# Service difficulty reports: N263WN

A list on [N263WN](https://openairdocs.org/aircraft/N263WN.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 6 · 288 reports

- [SDR SWAA2026072007194](https://openairdocs.org/sdr/SWAA2026072007194.md): Lamp · inoperative · Jul 14, 2026 · N263WN · Boeing 7377H4 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT RIGHT SIDE FWD OF AFT CARGO DOO INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP AT RIGHT SIDE FWD OF AFT CARGO DOOR IAW AMM 33-51-01.OPS CHECKED GOOD.
- [SDR SWAA2026072045852](https://openairdocs.org/sdr/SWAA2026072045852.md): Light · inoperative · Jul 14, 2026 · N263WN · Boeing 7377H4 · Emergency Lighting
  > LEFT SIDE CABIN AFT MOST OVERHEAD BIN EMERGENCY LIGHT IN OPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-01-201-NG.
- [SDR SWAA2026063016096](https://openairdocs.org/sdr/SWAA2026063016096.md): Web · cracked · Jun 26, 2026 · N263WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE INBD COWL WEB CRACKED AFT OF OIL SERVICE DOOR. REMOVED AND REPLACED NR 1 ENGINE INBD COWL WEB AFT OF OIL SERVICE DOOR PER SRM 51-40-02. REMOVED AND REPLACED NR 1 ENGINE INBD COWL WEB AFT OF OIL SERVICE DOOR IAW SRM 51-40-02.
- [SDR SWAA2025121043821](https://openairdocs.org/sdr/SWAA2025121043821.md): Megaphone · no discrepancy · Dec 7, 2025 · N263WN · Boeing 7377H4 · Emergency Equipment
  > MEGAPHONE IN AFT GALLEY INOPERATIVE. MEGAPHONE OPS CHECK GOOD IAW AMM 25-64-00
- [SDR SWAA2025102727936](https://openairdocs.org/sdr/SWAA2025102727936.md): Sensor · faulty · Oct 23, 2025 · N263WN · Boeing 7377H4 · Leading Edge Slat Position Indicating System
  > LE FLAPS TRANSIT AT FLAPS 10 AND BEYOND. ALL LE DEVICES APPEARED EXTENDED; NO ASYMMETRY WAS DETECTED NOR ANY SKEW. PERFORMED BYTE CHECK, FOUND FAULT 27-81215. SLAT 8 INBD SENSOR FAULTY PER FIM 27-88 TASK 804. R AND R S8 INBD SENSOR PER AMM 27-88-11. OPS CHK
- [SDR SWAA2025040721822](https://openairdocs.org/sdr/SWAA2025040721822.md): Transmitter · malfunctioned · Apr 4, 2025 · N263WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > ON APPROACH FLAP WOULD NOT GO BEYOND FLAPS 5 THE LEFT FLAP POSITION TRANSMITTER LAGGED THEN ASYMMETRY BYPASS INITIATED BUT LOOKS LIKE IT MIRROR UP AFTER. I WOULD CHANGE THE LEFT FLAP POSITION TRANSMITTER (T427) AND INDICATOR.<[01] PER FSEU FAULT HISTORY MSG 27
- [SDR SWAA2025033119766](https://openairdocs.org/sdr/SWAA2025033119766.md): Connector · loose · Mar 30, 2025 · N263WN · Boeing 7377H4 · Flight Control System Wiring
  > FLAPS FAILED BETWEEN 1 AND 2; EXTENDED FLAPS TO 15 USING ALT FLAP EXTENSION. RNO MX FOUND LEFT POSITION TRANSMITTER CONNECTOR LOOSE BARELY FINGER TIGHT. CLEANED AND CORRECTLY SECURED. SHOULD BE A GOOD FIX.<[01] ACCOMPLISHED FSEU BITE PER FIM 27-51 TASK 801. FO
- [SDR SWAA2025011384855](https://openairdocs.org/sdr/SWAA2025011384855.md): Sign · out of adjust · Jan 10, 2025 · N263WN · Boeing 7377H4 · Emergency Lighting
  > OVERWING EMERGENCY EXIT SIGN LOOSE / DANGLING<[01] REINSTALLED EMERGENCY EXIT SIGN PER AMM 33-51-02
- [SDR SWAA2025011384744](https://openairdocs.org/sdr/SWAA2025011384744.md): Handle · broken · Jan 10, 2025 · N263WN · Boeing 7377H4 · Galley Doors
  > AFT PASSENGER DOOR R2 DOOR HANDLE CAM SAFETY WIRE BROKEN.<[01] RE-SECURED AFT GALLEY SVC DOOR HANDLE CAM BOLTS AND SAFETY WIRE REF AMM 20-50-11.<BR>CORRECTION AFT GALLEY SERVICE DOOR.
