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.

SDR SWAA2021122053018Panel · nonePANEL 193D PANEL FRETTING WEAR ; 193D AFT EDGE SHOW FRETTING WEAR ALONG FLL WIDTH OF PANEL. / [01] REMOVED AND REPLACED 193D PANEL REF 53-51-21Dec 14, 2021 · N736SA · Boeing 7377H4SDR SWAA2021122053020Structure · debondedTHREE FILLERS HAVE DISBONDED FROM 194E SUPPORT STRUCTURE. / [01] FABRICATED PER SOPM 20-50-20Dec 14, 2021 · N736SA · Boeing 7377H4SDR SWAA2021122053042Panel · elongatedAFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES. ; / [01] PREPPED PANEL 193D; NEEDS SEAL INSTALLED AND PAINT; [02] REMOVED AN REPLACE PANEL PER AMM 53-51-21Dec 14, 2021 · N7848A · Boeing 7377H4SDR SWAA2021122053044Panel · elongatedCENTER WHEEL WELL PANEL 193D HAS ELONGATED FASTENER HOLES. ; / [01] REPLACED 193D PANEL WITH SERVICEABLE PANELDec 14, 2021 · N7848A · Boeing 737752SDR SWAA2022010552765Panel · pulledSUPPLEMENTAL INFORMATION: PANEL 194E HAS FASTENER HOLES PULLED THROUGH AND ELONGATED ON THE LEADING AND TRAILING EDGE FASTENER HOLES. ; PANEL 194E HAS FASTENER HOLES PLLED THROGH AND ELONGATED ON THE LEADING AND TRAILING EDGE FASTENER HOLES. / [01] IDENTIFIED Dec 13, 2021 · N7888A · Boeing 737SDR SWAA2022010552766Panel · pulledPANEL 193D HAS FASTENER HOLES PULLED THROUGH ON THE AFT SIDE FASTENER ROW. ; PANEL 193D HAS FASTENER HOLES PLLED THROGH ON THE AFT SIDE FASTENER ROW. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4B(2). REMOVED DAMAGED PLIES AND CLEADec 13, 2021 · N7888A · Boeing 737752SDR SWAA2021121452503Panel · elongatedPANEL 193D HAS SEVERAL HOLES ELONGATED. ; / [01] INSTALLED SERVICEABLE 193D PANEL IAW AMM 53-51-21 NO FURTHER DEFECTS NOTEDDec 11, 2021 · N7878A · Boeing 7377K9SDR SWAA2021121452504Panel · elongatedPANEL 194E HAS SEVERAL HOLES ELONGATED. ; / [01] ACQUIRED SERVICEABLE 194E PANEL AND MATCH DRILLED TO EXISTING SUPPORT STRUCTURE PER AMM 53-51-21.; [02] INSTALLED SERVICEABLE 194E PANEL IAW AMM 53-51-21 NO FURTHER DEFECTS NOTED AT THIS TIME.Dec 11, 2021 · N7878A · Boeing 7377K9SDR SWAA2021121452102Panel · elongatedSUPPLEMENTAL INFORMATION: PNL 193D HAS (1) HOLE ELONGATED ; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21Dec 10, 2021 · N7884G · Boeing 737SDR SWAA2021121452101Panel · delaminatedSUPPLEMENTAL INFORMATION: PNL 194E HAS (4) EACH HOLES DELAMINATED ; / [01] INSTALLED NEW PANEL IAW AMM 53-51-21Dec 10, 2021 · N7884G · Boeing 737SDR SWAA2021121452100Panel · delaminatedSUPPLEMENTAL INFORMATION: PNL 193D HAS (4) EACH HOLE DELAMINATED ; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21Dec 10, 2021 · N7884G · Boeing 737SDR SWAA2021121351581Panel · crackedSUPPLEMENTAL INFORMATION: 194E PANEL HAS CRACKED AND ELONGATED HOLES / [01] REPLACED PANEL 194E PER AMM 53-51-21Dec 9, 2021 · N567WN · Boeing 737SDR SWAA2021121351580Panel · crackedSUPPLEMENTAL INFORMATION: 193D PANEL HAS CRACKED HOLES / [01] REPLACED PANEL 193D PER AMM 53-51-21Dec 9, 2021 · N567WN · Boeing 737SDR SWAA2021121351555Panel · elongatedSUPPLEMENTAL INFORMATION: PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02 AND SRM 51-40-05; [02] C/WDec 9, 2021 · N449WN · Boeing 737SDR DALA2021121007626None · none(LOG 2046514) DURING INSPECTION FOUND WORN SETTLEMENT AREA OF THE 193D CENTER WHEEL-WELL PANEL. 