# Service difficulty reports: N304UP

A list on [N304UP](https://openairdocs.org/aircraft/N304UP.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 5 · 245 reports

- [SDR IPXA2026071310637](https://openairdocs.org/sdr/IPXA2026071310637.md): Strip · missing · Jul 5, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING. INSTALLED CAP STRIPE EDGE IAW DWG 232T4150, SHEET 1, REV A, AND PSDL 232T4150, SHEET DL, REV -.
- [SDR IPXA2026070610637](https://openairdocs.org/sdr/IPXA2026070610637.md): Strip · missing · Jul 5, 2026 · N304UP · Boeing 76734AF · Life Raft
  > FOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING.
- [SDR IPXA2026070694047](https://openairdocs.org/sdr/IPXA2026070694047.md): Rub Strip · chafed · Jun 28, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026070395239](https://openairdocs.org/sdr/IPXA2026070395239.md): Former · cracked · Jun 28, 2026 · N304UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING LE NR 9 SLAT INBD TRACK, OSS 565. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95, SREO-50900-REQ001, REV 2 AND DWG 114T2512, SH 1, REV D.
- [SDR IPXA2026070395238](https://openairdocs.org/sdr/IPXA2026070395238.md): Former · cracked · Jun 28, 2026 · N304UP · Boeing 76734AF · Leading Edge Devices
  > CRACKED FORMER, RT WING NR 8 SLAT OTBD TRACK, OSS 499. INSTALL A NEW FORMER IAW SRM 51-40-02-0G, REV 95, AND SREO-50900-REQ001, REV.2 AND DWG 114T2511, SH 1, REV D.
- [SDR IPXA2026070294028](https://openairdocs.org/sdr/IPXA2026070294028.md): Bracket · chafed · Jun 28, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 1 ENG LT CORE COWL OPEN ROD HOLD BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026070886027](https://openairdocs.org/sdr/IPXA2026070886027.md): Panel · debonded · Jun 27, 2026 · N304UP · Boeing 76734AF · Horizontal Stabilizer Structure
  > DEBONDED AT RIGHT SIDE HST LEADING EDGE FIXED PANEL INTERNAL SURFACE FROM FS STA 157 TO FS STA 194.
- [SDR IPXA2026070684487](https://openairdocs.org/sdr/IPXA2026070684487.md): Bracket · deformed · Jun 27, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > DEFORMED BRACKET, NR 1 ENG L1 CORE COWL UPPER FLANGE. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026070686680](https://openairdocs.org/sdr/IPXA2026070686680.md): Flange · chafed · Jun 27, 2026 · N304UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED FLANGE, NR 1 ENGINE LT THRUST REVERSER LOWER FWD FAIRING AFT SIDE. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-21, REV 96.
- [SDR IPXA2026070684503](https://openairdocs.org/sdr/IPXA2026070684503.md): Bracket · chafed · Jun 27, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 1 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 51.
- [SDR IPXA2026070384542](https://openairdocs.org/sdr/IPXA2026070384542.md): Angle · cracked · Jun 27, 2026 · N304UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACK ANGLE, RT WING LE CAVITY OSS 531. INSTALL A NEW ANGLE IAW SRM 51-40-02-0G, REV.95, AND DWG 114T2206, SH 1, REV B.
- [SDR IPXA2026070384515](https://openairdocs.org/sdr/IPXA2026070384515.md): Rib · cracked · Jun 27, 2026 · N304UP · Boeing 76734AF · Wing, Rib/Bulkhead
  > CRACKED RIB, LT WING OTBD L/E UPPER RIB LOWER ANGLE, OSS 549.75. INSTALLED THE NEW RIB ANGLE IAW SRM 51-40-02-0G, REV. 95 AND DWG 114T2207, SH 1, REV B.