- [SDR SWAA2025011384740](https://openairdocs.org/sdr/SWAA2025011384740.md): Seal · cracked · Jan 10, 2025 · N263WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > R/H HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED FWD EDGE<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2024121777620](https://openairdocs.org/sdr/SWAA2024121777620.md): Lamp · inoperative · Dec 15, 2024 · N263WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT AFT EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED LAMP IN REF TO AMM 33-51-00
- [SDR SWAA2024101547585](https://openairdocs.org/sdr/SWAA2024101547585.md): Light · inoperative · Oct 12, 2024 · N263WN · Boeing 7377H4 · Emergency Lighting
  > FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT BULB OUT<[01] RELAMPED FORWARD SERVICE DOOR FWD LOWER EXIT LIGHT AND PERFORMED GOD OPERATIONAL CHECK PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024101547587](https://openairdocs.org/sdr/SWAA2024101547587.md): Bulb · inoperative · Oct 12, 2024 · N263WN · Boeing 7377H4 · Emergency Lighting
  > RH EMERGENCY EXIT DORR LOWER EXIT LIGHT BULB OUT<[01] RELAMPED RH EMERGENCY EXIT DOOR LOWER EXIT LIGHT AND PERFORMED GOOD OPERATIONAL CHECK PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024101646714](https://openairdocs.org/sdr/SWAA2024101646714.md): Battery Pack · no test · Oct 9, 2024 · N263WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M1670; 1675; M1674) FAIL TEST; DO NOT HOLD CHARGE EMERGENCY BATTRIES PACK (M1672 M1673 M1668 M1670 M1675 M1674) FAIL TEST DO NOT HOLD CHARGE<[01] REMOVED AND REPLACED EMERGENCY BATTRIES PACK (M1672; M1673; N1668; M
- [SDR SWAA2024101642801](https://openairdocs.org/sdr/SWAA2024101642801.md): Insert · out of position · Sep 27, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF HAS NUMEROUS THROUGH INSERTS THAT DO NOT ALIGN WITH THE UNDERLYING STRUCTURE.<[01] NEW 241AF FLOOR PANEL FABRICATION HAS BEEN COMPLETED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE
- [SDR SWAA2024101639184](https://openairdocs.org/sdr/SWAA2024101639184.md): Stub Frame · cracked · Sep 18, 2024 · N263WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FOUND AT R1 DOOR ON STUB FRAME ABOVE SEAL DEPRESSOR BS 294+5 WL274<[01] REMOVED AND REPLACED STUB FRAME UPPER AREA R1 DOOR FWD SIDE PER SRM 51-40-02 AND DWG 141A8370 REV C;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024101637738](https://openairdocs.org/sdr/SWAA2024101637738.md): Web · corroded · Sep 14, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > SHEAR WEB AT BS 1016 RBL 36 WL 208 HAS CORROSION AROUND FASTENER HOLES ON UPPER SURFACE<[01] REMOVED AND REPLACED NEW SHEAR WEB PN#147A5744-14 FROM BS986-BS1016 RBL 36 PER SRM 51-40-02; PER DWG#147A5730 REV C AND PER DWG# 147A000 REV A;[02] VERIFIED CORRECTIVE
- [SDR SWAA2024101637286](https://openairdocs.org/sdr/SWAA2024101637286.md): Intercostal · cracked · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN COMPARTMENT STRUCTURE AREA; AT BS294.5 TO BS303.9 L/H SIDE STRINGER 15; INTERCOSTAL WITH CRACK MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD ENTRY DOOR BS294.5 TO BS303.9 L/H SIDE; STR15L IAW B-737-700 SRM 51-10-02. SRM 51-40-02-0G-0 AND D
