JASC 5300
Service difficulty reports · 8,205
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.
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
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 SWIA202306290009Unknown · corrodedCF III FLOOR STRUCTURE AT FR 90 STGR 17, HAVE CORROSION ON SPLICE BETWEEN LH AND RH BEAM. (C-CHECK RO 6/28/2023) REMOVED AND REPLACED CF III FLOOR STRUCTURE AT FR 90 STGR 17 REF EMB SRM 51-40-08SDR ABXA20230626135Support Beam · corrodedDURING N317CM C-CHECK AT AIRBORNE (TAMPA), THE FWD CARGO FLOOR SUPPORT BEAM (P/N 451T1604-2) AT STA 548, RBR 41.28 HAS CORROSION. THE DAMAGE WAS REMOVED BY BLEND-OUT PROCESS. THE FLOOR SUPPORT IS FABRICATED FROM 7075-T6511 AL ALLOY EXTRUSION (BAC1506-1898) PERSDR CALA2023061601886Frame · crackedCUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVEL, VIEW WITH MIRROR AND FLASHLIGHT UNDER CUSP WEB. (K. JONES V932161) CUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVESDR YENA2023061300627Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR69 AND FR70 AT LEVEL STR23R AT AFT GALLEY AREA. (CPCP-RELATED TASK 534195-01); (RESOLVED ON W/O: 1218468 TASKCARD: NR-00015 ) REMOVED AND REPLACED STRUCTURE WEB LOC. BTW FR69 AND FR70 AT LEVSDR MASA20230612002Floorbeam · crackedCRACK ON COCKPIT FLOORBEAM AT RBL 12.00, 2" FWD OF 280.00 BEAM. REPAIRED IAW MHI RJ AVIATION REO# 690-53-11-1562SDR DALA2023061204734Unknown · unknown(LOG 2808040) FUSELAGE FRAME CRACKED AT STA 727B BETWEEN STR 8R & 9R AT I/B HOLE FOR BIN SUPPORT BRACKET. REPAIRED FRAME STA 727B AT STR 8R-9R FOR BIN RAIL SUPPORT IAW DELTA WORKCARD 2526-01236-02B.SDR DALA2023061204733Unknown · unknown(LOG 2808030) FUSELAGE FRAME IS CRACKED AT STA 500D BETWEEN STR 8R-9R AT I/B ATTACH HOLE OF BIN SUPPORT BRACKET. REPAIRED FRAME STA 500D AT STR8R & 9R FOR BIN RAIL SUPPORT IAW DELTA WORKCARD 2526-01236-02B.SDR DALA2023061204732Unknown · unknown(LOG 2807884) FORWARD CARGO BAY HAS CRACKED BAFFLE CLIP ON L/H AFT SIDE AT STA 500K. REMOVED AND REPLACED FWD CARGO BAFFLE CLIP LH AFT SIDE STA 500K IAW B737 SRM 51-40-02 AND DWG 143A7505.SDR DALA2023061204731Unknown · unknown(LOG 2807853) FORWARD CARGO BAY HAS A DENT ON L/H FRAME AT STA 500G STR 26. REPAIRED FWD CARGO FRAME STA 500G LH STR 26 IAW B737 SRM 53-30-07-2R-1. DENT ON L/H FRAME STA 500G STR 26.SDR DALA2023061204730Unknown · unknown(LOG 2807753) MAIN CABIN FLOOR SUPPORT STA 951-967 LBL 30 CORRODED AROUND HOLE DOT 45/018. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-900 SRM 51-40-02.SDR 2023F00194Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND PRESSURE PLATE HOLES BETWEEN L/H FR 35 TO 36 HOLES #47, HOLE #67 AND HOLE #51
CRACKED AND OUT OF ROUND. S/O 193146 N/R 20087.SDR 2023F00193Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND PRESSURE PLATE HOLES BETWEEN L/H FR 35 TO 36 HOLES #47, HOLE #67 AND HOLE #51
CRACKED AND OUT OF ROUND. S/O 193146 N/R 20087.SDR 2023F00192Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND PRESSURE PLATE HOLES BETWEEN L/H FR 35 TO 36 HOLES #47, HOLE #67 AND HOLE #51
CRACKED AND OUT OF ROUND. S/O 193146 N/R 20087.SDR 2023F00191Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND PRESSURE PLATE HOLES BETWEEN L/H FR 35 TO 36 HOLES #47, HOLE #67 AND HOLE #51
