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.

SDR IPXA2023112637854Fairing · corrodedFAULT-FUS BELLY FAIRING AFT W/W CUTOUT SUPPORT FITTING WITH CORROSION SEVERAL PLACES. INSTALLED T-CHORD AT LBL 5750 BETWEEN STA 1180 TO 1240 IAW SRM 51-40-02-0G. WORK VERIFIED, NUTPLATES INSTALLED NUTPLATES P/N; BACN11P3A5C, BATCH #0004204060. RIVETS P/N: MS20Nov 10, 2023 · N456UP · Boeing 75724APFSDR CALA2023111503354Doubler · gougedUPON REMOVAL OF BELLY FAIRING AT FR 34, PREVIOUS REPAIR DOUBLER IS GOUGED FROM PANEL. GENERATED BY N078625 PER HAECO LCQ NR 9296 775/40775 REMOVED AND REPLACED REPAIR DOUBLER AT FR 34 IAW A319 EC/RA# 533 1-02275 REV IR. ACMP BY V925324 INSP BY V892285Nov 10, 2023 · N819UA · Airbus A319131SDR IPXA2023112316833Web · corrodedFAULT:WING TO BODY FAIRING STA 1.200 WEB RH HAS CORROSION.DOT119-048. INSTALLED NEW WEB AT STA 1200 RH WTB IAW SRM 51-40-02-0G. REVIEWED.Nov 9, 2023 · N459UP · Boeing 75724APFSDR IPXA2023111319733Unknown · unknown*** SDR FILED OPEN *** FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65 EVALUATED T-CHORD AT STA 1060 BETWEEN LBL 50 TO LBL 65, EXFOLIATED CORROSION NOTED, AFTER FUTHER INVESTIGATION FOUND TO BE OUT LIMITS I.A.W SRM 53-00-71-1A-1 FINov 9, 2023 · N456UP · Boeing 75724APFSDR TAMF20231109039Radome · dentedDURING WALK AROUND FOUND BIRD STRIKE ON RADOME. THE RADOME ASSY WAS REPLACED. RADOME ASSY PN/ OFF F53132110000, PN/ 0N F53132110000, SN/ OFF RADTA3519, SN/ ON RADTA3030.Nov 9, 2023 · N330QT · Airbus A330243FSDR IPXA2023111384377Unknown · unknownLEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 REMOVED T-CHORD FROM STA 1037.67 TO 1060 LH SIDE LBL 67 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA 1037.67 TO 1060 LH SIDE REMOVED.Nov 7, 2023 · N456UP · Boeing 75724APFSDR IPXA2023111384644Unknown · unknown*** SDR FILED OPEN *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 REMOVED T-CHORD AT AREA INTERIOR DOOR RAT I.A.W SRM 51-40-02-0G.- VERIFIED REMOVAL OF T-CHORD INTERIOR RAT DOOR AREA.Nov 7, 2023 · N456UP · Boeing 75724APFSDR DALA2023110909254Unknown · unknownSHIP 6816 CORROSION ON BODY FAIRING SETTLEMENT SUPPORTS (2 EA) STA 1240 BTW STR= 27LH / 27RH AT WING / BODY FAIRINGS. CORRECTIVE ACTION: SUMMARY OF NRC 00233: CORROSION ON BODY FAIRING SETTLEMENT SUPPORTS (2 EA) STA 1240 BTW STR= 27LH / 27RH AT WING WAS REPAIRNov 7, 2023 · N722TW · Boeing 757231SDR EBVR450D110723001Tail Cone · corrodedCORROSION FOUND ON R/H TAIL STINGER, STARTED REMOVING CORROSION FROM THE TAILCONE STINGER RH FWD SKIN AND NOTED SEVERE LEVEL 2 CORROSION THAT EXTENDS THROUGH THE ENTIRE THICKNESS OF THE SKIN. REMOVED AND REPLACED L/H AND R/H STRINGERS IN THE TAILCONE STINGER ,Nov 7, 2023 · N540QS · Cessna 680ASDR IPXA2023111356677Unknown · unknownWTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 REMOVED WEB ON FRAME STA 900 L/H