JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 SWAA2023101905296Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 LBL 30 TO LBL 45. MARKED LOCATION.<[01] HFEC INSPECTED CUT OUT EDGES IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 500D ID: IS000680 CAL DUE: 05/2024;[02SDR SWAA2023101905297Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 RBL 39 TO RBL 60. MARKED LOCATION.<[01] UPDATED MEASUREMENT TABLE;[02] STEP 11 PARTIAL UPDATE;[03] CRACK REPAIRED ON HORIZONTAL PRESSURE DECK WEB FROM BS663 - BS674; RBL31 - RBL63; WL202 WITH 1EA -SDR AALA202311081984Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND FRAME AT #7 DOOR STOP FITTING FASTENER HOLES AT FR 16. REPLACED FRAME PER EA 347843.SDR SWAA2023110105088Crease Beam · corrodedCORROSION CREASE BEAM LOCATED BS 639 LBL 64 WL 208.1 CENTER SECTION 2023-614905<[01] EQUIPMENT P/N 45MG; S/N 221859911; DUE DATE 07-NOV-23 AND EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WERE USED.;[02] REPLACED CREASE BEAM LOCATED BETWEEN BS 6SDR SWAA2023110105091Pressure Deck · crackedCRACK INDICATION ON WEB PRESSURE DECK RBL 40 PLUS 2 INCH BS 663; LENGTH OF CRACK 0.275 INCH APPROX; AT PASSENGER CABIN 2023-614907<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON WEB PRESDR DALA2023092807974Unknown · unknownCRACK ON BEAM 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00152: BEAM NBR 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2990273)SDR DALA2023121410244Unknown · unknown(LOG 2988080) DURING R3 WINDOW INSPECTION, CORROSION WAS FOUND ON R3 WINDOW FRAME EXTERIOR POST AND SILL. C/W ER/A 611949-14 REV ORIGINAL.SDR SWAA2023101606071Web · incorrectREJECTION: FOUND -1 REPLACEMENT WEB FOR FLIGHT DECK REPAIR (REF. TTG8Q00NHXHV STEP 10) IMPROPER FIT; NEED TO RE-FABRICATE WEB<[01] FABRICATED; TREATED; AND PRIMED RE-FABRICATED (-1 REPLACEMENT WEB) AS PER EA M-21-153-00734 [TTG8Q00NHXHV] STEP 10;STEP 13 AND 14SDR DALA2023100208048Unknown · unknown(LOG 2988156) E&E COMPARTMENT DOOR CUT-OUT DAMAGE AT STA 328 RBL 12. INSTALLED REPLACEMENT WEB AT STA 328+10 RBL 12 IAW B737-900 SRM 51-40-02-0G & BOEING DRAWING # 141A8512 LOT# 5047744SDR YENA2023092901157Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON COCKPIT FLOOR STRUCTURE CROSS BEAM ON FRAME 11 BTW -Y350 TO Y350; COCKPIT FLOOR STRUCTURE CROSS BEAM ON FRAME 11 BTW -Y350 TO Y350 WAS REPAIRED PER EMB 190 SRM 53-00-10 REPAIR 54 REF TOMX W.O. 239JB/ 2301 / E190 / B8 CHECSDR YENA2023092801133Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / LH TRACK FLOOR / BTW FR 19 & Y= 273.0 / DOUBLER CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR YENA2023092801132Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / COCKPIT FLOOR STRUCTURE / DOUBLERS / AT APROX X=3301.3 IN Y=373 & Y=-373 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR CALA2023092702883Deck Plate · corrodedMAIN CABIN STA 992.8, RIGHT HAND DECK WEB PLATE HAS AREAS OF CORROSION. REMOVED .010" CORRODED MATERIAL FROM ORIGINAL .020" THICKNESS. R EMAINING .010" MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-01-1 AND DWG 147A5712 REV-. REMOVE D AND REPSDR I5EA2023092600017Unknown · unknownFOUND CORROSION AT STA 992 AT WL 208 ON FWD AND I/B FACE OF THE DOOR FRAME. REMOVED CORRODED SECTION AND INSTALLED REPAIR ANGLE IAW B737-300 SRM 51-40-01 AND SRM 51-70-11.SDR AALA202309296248Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOORBOARD IS DELAMINATED AT STA 272, SEAT 1A. ACCOMPLISHED PERMANENT REPAIR ON CABIN FLOORBOARD. PER SRM B787-A-53-00-50-02A-663A-A AND SRM B787-A-53-00-50-01-030A-A.SDR SIMA20230925002Unknown · unknownAFTER TAKE OFF VIBRATION COMING FROM FLOOR /NOSE AREA BOTH CA/FO FELT IT,ALONG WITH NOISE (VIBE TYPE/PROP) COMING FROM THE NOSE /FIRE WALL-FRONT AREA,ENTIRE FLIGHT-C/A-REFERANCE LOGPAGE 4982952-1 FOUND BOTH RAM AIR SCOUP DOOR HINGES WORN, DEFERRED PER ERS-EJ-2SDR EE4Y2023092518462Frame · crackedDURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR LH SIDE FR68 DOORSTOP FITTING # 1 LOWER I/B HOLE HAS BEEN FOUND WITH CRACK INDICATION. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COSDR FDEA202309251644Crossbeam · crackedMDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR31, BTW -Y450 - -Y953 REPAIRED THE CRACK ON THE MDCC FLOOR CROSSBEAM FWD STIFFENER AT FR31, BTW -Y450 - - Y953 PER A300-600F SRM53-10-15-201 PARA.15 & EA:6-5310-T0376313 P1. THE REPAIR IS CAT A REPAIR, MAJOR RESDR AALA202401046631Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA LOWER INBOARD RADIUS AT FR 2 AND Y0. REPAIRED FRAME CENTER POST PER EA 348296.SDR AALA202401042645Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA LOWER INBOARD RADIUS AT FR 2 AND Y0. REPAIRED FRAME CENTER POST PER EA 348296.SDR AALA202312203660Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA EA 348296.SDR AALA202312209894Fitting · noneAIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING PER EA 348296 THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED. MAINTENANCE REPLACED THE RIGHT HAND CONTINUITY SDR AALA202311164566Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST LOWER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 348297.SDR AALA202311166058Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 348297.SDR SWAA2023100603955Panel · delaminatedA225-001 FUSELAGE195 AR AFT EDGE CENTER HAS DELAMINATION.<[01] UT IAW B737 NDT PART 4; 51-00-02. NO DEFECTS OUTSIDE OF VISIBLE DAMAGE. TOOL#40084; DUE 01AUG24;[02] EVALUATED PANEL 195AR AND FOUND DELAMINATION ON EDGE BAND. FOUND TO BE REPAIRABLE. IAW B 737-700SDR AWKA202406170002Structure · corrodedFOUND MULTIPLE SPOTS OF PITTING CORROSION ON RH SIDE OF DROP ISLE IN FRONT OF GALLEY BELLOW FLOOR BOARDS. *** ACCOMPLISHED FIELD REPAIR - CORROSION, FUSELAGE, LOWER SKINS AND STRINGERS, DROP AISLE, FS 166 TO FS 425 (FR-750-0220-11709 REV. B).SDR SWAA2023100603531Vapor Barrier · crackedCUSTOMER REQUEST-CRACK ON VAPOR BARRIER LOCATED BS663.75 BTW RBL45.64 TO RBL 54.21 AND WL166.5 WING CENTER SECTION AT MAIN WHEEL WELL COMPARTMENT 2023-568956<[01] REPAIRED VAPOR BARRIER LOCATED BS663.75 BTW RBL45.64 TO RBL 54.21 AND WL166.5 WING CENTER SECTIONSDR SWAA2023100603530Vapor Barrier · crackedCRACK ON VAPOR BARRIER LOCATED BS663.75 BTW RBL45.64 TO RBL 54.21 AND WL166.5 WING CENTER SECTION AT MAIN WHEEL WELL COMPARTMENT 2023-568955<[01] FAULT RESOLVED ON OTHER FAULT:TTG8Q00NLSWY;[02] FAULT RESOLVED ON OTHER FAULT:TTG8Q00NLSWYSDR AALA202309278175Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 7.SDR DALA2023092507861Unknown · unknownCORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00148: CORROSION LEVEL 2. PAN JAMB LOWER WAS REPLACED PER B-717-200 SRM 53-20-15 PROCEDURE 7 REPAIR 7, 51-41-02-0G PAR 4 B, AND 51-41-05-0G PARSDR JR2R20230923908Beam · corrodedFWD CARGO DOOR CUT OUT THRESHOLD BEAM CORRODEDSDR AALA202311284548Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND CENTER POST FRAMING UPPER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.SDR AALA202311286561Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND CENTER POST FRAMING UPPER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.SDR AALA202311285396Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND CENTER POST FRAMING LOWER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.SDR AALA202311280338Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND CENTER POST FRAMING LOWER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.SDR P5CA2023082400078Unknown · unknownFLIGHT COMPARTMENT L1 WINDOW STRUCTURE UPPER CHORD CORNER CHORD AT STA 288 BL 1.0 FOUND SLOT(<P>SLOT WAS CONFIRMED A PRODUCTION GAP BETWEEN THE CHORD AND THE CENTER WINDSHIELD POST AS PER ATLAS AIR EO #4853A118 REV 3 </P>)SDR DALA2023092207808Unknown · unknownSHIP 3117 CORROSION INTERNAL STRUCTURE LOC AT FRAME 26 AT LEVEL STRINGER 40R. CORRECTIVE ACTION: REPLACED FISHPLATE INTERNAL STRUCTURE LOC AT FRAME 26 AT LEVEL STRINGER 40R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11. (2980617)SDR CALA2023092202859Window Frame · crackedFLIGHT DECK LOWER NODE R/H AND L/H I/B HOLES HAVE CRACK INDICATIONS. ACCOMPLISHED INTERIM REPAIR OF THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS PER ECRA 5311-03068 REV- PT1, QC INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03068. PER PART 1 STEP 3-SDR DALA2023092107763Unknown · unknownSHIP 3323 LIGHTNING DAMAGE BY WINDOW FRAM AFT OF FR 22 & DAMAGE BY WINDOW AFT OF FR 24. CORRECTIVE ACTION: REF ER/A 612292-14. (2979714)SDR REXA2024100100761Fitting · crackedL/H FIGHT COMPARTMENT SIDE WINDSHIELD SUPPORT POST AFT LOWER FITTING IS CRACKED. LOCATED AND DRILLED NEW AFT LOWER FITTING PART #GC212-0045-3 FOR L/H FLIGHT COMPARTMENT SIDE WINDOW SUPPORT POST IAW CRJ 900 SRM 51-40-11-001-001-A01.INSTALLED LH FLIGHT COMPARTMESDR CALA2023110603297Window Frame · corroded(B737-06-3-0035) COCKPIT R/H #3 WINDOW FRAME HAS CORROSION ALE WO 3999. REPAIERD COCKPIT RH #3 WINDOW FRAME REF EO 5610-23032 REV A, REV B AND ECRA 5610-01531. DATA WAS TRANSCRIBED FROM PAPER DOC AERSSDR SWAA2023103002195Vapor Barrier · cracked(CUSTOMER REQUEST) CRACKS ON VAPOR BARRIER RH SIDE APROX. LOCATED BETWEEN RBL 31 TO RBL 51 2023-593974 AND WL155<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189527; DUE DATE: 26-DEC-23.;[02] TOOL USED; HOT BONDER PN: HCS9200B-AV; SN: 18196119; DUE DATE: 2SDR REXA2022101200860Fitting · crackedR/H FIGHT COMPARTMENT SIDE WINDSHIELD SUPPORT POST AFT LOWER FITTING IS CRACKED. REMOVED FITTING P/N:GC212-0045-4 IAW CRJ900 SRM 51-42-21-001-001-A01. REQUIRES REPLACE. INSTALLED NEW FITTING P/N:GC212-0045-4 IAW CRJ900 SRM 51-42-21-001-001-A01. AND COMPLETED FSDR R61A2023100700552Seal Rest · corrodedFWD CARGO DOOR CUTOUT LOWER FWD SEAL REST AT FR24, STR 26R CORRODED. R&R IAW SRM 20-10-01.SDR DALA2023092607909Unknown · unknownERA 612058-14 SECTION I ISSUED FOR CORROSION REPAIR TO AFT WASTE SERVICE INTERNAL DOUBLER. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II EVERY 1000 FH FROM SECTION I UNTIL SECTION III ACCOMPLISHMENT. SECTION III IS REQUIRED PRIOR TO 10000 FH FROM SECTION I.SDR JJBA20230921043Unknown · unknownCORROSION FOUND ON MIDDLE ALLEY CROSSBEAM AT FR 20 ON FLOOR STRUCTURE. CF1 MIDDLE ALLEY AT FR 20 ON FLOOR STRUCTURE AREA, CROSSBEAM REMOVED FOR INVESTIGATION. CF1 AT FR 20 ON FLOOR STRUCTURE AREA, CROSSBEAM BLENDED OUT OF LIMITS. ALTERNATE MATERIAL NEEDED FOR SDR SWI2023F00470Unknown · corrodedCORROSION FOUND ON R/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) CORROSION AT R/H CROSSBEAM AT FS 280.0 IS OUT OF LIMITS. REMOVED AND INSTALLED NEW R/H CROSSBEAM AT FS 280.0 REF DWG CC670-34010 REV K, CRJ 700 SRM 51-42-13-001-001-A01, CRJ700 SDR SWIA202311070918Unknown · corrodedCORROSION FOUND ON L/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) REMOVED AND REPLACED LH FLOOR CROSS BEAM WITH NEW DUE TO OUT OF LIMIT CORROSION REF. CRJ 700 SRM 51-42-06-001-001-A01,CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-00SDR SWAA2023102601883Tie Down · corrodedAFT CARGO BAY TIE DOWN HAS CORROSION AT BS 787+3; LBL 17; WL 162<[01] UPDATED STEP 1;[02] UPDATED STEP 2 AND MEASUREMENT TABLE.;[03] UPDATED STEP 3;[04] EDITED MEASUREMENT TABLE;[05] REMOVED CORROSION FROM ACB TIE DOWN AT BS 787 + 3'; LBL 17; WL 162; IAW SRM 5SDR CALA2023092002822Window Frame · damagedFRONT WINDSHIELD FRAME AND CONTINUITY FITTING HAVE REJECTABLE INDICATIONS "ACCOMPLISH INITIAL INSPS OF THE FRONT WINDSHIELD FRAMES OF ECRA 5311-03068 ON OR BEFORE THE AC REACHES 65681 TOTAL AND CONTINUITY FITTINGS PER PART 2 OFTHE LATEST REVISION AIRCRAFT FLIG
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