N472WN

Service difficulty reports · 281

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 = 'N472WN' 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 SWAA2022042090491Flap · debondedLT WING O/B AFT FLAP DISBONDED ON LOWER SURFACE AT I/B T/E / [01] LEFT WING O/B AFT FLAP LOWER SURFACE I/B CORNER WAS REPAIRED ON ATS COMPONENTS JOB # 548604; SWA RO # P2796384-1. L/W O/B AFT FLAP REMOVED AND INSTALLED ON FAULT TTG8Q00BMEUE;[02] VERIFIED CORREApr 1, 2022 · N472WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022041990171Strap · corrodedAFT CARGO BAY FLOOR PANEL SPLICE STRAP BS 767 HAS CORROSION; LBL 15; WL 156 / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02;STEP 9.;[02] RECEIVED NEW PART SPLICE STRAP AFT CARGO BAY BS 767 LBL1Mar 31, 2022 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041989264Floor Panel · crackedPASSENGER CABIN FLOOR PANEL 241ADF LOWER SKIN AT O/B AFT CORNER IS CRACKED. / [01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 6. THE DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.B.(1) AND WILL BE REPAIRED IAW SRM 53-00-50-2R-1. REMOVEMar 30, 2022 · N472WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022042088616Angle · crackedFWD SERVICE DOOR FWD LOWER STUB BEAM O/B ANGLE CRACKED BS294.5 RBL 58 WL 210 FWD SERVICE DOOR FWD LOWER STUB BEAM CRACKED BS294.5 RBL 58 WL 210 / [01] REMOVED FWD SERVICE DOOR FWD LOWER STUB BEAM O/B ANGLE FROM BS 294.5; RBL-58; WL- 210 IAW SRM 51-40-02-0G-0;[Mar 28, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022042088615Beam · crackedFWD SERVICE DOOR FWD LOWER STUB BEAM CRACKED BS294.5 RBL 58 WL 210 / [01] REMOVED FWD SERVICE DOOR FWD LOWER STUB FRAME FROM BS 294.5 RBL 58 WL 210 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLET FWD SERVICE DOOR FWD LOWER STUB FRAME BS 294.5 RBL 58 PER SRM 51-Mar 28, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022041988888Floor Panel · crackedPASSENGER CABIN FLOOR PANEL 242VF LOWER SKIN IS CRACKED ALONG I/B AFT EDGE. (MARKED) / [01] IDENTIFIED PANEL 242VF IAW SRM 53-00-50-0I-1 FIGURE 6. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.B.(1). DAMAGE WILL BE REPAIRED IAW SRM 53-00-Mar 28, 2022 · N472WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022041988007Stub Frame · crackedFWD SERVICE DOOR UPPER FWD CORNER STUB FRAME IS CRACKED BY LATCH FITTING / [01] LOCATED AND DRILLED NEW FWD SERVICE DOOR UPPER FWD CORNER STUB FRAME PER SRM 51-40-05 AND DWG 141A8370 OK TO INSTALL PART;[02] VERIFIED CORRECTIVE ACTION 1; OK TO INSTALL;[03] INSTMar 25, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022042085229Bracket · crackedLOWER BULB SEAL BRACKET AT ORSS 261+13 IS CRACKED. (MARKED) / [01] REMOVED AND REPLACED LOWER BULB SEAL BRACKET AT ORSS 261+13 IAW SRM 51-40-01-0G-0 PARA. 4.;[02] INSPECTION COMPLETEMar 18, 2022 · N472WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022042085225Panel · delaminatedRT WING L/E PANEL 621DB HAS DELAMINATION ALONG L/E / [01] PART/MATERIAL IDENTIFIED PER SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 2 .<BR>DELAMINATION ALONG THE L/E EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-41-01-1A-1. PARA 4 A ZONE 1.<BR>REPAIR TO BE PERFORMEDMar 18, 2022 · N472WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022042085226Panel · crackedRT WING L/E PANEL 621PB FWD O/B CORNER IS CRACKED / [01] PART/MATERIAL IDENTIFIED PER SRM 57-41-01-0I-4 FIGURE 3 TABLE 3 ITEM 1 .