# Service difficulty reports: N310UP

A list on [N310UP](https://openairdocs.org/aircraft/N310UP.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 · 169 reports

- [SDR IPXA2026072859394](https://openairdocs.org/sdr/IPXA2026072859394.md): Unknown · odor · Jul 25, 2026 · N310UP · Boeing 76734AF · Air Distribution System
  > ON DEPARTURE @ HIGH POWER SETTINGS STRONG SMELL OF DIRTY SOCKS? ON THE FLIGHT DECK. STAY UNTIL PASSING 10000 COULD NOT DUPLICATE PROBLEM UNPIN ARRIVAL. T/S PER FIM 21-00-00 NO EVIDENCE OF LEAKS. VERIFIED RAM AIR INLET IS CLEAR.
- [SDR IPXA2026070679800](https://openairdocs.org/sdr/IPXA2026070679800.md): Skin · dented · Jun 3, 2026 · N310UP · Boeing 76734AF · Leading Edge Devices
  > DENT ON LEADING EDGE SLAT #7. VIEW ATTACHMENTS. WILL REQUIRE LINE MX 8 HOURS EXTEND AND LOTO L/E SLATS. S/M SHOP 40 HOURS TO REPAIR PER SRM 57-43-01-2R-2 RP. 2 THIS IS PRIMARY STRUCTURE MAJOR REPAIR. HANGAR NOT REQUIRED WITH GOOD WEATHER AND MATERIALS IN STOCK
- [SDR IPXA2026040628817](https://openairdocs.org/sdr/IPXA2026040628817.md): A/C Pack · odor · Apr 3, 2026 · N310UP · Boeing 76734AF · Cabin Cooling System
  > ON TAKEOFF A PUNGENT SMELL ENTERD THE FLIGHT DECK. AFTER POWER REDUCTION, TURNED THE LEFT PACK OFF AND SMELL DISSAPATED. OPERATED L/H PACK SYSTEM FOR 30 MINUTES. NO ODOR NOTED. OPS CHECKS GOOD PER AMM 21-00-21-102-030.
- [SDR IPXA2025092255412](https://openairdocs.org/sdr/IPXA2025092255412.md): Unknown · odor · Sep 20, 2025 · N310UP · Boeing 76734AF · Air Distribution System
  > ON DEPARTURE AT HIGH POWER SETTING STRONG SMELL OF DIRTY SOCK.SMELL DISSUPTED APPROX 10000FT. ++PERFORMED OPS CHECKS IAW FIM 21-00 TASK SUPPORT - AIR CONDITIONING SYSTEM OIL SMOKE/FUME CONTAMINATION. NO DEFECTS NOTED
- [SDR IPXA2025072727420](https://openairdocs.org/sdr/IPXA2025072727420.md): Skin Panel · gouged · Jul 8, 2025 · N310UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > GROUND CREW REPORTS GOUGE ON DOUBLER OF PREVIOUSLY REPAIRED AREA OF DAMAGE ON THE LOWER FORWARD CARGO DOOR FRAME. FUSELAGE STATION 478, WL 121. INSTALLED LINER ON RIGHT SIDE FWD CARGO COMPARTMENT REF AMM 25-52-01.
- [SDR IPXA2025020201790](https://openairdocs.org/sdr/IPXA2025020201790.md): Rib · cracked · Jan 21, 2025 · N310UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > L/H WING OUTBD L/E UPPER RIB LOWER CHORD, OSS 531.71 (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 91. AND BOEING DWG NO. 114T2206 SH. 1 REV. B. JOB COMPLETED.
- [SDR IPXA2025020593203](https://openairdocs.org/sdr/IPXA2025020593203.md): Strap · corroded · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - A LOT OF SCREW HOLES OF CEILING SUPPORT CORROSION AT FWD CGO BETWEEN STA 478 TO STA 610, RBL 40 (REPLACE) 1.ACCOMPLISHED REPAIR I.A.W UPS EO-92566-REQ1 REV.1 2.INSTALL FABRICATED PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO:453T1001 SH1 REV.A,45
- [SDR IPXA2025020591355](https://openairdocs.org/sdr/IPXA2025020591355.md): Support · corroded · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CORROSION - FOUND FWD CGO PNL SUPPORT CORROSION AT STA 654+110 ~ 654+121, RBL 70 (REPAIR) 1. REMOVED AFFECTED FASTENERS TO GET ACCESS I.A.W SRM 51-40-02-0G REV. 91. 2. REPAIR DAMAGE AREA I.A.W SRM 51-70-12-0G-O DETAIL X REV. 91 AND EGAT WORK SHEET NO.5
- [SDR IPXA2025020693211](https://openairdocs.org/sdr/IPXA2025020693211.md): Channel · corroded · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CORROSION - FND AFT CGO RH CEILING PNL SUPPORT CORROSION BETWEEN STA 1197+132 TO STA 1351, RBL 63 (REPLACE) ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92666-REQ1 REV.1. JOB COMPLETED. REVIEWED.
