JASC 5350
Service difficulty reports · 6,121
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 SWAA2023081077915Bracket · crackedLEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8.<[01] REMOVED AND REPLACED ECS BAY DUCT SUPPORT BRACKET 212A1116 IAW SOPM 20-50-01;[02] VERIFIED PARTS REQUIREMENTS.;[03] VERIFIED CORRECTION ACTION 1;2 AND MEASUREMENT TASDR SWAA2023081476758Panel · crackedCRACK BULKHEAD PANEL 142NW PLATE THAT ATTACH THE LOWER EDGE LOCATED AT BS727 APPROX AT AFT CARGO COMPARTMENT 2023-443865<[01] REPLACED BULKHEAD PANEL 142NW PLATE THAT ATTACH THE LOWER EDGE LOCATED AT BS727 APPROX AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40SDR DALA2023071305675Unknown · unknownTHE TAIL CONE RELEASE CAM IS CLOCKED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED THE RELEASE CAM REF AMDS WORKCARD 5352-2001. (LP #2859456)SDR SWAA2023071076541Compound · damagedLEVEL FLT AT FL380; OBSERVED LOUD HUMMING AND VIBRATION CABIN PRIMARILY ROWS 2 THRU 8; WITH VIBRATION IN FLOOR. LEVEL FLT AT FL380 OBSERVED LOUD HUMMING AND VIBRATION CABIN PRIMARILY ROWS 2 THRU 8 WITH VIBRATION IN FLOOR. NOT CERTAIN HOW LONG THAT WAS PRESENT SDR SWAA2023071875272Bracket · crackedDOT A24-07 RH WING I/B L/E WING TO BODY FAIRING / L/E SUPPORT STRUCTURE ANGLE CRACKED AT FASTENER HOLE. MARKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PESDR SWAA2023070675186Panel · delaminatedFOUND DELAMINATION ON PANEL 194GR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.SDR SWAA2023070675185Panel · delaminatedFOUND DELAMINATION ON PANEL 194CR<[01] COMPLIED WITH EA 23-153-02086.;[02] C/WSDR SWAA2023070574255Panel · damagedWING-TO-BODY FAIRING PANEL 193AR; AFT ATTACH ANGLE HAS 4EA. OBLONG AND OVERSIZED NUT PLATE HOLES.<[01] C/W EA 23-153-02054 (N420WN - SWA - REPAIR - WING-TO-BODY FAIRING PANEL 193B; 193AL; 193AR ELONGATED HOLES AND SUPPORT STRUCTURE- TIME-LIMITED)SDR DALA2023063005251Unknown · unknownWHILE PARKED A UAL AL STRUCK OUR TAIL. DAMAGE ON TAILCONE. PREFORMED HFEC OF REWORKED AREA AND STRINGER 13LH, 17LH, AND 19LH OER ERA 609834-14 REV ORG. NO CRACKS FOUND. QC 5237. REMOVED TAILCONE SECTION AT STA 84 PER SRM 51-42. WIP PET 374796 . REINSTALLED TAISDR DALA2023063005243Unknown · unknownWORKING AA WORKCARD #5352-01038-01A WTB SUPPORT STRUCTURE INSPECTION. DURING WTB FAIRING SUPPORT STRUCTURE INSP IAW AD RELATED WORKCARD 5352-0138-01A FOUND CRACKS UNDER NUT PLATES ON RH LONGERON AT RBL 40.0 P/N 53-1111-502. CRACKS LOCATED ON OUTBOARD SIDE OF LSDR SWAA2023081472270Panel · delaminatedDELAMINATED ACCESS PANEL 193B AT LOWER FUSELAGE 2023-413130<[01] TOOL USED; CALIPER P/N: 500-197-30 S/N: 15120589 DUE DATE 13-FEB-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185733; DUE DATE: 23-JAN-24;[03] TOOL USED: SCALE P/N: CR5200; S/N: 834251SDR SWAA2023062370528Panel · delaminatedPANEL 193B LH AND RH EDGES DELAMINATED; REQUIRES REPLACEMENT<[01] R&R?D PANEL 193B REF AMM 53-51-21.SDR DALA2023062005005Unknown · unknownWHILE PERFORMING WORKCARD 5352-01038-01A, FOUND DAMAGE ON LONGERON STEP 10 D. R/R LT LONGERON P/N C02383111-001. C/W WORK CARD 5352-01038-07A. A/C OK FOR SVC. (LP# 4748362)SDR SWAA2023061959065Panel · pulledPANEL 