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 SWAA2021071279279Fairing · chafedCHAFE DAMAGE ON INNER SURFACE OF 192E FAIRING / [01] IDENTIFIED PANEL192E / MATERIAL IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM (3). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B.(6)(A). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-SDR IPXA2021062570958Tee Fitting · corrodedINSPECTION TYPE:3CR/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME AT STA 1521 IS CORRODED.REPAIRED CORRODED R/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME TEE AT STA 1521 IAW VT-SAA EA 011-5314-01-A9182 REV. IR AND UPS EO MD11-5320-80808-A. (MINOR)SDR SWAA2021060478898Fairing · chafedWING TO BODY FAIRING PANEL 194CL INNER SURFACE AREAS ARE CHAFED. CHAFING ALONG THE INNER EDGE BAND EXCEEDS THE ALLOWABLE LIMITS OF SRM 53-60-70-1A-1 PARA 4 B 3 A. REMOVED CHAFING DAMAGE FROM ALONG THE INNER EDGE BAND; CLEANED REPAIR AREA. FABRICATED REPAIRSDR DALA2021060203009Cable · corrodedTHE CABLE COMING FROM THE INTERIOR RELEASE HANDLE THAT GOES OUT TO A "Y" SPLIT CONNECTION HAS CORROSION ON IT. MARKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 001-0316:5353-2001/002 00183SDR DALA2021060203010Cam · out of adjustTHE TAILCONE RELEASE CAM IS OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 102-0001:5352-2001/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF. B717 AMM 53 -52-03. (LP #SDR 2021F00119Splice Strap · crackedREPAIR OF LH/RH CENTER FAIRING SUPPORTS CRACKS. NJA EO WC C68-53-0003_1 DATED: 02/15/2019, LH/RH CENTER FAIRING SUPPORT SPLICE STRAP REPAIR.SDR VNAA2021051699917Support Strap · corrodedFOUND THE LH AND RH OB BL 40-45 FUSELAGE FAIRING LOWER SUPPORT CORRODED AT FS 847 FS 27-36. INSTALLED NEW STRAP IAW CRJ700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01.SDR VNAA2021051699915Support Strap · corrodedFOUND THE LH AND RH LOWER OB BL 40-45 FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED. INSTALLED NEW SERVICEABLE SUPPORT STRAP IAW CRJ700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01SDR VNAA2021051699914Support Strap · corrodedFOUND THE RH FSL 36 FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED FROM FS 847-879. INSTALLED NUTPLATES AND NEW STRAP AT FUS FAIRING SUPPORT FS 847.0 TO 879, RBL 36.0 IAW CRJ700 SRM 51-42-06-001-001-A01SDR VNAA2021051699913Support Strap · corrodedFOUND THE LH BL 36 FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED FROM FS 847-879. INSTALLED NEW SREVICEABLE SUPPORT STRAP IAW CRJ 700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-06-001-001-A01.SDR VNAA2021051699912Support Strap · corrodedFOUND THE LH LOWER FS 879. FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED AND THE RH LOWER STRAP ALSO. INSTALLED NEW SERVICEABLE LH AND RH LOWER FS 879 FAIRING SUPPORT STRAP IAW CRJ 700 SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01SDR VNAA2021051699911Support Strap · corrodedFOUND THE FS 879.909 FUSELAGE FAIRING SUPPORT STRAP AT RBL 17 TO BE CORRODED. INSTALLED FUSELAGE FAIRING SUPPORT STRAP FROM FS 879-909 RBL 17 IAW CRJ 700 SRM 