# Service difficulty reports: N303UP

A list on [N303UP](https://openairdocs.org/aircraft/N303UP.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 · 190 reports

- [SDR IPXA2026101325515](https://openairdocs.org/sdr/IPXA2026101325515.md): Controller · faulted · Oct 13, 2026 · N303UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > FO`S R2 WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED LT FWD AND RT SIDE WINDOW HEAT CONTROLLER UNIT (M191) IAW AMM 30-41-01/401. BITE TEST PASSED IAW B767 AMM 30-41-01-404-007. REVERSED DMP, AND REMOVED PLACARD.
- [SDR IPXA2026092308451](https://openairdocs.org/sdr/IPXA2026092308451.md): Skin · ground damage · Sep 18, 2026 · N303UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, CAN BLEW OFF THE K LOADER DUE TO JET BLAST IS UNDER BELLY OF AIRCRAFT LT SIDE STATION 698-720 STRINGER S39-S36 FABRICATED FREEZE PLUG PER STEP 10 OF EO-98676-PRELIM2. SKIN REPAIR COMPLETED PER EO-98676-REQ1.
- [SDR IPXA2026032629120](https://openairdocs.org/sdr/IPXA2026032629120.md): Bracket · broken · Mar 18, 2026 · N303UP · Boeing 76734AF · Wing Main, Frame Structure
  > BROKEN BRACKET, LT WING NR 5 SLAT OTBD SIDE SEAL DOOR AREA. IAW AMM 57-41-50-004-001, REV 147, REPLACED THE BRACKET.
- [SDR IPXA2026032032584](https://openairdocs.org/sdr/IPXA2026032032584.md): Floor Support · cracked · Mar 18, 2026 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, MAIN DECK CARGO, BS 1043, RBL 9. ACCOMPLISHED THE REPAIR IAW EO-96900-REQ1, REV 1, & EGAT EI F2026A53M-563, REV 2.
- [SDR IPXA2026032611084](https://openairdocs.org/sdr/IPXA2026032611084.md): Pan · broken · Mar 17, 2026 · N303UP · Boeing 76734AF · Leading Edge Devices
  > BROKEN- PAN, R/H WING L/E NO.7 SLAT OUTBD. (REPLACE). INSTALL PART I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO: 114T3200 SH 3 REV: A. I.A.W PL 114T3200 REV. W DWG 114T3200 SHEET 3 REV. A & AMM 20-11-00-910-802 REV. 147 TO INSTALL THE SEAL PAN PN: 114T3187
- [SDR IPXA2026032793526](https://openairdocs.org/sdr/IPXA2026032793526.md): Strap · corroded · Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND FORWARD CARGO SIDEWALL, CEILING PANEL SUPPORT STRAP ASSY TOTAL: 3 AREA AT BS 674, BS 654+66, BS 632 - 654 LT. CHECK OK. ACCOMPLISHED THE REPAIR IAW EO-96926-REQ 1, REV 1, AND EGAT EI F2026A53M-557.
- [SDR IPXA2026032693515](https://openairdocs.org/sdr/IPXA2026032693515.md): Seal Depressor · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Cargo/Baggage Doors
  > CRACKED SEAL DEPRESSOR, FWD CARGO DOOR CUTOUT AFT EDGE. REMOVED DAMAGED DEPRESSOR IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW DEPRESSOR IAW SRM 51-40-02-0G, REV 94, AND DWG 143T8540, SH 1, REV B.
- [SDR IPXA2026032693506](https://openairdocs.org/sdr/IPXA2026032693506.md): Strut · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED STRUT, LT WING OTBD L/E CAVITY, INNER RIB LWR STRUT, NEAR OSS 531, ACCESS PANEL 521HB. INSTALL NEW STRUT IAW SRM 51-40-02-0G, REV.94, DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 12, REV B.
- [SDR IPXA2026032491333](https://openairdocs.org/sdr/IPXA2026032491333.md): Seat Track · worn · Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD AFT. IAW AMM 25-11-01-822-095-001, REV 147. REPLACED THE SEAT TRACK IAW AMM 25-11-01-822-095-001 REV 147. JOB COMPLETED AND CONDITION CHECK NORMAL
- [SDR IPXA2026032492359](https://openairdocs.org/sdr/IPXA2026032492359.md): Seat Track · worn · Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD FOWARD. IAW AMM 25-11-01-822-095-001, REV.147 REPLACED THE SEAT TRACK. JOB COMPLETED AND CONDITION CHECK NORMAL SERVICEABLE TAG NR 131706.