193AR HAS 1 PULLED THROUGH FASTENER AND SEVERAL OTHERS EITHER LOOSE OR PULLING THROUGH. (M)<[01] REMOVED DAMAGE PER SRM 51-70-05-2R-8-B00325;[02] 1. KENNETH KARNES (TECHNICIAN); 14-JUN-2023 18:51 UTC<BR>REMOVED DAMAGE PER SRM 51-70-05-2R-8-B00325. INSPECSDR SWAA2023061658986Panel · crackedPANEL 193B HOLE #9 HAS A CRACK 1.125 INCH LONG EXTENDING THROUGH THE FASTENER HOLE TO THE EDGE OF THE PANEL<[01] REMOVED WB PANEL 193B PER TASK CARD 5351-I-14108-NG.;[02] PANEL 193B HOLE #9 WAS REPAIRED IN REF TO EA 23-153-01896.;[03] VERIFIED PANEL 193B HOLE SDR DALA2023061304808Unknown · unknown(LOG 4798938) FOUND DAMAGE ON BODY PANEL 192F NEAR DME#1 ANTENNA. DAMAGE SIZE 1 1/2" BY 1/2". ACCOMPLISHED REPAIR PER B737 SRM 53-40-70-2R PROCEDURE 1.SDR SWAA2023071257574Panel · crackedPANEL 194GR HAS TWO CRACKS OF 1/2' AND 3/8' ON THE UPPER SIDE AS MARKED<[01] APPLIED REPAIR ON PANEL #194GR PER B737 SRM 51-70-04-2R-1 PARA 4.F. MATERIALS USED CLOTH P/O#1690463; RESIN P/O#1800550;[02] VERIFIED AND INSPECTED REPAIRED; PRIMED AND TOPCOAT ACCESSSDR SWAA2023071257577Panel · delaminatedPANEL 191FR HAS DELAMINATION AT THE UPPER SIDE 2.5' L. BY 1' W. AS MARKET<[01] APPLIED REPAIR ON PANEL #191FR PER B737 PARA 4.L. MATERIALS USED RESIN P/O1800550; CLOTH P/O#1690463;[02] APPLIED REPAIR ON PANEL #191FR AS PER B737 SRM 51-70-04-2R-13. MATERIALS USSDR SWAA2023071055311Panel · elongatedELONGATED HOLE ACCESS PANEL 191HR AT LOWER FUSELAGE 2023-365410<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] TOOL USED MICROMETER PN: 293-344-30 ; SN: 71735394 DUE DATE 23-NOV-23;[03] TOOL USED: TEMPERATURE CONTROLLER P/N SDR SWAA2023062054086Fairing · elongatedELONGATED HOLE ON BODY FAIRING PANEL 191D AT LOWER FUSELAGE 1 EA 2023-330451<[01] TOOL USED CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 22/JAN/24;[03] TOOL USED HOT BONDER P/N HSDR SWI2023F00107Unknown · corrodedAFT WING TO FUSELAGE FAIRING ATTACHMENT FLANGE HAS MULTIPLE AREAS OF CORROSION AT THE AFT 6 O'CLOCK POSITION. (C-CHECK RO 6/28/2023) REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING ATTACHMENT FLANGE (2 EA) AT THE AFT 6 O'CLOCK POSITION REF EMB SRM 51SDR DALA2023053004318Unknown · unknownSHIP 3351 CRACK SUPPORT WEB BELLY FAIRING LOC. ON FR53.2 L/H SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REF ER/A 608483-14. (2787995)SDR SWI2023F00149Unknown · damagedFOUND DOUBLE HOLE ON TAIL CONE 361AL (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DOUBLE HOLES IN TAILCONE PANEL 361AL PER MHIRJ REO 601R-53-84-335 REV -- DATED 07-10-2023, SEE CONTINUE CARD FOR DETAILS OF REO REPAIR.COMPLIED WITH SKYWEST TASK CARD 51-900-1SDR DALA2023052604201Unknown · unknownSHIP 660 CORROSION ON WING TO BODY FRAME BSTA 1040 BTW RBL 5 TO RBL 25. CORRECTIVE ACTION: SUMMARY OF NRC 00283: BODY FRAME BSTA 1040 BTW RBL 5 TO RBL 25 WAS REPLACED PER B757-200 SRM. (2782548)SDR CALA2023052601662Seal · vibrationABNORMAL AIRFRAME VIBRATION FLAPS 1 IN CLMB FLAPS 2 3 4 IN DESEN T REPAIR REF SRM 53-45-00-005. DAILY REINSPECT OF TAPE REQ. SEAL FLT HOURS. TO BE REPLACED AT EARLIEST OPPORTUNITY BUT NOT LATER THAN 600 FOUND AFT RIGHT EDGE SEAL LOOSE ON BELLY FAIRING PANEL 1SDR SWAA2023052551686Panel · elongated193B PANEL HAS ELONGATED FASTENER HOLES AT POSITIONS 2; 4; 5; 6; 7; 9; 10; 13; 14; 15; 16; 18; 19; 21; 24; 25; 28; 29; 30; 31; 33; 35; 36; 37 AND 38. 