CRACKED AND OUT OF ROUND. S/O 193146 N/R 20087.SDR 2023F00190Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H PRESSURE PLATE HOLES AT FR 36 HOLE #10 AND #11 CRACKED AT APPROX. 5 O'CLOCK POSITIONS AND HOLE #12 CRACKED AT APPROX. 6 O'CLOCK POSITION. S/O 193146 N/R 20086SDR 2023F00189Pressure Panel · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H PRESSURE PLATE HOLES FR 36 HOLE #18, HOLE #19 AND HOLE #20 ALL THREE HOLES
WERE CRACKED AT APPROX. 6 O'CLOCK POSITIONS. ALL THREE HOLES ARE OUTSIDE THE REPAIR AREA.. S/O 193146 N/R 20085SDR 2023F00188Pressure Plate · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H PRESSURE PLATE HOLES FR 36 HOLE #4 (OUTSIDE THE REPAIR AREA) CRACKED AT 4 O'CLOCK POSITION, HOLE #5 CRACKED AT 12 AND 6 O'CLOCK POSITION, HOLES #6 AND #7 CRACKED AT THE 6 O'CLOCK POSITIONS, SSDR 2023F00186Pressure Panel · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H FR 35 TO 36 PRESSURE PANEL HAS A CRACK INDICATION AT INBD HOLE "A" PRESSURE PANEL LAYER, IN THE AFT DIRECTION. AD 2018-06-04 RELATED TASK. S/O 193146 N/R 20024SDR JJBA20230613009Unknown · unknownWINDOWS FLIGHT COMPARTMENT, OVERHEAD ANGLE SPLICE BEAM CRACKED AT TWO PLACES. LH & RH FWD FUSE 2 WINDOW FLIGHT COMPARTMENT OVERHEAD PANEL RIB REPAIRED WITH 2 REPAIR DOUBLERSSDR DALA2023061204729Unknown · unknown(LOG2806940) CRACKED BRACKET LOCATED BS500K FWD AND AFT FRAME STR26L AT FWD CARGO COM. REPLACED BRACKET (2E/A) AND FASTENERS LOCATED ON STA500K AT LEVEL STGR 26L AS PER B737-900 SRM 51-10-02-0G, ITEM 9 AND DWG #143A7505.SDR DALA2023061204727Unknown · unknown(LOG 2806288) FWD CARGO BAY HAS DAMAGED BAFFLE BETWEEN STA 500I TO 500J LH. REMOVED, REPLACED AND REPAIRED FWD CARGO BAFFLE STA 500I-500J IAW B737 SRM 51-40-02, 53-30-53-2R-1 AND DWG 143A7505.SDR DALA2023060804674Unknown · unknownSHIP 3422 DURING THE TASK OF REMOVING FRAME CLIPS, ACCIDENTALLY MADE ABOUT 3.2 MM PUNCHED HOLE & MISSED-HIT DENTS AT FRONT OF FR62 STR 3R, JUST BELOW CORNER OF STRINGER. ALSO, MIS-DRILLED A STRINGER & SKIN HOLE DURING PREP OF STR REPLACEMENT. CORRECTIVE ACTIONSDR ABXA20230623126Skin · faultyDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MX WAS REQUIRED TO RE-INSPECT AND REPLACE (5/32”) BLIND FASTENERS IN AN EXISTING REPAIR DESCRIBED IN ABX “WATCH ITEM” WI-220CY-06202022. UPON REMOVAL OF THE REPAIR AND EVALUATION, IT WAS FOUND THAT REPLACEMENT FASDR SWIA202306130007Unknown · corrodedCORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 27R-28R. (C-CHECK RO 6/9/2023) REMOVED AND REPLACED SHEAR CLIP AT FR 88 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08SDR IPXA2023060993406Fairing · crackedINSPECTION TYPE:C611AB OPENING HAS A CRACKREPAIRED AREA IAW SRM 53-15-63SDR DALA2023061004716Unknown · unknownSHIP 171 FOUND SKIN DAMAGE AFT LH FUSELGE FWD OF BULK CARGO DOOR BELOW PRIOR SKIN REPAIR. CORRECTIVE ACTION: INSTALLED REPAIR DOUBLER PER B767 SRM 53-00-01-2R PROCEDURE 29 (2803876)SDR ASAA2023060743501Unknown · overtempSTRONG SMELL OF HOT BURNING PLASTIC ROW 31 THROUGH AFT GALLEY. GROUNDED - YES. FOUND THE STAND ALONE