N940WN

Service difficulty reports · 248

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N940WN' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2021080489397Doubler · crackedCRACK ON DOUBLER ON FWD SIDE OF R/H BS 663 VAPOR BARRIER AT RBL 25 WL 146 ; / [01] RECEIVED FROM OSS NEW DOUBLER VERIFIED HEAT TREATMENT AND FABRICATION IAW DWG 111A1511-28 AND BAC 5602 MAT. USED 2024 T42 0.040' LOT#1453744-1; LOCATED AND DRILLED;APPLIED CHEMIJun 29, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080489398Floor Panel · damagedREJECT- PANEL 193AR INCORRECT REPAIR PERFORMED DUE TO DAMAGE THROUGH BOTH SKINS AND CORE; REPAIR FOR DAMAGE THROUGH ONE SKIN AND CORE WAS PERFORMED ; / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 18. <BR><BR>FOUND DAMAGE TO BE OUTJun 29, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080488665Bear Strap · crackedCRACK ON F.S.D. FWD BEAR STRAP; BS 294.5 +4; BETWEEN S-7R AND S-8R; WL 266 (MARKED) ; / [01] REMOVED STUB FRAME REVEAL FOR ACCESS PER SRM 51-40-02-0G-0; [02] ET INSPECTED IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID ATS1465 N600; [Jun 27, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021080488338Floor Support · crackedCRACKED FLOOR SUPPORT UPPER ANGLE BS 380-400 LBL 1 WL 208. ; / [01] REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0; [02] LOCATED/DRILLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OKJun 25, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080488339Floor Support · crackedCRACKED FLOOR SUPPORT UPPER ANGLE BS 380-400 LBL 13 WL 208. ; / [01] REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0; [02] LOCATED/DRILLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. Jun 25, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080488347Seat Track · corrodedCORROSION ON SEAT TRACK CROWN ON TOP AND IN WELL STA 492-520; LBL 25; WL 208 ; / [01] REMOVED CORROSION ON SEAT TRACK CROWN ON TOP AND IN WELL STA 492-520; LBL 25; WL 208. MAX MATERIAL REMOVED ON TOP WAS .025' .5' BY 2'; .003' 1' BY 1' IN WELL. OUT OF LIMITS PJun 25, 2021 · N940WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021080488341Seat Track · corrodedCORROSION ON SEAT TRACK CROWN IN WELL STA 465; LBL 45; WL 208 ; / [01] REMOVED CORROSION ON SEAT TRACK CROWN IN WELL STA 465; LBL 45; WL 208. MAX MATERIAL REMOVED IN WELL WAS; .006' 1' BY 1'. IN LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WJun 25, 2021 · N940WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021080488334Channel · corrodedCORROSION ON AFT ENTRY DOOR MOP SILL BS 964-986 LBL 52 WL 208. ; / [01] REMOVED CORROSION ON AFT ENTRY DOOR MOPSILL STA 964-986; LBL 52; WL 208. MAX MATERIAL REMOVED WAS .015' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-Jun 24, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080488335Channel · corrodedCORROSION ON AFT SERVICE DOOR MOP SILL BS 960-986 RBL 52 WL 208. ; / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOPSILL STA 960-986; RBL 52; WL 208. MAX MATERIAL REMOVED WAS .012' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRMJun 24, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487604Door Frame · damagedFWD ENTRY DOOR MAIN FRAME DAMAGED IN 3 EA PLACES ALONG AFT UPPER EDGES (ALL MARKED) ; / [01] REMOVED DAMAGE ON FED MAIN FRAME BS344 LBL56 WL283 0.750'X0.500';BS344 LBL58 WL280 0.500'X0.0500' AND BS344 LBL60 WL270 1.250'X0.250' I.A.W SRM 51-10-02-0G-0 AND SRM 5Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021080487616Floor Support · crackedCRACKED FLOOR SUPPORT BS 344-360 LBL 11 WL 208. ; / [01] REMOVED CRACKED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05-0G-0 AND DWG 141A5410.; [03] UPDATED MEASUREMENT TABLE AND