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 SWAA2023040511133Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS867 AND BTW LBL8.1 AND LBL12.5 AT AFT CARGO COMPARTMENT 2023-142895<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW LBL8.1 AND LBL12.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A8102 REV: ?.SDR SWAA2023040510719Angle · crackedCRACK ON SUPPORT ANGLE ON CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-142814<[01] REPLACED SUPPORT ANGLE AND FASTENERS ON CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN; IAW BOEING 737-700 SRM 51-40-02; BOEING SDR ASAA2023022342472Cargo Track · crackedFWD PIT R/H CARGO TRACK IS CRACKED AT STA 460. GROUNDED - YES. REPAIRED FWD PIT /RH CARGO TRACK AT STA 460 IAW B737-700 SRM 53-00-53-2R-3.SDR ASAA2023022342463Web · corrodedFWD PIT CARGO DOOR SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT CARGO DOOR SILL WEB IAW B737-700 SRM 51-40-02-0G-0.W= 1" O= .045" R= .038" L= 3" D= .007".SDR SWAA2023040509428Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION 2023-142550<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] RSDR SWAA2023040509429Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 CENTER SECTION 2023-142553<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[SDR SWAA2023040509430Angle · crackedCRACK SUPPORT ANGLE LOCATED BS 695 BL 0 RH SIDE CENTER SECTION 2023-142554<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 695 BL 0 RH SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: A. SEE INDIVIDUAL SISDR FDEA202302190302Web · crackedTAILCONE - LH PATIO DOOR AFT EDGE ABOUT 15" UP FROM PATIO DOOR HING SIDE IS BENT AND CRACKED. REPAIRED LH PATIO DOOR AFT EDGE REF SRM 52-00-00-2R FIG 204SDR LR7A2023020803270Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FRAME UPPER ATTACH FITTING CRACKED AT FS946, LBL61, WL260. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000897086. / PSE# 53-50-09, AD 2012-06-09SDR CALA2023022000479Stop · crackedDURING ROTO INSP ON LH FR68 DOOR STOP #1. CRACK INDICATION NOTED IN LWR I/B HOLE. REPAIR BEFORE NEXT FLIGHT, REPAIRED LH FR68 DOOR STOP #1 LOWER I/B HOLE PER SRM 53-41-12-30 0-011. EMP: V934143 WC: 45467 STA: ST ENG BFMSDR ASAA2023021342015Plate · corrodedWHILE WORKING CUSTOMER CARD P092915 FOUND ADDITIONAL CORROSION ON THE RH AFT BULKHEAD CANTED SUPPORT AT FR33+16, Y+765, Z-1912 GROUNDED - YES. REMOVED THE DAMAGED PLATE IN FCB R/H AFT BULKHEAD CANTED AT FR33+16, Y+765, Z-1912 IAW A320 SRM 51-52-11. LOCATED, DRSDR ASAA2023021342014Plate · corrodedWHILE WORKING CUSTOMER CARD P092915 FOUND ADDITIONAL CORROSION ON THE LH AFT BULKHEAD CANTED SUPPORT AT FR33+16, Y+765, Z-1912 GROUNDED - YES. REMOVED THE DAMAGED PLATE IN FCB L/H AFT BULKHEAD CANTED AT FR33+16, Y+765, Z-1912 IAW A320 SRM 51-52-11. LOCATED, DRSDR SWAA2023032001756Vapor Barrier · crackedRT BS 663 VAPOR BARRIER CRACK AT RBL 48<[01] PREPARED DAMAGED AREA FOR REPAIR; AND PERFORMED DRY OUT; FOUND NO WATER; AS PER B737 SRM 51-70-04-2R-10.;[02] VERIFIED STEP 1; OK TO INSTALL REPAIR.;[03] APPLIED REPAIR AT R\H ON VAPOR BARRIER PER B737SRM 51-70-04-2SDR SWAA2023021601493Fork · crackedFUSELAGE BS 663 PICKLE FORK HAS EVIDENCE OF CRACK AT #6 FASTENER ABOVE S18R.