CONTENT LOADER (SACL) TO SMELL HOT AND WAS VERY HOT TO TOUCH, REQUIRES REPLACEMENT FTO FIX SMELL IN CABIN. SACL HAS STRONG ELEC SMELL. REMOVED & REPLACED SACL SDR CALA2023060901797Unknown · crackedSUPPORT TASK - AD 2022-06-07 / EA 5380-01117 - RH BS 2370 PIVOT BULKHEAD FORWARD CHORD FOUND CRACKED, RESOLVE THE DAMAGE BY PERFORMING OP 026 MODIFICATION. TRANSFER REF NR HX WO.1827344 AND ORIGINATED BY EMP V896827. RH BS2370 PIVOT BULKHEAD FWD CHORD REPLACEMSDR CALA2023060901791Unknown · puncturedRAMP REPORTED PUNCTURED IN THE AFT CARGO FLOOR. PER SRM 53-00-53-1A-1. PARAGRAPH 2 APPLIED SPEED TAPE. TOMC APPROVED DIP TO DUE A VUSUAL INSPECTION AT 400 FLIGHT TOMC-APPROVAL FROM SC1ELBYC COMMENT CYCLES OF THE SPEED TAPE AND REAPPLY AS NECESSARY. A PERMANENTSDR CALA2023060901804Frame · unknownEA 5310-07582 REV A: AFT CARGO COMPARTMENT STA 1300 R/H S26-S27 HAS AN EXISTING REPAIR WITHOUT SRM STANDARDS. PER ECRA 5360-01712 PART 1.2. IT STATES TO CREATE A DIP TO READ: 5360-01712 ON OR BEFORE 26 MAY 2024. EXISTING REPAIR WAS FOUND PERFORM AN INSPECTION SDR CALA2023060701777Unknown · crackedSUPPORT TASK - AD 2022-06-07 / EA 5380-01113 - LH BS2370 PIVOT BULKHEAD FORWARD CHORD FOUND CRACKED, RESOLVE THE DAMAGE BY PERFORMING OP 025 MODIFICATION. TRANSFER REF NR HX WO.1827358 AND ORIGINATED BY EMP V896827. LH BS2370 PIVOT BULKHEAD FORWARD CHORD REPLASDR SWIA202306130006Unknown · corrodedCORROSION ON WASTE BOX DOUBLER SURFACE AT WASTE DOOR HINGE AS MARKED. (C-CHECK RO 6/9/2023) REMOVED CORROSION AT WASTE BOX DOUBLER BY INSTALLING OUTER REPAIR DOUBLER AT FRAME 88, STRGS 26R-27R. SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 53-23-60SDR YENA2023060900618Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16LH DOOR STOP FITTING Ñ7 HOLE 3. CRACK DIRECTION IS 1 O'CLOCK; REF AEROMAN W/O 2023-11/1 NR 2023-255756. REMOVED AND REPLACED INTERCOSTAL FITTING LOC.FR16LH DOOR STOP FITTING #7 HOLE 3 IAW A320 SRM 51-72-SDR YENA2023060900617Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR20RH DOOR STOP FITTING Ñ7 HOLE 2. CRACK DIRECTION IS 4 O'CLOCK; REMOVED AND REPLACED INTERCOSTAL FITTING LOC.FR20RH DOOR STOP FITTING #7 IAW SRM 51-11-12-300-10 AND SRM 51-72-11 AND DWG 53114224.SDR YENA2023060900609Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION STRINGER 42R LOC. BTW FR.31 TO FR. 35 IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1209138 TASKCARD: NR-00021 ) REMOVED AND REPLACED SECTION STRINGER 42R BTW FR31 TO FR35 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-72-11, SRM 51SDR YENA2023060900608Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 66 RH, DOOR STOP 1 HOLE POSITION IS INBOARD /UPPER, DIRECTION OF CRACK IS 6 O'CLOCK; (RESOLVED ON W/O: 1209138 TASKCARD: NR-00022 ) FUR-A320-53-00734, REF AEROMAN N/R 2023-255848, PERFORMED REPAIR LOC. FSDR YENA2023060900607Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 66 RH, DOOR STOP 1 HOLE POSITION IS INBOARD /UPPER, DIRECTION OF CRACK IS 6 O'CLOCK; REF AEROMAN N/R 2023-255848, FUR A320-53-00734, PERFORMED REPAIR LOC. FR66RH DOOR STOP 1 IAW A320 SRM 51-41-12-300-010, SDR YENA2023060900606Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16LH