JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2023111709480Unknown · unknownSHIP 3021 SKIN WAS DAMAGED BY TOW BAR. CORRECTIVE ACTION: COMPLIED WITH ERA 600716-00. (2859085)SDR R61A2023090700479Skin · corrodedFRAME 90-91 STRINGERS 29L-29R HAS CORROSION ON INTERNAL SKIN AS MARKED. PERFORMED TEMPORARY REPAIR BY CUTOUT AND DOUBLER REPAIR AT 90-91 STRINGERS 29L-29R ON INTERNAL SKIN IN ACCORDANCE WITH, REF ETD2023--170-020249.SDR ABXA20230814162Stringer · crackedDURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED A 1.10-INCH CRACK DAMAGE ON STRINGER S2R APPROXIMATELY AT STA. 665.00. THE SUBJECT STRINGER APPEARS TO BE PRIMARY STRUCTURE, PSE AND FCBS. THE SUBJECT STRINGER IS STILL UNDER I.A.I STC. THE I.SDR SWIA20230718000Unknown · damagedCOMPLY WITH REO 670-53-61-2139 - REPAIR TO LH FUSELAGE SKIN BETWEEN FS1000.00 - FS1015.00 AND STR22L - STR24L THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1168567, EAML 1168260, ML 26861368 (FILED CLOSED)COMPLIED WITH PERMANESDR SWIA202307170001Unknown · dentedFINAL REWORK DIMENSONS OF DENT LOCATED AT FS 650.00 BETWEEN STR21R AND STR22R ARE W 1.30" X L 1.80" X D 0.080". REWORKED DENT IS OUT OF LIMITS PER CRJ 200 SRM 53-00-31 AND HAS BEEN CLASSIFIED AS A MAJOR REPAIR. REFERENCE CP 26856814 FOR INITIAL DISCREPANCY. FOSDR SWIA202307110002Unknown · damagedCOMPLY WITH REO 670-53-61-2139 - REPAIR TO LH FUSELAGE SKIN BETWEEN FS1000.00 - FS1015.00 AND STR22L - STR24L THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1168567, EAML 1168260, ML 26861368 (FILED OPEN)THIS IS CURRENTLY A WORSDR AALA202307170765Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN RIGHT DRAIN RECEPTACLE HAS CORROSION AT BS 727E BETWEEN S26R AND 27R. REPAIRED SKIN PER SRM 53-60-01-2R AND EA 345943SDR DALA2023071005570Unknown · unknownSHIP 3123 CORROSION TANK 1 LOCATED EXTERNAL SKIN UPPER SURFACE AT FR 42 AND Y129 2 IN CENTER FUEL TANK. CORRECTIVE ACTION: REPAIRED PER ER/A 609169-14. (2856362)SDR SWI2023F00331Unknown · cracked*CRACK NOTED AT R/H TRU SKIN ADJACENT TO ADG STOW PUMP ON OTBD SIDE (MARKED) (C-CHECK RO 9/13/2023) PERFORMED REPAIR AT R/H TRU SKIN ADJACENT TO ADG STOW PUMP ON OTBD SIDE IAW ALL STEPS OF REO 601R-53-11-245 REV-C 2019-05-13. COMPLIED WITH TASK CARD 51-SDR SWI2023F00306Unknown · damagedFUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE HAS DAMAGE. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED FUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE REF REO 601R-53-21-3643 REV -- DATED 2023-08-07. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECK GOOSDR R61A2023071400104Skin · damagedDURING ASSESSMENT OF PREVIOUS THROUGH DAMAGE REPAIR JUST AFT OF FR. 20 BETWEEN STGR 22R - 23R, FOUND SKIN TO HAVE AN OIL CANNING CONDITION. REPAIRED DAMAGE JUST AFT OF FR20 BETWEEN STGR 22R-23R BY PERFORMING A CUT OUT AND INSTALLATION OF REPAIR DOUBLER PER ETDSDR SWIA2023071207Unknown · damagedFORWARD FUSELAGE SKIN HAS AREA OF THROUGH DAMAGE LOCATED NEAR THE INTERSECT OF FRAME 22 AND STRINGER 14L. THE DAMAGED AREA MEASURES APPROX 3.0 INCHES LONG AND 1.5 INCHES HIGH. THE ACTUAL THROUGH DAMAGE MEASURES APPROX 1.0 INCH LONG AND 3/4 INCHES HIGH.