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 AALA202404228211Door Sill · unsecureAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS STICKY AND HARD TO OPEN AND CLOSE. FOUND FORWARD LAVATROY DOOR LOWER DOOR SILL 2EA SCREWS STICKING UP AND LOOSE. SECURED SCREWS AS REQUIRED. OPERTIONAL CHECKED OKAY.Apr 21, 2024 · N936AN · Boeing 737823SDR DALA2024042204625Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160. SUMMARY OF NRC 00191: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDER 3 REPAIR 3. (LP #0305244)Apr 21, 2024 · N988AT · Boeing 717200SDR DALA2024042204624Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200. SUMMARY OF NRC 00193: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0305238)Apr 21, 2024 · N988AT · Boeing 717200SDR SWI2024F00510Bracket · corrodedFORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR22L 23L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED MACHINED BRACKET IN FWD CARGO, F.S. 533 STGR 22-23L, WITH NEW, REF CRJ 700 SRM 51-42-20-001-001-A01 REVISION 38: JUL 25/2020, CRJApr 20, 2024 · N722EV · Cndair CL6002C10SDR SWI2024F00508Bracket · corrodedFORWARD BAGGAGE BAY - CORROSION ON BRACKET FS581.00 STGR27 - 26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED WITH NEW BRACKET P/N SH670-33389-2 AT FS581.00 STGR27 - 26L. REF. CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, AND 51Apr 20, 2024 · N722EV · Cndair CL6002C10SDR SWI2024F00502Bracket · corrodedFORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR27. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED FORWARD BAGGAGE BAY BRACKET FS533.00 STGR27 (PN SH670-33389-1) PER CRJ700 SRMS 51-42-21-001-001-A01, 51-42-22-001-001-A01 AND DWG NOApr 20, 2024 · N722EV · Cndair CL6002C10SDR SWIA2024061900420Bracket · corrodedFORWARD BAGGAGE BAY - CORROSION ON BRACKET FS549.00 - FS565.00 STGR25R - 24R. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED BRACKET BETWEEN F.S. 549 AND F.S. 565 STGR 25R-24R WITH NEW, PN SH670-33852-1, REF CRJ 700 SRM 51-42-06-001-001-A01,Apr 20, 2024 · N722EV · Cndair CL6002C10SDR IPXA2024061296583Bracket · crackedCRACKED BRACKETS AT FWD CARGO BULKHEAD FR38.2 INNER SIDE OF AFR CARGO WALL. VERIFIED INSTALLATION OF 5 EA BRACKETS ON FWD CARGO BULKHEAD FR38.2 IAW-A300-600 SRM-51-40-21.Apr 20, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024061296571Bracket · brokenBROKEN BRACKETS SUPPORT AT FWD CARGO BULKHEAD FR 38.2 L/H WALL (2 EA). APPLIED PROTECTIVE SURFACE TREATMENT IAW SRM 51-21-10 AND EO M-5100-2780-L REQUEST TO INSTALL. INSTALLED BRACKETS (2EA) IAW SRM A300-600 51-40-21.Apr 20, 2024 · N159UP · Airbus A300F4622RSDR SWAA2024053077456Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-270010<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DRAWING 141A1110 SHEET 18 REV.-. AND DRAWING 141A8380 SHEET 14 REV.-. SEE INDIApr 20, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053077448Angle · crackedCRACK ON ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-270014<[01] REPLACED ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER IAW B737-700 SRM 51-40-02; DWG N:146A7901 SHEET: 58 REV:- AND IAWB737-700 SRM 51-10-02 Ï¿½TEM 9 .;[02] REPLACApr 20, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053077454Support Channel · corrodedCORROSION CHANNEL SUPPORT LOCATED BS847 TO BS867 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT 2024-270003<[01] TOOL USED ON STEP 3 IS THICKNESS EQUIPMENT PN: 45MG; SN: 221860711; DUE DATE: 21-NOV-24;[02] REPLACED CHANNEL SUPPORT LOCATED BS847 TO BS867 AT LEApr 20, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053077455Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS907 TO BS927 BTW STR27R TO STR25R AT AFT CARGO COMPARTMENT (2 EA) 2024-270004<[01] REPLACED ANGLE - SUPPORTS LOCATED BS907 TO BS927 BTW STR27R TO STR25R AT AFT CARGO COMPARTMENT (2 EA) I.A.W B737-700 SRM 51-40-02 DWG 147A7221 REApr 20, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053077457Bracket · crackedCRACK BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2024-270005<[01] REPLACED BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 149A8103 SHEET: 6 REV: - SEE INDIVIDUAL SIGN OFApr 20, 2024 · N470WN · Boeing 7377H4SDR SWAA2024053077452Support Channel · corrodedCORROSION CHANNEL SUPPORT LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT 2024-270000<[01] REPLACED CHANNEL SUPPORT AND FASTENERS LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-Apr 20, 2024 · N470WN · Boeing 7377H4SDR CALA2024053001645Shear Plate · corrodedAFT WET AREA FR69 - FR70, L/H SHEAR PLATE SHOWS CORROSION. () REMOVED SHEAR PLATE AND SUPPORT FRAME IAW SRM 51-42-11, RECIEVED STA:STENGBFM NEW SHEAR PLATE P/N D5347112420200 SUPPORT FRAME P/N: D53471123 20200, LOCATED AND DRILL HOLE IAW SRM 51-44-11/001, INSTApr 20, 2024 · N897UA · Airbus A319132SDR CALA2024053001644Shear Plate · corrodedAFT WET AREA FR69 - FR70, R/H SHEAR PLATE SHOWS CORROSION. () REMOVED SHEAR PLATE AND SUPPORT FRAME IAW SRM 51-42-11 RECIEVED 9 STA:STENGBFM NEW SHEAR PLATE D5347112420300 SUPPORT FRAME D5347112320300, LOC ATED AND DRILL HOLE IAW SRM 51-44-11/001. INSTALLED NEApr 20, 2024 · N897UA · Airbus A319132SDR SWAA2024052377288Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500H - 500I LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377290Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500F - 500G LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377294Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500C - 500D LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377297Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500 - 500A LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10-Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377292Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500E - 500F LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377293Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500D - 500E LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377289Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500G - 500H LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377295Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500B - 500C LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377296Angle · corrodedFWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500A - 500B LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377264Angle · corrodedAFT CARGO COMPARTMENT STA 727 D-5 RBL 21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE FROM STA 727 TO SApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377265Angle · corrodedAFT CARGO COMPARTMENT STA 727 F RBL21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.011; MAT THICKNESS REMAINING IS 0.029; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE FROM STA 727 TO STA 767 FOR REPApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377274Angle · corrodedAFT CARGO COMPARTMENT STA 727 F+6 LBL 21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE FROM STA 767 TO STA 847 FOR RApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377276Angle · corrodedAFT CARGO COMPARTMENT STA 727 G THRU STA727 H LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.011; MAT THICKNESS REMAINING IS 0.029; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED ANApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377277Angle · corrodedCORROSION ON UPPER SURFACE OF TRANSITION ANGLE IN AFT CARGO BIN AT STATION 827 LBL 22. MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.007; MAT THICKNESS REMAINING IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED AND REPLACED Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377267Angle · corrodedAFT CARGO COMPARTMENT STA 727G THRU STA727 H RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSIONS; MAT DEPTH REMOVED IS 0.008; MAT THICKNESS REMAINING IS 0.032; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE FApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377278Angle · corrodedAFT CARGO COMPARTMENT STA 727H THRU STA727 I LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.012; MAT THICKNESS REMAINING IS 0.028; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED ANDApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377280Web · corrodedFWD CARGO THRESHOLD WEB UPPER SURFACE HAS NUMEROUS AREAS OF CORROSION AT N/P AND FASTNER HOLES. STA 440 - 492 RBL 29-30 WL 156. MRKD<[01] BLENDED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-30-15-1A-1;[02] C/W INSP. BLENDED CORROSION PER Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377279Angle · corrodedAFT CARGO COMPARTMENT STA 727H THRU STA727 I RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.012; MAT REMAINING IS 0.028. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE FROM STA 727Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377268Angle · corrodedAFT CARGO COMPARTMENT STA 727 I THRU STA 727 J LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377282Angle · corrodedAFT CARGO COMPARTMENT STA 727 I THRU STA 727 J RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.010; MAT THICKNESS REMAINING IS 0.030; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE FApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377283Angle · corrodedAFT CARGO COMPARTMENT STA 727 J THRU STA 747 LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.007; MAT THICKNESS REMAINING IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED ANDApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377285Angle · corrodedAFT CARGO COMPARTMENT STA 727 J THRU STA 747 RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] CORRECTION ON BL AND RII LABApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377269Angle · corrodedAFT CARGO COMPARTMENT STA 747 THRU STA 767 LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.010; MAT THICKNESS REMAINING S 0.030; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED AND RApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377270Angle · corrodedAFT CARGO COMPARTMENT STA 747 THRU STA 767 RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.011; MAT REMAINING THICKNESS IS 0.029; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] CORRECTION ON BL AND RII LABORApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377286Support Angle · corrodedFWD CARGO STA 500I BULKHEAD FLOOR SUPPORT ANGLE IS CORRODED LBL24-RBL24 WL 156. MRKD<[01] REMOVED DAMAGE PER SRM 51-10-02. DAMAGE OUT OF LIMITS PER SRM 53-30-08-1A-1;[02] INSPECTED / VERIFIED THE WORK ACCOMPLISHED ON CORRECTIVE ACTION #1; NO DEFECTS NOTED.;[03Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377287Angle · corrodedAFT CARGO COMPARTMENT STA 767 THRU STA 787 LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.013; MAT THICKNESS REMAINING IS 0.027; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED AND Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377271Angle · corrodedAFT CARGO COMPARTMENT STA 767 THRU STA 787 RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.044' REMAINING THICKNESS). SHIELD (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] DRILL AND CApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377272Angle · corrodedAFT CARGO COMPARTMENT STA 787 +12 LBL21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED AND REPLACED ON N/R CARD LINE Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377291Angle · corrodedAFT CARGO COMPARTMENT STA 807 LBL21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED AND REPLACED ON N/R CARD LINE # 24Apr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377299Angle · corrodedFWD CARGO R/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500G - 500H RBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] INSPECTED/ VERIFIED THE WORK PERFORMED ONApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377302Angle · corrodedFWD CARGO R/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500D - 500E RBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REFERENCE FAULT TTG8Q00SVS21: R/H TRANSITApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377298Angle · corrodedFWD CARGO R/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500H - 500I RBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-40-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] WRONG REFERENCE WAS USED FOR DAMAGE REMOVApr 20, 2024 · N8573Z · Boeing 7378H4SDR SWAA2024052377300Angle · corrodedFWD CARGO R/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500F - 500G RBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] INSPECTED/ VERIFIED THE WORK PERFORMED ONApr 20, 2024 · N8573Z · Boeing 7378H4
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