# Service difficulty reports: N218WN A list on [N218WN](https://openairdocs.org/aircraft/N218WN.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 · 281 reports - [SDR SWAA2026102116002](https://openairdocs.org/sdr/SWAA2026102116002.md): Lamp · inoperative · Oct 17, 2026 · N218WN · Boeing 7377H4 · Emergency Lighting > RIGHT FWD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LAMP IAW AMM 33-51-04. OPS CHKD SATISFACTORY. - [SDR SWAA2026100556763](https://openairdocs.org/sdr/SWAA2026100556763.md): Collector · abnormal · Oct 3, 2026 · N218WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle > NR 1 ENGINE CANDLING AFTER SHUT DOWN FOR ABOUT 5-7 MINUTES. REMOVED AND REPLACED IAW AMM 71-00-00-800-803-F00, INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTINGUISHING AGENTS OR HIGH NACELLE TEMPERATURE. - [SDR SWAA2026092906455](https://openairdocs.org/sdr/SWAA2026092906455.md): Lamp · inoperative · Sep 25, 2026 · N218WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHT AT R1 DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-04-960-801. - [SDR SWAA2026090301846](https://openairdocs.org/sdr/SWAA2026090301846.md): Strut · cracked · Aug 30, 2026 · N218WN · Boeing 7377H4 · Engine Mount Section > NR 1 ENGINE TURBINE REAR FRAME HAD A CRACK ON STRUT NR 15 AT C2, LOCATION MEASURING 0.0895" CW EA M-21-172-00808 NR 1 ENG TURBINE REAR FRAME TO REINSP EVERY 4700CYC - [SDR SWAA2026081077807](https://openairdocs.org/sdr/SWAA2026081077807.md): Light · inoperative · Aug 5, 2026 · N218WN · Boeing 7377H4 · Emergency Lighting > FO EMERGENCY EXIT DOOR INTERNAL EMERGENCY LIGHT INOPERATIVE. R & R IAW AMM 33-51-04-960-801. - [SDR SWAA2026062314655](https://openairdocs.org/sdr/SWAA2026062314655.md): Seat · faulted · Jun 21, 2026 · N218WN · Boeing 7377H4 · Passenger Compartment Equipment > SEAT 15 DEF WONT STAY UP. TIGHTENED AFFECTED SEAT ROW AS REQUIRED IAW CMM 25-21-45. - [SDR SWAA2026061511252](https://openairdocs.org/sdr/SWAA2026061511252.md): Sign · broken · Jun 10, 2026 · N218WN · Boeing 7377H4 · Emergency Lighting > MID-CABIN CEILING EXIT SIGN BROKEN. REMOVED AND REPLACED OVERWING CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01. - [SDR SWAA2025091113796](https://openairdocs.org/sdr/SWAA2025091113796.md): Battery · no test · Sep 11, 2025 · N218WN · Boeing 7377H4 · Emergency Equipment > FA REPORTS AFT EMERGENCY FLASH LIGHT WONT TEST. REPLACED AFT INBOARD FLASHLIGHT BATTERY. OPS CHECK OKAY. REF AMM 25-64-00 - [SDR SWAA2025082206432](https://openairdocs.org/sdr/SWAA2025082206432.md): Acm · seized · Aug 19, 2025 · N218WN · Boeing 7377H4 · Cabin Cooling System > WITH MAX COOLING FROM THE APU; AFTER ABOUT 10 MINUTES; SMOKE FILLED THE CABIN AND AN ACRID SMELL WAS NOTICED. THE PACKS AND RECIRC FAN WERE TURNED OFF AND THE SMOKE DISAPATED.<[01] DURING INSPECTION OF FAULT FOUND RIGHT ACM SEIZED.;[02] PERFORMED SMOKE OR FUME - [SDR SWAA2025051670801](https://openairdocs.org/sdr/SWAA2025051670801.md): Flashlight · inoperative · May 13, 2025 · N218WN · Boeing 7377H4 · Emergency Equipment > FWD FLASHLIGHT (FA) INOP<[01] R+R FWD FA FLASHLIGHT PER AMM 33-55-00.