193D CENTER WHEEL-WELL PANEL WAS REPAIRED PER B 737-800 SRM 53-40-70-2R REPAIR 1 PAR 4 TABLE 202 AND B737-800 SRM 51-70-05-2R REPAIR 6.Dec 9, 2021 · N3736C · Boeing 737832SDR SWAA2021121351246Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 193D HAS 2 CRACKED HOLES / [01] INSTALLED NEW PANEL 193D PER AMM 53-51-21Dec 8, 2021 · N564WN · Boeing 737SDR SWAA2021121351222None · crackedSUPPLEMENTAL INFORMATION: AFTER REMOVING 193D PANEL FOUND AFT LEFT SUPPORT STRUCTURE WEB ? T ? AND VERTICAL CLIP CRACKED . ; / [01] RPL VERTICAL CLIP AND T CLIP PER SRM 51-40-02Dec 8, 2021 · N436WN · Boeing 737SDR SWAA2022012451326Fairing · crackedFAIRING 195CL IS CRACKED IN RADIUS AT AFT EDGE. ; / REMOVED DAMAGE FROM AFT RADIUS; AFT EDGEBAND; AND UPPER EDGEBAND; ALL ON INNER SURFACE; ALL DAMAGES CONNECT; VALIDATED REPAIR PER SRM 51-70-05-2R-6; FABRICATED REPAIR PLIES OUT OF BMS 8-79 ST 120 LOT#1476632-Dec 8, 2021 · N7865A · Boeing 7377Q8SDR SWAA2021121351179Panel · elongatedPANEL 193B HAS ELONGATED HOLES / [01] R/R?D 193B PANEL PER SRM 51-40-02Dec 8, 2021 · N298WN · Boeing 7377H4SDR SWAA2021121351008Panel · delaminatedSUPPLEMENTAL INFORMATION: 193D PANEL HAS AREA OF DELIMITATION ON EXTERIOR SKIN CENTER OF PANEL / [01] PREPARED PANEL FOR INSTALLATION; AND INSTALLED PANELDec 7, 2021 · N499WN · Boeing 737SDR SWAA2021121350803None · crackedSUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD TEE CLIP. ; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD TEE CLIP. / [01] INSTALLED NEW TEE CLIP PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED NEW TEE CLIP PER SRM 51-40-02 ANDDec 7, 2021 · N432WN · Boeing 737SDR SWAA2021121350788Panel · elongatedSUPPLEMENTAL INFORMATION: 194E PNL LEADING EDGE HAS 2 ELONGATED HOLES AND 2 DIMPLED AND CRACKED HOLES. TRAILING EDGE HAS 4 DIMPLED HOLES AND 3 OVERSIZED HOLES ; / [01] REMOVED AND REPLACED PANEL IAW AMM 53-51-21Dec 7, 2021 · N417WN · Boeing 737SDR SWAA2021121350802Support Angle · crackedSUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD VERTICAL SUPPORT ANGLE. ; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD VERTICAL SPPORT ANGLE. / [01] INSTALLED NEW VERTICAL ANGLE PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED Dec 7, 2021 · N432WN · Boeing 737SDR SWAA2021121350799Panel · elongatedSUPPLEMENTAL INFORMATION: 194E PANEL HAS ELONGATED HOLES WITH CRACKS EXTENDING FROM HOLES AT SEVERAL PLACES. / [01] DRILLED ; COUNTERSUNK ; TRIMMED NEW 194 E PANEL <BR>REF SRM 51-20-07Dec 7, 2021 · N432WN · Boeing 737SDR SWAA2021120950189Panel · elongatedSUPPLEMENTAL INFORMATION: 194E PANEL HAS 2 ELONGATED HOLES / [01] INSTALLED PANEL 194EDec 6, 2021 · N492WN · Boeing 737SDR SWAA2021120950188Panel · crackedSUPPLEMENTAL INFORMATION: 194E PANEL HAS 3 CRACKED HOLES / [01] REPLACED PANEL 194EDec 6, 