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 SWAA2022071113445Access Panel · corrodedCORROSION STRAP LOCATED ACCESS PANEL 120CF AT BS 500D AND BTW STR 26R TO STR 26L FWD CARGO COMPARTMENT 2022-305571 / [01] NO FOUND ALLOWABLE DAMAGE IN B737-700 SRM. REPLACED STRAP LOCATED ACCESS PANEL 120CF AT BS 500D AND BTW STR 26R TO STR 26L FWD CARGO COMPASDR SWAA2022070113243Access Panel · crackedCRACK ACCESS PANEL 191AL BODY FAIRING AT LOWER FUSELAGE 2022-287621 / [01] TOOL USED: CALIPER P/N: 500-464 S/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 SCALE P/N: CL5000; S/N: AE-SDR DALA2022052703694Panel Support · corroded(LOG 2251341) DURING INSPECTION FOUND WEAR AND CORROSION ON FASTENERS HOLES AT PANEL SUPPORT STRUCTURE WERE ATTACHING AFT FAIRING PANELS 194E AND 193D STA 727. FASTENERS HOLES AT PANEL SUPPORT STRUCTURE WERE ATTACHING AFT FAIRING PANELS 194E AND 193D STA 727 ISDR SWAA2022070111104Access Panel · crackedCRACK ON LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE 2022-265989 / [01] REPLACED LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02.;[02] REPLACED LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-SDR IPXA2022060782932Floorboard · corrodedINSPECTION TYPE:CEXTERNAL WING TO BODY STRUCTURE LOWER T CHORD AT FS 1060 LBL WL 133 TO WL 211 HAS EXFOLIATION ON LOWER T CHORD LEGREMOVED EXFOLIATED T CHORD AND INSTALLED REPLACEMENT T CHORD PER SRM 51-40-02SDR 9LVA202206060001Fairing · crushedDURING GROUND HANDLING AT KTUL, LINE PERSONNEL FAILED TO DISCONNECT GPU FROM TUG BEFORE MOVING TUG. GPU CORD WRAPPED UNDERNEATH AFT FUSELAGE FAIRING AND CRUSHED FAIRING SKIN AND ATTACH SUPPORTS.SDR SWAA2022052610216Panel · delaminatedWTB FAIRING 194E HAS EXTERIOR COMPOSITE DELAM. (MARKED RED DOT 237-1) / [01] CLEANED DAMAGE AREA; CUT OUT DAMAGE SIZE .500' DIA. NO CORE DAMAGE; PERFORMED DRY OUT ; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-1;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPSDR SWAA2022053110098Panel · delaminatedPANEL 193AR HAS DELAMINATIONS ON THE OUTER SURFACE (2EA) UPON INSPECTION OF PANEL FOUND 1EA ADDITIONAL DELAMINATION ON OUTER SURFACE 5' FROM FWD EDGE; 21.5' FROM I/B EDGE. ORIGINAL DAMAGE NOTED; AND DAMAGE FOUND; IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-4SDR SWAA2022060609039Panel · debondedPANEL 195BL OUTER SKIN IS DISBONDED NEAR AFT EDGE. ( MARKED) / [01] IDENTIFIED PANEL 195BL IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 3.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6).<BR><BR>REPAIR TO BE ACCOSDR N6WA2022051902Attach Angle · corrodedFROM NRWO -185 BELLY AFT FAIRING BOTTOM ATTACH ANGLE IS CORRODED AT FS939. REMOVED AND INSTALLED NEW FAIRING BOTTOM ATTACHING ANGLE IAW CRJ SRM 51-42-06SDR SIMA20220517007Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP CORRODED FR-83 STR-28R MARKED. (LEVEL 2 CORROSION)-C/A-REMOVED CORRODED SHEAR CLIP AT FR-83 STR-28R FABRICATED AND INSTALLED NEW SHEAR CLIP IAW EMB-175 SRM 51-40-08, 51-40-02, AND ENVOY GPM 17-13.SDR SIMA20220517005Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP CORRODED FR-82 STR-28R MARKED (LEVEL 2 CORROSION)-C/A-REMOVED CORRODED FR-82 STR-28R SHEAR CLIP AND