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 SWAA2022041992193Panel · crackedFUSELAGE FAIRING 191AL; AFT SUPPORT FRAME IS CRACKED; O/B OF STR 19L; VIEWED FROM AFT SIDE / [01] REMOVED SUPPORT FRAME IAW ARM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FAIRING SUPPORT FRAME PN: 116A3118U9 A-TAG: A123107 IAW DWG 116A3110 REV. B;[03] VERIFIEDSDR IPXA2022042081326Stiffener · crackedINSPECTION TYPE:4CLOWER FUSELAGE R/H WING TO BODY HAS A STIFFENER P/N AYB7104-526 WITH A CRACK AT STA 1298.REMOVED,FAB AND REPLACED THE CRACK STIFFENER P/N AYB7104-526 IAW DWG AYB7104 AND MD11 SRM 51-33-01. (MINOR)SDR A6WA202204068165Bulkhead · noneREAR PRESSURE BULKHEAD WEB REQUIRES MODIFICATION PER E17/003/453 ****AIRCRAFT REMOVED FROM SERVICE**** MODIFIED THE REAR PRESSURE BULKHEAD WEB FS 621.00 IAW GREO 601-53-61-1240 REV DSDR SWAA2022050291398Panel · delaminatedLOWER FUSELAGE ACCESS PANEL 194FL DRAIN MAST DELAMINATED / [01] REMOVED APU FUEL FEED LINE SHROUD DRAIN MAST. REF B737 AMM 28-25-07-020-801;[02] INSTALLED APU DRAIN MAST TO PANEL 194DL IAW B737 AMM 28-25-07;[03] INSTALLED APU DRAIN MAST AND PANEL 194DL IAW B73SDR SWAA2022050293640Panel · crackedFOUND PANEL 194E WITH 11 EACH FASTENER HOLES WITH STRESS CRACKS AND/OR ELONGATED HOLES (MARKED) / [01] MEASUREMENTS;[02] CLEANED AND PREPARED PANEL FOR REPAIR; PERFORMED DRY OUT; FOUND NO WATER AS PER B737 SRM 51-70-05-2R-8;[03] VERIFIED STEPS 1 AND 2;[04] OK SDR VNAA202204049995Skin · corrodedCORROSION ON SKIN REAR FUSELAGE FAIRING SEATLEMENT AREA BTW FS. 879 - 1015 (UNDER ACCESS 195AE, 195BB, 195DL, 196AR AND 196DR). SDR SWAA2022050490638Panel · elongatedELONGATED HOLE ACCESS PANEL 191HR AT LOWER FUSELAGE (2 EA) 2022-168723 / [01] REPLACED PANEL 191HR AT LOWER FUSELAGE (2 EA) IAW B737-700 AMM 53-51-400-803;[02] CORRECTED STEP 1<BR>REPLACED PANEL 191HR AT LOWER FUSELAGE (2 EA) IAW B737-700 AMM 53-51-21-400-803;SDR SWAA2022050390311Panel · elongatedLEFT HAND LOWER FAIRING ACCESS PANEL 194HL; FASTENER HOLES SHOWS ELONGATION AND WEAR. (DOT-010). / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #194HL AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL AS PER B737 NDTM 51-05-01;[02] PSDR SWAA2022040489896Panel · elongatedPANEL 193 B HAS NUMEROUS FASTENER HOLES ELONGATED / [01] R & R PANEL PER SRM 51-40-02.SDR SWAA2022050389454Panel · elongatedLH EQUIPMENT COOLING BAY PANEL #192JL; FASTENER HOLES ELONGATED. (DOT-002) / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #192JL AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL AS PER B737 NDTM 51-05-01;[02] PREPARED THE DAMAGED LOSDR SWAA2022040489531Panel · cracked-RIGHT WTB PNL 191AR TO 191FR VERTICAL SUPPORT CRACKED JUST I\B OF LANDING LIGHT. / [01] REMOVED AND REPLACED VERTICAL SUPPORT AT RIGHT WTB PNL 191AR TO 191FR JUST I/B OF LANDING LIGHT PER SRM 51-40-02SDR IPXA2022032680533Frame · corrodedINSPECTION TYPE:SEG2WING TO BODY STRUCTURE T CHORD AT FS 1060 WL 133 RBL 32 TO RBL 40 HAS CORROSION LOWER SURFACEREPAIRED T CHORD STRUCTURE PER SRM 51-70-12-0GSDR AALA202203308189Flap · damagedAIRCRAFT WAS GROUNDED: DURING DEPARTURE FROM BCN, LEFT WING # 2 FLAP FAIRING SEPARATED FROM AIRCRAFT DAMAGING THE LEFT AFT OUTBOARD FLAP. