 · N323UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED BULKHEAD OUTER CHORD STRAP AT BS 1725 S-7R. (REPAIR). COMPLETED REPAIR I.A.W EGAT WORK SHEET NO.40938 STEP D.5 AND D.6 AND D.8 AND D.10 AND D.11 AND D.13~D.19. ACCOMPLISHED UPS EO NO. EO-24301-JIC003 REV. 4 AND EGAT WORK SHEET NO. 40938.
- [SDR IPXA2024110450317](https://openairdocs.org/sdr/IPXA2024110450317.md): Floor Panel · broken · Nov 3, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO. 241DFF BROKEN AT STA 731 TO STA 834 LBL-65, P/N: 145T5876-63.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338489](https://openairdocs.org/sdr/IPXA2024110338489.md): Floor Panel · damaged · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 1040 TO STA 1114 LBL-45, P/N: 145T5876-43, PANEL NO 241BGF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110436353](https://openairdocs.org/sdr/IPXA2024110436353.md): Skin · damaged · Nov 2, 2024 · N323UP · Boeing 76734AF · Leading Edge Devices
  > BIRD STRIKE - SKIN, UPPER FACE OF L/H WING NO.4 SLAT T/E SKIN, OSS 545.75.JOB COMPLETED AND CONDITION CHECK NORMAL AND ATTACHMENT ARE UPLOADED. I.A.W AMM 27-81-02-424-099 REV.143 STEP 3A TO H (16) INSTALLED NO.4 SLAT OF THE LH WING.
- [SDR IPXA2024110338863](https://openairdocs.org/sdr/IPXA2024110338863.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO.241EFF DENT AT STA 746 TO STA 876 LBL 80, P/N:145T5876-1.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338708](https://openairdocs.org/sdr/IPXA2024110338708.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO.241WFF DENT AT STA 980 TO STA-1114 LBL11, P/N: 145T5876-73. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338469](https://openairdocs.org/sdr/IPXA2024110338469.md): Floor Panel · debonded · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO.241BFF DISBOND AT STA 731 TO STA 834 LBL-22, P/N:145T5876-70. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338198](https://openairdocs.org/sdr/IPXA2024110338198.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > DENT - FOUND M/D FLOOR PNL NO.242FFF AT STA 834 TO STA 933 RBL -45, P/N: 145T5876-61.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338212](https://openairdocs.org/sdr/IPXA2024110338212.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL DISBOND AND DENT AT STA 746 TO STA 876 RBL -80 PNL NO.242DFF, P/N: 145T5876-7. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338861](https://openairdocs.org/sdr/IPXA2024110338861.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO.241CFF DENT AND INSERT DAMAGE AT STA 731 TO STA 834 LBL-45, P/N:145T5876-65. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338563](https://openairdocs.org/sdr/IPXA2024110338563.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND FLOOR PNL NO.241QFF DENT AT STA 933 TO STA 980 LBL-80, P/N: 145T5876-78. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338943](https://openairdocs.org/sdr/IPXA2024110338943.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL DENT AND INSERT DAMAGE AT STA 988 TO STA 1114 LBL 65 PNL NO.241ZFF, P/N:145T5876-77.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338453](https://openairdocs.org/sdr/IPXA2024110338453.md): Floor Panel · dented · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND M/D FLOOR PNL NO.241GFF DENT AT STA 834 TO STA 933 LBL-22, P/N: 145T5876-59. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110336507](https://openairdocs.org/sdr/IPXA2024110336507.md): Floor Panel · broken · Nov 2, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > BROKEN - FOUND M/D FLOOR PNL BROKEN AT STA933 TO STA980 RBL-80 P/N: 145T5876-84, PANEL NO.242MFF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024112108973](https://openairdocs.org/sdr/IPXA2024112108973.md): Trim Panel · broken · Nov 1, 2024 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.143 AND AMM 52-12-02-404-025 REV.143.