- [SDR SWAA2024101637293](https://openairdocs.org/sdr/SWAA2024101637293.md): Web · corroded · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-TRHESHOLD WEB FROM STA 807 TO STA 827+8 RBL 27; WL 158.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB P/N 146A8123U25 LOT# 1577334-1 IAW SRM 51-40-02 AND DWG 146A8340.;[02] UPDATE STEP 1.<BR>REMOVED AND REPLACE
- [SDR SWAA2024101637294](https://openairdocs.org/sdr/SWAA2024101637294.md): Shield · corroded · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO DOOR CUT-OUT FWD SHIELD AT STA 767+2 & 767+15; WL 158; RBL 22.<[01] REMOVED AND REPLACED AFT CARGO DOOR CUT-OUT FWD SHIELD BS 767 TO BS294 RBL22 WL158 P/N 146A8127-12 LOT#1572705-1 IAW SRM 51-40-02 AND DWG 146A0081 REV A.;[02] VERIFIED A
- [SDR SWAA2024101637291](https://openairdocs.org/sdr/SWAA2024101637291.md): Sidewall Support · corroded · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727B+6 TO STA 767; RBL 22; WL 158.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL BS727 TO BS767 RBL22 WL158. IAW SRM 51-40-02-0G-0 & DWG 146A7500 REV: A;[02] VERIFIED RII CORRECTIVE ACT
- [SDR SWAA2024101637292](https://openairdocs.org/sdr/SWAA2024101637292.md): Sidewall Support · corroded · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727C+5 TO STA 787+2 LBL 22; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLEE FROM STA 727 TO STA 847 LBL 22; WL 158. IAW SRM 51-40-02 AND DWG 1
- [SDR SWAA2024101637295](https://openairdocs.org/sdr/SWAA2024101637295.md): Support · corroded · Sep 13, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REJECT: CORROSION NOT REMOVED ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194<[01] REPAIRED PER EA 24-153-02618;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024101637280](https://openairdocs.org/sdr/SWAA2024101637280.md): Attach Angle · cracked · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FCB ATTACH ANGLE CRACKED AT BS 500C LBL 26 WL 156.<[01] REMOVED AND REPLACE FCB ATTACH ANGLE BS 500C LBL 26 WL 156 P/N 143A7502-157 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV A.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024101637261](https://openairdocs.org/sdr/SWAA2024101637261.md): Web · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1016; WL 208.1 & LBL 38 APPROX.<[01] ?REFER TO FAULT TTG8Q00VTXK7 WHERE EA 24-153-02532 WAS ADDED AS A SUBTASK?<BR>'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCE IS SELECTED.;[02] VERIFIED CORREC
- [SDR SWAA2024101637043](https://openairdocs.org/sdr/SWAA2024101637043.md): Sill Drain · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN WET AREA; AFT RH DOOR MOPSILL FOUND CORROSION AROUND SEVERAL FASTENER HOLES BTWN STA 967 TO 985; WL 208.1 APPROX.<[01] REMOVED AND REPLACED RH MOPSILL PN#147A8540U8 IAW SRM 51-40-02; PER DWG#147A8501 REV: A; DWG#147A0000 REV: A AND PER DWG#147A
- [SDR SWAA2024101637038](https://openairdocs.org/sdr/SWAA2024101637038.md): Strap · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1027; WL 208.1 & RBL 18 APPROX.<[01] REMOVED AND REPLACED NEW PASSENGER CABIN AFT WET AREA TENSION STRAP BS 1027 RBL 18 IAW SRM 51-40-02-0G-0 AND DWG #147A5730.;[02] REMOVED AND REPLACED NEW PA
- [SDR SWAA2024101637041](https://openairdocs.org/sdr/SWAA2024101637041.md): Strap · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & LBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1; LBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5600.;[02] REMOVED AND REPLACED
