JASC 5350
Service difficulty reports · 6,123
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 SWAA2021081294036Radome · damagedNOSE RADOM IS DAMAGED. / R&R NOSE RADOME IAW AMM 53-52-00 ONLY POS TAG 682102 - P/N OFF: 1001002-2 S/N OFF: WN0030 P/N ON: 1001002-7B S/N ON: C184366-05SDR SWAA2021072995052Fairing · debondedFAIRING 195BR OUTER SKIN HAS A DISBONDED DENT NEAR AFT EDGE OF PANEL. (MARKED) / REPAIRED FAIRING 195BR OUTER SKIN DISBONDED DENT NEAR AFT EDGE OF PANEL IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11SDR SWIA2020072751486Support · corrodedAFT WING-TO-BODY SUPPORT STRUCTURE- STRAP LOCATED AT RBL 17.63 BETWEEN FS879 AND FS909 IS CORRODED (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW WING TO BODY SUPPORT STRAP LOCATED AT RBL 17.63 BETWEEN FS879 AND FS909 AND RESTORED FINISH IAW CRJ700 SRM.SDR SWIA2020072751485Support · corrodedAFT WING-TO-BODY SUPPORT STRUCTURE- STRAP LOCATED AT LBL 17.63 BETWEEN FS879 AND FS909 IS CORRODED. REMOVED AND INSTALLED 1EA NEW LBL 17.63 STAP BETWEEN F.S. 879 AND 909 AND RESTORED FINISH IAW SRM.SDR SWAA2021081293567Radome · damagedON WALK AROUND FOUND DAMAGE ON NOSE RADOME / R/R NOSE RADOME REF AMM 53-52-00 POS ONLY TAG 678511 - P/N OFF: 1001002-6A S/N OFF: 0007214 P/N ON: 1001002-7B S/N ON: C167202-3SDR SWIA2020072751484Support · corrodedAFT WING-TO-BODY SUPPORT STRUCTURE €“ MID ANGLE AT FS847 HAS CORROSION. REMOVED CORROSION FRM AFT WING TO BODY SUPPORT STRUCTURE-MID ANGLE AT FS847. REF CRJ 700 SRM. PART OUT OF LIMITS. REF CRJ 700 SRM. REMOVED AND REPLACE PART WITH A NEW PART. REF CRJ 700 SSDR SWIA2020072751483Support · corroded*AFT WING-TO-BODY SUPPORT STRUCTURE AT LEFT AND RIGHT CENTER STRAPS AT FS879 HAVE CORROSION/FRETTING. (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED 2EA NEW RBL36 AND LBL36 STAPS AT F.S. 879, AND RESTORED FINISH IAW CRJ700 SRM.SDR SWIA2020072751482Support · corroded*AFT WING-TO-BODY SUPPORT STRUCTURE €“ MID STRAP AT FS909 HAS CORROSION. REPLACED CORRODED AFT WING-TO-BODY SUPPORT STRUCTURE MID STRAP AT FS909 WITH NEW STRAP (P/N: SH670-39338-3) REF CRJ-700 SRM, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020072751481Support · corrodedAFT WING-TO-BODY SUPPORT STRUCTURE €“ CENTER FAIRING ATTACH ANGLE AT FS939 HAS CORROSION. BLENDED OUT CORROSION ON THE CENTER FAIRING ATTACH ANGEL AT FS939, AFT WING TO BODY SUPPORT STRUCTURE. REF CRJ 700 SRM. BLEND OUT OF LIMITS. REMOVED AND REPLACED AFT WISDR IPXA2020071457782Filler · chafedINSPECTION TYPE:3C TAIL CONE RT PRODUCTION FILLER IS CHAFED. REMOVED, FABRICATED AND REPLACED FILLERS IAW EO MD11-5350-66790-A. (MINOR)SDR SWAA2021081291425Boot · damagedNOSE RADOME BOOT IS DAMAGED / REMOVED RADOME BOOT IAW AMM 53-52-00-000-802 TAP TESTED. NO DISBONDS NOTED IAW SRM 51-10-06-0G-0 PARA 5&7 13742C 06-12-20 INSP 357 JUN 12 2020 INSTALLED NEW NOSE RADOME PROTECTIVE BOOT IAW AMM 53-52-00-400-802 PAR 5.E(1)-(14). 