JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous 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 = '5320' 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 = '5320' 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 SWAA2024062890217Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500C-500D. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION SDR SWAA2024062890218Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500B-500C. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITIONSDR SWAA2024062890219Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500A-500B<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. STEP 1 FWD CARGO R/H TSDR SWAA2024062890223Angle · corrodedFWD CARGO COMPT RH SHORT TRANSITION ANGLE AFT OF DOOR CORRODED STA 492-500A<[01] REMOVED CORROSION AT FWD CARGO R/H SHIELD SIDEPLATE ASSY STA 492 TO STA 500A PER SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS OUT OF LIMITS PER SRM 53-30-15-1A-1 FIG.103; DSDR SWAA2024062790213Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500H-500I<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E.;[02] RESOLVED ON FAULT TSDR SWAA2024062790212Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500B-500C<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .008?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790206Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500C-500D<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .004?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790211Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .0010?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIOSDR SWAA2024062790210Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500E-500F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .005?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790209Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500H-500I. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .008. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM BS 480SDR SWAA2024062790208Angle · corrodedFWD CARGO COMPT 500I BULKHEAD ANGLE AT FLOOR CORRODED. REMOVED CORROSION AT FWD CARGO COMPT. AFT BULKHEAD LOWER RAIL ANGLE BS 500I, RBL 22 TO LBL 22 IAW SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS, OUT OF LIMITS IAW SRM 53-30-08-1A-1 FIG. 103, DETAIL SDR SWAA2024062790485Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS847 LBL21 WL157. MARKED<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS 727 TO BS 847 LBL 21 IAW SRM 51-40-02 AND DWG 146A7500 ID: 0081;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED SDR SWAA2024062790468Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157. MARKED<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157 I.A.W SRM 51-10-02; SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED RII CORRECTIVE ACTION ITESDR SWAA2024062790487Web · corrodedCORROSION ON INTERCOSTAL AT ACB BS770 RBL6 WL151.<[01] REMOVED AND REPLACED INTERCOSTAL WEB LOCATED AT ACB BETWEEN BS. 767 - BS 787 RBL 6 WL 151 IAW B-737-700 SRM 51-10-02 AND SRM 51-40-02 DWG#146A8130 REV: B;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MESDR FDEA202405270866Strap · crackedFUSELAGE STRUCTURAL S-33R WEB FOUND STRAP CRACK AT FR85 PLUS 10" AREA. REPLACED THE CRACK STRAP WITH NEW PART. LOCATE AT FUSELAGE FR85 PLUS 10" S-33R WEB. I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE,7B~PAGE,23 AND 51-40-21- 001, PARASDR FDEA202405270814Plate · crackedFWD CARGO COMP'T UNDER FLOOR AREA LH SIDE PLATE SHEAR CRACK AT S-43L~S-44L,FR38.1- FR38.2 POSITION INSTALLED THE NEW PLATE WITH FASTENERS AT FWD CARGO FLOOR AREA FR38.1~38.2 S- 43L~44L I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001,PARA.6-7, PAGE.7B-SDR FDEA202405270813Plate · crackedFWD CARGO COMP'T UNDER FLOOR AREA RH SIDE PLATE SHEAR CRACK AT S-43R~S-44R,FR36- FR37 POSITION INSTALLED THE NEW PLATE WITH FASTENERS AT FWD CARGO FLOOR AREA FR36~37 S-43R~44R I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6-7, PAGE.7B-50, THESDR AALA202406047314Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL FROM STA 927 TO STA 933, S27L. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR IXXA2024060201Floor Support · crackedFLOOR SUPPORT BRACKET IS CRACKED IN HALF, AT STA.1562, LBL79, JUST BELOW THE CABIN FLOOR, CLOSE TO STR 20LSDR AALA202405313740Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 958, LBL 49. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202405311694Intercostal · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES IN INTERCOSTAL FROM STA 986 TO STA 1006, LBL 32. REPLACED INTERCOSTAL PER AARD 51-00-05.SDR AALA202405312131Door Sill · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN L1 DOOR SILL INNER CHORD AT STA 312, LBL 55. REPLACED INNER CHORD PER AARD 51-00-05-1.SDR UIEA2024052800455Channel · crackedFOUND M/D R/H TENSION TIE AFT CHANNEL CRACK AT STA 800.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40389 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800456Channel · crackedFOUND M/D L/H TENSION TIE AFT CHANNEL CRACK AT STA 760.