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 SWAA2024112753522Angle · crackedCRACK ANGLE LOCATED BS663 AND RBL55 AT CENTER WING BOX 2024-672307<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] REPLACED ANGLE LOCATED BS663 BETWEEN RBL 5 AND RBL 65 AT CENTER WING BOX IAW B737-700 SRM 5Oct 26, 2024 · N201LV · Boeing 7377H4 · Wing, Center BoxSDR SWAA2024112753520Frame · crackedCRACK FRAME BS 312 AT LEVEL STRINGER 5L AT PASSENGER CABIN 2024-672290<[01] REPAIRED FRAME BS 312 AT LEVEL STRINGER 5L AT PASSENGER CABIN IAW B737-700 EA M-22-153-01244 SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BEOct 26, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024112753517Intercostal · crackedCRACK WEB BS 294.5 AT LEVEL STRINGER 16L PASSENGER CABIN 2024-672277<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BS 294.5 TO BS 303.81 AT LEVEL STRINGER 16L PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG# 141A8180; SHEET:27; REV:C.;[02] CORRECTED STOct 26, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024112753518Tie Clip · crackedCRACK TIE CLIP BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN 2024-672281<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9; DRAWING 141A8380 SHEET: 21 REV: - AND DWG 141A1110 SHOct 26, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2024112753519Stub Frame · crackedCRACK LOWER STUB FRAME BS 294.5 AT LEVEL STRINGER 17R PASS CABIN 2024-672285<[01] REPLACED LOWER STUB FRAME LOCATED BS 294.5 BETWEEN STR 13R TO STR 17R IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 141A8370 SHEET: 9 AND 10 REV: D. SEE INDIVIDUAL SIOct 26, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024112753521Angle · crackedCRACK ANGLE BS 867 BETWEEN STRINGER 1R TO STRINGER 2R AT PASSENGER CABIN 2024-672296<[01] REPLACED ANGLE BS 867 BETWEEN STRINGER 1R TO STRINGER 2R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWING 146A7901 SHEET 58 REV - MEOct 26, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024112752940Panel · crackedCRACK SUPPORT BRACKET ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER 2024-672264<[01] REPLACED SUPPORT BRACKET ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 186A3101 REV C SH 13;[02] CORRECTED STEP 1 <BR>REPLACEOct 25, 2024 · N201LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024112752938Panel · crackedCRACK SUPPORT BRACKET ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2024-672263<[01] REPLACED SUPPORT BRACKET ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 ITEM 9 AND DWG 186A3101 SHEET:13 REV: C;[02] CORRECTED STEP 1 <BR>REPLACED BLADE ASSY (SOct 25, 2024 · N201LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024112752934Rail · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS449 INTERNAL CAVITY LEADING EDGE AT RT WING 2024-672255<[01] REPLACED RAIL NUT PLATES LOCATED OFSS449 INTERNAL CAVITY LEADING EDGE AT RT WING IAW B7E7-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 13 REV Oct 25, 2024 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024112752936Rail · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS293 LEADING EDGE INTERNAL CAVITY AT RT WING 2024-672257<[01] REPLACED RAIL NUT PLATES LOCATED OFSS293 LEADING EDGE INTERNAL CAVITY AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 13 REV Oct 25, 2024 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024120252916Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 1 OUTBOARD POSITION AT LT WING 2024-672240<[01] REPLACED SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 1 OUTBOARD POSITION AT LT WING I.A.W. B737-700 SOPM 20-50-01 AND DWG-114A5010-3. REV D - SHEET 6.;[02]Oct 24, 2024 · N201LV · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2024112752914Rib · crackedCRACK FRONT SPAR INSPAR RIB LOCATED STAB STA 129.50 AND 27 INCH RT HORIZONTAL STAB 2024-672236<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 21013650Oct 24, 2024 · N201LV · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2024112752691Support · crackedCRACK