JASC 5340
Service difficulty reports · 22,406
Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340' 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 = '5340' 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 SWAA2022121273956Fitting · crackedAFT CARGO BAY FITTING CRACKED AT BS 947.5, LBL 10. REMOVED CRACKED FITTING IAW SRM 51-40-02, AND 51-40-05. LOCATED AND DRILLED IAW DWG 149A8103, REV A, AND 51-40-02. INSTALLED THE NEW FITTING IAW DWG 149A8103, REV A, AND SRM 51-40-05.SDR VNAA2022112099914Support Bracket · crackedDURING ACCESS FOUND SUPPORT BRACKET BETWEEN PANELS 195DL AND 196DR TO BE CRACKED TOWARDS THE AFT SECTION OF THE BRACKET.
CORRECTIVE ACTION:
LOCATED, DRILLED CHANNEL PN# CC670-39251-1 IAW CRJ700 SRM 51-40-11-001-001-A01 AND INSTALLED IAW CRJ700 SRM 51-42-06-SDR SWAA2022122073500Tie Down · corrodedFWD CABIN, BS 312, LBL 55, WL 208.1 FLOOR FITTING WAS CORRODED. REMOVED AND REPLACED THE FLOOR TIEDOWN FITTING IAW 51-10-15-1A-1 AND 51-40-02-0G-0.SDR SWAA2022121273217Fitting · crackedCRACKED FITTING, BS 945.5, S26L, IN THE AFT CARGO BAY. REPLACED THE FITTING AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 149A8103, SHEET 7, REV A.SDR REXA2022112102595Fitting · crackedWHILE PERFORMING SB 670BA-53-045 FOUND L/H 220 FRAME TOP FITTING P/N CC67-51720-1 TO BE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.SDR SWAA2022112972974Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 LBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 5;[02] VERIFIED ITEM 2 OF STEP 8;[03] VERIFIED STEP 9;[04] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[05] NO LEAKS NOTED<BR>AUDIT C/WSDR SWAA2022112972975Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 RBL 8 (WL 167) / [01] VERIFIED ITEM 2 OF STEP 8;[02] VERIFIED STEP 9;[03] LEAK CHECKED REPAIR AREA NO LEAK NOTED I.A.W MM 28-11-00-400-801;[04] LEAK CHECK GOOD<BR>AUDIT C/WSDR SWAA2022120772033Attach Angle · crackedAFT CARGO LEFT SIDE BS 867 ATTACH ANGLE CRACKED AT LOWER FRAME LAVATORY POST. LOCATED, DRILLED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.SDR R61A2022112900754Anchor Fitting · corrodedCORROSION AT ANCHOR NUT SUPP PLATE L2 DOOR, FWD GIRT BAR, AFT SUPP PLATE. R&R IAW SRM 51-41-01 & 51-41-02.SDR R61A2022112900753Anchor Fitting · corrodedCORROSION AT ANCHOR NUT SUPP PLATE L2 DOOR, AFT GIRT BAR, AFT SUPP PLATE. R&R IAW SRM 51-41-01 & 51-41-02.SDR AALA202211183537Stringer Clip · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER CLIP LOCATED AT BS 500E AND S6L. REPLACED STRINGER CLIP PER SRM 51-40-02-0GSDR SWAA2022121371329Attach Angle · crackedMID CABIN ATTACH ANGLE CRACKED AT BS 663+29, RBL 24. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02. FABRICATED A NEW ATTACH ANGLE. LOCATED AND DRILLED THE NEW ATTACH ANGLE IAW DWG 273A9112, REV -. TREATED AND PRIMED THE NEW ATTACH ANGLE. INSTALLED THE NEW ASDR SWAA2022121371327Attach Angle · crackedMID CABIN ATTACH ANGLE FOUND CRACKED, BS 663+29, LBL 24. REMOVED ATTACH ANGLE IAW SRM 51-40-02. FABRICATED A NEW ATTACH ANGLE, LOCATED, AND DRILLED IAW DWG 273A9112, REV -. TREATED AND PRIMED THE NEW ATTACH ANGLE. INSTALLED THE NEW ATTACH ANGLE IAW DWG 273A9SDR SWAA2022112970621Bracket · brokenAFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET BROKEN BS867 LBL10 WL166 / [01] REMOVED DAMAGED ACB LAV TANK LOWER BULKHEAD BRACKET; BS867 LBL10; WL 166; LOCATED AND DRILLED; AND INSTALLED NEW BRACKET; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0-G-0; DWG 149A8104.;[02SDR SWAA2022112370623Attach Angle · corrodedAFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATES BS 767 - 787, RBL 21, WL 156. CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED ACB ANGLE SHIELD IAW SRM 51-40-02-0G-0. SDR SWAA2022112969825Attach Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[06] RECEIVED REPAIR PARTS FOR BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL20 WL167.68: SPLICE ANGLE RO#891810-SWA REPLACEMENT ANGLE RSDR SWAA2022120169150Fitting · crackedCRACK TIE FITTING, BS 277, S10R. REPLACED WITH A NEW TIE FITTING IAW SRM 51-10-02, SRM 51-40-02, AND DRAWING 141A1110, SHEET 18, REV-.SDR SWAA2022120169422Stringer Clip · crackedCRACKED STRINGER CLIP, BS 706, S4L. REMOVED THE STRINGER CLIP IAW SRM 51-40-02-0G-0. INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 144A1125.SDR SWAA2022120968650Fitting · crackedCRACKED FITTING, BS 727B CEILING AREA LBL 46 IN THE AFT CARGO BAY. REPLACED THE FITTING IAW SRM 51-10-02, SRM 51-40-02, AND DRAWING 146A5502, SHEET 9, REV A.SDR SWAA2022111668454Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE AT RBL 40 STA 663 (WL 167) / [01] VERIFIED ITEM 1 OF STEP 1;[02] RECEIVED -1 REPLACEMENT ANGLE 2024-T3 .063' AND -2 SPLICE ANGLE 2024-T3 .071' FROM BACKSHOP ON W/O#'S 44275-6000-0001 AND 44275-6000-0002 IAW SRM 57-10-10-2R-5 TSDR SWAA2022111668451Attach Angle · crackedCRACK FOUND ON LOWER ATTACH ANGLE AT RBL 45 STA 663 (WL 193) / [01] VERIFIED ITEM 1 OF STEP 1;[02] VERIFIED ITEM 1 OF STEP 2;[03] VERIFIED STEP 6 AND 7;[04] UPDATED MEASUREMENTS;[05] UPDATED MEASUREMENTS;[06] LEAK CHECKED REPAIR AREA NO LEAK DETECTED I.A.W MM SDR SWIA202266999Bracket · crackedLEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE AFT BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. NO LEAKS NOTEDSDR SWIA202266998Bracket · crackedLEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE FORWARD BRACKET IS CRACKED. REMOVED THE LT MAIN LANDING GEAR WHEEL WELL, HYDRAULIC FUSE FWD BRACKET IAW SRM 51-42-06, INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. LEAK CHECK GOODSDR SWAA2022120167964Attach Angle · crackedCRACKED CARGO BAY FRAME TO BAFFLE ATTACH ANGLE, LBL 24, BS 400+1. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0, AND DWG 143A7505. INSTALLED THE NEW ATTACH ANGLE IAW SRM 51-40-02.SDR AALA202211148478Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE STRINGER CLIP LOCATED AT BS 500G AND S26L. REPLACED STRINGER CLIP PER SRM 51-40-02-0G,SDR R61A2022111700711Support · corrodedCORROSION FOUND ON AFT PAX DOOR SURROUND LOWER CENTER SEAL REST. R&R'ED AFT PAX SURROUND LOWER CENTER SEAL REST IAW SRM 51-41-01SDR AALA202301199494Fitting · crackedAIRCRAFT WAS GROUNDED: DURING UT INSPECTION OF LEFT STA 663.75 FAIL SAFE STRAP FOUND A CRACK INDICATION AT THE UPPER AFT FASTENER. REMOVED AND REPLACED LEFT PICKLE FORK FITTING DUE TO CRACK.SDR AALA202211146623Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD SIDE ATTACH STRINGER CLIP LOCATED AT BS 500G AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-OG AND SRM 53-30-53.SDR AALA202211141112Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26L. REPLACED STRINGER CLIP PER SRM 53-30-53 AND AND 51-40-02-0G.SDR AALA202211154888Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-0G.SDR AALA202211145678Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-0G.SDR AALA202211140702Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE LOCATED AT BS 500H AND RBL 26. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.SDR ASAA2022102940958Fitting · gougedMAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING UPPER SURFACE GOUGED AT FR70 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING AT FR70 IAW A320 SRM 51-72-11-911-002SDR COEA2022120809807Stringer Clip · corrodedDURING HEAVY CHECK, FRAME 35 STRINGER 10R CLIP HAS LEVEL 2 CORROSION. REPLACED THE STRINGER CLIP IAW SRM 51-25-01 AND 51-21-28.SDR COEA2022120707807Stringer Clip · corrodedDURING HEAVY CHECK, FRAME 28D, STRINGER 21L CLIP HAD LEVEL 2 CORROSION. REPLACED THE STRINGER CLIP WITH NEW IAW SRM 51-25-01.SDR ASAA2022102741030Fitting · corrodedR1 DOOR CUTOUT HAS 3EA AREAS OF CORROSION UNDER LWR SCUFF PLATE GROUNDED - YES. REMOVED AND REPLACED CORRODED FITTING IAW A320 SRM 51-42-11 REV 143 01 NOV 2022SDR A6WA202210278365Support Bracket · crackedRH SUPPORT BRACKETS 3EA. FOR BRAKE XDUCERS AND VOLUMETRIC FUSES ARE CRACKES ****AIRCRAFT REMOVED FROM SERVICE**** INSTALLED NEW R/H WHEEL WELL BRAKE XDUCER BRACKETS P/N 601R75262-155 AND 601R75262-157 AND RH TRANSDUCER BRACKETSDR A6WA202210278362Support Bracket · crackedSUPPORT BRACKET IN L/H WHEEL WELL FOR BRAKE XDUCER IS CRACKED ****AIRCRAFT REMOVED FROM SERVICE**** REPLACE BRACKETSDR UIEA2022092101015Fitting · not reportedFUSELAGE STA 2598 BULKHEAD FRAME FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A770 2&&3(<P>FRAME FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A770 2&3 AND EXISTING FASTENERS INSTALLED (6EA) AS PER RI NO: RI-53-80-15889 REV A</P>)SDR UIEA2022092101018Lug · crackedFUSELAGE - CENTER SECTION - BS1000 FRONT SPAR INTERCOSTAL LUG FITTING FOUND CRACK AT RBL 11.33 LOCATION.(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 PART 7 STEP 3</P>)SDR UIEA2022092101019Lug · crackedFUSELAGE - CENTER SECTION - BS1000 FRONT SPAR INTERCOSTAL LUG FITTING FOUND CRACK AT RBL 11.33 LOCATION.(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 PART 7 STEP 3</P>)SDR SWAA2022111464774Nut Plate · corrodedCORROSION ON NUTPLATE STRAP BS 847 RBL 18 WL 156. REMOVED NUT PLATE STRAP IAW SRM 51-40-02-0G-0. LOCATED AND DRILL A NEW NUT PLATE STRAP IAW SRM 51-40-05-0G-0 AND DWG 146A8340 REV A. INSTALLED THE NEW NUT PLATE STRAP IAW SRM 51-40-02-0G-0, AND DWG 146A0SDR AALA202211048681Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD ATTACH ANGLE HAS CRACKS LOCATED AT STA 500G AND STR 26L. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.SDR DALA2022102806988Fitting · corrodedSHIP 197 FOUND CORROSION AT BODY STATION 955 REF TO CPCP TASK W/C 53-524- 00. CORRECTIVE ACTION: LH W/W AT STA 955 SIDE FRAME FITTING AND REAR SPAR WEB CORROSION REPAIRED AS PER PRI: 602469-14. (2468608)SDR 2022FA0000645Stringer Clip · crackedCRACK ON STRINGER CLIP BS277 S15LSDR A6WA202210258416Anchor Fitting · corrodedPASSENGER DOOR COUNTERBALANCE TWO ANCHOR FITTINGS, BS 310 - 349, LBL 44 HAVE SEVERE CORROSION OVER ENTIRE SURFACE OF FITTINGS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ANCHOR FITTINGS, IAW SRM 51-40-11 REV 39 AND AMM 52-11-17 REV 66.SDR SWAA2022111564427Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE BS 380-400, RBL 9, WL 208. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0 & DWG 143A5400. INSTALLED THE NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0 & DWG 143ASDR SWAA2022111564428Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE BS 380-400, LBL 13, WL 208. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0, & DWG 143A5400. INSTALLED THE NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0 & DWG 143ASDR SWAA2022111564422Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE BS 380-400, LBL 51, WL 208. HFEC INSPECTED CRACK IAW NDTM PT6 51-00-00, PROCEDURE 23. CRACK LENGTH IS 0.700 INCH. INTERCOSTAL ATTACH ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1, FIG 102 (A). REMOVED THE ASDR FDEA202210242646Fitting · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER HOLE 165 FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER HOLE 165
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