JASC 5320

Service difficulty reports · 216,159

Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320'
  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 DALA2024041904610Fitting · corrodedAIRCRAFT 3043, CORROSION CENTER FITTING LOC STR 23L AND BTW FR66 TO FR68 AFT GALLEY AREA. MEASURE OF CORRODED AREA IS L= 1.105 INCHES W= 0.331 INCHES. CORRECTIVE ACTION: REPLACED CENTER FITTING AND FASTENERS.LOC STR23L AND BTW FR66 TO FR68 AFT GALLEY AREA AS PApr 19, 2024 · N343DN · Airbus A321211SDR DALA2024041904609Shear Plate · crackedAIRCRAFT 3050, CRACK SHEAR PLATE STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURES OF CRACK AND MEASURES ARE: L: 0.204 INCHES. CORRECTIVE ACTION: INSTALLED NEW SHEAR PLATE AND BRACKETS (3 E/A) LOCATED STR 23LH BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER Apr 19, 2024 · N350DN · Airbus A321211SDR DALA2024041904571Membrane · corrodedCORROSION ON LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN IN REFERENCE NRC 00391. SUMMARY OF NRC 00591: CORROSION LEVEL 2. LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0301180)Apr 19, 2024 · N993AT · Boeing 717200SDR DALA2024041904570Cusp Web · corrodedCORROSION ON LH CUSP WEB, OUT OF LIMITS PER B717 SRM 53-00-55-1A-1 ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00701: CORROSION LEVEL 2. RING DOUBLER ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND REPLACEApr 19, 2024 · N988AT · Boeing 717200SDR SWIA2024061900418Angle · crackedAFT EQUIPMENT COMPARTMENT - FS1098.20 STGR24R INBOARD CLIP IS CRACKED. (MARKED) (C-CHECK RO 6/17/2024) REMOVED FROM FS1098.20 STGR24R CRACKED INBOARD CLIP REF.CRJ-700 SRM 51-42-06-001-001-A01 INSTALLED NEW CLIP REF.CRJ-700 DRAWING MM670-35012 REV. G AND Apr 18, 2024 · N722EV · Cndair CL6002C10SDR VNAA20240531024Fitting · corrodedCORROSION ON SETTLEMENT FITTING OF GALLEY 1 (2EA) (FLOOR STRUCTURE AREA) FITTING OF GALLEY 1 (2EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03, AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Apr 18, 2024 · N567NN · Cndair CL6002D24SDR SWAA2024053076750Shield · corrodedCORROSION ON SHIELD PLATE LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R WL 156 AT FWD CARGO COMPARTMENT 2024-269950<[01] REPLACED SHIELD PLATE AND FASTENERS LOC. BTW BS 492.4 TO BS 500A AT LEVEL STRG 26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-Apr 18, 2024 · N470WN · Boeing 7377H4SDR ASAA2024041849918Web · corrodedAFT PIT WEB HAS CORROSION. GROUNDED - YES. REMOVED CORR.FROM AFT PIT WEB ORIG. THICKNESS .045 I.A.W B737-800 SRM53-60-15. MAT LOSSED .040 REMAINING THICKNESS .005 FOUND TO BE OUT OFLIMITS I.A.W B737-800 SRM 53-60-15.TOOL#T8224K DUE 25/OCT/24.REMOVED AND REPLAApr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849917Transition Panel · corrodedAFT PIT TRANSITION PANEL @ STA727E+16 TO STA767 IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT R/H TRANSITION PNL AT STA727E+16 TO ST767 ORIG THICK .040 I.A.W B737-800 SRM 53-60-53. AREA FOUND TO BE OUT OF LIMITS AND PUNCTURED I.A.W B737-800 SRM 53-0Apr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849842Shield · corrodedAFT PIT DOOR SURROUND FWD SHIELD HAS CORROSION. GROUNDED - YES. EVALUATED AFT PIT FWD SHIELD ORIG THICKNESS IS .050" IAW B737-800 SRM 53-60-15-0I-1 REMOVED .007" REMAINING .043" AND IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1 4.G.2 TOOL# T8224KApr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849841Transition Panel · corrodedAFT PIT RH TRANSITION PANEL @ STA727 TO STA727E+15 IS CORRODED. GROUNDED - YES. REMOVED CORR. FROM AFT PIT R/H TRANSITON PNL AT STA.727 TO STA.727E+15 ORIG. THICKNESS .040 I.A.W B737-800 SRM 53-60-53 MAT. LOSSED .010 REMAIING THICKNESS .030 FOUND TO BE OUT OFApr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849840Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727I+14 TO STA827. