# Service difficulty reports: N277WN

A list on [N277WN](https://openairdocs.org/aircraft/N277WN.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 7 · 325 reports

- [SDR SWAA2026091609662](https://openairdocs.org/sdr/SWAA2026091609662.md): Floor Panel · cracked · Sep 12, 2026 · N277WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR CRACKED PATCHED AFT CARGO FLOOR CRACK REF AMM 25-52-01
- [SDR SWAA2026082880719](https://openairdocs.org/sdr/SWAA2026082880719.md): Landing Gear · malfunctioned · Aug 24, 2026 · N277WN · Boeing 7377H4 · Landing Gear Retraction/Extension System
  > WHILE MOVING THE LANDING GEAR HANDLE FROM UP TO OFF, THE GEAR INADVERTENTLY EXTENDED. RETRACTED LANDING GEAR AT 245 KTS WHILE MOVING THE LANDING GEAR HANDLE FROM UP TO OFF THE GEAR INADVERTENTLY EXTENDED. RETRACTED LANDING GEAR AT 245 KTS ACCOMPLISHED LANDING
- [SDR SWAA2026081229979](https://openairdocs.org/sdr/SWAA2026081229979.md): Handle · loose · Aug 8, 2026 · N277WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR CABIN SIDE AFT DOOR ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR AFT SIDE ASSIST HANDLE IAW AMM 52-11-31. CONFIRMED FWD ENTRY DOOR AFT DOOR ASSIST HANDLE SECURED IAW 52-11-31.
- [SDR SWAA2026073070458](https://openairdocs.org/sdr/SWAA2026073070458.md): Bulb · inoperative · Jul 26, 2026 · N277WN · Boeing 7377H4 · Emergency Lighting
  > AFT LAV EMERGENCY LIGHT BULB OUT RELAMPED AFT LAV AUXILIARY LIGHT IAW AMM 25-42-60. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-00.
- [SDR SWAA2026030274512](https://openairdocs.org/sdr/SWAA2026030274512.md): Cowl Door · pulled · Feb 26, 2026 · N277WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > NR 2 ENG INLET COWL HAS TWO PULLED THRU FASTENERS AND ONE MISSING FASTENER ON AFT BULKHEAD AT 3 O`CLOCK POSITION VIEWING AFT FACING FWD. R & R THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01.
- [SDR SWAA2025081804817](https://openairdocs.org/sdr/SWAA2025081804817.md): Lens · loose · Aug 15, 2025 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR EMERGENCY EXIT LIGHT LENS AT L1 DOOR APPEARS LOOSE. SECURED LIGHT ASSEMBLY PER AMM 33-51-04.
- [SDR SWAA2025060577224](https://openairdocs.org/sdr/SWAA2025060577224.md): Light · inoperative · Jun 2, 2025 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BY L1 DOOR INOP <[01]. RELAMPED L1 OUTSIDE EMERGENCY LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025041423361](https://openairdocs.org/sdr/SWAA2025041423361.md): Handle · out of adjust · Apr 9, 2025 · N277WN · Boeing 7377H4 · Passenger/Crew Doors
  > 2L DOOR HANDLE HAS MORE PLAY THAN OTHER DOORS WHEN CLOSED<[01] INSPECTED ATTACH HARDWARE ON AFT L2 DOOR FOR PROPER INSTALLATION AND SECURITY. PERFORMED DOOR ENTRY SYSTEM TEST PER AMM 52-13-00. A/C OK TO CONTINUE
- [SDR SWAA2024121674393](https://openairdocs.org/sdr/SWAA2024121674393.md): Sign · loose · Dec 5, 2024 · N277WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR (L-1) EMERGENCY EXIT SIDEWALL LENS FELL OFF<[01] REMOVED & REPLACED SIDEWALL EXIT SIGN ASSAY. IAW M/M 33-51-06 & 33-51-14
- [SDR SWAA2024121673745](https://openairdocs.org/sdr/SWAA2024121673745.md): Battery · inoperative · Dec 4, 2024 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP.<[01] REPLACED AND TESTED M1672 EMERGENCY LIGHTING BATTERY M1672 PER AMM 33-51-06-960-805 AND WDM 33-51-14. ALL LIGHTS OPERATED CORRECTL
- [SDR SWAA2024121673747](https://openairdocs.org/sdr/SWAA2024121673747.md): Light · inoperative · Dec 4, 2024 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SLIDE LIGHT OUTSIDE OF FORWARD SERVICE DOOR INOP<[01] CLEANED TERMINAL LUGS AT EMERGENCY EXIT SLIDE LIGHT OUTSIDE OF FWD SERVICE DOOR. PERFORMED GOOD OP CHECK. IAW SWPM 20-10-04 AND AMM 33-51-00-710-801.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLE
- [SDR SWAA2024121673748](https://openairdocs.org/sdr/SWAA2024121673748.md): Light · inoperative · Dec 4, 2024 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LOCATOR SIGN FOR FWD ENTRY DOOR INOP<[01] REPLACED EMERGENCY EXIT LOCATOR LIGHT ASSEMBLY ON FWD LAV PER AMM 33-51-14-960-802. TERMINATED WIRE W4142-0152 INTO GROUND BLOCK GD3782 PER SWPM 20-90-15 AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY
- [SDR SWAA2024121673749](https://openairdocs.org/sdr/SWAA2024121673749.md): Light · inoperative · Dec 4, 2024 · N277WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT L/H AND R/H GROUND ILLUMINATION SLIDE LIGHTS INOP COMMON TO M1670 BATTERY PACK SEE WDM 33-51-13<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF L/H AND R/H GROUND ILLUMINATION SLIDE LIGHTS IAW AMM 33-51-04-960-801.;[02] JOB COMPLETE.
