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 A6WA202208158276Seat Track · corrodedLH SIDE SEAT RAIL FS559+80 TO FS544 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW FLOOR SEAT TRACK REF REO 601R-53-00-055 REV (C) 2017-03-21SDR A6WA202208158275Seat Track · corrodedRH SIDE SEAT RAIL FS559+80 TO FS544 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE *** INSTALLED NEW RH SIDE SEAT RAIL FS559+80 TO FS544 REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B" STEP 3. TORQUE WRENCH TUC 4980, DUE DATE 28/02/202SDR CALA2022081602106Door Sill · corrodedMAIN CABIN R2 DOOR SILL AT FR68 LOWER CORNER AND UNDER GIRT BAR FITTING HAS CORROSION A3NB-05-3-6059 PER NR9296497/42497 GEM BY V935513SDR VNAA202210119993None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17LHSDR VNAA202210119992None · gougedSCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17RHSDR VNAA202208149992Skin · dentedDENT ON EXTERNAL FUSELAJE SKIN BTW FS STA 394 AND FS STA 409 BTW STGR 20RH AND STGR 19RHSDR A6WA202208148274None · corrodedRBL 9 FLOOR BEAM (FS559+16 FS559+80) HAS CORROSION IN SEVERAL AREAS ****AIRCRAFT REMOVED FROM SERVICE *** INSTALLED NEW RBL 9 FLOOR BEAM BETWEEN FS559+16 - FS559+80 REF. CRJ200 SRM 51-42-36 & REO 601R-53-51-623 REV -- DATED 2022-08-11.SDR A6WA202208138273Seat Track · corrodedFLOOR TRACK AT FS559+80 ON RBL27 HAS CORROSION ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND INSTALLED NEW SEAT TRACK SECTION REF CRJ200 AMM 53-01-11-400-802 AND DWG 601R38312 REV-HSDR CALA2022081602097Structure · crackedEA 5380-01113 REV B OP 018 - RH BS 2370 PIVOT BULKHEAD FORWARD CHORD CRACK FOUND AS MARKED. PLEASE GENERATE EA 5380-01113 REV B OP 26. TRANSFER REF NR HX WO.999862 AND ORIGINATED BY EMP V914732. RH BS 2370 PIVOT BULKHEAD FORWARD CHORD REPLACEMENT AS PER EA 538SDR IXXA2022081301Skin · crackedFUSELAGE SKIN CRACKEDSDR NACA2022081200001None · noneSUPPLEMENTAL INFORMATION: REMOVED DAMAGE, PERFORMED NDT. FABBED AND INSTALLED REPAIR REF ASAP EO 53-22-037 AND B737-300 SRM AS REF IN EO. EO AND 8110-3 ON FILE.SDR UIEA2022073000794Radome · delaminatedRADOME OUTER SKIN, HONEYCOMB AREA WITH IMPACT(<P>RADOME WAS REPLACED (NEW RADOME P/N 284T0052-39 S/N 000673) IAW AMM 53-12-01-A02-054</P>)SDR CALA2022081202058Doubler · noneNO DOCUMENTS FOUND DURING THE AAI RECORD REVIEW AND INSPECTION FOR THE FUSELAGE EXTERNAL REPAIR DOUBLER AT APROX STATION 1060, S TR 15R-18R, CUSTOMER REQUEST (UAL QC) (REF AAR NR 99940419) COMPLIED WITH EA NO. 22195, REV P2 AND EC/RA 5331-C2929 (WORK AC COMPLISDR SWIA202266578None · corrodedPAX DOOR SILL LOWER FLOOR SUPPORT ATTACH ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) PAX DOOR SILL LOWER ATTACH ANGLE FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 DUE TO THE AMOUNT OF CORROSION ANGLE REQUIRES REPLACEMENT. REMOVED PAX DOOR UPPER SILSDR SWIA202266570None · crackedFS280 FLOOR BEAM ANGLE AT RBL9 IS CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS 280, RBL 9, OUTBOARD CLIP IAW CRJ 200 SRM 51-42-21SDR DALA2022081605570None · noneAUTOLAND FAILED TO FLARE LANDING TO HARD LANDING. 2144,MSP MTC. LOAD 15 REPORTS VRTA OF 0305 PER A321 AMM 05-51-11 SEVERE HARD LANDING INSPECTION REQUIRED. WIP 960782. TALKED TO MC, A/C LANDED ON ALL THREE GEARS. THE TOUCHDOWN WAS STRAIGHT, FUEL LOAD LEFT WINGSDR VNAA2022080999926Skin · corrodedAFTER AUTOMATIOC DIRECTION FINDER ANTENNA REMOVAL, CORROSION AND WEAR WAS FOUND ON THE FUSELAGE SKIN (SETTLEMENT AREA OF ADF ANTENNA) FUSELAGE SKIN (SETTLEMENT AREA OF ADF ANTENNA) WAS REPAIRS PER EA 22-C9-53-0880 REV IRSDR VNAA2022080999916Skin · dentedDENT AT UPPER FUSELAGE SKIN BETWEEN FS1162 AND FS1181 AND BETWEEN STRG 8L AND STGR 9L
DENT AT UPPER FUSELAGE SKIN BETWEEN FS1162 AND FS1181 AND BETWEEN STRG 8L AND STGR 9L WAS REPAIRED PER EA 22-C9-53-0829 REV.IR SECTION III-PERMANENT REPAIR.SDR VNAA2022080999915Skin · crackedEXISTING BLEND REPAIR AND ELONGATE HOLE ON THE FUSELAGE SKIN AT FS969 BETWEEN STR6R - STR7R