<[01] PERFORMED HFEC TO PICKLE FORK RIGHT LEG ABOVE S18R. #6 FASTENER IS VERIFIED TO BE CRACKED TO THE EDGE PER PART 6 51-00-00 PROCEDURE 23.SDR YENA2023021400167None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 3 ZONE 2. THE CRACK DIRECTION IS 12 O'CLOCK. REF AEROMAN NRC 2022-676209; REF: ARM W/O 2022 453/1 N/R 2022-676209 REPAIRED IAW EC NO. A23-034-01 AND EA 53-0635-22, REV 0 (COVER, PART 1 AND SDR YENA2023021400166None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 4 ZONE 2. CRACK DIRECTIONS ARE 12 O'CLOCK AND 8 O'CLOCK. REF AEROMAN NRC# 2022-676210; REF: ARM W/O 2022 453/1 N/R 2022-676210. REPAIRED PER EC NO. A23-034-01 AND EA 53-0635-22. ITEM IS CATSDR YENA2023021400165None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR36 VERTICAL STRG FLOOR BEAM 5 ZONE 2. THE CRACK DIRECTION IS 11 O'CLOCK. REF AEROMAN NRC 2022-676220; REF: W/O 2022 453/1 N/R 2022-676220 REPAIRED PER EC A23-034-01 AND EA 53-0635-22 REV 0 (COVER PART 1 AND PARTSDR SWAA2023021697520Gusset · crackedFWD CARGO COMP. GUSSET TIE CRACKED AT BS 500D AND LBL 25.<[01] REMOVED DAMAGED CLIP AT FWD CARGO STA 500D AND STR 25L AS PER B-700 SRM 51-40-02-0G-0.;[02] RECEIVED NEW CLIP P/N 143A1010-47 AND LOCATED NEW FASTENER HOLES AS PER B-700 SRM 51-40-02-0G-0.;[03] VERSDR SWAA2023030897000Retainer · crackedLH VAPOR BARRIER SEAL RETAINER FOUND CRACKED<[01] RECIEVED; LOCATED AND DRILLED NEW L/H VAPOR BARRIER SEAL RETAINER PN: 111A1512U1 PO:1792296 PER REF SRM 51-40-05-0G-0.;[02] TREATED AND PRIMED NEW HOLES PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03SDR WX0A1900010031734None · noneNRC 2000-0119: 32779-05 AT L2 DOOR SILL PLATE BETWEEN FR 67-68 STRG 23L CORROSION FOUND AROUND FASTENER HOLES. / L2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23LH, SILL BEAM CORROSION REPAIRED AS PER SRM TASK 53-41-14-300-001 REV 143, REPAIR PRINCIPLE 7. REPAISDR WX0A1900010031733None · noneNRC 2000-0115: 32779-02 ON R2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23 RH CORROSION FOUND. / R2 DOOR SILL BEAM BETWEEN FR 67-68 AND STRG 23RH, SILL BEAM CORROSION REPAIRED AS PER SRM TASK 53-41-14-300-001 REV 143, REPAIR PRINCIPLE 7. REPAIR CATEGORY A, NO SDR FDEA202301300263Doubler · noneTAILCONE LH INNER SKIN - APPROX STA.2163 UPPER AREA - SKIN CHAFED. REPAIRED CHAFED AREA REF E.A.# 1-5352-T0372823 '' TAILCONE & PLATFORM - LH INNER DOUBLER WORN - REPAIR''.SDR FDEA202301290177Skin · chafedTAILCONE RH INNER SKIN - APPROX STA.2163 UPPER AREA - WORN/CHAFED. TAILCONE RH INNER SKIN STA Y=2163 - Y=2165, Z=45 - Z=61 STRUCTUAL REPAIR PERFORMED IAW EA#1-5253-TO372704 PART 1 "FUSELAGE -TAILCONE AND PLATFORM- RH INNER DOUBLER WORN- REPAIR"SDR CALA2023013000264Fastener · missingL/H FWD AND AFT OTBD FASTENERS ATTACHING ACTUATOR FITTING TO HIN GE FITTINGS ARE MISSING THEIR TENSION HEADS. L/H OTBD AFT IS MAR KED DOT LH1 AND L/H OTBD FWD IS MARKED LH2 PER HAECO LCQ NON ROU TINE 9296007/28007 REV IR PART 1, PERFORMED INTERIM REPAIR OF SDR SWAA2023030207954Panel · exposedPANEL 192AR OUTER SKIN PREVIOUS REPAIR HAS EXPOSED FIBERS.<[01] IDENTIFIED PANEL 192AR IAW SRM 53-40-70-OI-1 PARA FIGURE 2; ITEM 2; TABLE 2.<BR>FOUND DAMAGE TO BE OUT ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A.