N201LV

Service difficulty reports · 350

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 = 'N201LV' 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 SWAA2022110956372Panel · delaminatedPANEL 661CB FOUND DELAMINATED ON INNER SURFACE / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [10]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARAGRAPH 4.A.(5).(B) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-1 PER SRM 57-51-01-2R-Oct 5, 2022 · N201LV · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2022110954521Wedge · delaminatedL/H I/B MAIN FLAP T/E WEDGE UPPER AND LOWER SKINS ARE DELAMINATED. / [01] REMOVED AND REPLACED L/H I/B MAIN FLAP T/E WEDGE P/N 113A2500-13 IAW SRM 51-40-02 AND AIPC 27-51-11-01B<BR>SCREW GUN ID PER2058 S/N A97G23100 CAL DUE 11/2022;[02] CORRECTED REPAIR TYPE;[Oct 5, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110956373Panel · crackedPANEL 193AL HAS SEVERAL CRACKED PULLED THROUGH FASTENER HOLES / [01] IDENTIFIED PANEL 193AL MATERIAL ACCORDING TO SRM 53-40-70-0I-1; FIG. 2; TABLE 2; ITEM 7.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA'S 2.D AND 4.B.(2). <BR><Oct 5, 2022 · N201LV · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022110954519Gusset · crackedFCB GUSSET CRACKED AT BS 500D S-19R / [01] REMOVED GUSSET FCB AT BS 500D S-19R WL 190 SRM 51-40-02.-;[02] RECEIVED NEW GUSSET P/N 143A9481-5; LOCATED AND DRILLED NEW GUSSET AT FWD CARGO BAY BS 500D STR 19R IAW SRM 51-40-05-OG-0 DWG#143A7902.;[03] REQUESTING OKOct 4, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022110954520Gusset · crackedFCB GUSSET CRACKED AT BS 500D S-19L / [01] REMOVED GUSSET FCB AT BS 500D S-19L WL 190 SRM 51-40-02.-;[02] RECEIVED NEW GUSSET P/N 143A9481-6; LOCATED AND DRILLED NEW GUSSET AT FWD CARGO BAY BS 500D STR 19L IAW SRM 51-40-05-OG-0 DWG#143A7902.;[03] REQUESTING OKOct 4, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022110950885Intercostal · crackedINTERCOSTAL COMMON TO BS 1016 BULKHEAD FWD SIDE; LBL 18; WL 208 IS CRACKED / [01] REMOVED INTERCOSTAL COMMON TO BS 1016 BULKHEAD FWD SIDE; LBL 18; WL 208 SRM 51-40-02.-;[02] RECIVED NEW INTERCOSTAL COMMON ITEM:148A2261-15;LOCATED AND DRILLED NEW INTERCOSTAL COSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022110950884Intercostal · crackedINTERCOSTAL COMMON TO BS 1016 BULKHEAD FWD SIDE; LBL 2; WL 208 IS CRACKED / [01] REMOVED INTERCOSTAL COMMON TO BS 1016 BULKHEAD FWD SIDE; LBL 2; WL 208 SRM 51-40-02.-;[02] RECIVED NEW INTERCOSTAL COMMON ITEM:148A2261-15 PO: 885663 LOCATED AND DRILLED NEW INTERSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110950889Bracket · crackedCRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL 12. / [01] REMOVED BRACKET ACB WATER SERVICE AT BS 907+12 RBL 12 IAW SRM 51-40-02-0G-0; PART WILL BE REPAIRABLE BY REPLACEMENT;[02] LOCATED AND DRILLED NEW BRACKET AT WATER SERVICE PANEL; AS PER SRMSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950902Shield · corrodedCORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+3; BS 847+8. / [01] CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+3; BS 847+8 P/N 146A8127-10;AREA OT= 0.050; RT=0.044;X=0.006;L=1.400' W=0.750' WITH DEPTH GAGE ID:ATS1225<BR>S/N:UNKNOWNSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950904Threshold · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 20 BS 787+9; BS 787+13; BS 787+15; BS 787+18; BS 807+2; BS 807+5; BS 807+17; BS 827+9; BS 827+15. / [01] PARTIAL STEP 1-9.;[02] RECEIVED NEW REPLACEMENT ACB THRESHOLD WEB P/N 146A8123U25 ; LOCATED AND DRILLED IAW SRMSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950905Threshold · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 25 BS 787+12; BS 787+16; BS 807+3; BS 807+10; BS 807+18; BS 827+1-827+4; BS 827+8; BS 827+11-827+13. / [01] PARTIAL STEP 1-10.;[02] COMPLETED ALL STEPS.