51-42-06-001-001-A01,SRM51-45-00-001-001-A01, SRM 51-42-06-001-001-A01.SDR VNAA2021051699910Strap · corrodedFOUND THE FS 879.909 FUSELAGE FAIRING SUPPORT STRAP AT LBL 17 TO BE CORRODED. INSTALLED NEW SREVICEABLE SUPPORT STRAP IAW CRJ 700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01SDR VNAA 202105169999Strap · corrodedFOUND THE FS 909 FUSELAGE FAIRING SUPPORT MID STRAP TO BE CORRODED. INSTALLED NEW SERVICEABLE FS 909 MID STRAP IAW CRJ700 SRM'S 51-42-06-001-001-A01 AND 51-42-10-001-001-A01.SDR SWIA2021072159642Intercostal · cracked*LEFT HAND WING TO BODY FAIRING SUPPORT STRUCTURE ON INTERCOSTAL IS CRACKED FS449.85. (MARKED & FLAGGED) (C-CHECK RO 7/18/2021) INSTALLED NEW SUPPORT ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-45-00 AND DWG 601R-31037 REV. FSDR SWIA2021072159641Support · cracked*RIGHT HAND WING TO BODY FAIRING SUPPORT STRUCTURE ON INTERCOSTAL IS CRACKED JUST FORWARD OF FS473.15. (MARKED & FLAGGED) (C-CHECK RO 7/18/2021) INSTALLED NEW SUPPORT ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-45-00 AND DWG 601R-SDR SWIA2021072159640Support · cracked*LEFT HAND WING TO BODY FAIRING SUPPORT STRUCTURE ON INTERCOSTAL IS CRACKED JUST AFT OF FS473.15. (MARKED & FLAGGED) (C-CHECK RO 7/18/2021) INSTALLED NEW SUPPORT ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-45-00 AND DWG 601R-31037SDR SWIA2021072259741Support · corrodedCORROSION ON SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE FAIRING FS 909 MID ANGLES. MARKED. (C-CHECK RO 7/20/2021) CORROSION COVERS MORE THAN 30% OF AFT WING-TO-FUSELAGE FAIRING FS 909 MID ANGLES AND IN MULTIPLE SPOTS NEXT TO FASTENER HOLES CORROSION IS 10SDR DALA2021051002604Panel · missing(LOG 7474400) DURING WALK AROUND, FOUND LWR FUSELAGE PANEL 194E MISSING. DRILLED, INSTALLED PANEL REF IPC B737 53-51-00-15 ITEM 090J AND IAW B737 AMM 53-51-21-400-801.SDR DALA2021051002613Support · crackedSHIP 3244 CRACK SUPPORT WEB BELLY FAIRING AT LEVEL OF FR47 AND Y305 APPROX AND BTW STR 40/41 LH AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 591232-14 REV.ORIGINAL AND PRI REV.0. (1802877)SDR SWAA2021050568135Panel · wornPANEL 194E HAS SEVERAL HOLES ENLARGED/ WORN TO .238 FOR A .187 FASTENER. ; / PER TSR 2021001997 REMOVED AND REPLACED WING TO BODY PANEL 194E IAW AMM 53-51-21SDR WX0A2021050573705Access Panel · corrodedDURING THE 24MO CHECK, THE LOWER FUSELAGE WING TO BODY FAIRING ACCESS PANEL 191BB ANGLE AT FWD KEELBEAM CORRODED. / REPLACED T-ANGLE AT FWD KEEL BEAM AREA AT LOWER FUSELAGE WING TO BODY FAIRING ACCESS PANEL AT 191BB PER SRM 51-42-11. SEE AWS FOR DETAILS OF ACCSDR IPXA2021051069213Web · crackedINSPECTION TYPE:C2FWD TAILCONE LH PATIO DOOR INNER WEB CRACKREPAIRED CRACK WEB IAW SRM 53-80-02 REPAIR 5 (MINOR).SDR IPXA2021050769121Skin · damagedINSPECTION TYPE:C2FWD TAILCONE LH DOOR SKIN HAS EDGE DAMAGE AT LWR AFT END.REPAIRED SKIN EDGE DAMAGE AT TAILCONE IAW SRM 52-00-00 FIG 204 (MINOR).SDR IPXA2021052169656Filler · wornINSPECTION TYPE:2CTAIL CONE R/H UPPER PRODUCTION DOUBLER FILLER IS WORN STA2165, X=36.5 AND BETWEEN Z= 35 TO 60.1.REMOVED FABRICATED AND REPLACED FILLER IAW UPS EO MD11-5350-66790-B. (MINOR)SDR IPXA2021050368892Intercostal · crackedINSPECTION TYPE:2CTAIL CONE INTERCOSTAL IS CRACKED 2ND FROM BOTTOM GUIDE PIN.