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 SWAA2022102060248Panel · delaminated193B PANEL FWD R/H I/B CORNER HAS EDGE DAMAGE OF 0.100 IN AND DELAMINATION MEASURES 0.300 FROM CORNER. / [01] REPLACED PANEL 193B IAW AMM 20-50-11SDR AALA202211035143Panel · crackedAIRCRAFT WAS GROUNDED: RIGHT WING TO BODY PANEL CRACKED 195CR. REPAIRED WING TO BODY PANEL 195CR AND COMPLETELY INSTALLED PER AMM 53-51-21 AND SRM 51-70-06.SDR SWAA2022102859223Panel · damagedPANEL 193CR OUTER SKIN IS DISBONDED 6.5' FROM TOP EDGE AND 4.5' FROM L/E. / FOUND DELAMINATION DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA'S 2 AND 4.A.(6).<BR><BR>DAMAGED AREA WILL BE REPAIRED ACCORDING TO SRM 51-70-05-2R-1 AS REQUIRED BY SDR SWAA2022101056704Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. / [01] REPLACED PANEL 193B PER SRM 51-40-02SDR SWAA2022101057020Panel · delaminatedWING TO BODY FAIRING PANEL 193B HAS OUTER SKIN DELAMINATION AND LARGE AREA WITH FIBERGLASS PLYS TORN AND MISSING. / [01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B IAW 53-51-21.SDR SWAA2022100656579Panel · elongatedWING TO BODY FAIRING PANEL 193B HAS SEVERAL ENLARGED HOLES. / [01] DRILLED NEW PANEL PER SRM 51-40-05;[02] R&R WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.SDR SWAA2022110956373Panel · crackedPANEL 193AL HAS SEVERAL CRACKED PULLED THROUGH FASTENER HOLES / [01] IDENTIFIED PANEL 193AL MATERIAL ACCORDING TO SRM 53-40-70-0I-1; FIG. 2; TABLE 2; ITEM 7.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA'S 2.D AND 4.B.(2). <BR><SDR SWAA2022101054162None · crackedPANEL #192E FWD L/H ATTACH BRACKET CRACKED / [01] REMOVED AND REPLACED #192E FWD L/H ATTACH BRACKET PER SRM 51-40-02SDR AALA202212215819Support Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING TO BODY AFT FAIRING SUPPORT FRAME ASSEMBLY LOCATED AT BS 727 +2 AND RBL 9.5. REPAIRED FRAME ASSEMBLY PER EA 340107.SDR SWAA2022100652179Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. / [01] REMOVED AND REPLACED PANEL PER SRM 51-40-02.SDR FDEA202210032524Frame · crackedTAILCONE; AFT EXTENDED TAILCONE LOWER HINGE HAS CRACK @ INTERNAL SECTION OF FRAME. STA.2259 NOTE: VERIFY BORESCOPE/NDT METHOD DOT # 23 REMOVED AND REPLACED FROM AKC7602-3 FRAME IAW DWG AKC7602.SDR FDEA202210032523Fitting · crackedAFT EXTENDED TAILCONE STA. 2267 LOWER LONGITUDINAL STRUCTURE FITTING CRACKED AFT OF LOWER HINGE. DOT# 24 REMOVED, FABRICATED AND INSTALLED NEW JAMB AKC7610-5 IAW DWG AKC7610 AND AKC7608SDR FDEA202210032462Frame · crackedTAILCONE; AFT EXTENDED TAILCONE LOWER HINGE HAS CRACK @ INTERNAL SECTION OF FRAME. STA.2259 NOTE: VERIFY BORESCOPE/NDT METHOD DOT # 23SDR SWAA2022093049110Panel · damaged193B MOUNTING HOLE LOCATIONS 1; 14 ; AND 19 HAVE ELONGATED OVERSIZED HOLES / [01] INSTALLED WASHERS AT HOLE LOCATIONS 1; 14; AND 19 PER EA 22-153-02942.SDR SWAA2022101171699Panel · deterioratedDETERIORATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR 2022-518190 / [01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000285 DUE DATE: 10-DEC-22.