<BR>FURTHER EXAMINATION FOUND 3 ADDITIONAL DAMAGED AREAS ALONG THE EDGE BAND AT FASTENER HOLES THAT EXCEED THE ALLOWABLE DAMAGE LIMMar 18, 2022 · N472WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2022042085224Frame · crackedCRACK IN RADIUS OF FRAME AT B.S. 312 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] REMOVED DAMAGE BY TRIMMING FRAME RADIUS AND FLANGE L=0.6' X W=0.5' MAINTAINING 0.5' RADIUS IAW SRM 51-10-02.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REQUEST HFEC INSPECTION ALONMar 17, 2022 · N472WN · Boeing 737* · Fuselage Main, FrameSDR SWAA2022042084733Angle · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED FROM STA 727B+10 TO STA 767; WL 156; RBL 22. / [01] REMOVED CORROSION ON AFT CARGO TO SIDEWALL SUPPORT AT STA 727B+10; STA767 .AT DISCREPANCY AREA FOUND TO BE OF LIMITS AT STA 727B+10 L=1.5' W=0.700' D=0.014'Mar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042084734Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED FROM STA 727C+6 TO STA 787+6; WL 156; LBL 22. / [01] REMOVED CORROSION ON AFT CARGO TO SIDEWALL SUPPORT AT STA 727C+6; STA 787+6 AT DISCREPANCY AREA FOUND TO BE OUT OF LIMITS AT STA 727C+6 L=2' W=0.800' D=0.0Mar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042084735Shield · corrodedAFT CARGO BAY DOOR CUTOUT FWD SHIELD FROM STA 767+3 TO STA 767+16; WL 156; RBL 23. / [01] THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9C.-;[02] VERIFIED APPLICABILITY OMar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042084736Shield · corrodedAFT CARGO BAY DOOR CUTOUT AFT SHIELD IS CORRODED AT STA 847+19; WL 165; RBL 23. / [01] THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9C.-;[02] VERIFIED APPLICABILITY OF SMar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042084737Support · corrodedAFT CARGO BAY AFT BULKHEAD SUPPORT IS CORRODED AT STA 947; RBL 24; WL 179. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS FOR ALLOWABLE DAMAGE AND SO PART ISREPAIRABLE BY REPLACEMENT;PER SRM 51-10-02-OG-0 STEP 9;[02] REMOVED AFT BULKHEAD SUPPORT ANGLMar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042085161Shear Web · corrodedCORROSION ON SHEAR WEB AT B.S. 1016+5 - B.S. 1016+12; L.B.L. 5 - L.B.L. 19; W.L. 208.1. / [01] THIS STRUCTURAL ITEM DOES NOT HAVE ENTRIES IN SRM FOR ALLOWABLE DAMAGE LIMITS; WILL BE REPAIRED BY REPLACEMENT. PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] VERIFIED CORREMar 17, 2022 · N472WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022042085162Tension Tie · corrodedCORROSION ON SHEAR WEB TENSION STRAP AT B.S. 1006+3 - 1016+12; L.B.L. 3; W.L. 208.1. / [01] THIS STRUCTURAL ITEM DOES NOT HAVE ENTRIES IN SRM FOR ALLOWABLE DAMAGE. TENSION STRAP WILL BE REPAIRABLE BY REPLACEMENT. PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] VERIFIEDMar 17, 2022 · N472WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022042085158Tension Tie · corrodedCORROSION ON SHEAR WEB TENSION STRAP AT B.S. 1016+7 - 1016+12; R.B.L. 3; W.L. 208.1. / [01] THIS STRUCTURAL ITEM DOES NOT HAVE ENTRIES IN SRM FOR ALLOWABLE DAMAGE IS REPAIRABLE BY REPLACEMENT. PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION #Mar 17, 2022 · N472WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022042085159Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; L.B.L. 