OPS CHECKS GOOD. - [SDR SWAA2025040721696](https://openairdocs.org/sdr/SWAA2025040721696.md): Lens · out of adjust · Apr 4, 2025 · N218WN · Boeing 7377H4 · Emergency Lighting > R1 OVERDOOR EXIT SIGN LENS FALLING<[01] R&R OVERDOOR EXIT SIGN ASSY PER AMM 33-51-01 - [SDR SWAA2025032608223](https://openairdocs.org/sdr/SWAA2025032608223.md): Handle · broken · Mar 22, 2025 · N218WN · Boeing 7377H4 · Passenger/Crew Doors > L-2 DOOR ASSIST HANDLE IS BROKEN IN TWO HALVES. REPLACED L-2 DOOR ASSIST HANDLE IAW AMM-52-13-31-400-802 ITEM G STEP 2. - [SDR SWAA2025032607422](https://openairdocs.org/sdr/SWAA2025032607422.md): Battery Pack · inoperative · Mar 19, 2025 · N218WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY M1668 IAW AMM 33-51-06-960-805.
OPS CHECK GOOD.
WN50148;[02] VERIFIED ITEM 1
C/W - [SDR SWAA2025032601595](https://openairdocs.org/sdr/SWAA2025032601595.md): Floor Panel · pulled · Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > PASSENGER CABIN FLOOR PANEL 231UF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032601596](https://openairdocs.org/sdr/SWAA2025032601596.md): Floor Panel · pulled · Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > PASSENGER CABIN FLOOR PANEL 231LF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032601597](https://openairdocs.org/sdr/SWAA2025032601597.md): Floor Panel · pulled · Mar 3, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > PASSENGER CABIN FLOOR PANEL 231KF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032601326](https://openairdocs.org/sdr/SWAA2025032601326.md): Attach Angle · cracked · Mar 2, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CENTER TANK REAR SPAR LEFT HAND LOWER ATTACH ANGLE COMMON TO STA663 VAPOR BARRIER WEB IS CRACKED AT FASTENER HOLE OUTBOARD OF LBL 6.13; WL 169<[01] REMOVED AND REPLACED CENTER TANK REAR SPAR LEFT HAND LOWER ATTACH ANGLE IAW B737-700 SRM 57-10-10-2R-5;[02] EDIT - [SDR SWAA2025032601193](https://openairdocs.org/sdr/SWAA2025032601193.md): Skin · cracked · Mar 1, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > #2 TANK UPPER SKIN (INTERNAL) BETWEEN RIB 21 AND RIB 22; AFT UPPER STRINGER END IS CRACKED.<[01] CRACK ON #2 FUEL TANK (INTERNAL). AFT UPPER STRINGER; BETWEEN RIBS 21 AND 22 WAS REPAIRED IAW EA 25-157-00566-WIP1 AND EA 25-157-00566;[02] C/W - [SDR SWAA2025032600387](https://openairdocs.org/sdr/SWAA2025032600387.md): Floor Panel · pulled · Feb 27, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > DOT A24-12 AFT CABIN FLOOR PANEL 241ADF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032600477](https://openairdocs.org/sdr/SWAA2025032600477.md): Floor Panel · pulled · Feb 27, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > DOT A24-12 FORWARD CABIN FLOOR PANEL 222DF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032600043](https://openairdocs.org/sdr/SWAA2025032600043.md): Support Angle · corroded · Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (147-91) R1 DOOR CREASE BEAM SUPPORT ANGLE HAS CORROSION AT STA 332.1-10' TOP SIDE (MARKED)<[01] REMOVED DAMAGE IAW SRM 53-10-15-1A-2 STEP: 4.C