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 16/JAN/23.;[03] TOOL USED: SCALE P/N: 91847 S/N: AESDR SWAA2022101446003Panel · perforatedCUSTOMER REQUEST: PERFORATION ON ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2022-510212 / [01] TOOL USED: CALIPER P/N:500-197-30 S/N:15120589 DUE DATE:28-NOV-22.;[02] TOOL USED: SCALE P/N: 91847; S/N: AE-409317; DUE DATE: 06-JUN-23.;[03] TOOL USED: HSDR SWAA2022101052780Panel · elongatedPANEL 193D HAS ELONGATED FASTENER HOLES 'MARKED' (TRANSFERRED FROM FAULT TTG8Q009AWK9) / [01] IDENTIFIED PANEL 193D MATERIAL ACCORDING TO SRM 53-40-70-0I-1; FIG. 2; ITEM 12; TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARASDR SWAA2022101052781Panel · elongatedPANEL 194E HAS ELONGATED FASTENER HOLES 'MARKED' (TRANSFERRED FROM FAULT TTG8Q009AWK9) / [01] IDENTIFIED PANEL 194E MATERIAL ACCORDING TO SRM 53-60-70-0I-4; FIG. 2; ITEM 8; TABLE 2. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1; PARASDR SWAA2022091552444Panel · elongatedPANEL 193B PANEL HAS ELONGATED HOLES. / [01] REMOVED AND REPLACED PANEL 193B PER SRM 51-40-02.SDR FDEA202209122536Frame · crackedTAILCONE, L/H AKC7539-3 FRAME, BEHIND UPPER HINGE POINT HAS A 4 CRACK. REMOVED AND REPLACED CRACKED AKC7539-3 FRAME, REF DWG AKC7539.SDR SWAA2022091251428Panel · elongatedPANEL 193B HOLES ELONGATED / [01] REMOVED MATCH DRILLED AND INSTALLED NEW 193B PANEL PER SRM 51-40-02.SDR SWAA2022091251357Panel · pulledPULLED FASTENER HOLE ON PANEL 192AR. / [01] SANDED AND REMOVED DAMAGE AT HOLE IN PREPARATION FOR REPAIR I/A/W SRM 51-70-04-2R-9.;[02] VERIFIED C/A # 1 :ADAM HUNTER (TECHNICIAN); 09-SEP-2022 01:17 UTC<BR>SANDED AND REMOVED DAMAGE AT HOLE IN PREPARATION FOR REPASDR SWAA2022100651472Panel · elongatedELONGATED HOLE ACCESS PANEL 193B AT LOWER FUSELAGE 2022-486122 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01/OCT/22.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24/FEB/23.;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV SDR SWAA2022100678902Panel · elongatedELONGATED HOLE ACCESS PANEL 193B AT LOWER FUSELAGE 2022-486122 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01/OCT/22.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24/FEB/23.;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV SDR SWAA2022091251356Panel · pulledPANEL #192AR PANEL LEADING EDGE HAS WEAR AND ONE FASTENER PULLED THROUGH. / [01] SANDED AND REMOVED DAMAGE AT HOLE IN PREPARATION FOR REPAIR I/A/W SRM 51-70-04-2R-9.;[02] SANDED LEADING EDGE DAMAGE IN PREPARATION FOR REPAIR I/A/W SRM 51-70-05-2R-6.;[03] NON-ROSDR SWAA2022090851132Panel · elongatedSEVERAL 193B PANEL FASTENER HOLES ARE ELONGATED AND HAS WORN THROUGH THE COMPOSITE MATERIAL. / [01] R&R 193 PANELSDR SWAA2022100650209Panel · elongatedELONGATED HOLE ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR 2022-486050 / [01] TOOL USED CALIPER P/N 500-193-30 S/N 0000285 DUE DATE 10 DEC 22;[02] TOOL USED HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE 28/FEB/23;[03] REPAIRED ACCESS PANEL 193AL BODY SDR SWAA2022100678881Panel · elongatedELONGATED HOLE ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR 2022-486050 / [01] TOOL USED CALIPER P/N 500-193-30 S/N 0000285 DUE DATE 10 DEC 22;[02] TOOL USED HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE 28/FEB/23;[03] REPAIRED ACCESS PANEL 193AL BODY SDR VNAA202209229995Strip · corrodedCORROSION ON METALIC STRIP (1EA) AT FORWARD UNDERWING FAIRNG 193AB.SDR SWAA2022091548533Panel · pulledPANEL 193AL HAS PULLED THROUGH FASTENER HOLES ON AFT EDGE / [01] IDENTIFIED PANEL 193AL IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 7. <BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4B(6).<BR><BR>REPAIR TO BE ACCOMPSDR DALA2022090105879None · none(LOG 2384527) DURING INSPECTION FOUND ELONGATED FASTENER HOLES AT CENTER WHEEL-WELL PANEL 193D. PANEL 193D WAS REPAIRED PER B737-800 S.R.M. 51-70-05-2R REPAIR GENERAL. PAR. 4. IN REFERENCE PER B737-800 S.R.M. 51-70-05-2R PROCEDURE 6 REPAIR 6.SDR DALA2022090105877None · none(LOG 2383980) DURING INSPECTION FOUND CORROSION ON PANEL SUPPORT STA 727 + 2.7 BTW LBL 24 AND RBL 24 AT LOWER FUSELAGE. PANEL SUPPORT STA 727 + 2.7 BTW LBL 24 AND RBL 24 AT LOWER FUSELAGE WAS REPAIRED PER PRI 601657-14 REV. 1 AND ERA 601657-14AD REV.ORIGINAL.SDR DALA2022082505726None · none(LOG 2377304) DURING INSPECTION FOUND ELONGATED HOLES ON SUPPORT STRUCTURE BS 727+2.7, AREA WHERE FAIRING PANEL ATTACH (193D). OLES ON SUPPORT STRUCTURE P/N 149A7593 BS 727+2.7, AREA WHERE FAIRING PANEL ATTACH (193D) WERE REPAIRED PER ERA 601629-14AD.SDR IPXA2022090185816None · dentedINSPECTION TYPE:C18AFT PIT FRAME STA 1320 RH SIDE HAS TWO DENTS ON UPPER FLANGEREPAIRED FRAME PER EA# 757-5360-27-A3010SDR SWAA2022081843182Panel · delaminatedPANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6; 8; 10; 11; 13; 14; 17; 22; 33; AND 34. PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6 8 10 11 13 14 17 22 33 AND 34. / [01] R/R 193B PANEL IAW AMM 53-51-21.SDR SWAA2022093042675Access Panel · damagedLEFT SIDE BODY OVERWING FAIRING ACCESS PANEL #195CL; SEVERAL SCREW HOLES ELONGATED/SURFACE BULGE AND INTERNAL WEAR NOTED. / [01] REMOVED LEFT SIDE BODY OVERSWING FAIRING ACCESS PANEL #195CL SRM51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.;[03] CLEANED ANDSDR SWAA2022093065315Access Panel · damagedRIGHT BODY FAIRING ACCESS PANEL #194BR; SEVERAL SCREW HOLES ELONGATED (DOT 223-BF002). / [01] CLEANED AND PREPARED SEVERAL SCREW HOLES FOR REPAIRED AND R/H BODY FARING ACCESS PANEL 194 BR AS PER B737 SRM 51-70-04-2R-9;[02] VERIFIED STEP NO 1 AND OK TO APPLY RESDR SWAA2022092842845Access Panel · elongatedRIGHT BODY FAIRING ACCESS PANEL #194BR; SEVERAL SCREW HOLES ELONGATED (DOT 223-BF002). / [01] CLEANED AND PREPARED SEVERAL SCREW HOLES FOR REPAIRED AND R/H BODY FARING ACCESS PANEL 194 BR AS PER B737 SRM 51-70-04-2R-9;[02] VERIFIED STEP NO 1 AND OK TO APPLY RESDR U2RA2022082300043Skin Panel · delaminatedDURING HEAVY MAINTENANCE VISIT, AIRCRAFT INSPECTION REVEALED WATER/OIL INTRUSION IN THE LEFT / AFT CORNER OF ACCESS PANEL #193R (P/N 65B13883-1) FOR THE