IAW B757 SRM 51-40-02. VERIFIED WEB ON FRAME STA. 900 LH REMOVED.Nov 6, 2023 · N456UP · Boeing 75724APFSDR SWAA2023112016525Tail Cone · elongatedLH WING #3 CANOE FAIRING TAIL CONE BOLT HOLES ELONGATED<[01] REMOVED AND REPLACED TAIL CONE PER AMM 27-51-18Nov 1, 2023 · N8673F · Boeing 7378H4SDR SWAA2023120715976Access Panel · crackedCRACK ACCESS PANEL 193AL WING TO BODY FAIRING FUSELAGE EXTERIOR 2023-681916<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A21303945 DUE DATE: 07-NOV-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196119 DUE DATE: 23-MAY-24.;[03] UT EQUIPMENT USED P/N: EOct 29, 2023 · N7846A · Boeing 73776NSDR SWIA2023111029Unknown · corrodedCENTER BELLY FAIRING RACK: PNL 192CR CORRODED AT MOUNTING DOUBLER. (C-CHECK RO 11/13/2023) DOUBLER FOUND TO BE CORRODED THROUGH, REMOVED AND REPLACED DOUBLER PER SRM 51-40-08Oct 29, 2023 · N198SY · Emb ERJ170200LRSDR DALA2023103008924Unknown · unknownSHIP 3166 DAMAGE TO 191BB PANEL LEADING EDGE. CORRECTIVE ACTION: REPAIRED PER ER/A 542077-14TR. (0039475)Oct 28, 2023 · N366NB · Airbus A319114SDR SWAA2023121115242Panel · delaminatedFAIRING PANEL 193CL HAS DELAMINATED PLIES ON INNER SURFACE FWD LEADING EDGE<[01] REPAIRED DELAMINATED PLIES ON INNER SURFACE FWD LEADING EDGE ON PANEL 193CL IAW SRM 51-70-05-2R-6;[02] FINAL INSPECTION. JOB COMPLETE.Oct 27, 2023 · N8309C · Boeing 7378H4SDR SWAA2023112015218Tail Cone · delaminatedTAIL CONE HAS 2EA. SMALL AREAS OF DELAMINATION R/H SIDE UPPER AFT MKD.<[01] REMOVED DAMAGE PER SRM 51-70-05 REPAIR 1.;[02] VERIFIED REMOVED DAMAGE PER SRM 51-70-05 REPAIR 1.;[03] REPAIRED DAMAGE PER SRM 53-80-70-2R-1;[04] REPAIRED PER SRM 51-70-05-2R-1Oct 26, 2023 · N8673F · Boeing 7378H4SDR SWAA2023102715095Panel · debondedDISBONDING IN MULTIPLE LOCATIONS AROUND FASTENER HOLES ON 193B PANEL<[01] #1 FASTENER HOLE 3 LAYERS DISBONDED;[02] #33 FASTENER HOLE 2 LAYERS DISBONDED;[03] #34 FASTENER HOLE 1 LAYER DISBONDED;[04] DISREGARD ABOVE ENTRIES.<BR>#1 FASTENER HOLE 3 LAYERS DISBONDEOct 26, 2023 · N244WN · Boeing 7377H4SDR SWAA2023112014274Tail Cone · delaminatedTAIL CONE HAS MULTIPLE DELAMINATED DENTS BETWEEN MULTIPLE COMPOSITE REPAIRS ON UPPER ON L/H SURFACES<[01] REMOVED DAMAGE IN AREAS OF DENTS MARKED PER SRM 51-70-5-05. REPAIR 1;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] POTTED CORE ON AFFECTED REPAIR AREAS PR Oct 24, 2023 · N8673F · Boeing 7378H4SDR SWAA2023102613720Panel · delaminatedWING TO BODY FAIRING PANEL 193AL HAS EDGE DAMAGE AT UPPER AFT TRAILING EDGE THAT IS DELAMINATED APPROXIMATELY 2 AFT OF TE TO 4 DOWN FROM UPPER END (AFT UPPER CORNER OF PANEL).