# Service difficulty reports: N212WN A list on [N212WN](https://openairdocs.org/aircraft/N212WN.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 · 302 reports - [SDR SWAA2026081943593](https://openairdocs.org/sdr/SWAA2026081943593.md): Packing · leaking · Aug 15, 2026 · N212WN · Boeing 7377H4 · Engine Fuel Distribution > OTS - NR 1 ENGINE FLUID LEAK FROM FAN COWLS, COMPLIED WITH E.A. M-21-173-01075 PERFORMED NR 1 ENG. IDLE LEAK CHECKED IAW AMM 71-00-00. - [SDR SWAA2026081794365](https://openairdocs.org/sdr/SWAA2026081794365.md): Battery Pack · inoperative · Aug 12, 2026 · N212WN · Boeing 7377H4 · Emergency Lighting > LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK M1670 IAW AMM 33-51-06-960-805. OPS TESTED GOOD. NO DEFECTS NOTED. - [SDR SWAA2026081727766](https://openairdocs.org/sdr/SWAA2026081727766.md): Battery Pack · inoperative · Aug 12, 2026 · N212WN · Boeing 7377H4 · Emergency Lighting > RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK M1670 IAW AMM 33-51-06-960-805. OPS TESTED GOOD. - [SDR SWAA2026062213163](https://openairdocs.org/sdr/SWAA2026062213163.md): Slide · out of position · Jun 16, 2026 · N212WN · Boeing 7377H4 · Escape Slide > CREW REPORTS AFT LT SLIDE NEEDS REPOSITIONED. RE-PACKED SLIDE AS REQUIRED AFT LT IAW MT 725-66-01 - [SDR SWAA2026061110418](https://openairdocs.org/sdr/SWAA2026061110418.md): Slide · dislodged · Jun 8, 2026 · N212WN · Boeing 7377H4 · Escape Slide > FWD ENTRY DOOR SLIDE L1 FELL OUT OF CONTAINER. REMOVED AND REPLACED L1 DOOR SLIDE IAW MT 75-61-06. - [SDR SWAA2026033183502](https://openairdocs.org/sdr/SWAA2026033183502.md): Window · cracked · Mar 26, 2026 · N212WN · Boeing 7377H4 · Flight Compartment Windows > FO RIGHT SIDE WINDOW CRACKED. REMOVED & REPLACED #2 OPENABLE WINDOW ASSY PER MT#756-12-03. - [SDR SWAA2025110631582](https://openairdocs.org/sdr/SWAA2025110631582.md): Girt Bar · loose · Nov 4, 2025 · N212WN · Boeing 7377H4 · Emergency Equipment > R1 SERVICE DOOR SLIDE FWD GIRT BAR CLIP LOOSE CORRECTED GIRT BAR CLIP PER AMM 25-66-01, NO DEFECTS NOTED. - [SDR SWAA2025050566439](https://openairdocs.org/sdr/SWAA2025050566439.md): Attach Bracket · cracked · May 2, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > FWD KEEL BEAM PANEL #192E L/H FWD ATTACH BRACKET CRACKED<[01] REMOVED AND REPLACED FWD KEEL BEAM PANEL #192E L/H FWD ATTACH BRACKET PER SRM 51-40-02. - [SDR SWAA2025041423860](https://openairdocs.org/sdr/SWAA2025041423860.md): Handle · loose · Apr 11, 2025 · N212WN · Boeing 7377H4 · Passenger/Crew Doors > ASSIST HANDLE JUST AFT OF FWD ENTRY DOOR IS LOOSE<[01] TIGHTENED ASSIST HANDLE JUST AFT OF FWD ENTRY DOOR IAW AMM 25-21-31-420-802 STEP 3.B(6).;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE. - [SDR SWAA2025041423859](https://openairdocs.org/sdr/SWAA2025041423859.md): Handle · loose · Apr 11, 2025 · N212WN · Boeing 7377H4 · Service Doors > FWD SERVICE DOOR ASSIST HANDLE IS LOOSE<[01] TIGHTENED FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31-400-802 STEP 3.F(2).;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE. - [SDR SWAA2025041423238](https://openairdocs.org/sdr/SWAA2025041423238.md): Fuse · blown · Apr 10, 2025 · N212WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 INOP<[01] REPLACED BLOWN FUSE 1F IN M1672 BATTERY CHARGER AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTERY PACK IAW AMM 33-51-06-960-804.;[02] VERIFIED ACTION 1.
