JASC 5330

Service difficulty reports · 79,329

Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 jasc_code = '5330'
  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 R61A2022072600469Shear Plate · corrodedFWD CARGO SHEAR CLIP AT FR 17 RH BTWN STR RH 25 & 26 CORRODED. R&R IAW SRM 51-41-01 7 51-41-02.Jul 9, 2022 · N635RW · Emb ERJ170100SESDR CALA2022071101702Panel · crackedFR36 PRESSURE DECK BETWEEN LH 765 AND RH, HOLES 2,4,10,11,13,15, 16,19,20,21,24,29,31,32,40 HAVE CRACK IN PRESSURE DECK LAYER GEN ERATED BY V892444 AT HAECO LCQ PER NR 9294638 (30638) AD RELATED SUPPORT TASK INTERIM REPAIR PERFORMED ON FR36 PRESSURE DECK BETWEJul 9, 2022 · N430UA · Airbus A320232SDR CALA2022071101701Pressure Deck · crackedFR36 PRESSURE DECK BETWEEN RH 765 AND RH 1523, HOLES 5,10,12,13, 14,15,16,17,18 HAVE CRACK INDICATIONS IN PRESSURE DECK LAYER AD RELATED SUPPORT TASK, GENERATED BY V892444 AT HAECO LCQ PER NR 9 294640 (30640) 1-7 FOR AFFECTED HOLE LOCATIONS. PER PART 1 STEP.2Jul 9, 2022 · N430UA · Airbus A320232SDR SWAA2022072827077Baffle · crackedFWD CARGO COMPARTMENT BAFFLE RBL 24 CRACKED. STA 500B-500C WL-156.4 / [01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BAFFLE AT RBL 24 STA 500B-500C PER B737-700 SRM 51-40-02-0G-0. HUMBERTO MEDINA 26340.;[02] VERIFIED 1Jul 8, 2022 · N485WN · Boeing 7377H4SDR SWAA2022072827078Baffle · crackedFWD CARGO COMPARTMENT BAFFLE LBL 24 CRACKED. STA 500-500A WL-156.4 / [01] REMOVED AND REPLACED BAFFLE AT STA 500-500A LBL 24 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[02] VERIFIED 1Jul 8, 2022 · N485WN · Boeing 7377H4SDR DALA2022071104823Stringer · dented(LOG 2311631) DURING INSPECTION FOUND DENT BETWEEN STA 727G AND 727H JUST O/B OF STR 2R. REPAIRED PER ERA 600408-14 REV. ORIG.Jul 8, 2022 · N371DA · Boeing 737832SDR DALA2022071104822None · none(LOG 2311630) DURING INSPECTION FOUND DENT AT STA 727G BETWEEN STR 2R AND STR 3R. REPAIRED PER ERA 600408-14 REV. ORIG.Jul 8, 2022 · N371DA · Boeing 737832SDR FDEA202207071691Skin · crackedEMPENNAGE: AFT FUSELAGE RIGHT HAND SKIN AT APU EXHAUST DOOR CUTOUT AREA APPROXIMATELY STATION 2140 LONGERON -36 RIGHT FOUND WITH 1 INCH LENGTH CRACK AS MARKED. EMPENNAGE : AFT FUSELAGE RIGHT HAND SKIN AT APU EXHAUST DOOR CUTOUT AREA APPROXIMATELY STATIONJul 7, 2022 · N593FE · Doug MD11FSDR IPXA2022072384468Stiffener · crackedINSPECTION TYPE:3CAFT CARGO COMPARTMENT VERTICAL STIFFENER CRACK AT STA.1841 LON 47R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR).Jul 7, 2022 · N250UP · Doug MD11FSDR DALA2022070804768None · none(LOG 2310538) DURING ACCOMPLISHMENT OF THE IDTV DE-MOD AND VIASAT PROTOTYPE INSTALLATION IN ATL, SEVERAL DEVIATIONS TO THE PROJECT WERE NOTED. THESE DEVIATIONS ARE THE FOLLOWING: MTC REPORTED TWO (2) DENTS COMMON THE SKIN JUST OUTBOARD OF S-2R AND BETWEEN STA Jul 7, 2022 · N371DA · Boeing 737832SDR CALA2022070801686Fitting · damagedLH KEEL BEAM & MLG DOOR FITTING HAS DISCREPANT HOLES. LOCATIONS & DETAILS. PER PART 1.2 OF ECRA "ACCOMPLISH A PART 3 OF LATEST REVISION OF ECRA 