01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - - [SDR SWAA2025032600040](https://openairdocs.org/sdr/SWAA2025032600040.md): Floor Panel · pulled · Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > (151- DOT 015) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241DF.<[01] ALL STEPS EA 25-153-00560; WORK ACCOMPLISHED IAW B737 SRM 53-00-50-2R-1.;[02] COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032600041](https://openairdocs.org/sdr/SWAA2025032600041.md): Floor Panel · pulled · Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > (151- DOT 016) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242DF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE AND AUDIT COMPLETE.;[03] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032600045](https://openairdocs.org/sdr/SWAA2025032600045.md): Floor Panel · pulled · Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > (151- DOT 017) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 241EF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE;[04] COMPLETE AND AUDIT COMPLETE - [SDR SWAA2025032600042](https://openairdocs.org/sdr/SWAA2025032600042.md): Floor Panel · pulled · Feb 26, 2025 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > (151- DOT 018) PULLED FIBERS ON TOP SIDE OF CABIN FLOOR PANEL 242CF.<[01] REFER TO FAULT TTG8Q00YYRBQ WHERE EA 25-153-00560 WAS ADDED AS A SUBTASK.;[02] COMPLETE.;[03] COMPLETE;[04] COMPLETE AND AUDIT COMPLETE. - [SDR SWAA2025032699636](https://openairdocs.org/sdr/SWAA2025032699636.md): Panel · cracked · Feb 25, 2025 · N218WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > (147-80) L/H HORZ PANEL 333AT GAP COVER FIN HAS CRACK<[01] REMOVED AND REINSTALLED GAP COVER SEAL TO F.O.M ON PANEL 333AT; THEN THE GAP COVER FIN WAS REMOVED DUE TO A CRACK; AND A NEW FIN WAS INSTALLED ON PANEL 333AT. MAINTENACE WAS DONE PER SRM 51-40-02-0G-0 - [SDR SWAA2025032699171](https://openairdocs.org/sdr/SWAA2025032699171.md): Strap · corroded · Feb 24, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > DOT#07 A-043 AFT CARGO COMPARTMENT FLOORBOARD STRAP CORRODED AT STA 887 RBL 20 TO LBL 10 WL 156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO COMPARTMENT FLOORBOARD STRAP AT STA 887 RBL 20 TO LBL 10 WL 156 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED ON SHEL - [SDR SWAA2025032698984](https://openairdocs.org/sdr/SWAA2025032698984.md): Pressure Deck · cracked · Feb 24, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Structure > A177-001 HORIZONTAL PRESSURE DECK WEB STA 665; RBL 43; WL 202 HAS A.50' CRACK IN WEB. VERIFIED WITH HFEC AND MARKED ENDS IN BLACK.<[01] 04 - REPAIRED HORIZONTAL PRESSURE DECK WEB BETWEEN RBL 38.5 TO RBL 60 AND BETWEEN STA 663.75 TO STA 675PER [SRM 53-40-51-2R - [SDR SWAA2025032699172](https://openairdocs.org/sdr/SWAA2025032699172.md): Angle · corroded · Feb 24, 2025 · N218WN · Boeing 7377H4 · Cargo Compartments > DOT#08 A-043 AFT CARGO COMPARTMENT AFT BKHD LOWER STAINTION ANGLE CORRODED AT STA 947.5 RBL 20 TO LBL 10 WL 156<[01] REMOVED CORROSION AFT CARGO COMPARTMENT AFT BKHD LOWER ANGLE IAW SRM 51-10-02-0G-0 ITEM 15 EVALUATED ALLOWABLE LIMITS.090 ORIG 'T'.045 REMAIN - [SDR SWAA2025032699175](https://openairdocs.org/sdr/SWAA2025032699175.md): Escape Rope · frayed · Feb 24, 2025 · N218WN · Boeing 7377H4 · Emergency Equipment > RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE STARTING TO FRAY<[01] REPLACED RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE I/A/W AMM 25-61-10-400-802 STEP 6;[02] REMOVED & INSTALLED RIGHT EMERGENCY ESCAPE HATCH ESCAPE ROPE I/A/W AMM 25-61-10-000-802 & AMM 25-61-10-400-8 - [SDR SWAA2025032699174](https://openairdocs.org/sdr/SWAA2025032699174.md): Skin · delaminated · Feb 24, 2025 · N218WN · Boeing 7377H4 · Trailing Edge Flaps > DOT#09 A-043 LH WING; OTBD AFT FLAP INBD LOWER CORNER DELAMINATED<[01] REPAIRED LH WING OUTBD AFT FLAP INBD CORNER IAW B737 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0.;[02] VERIFIED ITEM 1