- [SDR IPXA2026070283407](https://openairdocs.org/sdr/IPXA2026070283407.md): Wedge · cracked · Jun 27, 2026 · N304UP · Boeing 76734AF · Trailing Edge Flaps
  > CRACKED WEDGE, RT WING OUTBD FLAP INBD WEDGE. REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W UPS SREO-70175-REQ001 REV.1
- [SDR IPXA2026070866895](https://openairdocs.org/sdr/IPXA2026070866895.md): Angle · worn · Jun 26, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > WORN ANGLE ASSY AND BEARING, NR 2 PYLON LT FAIRING DOOR NR 3 HINGE. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3310 SHT 2, REV G.
- [SDR IPXA2026070867122](https://openairdocs.org/sdr/IPXA2026070867122.md): Angle · worn · Jun 26, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > WORN ANGLE ASSY BEARING, NR 2 PYLON RT FAIRING DOOR NR 4 HINGE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 311T3310, SHT 1, REV L.
- [SDR IPXA2026070666884](https://openairdocs.org/sdr/IPXA2026070666884.md): Channel · cracked · Jun 26, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 2 PYLON LOWER FAIRING T/E OTBD SIDE. REMOVED DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW CHANNEL IAW SRM 51-40-02-0G, REV 95, DWG 313T3380 SH. 5 REV. H, AND DWG 313T3360, SH 15, REV B.
- [SDR IPXA2026070267641](https://openairdocs.org/sdr/IPXA2026070267641.md): Bracket · worn · Jun 26, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > WORN OUT BRACKET ASSY, NR 2 ENG LT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026070267274](https://openairdocs.org/sdr/IPXA2026070267274.md): Bracket · worn · Jun 26, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > WORN OUT BRACKET ASSY, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026072622413](https://openairdocs.org/sdr/IPXA2026072622413.md): Strut · damaged · Jun 24, 2026 · N304UP · Boeing 76734AF · Main Landing Gear Attach Section
  > FOUND THE LT MLG OUTER CYLINDER INNER SURFACE SCRATCH AND THE GLAND NUT THREADS CORROSION. TASK CARD MXP-32-045-02-1-JIC T3F18E00983AV ISSUED TO REPLACE LT MAIN LANDING GEAR, REMOVAL AND INSTALLATION OF LT MAIN GEAR HAS BEEN COMPLETED AND DOCUMENTED ON THI
- [SDR IPXA2026070819890](https://openairdocs.org/sdr/IPXA2026070819890.md): Channel · cracked · Jun 24, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE U CHANNEL ON THE AFT MAIN DECK CARGO DOOR AT BS 632 WAS CRACKED. IAW DWG 453T7019, SHT 1 REV A. REMOVED & REPLACED THE U CHANNEL IAW AMM 20-11-00-910-802, REV 148.
- [SDR IPXA2026070822555](https://openairdocs.org/sdr/IPXA2026070822555.md): Angle · cracked · Jun 24, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND FIRE DETECTION LOOP FASTENER ANGLE CRACKED AT BS 1562, LBL 96 IN BULK CARGO BAY. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 95, & DWG 218T4100, SHT 3, REV B.
- [SDR IPXA2026070121828](https://openairdocs.org/sdr/IPXA2026070121828.md): Antenna · eroded · Jun 24, 2026 · N304UP · Boeing 76734AF · Communications System
  > FOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.
- [SDR IPXA2026070222600](https://openairdocs.org/sdr/IPXA2026070222600.md): Angle · corroded · Jun 24, 2026 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND FLOOR SUPPORT CORRODED IN THE AREA AFT OF BULK CARGO BAY AT BS 1588, LBL 33. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV 95, DWG 146T5650, SHT 2 REV A AND 146T5650, SHT 3, REV A.
- [SDR IPXA2026070121913](https://openairdocs.org/sdr/IPXA2026070121913.md): Bumper · missing · Jun 24, 2026 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.
- [SDR IPXA2026062421913](https://openairdocs.org/sdr/IPXA2026062421913.md): Bumper · missing · Jun 24, 2026 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.
