JASC 5300

Service difficulty reports · 8,204

Reports filed under 5300 · Fuselage Structure (General), 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 = '5300'
  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 JJBA20230821013Unknown · unknownCF1, CORROSION FOUND ON RH OMEGA BEAM AT FR 18 ON FLOOR STRUCTURE AREA. BEAM REPAIRED WITH A DOUBLERAug 15, 2023 · N11192 · Emb EMB145XRSDR JJBA20230821012Unknown · unknownEXISTING REPAIR TO INVESTIGATE ON LH FWD FUSE 1 SKIN, BTW FR 6-7 AND AT STR 15L, UNDER GPU ACCESS DOOR. SKIN REPAIRED WITH A DOUBLERAug 15, 2023 · N11192 · Emb EMB145XRSDR IPXA2023081693921Unknown · damagedINSPECTION TYPE:NALEFT SIDE FUSELAGE DAMAGED AT STA3670 BETWEEN FR 57 AND FR 57.1REMOVED DAMAGE IAW EO A300-5310-87913A 6354368 08/14/23. ACCOMPLISHED STEPS 6-11 (A) VERIFIED DAMAGE REMOVED PER EO 87913A, 0557771 QC 08/15/23. ACCOMPLISHED STEPS 12-15 IAW EO A3Aug 15, 2023 · N136UP · Airbus A300F4622RSDR CALA2023081602532Beam · corrodedAFT WET AREA STA 986 AT RBL 17 TO RBL 48: FLOOR BEAM UPPER FLANGE PREVIOUS REPAIR HAS CORROSION (DOT 56-011). (REF AAR N/R 9204644) REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW REPAIR AT AFT WET AREA STA 986.5 BETWEEN RBL 48 TO RBL 50 PER REF. B737-70Aug 15, 2023 · N23707 · Boeing 737724SDR WX0A2023081631814Unknown · unknownEVIDENCE OF CORROSION (MARKED) ON THE RIGHT SIDE OF THE FUSELAGE. FREAM 16, STRINGER 37R / AIRCRAFT IS CURRENTLY IN STORAGE, THIS REPORTING IS JUST PRECAUTIONARY. THE FINAL CORRECTIVE ACTION WILL BE REPORTED ONCE THAT ACTION IS COMPLETED."Aug 14, 2023 · N231NV · Airbus A320214SDR UIEA2023063000673Doubler · unknownLOWER FUSELAGE, EXTERNAL POWER RECEPTACLE, INNER DOUBLER WITH CRACK.(<P>R/R INNER DOUBLER P/N: 141A3722-12 AT EXTERNAL POWER RECEPTABLE IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9 </P>)Aug 13, 2023 · N5179A · Boeing 73783NSDR SWAA2023083188731Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2023-508412<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-40-02 AND DWG 143Aug 12, 2023 · N410WN · Boeing 7377H4SDR SWAA2023083195741Fastener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION 2023-508412<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS540 BETWEEN BL0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-40-02 AND DWG 143Aug 12, 2023 · N410WN · Boeing 7377H4SDR SWAA2023083188732Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION 2023-508413<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 1Aug 12, 2023 · N410WN · Boeing 7377H4SDR SWAA2023083195742Fastener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION 2023-508413<[01] REPLACED STIFFENER AND FASTENERS ON FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 1Aug 12, 2023 · N410WN · Boeing 7377H4SDR NACA2023081100002Unknown · unknownSTRINGER TIE CLIP CRACKS WAS FOUND AT STA 727A S-7R. RESOLVED ON W/O: 121696 TASKCARD: N/R-00262 ) DAMAGE PARTS REPLACED AT STA 727AS-7R PN:69-35352U14.I.A.W B737-300 SRM 51-40-02 PARA 4 PAGE 2.3 (REV30).Aug 11, 2023 · N303KH · Boeing 737330SDR CALA2023081402495Unknown · damagedDAMAGE FOUND ON R2 DOOR CUT-OUT OUTER CHORD IN TWO SPOTS BTWN STA 965 TO STA 983 LOG PAGE CREATED FOR SFR REPORTING. SFR #1033393 CREATED. REPAIR COMPLETED AT IHC HEAVY D CHECK VISIT ON BAM NR 1482301 & 1482299 PER ECRA 5370-01086. DIP LP 5432529 & 5432657 CRAug 11, 2023 · N24706 · Boeing 737724SDR NACA2023081000004Unknown · unknown2 EA SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BWTWEEN S-11C AND S-12C LBL41-53. PERFORM AIR ASIA WPS CODE EI-737-230801 COMPLETED.Aug 10, 2023 · N303KH · Boeing 737330SDR P5CA2023080900070Unknown · unknownMAIN DECK FLOOR STRUCTURE STA 654+88 LBL 5 SEAT TRACK WITH CRACK(<P>MAIN DECK FLOOR STRUCTURE AT STA 