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO BCN, LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203218189: REPLACED FLASDR AALA202203300656Fairing · separatedAIRCRAFT WAS GROUNDED: DURING DEPARTURE FROM BCN, LEFT WING # 2 FLAP FAIRING SEPARATED FROM AIRCRAFT DAMAGING THE LEFT AFT OUTBOARD FLAP. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO BCN, LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203218189: REPLACED FLASDR AALA202203218189None · noneAIRCRAFT WAS GROUNDED: DURING DEPARTURE FROM BCN, LEFT WING FLAP FAIRING SEPARATED FROM AIRCRAFT DAMAGING THE FLAP. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO BCN, LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR SWAA2022042593959Panel · elongatedACCESS PANEL 193CL SCREW HOLES ENLONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 CL AS PER B737- SRM 51-70-06-2R-9;[02] VERIFIED STEP #1.;[03] REPAIRED AT PANEL 193 CL AS PER B 737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 ;PO. 1760049;[04] VERIFIED STEPSDR SWAA2022040585585Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS 767 TO 787 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT 2022-144888EXACTLY LOCATION BTW BS 727 TO 767 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT / [01] FABRICATED SUPPORT ZEE LOC BTW BS 727 TO BS 767 I.A.W DRAWING# 146A7502-SDR SWAA2022041984727Panel · delaminatedPANEL 193AR OUTER SKIN IS DELAMINATED. (MARKED) / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 18. <BR>UPON INSPECTION OF PANEL FOUND 1EA ADDITIONAL AREA OF DELAMINATED SKIN ON OUTER SURFACE 36' FROM I/B EDGE; 16' FROM FWDSDR SWAA2022041885124Panel · damagedREF TTG8Q003883M: LOWER WING TO BODY FAIRING 193D INNER SURFACE WITH FRETTING / [01] CLEANED DAMAGE AREA AND REPAIRED SMALL AREA OF FRETTING ON INNER SURFACE AFT AREA OF LOWER WING TO BODY FAIRING #193D AS PER B737 SRM 51-70-05-2R-8. MATERIALS USED PO#1759850 SDR SWAA2022041885125Panel · elongatedREF TTG8Q003883M: LOWER WING TO BODY FAIRING 193D WITH MULTIPLE FASTENER HOLES ELONGATED / [01] ACCOMPLISH A PERMANENT REPAIR ON DAMAGE FASTENER HOLES ON NON ROUTINE TTG8Q00BCUSS;[02] VERIFIED 1;COMPLETESDR SWAA2022041885123Fairing · crackedREF TTG8Q003883M: LOWER WING TO BODY FAIRING 193D WITH MULTIPLE FASTENER HOLES CRACKED / [01] CLEANED FAIRING PANEL 193D FOR REPAIR AND PERFORMED DRY OUT; FOUND NO WATER AS PER B737 SRM 51-70-05-2R-8;[02] VERIFIED 1;OK TO INSTALL REPAIR;[03] REPAIRED ALL DAMAGSDR SWAA2022041885126Panel · elongatedREF TTG8Q003883M: LOWER WING TO BODY FAIRING 194E WITH MULTIPLE FASTENER HOLES ELONGATED / [01] PERFORMED VISUAL INSPECTION AT PANEL 194E ON ALL FASTENER HOLE FOUND MULTIPLE DAMAGED PER B737 NTM 51-05-01 AND PREPARED DAMAGED AREA TO APPLY DRY PROCESS PER B737 SDR SWAA2022040884674Fairing · elongatedREF TTG8Q002CAFX: LOWER WING TO BODY FAIRING 194E WITH MULTIPLE ELONGATED HOLES / [01] PERFORMED VISUAL INSPECTION AT PANEL 194E AROUND ALL FASTENER HOLES FOUND DAMAGED PER B737 NTM 51-05-01 AND PREPARED AREAS TO APPLY DRY PROCESS PER B737 SRM 51-70-05-2R-0 PASDR SWAA2022040884676Fairing · elongatedREF TTG8Q002CAFX: LOWER WING TO BODY FAIRING 193D WITH MULTIPLE ELONGATED HOLES / [01] PERFORMED VISUAL INSPECTION AT PANEL 193D AROUND ALL FASTENER HOLE FOUND MULTIPLE ELONGATED AND CRACK PER B737 NTM 51-05-01;[02] PREPARED PANEL193D TO APPLY DRY PROCESS PER SDR SWAA2022040584781Panel · brokenBROKEN ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE 2022-144875 / [01] REPLACED ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0;[02] REPLACED ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0 SESDR SWAA2022041283126Access Panel · crackedCRACK BELLY FAIRING HOLES ON FWD FACE OF ACCESS PANEL 194E AT LOWER FUSELAGE 2022-131657 / [01] TOOL USED: HOT BONDER P/N HCS9200B S/N 16122983 DUE DATE 16-JAN-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B; SN: 16122983; D/D: 16/JAN/23.;[03] TOOL USED: HOT BONDESDR SWAA2022041283131Access Panel · crackedCRACK BELLY FAIRING HOLES ON AFT POSITION OF ACCESS PANEL 193D AT LOWER FUSELAGE 2022-131658 / [01] TOOL USED: HOT BONDER P/N HCS9200B S/N 16122983 DUE DATE 16-JAN-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; SN: 16122983; D/D: 16/JAN/23.;[03] TOOL USED: HOT SDR SWAA2022041183070Panel · debondedPANEL 193CR HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1; TABLE 2; FIG. 2; ITEM 9. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA. 4.B.(5). <BR><BR>AREA IS TO BE REPSDR SWAA2022041183073Panel · debondedPANEL 193CL HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED MATERIAL OF PANEL 193CL IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(5)<BR><BR>REPSDR SWAA2022040883068Panel · debondedPANEL 193AR HAS SEVERAL DISBONDS TO INNER SURFACE OF PANEL CORE AREA; MARKED / [01] IDENTIFIED PART AND MATERIALS IAW SRM 53-40-70-0I-1 FIGURES 1-2; TABLE 2; ITEM[16] APPLIED BMS10-103 PRIMER & BMS10-60 ENAMEL IAW SRM 51-70-05-2R-2 PARA 4 STEP K.<BR>RE INSTALLSDR SWAA2022040683133Panel · elongatedELONGATED HOLE ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR 2022-129653 / [01] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED FLUKE -87 S/N 1937007SDR SWAA2022033182972Panel · delaminatedPANEL 193AR HAS DELAMINATION TO OUTER SKIN OVER CORE AREA (MARKED) / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 18. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIR TO BE ACCOMPLISHESDR SWAA2022041982729Access Panel · crackedCRACK ACCESS PANEL HOLES 194E WING TO BODY AT LOWER FUSELAGE 2022-122232 / [01] TOOL USED CALIPER P/N 500-196-30 S/N A21033416 DUE DATE 07-OCT-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 16-JAN-23.;[03] TOOL USED: HOT BONDER P/N: HCS9SDR SWAA2022032882646Fitting · crackedNOSE RADOME RH HINGE FITTING IS CRACKED / [01] REMOVED AND REPLACED NOSE RADOME HINGE FITTING I.A.W AMM 53-52-00-400-801;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2022041881510Panel · elongatedLOWER FUSELAGE FAIRING PANEL #194E SEVERAL SCREW HOLES ARE ELONGATED. / [01] CLEANED AND PREPARED LOWER FUSELAGE FAIRING PANEL #194E FOR REPAIR ON ALL ATTACHMENT HOLES AS PER B737 SRM 51-70-05-2R-8 AND AD 2020-03-10;[02] PERFORMED DRY OUT ON LOWER FUSELAGE FAISDR SWAA2022041881511Panel · elongatedLOWER FUSELAGE FAIRING PANEL #193D SEVERAL SCREW HOLES ARE ELONGATED. / [01] CLEANED AND PREPARED LOWER FUSELAGE FAIRING PANEL #194D FOR REPAIR ON ALL ATTACHMENT HOLES AS PER B737 SRM 51-70-05-2R-8 AND AD 2020-03-10;[02] PERFORMED DRY OUT ON LOWER FUSELAGE FAISDR SWAA2022032380567Fairing · delaminatedFAIRING PANEL # 194DL IS DAMAGED 14' AFT OF LEADING EDGE 16' FROM OUTBOARD EDGE OF PANEL / 2.40' DIAMETER DELAMINATION EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-60-70-1A-1 PARA 4 A (6).