(6)<BR>WILL PERFORM REPAIRS IAW SRM 51-70-05-SDR DALA2023012600642Fitting · corrodedSHIP 3122 - CORROSION CENTER FITTING LH SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING LH SIDE AT FWD GALLEY AREA AS PER A319 SRM 51-42-11. (2599499)SDR DALA2023012400556Stringer Clip · crackedDURING INSPECTION FOUND CRACK STRINGER 26R TIE CLIP FR STA. 500L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC. BS 500L AT STRG 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A1223.SDR DALA2023012200461Stringer Clip · bentDURING INSPECTION FOUND BENT STRINGER 24R FR STA. 500J TIE CLIP AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOC. STR24R STA 500J AT FWD CARGO COMPARTMENT AS PER SRM 51-10-02 ITEM 9 AND DWG 143A1260 SHEET 16REV -.SDR FDEA202301180128Skin · crackedCABIN: R3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 - STATION 1315.42 LONGERON 26 RIGHT - LONGERON 27 RIGHT FOUND CRACK. CABIN AT R3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 BETWEEN LONGERON 26 RIGHT TO LONGERON 27 RIGHT, CRACKED SKSDR CALA2023011600129Bracket · crackedDURING FRAME REPAIR PER SRM 53-00-07-2R-8, REPAIR 8 - A/C BRKT LOCATION STA 1540 LT SIDE, A CRACK INDICATION WAS FOUND AT STR 9LT STR TIE I/B FASTENER LOCATION. AT THE STR 8LT STR TIE LOCATION, THE O/B FASTENER LOCATION WAS DRILLED IN ERROR TO .430. THIS LOG SDR IPXA2023012650261Support Fitting · crackedINSPECTION TYPE:C1, AFT CARGO FR54 Y953 SUPPORT FITTING CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.SDR IPXA2023012590258Support Fitting · crackedINSPECTION TYPE:C1, AFT CARGO FRAME 54 Y1959 SUPPORT FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED IAW SRM 51-40-21 AND SRM 51-26-10SDR YENA2023011800050Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 9 OCLOCK, AT FWD G ALLEY AREA (1 EA); REF AEROMAN N/R 2022-662874, REMOVED AND REPLACED INTERCOSTAL FITTING LOC.SDR YENA2023011800049Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 2 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, AT THE FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2022-662873, REMOVED AND REPLACED INTERCOSTAL FITTINGSDR YENA2023011800048Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 3 OCLOCK, AT FWD G ALLEY AREA (1 EA); REF AEROMAN N/R 2022-662872, REMOVED AND REPLACED INTERCOSTAL FITTING LOC SDR SWAA2023020291261Fitting · crackedCRACK ON FITTING LOCATED BS947.5 AND LBL 12.1 AT AFT CARGO COMPARTMENT 2023-37233<[01] REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND LBL 12.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV-D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] RESDR SWAA2023020290499Panel · crackedCRACKED BREAK PANEL STA 540; RBL 1; WL 207.<[01] REMOVED CRACKED BREAK PANEL AT STA 540 RBL1 WL 207 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILL NEW BREAK PANEL AT STA540 BLO-RBL25 PER SRM 51-40-05. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION #2;[04] ADDED TSDR SWAA2023020290498Panel · crackedCRACKED BREAK PANEL STA 540; LBL 1; WL 207.<[01] REMOVED CRACKED BREAK PANEL AY STA 540 WL207 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILL NEW BREAK PANEL AT STA 540 BLO-LBL25 WL 207 PER 51-40-05-0G-0. