N444WN

Service difficulty reports · 336

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 = 'N444WN' 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 SWAA2021081895094Angle · crackedCRACKED ANGLE AT BS 294 RBL 50 WL 208 AT STUB FRAME ; / [01] REMOVED CRACKED ANGLE AT BS 294 RBL 50 WL 208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW ANGLE AT BS 294 RBL 50 WL 208 AT SUB FRAME PER SRM 51-40-02; SRM 51-40-05; AND DWG#141A8310. OK TO IJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895081Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER CHORD BS 986 LBL 45 WL 208 ; / [01] BLENDED CORROSION ON FLOOR BEAM UPPER CHORD BS 986 LBL 45 WL 208 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 1'X1'X.065'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02] VERIFIED; [03]Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021081895096Frame · corrodedCORROSION ON BS 303 FRAME ABOVE MOPSILL LBL 51 WL 210 ; / [01] REMOVED CORROSION ON BS303 FRAME ABOVE MOPSILL LBL51 WL210 PER SRM 51-10-02-0G-0; [02] UPDATED MEASUREMENTS TABLE.; [03] VERIFIED CORROSION REMOVAL PER SRM 51-10-02-0G-0.;[05] REQUEST NDI TO PERFORJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021081895093Floor Support · crackedFLOOR SUPPORT CRACKED BS 312-328 RBL 30 WL 208 ; / [01] REMOVED CRACKED FLOOR SUPPORT BS 312-328 RBL 30 WL 208 PER SRM 51-40-02-0G-0. MATERIAL THICKNESS IS 0.040.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05-0G-0 AND DWG 141A5410. OK TO INSTALLJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895103Floor Support · crackedFLOOR SUPPORT CRACKED BS 277-294 BL 0 WL 208 ; / [01] REMOVED CRACKED SUPPORT AT BS 277-294 BL 0 WL 208; LOCATED AND DRILL NEW SUPPORT IAW WITH SRM 51-40-02; SRM 51-40-05 AND DWG 141A5400. REQUEST OKAY TO INSTALL; [02] VERIFIED CORRECTIVE ACTION #1<BR>OK TO INJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895085Floorbeam · corrodedCORROSION ON FLOOR BEAM EXISTING REPAIR BS 986 RB L31-45 WL 208 ; / [01] BLENDED CORROSION ON FLOOR BEAM UPPER CHORD BS 986 RBL 31-RBL 45 WL 208 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 14'X1'X.045'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.[11] IJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2021081895074Channel · corrodedCORROSION ON AED MOPSILL BS 947-993 LBL 50 SL 208 ; / [01] REMOVED CORROSION ON MOPSILL BS 983-984 LBL 50 WL 208 PER SRM 51-10-02-0G-0. REMOVED AMOUNT 1X1X .013 ORIGINAL THICKNESS .080. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1-A00707. DIAL DEPTH GUAGE IJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895082Support · corrodedCORROSION ON SUPPORT BS 986+9 LBL 22 WL 208 ; / [01] REMOVED CORROSION FROM BS 986+9 LBL 22 WL208 IAW SRM 51-10-02-0G-0. REMOVED AMOUNT 1'X1'X 0.045' . ORIGINAL THICKNESS OF MATERIAL 0.080' DUE TO NO LIMITS IN SRM ; SUPPORT FOUND TO BE OUT OF LIMITS. SUPPORT WJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895083Strap · corrodedCORROSION ON STRAP BS 1016-1023 LBL 3 WL 208 ; / [01] REMOVED CORROSION FROM STRAP BS 1016-1023 LBL 3 WL 208 PER SRM 51-10-02-0G-0. AMOUNT REMOVED 1'X1'X0.007'.ORIGINAL THICKNESS .071'. DUE TO NO LIMITS IN SRM; FOUND TO BE OUT OF LIMITS. STRAP WILL BE REMOVED Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895084Strap · corrodedCORROSION ON STRAP BS 1023 RBL 18 WL 208 ; / [01] REMOVED CORROSION FROM STRAP BS 1023 RBL 18 WL 208 PER SRM 51-10-02-0G-0. AMOUNT REMOVED 1'X1'X0.009'.ORIGINAL THICKNESS .071'. DUE TO NO LIMITS IN SRM; FOUND TO BE OUT OF LIMITS. STRAP WILL BE REMOVED AND REPLJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895097Channel · corrodedCORROSION ON FSD MOPSILL INNER CHORD BS 294+10-328+10 RBL 52 WL 208 ; / [01] REMOVED CORROSION IN AREA OF 34' BY 2' BY 0.030' PER SRM 51-10-02-0G-0 AND SRM 53-10-15-1A-2. OUT OF LIMITS PER SRM 53-10-15-1A-2.; [02] VERIFIED CORRECTIVE ACTION #1; [03] REMOVED FSJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895104Attach Angle · corrodedCORROSION ON FSD THRESHOLD ATTACH ANGLE BS 294+12-312+12 RBL52 WL 209 ; / [01] REMOVED CORROSION IN AREA OF 1' BY 1.2' BY 0.012' PER SRM 51-10-02-0G-0 AND SRM 53-10-15-1A-2. OUT OF LIMITS PER SRM 53-10-15-1A-2.; [02] VERIFIED CORRECTIVE ACTION #1; [03] REMOVEDJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021081895105Frame · crackedCRACK IN RADIUS OF BS312 FRAME ABOVE STR5L ; / [01] TRIMMED OUT DAMAGE IN RADIUS OF BS 312 FRAME ABOVE STR 5L PER SRM 51-10-02-0G-0. REMOVED 0.30' FROM EDGE OF FRAME. FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1.; [02] VERIFIED CORRECTIVE ACTION #1<BR> FOUNJul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021071995102Floor Support · crackedFLOOR SUPPORT CRACKED BS 312-328 LBL 45 WL 208. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 AND DWG 141A5410. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400.Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021071995095Support Angle · corrodedCORROSION ON THRESHOLD SUPPORT ANGLE AT FED BS 312-328 LBL 52 WL 209. REMOVED CORROSION ON THRESHOLD SUPPORT ANGLE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-0I-1. REMOVED THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW Jul 15, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895059Cargo Track · corrodedCORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL3 WL156. ; / [01] REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727B+3; LBL3; WL156 L=1'' X W=1'' D=0.008'' MATERIAL REMOVED 0.008'' FROM 0.070'' ALLOWABLE; REMAINING THICKNESS 0.062' THEREFOREJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895037Floor Panel · damagedFLOOR PANEL 242UF HAS FIBER DAMAGE ON UPPER SURFACE. ; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO UPPER FACESHEET TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-0Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021081895042Support Angle · crackedCRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL12 WL170. ; / [01] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918; RBL12; WL170 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895047Cargo Track · corrodedCORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL156. ; / [01] CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL156 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] UPDATED MEASUREMENTS; [03] CUTOUT DAMAGJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895015Shield · corrodedFWD CARGO COMPARTMENT FWD SHIELD HAS CORROSION BS 426-433 RBL 24 WL 156 ; / [01] ADDED MESUREMENTS; [02] CORROSION ON SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] VERIFIED NO LIMITS IN SRM; [04] UPDATED MEASUREMENTS; [05] VERIFIJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895048Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS761 - BS773 LBL22 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] UPDATED MEJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895026Support · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD TO SIDEWALL SUPPORT HAS CORROSION BS 500D LBL 25 WL 156 ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED NO LIMITS IN THE SRM FOR AFT BULKHEAD SIDEWALL SUPPORT; Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895025Support · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD TO SIDEWALL SUPPORT HAS CORROSION BS 500D RBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] VERIFIED NO LIMITS IN SRM FOR AFT BULKHEADJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895016Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 494 LBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] CORROSION Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895018Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 500C+6 LBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] CORROSIJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895020Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 466-470 LBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] CORROSJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895021Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 500A+6 TO 500B+6 LBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D. SUJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895022Shield · corrodedFWD CARGO COMPARTMENT AFT SHIELD HAS CORROSION BS 494-BS 500+14 RBL 25 WL 156 ; / [01] ADDED MEASUREMENTS; [02] CORROSION ON SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] VERIFIED NO ALLOWABLE SRM LIMITS; [04] REMOVED FWD CARGO AJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895023Support · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD TO FLOOR SUPPORT HAS CORROSION BS 500D RBL 4 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] UPDATED MEASUREMENTS; [04] VERIFIED UPDATEJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021081895024Support · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD TO FLOOR SUPPORT HAS CORROSION BS 500C+19 RBL 12-17 WL 156 ; / [01] UPDATED MEASUREMENT; [02] VERIFIED NO ALLOWABLE LIMITS IN SRM; [03] REMOVED AFT BULKHEAD TO FLOOR SUPPORT BS 500C+19 RBL 12-17 WL156 PER SRM 51-40-02-0G-0. RJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895028Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 500A+1 TO 500B+17 RBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895044Frame Splice · corrodedCORROSION ON FRAME AT AFT CARGO BAY BS787 RBL27 WL156. MARKED ; / [01] CORROSION ON FRAME SPLICE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM PART WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.; [02] VERIFIED CORROSION OJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2021081895045Support Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO ABY BS773 BL0 TO RBL14 WL157. ; / [01] CORROSION ON SPLICE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. SPLICE WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.; [02] VERIFIEDJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895046Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS764 LBL17 