- [SDR SWAA2024121673300](https://openairdocs.org/sdr/SWAA2024121673300.md): Scuff Plate · cracked · Dec 2, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > ACB FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AND INSTALLED ACB FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1;AND JOB CARD TTG8Q00WWT6Z.;[02] REJECTION; INCORRECT SEALANT APLICATION.;[03] RE-APPLIED SEALANT TO AFT CARGO BAY FWD CORNER PER AMM 53-11-02-420
- [SDR SWAA2024121673301](https://openairdocs.org/sdr/SWAA2024121673301.md): Scuff Plate · cracked · Dec 2, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > ACB AFT CORNER SCUFF PLATE IS CRACKED<[01] REPLACED AND INSTALLED ACB AFT CORNER SCUFF PLATE PER SRM 51-10-02; AND JOB CARD TTG8Q00WWT6Z;[02] REJECTION; INCORRECT SEALANT APLICATION.;[03] RE-APPLIED SEALANT TO AFT CARGO BAY AFT CORNER PER AMM 53-11-02-420-801;
- [SDR SWAA2024121670986](https://openairdocs.org/sdr/SWAA2024121670986.md): Intercostal · cracked · Nov 23, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Structure
  > ACB; DURIN OK TO INSTALL WAS FOUND A CRACK ON INTERCOSTAL BS 947 RBL 25 BETWEEN S23R AND S24R.<[01] REMOVED AND REPLACED INTERCOSTAL BS927 TO BS947 RBL25 WL 164 BETWEEN STR23R AND STR24R IAW SRM 51-40-02-0G-0 AND DWG 147A7500 REV C.;[02] VERIFIED COMPLETION CO
- [SDR SWAA2024121670325](https://openairdocs.org/sdr/SWAA2024121670325.md): Floorbeam · corroded · Nov 21, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BEAM ASSY LOWER PANEL MIDSPAN FIXED T.E. ORSS 452; 455; 459; 466.5; 471.5; 473.5; 475.5; 477.5 (MARKED)<[01] REMOVED AND REPLACED BEAM ASSY LOWER PANEL MIDSPAN FIXED T.E. IAW SRM 51-40-02-0G-0 STEP 7;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AN
- [SDR SWAA2024121669918](https://openairdocs.org/sdr/SWAA2024121669918.md): Vapor Barrier · cracked · Nov 20, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Keel
  > L/H B.S. 663 VAPOR BARRIER IS CRACKED AT 4' I/B OF THE O/B EDGE<[01] L/H B.S. 663 VAPOR BARRIER; CRACK AT 4' I/B OF THE O/B EDGE; WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] JOB COMPLETE.