- [SDR IPXA2026032490512](https://openairdocs.org/sdr/IPXA2026032490512.md): Drain Valve · broken · Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND DRAIN VALVE ASSEMBLY BROKEN DURING PERFORM TASK CARD EO-89877-REQ1. REPLACED THE DRAIN VALVE ASSEMBLY IAW AMM 51-41-01-004-001 REV 147 AND AMM 51-41-01-404-003 REV 147.
- [SDR IPXA2026032091965](https://openairdocs.org/sdr/IPXA2026032091965.md): Bracket · worn · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > ENLARGED HOLE, NR 1 ENG RT THRUST REVERSER, FWD LWR CLOSURE DOOR T/E AREA.. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22 REV.94.
- [SDR IPXA2026032593477](https://openairdocs.org/sdr/IPXA2026032593477.md): Channel · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON INBD AFT FAIRING PNL NR 437DB INNER FWD CHORD. INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3380, SHT 5, REV H, & DWG 313T3360, SHT 15, REV B.
- [SDR IPXA2026032593408](https://openairdocs.org/sdr/IPXA2026032593408.md): Channel · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACK - CHANNEL, NO. 2 PYLON AFT FAIRING PNL 447DB INNER. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, & DWG 313T3360, SHEET 15, REV B.
- [SDR IPXA2026032590344](https://openairdocs.org/sdr/IPXA2026032590344.md): Angle · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING PANEL 437DB, INNER UPPER SUPPORT BEAM AREA. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3360, SH 15, REV B.
- [SDR IPXA2026032392386](https://openairdocs.org/sdr/IPXA2026032392386.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOW BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.94. 2.INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-23 REV. 47. 3.
- [SDR IPXA2026032092119](https://openairdocs.org/sdr/IPXA2026032092119.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94. AND CMM IPL 71-13-23, REV. 47.
- [SDR IPXA2026032092047](https://openairdocs.org/sdr/IPXA2026032092047.md): Adapter · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED BRACKET, NR 2 ENGINE LT CORE COWL HOLD OPEN ROD STOW ADAPTER. INSTALL A NEW BRACKET I.A.W SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-23 REV 47.
- [SDR IPXA2026032091871](https://openairdocs.org/sdr/IPXA2026032091871.md): Blowout Door · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED SKIN, NR 1 ENG RT THRUST REVERSER LWR BLOWOUT DOOR L/E AREA. (REPLACE). INSTALL NEW BLOWOUT DOOR IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-22 REV.94 AND AMM 78-31-19-402-008 REV.147.
- [SDR IPXA2026032091850](https://openairdocs.org/sdr/IPXA2026032091850.md): Blowout Door · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED SKIN, NR 2 ENG RT THRUST REVERSER BLOWOUT DOOR L/E. (REPLACE). INSTALL NEW BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 78-31-51-03 REV.141 AND AMM 78-31-19-402-008 REV.147.
- [SDR IPXA2026032391455](https://openairdocs.org/sdr/IPXA2026032391455.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR.1 ENG R/H CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24 REV 50.
- [SDR IPXA2026032393518](https://openairdocs.org/sdr/IPXA2026032393518.md): Rib · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > CRACKED LT WING OUTBD L/E CAVITY INNER RIB, NEAR OSS 549, ACCESS PANEL 521HB. INSTALLED A NEW RIB IAW SRM 51-40-02-0G, REV 94, & DWG 114T2207, SH 1, REV B.
- [SDR IPXA2026032393496](https://openairdocs.org/sdr/IPXA2026032393496.md): Rib · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > CRACKED RIB, LT WING OTBD L/E CAVITY INNER RIB, NEAR OSS 514, ACCESS PANEL 521HB. INSTALL NEW RIB IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2205, SH 1, REV B.
- [SDR IPXA2026032391466](https://openairdocs.org/sdr/IPXA2026032391466.md): Fairing · debonded · Mar 16, 2026 · N303UP · Boeing 76734AF · Aerodynamic Fairings
  > DISBOND, FUSELAGE RT SIDE AFT WING TO BODY PANEL 198CR EXTERNAL SURFACE. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W 767 NTM PART1 51-01-01 REV:143. RESULT:NO DEFECT FOUND. IAW SRM 51-70-14-0G-0 REV.94, & AMM 51-21-10-377-003 REV.147
- [SDR IPXA2026032091829](https://openairdocs.org/sdr/IPXA2026032091829.md): Angle · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACK - CLIP, NO. 2 PYLON AFT FAIRING PNL 447DB INNER SUPPORT CLIP L/H. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO: 313T3360 SH 15 REV: B.