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40388 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052300410Structure · corrodedFX - LH AIRCON BAY STA 1220 - 1240 CENTER TANK LWR SURFACE O/B CHORD CRACK(<P>LH AIR COND BAY STA 1220-1240 CENTER TANK LWR SURFACE O/B CHORD REPAIR AS PER RI NO : RI-57-00-16879 REV A. NO FURTHER DEFECTS NOTED</P>)SDR SWIA2024F00644Floor Support · corrodedPASSENGER DOOR BELOW FLOOR STRUCTURE BETWEEN FS333.00 AND FS349.00 AT STGR21L CORRODED AS MARKED (C-CHECK RO 8/4/2024) REPLACED CORRODED BACKUP SILL AT STR 21L BETWEEN FS333 - FS349 WITH NEW PN SH670-31823-1 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SDR SWAA2024071690031Tie Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-345554<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-; DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUASDR SWAA2024071690247Support Angle · crackedCRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-345574<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02-SDR HNAA2024070800531Floor Support · corrodedE040363 CENTER FUSELAGE III INTERNAL, LH FLOOR GUSSET CORRODED BETWEEN FR39/45. REMOVED AND REPLACED CENTER FUSELAGE III INTERNAL, LH FLOOR GUSSET IAW EMB 145 SRM 51-40-02SDR SWAA2024070190233Support Bracket · crackedCRACK SUPPORT BRACKET OF THE PNEUMATIC DUCT BS 540 AND LBL 6 AIR CONDITIONING BAY 2024-341156<[01] REPLACED SUPPORT BRACKET OF THE PNEUMATIC DUCT BS 540 AND LBL 6 AIR CONDITIONING BAY IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9;[02] REPLACED SUPPORT BRACKET SDR SWAA2024070190181Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727H-727I LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727H-727I TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] REMOVED DAMAGED SECTION OF L/H SIDE PLATE FROM STA.727G+12-SDR SWAA2024070190192Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.727J-747; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND SDR SWAA2024070190193Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.747-767; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOSDR SWAA2024062890198Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.767-787; RBL 21-RBL 22 HAS SURFACE CORROSION. MRKD<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] SHIELD ASSDR SWAA2024062889980Floor Support · corrodedAFT CABIN WET AREA FLOOR STRUCTURE INTERCOSTAL AT STA 947+4'; AFT OF RIGHT HAND LAV MOUNTS HAS CORROSION AROUND FASTENER HOLE. (MARKED)<[01] BLENDED OUT CORROSION AT AFT CABIN FLOOR STRUCTURE SUPPORT ANGLE STA 947+4?; RBL 28 PER SRM 51-10-02. MEASURED REMAININSDR SWAA2024062890180Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727G-727H LBL 21-22 WL 156. REMOVED CORROSION FROM STA.727G-727G+12 PER SRM 51-10-02. REMOVED .002? OF MATERIAL THICKNESS; REMAINING THICKNESS IS .038?.FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-0SDR SWAA2024062890182Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727I-727J LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 727I-727J TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 ASDR SWAA2024062890183Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727J-747 LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727J-747 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53SDR SWAA2024062890185Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 747-767 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 747-767 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2. L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND A SESDR SWAA2024062890199Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 767-787 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 767-787 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND ASDR SWAA2024062890204Shield · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURES SHIELD BETWEEN BS 767 & 767+25, RBL 21-22 HAS SURFACE CORROSION. REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD IS OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED SHIELD ASSY IAW SRM 51-40-02.SDR SWAA2024062790197Support Bracket · crackedAFT CARGO COMPARTMENT WASTE TANK ACCESS PANEL STANCHION SUPPORT BRACKET AT STA 867 LBL 15 CRACKED. REMOVED AND REPLACED AFT CARGO BLKHD STANCHION SUPPORT BRACKET AT STA. 867 LBL 15 IAW SRM 51-40-02.SDR AALA202405313856Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CABIN INTERCOSTAL LOCATED FROM STA 328 TO STA 355, LBL 47. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR IPXA2024052960336Angle · crackedCRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEW COMPLETEDSDR IPXA2024052960326Angle · crackedCRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR SWIA20240808525Intercostal · chafedIN THE AEB, INTERCOSTAL AT STGR9R BETWEEN FS1144.00 - FS1162.00 IS CHAFFED (C-CHECK RO 8/4/2024) REPLACED INTERCOSTAL PN: AF670-36540-002 BETWEEN FS1144 AND FS1162 AT STGR 9R PER CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG # MM670-SDR SWAA2024071689687Scuff Plate · crackedCRACK ON CENTER SCUFF PLATE AT FWD SERVICE DOOR. 2024-345515<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23272782; DUE DATE: 06-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1859843; DUE DATE 24-JUL-24 WAS USED ON STEP 4;[03] REPAIRED CENTER SCUFF PLATE ASDR SWAA2024071690021Strap · corrodedCORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA 2024-345534<[01] REPLACED STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING# 147A5730 SHEET 23 RSDR SWAA2024071690022Strap · corrodedCORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA 2024-345535<[01] REPLACED STRAP AND FASTENERS LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 147A5600 SDR AALA202407118757Plate · damagedAIRCRAFT IN BASE MAINTENANCE: AFT RIGHT HAND PASSENGER / CREW DOOR CUT OUT AFT FLOOR MOUNTED GIRT BAR FITING PLATE ASSEMBLY DAMAGED BETWEEN FR 66 AND FR 68 AT S23R. REPLACED PLATE PER SRM 51-42-11.
Back to JASC 5320