# Service difficulty reports: N405KZ

A list on [N405KZ](https://openairdocs.org/aircraft/N405KZ.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 2 · 54 reports

- [SDR UIEA2026022500068](https://openairdocs.org/sdr/UIEA2026022500068.md): Duct · damaged · Feb 28, 2026 · N405KZ · Boeing 7474KZF · Air Distribution System
  > R/H W/W PACK #3 DUCT ASSEMBLY DAMAGE. IT WAS FOUND HANGING IN THE R/H WING GEAR WHEEL WELL. IT HAD SEPARATED/FAILED AT THE CONTROL VALVE AT THE TOP OF THE WHEEL WELL. R & R DUCT ASSY PER AMM 21-21-01. LK CHK OK.
- [SDR UIEA2025091101180](https://openairdocs.org/sdr/UIEA2025091101180.md): Idg · faulted · Sep 9, 2025 · N405KZ · Boeing 747400 · AC Generator-Alternator
  > ELEC DRIVE 1 ILLUMINATED ON EICAS. REMOVED AND REPLACED #1 IDG PER AMM 24-11-01. OPS/LEAK CHECK GOOD. MESSAGE CLEARED.</P>)
- [SDR UIEA2025062700816](https://openairdocs.org/sdr/UIEA2025062700816.md): Cooling Fan · failed · Jun 27, 2025 · N405KZ · Boeing 7474KZF · Air Distribution Fan
  > ELECTRICAL BURNING SMELL, SMOKE IN COCKPIT ON INITIAL CLIMB. EQUIP COOLING EICAS FOLLOWED, THEN EICAS SCREEN BLANKED AFTER APPROX 60 SEC. PERFORMED AMM 05-51-56 SMOKE INSPECTION. FOUND COOLING FAN AT FAULT. REPLACED E/E COOLING FAN PER AMM 21-58-01. CMC TEST
- [SDR UIEA2024111401089](https://openairdocs.org/sdr/UIEA2024111401089.md): Line · damaged · Nov 14, 2024 · N405KZ · Boeing 7474KZF · Hydraulic System, Main
  > GEAR TILT EICAS MESSAGE ON TAKEOFF. LEFT BODY GEAR.(<P >FOUND HYDRAULIC LINE DAMAGED IN LH WHEEL WELL BODY FROM BODY GEAR TILT ACTUATOR HYD FUSE. RMVD FLEX LINE AND INSTALLED RIGID LINE AMM 20-11-05. OPS AND LEAK CHECK GOOD PER AMM 29-00-00. GEAR TILT MESSAGE
- [SDR UIEA2024080200777](https://openairdocs.org/sdr/UIEA2024080200777.md): Fmc · faulted · Aug 2, 2024 · N405KZ · Boeing 7474KZF · Auto Throttle System
  > REJECTED TAKE OFF @ 70 KNOTTS AUTOTHROTTLE DISCONNECT MASTER CAUTION.(<P>R/R LH FMC IAW AMM 34-61-01. OPS CHECK GOOD. DMI 214021 CLOSED.</P>)
- [SDR UIEA2023110200934](https://openairdocs.org/sdr/UIEA2023110200934.md): Aoa · unknown · Nov 1, 2023 · N405KZ · Boeing 7474KZF · Stall Warning System
  > PITCH LIMITING INDICATOR DISPLAYED WHEN FLAPS WERE RETRACTED DURING CRUISE(<P>REPLACED LH AOA SENSOR IAW B747 AMM 34-12-03. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023100700891](https://openairdocs.org/sdr/UIEA2023100700891.md): Wire Harness · unknown · Oct 5, 2023 · N405KZ · Boeing 7474KZF · Fire Protection System Wiring
  > ENG 3 FIRE LOOP A & B FAILED(<P>R/R UPPER & LWR AFT DETECTOR ASSY IAW AMM 26-11-02. R/R HARNESS 61B45322 IAW AMM 26-11-02. R/R HARNESS WIRE AND ENG IDLE TEST RUN NORMAL IAW AMM 71-00-00. PERFORMED OPS CHECK, NO FAULTS FOUND FOR ENG 3 FIRE LOOP.</P>)
- [SDR UIEA2022061200579](https://openairdocs.org/sdr/UIEA2022061200579.md): Shock Mount · warning message · Jun 10, 2022 · N405KZ · Boeing 7474KZF · Landing Gear Actuator
  > GEAR TILT MSG AFTER TAKEOFF. GEAR WOULD NOT RETRACT. QRH CHECKLIST COMPLETED. INSTALLED LH BODY GEAR SHOCK STRUT O/B DOOR AND ADJUSTMENT BODY GEAR DOOR AS PER AMM 32-14-06 & 32-14-00. L/G OPERATIONAL TEST NORMAL AS PER AMM 32-33-00. REMOVED AND REPLACED NEW LH
- [SDR UIEA2021050701087](https://openairdocs.org/sdr/UIEA2021050701087.md): Skin · broken · May 4, 2021 · N405KZ · Boeing 747400 · Ailerons
  > BROKEN SKIN, LH WING INBD AILERON T/E OUTBD EDGE(<P>REPAIR BROKEN SKIN, <SPAN>LH WING INBD AILERON T/E OUTBD EDGE. SEE J/C ATTACHING SHEET NO. 0237793, 0237794, 0237673 FOR REPAIR DETAIL. CONDITION CHECK IS SATISFACTORY.</SPAN></P>)
