# Service difficulty reports: N309UP

A list on [N309UP](https://openairdocs.org/aircraft/N309UP.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 · 172 reports

- [SDR IPXA2026083182839](https://openairdocs.org/sdr/IPXA2026083182839.md): Escape Rope · unwanted deploy · Aug 8, 2026 · N309UP · Boeing 76734AF · Emergency Equipment
  > ESCAPE ROPE AT CREW ENTRY DOOR DEPLOYED. REPLACED FLIGHT COMPARTMENT DESCENT ROPE COVER ASSY AND REINSTALLED DESCENT ROPE PER AMM 25-61-04
- [SDR IPXA2026013054938](https://openairdocs.org/sdr/IPXA2026013054938.md): Driver Unit · faulted · Jan 11, 2026 · N309UP · Boeing 76734AF · Cargo/Baggage Doors
  > EMERGENCY DECLARED, CARGO DOOR INDICATION EICAS PERFORMED BITE TEST ON PSEU IAW FIM 32-09 FAULT TREE 803. FOUND INTERNAL PSEU DRIVER CARD 006 AND SENSOR 892 FAULTED. REPLACED DRIVER CARD 006 IAW AMM 32-09-06, OPS CHECK GOOD. CHECKED ADJUSTMENT OF S892 SENSOR
- [SDR IPXA2026011154938](https://openairdocs.org/sdr/IPXA2026011154938.md): Warning Message · illuminated · Jan 11, 2026 · N309UP · Boeing 76734AF · Door Warning System
  > EMERGENCY DECLARED. CARGO DOOR INDICATION EICAS ITEM PLACED ON MEL 52-71-1-2 ACCOMPLISHED DMP AND PLACARD INSTALLED
- [SDR IPXA2025071525054](https://openairdocs.org/sdr/IPXA2025071525054.md): Skin · corroded · Jul 2, 2025 · N309UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, CORROSION-SKIN, AFT CGO COMPT FWD SIDE LWR SKIN, NEAR STA 1081 S-39L~S-39R. ACCOMPLISHED REPAIR I.A.W UPS EO NO:EO-94375-REQ1 REV.1 AND BOEING DWG NO.140T0130 SH.16 REV.C;140T0130 SH.7 REV.C;146T1201 SH.1 REV.H AND 146T3261 SH.3 REV.-.
- [SDR IPXA2025071524693](https://openairdocs.org/sdr/IPXA2025071524693.md): Shaft · corroded · Jul 2, 2025 · N309UP · Boeing 76734AF · Trailing Edge Flaps
  > CORROSION AT LH SIDE NO.4 FLAP SUPPORT MECHANISM 6-6 OUTER SHAFT, STEP 3. PERFORM OK TO INSTASLL CHECK SATISFIED & INSTALL NEW LH WING NO.4 FLAP SUPPORT MECHANISM 6-6 OUTER SHAFT & CONDITION CHECK NORMAL. (RII ITEM) CHECKED COMPLETED.
- [SDR IPXA2025071521351](https://openairdocs.org/sdr/IPXA2025071521351.md): Channel · corroded · Jul 2, 2025 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, CORROSION AT CARGO COMPARTMENT CEILING PANEL SUPPORT BETWEEN STA 1219 AND STA 1351, RBL 63.5. ACCOMPLISHED CHANNEL REPAIR I.A.W UPS EO NO: EO-94397-REQ1 REV1. 2.INSTALLED NEW WEB AND CHANNEL IAW SRM 51-40-02-0G REV. 92 AND DWG 146T5401 SH 11
- [SDR IPXA2025071120737](https://openairdocs.org/sdr/IPXA2025071120737.md): Support · broken · Jul 2, 2025 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, BROKEN FORWARD CARGO COMPARTMENT CEILING SUPPORT AT STA 610 AND RBL 64.50. COMPLETED STRAP REPAIR IAW EO NR EO-94373-REQ1 REV1.
