JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 SWIA202164460None · cracked*FORWARD EQUIPMENT COMPARTMENT FLOOR HAS CRACK IN LEFT CORNER AREA @FS200.00 & WL79.50 (C CHECK RO 2/17/2022) REPAIRED FWD EQUIPMENT COMPARTMENT FLOOR FS200.00 WL79.50 REF CRJ700 SRM 53-11-43-201-001-A01. SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITHSDR IXXA2022021403Support Web · corrodedPRESSURE DECK IMMEDIATELY INSIDE OF ALC DOOR STA 1263~1285 IS CORRODED.SDR SWIA202164186None · corrodedFWD INNER CORD ON AFT CARGO DOOR SILL FS 1000 HAS CORROSION. (C CHECK RO 02-03-22) REMOVED AND REPLACED FWD INNER CORD ON AFT CARGO DOOR SILL IAW CRJ700 SRM 51-42-06-001-001-A01SDR SWIA202162959None · damagedREF CP 23937463 FOR ORIGINAL DISCREPANCY AND CP23943655 FOR DAMAGE DETERMINATION. FOUND TWO HOLES TO BE ELONGATED WHILE REMOVING THE PAX DOOR AFT SEAL RETAINER THIS DAMAGE HAS BEEN DETERMINED TO BE MAJOR PER GMM 3-26 REPAIR PER REO 670-52-11-1272. (FILED CLSDR SWIA202164459None · corroded*LEFT MLG AUXILIARY SPAR PANEL 542AZ MATTING SURFACES ARE CORRODED. (C CHECK RO 2/17/2022) REMOVED AND REPLACED THE LH MLG AUXILIARY SPAR ANGLE UNDER PANEL 542AZ REF CRJ700 SRM 51-42-21-001-001-A01, DRAWING CC670-10320 REV -F. COMPLIED WITH ST 51-900-100SDR SWIA202164458None · corroded*RIGHT MLG AUXILIARY SPAR PANEL 642AZ MATTING SURFACES ARE CORRODED. (C CHECK RO 2/17/2022) REMOVED AND REPLACED RH MLG AUXILIARY SPAR ANGLE UNDER PANEL 642AZ REF CRJ700 SRM 51-42-21-001-001-A01, DRAWING CC670-10320 REV -F. LEAK CHECKS GOOD. COMPLIED WISDR SWIA202164272None · corrodedANGLE ATTACHING TO LEFT WING AFT SPAR HAS LIGHT SURFACE CORROSION AT APPROX. WS 176 (C CHECK RO 2-11-2022) FOUND CORROSION ON L/H WING T/E ATTACH ANGLE (P/N 601R10217-1) TO BE WITHIN ALLOWABLE LIMITS OF CRJ-200 SRM 57-51-14 AND 57-00-00. REMOVED MINOR CORRSDR IXXA2022021402Bear Strap · corrodedCORROSION NOTED ON ALC DOOR SURROUND, LWR LIP, UNDER SEAL DEPRESSOR INSIDE, STA 1273~1282.SDR A6WA202101178072Skin · dentedSTRINGER HAS 4 OUTWARD DENTS COMMON TO EXTERIOR SKIN PN 601R35004-145 AT FS625.30 TO FS640.00 AND STR16R TO STR17R. ****AIRCRAFT REMOVED FROM SERVICE**** VERIFIED NO LOOSE OR PULLED FASTENERS IN THE SURROUNDING AREA AT STRINGER COMMON TO EXTERIOR SKIN AT FSSDR SWIA202163106None · dented3 SMALL DENTS NEAR GPU PLUG ACCESS DOOR ON FORWARD #2 SIDE OF AC BETWEEN FS 177.00 €“ FS 193.00 AND STGR 22R €“ STGR 24R EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-31. DENT #1 IS L= 2.5€? X W= 3.5€? X D= .045, DENT #2 IS L=2.0€? X W= 3.0€? X DSDR JJBA20211202014None · noneMAIN CABIN OMEGA BEAM AT FR 57-61 Y+0 HAS CORROSION. REMOVED AND REPLACED MAIN CABIN OMEGA BEAM AT FR 57-61 Y+0. CORROSION LEVEL IISDR CALA2021120602241Skin · noneREF FLEET CYCLE LOG PAGE 9790017. INITIATE A DIP TO STATE "ACCOMPLISH INITIAL INSPECTION OF FUSELAGE REINFORCED AREA AT STA 500F TO STA 500H AND S2R TO S-3L ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES" PER