- [SDR SWAA2024121661353](https://openairdocs.org/sdr/SWAA2024121661353.md): Fitting · cracked · Nov 18, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > ACB WATER TANK ENCLOSURE FRAME ATTACH FITTING CRACKED AT BS947 LBL 9 WL156<[01] REMOVED AND INSTALLED NEW ACB WATER TANK ENCLOSURE FRAME ATTACH FITTING AT BS947 LBL 9 WL156 PER SRM 51-40-02 AND DWG 147A7500 AND DWG 149A8113 REV -;[02] VERIFIED COMPLETION CORRE
- [SDR SWAA2024121660496](https://openairdocs.org/sdr/SWAA2024121660496.md): Intercostal · corroded · Nov 15, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON INTERCOSTAL RBL21 BS500A TO BS500B WL 156 (MARKED).<[01] THE DISCREPANCY AREA WAS MANUALLY CLEANED WITH SOLVENT AND ABRASIVE PAD AND FOUND BARE METAL ONLY WITH NO MATERIAL LOSS PER SOPM 20-30-03 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER A
- [SDR SWAA2024121060497](https://openairdocs.org/sdr/SWAA2024121060497.md): Baffle · corroded · Nov 15, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL RBL21 BS500B TO BS500C WL 156 (MARKED).<[01] REMOVED AND REPLACED AT FCB BAFFLE ASSY (INTERCOSTAL) BETWEEN BS.500B - BS.500C RBL.21 WL.156 IAW B-737-700 SRM 51-40-02 DWG# 143A7505 ID:0082 REV: -;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2024121660092](https://openairdocs.org/sdr/SWAA2024121660092.md): Sidewall Support · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT FROM BS727 TO BS767;RBL21 WL157;IAW DWG#146A7500 REV A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121660097](https://openairdocs.org/sdr/SWAA2024121660097.md): Sidewall Support · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS847 LBL21 WL157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS847 LBL21 WL157 IAW SRM 51-40-02 AND DWG 146A7500 REV: A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121660106](https://openairdocs.org/sdr/SWAA2024121660106.md): Intercostal · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON INTERCOSTAL AT ACB BS773 RBL20 WL157.<[01] UPDATED MEASUREMENTS;[02] REMOVED AND REPLACED THE WEB (INTERCOSTAL) AT ACB BETWEEN BS.767 - BS.787 RBL.20 WL.157 IAW B-737-700 SRM 51-40-02 DWG#146A0081 REV: - AND DWG#146A8123 REV:;[03] UPDATE ACTION CO
- [SDR SWAA2024121660113](https://openairdocs.org/sdr/SWAA2024121660113.md): Floor Panel · delaminated · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241UF HAS UPPER SURFACE DELAMINATION<[01] FABRICATION OF NEW 241UF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS
- [SDR SWAA2024121660107](https://openairdocs.org/sdr/SWAA2024121660107.md): Track · cracked · Nov 14, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > CRACKED TRACK AT ACB BS767 RBL13 WL157<[01] REMOVED AND REPLACED ACB TRACK ON CUSTOMER CARD NO TTG8Q00X2G0N
- [SDR SWAA2024121660093](https://openairdocs.org/sdr/SWAA2024121660093.md): Support Angle · cracked · Nov 14, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL12 WL172. MARKED<[01] REMOVED AND REPLACED THE STIFFENER AT ACB BEHIND WATER SERVICE PANEL BS918 RBL12 WL172 IAW SRM 51-40-02.DWG#147A7221 REV: -;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND
- [SDR SWAA2024121660101](https://openairdocs.org/sdr/SWAA2024121660101.md): Track · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TRACK TIEDOWNS AT ACB RBL13 BS867; BS727B WL157.<[01] REMOVED AND REPLACED ACB TRACK ON CUSTOMER CARD NO. TTG8Q00X2G0N;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024121660096](https://openairdocs.org/sdr/SWAA2024121660096.md): Rail · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON RAIL AT ACB BS767+6 LBL3 WL157. MARKED<[01] REPAIRED RAIL WITH (1EA.) REINFORCING CHANNEL ON UPPER FLANGE AT JOGGLE LOCATION FROM ACB BS.767+6' LBL.3 WL157 IAW B-737-700 SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5 FIG.203;[02] VERIFIED COMPLETION COR
- [SDR SWAA2024121060099](https://openairdocs.org/sdr/SWAA2024121060099.md): Angle · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 LBL8 TO RBL16 WL179. MARKED<[01] REMOVED AND INSTALLED NEW BULKHEAD SUPPORT ANGLE ACB BS947 BETWEEN LBL 8 TO RBL 16 WL 179 PER SRM 51-40-02 AND DWG 149A8110 REV -;[02] VERIFIED COMPLETION CORRECTIVE
- [SDR SWAA2024121060108](https://openairdocs.org/sdr/SWAA2024121060108.md): Track · cracked · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED TRACK AT ACB BS727E RBL13 WL157<[01] REMOVED AND REPLACED ACB FLOOR TRACK FROM BS-727 TO BS-887; RBL 13 WL 157.IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV: A;[02] TASK CARD COMPLETE.