- [SDR IPXA2025070100627](https://openairdocs.org/sdr/IPXA2025070100627.md): Floor Panel · damaged · Jul 1, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NR 231GFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK RESULT WAS NORMAL. IAW AMM 53-01-06-000-801 REV.145, REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT
- [SDR IPXA2025070100576](https://openairdocs.org/sdr/IPXA2025070100576.md): Floor Panel · damaged · Jul 1, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-90 PANEL NO.232JFF. IAW AMM 25-57-02-404-016 AND AMM 25-58-04-404-015 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2025070100773](https://openairdocs.org/sdr/IPXA2025070100773.md): Floor Panel · damaged · Jul 1, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:141T5856-13 PANEL 222DFF, IAW AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
- [SDR IPXA2025070100572](https://openairdocs.org/sdr/IPXA2025070100572.md): Floor Panel · damaged · Jul 1, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-75 PANEL NO.231CFF. IAW AMM 25-57-02-404-016, AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
- [SDR IPXA2025070100500](https://openairdocs.org/sdr/IPXA2025070100500.md): Floor Panel · damaged · Jul 1, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NO.231AFF (REPAIR) 1.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK RESULT WAS NORMAL. 2.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR P
- [SDR IPXA2025070885769](https://openairdocs.org/sdr/IPXA2025070885769.md): Angle · cracked · Jun 30, 2025 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 INBD SIDE (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
- [SDR IPXA2025070885761](https://openairdocs.org/sdr/IPXA2025070885761.md): Angle · cracked · Jun 30, 2025 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 OUTBD SIDE (REPLACE) I.A.W AMM 25-59-01-404-019 REV.145 INSTALL MAIN DECK CARGO DADO PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2025070185943](https://openairdocs.org/sdr/IPXA2025070185943.md): Floor Panel · dented · Jun 30, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT PANEL NR 232NFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK RESULT WAS NORMAL. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL SE
- [SDR IPXA2025070186019](https://openairdocs.org/sdr/IPXA2025070186019.md): Floor Panel · cracked · Jun 30, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT PANEL NR 232BFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK RESULT WAS NORMAL. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL SEALA
- [SDR IPXA2025070185937](https://openairdocs.org/sdr/IPXA2025070185937.md): Floor Panel · cracked · Jun 30, 2025 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT NR 251XFF I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK RESULT WAS NORMAL. 2.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL SEALAN
- [SDR IPXA2025031297838](https://openairdocs.org/sdr/IPXA2025031297838.md): Heater · inoperative · Mar 12, 2025 · N309UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > DURING PREFLIGHT, €ŒL SIDE WINDOW€? EICAS MESSAGE DISPLAYED. €ŒINOP€? LIGHT OBSERVED.CW ADDITIONAL 2 TORQUES OF WINDOW BOLTS REF AMM 56-11-10. VERIFIED WIRES FROM L3 WINDOW TO WINDOW CONTROL UNIT ARE GOOD. REF WDM 30-41-12. REMOVED TERMINALS J9 AND J12 FR
- [SDR IPXA2025021843128](https://openairdocs.org/sdr/IPXA2025021843128.md): Sliding Window · inoperative · Feb 3, 2025 · N309UP · Boeing 76734AF · Flight Compartment Windows
  > CAPT. WINDOW ASSY-NO. 2 OPENABLE LH (CAPT.) WINDOW ASSY NR 2 OPENABLE INSPECTED IAW AMM 56-11-02/401 REV 144. TEST SATIS.
- [SDR IPXA2025020343128](https://openairdocs.org/sdr/IPXA2025020343128.md): Window · leaking · Feb 3, 2025 · N309UP · Boeing 76734AF · Flight Compartment Windows
  > CAPT. WINDOW ASSY-NO. 2 OPENABLE CAPTAIN WINDOW ASSY-NO.2 OPENABLE STILL HAS MOISTURE INGRESS/HAZING AFTER PERFORMING METHOD 2 (ALTERNATIVE) PER AMM 57-11-00-216-016
- [SDR IPXA2024082151039](https://openairdocs.org/sdr/IPXA2024082151039.md): Window · damaged · Aug 20, 2024 · N309UP · Boeing 76734AF · Flight Compartment Windows
  > WINDOW R2 IS OPAQUE. DIFFICULT TO VIEW AT NIGHT. ESPECIALLY ON THE GROUND. AIR TRAFFIC HARD TO SEE AS WELL. R&R R2 WINDOW IAW AMM 56-11-02-404-026. OPS CHECK AND LEAK CHECK GOOD.