35 - L.B.L.45; W.L. 208.1. / [01] SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE TO THIS A/C;[02] REMOVED SEVERAL AREAS OF CORROSION ON FLOOR BEAM UPPER SURFACE AT BS 986.5 FROM LBL35-LBL45; WL 20Mar 17, 2022 · N472WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022042085163Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; R.B.L. 35 - R.B.L.45; W.L. 208.1. / [01] SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE TO THIS A/C;[27] FABRICATED; LOCATED AND DRILLED FLOOR BEAM REPAIR PARTS AT BS 986 ; FROM LBL 55 TO RBL 55 WL 208.1Mar 17, 2022 · N472WN · Boeing 737* · Fuselage Main, Floor BeamSDR SWAA2022042085160Channel · corrodedCORROSION ON AFT SERVICE DOOR MOP SILL AT B.S. 947+10 - B.S. 986.5; L.B.L.53; W.L. 208.1. CORROSION ON AFT SERVICE DOOR MOP SILL AT B.S. 947+10 - B.S. 986.5 R.B.L.53 W.L. 208.1. / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOP SILL AT B.S. 947+10- B.S. 986.5 RMar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042085165Shield · corrodedCORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23. / [01] FWD CARGO BAY; AFT SHIELD ON UPPER SURFACE CORRODED NO HAVE ENTRIES ALLOWABLE DAMAGE IN SRM; MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 ITEM 9.C.;[02] REMOVED AFT SHIELD AT FWD CARGMar 17, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042085214Channel · corrodedCORROSION ON FORWARD SERVICE DOOR MOP SILL AT B.S. 294.5 - B.S. 328; R.B.L. 60; W.L. 208.1. / [01] REMOVED CORROSION FROM FSD MOP SILL IN AREA OF 6' X 2' ORIGINAL MATERIAL THICKNESS 80' REMAINING MATERIAL THICKNESS 0.040' FOUND TO BE OUT OF LIMIT IAW SRM 53-10Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042085181Fitting · corrodedCORROSION ON FORWARD ENTRY DOOR GIRT BAR ATTACH POINT BRACKET AT B.S. 344; L.B.L. 56; W.L. 208.1. / [01] NO FOUND ALLOWABLE DAMAGE ON SRM 53-10-15-1A-1 FOR CORROSION ON GIRT BAR FITTING FWD ENTRY DOOR BS 344 LBL56 WL. 208.1; PART REPAIRABLE BY REPLACEMENT IAW Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022042085180Fitting · corrodedCORROSION ON FORWARD ENTRY DOOR GIRT BAR ATTACH POINT BRACKET AT B.S. 312; L.B.L. 56; W.L. 208.1. / [01] NO FOUND ALLOWABLE DAMAGE ON SRM 53-10-15-1A-1 FOR CORROSION ON GIRT BAR FITTING FWD ENTRY DOOR BS 312 LBL56 WL. 208.1; PART REPAIRABLE BY REPLACEMENT IAW Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022042085217Channel · corrodedCORROSION ON FORWARD LAVATORY FLOOR SUPPORT CHANNEL AT B.S. 294.5 - B.S. 312; L.B.L. 10; W.L. 208.1. / [01] REMOVED CORROSION ON FWD LAV SUPPORT CHANNEL BS 294-312 LBL 10 WL 208.1 AREA OF 6'X1.5' 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS I.A.W SRM 53-10-51-Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042085216Channel · corrodedCORROSION ON FORWARD LAVATORY FLOOR SUPPORT CHANNEL AT B.S. 277 - B.S. 294.5; L.B.L. 11; W.L. 208.1. / [01] REMOVED CORROSION ON FWD LAVATORY FLOOR SUPPORT CHANNEL BS 277-294.5 LBL11 WL 208.1 AREA OF 2'X2'X.030' ORIGINAL THICKNESS .188 FOUND TO BE OUT OF LIMITMar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042085179Scuff Plate · corrodedCORROSION ON FORWARD ENTRY DOOR CENTER SCUFF PLATE INBOARDSUPPORT AT B.S. 328 - B.S. 360; L.B.L. 60; W.L. 208.1. / [01] REMOVED CORROSION ON FWD ENTRY DOOR CENTER SCUFF PLATE INBOARDSUPPORT AT BS 328 TO BS 360 ;LBL 60; WL 208.1. IAW SR 51-10-02 