- [SDR SWAA2024121074920](https://openairdocs.org/sdr/SWAA2024121074920.md): Rail · corroded · Nov 14, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON RAIL AT ACB BS727D+6 RBL13 WL157.<[01] REMOVED AND REPLACED ACB TRACK ON CUSTOMER CARD NO. TTG8Q00X2G0N
- [SDR SWAA2024121659718](https://openairdocs.org/sdr/SWAA2024121659718.md): Scuff Plate · cracked · Nov 13, 2024 · N277WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED THE RADIUS OF THE FWD CARGO FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARA 4.B(4). REFERRED TO BAC5975<BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO TH
- [SDR SWAA2024121659035](https://openairdocs.org/sdr/SWAA2024121659035.md): Stringer · corroded · Nov 12, 2024 · N277WN · Boeing 7377H4 · Fuselage Floor Panel
  > DURING OK TO CIC FOUND CORROSION ON BILGE AREA OF ELECTRICAL AND ELECTRONICS COMPARTMENT AT S-28R; BS 368 WL 148.8. (MARKED)<[01] REMOVED DAMAGE FOR CORROSION ON BILGE AREA OF ELECTRICAL AND ELECTRONICS COMPARTMENT AT S-28R; BS 368 WL 148.8. IAW SRM 53-00-03-2
- [SDR SWAA2024121658797](https://openairdocs.org/sdr/SWAA2024121658797.md): Shield · corroded · Nov 11, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > ACB; FLOOR SHIELD HAS CORROSION AT BS 767+7; BS 767+11; RBL 25; WL 160.<[01] REMOVED AND REPLACED FWD SHIELD ON ACB BETWEEN BS 767 -BS 794.25 RBL.25 WL.160 IAW B-737-700 SRM 51-40-02 DWG#146A0081 REV:-;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREME
- [SDR SWAA2024121658799](https://openairdocs.org/sdr/SWAA2024121658799.md): Shield · corroded · Nov 11, 2024 · N277WN · Boeing 7377H4 · Cargo Compartments
  > ACB; FLOOR SHIELD HAS CORROSION AT BS 847+11; RBL 25; WL 160.<[01] REMOVED AND REPLACED AT ACB AFT SHIELD BETWEEN BS.847 - BS.867 RBL.25 WL.160 IAW B-737-700 SRM 51-40-02 & DWG# 146A0081 REV: -;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
- [SDR SWAA2024121658778](https://openairdocs.org/sdr/SWAA2024121658778.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STR CLIP 4L IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 4L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658785](https://openairdocs.org/sdr/SWAA2024121658785.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 4L IS CRACKED AT BS 727E.<[01] REMOVED AND EPLACED STRINGER CLIP 4L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024121658779](https://openairdocs.org/sdr/SWAA2024121658779.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 5L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658780](https://openairdocs.org/sdr/SWAA2024121658780.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727A.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727A STR 5R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658781](https://openairdocs.org/sdr/SWAA2024121658781.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 5R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658782](https://openairdocs.org/sdr/SWAA2024121658782.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 6R IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 6R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658783](https://openairdocs.org/sdr/SWAA2024121658783.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 4R IS CRACKED AT BS 727D.<[01] REMOVED AND REPLACED NEW STRINGER CLIP P/N#143A1010-1 AT BS 727D STR 4R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658795](https://openairdocs.org/sdr/SWAA2024121658795.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 5R BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024121658784](https://openairdocs.org/sdr/SWAA2024121658784.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 6R IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 6R BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024121658786](https://openairdocs.org/sdr/SWAA2024121658786.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 5L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-.AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024121658787](https://openairdocs.org/sdr/SWAA2024121658787.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 6L IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 6L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024121658788](https://openairdocs.org/sdr/SWAA2024121658788.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 4L IS CRACKED AT BS 767.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 767 STR 4L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658789](https://openairdocs.org/sdr/SWAA2024121658789.md): Stringer Clip · cracked · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > INTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 767.<[01] REMOVED AND REPLACED NEW STRINGER CLIP P/N#143A1010-1 AT BS 767 STR 5L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024121658798](https://openairdocs.org/sdr/SWAA2024121658798.md): Web · corroded · Nov 11, 2024 · N277WN · Boeing 7377H4 · Fuselage Main, Structure
  > ACB; FLOOR THRESHOLD WEB HAS CORROSION FROM BS 787+18 TO BS 827+11; RBL 28 WL 160 IN VARIOUS LOCATIONS MARKED.<[01] REMOVED AND REPLACED THRESHOLD WEB FROM BS794.37 TO BS847;IAW SRM 51-40-02 AND DWG#146A8340 REV A.;[02] VERIFIED CORRECTIVE ACTION #1

Next page: https://openairdocs.org/aircraft/N277WN/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 = 'N277WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N277WN/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.