- [SDR IPXA2024081357668](https://openairdocs.org/sdr/IPXA2024081357668.md): Control Panel · faulted · Aug 8, 2024 · N309UP · Boeing 76734AF · Cabin Pressure Control System
  > *** EMERGENCY DECLARED *** SUPPLEMENTAL SDR *** FL 370 CABIN ALT EICAS MESSAGE MODE SELECT WAS AUTO 2 WITH BOTH PACKS IN AUTO. CABINDIFFERENTIAL WAS APPROXIMATELY 6PSI AND CABIN ALTITUDE INDICATED 11,00-12000 FEET (SEE PHOTO FOR REMAINING WRITE-UP) PERFORMED F
- [SDR IPXA2024080857668](https://openairdocs.org/sdr/IPXA2024080857668.md): Outflow Valve · faulted · Aug 8, 2024 · N309UP · Boeing 76734AF · Pressure Regulator/Outflow Valve
  > *** EMERGENCY DECLARED *** SDR FILED OPEN *** FL 370 CABIN ALT EICAS MESSAGE MODE SELECT WAS AUTO 2 WITH BOTH PACKS IN AUTO. CABINDIFFERENTIAL WAS APPROXIMATELY 6PSI AND CABIN ALTITUDE INDICATED 11,00-12000 FEET (SEE PHOTO FOR REMAINING WRITE-UP) PERFORMED FIM
- [SDR IPXA2024080969072](https://openairdocs.org/sdr/IPXA2024080969072.md): Pawl · worn · Aug 8, 2024 · N309UP · Boeing 76734AF · Passenger/Crew Doors
  > L FWD ENTRY DOOR WON€™T LATCH. FOUND EXTERIOR DOOR HANDLE CLOSING PAWL WORN, REPLACED SAME USING 20-11-00 AND 52-12-00 DOOR CLOSES NORMALLY AND ALL DOOR WARNINGS OUT
- [SDR IPXA2024040774919](https://openairdocs.org/sdr/IPXA2024040774919.md): Skin · damaged · Apr 6, 2024 · N309UP · Boeing 76734AF · Leading Edge Devices
  > L/E SKIN DAMAGE AT #1 SLAT O/B CURTAIN SEAL SCREW HOLES-L/E SKIN DAMAGE AT #1 SLAT O/B CURTAIN SEAL SCREW HOLES. DAMAGE TO UPPER SKIN CONSISTING ON 4 GOUGES, 2 ELONGATED SCREW HOLES, AND ONE PUNCTURE. 6. REPAIRED DAMAGED SECTION OF LEADING EDGE AND ELONGATED
- [SDR IPXA2023082060594](https://openairdocs.org/sdr/IPXA2023082060594.md): Control Panel · unknown · Aug 20, 2023 · N309UP · Boeing 76734AF · Cabin Pressure Control System
  > CAB ALT AUTO1 STS MSG REF FIM 21-31 TASK 801, 21-31 TASK 809 AND 21-31 FAULT TREE 803 CANBIN PRESSURE CONTROLLER BITE PROCEDURE. FOUND THE "SELECTOR" FAULT LT ON. REPLACED THE CABIN PRESSURE SELECTOR PANEL AND TEST OK, PER AMM 21-31-01-401. MEL CLOSED AND P
- [SDR IPXA2023071004096](https://openairdocs.org/sdr/IPXA2023071004096.md): Battery · expired · Jul 4, 2023 · N309UP · Boeing 76734AF · Emergency Lighting
  > FAULT - FOUND BATTERY PACK EXPIRY DATE JUN 30 (REPLACE) ++ I.A.W AMM 33-51-07-422-012 REV 139 PERFORMED BATTERY PACK TEST, RESULT WAS SATISFACTORY. REVIEW COMPLETE
- [SDR IPXA2022120788797](https://openairdocs.org/sdr/IPXA2022120788797.md): Shutoff Valve · faulted · Dec 7, 2022 · N309UP · Boeing 76734AF · Cabin Cooling System
  > EICAS MESSAGE FWD EQPT VAL LIGHT ILLUMINATED ON CLIMB OUT. RAN QRH PROCEDURE EQUIPMENT VALVE SELECTOR TO STBY LIGHT EXTINGUISHED. R&R FDAR SHUTOFF VALVE PER MM 21 58 43 401 OPS CHECK GOOD ESR 21 22 52 04A
- [SDR IPXA2022111488114](https://openairdocs.org/sdr/IPXA2022111488114.md): Floor Panel · damaged · Nov 13, 2022 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO POS 11 CENTER FLOOR PANEL REPAIRFLOOR BOARD POS 11 CENTERLINE ROUTED TO SHEET METAL FOR REPAIR, REF AMM 25-58-1. [JPC 1984163 11-12-22] THIS IS A MAJOR REPAIR. TRANSFERED TO NRC #684232 FOR REPAIR. [CS 1195530 11-12-22] COMPLETED AND CLEARED NON-ROU
- [SDR IPXA2021062670984](https://openairdocs.org/sdr/IPXA2021062670984.md): Battery Pack · failed · Jun 26, 2021 · N309UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:C13CREW REST MODULE(STC ST02568SE) - EMERGENCY LIGHT BATTERY PACK FAILED. REPLACED EMERGENCY LIGHT BATTERY PACK AND PERFORMED BATTERY PACK TEST, RESULT WAS SATISFACTORY IAW B767-2520-65582-H.