<BR>REPAIR TO BE PERFORMED IAW SRM51-70-05-2R-2 AS GIVEN IN SRM 53-60SDR SWAA2022030980410Panel · delaminated193B PANEL DELAMINATED ON INTERIOR SURFACE. / [01] DRILLED UP NEW 193B PANEL PER SRM 51-40-02;[02] REMOVED AND REPLACED 193B PANEL PER SRM 51-40-02SDR SWAA2022041880348Panel · corrodedTOILET SERVICE PANEL DOOR HAS SPOTS (02 EA) OF CORROSION AT INB CORNERS. / [01] REMOVED TOILET SERVICE PANEL DOOR FOR ACCESS AS PER REF B737-700 AMM 52-49-07-000-801;[02] FOUND EXFOLIATON AT TOILET SERVICE PANEL DOOR UPPER FWD AND AFT CORNER AND BONDING WIRE HSDR SWAA2022030980240Support Frame · cracked1.30' CRACK IN WING-TO-BODY FAIRING SUPPORT FRAME AT BS 500D; RBR 60; WL 192; MARKED IN BLACK. / [01] REMOVED R/H WTB PANEL 195AR AND 191AR IAW B737 AMM 53-51-21-000-803<BR><BR>REMOVED LOWER FAIRING SUPPORT AT STA 500D RBR60 WL 192 FOR PANELS 191AR AND 191FR ISDR SWAA2022032879973Fitting · crackedNOSE RADOME LH HINGE FITTING IS CRACKED / [01] REMOVED AND REPLACED NOSE RADOME LH HINGE FITTING PER REF AMM 53-52-00-400-801;[02] VERIFED CORRECTIVE ACTION 1SDR SWAA2022030379139Support · crackedRH LOWER WING TO BODY FAIRING 191AR PANEL LOWER SUPPORT FRAME CRACKED. / [01] REMOVED AND REPLACED SUPPORT FRAME REF SRM 51-40-02SDR DALA2022030201327None · noneTHE FORWARD RETAINER CLIP, ON THE COVER ASSEMBLY AT THE TAILCONE SLIDE, WAS FOUND BROKEN DURING STEP 13 OF JIC 5352-4002. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00286: A NEW CSDR SWAA2022032578145Panel · crackedPANEL 194E FWD & AFT EDGE HOLES SHOW SMALL CRACKS. (COUNTERSINK INCORRECT). / [01] REMOVED THE DAMAGED PLIES AROUND THE HOLES AND PREPARED REPAIR AREA TO DRY OUT. REF B737-700 SRM 51-70-05-2R-8 PARAGRAPH 4 AND SRM 51-70-05-2R-0 PARAGRAPH 4.;[02] VERIFIED STEP SDR SWAA2022031777860Panel · elongatedLOWER WING TO BODY FAIRING ACCESS PANEL 194E WITH MULTIPLE ELONGATED HOLES / [01] RECEIVED PANEL 194E. REF. TASK CARD TTG8Q002BGLR FOR PANEL INSTALLATION;[02] VERIFIED STEP 1.SDR SWAA2022031777861Panel · elongatedWING TO BODY FAIRING 193D WITH MULTIPLE ELONGATED HOLES / [01] REF. TASK CARD TTG8Q00B11LW FOR FAULT RESOLUTION.;[02] PANEL REPLACED ON TTG8Q00B11LWSDR SWAA2022032577098Panel · crackedPANEL 193D AFT EDGE HOLES SHOW SMALL CRACKS. (COUNTERSINK INCORRECT). / [01] PREPARED THE REPAIR AREA; NO CONTAMINATION AND WATER NOTE AT REPAIR AREA. REF B737 - 700 SRM 51-70-04-2R-9 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.;07] REPAIRED PANEL #193E AT ASDR SWAA2022040476539Panel · elongatedAFT WING TO BODY FAIRING PANEL 194E SHOWS 6 EACH ELONGATED FASTENER HOLES (MARKED) / [01] PERFOREMED VISUAL AND TAP TEST INSPECTION ON PANEL 194E AND FOUND ELONGATED FASTENER HOLES ALL AROUND THE PANEL AS PER B737 NDTM 51-05-01;[02] PREPARED DAMAGED AREA FOR DSDR SWAA2022032876811Fairing · erodedEROSION ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR 2022-98587 / [01] TOOL USED CALIPER P/N: 500-464 S/N: 15331932 DUE DATE: 26-OCT-22.;[02] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. TOOLSDR SWAA2022031176587Panel · elongatedLOWER FUSELAGE FAIRING PANEL 194E SEVERAL FASTENER HOLE ELONGATED / [01] RECEIVED NEW PANEL P/N: 149A7555-8; PO#1755416; ISSUE TAG: LC1394. THIS PANEL WILL BE INSTALLED ON CARD:TTG8Q002AL1C.;[02] VERIFIED STEP 1
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