JOB COMPLETE. - [SDR SWAA2025041423239](https://openairdocs.org/sdr/SWAA2025041423239.md): Bulb · inoperative · Apr 10, 2025 · N212WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LOCATOR LIGHT FWD OF R/H OWE HAS INOP BULBS<[01] RELAMPED INOP BULBS AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LOCATOR FWD OF RH OWE I.A.W AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.
JOB COMPLETE. - [SDR SWAA2025041420672](https://openairdocs.org/sdr/SWAA2025041420672.md): Scuff Plate · cracked · Apr 2, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ACB AFT CORNER SCUFF PLATE IS CRACKED.<[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975. - [SDR SWAA2025042108277](https://openairdocs.org/sdr/SWAA2025042108277.md): Web · corroded · Mar 22, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB LOWER MAIN SILL AT STA 787+7 TO STA 787+14; 787+16.5; AND 787+18; RBL18; WL152< - [SDR SWAA2025041415507](https://openairdocs.org/sdr/SWAA2025041415507.md): Web · corroded · Mar 22, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB LOWER MAIN SILL AT STA 787+7 TO STA 787+14; 787+16.5; AND 787+18; RBL18; WL152<[01] REMOVED AND REPLACED ACB LOWER MAIN SILL WEB BS 787+6 TO BS 847 RBL18; WL152 IAW SRM 51-40-02 AND DWG# 146A8120 ID:0031 REV: - AND DWG# 146A8121 ID:0005 REV: - - [SDR SWAA2025041407820](https://openairdocs.org/sdr/SWAA2025041407820.md): Stringer Clip · cracked · Mar 20, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STR CLIP AT PAX CABIN BS727E S-4R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP BS 727E; S-4R PER SRM 51-10-02; 51-40-02 AND DWG 146A1112 REV:-;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025041407821](https://openairdocs.org/sdr/SWAA2025041407821.md): Stringer Clip · cracked · Mar 20, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP BS 727D; S-4R PER SRM 51-10-02 51-40-02 AND DWG 146A1111 REV:-;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025041407822](https://openairdocs.org/sdr/SWAA2025041407822.md): Stringer Clip · cracked · Mar 20, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STR CLIP AT PAX CABIN BS727D S-6R. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6R IAW SRM 51-40-02-0G-0 AND DWG 146A1111.;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025041407823](https://openairdocs.org/sdr/SWAA2025041407823.md): Stringer Clip · cracked · Mar 20, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STR CLIP AT PAX CABIN BS727C S-5R. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP PN# 143A1010U1; LOT#1598900-1 AT DISCREPANCY AREA PER SRM 51-40-02; DWG#146A1103 REV:- TASK CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025041407824](https://openairdocs.org/sdr/SWAA2025041407824.md): Stringer Clip · cracked · Mar 20, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STR CLIP AT PAX CABIN BS727B S-6R. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP PN# 143A1010U1; LOT#1598900-1 AT DISCREPANCY AREA PER SRM 51-40-02; DWG#146A1102 REV:- TASK CARD COMPLETED.;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025042107434](https://openairdocs.org/sdr/SWAA2025042107434.md): Seat Track · cracked · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > F/O'S FWD I/B SEAT TRACK CRACKED<[01] F/O'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W;[02] VERIFIED - [SDR SWAA2025042107113](https://openairdocs.org/sdr/SWAA2025042107113.md): Shield · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO 440; RBL 24; WL 156.<[01] REMOVED AND REPLACED FWD SHIELD BS 420-BS440 RBL 24 WL 156
IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG# 143A0080 REV:-