*THIS DASDR DALA2023071105604Unknown · unknownSHIP 3422 DAMAGE TOLERANCE EVALUATION (DTE) TRACKING ER/A 610110-14. CORRECTIVE ACTION: REF ER/A 610110-14. (2853687)SDR SWIA2023071007Unknown · damagedFORWARD FUSELAGE SKIN HAS AREA OF THROUGH DAMAGE LOCATED NEAR THE INTERSECT OF FRAME 22 AND STRINGER 14L. THE DAMAGED AREA MEASURES APPROX 3.0 INCHES LONG AND 1.5 INCHES HIGH. THE ACTUAL THROUGH DAMAGE MEASURES APPROX 1.0 INCH LONG AND 3/4 INCHES HIGH.*THIS DASDR CALA2023071002199Skin · dentedAIRCRAFT MOVE TEAM FOUND DENTS FWD OF THE L2 DOOR, DENT FOUND IS AROUND 84 INCHES FWD OF THE L2 DOOR ABOVE THE WATER LINE INBETWEEN STRINGER 15 AND 14. FURTHER INSPECTION IS REQUIRED TO DETERMINE IF IT IS A NEW DENT. REFERANCE LOG PAGE 6875361 FOR PRIOR DENT. SDR FDEA202307061183Unknown · unknownAIRCRAFT STRIKE. FUSELAGE DAMAGE AFT OF RADOME. COMPLIED WITH EA # 6-5310-T0375157 PART 1 & 2 FUSELAGE MAINFRAME FRAME 0-FRAME 1/ LOWER FUSELAGE SKIN AT 6 O'CLOCK POSITION STRUCTURALE REPAIR FOR DENT/CREASE TO FRAME AND SKIN.SDR FDEA202307061160Skin · crackedCABIN, R3 AFT LOWER DOOR JAMB STATION 1315 TO 1305 FOUND CRACK. CABIN - CRACK AT R3 DOOR CUT OUT AFT LOWER JAMB STATION 1315 TO STATION 1305 REPAIR CARRIED OUT AS PER SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SWAA2023081574720Panel · debondedPANEL 193AR INNER SKIN PREVIOUS REPAIR IS DISBONDED. (MARKED)<[01] PANEL 193AR WITH INNER SKIN PREVIOUS REPAIR THAT'S DISBONDED AS MARKED WAS REPLACED WITH A SERVICEABLE PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.1.;[02] VERIFIED CORRECTISDR CALA2023070702182Skin · damagedRAMP REPORTED DAMAGE (GAUGE) ABOUT 5" FWD FOR THE FWD CARGO AT THE LAP SEEM. CORRECTION, DAMAGE IS 5 FEET FORWORD OF THE FORWARD CARGO DOOR. DAMAGE IS 66.5" FWD OF FWD CARGO DOOR CUTOUT BETWEEN STATIONS REMOVED FASTENERS ON SKIN LAP AND STRINGER JUST BELOW. CUSDR FDEA202307051151Skin · wornFOUND FUSELAGE SKIN A ABRASION (DEPTH:0.016 IN) AT STA 1014, S36R-S37R, WHICH EXCEEDS 0.005 IN DEPTH. COMPLETED AS PER EA G-5710-T0375107 P2 STEP 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UIEA2023070600720Doubler · unknownWATER FILL CONNECTION AREA DOUBLER CORROSION AT STA 980 S45R - S46R(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PARTS SRM 51-40-02-0G-0 REV 97, DWG 142U3780 SHEET 12 REV F, DWG 140U0999 SHEET 30 REV -, DWG 142U0130 SHEET 1 REV A AND SDR YENA2023070500762Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON OPEN HOLE H2 LOC FRAME 16 LH CROSSBEAM SPLICING AT PASSENGER CABIN LAYER AFFECTED IS THE FRAME LAYER. CRACK DEPTH: 0.063 INCH; REF: ARM W/O 2023 128/1 N/R 2023-355606 PERFORMED PERMANENT REPAIR ON HOLE H2 LOCATED ASDR SWAA2023081474235Baffle · crackedFWD CARGO LEFT SIDE BAFFLE IS CRACKER AT 440 BELOW 'Z' CHANNEL STRINGER 25 L<[01] REMOVED AND REPLACED SIDE BAFFLE AT FWD CARGO STA 440 STRINGER 25L PER B737-700 SRM 51-40-02-0G-0 & DRWN# 143A7505.;[02] CERTIFIED WORK PERFOMED SIDE BAFFLE AT FWD CARGO STA 440 SDR VNAA202308040025Skin · nickedSEVERAL NICKS AT LOWER SKIN OF AFT FUSELAGE BTW FS1000.0 AND FS1069.75 AND BTW STGR 21LH AND STGR 21RH. SEVERAL NICKS AT LOWER SKIN OF AFT FUSELAGE BTW FS1000.0 AND FS1069.75 AND BTW STGR 21LH AND STGR 