FABRICATED AND INSTALLED NEW SHEAR CLIP FOR FR-82 STR-28R IAW EMB-175 SRM 51-40-08, 51-30-01, SRMI 53-23-04 FIGURE 35 AND ITEM 230 AND SDR SIMA20220517006Clevis Pin · corrodedSSI 53-23-003 SHEAR CLIP CORRODED FR-84 STR-28R MARKED. (LEVEL 2 CORROSION)-C/A-REMOVED CORRODED FR-84 STR-28R SHEAR CLIP AND FABRICATED AND INSTALLED NEW SHEAR CLIP FOR FR-84 STR-28R IAW EMB-175 SRM 51-40-08, 51-30-01, SRMI 53-23-04 FIGURE 35 AND ITEM 230 ANDSDR SIMA20220517004Track · corrodedGALLEY LH FLOOR BEAM CORRODED JUST FWD OF LH LOWER SEAT TRACK. (LEVEL 2 CORROSION) -C/A-PERFORMED CUTOUT AS REQUIRED AND FABRICATED AND INSTALLED DOUBLER AND FILLER FOR REPAIR OF FWD GALLEY LH FLOOR BEAM JUST FWD OF LH LOWER SEAT TRACK IAW ERS-EJ-53MR-4547SDR SIMA20220517003Floor Skin · corrodedRH FLOOR SILL IN FWD GALLEY CORRODED AT FRAME 14 (LEVEL 2 CORROSION)-C/A-RAR RH FLOOR SILL IN FWD GALLEY AT FR 14 IAW EMB-175 SRM 51-40-08SDR DALA2022052003473None · none(LOG 2238208) DURING INSPECTION FOUND DELAMINATED AND ELONGATED FASTENERS HOLES AT AFT-WING-TO-BODY FAIRING 193D. FAIRING 193D WAS REPAIRED PER B737-800 S.R.M. 53-40-70-2R AND B737-800 S.R.M. 51-70-05-2R.SDR SIMA20220515005Floor Panel · corrodedSSI 53-23-005 : AFT GALLEY AREA RH FLOOR PANEL SUPPORT AFT OF SERVICE DOOR CORRODED IN MULTIPLE AREAS-C/A-RAR AFT GALLEY AREA RH FLOOR PANEL SUPPORT AFT OF SERVICE DOOR IAW EMB-175 SRM 51-40-08SDR SIMA20220515004Shear Tie · corrodedSSI 53-23-005 AFT GALLEY AREA CENTER SHEAR PANEL CORRODED IN MULTIPLE AREAS. (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY AREA CENTER SHEAR PANEL IAW EMB 175 SRM 51-40-08SDR SIMA20220515003Panel Support · corrodedSSI 53-23-005 : AFT GALLEY AREA RH SHEAR PANEL CORRODED IN MULTIPLE AREAS (LEVEL 2 CORROSION) -C/A-RAR AFT GALLEY RH SHEAR PANEL IAW ERJ 175 SRM 51-40-08SDR SWAA2022051908078Panel · delaminated193B PANEL HAS LEADING EDGE DELAMINATION AND EDGE EROSION IN BOTH FWD CRONERS OF PANEL APPROX 3.00X3.00 AREA. / [01] REMOVED AND INSTALLED NEW PANEL #193 IAW AMM 51-51-21.SDR SWAA2022061407709Panel · corrodedPANEL 192F LWR SURFACE HAS CORROSION AT 3 ANTENNA MOUNT AREAS. 8-80 / [01] RECEIVED NEW PANEL 192F ; THIS PANEL WILL BE INSTALL ON TTG8Q00BGPCF;[02] VERIFIED 1SDR SWAA2022051707250Panel · damagedPANEL 193B HAS SEVERAL ELONGATED HOLES / [01] REMOVED AND REPLACED PANEL PER SRM 51-40-02;[02] C/W INSPECTIONSDR SWAA2022060807573Panel · crackedCRACK ACCESS PANEL 194HR BODY FAIRING AT LOWER FUSELAGE 2022-283834 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:15120589 DUE DATE: 28 NOV 22.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 16/JAN/23.;[03] TOOL USED: SCALE P/N SCA-301 S/N AE-41SDR SWAA2022051607382Panel · crackedREF L/P 1995181; DAMAGE TO PANEL 194 GL ; MINOR CRACK (2ND) / [01] COMBINED THIS MINOR CRACK INTO THE FIRST CRACK PER ENGINEERING AND SRM 53-60-70-1A-1 FIG 104SDR VNAA2022062699911Fairing · corrodedCORROSION ON SETTLEMENT AREA OF FAIRING 193AB EXTERNAL STRUCTURE FS800.SDR SWAA2022053105676Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR 2022-239313 / [01] TOOL USED: CALIPER: P/N:500-197-30 S/N:15120589 DUE DATE:28-NOV-22;[02] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18164925 DUE DATE: 16-JAN-23;[03] TOOL USED SCALE PN SCA-301 SNSDR SWAA2022061405222Panel · bulgedPNL 193B HAS INNER SURFACE AT SCREW HOLES BULGING. 