<BR><BR>THIS FAULT WAS ACCOMPLISHED ON CARD# TTG8Q00F4L7J;[03] VSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950906Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+8; BS 767+12; BS 767+16. / [01] CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+8; BS 767+12; BS 767+16 P/N 146A8127-12;AREA OT= 0.050; RT=0.043;X=0.007;L=0.850' W=0.650' WITH DEPTH GAGE ISep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950913Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A+6; BS 727A+10; BS 727A+14; BS 727B+5; BS 727B+10; BS 727B+11; BS 727B+14; BS 727C+6; BS 727C+10; BS 727C+12. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE 53-00-53-1A-2<BR>AND IDENTIFISep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950911Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 747+2; BS 747+6; BS 747+10; BS 747+14; BS 747+18. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE 53-00-53-1A-2<BR>AND IDENTIFICATION 53-60-53-01-2<BR><BR>REMOVED CORROSION ON AFT CARGO BAY FSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950910Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727D+6; BS 727D+8; BS 727D+10; BS 727D+14; BS 727E+2; BS 727E+10; BS 727E+14. / [01] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727D+6 IAW IAW SRM 51-10-02 PARAGRASep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110950915Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727A+6; BS 727B+10; BS 727D+6; BS 727D+14; BS 747+2; BS 747+14; BS 747+18; BS 767+6; BS 767+10. / FABRIACATED ;LOCATED AND DRILLED ON AFT CARGO BAY L/H NEW FLOOR TO SIDEWALL SUPPORT BS 727 TO BSSep 30, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110946509Support · corrodedFWD CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT IS CORRODED FROM STA 440 TO STA 500D; WL 156.5; LBL 22 TO 24. / ;FOUND PART TO BE OUT LIMITS;IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 AND SRM 53-30-53-0I-2 IDENTIFICATION 2;TOOL USED ID ATS2678;S/N UNKNOWN;DUSep 29, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110946510Support · corrodedCORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO 500C+8; RBL 24; WL 156.5 / [01] REMOVED CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BETWEEN STA 500B+13' RBL 24; WL 156.5 MEASURE MAX.MATERIAL LOSS L=1.7' X W=.6' D=Sep 29, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110946503Track · corrodedPASSENGER CABIN SEAT TRACK HAS CORROSION BS 807+5 - 807+7 LBL 45 / [01] VERIFIED APPLICABILITY AS PER SRM 53-00-52-1A-1<BR><BR>REMOVED CORROSION ON CABIN SEAT TRACK AT DISCREPANCY REWORKED AREA: L=2'; W=1'; MAX. MATERIAL LOSS=0.021'; WAS FOUND WITHIN LIMIT IAWSep 28, 2022 · N201LV · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2022110946506Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN WING STATION 184.70 - .5' CRACK NOTED TO BE 26.5' FROM L/E / [01] TRIMMED OUT THE DAMAGED PART OF THE SKIN AT DISCREPANCY AREA; CUT OUT DIMENSIONS 1.7' X 1.0' IAW SRM 51-10-02;[02] HEFC REQUEST AT THE EDGES OF THE CUT OUT ANSep 28, 2022 · N201LV · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022110946504Plate · crackedRIGHT WING LOWER AFT T/E WAFFLE PLATE CRACKED AND ATTACH RIVETS SHEARED JUST I/B OF #2 PYLON AFT TIP / [01] REMOVED AND REPLACED RIGHT WING LOWER AFT T/E WAFFLE PLATE JUST I/B OF #2 PYLON AFT TIP IAW SRM 51-40-02 AND AIPC 57-50-00-30;[02] VERIFIED CORRECTIVE ASep 28, 2022 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022110946505Angle · crackedT/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP / [01] RECEIVED FITTING P/N 115A2953-2 LOT#1504969-1 REMOVED & REPLACED FITTING LOCATED AT DISCREPANCY AREA IAW SRM 51-40-02-0G-0 & DWG# 115A2930 REV: A.;[02] VERIFIED CORRECTIVE ACTION #1.Sep 28, 2022 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022110939802Rib · crackedLT HORIZONTAL STAB INSPAR RIB AT STAB STA 120.30 HAS CRACK ON 4TH STIFFENER FROM FWD END ON LOWER SIDE. / [01] TRIMMED OUT THE DAMAGED PART ON INSPAR RIB 120.3' 4TH STIFFENER; CUT OUT DIMENSIONS 0.5' X 0.340' IAW SRM 55-10-09-2R-4.2' CRACK NOTED IN INSPECTION Sep 27, 2022 · N201LV · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022110930700Web · corrodedCORROSION ON 1016 WEB AT AFT PASSENGER CABIN BS1016+12 LBL6 TO LBL14. MARKED. / [01] SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE TO THIS A/C<BR>REMOVED CORROSION ON ON 1016 WEB AT AFT PASSENGER CABIN BS1016+12 LBL6 TO LBL14.WL 208.1 IAW SRM 51-10-02. RESep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110930692Door · corrodedCORROSION ON AFT SERVICE DOOR MOP SILL RBL47 BS947+4 - BS986+6. MARKED. / [01] REMOVED CORROSION ON AFT DOOR MOP SILL RBL 47 BS 947+4. WL 208 P/N 147A8540-8 ORIGINAL THICKNESS IS 0.080' PER SRM 53-70-15-0I-1 IDENTIFICATION 1 TABLE 2 ITEM[20] POINT (1) MEASURE:Sep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110930697Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL44 TO RBL44. MARKED. / [01] VERIFIED APPLICABILITY OF SRM 53-70-51-01-1 FOR IDENTIFICATION AND SRM 53-70-51-1A-1 FOR ALLOWABLE LIMIT;[02] DAMAGE FOUND ON BS 986.5 FLOOR BEAM UPPER SURFACE FOUND TO BE OUT OF REPASep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022110930677Beam · crackedRT WING T/E HAS A CRACKED NUTPLATE BEAM ASSY AFT OF REAR SPAR AT RSS 290. MARKED. / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED NUTPLATE BEAM ASSEMBLY AFT OF REAR SPAR AT RSS 290; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. INSTALLSep 26, 2022 · N201LV · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2022110930684Panel · pulledPANEL 661CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION IAW SRM 51-70-04-2R-9 PARA 4 STEPS A-C .; CHOPPED FIBERS FILLED THE DEFECTIVE FASTENER HOLES & SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & Sep 26, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110930670Panel · pulledPANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / STARTED DAMAGE REMOVAL PER SRM 51-70-04-2R-9 PARA 4 STEPS A & B .;[04] COMPLETED DAMAGE REMOVAL CHOPPED FIBERS FILLED THE DEFECTIVE FASTENER HOLES & SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STESep 26, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110930669Panel · pulledPANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / STARTED DAMAGE REMOVAL PER SRM 51-70-04-2R-9 PARA 4 STEPS A & B CHOPPED FIBERS FILLED THE DEFECTIVE FASTENER HOLES & SET TO CURE IAW SRM 51-70-04-2R-9 PARA 4 STEPS D & E .;[07] USING BMS8-301/ESep 26, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110930667Panel · pulledPANEL 561BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / ] STARTED DAMAGE REMOVAL PER SRM 51-70-04-2R-9 PARA 4 STEPS A & B .;[04] COMPLETED DAMAGE REMOVALVALIDATED REPAIR PER SRM 51-70-04-2R-9;[06] USING BMS8-301/EA 9390 RESIN LOT JN1HAA6331 & CHOPPESep 26, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110930666Panel · pulledPANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) / VALIDATED REPAIR PER SRM 51-70-04-2R-9;[03] STARTED DAMAGE REMOVAL PER SRM 51-70-04-2R-9 PARA 4 STEPS A & B .;[04] COMPLETED DAMAGE REMOVAL CURED THE RESIN MIXTURE & PERFORMED THE SURFACE PREPASep 26, 2022 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022110930701Web · corrodedCORROSION ON 1016 WEB AT AFT PASSENGER CABIN BS1016+12 RBL5. MARKED. / [01] SRM 53-70-51-0I-1 IDENTIFICATION 1 AND SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 ARE APPLICABLE TO A/C N201LV.<BR> REMOVED CORROSION ON UPPER SURFACE IAW SRM 51-10-02-0G-0 . <BR>REMOVED (2ESep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110930704Strap · corrodedCORROSION ON TENSION STRAP AT AFT PASSENGER CABIN RBL3 BS1016+6 - BS1016+14. MARKED. / [01] SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 IS APPLICABLE TO THIS A/C<BR>REMOVED CORROSION ON PASSENGER CABIN FLOOR AFT STRAP AT RBL 3 BS 1016+6 TO BS1016+14 WL 208.1 IAW SRM Sep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110930695Support · corrodedCORROSION ON FLOOR SUPPORT AT AFT PASSENGER CABIN BS947+9 RBL8. MARKED. / [01] REMOVED CORROSION ON FLOOR SUPPORT AT AFT PASSENGER CABIN BS947+9 RBL 8 WL 208.1. IAW SRM 51-10-02. REWORKED AREA L=4'X W=2' MAX MATERIAL LOSS 0.009' REMAINING THICKNESS IS 0.065' OSep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110930696Support · corrodedCORROSION ON FLOOR SUPPORT AT AFT PASSENGER CABIN BS947+9 RBL12. MARKED. / [01] REMOVED CORROSION ON FLOOR SUPPORT AT AFT PASSENGER CABIN BS947+9 RBL 12 WL 208.1. IAW SRM 51-10-02. REWORKED AREA L=5'X W=2' MAX MATERIAL LOSS 0.008' REMAINING THICKNESS IS 0.066'Sep 26, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110930680Gusset · crackedRSS274; UPPER FIXED T/E PANEL SUPPORT GUSSET CRACKED AT ATTACH POINT ABOVE #1 PYLON AFT TIP / [01] RECEIVED FITTING P/N 115A2953-1 LOT#1505243-1. REMOVED & REPLACED FITTING LOCATED AT DISCREPANCY AREA IAW SRM 51-40-02-0G-0 & DWG# 115A2930 REV: A.;[02] VERIFIEDSep 26, 2022 · N201LV · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022110930362Panel · brokenAFT CABIN FLOOR PANEL 242XF IS BROKEN / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.B.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED DAMAGED SKIN Sep 25, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110922153Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 268.25+5; LBL 10; WL 208. / [01] VERIFIED THE APPLICABILITY OF SRM 53-10-51-0I-2 AND SRM 53-10-51-1A-1;[02] REMOVED CORROSION ON INTERCOSTAL AT STA 268.25 +5 ; LBL 10 ; WL 208 IAW SRM 51-10-02 ; ORIGINAL THICKNESS IS 0.080' MAXISep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110922155Door · corrodedCORROSION ON FWD ENTRY DOOR MOP SILL AT STA 312+4; 312+13; AND 328+14; LBL 58; WL 208. / [01] VERIFIED THE APPLICABILITY OF SRM 53-10-15-0I-1 AND SRM 53-10-15-1A-1;[02] UPDATED STEPS 1 ; 2 AND 3;[03] VERIFIED PARTIAL STEPS 1;2 AND 3.;[04] VERIFIED MEASUREMENT Sep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110922154Flange · corrodedCORROSION ON STA 344 FLOOR BEAM UPPER FLANGE FROM LBL 7 TO LBL 