# Service difficulty reports: N305UP

A list on [N305UP](https://openairdocs.org/aircraft/N305UP.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 · 216 reports

- [SDR IPXA2026090398854](https://openairdocs.org/sdr/IPXA2026090398854.md): Fitting · cracked · Aug 30, 2026 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK CARGO FLOOR FITTING CRACK DAMAGE AT BS 1109 BL 0. REMOVED DAMAGE FITTING IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FITTING IAW SRM 51-40-02-0G REV. 96 AND DWG 457T4000 SH. 11 REV. B.
- [SDR IPXA2026090447613](https://openairdocs.org/sdr/IPXA2026090447613.md): Nose Cowl · dented · Aug 27, 2026 · N305UP · Boeing 76734AF · Engine Air Intake System
  > FAULT - DENT - SKIN, NO. 2 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA: 0.2", 16" FROM L/E AND AT 9 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR
- [SDR IPXA2026090443491](https://openairdocs.org/sdr/IPXA2026090443491.md): Nose Cowl · dented · Aug 27, 2026 · N305UP · Boeing 76734AF · Engine Air Intake System
  > DENT - SKIN, NO.1 ENG NOSE COWL INNER BARREL NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA: 0.3", 9" FROM AFT EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.
- [SDR IPXA2026090446102](https://openairdocs.org/sdr/IPXA2026090446102.md): Strap · corroded · Aug 27, 2026 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND FORWARD CARGO CEILING STRUCTURE CORROSION AT STA 566 RIGHT SIDE. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV. 96. ACCOMPLISHED REPAIR I.A.W EO-98506-REQ1 REV. 1, BOEING DWG NO. 453T1001 SH. 1 REV. A AND BOEING DWG NO. 453T1183 SH. 6 REV. -.
- [SDR IPXA2026090346191](https://openairdocs.org/sdr/IPXA2026090346191.md): Angle · cracked · Aug 27, 2026 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G RE.96. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 218T4100 SHEET 3 REV. B AND
- [SDR IPXA2026090346129](https://openairdocs.org/sdr/IPXA2026090346129.md): Former · cracked · Aug 27, 2026 · N305UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING CAVITY FORMER OF THE CRACK AT OSS 648. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV 96, & DWG 114T2513, SHT 1, REV D, AND SREO-50900-REQ001, REV 2.
- [SDR IPXA2026090428170](https://openairdocs.org/sdr/IPXA2026090428170.md): Support Angle · cracked · Aug 26, 2026 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND FWD CARGO DOORWAY CEILING SUPPORT CRACK AT BS 600. REMOVED DAMAGE SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96 AND DWG 143T8540, SHT 2, REV B.
- [SDR IPXA2026090324513](https://openairdocs.org/sdr/IPXA2026090324513.md): Bulkhead · cracked · Aug 26, 2026 · N305UP · Boeing 76734AF · Nacelle/Pylon, Bulkhead/Firewall
  > CRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL 437DD, INNER AREA. REMOVED DAMAGE BULKHEAD IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW BULKHEAD IAW SRM 51-40-02-0G, REV 96 AND DWG 313T3360, SHT 15, REV B.
- [SDR IPXA2026090324466](https://openairdocs.org/sdr/IPXA2026090324466.md): Bracket · cracked · Aug 26, 2026 · N305UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 1 AFT FAIRING INNER DRAIN TUBE SUPPORT BRACKET. REPLACEED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96 AND DWG 272T0333, SHT 8, REV-.
- [SDR IPXA2026090126837](https://openairdocs.org/sdr/IPXA2026090126837.md): Bracket · chafed · Aug 26, 2026 · N305UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 1 ENG RT CORE COWL INNER OPEN ROD STOW AREA. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.
- [SDR IPXA2026090123388](https://openairdocs.org/sdr/IPXA2026090123388.md): Bracket · chafed · Aug 26, 2026 · N305UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN HOLE ROD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026090123395](https://openairdocs.org/sdr/IPXA2026090123395.md): Bracket · chafed · Aug 26, 2026 · N305UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN HOLD ROD BRACKET. REMOVED THE DAMAGED BRACKETS IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.
- [SDR IPXA2026082726958](https://openairdocs.org/sdr/IPXA2026082726958.md): Doubler · cracked · Aug 26, 2026 · N305UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED DOUBLER, LT WING OTBD L/E CAVITY UPPER FIXED PANEL LOWER RIB LWR CHORD. REPAIRED AREA, NEAR OSS 531. ACCOMPLISH REPAIR ON DAMAGE AREA IAW SRM 57-41-09-2R-4, REV 96, & EGAT WORK SHEET 60681.