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA 727I +14 TO STA 827 IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS AApr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849839Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727C+7 TO STA727I+13. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION @ STA727C+7 TO 727I+13 IAW B737-800 SRM 53-00-53-1A-2.R.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-OI-1 REMOVED: .007, REMAINIApr 18, 2024 · N508AS · Boeing 737890SDR ASAA2024041849838Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727 TO STA727C+6. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA727 TO STA727C+6 IAW B737-800 SRM 53-00-55-1A-2. ORIG THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS AND IS FOUNApr 18, 2024 · N508AS · Boeing 737890SDR VNAA202405130028Fitting · corrodedWORK SHOP INTERIOR SHEET METAL: CORROSION ON FITING (1EA) BELOW THE SERVICE TABLE AT FWD LAV. FITTING P/N: A414252-3 (1EA) BELOW THE SERVICE TABLE AT FWD LAV. WAS REPLACED PER SAFRAN CMM 25-40-40Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA202405130021Floor Support · corrodedCORROSION ON LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT. LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT WAS REPAIRED PER REO 690-53-61-1379. REV. --Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA202405130012Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM 51-Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA202405130011Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA20240513003Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. : BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR SWAA2024051076603Pan · crackedAFT GALLEY SERVICE DOOR LOWER PAN ASSY CRACKED<[01] REMOVED AND REPLACED AFT GALLEY SERVICE DOOR LOWER PAN ASSY PER B737 SOPM 20-50-01;[02] VERIFIED REPLACEDApr 18, 2024 · N472WN · Boeing 7377H4SDR SWAA2024050876651Scuff Plate · cracked**CRACK** FWD CARGO DR CUTOUT AFT LWR CORNER SCUFF PLATE<[01] RECEIVED AND LOCATED AND DRILLED NEW FWD CARGO DOOR CUTOUT AFT LWR CORNER SCUFF PLATE PER SRM 51-40-05-0G-0<BR> PN:143A8331-4 PO:1728471<BR> LOT #BN 219491 ISSUE TAG: WN14938.<BR>FOR INSTALLATION REApr 18, 2024 · N923WN · Boeing 7377H4SDR SWAA2024050876393Floor Support · cracked[DOT B765] FWD CARGO UNDER FLOOR AT STA 400; LEFT TRANSITION PANEL ATTACH INTERCOSTAL CRACKED AS MARKED.<[01] REMOVED; FABRICATED; LOCATED; DRILLED; AND INSTALLED NEW BAFFLE (INTERCOSATAL) REF BAC DWG 143A7505 REV:-; B737-NG SRM 51-40-02;[02] REMOVED; FABRICATApr 18, 2024 · N8688J · Boeing 7378H4SDR AALA202404291140Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BULK CARGO DOOR SILL BEAM AROUND 1EA FASTENER AT FR-61 -Y26. REPAIRED DOOR SILL BEAM PER SRM 53-41-49-300-003.Apr 18, 2024 · N926VA · Airbus A321253NSDR CALA2024042201187Web · damagedE & E BAY WEB BS 323.7 TO 351.2 DAMAGED.Apr 18, 2024 · N35204 · Boeing 737824SDR DALA2024041904593Plate · corrodedSHIP 6809 CORROSION ON LH SIDE PLATE SECTION STA Y= 1410-1530 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00197: CORROSION ON LH SIDE PLATE SECTION STA Y=1410-1530 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2) WAS RApr 18, 2024 · N713TW · Boeing 7572Q8SDR DALA2024041904569Cusp