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 CALA2021071601108Stiffener · crackedLH WINDSHIELD FRAME UPPER JUNCTION FASTENER HOLE IS CRACKED IN T HE FRAME LAYER AT 11:00 CONTACT ENGINEERING FOR REPAIR INSTRUCTI ONS PER NR 9290550 / 30550 AD 2020-19-03 GEN BY V061633 ACP REPAIR AT LH LATERAL WINDSHIELD FR4 UPPER STIFFENER FASTENER HOLE PER SDR SWIA202161213None · incorrectFLOOR SEAT TRACK IS LACKING 1 EA SET OF TABS AT L/H FS974 REQUIRED TO SECURE AFT INBOARD FLOOR FITTING LUG ON PAX SEAT 17AB €“ FOR SEAT PITCH REF SKYWEST EA 7RJ3178-25 FIG 15. FABRICATE REPLACEMENT FLOOR SEAT TRACK AS REQUIRED. (C-CHECK RO 9-21-21) REMOVSDR SWIA202161344None · corroded*EVALUATE CORROSION ON WING-TO-BODY PANEL SUPPORT STRUCTURE AT FS 939, 6 O'CLOCK POSITION (MARKED) (C-CHECK RO 9/27/2021) REMOVED AND REPLACED SUPPORT STRUCTURE ANGLE PN SH670-39189-1 PO # T-61766/8 PER CRJ 700 SRM 51-42-06-001-001-A01SDR V0XD20210915001Arm · crackedCRACKED ON LEFT HAND IDLE ARM ASSEMBLY. CORRECTIVE ACTION; REMOVED AND REPLACED LEFT HAND IDLE ARM ASSEMBLY (PN: BA670-92318-3) IAW CRJ900 SRM 51-41-02.SDR SWIA202161804None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA66905-690-53-11-1303 554CA MXCODEID54940-PR - DAMAGE FOUND ON FUSELAGE SKIN LOCATED BETWEEN FS193.00- FS202.75 AND STR 14R-STR16R (RVSM ZONE). COMPLIED WITH TEMPORARY REPAIR PER REO 690-53-11-1303 REV-- DATED 2021-02-SDR JJBA20210712020Doubler · unknownINSPECT THE FWD PRESSURE BULKHEAD TO LOCATE 9 CIRCULAR DOUBLER AND REMOVE DOUBLER. ACCOMPLISH A PERMANENT REPAIR. REMOVED CIRCULAR DOUBLER. DRILLED FASTENER HOLE TO OVERSIZED. TREATED AND PRIMED. RESTOWED TO ORIGINAL FINISH. REINSTALLED REMOVED DOUBLER AS PERMSDR ASMF202110004None · noneDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL LIGHTNING STRIKES ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEMSDR SWIA202161241None · crackedFWD EQUIPMENT COMP - HYD HAND PUMP DOUBLER HAS SUSPECTED CRACK IN RADIUS (C-CHECK RO 9/27/2021) REMOVED AND REPLACED THE FORWARD EQUIMENT COMPARTMENT HAND PUMP DOUBLER REF REO 670-53-11-509 REV E DATED 2018-02-08 AND CRJ 700 SRM 51-42-06-001-001-A01. CSDR QMLA2021071420036Unknown · noiseLOUD ABNORMAL POPPING NOISE DURING TAKEOFF. INTERROGATED ECU FOR FAULTS NONE FOUND, INSPECTED ALL ROTATING COMPONENTS NO DEFECT FOUND, INSPECTED FLIGHT CONTROLS UNDER PILOT AND COPILOTS SEAT AND BROOM CLOSET, NO DEFECTS FOUNDINSPECTED ENGINE AND COMPRESSOR NSDR SWIA202161755None · damagedFUSELAGE EXTERNAL SKIN, FS 501, BETWEEN STR 20R & STR21R COUNTERSINK UNEVEN, RIVET HEAD NOT FLUSH WITH SURFACE AFT OF HOLE. (C-CHECK RO 10/9/2021) REPAIR OF FASTENER HOLE ON EXTERNAL FUSELAGE SKIN AT FS 501.00 BETWEEN STGR 20R AND STGR 21R PER STRUCTURASDR JJBA20210708017Gusset · corrodedFF2 LH INBD FLOOR GUSSET FOUND CORRODED FR 8-13. DOUBLER CUT. FF2 LH INBD FLOOR GUSSET BTW FR 8-13 REPLACED WITH REPAIR DOUBLER.SDR JJBA20210708011Beam · corrodedCF1 ON LH FUSE OMEGA BEAM LH AND REPAIR ANGLE CORRODED. OMEGA BEAM REPLACED AND INSTALLEDSDR R61A2021071800576Angle · crackedFWD FUSELAGE CRACK FOUND ON ANGLE SUPPORT AT FR 12 BL 0. REPLACED ANGLE SUPPORT @ FR 12 BL 0 IAW SRM 51-41-01SDR DALA2021070603706Fitting · crackedDURING INSPECTION MAINTENANCE FOUND 1EA CRACK ON RH LOWER UNDER -WING LONGERON FITTING. LONGERON FITTING REPLACED. (LP 1864036)SDR SWIA202161496None · corrodedPAX DOOR FRAME FS 313.5 BETWEEN DD4 AND DD5 INTERCOSTAL FOUND TO HAVE CORROSION (C-CHECK RO 9/27/2021) REPLACED PAX DOOR FRAME FS 313.5 BETWEEN DD4 AND DD5 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED SDR R61A2021071800570Hinge · corrodedWHILE AC WAS IN FOR HVY CK FOUND CF3 LAV WASTE ACCESS DOOR HINGE PN 170-85090-003 HAS CORROSION. REPLACED DOOR HINGE IAW SRM 51-41-02 SEE AAR NRC# 4500928-1000-0042 FOR DETAILS OF WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR 2022FA0000633Actuator · brokenAFTER TAKEOFF, GEAR WAS SELECTD UP AND THE GEAR UNLOCK LIGHT ILLYMINATED. CYCLED THE GEAR ONCE WITH THE SAME EFFECT. AT LANDING, GEAR WAS SELECTED DOWN WITH 3 GREEN. MAINTENANCE FOUND MAIN GEAR ACTUATOR BROKE FROM WING ATTACH POINT. COMPONENT HAD 6016 LANDINGSSDR JJBA20210629008Doubler · corrodedCF 1 ON RH FUSE BTW FR 19-20 SILL ASSEMBLY FWD AND DOUBLER SILL AFT CORRODED. CF1 ON RH FUSE BTW FR 19-20 SILL ASSY FWD CORROSION REMOVED WITHIN LIMITS AND REPROTECTED. LESS THAN .001" REMOVED. DVI INSP C/OUT WITH MAGN GLASS 30X NO FAULT FOUND. CF1 RH SILL AFTSDR JJBA20210629007Flange · corrodedFRAME 65 LOWER FLANGE AT STR 16L CORRODED. FRAME 65 LOWER FLANGE AT STR 16L BLENDED OUT OF LIMIT. CUT OUT ON FR65 LOWER FLANGE AT STR 16L REPAIRED.SDR JJBA20210629006Door Frame · corrodedCORROSION FOUND ON CARGO DOOR FRAME 65 BTW STR 16 & 17. CARGO DOOR FR65 BTW STR 16L AND 17L CORROSION REMOVED OUT OF LIMITS. FR65 CUT AND SPLICE MFG BTW STR 14L-15L. CARGO DOOR FRAME 65 LH BTW STR 14-15 REPAIRED.SDR YENA2021070200422Unknown · vibrationFLT 773, BOS-JFK. A/C TAIL VIBRATION PASSING ON CLIMB @ 300 KNOTS FL29000 STRONG VIBRATION FROM REAR OF A/C HAPPENED TWICE VERY STRONG FA'S REPORTED LOWER LEVEL AFTER 1ST 2 (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR 2022FA0000635Fuel · nonePISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANKSDR 2022FA0000634Fuel · nonePISTONS STICK CAUSING FUEL TO BURN OUT OF ONLY ONE TANKSDR R61A2021071000560Support Bracket · corrodedFLOOR STRUCTURE CENTER FUS III, FLOOR SUPPORT BRACKET CRACKED AT FR 86, RBL 30. FLOOR SUPPORT BRACKET AT FR 86 RBL 30 HAS BEEN