654+88 AND AT RBL 11 SEAT TRACK WAS REPAIRED PER SUPPLEMENT SRM 53-00-52 REPAIR 2 REV.4 30 SEP 2017</P>)Aug 10, 2023 · N642GT · Boeing 7673Y0SDR YENA2023081100933Unknown · unknownFLT#869, JFK-PUJ. ' AIRSTAIRS STRUCK THE AIRCRAFT AT THE L1 DOOR, AFTER OPENING THE L1 DOOR WE WERE TOLD BY PUJ GROUND PERSONAL THE AIRSTAIR PUT A DENT ON THE AIRCRAFT; DAMAGE WITHIN LIMITS IAW SRM TASK 53-11-11-283-012, FIGURE 007 SHEET 9/10 ZONE 1 AREA 1. DEAug 10, 2023 · N623JB · Airbus A320232SDR I5EA2023081100015Unknown · unknownFUSELAGE FRAME CORRODED AFT BAGGAGE FLOOR STA 907 BETWEEN RBL 2 AND RBL 8. REMOVE DAMAGED SECTION OF FRAME AND INSTALLED REPAIR IAW B737-300 SRM 51-40-02 AND B737-300 SRM 53-00-07.Aug 10, 2023 · N629SW · Boeing 7373H4SDR JGVR20230810002Unknown · unknownBLENDED 2 AREAS OF CORROSION ON THE EXTERIOR OF THE FUSELAGE SKIN LOCATED JUST AFT OF THE EMERGENCY EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOP COATED REPAIR AREAS IAW TEXTRON REPAIR MEMO.Aug 10, 2023 · N320QS · Cessna 680CESDR V0XD20230829002Unknown · unknownPITTING AND CORROSION ON FUSELAGE UPPER SKIN AT FS 629-645 BETWEEN STR 1L TO STR 1R AT THE VHF ANTENNA #3. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW OLIVER WYMAN CAVOK EA 23-C7-53-0586 REV. B PART III. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE Aug 9, 2023 · N517AE · Cndair CL6002C10SDR V0XD20230829001Unknown · unknownGOUGE ON FUSELAGE UPPER SKIN AT FS 629-645 BETWEEN STR 1L TO STR 0L AT THE VHF ANTENNA #3. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW OLIVER WYMAN CAVOK EA 23-C7-53-0587 REV. B PART III. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICAug 9, 2023 · N517AE · Cndair CL6002C10SDR DALA2023081506633Unknown · unknownPERFORMED AD RELATED INSPECTION WC 5352-01038-01A. FOUND CRACK ON LONGERON (P/N 53-1111-502) RT, STARTING 16" FROM FWD EDGE RUNNING AFT FOR APPROX. 16". REMOVED LONGERON WIP 234225. REPLACED RH LONGERON IAW AMDS WORKCARD 5352-01038-07B. (LP# 2908918)Aug 9, 2023 · N128DU · Airbus BD5001A10SDR SWAA2023090587189Gusset · crackedCRACK GUSSET STR 19L STA 500D FWD CARGO COMPARTMENT 2023-491797<[01] REPLACED GUSSET LOC. STR 19L STA 500D FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 143A7902 SHEET 209 REV.-;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNAug 8, 2023 · N903WN · Boeing 7377H4SDR SWAA2023090587188Gusset · crackedCRACK GUSSET STG 19R STA 500D FWD CARGO COMPARTMENT 2023-491796<[01] REPLACED GUSSET LOC. STG 19R STA 500D FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 143A7902 SHEET 209 REV.-;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNAug 8, 2023 · N903WN · Boeing 7377H4SDR SIMA20230808001Unknown · unknownSSI 53-10-016 CORROSION ON SHEAR CLIP IN FWD CARGO AT FRAME 17 BETWEEN STRINGERS 25L-26L (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED SHEAR CLIP IN FWD CARGO AT FRAME 17 BETWEEN STRINGERS 25L-26L IAW EMB 170 SRM 51-40-08.Aug 8, 2023 · N783LC · Emb ERJ170100SUSDR R61A2023082500443Drain Mast · corrodedCORROSION ON DRAIN MAST DOUBLER FR86-87 STGR 29R-28R: REMOVED AND REPLACED AFT DRAIN MAST DOUBLER, 2EA INTERCOSTALS, AND 2EA NUT HOLDERS. FR86-87,STGR 28-29R. REF EMB SRM 51-40-08, 51-23-00. SEE ATTACHED WIP'S AND TASKS FOR WORK ACCOMPLISHEDAug 8, 2023 · N240JQ · Emb ERJ170200LRSDR SWAA2023082186723Panel · debondedREJECT - DURING INSPECTION OF PANEL 195CR; NOTED DISBOND WITHIN INSPECTION AREA AND MARKED LOCATION ON PANEL. REWORK AREA TO REMOVE DISBOND. REWORK AREA TO REMOVE DISBOND.