N951WN

Service difficulty reports · 178

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 = 'N951WN' 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 SWAA2022081027371Floor Panel · delaminatedFLOOR PANEL 221DF HAS DELAMINATION ON LOWER SURFACE / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BRJul 9, 2022 · N951WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022081027271Stub Frame · crackedPASSENGER CABIN FSD CUTOUT BARE STRAP CRACKED BS299; 3' BELOW FWD UPPER DOOR STOP FITTING. MARKED. / [01] BEGUN ACCESSING FSD UPPER STUB FRAME BY DRILLING OUT RIVETS PER SRM 51-40-02;[02] REMOVED FSD UPPER SUB FRAME IAW SRM 51-40-02.;[03] REQUEST NDI ON FSD BAJul 8, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022081226111Floor Panel · debondedFLOOR PANEL 242UF DRAIN FITTINGS ARE DISBONDED. (MARKED) / [01] DRAIN FITTINGS FOR FLOOR PANEL 242UF WILL BE INSTALLED WITH PANEL INSTALLATION.;[02] VERIFIED CORRECTIVE ACTION #1Jul 6, 2022 · N951WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022081126114Floor Panel · pulledFLOOR PANEL 241NF HAS A PULLED-THROUGH INSERT AT FWD EDGE. (MARKED) / [01] IDENTIFIED FLOOR PANEL 241NF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5<BR><BR>DUE TO EXTENT OF DAMAGE NEW FLOOR BOARD WILL BE FABRICATED IAW SRM 53-00-50-2R-0 PAR.1 A(NOTE) <BR><BJul 6, 2022 · N951WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022081026101Floor Panel · brokenFLOOR PANEL 242XF IS BROKEN. / [01] IDENTIFIED PANEL 242XF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED DAMAGED SKIN; REMOVEDJul 6, 2022 · N951WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022080926386Light · crackedCABIN SIDE WALL PANEL 231YHW EMERGENCY EXIT LIGHT LENSE BACKING IS CRACKED. / [01] REPLACE SIDE WALL PANEL 231 YHW EMERGENCY EXIT LIGHT LENSE <BR>IAW RSM 50-40-2 SECTION 4-9;[02] REMOVED AND REINSTALLED SIDE WALL PANEL 231 YHW EMERGENCY EXIT LIGHT LENSE BACKINJul 6, 2022 · N951WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022081025447Floor Panel · debondedPANEL 222BF UPPER SURFACE IS DISBONDED / [01] IDENTIFIED PANEL 222BF IAW SRM 53-00-50-0I-1 TABEL 2 FIG 2. DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1<BR><BR>REMOVED ALL INSERTS TO Jul 3, 2022 · N951WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022080925445Intercostal · crackedINTERCOSTAL IS CRACKED AT RBL 32; BETWEEN BS 312-328 WL 208 / [01] REPLACED INTERCOSTAL AT RBL 32 BETWEEN BS 312-328 WL 208 PER<BR>SRM 51-40-05-0G-0.;[02] INSTALLED EIGHT HI-LOCKS ON INTERCOSTAL AT RBL 32 BETWEEN BS 312-328 PER SRM 51-40-02-0G-0 STEP 7.;[03] UJul 3, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022081024576Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 BS 500+7; BS 500A+4; BS 500B+16; BS 500D+7. / [01] SEAT TRACK IS BEING REPLACED ON CUST CARD TTG8Q00DARRK.;[02] CORRECTED ITEM 14 OF MEASUREMENTS CHART.;[03] SEAT TRACK IS BEING REPLACED ON CUST CARD TTG8Q00DARJun 30, 2022 · N951WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2022081224207Doubler · crackedLH BS 663 VAPOR BARRIER DOUBLER LBL 6 TO LBL 30 IS CRACKED / [01] FABRICATED DOUBLER ON CUSTOMER RO NO 874526-SWA. LOCATED AND DRILLED IAW SRM 51-40-05-0G-0. REQ OK TO TREAT AND PRIME;[02] VERIFIED CORRECTVE ACTION 1.