- [SDR IPXA2026082598212](https://openairdocs.org/sdr/IPXA2026082598212.md): Pawl · worn · Jun 23, 2026 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > *** SUPPLEMENTAL SDR *** FAULT - THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE. I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148. TORQUED THE SCREW TO 35 I
- [SDR IPXA2026062398212](https://openairdocs.org/sdr/IPXA2026062398212.md): Pawl · worn · Jun 23, 2026 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.
- [SDR IPXA2026062915824](https://openairdocs.org/sdr/IPXA2026062915824.md): Fan Cowl · dented · May 10, 2026 · N304UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > RIGHT ENGINE OTBD FAN COWL OUTER SKIN TWO DENTS AT 1 O'CLOCK POSITION IAW AMM 71-11-04-714-002-H00, REV 148, INSTALLED THE FAN COWL OF NR 2 ENGINE. CONDITION CHECKED IS SATISFACTORY.
- [SDR IPXA2025052801275](https://openairdocs.org/sdr/IPXA2025052801275.md): Crank Assy · inoperative · May 21, 2025 · N304UP · Boeing 76734AF · Flight Compartment Windows
  > **SUPPLEMENTAL SDR** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN FOUND AFT OUTBOARD GEARBOX TO BE SERVICEABLE, RE-INSTALLED SAME AFT OUTBOARD GEARBOX, FINISHED INSTALLING FORWARD GEARBOX AND INSTALLED A SERVICEABLE AFT INBOARD GEARBOX WITH A NEW RUBBER
- [SDR IPXA2025052101275](https://openairdocs.org/sdr/IPXA2025052101275.md): Roller · out of adjust · May 21, 2025 · N304UP · Boeing 76734AF · Flight Compartment Windows
  > *** SDR FILED OPEN *** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN ADJUSTED AFT LINK ARM AND AFT UPPER ROLLER CLUSTER PER AMM 56-11-02. CRANK CLUTCH STILL BREAKING OVER WHEN CLOSING.
- [SDR IPXA2024071613354](https://openairdocs.org/sdr/IPXA2024071613354.md): Skin · gouged · Jul 15, 2024 · N304UP · Boeing 76734AF · Leading Edge Devices
  > MAJOR REPAIR - GOUGES - SKIN, R/H WING NO.8 SLAT INNER SURFACE UPPER SIDE. (REPAIR) REPAIR I/A/W B767-300F (REV. 89) SRM 51-70-10-2R-4 AND 51-70-10-2R-0 PER SRM 57-43-02-2R-1 (DETAIL III).
- [SDR IPXA2024072905616](https://openairdocs.org/sdr/IPXA2024072905616.md): Spline · cracked · Jul 14, 2024 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK IAW AMM 52-12-02-004-001 REV.142 AND AMM 52-12-02-404-025 REV.142 REPLACED DOORWAY SPLINE TRIM. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024071505616](https://openairdocs.org/sdr/IPXA2024071505616.md): Liner · cracked · Jul 14, 2024 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK. OK TO WORK. OPEN
- [SDR IPXA2024072975073](https://openairdocs.org/sdr/IPXA2024072975073.md): Hinge · deformed · Jul 12, 2024 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) I.A.W AMM 52-12-02-404-025 REV.142 INSTALLED DOORWAY LINING. I.A.W AMM 33-51-01-402-030 REV.142 PERFORM EXIT SIGN LAMP TEST WAS NORMAL. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024072677503](https://openairdocs.org/sdr/IPXA2024072677503.md): Stringer · corroded · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Main, Longeron/Stringer
  > *SUPPLEMENTAL SDR* FAULT - CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-98978-REQ1 REV.1 AND EGAT EI NO.F2024A53M-1771 REV.2. REVIEWED
- [SDR IPXA2024072076571](https://openairdocs.org/sdr/IPXA2024072076571.md): Bracket · cracked · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED BRACKET MEC INTERIOR COMPARTMENT LH FWD UPPER FLIGHT DECK COCKPIT FLOOR BEAM SUPPORT AT STA 246 LBL 50. (REPLACE) 1.FABRICATE P/N(141T5146-16) PER BOEING DWG NO.141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-"AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX
- [SDR IPXA2024071976451](https://openairdocs.org/sdr/IPXA2024071976451.md): Angle · cracked · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60. (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED M
