JASC 5350
Service difficulty reports · 6,118
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 JJBA20240611019Angle · crackedCENTER FUSELAGE 3, LH UPPER SURFACE OF WING TO FUSELAGE FAIRING STRUCTURE, ANGLE 1, 2, 3 FROM FWD FOUND CRACKED. ANGLE 2 FROM FWD END REMOVED AND REPLACEDSDR JJBA20240611018Angle · crackedCENTER FUSELAGE 3, RH UPPER SURFACE OF WING TO FUSELAGE FAIRING STRUCTURE, ANGLE 2, 4, 7 FROM FWD FOUND CRACKED. ANGLE 4 FROM FWD END REMOVED AND REPLACEDSDR MK1Y2024052200380Failsafe · corrodedFOUND SIX LOCATION OF CORROSION DMAGE TO FAIL SAFE INNER CHORD, SEC 45, STA 859.5, STR 13 TO STR 20 - L/H AND R/H SIDESSDR IPXA2024061488935Tee Angle · corrodedL/H STA. 1040-1060 LBL 20 T-CHORD HAS CORROSION. DOT 33-013 INSTALLED T-CHORD IAW SRM 51-40-02,P/N FASTENERS BACB30NX6K3 BATCH 0004216302, COLLAR HI-LOCK P/N HL79-6 BATCH 0004255765.SDR AALA202405249056Panel · delaminatedAIRCRAFT WAS NOT GROUNDED: FOUND PANEL WING TO BODY 196BR DELAMATED.**SUPPLEMENTAL REPORT FOR (AALA202405229056): INSTALLED WING TO BODY FAIRING 196BR. PER AMM 53-46-01**(CLOSED).SDR AALA202405229056Panel · delaminatedAIRCRAFT WAS NOT GROUNDED: FOUND PANEL WING TO BODY 196BR DELAMATED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).SDR SWAA2024052287242Panel · damagedWING-TO-BODY FAIRING PANEL 193B HAS SEVERAL ELONGATED FASTENER HOLES AND NUMEROUS COUNTERSINKS THAT ARE TOO DEEP.<[01] MATCH DRILLED NEW PANEL 193B PER SRM 51-10-02.SDR SWAA2024062786815Support Fitting · crackedWING TO BODY PANEL SUPPORT FITTING CRACKED BS540+11 RBL5 ACCESS PANEL 192E. MARKED<[01] REMOVED AND REPLACED WING TO BODY PANEL SUPPORT FITTING BS540+11 RBL5 ACCESS PANEL 192E IAW BOEING DWG 149A7701 AND SRM 51-40-02.;[02] VERIFIED STEPS 1;2;3 COMPLETE; MEASURSDR SWAA2024062786816Support Fitting · crackedWING TO BODY PANEL SUPPORT FITTING CRACKED BS577 LBL5 ACCESS PANEL 192E. MARKED<[01] REMOVED AND REPLACED WING TO BODY PANEL SUPPORT FITTING BS577 LBL5 ACCESS PANEL 192E IAW BOEING DWG 149A7701 AND SRM 51-40-02.;[02] VERIFIED STEPS 1;2;3 COMPLETE; AND MEASUREMSDR AALA202405200031Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: WING TO BODY PANEL 192BL IS DELAMINATED ON FORWARD SIDE OF PANEL. APPLIED ALUMINUM WIRE MESH PERMANENT REPAIR AND CARBON FIBER PLIES PERMANENT REPAIR ON LEADING EDGE AREA OF WING TO BODY FAIRING ACCESS PANEL 192BL PER B737-NG SRM SDR DALA2024051605254Pin · out of positionINCORRECT HRS POSITION OF TAILCONE RELEASE MECHANISM CAM PIN STA Y=1225 CANT AT AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00817: TAILCONE RELEASE MECSDR VNAA20240619020Access Panel · crackedCRACK IN ACCESS PANEL 171CL. ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430. REV--SDR SWAA2024061484912Panel · crackedFAIRING PANEL 191D HAS A CRACK ON BOLT HOLE 1 INCH FROM INNER LEFT EDGE AND 24 INCHES FROM INNER FWD EDGE.<[01] APPLIED REPAIR AT PANEL#191D PER B737 SRM 51-70-04-2R-0 PARAGRAPH(4;N) MATERIAL USED RESIN EA9390 PO#1791128 AND FIBER GLASS PO#1690463 TOOL USED TESDR SWAA2024060684742Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2.SDR AALA202405134145Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE: PART OFF THE AIRPLANE, RH WING TO BODY FARING PANEL 191BL HAS SEVERAL DISBONDED INTERNAL REIFORMENT PANELS, IDENTIFIED WITHORANGE STICKER # 118-021. MAINTENANCE ACCOMPLISHED A PERMANENT REPAIR ON R/H WING TO BODY FAIRINGSDR DALA2024050905040Panel · detachedSHIP 1812 RIGHT SPHERICAL BEARING PANEL DEPARTED THE A/C. CORRECTIVE ACTION: INSTALLED PANEL 196CR PER B767 AMM 53-52 . A/C OK FOR SVC. (5642434)SDR JJBA20240520030Latch · brokenFWD FUSELAGE 1, FR 1A LH & RH UPPER RADOME LATCHE FAIRING BROKEN. LH AND RH UPPER RADOME LATCHE REMOVED AND REPLACEDSDR SWAA2024052080746Fairing · delaminated(A204 DOT 62) WING TO BODY FAIRING 191CR; EXTERIOR SURFACE HAS A DENT WITH POSSABLE DELAMINATION; 14' FROM AFT EDGE AND 8' FROM OUTBOARD EDGE.<[01] REPAIRED DAMAGE TO PANEL 191CR IAW SRM 53-60-70-2R-1 TABLE 201; RM 51-70-04-2R-11; SRM 51-70-04-2R-0 REPAIR GENESDR DALA2024043004790Release Cable · corrodedRUSTED CABLES AND ALL PINS ON TAILCONE RELEASE CABLE AND PULLEY MECHANISMS. ALSO BROKEN STRANDS OF CABLE AT 10 HRS POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00180: CABSDR JR2R20240425841Panel · corrodedWTB FAIRING PANEL 192CR PANEL AND SPACER CORRODED. REPAIRED PANEL / REPLACED SPACERSDR UIEA2024042200304Intercostal · deformedFUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL, P/N: 65B07241-1 BETWEEN STA 1480 +60 TO STA 1520 LBL 45. DEFORMATION DAMAGE - TEMPORARY REPAIR REFER EA-4853A0088(<P>FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL REPLACED AS PER SRM 51-10-02, SRM 51-40-02 AND RI-53SDR DALA2024062006273Tee Angle · corrodedSHIP 6809 CORROSION ON FWD SETTLEMENT AREA OF ACCESS PANEL197NL. CORRECTIVE ACTION: SUMMARY OF NRC 00596: FUSELAGE FAIRING STRUCTURE CHORD TEE AT STA 1240 BTW RBL 10 TO LBL 10 WAS REPAIRED PER ER/A 616892-14 REV ORIGINAL SECTION I: PERMANENT REPAIR (0302949)SDR SWAA2024052876668Panel · damagedFOUND ELONGATED HOLES ON PANEL 551GB<[01] APPLIED REPAIR AT PANEL#551GB PER B737SRM 57-51-01-2R-1 51-70-04-2R-0PARAGRAPH(4.N.2) MATERIAL USED RESIN 3804 PO#2066364 FIBER GLASS PO#1690463. TOOL USED<BR>TEMPERATURE CONTROL ID:160354 DUE DATE:03/07/25 VACUMM GAGESDR JJBA20240513016Angle · crackedL/H WING TO BODY FAIRING UPPER ANGLE #1 AND #3 FOUND