- [SDR IPXA2025020593206](https://openairdocs.org/sdr/IPXA2025020593206.md): Strap · cracked · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CEILING SUPPORT CRACK AT FWD CGO STA 610, RBL 64 (REPLACE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92665-REQ1 REV.1. JOB COMPLETED. REVIEWED.
- [SDR IPXA2025020290828](https://openairdocs.org/sdr/IPXA2025020290828.md): Tee Fitting · cracked · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > TEE CHORD AT STA 246 LBL 40 (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92600-REQ1 REV.1. JOB COMPLETED. ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92666-REQ1 REV.1. OSD: 2/4/2025
- [SDR IPXA2025012193764](https://openairdocs.org/sdr/IPXA2025012193764.md): None · none · Jan 20, 2025 · N310UP · Boeing 76734AF · Standard Practices/Structures
  > (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). COMPLIED WITH EO-82173. CONDITION CHECK OK.
- [SDR IPXA2025012691492](https://openairdocs.org/sdr/IPXA2025012691492.md): Latch · corroded · Jan 20, 2025 · N310UP · Boeing 76734AF · Fuselage Main, Keel
  > FAULT - CORROSION - LATCH, KEEL BEAM ACCESS PNL NO.149BL AFT LATCH INNER FACE. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 91. AND BOEING DWG NO. 145T8629 SH. 3 REV. C.
- [SDR IPXA2025011969709](https://openairdocs.org/sdr/IPXA2025011969709.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-83 PANEL NO: 231GFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018 AND AM
- [SDR IPXA2025011969781](https://openairdocs.org/sdr/IPXA2025011969781.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-81 PANEL NO: 231HFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018, AMM 2
- [SDR IPXA2025011969787](https://openairdocs.org/sdr/IPXA2025011969787.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-78 PANEL NO: 231AFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018, AMM 2
- [SDR IPXA2025011969801](https://openairdocs.org/sdr/IPXA2025011969801.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-84 PANEL NO: 232FFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018 AND AM
- [SDR IPXA2025011966777](https://openairdocs.org/sdr/IPXA2025011966777.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-19 PANEL NO: 232OFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 2
- [SDR IPXA2025011969803](https://openairdocs.org/sdr/IPXA2025011969803.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-77 PANEL NO: 231BFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHECK IS SATISFACTORY. 3.ATTACHMENT ARE UPLOAD. I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018, AMM 2
- [SDR IPXA2025012169709](https://openairdocs.org/sdr/IPXA2025012169709.md): Floor Panel · damaged · Jan 18, 2025 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-83 PANEL NO: 231GFF (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK.<BR> P/N:143T5876-83, PANEL NO. 231GFF OPEN
- [SDR IPXA2024121869082](https://openairdocs.org/sdr/IPXA2024121869082.md): Fmc · failed · Dec 18, 2024 · N310UP · Boeing 76734AF · Flight Management Computing Hardware System
  > *AIR TURN BACK* ATB LFMC FAIL QRH PROCEDURE COMPLETE BOTH ND DISPLAYS BLANKED, R FMC UNABLE TO LOAD NAV DATA, QRH BOTH FCM FAIL PROCEDURE. NO ACCESS TO ANY ROUTE DATA ONLY ACARS AVAILABLE VIA NOTH CDUS. R&R LH AND RH FMC'S PER AMM 34-61-01. UPLOADED ALL SOFTWA
- [SDR IPXA2024060320163](https://openairdocs.org/sdr/IPXA2024060320163.md): Window · scratched · May 30, 2024 · N310UP · Boeing 76734AF · Flight Compartment Windows
  > **SUPPLEMENTAL SDR** PILOT SIDE WINDOW HAS TOO MANY SCRATCHES. VERY HARD TO SEE OUT OF IT WHEN SUN HITS IT. OS VISION. REMOVED AND REPLACED L2 WINDOW IAW AMM 56-11-02. OPS AND LEAK CHECK GOOD.