EC/RA 5331-02792 STEP E.1. EC/RA #53SDR CALA2021120602243Shear Tie · corrodedB767-53-3-7010 - BULK CARGO STA1562 FRAME TO SKIN SHEAR TIE BETWEEN S38L-S39L FOUND CORROSION TRANSFER REF NON-ROUTINE LP9132035 AND ORIGINATED BY EMP V896798 BULK CARGO STA1562 S38L-S39L SHEAR TIE REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM SDR SWIA202164825None · chafedCARGO DOOR OUTER SKIN IS CHAFED AT THE FORWARD AND AFT LOWER CORNERS FROM CONTACT WITH THE DOOR SCUFF PLATE. (C CHECK RO 3/11/2022) REPAIRED CARGO DOOR I.A.W. MHIRJ REO 601R-52-31-361 REV.--, DATED 2022-01-04. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NSDR SWIA202163273None · dentedUPON REMOVAL OF STRINGER FOUND DENT PROTRUDING ON FUSELAGE SKIN AT FS319.70 TO FS333.00 STRINGER 25R. (C-CHECK RO 12/26/2021) EVALUATED DENT AT STRINGER 25R BETWEEN FS319.70 TO FS333.00. DENT MEASURES 6.20€? L 0.013€? D AND 0.20€? W. WITH A W/D RASDR R61A2021121601018Tail Cone · crackedTAILCONE CRACKED ON LH SIDE AFT OF FRAME 100. REPAIRED TAILCONE IAW ETD2021-170-040952SDR JJBA20211201004None · noneLH OB FLOOR SILL SHOWS SIGNS OF CORROSION BETWEEN FRAMES 42-49. REMOVED AND REPLACED DAMAGE SILL BETWEEN FRAMES 42-49 LH SIDESDR CALA2021120202239None · gougedUPPER CABIN INNER CHORD FRAME AT STA 1640, BETWEEN S5L - S6L IS GOUGED. MARKED REPAIRED PER ECRA 5362-01034.PER PART 1,2.0, "CREATE A LOG PAGE TO PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF E RA 5362-01034 ON OR BEFORE 22-MAY-2023.SDR JR2R20218327577Beam · corrodedFLOORBEAM AND SEAT TRACK CORRODED AT RBL9 FR84SDR JR2R20218327576Beam · corrodedFLOOR BEAM CORRODED AT RBL9 BETWEEN FR85 AND FR86SDR IXXA2021120104HShear Tie · corrodedCORRODED SHEAR TIE STA.1263SDR CALA2021120102234Skin · dentedDENTS INFUSELAGE SKIN PANEL 143A3131-77 STA 480 AT S5L. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 480 AND S5L REF ECRA 5331-02794 SEE F/C NR 9794173 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORK PERFORMED REF EC/RA SDR CALA2021120102230Skin · dentedDENTS IN FUSELAGE SKIN PANEL 143A3131-77 STA 500A AT S5L.DENTS #9,#10,#11. REPAIRED FUSELAGE SKIN PANEL 143A3131-77 AT STA 500A AND S5L REF ECRA 5331-02794 SEE F/C NR 9794174 FOR WORK ACCOMPLISHED.ISSUED DTA DIP L/P 7539934 FOR PERMANENT REPAIR. VERIFIED WORKSDR CALA2021120102227Structure · dentedUPON INSPECTION OF REPAIR IN NOSE AREA STA.200 R/H SIDE JUST UNDER WINDSHIED. A DENT WAS FOUND ABOUT 3" O/B OF CUTOUT(MARKED). REF. LOGPAGE 7514449 & AVO#7251-21-11-28-01. DENT WIDTH IS 0.70", LENGTH 0.50" ,& (DEPTH Y = 0.005") W/Y= 140 VERIFIED DENT MEASUREMESDR CALA2021120102224None · damagedAC 267 RIGHT WINGLET STRUCK UPPER SECTION OF RADOME, DAMAGE RUNS FROM 1OCLOCK TO 3OCLOCK 6 " FROM FUSELAGE PLUS DAMAGED 5 VORTEX GENERATORS ON CAPT SIDE, FO WINDSHIELD WIPER DAMAGED, R1 WINDOW SEAL SMALL DAMAGE TO RUBBER SEAL LOWER LEFT CORNER AND MIDDLE OF SSDR CALA2021120102223Structure · damagedREFERENCE 7504156 