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 SWAA2024061484288Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS1016 LBL5 WL208.<[01] CORROSION REPAIR ON 1016 WEB AT AFT WET AREA BS 1016 LBL5 WL208 COMPLETED IAW EA 24-153-01371.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061484283Channel · corrodedCORROSION ON ASD MOP SILL BS958 - BS992 RBL52 WL208. MARKED<[01] REMOVED AND REPLACED ASD MOP SILL I.A.W SRM 51-10-02-0G-0; SRM 51-40-02 AND DGW#147A8501.;[02] UPDATED PARTS USAGESDR SWAA2024061484290Channel · corrodedCORROSION ON AED MOP SILL BS948 - BS986 LBL52 WL208. MARKED<[01] REMOVED AND REPLACED ASD MOP SILL LBL 52;WL 208 I.A.W SRM 51-40-02; AND DGW#147A8540 REV B..;[02] VERIFIED CORRECTIVE ACTION #1 (NOTE: ONLY THE INNER CHORD OF THE MOP SILL WAS CHANGED)SDR JJBA20240611025Tee Angle · bentCARGO DOOR ENTRANCE, LOWER STRUCTURE, T-PROFILE AT FRAME 67 FOUND BENDED. CARGO DOOR ENTRANCE, LOWER STRUCTURE, T-PROFILE AT FR67 REMOVED AND REPLACEDSDR JJBA20240611020Support · corrodedRH SILL #1 FOUND CORRODED. BLENDED OUT OF LIMITS. REMOVED AND REPLACEDSDR SWAA2024060684067Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT BS 947 RBL 50 WL 208<[01] REMOVED DAMAGE ON BS 947-967 RBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.205' REMAINING THICKNESS IS 0.130' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51-1A-1SDR SWAA2024060683902Floor Support · corrodedCORROSION AROUND FITTING ON FLOOR SUPPORT BS 947+3; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947-967 LBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.205' REMAINING THICKNESS IS 0.105' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SDR ASAA2024050949964Baffle · corrodedL/H BAFFLE 500C TO 500D HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED L/H BAFFLE 500C TO 500D IAW B737-800 SRM 51-40-02-0G-0W =.75" O=.020" R=.015" L=1" D=.005".SDR ASAA2024050949963Floor Support · corrodedAFT WET AREA FLOOR SUPPORT RBL 45 STA 990 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED IAW B737-800 SRM 51-40-02-0G-0W 1 O .050 R .032 L 1 D .018.SDR ASAA2024050949962Floor Support · corrodedAFT WET AREA FLOOR SUPPORT RBL 40 STA 996 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SUPPORT IAW B737-800 SRM 51-40-02-0G-0W 1 O .050 R .028 L 1 D .022.SDR ASAA2024050949941Baffle · corrodedL/H BAFFLE 500C TO 500D HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED L/H BAFFLE 500C TO 500D IAW B737-800 SRM 51-40-02-0G-0SDR ASAA2024050949920Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STA 947 TO 967 RBL 50 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED AND REPLACED PART FLOOR SUPPORT IAW B737-900 SRM 51-40-02W= 2.0" O= .080 R= .040 L= 2.0" D= .040.SDR SWAA2024052984053Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK BETWEEN BS 540; BL;0. - RBL24; WL 208 IAW B-737-800. SRM 51-10-02; SRM 51-40-02 & DWG# 143A0060.;[02] ALL MAINTENANCE ACTION ARE COMPLETE REQUEST FINAL BUY OFF.;[03SDR SWAA2024052984054Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK BETWEEN BS 540; BL;0. - LBL24; WL 208 IAW B-737-800. SRM 51-10-02; SRM 51-40-02 & DWG# 143A0060.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR JJBA20240528061Support · corrodedRH SILL #2 FOUND CORRODED. ON RH SILL #2, CORROSION BLENDED AND FOUND OUT OF LIMIT. RH SIDE BTW FR 25-35, RH SILL #2 REMOVED FOR REPLACEMENT AND INSTALLEDSDR R61A2024052700237Beam · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII FR86-89 LBL10 FOUND TO HAVE CORRODED BEAM. REMOVED AND REPLACED FLOOR BEAM ON CFIII AT FR86-89 AND LBL10 IAW EMB 175 SRM 51-41-01 AND 51-43-03.SDR ASAA2024050949667Floor Support · crackedFWD WET AREA INTERCOSTL CRACKED RBL 40 STA 312 TO 328. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02-0G-0, 51-40-05-0G-0.SDR ASAA2024050949666Floor Support · crackedFWD WET AREA INTERCOSTAL CRACKED LBL 34 STA 312 TO 328. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02-0G-0, 51-40-05-0G-0.SDR SWAA2024052083843Support · corrodedFORWARD CARGO AFT BULKHEAD LH LOWER CURVED SUPPORT IS CORRODED AT STA 500I LBL 30<[01] ANSWERED MEASUREMENT QUESTIONS AND PARTS DATA UPDATE. REMOVED FWD CARGO LT LOWER CURVED SUPPORT DUE TO DETERMINED TO BE OUT OF LIMIT IAW SRM 53-30-08-1A-1. LOCATED AND DRSDR FDEA202405090681Header · bentAFT CGO DOOR CUTOUT UPPER FWD CORNER FOUND A PLATE DEFORMED, POS: FR59A-FR61 STGR28R REPLACED THE DEFORMED HEADER WITH NEW PART ON AFT CGO DOOR CUTOUT UPPER FWD CORNER AT FR59A~FR61, STGR28R I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARASDR FDEA202405090662Bracket · damaged#4 SUPPORT BRACKET BROKEN FOR AFT CARGO COMP'T DOOR AT FR61A~FR62,S-43R POSITION. REPLACED THE BRACKET WITH NEW PART AND FASTENERS AT AFT CARGO DOOR FR61A~FR62 S- 43R, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 I.A.W A300-600F SRM 51-72-10-001, PAGE.2 &SDR UIEA2024050800356Bracket · corrodedCORROSION - BRACKET, RH WING GEAR W/W CENTER WALL HYD TUBE SUPPORT BRACKET, STA 1301(<P>1. REMOVE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 100 2. FABRICATE NEW BRACKET IAW WORK SHEET 40263 3. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV 100 AND BOEING DWG 2SDR CALA2024051001423Bracket · crackedREF AMES NR 170224-0100-00175 GEN ITEM EA 5100-02129 REV H OP 00 1 DURING AGING INSPECTION, FOUND L-BRACKET CRACKED FOR FUSELAGE FA IRING SUPPORT CRACKED, JUST AFT OF RWW RBL-12SDR CALA2024051001421Shear Plate · corrodedRH SHEAR PLATE IS CORRODED . REMOVED AND REPLACED RH SHEAR PLATE BTW FR69/FR70 IAW A319 SRM 51-42-11/001.SDR CALA2024051001420Door Sill · corrodedAFT CABIN L-2 DOOR SILL HAS BUBBLED PAINT POSSIBLE CORROSION PER HAECO LCQ N/R 9298286/42286 GEN BY V061642 REPAIRED AFT CABIN L-2 DOOR SILL AT FR68/67 Y1292 IAW A319 SRM 53-41-14-300-001 REPAIR PRINCIPLE 7 BY MECH V061742 INSP BY V892442SDR CALA2024051001419Floor Support · crackedREF AMES NR 170224-0100-0149 GEN ITEM 53-5310-1-2606 FLC FS676 LBL24 SLOPE WALL FLOOR SUPPORT CRACKED. REPAIRED SLOPE WALL FLOOR SUPPORT FS676 LBL24 IN FLC IAW B757 SR M 51-70-0G-0 TABLE 1SDR DALA2024051005102Shear Plate · corrodedSHIP 3132 CORROSION SHEAR PLATE LOCATED FR 69 TO FR 70 AND STR 23L AT AFT GALLE Y AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE LOCATED FR 69 TO FR 70 AND STR 23L AT AFT GALLEY AREA AS PER A319 SRM 51-72-11.SDR JR2R20240509133Floor Support · corrodedFLOOR SUPPORT AT FR89 LBL10 CORRODED. REPLACEDSDR JR2R20240509134Shear Panel · corrodedRH SHEAR PANEL CORRODED AT FR87 - FR88 RBL10 - RBL30 CORRODED. REPLACEDSDR JR2R2024050900002Channel · corrodedRH FLOOR MOP SILL AT FR88-FR90 CORRODED. REPLACEDSDR JR2R20240509232Floor Support · corrodedGALLEY SUPPOR FITTING AT FR87 - FR88 RBL24 CORRODED. REPLACEDSDR FDEA202405090629Floor Support · crackedCABIN - STATION 1887, X = 57.5 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN - CRACKED FLOOR SUPPORT AT STATION 1887, X = 57.5 REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 57.5 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICSDR FDEA202405090628Floor Support · crackedCABIN - STATION 1887, X = 24 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN AT STATION 1887, X = 24 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G AT STATION 1887 TO STATION 2007, X = 24. FLOOR