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. AKC7520 AND SRM 51-33-01. (MINOR)SDR AALA202104229002Radome · damagedAIRCRAFT WAS GROUNDED: LIGHTNING STRIKE ON RADOME SHORTLY AFTER TAKEOFF WITH DISCHARGE FELT THROUGH RUDDER PEDALS; NO OTHER INDICATIONS OR ISSUES, FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD AS A PRECAUTION. ACCOMPLISHED LIGHTNING STRIKE CHECK IAW WORKCARDSDR U2RA2021042300014Support · crackedREFER TO LP 43984-3 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1620, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 162SDR U2RA2021042300013Support · crackedREFER TO LP 43984-1 AND FVCI ENGINEERING ORDER #21077-1: UPON REMOVAL OF WTB FAIRING PANELS 194BR, 194 CR, AND 194DR, FOUND DAMAGE TO THE WTB FAIRING SUPPORT RIB STRUCTURE AT BS 1540, R/H SIDE. ACCOMPLISHED INTERIM ANGLE REPAIR TO RIB CHORD MEMBERS AT BS 154SDR SWIA2021080960129Nut Plate · brokenAFT BELLY FAIRING 196AL HAS 1EA BROKEN NUT PLATE. REPLACEMENT REQUIRED. (MARKED W/ TAPE) (C-CHECK RO 8/5/2021) PERFORMED REPAIR TO FUSELAGE SKIN AT BROKEN NUTPLATE AREA IAW MHIRJ REO 601R-53-51-589 REV. --, DATED 06/15/2021. FORM 337 AND MAJOR REPAIR TSDR R61A2021051200401Strap · corrodedCFI CORROSION FOUND ON FWD WING TO FUSELAGE FAIRING FWD LANDING BTWN STR 17L-17R. REPLACED FWD LANDING IAW SRM 51-41-02 & 51-42-02.SDR 2021F00078Tail Cone · gougedFORWARD (LEFT) TAILCONE SKIN DAMAGE (GOUGE/BAR MARK). REF ENGINEERING MEMO DQ29509M1SDR SWAA2021042164859Radome · damagedNOSE RADOME REQUIRES REPLACEMENT TO COMPLY WITH REPAIR 53EA07177. REMOVED AND REPLACED NOSE RADOME PER AMM 535200.POS: ONLY GRB: 856196 PN OFF ON: 284A18014 SN OFF: 0098 SN ON: 290.SDR SWAA2021041964510Boot · deterioratedRADOME EROSION BOOT DETERIORATED. (NO DAMAGE TO RADOME) / DMA 0296132 CL # 77013 REMOVED AND REPLACED NOSE RADOME PER AMM 53-52-00 RAR # 95764 P/N ON/OFF: 1001002-7B S/N OFF: C177999 S/N: C163769-08SDR DALA2021041302152Handle · malfunctionedSHIP 9524 - THE CREW RETURNED THE AIRCRAFT BACK TO ATL FOLLOWING THE "TAILCONE UNLOCK" INDICATION ILLUMINATING. CORRECTIVE ACTION: MAINTENANCE FOUND THE AFT INSIDE RELEASE HANDLE LOWER BALL OUT OF THE SWITCH. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PSDR SWAA2021050663379Fairing · delaminatedWING TO BODY FAIRING 194HR HAS AN AREA OF DELAMINATION 8 INCHES FROM INBOARD END / REPAIRED WING TO BODY FAIRING 194HR AREA OF DELAMINATION IAW B737 SRM 53-60-70-2R-1 AND B737 SRM 51-70-04-2R-2SDR SWAA2021050762248Support Bracket · chafedWING-TO-BODY SUPPORT BRACKET CHAFED ABOVE #5 FLAP TRACK FLAPPER DOOR AFT END ( MAKRED ) . / REPLACED SUPPORT BRACKET PER SRM 51-40-02SEE S-AM 326: A1184648SDR SWAA2021050762247Support Bracket · chafedWING-TO-BODY SUPPORT BRACKET CHAFGED ABOVE #4 FLAP TRACK FLAPPER DOOR AFT END ( MARKED) . / REPLACED SUPPORT BRACKET PER SRM 51-40-02.SEE SA-M 326: A1184647SDR IPXA2021033167573Skin · delaminatedINSPECTION TYPE: SEG DELAMINATION ON THE UPPER