- [SDR IPXA2021062670972](https://openairdocs.org/sdr/IPXA2021062670972.md): Tee Fitting · corroded · Jun 17, 2021 · N309UP · Boeing 76734AF · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C13CORROSION WAS FOUND ON 2EA SPLICE TEES (P/N:145T8629-3) OF FAIRING INSTL, KEEL BEAM NEAR STA 917, STA 962 BETWEEN RBL 10 - LBL 10.INSTALL NEW PART I.A.W. BOEING DWG 145T8629 SH 2, REV "A" AND 767-300F SRM 51-40-02 REV.80.03.
- [SDR IPXA2021062670976](https://openairdocs.org/sdr/IPXA2021062670976.md): Tee Fitting · corroded · Jun 17, 2021 · N309UP · Boeing 76734AF · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C13CORROSION WAS FOUND ON SPLICE TEE(P/N: 145T8629-2) OF FAIRING INSTL, KEEL BEAM NEAR STA 872, BETWEEN RBL 10 - LBL 10.INSTALL NEW PART I.A.W. BOEING DWG 145T8629 SH 1, REV "B" AND 767-300F SRM 51-40-02 REV.80.03.
- [SDR IPXA2021062770996](https://openairdocs.org/sdr/IPXA2021062770996.md): Seat Track · corroded · Jun 14, 2021 · N309UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C13CORROSION ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 434 AND STA 654, RBL 88.5REPAIR I.A.W. BOEING SR: 4-5138071445 AND UPS EO B767-5310-80813-A
- [SDR IPXA2021012965044](https://openairdocs.org/sdr/IPXA2021012965044.md): Light · loose · Jan 29, 2021 · N309UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE: NA O/H EMERGENCY LIGHT SW GUARD SPRING IS LOOSE. REMOVED & REPLACED EMERGENCY LIGHT PANEL. THEN EMERGENCY LIGHT FUNCTION CHECK SATISFIED. ALSO GUARD FUNCTION SATISFIED AMM 33-51-08-01 AIPC 31-12-11-51A ITEM 015.
- [SDR IPXA2020081438999](https://openairdocs.org/sdr/IPXA2020081438999.md): Switch Panel · inoperative · Aug 11, 2020 · N309UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/AEMERG EXIT LIGHT WILL NOT DISARM.R&R EMERGENCY LIGHT SWITCH PANEL OPS CHK OK REF. AMM 33-51-08.
- [SDR IPXA2019103048466](https://openairdocs.org/sdr/IPXA2019103048466.md): Pneumatic System · inoperative · Oct 29, 2019 · N309UP · Boeing 76734AF · APU Bleed Air System
  > INSPECTION TYPE:N/AAFTER INITIAL APU START, APU WOULD NOT SUPPLY PNEUMATIC AIR, APU OPERATION NORMAL AFTER SHUTDOWN & RESTARTED IAW AOM PROCEDURE.ACCOMPLISHED APU BITE PER FRMFIM 49-11-00-815-803. NO FAULTS NOTED, OK FOR FLIGHT.
- [SDR IPXA2019062103530](https://openairdocs.org/sdr/IPXA2019062103530.md): Floor Panel · damaged · Jun 13, 2019 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE: C12, DAMAGE ON M/D CARGO FLOOR PANEL 232FFF AT BS 533 - 654 +22, RBL 11 - RBL 33, FABRICATED A REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA201906213529](https://openairdocs.org/sdr/IPXA201906213529.md): Filler · damaged · Jun 11, 2019 · N309UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE: C12, BURN DAMAGE ON FILLER AND DOUBLER OF FWD UPR SPAR WEB ON #1 PYLON NEAR NAC STA 228.19.REPAIR IAW SRID: 4-4504150598 AND EO B767-5410-72969-A.
- [SDR IPXA2019061943475](https://openairdocs.org/sdr/IPXA2019061943475.md): Stiffener · cracked · Jun 10, 2019 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12, CRACK ON THE CENTER WING FRONT SPAR STIFFENER. UPPER SIDE AT STA 785.9, RBL55. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV.74.00 AND EO B767-5740-58151-.
