N488WN

Service difficulty reports · 352

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 = 'N488WN' 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 SWAA2024081610307Seal · crackedLT. HORIZONTAL STAB UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED RT HORIZONTAL STAB UPPER SLIDE SEAL IAW AMM 53-31-31-000-802. INSTALLED ATTACHING HARDWARE TO NEW RT STAB FWD UPPER SLIDE SEAL IAW SRM 51-40-02-0G-0;[02] SHOULD SAY:<BR>REMOVED LT HORIZONTAL STAB UJul 8, 2024 · N488WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024081410303Stiffener · crackedLH HORIZONTAL STAB RIB #5 (STAB STA 129.50); 3RD VERTICAL STIFFENER CRACKED.<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; .400-INCH CRACK NOTED.<BR>EQUIP ID ATS2353 DUE 01/25;[02] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER Jul 8, 2024 · N488WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2024081509556Scuff Plate · crackedFWD GALLEY DOOR SCUFF PLATE CRACKED ON AFT OUTBOARD CORNER<[01] WELDED CRACKED SCUFF PLATE IAW SRM 53-10-15-2R-2 AND SOPM 20-30-03;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.Jul 6, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024081409549Floor Panel · debondedFLOOR PANEL 241BF UPPER SKIN HAS LARGE DISBOND NEAR CENTER OF PANEL. (MARKED)<[01] DUE TO THE EXTENT OF THE DAMAGE; FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION #1Jul 6, 2024 · N488WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024081409550Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL WAS ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0128.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION #1Jul 6, 2024 · N488WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024081409551Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED PANEL 241EF IAW SRM 53-00-50-2R-0 ALONG WITH DWG 144A5810 SHEET: 129.;[02] VERIFIED COMPLETEJul 6, 2024 · N488WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024081309870Support · corrodedFWD CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION ON 18EA LOCATIONS FROM BS 396-500D; WL 156; RBL 25 FWD CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FRAME HAS CORROSION ON 18EA LOCATIONS FROM BS 396-500D WL 156 LBL 25<[01] REMOVED AND RJul 6, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024070207411Bulb · inoperativeAFT PAX DOOR EXTERIOR EMERGENCY LIGHT IS OUT<[01] REMOVED AND REPLACED THE AFT PAX EXT LIGHT BULB REF AMM 33-51-04; OPS. CHECK GOOD.Jun 30, 2024 · N488WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024062505481Bracket · out of positionFWD R1 GIRT BAR DOESNT CENTER ON FLOOR BRACKETS<[01] 04 - REPAIRED PER [AMM 25-66-00-201-NG (DOOR-MOUNTED ESCAPE SYSTEM - MAINTENANCE PRACTICES - PERMANENT)]Jun 24, 2024 · N488WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024021552519Lamp · inoperativeENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RE-LAMPED ENTRY DOOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.Feb 15, 2024 · N488WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023113025268Flashlight · inoperativeFWD GALLEY EMERGENCY EQUIPMENT CABINET LOWER FLASHLIGHT INOP<[01] R&R'D FLASHLIGHT BATTERY PER AMM 25-64-00Nov 28, 2023 · N488WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2023080385034Light · inoperativeLH COVE LIGHT INOP AT ROW 1<Aug 3, 2023 · N488WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023071477272Stiffener · missingSTIFFENER MISSING STIFFENER MISSING UNDER HANDLE.<[01] REPLACED MISSING STIFFENER PER CMM 56-10-02.Jul 10, 2023 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023051849848Wheel · damagedAFTER GEAR RETRACTION; BOTH PILOTS HEARD A THUMPING NOISE FROM NOSE GEAR WELL AREA FOLLOWED BY THE SMELL OF BURNING RUBBER.