ANGLE - SUPPORT LOCATED BS500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2024-672228<[01] REPLACED ANGLE-SUPPORT AND FASTENERS LOCATED BS500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 14Oct 24, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112752689Support · crackedCRACK ANGLE - SUPPORT LOCATED BS500C AFT SIDE AND S-26L FWD CARGO COMPARTMENT 2024-672226<[01] REPLACED ANGLE-SUPPORT AND FASTENERS LOC. BS500C AFT SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 AND DWG#143A7505 SHEET:9;Oct 24, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112752692Support · crackedCRACK ANGLE - SUPPORT LOCATED BS500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2024-672225<[01] REPLACED ANGLE-SUPPORT AND FASTENERS LOC. BS500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 AND DWG#143A7505 SHEET:5;Oct 24, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112752690Support · crackedCRACK ANGLE - SUPPORT LOCATED BS 500C FWD SIDE AND S-26R FWD CARGO COMPARTMENT 2024-672224<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS 500C FWD SIDE AND S-26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02; DWG 143A7505 SHEET: 6 REV: Oct 24, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112752693Support · crackedCRACK ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT 2024-672230<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG: 143A7505 SHEET: 2 REVOct 24, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112752918Rail · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS335 LEADING EDGE INTERNAL CAVITY AT LT WING 2024-672241<[01] REPLACED RAIL NUT PLATES LOCATED OFSS335 LEADING EDGE INTERNAL CAVITY AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 112A4402 SHEET: 1Oct 24, 2024 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024112752920Rail · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS303 LEADING EDGE INTERNAL CAVITY AT LT WING 2024-672242<[01] REPLACED RAIL NUT PLATES LOCATED OFSS303 LEADING EDGE INTERNAL CAVITY AT LT WING IAW B737-700 SRM 51-10-02 ITEM9 AND DWG#112A4402; SHEET:13; REV:-.;[02] CORREOct 24, 2024 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024112752922Rail · corrodedCORROSION ON RAIL NUT PLATES LOCATED OFSS288 LEADING EDGE INTERNAL CAVITY AT LT WING 2024-672243<[01] REPLACED RAIL NUT PLATES LOCATED OFSS288 LEADING EDGE INTERNAL CAVITY AT LT WING IAW B737-700 SRM 51-10-02 ITEM9 AND DWG#112A4402 SHEET:13; REV:- SEE INDIVIDUOct 24, 2024 · N201LV · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2024112752171Panel · crackedCRACK ON HOLE OF ACCESS PANEL 561BB ON TRAILING EDGE AT LT WING 2024-672178<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189443; DUE DATE: 06-MAR-25.;[02] TOOL USED: HOT BONDER PN: HCS9200B; SN: 18165044; DUE DATE: 11-APR-25;[03] TOOL USED: HOT BONDER P/N: HOct 23, 2024 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024112751458Battery Pack · inoperativeINOP BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN 2024-671987<[01] REPLACED BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E.(5)(6) TOct 22, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024112751463Light · delaminatedDELAMINATED PHOTOLUMINESCENT STRIP PAX CABIN (10EA) 2024-671993<[01] REPLACED PHOTOLUMINESCENT STRIP PAX CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802; FOR INSTALLATION STEPS SEE TASK 733-50-01-SW (TTG8Q00WK8JP);[02] CERTIFIED.