COMPLETED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02...AWAITING AVO/EC/RA FOR FURTHER INSTRUCTIONS. HFEC INSPECTION REQUIRE AROUND THE CUTOUT. HFEC INSPECTION REQUIRE OF ALL REMOVED INITIAL FASTENERS. PERFORMED HFEC OF TRIM OUT REF 73SDR IXXA2021120103HShear Tie · corrodedSHEAR TIE CORRODED AT STA. 1241 IN AFT LOWER CARGOSDR IXXA2021120102HIntercostal · bentINTERCOSTAL IN MCD AT RBL82 IS BENTSDR IXXA2021120101HShear Tie · corrodedFORWARD LOWER CARGO CORROSION FUS.. STA. 566 SHEAR TIE BETWEEN STR. 38L AND 39LSDR 2021F00378Power Supply · dischargedEMERGENCY LIGHT FAILED OPERATIONAL TEST. BATTERY WAS NOT CHARGINGSDR SWIA202164132None · corroded*RH FUSELAGE FLOOR SILL AT APPROX. FS.295-FS.319 HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C CHECK RO 02-03-22) REPLACED RH FLOOR SILL FROM FS295 - FS319. REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01SDR SWIA202163846None · corrodedFOUND EXFOLIATED R/H MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER ANGLE (C CHECK RO 1/16/2022) REMOVED ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01, INSTALLED NEW ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01, 51-23-00-001-001-A01, DWG CC670-10320 REV-F & DWG CC670-SDR SWIA202163845None · corrodedFOUND EXFOLIATED L/H MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER ANGLE (C CHECK RO 1/16/2022) REMOVED ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01, INSTALLED NEW ANGLE P/N CC670-10338-1 IAW CRJ700 SRM 51-42-21-001-001-A01, 51-23-00-001-001-A01, DWG CC670-10320 SDR CALA2021120102215Skin · wornSKIN WRINKLE AND WORN BETWEEN STA.1720 AND STA.1743 AFT OF APB BETWEEN S-27RT AND S-27LT. ( REF. L/P 7137422 ) REF COLLECTOR ECRA 5380-01303 FOR MAJOR REPAIR ACCOMPLISHED BY BOEING CONTRACTORS. NO FURTHER MX REQ''D AT THIS TIME. REF COLLECTOR ECRA 5380-01303 FSDR CALA2021120102214Bulkhead · noneREF ECRA 5380-01304, NEED TO INITIATE A DTA DIP PER PART 1 STEP #2 IN REGARDS TO A REPAIR ON THE APB CENTER WEB & FWD LOWER CHORD. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL CYCLES. ITEM PLACED ON DIP. PER ECRASDR CALA2021120102213Skin · noneREF ECRA 5360-01621, NEED TO INITIATE A DTA DIP PER PART 1 STEP #7 TO ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL CYCLES. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOSDR CALA2021120102209Skin · dentedDENTS IN SKIN PANEL 146A3101-35 NEAR STA 787 AND S2L REQUIRE DOUBLER /TRIPLER INSTALLATION REF ECRA 5331-02800. MAJOR REPAIR UPGRADED TO RII REPAIRED FUSELAGE SKIN PANEL 146A3101-35 NEAR STA 787 AND S2L.REF ECRA 5331-02800.SEE F/C L/P 9794510 FOR WORK ACCOMPLISDR JR2R20218327583Doubler · corrodedLH FLOOR DOUBLER P/N 170-07331-003 CORROED BEYOND LIMITSSDR MASA20211130591None · noneFUSELAGE LOWER SKIN PANEL BETWEEN FS 485 -FS 517, STR 24R -STR 26R WAS FOUND WITH SIX AREAS OF DAMAGE DUE TO LIGHTNING STRIKE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, "SKIN, LOWER PANEL FS477.40 TO FS693.00 -STRUCTURAL