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 SWIA20240824Tail Cone · crackedSUSPECTED CRACK ON THE TAILCONE RIGHT SIDE AFT DRAG. (C-CHECK RO 12/21/2024) (FILED OPEN)COMPLIED WITH BOMBARDIER R.E.O. 670-55-31-018 REV. A IN REPAIR TO V/STAB TO FUSE ATTACHMENT R/H AFT DRAG ANGLE. COMPLIED WITH 51-900-1002-SKYSDR SWAA2024100729951Bracket · crackedCRACK BRACKET WING TO BODY FAIRING UPPER AREA OF AIR CONDITIONING COMPARTMENT RT SIDE AT LEVEL BS 540 AT LOWER FUSELAGE 2024-533371<[01] REPLACED BRACKET WING TO BODY FAIRING UPPER AREA OF AIR CONDITIONING COMPARTMENT RT SIDE AT LEVEL BS 540 AT LOWER FUSELAGE SDR SWAA2024093027222Panel · elongatedWING TO BODY FAIRING PANEL 194FR HAS ELONGATED HOLE (MARKED)<[01] REPAIRED DAMAGED FASTER HOLES ON WING TO BODY FAIRING PANEL 194FR IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024091231604Shield · corrodedCORROSION ON FCB FWD SHIELD BS 420+2; BS 420+6.5; BS 420+12.5; BS 420+16; RBL 24.75 WL 156 (MARKED)<[01] VERIFIED;[02] REMOVED AND REPLACED SHIELD FROM BS 420 TO BS 440; RBL 24.75 IAW SRM 51-40-02 AND DWG 143A0080 REV:-;[03] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2024081324965Panel · delaminatedWING TO BODY FAIRING PANEL 193B IS DELAMINATED AT ONE FASTENER HOLE ON FWD EDGE OF PANEL.<[01] REMOVED AND REPLACED WING TO BODY PANEL 193B IAW AMM 53-51-21.SDR SWAA2024081325065Panel · delaminated24-153-02197-TLD (N456WN - SWA - REPAIR - FUSELAGE SECTION 44 EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BL - PERMANENT)<[01] REMOVED AND REPLACED LH WING TO BODY FAIRING PANEL 192BL IAW AMM 53-51-21.;[02] UPDATED INSTALLED P/N IS - 149A725SDR VNAA202408070028Diaphragm · crackedCRACK FOUND COMMON TO WING TO BODY FAIRING DIAPHRAGM AT F.S 913 , RBL 17.3 ON P/N SH670-39241-3. REPAIRED CRACK IAW BOMBARDIER REO 670-53-82-478 REV-A DATED 2014-11-12.SDR SWAA2024081622822Skin · debondedFOUND AREA OF DISBOND ON TAILCONE; RT SIDE LOWER APPROX 10 INCHES AFT OF FWD EDGE. (MARKED)<[01] DISBONDED AREA ON TAIL CONE; RIGHT SIDE LOWER APPROX. 10 INCHES AFT OF FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024090322286Tail Cone · delaminatedAFTER STA 1156; UNDER PANEL 318BR. SPOT OF DELAMINATION ON TAIL CONE SKIN.<[01] REPAIRED DELAMINATION DAMAGE ON TAIL CONE OUTER SKIN ON R/H SIDE STA 1156 UNDER PANEL 318BR WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-1; MATERIALS USED PO#2061896 AND PO#SDR HNAA2024091100742Support Bracket · broken53-2319 RH WING TO FUSE LATERERAL FAIRING SUPPORT BRACKET BROKEN. RAR SUPPORT BRACKET IAW SRM 51-40-02SDR SWAA2024082821854Panel · delaminatedWING TO BODY FAIRING 191FR HAS DELAMINATION AT FWD LOWER CORNER<[01] DAMAGE REMOVAL ACCOMPLISHED FOR LAY UP OF REPAIR PLIES IAW SRM 51-70-05-2R-10 REPAIR #10.