- [SDR IPXA2026090407154](https://openairdocs.org/sdr/IPXA2026090407154.md): Flap Track · eroded · Aug 25, 2026 · N305UP · Boeing 76734AF · Trailing Edge Flaps
  > ERODED SKIN, LT WING NR 1 FLAP TRACK FWD FAIRING EXTERNAL SKIN. REMOVED THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-53-70-2R-1, REFER TO SRM 51-70-17-0G-0 REV. 96
- [SDR IPXA2026090907726](https://openairdocs.org/sdr/IPXA2026090907726.md): Pawl · worn · Aug 25, 2026 · N305UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. IAW AMM 52-11-26-004-001, REV 149 AND AMM 52-11-26-404-003, REV 149. REPLACED THE PAWL.
- [SDR IPXA2026090307096](https://openairdocs.org/sdr/IPXA2026090307096.md): Fairing · debonded · Aug 25, 2026 · N305UP · Boeing 76734AF · Trailing Edge Flaps
  > DISBOND - SKIN, L/H WING NO. 3 FLAP TRACK MID FAIRING INBD T/E SKIN. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-53-70-2R-1 REFER TO SR
- [SDR IPXA2026090107073](https://openairdocs.org/sdr/IPXA2026090107073.md): Skin · eroded · Aug 25, 2026 · N305UP · Boeing 76734AF · Leading Edge Devices
  > EROSION SKIN, L/H WING NO. 2 SLAT OUTBD CLOSURE PANEL. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-43-01-2R-3 REFER T
- [SDR IPXA2026090107012](https://openairdocs.org/sdr/IPXA2026090107012.md): Skin · eroded · Aug 25, 2026 · N305UP · Boeing 76734AF · Leading Edge Devices
  > EROSION SKIN, L/H WING NO. 2 SLAT INBD CLOSURE PANEL AREA. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. MEASURE THE DAMAGE SIZE AND LOCATION ( L: 1", W: 0.5", 1.2" FROM AFT EDGE, 38.5" FROM INBD EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE
- [SDR IPXA2026082507726](https://openairdocs.org/sdr/IPXA2026082507726.md): Pawl · worn · Aug 25, 2026 · N305UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)
- [SDR IPXA2026090192196](https://openairdocs.org/sdr/IPXA2026090192196.md): Bracket · chafed · Aug 24, 2026 · N305UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENGINE, LT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & IPC 78-32-31, REV 96.
- [SDR IPXA2026090192222](https://openairdocs.org/sdr/IPXA2026090192222.md): Bracket · chafed · Aug 24, 2026 · N305UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & IPC 78-32-31, REV 96.
- [SDR IPXA2025043003663](https://openairdocs.org/sdr/IPXA2025043003663.md): Door · binding · Apr 29, 2025 · N305UP · Boeing 76734AF · Landing Gear Door Retract Section
  > GEAR DISAGREE JACKED AIRCRAFT REF MM 07-11-01. RETRACTED GEAR SEVERAL TIMES REF MM 32-32-00. OBSERVED THAT WHEN GEAR WAS EXTENDING, THERE APPEARED TO BE BINDING IN THE LEFT MAIN GEAR DRAG BRACE WITH VIBRATION AND NOISE. LUBED LEFT MAIN GEAR REF MM 12-21-14. TH
- [SDR IPXA2025042903663](https://openairdocs.org/sdr/IPXA2025042903663.md): Warning Message · illuminated · Apr 29, 2025 · N305UP · Boeing 76734AF · Landing Gear Position and Warning
  > *** SDR FILED OPEN *** GEAR DISAGREE
- [SDR IPXA2025042353243](https://openairdocs.org/sdr/IPXA2025042353243.md): Sequence Valve · faulted · Apr 20, 2025 · N305UP · Boeing 76734AF · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF DURING GEAR RETRACTION RECEIVED €ŒGEAR DISAGREE AMD GEAR DOORS€? EICAS MESSAGES. FELT VIBRATION AS IF GEAR DOORS WERE EXTENDED. GEAR DID NOT FEEL FULLY RETRACTED, BUT NOT EXTENDED EITHER. REMOVED AND REPLACED LEFT MLG OPERATED SEQUENCE VALVE
- [SDR IPXA2025042153243](https://openairdocs.org/sdr/IPXA2025042153243.md): Landing Gear · faulted · Apr 20, 2025 · N305UP · Boeing 76734AF · Landing Gear Retraction/Extension System
  > ATB, AFTER TAKE OFF DURING GEAR RETRACTION RECEIVED €ŒGEAR DISAGREE AMD GEAR DOORS€? EICAS MESSAGES. FELT VIBRATION AS IF GEAR DOORS WERE EXTENDED. GEAR DID NOT FEEL FULLY RETRACTED, BUT NOT EXTENDED EITHER. OPEN
- [SDR IPXA2025031312341](https://openairdocs.org/sdr/IPXA2025031312341.md): Lock · inoperative · Mar 12, 2025 · N305UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN ENTRY DOOR SECONDARY LOCK WILL NOT CLOSE PERFORMED ADJ/TEST OF CREW ENTRY DOOR HANDLE AND SECONDARY LOCK REF MM 52-12-25/201. OPS CK NORMAL.