- [SDR SWAA2024101637282](https://openairdocs.org/sdr/SWAA2024101637282.md): Floor Support · cracked · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL FOUND WITH CRACK AT BS312 TO BS328 WL 208 RBL30 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410-140. LOT:1574381-1. LOCATED BETWEEN BS.312 - BS.328 RBL.30 WL.208 IAW B-737-700. SRM 51-40-02. & DWG#141A540
- [SDR SWAA2024101637279](https://openairdocs.org/sdr/SWAA2024101637279.md): Floor Support · cracked · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL BS 380 TO BS 400 WL 208 RBL 10 FOUND WITH CRACK (R/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) ANGLE IN THE FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE BETWEEN BS 380 AND BS 400 WL 208 RB
- [SDR SWAA2024101637040](https://openairdocs.org/sdr/SWAA2024101637040.md): Strap · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT TENSION STRAP STA 1028; WL 208.1 & RBL 3 APPROX.<[01] REMOVED AND REPLACED PASSENGER CABIN AFT WET AREA TENSION STRAP STA 1028; WL 208.1 & RBL 3 IAW SRM 51-40-02-0G-0 AND DWG# 147A5730.;[02] REMOVED AND REPLACED
- [SDR SWAA2024101637263](https://openairdocs.org/sdr/SWAA2024101637263.md): Nut Plate · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > MULTIPLE SPOT WITH CORROSION ON FCB FWD BULKHEAD CENTER SUPPORT NUTPLATE (6 EACH).<[01] REMOVED AND INSTALLED NEW 6EA RECEPTACLES<BR>IAW SRM 51-40-02 AND DWG 453A1600 REV -<BR>FCB FWD BULKHEAD CENTER SUPPORT<BR>BS400 LBL20-RBL20 WL158;[02] VERIFIED CORRECTIVE
- [SDR SWAA2024101637265](https://openairdocs.org/sdr/SWAA2024101637265.md): Support · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCB AFT BULKHEAD RH SIDE SUPPORT TOP CORNER AT BS 500D; WL194.<[01] FAULT RESOLVED ON FAULT TTG8Q00VUEL8;[02] REPAIRED ON TTG8Q00VUEL8 PER EA 24-153-02618;[03] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024101639183](https://openairdocs.org/sdr/SWAA2024101639183.md): Shield · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCB AFT SHIELD AT BS 500+24 RBL 25 WL 156.<[01] REMOVED AND REPLACED FCB AFT SHIELD <BR>IAW SRM 51-40-02 <BR>AND DWG # 143A0080 REV: -;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024101637281](https://openairdocs.org/sdr/SWAA2024101637281.md): Floor Support · cracked · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; INTERCOSTAL FOUND WITH CRACK AT BS 277 TO BS 294.5 WL 208 BL 0 MARKED.<[01] REMOVED AND REPLACED INTERCOSTAL BS 277 TO BS 294.5 WL 208 BL 0. P/N 141A5410U3 LOT#240023 IAW SRM 51-40-02 AND DWG 141A5400 REV-;[02] VERIFI
- [SDR SWAA2024101637283](https://openairdocs.org/sdr/SWAA2024101637283.md): Floor Support · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN COMPARTMENT FLOOR STRUCTURE; BRACKET FOUND WITH CORROSION AT BS312 LBL55 WL208 MARKED.<[01] REMOVED AND REPLACED BRACKET AT BS 312 LBL 55 WL 208.1 IAW SRM 51-40-02; AMM 20-50-11 AND DWG 141A5220 REV:-;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; C
- [SDR SWAA2024101637289](https://openairdocs.org/sdr/SWAA2024101637289.md): Sill Drain · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WITH CORROSION; BS294 TO BS312 WL208 LBL55 (MARKED).<[01] REMOVED AND REPLACED FORWARD CABIN COMPARTMENT ON FLOOR WET AREA MOP SILL WL208 LBL55 BS 277 - BS 360. PER SRM 51-40-02 AND DWG 141A8110.;[02] REMOVE