- [SDR IPXA2024053120163](https://openairdocs.org/sdr/IPXA2024053120163.md): Window · scratched · May 30, 2024 · N310UP · Boeing 76734AF · Flight Compartment Windows
  > **SDR FILED OPEN** PILOT SIDE WINDOW HAS TOO MANY SCRATCHES. VERY HARD TO SEE OUT OF IT WHEN SUN HITS IT. OS VISION.
- [SDR IPXA2024032667475](https://openairdocs.org/sdr/IPXA2024032667475.md): Unknown · leaking · Mar 26, 2024 · N310UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > FUEL LEAKING FROM LEFT ENGINE ACCOMPLISHED LEFT ENGINE RUN AT IDLE (CREW RAN IT) AS PER B767 71-00-00 TEST NO.3 IDLE LEAK CHECK AND CHECKED DRAINS PER B767 AMM 71-71-00. NO LEAKS NOTED
- [SDR IPXA2023021290912](https://openairdocs.org/sdr/IPXA2023021290912.md): Battery · no test · Feb 10, 2023 · N310UP · Boeing 76734AF · Lighting System
  > INSPECTION TYPE:C14FOUND EMERGENCY LIGHT POWER SUPPLY DEEP CYCLING TEST FAIL.1.I.A.W AMM 33-51-07-022-001 AND 33-51-07-422-012 REV.138.01 REPLACED EMERGENCY LIGHT POWER SUPPLY AT COCKPIT. 2.I.A.W AMM 33-51-07-422-012 REV.138.01 PERFORMED BATTERY PACK TEST,RESU
- [SDR IPXA2023021090850](https://openairdocs.org/sdr/IPXA2023021090850.md): Skin · cracked · Feb 9, 2023 · N310UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C14*MAJOR REPAIR* CRACK WAS FOUND ON RH SKIN(P/N:148T3121-2)AT STA 1725.5,S-7R.REPAIR I.A.W 767-300F SRM 53-80-01 REPAIR 5,DETAIL III,REV.85.01
- [SDR IPXA2023020490595](https://openairdocs.org/sdr/IPXA2023020490595.md): Angle · cracked · Jan 31, 2023 · N310UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C14CRACK ON ANGLE(P/N:146T5651-6)OF CANTILEVER INSTL IN BULK CARGO COMPARTMENT AT STA 1578,RBL 60.REPLACE THE PART PER 767-300F SRM 51-40-02-0G,REV.85.01.
- [SDR IPXA2023020490594](https://openairdocs.org/sdr/IPXA2023020490594.md): Angle · cracked · Jan 31, 2023 · N310UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C14CRACK ON ANGLE(P/N:146T5651-5)OF CANTILEVER INSTL IN BULK CARGO COMPARTMENT AT STA 1578,LBL 60.REPLACE THE PART PER 767-300F SRM 51-40-02-0G,REV.85.01
- [SDR IPXA2023020790724](https://openairdocs.org/sdr/IPXA2023020790724.md): Skin · cracked · Jan 30, 2023 · N310UP · Boeing 76734AF · Wing Structure
  > INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N: 114T4104-4) OF NO. 9 SLAT AT OSS 572.55REPAIR I.A.W. 767-300F SRM 57-43-01-2R-2 REV.85.01.