CARD COMPLETED;[02] CORRECTI - [SDR SWAA2025042107121](https://openairdocs.org/sdr/SWAA2025042107121.md): Web · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB AT STA 787+8; RBL 23; AND AT STA 827 TO 827+5; RBL 25; WL 156. - [SDR SWAA2025042107112](https://openairdocs.org/sdr/SWAA2025042107112.md): Sidewall Support · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 480+12 TO STA 500D; LBL 24; WL 157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS.480+12' - BS.500D LBL 24; WL156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [1] & SRM 51-40-02 AND DWG# 1 - [SDR SWAA2025041515494](https://openairdocs.org/sdr/SWAA2025041515494.md): Seat Track · cracked · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CAPTAIN'S FWD I/B SEAT TRACK CRACKED <[01]. CAPTAIN'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W; [02] VERIFIED ITEM 1 AND TASK CARD CLOSED. - [SDR SWAA2025041515495](https://openairdocs.org/sdr/SWAA2025041515495.md): Seat Track · cracked · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > F/O'S FWD I/B SEAT TRACK CRACKED <[01]. F/O'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W; [02] VERIFIED. - [SDR SWAA2025041407116](https://openairdocs.org/sdr/SWAA2025041407116.md): Support · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 24; FROM STA 727+18 TO STA 808+15; WL 156.<[01] REMOVED AND REPLACED FLOOR/SIDEWALL SUPPORT
IAW SRM 51-40-02 AND DWG 146A7500
ACB BS 727 TO BS 847 LBL24 WL 156;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COM - [SDR SWAA2025041407117](https://openairdocs.org/sdr/SWAA2025041407117.md): Support · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 24; FROM STA 727+4 TO STA 767; WL 158.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE. - [SDR SWAA2025041407120](https://openairdocs.org/sdr/SWAA2025041407120.md): Cargo Track · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON AFT CARGO BAY RBL 14 FLOOR RAIL AT STA 847+4; WL 156.<[01] ACB TRACK TIEDOWN WAS REPLACED IN CUSTOMER CARD TTG8Q00ZC6JA BETWEEN BS767+14 AND BS887 RBL14 WL156.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE. - [SDR SWAA2025041407109](https://openairdocs.org/sdr/SWAA2025041407109.md): Threshold Web · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO COMPARTMENT SUB THRESHOLD WEB FROM STA 440+7 TO 480+4; RBL 29; WL 156.<[01] STEPS 1-3 COMPLETED.;[02] REMOVED AND REPLACED FWD CARGO COMPARTMENT SUB THRESHOLD WEB BS 440 TO BS 500 RBL 29; WL 156 IAW SRM 51-40-0; 51-40-02 AND DGW:143A8330 - [SDR SWAA2025041415488](https://openairdocs.org/sdr/SWAA2025041415488.md): Support Angle · cracked · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE IN FCB AT STRINGER S-18L STA 500D.<[01] REMOVED AND REPLACED GUSSET WITH P/N 143A9481-6 LOT:1583773-1 AT FCB STR19L STA 500D. IAW SRM 51-40-02 & DWG#143A7902 REV: -;[02] VERIFIED - [SDR SWAA2025041415490](https://openairdocs.org/sdr/SWAA2025041415490.md): Shield · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO 440; RBL 24; WL 156.<[01] REMOVED AND REPLACED FWD SHIELD BS 420-BS440 RBL 24 WL 156
IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG# 143A0080 REV:-
CARD COMPLETED;[02] CORRECTI - [SDR SWAA2025041407118](https://openairdocs.org/sdr/SWAA2025041407118.md): Shield · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767+6 TO 767+12; RBL 25; WL 156.<[01] REMOVED AND REPLACED ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767 TO STA 787+6 RBL 25 WL 156 IAW SRM 51-40-02 AND DGW 146A0081 REV: A. - [SDR SWAA2025041415493](https://openairdocs.org/sdr/SWAA2025041415493.md): Web · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB AT STA 787+8; RBL 23; AND AT STA 827 TO 827+5; RBL 25; WL 156.<[01] REMOVED AND REPLACED NEW ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB BS794 TO BS847 RBL 23. IAW SRM 51-40-02 AND DWG 146A8340 ID:0021 REV: - [SDR SWAA2025041415489](https://openairdocs.org/sdr/SWAA2025041415489.md): Support Angle · corroded · Mar 19, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 480+12 TO STA 500D; LBL 24; WL 157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS.480+12' - BS.500D LBL 24; WL156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [1] & SRM 51-40-02 AND DWG# 1 - [SDR SWAA2025042106443](https://openairdocs.org/sdr/SWAA2025042106443.md): Pressure Deck · corroded · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Structure > CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+8 RBL 65; WL 200.<[01] 'REFER TO FAULT TTG8Q00ZBDUT WHERE EA 25-153-00723 WAS ADDED AS A SUBTASK'.