WL157. ; / [01] CORROSION ON RAIL AT AFT CARGO BAY BS764 LBL17 WL157 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] UPDATED MEASUREMENTS; [03] INSPECTEDJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895049Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727E+6 LBL22 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED CORROSJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895050Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS727D+7 LBL17 WL156. ; / [01] CORROSION ON CARGO TRACK AT AFT CARGO BAY BS727D+7 LBL17; WL156 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] CARGO TRACK WILL BE REJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895053Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS862 RBL22 WL165. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. SHIELD WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.; [02] VERIFIED CORRECTIVE ACTIOJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895054Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727E+2 LBL22 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED CORROSJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895057Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT AFT CARGO BAY BS847 LBL5 WL158. ; / [01] CORROSION ON CLIP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. CLIP WILL BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PARAGRAPH 9.; [02] VERIFIED CORRECTIVE ACTION Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021081895064Cargo Track · corrodedCORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL17 WL156. ; / [01] CORROSION ON CARGO TRACK AT AFT CARGO BAY BS727D+3 LBL17; WL156 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] CJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895039Channel · corrodedCORROSION AROUND FASTENER HOLE AT AFT CARGO BAY BS904 RBL8 WL171. ; / [01] CORROSION ON RAIL AT AFT CARGO BAY BS904 RBL8 WL171 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] UPDATED MEASUREMENTS; [03]Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895017Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 500+10 TO 500+14 LBL 25 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [0Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021081895052Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS727D+6 RBL3 WL156. ; / [01] CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL3 WL156 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION PER SRM 53-00-53-1A-2 FIG. 103 DETAIL D; [02] INSPECTED AND VERIFIED CORROSIONJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895051Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY BS727D+5 LBL3 WL156. ; / [01] CORROSION ON RAIL AT AFT CARGO BAY BS727D+5; LBL3; WL156 IS OUT OF LIMITS DUE TO FASTENER HOLE PROXIMITY TO CORROSION SRM 53-00-53-1A-2. FIG 103. DETAIL D; [02] UPDATED MEASUREMENTS; [03] VERIFIJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021081895038Support · crackedCRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL12 WL170. ; / [01] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914; RBL12; WL170 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AJul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021071995067Floor Panel · damagedFIBER DAMAGE UPPER SURFACE OF FLOOR PANEL 221GF IAW SRM 53-00-50-0I-1 FIGURE 2. TABLE 2. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C.(3).(A). DAMAGE IS TO BE REPAIRED IAW SRM 53-00-50-2R-1. REMOVED ALL INSERTS IAW SRM 53-00-50-2Jul 14, 2021 · N444WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021081894191Floor Panel · damagedFLOOR PANEL 241DF HAS DAMAGE AT THE CORNER ; / [01] IDENTIFIED FLOOR PANEL 241DF IAW SRM 53-00-50-0I-1 FIGURE 4. TABLE 4. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C.(3).(A).<BR><BR>DAMAGE IS TO BE REPAIRED IAW SRM Jul 13, 2021 · N444WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021081894184Rib · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER RIB ASSY AT STAB STA 120.3 3RD VERTICAL STIFFENER FROM FWD END ; / [01] REMOVED R/H HORIZ STAB INSPAR RIB AT STAB STA 120.30 FOR ACCESS FOR STAB RIB REPAIRS IAW SRM 55-10-09-2R4 PARA 4A AND SRM 51-40-02-0G-0 PARA 4 AND 7Jul 13, 2021 · N444WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2021081894188Skin · corrodedCORRISION ON LAV SERVICE DOOR SKIN ; / [01] CORROSION ON LAV SERVICE DOOR WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 52-40-01-1A-4 FIG 103 DETAIL D; [02] VERIFIED CORROSION ON LAV SERVICE DOOR WAS FOUND TO BE OUT OF LIMITS DUE TO Jul 13, 2021 · N444WN · Boeing 7377H4 · Service DoorsSDR SWAA2021081892880Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1673 INOP ; / [01] ALLOWED M1673 TO CHARGE AND PERFORMED OPERATIONAL CHECK PER AMM 33-51-06-960-805 LIGHTS ASSOCIATED WITH M1673 CHECKED GOOD; [02] VERIFIED ALLOWED M1673 TO CHARGE AND PERFORMED OPERATIONAL CHECK Jul 10, 2021 · N444WN · Boeing 7377H4 · Emergency Lighting
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