<BR>OK TO TREAT AND PRIME;[03] VERUFIED APPJun 29, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022081224208Stiffener · crackedLH BS 663 VAPOR BARRIER STIFFENER LBL 25 IS CRACKED / [01] REMOVED STIFFENER IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STIFFENER P/N 111A1308U15 PO # 835745 IAW SRM 51-40-05-0G-0;[03] REQ. OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 1-3 OK TO INSTALJun 29, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022081223572Fitting · corrodedCORROSION ON FWD ENTRY DOOR AFT GIRT BAR ATTACH FITTING AT STA 344; LBL 59; WL 208.6. / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED CORROSION ON UPPER SURFACE OF GIRT BAR FITTING IAW SRM 51-10-02-0G-0. DEPTH OF REMOVAL 1X1X.012'. SRM DOES NOT HAVE REMOVAL LIMIJun 28, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081123576Intercostal · corrodedCORROSION ON PASSENGER FLOOR INTERCOSTAL FROM STA 294.5+2 TO STA 294.5+13; WL 208.1; LBL 11. / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED CORROSION IN SEVERAL AREAS ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 294.5 TO BS 312 LBL 312 IAW SRM 51-10-02-0G-0. MAX Jun 28, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081023783Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT PASSENGER CABIN BS986.5 RBL43. / [01] REMOVED GIRT BAR DOME NUT PLATE ON BS986.5 RBL43 IAW SRM 51-40-02-0G-0;[14] SHOT PEENED CUT EDGE I.A.W. B737-700 SRM 53-70-51-2R-4 STEP 4(D);[15] VERIFIED CORRECTIVE ACTIONS 13 AND 14.<BR>PERJun 28, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022080923790Floor Support · crackedCRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 1.(MARKED) / [01] REMOVED AND REPLACE FLOOR SUPPORT WITH NEW SUPPORT AT BS 540 LBL1-LBL24 IAW SRM 51-40-02 AND DRAWING143A0060 REV A;[02] VERIFIED CORRECTIVE ACTION #1Jun 28, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022080923791Floor Support · crackedCRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 1-3. / [01] REMOVED AND REPLACE FLOOR SUPPORT WITH NEW SUPPORT AT BS 540 RBL1-RBL24 IAW SRM 51-40-02 AND DRAWING143A0060 REV A;[02] VERIFIED CORRECTIVE ACTION #1Jun 28, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081123571Beam · crackedFWD SERVICE DOOR #4 BEAM: ON HFEC INSPECTION; FOUND CRACKS IN INSPECTION AREA PER TASK 52-41-EG-SWA-001 FIG 1. / [01] UPDATED DOOR PN# AND SERIAL #;[02] FSD WAS REPAIRED ON CUSTOMER RO # P3564514-1 JOB # 550905; FSD WAS REMOVED ON AND WILL BE INSTALLED ON TTG8Jun 27, 2022 · N951WN · Boeing 7377H4 · Galley DoorsSDR SWAA2022081122375Girt Bar · corrodedCORROSION ON FED FWD GIRT BAR MOUNTING BRACKET BS 312 + 1.25; LBL 54; WL 208.3 (MARKED) / [01] FOUND CORROSION ON FED FWD GIRT BAR FITTING TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM ;REPLACE PER SRM 51-10-02-0G-0 STEP 9;[02] VERIFIED ITEM 1 CORRECTIJun 24, 2022 · N951WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2022081022376Support Angle · corrodedCORROSION ON FSD MOP SILL WL 208.2; BS 312+7; RBL 57.5 & BS 312+14; RBL 58.3 (MARKED) / [01] REMOVED CORROSION ON FSD MOPSILL AT BS 312+7 IN A .8 X 2' X.003 AND BS312+14 WL208 IN A 3'X 1.5' X .016 ORIGINAL THICKNESS .080 FOUND TO BE OUT OF LIMITS PER SRM 53-10Jun 24, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081222226Track · crackedCRACK ON AFT CARGO BAY TRACK AT RBL 14 BS 747; BS 767. / [01] CRACK ON AFT CARGO BAY TIE DOWN AT RBL 14 ; BS 747 AND BS 767 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 ; PART WILL BE REPLACE AIW SRM 51-10-02-0G-0;[10] INSTALLED NEW ACB TRACK AT RBL 14; BS 727-88Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081222229Angle · crackedCRACK ON AFT CARGO BAY AFT BULKHEAD SUPPORT ATTACH ANGLE AT LBL 10 BS 847+19. / [01] ENTERED MEASUREMENTS.;[02] REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02.