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] APPLIED REPAIR PLIES IAW SRM 51-70-05-2R-10 REPSDR SWIA2024080500731Tail Cone · dentedREF EAML 1400473 INSPECTED LOWER AFT TAILCONE IMPACT AREA AND FOUND DENT MEASURING 6.95" L X 2.6" W X 0.38" D AND DETERMINED TO BE OUT OF LIMITS PER ERJ 175 SRM 53-31-01. NO OTHER DAMAGE FOUND (FLIGHT 5511 - FILE CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMPSDR SWAA2024090934940Support Angle · crackedCRACK BODY FAIRING SUPPORT ANGLE BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-473102<[01] REPLACED BODY FAIRING SUPPORT ANGLE AND FASTENERS LOC BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 149A7101 SHEET 7 RESDR SWAA2024090618645Fairing · crackedCRACK BODY FAIRING SUPPORT ANGLE BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-473102<[01] REPLACED BODY FAIRING SUPPORT ANGLE AND FASTENERS LOC BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 149A7101 SHEET 7 RESDR SWAA2024090317220Access Panel · crackedCRACK ACCESS PANEL 195BL BODY FAIRING HOLE FUSELAGE EXTERIOR 2024-454519<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 11/APR/25.;[03] ON STEP 10 TOOL USED ULTRASOSDR SWAA2024090332036Radome · peelingPEELED PAINT NOSE RADOME AT RADOME 2024-454518<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N A24028535 DUE DATE: 06 JUN 24.;[02] FAULT RESOLVED ON OTHER FAULT PLEASE SEE TTG800VGEDR;[03] FAULT RESOLVED ON OTHER FAULT PLEASE SEE TTG800VGEDRSDR SWAA2024090314928Support Angle · crackedR/H FWD WING TO BODY FAIRING SUPPORT ANGLE ATTACHED TO FIXED L/E I/B CRACKED AT FASTENER TAIL MKD DOT CORRECTION LEFT HAND<[01] REMOVED AND REPLACED L/H FWD WING TO BODY FAIRING SUPPORT ANGLE ATTACHED TO FIXED L/E I/B SIDE AS PER B737-700 SRM 51-40-02-0G-0 ANDSDR SWAA2024091014080Access Panel · elongatedELONGATED HOLE ACCESS PANEL 195CR BODY FAIRING AT LOWER FUSELAGE 2024-455036<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B-AV; S/N:18196126; DUE DATE:03-APR-25.;[03] TOOL USED SCALE P/N: CR5SDR SWAA2024071913652Fairing · crackedWING TO BODY PANEL 192AR HAS A CRACKED AREA.<[01] 04 - REPAIRED PER [SRM 53-40-70-2R-1-B00375 (REPAIR 1 - SECTION 44 WING-TO-BODY FAIRING SKIN PANELS MADE OF COMPOSITE MATERIALS - PERMANENT)];[02] 02 - INSPECTED PER [SRM 53-40-70-2R-1-B00375 (REPAIR 1 - SECTIOSDR SWAA2024071713241Panel · delaminatedR/H FWD O/B WING-TO-BODY FAIRING PANEL 193AR DELAMINATION DAMAGE<[01] R&R PANEL PER SRM 51-40-02 AND 24-153-01717;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR UATA202408024531Fairing · crackedTHE FUSELAGE TO WING FILLET FAIRING, WHERE IT WRAPS AROUND THE FUSELAGE TO ATTACH AT FRAME 5 WAS FOUND CRACKED. THIS IS THE THIRD AIRCRAFT IN OUR FLEET THIS YEAR WITH A SIMILAR CRACK. THERE IS AN AD NOTE ON THE FRAME 5 AND FUSELAGE SKIN CRACKING IN THIS AREASDR SWIA2024092032Buttstrap · corrodedMLG FAIRING PANEL 194AB R/H TOP BUTTSTRAP FUSELAGE MULTIPLE AREA HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE M/C BEAM AT RBL48 BETWEEN FS826 - FS836 REF REO 670-53-42-100 REV -- 2024-08-28. COMPLIED WITH TASK CARD 51-900-10SDR SWAA2024081610456Panel · debondedPANEL 194DL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] 'PANEL 