21RH WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 SDR VNAA202308040015Skin · scratchedFUSELAGE SKINS AND PLATING ALLOWABLE DAMAGE PERM REPAIR DUE IN 6000FH FROM INCORP. SCRATCH ON FUSELAGE SKIN BTW FS1162 AND STGR 19L WAS REPAIRED PER EA 23-C9-53-1022 REV. IR. SECTION III PERMANENT REPAIRSDR VNAA202308040013Skin · unknownSEVERAL LIGHTNING STRIKES ON EXTERNAL FUSELAGE SKIN BTW FS280.00 TO FS693.00 AND STGR21LH TO STGR 21RH. REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03 AND EA 23-C9-53-1002 REV IR SECTION III.SDR I5EA2023070200001Skin · dentedDENT FUSELAGE SECTION 46 UPPER PLATING BS 993 STR 15LHSDR SWAA2023080474154Bear Strap · crackedCRACK ON BEAR STRAP LOCATED BTW BS 303.9 TO BS 294 AT LEVEL STR 9R AT FWD GALLEY AREA 2023-422362<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; SSDR DALA2023070505407Unknown · unknown(LOG 2844472) AFT REMOVAL OF ADF ANTENNA #1 AND #2 FOUND MULTIPLE DOME NUT DAMAGE. REPAIRED ADF ANTENNA #1 AND #2 DOME NUTS PER DELTA ERA 608966-14 REV ORIGINAL.SDR IPXA2023070179128Unknown · unknown*** SDR FILED OPEN *** DENT AND GOUGE BETWEEN STA: 456 AND STA: 434, AT AND BELOW S -26R ***AWE - SM EVAL REQ*** **LINK 22E79** C/W EO87526-REQ2 DEFERRAL REMAINS AT THIS TIMESDR SWI2023F00295Unknown · gougedMULTIPLE GOUGES ON EXTERIOR FUSELAGE SKIN AROUND THE LOW PRESSURE GROUND AIR DOOR, FROM APPROXIMATELY FS1000 TO FS1051, AND STRG27 TO STRG21R (C-CHECK RO 8/31/2023) COMPLIED WITH REPAIR OF GOUGES ON EXTERIOR FUSELAGE SKIN AROUND THE LOW PRESSURE GROUND SDR SWI2023F00294Unknown · damagedCOMPLY WITH REO 670-53-00-290 (REPAIR TO FUSELAGE SKIN FS977-985 STG 27) LATEST REVISION. TO REPLACE/UPGRADE PRE-EXISTING CHAFED DOUBLER. (C-CHECK RO 8/31/2023) COMPLIED WITH REO 670-53-00-290 REV -F DATED 2019-04-26 SOLUTION 1 (CRJ700) - FIGURE 7) REMOSDR SWIA20230629Unknown · corrodedEXTERIOR FUSELAGE SKIN SURROUNDING THE AFT DRAIN MAST BETWEEN FS1031 AND FS1051, STRG27 AND STRG26R IS CORRODED (C-CHECK RO 8/31/2023) REPAIRED EXTERIOR FUSELAGE SKIN SURROUNDING THE AFT DRAIN MAST BETWEEN FS1031 AND FS1051, STRG27 AND STRG26R REF REO 6SDR DALA2023070305325Unknown · unknown(LOG 2840745) FWD ADF ANTENNA AREA, ON TOP OF THE FUSELAGE, CORROSION AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609634-14 REV. ORIGINAL.SDR DALA2023070305324Unknown · unknown(LOG 2840722) AFT ADF ANTENNA AREA, CORROSION FOUND AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609424-14 REV ORIGINAL.SDR FDEA202306291128Skin · corrodedEMPENNAGE-AFT ACCESSORY COMPARTMENT RIGHT HAND SIDE APPROXIMATE STATION 2135- 2145 AROUND LONGERON 35 RIGHT FOUND CORRODED. CORROSION AT EMPENNAGE-AFT ACCESSORY COMPARTMENT ON SKIN RIGHT HAND SIDE APPROXIMATE STATION 2135-2145 AROUND LONGERON 35 RIGHT REMSDR CALA2023063002089Skin · gougedGOUGE ON FUSELAGE SKIN BTW FR27-28 STGR21-22 L/H. AS NOTED ON LTPR NR #5001243275-0010. ON LH FUSELAGE SKIN BTW FR27-28 STGR 21-22 IS PERMANENT CAT "B" FIED AS MAJOR PER UAL GMM 03-20-20. CUTOUT DEM:X=41MM, Y=28MM. D MBODIMENT 60000FC/120000FH. SUB INSP TBD, MSDR CALA2023063002097Skin · crackedCRACK INDICATION FOUND ON FUSELAGE SKIN AT BS 1654.50 PLUS 7.5 INCHES, BELOW STR 13R. CRACK