<BR>REPLACED PHOTOLUMINESCENT STOct 22, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024112751842Lens · brokenBROKEN EMERGENCY LIGHT LENS OVER BULLNOSE OHSB LH SIDE AT PASSENGER CABIN (9EA) 2024-672142<[01] REPLACED EMERGENCY LIGHT LENS OVER BULLNOSE OHSB LH SIDE AT PASSENGER CABIN (9EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D(3) (A) AND (C).;[02] REPLACED EMERGENCYOct 22, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024112751841Lens · brokenBROKEN EMERGENCY LIGHT LENS OVER BULLNOSE OHSB RH SIDE AT PASSENGER CABIN (8EA) 2024-672143<[01] REPLACED EMERGENCY LIGHT LENS OVER BULLNOSE OHSB RH SIDE AT PASSENGER CABIN (8EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D(3)(A) AND (C).;[02] REPLACED EMERGENCY Oct 22, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024112751745Structure · crackedCRACK ANGLE FLOOR STRUCTURE BS 540 BETWEEN BL 0 T0 RBL 24.75 AT PASSENGER CABIN 2024-672012<[01] REPLACED ANGLE FLOOR STRUCTURE BS 540 BETWEEN BL 0 T0 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A0060 SHEET 36 REV.A<BROct 22, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112751747Structure · crackedCRACK ANGLE FLOOR STRUCTURE BS 694 AND RBL 1 CENTER SECTION 2024-672045<[01] REPLACED ANGLE FLOOR STRUCTURE BS 694 AND RBL 1 CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6 REV.A <BR>SEE INDIVIDUAL SING-OFF BELLOW.;[02] CEOct 22, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112751748Structure · crackedCRACK ANGLE FLOOR STRUCTURE BS 694 AND LBL 1 CENTER SECTION 2024-672049<[01] REPLACED ANGLE FLOOR STRUCTURE BS 694 AND LBL 1 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACOct 22, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024112651459Battery Pack · inoperativeINOP BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 LH SIDE ON PASSENGER CABIN 2024-671988<[01] REPLACED BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 LH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E.(5)(6) TOct 22, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024112651746Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE BS 694 AND RBL 24.75 CENTER SECTION 2024-672040<[01] REPLACED ANGLE FLOOR STRUCTURE BS 694 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02; DWG 111A6000 SHEET:236 REV: - AND DRAWING 273A9110 SHEET: 6 REV: A. SEEOct 22, 2024 · N201LV · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024120251456Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE AT LT WING 2024-671984<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B23316997; DUE DATE: 14-JAN-25.;[02] TOOL USED: ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; CAL DUE DATE: 11-JAOct 21, 2024 · N201LV · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2024081224996Plate · elongatedFWD RIGHT METAL CONNECTING PLATE HOLE WALLOWED OUT. FOR AFT CARGO CAP STRIP RH SIDE<[01] REMOVED AND REPLACED FWD RIGHT CONNECTING PLATE ON AFT CARGO FLOOR PANEL REFERENCE AMM25-52-10.Aug 9, 2024 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024051485123Rivet · looseGIRT BAR CAME OUT OF STOWAGE HOOK WHILE CLOSING FWD ENTRY DOOR ESCAPE SLIDE REMAINED IN STOWAGE COMPARTMENT<[01] REPOSTIONED SLIDE IN CASE PER MT 725-61-06 AND AMM 25-66-01. REPLACED LOOSE RIVET FOR GIRT BAR HOOK PER SRM 51-40-02May 12, 2024 · N201LV · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024041674549Slide · out of adjustFWD SERVICE GIRT BAR FELL WHEN DOOR OPENED<[01] ADJUSTED SLIDE IN COVER PER MT725-61-06Apr 13, 2024 · N201LV · Boeing 7377H4 · Escape SlideSDR SWAA2024022053293Charger · inoperativeFWD ENTRY DOOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED POWER SUPPLY/ BATTERY CHARGER AND BATTERY PACK PER AMM 33-51-06.Feb 17, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2024022054001Battery Pack · inoperativeFWD ENTRY DOOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED POWER SUPPLY/ BATTERY CHARGER AND BATTERY PACK PER AMM 33-51-06.Feb 17, 2024 · N201LV · Boeing 7377H4 · Emergency LightingSDR SWAA2023081487945Slide · out of adjustDUE TO PASSENGER FWD SLIDE PULLED OUT OF COMPARTMENT; DID NOT INFLATE; REQUIRES MT TASK CARD.