N207WN

Service difficulty reports · 380

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 = 'N207WN' 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 SWAA2022111561836Floor Panel · delaminatedFLOOR PANEL 232DF HAS THREE SPOTS OF DELAMINATION (STA 430) / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 232DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIROct 19, 2022 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022111561866Floor Panel · damagedCABIN FLOOR PANEL 242DF;FIBER GLASS IS PEELING (STA 680). / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 242DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIREDOct 19, 2022 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022111561869Floor Panel · damagedCABIN FLOOR PANEL 241AF;FIBER GLASS IS PELLING. / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED WITH A PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEOct 19, 2022 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022111561256Door Sill · crackedFWD CABIN L/H WET AREA L-1 DOOR LOWER SILL INNER CHORD HAS 3' CRACK @ STA 303.9 MKD DOT / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 2.25'<BR>[NORTEC 600 ; B/C 172389 ; CALIB.DUE- 3/23];[02] STARTED REMOVING FWD CABIN L/H WET AOct 18, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111561257Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #242UF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #242UF BY OUTSIDE VENDOR WITH R.O #1792601 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTALOct 18, 2022 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022111561262Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #241ABF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #241ABF BY OUTSIDE VENDOR WITH R.O #1792603 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTOct 18, 2022 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022111660707Fitting · corrodedCORROSION AT L-1 DOOR LOWER SILL FWD SLIDE LATCH FITTING FASTENER HOLES. REMOVED CORROSION AT FWD SLIDE LATCH (GIRT BAR SUPPORT) AT L1 DOOR LOWER SILL AREA SRM 51-40-01-0G-0. AFTER REMOVED CORROSION ON MAIN CABIN FWD GIRT BAR SUPPORT FOUN OUT LIMITS IAW SRMOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660708Door Sill · corrodedL-1 DOOR. CUTOUT LOWER SILL INNER CHORD FROM BS 312 TO 344 CORRODED. L1 DOOR LOWER SILL INNER CHORD WAS REPLACED ON FAULT TTG8Q00FJNG5.Oct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660709Door Sill · corrodedCORROSION @ R-1 DOOR LOWER SILL INNER CHORD FROM STA 294.5 TO STA 328 MKD DOT / [01] REMOVED CORROSION AT R1 DOOR LOWER SILL INNER CHORD;STA 294.5 TO STA 328.PER B 737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP #1;[03] PERFORMED UT THICKNESS ON REWORKED AREA ASOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660909Door Sill · corrodedCORROSION ON R2 DOOR SILL, BS 947.5-992.8. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT PART 4 51-00-00, PROC 3. EVALUATED REWORKED AREA AND FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED THE DOOR SIOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660900Door Sill · corrodedCORROSION ON LT SIDE WALL BS 344-360. L1 DOOR LOWER SILL WAS REPLACED ON TTG8Q00FJNG5.Oct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660915Web · corrodedCORROSION AFT CABIN WET AREA FLOOR SUPPORT WEB FROM BL-0 TO LBL17 STA 1016. EVALUATED CORRODED AREA, FOUND EXFOLIATING CORROSION OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED DAMAGE WEB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW WEB IAW SRM 51-40-05-0Oct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660916Strap · corrodedCORROSION AT AFT CABIN WET AREA GALLEY FLOOR WEB STRAP LBL 3, BS 1016. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00, PROC 3. EVALUATED REWORKED AREA AND FOUND OUT OF LIMITS IAW 53-70-51-1A-1. ROct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111660918Floorbeam · corrodedCORROSION AT AFT CABIN WET AREA FLOORBEAM UPPER TEE BS 986.5, RBL 45. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FABRICATED A NEW TEE IAW SRM 53-70-51-2R-4, AND EA 1-753-30838. INSTALLED REPAIR PARTS, TEE, SPLICES, & INTERCOSTAL IAW SRM 53-70-51-2R-4, AND EOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022111560901Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ RBL 10 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED INTERCOSTAL FLOOR SUPPORT AT FWD CABIN BET. STA 380 TO STA 400;BL-0.PER B 737-700 SRM 51-40-02;[02] LOCARED AND DRILL NEW INTERCOASTAL AT STA 3Oct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111560902Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ BL-0 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED INTERCOASTAL FLOOR SUPPORT AT FWD CABIN WET AREA BET. STA 380 TO STA 400;BL-0.PER B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILL NEW INTERCOOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111560903Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ LBL 13 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED FLOOR SUPPORT INTERCOSTAL AT FWD WET AREA;LBL 13' BETWEEN STA 380 TO STA 400;PER B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILL NEW INTERCOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111560914Floorbeam · corrodedCORROSION. @ FASTENER HOLE FLOOR BEAM STA 986.5 RBL-5 MKD DOT / [01] REMOVED CORROSION AT FASTENER HOLE FLOOR BEAM STA 986.5 RBL-5 AS PER REFERENCE B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ FASTENER HOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022111560917Floorbeam · corrodedCORROSION. AFT CABIN WET AREA FLOOR BEAM UPPER CAP STA 986.5 LBL 45 MKD DOT / [01] REMOVED CORROSION AT AFT CABIN WET AREA FLOOR BEAM UPPER CAP STA 986.5; LBL 45 AS PER REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AOct 17, 2022 · N207WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022111660587Support Bracket · crackedLOWER FUS. CENTER WING L/H A/C BAY FWD INB CROSSOVER AIR DUCT SUPPORT BRACKET CRACKED. REMOVED & REPLACED AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0.Oct 16, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111560583Floor Support · crackedFWD CABIN WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED AT UPPER CAP BETWEEN STA 277 AND STA 294.5 BL-0 MKD DOT / [01] REMOVED INTERCOASTAL AT FWD WET AREA ;STA 277 TO STA 294.5;BL-0;PER B 737-700 SRM 51-40-01-0G-0.;[02] LOCATED AND DRILL INTERCOSTAL AT FWD WETOct 16, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111560582Door Sill · crackedFWD CABIN FUSELAGE INTERNAL FRAME CUTOUT FLANGE CRACKED ABOVE L-1 DOOR CUTOUT UPPER SILL @ STA 312 MKD DOT / [01] ACCOMPLISHED REPAIR PER EA 22-153-01244 TTG8Q00FQNL3.;[02] VERIFIED STEP 1.;[03] C/WOct 16, 2022 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022111659748Bear Strap · cracked0.300' CRACK EXTENDING FWD OF FASTENER ON R1 BEAR STRAP INTERIOR SIDE . REMOVED RAIN GUTTERS (2EA) FROM REPAIR AREA IAW SRM 51-40-02-0G-0. FABRICATED TAPERED SHIM IAW EA 21-153-03542 STEP 10 FIG.1. COMPLETED FABRICATION OF REPAIR IAW EA 21-153-03542 STEPOct 14, 2022 · N207WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022111660018Rib · crackedLT HORIZONTAL STABILIZER NR 5 RIB CRACKED AT STIFFENER 3. TRIM OUT DAMAGE AREA IAW SRM 55-10-09-2R-4. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6, 51-00-00, PROCEDURE 23, NO CRACKS NOTED. PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIOct 14, 2022 · N207WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022111660023Rib · crackedRT HORIZONTAL STABILIZER RIB 5 CRACKED AT STIFFENER 2. REMOVED DAMAGE FROM RIB IAW SRM 55-10-09-2R-4. PERFORMED HFEC INSP ON REWORKED AREA IAW NDT P6 51-00-00 PROC.23, CRACK CONFIRMED. PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW NDT P6 51-00-00, PROCOct 14, 2022 · N207WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022111660024Rib · crackedRT HORIZONTAL STABILIZER RIB 5 CRACKED AT STIFFENER 3. REMOVED DAMAGE FROM RIB IAW SRM 55-10-09-2R-4. PERFORMED HFEC INSP ON REWORKED AREA IAW NDT P6 51-00-00, PROC.23. CRACK CONFIRMED. PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW NDT P6 51-00-00, PROCOct 14, 2022 · N207WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022111659949Panel · elongatedRIGHT WING LOWER INBOARD FIXED T/E ACCESS PANEL #651GB INNER CENTER FITTING WITH ELONGATED HOLES / [01] REMOVED AND REPLACED FITTING AT RT WING LOWER I/B FIXED T/E ACCESS PANEL #651GB PER B737-700 SRM 51-40-02-0G-0. (PERFORMED BY KV 34707);[02] VERIFIED STEP 1Oct 14, 2022 · N207WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022111660021Bracket · crackedLEFT WING UPPER SEAL SUPPORT OF DEFLECTOR PANEL IS CRACKED / [01] BRACKET WIL BE REPLACED IN THE ITEM TTG8Q00FFE2B;[02] VERIFIED STEP 1.Oct 14, 2022 · N207WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022111659744Bracket · crackedLT WING T/E; DEFLECTION CONTROL RIB UPPER PANEL CENTER AFT SEAL BRACKET CRACKED. REMOVED BRACKET IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.Oct 13, 2022 · N207WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022111659727Bracket · crackedLEFT WING LOWER INBOARD T/E ACCESS PANEL #551FB INNER FWD CENTER BRACKET CRACKED. AFTER REMOVED SEAL TO REPLACE BRACKET FOUND SEAL WORN OUT. REMOVED SEAL FOUND ON STEP 1 IAW SOPM 20-50-02. REMOVED AND REPLACED THE BRACKET IAW SRM-51-40-02-0G-0.Oct 13, 2022 · N207WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022111659284Panel · damagedRT WING;LOWER MID TRAILING EDGE PANEL #661AB WITH ELONGATED HOLE AT O/B AREA / [01] PREPARED AREA FOR REPAIR FASTENER HOLE AT R/T WINGLOWER MID TRAILING EDGE PANEL#661AB PER B737 SRM 51-70-04-2R-9;[02] OK TO ACCOMPLISH REPAIR.;[03] REPAIRED PANEL AT ELONGATED Oct 12, 2022 · N207WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022060613417Light · missingRIGHT HAND EMERGENCY EXIT WINDOW LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / [01] REMOVED AND REPLACED EXIT SIGN COVER REF AMM 33-51-01;[02] C/WMay 31, 2022 · N207WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022060613416Light · missingR1 DOOR LOWER EMERGENCY SIGN MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED EXIT SIGN COVER REF AMM 33-51-01;[02] C/WMay 31, 2022 · N207WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022051205633Bracket · looseFWD ENTRY DOOR STOWAGE BRACKET FOR GIRT BAR LOOSE. / [01] ADJUSTED FWD DOOR GIRT BAR BRACKET PER AMM 25-66-01May 8, 2022 · N207WN · Boeing 7377H4 · Escape SlideSDR SWAA2022031783154Flashlight · inoperativeFWD GALLEY LOWER EMER FLASHLIGHT INOP / [01] R&R FWD GALLEY LOWER FLASHLIGHT REF CMM 25-60-02Mar 13, 2022 · N207WN · Boeing 737* · Emergency EquipmentSDR SWAA2022013164122Light · inoperativeLH OVERWING EXIT SIDEWALL LIGHT INOP / [01] RELAMPED AND REMOVED & REPLACED FUSE IAW AMM 33-21-00. OPS CHECK GOOD. THIS CLEARS MEL.Jan 26, 2022 · N207WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021101127215Panel · elongatedCENTER WHEEL WELL PANEL 193D HAS MULTIPLE WORN AND/OR ELONGATED HOLES. ; / [01] TSR 2021006242 SUBMITTED WITH PICS.; [02] EA 21-153-02953 ADDED TO FAULT.; [03] C/W EA 21-153-02953Oct 6, 2021 · N207WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021062886370Lamp · burned outOVERWING EMERGENCY EXIT SIGNS HAVE BURNT OUT BULBS ; / [01] RELAMPED OVERWING EMERGENCY EXIT SIGNS AND PERFORMED A GOOD OPS TEST PER AMM 33-51-01-960-801; [02] VERIFIED RELAMPED OVERWING EMERGENCY EXIT SIGNS AND PERFORMED A GOOD OPS TEST PER AMM 33-51-01-960-8Jun 22, 2021 · N207WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021062882160Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 887; RBL 20-LBL 8; WL 154 ; / [01] NO ALLOWABLE DAMAGE FOUND ON SRM FOR THIS PART... PART REQUIRED TO BE REMOVE AND REPLACE IAW SRM 51-10-02-OG-0 STEP 9.; [02] CONFIRMED; OK