LENGTH=1.500 INCHES. REFER TO AEROMAN NON ROUTINE 2023-350701. ALUMINUM SHEET 7075-T6 0.050" PO #2012545969 THIS REPAIR IS EXTERNAL DETAILED INSPECTION AT INTERVALS 7,5SDR SWAA2023081472583Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR28L AT FWD CARGO COMPARTMENT 2023-413167<[01] REPLACED ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV. A SEE INDIVIDUALSDR IXXA2023071003Skin · damagedLMLG WHEEL WELL FUSELAGE FORWARD OF BODY DOOR IS DAMAGED AT AND AROUND DOUBLER REPAIRSDR CALA2023063002084Bear Strap · unknownAS REQUIRED BY AD 2012-25-11 ACCOMPLISH AN NDT INSPECTION OFTHE BEAR STRAP AND INNER CORD IN THE AREA OF THE REPAIR BEFORE 50,000 TOTAL AIRCRAFT CYCLES.AFTER THE ACCUMULATION OF 46,500 TOTAL A IRCRAFT FLIGHT CYCLES BUT BEFORE 47,000 TOTAL AIRCRAFT FLIGHT CY CLSDR DALA2023063005249Unknown · unknownER/A 596427-14 / SECTION III ONE-TIME INSPECTION. ER/A 596427-14AD, REV B / AT, OR PRIOR TO 26JUL23 ACCOMPLISH ONE-TIME SECTION III INSTRUCTIONS. A321 / FUSELAGE / FR30-32, STR 26L-STR 27L / GROUND DAMAGE. (LP# 2837526).SDR VNAA202306270001Skin Panel · damagedLEFT FUSELAGE HAS DAMAGE BELOW N AND E IN THE LOGO ( DENT ABOUT 3 INCHES)SDR IPXA2024081812684Skin · crackedHFEC REINSPECT REVEALED CRACK INDICATION AND NEW DAMAGED IDENTIFIED VISUALLY (T3F18E001Y856 CLOSED IN ERROR) FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01-2R. MATERIAL ID FOR FILLER IS .100" 2024-T3 PO.#SP2586586, AND FOR DOUBLER .125" 2024 T-3 PO.#SP2SDR SWAA2023081471941Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AND STR26L AT FWD CARGO COMPARTMENT 2023-413056<[01] ET TOOL USED: PN: NORTEC 600D ; SN: 220273012; DUE DATE: 17-DEC-23;[02] REPLACED WEB-INTERCOSTAL AND LOCATED BETWEEN BS500A TO BS500B AND STR26L AT FWSDR IXXA2023080301Skin · damagedDURING ZONAL INSP, A SCRATCH WAS FOUND AT FUSELAGE SKIN SECTION 43 BETWEEN STA 478 AND STA 500, BETWEEN STRINGERS STR-26R AND STR-27RSDR SWAA2023072773243Panel · damagedPANEL 192HL HAS SEVERAL FASTENER HOLE ELONGATED.<[01] APPLIED REPAIR IN FASTENER HOLES AREA AT PANEL #192HL AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED PO#1776837; PO#2012656 AND PO#1738579.APPLIED TOPCOAT ON PANEL 192HL REF B737 AMM 51-21-73-370-803;[02] VERSDR CALA2023062602027Skin · dentedDENT ON LH UPPER FUSELAGE BETWEEN FR''S 45-46, STR''S13-14 D IS GREATER THAN .080", OUT OF LIMITS IAW SRM 53-31-11-283-002 NOTED, TRIMMED OUT DAMAGE & REP''D AREA PER SRM 53-00-11 PROTECTION AS REQ''D, INITIAL INSP THRESHOLD FROM TIME OF 5000FC/10000FH, METHODSDR DALA2023062705144Unknown · unknownUPON AIRCRAFT ARRIVAL AND WHILST POSITIONING LOADER AT AFT CARGO DOOR FOR UNLOADING EQUIPMENT STRUCK THE AIRCRAFT AT FRAME 58 AND STGR 46RH AND 45RH CAUSING A PUNCTURE TO THE FUSELAGE. CORRECTIVE ACTION: ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR IAW ERA 60987SDR CALA2023062602014Doubler · corrodedFWD CARGO PIT R/H BETWEEN FR30-34 AND BETWEEN STRINGERS 43R-44 HAS CORROSION ON SKIN DOUBLER PER HAECO LCQ N/R 9298727/44727 GEN BY V919150 RMVD AND FABRICATED AND INSTALLED DOUBLER AT FWD CARGO FR30-FR34 BETWEEN STRINGER 43R-44 IAW A319 SRM 53-21-11-08-A DWG
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