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2025042106441](https://openairdocs.org/sdr/SWAA2025042106441.md): Floorbeam · cracked · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Floor Beam > STA 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-64 LOT: 1598659-1; BETWEEN BS540 BL0 TO RBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 REV:A;[02] VERIFIED CORRECTIVE ACTION ETNRY 1. - [SDR SWAA2025041706429](https://openairdocs.org/sdr/SWAA2025041706429.md): Floor Panel · pulled · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] PANEL 241DF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025041706433](https://openairdocs.org/sdr/SWAA2025041706433.md): Floor Panel · pulled · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 242AF LOWER SKIN HAS AN AREA OF PULLED STRANDS. <[01] PANEL 242AF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025041515486](https://openairdocs.org/sdr/SWAA2025041515486.md): Skin · corroded · Mar 18, 2025 · N212WN · Boeing 7377H4 · Vertical Stabilizer, Plate/Skin > CROWN SKIN UNDER VERT STAB HAS AREAS OF SURFACE CORROSION FROM STA 1016 TO STA 1040 AND S-2AL TO S-2AR (MARKED) <[01]. AS PER EA 25-153-00790; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION - [SDR SWAA2025041415461](https://openairdocs.org/sdr/SWAA2025041415461.md): Floor Panel · pulled · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025041415470](https://openairdocs.org/sdr/SWAA2025041415470.md): Stiffener · corroded · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+2; RBL 61; WL 200.<[01] REPAIR PER EA# 25-153-00723

EA-GENERAL' REPAIR REFERENCE IS SELECTED.;[02] REMOVED CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+2; RBL 61; WL 200 AND REWORKED ARE - [SDR SWAA2025041415468](https://openairdocs.org/sdr/SWAA2025041415468.md): Floorbeam · cracked · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Floor Beam > STA 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-64 LOT: 1598659-1; BETWEEN BS540 BL0 TO RBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 REV:A;[02] VERIFIED CORRECTIVE ACTION ETNRY 1. - [SDR SWAA2025041406440](https://openairdocs.org/sdr/SWAA2025041406440.md): Floorbeam · cracked · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Floor Beam > STA 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-63 BETWEEN BS540 BL0 TO LBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 ID: 001 REV: -;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. - [SDR SWAA2025041407108](https://openairdocs.org/sdr/SWAA2025041407108.md): Stringer Clip · cracked · Mar 18, 2025 · N212WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > SMALL CRACK ON STRINGER CLIP - BS 440; STR. 14R<[01] REMOVED AND INSTALLED STRINGER CLIP - BS 440; STR. 14R. IAW SRM 51-40-02; DWG 143A0082 REV:- AND DWG 143A0102 REV:B;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025042106424](https://openairdocs.org/sdr/SWAA2025042106424.md): Seal · cracked · Mar 17, 2025 · N212WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED. - [SDR SWAA2025041406430](https://openairdocs.org/sdr/SWAA2025041406430.md): Seal · cracked · Mar 17, 2025 · N212WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > LT HORIZONAL STAB UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025041415456](https://openairdocs.org/sdr/SWAA2025041415456.md): Seal · cracked · Mar 17, 2025 · N212WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED. - [SDR SWAA2024120273257](https://openairdocs.org/sdr/SWAA2024120273257.md): Release System · broken · Dec 1, 2024 · N212WN · Boeing 7377H4 · Escape Slide > UPON ARRIVAL; FLIGHT ATTENDANTS REPORT THAT PLASTIC GUIDE LOOP IS BROKEN OFF OF FORWARD SERVICE DOOR GIRT BAR.<[01] REPLACED FWD SVC DOOR GIRT BAR RELEASE STOP ASSY PER
MM 25-66-01 - [SDR SWAA2024101045786](https://openairdocs.org/sdr/SWAA2024101045786.md): Cover · missing · Oct 7, 2024 · N212WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT COVER AT ROW 12DEF MISSING<[01] REINSTALLED EMERGENCY OVERWING EXIT LIGHT SIGN/COVER IAW AMM SIP 20-00-00 Next page: https://openairdocs.org/aircraft/N212WN/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 = 'N212WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N212WN/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.