CRACKED. ON L/H WING TO BODY FAIRING UPPER ANGLE #1 AND #3 REPAIRED.SDR SWAA2024041775469Radome · damagedCHIP ON FRONT OF RAY DOME<[01] REMOVED AND REPLACED NOSE RADOME REF AMM 53-52-00SDR DALA2024041504410Radome · damagedSHIP 3142 RADOME HAS IMPACT DAMAGE. CORRECTIVE ACTION: REMOVED AND REPLACED RADOME PER A319 AMM 53-15-11. (5402312)SDR YENA2024041600557Tail Cone · dentedDURING HEAVY MAINTENANCE: FUSELAGE / REAR / TAILCONE/DENT BTWN FRAME 78-80 BETWEEN LH STR 1 AND 2 SPLICE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR SWIA202404250010Fairing · damagedCHAFING DAMAGE FROM MLG FAIRING ON WING LWR AFT SKIN PLANK LBL45 AND RBL45 AT WING REAR SPAR DATUM/TRAILING EDGE OF WING PLANK. (C-CHECK RO 4/24/2024) REPAIRED CHAFING DAMAGE FROM MLG FAIRING ON WING LWR AFT SKIN PLANK LBL45 AND RBL45 AT WING REAR SPAR DATSDR CALA2024041601108Pad · gougedACFT LOWER TAIL CONE SAFETY STAY MOUNTING PAD CUT OUT INNER SURF ACE GOUGED PER HAECO LCQ N/R 9290786/30786 GEN BY V901665SDR SWAA2024052072072Support Angle · crackedCRACK ANGLE SUPPORT STRUCTURE WING TO BODY FAIRING LEVEL BS 500D AND STRINGER 19R AT LOWER FUSELAGE 2024-253249<[01] REPLACED ANGLE SUPPORT STRUCTURE LOC.WING TO BODY FAIRING LEVEL BS 500D AND STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 ;51-10-02 SDR 4EZF240409N304AGRadome · crackedBIRD STRIKE AT THE RADOME DURING LANDING OR APPROACH IN CURACAO (TNCC). MTX ACTION: FOUND RADOME WITH CRACK. RADOME HAS BEEN REMOVED & REPLACED IAW S340 AMM 53-50-10-04SDR QXEA2024040500092Tail Cone · contaminatedPASSENGER REPORTS SMOKE FROM TAIL CONE. REMOVED FROM SERVICE. PERFORMED GVI OF TAILCONE AREA. FOUND DE-ICE FLUID TO BE PROBABLE CAUSE OF SMOKE RAN APU NO SMOKE NOTED. RETURNED TO SERVICE.SDR SWAA2024040570317Panel · debondedFAIRING PANEL 193B; FWD RIGHT CORNER DISBANDED APPROXIMATE 1BY 2 INCHES LONG. FAIRING PANEL 193B FWD RIGHT CORNER DISBOUNDED APPROXIMATE 1BY 2 INCHES LONG.<[01] REPAIRED PNL 193B PER EA 24-153-00-883.SDR UIEA2024040500262Fairing · corrodedCORROSION ON AFT WTB FAIRING LWR CHORD AT STA 1480. LBL 16 ~ RBL 16(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. FABRICATED PART IAW WORKSHEET 40232 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B15085 SH4 REV L & 65B15085 SSDR DALA2024040804149Radome · delaminatedSHIP 3248 DISC: DURING LIGHTNING STRIKE INSPECTION FOUND DELAMINATION ON RADOME. C/A: MEASURED DELAMINATED AREA TO BE 2.2" IN ZONE A OF RADOME. PERFORMED TEMPORARY REPAIR WITH POLYURETHANE TAPE PER A320 AMM 53-15-11. PLACED RADOME REPLACEMENT ON MON FOR 600FH SDR N6WA2024050202Diaphragm · crackedWING TO FUSE SUPPORT STRUCTURE DIAPHRAGM LBL17.63 BOTTOM CRACKED AT FS910.REPAIRED SUPPORT STRUCTURE