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 SWAA2023102601355Bracket · crackedLEFT WING-TO-BODY FAIRING - CRACKED BRACKET ASSY-DUCT SUPPORT; L/H PACK BAY (MARKED)<[01] LH PACK BAY SUPPORT BRACKET CRACKED NO ALLOWABLE DAMAGE NOTED ON SRM. PART TO BE REPAIR BY REPLACEMENT. PN 212A1116-1. IAW SRM 51-10-02-0G-0 PARA 9.;[02] REMOVED AND REPLSDR SWAA2023102401030Tail Cone · debondedTAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE<[01] TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-04-2R-2.;[02] VERIFIED THE REPAIR OF THE TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROSDR SWAA2023101701226Panel · delaminatedBODY FAIRING PANEL# 192BL EXTERIOR SURFACE LEADING EDGE AND CORNER ERODED AND DELAMINATED.<[01] APPLIED REPAIR IAW SRM 51-70-05 REPAIR #10.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] REPAIRED IAW SRM 51-70-05 REPAIR # 10; SEALED REPAIR IAW SRM 51-70SDR FDEA202309151629Panel · damagedPANEL 195GL PN 113T1740-275 DAMAGED. REPAIRED PANEL IN REF. TO EA# H-5350-T0376218 P1SDR IPXA2023092794259Support Frame · crackedINSPECTION TYPE:1C#1 PACK FAIRING 143FL AFT SUPPORT FRAME CRACKED ON I/B END.REMOVED, FABRICATED, AND REPLACED IAW SRM 51-40-21.SDR DALA2023092107774Unknown · unknownWEAR ON CAM ASSY OF TAIL CONE RELEASE MECHANISM AT THE 10:00 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC #00025: BASE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52SDR LR7A2023091303302Fairing · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND CENTER WING FUSELAGE FAIRING CRACKED AT FS598, WL282, RBL18. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001002070.SDR SWAA2023101999696Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR 2023-584194<[01] TOOL USED: HOT BONDER PN: HOT BONDER PN: HCS9200B SN: 15102320; DUE DATE:22-JAN-24;[02] TOOL USED: MULTIMETER P/N: FLUKE-289; S/N: 57780044; DUE DATE: 22-JUL-24.;[03] REPAIRED ACCESS PANEL 19SDR SWAA2023092199201Panel · crackedPANEL 194E HAS 2EA FASTENER ATTACH HOLES CRACKED OUT; REQUIRES COMPOSITE REPAIR. (FASTENERS CIRCLED) PANEL 194E HAS 2EA FASTENER ATTACH HOLES CRACKED OUT REQUIRES COMPOSITE REPAIR. (FASTENERS CIRCLED)<[01] PREPARED AREA FOR REPAIR; ON WING TO BODY FAIRING PANESDR ASAA2023090546230Plate · corrodedLESSOR ITEM 211; (66539) BELLY FAIRING PANEL, FWD FUSELAGE ATTACHMENT CORRODED. (UNDER PANEL 191BB) GROUNDED - YES. REPLACED BELLY FAIRING PANEL, FWD FUSELAGE ATTACHMENT PLATE PN: E5321010120000. PO# 107232401 IAW AIRBUS DWG# E53210101. ISSUE: C AND A320 SRM SDR DALA2023090507228Unknown · unknownSHIP 3357 CRACK SUPPORT WEB BELLY FAIRING FR53.2 LH LATERAL SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SUPPORT WEB BELLY FAIRING FR53.2 LH LATERAL SIDE AT LOWER FUSELAGE AS PER A330 SRM 53-35-14. (2952835)SDR SWAA2023090596329Fairing · crackedCRACK; #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY<[01] REMOVED