C/W - [SDR SWAA2025033198409](https://openairdocs.org/sdr/SWAA2025033198409.md): Support Bracket · cracked · Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A125-13) AFT CARGO BAY; PANEL SUPPORT BRACKET ATTACHED TO FWD BULKHEAD CRACKED; BS727; RBL04; WL162<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] AUDIT C/W - [SDR SWAA2025032698397](https://openairdocs.org/sdr/SWAA2025032698397.md): Threshold · corroded · Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A125-01) AFT CARGO BAY; DOOR LOWER THRESHOLD CORRODED; BS787+8' - BS847; RBL21-RBL29; WL156<[01] REMOVED CORROSION AND EVALUATED.045 ORIG 'T'.033 REMAINING.012 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND DW - [SDR SWAA2025032698398](https://openairdocs.org/sdr/SWAA2025032698398.md): Shield · corroded · Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A125-02) AFT CARGO BAY; DOOR FWD SHIELD CORRODED; BS767 - BS787+8'; RBL21; WL156<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] COMPLETE
AUDIT C/W;[03] COMPLETE;[04] C - [SDR SWAA2025032698399](https://openairdocs.org/sdr/SWAA2025032698399.md): Floor Support · corroded · Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A125-03) AFT CARGO BAY; FLOOR LATERAL UNION CORRODED; BS767+5'; RBL22-LBL22; WL156<[01] REMOVED AND REPLACED ON SHELF AFT CARGO BAY; FLOOR LATERAL UNION P/N 146A9401-4 ISSUE TAG WN49235 IAW IPC 53-42-11-30; SRM 51-40-02-0G-0;[02] VERIFIED TASK COMPLETE

(A125-04) AFT CARGO BAY; DOOR FWD SHIELD; UNDERLYING STRUCTURE - ANGLE CORRODED; BS767 - BS787+8'; RBL22; WL156<[01] VERIFIED 100% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLAED ANGLE IAWSRM 51-40-02-0G-0 AND DWG 146A8123 REV:-;[02 - [SDR SWAA2025032698925](https://openairdocs.org/sdr/SWAA2025032698925.md): Skin · pulled · Feb 23, 2025 · N218WN · Boeing 7377H4 · Wing, Plate/Skin > (147-73) R/H WING L/E INBOARD OF THE NACELLE STRUT SKIN HAS PULLED FASTENERS (MARKED) AFT END<[01] 04 - REPAIRED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIR - PERMANENT)];[02 - [SDR SWAA2025032698926](https://openairdocs.org/sdr/SWAA2025032698926.md): Skin · pulled · Feb 23, 2025 · N218WN · Boeing 7377H4 · Wing, Plate/Skin > (147-74) R/H WING L/E SKIN INBOARD OF THE NACELLE STRUT HAS PULLED FASTENER (MARKED) AFT AND I/B END<[01] 01 - REMOVED AND REPLACED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIR - [SDR SWAA2025032698406](https://openairdocs.org/sdr/SWAA2025032698406.md): Angle · corroded · Feb 23, 2025 · N218WN · Boeing 7377H4 · Cargo Compartments > (A125-07) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS767; RBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS767; RBL22 ACCOMPLISHED 10X MAG IAW SRM 51-10-02 VERIFIED MATERIAL LOSS TO BE ORIG.040'; LOSS.008'; REMAINING.032' FOUND TO BE OUT O - [SDR SWAA2025032698407](https://openairdocs.org/sdr/SWAA2025032698407.md): Angle · corroded · Feb 23, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A125-08) AFT CARGO BAY; Z-ANGLE CORRODED; BS727 - BS847; LBL22; WL156<[01] BLENDED CORROSION ON AFT CARGO Z-ANGLE BS727 - BS847; LBL22 VERIFIED TO 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO L/H Z-ANGLE STA 727 - STA 847 IAW S - [SDR SWAA2025032698383](https://openairdocs.org/sdr/SWAA2025032698383.md): Baffle · cracked · Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A204 DOT 45) FORWARD CARGO STA 500 TO 500A; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED IN 2EA PLACES.