- [SDR IPXA2019062104531](https://openairdocs.org/sdr/IPXA2019062104531.md): Floor Panel · damaged · Jun 9, 2019 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > DAMAGE ON M/D CARGO FLOOR PANEL 231FFF AT STA 533 - STA 654 PLUS 22, RBL 11 - LBL 11,.FABRICATED A REPLACEMENT FLOOR PANEL PER EO B767-5320-9693-I.
- [SDR IPXA2018092654401](https://openairdocs.org/sdr/IPXA2018092654401.md): Skin · punctured · Sep 24, 2018 · N309UP · Boeing 76734AF · Elevator, Plate/Skin
  > LEFT INBD ELEVATOR UPPER SURFACE HAD A PUNCTURE, 21.75 INCHES FROM T/E AND 13 INCHES FROM THE INBD END, ELEVATOR STATION 61. REPAIRED THE SKIN IAW SRM 51-70-17-0G, PARA 4B, AND SRM 55-20-01-2R-1, REPAIR 1. MAJOR.
- [SDR IPXA2016101909605](https://openairdocs.org/sdr/IPXA2016101909605.md): Warning System · false activation · Oct 18, 2016 · N309UP · Boeing 76734AF · Airspeed/Mach Indicator
  > INSPECTION TYPE:N/A, EMERGENCY DECLARED, RECEIVED IAS DISAGREE EICAS MSG. THEN RECEIVED AILERON LOCKOUT, EEC, RUDDER RATIO, ETC EICAS MSG. ACCOMPLISHED FIM 34-12-00-815-804 FIG 104 STEPS 1 &22 & FIM 34-11-00-815-806 FIG 104 STEPS 1,2, 25. NO LEAKS, OBSTRUCT
- [SDR IPXA2016032301151](https://openairdocs.org/sdr/IPXA2016032301151.md): Charger · inoperative · Mar 23, 2016 · N309UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COME ON INTERMITTENTLY WITH SWITCH IN ARMED POSITION. LIGHTS GO OUT WITH SWITCH OFF, REPLACED CHARGER ASSY AND TEST OK, IAW AMM 33-51-04, PN:2012-1. SN ON/OFF:10174/39205.
- [SDR IPXA2015063090668](https://openairdocs.org/sdr/IPXA2015063090668.md): Stiffener · cracked · Jun 18, 2015 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID 4-2928737651 AND EO: B767-5710-57865-A.
- [SDR IPXA2015063090667](https://openairdocs.org/sdr/IPXA2015063090667.md): Stiffener · cracked · Jun 18, 2015 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID: 4-2928737651 AND EO: B767-5710-57865-A.
- [SDR IPXA2015063090666](https://openairdocs.org/sdr/IPXA2015063090666.md): Stiffener · cracked · Jun 18, 2015 · N309UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID: 4-2928737651 AND EO: B767-5710-57865-A.
- [SDR IPXA2015063090665](https://openairdocs.org/sdr/IPXA2015063090665.md): Stringer · damaged · Jun 17, 2015 · N309UP · Boeing 76734AF · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C10, CRACK DAMAGE ON LT SIDE FUSELAGE STRINGER S-20L AT BS 1511 AND BS 1518. REPAIR IAW SR 4-2916528521.
- [SDR IPXA2015020985625](https://openairdocs.org/sdr/IPXA2015020985625.md): Floor Panel · damaged · Feb 9, 2015 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > DAMAGED FLOOR PANEL MAIN DECK, PN 145T5876-82 FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H & EOB767-5320-56659.
- [SDR IPXA2014071483580](https://openairdocs.org/sdr/IPXA2014071483580.md): Control Unit · malfunctioned · Jul 10, 2014 · N309UP · Boeing 76734AF · Brake Anti-Skid Section
  > ANTI-SKID EICAS AND LIGHT ILLUMINATED AT TOP OF CLIMB, FL 390. ALTN ANTI-SKID FAULT MESSAGE ALSO DISPLAYED. LIGHT AND EICAS EXTINGUISHED AFTER 25 MINUTES, ACFT DIVERTED. PERFORMED BITE CHECK IAW FIM 32-42-00. FOUND MESSAGE BOX 4-8. R & R ANTI-SKID AUTO-
- [SDR IPXA3678780](https://openairdocs.org/sdr/IPXA3678780.md): Floor Panel · dented · Jun 3, 2013 · N309UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C09, DENT ON MAIN DECK CARGO FLOOR PANEL 232AFF AT BS 493, RBL 30. DIMENSIONS OF DAMAGE:1.5"L X 1.0" W. REPAIR IAW EO NR B767-5320-9693-H.

Next page: https://openairdocs.org/aircraft/N309UP/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 = 'N309UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N309UP/reports

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