- [SDR SWAA2024101537277](https://openairdocs.org/sdr/SWAA2024101537277.md): Floor Support · cracked · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BS 380 TO BS 400 WL 208 LBL 13 FOUND WITH CRACK (L/H) MARKED.<[01] REMOVED AND REPLACED (1EA.) UPPER CHORD IN THE FORWARD CABIN PASSENGER COMPARTMENT FLOOR STRUCTURE BETWEEN BS 380 AND BS 400 WL 2
- [SDR SWAA2024101537039](https://openairdocs.org/sdr/SWAA2024101537039.md): Web · corroded · Sep 12, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN AFT WET AREA; FOUND CORROSION AT FLOOR WEB STA 1030; WL 208.1 & RBL 5 APPROX.<[01] REMOVED CORROSION AND REWORKED AFFECTED AREA AT PASSENGER CABIN AFT WET AREA; AT FLOOR WEB STA 1030; WL 208.1; RBL 5 APPROX. IAW EA 24-153-02532.;[02] VERIFIED C
- [SDR SWAA2024101636350](https://openairdocs.org/sdr/SWAA2024101636350.md): Floor Panel · pulled · Sep 11, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241UF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024101635741](https://openairdocs.org/sdr/SWAA2024101635741.md): Scuff Plate · cracked · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FORWARD SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] AFT CARGO BAY FWD SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1;[03] CORRECTED MEASUREMENTS;[04] CORRECTED MEASUREMENTS;[05] VERIFIED COMPLETE
- [SDR SWAA2024101635740](https://openairdocs.org/sdr/SWAA2024101635740.md): Scuff Plate · cracked · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED.<[01] ALL STEPS COMPLETED;[02] REPAIRED FCB AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.<BR>WILL BE INSTALLED ON CUSTOMER CARD:TTG8Q00VRMF3.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREME
- [SDR SWAA2024101635950](https://openairdocs.org/sdr/SWAA2024101635950.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0007.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024101635951](https://openairdocs.org/sdr/SWAA2024101635951.md): Floor Panel · debonded · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF LOWER SKIN HAS AREAS OF DISBONDS. (MARKED)<[01] FLOOR PANEL 231ZF LOWER SKIN WITH AREAS OF DISBONDS AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE A
- [SDR SWAA2024101635965](https://openairdocs.org/sdr/SWAA2024101635965.md): Floor Panel · damaged · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242XF CENTER AREA OF PANEL IS SOFT.<[01] AFT FLOOR PANEL 242XF WITH CENTER AREA OF PANEL BEING SOFT WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024101635953](https://openairdocs.org/sdr/SWAA2024101635953.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024101635955](https://openairdocs.org/sdr/SWAA2024101635955.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024101635957](https://openairdocs.org/sdr/SWAA2024101635957.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ABF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE
- [SDR SWAA2024101635961](https://openairdocs.org/sdr/SWAA2024101635961.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF; UPPER SKIN; AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024101635963](https://openairdocs.org/sdr/SWAA2024101635963.md): Floor Panel · pulled · Sep 10, 2024 · N263WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH PULLED STRANDS ON UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Next page: https://openairdocs.org/aircraft/N263WN/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 = 'N263WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N263WN/reports

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