<[01] DISBOND ON PANEL 195CR NOTED AND MARKED DURING INSPECTION WAS REPAIRED IAW SRM 51-7Aug 7, 2023 · N292WN · Boeing 7377H4SDR ABXA20230809156Unknown · unknownAIRCRAFT BLOCKED OUT AND DURING TAXI THE FLIGHT CREW WAS NOTIFIED THAT THE LOG BOOK HAD AN OPEN ENTRY FOR THE MAIN CARGO DOOR REINSPECT. THE AIRCRAFT RETURNED TO BLOCK AND MAINTENANCE PERFORMED MAIN CARGO DOOR REINSPECT AND VERIFIED THE DOOR WAS CLOSED AND LOCAug 7, 2023 · N219CY · Boeing 767383SDR IPXA2023080793821Stiffener · crackedINSPECTION TYPE:1C3CL/H MLG W/W LWR AFT O/B WALL 1EA STIFFENER HAS A CRACKREMOVED AND REPLACED STIFFENER IAW SRM 51-31-01,51-35-01 AND 51-33-01, CIC APPLIED PER E.O. M-5100-2780-M. MINORAug 7, 2023 · N274UP · Doug MD11FSDR SIMA20230806009Unknown · unknownSSI 53-23-003 FR 88 STGR 27R-28R SHEAR CLIP CORRODED. (LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED FR 88 STGR 27R-28R SHEAR CLIP IAW EMB 170 SRM 51-40-08.Aug 6, 2023 · N783LC · Emb ERJ170100SUSDR SIMA20230806008Unknown · unknownSSI 53-23-003 FR 88 STGR 26R-27R SHEAR CLIP CORRODED. (LEVEL 2 CORROSION) -C/A- REMOVED AND REPLACED FR 88 STGR 26R-27R SHEAR CLIP IAW EMB 170 SRM 51-40-08. REMOVED AND REPLACED FR 88 STGR 26R-27R SHEAR CLIP IAW EMB 170 SRM 51-40-08.Aug 6, 2023 · N783LC · Emb ERJ170100SUSDR SWAA2023082185925Panel · crackedPANEL 195CR HAS CRACK TO AFT LOWER CORNER EDGEBAND ON INNER SURFACE<[01] CRACK AT AFT LOWER CORNER EDGEBAND ON INNER SURFACE OF PANEL 195CR WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.Aug 5, 2023 · N292WN · Boeing 7377H4SDR IPXA2023081296740Stiffener · crackedFAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4.O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5202 SH.2 REV.- AND BOEING DAug 5, 2023 · N324UP · Boeing 76734AFSDR IPXA2023081296743Stiffener · crackedFAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 RBL 11 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4. O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5201 SH.2 REV.A AND BOEING Aug 5, 2023 · N324UP · Boeing 76734AFSDR YENA2023080800923Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 43R & STR 44 IN FED CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC FR34 BTW STR 43RSTR44 INFWD CARGO COMPARTMENT IAW A320- SRM 51-42-11 & 51-71-11 DWG D53231375.Aug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800922Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION BELLY FAIRING KEEL BEAM STRUCTURE LOCATED AT LEVEL STR 42L AN D BTW FR.35 AND FR 36 AT LOWER FUSELAGE; ACCOMPLISHED REPAIR OF CORROSION AFFECTING STRINGER 42L AT THE KEEL BEAM BOX STRUCTURE AREA BETWEEN FR35 TO FR36 IN ACCORAug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800921Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT ( CPCP RELATED REFER TO MPD TASK 532180-01); REF AEROMAN N/R 2023-403474, R&R SHEAR TIE LOC FR 34 BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT IAW A320 SRM Aug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800919Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FRAME 32 SHEAR TIE BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF AEROMSAN WO1222982-NR2023-403471; REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM 51-Aug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800917Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION BELLY FAIRING KEE BEAM STRUCTURE LOCATED AT LEVEL STR 42L AN D BTW FR.35 AND FR 36 AT LOWER FUSELAGE; REF AEROMAN WO 2023 132/1 NR 2023-403355 -- ACCOMPLISHED REPAIR OF CORROSION AFFECTING STRINGER 42L AT THE KEEL BEAM BOX SAug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800916Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 43R & STR 44 IN FWD CARGO COMPARTMENT; REF AEROMAN WO 2023-132/1 NR 2023-403476 - REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR 43R AND 44 IN FWD CARGO COMPARTMENT IAW WITH A320 SRM 51-42-11, SRAug 5, 2023 · N657JB · Airbus A320232SDR YENA2023080800913Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING" CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO2268 