<[01] INSPECTED NOSE GEAR WHEEL WELL SPIN-DOWN SHOES & COMPONENTS FOR DAMAGE & DEGRADATION. NO DAMAGE NOTED. REMOVED AND REPLACED NOSE WHMay 18, 2023 · N488WN · Boeing 7377H4 · Wheel/Ski/FloatSDR SWAA2022072733556Trim System · failedSHORTLY AFTER TAKE OFF ELECTRIC STAB TRIM FAILED. RAN STABILIZER TRIM INOPERATIVE CHECKLIST IN QRH; MANUAL TRIM WORKED FINE. / [01] C/W FIM 27-41 TASK 803. STAB TRIM OPS CHK GOOD; NO DEFECTS NOTED. A/C OK FOR SERVICEJul 25, 2022 · N488WN · Boeing 7377H4 · Stabilizer Control SystemSDR SWAA2022071427366Light · inoperativeFWD ENTRY DOOR EXTERNAL EMERGENCY SLIDE LIGHT- LIGHT BULB IS BURNT OUT / [01] REMOVED AND REPLACED FWD ENTRY DOOR EXTERNAL EMERGENCY SLIDE LIGHT AND PERFORMED GOOD TEST OF THE NEW LAMP PER AMM 33-51-04-960-801;[02] VERIFIED REPLACEMENT OF FWD ENTRY DOOR EXTERNJul 9, 2022 · N488WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022071426365Frame · crackedRECORD MEASUREMENTS FOR CRACK ON FUSELAGE FRAME AT STA 312; ABOVE FED. (ATTACHED TO FAULT TTG8Q00DOUC0) / [01] UPDATED MEASUREMENT FIELD;[02] REPAIR ACCOMPLISHED ON CUSTOMER CARD # TTG8Q00DOUC0;[03] REPAIR ACCOMPLISHED ON CUSTOMER CARD # TTG8Q00D8QGS (M-22-153Jul 6, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022071420788Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / [01] WELDED CRACKS ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR><BR>CALIBRATED EQUIPMENT USED:<BR>WELDING MACHINE: E10583; DUE 12/22;[Jun 20, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071419123Support Bracket · crackedCRACKED SUPPORT BRACKET AT LH PORTABLE WATER TANK SUPPORT ANGLE FRONT SIDE BS 950 LBL 10 WL 180 MARKED / [01] REMOVED CRACKED SUPPORT ANGLE FROM BS 950 LBL 10 WL 180 IAW SRM 51-40-02-0G-0;[02] RECIEVED NEW SUPPORT ANGLE P/N 149A8113U6 LOCATED AND DRILLED IAW SJun 16, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022081719114Support Angle · crackedLEFT WING IB UPPER FIXED TE PANEL SUPPORT ANGLE/SEAL RETAINER CRACKED AT ORSS 265; AFT / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED LEFT WING IB UPPER TE PANEL SUPPORT/SEAL RETAINER ORSS 265 AFT; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARJun 15, 2022 · N488WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022071418837Frame · crackedFUSELAGE STA 312 FRAME IS CRACKED AT RADIUS ABOVE FWD ENTRY DOOR. (MARKED) / [01] DISCREPANCY ACCOMPLISHED ON EA NO:M-22-153-01244;[02] VERIFIED REWORK PERFORMED ON EA NO:M-22-153-01244Jun 15, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022071419109Frame · corrodedCORROSION ON PASSENGER CABIN FRAME AT BS 277 BETWEEN STRINGER 1 AND STRINGER 2L. / [01] CORROSION FOUND AT BS 277 FRAME SPLICE ANGLE BETWEEN STR 1 AND STR 2 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-Jun 15, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418835Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+5 TO STA 1016+61; RBL 13 TO LBL 13; WL 306.5. / [01] REMOVED FASTENERS ON FUSELAGE CROWN SKIN FROM STA 1016+5 TO STA 1016+61; RBL 13 TO LBL 13; WL 306.5. PER REF SRM 51-40-02 -0G;[02] REMOVED CORROSION FROM CROWN Jun 15, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022071419110Panel · delaminatedPANEL 621SB PREVIOUS REPAIR IS DELAMINATED ON OUTER SURFACE / [01] IDENTIFIED PANEL 621SB IAW SRM 57-41-01-0I-4 FIGURE 3; TABLE 3; ITEM 1. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4. A. (5). (A) - (B). DAMAGE TO BE REPAIRED IAW SRM 51-70-05Jun 15, 2022 · N488WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2022071418636Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER (TANG) IS BROKEN / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO AFT 0/B CORNER TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRMJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022071418666Angle · corrodedCORROSION ON PASSENGER CABIN SCALE ANGLE AT LBL 60 BS 312+7; BS 312+10; BS 312+13; BS 328+3; BS 328+5; BS 328+10. FWD ENTRY MOP SEAL ATTACH ANGLE. / [01] PARTIALLY COMPLETED STEPS 1-6;[02] STEPS 1 - 6 COMPLETE.