REQUEST Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487601Support · corrodedBS 500B-500C RBL24.5 WL157 FLOOR TO SIDEWALL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FROM BS 500B-500C FOUND DEEPEST LOCATION AT BS 500B+10 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A SJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487613Support · corrodedCORROSION ON FLOOR TO SIDE WALL SUPPORT BS 767-793; RBL 21; WL 156 ; / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487611Support · corrodedCORROSION ON FLOOR TO SIDE WALL SUPPORT BS 727+4-847; LBL21; WL 156 ; / EVALUATED CORROSION FROM BS 727+4 TO 847 FOUND DEEPEST LOCATION AT BS 787 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/NJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487610Web · corrodedFORWARD CARGO BAY BS440-494 RBL 25 WL157 SUBWEB THRESHOLD IS CORRODED. / [01] EVALUATED CORROSION FROM BS 440-494 FOUND DEEPEST LOCATION AT BS 460 FOUND 0.015 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487609Support · corrodedBS500D LBL24.5-RBL24.5 WL157 AFT BULKHEAD PANEL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487608Support · corrodedBS500-500C LBL24.5 WL157 FLOOR TO SIDEWALL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FROM BS 500-500C FOUND DEEPEST LOCATION AT BS 500B FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487607Support · corrodedCORROSION ON FLOOR TO SIDE WALL SUPPORT BS 727+4-767 RBL 21; WL 156 ; / [01] EVALUATED CORROSION FROM BS 727+4 TO 767 FOUND DEEPEST LOCATION AT BS 747 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487606Shield · corrodedBS 420-440 RBL24.5 WL157 FLOOR TO SIDEWALL SHIELD IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487605Shield · corrodedBS 494-500A RBL24.5 WL157 FLOOR TO SIDEWALL SHIELD IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487621Web · corrodedCORROSION ON ACB DOOR SUB THRESHOLD WEB BS 793-847; RBL 15-23 WL 156 ; / [01] EVALUATED CORROSION FROM BS 793-847 FOUND DEEPEST LOCATION AT BS 827 FOUND 0.015 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DEPTH GAUGE P/N ATS400 Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487617Support Angle · corrodedCORROSION ON FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE BS 316 -338 LBL 60 WL 208. ; / [01] REMOVED CORROSION ON FWD ENTRY DOOR I/B SUPPORT ANGLE STA 316-338; LBL 60; WL 208. MAX MATERIAL REMOVED WAS .014'; 22' BY 1' FROM .080' OUT OF LIMITS PER SRM 51-10-02-0Jun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487615Frame · crackedCRACK ON FRAME BS 312 ABOVE FWD ENTRY DOOR UPPER SILL WEB. ; / [01] ET INSPECTED CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK AND MARKED ENDS.<BR><BR>CAL ID ATS1465 N600; [02] REMOVED CRACK ON FRAME STA 312 ABOVE FWD ENTRY DOOR UPPER SILL WEJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021080487602Angle · crackedFWD ENTRY DOOR TARGET ANGLE CRACKED (MARKED) ; / [01] REMOVED AND REPLACED CRACKED FED TARGET ANGLE IAW SRM 51-40-02-0G-0 DWG 141A6124; [02] PERFORMED FORWARD ENTRY DOOR INDICATION SENSOR ADJUSTMENT TEST PER AMM 52-71-11-820-801. OPS CHECK TEST GOOD; [03] VERIJun 23, 2021 · N940WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2021080487620Floor Panel · corrodedCORROSION ON ACB FLOOR PANEL SPLICE AT BS 727D+6 LBL 20 - RBL 20; WL156 ; / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLJun 23, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487186Floor Panel · damagedFWD FLOOR PANEL 221BF HAS DAMAGED INSERTS ON O/B EDGE ; / [01] IDENTIFIED FORWARD FLOOR PANEL 221 BF<BR>IAW SRM 53-00-50-0I-1 FIGURE 2; TABLE 2<BR>FOUND DAMAGE TO ENTIRE UPPER SURFACE AND BROKEN TANG TO<BR>EXCEED ALLOWABLE DAMAGE LIMITS.