AFT MAIN LANDING GEAR DOOR SUPPORT STRUCTURE, LOCATED AT APPROXIMATE STATION 1405.3 TO 1437.09, CAUSING DELSDR SWAA2022081842449Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS. / [01] R&R PANEL 193B PER SRM 51-40-02SDR SWAA2022081541586Panel · delaminatedGENERAL VISUAL INSPECTION OF THE INTERIOR SURFACE OF THE 193B FAIRING PANEL REVEALS AREAS OF DELAMINATION; PRESENT ON THE FAIRING PANEL AT FASTENER LOCATIONS NUMBER 3; 5; 9; 19; 20; 34; 35; 36; 37; 38 / [01] DRILLED AND COUNTERSUNK HOLES ON NEW PANEL PER AMM 5SDR DALA2022081605558None · none(LOG 2363844) DURING INSPECTION FOUND CORROSION AND ELONGATED FASTENER HOLES ON SETTLEMENT AREA OF FAIRING PANEL 194E BTW STA 727+2.7 AND LBL23-RBL23. FASTENER HOLES ON SETTLEMENT AREA OF FAIRING PANEL 194E BTW STA 727+2.7 AND LBL23-RBL23 WERE REPAIRED PER ER/SDR SWAA2022083041372Plate · debondedPANEL #192F FWD AND AFT ANTENNA MOUNTING PLATES ARE DISBONDED FROM PANEL / [01] BONDED 4 EACH NUT PLATES TO PANEL 192F USING BMS5-95 B-1/2 LOT# 45101031F-14 AND CURED IAW BAC DWG 149A7752 ID: 0001 FLAG NOTE 1; AND BAC5010 TY93 SUB PARAGRAPH 8.2.34. THERMOMETERSDR FDEA202208102535Frame · crackedTAIL CONE; AFT RIGHTHAND UPPER FRAME HAS 5" CRACK @ UPPER LATCH STRUCTURE. DOT #9 REPAIRED DAMAGED AKC7539-7 FRAME, REF SRM 53-80-07-2R REPAIR 4, FIG 202.SDR SWAA2022082940354Panel · elongatedELONGATED HOLE ACCESS PANEL 193CR WING TO BODY FAIRING AT LOWER FUSELAGE 2022-418575 / [01] TOOL USED: CALIPER P/N:500-464 P/N:15331926 DUE DATE: 28-SEP-22;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE:28-FEB-23.;[03] TOOL USED MULTIMETER P/N: SDR SWAA2022081040177Radome · delaminatedRADOME ASSY HAS DELAMINATION. / [01] REMOVED AND REPLACED RADOME PER AMM 53-52-00.;[02] VERIFIED DALE BOMGARDNER (TECHNICIAN); 10-AUG-2022 07:23 UTC<BR>REMOVED AND REPLACED RADOME PER AMM 53-52-00.SDR IPXA2022082485571None · crackedINSPECTION TYPE:3CLH AFT FUSELAGE HORIZONTAL STABILIZER BODY FAIRING SUPPORT BRACKET CRACK.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT BRACKET IAW SRM 51-33-01 AND SRM 51-35-01 (MINOR).SDR SWAA2022081039678Panel · crackedUNDERWING RIGHT FAIRING PANEL 192BR; AFT END CRACK NOTED. PREPARED & APPLIED DRY OUT PROCESS AT PANEL 192BR ON DAMAGED AREA IAW SRM 51-70-072R-0 PARAGRAPH (4.D). REPAIRED DAMAGED AREA TA PANEL 192BR IAW SRM51-70-04-2R-0 & PERFORMED TAP TEST ON REPAIR AREA NOSDR SWAA2022083043557Access Panel · deterioratedDETERIORATED ACCESS PANEL 193AL BODY FAIRING AT AT LOWER FUSELAGE 2022-418564 / [01] TOOL USED CALIPER P/N 500-752-20 S/N B16101225 DUE DATE 21/MAY/23;[02] TOOL USED: HOT BONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE:16-JAN-23.;[03] TOOL USED SCALE P/N:91847 S/SDR SWAA2022083043556Access Panel · deterioratedDETERIORATED ACCESS PANEL 193AR AT LOWER FUSELAGE 2022-418563 / [01] TOOL USED CALIPER P/N 500-752-20 S/N B16101225 DUE DATE 21/MAY/23;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:16-JAN-23.;[03] TOOL USED SCALE P/N:91847 S/N:AE-409320 DUE DAT
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