- [SDR IPXA2024110905997](https://openairdocs.org/sdr/IPXA2024110905997.md): Skin · corroded · Nov 1, 2024 · N323UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > CORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. ACCOMPLISH REPAIR PER EO-91974-REQ1 AND EGAT EI F2024A53M-2800, REV. 0 AND 1.
- [SDR IPXA2024110908905](https://openairdocs.org/sdr/IPXA2024110908905.md): Adapter · cracked · Nov 1, 2024 · N323UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1109 BL 0.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 90. AND BOEING DWG NO. 457T4000 SH. 11 REV. B
- [SDR IPXA2024110207456](https://openairdocs.org/sdr/IPXA2024110207456.md): Floor Panel · dented · Nov 1, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND THE MAIN DECK CARGO FLOOR PANEL DENT, P/N: 146T5869-134. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110207366](https://openairdocs.org/sdr/IPXA2024110207366.md): Floor Panel · dented · Nov 1, 2024 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND THE MAIN DECK CARGO FLOOR PANEL DENT, P/N: 146T5869-135. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110108973](https://openairdocs.org/sdr/IPXA2024110108973.md): Spline · broken · Nov 1, 2024 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. (REPLACE) OK TO WORK.
- [SDR IPXA2024103178075](https://openairdocs.org/sdr/IPXA2024103178075.md): None · none · Oct 31, 2024 · N323UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. REVIEW COMPLETED PER EO-82173-J1C001.CONDITION CHECK OK
- [SDR IPXA2024100427643](https://openairdocs.org/sdr/IPXA2024100427643.md): Fire Seal · damaged · Oct 3, 2024 · N323UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > *SUPPLEMENTAL SDR* #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19. RE-INSTALLED PANEL PER SRM 51-40-02.
- [SDR IPXA2024100327643](https://openairdocs.org/sdr/IPXA2024100327643.md): Fire Seal · damaged · Oct 3, 2024 · N323UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19.
- [SDR IPXA2024060603700](https://openairdocs.org/sdr/IPXA2024060603700.md): Slat Track · damaged · Jun 5, 2024 · N323UP · Boeing 76734AF · Leading Edge Devices
  > R/H WING #7 SLAT TRACK LEADING EDGE PANEL DAMAGED. REMOVE AND REPLACED LEADING EDGE SUPPORT LINK DOOR R/H INB AS PER 57-41-59 404-009, OPS CHKS GOOD-
- [SDR IPXA2024010917389](https://openairdocs.org/sdr/IPXA2024010917389.md): Spring · broken · Dec 30, 2023 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > *** SUPPLEMENTAL SDR *** CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN REPLACED CREW ENTRY DOOR ARMING HINGE COVER REF MM 52-12-02 OPS CK GOOD THIS CLEARS DEFERRAL
- [SDR IPXA2023123017389](https://openairdocs.org/sdr/IPXA2023123017389.md): Unknown · unknown · Dec 30, 2023 · N323UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN DEFERRED CREW ENTRY DOOR HINGED COVER IAW MEL 52-11-2, PLACARDS INSTALLED. OPEN
- [SDR IPXA2023030191440](https://openairdocs.org/sdr/IPXA2023030191440.md): Slat · inoperative · Mar 1, 2023 · N323UP · Boeing 76734AF · Leading Edge Slat Control System
  > INSPECTION TYPE:NA*EMERGENCY DECLARED* LEADING EDGE SLATS DISAGREE RAN CHECKLIST AND CONFIGURED SUCCESFULLYBITE CARRIED OUT IAW FIM 27-51-00-815-809 FLAPS/SLATS EXTENDED/RETRACTED WITH NO FAULTS
