JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 SWAA2022031165307Access Panel · crackedCRACK ACCESS PANEL HOLES ON PANEL 193D AT LOWER FUSELAGE (11 EA) 2022 - 67581 / [01] TOOL USED: CALIPER: P/N:500-464 S/N:15331926 DUE DATE:28-SEP-22;[02] TOOL USED HOTBONDER P/N: HCS9000B-AV S/N: 18164925 DUE DATE: 16/JAN/23;[03] TOOL USED MULTIMETER P/N: FLUKSDR SWAA2022020265510Panel · cracked193D PANEL HAS TWO FASTENER HOLE WITH CRACKS EMANATING FROM HOLES.(MARKED) / [01] REPLACED PANEL 193D; REF AMM 53-51-21; TSR 202200756SDR SWAA2022020265511Panel · cracked194E PANEL HAS TWO FASTENER HOLES WITH CRACKS EMANATING FROM HOLES. (MARKED) / [01] INSTALLED NEW PANEL IAW 53-51-21. REF TSR 202200756SDR SWAA2022020265572Panel · elongatedPANEL 194E HAS SEVERAL OUT OF ROUND HOLES. ; / [01] FABRICATED NEW PANEL; BACK DRILLED HOLES PER 51-40-05; COUNTER SINK PER 51-40-08 AND APPLIED DECORATIVE FINISH PER AMM 51-21-99.SDR CALA2022013100263Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645SDR SWAA2022020165076Angle · crackedVERTICAL ANGLE (CLIP) @STA 727 PNL 193 HAS CRACK APPROX .75? LONG ; ANGLE CLIP IS ON LH SIDE OF WHEELWELL WING-TO-BODY FAIRING. / [01] FABRICATED AND INSTALLED NEW VERTICAL ANGLE PER<BR> SRM 51-40-02SDR SWAA2022020165077Panel · crackedCLIP @STA 727 PANEL 193 HAS CRACK APPROX .75? LONG. ; / [01] CLIP WAS REMOVED AND REPLACED WITH ONE FABRICATED PER EA INSTRUCTIONSSDR SWAA2022013164595Panel · elongated193D PANEL HAS MULTIPLE ELONGATED HOLES ; / [01] REPLACED PANEL 193D PER AMM 53-51-21. <BR><BR>TSR#202200680SDR SWAA2022013164594Panel · elongated194E PANEL HAS MULTIPLE ELONGATED HOLES. ; / [01] REMOVED AND REPLACED PANEL 194E REF AMM 52-51-11SDR SWAA2022013164775Panel · cracked194 E PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS ; / [01] DRILLED; AND PREPARED NEW PANEL; [02] INSTALLED PANEL PER AMM 53-51-21SDR SWAA2022013164776Panel · cracked193D PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS AND SERVAL COUNTERSUNK WITH EXCESSIVE WEAR ; / [01] DRILLED; TRIMMED AND PREPARED HOLE IN NEW PANEL; [02] INSTALLED PANEL 193D PER AMM 53-51-21SDR SWAA2022031764474Panel · delaminatedPANEL 191CL HAS A DELAMINATED DENT ON THE EXTERNAL SKIN (MARKED) / [01] IDENTIFIED PANEL 191CL MATERIAL IAW SRM 53-30-70-0I-1 FIGURE 2 TABLE 2 ITEM 8. DAMAGED AREA EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-70-1A-1 PAR.4 A (4). DAMAGE IS REPAIRABLE IAW SRM SDR SWAA2022021164585Access Panel · corrodedCORROSION ACCESS PANEL 192F MARKER BEACON ANTENA AREA LOWER FUSELAGE A T LOWER FUSELAGE ; 2022-011546 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331932 DUE DATE 26/OCT/22; [02] TOOL USED SCALE P/N CL5000 S/N AE-37099 DUE DATE 16/AUG/22; [03] TOOL USED HOT BONDSDR SWAA2022013164436Panel · elongated194E PANEL HAS SEVERAL ELONGATED HOLES. ; 194E PANEL HAS SEVERAL ELONGATED HOLES; / [01] REPLACED PANEL 194E WITH SERVICEABLE PANEL; REF. AMM 53-51-21; [02] REPLACED PANEL 194E; REF AMM 53-51-21SDR SWAA2022013164437Panel · elongated193D PANEL HAS SEVERAL ELONGATED HOLES. / [01] REPLACED PANEL 193D WITH SERVICEABLE PANEL; REF AMM 53-51-21SDR SWAA2022013164132Panel · elongated194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWD EDGE. BOTH LH AND RH LEADING EDGE 3RD ONE BOTH SIDE COMING INDRD IF COUNTING LH TO RH 3RD HOLE AND 7TH HOLE ELONGATED MARKED PANEL ; 194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWDSDR DALA2022012700564None · noneSHIP 3247 CRACK ACCESS PANEL 191KB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI #596507-14 VALIDATED ER/A #596507-14. (2099901)SDR SWAA2022013163706Panel · elongatedPNL 194E HAS ELONGATED HOLES ; / [01] REMOVED AND REPLACED 194E PANEL PER AMM 53-51-21.SDR SWAA2022013163707Panel · elongatedPNL 193D HAS ELONGATED HOLES ; / [01] REMOVED AND REPLACED 193D PANEL PER AMM 53-51-21.SDR SWAA2022013164118Panel · elongated193D PANEL HAS ELONGATED FASTENER HOLES ; 193D PANEL HAS ELONGATED HOLES. / [01] ACCOMPLISH EA 22-153-00260 ASSIGNED AS A SUBTASK.; [02] COMPLIED WITH TSR 202200634SDR SWAA2022013164119Panel · elongated194E PANEL HAS ELONGATED HOLES ; 194E PANEL HAS ELONGATED HOLES. / [01] REMOVED AND REPLACED 194E PANEL PER SRM 51-40-02. REF TSR 202200632.SDR SWAA2022012763661Panel · elongated193D ELONGATED HOLE ; / [01] INSTALLED NEW 193D PANEL REF B737 AMM53-51-21.SDR SWAA2022012763662Panel · elongated194E PANEL ELONGATED HOLES ; / [01] INSTALLED NEW 194E PANEL REF B737 AMM53-51-21.SDR SWAA2022012763617None · cracked193 D PANEL LEFT HAND T CLIP CRACKED / [01] INSTALLED T- CLIP THAT WAS FABRICATED PER EA 22-153-00243 PER SRM 51-40-02SDR SWAA2022012763220Panel · none193D PANEL WEAR ; 193D PANEL HAS FRETTING WEAR ALONG AFT EDGE. / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21SDR SWAA2022012763242Panel · elongatedPANEL 193B FASTENER HOLES ENLARGED. ; FASTENER HOLES AT LOCATIONS 5;11;18;21;23;30;31;32 ARE ENLARGED IN PANEL. / REMOVED AND REPLACE PANEL 193B REF AMM 53-51-21.SDR 2022F00037Screen · cracked2 INCH CRACK IN APU INLET SCREEN. TEXTRON AVIATION ENGINEERING MEMO DQ33270, DATED JANUARY 22, 2022, HAS GRANTED A FLIGHT EXTENSION FOR 100 FLIGHT HOURS OR UNTIL FEBRUARY 28, 2022, WHICHEVER OCCURS FIRST. INSPECTION OF THE SCREEN PER DQ33270 HAS VERIFIED THAT SDR SWAA2022021663335Panel · crackedCRACK ACCESS PANEL 194E BODY FAIRING AROUND HOLES AT LOWER FUSELAGE 2022-58095 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331932 DUE DATE 26/OCT/22.;[02] TOOL USED HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-SDR SWAA2022012663157Panel · debonded193D PANEL FWD L/H SIDE CRACKED AND DISBONDED. (MARKED) ; 193D PANEL FWD LH SIDE CRACKED AND DISONDED. (MARKED) / [01] REMOVED AND REPLACED PANEL 193D IAW AMM53-51-21.SDR SWAA2022012663158Panel · elongated194E PANEL HAS 4 ELONGATED FASTENER HOLES. (MARKED) / [01] INSTALLED NEW PANEL PER TSR 202200555; E.O. 5351-I-14642-NG AND AMM 53-51-21SDR SWAA2022012663159Panel · elongated193D PANEL HAS 5 ELONGATED FASTENER HOLES. (MARKED) / [01] REMOVED AND REPLACED PANEL 193D IAW AMM 53-51-21.; [02] C/WSDR SWAA2022012663290Panel · cracked194E PANEL HAS 3 EACH HOLES ON LEADING EDGE OF PANEL THAT HAVE CRACKING ON BACKSIDE OF PANEL ; 194E PANEL HAS 3 EACH HOLES ON LEADING EDGE OF PANEL THAT HAVE CRACKING ON ACKSIDE OF PANEL / [01] REMOVED AND REPLACED PANEL REF AMM 53-51-21.SDR SWAA2022012663291Panel · cracked193D PANEL HAS 6 OVERSIZED