<BR> <BR>VERIFIED ALL AREAS OF CORROSION NOTED AREJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418388Door · corrodedDOOR 145AL (TOILET SERVICE DOOR) INNER SURFACE IS CORRODED AT SEVERAL LOCATIONS. / [01] REMOVED TOILET SERVICE DOOR 145AL PER AMM#52-49-07-000-801;[02] FOUND SRM 52-40-01-1A-4 TO BE APPLICABLE TO THIS REPAIR.<BR><BR>REMOVED DAMAGE IN MULTIPLE LOCATIONS LOCATEDJun 14, 2022 · N488WN · Boeing 7377H4 · Service DoorsSDR SWAA2022071418661Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT RBL 12 BS 344+6; BS 344+10. / [01] CRACKED ON PASSENGER CABIN INTERCOSTAL AT RBL 12 BS 344+6; BS 344+10 WL 208 P/N 141A5410-24 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418657Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7; BS 277+14. / [01] CRACKED ON PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7; BS 277+14 WL 208 P/N 141A5410-3; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418658Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT RBL 31 BS 312+5; BS 312+11. / [01] CRACKED ON PASSENGER CABIN INTERCOSTAL AT RBL 31 BS 312+5; BS 312+11WL 208 P/N 141A5410-12 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMEJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418659Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 45 BS 312+9. / [01] CRACKED ON PASSENGER CABIN INTERCOSTAL AT LBL 45 BS 312+9 WL 208 P/N 141A5410-12 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418660Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 344+9. / [01] CRACKED ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 344+9 WL 208 P/N 141A5410-22 ; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418651Intercostal · crackedCRACK ON PASSENGER CABIN INTERCOSTAL AT BL 0 BS 927+6. / [01] REMOVED PASSENGER CABIN INTERCOSTAL UPPER ANGLE AT BL 0 BETWEEN BS 927 TO BS 947 PER SRM 51-40-02.<BR><BR>LOCATED AND DRILLED NEW INTERCOSTAL UPPER ANGLE BETWEEN BS 927 TO BS 947 BL 0 PERE SRM 51-40Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418646Channel · corrodedCORROSION ON PASSENGER CABIN MOP SEAL AT RBL 53 BS 947+5-987+7. / [01] REMOVED ON PASSENGER CABIN MOP SEAL AT RBL 53 BS 947+5-987+7 W.L 208.1 P/N 147A8540-8;AREA OT=0.080;RT=0.068 ;L=43.200'W=1.200'' ;X=0.012 WITH WITH MICROMETER ID:ATS1671<BR>S/N:65093024<BR>Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418652Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM AT BS 987 LBL 5; 8; RBL 5; 39; 43. / [01] REMOVED CORROSION ON THE UPPER CHORD OF THE BS 986.5 FLOOR BEAM IN MULTIPLE PLACES; BETWEEN LBL5-RBL43 IAW SRM 51-10-02. MAX MATERIAL REMOVED IN AREA AT RBL 43( NUTPLACE HOLE): 1.Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022071418647Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM AT BS 987 LBL 9; 18; 29; 32; 35; 38; 43. / [01] REMOVED CORROSION ON THE UPPER CHORD OF THE BS 986.5 FLOORBEAM IN MULTIPLE PLACES; BETWEEN LBL9-LBL43. MAX MATERIAL REMOVED IN AREA AT LBL 43( NUTPLACE HOLE): 1.2'LX1.0'WX0.Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022071418669Intercostal · corrodedCORROSION ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 312+5. / [01] REMOVED CORROSION ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 312+5 W.L 208.1 P/N 141A5410-13 ;AREA OT=0.080;RT=0.068 ;L=1.900'W=0.900'' ;X=0.012 WITH MICROMETER ID:E8089<BR>S/N:UNKNOWN<BR>DATJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418662Intercostal · corrodedCORROSION ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 294+9. / [01] CORROSION ON PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 294+9'' W.L 208 P/N 141A5690-1; FOUND TO BE OUT LIMITS DUE TO MISSING MATERIAL REMAINING THICKNESS=0 I.A.W SRM 53-10-51-1A-1 FOR ALLOWABLEJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418663Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM AT LBL 12 BS 294. / [01] REMOVED CORROSION ON