- [SDR IPXA2024112569925](https://openairdocs.org/sdr/IPXA2024112569925.md): Hf Comm · malfunctioned · Nov 24, 2024 · N305UP · Boeing 76734AF · HF Communications System
  > *AIR TURN BACK* TRANSMISSION FROM ANY CREW POSITION ON LHF NOT POSSIBLE. LH HF OPS NML REF AMM 23-11-00.
- [SDR IPXA2024080555098](https://openairdocs.org/sdr/IPXA2024080555098.md): Floorbeam · cracked · Aug 2, 2024 · N305UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM MID CHORD CRACK AT STA 246 NEAR LBL 40 (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-91052-REQ1 REV1.
- [SDR IPXA2024072218159](https://openairdocs.org/sdr/IPXA2024072218159.md): Drain · discovered · Jul 20, 2024 · N305UP · Boeing 76734AF · Stabilizer Control System
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR PER EO 82173-JIC001
- [SDR IPXA2024080596006](https://openairdocs.org/sdr/IPXA2024080596006.md): Support · cracked · Jul 19, 2024 · N305UP · Boeing 76734AF · Wing, Control Surface Attach Fittings
  > **SUPPLEMENTAL SDR**FAULT - CRACK - BRACKET, R/H WING NO.7 SLAT LOWER DOOR. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 89. PERFORMED CHROMIC ACID ANODIZE IAW EGAT WORK SHEET NO. 40586 STEP 7 & SPWPS-AN-004 REV 23 AND SPDS-AN REV 39 (REPLACE) REVIEWED TASK PER G
- [SDR IPXA2024080170071](https://openairdocs.org/sdr/IPXA2024080170071.md): Intercostal · corroded · Jul 18, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CORROSION - INTERCOSTAL, BULK CARGO COMPARTMENT FLOOR BEAM SUPPORT INTERCOSTAL AT STA 1602 LBL 40 - LBL 54" (EVALUATE) REVIEWED TASK PER GMM-MTX 09.05.01.09.PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T62 CONDITION. I.A.W. WORK SHEET NO.:40598 STEP 3
- [SDR IPXA2024080169998](https://openairdocs.org/sdr/IPXA2024080169998.md): Floor Support · corroded · Jul 18, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR SUPPORT INSTERCOSTAL AT STA 1602 RBL 10" ~ 15" (EVALUATE) CONDITION CHECK OK. REMOVED DAMAGED PART I.A.W. SRM 51-40-02-0G REV. 89. FABRICATED INTERCOSTAL I.A.W. EGAT WORK SHEET NO 40600 STEP 2.
- [SDR IPXA2024080169950](https://openairdocs.org/sdr/IPXA2024080169950.md): Floor Support · corroded · Jul 18, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR SUPPORT AT 1602 RBL 54". REMOVED DAMAGED PART. FRABRICATED FLOOR SUPPORT IAW EGAT WORK SHEET NO. 40599 STEP 2.
- [SDR IPXA2024080169472](https://openairdocs.org/sdr/IPXA2024080169472.md): Support Bracket · corroded · Jul 18, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CORROSION, PANEL 149BL FWD SIDE SUPPORT BRACKET, ACCOMPLISHED REPAIR PER EO-90997-REQ1 AND EGAT EI F2024A53M-1830, REV. 0.