664SDR SWIA2020070151285Support Rib · crackedCENTER BELLY FAIRING AFT SUPPORT (RIB) AT FR 52 HAS CRACK IN RADIUS ON UPPER EDGE OF LEFT SIDE (NEAR PILOT'S AILERON TORQUE TUBE). (C-CHECK) RO 6/29/2020 REMOVED AND REPLACED CENTER BELLY FAIRING AFT SUPPORT RIB AT FR52 LT SIDE, REF SRM.SDR SWAA2021081290662Boot · damagedNOSE RADOME BOOT IS DAMAGED / REMOVED AND REPLACED DAMAGED RADOME BOOT IAW AMM 53-52-00-400-802SDR IPXA2020070157158Frame · damagedINSPECTION TYPE:2C TAIL CONE LT PATIO DOOR AFT FRAME IS BENT AND DAMAGED. REMOVED, FABRICATED AND REPLACED FRAME IAW DWG AKC7820 AND SRM 51-35-01. (MINOR)SDR IPXA2020062456949Frame · chafedINSPECTION TYPE:2CTAILCONE FWD UPPER FRAME (BEAM) IS CHAFED IN 4 AREAS.REPAIRED TAILCONE FWD UPPER FRAME (BEAM) CHAFE DAMAGE IAW MD-11 SRM 53-00-00 FIG. 210. (MINOR)SDR SWAA2021081289939Radome · damagedNOSE RADOME HAS FIBER DAMAGE / REPLACED RADOME REF MM 53-52-00 TAG NO: 663058 PN ON: 10010027B SN ON: C152308 PN OFF: SN OFF: 9810012CSDR FDEA2020061241127Repair · delaminatedTAILCONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 OCLOCK POSITION. ACCOMPLISHED REPAIR ON TAIL CONE EXTERIOR LT SIDE BS 1960 IAW SRM 53-80-01-2R AND IAW SRM 51-70-10-2R REP 2.SDR FDEA2020060541127Skin · delaminatedTAIL CONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 O’CLOCK POSITION.SDR SWAA2021082789547Panel · damagedLOWER FUSELAGE BODY FAIRING PANEL # 193 AR HAS 5 EA HOLES THAT ELONGATED MKD DOT 60-009 / REPAIRED DAMAGE AREA AT LOWER FUSELAGE BODY FAIRING PANEL #193AR AS PER BOEING 737 SRM 51-770-02R-9 REPAIR 9 MATERIAL USED EY3804A/B P/O 1675204 PLUS BM59-3-TY-H3 P/O 148SDR IPXA2020062256791Intercostal · crackedINSPECTION TYPE:2C TAILCONE INTERCOSTAL IS CRACKED AT FWD UPPER GUIDE PIN. REMOVED AND REPLACED CRACKED INTERCOSTAL AT UPPER FWD TAILCONE GUIDE PIN IAW SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2020061256464Filler · chafedINSPECTION TYPE:2C TAILCONE LT FWD UPPER PRODUCTION DOUBLER REPAIR FILLER IS CHAFED. REPAIRED CHAFED TAILCONE LT FWD UPPER PRODUCTION DOUBLER FILLER IAW EO MD11-5350-66790-A APPENDIX B. (MINOR).SDR IPXA2020070857530Skin · damagedINSPECTION TYPE:3C AFT EXTENDED TAIL CONE LOWER T/E CAP SKIN AT STA 2318-2325 AND Z=25.925 TO Z=64.075. REPAIRED DAMAGED AFT EXTENDED TAIL CONE IAW EA 011-5380-01-A8354 REV I/R AND EO MD11-5350-77103-A. (MINOR)SDR IPXA2020070857528Doubler · chafedINSPECTION TYPE:3C TAIL CONE INTERNAL PRODUCTION DOUBLER AT STA 2163 AND BETWEEN Z= 40 TO Z= 60 HAS CHAFE DAMAGE. REPAIRED DAMAGED TAIL CONE PRODUCTION DOUBLER IAW EA 011-5350-01-A8337 REV I/R AND EO MD11-5330-77105-A. (MINOR)SDR IPXA2020070357257Angle · puncturedINSPECTION TYPE:3C EXTENDED TAILCONE HAS PUNCTURED THROUGH THE RT Z-FRAME. REPAIRED EXTENDED TAILCONE RT Z-FRAME IAW EA 011-5300-1-A8334 REV IR AND EO MD11-5350-77041-A. (MINOR)SDR SWAA2021082581109Support Bracket · crackedLH FWD UPPER WTB FAIRING AFT SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED LH FWD UPPER WTB FAIRING AFT SUPPORT BRACKET PER SRM 51-40-02.SDR SWAA2021061580768Fairing · delaminatedLOWER FUSELAGE BODY FAIRING PANEL # 194DL HAS SPOT DELAMINATION 31/2 INCHES FROM EDGE UPPER SURFACE SKIN / CLEANED & REPAIRED 3.4 DIA SPOT DELAMINATION ON LOWER FUSEAGE BODY FAIRING PANEL #194DL AS PER B737-700 SRM 51-70-04-2R-1 MATERIAL USED PO# 1480720 & PO#SDR IPXA2020061056397Doubler · chafedINSPECTION TYPE:4C TAILCONE RT FWD PRODUCTION DOUBLER CHAFED. REPAIRED CHAFED RT FWD PRODUCTION DOUBLER ON TAILCONE IAW EO MD11-5350-66790-A. (MINOR)SDR SWAA2021060980788Support · chafedWING TO BODY FAIRING FORMER SUPPORT HAS CHAFING DAMAGE BS727A JUST ABOVE NO.5 FLAP TRACK. MARKED / REMOVED AND REPLACED WTB FAIRING FORMER SUPPORT AT 727A ABOVE #5 FLAP TRACK IAW BOEING DWG 149A7506 REV A AND SRM 51-40-02SDR SWAA2021060980787Support · chafedWING TO BODY FAIRING FORMER SUPPORT HAS CHAFING DAMAGE BS727A JUST ABOVE NO.4 FLAP TRACK. MARKED / REMOVED AND REPLACED WTB FAIRING FORMER SUPPORT AT 727A ABOVE #4 FLAP TRACK AS MARKED IAW BOEING DWG 149A7506 REV A AND SRM 51-40-02SDR UIEA2020052101029Skin · dentedDENT WITH CREASE WAS FOUND ON FUSELAGE TAIL CONE SKIN BETWEEN STA 1832 / STA 1843 RH SIDE(<P ><SPAN>DAMAGE REPAIRED IN / ACCORDANCE WITH MEXICANA MRO TRE6753348.</SPAN></P>)SDR SWAA2021082780812Access Panel · delaminatedDELAMINATED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE / REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-1 REPAIR 1. TOOL USED CALIPER PN 500-196-30 SN 14334575 DUE DATE 19-DEC-20; HOT BONDER PN HCS8800 SN 011125SDR SWAA2021081278774Boot · damagedNOSE RADOME BOOT IS DAMAGED / REMOVED DAMAGED RADOME BOOT; NO COMPOSITE DAMAGE NOTED IAW AMM 53-52-00-000-802 PAR 4C(1-4). 6042U 19MAY20. 10537C 05/19/20 INSP 14 05/19/20 INSTALLED NEW RADOME BOOT DB-1 IAW AMM 53-52-00-400-802 PAR 5E(1-14) 6042U 25MAY20. 10537SDR YENA2020051950347Web · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION BELLY FAIRING WEB FASTENER COMMON TO THE TI -ANGLE LOCATED FR41-42 RH SIDE; (REF AEROMAN NR 168606 WO 2020 156/1) PERFORMED PERMANENT REPAIR ON BELLY FAIRING SUPPORT WEB FR41-42 RH SIDE IAW EC # A20-438-01.SDR IPXA2020051355233Plate · damagedINSPECTION TYPE:SEGPANEL 485A HAS SEVERAL HOLES ELONGATED I/B FLANGEREPLACED (2EA) LONGERONS/PLATE IAW SRM 51-40-21SDR IPXA2020051355245Plate · damagedINSPECTION TYPE:SEGPANEL 485AL (3)HOLES ELONGATED ON I/B ATTACH FLANGE, FWD PORTIONREMOVED AND REPLACED PLATE IAW SRM 51-40-21SDR DALA2020051302388Frame · crackedDURING ACCOMPLISHMENT OF AMDS W/C 5352-01036-02 FOUND L/H FRAME ASSY P/N C02383117-001 CRACKED ALONG LOWER FLANGE-CONTACTED LIAISON ENGINEERING. ADDITIONAL ENGRS DOCUMENTATION REQUIRED PRIOR TO FURTHER FLIGHT CRACK MEASURES 14" LONG C/A R&R FRAME ASSY PER A220SDR SWIA2020061251115Support · corrodedAFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE AT FS939 IS CORRODED. (C-CHECK) RO 6/8/2020 AFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE AT FS939 REPLACED. REF: SRM AND DWG.SDR UIEA2020051200769Support · corrodedFX KEEL BEAM L/H BODY FAIRING ( 191JJ ) ACCESS PANEL SUPPORT FOUND CORROSION.(<P>FX KEEL BEAM LH BODY FAIRING ( 191JJ ) ACCESS PANEL SUPPORT CORROSION AREA REPAIRED AS PER SRM 53-00-71 FIG 101.</P>)SDR UIEA2020051200770Support · corrodedFX KEEL BEAM RH BODY FAIRING ( 191JJ ) ACCESS PANEL SUPPORT FOUND CORROSION.