WITH REPLACED WITH NEW AND INSTALLED IAW EMBRAER SRM 51-41-01SDR JJBA20210626010Support Bracket · crackedFRM SUPPORT BRACKET CRACKED IN AFT CARGO COMP AT AFT BLK HEAD UPPER SURFACE BETWEEN O1L AND O1R, X=24389.5. REMOVED SHEAR CLIP IN AFT CARGO COMP AFT BLK HEAD, FAB SUPPORT BRACKET, SHEAR CLIP. INSTALLED SHEAR CLIP ON AFT CARGO AT BLK HEAD UPPER SURFACE BETWEEN SDR SWIA202161752None · corrodedFS280 SKIN JOINT SPLICE CORRODED BETWEEN STR 20R & 22R. (C-CHECK RO 10/9/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER#670-53-21-2092 FASTENERS REMOVED 3 AREAS BLENDED AT FS280.00 SKIN JOINT SPLICE BETWEEN STR20R AND STR22R ALL FASTENERS REINSTALLESDR CALA2021061400863Beam · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y1732 HAS CORROSION AT FR68. (DOT 38-42) ()SDR P5CA2021052400193None · noneNLG L/R FWD CORNER DOUBLER MOD FOUND L/R TOTAL 8EA FASTENER AND 8 WASHER INTERTERING INSTALLATION. NLG L/R FWD CORNER DOUBLER AND 8EA RIVETS AND 8EA WASHER INSTALLED AS PER RI 53-10-14631 REV A.SDR CALA2021060700801Intercostal · damagedPLS PROVIDE REPAIR RECORD REFER HAECO NON-ROUTINE LP 9439170. EA5311-02164 REV ORIG OP002 STEP 2.1 C AND STEP 2.2 C). RH FR16 NO.7 INTERCOSTAL FTG REPLACED REF DWG 53114236 REV S,SRM 51-42-11 REV 135,OTHERS FOLLOW UP PER EA5311-02164 REV ORIG OP002 STEP 2.1 SDR ASAA2021060535068Track · crackedAFT PIT R/H TRACK IS CRACKED IN RADIUS OF FRAME ATTACH POINT STA 727I. GROUNDED - YES. CUT OUT AND REPAIRED DAMAGED SECTION OF TRACK IAW B737-900ER SRM 53-00-53-2R-3.SDR CALA2021060700794Skin · scratchedMOVE CREW FOUND SCRATCHES ON LEFT SIDE FORWARD OF DOOR 2L JUST AFT OF WING SCAN LIGHT LENS. AS REQUESTED BY ENGNR AND SM, PERFORMED NDT ULTRASONIC PER NTM PT 4-00-04-02, OLYMPUS 35 THICKNESS MEASUREMENT. PICTURES OF RESULTS ATTACHED BLENDED THE SKIN GOUGES INSDR SWIA202161750None · dentedDENT LOWER OUTER BOTTOM REAR FUSELAGE SKIN RBL 8, F.S. 1053 (C-CHECK RO 10/9/2021) REPAIRED DENT OF LOWER OUTER FUSELAGE SKIN AT RIGHT BUTT LINE 8 AT FUSELAGE STATION 1035. PER MHIRJ REO 670-53-61-1923 REV. -- DATED: 18 AUG 2021. ANALYSIS TO BE COMPLETESDR DALA2023070605477Unknown · unknownSHIP 676 DTA MONITOR INSPECTION LOG REF ERA 591619-14AD. CORRECTIVE ACTION: REF ERA 591619-14AD. (1822721)SDR DALA2023042603255Unknown · unknownSHIP 685 DTE - ER/A 384434-14 REV B, FUSELAGE SKIN AND TEAR STRAP REPAIR WAS NOTED AT STA 1320, S1-2L DURING INSPECTIONS PER EM 5331-0123 8. ER/A 384434-14 REV B SECTION II REPAIR WAS PERFORMED. CORRECTIVE ACITON: REF ERA 384434-14. (1822696)SDR ASAA2021052134867Satcom · malfunctionedSATCOM 2 WHEN YOU DIAL OUT TO MEDLINK DID NOT ALLOW YOU TO HEAR THE RINGING OR WHEN IT ANSWERED YOU COULD NOT HEAR ANYTHING WHEN YOU MAKE THE CALL ON SATCOM ONE YOU CAN