Web · crackedCRACK (3 EA) ON LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX. SUMMARY OF NRC 00717: LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 205. (LP #0300923)Apr 18, 2024 · N988AT · Boeing 717200SDR DALA2024041904567Cusp Web · crackedCRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN PAX. SUMMARY OF NRC 00393: CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN, WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0300915)Apr 18, 2024 · N993AT · Boeing 717200SDR DALA2024041904566Diaphragm · crackedCRACK ON DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX (W1). SUMMARY OF NRC 00689: DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10- 2R REPAIR 2 FIG 201. (LP #0300282)Apr 18, 2024 · N923AT · Boeing 717200SDR 2024FA0000329Bracket · crackedFLAP HANDLE FORWARD SUPPORT BRACKET FOUND CRACKED. NOTED AREA OF STRESS/CRACK A LACK OF RADIUS. REPLACED WITH FACTORY NEW BRACKET.Apr 18, 2024 · N952A · Piper PA28181SDR SWAA2024060775641Floor Support · crackedCABIN FLOOR STRUCTURE INTERCOASTAL CRACKED AT FASTENER HOLES BETWEEN STA 380-400 LBL 13.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL AT CABIN FLOOR STRUCTURE BETWEEN STA 380-400 LBL 13 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1Apr 17, 2024 · N8318F · Boeing 7378H4SDR SWAA2024053076060Angle · crackedCRACK ON ANGLE LOCATED BS 695 BL 0 FWD POSITION RT SIDE AT PASSENGER CABIN 2024-269926<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAApr 17, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053076059Angle · crackedCRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2024-269925<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLAApr 17, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053076061Angle · crackedCRACK ON ANGLE LOCATED BS 695 BL 0 AFT POSITION RT SIDE AT PASSENGER CABIN 2024-269927<[01] REPLACED ANGLE LOCATED BS 695 BL 0 AFT POSITION RT SIDE AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6. REV. A. SEE INDIVIDUAL SIGNOFF BELOW.;[Apr 17, 2024 · N470WN · Boeing 7377H4SDR SWAA2024052876035Floor Support · corrodedCORROSION ON FLIGHT DECK FLOOR INTERCOSTAL UPPER SURFACE B.S. 268.25 B.L. 0 W.L. 208. (DOT 51-001)<[01] REMOVED AND REPLACED INTERCOSTAL (SUPPORT CHANNEL) AT FLIGHT DECK FLOOR BETWEEN STA 260 AND STA 270 BL 0 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5210.;[Apr 17, 2024 · N473WN · Boeing 7377H4SDR IPXA2024052546477Floor Support · corrodedCOURIER FLOOR AREA FWD OF R1 DOOR UNDER LAVATORY HAS CORROSION. INSTALLED FLOOR SUPPORT AT CURIER AREA FWD OF RI DOOR UNDER LAVATORY IAW SRM 51-33-01-51-35-01. REMOVED AND REPLACED FLOOR SUPPOR IAW DWG ABA7341, DWG SP11530074 AND SRM 5100 GUIDELINES.Apr 17, 2024 · N276UP · Doug MD11FSDR SWAA2024052276165Support Angle · corrodedCORROSION ON AFT CARGO COMPARTMENT BS 907 SIDEWALL LINING SUPPORT ANGLE RBL 24 WL 166<[01] REMOVED AND REPLACED FRAME SPLICE AT BS 907; BETWEEN STR 24R AND STR 25R WL 166 PER SRM 51-40-02-0G-0 AND BOEIN DWG 147A9409.;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLApr 17, 2024 · N474WN · Boeing 7377H4SDR SWAA2024052276453Support Angle · crackedCRACK AT SUPPORT ANGLE STA-685+10'' RBL-25 WL-208<[01] UPDATED MEASUREMENT TABLE.;[02] INSTALLED NEW BRACKET AT BS 685+10'; RBL 25; WL 204 PER SRM 51-40-02-0G-0.