<[01] DELAM IS 6 INCHES FROM TOP OF TRAILING EDGE OF PANEL 193AL AND 2 1/2 INCHES IN Oct 23, 2023 · N225WN · Boeing 7377H4SDR WX0A1900010031885Unknown · unknownTAIL CONE UPPER SKIN DENTED ON L/H SIDE / TAIL CONE UPPER SKIN ON L/H SIDE DENT WAS EVALUATED AS PER SRM 53-51-11-283-024 REV. 146 AND REPAIRED AS PER SRM 53-51-11-300-010 REV 146 FIG 001. PERMANENT MAJOR REPAIR CATEGORY A. NO FURTHER ACTION REQUIRED. SEE AWS Oct 21, 2023 · N312NV · Airbus A319111SDR WX0A1900010031874Tail Cone · unknownTAIL CONE UPPER SKIN DENTED ON LH SIDE / TAIL CONE UPPER SKIN ON L/H SIDE DENT WAS EVALUATED AS PER SRM 53-51-11-283-024 REV. 146 AND REPAIRED AS PER SRM 53-51-11-300-010 REV 146 FIG 001. PERMANENT MAJOR REPAIR CATEGORY A. NO FURTHER ACTION REQUIRED."Oct 21, 2023 · N312NV · Airbus A319111SDR SWAA2023113012874Access Panel · crackedCRACK ACCESS PANEL 191CR BODY FAIRING AT LOWER FUSELAGE 2023-650078<[01] TOOL USED: HOT BONDER P/N HCS9200B-AV; S/N: 18196127; DUE DATE: 22-JAN-24;[02] TOOL USED: SCALE: P/N: SPX621 S/N 8340225451 DUE DATE: 16/AUG/24.;[03] TOOL USED: HOT BONDER : P/N:HCS9200B-Oct 20, 2023 · N8604K · Boeing 7378H4SDR SWAA2023111311737Panel · debondedPANEL 194AL OUTER SKIN AT LOWER FWD EDGE IS DISBONDED. (MARKED)<[01] PANEL 194AL OUTER SKIN AT LOWER FWD EDGE WITH DISBOND AS MARKED WAS REPAIRED PER SRM 51-70-05-2R-6.;[02] VERIFIED PANEL 194AL WAS REPAIRED PER SRM 51-70-05-2R-6.Oct 18, 2023 · N7863A · Boeing 7377Q8SDR N6WA2023102601Fairing · crackedR/H #3 OVERWING FAIRING PANEL IS CRACKED AT RIVET (PANEL 172CR). REPAIRED IAW STS EA 109-2023-148.Oct 18, 2023 · N541GJ · Cndair CL6002C11SDR DALA2023101808595Unknown · unknownSHIP 5642 RH WTB PANEL192DR, BEHIND PANEL THERE IS 1EA SUPPORT ANGLE HAS CORROSION I-14. CORRECTIVE ACTION: REMOVED CORROSION AT SUPPORT ANGLE FOUND TO BE OUT OF LIMITS IAW B737 SRM 51-10 SRM 53-00-71, FABRICATED NEW SUPPORT AND INSTALLED IAW B757 DRAWING 149NOct 16, 2023 · N542US · Boeing 757251SDR DALA2023101608482Unknown · unknownIMPROPERLY INSTALLED TAIL-CONE KEVLAR LANYARD (CAT). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00703: TAIL-CONE KEVLAR LANYARD WAS INSTALLED CORRECTLY PER B717 AMM 53-52-01 400-8Oct 13, 2023 · N966AT · Boeing 717200SDR DALA2023101408441Unknown · unknownA MISSING CLAMP WAS FOUND ON THE LATCH CABLE (2 EA) FOR THE TAILCONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00700: LATCH CABLE CLAMPS (2 EA) WERE INSTALLED, LUBE ANDOct 12, 2023 · N961AT · Boeing 717200SDR IPXA2023101218618Fairing · damagedFUSELAGE AERODYNAMIC FAIRING BELOW INBD FLAP DAMAGED ACCOMPLISHED EO-88442-REQ1 (LEFT INBOARD TRAILING EDGE FLAP FAIRING PANEL AND S.O.B. DOOR DAMAGE - TEMPORARY REPAIR REFERENCE IPC 53-66-59-05A, ITEM 50) [T3F18E0034ACW]Oct 11, 2023 · N311UP · Boeing 76734AFSDR IPXA2023101118618Unknown · unknown*** SDR FILED OPEN *** FUSELAGE AERODYNAMIC FAIRING BELOW INBD FLAP DAMAGEDOct 11, 2023 · N311UP · Boeing 76734AFSDR SWAA2023121817969Access Panel · crackedR/H OVERWING FAIRING ACCESS PANEL # 195CR CRACKED<[01] REPAIRED R/H OVERWING FAIRING ACCESS PANEL # 195CR. AS PER SRM 