<BR>IAW SRM 53-00-50-1AJun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487183Floor Panel · damagedFWD FLOOR PANEL 221EF HAS DAMAGED UPPER SURFACE PLIES ; / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 221EF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 295.; [02] PANEL REPLACED. JOB COMPLETE.Jun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487184Floor Panel · damagedFWD FLOOR PANEL 222BF HAS UPPER SURFACE PLY DAMAGE ; / [01] DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 222BF; REPLACED WITH<BR>NEW PANEL.<BR>IAW SRM 51-10-02-0G-0 PARA 9 A. (1) AND<BR>AIPC 52-21-51-21L ITEM 135; [02] VERIFIED PANEL REPLACEMENTJun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487187Floor Panel · damagedFWD FLOOR PANEL 221CF HAS DAMAGED INSERTS ; / [01] DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 221CF; REPLACED WITH NEW.<BR>IAW SRM 51-10-02-0G-0 PARA 9 A(1) AND<BR>AIPC 53-21-51-21L ITEM 175; [02] FLOOR PANEL REPLACED. JOB COMPLETE.Jun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487185Floor Panel · damagedFWD FLOOR PANEL 221DF HAS DAMAGED UPPER SURFACE PLIES ; / [01] IDENTIFIED FORWARD FLOOR PANEL 221DF<BR>IAW SRM 53-00-50-0I-1 FIGURE 2; TABLE 2<BR>FOUND DAMAGE TO UPPER SURFACE TO EXCEED ALLOWABLE LIMITS<BR>IAW SRM 53-00-50-1A-1 PARA 4 F.<BR><BR>REPAIR TO BE EFJun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487182Floor Panel · damagedAFT FLOOR PANEL 241AEF HAS PLY DAMAGE ON THE AFT EDGE UPPER SURFACE SKIN ; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-Jun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080487204Floorbeam · corrodedCORROSION FOUND ON FLIGHT DECK FLOOR UPPER FLANGE OF BS 259.5; LBL 11 - RBL 11; WL 208 ; / [01] REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; [02] NO APPLICABILITY ENTRIES FOUND ON SRM <BR>DAMAGE TO BE REMOVE PER SRM 51-10-02-0G-0; [03] Jun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021080487205Support Channel · corrodedCORROSION FOUND ON FLIGHT DECK FLOOR INTERCOSTAL SUPPORT CHANNEL BETWEEN BS 259.5 AND BS 270; BL 0; WL 208 ; / [01] VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 PAR 4.B(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [02] REMOVED CORROSION ON SUPPORT CHANNEL BS2Jun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080487203Floorbeam · corrodedCORROSION FOUND ON LATERAL BEAM UPPER FLANGE AT BS 270; LBL 11 - RBL 11; WL 208 ; / REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [03] REMJun 22, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021080487188Skin · crackedLT HORIZONTAL STAB. LWR SKIN STAB STA 193.90-1; CRACK NOTED 16' AFT OF FRONT SPAR LE. CRACK LENGTH 1.3' / [01] -CUT OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11 STEP 4 B;C. CUT OUT DIMENSIONS: L=1.70'; W=1.60'; [02] VERIFIED CJun 22, 2021 · N940WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021080489921Bulkhead Web · crackedL/H B.S 663 VAPOR BARRIER IS CRACKED ; / [01] REMOVED CHORD AND 3 EA BRACKETS TO FACILITATE REPAIR.<BR>IAW SRM 51-40-02-0G-0 PARA 4 E. & FIGURE 8; [02] REMOVED 5 EA. DOUBLERS AND 2 EA. STIFFENERS IAW SRM 51-40-02-0G-0 PARA 4 STEP E; PARA 7 STEP D AND AMM 51-31Jun 21, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080488974Bulkhead Web · crackedR/H B.S 663 VAPOR BARRIER IS CRACKED ; / [01] REMOVED 6 EACH VERTICAL STIFFENERS TO ACCESS CRACKED AREA AT RBL 25 TO RBL 40 IAW SRM 51-40-02 PAR.7 D (6);DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-10<BR>PER SRM 57-10-10-2R-2 PARA 1C(NOTE).Jun 21, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080486765Stiffener · crackedCRACK IN 3RD VERTICAL STIFFENER ON RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50. ; / [01] -ACCESSED RT HORIZONTAL STABILIZER FRONT SPAR WEB FROM STAB STATION 