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] AND BOEING DWG: 143A7505 REV - [SDR SWAA2025032698384](https://openairdocs.org/sdr/SWAA2025032698384.md): Baffle · cracked · Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A204 DOT 46) FORWARD CARGO. STA 440+10; STR 26L; Z-ANGLE BAFFLE PLATE IS CRACKED AT FASTNER HOLE.<[01] REMOVED BAFFLE IAW SRM 51-40-02-0G-0 RECEIVED REPLACEMENT BAFFLE PN 143A7510-9 TAG WN3413 AND VERIFIED IT TO BE CORRECT REPLACEMENT PART IAW BOEING DWG 143A - [SDR SWAA2025032698389](https://openairdocs.org/sdr/SWAA2025032698389.md): Stringer Clip · cracked · Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > (A204 DOT 54) FORWARD CARGO. STA 500D; STR 19L; STRINGER CLIP GUSSET IS CRACKED IN RADIUS COMMON TO BULKHEAD SUPPORT.<[01] REMOVED AND REPLACED STA 500D; STR 19L; STRINGER CLIP GUSSET I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 143A7902; SHEET 172; REV -;[02] VERI - [SDR SWAA2025032698394](https://openairdocs.org/sdr/SWAA2025032698394.md): Stringer Clip · cracked · Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > (A204 DOT 55) FORWARD CARGO; STA 500D; STR 21L; STRINGER CLIP GUSSET CRACKED COMMON TO BULKHEAD SUPPORT.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
APPLIED CIC IAW AMM 5 - [SDR SWAA2025032698385](https://openairdocs.org/sdr/SWAA2025032698385.md): Angle · corroded · Feb 22, 2025 · N218WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > (A204 DOT 47) FORWARD CARGO STA 500A TO 500D; LBL 21; WL 159; Z-ANGLE HAS CORROSION AROUND NUTPLATE HOLES.<[01] 04 - REPAIRED PER [SRM 53-00-53-2R-5-A00957 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[02] VERIFIED S - [SDR SWAA2024111858841](https://openairdocs.org/sdr/SWAA2024111858841.md): Battery Pack · failed · Nov 12, 2024 · N218WN · Boeing 7377H4 · Emergency Lighting > PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK M1675 IAW AMM 33-51-06. - [SDR SWAA2024111858820](https://openairdocs.org/sdr/SWAA2024111858820.md): Panel · cracked · Nov 12, 2024 · N218WN · Boeing 7377H4 · Fuselage Floor Panel > -CABIN FLOORBOARD PNL BREAKS CRACKED STA. 540 BETWEEN FLOORBOARDS 231XF AND 231UF BOTH SIDES LEFT AND RIGHT.<[01] R&R CABIN FLOORBOARD PANEL BREAKS/INTERCOSTALS LH & RH SIDES AT STA. 540 BETWEEN FLOORBOARDS 231XF & 231UF IAW SRM 51-40-02. STILL NEEDS FLOORBOAR - [SDR SWAA2024111858821](https://openairdocs.org/sdr/SWAA2024111858821.md): Girt Bar · loose · Nov 12, 2024 · N218WN · Boeing 7377H4 · Escape Slide > R1 DOOR SLIDE AFT GIRT BAR BRACKET RIVET LOOSE<[01] REMOVED AND REPLACED RIVETS FOR R1 DOOR SLIDE AFT GIRT BAR BRACKET PER SRM 51-40-02. - [SDR SWAA2024111858822](https://openairdocs.org/sdr/SWAA2024111858822.md): Girt Bar · out of adjust · Nov 12, 2024 · N218WN · Boeing 7377H4 · Escape Slide > L1 DOOR SLIDE GIRT NOT SECURED WITH VELCRO<[01] RE-SECURED L1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01. - [SDR SWAA2024111858835](https://openairdocs.org/sdr/SWAA2024111858835.md): Seal · cracked · Nov 12, 2024 · N218WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > R/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL IS CRACKED 4 PARALLEL TO SLIDING SEAL LEADING EDGE.<[01] R&R RH HORIZONTAL STABILIZER FRONT UPPER SLIDING SEAL REF. AMM 53-31-31. Next page: https://openairdocs.org/aircraft/N218WN/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 = 'N218WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N218WN/reports --- 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.