8-48 / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #193B AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL PER B737 NDTM 51-05-01;[02] PREPARED PANEL 193B AT DAMAGED AREA FOR REPAIRSDR IPXA2022050681822Bracket · brokenINSPECTION TYPE:SEGFUSELAGE TAIL CONE 317AL HOLD OPEN ROD ATTACHMENT BRACKET WORN.REMOVED AND REPLACED IAW SRM 54-42-21SDR SWAA2022050402937Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. / [01] REPLACED PANEL 193B PER SRM 51-40-02;[02] C/W INSPECTION.SDR SWAA2022052602073Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-228392 REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP.2; REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-SDR SWAA2022052602063Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-230783 / REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP. 2; REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-SDR SWAA2022052601666Panel · elongatedFILLET FAIRING 193B HAS SEVERAL ELONGATED FASTENER HOLES / [01] PERFORMED VISUAL INSPECTION AND TAP TEST AT FAIRING PANEL #193B FOUND SEVEN ELONGATED FASTENER HOLES AS PER B737 NTM 51-05-01;[02] VERIFIED STEP 1;[03] PREPARED DAMAGED AREA TO APPLY REPAIR AT PANSDR SWAA2022060601130Fairing · crackedWING TO BODY FAIRING 194HL HAS CRACKS AROUND FASTENER HOLES. / [01] PREPARED 3EA FASTENER HOLE TO APPLY REPAIR AT PANEL 194HL PER B737 SRM 51-70-04-2R-0;[02] VERIFIED STEP 1;[03] OK TO INSTALL REPAIR;[04] REPAIRED 3EA FASTENER HOLE AT PANEL 194HL PER B737SRM 5SDR SWAA2022060601137Fairing · crackedWING TO BODY FAIRING 191FR WITH CRACKS AROUND FASTENER HOLES. / [01] CLEANED AND PREPARED DAMAGE FASTENERS HOLES FOR REPAIR ON WING TO BODY FAIRING 191FR;PERFORMED DRY OUT ;FOUND NO WATER AS PER B737 SRM 51-70-04-2R-9;[02] VERIFIED CLEAN.<BR>OK TO INSTALL REPASDR SWAA2022060601135Fairing · delaminatedWING TO BODY FAIRING 194HL; CORNER DELAMINATED. / [01] PERFORMED VISUAL INSPECTION & TAP TEST AT FAIRING PANEL 194 HL ON DAMAGED AREA NO WATER FOUND ONLY DELAMINATION FOND SIZE 3X2'' PER B737 SRM 51-70-04-2R-0 AND B737NTM 51-05-01;[02] PREPARED DAMAGED AREA TOSDR SWAA2022050200068Panel · elongated193B PANEL HAS NUMEROUS ELONGATED FASTENER HOLES. / [01] REPLACED 193B PANEL PER SRM 51-40-02SDR SWAA2022051100073Panel · pulledPANEL 191FR FWD AND AFT ENDS HAS SEVERAL PULLED FASTENER HOLES. / [01] IDENTIFIED MATERIAL OF PANEL 191FR ACCORDING TO SRM 53-30-70-0I-1; FIG. 2; ITEM# 4; TABLE 2.<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS ACCORDING TO SRM 53-30-70-1A-1; TABLE 101; PARA SDR SWAA2022050397141Panel · crackedPANEL 194HL HAS HOLE AND CRACK IN CENTER O/B SURFACE. / [01] PERFORMED TAP TEST AT PANEL 194HL FOUND NO DELAMINATION AND NO WATER ; NO CORE DAMAGE AS PER B737 NTM 51-05-01;[02] PREPARED FOR REPAIR 2 SMALL AREA AT PANEL 194HL CENTER O/B SURFACE AS PER B737 SRM SDR SWAA2022050296312Skin · debondedINNER SKIN DISBONDED FROM CORE. MARKED IN RED. / [01] IDENTIFIED PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 9.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6).