- [SDR IPXA2024080449680](https://openairdocs.org/sdr/IPXA2024080449680.md): Skin · corroded · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > **SUPPLEMENTAL SDR**FAULT - CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O-100 BARE TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1821 SEQUENCE A PART A STEP 1.8) REV.0 A
- [SDR IPXA2024080549718](https://openairdocs.org/sdr/IPXA2024080549718.md): Skin · corroded · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER SKIN AT STA 1197+88~STA 1197+132 S-35R~S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1838 SEQUENCE A PART A STEP 1.8) REV.0 AND SPWPS-HT-008 REV.32 AND SPDS-HT-005 RE
- [SDR IPXA2024080549715](https://openairdocs.org/sdr/IPXA2024080549715.md): Stringer · corroded · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Main, Longeron/Stringer
  > CORROSION - STRINGER, AFT CARGO COMPARTMENT LOWER SIDE SKIN AT STA 1197+66~STA 1197+88 S-34R. PERFORMED THE HEAT TREATMENT FROM 7075-O-080 CLAD TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1832 SEQUENCE A STEP 9 REV.0
- [SDR IPXA2024080249680](https://openairdocs.org/sdr/IPXA2024080249680.md): Skin · corroded · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > CORRODED SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R. (REPAIR) I.A.W. EGAT EI NO.F2024A53M-1821 REV.2 SEQUENCE:C PAGE:1 OF 9 STEP:3.A.B, COMPLETED TO MACHINE THE BASE DOUBLER/FLAT FILLER THE THICKNESS FROM 0.125" TO 0.11
- [SDR IPXA2024080246010](https://openairdocs.org/sdr/IPXA2024080246010.md): Angle · cracked · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2024080245873](https://openairdocs.org/sdr/IPXA2024080245873.md): Angle · cracked · Jul 17, 2024 · N305UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89, INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2024072945731](https://openairdocs.org/sdr/IPXA2024072945731.md): Rib · cracked · Jul 17, 2024 · N305UP · Boeing 76734AF · Leading Edge Devices
  > CRACKED RIB, L/H WING NO.3 SLAT OUTBD AUXILIARY TRACK FWD ARM AREA.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 114T4103 SH. 7 REV. B AND NO. 114T4103 SH. 8 REV. A.
- [SDR IPXA2024080727695](https://openairdocs.org/sdr/IPXA2024080727695.md): Master Caution · inoperative · Jul 16, 2024 · N305UP · Boeing 76734AF · Central Warning
  > DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) I.A.W AMM 33-13-00-902-045 REV 142 REPLACED MASTER WARNING SWITCH S507, AND CONDITION CHECK NORMAL.
- [SDR IPXA2024071728963](https://openairdocs.org/sdr/IPXA2024071728963.md): Floor Panel · dented · Jul 16, 2024 · N305UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 251FFF P/N: 146T5869-17.FLOOR PANEL SEALANT REMOVE AND OK TO INSTALL CHECK OK.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2024071728884](https://openairdocs.org/sdr/IPXA2024071728884.md): Floor Panel · dented · Jul 16, 2024 · N305UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231LFF P/N: 143T5876-51.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY
- [SDR IPXA2024071728900](https://openairdocs.org/sdr/IPXA2024071728900.md): Floor Panel · dented · Jul 16, 2024 · N305UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231CFF P/N: 143T5876-39.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2024071728851](https://openairdocs.org/sdr/IPXA2024071728851.md): Floor Panel · dented · Jul 16, 2024 · N305UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231DFF P/N: 143T5876-37.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3 CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2024071728936](https://openairdocs.org/sdr/IPXA2024071728936.md): Floor Panel · dented · Jul 16, 2024 · N305UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231EFF P/N: 143T5876-63.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2024071627695](https://openairdocs.org/sdr/IPXA2024071627695.md): Warning System · failed · Jul 16, 2024 · N305UP · Boeing 76734AF · Central Warning
  > DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) OK TO WORK.
- [SDR IPXA2023110763529](https://openairdocs.org/sdr/IPXA2023110763529.md): Cover · broken · Nov 1, 2023 · N305UP · Boeing 76734AF · Fuselage, Door Hinge
  > *** SUPPLEMENTAL SDR *** CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION R&R CREW DOOR CLEAR PLASTIC COVER HINGE PER IPC 52-11-02-10A ITEM 170 REMOVED PLACARD
- [SDR IPXA2023110163529](https://openairdocs.org/sdr/IPXA2023110163529.md): Unknown · unknown · Nov 1, 2023 · N305UP · Boeing 76734AF · Passenger/Crew Doors
  > *SDR FILED OPEN* CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION DEFERRED AS PAR MEL 52-11-2 PLACARDS INSTALLED

Next page: https://openairdocs.org/aircraft/N305UP/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 = 'N305UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N305UP/reports

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