13; WL 208. / [01] SRM 53-10-51-0I-2 IDENTIFICATION 2 AND SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 ARE APPLICABLE TO THIS A/C;17] FABRICATED 2 EA REPAIR STRAPS FROM MATERIAL 7075T6 #.125 LOT NBR 136971Sep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022110922151Beam · corrodedCORROSION ON STA 328 FLOOR BEAM AT RBL 42 AND RBL 55; WL 208. / [01] SRM 53-10-51-0I-2 IDENTIFICATION 2 AND SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 ARE APPLICABLE TO THIS A/C;[02] REMOVED CORROSION ON THE FLOOR BEAM UPPER FLANGE OF BS 328 AT RBL 42 AND RBL 55; WLSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022110922150Intercostal · corrodedCORROSION ON INTERCOSTAL UPPER FLANGE AT STA 328+12; LBL 11; WL 208. / [01] CORROSION ON INTERCOSTAL UPPER FLANGE AT STA 328+12; LBL 11; WL 208 P/N 141A5410-17 AREA OT= 0.080''; RT=0.065'';X=0.015'';L=1.500'' WITH DEPTH GAGE ID:ATS2473<BR>S/N:UNKNOWN<BR>DATE:0Sep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110922143Intercostal · corrodedCORROSION ON INTERCOSTAL UPPER FLANGE AT STA 312+2 TO 312+5; RBL 11; WL 208. / [01] ORROSION ON INTERCOSTAL UPPER FLANGE AT STA 312+2 TO 312+5; RBL 11; WL 208 P/N 141A5410-14 AREA OT= 0.080''; RT=0.068'';X=0.012'';L=2.100'' WITH DEPTH GAGE ID:ATS2473<BR>S/N:UNSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110922142Intercostal · brokenBROKEN INTERCOSTAL AT STA 277+8; WL 208; RBL 2. / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-01-2 FOR IDENTIFICATION AND SRM 53-30-53-1A-1 FOR ALLOWABLE LIMIT;[02] DAMAGE FOUND AT INTERCOSTAL BS 277+8; WL 208; RBL 2; P/N 141A5410-12 1' LONG FOUND TO BE OUT OFSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110922144Intercostal · crackedCRACKED INTERCOSTAL AT STA 312+4 AND 312+10; RBL 31; WL 208. / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-01-2 FOR IDENTIFICATION AND SRM 53-30-53-1A-1 FOR ALLOWABLE LIMIT;[02] DAMAGE FOUND AT INTERCOSTAL BS 312+4 ; RBL 31; WL 208 P/N 141A5410-12 1' LONG; FOUSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110922145Intercostal · crackedCRACKED INTERCOSTAL AT STA 312+6; LBL 48; WL 208. / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-01-2 FOR IDENTIFICATION AND SRM 53-30-53-1A-1 FOR ALLOWABLE LIMIT;[02] DAMAGE FOUND AT INTERCOSTAL BS 312+6; LBL 48; WL 208; P/N 141A5410-12 1' LONG FOUND TO BE OUTSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110922149Intercostal · crackedCRACKED INTERCOSTAL AT STA 328+6; LBL 48; WL 208. / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-01-2 FOR IDENTIFICATION AND SRM 53-30-53-1A-1 FOR ALLOWABLE LIMIT;[02] DAMAGE FOUND AT INTERCOSTAL BS328+6; LBL 48; WL 208 P/N 141A5410-16 1' LONG FOUND TO BE OUT OSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110922141Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 277+5 TO 277+15; LBL 12; WL 208. / [01] CORROSION ON INTERCOSTAL AT STA 277+5 TO 277+15; LBL 12; WL 208 P/N 141A5650-3 AREA OT= 0.070''; RT=0.055'';X=0.015'';L=1.800'' WITH DEPTH GAGE ID:ATS2473<BR>S/N:UNKNOWN<BR>DATE:08/2022<BRSep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110922146Intercostal · corrodedCORROSION ON INTERCOSTAL FROM STA 294.5 TO 312; LBL 11; WL 208. / [01] CORROSION ON INTERCOSTAL FROM STA 294.5 TO 312; LBL 11; WL 208 P/N 141A5690-1 AREA L=15.00'' WITH DEPTH GAGE ID:ATS2473<BR>S/N:UNKNOWN<BR>DATE:08/2022<BR>DUE:08/2023<BR>FOUND TO BE OUT LIMISep 24, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
Back to N201LV