- [SDR IPXA2024071976402](https://openairdocs.org/sdr/IPXA2024071976402.md): Angle · cracked · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MAIN DECK
- [SDR IPXA2024071877503](https://openairdocs.org/sdr/IPXA2024071877503.md): Skin · corroded · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) PERFORM NDT INSPECTION I.A.W EGAT EI NO.F2024A53M-1771 SEQUENCE B PARTA STEP 1.2)~1.4)
- [SDR IPXA2024071276599](https://openairdocs.org/sdr/IPXA2024071276599.md): Floor Panel · dented · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231DFF, P/N: 143T5876-37. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-03-404-
- [SDR IPXA2024071276585](https://openairdocs.org/sdr/IPXA2024071276585.md): Floor Panel · dented · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-39. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-
- [SDR IPXA2024071275073](https://openairdocs.org/sdr/IPXA2024071275073.md): Hinge · deformed · Jul 12, 2024 · N304UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) OK TO WORK
- [SDR IPXA2024071276610](https://openairdocs.org/sdr/IPXA2024071276610.md): Floor Panel · dented · Jul 12, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 252WFF, P/N: 146T5869-55. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-
- [SDR IPXA2024071259276](https://openairdocs.org/sdr/IPXA2024071259276.md): Floor Panel · dented · Jul 11, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.251SFF, P/N:146T5869-37 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV 142 RESTORED MAIN DECK CARGO HANDLING. I.A.W
- [SDR IPXA2024071259270](https://openairdocs.org/sdr/IPXA2024071259270.md): Floor Panel · dented · Jul 11, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.231QFF, P/N:143T5876-19 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-58-04-404-015
- [SDR IPXA2024071259282](https://openairdocs.org/sdr/IPXA2024071259282.md): Floor Panel · dented · Jul 11, 2024 · N304UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO.232AFF, P/N: 143T5876-40 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-01
- [SDR IPXA2024071041602](https://openairdocs.org/sdr/IPXA2024071041602.md): Inspection · none · Jul 10, 2024 · N304UP · Boeing 76734AF · Standard Practices/Structures
  > *SUPPLEMENTAL SDR* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173.
- [SDR IPXA2024070572572](https://openairdocs.org/sdr/IPXA2024070572572.md): Light · inoperative · Jul 5, 2024 · N304UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHT IN COCKPIT AND PRM CAME ON INFLIGHT. WE HAD NO EICAS MESSAGE. WE CYCLED THE EMERGENCY LIGHT OFF+ON SEVERAL TIMES. FINALLY THE LIGHTS WOULD STAY OFF IN THE ARMED POSITION. EMERGENCY OPERATION CHECK OK PER AMM33-51-00.
- [SDR IPXA2022102187349](https://openairdocs.org/sdr/IPXA2022102187349.md): Warning Message · illuminated · Oct 21, 2022 · N304UP · Boeing 76734AF · Hydraulic System, Main
  > INSPECTION TYPE:N/A**ATB** **EMERGENCY DECLARED** C" HYDR SYS PRESS" CAUTION MESSAGER/R'D CENTER HYD PRESSURE SWITCH AND THEN CENTER HYD SYS OPS CHKD NML. HYD LEAK CHKD OK PER AMM 2911-09-401. AMM 05-51-33 PN ON: 211C223-534, OFF: 211C223-301 SN ON: J019718AC
- [SDR IPXA2022100386790](https://openairdocs.org/sdr/IPXA2022100386790.md): Skin · cracked · Sep 21, 2022 · N304UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C14CORROSION AND CRACK DAMAGE WAS FOUND ON FUSELAGE SKIN(P/N:146T3241-14) BETWEEN STA 1395-STA 1417,S-38R-S-39R.REPAIR I.A.W BOEING SRID:4-5611978450 AND UPS EO B767-5330-84909-A.

Next page: https://openairdocs.org/aircraft/N304UP/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 = 'N304UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N304UP/reports

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