- [SDR IPXA2022102587489](https://openairdocs.org/sdr/IPXA2022102587489.md): Skin · misrepaired · Oct 24, 2022 · N323UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > TEMP BLIND FASTENER INSTALLED FUSELAGE 8" FWD OR STA 676 - 1 INCH O/B OF S39LREPAIRED IAW E.O. B767-5330-85085-B ON NRC 684229
- [SDR IPXA2022102487432](https://openairdocs.org/sdr/IPXA2022102487432.md): Skin · misinstalled · Oct 24, 2022 · N323UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/ATEMP BLIND FASTENER INSTALLED FUSELAGE 8 INCH FWD OR STA 676 - 1 INCH O/B OF S39LFABRICATED REPAIR DOUBLER IAW UPS E.O.B767-5330-85085-A ON NRC 684228
- [SDR IPXA2022032480431](https://openairdocs.org/sdr/IPXA2022032480431.md): Thrust Reverser · inoperative · Mar 24, 2022 · N323UP · Boeing 76734AF · Engine Thrust Reverser
  > INSPECTION TYPE:**ETOPS FILED OPEN** ON LANDING, L THRUST REV WOULD NOT DEPLOY. DEFERRED LEFT ENG T/R PER MEL 78-31-1 C/W DMP 78-31-
- [SDR IPXA2021092074049](https://openairdocs.org/sdr/IPXA2021092074049.md): Engine · surges · Sep 18, 2021 · N323UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > IFSD, ATB, EMERGENCY DECLARED, AIRCRAFT OOS, APPROXIMATELY 200' AFTER TAKE OFF, ENG STARTED TO SURGE. DURING THE CLIMB THE L ENG HAD NO RESPONSE FROM THE L THRUST LEVER. RAN APPROPRIATE CHECKLIST AND SHUTDOWN L ENG. A/C AWAITING LEFT ENG CHANGE.R/R #1 ENGINE
- [SDR IPXA2021020565355](https://openairdocs.org/sdr/IPXA2021020565355.md): Panel · damaged · Jan 31, 2021 · N323UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE: C12 DAMAGE ON MD CARGO FLOOR PANEL BETWEEN STA 510 - 620, LBL 11 - RBL 11. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2021020665376](https://openairdocs.org/sdr/IPXA2021020665376.md): Floorbeam · corroded · Jan 27, 2021 · N323UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C12CORROSION WAS FOUND ON FLOOR BEAM (P/N: 146T5143-5) OF MAIN DECK FLOOR STRUCTURE AT STA 1518, RBL 70 - RBL 90REPAIR I.A.W BOEING SR 3-4942597086 AND UPS EO B767-5310-79232-A
- [SDR IPXA2021020565350](https://openairdocs.org/sdr/IPXA2021020565350.md): Floorbeam · corroded · Jan 27, 2021 · N323UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, LBL 60 - LBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.
- [SDR IPXA2021020565349](https://openairdocs.org/sdr/IPXA2021020565349.md): Floorbeam · corroded · Jan 27, 2021 · N323UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, RBL 60 - RBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.
- [SDR IPXA2021020365255](https://openairdocs.org/sdr/IPXA2021020365255.md): Stiffener · cracked · Jan 24, 2021 · N323UP · Boeing 76734AF · Fuel Storage
  > INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-11) ON STA 785.9, LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C
- [SDR IPXA2021020365254](https://openairdocs.org/sdr/IPXA2021020365254.md): Stiffener · cracked · Jan 24, 2021 · N323UP · Boeing 76734AF · Fuel Storage
  > INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-5) ON STA 785.9, LBL 55REAPIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C
- [SDR IPXA2021011864585](https://openairdocs.org/sdr/IPXA2021011864585.md): Actuator · leaking · Jan 18, 2021 · N323UP · Boeing 76734AF · Hydraulic System, Main