- [SDR UIEA2021050701088](https://openairdocs.org/sdr/UIEA2021050701088.md): Skin · chafed · May 4, 2021 · N405KZ · Boeing 747400 · Ailerons
  > CHAFFING SKIN PANEL, RH WING INBD AILERON OUTBD END T/E AREA(<P>REPAIR CHAFFING SKIN PANEL, <SPAN>RH WING INBD AILERON OUTBD END T/E AREA. SEE J/C ATTACHING SHEET NO. 0237792, 0237674 FOR REPAIR DETAIL. CONDITION CHECK IS SATISFACTORY.</SPAN></P>)
- [SDR UIEA2021050701089](https://openairdocs.org/sdr/UIEA2021050701089.md): Door Frame · broken · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Structure
  > FOUND MAIN DECK CGO L5 ENTRY DOOR FWD FRAME BROKEN(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 91. REPAIRED DAMAGED AREA IAW SRM 53-60-15-2R-3 REPAIR 3 REV 91 AND EI NO. T2021A53M-1269 REV 1. REINSTALLED FASTENERS IAW <SPAN>SRM 51-40-02 RE
- [SDR UIEA2021050701090](https://openairdocs.org/sdr/UIEA2021050701090.md): Rib · cracked · May 4, 2021 · N405KZ · Boeing 747400 · Horizontal Stabilizer, Spar/Rib
  > CRACKED RIB, RH HORIZONTAL STAB INTERNAL RIB. STAB BL 421(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 91. REPAIR DAMAGE AREA IAW SRM 55-10-09-2R-13 REPAIR 13 REV 91. INSTALLED FASTENERS IAW SRM 51-40-02 REV 91. AND DWG NO. 65BO3520 SHEET 2
- [SDR UIEA2021050701091](https://openairdocs.org/sdr/UIEA2021050701091.md): Seal · out of position · May 4, 2021 · N405KZ · Boeing 747400 · Cargo/Baggage Doors
  > FOUND THE PRESSURE SEAL INTERFERE WITH ARM SWITCH IN AFT CGO DOOR CONTROL PANEL(<P>ACCOMPLISHED EGAT EI NO. T202152E-1450 REV. 0 AND W/O NO. 5881407 CLOSE</P>)
- [SDR UIEA2021050701092](https://openairdocs.org/sdr/UIEA2021050701092.md): Stiffener · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Wing Miscellaneous Structure
  > EXFOLIATION CORROSION - STIFFENER, LH WING CTR L/E REFUELING DOOR(<P>REMOVED AND REPLACED DAMAGED PARTS IAW SRM 51-40-02 REV 91 AND DWG NO. 65B10882 SH 7 REV C. CONDITION CHECK NORMAL.</P>)
- [SDR UIEA2021050701093](https://openairdocs.org/sdr/UIEA2021050701093.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEM ASSEMBLY INTERIOR STRUCTURE, STA 1271 RBL 9(<P>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP REFER TO J/C ATTACHING SHEET NO. 0291702 AND DATA SHEET NO. 5767394-1. ACCOMPLISHED EI NO. T202153M-1167 REV 1. C
- [SDR UIEA2021050701094](https://openairdocs.org/sdr/UIEA2021050701094.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1400 LBL 9(<P>BLENEDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORM NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291706 AND DATA SHEET NO. 5767375-1. ACCOMPLISHED EI NO. T202153M-1167 REV 1 AN
- [SDR UIEA2021050701095](https://openairdocs.org/sdr/UIEA2021050701095.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE, STA 1383 LBL 9(<P>BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291704 AND DATA SHEET NO. 5767374-1. ACCOMPLISHED EI NO. T202153M-1167 REV 1
- [SDR UIEA2021050701096](https://openairdocs.org/sdr/UIEA2021050701096.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1441, RBL 9(<P>BLENDED OUT THE DAMAGE AREA IAW SRM 51+10+02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291711 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. CONDITION
- [SDR UIEA2021050701097](https://openairdocs.org/sdr/UIEA2021050701097.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1425, RBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291709 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. COND