51-70-04-2R-6 MATERIAL USED PO.1791128 AND PO.1473815;[02] VERIFIED STEP 1Oct 9, 2023 · N7868K · Boeing 73779PSDR SWAA2023110809222Access Panel · delaminatedDELAMINATED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR 2023-637719<[01] TOOL USED CALIPER P/N: 700-113-10; S/N 0031753; DUE DATE: 27-NOV-23.;[02] TOOL USED: THERMAL CAMERA; P/N: FLIR-T530; S/N: 79316001; DUE DATE: 23 JAN 24.;[03] TOOL USED HOOct 9, 2023 · N907WN · Boeing 7377H4SDR DALA2023101208382Unknown · unknownSHIP 3158 PANEL 191AB FORWARD LOWER LT WING TO BODY FAIRING HAS SEVERAL AREAS WITH EXPOSED AND MISSING ALUMINUM MESH. CORRECTIVE ACTION: REPAIRED PER ER/A 612716-14. (4296422)Oct 8, 2023 · N358NB · Airbus A319114SDR SWAA2023101108866Fairing · delaminatedWTB FAIRING PANEL 193AR APPEARS TO BE DELAMINATED AND SHOWS EXPOSED COMPOSITE FIBERS NEAR THE HYDRAULIC SERVICING HOSE HOLSTER BRACKET ATTACH SCREWS.<[01] INSTALLED REPAIR REF. ?EA-GENERAL?.Oct 8, 2023 · N259WN · Boeing 7377H4SDR A6WA202310068679Unknown · damagedCRUSHED RADOME, WEATHER RADAR UNIT, AND BULKHEAD DAMAGE AT FS 169, FUSELAGE SKIN, STRINGERS & FRAME DAMAGE FROM FS169 TO FS193 ON RH AND LH SIDES OF FUSELAGE *******AIRCRAFT REMOVED FROM SERVICE********* FORWARD FUSELAGE AT FS169 TO FS193 REPAIR COMPLETED BY Oct 6, 2023 · N457AW · Cndair CL6002B19SDR SWAA2023110307626Panel · crackedPANEL 195CL AFT CORNER RADIUS IS CRACKED.<[01] CRACKED AFT CORNER RADIUS ON PANEL 195CL WERE REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CRACKED AFT CORNER RADIUS ON PANEL 195CL WERE REPAIRED IAW SRM 51-70-05-2R-6.Oct 5, 2023 · N908WN · Boeing 7377H4SDR SWAA2023102007096Panel · delaminatedWING TO BODY PANEL 194FL HAS A SMALL DENT WITH DELAMINATION. DAMAGE IS MARKED<[01] REMOVED DAMAGE PER SRM 51-70-05-2R-1. POTTED CORE PER SRM 51-70-05-2R-11.;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] INSTALLED REPAIR PLIES IAW SRM 51-70-05-2R;[04] INSPECTED Oct 4, 2023 · N8674B · Boeing 7378H4SDR SWAA2023100406151Panel · delaminatedWTB PANEL 193B HAS SMALL AREA OF EROSION AND DELAMINATION AT L/E R/H CORNER (MARKED).<[01] R & R WTB PANEL 193B PER SRM 51-40-02Oct 1, 2023 · N951WN · Boeing 7377H4SDR SWAA2023100306175Panel · delaminatedPANEL 193AL HAS LEADING EDGE DELAMINATION APPROXIMATELY 12 FROM TOP OF PANEL<[01] DELAMINATION DAMAGE FOUND ON PANEL 193AL LEADING EDGE 12? FROM TOP; FOUND TO BE OUT OF LIMITS IAW SRM 53-40-70 4. B. (6);[02] C/W EA 23-153-02955Sep 30, 2023 · N7881A · Boeing 7377CTSDR SWAA2023103105867Fairing · cracked53-60-70-1A-1-B00771-TLD (PERMANENT REPAIR OF TEMPORARY SEAL - SECTION 46 WING-TO-BODY FAIRING SKIN PANELS) - LH AFT WING-TO-BODY FAIRING HAS CRACK L= 0.25 W= 0.125 D= .03. 