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 DALA2024073007609Support · corroded(LOG 0469195) CORROSION AT FWD CARGO COMPARTMENT AFT BULKHEAD PANEL SUPPORT WL-156 STA-500L FROM LBL-25 TO RBL25. REMOVED AND REPLACED FWD CARGO AFT BULKHEAD LOWER SUPPORT IAW B737 SRM 51-40-02, B737 SRM 51-40-05 AND DWG #143A7902 REV B."SDR DALA2024072907575Shield · corroded(LOG 0467690) CORROSION AFT CARGO BAY AFT DOOR SHIELD STA 847-867, RBL 28, WL 156. REMOVED AND REPLACED IAW B737 SRM 51-10-02-0G, SRM 51-40-02-0G AND DWG 1460081 REV A.SDR DALA2024072907574Scuff Plate · corroded(LOG 0467540) CORROSION ON R1 DOOR SCUFF PLATE FLOOR "Z" ANGLE SUPPORT. ACCOMPLISHED ERA 619544-14 REV ORG ON R1 DOOR SCUFF PLATE FLOOR "Z" ANGLE SUPPORT.SDR DALA2024072907537Cusp Web · crackedCRACKS ON CUSP WEB BTW STA Y=579/598 AND BTW STA X=44/60 AT PAX CABIN. SUMMARY OF NRC 00443: CUSP WEB BTW STA Y=579/598 AND BTW STA X=44/60 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4 AND 51-41-02-0G. (LP #0467746)SDR DALA2024072907535Pan · corrodedCORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB PAN. SUMMARY OF NRC 00131: CORROSION LEVEL 2. LOWER DOOR JAMB PAN ON AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R REPAIR 7. (LP #0467185)SDR CALA2024072602114Floor Support · crackedFLIGHT DECK HAS 1 EA CRACKED FLOOR WEBS 1 ON CAPT. SIDE. GENERAT ED BY PER HAECO LCQ NR9298360/36360 REMOVED AND REPLACED WEB IN FLIGHT DECK L/H FR 8-11 IAW A320 SRM 51-72-11. ACCOMPLISHED BY INSPECTED BYSDR CALA2024072602113Floor Support · crackedRH FLIGHT DECK CRACKED FLOORBEAM AT FR8-11. GENERATED BY ON HAECO LCQ NR 9298874/36874 REMOVED AND REPLACED WEB IN FLIGHT DECK R/H FR 8-11 IAW A320 SRM 51-72-11. PERFORMED BY INSPECTED BYSDR IXXA20240726003Angle · crackedTHE ATTACH ANGLES ARE CRACKED AT THE TOP, ON THE FWD AND AFT SIDES OF FRAME 1087, JUST BELOW THE ALC FLOOR, LBL26.SDR DALA2024072607479Cusp Web · damagedTOOL MARK ON CUSP WEB (LOWER FACE) STA Y=614 AND STA X=-54 AT PAX CABIN. SUMMARY OF NRC 00452: CUSP WEB STA Y=614 AND STA X=-54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0466500)SDR HNAA2024091800829Gusset · corroded53-2037 CTR FUSE IV, RH GUSSET CORRODED BTW FR59-61. R & R GUSSET IAW SRM 51-40-02SDR HNAA2024091100746Floor Support · corroded53-2036 CTR FUSE IV, RH OMEGA BEAM CORRODED UNDER 2 NUTPLATES BTWFR59-61. REPAIRED IAW EO 1-53-24-0457SDR HNAA2024091100744Angle · cracked53-2032 FF2, UPPER ANGLE CRACKED IN NOSE HYDRAULIC COMPARTMENT BTW FR6-7. REPAIRED IAW EO 1-53-24-0484SDR SWAA2024090316725Web · crackedCRACK ON WEB LOCATED BETWEEN STA500D TO STA520 AND RBL7 AT FWD CARGO COMPARTMENT 2024-454445<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATSDR SWAA2024090316752Floor Support · crackedCRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA 2024-458672<[01] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG-141A5400 SHEET 33 REV : - SEE INDIVSDR SWAA2024090316746Web · crackedCRACK ON WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-458667<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A5400 SHEET: 20 REV: - AND SRM 51-10-02 Ï¿½TEM 9; SEE INDSDR SWAA2024083016478Scuff Plate · crackedCRACK ON SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA 2024-458655<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24.;[02] TOOL USED RADIOMETER PN. XRP-3000; SN. 1753759; DUE DATE. 07-DEC-24;[03] REPAIRED THE CENTER SCUFF PSDR SWAA2024083016483Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT AREA. 2024-458660<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: A21042057; DUE DATE 17-APR-25.;[02] STEP #1 CORRECTED:<BR><BR>TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: A23217720; DUE DASDR SWAA2024083016750Floor Support · crackedCRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA 2024-458671<[01] REPLACED INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 13 REV: - <BR>SEE INDIVIDUAL SDR SWAA2024083016748Web · crackedCRACK ON WEB LOCATED BTW BS 270 TO BS 277 BL 0 AT FWD GALLEY AREA 