<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SSDR N6WA2022042502Web · crackedCRACK FOUND APPROX 1.0" ON FUSELAGE WEB AFT LOWER CORNER RADIUS. STA 909 BL 20L WL 50. AS MARKED. REPAIR ON FUSELAGE WEB L/H AFT LOWER CORNER IAW EO C550-53MIR-002-OSDR SWAA2022051194596Panel · delaminatedPANEL 194CL HAS A DELAMINATED DENT ON THE OUTER SKIN. (MARKED) / [01] IDENTIFIED PART AND MATERIAL IAW SRM 53-60-70-0I-1; FIGURES 1-2; TABLE 3; ITEM [6].<BR>FOUND DAMAGE TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PAR 4.A (4) BUT WILL ACCOMPLISHSDR SWAA000094360Panel · delaminatedFAIRING PANEL 193CL DELAMINTAED FWD EDGE / [01] IDENTIFIED FAIRING PANEL 193CL IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 9.<BR><BR>UPON INSPECTION OF PANEL FOUND DELAMINATION TO EXTEND OVER HONEYCOMB CORE ON FWD EDGE. DAMAGES ARE OUT OF ALLOWABLE SDR SWAA2022050294357Panel · delaminatedFAIRING PANEL 193CR DELAMINTAED FWD EDGE / [01] IDENTIFIED FAIRING PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 9.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4B(8). <BR><BR>REPAIR TO BE ACCOMPLISHED IASDR SWAA2022050393747Panel · elongatedMID LOWER FWD BODY FAIRING PANEL #191D; FASTENER HOLES ELONGATED/CRACK/DELAMINATED. (DOT-009). / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #191D AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL AS PER B737 NDTM 51-05-01;[02] PREPSDR SWAA2022050394089Panel · delaminatedPANEL 193AL SEVERELY DELAMINATED- MARKED / [01] REMOVED DAMAGE PER SRM 51-70-05-2R-1 AND SRM 51-70-14-2R-4.;[02] VERIFIED REMOVED DAMAGE PER SRM 51-70-05-2R-1 AND SRM 51-70-14-2R-4.;[03] REPAIRED IAW SRM 53-60-70-2R-1; SRM 51-70-05-2R-1; AND SRM 51-70-14-2R-1.SDR SWAA2022050493536Panel · elongatedELONGATED HOLE ACCESS PANEL 193D (9EA) AT LOWER FUSELAGE 2022-165397 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE:28-SEP-22.;[02] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N: 18185781 DUE DATE: 16-JAN-23;[03] TOOL USED P/N HCS9200B-AV S/N 18196127SDR SWAA2022042694053Panel · elongatedPANEL 194 E MULTIPLES ENLONGATED FASTENERS HOLES (ALL AROUND) / [01] MEASUREMENTS;[02] CLEAN AND PREPARED DAMAGE FASTENERS HOLES FOR REPAIR ON LOWER WING TO BODY FAIRING PANEL 194E AS PER B737 SRM 51-70-05-2R-8;[03] PERFORMED DRY OUT ON DAMAGE AREA ; FOUND NO SDR SWAA2022042193523Panel · delaminatedPANEL 193AR HAS 2 DELAMINATED AREAS ON OUTER SURFACE SKIN AS NOTED ON FAULT TTG8Q00BMNQU / [01] IDENTIFIED PANEL 193AR MATERIAL IAW SRM 53-40-70-0I-1 TABLE 2 FIGURE 2 ITEM 18. DELAMINATED SKIN AT DISCREPANT LOCATIONS OVER HONEYCOMB CORE EXCEED ALLOWABLE DAMAGESDR SWAA2022050293166Panel · delaminatedPANEL 193AR IS DELAMINATED ON INNER SURFACE 7.5' AFT OF FWD EDGE; 20' OB OF IB EDGE / [01] IDENTIFIED MATERIAL OF PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 18; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PASDR SWAA2022050293168Panel · delaminatedPANEL 193AL HAS DELAMINATION OF OUTER SURFACE ALOND LEADING EDGE; 38' OB OF IB EDGE / [01] IDENTIFIED MATERIAL OF PANEL 193AL IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 7; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PAR
Back to JASC 5350