  > INSPECTION TYPE: NA, ATB, NO EMERGENCY DECLARED & NO EQUIPMENT USED. T/O & 38 MINS GOT L HYD QUANTITY EICAS LT QUANTITY L HYD PRIM PUMP. EICAS LIGHT CAME ON WHEN USING SPEEDBRAKES. ARRIVED WITH ZERO FLUID IN LT SYS. NEVER LOST SYSTEM PRESSURE FOUND ELECTRO
- [SDR IPXA2020092160443](https://openairdocs.org/sdr/IPXA2020092160443.md): Module · malfunctioned · Sep 20, 2020 · N323UP · Boeing 76734AF · Central Warning
  > INSPECTION TYPE: N/A ATB- EMERGENCY DECLARED. RECEIVED FIRE WARNING BELL ON TAKE OFF ROTATION COULD NOT EXTINGUISH. R & R M1000 BELL CHIME MODULE BOARD, PER MM 31-51-04-004-133/404-014. TEST PER AMM 31-51-04-724-154. PN ON AND OFF 285T0385-5. SN OFF 01860
- [SDR IPXA201902138893](https://openairdocs.org/sdr/IPXA201902138893.md): Stiffener · cracked · Jan 27, 2019 · N323UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C11CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL 25, WL 159.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL, FIGURE 1, REV 73.01
- [SDR IPXA2018121436920](https://openairdocs.org/sdr/IPXA2018121436920.md): Shutoff Valve · faulty · Dec 14, 2018 · N323UP · Boeing 76734AF · Cabin Cooling System
  > INSPECTION TYPE:N/A ATB - DUE TO CABIN ALTITUDE. AFTER ACCOMPLISHING THE QRH PROC CABIN REMAINED UNCONTROLLABLE. PERFORMED PRESSURE CONTROLLER BITE PROCEDURE FOUND NR 2 LOW IN FLOW FAULT FIM 21-31-00-815-803/REF TS-B767-2150-00007 FOUND LEFT PACK "LO" FLOW 25%
- [SDR IPXA2018110213543](https://openairdocs.org/sdr/IPXA2018110213543.md): Controller · malfunctioned · Nov 1, 2018 · N323UP · Boeing 76734AF · Cabin Temperature Control System
  > EICAS MESSAGE FOR THE AFT CABIN TEMP INOPERATIVE. OPEN
- [SDR IPXA2018093034543](https://openairdocs.org/sdr/IPXA2018093034543.md): Blade · missing · Sep 29, 2018 · N323UP · Boeing 76734AF · Turbine Engine Air Inlet Section
  > INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DIMENSION GREATER THAN 5 EDGE HOLES. REFER TO AMM 72-00-00-206-363-H00 TABLE 680 FOR MAX SVCABLE LIMI
- [SDR IPXA2018100194543](https://openairdocs.org/sdr/IPXA2018100194543.md): Blade · damaged · Sep 29, 2018 · N323UP · Boeing 76734AF · Turbine Engine Compressor Section
  > PERFORMED A BORESCOPE INSPECTION ON THE NR 2 ENGINE IAW PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON THE LEADING EDGE, MEASURING DIMENSION GREATER THAN 5 EDGE HOLES IAW MM 72-00-00-206-363-H00, TABLE 680 FOR MAX SERVICABLE LIMITS.
- [SDR IPXA2018090533586](https://openairdocs.org/sdr/IPXA2018090533586.md): Pump · malfunctioned · Sep 4, 2018 · N323UP · Boeing 76734AF · Fuel Boost Pump
  > ENGINE FUEL FEED SYSTEM L, FWD FUEL PUMP EICAS MSG SHOWS AND L FWD PUMP PRESS LIGHT IS ON WITH SWITCH ON. REPLACED L FWD FUEL PUMP GFI, RELAY REF FIM 28-22-00 FIG 114 & WDM 28-22-11, RELAY K10703 [TJQ 0558733 9-4-18] SYSTEM OPS CHECKS OK. REF FIM FIG 114, 28-2
- [SDR IPXA2018041628640](https://openairdocs.org/sdr/IPXA2018041628640.md): Module · faulted · Apr 12, 2018 · N323UP · Boeing 76734AF · Rudder Control System
  > AIR TURNBACK. AFTER TAKEOFF, THE RUDDER RATIO EICAS ILLUMINATED. FOUND THE RIGHT RUDDER RATIO CHANGER MODULE FAULTED. R & R THE MODULE IAW MM 27-09-00. OPS CHECKED GOOD IAW MM 27-21-00.

Next page: https://openairdocs.org/aircraft/N323UP/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 = 'N323UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N323UP/reports

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