PARA#15;EVALUATMar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022042085215Channel · corrodedCORROSION ON FORWARD ENTRY DOOR MOP SILL AT B.S. 328 - B.S. 360; L.B.L. 60; W.L. 208.1. / [01] REMOVED CORROSION FROM FWD ENTRY DOOR MOP SILL IN AREA OF 2' X 2' ORIGINAL MATERIAL THICKNESS 0.090' REMAINING MATERIAL THICKNESS 0.020' FOUND TO BE OUT OF LIMIT IAWMar 17, 2022 · N472WN · Boeing 7377H4 · DoorsSDR SWAA2022041985196Floor Panel · pulledFLOOR PANEL 242AF UPPER SURFACE HAS MULTIPLE COMPOSITE STRANDS PULLED IN MULTIPLE AREAS. / [01] IDENTIFIED PANEL 242 AF IAW DRAWING 144A5810 SHEET 132. DUE TO THE EXTENT OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL USING BMS4-17 TYPE VI LOT NUMBER 1482614-1Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022041985211Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 277-294.5; R.B.L. 1; W.L. 208.1. / [01] LOCATED AND DRILLED NEW INTERCOSTAL AT B.S 277 - 294.5 ; RBL 1 WL 208.1 IAW SRM 51-40-05 AND DWG# 141A5410 ; OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.<BR><BR>OK TO INSTALL NEW PART.;[03Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022041985212Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 294.5 - 312; R.B.L. 15; W.L. 208.1. / [01] REMOVED INTERCOSTAL AT BS294.5 - BS 312 RBL 15 WL 208.1 IAW SRM 51-40-02;[02] SRM 51-10-51-0I-2 FOR IDENTIFICATION AND SRM 53-10-51-1A-1 FOR ALLOWABLE DAMAGE ARE APPLICABLE;[03] EVALUATED CMar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022041985213Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 312-328; R.B.L. 32; W.L. 208.1. / [01] LOCATED AND DRILLED NEW INTERCOSTAL AT B.S 312 - 328 ; RBL 32 WL 208.1 IAW SRM 51-40-05 AND DWG# 141A5410 ; OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1. <BR><BR>OK TO INSTALL NEW PART.;[03]Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022041985223Bear Strap · crackedCRACK IN BEAR STRAP AT B.S. 294.5 BETWEEN STRINGERS 8 RIGHT AND 9 RIGHT JUST FORWARD OF FORWARD SERVICE DOOR. / [01] TRIMED DAMAGED AREA AT BEARSTRAP BS 294.5 BETWEEN STR 8 - STR 9 RIGHT JUST FWD OF FWD SERVICE DOOR L=1.2 W= 1.0 PER SRM 53-10-01-2R-6 REP. 6 STMar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2022041984727Panel · delaminatedPANEL 193AR OUTER SKIN IS DELAMINATED. (MARKED) / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 18. <BR>UPON INSPECTION OF PANEL FOUND 1EA ADDITIONAL AREA OF DELAMINATED SKIN ON OUTER SURFACE 36' FROM I/B EDGE; 16' FROM FWDMar 17, 2022 · N472WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022041984731Bulkhead · crackedAFT CARGO BAY FWD BULKHEAD SUPPORT BRACKET IS CRACKED AT STA 727+2; WL 163; RBL 5. / [01] THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION Mar 17, 2022 · N472WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2022042084686Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8; W.L. 163. / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT);08] FABRICATED; LOCATED AND DRILLED REPLACEMMar 16, 2022 · N472WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022042084687Barrier · crackedB.S. 663 VAPOR BARRIER IS CRACKED AROUND LEFT HAND PACK EXHAUST DUCT CUT OUT AT L.B.L. 14; W.L. 150. FORWARD SIDE OF VAPOR BARRIER. / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 57-10-10-0I-2 FIG.2; SHT.1; TABLE 2; AND ITEM 4. FOUND CRACKS TO BE OUT OF ALLOWAMar 16, 2022 · N472WN · Boeing 7377H4 · Wing StructureSDR SWAA2022042084211Beam · corrodedCORROSION ON UPPER SURFACE OF B.S. 270 LATERAL BEAM AT L.B.L. 10 - R.B.L. 10; W.L 207.54. / [01] SRM 53-10-51-0I-2 FOR IDENTIFICATION AND SRM 53-10-51-1A-1 FOR ALLOWABLE DAMAGE ARE APPLICABLE;[02] REMOVED CORROSION AT DISCREPANCY AREA; L=20.' X W=.90' X D=0.02Mar 15, 2022 · N472WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022042084212Intercostal · corrodedCORROSION ON UPPER SURFACE OF SUPPORT INTERCOSTAL AT B.S. 259-270 AT L.B.L. 3 - R.B.L. 3; W.L 207.54. / [01] SRM 53-10-51-0I-2 FOR IDENTIFICATION AND SRM 53-10-51-1A-1 FOR ALLOWABLE DAMAGE ARE APPLICABLE;[02] REMOVEVED CORROSION AT DISCREPANCY AREA L=3.' X W=1Mar 15, 2022 · N472WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022042084186Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 163. / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT);07] FABRICATED; LOCATED AND DRILLED REPLACEMMar 15, 2022 · N472WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2021050598799Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31Jul 9, 2020 · N472WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2020071098807Battery Pack · no testEMERGENCY LIGHTING BATTERY PACKS IN LOCATIONS M1669; M1672; AND M1675 FAILED CAPACITY TEST. / R&R EMERGENCY LIGHTING BATTERY PACKS IN LOCATIONS M1669; M1672; AND M1675 PER AMM 33-51-06.Jul 9, 2020 · N472WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020051876443Light · inoperativeRH OVER WING EXIT EMERGENCY LIGHT AT AFT FRAME HAS 2 EA BULBS INOP / RELAMPED RH OVER WING EXIT EMERGENCY LIGHT AT AFT FRAM; AND PERFORMED GOOD NEW LAMP TEST PER AMM 33-51-01-960-801. 81136U 10MAY20May 10, 2020 · N472WN · Boeing 7377H4 · Emergency LightingSDR SWAA2020051176437Connector · disconnectedLH OVER WING LOWER EMERGENCY EXIT LOCATOR INOP / TROUBLESHOT L/H OVERWING LOWER EMERGENCY EXIT LOCATOR; FOUND CONNECTOR D03670 NO CONNECTED; RE-CONNECTED CONNECTOR D03670 AND PERFORMED GOOD OPS TEST OF EMERGENCY LIGHTS AS PER AMM 33-51-00-710-801 59391U 10MAY2May 10, 2020 · N472WN · Boeing 7377H4 · Light System WiringSDR SWAA2020051846169Support Angle · corroded***CORROSION*** ON ACB SHIELD SUPPORT ANGLE BS 767-787; RBL 20; WL 165 / REMOVED AND REPLACED ON ACB SHIELD SUPPORT ANGLE FROM BS 767 - 787 RBL20; WL765 P/N 146A8125-53: PO #777752/1; IAW SRM 51-40-02; DWG 146A8123 AND DWG 146A0081.Apr 29, 2020 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020051846168Intercostal · crackedFCB HAS A CRACKED INTERCOSTAL AT BS500-500A LBL24 / REMOVED AND REPLACED INTERCOSTAL AT BS 500-500A LBL24 IAW DWG # 143A7505; PN# 143A7510-15. PO# 776873Apr 29, 2020 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021082745154Balance Weight · corroded***CORROSION*** AT VERTICAL STAB ON RUDDER COUNTER BALANCE WEIGHT. MARKED / REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT PER CMM 55-40-09 PG 301 & 302 STEP 2C(2) AND CMM 55-40-09 PG 704 & 705 STEPS 2C(3)&(4) VERIFIED TORQUE PER SOPM 20-50-18 TABLE 6Apr 25, 2020 · N472WN · Boeing 7377H4 · Rudder StructureSDR SWAA2021081545180Shield · corroded***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL158 / REMOVED AND REPLACED FWD SHIELD AT ACB FROM BS 767 TO BS 787 RBL21 WL158; P/N 146A8127-12; PO #774635/1; IAW SRM 51-40-02; DWG 146A0081Apr 25, 2020 · N472WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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