- [SDR IPXA2023020690650](https://openairdocs.org/sdr/IPXA2023020690650.md): Not Reported · damaged · Jan 30, 2023 · N310UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C14DAMAGE ON M/D CGO FLOOR BEAM SUPPORT AT STA 246,LBL 40.REPLACE PART I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG NO.141T5600SHEET 2,REV''E''
- [SDR IPXA2022101287098](https://openairdocs.org/sdr/IPXA2022101287098.md): Indicator · inoperative · Oct 12, 2022 · N310UP · Boeing 76734AF · Fuel Quantity Indicator
  > **ATB**-SUSPECT L MAIN FUEL INDICATOR GIVING INACCURATE INDICATIONS. POSSIBLE FUEL LEAK. NO FUEL LEAK DETECTED. DEFERRED RH FUEL QTY INDICATION INOP PER MEL 28-41-1-1A. R & R RT MAIN TANK DENSITOMETER IAW AMM 28-41-03-401-2. OPS CHECK GOOD IAW AMM 28-41-00-71
- [SDR IPXA2022012678291](https://openairdocs.org/sdr/IPXA2022012678291.md): None · none · Jan 25, 2022 · N310UP · Boeing 76734AF · Fuel Quantity Indicator
  > INSPECTION TYPE:NASUPPLEMENATAL ATB SDR FILED * NO EMERG DEC'D* CRUISE, FUEL CONFIG LIGHT/INDICATIONS & DROPPING FUEL QTY IN R MN TANK. FUEL QTY FLUCTUATED, THEN RETURN NRML. DEFERRED R/H MN TANK FUEL QTY IND SYS IAW MEL 28-41-1-1A. ASSIGNED CONTROL # M770895
- [SDR IPXA2021122977388](https://openairdocs.org/sdr/IPXA2021122977388.md): None · none · Dec 29, 2021 · N310UP · Boeing 76734AF · Fuel Quantity Indicator
  > INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** DIVERSION ** IFSD** FL 370 GOT FUEL CONFIG EICAS RIGHT ENG FUEL QUANTITY DROPPING L12.5 R 6.5 ALSO GOT FUEL DISAGREE ON PROG PAGE 2 ON FMC. CREW SHUTDOWN #2 ENGINE. RAN FUEL LEAK CHECKLIST NON NORMAL.C/W FIM 28-41-00-8
- [SDR IPXA2021021665720](https://openairdocs.org/sdr/IPXA2021021665720.md): Stiffener · cracked · Feb 3, 2021 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C13CRACK 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.79.01 AND UPS EO B767-5740-58151-C
- [SDR IPXA2021021665719](https://openairdocs.org/sdr/IPXA2021021665719.md): Stiffener · cracked · Feb 3, 2021 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-8) ON STA 785.9,RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C
- [SDR IPXA2019122450353](https://openairdocs.org/sdr/IPXA2019122450353.md): Circuit Card · malfunctioned · Dec 21, 2019 · N310UP · Boeing 76734AF · Door Warning System
  > FWD CARGO DOOR EICAS AND LT ILLUM AFTER TAKEOFF AT APPROX 4000 FT AGL, COMPLETED QRN PROD. RETURNED TO DEPARTURE AIRPORTT/S AND FOUND CODE "006" ON PSEU BITE CK. R/R CARD #6 W/REF TO AMM 32-09-06. OPS CK IAW AMM 32-09-06-704-011. OPS CK OK.
- [SDR IPXA2019020438590](https://openairdocs.org/sdr/IPXA2019020438590.md): Stiffener · cracked · Jan 26, 2019 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER(P/N:111T2008-12) UPPER SIDE AT STA 785.9, RBL 33.REPAIR I.A.W. 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 73.01 AND UPS EO B767-5740-58151-A.
- [SDR IPXA2018090733665](https://openairdocs.org/sdr/IPXA2018090733665.md): Valve · defective · Sep 5, 2018 · N310UP · Boeing 76734AF · Brake
  > WHEN PARKING BRAKE WAS SET, WITH BRAKE LIGHT ON AND WHITE PARKING BRAKE LIGHT ON, ACFT ROLLED FWD 1 1/2 FEET. RESET BRAKE AND IT SELF RELEASED 3 TIMES. REMOVED OLD VALVE AND REPLACED WITH NEW SERVICEABLE UNIT REF AMM 32-44-04. OPS CHECKS REF AMM 32-44-00-735-0
- [SDR IPXA2018032927976](https://openairdocs.org/sdr/IPXA2018032927976.md): Acoustic Liner · punctured · Mar 29, 2018 · N310UP · Boeing 76734AF · Turbine Engine Compressor Section
  > RIGHT ENGINE HAS SMALL HOLE IN FWD FAN CASE LINER ON PANEL 5,M APPROXIMATELY 8 INCHES FROM LOWER EDGE AND 15/16 INCH AFT PANEL EDGE 11/16 INCH LONGX 5/16 TALL. R & R THE ACOUSTIC LINER SEGMENT IAW MM 72-33-01-4.
- [SDR IPXA2018010425113](https://openairdocs.org/sdr/IPXA2018010425113.md): Panel · inflt separation · Jan 3, 2018 · N310UP · Boeing 76734AF · Airfoil Anti/De-ice System
  > L/E THERMAL ANTI-ICE PANEL MISSING FROM RT WING NR 10 SLAT, THE PANEL 624AT DEPARTED THE ACFT. REPLACED L/E ANTI-ICE PANEL IAW AMM 57-41-01-404-003, CHECKED OK, OK FOR SERVICE.