(<P>FX KEEL BEAM RH BODY FAIRING ( 191JJ ) ACCESS PANEL SUPPORT CORROSION AREA REPAIRED AS PER SRM 53-00-71 FIG 101.</P>)SDR UIEA2020051201017Support · corrodedFX KEEL BEAM BODY FAIRING STA 1480 - 1490 BL0 SUPPORT FOUND CORROSION.(<P><SPAN>FX KEEL BEAM BODY FAIRING STA 1480 - 1490 BL0 SUPPORT CORROSION AREA REPAIRED AS PER SRM 53-00-71 FIG 101.</SPAN><BR /></P>)SDR V0XD20200515001Angle · crackedRH LATERAL WING TO BODY FAIRNING LOWER SUPPORT BRACKET #2 (P/N: 145-67291-002) CACKED. SEE AVMAX W/O: 80859 W/C: 6013 FOR REPAIR.SDR UIEA2020050700967Frame · corrodedCORROSION - TEE, R/H WING TO BODY FAIRING FRAME, STA 960 RBL 1.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 45. INSTALL REPAIR PART IAW SRM 51-40-02 REV. 45 AND DWG 65B061756, SH2, REV. K, AND EI T2020A53M-1130 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMASDR UIEA2020050700968Bracket · corrodedCORROSION - BRACKET, R/H WING TO BODY FAIRING FRAME FWD AND AFT SIDE, STA 840, RBL 32. TOTAL 2EA.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 45. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 45 AND DWG NO. 65B06703 SHEET 2, REV. 1, AND DWG NO. 65B04117 SHEET 2 RSDR UIEA2020050700969Angle · corrodedCORROSION - ANGLE L/H WING TO BODY FAIRING FRAME FWD AND AFT SIDE, TOTAL 2EA, STA 840, LBL 32.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 45. INSTALLED NEW PARTS IAW SRM 51-40-02 REV. 45 AND DWG NO 65B06703 SHEET 2 REV L AND DWG NO 65B04117 SHEET 2 REV N ASDR UIEA2020050700980Angle · corrodedCORROSION ON ANGLE OF FUSELAGE FAIRING AT STA 933 LBL 5.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV 45. FABRICATED NEW PARTS IAW EI NO T2020P53M-1126, REV 0. INSTALLED NEW PARTS IAW SRM 51-40-02 REV 45 AND DWG NO 65B06712 SHEET 3, REV G AND DWG NO 65B06712 SDR DALA2020050402339Cable · out of positionMAINTENANCE FOUND THE TAILCONE DEPLOYMENT KEVLAR CABLE TO BE INSTALLED/ROUTED INCORRECTLY. THE CABLE WAS RE-INSTALLED AND ROUTED CORRECTLY IN ACCORDANCE WITH B717 AMM 53-52. THE REQUIRED INSPECTION IS COMPLETE. (LP #6898954)SDR IPXA2020052055532Intercostal · crackedINSPECTION TYPE:2CTAILCONE L/E INTERCOSTAL AT R/H SIDE CENTER PIN IS CRACKED.REMOVED AND REPLACED CRACKED TAILCONE L/E INTERCOSTAL AT R/H CENTER PIN IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR YENA2020050470321Skin · dentedDURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN ON TAIL CONE 1"" AFT TO LH LOWER PANEL; REF AEROMAN NR 2020-125440 ACCOMPLISHED REPAIR OF THE BULGE AND CORROSION DAMAGES ON LH & RH SKINS OF THE TAIL CONE ASSY (P/N 170-98035-415 S/N 0132001) IAW AEROMAN EA 53-0276SDR SWAA2021082786854Fairing · damagedLOWER WING TO BODY FAIRING 193AL; LEFT FWD. WHEEL WELL PANEL; INFOARD FASTENER HOLE ELONGATED/WORN THROUGH COMPOSITE. / REPAIRED FASTENER HOLE I/B EDGE OF FAIRING 193AL; WORK ACCOMPLISHED ON N/R #40847-1700-0021; (Y218619)SDR SWAA2021060943985Former · chafedFAIRING FORMER BS 657-665 RBL 28 HAS CHAFE DAMAGE / REMOVED AND REPLACED FAIRING FORMER BS 657-665 RBL 28 IAW SRM 51-40-02-0G-0 AND DWG 149A7216
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