111.10 TO STAB STATION 147.90 IAW SRM 51-40-02-0G-0<BR><BR>-REMOVED RT HORJun 21, 2021 · N940WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2021080486771Support Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE SUPPORT IS CRACKED AT L.B.L. 27; W.L. 150. ; / [01] UPDATED MEASUREMENT TABLE; [02] REMOVED BS 663 LWR VAPOR BARRIER VERTICAL 'L' ANGLE SUPPORT LBL27 WL150 IAW SRM 51-40-02.; [03] LOCATED AND DRILLED NEW VERJun 21, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021080486287Support · chafedBS 663+4 LBL30 WL140 WING TO BODY (193D) FAIRING PANEL SUPPORT STRUCTURE HAS CHAFED DAMAGE. / [01] REMOVED BS 663+4 LBL30 WL140 WING TO BODY (193D)FAIRING PANEL SUPPORT STRUCTURE IAW SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FAIRING PANEL SUPPORT STRUCTURE BJun 20, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080486288Support · chafedBS 663+4 RBL30 WL140 WING TO BODY (193D) FAIRING PANEL SUPPORT STRUCTURE HAS CHAFFED DAMAGE. / [01] LOCATED AND DRILLED NEW FAIRING SUPPORT P/N 146A7214-20 IAW SRM 51-40-02-0G-0 AND DWG 149A7216. REMOVAL AND INSTALLATION TO BE DOCUMENTED ON TTG8Q005KR5K.; [02]Jun 20, 2021 · N940WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080486009Slide · out of positionAFT ENTRY DOOR SLIDE AND GIRT REQUIRE REPOSITIONING. ; / [01] REMOVED AFT ENTRY DOOR ESCAPE SLIDE AND COVER FROM AFT ENTRY DOO FOR ACCESS PER AMM 25-66-01-000-801; [02] REPOSITIONED SLIDE IN PACK; REINSTALLED SLIDE; AND PEFORMED GOOD OPS CHECK PER CUSTOMER CARJun 18, 2021 · N940WN · Boeing 7377H4 · Escape SlideSDR SWAA2021080485996Floor Panel · chafedPANEL 193AL MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 193AL IAW SRM 53-40-70-0I-1.FIG2; ITEM[7]. FOUND DAMAGE ALONG I/B EDGE ON INNER SURFACE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1.PARA 4.B.(6). REQUIRES REPAIR PER SRM 51-70-05-2R-6 IAW SRJun 18, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080485997Floor Panel · chafedPANEL 193AR MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 9.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.B.(2).<BR><BR>REPAIR IS TO BE ACCOMPLISHED IAW SRM 51-70-Jun 18, 2021 · N940WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021080489920Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] EVALUATED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4 - LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED; THEREFORE; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIG. 10Jun 15, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021042065017Bulkhead Web · crackedLH MLG WHEEL WELL VAPOR BARRIER HAS A CRACK MEASURING 15.5' AT LBL 30. ACCOMPLISHED INTERIM REPAIR IAW SRM 5710101A2.Apr 16, 2021 · N940WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2020072202601Slide · unsecureAFT SERVICE DOOR SLIDE RUBBING ON THRESHOLD. SECURED THE SLIDE IN ITS HOUSING IAW MM 25-66-01, AND MT 725-61-06.Jul 20, 2020 · N940WN · Boeing 7377H4 · Escape SlideSDR SWAA2020042041964Seat Track · wornFLIGHT DECK; FO'S SEAT TRACK AFT INBOARD IS WORN. / R & R FLIGHT DECK; FO'S SEAT TRACK AFT INBOARD; PER AMM 25-11-11.Apr 14, 2020 · N940WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020042041965Battery Pack · failedPASSENGER CABIN; TWO EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. / R & R TWO EMERGENCY LIGHTING BATTERY PACKS (M01672 & M01673) PER DWG# 33500005 AND AMM 33-51-06.Apr 14, 2020 · N940WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020041541958Sign · looseOVERWING EMERGENCY EXIT CABIN CEILING SIGN IS LOOSE / RESECURED OVERWING EMERGENCY EXIT CABIN CEILING SIGN PER MM 33-51-00Apr 14, 2020 · N940WN · Boeing 7377H4 · Emergency Lighting
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