2024-458669<[01] REPLACED WEB LOCATED BTW BS 270 TO BS 277 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG #141A5210 SHEET 18 REV:-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB LSDR SWAA2024083017307Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-458675<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 143A5400 REV A SHEET 38 SEE INDIVIDUAL SIGN OFF BSDR SWAA2024083017306Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-458676 CORRECTED LOCATED: CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSDR SWAA2024083017308Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-458677<[01] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS380 TO BS400 LBL 13 AT PASSEGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 143A5400 REV A SHEET 38.;[02] CORRECTED STEP 1<BSDR SWAA2024083016749Floorbeam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5; RBL 43; WL208.1 AFT GALLEY AND LAV 2024-458670<[01] TOOL USED IN STEP 5: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] TOOL USED ON STEP 9: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 200053SDR SWAA2024082616738Angle · crackedR/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED<[01] REMOVED AND REPLACED 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 51-40-02; DWG 111A1000; AND DWG 111A1001.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-11SDR SWAA2024081616408Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE AROUND FITTING BS 947.5; LBL 50<[01] REMOVED DAMAGED ON FLOOR SUPPORT (INTERCOSTAL) AT BS 947.5 LBL 50 WL 208 IN AN AREA OF 1.1' X 1.1'; REMOVED 0.048'; ORIGINAL MATERIAL THICKNESS 0.200'; REMAINING MATERIAL THICKNESS 0.152SDR SWAA2024081617177Support · crackedBREAKER PANEL CRACKED AT BS 540 LBL1 WL 208.<[01] REMOVED AND REPLACED CRACKED BREAKER PANEL BS 540; LBL 1; WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED CRACKED BREAKER PANEL BS 540; RBL 1-24; WL 208 IAW SRM 51-40-02-0G-0;[03] CORRECTION; STEP 2;3 ISSDR SWAA2024081617178Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 396 LBL12 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 396 LBL 12 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID: 0184 REV: -; AND BOEING DWG 143A5400 ID: 0140 REV: -.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024081617179Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 390 LBL52 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 390 LBL 52 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID:0183 REV: - AND BOEING DWG 143A5400 ID:182 REV: -.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024081617180Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT BS 317 RBL11 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 312-328 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 ID:0001 REV: -.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024081617181Plate · corrodedCORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS 345 LBL59 WL208<[01] EVALUATED CORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS 345 LBL59 WL208 & DETERMINED TO BE OUT OF LIMITS. REMOVED & REPLACED FED MOPSILL IAW SRM 51-40-02; SDR IXXA20240816003Seal Depressor · crackedMCD CUTOUT FWD LOWER SEAL DEPRESSOR ATTACH FITTING IS CRACKEDSDR SWAA2024081517238Scuff Plate · cracked*PARTS RACK ITEM* FWD CARGO DOOR FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED FWD CARGO DOOR FWD CORNER SCUFF PLATE PER B737-800 SRM 53-00-01-2R-21 REPAIR 21; BAC. DWG. 143A8331 REV. C; B737-800 SRM 51-40-06; AND SRM 51-40-05.;[02] REPAIRED FWD CARGO DOOR FWD SDR SWAA2024081517182Angle · corrodedCORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 LBL60 WL208<[01] EVALUATED CORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 LBL60 WL208 & DETERMINED TO BE OUT OF LIMITS. REMOVED & REPLACED FED MOPSILL SCUFF PLATE ATTACH ANGSDR SWAA2024081517183Angle · corrodedCORROSION ON FSD MOPSILL SCUFF PLATE ATTACH ANGLE AT BS 322 AND 331 RBL 59 WL208<[01] COMPLETED MEASURMENT TABLE;[02] DAMAGE OUT OF LIMITS PER SRM 