TO PROCEED; [03] RECEIVED AND REPLACEJun 12, 2021 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021062882159Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 767; RBL 20-LBL 20; WL 154 ; / [01] UPON INVESTIGATION; NO ALLOWABLE DAMAGE LIMITS IN SRM FOR THIS PART. WILL BE REMOTED AN REPLACED; [02] CONFIRMED; OK TO PROCEED; [03] RECEIVED AND REPLACED NEW AFT CARGO BAY FJun 12, 2021 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021062882158Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 727D; RBL 20-LBL 20; WL 154 ; / [01] UPON INVESTIGATION; NO ALLOWABLE DAMAGE LIMITS IN SRM FOR THIS PART. WILL BE REMOVED AND REPLACED; [02] CONFIRMED; OK TO PROCEED; [03] CONFIRMED; OK TO PROCEED; [04] RECEIVEDJun 12, 2021 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021062879847Support · out of toleranceREJECTION FWD O/B HOLE OF 887-947 FLOOR TO SIDEWALL SUPPORT REPLACEMENT OUT OF ROUND ; / [01] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL P/N 147A7501-17 AT BS 887-947 RBL 21 WL 164; IAW B 737-700 SRM 51-40-05-OG-0 DWG 147A7501; [02] VERIFIED APPLICABILITY OF SRJun 4, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062877523Floor Panel · corrodedPANEL 140CF IS CORRODED; AFT CARGO BAY ; / [01] FABRICATED NEW ACB FLOOR PANEL 140CF FROM 080 2024T3; LOT# 1457312-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] UPDATED FAULT INFORMATION; [03] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610May 26, 2021 · N207WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021062877519Panel · chafedPANEL 192DR HAS CHAFING DAMAGE AT I/B EDGE / [01] VERIFIED APPLICABILITY OF SRM 53-40-70-OI-1 FOR IDENTIFICATION AND SRM 53-40-70-1A-1 FOR ALLOWABLE DAMAGE; [02] DAMAGE FOUND ON PANEL 192DR ON WING TO BODY FAIRING AT I/B EDGE; 5'X0.6'X0.020'; ORIGINAL THICKNESMay 26, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876861Panel · chafedPANEL 192F HAS CHAFING DAMAGE AT L/E INNER SURFACE ; / [01] IDENTIFIED PANEL 192F MATERIAL IAW SRM 53-40-70-OI-1 TABLE 2 FIGURE 2 ITEM 15. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PAR 4B(2). DAMAGE IS REPAIRABLE PER 51-70-05May 25, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876859Panel · chafedPANEL 194CR HAS CHAFING DAMAGE ON L/E AT I/B END ; / [01] IDENTIFIED PANEL/MATERIAL IAW SRM 53-60-70-0I-1 FIG.2. TABLE 2. ITEM (6). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PAR 4. B. (6) (B). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2May 25, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876857Panel · chafedPANEL 194CL HAS CHAFING DAMAGE AT FWD I/B CORNER INNER SURFACE. ; / [01] IDENTIFIED PANEL 194CL IAW SRM 53-60-70-0I-1 FIGURE 2. TABLE 2. ITEM 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PARA. 4.B.(7). DAMAGE IS TO BE REPAIRED IAWMay 25, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876846Panel · chafedPANEL 192BR HAS CHAFFING DAMAGE AROUND ENTIRE PERIMETER OF INNER SURFACE ; / [01] IDENTIFIED MATERIAL ID IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 6. UPON INSPECTION OF PANEL FOUND DAMAGE TO BE LIMITED TO AFT I/B CORNER. DAMAGE IS OUT OF ALLOWABLEMay 25, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876845Panel · chafedPANEL 194DL HAS CHAFFING DAMAGE AT INNER SURFACE AFT EDGE ; / [01] IDENTIFIED PANEL/MATERIAL IAW SRM 53-60-70-0I-1 FIG. 2. TABLE 2. ITEM (7). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA4.B.(6)(B). REPAIR TO BE ACCOMPLISHED IAW SRM 51-May 25, 2021 · N207WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021062876836Support · chafedFAIRING FORMER SUPPORT HAS CHAFING DAMAGE AT BS727A JUST ABOVE NO.5 FLAP TRACK. ; / [01] LOCATED AND DRILLED FAIRING FORMER SUPPORT AT BS 727A JUST ABOVE NO.5 FLAP TRACK PER SRM 51-40-05 & BOEING DWG: 149A7902; [02] OK TO INSTALL FAIRING FORMER SUPPORT; [03] OMay 25, 2021 · N207WN · Boeing 7377H4 · Trailing Edge Flaps
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