<[01] C/W MT 725-61-06 NO DEFECT NOTEDAug 10, 2023 · N201LV · Boeing 7377H4 · Escape SlideSDR SWAA2023081487944Slide · pulledPASSENGER FWD SLIDE PULLED OUT SLIDE COMPARTMENT DID NOT INFLLATE<[01] RESECURED PASSENGER FWD SLIDE IAW AMM 25-66-00 OPS CK GOOD;[02] C/W;[03] AND C/W MT 725-61-06. (REFERENCE ADDED TO SIGNOFF ON BEHALF OF ENDALKACHEW BELACHEW BY MOC E91172)Aug 10, 2023 · N201LV · Boeing 7377H4 · Escape SlideSDR SWAA2023030610184Skin · corrodedREF: 53-00-01-1A-5-A00015-TLD; FUSELAGE SKIN AT STA 460; BL 0 IS CORRODED ON MATING SURFACE OF RA1 TRANSMIT ANTENNA AND REQUIRES REPAIR<[01] UPDATED MEASUREMENTS;[02] VERIFIED PARTIAL FOR STEP 6;[03] OK TO PAINT REPAIR;[04] APPLIED PAINT TO REPAIR IAW AMM 51-2Feb 25, 2023 · N201LV · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022111068279Girt Bar · out of adjustAFT ENTRY DOOR GIRT FABRIC GETS CAUGHT ON THRESHOLD WHEN CLOSING DOOR / [01] REINSTALLED AFT ENTRY DOOR GIRT FABRIC PER AMM 25-66-01-400-804 STEPS 6.D. (1).(C-F) AND (H).;[02] VERIFIED CORRECTIVE ACTION ITEM; INSTALLED FABRIC PROPERLY; CARD COMPLETE.Nov 6, 2022 · N201LV · Boeing 7377H4 · Escape SlideSDR SWAA2022110958627Intercostal · crackedCRACK FOUND AT INTERCOSTAL BS 946 RBL 20 WL 160 / [01] CRACKED AT INTERCOSTAL BS 946 RBL 20 WL 160 P/N 147A7580-22; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[02] FABRICATED; LOct 12, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022110758628Seal · chafedLT HORIZONTAL STAB FWD SLIDE SEAL FWD TRACK IS CHAFFED / [01] REMOVED L/H HORIZONTAL STAB FWD LOWER SLIDE SEAL FOR ACCESS PER AMM 53-31-31-000-803 STEPS 4. E. (1)-(4).;[02] REMOVED SKIN PANEL FWD OF L/H HORIZONTAL STAB FWD SLIDE SEAL TRACK FOR ACCESS PER AMM 2Oct 12, 2022 · N201LV · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022110956753Panel · pulledFLOOR PANEL 231LF UPPER SURFACE HAS MULTIPLE AERAS OF PULLED STRANDS. / [01] IDENTIFIED PANEL 231LF IAW SRM 53-00-50-0I-1 FIG 3 TABLE 3 <BR><BR>DUE TO EXTENT OF DAMAGE NEW BOARD TO BE FABRICATED IAW SRM 53-00-50-2R-0; PARA 1.A NOTE.<BR><BR>FABRICATED NEW BOARDOct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110956749Panel · delaminatedPANEL #241ZF; UPPER SURFACE PLYIS DELAMINATED / [01] IDENTIFIED PANEL 241ZF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1<BR><BR>REMOct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110956750Panel · corrodedPANEL #241AEF; HAS CORRODED INSERTS AND EDGE DAMAGE / REMOVED DELAMINATED SKIN PLIES; REMOVED SURFACE CONTAMINANTS; PREPARED REPAIR AREA APPLICATION OF POTTING COMPOUND/REPAIR PLIES; AND CLEANED REPAIR AREA; ALL ACCORDING TO SRM 53-00-50-2R-1; PARA'S 3.A; AND Oct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110956751Panel · corrodedPANEL #241ADF; HAS CORRODED INSERTS; AND EDGE DAMAGE / REMOVED DELAMINATED SKIN PLIESAPPLIED BMS 5-28; TY 19 POTTING COMPOUND (LOT# AK2DP3091K) TO AREAS OF EXPOSED CORE ACCORDING TO SRM 53-00-50-2R-1; PARA. 3.G. <BR><BR>AREAS REQUIRE ELEVATED TEMPERATURE CURE.Oct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110956752Panel · delaminatedPANEL#; 242WF HAS LOWER SURFACE DELAMINATION / POTTED REPAIR AREA WITH BMS5-28 TYPE 19 LOT NUMBER AK2DP3091K; CURED POTTING; UNDER A HEAT LAMP USING THERMOMETER ID: ATS1776 DUE: 08/2023 SANDED FLUSH; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FROM BMS9-3 Oct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110957268Panel · brokenFLOOR PANEL 241ADF HAS BROKEN CORNER ON FWD EDGE / REMOVED DELAMINATED SKIN PLIES; TAP TESTED AREA (NO DISBONDS NOTED); REMOVED SURFACE CONTAMINANTS; PREPARED REPAIR AREA FOR REPLACEMENT CORE/REPAIR PLIES; AND CLEANED REPAIR AREA; ALL ACCORDING TO SRM 53-00-50Oct 7, 2022 · N201LV · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022110956747Frame · corroded947 FRAME RBL 17-22 UPPER SURFACE IS CORRODED AND HAS GOUGE IN FRAME WL160 / FOUND TO BE OUT LIMITS I.A.W SRM 53-70-07-0L-1 FOR IDENTIFICATION AND SRM;53-00-07-1A-1.;[02] UPDATED MEASUREMENTS.;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS;[04] CUOct 6, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022110857193Intercostal · crackedINTERCOSTAL TOP ANGLE AT BL 0; BS 500D TO BS 520; WL 208 HAS MULTIPLE CRACKS / [01] NO ALLOWABLE DAMAGE FOUND ON SRM . PART TO BE REPAIR BY REPLACEMENT PER SRM 51-10-02 PARAGRAPH 9.C;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] INSTALLED FOD PROTECTION OF ELEOct 6, 2022 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
Back to N201LV