8 DAY GVI REQUIRED. PERMAN 53-60-70-1A-1-B00771-TLD (PERMANENT REPAIR OF TEMPORARY SEALSep 29, 2023 · N8305E · Boeing 7378H4SDR SWIA2023100528Unknown · crackedAFT BELLY FAIRING R/H CTR UPPER ATTACH FLANGE HAS CRACK THROUGH FASTENER HOLE AT SUPPORT BRACKET FWD OF FR 58 BETWEEN STGR 19R- STGR 17R AS MARKED. (C-CHECK RO 10/3/2023) PERFORMED PERMANENT REPAIR TO AFT BELLY FAIRING R/H CTR UPPER ATTACH FLANGE REF EMB 1Sep 28, 2023 · N183SY · Emb ERJ170200LRSDR IPXA2023092494235Stiffener · gougedINSPECTION TYPE:2CTAIL CONE COMP RH PATIO DOOR FWD SIDE FRAME AND METAL PLATE HAS DEEP GOUGEDREPLACED SUPPORT ANGLE FRAME AT TAIL CONE COMP. R/H PATIO DOOR FWD SIDE FRAME AND METAL PLATE IN REF.MD11 SRM 51-35-01-0G-0 AND SRM 51-33-01-0G-0(MINOR)Sep 24, 2023 · N259UP · Doug MD11FSDR IPXA2023092494234Frame · gougedINSPECTION TYPE:2CTAIL CONE FWD HORIZONTAL FRAME HAS A GOUGE R/H SIDEREPAIRED WITH DOUBLER IAW SRM 53-00-00-2R-1 FIG. 201 AND 53-80-02-01-1 . (MINOR)Sep 24, 2023 · N259UP · Doug MD11FSDR SWAA2023092603243Tail Cone · delaminatedN0. 3 CANOE FAIRING TAIL CONE HAS 2'X2' AREA DELAMINATION ON OUTBOARD SIDE<[01] REMOVED AND REPLACED PER SRM 51-40-02;[02] C/W INSPECTION REQUIREMENT FOR REMOVAL AND INSTALLATION OF #3 CANOE FAIRING TAIL CONE PER SRM 51-54-02Sep 22, 2023 · N7738A · Boeing 7377BDSDR DALA2023092507883Unknown · unknownSHIP 3142 DAMAGE TO BELLY FAIRING PANEL 191KB. CORRECTIVE ACTION: REPAIRED PER ERA 612263-14. (2981962)Sep 22, 2023 · N342NB · Airbus A319114SDR IPXA2023103120357Unknown · corrodedWING TO BODY T-CHORD AT FR. 1037.67 BETWEEN LBL 63 TO RBL. 63, HAS CORROSION DOT. 65-046. INSTALLED NEW T-CHORD IAW B757 SRM 51-40-02-0G. REVIEWED.Sep 21, 2023 · N425UP · Boeing 75724APFSDR IPXA2023100620357Unknown · unknown*** SDR FILED OPEN *** FAULT: WING TO BODY T-CHORD AT FR. 1037.67 BETWEEN LBL 63 TO RBL. 63, HAS CORROSION DOT. 65-046 INSTALLED NEW T-CHORD IAW B757 SRM 51-40-02-0GSep 21, 2023 · N425UP · Boeing 75724APFSDR IPXA2023100619871Unknown · unknown*** SDR FILED OPEN *** FAULT: WING TO BODY T-CHORD, AT FR, 900 BETWEEN LBL 63 TO RBL 64 HAS CORROSION. DOT. 65-044 VERIFIED MATERIAL RECEIVED ON TRAVELER. T23/1707760.Sep 21, 2023 · N425UP · Boeing 75724APFSDR SWAA2023102502239Skin · corrodedEXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+10 TO BS 747+17 BETWEEN LBL 13 TO RBL (MARKED) STC LARGE EXTERNAL DOUBLER ROW 44 WI-FI -HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+4 TO BS 747+10Sep 19, 2023 · N969WN · Boeing 7377H4SDR SWAA2023102502238Skin · corrodedEXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727B+15 TO BS 727C+14 BETWEEN LBL 10 TO RBL 10 APPROX. 53 EA (MARKED)<[01] 'REFER TO FAULT TTG8Q00NJ6Y7 WHERE EA 23-153-02981 WAS ADDED AS A SUBTASK.';[02Sep 19, 2023 · N969WN · Boeing 7377H4SDR R61A2023100700553Splice Strap · corrodedAFT WING TO FUSE FAIRING STRAP SPLICE BTW FR 73-74, BL 0 CORRODED. R&R IAW SRM 51-42-02 & 51-43-03.Sep 19, 2023 · N431YX · Emb ERJ170200LR
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