SKIN SECTION 48. REPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R FIG 201.SDR DALA2021070203656Fairing · crackedSHIP 3302 CRACK WEB BELLY FAIRING AT FR53.2 RIGHT SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REAPIR ON WEB BELLY FAIRING AT FR53.2 RIGHT SIDE AT LOWER FUSELAGE AS PER ERA 590276-14 PRI REV 0 AND ERA 590276-14 REV ORIGINAL. (1768702)SDR DALA2021070203654Fairing · crackedSHIP 3302 CRACK WEB BELLY FAIRING AT FR53.2 LEFT SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REAPIR LOCATED ON WEB BELLY FAIRING AREA AT FRAME 53.2 LEFT SIDE AT LOWER FUSELAGE AS PER ERA 590277-14. (1768696)SDR DALA2021040501972Angle · corrodedSHIP 3302 CORROSION WEB BELLY FAIRING ANGLE FR 53.4 LEFT SIDE LOWER POSITION AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION SECCION 1 LOC. BELLY FAIRING FRAMEWORK AT FR53.4LH SIDE AS PER ER/A 590760-14. (1767355)SDR SWAA2021050359194Support Fitting · crackedLT WING; WIN TO BODY FAIRING SUPPORT FITTING CRACKED BS 500D BETWEEN STG-18L AND STG-19L.MKD 126-010. / REMOVED AND REPLACED FAIRING SUPPORT FITTING (FRAME) AT L/W TO BODY FAIRING BS 500D BETWEEN STG 18L AND STG 19L AS PER B737-7 SRM 51-40-02-0G-0 AND DRAWING SDR SWAA2021042258211Fairing · erodedFAIRING 643AB HAS EROSION DAMAGE ON OUTER SKIN FAIRING 643AB WITH EROSION DAMAGE ON OUTER SKIN WAS REPALCED WITH A SERVICEABLE FAIRING. (POS: #7; TAG NO.: 782236; PN OFF: 113A92102; SN OFF: WN551; PN ON: 113A92102; SN ON: 7827 #1)SDR SWIA202158589Angle · corrodedCORROSION ON ANGLE ON WING TO BODY FAIRING 195DL(MARKED) (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS REF CRJ-900 SRM 53-00-00-101-A01. REPLACED STRAP PN: CC690-39171-7SDR YENA2021032500187Angle · damagedDURING HEAVY MAINTENANCE, R/H TI ANGLE AT FR 40-41 HAS LWR AFT HOLE OUT OF ROUND; (REF FAS SO# N563JB-01-01 NR# 00283 FAS EO# 21018 & JB E# A321-226) ACCOMPLISHED REPAIR OF ELONGATED HOLE AT THE WING FUSELAGE FAIRING R/H SUPPORT STRUCTURE SHEAR WEB BETWEEN FR SDR SWAA2021050357868Web · crackedCRACK WING TO BODY FAIRING WEB LOCATED ON RAM AIR INLET LH SIDE AT LOWER FUSELAGE / REPLACED WEB LOC ON WING TO BODY FAIRING ON RAM IAR INLET LH SIDE AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG #213A7131 SHEET 1 REV.- MATERIAL USED ALUMINUM SHEET PN 70SDR SWAA2021050357864Bracket · crackedCRACK WING TO BODY FAIRING BRACKET LOCATED AFT OF BS 540 ON AIR CONDITIONING COMPARTMENT LH SIDE AT LOWER FUSELAGE / REPLACED BRACKET LOCATED AFT BS540 ON AIR CONDITIONING COMPARTMENT LH SIDE AT LOWER FUSELAGE DUE TO CRACK NOT FOUND ALLOWABLE DAMAGE PART NUMBESDR SWAA2021050357686Bracket · crackedCRACK WING TO BODY FAIRING BRACKET LOCATED AFT OF BS 540 ON AIR CONDITIONING COMPARTMENT RH SIDE AT LOWER FUSELAGE / REPLACED WING TO BODY FAIRING BRACKET LOC AFT OF BS 540 ON AIR CONDITIONING COMPARTMENT RH SIDE AT LOWER FUSELAGE PART USED 212A1116-1 PO 2019-SDR IPXA2021032067038Tee Fitting · corrodedINSPECTION TYPE:SEG4RH WTB FAIRING STRUCTURE TEE CHORD AT STA 1180-1186 RBL 30.75REMOVED AND REPLACED TEE CHORD IAW SRM 51-40-02-OG
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