- [SDR UIEA2021050701098](https://openairdocs.org/sdr/UIEA2021050701098.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE, STA 1442, LBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291712 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. CON
- [SDR UIEA2021050701099](https://openairdocs.org/sdr/UIEA2021050701099.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1413, RBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291708 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. COND
- [SDR UIEA2021050701100](https://openairdocs.org/sdr/UIEA2021050701100.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1270 LBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291701 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. CONDI
- [SDR UIEA2021050701101](https://openairdocs.org/sdr/UIEA2021050701101.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY, INTERIOR STRUCTURE STA 1387, RBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291705 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. CON
- [SDR UIEA2021050701102](https://openairdocs.org/sdr/UIEA2021050701102.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1331.5, RBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291703 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. CO
- [SDR UIEA2021050701103](https://openairdocs.org/sdr/UIEA2021050701103.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1400, RBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291707 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. COND
- [SDR UIEA2021050701104](https://openairdocs.org/sdr/UIEA2021050701104.md): Keelbeam · corroded · May 4, 2021 · N405KZ · Boeing 747400 · Fuselage Main, Keel
  > CORROSION - CHORD, KEEL BEAM ASSEMBLY INTERIOR STRUCTURE STA 1433, LBL 9(<P><SPAN>BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 91. PERFORMED NDT INSP. REFER TO J/C ATTACHING SHEET NO. 0291710 AND DATA SHEET NO. 5767371-1. ACCOMPLISHED EI NO. T202153M. COND
- [SDR UIEA2021050701105](https://openairdocs.org/sdr/UIEA2021050701105.md): Wire · misrouted · May 4, 2021 · N405KZ · Boeing 747400 · Electrical Power System Wiring
  > FOUIND WIRE NO. W4698-705-20 NOT ROUTE CORRECTLY IAW SB 747-21-2550 (AD)(<P>TRANSFER TO EO NO. 4421A098 REV 9 AND W/O NO. 5775917 CLOSE.</P>)
- [SDR UIEA2020080421682](https://openairdocs.org/sdr/UIEA2020080421682.md): Warning Message · false activation · Aug 3, 2020 · N405KZ · Boeing 7474KZF · Landing Gear System
  > GEAR TILT EICAS MESSAGE AFTER TAKE OFF. PERFORMED A LEAK CHECK AND NO LEAKS NOTED ON HOSE ASSY FOR BODY GEAR TRUCK POSITIONING ACTUATOR. BLED THE ACTUATOR AND PUT THE HYDRAULIC FUSE IN THE NORMAL POSITION IAW AMM 32-13-15-404-010. PERFORMED PSEU GROUND TEST
- [SDR UIEA2020072731609](https://openairdocs.org/sdr/UIEA2020072731609.md): Line · broken · Jul 23, 2020 · N405KZ · Boeing 7474KZF · Landing Gear Actuator
  > LEFT BODY GEAR TILT ACTUATOR LINE BROKEN(<P ><SPAN>INSTALLED TEMP HOSE AND / DEFERRED IAW AMM 32-13-15.</SPAN></P>)
- [SDR UIEA2020031300429](https://openairdocs.org/sdr/UIEA2020031300429.md): Pseu · malfunctioned · Mar 10, 2020 · N405KZ · Boeing 7474KZF · Landing Gear Position and Warning
  > LANDING GEAR TILT/DOOR MESSAGE ON CLIMB OUT. CREW CONTINUED FLIGHT WITH GEAR DOWN FROM KKJ TO NRT.(<P ><SPAN>LANDING GEAR PROX SENSORS CONDITION CHECK OK. REMOVED AND REPLACED PSEU AND DAMAGED / HYD LINE ON LH BLG TILT ACTUATOR. THEN PSEU SYSTEM GROUND TEST PA