DIAPHRAGM IAW EO C550-53MIR-002-O.SDR N6WA2024050201Strap · corrodedAFT WING TO BODY FAIRING SPLICE STRAP STIFFENER CORRODED/ CRACKED. R&R AFT WING TO BODY FAIRING SPLICE STRAP AND STIFFENERS IAW CRJ SRM 51-42-00SDR FDEA202403290408Fairing · gougedSEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-03 AND AFTER EVALUATION TWO DIFERENT AREAS FOUND # 1 AREA AT STA 1862 TO STA 1865 FOUND WITHISDR IPXA2024032980835Radome · damagedBIRD STRIKE APPROXIMATELY 9000€™ AT 286 KNOTS ON CLIMB OUT REPLACED NOSE RADOME IAW. AMM 53-52-01 PB 201 REV. 44.SDR IPXA2024032780835Radome · damagedBIRD STRIKE APPROXIMATELY 9000€™ AT 286 KNOTS ON CLIMB OUT BIRD STRIKE INSPECTION CARRIED OUT I.A.W. AMM 05-51-14-202-001 REV. 44. FOUND BIRDSTRIKE ON UPPER PART OF RADOME. DELAMINATED AREA BETWEEN BOTH UPPER DIVERTER STRIPES OF 32 INCHES LENGTH AND WIDTH. UPSDR SWAA2024032566976Fairing · damagedWING TO BODY PANEL 193B HAS NUMEROUS COUNTERSINK HOLES THAT ARE PULLING THRU AND THE HOLES ARE ELONGATED.<[01] REMOVED AND REPLACED PANEL 193B PER SRM 51-10-02 AND 51-40-02.SDR JR2R20240322532Frame · corrodedLH WING TO BODY ATTACH FRAME 52 P/N 170-19903-401 CRACKED BEYOND SRM REPAIRABLE LIMITSSDR DALA2024032003550Tail Cone · corrodedSHIP 3311 TAILCONE FR92 ASSY/MULTIPLE CORROSION AREAS ON LH AND RH FRAME. CORRECTIVE ACTION: COMPLIED WITH ERA 616528-14 REV ORIGINAL. (0252999)SDR JJBA20240404016Angle · crackedWING TO BODY FAIRING, ANGLE #4 ON WING FOUND CRACKED ON WING TO BODY, ANGLE #4 REMOVED FOR REPLACEMENT, ANGLE #4 DRILLED. ON WING TO BODY, ANGLE #4 REPLACED WITH NEW ONE.SDR 2024FA0000229Fairing · corrodedR/H ELEVATOR WEDGE FAIRING SKIN CORROSION BLEND-OUT.SDR CALA2024031800753Fairing · missingPDA 1 REF LP 7357370 LEFT WING TO BODY FAIRING PANEL 193CL FOUND MOSTLY MISSING AND PARTIALLY DAMAGED ON WALK AROUND. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTSDR SWAA2024041762601Tail Cone · delaminatedTAIL CONE LOWER LOBE RIGHT SIDE WAS FOUND A DELAMINATION SPOT; 9 IN BEHIND STA 1156 L=3 IN W= 2.750 IN. REPAIRED IAW SRM 51-70-05-2R-2.SDR AALA202403195459Tail Cone · corrodedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. REPAIRED PER AARD 11-20-00-1 REPAIR 1.SDR AALA202403155459Tail Cone · deterioratedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. Ï¿½ **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPSDR DALA2024031203274Fairing · degradedSHIP 5810 -DIV- TO MEM DUE TO VIBRATION FELT IN CABIN. FOUND LEFT OVERWING TO BODY PANEL SEAL DEGRADED. PERFORMED TIME LIMITED REPAIR. R/R LH WING TO BODY FAIRING OVERWING PANEL 191DL SEAL REF ERA 616536-14, REV ORG, SEC III PERMANENT REPAIR.
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