5330-06961 ON OR BEFORE PERMANENT REPAIR OF THE LH MLG DOOR FITTING KEEL BEAM HOLES PER 24-JUN-2023." PERFORMED INTJul 7, 2022 · N430UA · Airbus A320232SDR MK1Y20220706013Skin · out of limitsEXTERNAL FUSELAGE SKIN, STA 226 – STA 347, STR-28L – STR-29L: NRC M0143-EXTERNAL FUSELAGE SKIN BS 226.5 AND 2.2” BELOW STR 29L: SKIN THICKNESS: 0.080”. REMOVED FASTENER: JO-BOLT 0.185” DIA.OS-1 EXISTING REPAIR WASHER: DIAMETR: 0.580”, THICKNESS: 0.065”. NRC MJul 6, 2022 · N203CM · Boeing 767323SDR MK1Y20220706009Skin · damagedDURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 212 AND STA 303, STR-29L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT AREA IS LOCATED COMMON TO THE EXISTING FASTENERS. AFTER INSPECTIJul 6, 2022 · N203CM · Boeing 767323SDR MK1Y20220706005Skin · scratched: EXTERNAL FUSELAGE SKIN, STA 1487, STR-22L – STR-23L: DURING MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AT DATUM LOCATION. THE DAMAGE WAS BLENDED OUT AND FOUND WITHIN LIMITS, HOWEVER, THE BLEND OUT IS AMONG THE FASTENERS THAT PROHIBITED PER SRM 53-0Jul 6, 2022 · N203CM · Boeing 767323SDR CALA2022070601651None · crackedRH FRAME 35 STR 30 RH HOLES #1 AND #2 HAVE CRACK INDICATIONS. PERMANENT RPR AT FR 35 STR 30 RH PER PART 3 OF THE LATEST REV OF 9290225 AND 9290224 IAW ECRA 5330-06963 PART 1.2. ECRA 5330-06963 ON OR BEFORE 30-DEC-22.ALL WORK ACMP ON HAECO NR ACMP INTERIM RPR AJul 6, 2022 · N434UA · Airbus A300*SDR DALA2024070506795Skin · dented(LOG 2307066) DURING MAINTENANCE INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN (P/N: 141A3721-46) AT APPROX. BS 255.6, ABOVE STR 17R. DAMAGE REPAIRED PER ERA 600528-14.Jul 5, 2022 · N865DN · Boeing 737932ERSDR ASAA2022070539338Skin · corrodedLOWER FUSELAGE, JSUT FWD OF APU COMPT LEFT SIDE, SKIN IS CORRODED AT LAP SPLICETIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN, FWD OF APU COMPT, ORIGINAL THICKNESS 0.080", WITH LOSS OF 0.004", AND 0.076" REMAINING. FOUND TO BE WITHIN LIMITS IAW B7Jul 5, 2022 · N562AS · Boeing 737890SDR ASAA2022070539334Skin · corrodedLOWER FUSELAGE, SKIN AFT AFT TAIL JACKING POINT IS CORRODED, JUST FWD OF APUL COMPTTIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT AFT TAIL JACKING POINT. ORIGINAL THICKNESS OF 0.080", LOSS OF 0.004", AND 0.076" REMAINING FOUND TO BE WITHIN LIMIJul 5, 2022 · N562AS · Boeing 737890SDR SWAA2022080125916Angle · crackedCRACK ANGLE LOCATED BS294.5 AT LEVEL STR17R SIDE AT PASSENGER CABIN 2022-373017 / [01] REPLACED NGLE LOCATED BS294.5 AT LEVEL STR17R SIDE AT PASSENGERS IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING # 141A8310 REV B SEE INDIVUDUAL SIGN OFF BELOWJul 5, 2022 · N494WN · Boeing 7377H4SDR AALA202207255004Skin · damagedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO BALL MAT 151SF UPPER SKIN SURFACE IS TORN AT BOLT ACCESS HOLE LOCATION.