- [SDR IPXA2017080620164](https://openairdocs.org/sdr/IPXA2017080620164.md): Rib · debonded · Aug 5, 2017 · N310UP · Boeing 76734AF · Engine Thrust Reverser
  > NR 2 ENGINE RT THRUST REVERSER INNER BARREL ZEE RIB DISBONDED, THIRD INNER BARREL FRAME. COMPLIED WITH EO B767-78-30-65175-A.
- [SDR IPXA2017031415103](https://openairdocs.org/sdr/IPXA2017031415103.md): Roller Tray · corroded · Mar 9, 2017 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE: C11, CORROSION ON AFT CARGO ROLLER TRAY AT BS 1197 + 44 TO 1197 + 132, RBL 6.5. REPLACED THE ROLLER TRAY.
- [SDR IPXA2017031415102](https://openairdocs.org/sdr/IPXA2017031415102.md): Roller Tray · corroded · Mar 9, 2017 · N310UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE: C11, CORROSION ON AFTER CARGO ROLLER TRAY AT BS 1197 + 44 TO 1197 + 132, RBL 20. REPLACED THE ROLLER TRAY.
- [SDR IPXA2017031415106](https://openairdocs.org/sdr/IPXA2017031415106.md): Bulkhead · corroded · Mar 7, 2017 · N310UP · Boeing 76734AF · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C11, CORROSION ON PRESSURE BULKHEAD CENTER UPPER SIDE AT BS 1809, BL 0. REPAIRED THE BULKHEAD.
- [SDR IPXA2017031415105](https://openairdocs.org/sdr/IPXA2017031415105.md): Splice · corroded · Mar 7, 2017 · N310UP · Boeing 76734AF · Fuselage Main, Keel
  > INSPECTION TYPE: C11, CORROSION ON KEEL BEAM SPLICE TEE AT BS 916, BL 0. THE SPLICE WAS REPLACED.
- [SDR IPXA2017031415104](https://openairdocs.org/sdr/IPXA2017031415104.md): Splice · corroded · Mar 7, 2017 · N310UP · Boeing 76734AF · Fuselage Main, Keel
  > INSPECTION TYPE: C11, CORROSION ON THE FUSELAGE KEEL BEAM SPLICE TEE, BS 962, BL 0. REPLACED THE KEEL. SPLICE TEE
- [SDR IPXA2017031315037](https://openairdocs.org/sdr/IPXA2017031315037.md): Panel · corroded · Mar 7, 2017 · N310UP · Boeing 76734AF · Fuselage Main, Keel
  > INSPECTION TYPE: C11, CORROSION ON FUSELAGE KEEL BEAM PANEL 149BL NEAR BS 1013, LBL 6. PART REPLACED
- [SDR IPXA2017031515161](https://openairdocs.org/sdr/IPXA2017031515161.md): Channel · corroded · Mar 5, 2017 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C11, CORROSION ON MOP SILL OF MAIN DECK CARGO FLOOR BS 1605, LBL 54. REPLACED THE MOP SILL.
- [SDR IPXA2017031515160](https://openairdocs.org/sdr/IPXA2017031515160.md): Floor Support · corroded · Mar 5, 2017 · N310UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C11, CORROSION ON THE FLOOR SUPPORT OF MAIN DECK CAGRO BS 1605, LBL 54. REPLACED THE FLOOR SUPPORT.
- [SDR IPXA2016061704751](https://openairdocs.org/sdr/IPXA2016061704751.md): Warning System · false activation · Jun 17, 2016 · N310UP · Boeing 76734AF · Brake Anti-Skid Section
  > EMERGENCY DECLARED ON APPROACH. ANTI-SKID LIGHT ON APPROACH, RAN CHECKLIST. DEFERRED ANTI-SKID SYSTEM IAW MEL 32-42-1-0-1 AND C/W CMP-32-42-1-0-1, INSTALLED CIRCUIT BREAKER COLLARS AND PLACARDS. PERFORMED BITE PER FIM 32-42-00-815-811 NO FAULTS FOUND

Next page: https://openairdocs.org/aircraft/N310UP/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 = 'N310UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N310UP/reports

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