2021 · N492WN · Boeing 737SDR SWAA2021120950127Panel · elongatedSUPPLEMENTAL INFORMATION: 193D PANEL HAS 9 FASTENER HOLES THAT ARE OVERSIZED / ELONGATED ; 193D PANEL HAS 9 FASTENER HOLES THAT ARE OVERSIZED ELONGATED / [01] EA 21-153-03624 DRAFTED AND ASSIGNED.; [02] REPAIRED 193D PANEL PER EA 21-153-03624.Dec 5, 2021 · N427WN · Boeing 737SDR SWAA2021120850182Panel · elongatedSUPPLEMENTAL INFORMATION: WING TO BODY PANEL 193D HAS 5(EA) FASTENER HOLES ELONGATED (MARKED) ; / [01] ACCOMPLISH EA 21-153-03619 ASSIGNED AS A SUBTASK.; [02] C/W AS PER EA GENERALDec 4, 2021 · N487WN · Boeing 737SDR SWAA2021120749830Panel · elongatedWING TO BODY PANEL 193D HAS 1(EA) FASTENER HOLE ELONGATED ; / [01] REPAIRED PANEL PER EA TTG8Q009MJZQDec 3, 2021 · N7811F · Boeing 73776NSDR SWAA2021122749358Panel · damagedDURING POST REPAIR UT INSPECTION FOUND DISBONDED SECTION IN REPAIRED AREA. FOUND ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIRED IAW SRM 51-70-05-2R-1 IAW SRM 53-40-70-2R-1 PAR 4B(1).Dec 2, 2021 · N455WN · Boeing 7377H4SDR SWAA2021122749590Panel · damagedPANEL 193CL HAS DISBOND OVER CORE ON INNER SURFACE NEAR I/B END. DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIRED IAW SRM 51-70-05-2R-1Dec 2, 2021 · N455WN · Boeing 7377H4SDR SWAA2021120649348Panel · cracked193D PANEL HAS 3 CRACKED HOLES / [01] INSTALLED NEW PANEL 193D PER AMM 53-51-21Dec 2, 2021 · N298WN · Boeing 7377H4SDR SWAA2021120649384Panel · delaminated194E PANEL ; THE 194E PANEL HAS 2 AREAS OF DELAMINATION ON SKIN FACE. / [01] REPLACEDec 2, 2021 · N709SW · Boeing 7377H4SDR SWAA2021120349526Panel · elongatedREF ID #TTG8Q009L8BP PANEL 194E HAS AN ELONGATED HOLE ON THE LEADING EDGE ; REF ID #TTG8Q009L8BP PANEL 194E HAS AN ELONGATED HOLE ON THE LEADING EDGE THE FIFTH FASTENER HOLE OVER CENTER OF PANEL MEASRING .400 AT LONGEST POINT AND .303 AT SMALLEST / [01] C/W EADec 2, 2021 · N211WN · Boeing 7377H4SDR DALA2021120607526None · noneTHE TAIL CONE RELEASE CABLE TURNBUCKLE IS BENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/001 00349: REPLACED BENT TURNBUCKLE REF B717 AMM 53-52- 01. (LP #203Dec 1, 2021 · N964AT · Boeing 717200SDR SWAA2021120349196Panel · elongatedFASTENER HOLE ELONGATED ; FASTENER HOLE ELONGATED PNL 194E FWD #6 FROM OTOARD. THIS TASK STEP #7. / [01] REPAIRED PER AMM 20-6?11-210<BR>INSTALLATION OF TINNERMAN WASHER; [02] ABOVE REFERENCE IS INCORRECT. REFERENCE SHOULD BE AMM 20-60-11-201; [03] VERIFIED C/Dec 1, 2021 · N211WN · Boeing 7377H4SDR SWAA2021120349223Panel · noneWING TO BODY PANEL 193D HAD FRETTING DAMAGE ; / [01] R AND R PANEL 193D PER AMM 53-51-21Dec 1, 2021 · N473WN · Boeing 7377H4SDR SWAA2021120349056Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02 AND SRM 51-40-04Dec 1, 2021 · N7828A · Boeing 7377CTSDR SWAA2021122748729Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ON FASTENERS HOLES ON PANEL 193D AT BODY FAIRING LOWER FUSELAGE ; 2021-544996 / [01] TOOL USED: CALIPER P/N 500-196-30 S/N A21029144 DUE DATE 07/OCT/22.; [02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 