<BR>LOCATED; DRILLED AND INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 149A8102.;[03] VERIFIJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122233Threshold · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 23 BS 807+1; RBL 23 BS 807+3; RBL 23 BS 807+4; RBL 23 BS 807+11; RBL 26 BS 807+4; RBL 26 BS 807+6; RBL 26 BS 807+12; RBL 26 BS 807+18. / [01] SRM 53-60-15-1A-1 IS APPLICABLE FOR THIS;[02] BLENDED CORROSION ON AFT CARJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122234Shield · corrodedCORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+9; BS 847+15. / [01] ENTERED MEASUREMENTS;[02] PARTIAL ON STEP 1.;[03] PARTIAL ON STEP 2.;[04] VERIFIED CORRECTIVE ACTION 2-3.;[05] PARTIAL ON STEP 3.<BR>FAULT TTG8Q00D6D40 COMPLETE.;[06] VERIFIED CORJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122246Bulkhead Web · corrodedCORROSION ON AFT CARGO BAY AFT R/H BULKHEAD SUPPORT AT RBL 22 BS 947. / [01] NO ALLOWABLE DAMAGE FOUNDED; REPLACED PART FOR REPAIR IAW SRM 51-10-02;[02] LOCATED AND DRILLED NEW SHIELD P/N143A8126-31 PO#869254/1 IAW SRM 51-40-02 AND SRM 51-40-05;[03] DISREGARD Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122222Baffle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500B+19. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW CLIP P/N:143A7502U159 ; LOT:1494686-4 AND LOCATED AND DRILLED AT FCB LBL 24 BS 500B+19' IAW SRM 51-40-05 . REQUEST OK TO INSTJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022081122220Baffle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 400+1. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGLE P/N 143AU155 IAW SRM 51-40-05-0G-0. REQ. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION #2<BR>OK TO INSTALL GIVJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022081122221Tie Clip · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500A+19. / [01] REMOVED ANGLE IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW CLIP P/N:143A7502U159 ; LOT:1494686-4 AND LOCATED AND DRILLED AT FCB LBL 24 BS 500A+19' IAW SRM 51-40-05 . REQUEST OK TO INSTJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022081122230Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727B+10; BS 727B+14; BS 727C+6; BS 727C+7; BS 727D+6. / DAMAGE FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .035' OF ORIGINAL THICKNESS OF .040'. IAW SRM 53-60-53-0I-2 AND SRM 53-00-53-Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122232Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 767; BS 767+3; BS 767+10; BS 807+6; BS 807+10. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] EVALUATED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT LBL 21 BS767 L=1'XW=.3'XD=.0005'; BS76Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122244Strap · corrodedCORROSION ON AFT CARGO BAY TENSION STRAP TO INTERCOSTAL ATTACH DOUBLER AT RBL 20 BS 787+2. NUT PLATE DOUBLER / [01] SRM 53-60-15-1A-1 IS APPLICABLE FOR THIS DAMAGE;[02] BLENDED CORROSION ON AFT CARGO BAY INTERCOSTAL AT RBL 20; WORK AREA ; BS 787+2 ; L 2.0' X WJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081122243Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+2; BS 767+4; BS 767+8; BS 767+16. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0. RECEIVED NEW SHIELD P/N: 146A8127U12ATSMRO LOT: 1493681-1. LOCATED AND DRILLED NJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022000Support Angle · corrodedFWD CARGO BAY DOOR CUTOUT SUB-THRESHOLD WEB IS CORRODED FROM STA 440+8 TO STA 480+5; RBL 27.5 TO RBL 29; WL 156.5 / [01] PARTIAL ON STEP 1.<BR>ENTERED MEASUREMENTS.;[02] PARTIAL ON STEP 2.;[03] PARTIAL ON STEP 3.;[04] PARTIAL ON STEP 4.;[05] VERIFIED COMPLETE Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022002Sidewall Support · corrodedCORROSION ON FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT AT STA 500C+14 ; RBL 25; WL 156 / [01] REMOVED CORROSION ON FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT AT BS 500C; RBL 25; WL 156 ; WORK AREA ; L 1.0' X W 1.0' X D 0.014' FOUND TO BE OUT OF LIMITS IAW SJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022003Sidewall Support · corrodedFWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT IS CORRODED AT STA 400+6; 400+14; AND 400+18; RBL 25; WL 156. / [01] REMOVED CORROSION ON FWD CARGO BAY R?H FLOOR TO SIDEWALL SUPPORT RBL 25; WL 156 ; WORK AREA BS 400+6 ;L 1.0' X W 1.0' X D 0.015' ; BS 400+14; L 1.0Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022005Bulkhead Web · corrodedFWD CARGO BAY AFT BULKHEAD SUPPORT IS CORRODED; STA 500D; RBL23 TO LBL 25; WL 156. / [01] REMOVED CORROSION ON FWD CARGO AFT BULKHEAD SUPPORT AT BS 500D ;RBL 23 TO LBL 25; WL 156 ; DIMENSIONS L=1.5' W= 0.900' DEPTH:0.023' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUAJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022001Bulkhead Web · corrodedFWD CARGO BAY AFT R/H BULKHEAD SUPPORT IS CORRODED AT STA 500D; WL 157; RBL 26. / [01] REMOVED CORROSION ON FWD CARGO AFT R/H BULKHEAD SUPPORT AT BS 500D ;WL 156 ;RBL 26 DIMENSIONS L=2.' W= 0.800' DEPTH:0.021' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUATED REWORKEDJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022223Support Frame · corrodedCORROSION ON FWD CARGO BAY AFT L/H BULKHEAD SUPPORT AT LBL 25 BS 500D. / [01] REMOVED CORROSION ON FWD CARGO AFT L/H BULKHEAD SUPPORT AT BS 500D ;WL 156 ;LBL 25DIMENSIONS L=1.' W= 0.800' DEPTH:0.021' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUATED REWORKED AREA ;ORIJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022238Track · corrodedCORROSION ON AFT CARGO BAY TRACK AT RBL 14 BS 927+8. / [01] BLENDED CORROSION ON AFT CARGO BAY TRACK AT BS 927+8 ; RBL 14 WORK AREA ; L 1.0' X W 0.500' X D 0.021' ; FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 ; USE DEPTH GAGE; ID: ATS2678; S/N: UNKNOWN; DUE: 04/Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022240Support Angle · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A+10; BS 727B+1; BS 727B+6; BS 727C+10; BS 727D+3; BS 727D+5; BS 727D+8; BS 727D+10. / REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT AT RBL 21; BS 727D+10' MEASURED L= 1.400'; W=1.000'Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081022004Support · corrodedFWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT IS CORRODED AT LBL 25; WL 156; STATIONS: 400+15; 420+5; 440+18; 500+9; 500+13; 500A+2; AND 500B+7. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT;LBL 25 WL 156 ; IAW SRM 53Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022080922225Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. / [01] REMOVED GUSSET AT FCB BS 500D R/H STR 19 IAW SRM 51-40-02.;[02] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM ; GUSSET MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[03] LOCATED AND DRILLED DRILLED NEWJun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022080922224Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D L/H STRINGER 19. / [01] REMOVED GUSSET AT FCB BS 500D L/H STR 19 IAW SRM 51-40-02;[02] NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM ; GUSSET MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[03] LOCATED AND DRILLED NEW GUSSET Jun 23, 2022 · N951WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022081021999Shield · corrodedCORROSION; FWD CARGO FLOOR TO SIDEWALL SUPPORT SHIELD; BS 500 + 9; RBL 24; MARKED / [01] NO ALLOWABLE DAMAGE FOUNDED; REPLACED PART FOR REPAIR IAW SRM 51-10-02;[02] LOCATED AND DRILLED NEW SHIELD P/N143A8126-31 PO#869254/1 IAW SRM 51-40-02 AND SRM 51-40-05;[03Jun 22, 2022 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081120790Rib Doubler · crackedRH HORIZ STAB INSPAR RIB ASSY 4 (STA 120.30) CRACKED AT 2ND VERTICAL STIFFENER APPROX 1' FROM BOTTOM. / [01] REMOVED DAMAGE AT 2ND STIFFENER L:1.800' W:.500' IAW SRM 55-10-09-2R-4APPLICABILITY STATEMENT SRM 55-10-09-2R-1 IT'S APPLICABLE FOR REPAIR;[04] VERIFIEJun 20, 2022 · N951WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022081120971Skin · crackedCRACK NOTED ON L/H HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.9 LOCATED 9 INCHES FROM THE FRONT SPAR. CRACK LENGTH IS .8 INCHES / [01] REQUEST NDI TO MARK ENDS OF CRACK;[02] HFEC INSPECTED STAB SKIN AT CRACK PER 737NDT PART 6 51-00-00 PROCEDURE 23. CRACKJun 20, 2022 · N951WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022081120503Rib Doubler · crackedL/H HORIZONTAL STAB REMOVABLE L/E 331B RIB #4 IS CRACKED / [01] REMOVED AND REPLACED #4 RIB ON L/H HORIZONTAL STAB. REMOVABLE L/E #331B IAW SRM 51-40-01-0G-0 PARA. 4.;[02] REFERANCE DWG 186A1001 FOR FASTENER CALLOUT;[03] VERIFIED CORRECTIVE ACTION 1 AND 2Jun 19, 2022 · N951WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022081019616Angle · crackedCRACK ON LOWER L/H COMPOSITE BULKHEAD I/B UPPER ATTACH ANGLE AT LBL 7 BS 663. / [01] VERIFIED APPLICABILITY IAW SRM 57-10-10-2R-5;[02] REMOVED 8 EA FASTENERS COMMON TO FUEL TANK AND CUT OUT DAMAGE ANGLE IAW IAW SRM 57-10-10-2R-5;[03] VERIFIED CORRECTIVE ACTIONJun 16, 2022 · N951WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022081019617Bulkhead · crackedCRACK ON LOWER L/H COMPOSITE BULKHEAD AT LBL 35 BS 663. / [01] IDENTIFIED PANEL IAW SRM 57-10-10-0I-2 FIGURE 2 ITEM [4] AND TABLE 2 ITEM [4]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARAGRAPH 4.D.(1).(A) AND WILL BE REPAIRED IAW SRM 51-70-04-2RJun 16, 2022 · N951WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022081518695Slat · cracked#6 SLAT CRACKED AT L/E NOSE SKIN AT ACTUATOR RIB (MARKED) / [01] REQUEST NDI VERIFICATION CRACK CONDITION EXIST.[08] FABRICATED REPAIR DOUBLER FROM 7075T6; 0.071'; LOT #1478276-1. REPAIR FILLER FROM 7075T6; 0.063'; LOT#1461523-1. DRILLED COUNTERSUNK AND CHAMFJun 14, 2022 · N951WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022060915816Girt Bar · out of adjustFORWARD ENTRY GIRT BAR TOO SHORT; AFT SERVICE GIRT BAR TOO LONG / [01] RR?D BOTH GIRT BARS IAW AMM 25-66-01Jun 6, 2022 · N951WN · Boeing 7377H4 · Escape Slide
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