JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, 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 = '5321' 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.
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 = '5321' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2023061604911Unknown · unknownSHIP 3353 CORROSION FLOOR BEAM LOCATED Y1552.5 FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED Y1552.5 FR31 TO FR37 IN PASSENGER CABIN. (2817970)SDR FDEA202306151039Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1268.75/RBL112.75-115 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1268.75/RBL 112.75- 115 CRACK(OFF WING), THE CRACK SIZE:L=2.25", DAMAGE OUT OF ALLOWABLSDR FDEA202306151038Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1240-1241.5/LBL109 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1240-1241.5/LBL109 CRACK(OFF WING), THE CRACK SIZE:L=1.5", DAMAGE OUT OF ALLOWABLE LIMIT SDR DALA2023061504879Unknown · unknownCORROSION ON DOOR JAMB AFT LOWER SECTION STA =950 TO STA=992. SUMMARY OF NRC 00071: CORROSION LEVEL 2. DOOR JAMB AFT LOWER SECTION STA=950 TO STA=992 WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2816939)SDR SWAA2023081459114Floor Panel · crackedMAIN CABIN CENTER AREA FLOOR PANEL 242CF TOP FIBERGLASS SKIN WITH CRACK APROX. 5'<[01] REPAIRED FLOOR PANEL #242CF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-1 PARA 3.M. MATERIALS USED RESIN P/O#1783720; CLOTH P/O#1738579SDR IPXA2023070193568Floor Panel · damagedINSPECTION TYPE:1CPANEL 221FG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BSDR IPXA2023070193564Floor Panel · damagedINSPECTION TYPE:1CPANEL 232SG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BSDR IPXA2023070193563Floor Panel · damagedINSPECTION TYPE:1CPANEL 231WG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BSDR IPXA2023070193562Floor Panel · damagedINSPECTION TYPE:1CPANEL 231RG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.SDR DALA2023061604922Unknown · unknown(LOG 2815904) AFT CARGO ZEE CHANNEL AT STA 727L TO STA 847 LBL 25 WL 160 HAS CORROSION. REMOVED AND REPLACED L/H ZEE CHANNEL STA 727K + 10 TO STA 787 + 10 IAW B737 SRM 51-40-02, B737 SRM 53-00-53-2R PROCEEDURE 5, B737 SRM 51-20-01-0G, B737 AMM 51-21-72-370-804SDR DALA2023061604937Panel · corroded(LOG 2815290) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 500C + 15 LBL 26. LOCATED AND DRILLED NEW TRANSISTION PANEL AND SPLICE FROM BAC1496-444-7075-T6 IAW B-737-900 SRM 53-00-53-2SDR JR2R20230614617Doubler · corrodedDOUBLER ON TOP OF LH FLOOR SILL AND FLOOR WEB CORRODED BETWEEN FR87 AND FR88SDR DALA2023061604921Unknown · unknown(LOG 2814701) CRACKED ANGLE - SUPPORT LOCATED BS500L BETWEEN STR28LH AND STR28RH AT FWD CARGO COMPARTMENT. REPLACED ANGLE-SUPPORT (2 E/A) LOCATED BS500L BETWEEN STR28LH AND STR28RH AT FWD CARGO COMPARTMENT (2 EA) AS PER B737 900 ER SRM 51-40-02 AND DRAWING 143SDR DALA2023061604919Unknown · unknown(LOG 2814866) CRACKED BRACKET LOCATED BS500K FWD AND AFT FRAME STR26R AT FWD CARGO COMPARTMENT. REPLACED BRACKET LOCATED BS500K FWD AND AFT FACE FRAME STR 26R AT FWD CARGO COMPARTMENT (2 EA) AS PER B737-900ER SRM 51-40-02,B737-900ER SRM 51-10-02-0G AND DWG 143SDR DALA2023061604918Unknown · unknown(LOG 2814864) CRACKED BRACKET LOCATED BS500J AND STR26R AT FWD CARGO COMPARTMENT. REPLACED BRACKET LOCATED BS500J FWD FACE FRAME STR26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02-0G, B737-900ER SRM51-10-02-0G AND DWG 143A7505 SHEET 105 