11-DEC-21Nov 30, 2021 · N7846A · Boeing 737SDR SWAA2021120348701Panel · delaminatedL/H LOWER WING TO BODY PANEL AFT OF L/H MAIN GEAR W/W PANEL 193CL IS DELAMINATED ; DELAM DIMENSIONS ARE APPROXIMATELY 12? Y 9.5? / [01] REPLACED PANEL PER MM 53-51-21Nov 30, 2021 · N781WN · Boeing 7377H4SDR DALA2021113007344None · noneTAIL CONE EXTERNAL RELEASE CLAMP OUT OF RIG LEFT AND RIGHT CLAMPS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0113:5352-4002/003 00423: RIGGED CLAMPS PER B717 AMM 53-52-01. ONov 28, 2021 · N953AT · Boeing 717200SDR SWAA2022010348071Access Panel · brokenSUPPLEMENTAL INFORMATION: BROKEN ACCESS PANEL 192DR BODY FAIRING RH FWD LATCH FUSELAGE EXTERIOR ; 2021-544461 / [01] REPLACED FWD LATCH ON ACCESS PANEL 192DR BODY FAIRING RH FUSELAGE EXTERIOR IAW BOEING 737-700 SRM 51-40-02-0G-0; [02] TASK COMPLETEDNov 26, 2021 · N462WN · Boeing 737SDR MK1Y20211126None · noneDURING MAINTENENCE INSPECTION FOUND CORROSION AT THE LOWER CHORD OF FORGED STIFFENER LOCATED AT THE BOTTOM OF THE KEEL STRUCTURE AT APP. STA 1011, RBL 6.0.Nov 26, 2021 · N31KJ · Boeing 76733ASDR SWAA2022010347743Access Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 192F ANTENNA AT LOWER FUSELAGE ; 2021-544349 / [01] REPLACED MARKER BEACON ANTENNA AT LOWER FUSELAGE IAW B737-700 AMM 34-32-11 AND PERFORMED INSTALLATION TEST. TEST IS OK <BR>SEE INDIVIDUAL SIGNOFFS BELOW; [02] JOB Nov 25, 2021 · N462WN · Boeing 737SDR SWAA2021112947500Fairing · cracked194E PNL HAS 1 DIMPLED AND CRACKED HOLE; AND 3 ELONGATED HOLES ON THE TRAILING EDGE ; / [01] REMOVED AN REPLACED WING TO BODY FAIRING PER AMM 53-51-21-401Nov 25, 2021 · N449WN · Boeing 7377H4SDR SWAA2021112947501Fairing · elongated193D PANEL HAS 7 OVERSIZED AND ELONGATED HOLES ON THE TRAILING EDGE ; / [01] REMOVED AN REPLACED WING TO BODY FAIRINGS PER AMM 53-51-21-401Nov 25, 2021 · N449WN · Boeing 7377H4SDR SWAA2021122046230Access Panel · crackedCRACK ACCESS PANEL 194E BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546045 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 18175478 DUE DATE: 05/AUG/22.; [03] TOOL USED: HOT BONDER P/N HCNov 21, 2021 · N562WN · Boeing 737790SDR SWAA2021122046231Access Panel · crackedCRACK ACCESS PANEL 193D BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546044 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 18175478 DUE DATE: 05/AUG/22.; [03] REPAIRED ACCESS PANEL 193D BNov 21, 2021 · N562WN · Boeing 737790SDR SWAA2021112446248Fairing · delaminatedRH MLG AFT W/W FAIRING DENTED & DELAMINATED. PANEL 194GR MEASURES 1.75'H X 4.25'W X 2/32'DREF LOGBOOK#1831149 ; / [01] REF LOG# 178451. COMPLY WITH MPM 3 DAYS METALLIC TAPE REINSPECT WITHIN 3 DAYS. PERMANENT REPAIR REQUIRED WITHIN 20 DAYS. OK TO CONTINUE PER MNov 20, 2021 · N755SA · Boeing 7377H4SDR SWAA2021112345823Panel · elongated193B PANEL HAS SEVERAL ELONGATED/DAMAGED HOLES. ; / [01] REPLACED PANEL PER SRM 51-40-02 AND SIPNov 19, 2021 · N493WN · Boeing 7377H4
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