(096-011) REPAIRED BALL MAT UPPER SKIN AT AFT CARGO BALL MAT #151SF IAW B777-2 SRM 53-00-53-2R-6.Jul 5, 2022 · N750AN · Boeing 777223SDR IPXA2022072084380Skin · crackedINSPECTION TYPE:C18UPON HFEC OF A 15: DENT AT FS 1380 - FS 1400 BETWEEN STRINGERS 28L AND 27R NDT FOUND A 15" CRACK RUNNING ALONG THE RECESS OF DENT 15", CRACK DOES NOT GO ALL THE WAY THROUGH THE SKIN AND IS LOCATED ON THE OML OF SKIN PANEL.REPAIRED SKIN PANELJul 5, 2022 · N418UP · Boeing 75724APFSDR CALA2022070601662Frame · crackedRH FRAME 35 STR 30 RH HOLES #1 AND #2 HAVE CRACK INDICATIONS. PERMANENT RPR AT FR 35 STR 30 RH PER PART 3 OF THE LATEST REV OF 9290225 AND 9290224 IAW ECRA 5330-06963 PART 1.2. ECRA 5330-06963 ON OR BEFORE 30-DEC-22.ALL WORK ACMP ON HAECO NR ACMP INTERIM RPR AJul 5, 2022 · N434UA · Airbus A320232SDR DALA2023051003679Unknown · unknownSHIP 3319 LIGHTNING STRIKE 6 FASTENERS AFT OF FRAME 87 ON STRINGER 51L. CORRECTIVE ACTION: FASTENER(TEMPORERY REPAIR) REMOVED PER A330 SRM 53-51-11. FASTENER LOCATION IS NOT IDENTIFIED CORRECTLY IN ORIGINAL WRITE UP, THERE IS NO STRINGER 51 AT FRAME 87, CORRECJul 4, 2022 · N819NW · Airbus A330323SDR DALA2022091406113None · noneSHIP 6820 DURING SVC FOUND DENT ON LT SIDE OF A/C FUSELAGE 4" FWD OF WING ILLUMINATION LIGHTS, 2.5" AFT OF STA 640 AND 4.5 ABOVE WL 208.10 DENT IS 0.090" IN DEPTH AND 1" IN WIDTH. CORRECTIVE ACTION: REF ERA 600581-14 REV ORG.Jul 4, 2022 · N820DX · Boeing 75726DSDR ASAA2022070439331Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 500A-500G, BL-0, SKINIS CORRODED AT 5EA DRAIN PLUGS. DOTS N074 AND N073DOT: N074TIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT STA 500A-500G BL-0 AT 5EA DRAIN PLUGS ORIGINAL THICKNESS OF 0.080", LOSS OF 0.003", WITHJul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439330Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 887, LBL40-RBL40, LOWER SKIN IS CORRODED ON FWD SIDE OF BUTT SPLICEDOT: N076TIPR833K. GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN STA 877 BUTT SPLICE, ORIG THICKNESS 0.080", WITH 0.003" REMOVED, 0.077" REMAINING THICKNESS. FOUNJul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439329Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 887, LBL40-RBL40, LOWER SKIN IS CORRODED ON AFT SIDE OF BUTT SPLICE.DOT: N077TIPR833K. GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN ATA STA 887 BUTT SPLICE, ORIG THICKNESS 0.080" WITH 0.003" REMOVED, 0.077" REMAINING THICKNESS FJul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439317Skin · corrodedLOWER EXTERIOR FUSELAGE, AT LAV VENT, SKIN IS CORRODED BETWEEN VENT TUBE AND INTERIOR SKIN. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT LAV VENT, ORIGINAL THICKNESS 0.125", WITH 0.005" REMOVED, AND 0.120" REMAINING, FOUND TO BE WITHIN LIMITS IAW B737-Jul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439316Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 967, LBL6, LOWER SKIN IS CORRODED AROUND AFT DOOR SILL WATER DRAIN.DOT: N081TIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT STA967, LBL6, ORIGINAL THICKNESS 0.063", WITH 0.005" REMOVED, AND 0.058" REMAINING FOUND TO Jul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439315Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 