53-10-15-1A-2; REMOVED AND REPLACED SUPPORT ANGLE AT BS 296-331; RBL 59; WL 208; PER SRM 51-40-02-0G-0; REF BOEINSDR SWAA2024081316731Stiffener · crackedEGPR DOOR CUT OUT LOWER STIFFENER IS CRACKED<[01] INSTALLED NEW STIFFENER PN:141A3711-75 IAW B737-800 SRM 51-40-02 & REF. BOEING DWG NO. 141A0640 SHEET 178 LEAK CHECK GOOD.;[02] VERIFIED REMOVAL AND REPLACEMENT OF NEW STIFFENER P/N 141A3711-75 IAW B737-800 SRMSDR SWAA2024081316405Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE AROUND FITTING BS 947.5; LBL 25 (MARKED)<[01] ALL REPAIRS WILL BE ACCOMPLISHED ON CUSTOMER CARD#TTG8Q00UUSXR;[02] EDIT: ACTION 1 ENTERED IN ERROR;[03] REPAIRED DAMAGE ON FLOOR SUPPORT STRUCTURE AROUND FITTING AT BS 947.5; LSDR SWAA2024081316718Strap · corrodedAFT CARGO BAY FLOOR PNL T-STRAP HAS CORROSION BS 727D+5 LBL 20 - RBL 20<[01] RECIVED 'T' STRAP 146A9401-8ATSMRO; GOING TO BE INSTALL ON W/C TTG8Q00U29VL;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.SDR ASAA2024072551682Floor Support · corrodedFLOOR SUPPORT AT LBL-50 BETWEEN STA 947 TO STA 967 CORRODED. GROUNDED - YES. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-70-51-1A-1. REMOVED AND REPLACED SUPPORT IAW B737-700 SRM 51-40-02-0G-0.W= 1.00 O= .090 R= .079 L= 2.00 D= .011.SDR ASAA2024072551681Web · corrodedSILL WEB BETWEEN STA 986 TO STA 1006 LBL-36 TO LBL -41HAS LIGHT SURFACE CORROSION. GROUNDED - YES. UPON FURTHER EVALUATION FOUND TO HAVE 100%MAT LOSS. REMVOED AND REPLACED SILL WEB I.A.W. B737-700 SRM 51-40-02-0G-0.W= 1.0 O= .080 R= .000 L= 2.00 D= .080.SDR VNAA202408090021Angle · corrodedCORROSION ON ANGLE MOUNTING BTW FS 310.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE MOUNTING BTW FS 310.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND CRJ-900SDR AALA202408098267Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 500A TO STA 500G, LBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-01.SDR AALA202408099065Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 500B TO STA 500G, RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-01.SDR CALA2024080602169Bracket · corrodedCORROSION ON BOTH OF THE BRACKETS THAT HOLD THE LEFT OVERWING ESCAPE SLIDE RELEASE PIN INSIDE OF THE LEFT SLIDE COMPARTMENT.#3653 REMOVED AND REPLACED L/H OVERWING EXCAPE SLIDE RELEASE PIN BRACKET ASSY IAW B757 SRM 51-40-02 PARA 7. SEE PARTIAL WORK ACCOMPLISHESDR AALA202408055363Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR SILL INNER CHORD (CREASE ANGLE) AT STA 316, LBL 57. REPLACED INNER CHORD PER AARD 51-00-05.SDR AALA202408050958Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR SILL INNER CHORD (CREASE ANGLE) AT STA 330, LBL 57. REPLACED INNER CHORD PER AARD 51-00-05.SDR CALA2024073102146Door Sill · mechanic errorLEFT MID CABIN PLUG DOOR LOWER SILL CHORD OF OUTBD WEB HAS 6 HOLES MISDRILLED. CK OK AT LH MID EXIT PLUG DOOR LWR SILL PER AVO12967 ACCOMPLISHED OPEN HOLE HFEC INSP OF ALL OPEN HOLES PER NDT MANUAL PART 6. 51-00-00 PROCEDURE 16 CK OK. NO DEFECT NOTED. L/P UPGSDR AALA202407301662Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT ANGLE FOR INTERCOSTAL AT BS 500G, RBL 23. REPLACED ANGLE PER AARD 51-00-05-1.SDR DALA2024072907571Sill Drain · corroded(LOG 0467368) R/H MOPSILL HAS SEVERAL AREAS OF CORROSION FROM STA 285 TO STA 344, WL 208. INSTALLED REPLACEMENT FWD SERVICE DOOR LOWER SILL INNER CHORD (MOP SILL) FROM STA 259.5 RH TO STA 360 RH. WL 208 IAW B737 SRM 51-40-02-0G, DWG 141A8310 REV D.SDR DALA2024072907569Angle · corroded(LOG 0465884) DURING INSPECTIONS, CORROSION WAS FOUND ON THE FWD GALLY DOOR R/H LOWER MAIN SILL INNER CHORD ANGLE (PN 141A8312-5) BETWEEN BS 304 AND BS 324, RBL 58. REPAIRED CORROSION PER ERA 619544-14.SDR DALA2024072907562Plate · corroded(LOG 0465368) CORROSION ON LH SIDE PLATES (UPPER AND LOWER SURFACE) BTW STA 727 TO STA 847 AT AFT CARGO COMPARTMENT. LH SIDE PLATES (UPPER AND LOWER SURFACE) BTW STA 727 TO STA 847 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
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