IDENTIFICATISDR SWIA202164127None · corroded*ANGLE ON THE AFT SIDE OF FRAME FS333.00 BETWEEN STGR26R & STGR25R IS CORRODED. (MARKED) (C CHECK RO 02-03-22) REPLACED PREVIOUS REPAIR DOUBLER TO FRAME AT FS333 BETWEEN STGR 26R & STGR 25R REF STS EA 20-2015-365 REV - A 7/20/2016. COMPLIED WITH TASK CARD SDR SWIA202164124None · corroded*INTERNAL SKIN JUST AFT OF FRAME FS295.00 BETWEEN STGR 27 & STGR26R HAS ONE SMALL SPOT OF CORROSION. (MARKED) (C CHECK RO 02-03-22) REPAIRED INTERNAL SKIN JUST AFT OF FRAME AT F.S 295 BETWEEN STGR 27 AND STGR 26R REF. REO 670-53-21-2201 REV-- 2021-12-10, CSDR SWIA202164123None · corroded*INTERNAL SKIN BETWEEN FS280.00.00 & FS295.00 BETWEEN STGR 20L & STGR21L HAS ONE SPOT OF CORROSION. (MARKED) (C CHECK RO 02-03-22) REPAIRED INTERNAL SKIN BETWEEN F.S 280 TO F.S 295 BETWEEN STGR 20L AND STGR 21L REF. REO 670-53-21-2201 REV-- 2021-12-10 COMSDR SWIA202163447None · corrodedFORWARD WATER-WASTE DOOR SURROUND STRUCTURE PLATE SH670-32303-3 HAS CORROSION ON SEVERAL AREAS AROUND DRAIN VALVE. (C CHECK RO 12-31-21) BLENDED FORWARD WATER WASTE DOOR SURRROUND STRUCTURE PLATE AROUND DRAIN VALVE IN LIMITS AND RESTORED LEAK CHECK GOOD RSDR JJBA20211129018None · noneLH OMEGA BEAM FOUND CRACKED AT FR 24, AND FR 25 AND BOTTOM FLANG FOUND CORRODED. REPLACED WITH NEW PART LH OMEGA BEAM BTW FR 23-29SDR R61A2021121401013Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON RH SHEAR PANEL BTWN FR 87-88. MX REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-42-02 SEE AAR NRC# 4501021-1000-0095 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR R61A2021121401012Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON CENTER SHEAR PANEL BTWN FR 87-88. MX REPLACED SHEAR PANEL PN 170-65928-001 IAW SRM 51-42-01 SEE AAR NRC# 4501021-1000-0094 FOR WORK PERFORMED.AC REMAINS IN YQG FOR COMPLETION.SDR R61A2021121401011Splice · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON DOUBLER SPLICE ON RH SHEAR PANEL BTWN FR87-88. MX REPLACED SPLICE PN 170-65644-001 IAW SRM 51-42-01 SEE AAR NRC# 4501021-1000-0096 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPSDR R61A2021121401008Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE, CORROSION FOUND ON GUSSET PLATE AT FR 90 AT BL 0. CORRODED GUSSET PLATE AT FR90, BL 0 REPLACED WITH NEW IAW EMB SRM 51-43-03.SDR R61A2021121401007Beam · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII FLOOR STRUCTURE, CORROSION FOUND ON PREVIOUS REPAIR AT LH UPPER BEAM BETWEEN FR87-89. CORRODED PREVIOUS REPAIR AT LH UPPER BEAM BETWEEN FR87-89, REPLACED IAW EMB 170 SRM 53-23-10 AND 51-43-04.SDR 2021FA0000384Printed Ckt Board · backed outON CLIMB OUT FROM RDU A RIGHT GENERATOR FAIL CAS MSG ILLUMINATED. THE ACFT RETURNED TO RDU AND A VISUAL INSPECTION DISCOVERED THE RIGHT GCU PCB 6 IN THE RDCPC HAD MIGRATED OUT FROM THE MOTHER BOARD. RESEATED THE GCU WITH OPERATIONAL CHECKS GOOD. REPLACED DCPC
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