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Apr 17, 2024 · N474WN · Boeing 7377H4SDR REXA2024052200392Angle · corrodedPAX DOOR MID SILL ANGLE IS CORRODED AROUND SCREW HOLES. UPON FURTHER INVESTIGATION, FOUND PAX DOOR MID CAP ANGLE P.N. SH670-31825-7 TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELAMENTS AND IN EXCESS OF OVER 40% OF MATERIAL THICKNESS IAW CRJ900SRM TASK 53Apr 17, 2024 · N582CA · Cndair CL6002D24SDR SWAA2024052084498Angle · perforatedPERFORATION ON ANGLE LOCATED BS540 PLUS 8INCH AND RBL41 AT AIR CONDITIONING BAY 2024-259288<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED BS540 TO 540+13? AND RBL41 AT AIR CONDITIOApr 17, 2024 · N7736A · Boeing 7377BDSDR SWAA2024052076303Bracket · crackedCRACK BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY 2024-259286<[01] REPLACED BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540Apr 17, 2024 · N7736A · Boeing 7377BDSDR SWAA2024052076304Bracket · crackedCRACK BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY 2024-259287<[01] REPLACED BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540Apr 17, 2024 · N7736A · Boeing 7377BDSDR JJBA20240513020Angle · crackedVERTICAL U-SHAPE ANGLE BTW FR 67-68 AND BTW STR 3-4R CRACKED. VERTICAL U-SHAPE ANGLE BTW FR 67-68 AND BTW 3R-4R REPLACED.Apr 17, 2024 · N21197 · Emb EMB145XRSDR SWAA2024050976386Angle · corrodedMAIN CABIN AFT WET AREA; INTERCOSTAL CORRODED ON UPPER SURFACE APPROX. BS 947 LBL-24.5. MAIN CABIN AFT WET AREA INTERCOSTAL CORRODED ON UPPER SURFACE APPROX. BS 947 LBL-24.5.<[01] REMOVED AND REPLACE 147A5430-7 INTERCOSTAL ANGLE IAW B737-800 SRM 51-40-02 AND BApr 17, 2024 · N8688J · Boeing 7378H4SDR SWAA2024050976383Angle · corrodedMAIN CABIN AFT WET AREA; INTERCOSTAL CORRODED ON UPPER SURFACE APPROX. BS 947 RBL-24.5 MAIN CABIN AFT WET AREA INTERCOSTAL CORRODED ON UPPER SURFACE APPROX. BS 947 RBL-24.5<[01] REMOVED AND REPLACED UPPER ANGLE ON MAIN CABIN INTERCOSTAL RBL 24.5 STA 947 IAW B7Apr 17, 2024 · N8688J · Boeing 7378H4SDR SWAA2024050976385Floor Support · corrodedMAIN CABIN AFT WET AREA; INTERCOSTAL CORRODED ON UPPER SURFACE APPROX. BS 947 RBL-52.<[01] PERFORMED FPI ON PART IAW BAC 5423. NO CRACKS FOUND INSP ONLY;[02] FABRICATED AND INSTALLED INTERCOASTAL AT STA 947.5 AND RBL 52 PN 147A5660-30 IAW B737-800 SRM 51-40-02Apr 17, 2024 · N8688J · Boeing 7378H4SDR SWAA2024050276080Floor Support · crackedPASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 52; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 52; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 142A5400; SHEET 183; REV - DATED 03/2Apr 17, 2024 · N8684F · Boeing 7378H4SDR SWAA2024050276436Floor Support · crackedPASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 1; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 1; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 143A5400; SHEET 154.;[02] VERIFIED CORRApr 17, 2024 · N8684F · Boeing 7378H4SDR SWAA2024050276431Floor Support · crackedPASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 13; WL 208.<[01] REMOVED AND REPLACE PASSENGER CABIN FWD FLOOR SUPPORT AT BS 380-400; LBL 13; WL 208 PER SRM 51-40-02; SRM 51-40-05; AND DWG#143A5400.;[02] VERIFIED CORRECTIVE ACTION 1Apr 17, 2024 · N8684F · Boeing 7378H4SDR SWAA2024050276064Sidewall Support · corrodedCORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] REMOVED FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY R/H FLOOR TO SIDEWALApr 17, 2024 · N8684F · Boeing 7378H4SDR SWAA2024050276065Shield · corrodedCORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED FWD CARGO BAY AFT SHIELD; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY AFT SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143Apr 17, 2024 · N8684F · Boeing 7378H4
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