REV E.SDR DALA2023061604917Unknown · unknown(LOG 2814861) FWD CARGO COMPARTMENT L/H FLOOR BAFFLE STA 500I-500J CRACKED. REPLACED BAFFLE AT STA 500I TO 500J LBL 25, AND PERFORMED SRM REPAIR 53-30-53-2R-1, IAW B737 SRM 51-40-02 AND DWG# 143A7505 E.SDR DALA2023061604916Unknown · unknown(LOG 2814721) CRACKED BRACKET LOCATED BS500J AND STR26L AT FWD CARGO COMPARTMENT. REPLACED BRACKET LOCATED BS500J FWD FACE FRAME STR26L AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02-0G, B737-900ER SRM 51-10-02-0G AND DWG 143A7505 SHEET 105 REV : E.SDR DALA2023061604915Unknown · unknown(LOG 2814704) CRACKED SUPPORT ZEE RBL 21 BTW BS 727H TO BS 727I AND BTW BS 727L TO BS 747 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON SUPPORT ZEE RBL 21 BETWEEN BS 727H TO 727I AT AFT CARGO COMPARTMENT AS PER B737-900ER SRM53-00-53-2R PROCEDURE 5, SDR DALA2023061304795Unknown · unknownCRACKED MEMBRANE BTW STA Y=172 AND Y=187 APROX AND X54 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00577: MEMBRANE BTW STA Y=172 AND Y=200 APROX AND X54 AT CABIN FLOOR STRUCTURE WAS REPLACED PER DRAWING 9936534-5 REV BW AND PER B717-200 SRM 51-41-05-0G AND 51-41-SDR SWAA2023062058388Floor Panel · crackedWORKING MEL 25-16-01 AFT CARGO FLOOR PANEL 140BF HAS A 1 CRACK IN THE MIDDLE OF THE FLOOR PANEL 10 FROM THE AFT EDGE. AFT CARGO SIDEWALL PANEL 141BW HAS 1.5 CRACK 4 FROM THE AFT EDGE. AFT CARGO SIDEWALL PANEL 141DW HAS SEVERAL 1 CRACKS ON THE EDGE OF THE PANELSDR DALA2023061304822Unknown · unknownAIRCRAFT 3123, CORROSION FRAME 68 LOWER CORNER LH SIDE CUTOUT AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED LOWER CORNER FITTING LOC. AT FRAME 68 LH SIDE CUTOUT AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG D53480505. (LP 2812766)SDR DALA2023061504876Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1). SUMMARY OF NRC 00409: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1) WERE REPLACED PER DWG 9936534 REV BW AND PER B717-2SDR DALA2023061304805Unknown · unknown(LOG 2811059) DENTS ON SUPPORT ZEE LOCATED BTW STA 500A TO STA 500C AND STR 26R AT FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION DENTS SUPPORT ZEE LOCATED BTW STA 500A TO STA 500L AT LEVEL STR 26R AT FWD CARGO COMPARTMENT AS PER ER/A 608756-14REVISION ORSDR IPXA2023070193569Floor Panel · damagedINSPECTION TYPE:1CPANEL 231BH BROKENFABBED PNL IAW SREO A300-5320-40552-BSDR AALA202306197859Floor Panel · damagedAIRCRAFT WAS NOT GROUNDED: FLOOR NEAR ROW 18 AND 19 SOFT, SEEMS WEAK. **SUPPLEMENTAL REPORT FOR AALA202306147859: ACCOMPLISHED REPAIR PROCEDURE PER AARD 53-00-00-3.** (CLOSED).SDR DALA2023061304799Unknown · unknown(LOG 2809471) FLOORBEAM STA 328 LBL 12 CORROSION ON TOP. REPAIRED FLOORBEAM STA 328 LBL12 TOP IAW BOEING 737-800 SRM 53-10-51-2R REPAIR 8.SDR DALA2023061304793Unknown · unknownCORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1. SUMMARY CORROSION LEVEL 2. FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02-0G. (LP #2809951)SDR DALA2023061204754Unknown · unknownCRACK SHEAR PLATE STR 23 L LOCATED BTW FR 69 TO FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS STR 23 L LOCATED BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11-801, SRM51-72-11-911-001 AND DWG D53474180 RELEASE DATE 14-JUL-22 ISSUESDR IPXA2023070193575Floor Panel · damagedINSPECTION TYPE:IC2CPANEL DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BSDR IPXA2023070193566Floor Panel · damagedINSPECTION TYPE:1CPANEL 231NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.SDR ASAA2023060943604Floor Panel · unknownFLOOR PANEL HOLES REQUIRE FILLED TO FACILITATE FLOOR BEAM REPAIR ON PANEL NUMBER 147A5810-477. GROUNDED - YES. REMOVED 2 EA INSERTS AND POTTED HOLES. REPAIRED IAW ASA B737-NG SRM 53-00-50-2R-0.SDR FDEA202306091011Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 FOUND PUNCTURED AT STA1224 LBL29. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 PUNCTURED AT STA1224 LBL29 DAMAGE SIZE LXW=1.8"X 1.5" WITHIN ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 RSDR AALA202306303032Floorboard · delaminatedAIRCARFT IN BASE MAINTENANCE: FLOORBOARD 241UF IS DELAMINATED. REPLACED FLOORBOARD.SDR AALA202306303784Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD 222AAA IS DELAMINATED. REPLACED FLOORBOARD PER AMM 53-21-00.SDR AALA202306301802Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD 242EF IS DELAMINATED. REPLACED FLOORBOARD PER AMM 53-21-00.SDR AALA202306301195Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD 247ABA IS DELAMINATED. REPLACED FLOORBOARD.SDR AALA202306309853Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCED: FLOORBOARD 221CF IS DELAMINATED. REPLACED FLOORBOARD PER AMM 53-21-00.SDR SWAA2023060857170Floor Panel · crackedAFT CARGO PANEL 140BF CRACKED.<[01] REMOVED AND REPLACED AFT CARGO PANEL 140BF REF AMM 25-52-10.SDR FDEA202306081009Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081008Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081007Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306081006Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081005Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/22SDR SWAA2023071256984Panel · crackedAREA ABOVE WING BOX CENTER SECTION HAS CRACKED BREAK PANEL AT BS 540; LBL 1; WL 207<[01] REMOVED BREAK PANEL AT BS540 FROM LBL0-LBL25 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW BREAK PANEL AT BS 540; LBL 1; WL 207 IAW SRM 51-40-05-0G-0 AND DWG 143A5240; OK SDR SWAA2023071256985Panel · crackedAREA ABOVE WING BOX CENTER SECTION HAS CRACKED BREAK PANEL AT BS 540; RBL 1; WL 207<[01] REMOVED BREAK PANEL AT BS540 FROM RBL1-RBL25 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW BREAK PANEL AT BS 540; RBL 1; WL 207 IAW SRM 51-40-05-0G-0 AND DWG 143A5240; OK SDR SWAA2023062957127Floor Panel · corrodedDOT 075-33 AFT CARGO FLOOR PANEL 140AF CORROSION AROUND EDGES OF PANEL.<[01] JOB COMPLETE; AUDIT C/WSDR SWAA2023062957126Floor Panel · corrodedDOT 075-32 AFT CARGO FLOOR PANEL 140EF CORROSION AROUND EDGES OF PANEL.<[01] AUDIT COMPLETE.SDR SWAA2023062757123Floor Panel · corrodedDOT 075-29 AFT CARGO FLOOR PANEL 140DF CORROSION AROUND EDGES OF PANEL.<[01] STARTED FABRICATING FLOOR PANEL AND TRANSFERING HOLES I.A.W. SRM 50-10-04-400-801;[02] VERIFIED STEP 1;[03] FINISH TO FABRICATED FLOOR PANEL 140DF I.A.W AMM 50-10-04-400-801 AND SRM 5SDR SWAA2023062757124Floor Panel · corrodedDOT 075-30 AFT CARGO FLOOR PANEL 140CF CORROSION AROUND EDGES OF PANEL.<[01] VERIFIED MATERIAL I.A.W. SRM 53-00-53-1A-1 AND BOEING DWG 453A2610-32 REV D;[02] VERIFIED STEP 1;[03] STARTED FABRICATING FLOOR PANEL I.A.W. 50-10-04-400-801;[04] VERIFIED STEP 3;[05]SDR SWAA2023062757125Floor Panel · corrodedDOT 075-31 AFT CARGO FLOOR PANEL 140BF CORROSION AROUND EDGES OF PANEL.<[01] EVALUATED CORROSION ON FLOOR PANEL 140BF; FOUND TO BE GREATER THAN 3' IN LEGTH. MEASURED WITH STEEL RULE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 STEP 5. A. (B) 1);[02] VERIFI
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