194DL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)' IS COMPLETED IAW SRM 51-70-05-2R-2.;[02] 'PANEL 194DL DISBOND' IS REPAIRED IAW SRM 51-70-05-2R-2.;[03] VERIFIED CORRECTSDR DALA2024070806933Radome · delaminatedSHIP 3155 RADOME DELAMINATION/DAMAGE. CORRECTIVE ACTION: REPAIRED PER A319 AMM 53-15-11- 300-001-A. (6190650)SDR SWAA2024082609174Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL BODY FAIRING AFT EDGE AT LOWER FUSELAGE 2024-420703<[01] TOOL USED; CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 25/JAN/25.;[03] TOOL USED: HOT BONSDR HNAA2024090400224Rib · crackedCF3, WING TO FUSELAGE FAIRING RH AFT WHEELWELL RIB FOUND CRACKED.SDR JGVR202406264001Skin · corrodedREPAIRED CORRODED AREAS OF THE LOWER AFT FUSELAGE TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING AREAS BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITSDR SWAA2024072403312Panel · debondedDISBONDS NOTED ON INNER SURFACE OF PANEL 193AR<[01] REPAIRED DISBONDS ON INNER SURFACE OF PANEL 193AR IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11;[02] VERIFIEDSDR SWAA2024071803364Doubler · corrodedCORROSION R/H LOWER FWD WING TO BODY FAIRING PANEL # 191CR HAS CORROSION AT INNER DOUBLER DRAING MAST.<[01] EVALUATED DAMAGE AT R/H LOWER FWD WING TO BODY FAIRING PANEL # 191CR INNER DOUBLER DRAING MAST FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND RESDR SWAA2024070502514Fairing · crackedFAIRING PANEL 194HL FASTENER HOLE (1EA) CRACKED<[01] APPLIED REPAIR TO DAMAGED AREA AT PANEL 194HL AS PER B737 SRM 51-70-01-2R-0 PARAG 4.L-M-N. APPLIED TOPCOAT AT REPAIR AREA ON PANEL 194HL AS PER B737 AMM 51-21-99-300-802 PARAG 3.C.3.SDR CALA2024061701810Sealant · missingSEALANT ON UPPER FWD LEFT WING TO BODY FAIRING PEELING OFF. SHOULD BE RIGHT WING. RE-APPLIED SEALANT REF MM 53-51-21 AND 51-31-00.SDR CALA2024061701820Fairing · missingPDA 1 DURING PILOT WALKAROUND, FOUND FAIRING PANEL 194E IS MISSING FROM LOWER BELLY AFT OF THE WHEEL WELL.SDR WX0A2024061932078Skin · damaged(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 3000-0026: 1711-20 LIGHTNING STRICK FOUND ON TAIL CONE FUSELAGE RH SIDE AT FR77 / BETWEEN STRG 8R & 9R. / ON TAIL CONE FUSELAGE SKIN, R/H SIDE AT FR77 AND BTW STR 8R-9R LIGHTNISDR SWAA2024071100722Access Panel · delaminatedDELAMINATED ACCESS PANEL 191D AT LOWER FUSELAGE 2024-384279<[01] TOOL USED CALIPER PN: 500-464; SN: B17030933; DUE DATE: 07/NOV/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 15-FEB-25.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8342514502SDR HEEA202406110149Pylon · corrodedEXCESSIVE CORROSION FOUND INSIDE OF VERTICAL TAIL PYLON.SDR WX0A2024061932079Skin · damaged(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 3000-0017: 1711-20 LIGHTNING STRICK FOUND ON TAIL CONE FUSELAGE RH SIDE AT FR74 AND STGR 10R. / ON TAIL CONE FUSELAGE SKIN, R/H SIDE AT FR74 AND AT STR10R LIGHTNING STRIKE PERMSDR SWIA20240925606Radome · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA81072-601R-53-11-3808 