1016, LBL30-RBL40, SKIN IS CORRODED ON AFT SIDE OF BUTT SPLICE GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN STA 1016 BUTT SPLICE, ORIG THICKNESS, 0.080, WITH 0.003 REMOVED, 0.077" REMAINING. FOUND TO BE WITHIN LIMITS IAW B737-80Jul 4, 2022 · N562AS · Boeing 737890SDR ASAA2022070439314Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 1016, LBL30-RBL40, SKIN IS CORRODED ON FWD SIDE OF BUTT SPLICE GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN STA 1016 BUTT SPLICE, ORIG THICKNESS 0.063, WITH 0.004, AND 0.059 REMAINING FOUND TO BE WITHIN LIMITS IAW B737-800 SRM 5Jul 4, 2022 · N562AS · Boeing 737890SDR SWAA2022071125702Skin · missingFUSELAGE SKIN MISSING MATERIAL AT APPROX STA 1100 AT FWD HINGE OF APU DOOR. RAMP REPORTED SKIN MISSING IN DOUBLER BY FWD APU HINGE DOOR. PIC ATTACHED IN TASK INFORMATION. / [01] PERFORMED REPAIRED PROCEDURES UP TO STEP 4.C. UP TO NDT IAW SRM 53-80-01-2R-1 REPAJul 4, 2022 · N8653A · Boeing 7378H4SDR CALA2022070601656Skin · crackedAD-2008-16-12 - EA 5300-01986 REV A OP002 - LH STA 2221.65 STR 5L-6L 1EA CRACK AND 9L-10L 2EA CRACK FOUND AS MARKED AT FUSELAGE AROUND THE FASTENER TRANSFER REF. NON-ROUTINE HX NRC WO.812474 AND ORIGINATED BY EMP NO. V914372 EA 5300-01986 REV A OP 002 - LH STAJul 4, 2022 · N768UA · Boeing 777222SDR DALA2023051003678Unknown · unknownSHIP 3319 LIGHTIG STRIKE 1 FASTENER BELOW STRINGER 51L ON FRAME 72. CORRECTIVE ACTION: FASTENER (TEMPORARY REPAIR) REMOVED PER A330 SRM 53-41-11. FASTENER (TEMPORARY REPAIR) LOCATION AT FR 72 STRINGER 50L. PERFORMED ROTARY PROBE PER NTM 51-10-01. NO DEFECTS NOJul 3, 2022 · N819NW · Airbus A330323SDR DALA2023051003677Unknown · unknownSHIP 3319 LIGHTNING STRIKE 1 FASTENER ABOVE STRINGER 51L ON FRAME 85. CORRECTIVE ACTION: FASTENER (TEMPORARY REPAIR) REMOVED PER A330 SRM 53-51-11. FASTENER LOCATION IS NOT IDENTIFIED CORRECTLY IN ORIGINAL WRITE UP, THERE IS NO STRINGER 51 AT FRAME 85, CORRECTJul 3, 2022 · N819NW · Airbus A330323SDR 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 7377H4SDR DALA2022070704746None · noneSHIP 177 THE GAP BETWEEN THE FWD WASTE TANK VENT OUTLET AND FUSELAGE EXTERIOR SURFACE FOUND CORROSION. CORRECITVE ACTION: PERFORMED DOUBLER REPAIR AS PER B767-300 SRM53-60-01 & ER/A600267-14. (2304176)Jul 3, 2022 · N177DN · Boeing 767332SDR DALA2022070604704None · noneSHIP 3319 LIGHTNING STRIKE IN BETWEEN FRAMES 58-59 & IN BETWEEN STRINGERS 44-45-LEFT SIDE. CORRECTIVE ACTION: REMOVED PIT IN SKIN BY DRILLING HOLE TO .159" COUNTER SUNK FOR INSTALLATION OF SOLID RIVET . REF A330 SRM 51-44-11. PERFORMED HFEC. NO CRACKS. INSTALLJul 3, 2022 · N819NW · Airbus A330323SDR FDEA202207021667Skin · crackedCABIN - STATION 1250.75 TO STATION 1256.75 L3 DOOR CUT OUT FORWARD UPPER JAMB WEB BOX FOUND CRACKED. CABIN AT STATION 1250.75 TO STATION 1256.75 L3 DOOR CUTOUT FORWARD UPPER JAMB WEB BOX , CRACKED AREA REPAIRED AS PER E.A.