PASSENGER CABIN FLOORBEAM AT LBL 12 BS 294 AREA REWORKED: L: 5' W: 2.1' ORIGINAL THICKNESS 0.100' MATERIAL REMOVED MORE THAN 50% FOUND TO BE OUT OF LIMIT; IAW SRM 53-10-51-1A-Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022071418664Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM AT LBL 12 BS 312. / [01] REMOVED CORROSION ON PASSENGER CABIN FLOORBEAM AT LBL 12 BS 312 AREA REWORKED: L: 4' W: 2.1' ORIGINAL THICKNESS 0.125 MATERIAL REMOVED MORE THAN 50% FOUND TO BE OUT OF LIMIT; IAW SRM 53-10-51-1A-1Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022071418665Floorbeam · corrodedCORROSION ON PASSENGER CABIN FLOORBEAM AT RBL 48 BS 328. / [01] VERIFIED SRM 53-10-51-2R-8 REPAIR 8 IS APPLICABLE FOR THIS AIRPLANE;[02] REMOVED DAMAGE ON PASSENGER CABIN FLOORBEAM AT RBL 48 BS 328 WL 208.1 AREA 2.3'X 1' X .023 IAW SRM 51-10-02-0G-0. ORIGINAL Jun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022071418668Channel · corrodedCORROSION ON PASSENGER CABIN MOP SEAL AT LBL 55 BS 294+10; BS 312+2; BS 312+13; BS 328+4. / [01] VERIFIED SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE FOR THIS AIRCRAFT.;[02] REMOVED CORROSION ON PASSENGER CABIN MOP SEAL AT LBL 55 BS 294+10; BS 312+2; BSJun 14, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418382Retainer · crackedVERT FIN PANEL 323CL LOWER RETAINER IS BENT AND CRACKED / [01] NO APPLICABLE SRM REPAIR FOR BENT AND CRACKED VERTICAL FIN ACCESS PANEL 323CL LOWER RETAINER; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED WITH NEW PER Jun 14, 2022 · N488WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2022071418150Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+10; BS 727A+10; BS 727A+14; BS 727B+2; BS 727B+6; BS 727B+10; BS 727B+14; BS 727B+18; 727C+2; BS 727C+6. / [01] VERIFIED THE APPLICABILITY OF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2;[02] UPDJun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418151Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727C+10; BS 727C+14; BS 727D+2; BS 727D+6; BS 727D+10; BS 727D+14; BS 727D+18; BS 727E+2; BS 727E+6; BS 727E+10. / [01] VERIFIED THE APPLICABILITY OF SRM 53-60-53-0I-2 AND SRM 53-00--53-1A-2;[02Jun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418153Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 767+18; BS 787+2; BS 787+6; BS 787+10; BS 787+14; BS 787+18; BS 807+6. / [01] VERIFIED THE APPLICABILITY OF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2;[02] UPDATED STEPS 1 - 7;[03] UPDATED STEPS 1 Jun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418152Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+14; BS 727E+18; BS 747+6; BS 747+8; BS 747+10; BS 747+14; BS 747+18; BS 767+6; BS 767+8; BS 767+14. / [01] VERIFY THE APPLICABILITY OF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2;[02] UPDATED SJun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418165Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+4; BS 767+8; BS 767+16. / [01] CORROSION ON AFT CARGO BAY DOOR SHIELD AT RBL 22 BS 767+4; BS767+16; FOUND TO BE OUT OF LIMITS DUE NO ALLOWABLE DAMAGE ON SRM; PART WILL BE REPAIRED BY REMPLACEMENT IAW Jun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418161Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E+10; BS 727E+14; BS 747+2; BS 747+6; BS 747+8; BS 747+10; BS 747+14; BS 747+18. / [01] VERIFIED THE APPLICABILITY OF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2;[02] UPDATED STEPS 1 - 8;[03] UPDJun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022071418162Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 867+19. / [01] REMOVED FLOOR SUPPORT SPLICE ON AFT CARGO BAY BS887 LBL4 TO RBL20 WL168 IAW SRM 51-40-02;[02] UPON FURTHER INVESTIGATION FOUND TO BE NO ALLOWABLE LIMITS FOR DAMAGE IN SRM. PART TOJun 13, 2022 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
Back to N488WN