N494CA MXCODEID64640-PR - 2 DENT'S BETWEEN FS169 AND FS 173 AT RIGHT SIDE FORWARD EQUIPMENT COMPARTMENT DOOR AND NOSE RADOME. PERFORMED TEMPORARY REPAIR/DRESSBACK OF DENTS ACCEPTABLE FOR 2950 FHS SDR HNAA2024072600607Support Angle · cracked53-2216 ANGLE SUPPORT 1 AND 2 CRACKED ON LH UPPER SURFACE, WING TO BODY FAIRING. REPAIRED ANGLE SUPPORT 1 IAW EO1-05-24-0340. REPLACED ANGLE SUPPORT 2 IAW SRM 51-40-02SDR HNAA2024072600605Support Angle · cracked53-2213 AFT SUPPORT ANGLE CRACKED ON THE RH WING TO BODY FAIRING UPPER SURFACE, REPAIRED IAW EO1-05-24-0340SDR HNAA202407260002Support Angle · cracked53-2213 AFT SUPPORT ANGLE CRACKED ON THE RH WING TO BODY FAIRNG UPPER SURFACE. REPAIRED IAW EO1-05-24-0340SDR JGVR20240605001Skin · damagedREPAIRED THE TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER, FILLER, AND SHIM IN ACCORDANCE WITH TEXTRON FIELD REPAIRSDR DALA2024060505800Radome · damagedSHIP 3166 DAMAGE ON NOSE RADOME CENTER. CORRECTIVE ACTION: APPLIED EROSION PROTECTION TAPE PER A319 AMM 53-15-11-300-001-A. (4896208)SDR U2RA2024081500039Support Frame · corrodedDURING MAINTENANCE C CHECK AT GMF FOUND LOWER FUSALAGE STA 1000 CENTER TO RH SIDE SUPPORT FRAME FOR BODY FAIRING CORRISON . REAPIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-70-12 (REV59/20FEB2024) AND WAS A CAT A REPAIR.SDR SWAA2024070997361Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE 2024-361518<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: SCALE P/N: CR5200SDR SWAA2024062791779Skin · delaminatedFORWARD TAILCONE ASSEMBLY OUTER SURFACE SKIN HAS 2 AREAS OF DELAMINATED SKIN COMMON TO THE INNER SURFACE TAILCONE LIGHT SWITCH BRACKET. FORWARD TAILCONE ASSEMBLY OUTER SURFACE SKIN HAS 2 AREAS OF DELAMINATED SKIN COMMON TO THE INNER SURFACE TAILCONE LIGHT SWITSDR SWAA2024070390663Support Angle · crackedR/H WING-TO-BODY ACCESS PANEL 191AR AS SUPPORT ANGLE CRACKED<[01] REMOVED AND REPLACED NEW SUPPORT ANGLE AT R/H WING-TO-BODY ACCESS PANEL 191AR PER REF B 737 SRM 51-40-02-0G-0 AND DWG 116A3110.;[02] VERIFIED STEP 1. AUDIT C/W PER MPM 52.02.02.SDR AALA202405316369Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BRACKET OF BELLY FAIRING STRUCTURE LOCATED BETWEEN FR 42 TO FR 43 AT S43L. REPLACED BRACKET PER SRM 51-42-11-801 AND SRM 51-72-11-911.SDR SWAA2024062790465Skin · debondedAFT TAILCONE ASSEMBLY SKIN DISBOND AT 12 O'CLOCK; 6' FROM FWD EDGE. AFT TAILCONE ASSEMBLY SKIN DISBONDED AT 12 O'CLOCK; 6 INCHES FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2024062790466Skin · debondedFORWARD TAILCONE ASSEMBLY SKIN DEBONDED AT 5 O'CLOCK; 6' FROM FWD EDGE. FORWARD TAILCONE ASSEMBLY SKIN DISBOND AT 5 O'CLOCK; 6 INCHES FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-4.SDR DALA2024052405509Fairing · looseAIRCRAFT 3902, BODY FAIRING PANEL 192HR HAS A LOOSE PAD. CORRECTIVE ACTION: RESECURED PAD AND REMOVED AND INSTALLED PANEL 192HR PER B737 AMM 53-51-21. (LP 0357795
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