# : 1-5310 - T0369391 PART 1 , TITJul 2, 2022 · N617FE · Doug MD11FSDR IPXA2022070283714Seat Track · corrodedINSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT SEAT TRACK STA 1190 LBL 45 HAS CORROSIONAFTER TO REWORK AREA, FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1 REMOVE AND REPLACE SEAT PER SRM 51-40-02Jul 2, 2022 · N413UP · Boeing 75724APFSDR CALA2022070401636Skin · dentedLT FWD FUS.SKIN AT STA 211.8 BETWEEN S-17L AND 19L DENT FOUND OUT OF LIMITS.TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE EXTERNAL DOUBLER/TRIPLER REPAIR TO THE FUSELAGE SKIN BETWEEN STA 196.5 AND STA 219.6 STR 17L AND WL 190 ON A/C N78501 I.AJul 2, 2022 · N78501 · Boeing 737824SDR DALA2022082205669None · noneSHIP 6815 ON WALK AROUND FOUND SEVERAL SMALL DENTS NEAR E&E EXHAUST. CORRECTIVE ACTION: REF ERA 600543-14 REV ORG.Jul 1, 2022 · N718TW · Boeing 757231SDR SWAA2022072524689Shield · corrodedCORROSION ON FWD CARGO DOOR CUT-OUT FWD SHIELD AT STA 420+16; RBL 24.5; WL 156.5 / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENT TABLE;[03] REMOVED DAMAGJul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524691Support · corrodedCORROSION ON FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 440+5 TO STA 500H+17 ; LBL 24; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500E+14 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TJul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524692Support · corrodedCORROSION ON FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A TO STA 500H+19; RBL 25 TO RBL 23; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500F+11' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045Jul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524860Attach Angle · crackedCRACK ON AFT CARGO BAY BULKHEAD SUPPORT LOWER ATTACH ANGLE AT BS 847+19 LBL 10.(MAKRED) / [01] CRACKED ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; PART REPLACEMENT REQUIRED;[02] REMOVED ACB BULKHEAD SUPPORT LOWER ATTACH ANGLE AT BS 8Jul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524852Shield · corrodedCORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 22 BS 847+6; BS 847+15. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION ITEM 1;[03] REMOVED DAMAGED AFT CARGO BAY AFT DOOR SHIELD Jul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524856Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 22 BS 727D+3; BS 727D+8. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D+8' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PJul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524864Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727I+14; BS 727I+18; BS 727J+2; BS 727J+10. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727I+18' REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FJul 1, 2022 · N8641B · Boeing 7378H4SDR SWAA2022072524688Web · corrodedCORROSION ON FWD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB; STA 440+1 TO STA 480+12; RBL 23 TO RBL 29.5; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 470 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUNJul 1, 2022 · N8641B · Boeing 7378H4
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