PYLON STRUT AFT FAIRING IAW SRM 51-40-02.;[02] INSTALLED NEW PYLON STRUT AFT FAIRING FITTING PER SRM 51-40-02 AND SRM 51-10-02SDR IPXA2023092588707Unknown · corrodedFAULT: R/H WING TO BODY, T-CHORD, AT STA 1180, RBL 35 FOUND NUT PLATE HOLE, EXFOLIATED CORROSION. INSTALLED NEW T-CHORD AT STA 1180, RBL 35, IAW B757 SRM 51-40-02. REVIEWED.SDR IPXA2023092588988Unknown · corroded*** SUPPLEMENTAL SDR *** FAULT: FWD, WING TO BODY T-CHORD STA 900 BETWEEN RBL 48 TO LBL 34, FOUND EXFOLIATED CORROSION AND CHAFFING, MARKED ON RED INSTALLED T-CHORD AND SPLICE PLATES I.A.W. B757-200 S.R.M. 51-40-02. REVIEWED.SDR IPXA2023092594244Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H UPPER FWD PRODUCTION DOUBLER IS WORN AT STA Y=2165, X=36.5.REPAIRED PRODUCTION DOUBLER AT THE TAIL CONE R/H UPPER FWD AT STA Y=2165, X=36.5 IAW UPS EO MD11-5350-66790-B APPENDIX B. (MINOR)SDR SWAA2023083093376Fairing · debondedWING TO BODY FAIRING 194GR HAS AN APPROXIMATE 1' CRACK WITH DISBOND IN EXTERIOR SKIN. -MARKED-<[01] REMOVED AND REPLACED WING TO BODY FAIRING 194GR PER AMM 53-51-21.;[02] REJECT: FAULT CARD IS COMPLETED BY MECHANIC WITHOUT MEASUREMENT SECTION COMPLETED AND NO SDR DALA2023100208042Unknown · unknown(LOG 2993607) PANEL SUPPORT STRUCTURE OF AFT WING-TO-BODY FAIRING, WITH TWO LOCATIONS WITH WEAR. PANEL SUPPORT STRUCTURE OF AFT WING TO BODY FAIRING WAS REPAIRED IAW B737-800 SRM 53-60-71 REV.79.00 DATE AUG-18-2023 REP. 2R PROCEDURE 2.SDR SWAA2023082893019Bracket · cracked-RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET CRACKED AT STA 500.<[01] REMOVED AND REPLACED RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET PER SRM 51-40-02.SDR SWAA2023092192889Fairing · crackedMID FORWARD FAIRING PANEL 191D HAS CRACK AT INNER SKIN<[01] C/W REPAIRSDR SWAA2023092892261Fairing · peelingLEFT FWD OUTBOARD WING TO BODY FAIRING PANEL 193AL INNER SKIN AT LOWER AREA PEELING OFF<[01] CERTIFIED STEPS ACCOMPLISHED.SDR SWAA2023092891994Fairing · damagedRT SIDE #5 FLAP TRACK AFT FAIRING #194BR MISSING FIBERGLASS MATERIAL TOP AND BOTTOM SKIN AT AFT EDGE (MKD)<[01] REPLACED RT SIDE #5 FLAP TRACK AFT FAIRING #194BR REF. B737-700 AMM 53-51-21-400-801. PANEL 194BR WILL BE INSTALL ON FAULT TTG8Q00MLPRZ;[02] CESDR IPXA2023082293987Skin · crackedINSPECTION TYPE:COPENING AT PNL 513AB HAS A CRACK.REPAIRED IAW 53-15-63 FIG 201SDR SWAA2023082191189Panel · elongated193B FAIRING PANEL HAS SEVERAL ELONGATED HOLES<[01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.SDR IPXA2023081993958Fairing · crackedINSPECTION TYPE:COPENING AT 613AB HAS A CRACKREPAIRED IAW SRM 53-15-63 FIG 201SDR SWAA2023081789864Radome · delaminatedNOSE RADOME HAS A PREVIOUS TEMPORARY REPAIR THAT IS DELAMINATED. REMOVED AND REPLACED NOSE RADOME AS PER AMM 53-52-00-400-801.;[02] VERIFIED STEP 1.SDR SWIA202308154Unknown · delaminatedTRANSFER FROM EAML 1192174 : DURING WALK AROUND FOUND DELAMINATION DAMAGE ON NOSE RADOME, DETERMINED THE DAMAGED TO BE OUT OF LIMITS. (FILED CLOSED)REMOVED AND REPLACED NOSE RADOME IN REFERENCE WITH CRJ AMM 53-81-80.SDR SWAA2023081688795Fairing · delaminatedRT WTB MID FAIRING 191FR DELAM AT FWD TOP CORNER<[01] PERFORMED 23-153-02493 & APPLIED SPEED TAPE TO PANEL 191FR.SDR SWAA2023081588345Radome · delaminatedNOSE RADOME HAS IMPACT DAMAGE AND DELAMINATION MEASURING 2.00 IN LONG X 1.00 INCH WIDE ON MOST FORWARD POINT<[01] C/W EA TASK CARD 23-153-02479SDR DALA2023081106542Unknown · unknownSHIP 1809 RT SPHERICAL PNL 196CR MISSING AND PNL 196DR DMGD. CORRECTIVE ACTION: REPLACED 196CR PANEL (SPHERICAL COVER) PER B767-400 AMM 53-66. REPLACED 196DR PANEL PER B767-400 AMM 53-66 OK FOR SVC. (4975852)SDR DALA2023081006498Unknown · unknownOUTER EMERGENCY TAILCONE HANDLE IS ARMED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00731: EMERGENCY TAILCONE HANDLE WAS REINSTALLED CORRECTLY PER B717-200 AMM 53-52-SDR SWAA2023091186742Panel · debondedPANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR DIS BOND REPAIRED IAW 51-70-05-2R-2;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023082987056Panel · elongatedWTB FAIRING 193AL HAS SEVERAL ELONGATED FASTENER HOLES<[01] UPDATED STEP 4 AND 5;[02] VERIFIED STEPS 1;2; IN PARTIAL.;[03] VERIFIED STEPS 4;5 COMPLETE.;[04] DUE TO EXTENT OF DAMAGE PANEL WAS REPLACED WITH A SERVICEABLE UNIT IAW SRM 51-10-02-0G-0 PAR 9.;[05] VESDR SWAA2023082987057Panel · elongatedWTB FAIRING 193AR HAS SEVERAL ELONGATED FASTENER HOLES<[01] ACCOMPLISHED ELONGATED FASTENER HOLES REPAIR IAW SRM 51-70-05-2R-6;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2023081086401Bracket · crackedBRACKET CRACKED UNDER 193B PANEL AT APPROXIMATELY RBL15 STA.663 COMMON TO THE RH ACM EXHAUST DUCT SEAL ON THE I/B SIDE.<[01] CW;[02] C/W;[03] CWSDR IPXA2023080893844Fairing · crackedINSPECTION TYPE:COPENING AT 613AB HAS A CRACKREPAIRED CRACK IAW SRM 53-15-63-201SDR SWAA2023091184932Panel · crackedCRACK ACCESS PANEL 194FL BODY FAIRING APU SHROUD DRAIN MAST FUSELAGE EXTERIOR 2023-477631<[01] REMOVED AND REPLACED APU SHROUD DRAIN MAST ON ACCESS PANEL 194FL BODY FAIRING I.A.W. B737-700 AMM 28-25-07-020-801 AND 28-25-07-420-801 SEE INDIVIDUAL SING-OFF BELOWSDR SWAA2023081784916Access Panel · corrodedCORROSION ACCESS PANEL 193AR BODY FAIRING STRUCTURE AT LOWER FUSELAGE 2023-447823<[01] REPLACED FRAME LOC ON BODY FAIRING STRUCTURE AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A7216 SHEET 7 REV-A. SEE INDIVIDUAL SIGN OFF SDR SWAA2023090584574Fairing · corrodedCORROSION ACCESS PANEL 192HL BODY FAIRING ON PLATE FUSELAGE EXTERIOR 2023-477570<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 192HL BODY FAIRING IAW B737-700 SRM 51-10-02 AND DRAWING 149A7263 SHEET 2 REV