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION #2;[04] INSTSDR AALA202301181209Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN STRINGER CLIP LOCATED AT BS 500C AND S22R. REPLACED STRINGER CLIP PER SRM 51-40-02 AND DWG 143A1224.SDR DALA2023011000200Fitting · corrodedCORROSION FLOOR STRUCTURE CORNER FRAME 66 AT STRINGER 23LH AT AFT GALLEY AREA. REPLACED CORNER FRAME 66 AT STRINGER 23LH AT AFT GALLEY AREA ASPER A321 SRM 51-72-11 AND SRM 51-42-11 DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM MEASURES OF CORROSION ARE L=3.780 INCHSDR ASAA2023010642521Door Sill · corrodedCORROSION ON R-2 SUB-THRESHOLD SUPPORT BEAM PREVIOUS REPAIR AT FRAME 67+16 TO FRAME 68, -Y 47, FLOOR LEVEL. GROUNDED - YES. FOUND NO ALLOWABLE LIMITS ON CORROSION AT R-2 DOOR SUB-THRESHOLD SUPPORT BEAM PREVIOUS REPAIR. REMOVED AND REPLACED R-2 DOOR SUB-THRESHOSDR SWAA2023021088602Strip · elongatedAFT CARGO R/H FLOORS CAP STRIPS; HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO R/H FLOORS CAP STRIPS; P/ 453A2611-11; -13;-9 AND- 1; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1SDR SWAA2023021088608Strip · elongatedL/H AFT CARGO FLOORS CAP STRIPS WITH HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO.; L/H FLOORS CAP STRIPS; P/N 453A2611-8;-10;-13; AND-2; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1SDR SWIA2023012467164Stringer Clip · crackedCRACK ON FRAME TO STRINGER SHEAR TIE AT FR89R STGR 17R. REMOVED AND REPLACED STRINGER SHEAR TIE AT FR89R STGR 17R REF. EMB SRM 51-40-08.SDR DALA2023011000199Fitting · corrodedCORROSION FLOOR STRUCTURE CORNER FITTING ON FRAME 68 AT STRINGER 23RH AT AFT GALLEY AREA. REPLACED CORNER FITTING ON FRAME 68 AT STRINGER 23RH AT AFT GALLEY AREA AS PER A321 SRM 51-72-11 MEASURE OF CORROSION L= 1.022 IN W=0.665 IN.SDR ASAA2023010542460Door Sill · corrodedCORROSION ON L-2 DOOR SUB-THRESHOLD WEB AT FRAME 66+1-5, +Y 59-63, FLOOR LEVEL. GROUNDED - YES. DUE TO NO CORROSION OR REWORK LIMITS, REMOVED AND REPLACED L-2 DOOR SUB-THRESHOLD WEB (LOWER SILL BEAM) FR 65+ 23"- 68 + 7", STR 23L, LBL 56-65. IAW SRM 53-41-14-28SDR SWAA2023021388683Handle · brokenBROKEN SERVICE DOOR HANDLE AT FWD GALLEY AREA (1 EA) 2023-037669<[01] REPLACED SERVICE DOOR HANDLE AT FWD GALLEY AREA (1 EA) I.A.W. B737-700 AMM 53-41-31-400-802 STEP 3.F.(2) ITEM (C) AND (D).;[02] REPLACED SERVICE DOOR HANDLE AT FWD GALLEY AREA (1 EA) I.A.W. SDR SWAA2023020788652Fitting · corrodedCORROSION ON SUPPORT FITTING AT FWD WET AREA BS312 LBL55.<[01] NO FOUND ALLOWABLE DAMAGE FOR SUPPORT FITTING AT FWD WET AREA BS312 LBL55 WL208 IAW SRM 53-10-15-1A-1 PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9.C;[02] VERIFIED CORRECTIVE ACTION #SDR LR7A2023010403252Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER WING LOWER FORWARD CORNER FITTING CORRODED AT FS517, CWS220L, WL270. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR SWAA2023013190707Seat Track · wornMAIN CABIN L/H I/B SEAT TRACK EDGES WEAR MARKS @ LBL 24.75 STA 520 MKD DOT<[01] REMOVED WEAR MARKS AT LH I/B SEAT TRACK STA 520 LBL 24.75 AS PER REFERENCE SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] EVALUATED REWORKED AREA. MAXIMUM CLEANUP DEPTH ON THE TOP OF
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