NRC 00151 CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED AND EVAAug 5, 2023 · N279JB · Emb ERJ190100IGWSDR YENA2023080800912Unknown · unknownDURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON DOUBLER REPAIR IN L/H BEAM BTW FR 15/17 AND Y=300 LH AT CABIN FLOOR STRUCTURE (W1); (RESOLVED ON W/O: 1241004 TASKCARD: NR-00011 ) REF: TOMX W/O 2268 N/R 00152. REPAIRED IAW ETI -190-23-601 REV 1 AND ETD 223-Aug 5, 2023 · N279JB · Emb ERJ190100IGWSDR YENA2023080800907Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT AREA COVERED BY LIVE TV RADOME; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00025 ) CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT THE AREA COVERED BY LIVE TV RADOME WAS REMOVED ANAug 5, 2023 · N279JB · Emb ERJ190100IGWSDR YENA2023080800906Unknown · unknownDURING HEAVY MAINTENANCE: CPCP FINDING CORROSION ON DOUBLER REPAIR IN L/H BEAM BTW FR 15/17 AND Y=300 LH AT CABIN FLOOR STRUCTURE (W1); REF: TOMX W/O 2268 N/R 00152 REPAIRED IAW ETI -190-23-601 REV 1 AND ETD 223-190-017761 REV:/ (CONSIDERED AS A MAJOR REPAIR)Aug 5, 2023 · N279JB · Emb ERJ190100IGWSDR YENA2023080800905Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING" CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1); REF TOMX WO2268 NRC 00151 CORROSION ON RH BEAM BTW FR12/17 AND Y:300 RH AT CABIN FLOOR STRUCTURE (W1) WAS REMOVED AND EVAAug 5, 2023 · N279JB · Emb ERJ190100IGWSDR YENA2023080800904Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE / FR63 - FR64 & STGR 01L-02L / SKIN /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Aug 5, 2023 · N279JB · Emb ERJ190100IGWSDR DALA2023080706368Unknown · unknownCRACKS ON UPPER FWD CORNER STA Y=756, LOWER FWD CORNERS STA Y=794, Y=851, Y=908, AND UPPER AFT CORNERS STA Y=832, Y=870, Y=889 OF LH RING PANS AT INNER STRUCTURE OF PAX CABIN. SUMMARY OF NRC 00311: REPAIR ON UPPER FWD CORNER STA Y=756, LOWER FWD CORNERS STA Y=Aug 5, 2023 · N922AT · Boeing 717200SDR DALA2023080706367Unknown · unknownCRACKS ON UPPER AFT CORNERS STA Y=636, Y=696 , Y=832 AND LOWER AFT CORNER STA Y=870 OF RH RING PANS AT INNER STRUCTURE OF PAX CABIN. SUMMARY OF NRC 00309: REPAIR ON UPPER AFT CORNERS STA Y=636, Y=696, Y=832 AND LOWER AFT CORNER STA Y=870 OF RH RING PANS AT INNAug 5, 2023 · N922AT · Boeing 717200SDR SWAA2023083193836Access Panel · bulgedAFT CENTER LOWER WHEEL WELL ACCESS PANEL # 193D HAS BULGING/CRACKED FASTENER HOLES<[01] FILLED FASTENERS HOLES WITH RESIN AND CHOPPED FIBERS FOR CONTINUATION OF REPAIR; CURED REPAIR AS PER B737 SRM 53-40-70-2R-1; SRM 51-70-042R-9 PARAG. 4(D-I); AND SRM 51-70-0Aug 4, 2023 · N966WN · Boeing 7377H4SDR DALA2023080706363Unknown · unknownCORROSION OUT OF LIMITS ON STA=994 TO STA=1053. ORIGINAL THICKNESS OF 0.052 IN. AND MINIMUM REMAINING THICKNESS IS 0.009 IN ON SIDE PARTS, THEREFORE AREAS ARE OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 PAR 4 FIG 101 AND PER DC-MD/BOEAug 4, 2023 · N922AT · Boeing 717200SDR SWIA2023102700803Unknown · chafedCLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R (MARKED) (C-CHECK RO 10/29/2023) REPAIRED CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R REF CRJ200 SRM 51-42-06 , REO 601R-53-61-8077 REV -- DATE 2023-09-06 AND REO 601R-51-00-309 REV -A DATEAug 3, 2023 · N953SW · Cndair CL6002B19SDR SWIA2023092800803Unknown · corrodedINTERIOR FS409.0+128-FS559.0 RIGHT SILL HAS CORROSION IN VARIOUS AREAS (C-CHECK RO 9/26/2023) REPAIRED CORROSION ON THE R/H FLOOR SILL PANEL BETWEEN FS409.00+128 TO FS559.00 AT VARIOUS LOCATIONS ( 9 EA.) REF REO 601R-53-41-666 REV-C, DATED 2012-11-06. COMPAug 3, 2023 · N983SW · Cndair CL6002B19
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