- [SDR UIEA2019060654392](https://openairdocs.org/sdr/UIEA2019060654392.md): Unknown · odor · Jun 5, 2019 · N405KZ · Boeing 7474KZF · Air Distribution System
  > FUMES ON FLT DECK 40 DME FROM AIRPORT. NO EICAS MSG & NO PLF REPORTED. ACCOMPLISHED FIM 21-00, TASK 810. NO ABNORMALITIES FOUND WITH ALL ENGINES RUNNING, ALL PACKS, APU, AND ELECTRICAL SYSTEMS RUNNING. OK FOR SERVICE. PER MCC REQ, C/O INSPECTION OF EQUIPMENT
- [SDR UIEA2019040383675](https://openairdocs.org/sdr/UIEA2019040383675.md): Skin · chafed · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Ailerons
  > L/H WING T/E -I/B AILERON O/B AFT CORNER FOUND WITH CHAFING MARK.(<P>L/H WING T/E-I/B AILERON O/B AFT CORNER REPAIRED IAW B747-400F SRM 57-60-01-2R-7 REPAIR I AND SRM 51-70-06 REV 85 AND PAINTED IAW B747-400 AMM 51-24-11 REV 95</P>)
- [SDR UIEA2019040333712](https://openairdocs.org/sdr/UIEA2019040333712.md): Floor Panel · punctured · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1390, LBL 91 FOUND 1 PUNCTURE HAVING 0.88" MAX DIAMETER AND NO DELAMINATION(<P>MAIN DECK CARGO FLOOR PANEL AT STA 1390, LBL 91 REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040393676](https://openairdocs.org/sdr/UIEA2019040393676.md): Skin · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Ailerons
  > R/H WING I/B AILERON O/B T/E CORNER FOUND PANEL SEPARATION.(<P>RH WING I/B AILERON O/B T/E CORNER REPAIRED AS PER 747-400F SRM 57-60-01 REPAIR 1 AND SRM 51-70-06 REV 85 </P>)
- [SDR UIEA2019040333713](https://openairdocs.org/sdr/UIEA2019040333713.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL #261CF AT L/H STA 1750 FOUND 2 SCRATCHES & 1 CRACK WITH LARGEST HAVING 0.86 MAX DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANEL #261CF AT L/H STA 1750 REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333714](https://openairdocs.org/sdr/UIEA2019040333714.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, LBL 91 FOUND WITH 6 HOLES WITH LARGEST HAVING 1.4" MAX DIAMETER AND NO DELAMINATION.(<P>MAIN DECK CARGO FLOOR PANELS AT STA 1790 LBL 91 REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019033003715](https://openairdocs.org/sdr/UIEA2019033003715.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, LBL 66 FOUND 5 HOLES AND NO DELAMINATION.(<P>MAIN DECK CARGO FLOOR PANEL AT STA 1790 LBL 66 REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333716](https://openairdocs.org/sdr/UIEA2019040333716.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT 1790, LBL 42 FOUND 4 HOLES WITH LARGEST HAVING 0.25" MAX DIAMETER & NO DELAMINATION(<P>MAIN DECK CARGO FLOOR PANELS AT STA 1790 LBL 42 FLOOR PANEL REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333717](https://openairdocs.org/sdr/UIEA2019040333717.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL STA 1790, LBL 17 FOUND WITH 9 HOLES WITH LARGEST HAVING 1" MAX DIAMETER & NO DELAMINATION(<P>MAIN DECK CARGO PANELS AT STA 1790 LBL 17 FLOOR PANEL REPAIRED IAW <SPAN>EN#1051-19 REV-</SPAN></P>)
- [SDR UIEA2019040333718](https://openairdocs.org/sdr/UIEA2019040333718.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, RBL 17 FOUND WITH 8 HOLES WITH LARGEST HAVING 1.4" MAX DIAMETER AND NO DELAMINATION(<P>MAIN DECK CARGO FLOOR PANEL AT STA 1790 RBL 17 REPAIRED IAW FINAL EN#1051-19 REV-</P>)