- [SDR IPXA2026032091758](https://openairdocs.org/sdr/IPXA2026032091758.md): Angle · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER CAVITY INBD SIDE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026032091887](https://openairdocs.org/sdr/IPXA2026032091887.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG LT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G REV 94, AND IPC 78-32-21 REV 94.
- [SDR IPXA2026032091950](https://openairdocs.org/sdr/IPXA2026032091950.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENGINE RT THRUST REVERSER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-22, REV 94.
- [SDR IPXA2026032091954](https://openairdocs.org/sdr/IPXA2026032091954.md): Bracket · chafed · Mar 16, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG LT THRUST REVERSER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-21 REV.94..
- [SDR IPXA2026032091714](https://openairdocs.org/sdr/IPXA2026032091714.md): Clamp · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED CLAMP, NR 2 PYLON AFT FAIRING DOOR HOLD OPEN SUPPORT ROD STOW CLAMP. REMOVED DAMAGE CLAMP I.A.W SRM 51-40-02-0G REV.94. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3349, SH 2, REV B.
- [SDR IPXA2026031991691](https://openairdocs.org/sdr/IPXA2026031991691.md): Bracket · cracked · Mar 16, 2026 · N303UP · Boeing 76734AF · Wing, Attach Fittings
  > RIGHT WING L/E PNL NR 611KB TORQUE TUBE SUPPORT. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND DWG 114T1240, SH 2, REV E.
- [SDR IPXA2026031690471](https://openairdocs.org/sdr/IPXA2026031690471.md): Floor Panel · damaged · Mar 16, 2026 · N303UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW SREO-9693-REQ001, REV 4, FABRICATE A NEW FLOOR PANEL.
- [SDR IPXA2026032783724](https://openairdocs.org/sdr/IPXA2026032783724.md): Fairing · cracked · Mar 15, 2026 · N303UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED FAIRING, NR 2 ENG LT TRANSCOWL INNER LWR AREA. INSTALLED A NEW FAIRING IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-31, REV 94.
- [SDR IPXA2026032069539](https://openairdocs.org/sdr/IPXA2026032069539.md): Angle · cracked · Mar 14, 2026 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, INBD SIDE. REMOVED THE DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.94. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, AND DWG 146T5650, SH 5, REV C.
- [SDR IPXA2026032069514](https://openairdocs.org/sdr/IPXA2026032069514.md): Angle · cracked · Mar 14, 2026 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND A CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, OTBD SIDE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 146T5650, SH 5, REV C.
- [SDR IPXA2026031769683](https://openairdocs.org/sdr/IPXA2026031769683.md): Floor Panel · damaged · Mar 14, 2026 · N303UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND AFT CARGO FLOOR PANEL DAMAGE, P/N: 453T1996-17. (REPAIR). IAW SRM 53-00-50-2R-0 REV. 94, PERFORM REPAIR AS BELOW STEP: 1.1 CUT OUT THE DAMAGE AND CLEAN. 1.2 MEASURE THE CUT OUT ( L: 5", W: 0.5", AT L/H EDGE AND 13.5" FROM AFT EDGE) 1.3 APPLY THE
- [SDR IPXA2026032637236](https://openairdocs.org/sdr/IPXA2026032637236.md): Skin · cracked · Mar 12, 2026 · N303UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND CRACK ON THE NR 1 FWD ENTRY DOOR AFT LWR CORNER SKIN. ACCOMPLISHED THE REPAIR IAW EO-87307-REQ7, REV 2 & EGAT WORK SHEET 60151.
- [SDR IPXA2026032038208](https://openairdocs.org/sdr/IPXA2026032038208.md): Rib · cracked · Mar 12, 2026 · N303UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > CRACKED FITTING, RT WING T/E NR 10 SPOILER INBD LWR. INSTALLED A NEW FITTING IAW SRM 51-40-02-0G, REV 94, & DWG 112T1001, SH 45, REV -, 113T1653, SH 1, REV I, 112T1000, SH 14, REV B.
- [SDR IPXA2025012071786](https://openairdocs.org/sdr/IPXA2025012071786.md): Floor Panel · broken · Sep 30, 2024 · N303UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND STRUCTURE AND FLOOR PANEL COMMON TO CENTER GUIDE #262 TO BE BROKEN. INSTALLED LOCK 262 FLOOR FITTING IAW AMM 53-01-06-400-801. ALL REPAIRS FOR THIS DEFERRAL FOUND ON LINES ITEMS 6,14,15,16,17,19 OF THIS WORK PACKAGE. AIRCRAFT IS BACK TO NORMAL CONFIG.