TRANSMIT THE CALL BUT TO HEAR THE AUDIO YOU HAVE TO BE ON SATCOM 2/AUDIO SELECTED TO HEAR TSDR 2022FA0000019None · corrodedSKIN CORROSION FOUND UNDER ANTENNAS ON AIRCRAFT BELLYSDR SWAA2021062873215Panel · damagedPANEL 621ZB I/B BONDING FASTENER HOLE IS ELONGATED / [01] IDENTIFIED MATERIAL ID PER SRM 57-41-01-0I-4 FIG.2; SHT.1; TABLE 2; ITEM 2; AND FIG.7. FOUND ELONGATED FASTENER HOLE TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-41-01-1A-1 PAR.4A(2) STEP A. A REPAIRSDR CALA2021051000633Wing · dentedBIRDSTRIKE ON T/O CLIMBI NG THRU 2000 FT. 200KTS. LARGE BIRD 5FT SPAN HIT RT SIDE NOSE + WING. ACCOPLISHED BIRD STRIKE INSPECTION IAW SRM 53-00-01. FOUND DENT AT SECTION 41 STATION 219.8 W4" L380" D.085". ALLOWABLE DAMAGE 1 PARAGRAPH 4 SECTION 3 DENTS, DETAIL SDR EE4Y2023031017360Skin · noneDURING THE VISUAL INSPECTION PER ALLEGIANT TASK CARD 51-000-001_P1-VISUAL-INSP, LIGHTNING STRIKE WAS FOUND COMMON TO LOWER FUSELAGE SKIN AT FR32+144MM AND STR 43R. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER A320 SRM TASK 53-00-11-300-042 PARAGRSDR CALA2021051000625Intercostal · crackedR1 DOOR FRAME 16 STOP FITTING #1 LWR INBRD HOLE IS CRACKED IN TH E INTERCOSTAL FITTING REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEER ING FOR APPROVED INSTRUCTIONS PER NR 9292144 / 22144 AD 2019-20- 10 GEN BY V061633. ACCOMPLISHED INTERIM REPAIR AT R 1 DOOR FRAME SDR QMLA2021050620022Structure · crackedCRACK FOUND ON RH HORIZONTAL TRAILING EDGE, REPAIRED CRACK IAW SRM.SDR MASA20210506186Skin · gougedGOUGE ON FUSELAGE BETWEEN FRAMES 20-21 STR 5L-6L. REPAIRED GOUGE REF ETD2021-170-012736 REV ASDR DALA2023052504169Unknown · unknownSHIP 672 ERA 591149-14AD ISSUED FOR REPAIR TO STA 1640 S14R FRAME. CORRECTIVE ACTION: REF ERA 591149-14AD. (1786519)SDR ABXA2021317032Stringer · crackedFUSELAGE STRINGER 23L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S23L @ F.S. 676 IAW B767 SRM 53-00-03 REPAIR 2SDR CALA2021041600483Skin · corrodedVACUUM BLOWER EXHAUST VENT AT ST1968 S-35L-36L FUSELAGE SKIN CORROSION. (AFT VENT). DISCOVERED DURING D-1 CHECK HAECO XMN STA 1968 FUSELAGE SKIN VACUUM BLOWER EXHAUST VENT PORT CORROSION AREA REPAIRED AS PER SRM 53-70-01 REPAIR 1 REV 85 AND ECRA 5331-02712. INSDR JR2R20210408077Beam · corrodedFLOOR CROSS BEAM AT FR84 LBL9 TO LH FLOOR SILL CORRODEDSDR JR2R20210408063Intercostal · corrodedINTERCOSTAL AT RBL 9 FR89 TO FR90 CORRODEDSDR JR2R20210408064Support · corrodedLONGITUDINAL FLOOR BEAM SUPPORT AT RBL 9 CORRODED FROM FR90 - FR91SDR JR2R20210408060Shear Panel · corrodedRH FLOOR SHEAR PANEL AT FR87 CORRODESDR JR2R20210408074Strap · corrodedLONGITUDINAL FLOOR BEAM STRAP AT RBL 9 FROM FR85 - FR86 CORRODED
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