- [SDR UIEA2019040333719](https://openairdocs.org/sdr/UIEA2019040333719.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, RBL 42 FOUND WITH 8 HOLES WITH LARGEST HAVING 2.0" MAX DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANEL AT STA 1790, RBL 42 REPAIRED IAW FINAL EN#1051-19 REV-</P>)
- [SDR UIEA2019040333720](https://openairdocs.org/sdr/UIEA2019040333720.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, RBL 66, FOUND WITH 7 HOLES WITH LARGEST HAVING 1.0" MAX DIAMETER AND NO DELAMINATION.(<P>MAIN DECK CARGO FLOOR PANELS AT STA 1790 RBL 66 REPAIRED IAW <SPAN> </SPAN><SPAN>EN#1051-19 REV-</SPAN></P>)
- [SDR UIEA2019040333721](https://openairdocs.org/sdr/UIEA2019040333721.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1790, RBL 91 FOUND WITH 7 HOLES WITH LARGEST HAVING 0.5" MAX DIAMETER AND NO DELAMINATION(<P>MAIN DECK CARGO FLOOR PANEL AT STA 1790 RBL 91 REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333722](https://openairdocs.org/sdr/UIEA2019040333722.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANELS FROM STA 1800 -1915, RBL 42, 3 AREAS AT STA 1915 FOUND 3 HOLES, STA 1800 FOUND 3 HOLES, STA 1895 FOUND 3 SCRATCHES(<P>MAIN DECK CARGO FLOOR PANEL FROM STA 1800-1915 RBL 42 FLOOR PANEL REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040303723](https://openairdocs.org/sdr/UIEA2019040303723.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, LBL 91 FOUND WITH 7 HOLES WITH LARGEST HAVING 1.4" MAX DIAMETER AND NO DELAMINATION(<P>MAIN DECK CARGO FLOOR PANELS AT STA 1915 LBL 91 PANEL REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333724](https://openairdocs.org/sdr/UIEA2019040333724.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, LBL 66 FOUND WITH 4 SCRATCHES WITH LARGEST HAVING 0.25" MAX DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANEL AT STA 1915 LBL 66 PANEL REPAIRED IAW <SPAN>EN#1051-19 REV-</SPAN></P>)
- [SDR UIEA2019040333725](https://openairdocs.org/sdr/UIEA2019040333725.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, LBL 42 FOUND WITH 5 SCRATCHES WITH LARGEST HAVING 0.25" DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANELS AT STA 1915 LBL 42 PANEL REPAIRED IAW <SPAN>EN#1051-19 REV-</SPAN></P>)
- [SDR UIEA2019040333729](https://openairdocs.org/sdr/UIEA2019040333729.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, RBL 17 FOUND WITH 5 SCRATCHES OR HOLES WITH LARGEST HAVING 0.75" DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANELS AT STA 1915 RBL 17 FLOOR PANEL REPAIRED IAW EN#1051-19 REV-</P>)
- [SDR UIEA2019040333730](https://openairdocs.org/sdr/UIEA2019040333730.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, RBL 66 FOUND 2 HOLES AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANELS AT STA 1915 RBL 66 PANEL REPAIRED IAW <SPAN>EN# 1051-19 REV-</SPAN></P>)
- [SDR UIEA2019040333731](https://openairdocs.org/sdr/UIEA2019040333731.md): Floor Panel · damaged · Apr 1, 2019 · N405KZ · Boeing 7474KZF · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT STA 1915, RBL 91, FOUND WITH 7 HOLES WITH LARGEST HAVING 1.5" MAX DIAMETER AND NO DELAMINATION (<P>MAIN DECK CARGO FLOOR PANEL AT STA 1915 RBL 91 REPAIRED IAW <SPAN>EN# 1051-19 REV-</SPAN></P>)

Next page: https://openairdocs.org/aircraft/N405KZ/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 = 'N405KZ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N405KZ/reports

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