DOOR STOP FITTING N7 HOLE 3. THE CRACK DIRECTION IS 1 O'CLOCK; REF AEROMAN W/O 2023-11/1 NRC 2023-255756. REMOVED AND REPLACED INTERCOSTAL FITTING LOC.FR16LH DOOR STOP FITTING #7 HOLE 3 IAW A320 SRM 5SDR YENA2023060900605Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 68 LH DOOR STOP 1 HOLE POSITIONS IS INBOARD/LOWER, DIRECTION OF CRACK IS 6 O'CLOCK; REF AEROMAN W/O 2023-11/1 NR 2023-255849. ITEM CLOSED ON LOG PAGGE 3750828-2 ((RESOLVED ON W/O: 1209138 TASKCARD: NR-000SDR YENA2023060900603Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH, DOOR STOP 1 HOLE POSITION IS INBOARD/LOWER DIRECTION OF CRACK IS 6 O'CLOCK; (RESOLVED ON W/O: 1209138 TASKCARD: NR-00023 ) REF AEROMAN W/O 2023-11/1 NR 2023-255893. PERFORMED PERMANENT REPAIR LOC FRSDR YENA2023060900602Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH, DOOR STOP 1 HOLE POSITION IS INBOAR D/ LOWER DIRECTION OF CRACK IS HOLE 6 O CLOCK (INSPECTION AREAÑ 2 AS P ER SRI 53-41-12-205 -010 TABLE 006 FIGURE 001 ); (RESOLVED ON W/O: 1209138 TASKCARD: NR-0002SDR YENA2023060900601Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH DOOR STOP 1 HOLE POSITION IS INBD/LOWER DIRECTION OF CRACK IS 6 O'CLOCK; (RESOLVED ON W/O: 1209138 TASKCARD: NR-00025 ) PERFORMED PERMANENT REPAIR LOC. FR68LH AT LEVEL DOOR STOP FITTING 1 IAW A320 SRSDR YENA2023060900600Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 8 LH SIDE AFT FACE INNER CAP IN LATERAL SPLI CING AREA, THIRD FASTENER FROM UPPER TO LOWER, CRACK POSITION IS 12 OC LOCK, CRACK LENGTH IS 0.145 INCH APPROX, IN COCKPIT (1 EA); (RESOLVED ON W/O: 1209138 TASKCASDR YENA2023060900599Unknown · unknownDURING HEAVY MAINTENANCE: A CRACK INDICATION WAS FOUND ON RH WINDSHIELD FRAME NEAR TO LOWER RADIUS LOCATED ON THE CENTER LOWER NODE AT FR 2. THE CRACK LENGTH IS 0.265 INCHES APPROX. CRACK IS IN FLIGHT DIRECTION; REF TO AEROMAN WO 2023 11/1 NR 2023-255709, PERFSDR YENA2023060900597Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023060900596Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / CRACK ON 3RD HOLE OF UPPER FR8 LH / PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR TSAA20230606106Unknown · unknownCA 1464/100 CORROSION AT FUSELAGE SKIN BETWEEN STA579 AND STA616, S-14R AND S-15R ( L:4.5" W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 579 AND STA 616, S-14R AND S-15R (L:4.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LIMISDR TSAA20230606103Unknown · unknownCA 1464/9 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 20 STATION 767 TO 787, 867 TO 897, 927 TO 929. ALL CORROSION REMOVED AT STA500 & STA500E, S-1R & S-2R (L:3.1", W:2.2") (L:14", W:1.4") (L:0.9", W:0.5") L:0.5", W:0.4") (L:1.9",SDR TSAA20230606102Unknown · unknownCA 1464/303 LIGHT CORROSION AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. ALL CORROSION REMOVED AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-SDR TSAA20230606101Unknown · unknownCA 1464/302 LIGHT CORROSION AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. ALL CORROSION REMOVED AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-10
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