193B PANEL HAS ELONGATED FASTENER HOLES AT POSITIONS 2 4 5 6 7 9 10 13 14 15 16 18 19 21 24 25 28 29 30 31 33 SDR SWAA2023062950997Panel · delaminatedPANEL 194FR HAS A DELAMINATION ON THE OUTER SKIN (MARKED)<[01] IDENTIFIED PANEL IAW SRM 53-60-70-0I-1 FIGURE 2 ITEM [2] DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARAGRAPH 4.A.(6).(B) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-2 PER SRSDR CALA2023052401622Radome · damagedBIRDSTRIKE AFTER ROTATION FOUND BIRDSTRIKE ON LH SIDE OF RADOME JUST FWD OF PITOT. BIRD REMAINS WENT INSIDE OF THE CAPTAINS PITOT. PICTURES ATTATCHED PERFORMED BIRD STRIKE INSPECTION OF RADOME LEFT HAND AREA AND PITOT PROBE, NO DEFECTS NOTED. REF AMM 05-51-18-SDR CALA2023052201588Fairing · missingPDA 2 NO.4 M.L.G. HUBCAP MISSING ON ARRIVAL. NO DAMAGE NOTED. INSTALLED SERVICEABLE HUBCAB FAIRING REF TASK 32-45-11-400-801. OKAY FOR SERVICE. PARTS USED: 29-3242-3-0007,QTY :1 ADD EMP:U389132SDR SWAA2023062150067Plate · corrodedCORROSION BELLY FAIRING SUPPORT PLATE CUTOUT ON ACCESS PANEL 191E AT LOWER FUSELAGE 2023-330316<[01] REPLACED BELLY FAIRING SUPPORT PLATE CUTOUT ON ACCESS PANEL 191E AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED BELLY FAIRING SUPPORT SDR SWIA202306280515Unknown · corrodedRH WING TO FUSE/MLG SIDE BRACKET FWD, SEALANT COVERING NUT WAS NOT COMPLETLY SEALED AND APPEARS TO HAVE RUST BLEEDING FROM IT. SEALANT NEEDS TO BE REMOVED FOR INSPECTION. FLAGGED (C-CHECK RO 6/25/2023) REMOVED RH MLG SIDE-BRACE SHAFT FITTING CAP SEAL ANSDR SWAA2023061448619Panel · crackedCENTER LOWER AFT FAIRING ACCESS PANEL # 194E WITH MULTIPLE FASTENER HOLES BULGING AND CRACKED ON EDGES INNER SIDE<[01] REMOVED DAMAGED AND PREPARED AREA FOR REPAIR AS MARKED ON ACCESS PANEL #194E AS PER B737 SRM 51-70-04-2R-9; APPLIED THE GLASS FABRIC REPAIR PSDR SWAA2023062148301Panel · elongatedELONGATED HOLE ACCESS PANEL 192AR AT LOWER FUSELAGE 2023-330060<[01] TOOL USED CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18185733; DUE DATE: 23/JAN/24.;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV;SDR FDEA202305120864Filler · corrodedT-CHORD FILLER FOR UNDER WING TO BODY FAIRING IS CORRODED BETWEEN BS 900-BS 950 REMOVED AND REPLACED PER BOEING DWG # 149N7320 REV ESDR SWIA202306260508Unknown · elongatedUPON REMOVAL OF RH MLG BAY UPPER WING SKIN PANEL FOR JOB 27853101 OP 360 MXTRANS# 26587440, FOUND MOST INBOARD FWD HOLE TO BE ELONGATED (1 EA) (C-CHECK RO 6/20/2023) PERFORMED REPAIR TO OVERSIZED FASTENER HOLE ON WING BOX UPPER INBOARD SKIN AT WS48.30 ASDR SWIA2023062100013Unknown · corroded* AFT FUSELAGE TO WING FAIRING SUPPORT FRAME AT FS 939.00 HAS CORROSION ON LOWER FLANGE NEAR CENTER AND AROUND SEVERAL SCREW HOLES ON LOWER SIDE OF LOWER FLANGE. (C-CHECK RO 6/19/2023) REMOVED AND REPLACED PART P/N-SH670-39189-3 WITH NEW ONE . REF: CRSDR DALA2024011200550Unknown · unknownSHIP 5807 DENT FOUND ON TAIL CONE AFTER OF VERTICAL FIN ABOVE APU. CORRECTIVE ACTION: INSTALLED TIME LIMITED REPAIR PER B757-- 300 SRM 53-80-01-1A NOTE "C". (2755875)SDR SWAA2023051046553Radome · delaminatedPUNCTURE AND DELAMINATION<[01] FOUND RADOME PUNCTURE AND DELAMINATION; REMOVED AND REPLACED RADOME IAW AMM 53-52-00SDR SWAA2023050545460Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS.<[01] REMOVED AND REPLACED PER SRM 53-51-01.SDR DALA2023050903634Unknown · unknownWORKING AMDS CARD JIC 5352-01038-01A FOUND CRACK IN LONGERON AT LBL40.0 APPX 4 INC VERTICAL FROM TOP TO BOTTOM CAP AT JUNCTION OF FRAME. AD RELATED WORKCARD 5352-01038-01A. ATTACHED AMDS WORK CARD 5352-01038-07A FOR LONGERON REPLACEMENT. REPLACED LHS LONGERON SDR SWAA2023050544877Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS.<[01] REMOVED AND REPLACED PANEL PER SRM 51-40-02.SDR SWAA2023050343316Panel · elongatedPANEL 193B HAS SEVERAL ELONGATED; OVERSIZED FASTENER HOLES AND DAMAGED COUNTERSINKS.<[01] LOCATED HOLES IN NEW PANEL PER SRM 51-40-05;[02] REMOVED AND REPLACED 193BB PANEL PER AMM 53-51-21SDR SWIA2023050100021Unknown · gougedFOUND GOUGE ON RH SIDE OF AC TAIL (ZONE 310) FWD OF AFT EQUIPMENT DOOR (FILED CLOSED)COMPLETED PERMANENT REPAIR ON RH SIDE OF AC TAIL (ZONE 310) FWD OF AFT EQUIPMENT DOOR IAW ETD2023-170-011080 REV.:/ DATED 4/29/23SDR DALA2023101808594Fastener · looseSHIP 171 FOUND MISSING AND AN ADJACENT LOOSE FASTENER ON THE LOWER FWD END OF LEFT ENGINE AFT STRUT FAIRING PANEL #437DB. CORRECTIVE ACTION: C/W TIME-LIMITED REPAIR AS PER ERA 608419-14 REV ORIG. REQUUIRES REPETITIVE INSPECTIONS EVERY 100 FLIGHT HOURS WITH TERSDR SWAA2023061342523Panel · elongatedCENTER WHEEL WELL ACCESS PANEL 193D LOWER SKIN SURFACE HAS FASTENER HOLE ELONGATED.<[01] REPAIRED ACCESS PANEL #193D AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED RESIN PO#1800550 AND CLOTH PO#1738579.;[02] VERIFIED STEP 2;[03] CORRECTION: VERIFIED STEP 1SDR SWAA2023061343145Panel · elongatedACCESS PANEL 193B HAS ENLONGATED HOLES (COMPOSITE AREA)<[01] APPLIED REPAIR ON DAMAGED AREA AT ACCESS PANEL#193B AS PER B737 SRM 51-70-04-2R-9. MATERIAL USED RESIN PO#1800550 AND CAB PO#1776837 AND CLOTH PO#1738579 AND APPLIED TOPCOAT TO ACCESS PANEL 193B PER SDR CALA2023042801286Radome · damagedBIRD STRIKE AFTER TAKEOFF BELOW F/O''S WINDOW AND TOP END OF RADOME. PERFORMED BIRD/HAIL STRIKE CONDITIONAL INSPECTION IAW AMM TASK 05-51-18-210-801, CLEANED AREA IAW AMM 12-40-04-100-801, NO DAMAGE FOUND ON RADOME AND F/O''S R1 WINDOW.SDR SWAA2023060141585Skin · debondedPANEL 191D OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED MATERIAL OF PANEL 191D IAW SRM 53-30-70-0I-1 FIGURE 1-2; ITEM 9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-70-1A-1 TABLE 101; PARA 4.A(4)<BR><BR>REPAIR TO BE ACCOMPLISHED SDR SWAA2023060141589Skin · debondedPANEL 194FR OUTER SKIN HAS A DISBOND. (MARKED)<[01] IDENTIFIED MATERIAL OF PANEL 194FR IAW SRM 53-60-70-0I-1 FIGURE 1-2; ITEM 2; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 TABLE 101; PARA 4.A(4)<BR><BR>REPAIR TO BE ACCOMPLISHSDR SWAA2023053146362Panel · crackedR/H OVERWING FAIRING ACCESS PANEL # 195CR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REMOVED PANEL 195CL FOR ACCESS REF B-737-700 SRM 51-40-02-0G-0
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