- [SDR IPXA2024032349527](https://openairdocs.org/sdr/IPXA2024032349527.md): Skin · corroded · Mar 14, 2024 · N303UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT - CORROSION, BULK CGO RIGHT HAND INTERIOR LOWER FUSELAGE SKIN, NEAR STA 1404, S-33R (EVALUATE) ACCOMPILISHED EO-89882-REQ1 REV.1. JOB COMPLETED.
- [SDR IPXA2024032249527](https://openairdocs.org/sdr/IPXA2024032249527.md): Skin · corroded · Mar 14, 2024 · N303UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > *SDR FILED OPEN* *MAJOR REPAIR* FAULT - CORROSION, BULK CGO RIGHT HAND INTERIOR LOWER FUSELAGE SKIN, NEAR STA 1404, S-33R (EVALUATE) ACCOMPLISH REPAIR PER EO-89882-REQ1 AND EGAT EI F2024A53M-675, REV. 1 (REF. T3F18E0046661) PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2024032326496](https://openairdocs.org/sdr/IPXA2024032326496.md): Plate · cracked · Mar 13, 2024 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > *** SUPPLEMENTAL SDR *** FAULT - FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 LBL 66 (REPLACE) INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88 AND BOEING DWG NO: 146T5650 SH 5 REV.C AND 146T5650 SH 1 REV.A AND 146T5650 SH 4 REV.A
- [SDR IPXA2024032226466](https://openairdocs.org/sdr/IPXA2024032226466.md): Filler · corroded · Mar 13, 2024 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 RBL 66 (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMA
- [SDR IPXA2024032526906](https://openairdocs.org/sdr/IPXA2024032526906.md): Roller Tray · corroded · Mar 13, 2024 · N303UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND AFT CARGO ROLLER TRAY DAMAGE AT STA 1197+22 RBL 42 (REPLACE) ACCOMPLISHED REPAIR I.A.W UPS EO-89883-REQ1 REV.1 AND EGAT EI NO.F2024A53M-755 REV.0 C/W REVIEW
- [SDR IPXA2024031926466](https://openairdocs.org/sdr/IPXA2024031926466.md): Plate · corroded · Mar 13, 2024 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 RBL 66 (REPLACE) PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T42 CONDITION. I.A.W. W/S NO.:40273 STEP 3 AND SPWPS-HT-008 REV.31 AND SPDS-HT-005 REV.33 OPEN
- [SDR IPXA2024031926496](https://openairdocs.org/sdr/IPXA2024031926496.md): Channel · corroded · Mar 13, 2024 · N303UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 LBL 66 (REPLACE) PERFORMED THE CHROMIC ACID ANODIZE I.A.W. EGAT WORK SHEET NO:40274 STEP 7 AND SPWPS-AN-004 REV.22 AND SPDS-AN-001 REV.39. OPEN
- [SDR IPXA2024032583543](https://openairdocs.org/sdr/IPXA2024032583543.md): Drain · damaged · Mar 10, 2024 · N303UP · Boeing 76734AF · Fuselage Main, Structure
  > (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR
- [SDR IPXA2024031183543](https://openairdocs.org/sdr/IPXA2024031183543.md): None · none · Mar 10, 2024 · N303UP · Boeing 76734AF · Standard Practices/Structures
  > **SDR FILED OPEN** FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2023041292851](https://openairdocs.org/sdr/IPXA2023041292851.md): Light · inoperative · Apr 12, 2023 · N303UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/AEMERGENCY LIGHT UNARMED KERRY SWTICH WILL NOT STAY SEATEDREMOVED AND REPLACEED EMERGENCY LIGHTS CONTROL PANEL AIW AMM 33 51 08 404 010. OPS CHECK GOOD AIPC 33 13 01 06
- [SDR IPXA2022100586866](https://openairdocs.org/sdr/IPXA2022100586866.md): Unknown · odor · Oct 5, 2022 · N303UP · Boeing 76734AF · Air Distribution System
  > STRONG "FISH" ODOR IN COCKPIT. SEEM TO EMINATE FROM CARGO AREA. CLEAN UP REQUIREDUPS FIRST RESPONDER MAURICO POSADA INSP OF A/C NO SPILLS NOTED. PER GMM 03.31.01.01. A/C OK TO CONTINUE.

Next page: https://openairdocs.org/aircraft/N303UP/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 = 'N303UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N303UP/reports

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