SUPPORT FABRICATED BY MASDR FDEA202405090627Floor Support · crackedCABIN - STATION 1887, X - 2 FLOOR SUPPORT APPROXIMATELY OF 1.25 INCH FOUND CRACK. CABIN AT STATION 1887, X = - 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AT STATION 1887 TO STATION 2007, X = - 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MSDR FDEA202405090626Floor Support · crackedCABIN - STATION 1887, X = 2 FLOOR SUPPORT APPROXIMATELY OF 1.5 INCH FOUND CRACK. CABIN AT STATION 1887, X = 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHSDR ASAA2024050851784Threshold · corrodedR1 DOOR LOWER CUTOUT THRESHOLD CORROSION AT LOCATIONS FR 16 Y1896 TO Y1944 GROUNDED - YES. REPAIRED 1 FASTENER HOLE AT R-1 DOOR SILL BEAM IAW A320 SRM 53-11-14-283-005 REV 148-01FEB2024. CATEGORY B REPAIR. INSPECTION THRESHOLD FROM FIRST AIRCRAFT FLIGHT 60000 SDR ASAA2024050851783Threshold · corrodedL1 THRESHOLD HAS MULTIPLE AERAS OF CORROSION FR 16-20 -73Y GROUNDED - YES. REPAIRED 3EACH FASTENER HOLES AT L-1 DOOR SILL BEAM IAW A320 SRM 53-11-14-283-005 REV 148-01FEB2024. CATEGORY B REAPIR. INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT 60000 FC/FH NOT RSDR ASAA2024050851617Stiffener · corrodedCORROSION ON FWD STIFFENER IN CUTOUT FOR ACCESS DOOR 312AR GROUNDED - YES. REMOVED AND REPLACED FWD STIFFENER ON CUTOUT FOR ACCESS DOOR 312AR IAW A320 SRM 51-72-11-911-001 REV 148 AND AIRBUS DWG D53571510 REV KSDR AALA202408061312Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED RIGHT HAND LATERAL FORK END FITTING PER EA 354316.SDR AALA202407171312Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 354316.SDR AALA202407175255Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 354316.SDR AALA202406263961Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.SDR AALA202406218861Web · crackedAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL PYRAMID STRUCTURE WEB CRACKED BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL PYRAMID STRUCTURE WEB PER EA 354516.SDR AALA202406214328Angle · crackedAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL PYRAMID STRUCTURE ANGLE FITTING CRACKED BETWEEN FR 23 AND FR 24 AT+Y1292, BETWEEN S32L AND S33L. REPLACED LEFT HAND LATERAL PYRAMID STRUCTURE ANGLE FITTING PER EA 354516.SDR SWAA2024061283833Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED AFT POSITION BS 907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING 147A7221 REV D.SDR SWAA2024061283835Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED FWD POSITION BS907 TO BS927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG-147A7221 REV: D.SDR SWAA2024061183832Support Angle · crackedCRACK ANGLE SUPPORT LOCATED BS 947.5 AND S-26L AFT CARGO COMPARTMENT. REPLACED-SUPPORT AND FASTENERS LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 149A8103 SHEET 6 REV -.SDR SWAA2024061183834Angle · crackedCRACK ANGLE LOCATED BS867 AND S-26L AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS867 AND S-26L AFT CARGO COMPARTMENT IAW SRM 51-10-02; SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV -.SDR SWAA2024060683601Support · brokenAFT CARGO BAY FORWARD BULKHEAD FLOOR TO BULKHEAD SUPPORT IS BROKE BS 727+4 LBL 10 TO RBL 10 WL156<[01] IF REPAIR REFERENCE 25-52-10-400-801-NG-01 WAS ORIGINALLY SELECTED BUT IS NO LONGER REQUIRED TO SIGN OFF THE FAULT; MARK THIS STEP AS N/A.<BR>RECEIVED NEW AFSDR SWAA2024060683882Channel · crackedFWD ENTRY DOOR MOPSILL IS CRACKED AT BS 303 LBL 57 WL 208<[01] REMOVED AND REPLACED FWD ENTRY MOPSILL IAW SRM 51-40-02-0G-0 AND DWG 140A9810;[02] VERIFIED CORRECTIVE ACTION 1
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