HOLES ON TRAILING EDGE OF PANEL WITH EVIDENCE OF CRACKING ON BACKSIDE OF PANEL ; 193D PANEL HAS 6 OVERSIZED HOLES ON TRAILING EDGE OF PANEL WITH EVIDENCE OF CRACKING ON ACKSIDE OF PANEL / [01] REMOVED AND REPLACED PANEL REF AMM 53-51SDR SWAA2022012562815Panel · elongated193D PNL HAS 10 DIMPLED; CRACKED AND ELONGATED HOLES. ; / [01] INSTALLED NEW 193D PANEL PER AMM 53 51-21.SDR SWAA2022012562816Panel · cracked194E PNL HAS 9 DIMPLED AND CRACKED HOLES ; / [01] INSTALLED NEW 194E PANEL PER AMM 53-51-21.SDR SWAA2022013162782Panel · delaminatedPANEL 193D HAS DELAMINATION TO OUTER SURFACE (MARKED) ; IDENTIFIED PANEL IAW SRM 53-40-70-0I-1 FIG 2 ITEM 12. DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A (6)(C). DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-2 & SRM 51-70-04-2R-11 (CSDR SWAA2022012462770Bracket · cracked193D STATION 727 CRACKED BRACKET. ; 193D STATION 727 LEFT VERTICAL WE RACKET AND T-CLIP CRACKED. / [01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SDR SWAA2022012462366Panel · elongatedPANEL 194E HAS SEVERAL ELONGATED HOLES. / [01] R&R PANEL 194E PER AMM 53-51-21SDR SWAA2022012462384Panel · delaminated193D PANEL HAS 3EA DELAMINATED HOLES ON AFT EDGE ; / [01] REMOVED AND REPLACED 193D PANEL PER TSR# 202200438 AND AMM 53-51-21SDR SWAA2022012762260Panel · crackedLOWER FUSELAGE PANEL 193D HAS (3 EACH) FASTENER HOLES CRACKED ; / [01] REMOVED PANEL 193D FOR ACCESS AS PER AMM 53-51-21-000-802; [02] PREPARED FOR REPAIR AT PANEL 193D AS PER B 737-700 SRM 51-70-04-2R-9; [03] VERIFIED STEPS 1 AND 2; [04] REPAIRED AT PANEL 193SDR CALA2022011800178Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645SDR DALA2022030301343None · noneTHE FUSELAGE INTERCOSTAL WAS FOUND CRACKED AT BEND STA 1212 STA 1225, WHICH AFFECTED THE TAILCONE DEPLOYMENT CABLE ATTACH POINT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. A TEMPORARY REPAIR WASSDR SWAA2022012161687Panel · elongatedPANEL 193D HAS MULTIPLE ELONGATED HOLES ; / [01] REMOVED AND REPLACED WITH NEW SERVICEABLE PANEL 193D PER AMM 53-51-21.SDR SWAA2022012061933Panel · elongated193D PANEL HAS SEVERAL ELONGATED HOLES ; / [01] REPLACED PANEL WITH NEW.INSTALLED PER AMM 53-51-21SDR SWAA2022012061934Panel · elongated194E PANEL HAS SEVERAL ELONGATED HOLES WITH CRACKS ; / [01] INSTALLED NEW PANEL REF AMM 53-51-21SDR SWAA2022012061693Panel · elongated194E PANEL HAS ELONGATED AND CRACKED HOLES. / [01] CWSDR SWAA2022012061694Bracket · mislocatedRIGHT 'L' BRACKET MISS LOCATED ON THE 194E PANEL AFT ROW OF FASTENERS. ; RIGHT 'L' RACKET MISS LOCATED ON THE 194E PANEL AFT ROW OF FASTENERS. / [01] REMOVED L BRACKET TO FOM IAW SRM 51-40-02; [02] COW EASDR SWAA2022012061695Panel · elongated193D HAS ELONGATED AND CRACKED HOLES. / [01] REMOVED AND REPLACED 193D IAW AMM 53-51-21SDR SWAA2022011861660Panel · elongated194E HAS FOUR ELONGATED FASTENER HOLES. (MARKED) ; 194E PANEL HAS FOR ELONGATED FASTENER HOLES. (MARKED) / [01] INSTALLED NEW 194E PANEL IAW AMM 53-51-21.SDR SWAA2022011861661Panel · cracked193D PANEL AFT SIDE HAS ONE FASTENER HOLE WITH CRACKS EMANATING FROM HOLE. / [01] R&R PANEL 193D PER AMM 53-51-21.
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