A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED PLATE LSDR SWAA2023090584575Fairing · corrodedCORROSION ACCESS PANEL 192HR BODY FAIRING ON PLATE FUSELAGE EXTERIOR 2023-477572<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 192HR BODY FAIRING IAW B737-700 SRM 51-10-02 AND DRAWING 149A7263 SHEET 2 REV A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED PLATE LSDR JJBA20230803026Panel · damagedDURING WALKAROUND FOUND DAMAGE FROM GROUND EQUIPTMENT TO AFT RIGHT SIDE OF WTF FAIRING AND FUSELAGE FURTHER AFT. MAPPED WTF PANEL #198CB FOR RTS REPAIR OR ALLOWABLE DAMAGE REQUEST. NO FURTHER DAMAGE BEHIND PANEL AND NO BLEED LEAKS. NO DAMAGE NOTED AFT OF PANELSDR DALA2023080206255Unknown · unknown(LOG 2895946) EVALUATE & REPAIR PANEL PER B737-800 SRM 53-60-70. LAYED UP BAGGED AND CURED EXTERIOR REPAIR PLIES PER B737-800 SRM 53-60-70(418468)PERFORMED POST REPAIR NDT INSPECTION PER B737-800 SRM 53-60-70 REV 78.00. SEALED REPAIR PER B737-800 SRM 53-60-70.SDR SWAA2023073183551Fairing · delaminatedFAIRING 194FR REQUIRE REPLACEMENT REF TTG8Q00M0SWV FOR 194FR<[01] REPLACED 194FR PANEL PER AMM 53-51-21.SDR SWAA2023073183552Fairing · delaminatedFAIRING 194GR REQUIRE REPLACEMENT REF. TTG8Q00M0S0K FOR 194GR<[01] REMOVED AND REPLACED WING TO BODY FAIRING IAW AMM 53-51-21SDR SWAA2023073183554Fairing · delaminatedFAIRING 194CR REQUIRE REPLACEMENT REF FAULT TTG8Q00M0RW FOR 194CR<[01] REMOVED AND REPLACED FAIRING PANEL ASSY 194CR IAW AMM 53-51-21.SDR DALA2023072806120Unknown · unknownPUNCTURE TO THE 193BB PANEL ASSY (P/N F5332705601800). THE PUNCTURE MEASURES 2" WIDE X 2" LONG AND 0.5" DEEP. THE DAMAGE IS GREATER THAN 4D FROM THE NEAREST FASTENER. AS CONFIRMED BY MTC., THE DAMAGE IS THROUGH THE OUTER FACESHEET IN THE HONEYCOMB SANDWICH REGSDR DALA2023072806115Unknown · unknownDAMAGE TOLERANCE EVALUATION (DTE) IS REQUIRED. ER/A 609384-14 SECTION I WAS ISSUED FOR A FUSELAGE TAIL CONE SKIN REPAIR. REF LOGPAGE 2838224. CURRENT ER/A REVISION IS 'B'. REPAIR APPROVAL IS LIMITED TO 12 MONTHS FROM SECTION I (27JUN23). A DAMAGE TOLERANCE EVASDR SWAA2023072581652Panel · crackedPANEL 193D CRACKED . CRACK MEASURED 3 IN LENGTH.<[01] REMOVED AND REPLACED FAIRING PANEL 193D PER AMM. 53-51-21.SDR IPXA2023071893683Fairing · crackedINSPECTION TYPE:CPANEL 611AB OPENING HAS A CRACKREPAIRED AREA IAW SRM 53-15-63SDR SWAA2023071878213Panel · delaminated193B PANEL HAS MULTIPLE AREAS OR CHAFFING; DELAMINATION AND ELONGATED HOLES.<[01] REMOVED AND REPLACED 193B PANEL IAW AMM 53-51-21/401SDR DALA2023071405728Unknown · unknownSHIP 3353 WHILE WORKING PER CUSTOMER CARD 5300-2009, WHICH PROVIDES INSTRUCTIONS TO PERFORM INSPECTIONS PER MPDS 533123-01-1, 571131-01-1, 533122-01-1 AND 533036-01-1, A CRACK WAS FOUND AT SUBJECT LOCATION. A330 SRM 53-35-14-300-005 WAS REVIEWED AND FOUND OUT
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