ACTION
EXISTING BLEND REPAIR AND ELONGATE HOLE ON THE FUSELAGE SKIN AT FS969 BETWEEN STR6R - STR7R WAS REPAIR PER EA22-C9-53-0828 REV IR SECTION III- PERMANENT RSDR GTIA2022081136577None · none"FUME EVENT MID CABIN APPLIED COM PROCEDURE PER ELIMIATION OF ODOR /FUMES PACK 2 OFF SMELL DISSIPATED-PERFORMED TSM 05-50-00 FOR CAUSE OF ODOR , FOLLOWED DECISION TABLE AFTER INSPECTION AND FOUND RIGHT AS SOURCE OF ODOR SEE ITEM
2 FOR MEL
"SDR CALA2022080801993None · faulty#1 ENG HAS REPEAT FAULTS FOR HIGH OIL TEMP ADVISORY IN CLIMB. REMOVED AND REPLACED ADAPTER TUBE TO BOSS AND WASHER. PERFORMED HIGH POWER ENGINE RUN AND FOUND TO BE OPERATING NORMALLY.SDR 2022F00322Skin · crackedFUSELAGE AREA UPPER SIDE LH NEAR THE VHF2 ANTENNA WITH CRACK. CORRECTIVE ACTION: HAS BEEN REPAIRED ON S4L BETWEEN BS787 AND BS807.SDR SWIA202266521None · dentedEXTERNAL FUSELAGE SKIN HAS 2EA DENTS ON THE UPPER SKIN PANEL BETWEEN FS 654.50 - FS 672.20, STR 4L - STR 6L. (C-CHECK RO 9/28/2022) FOUND THE 2EA DENTS ON THE UPPER SKIN PANEL BETWEEN FS 654.50 - FS 672.20, STR 4L - STR 6L TO BE OUT OF LIMITS PER CRJ-20SDR SWIA202266338None · corrodedAFT WING TO FUSELAGE FAIRING LOWER ATTACH FLANGE SPLICE IS CORRODED. (C-CHECK RO 8/18/2022) / REMOVED AND REPLACEDAFT WING TO FUSELAGE FAIRING LOWER ATTACH FLANGE SPLICE IS CORRODED. REF EMB 170/175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAFSDR SWIA202266337None · corrodedAFT WING TO FUSELAGE FAIRING L/H LOWER ATTACH FLANGE IS CORRODED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING L/H LOWER ATTACH FLANGE REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS DOSDR SWIA202266336None · corrodedAFT WING TO FUSELAGE FAIRING R/H LOWER ATTACH FLANGEIS CORRODED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING R/H LOWER ATTACH FLANGE REF EMB 170/175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALLANCE.SDR WX0A2022080874194None · noneREF LP 1471030 MAINT REINSPECT REQUIRED FOR OUT STATION MAINTENANCE L1 DOOR LOWER EMERGENCY EXIT LLIGHT LENS BROKE OFF / PERFORMED MAINT REINSPECT OF OUTSTATION MAINTENANCE ON L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM SDR JJBA20210919018None · noneFUSELAGE AFT LWR SKIN UNDER RAD ALT #2 ANTENNA HAS CORROSION. REPAIRED REAR FUSEALGE I AFT LWR SKIN UNDER RAD ALT #2 ANTENNA.SDR 2A6R2022080564503None · noneDURING A SCHEDULED INSPECTION OF FRAME 5 REQUIRED BY ASB21-01, DAMAGE WAS DISCOVERED AT FS 4,709 MM THE DAMAGE IS ADJACENT TO THE MEDICAL WALL ATTACH FITTINGS.SDR CALA2022080801986Skin · dented2EA DENTS AT FUSELAGE L/H SIDE STA 375 STR 17L OUT OF LIMITS REF AAR N/R 9606052 ENGINEERING FOR INSPECTION REQUIREMENTS TO EXTERNAL DOUBLER/ IR TO THE FUSELAGE SKIN AT STA 374 BETWEEN STR 17L AND 18L ON AI 02928. TRIPLER AFTER THE ACCUMULATION OF 48,000 F/C TSDR CALA2022080801983Beam · corrodedCORROSION FLOOR BEAM +Y765 LOCATED FR66 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +765 LOCATED BTW INSPECTION ON AREA AND NOT FOUND ADDITIONAL W=0.115IN. TOOL USED: CALIPER PN:700-113-10, FR64 TO FR66 AT AFT GALLEY AREA IN PSSENGER CABIN DAMAGE IAW NSDR CALA2022080801982Fitting · corrodedCORROSION CENTER FITTING PASSENGER CREW DOOR AT AFT GALLEY AREA LH SIDE. SEE AEROMAN NON ROUTINE 2022-360080. REMOVED AND REPLACED CENTER FITTING PASSENGER AREA IAW NTM 51-90-00. PERFORMED SCEPTRE ENTRY ON LOGPAGE SEP-29-2022 CREW DOOR AT AFT GALLEY AREA LH SISDR CALA2022080801981Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CASDR CALA2022080801980Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IASDR CALA2022080801979None · corrodedCORROSION FLOOR STRUCTURE LOCATED FR68 Y160.5 IN IN PASSENGER CABIN REPLACED FLOOR STRUCTURE LOCATED FR68 Y160.5 NTM 51-90-00. PERFORMED SCEPTRE ENTRY IN PASSENGER CABIN IAW A320 51-72-11 AND ON LOGPAGE NUMBER IS:9153134. MEASURE OF CORROSION DRAWING #D534720SDR SWIA202266219None · crackedLH INTERCOSTAL PN CC670-33194-7 FOUND CRACKED UPON INSTALLATION OF THE HYDRAULIC COMPARTMENT SKIN. (FILED CLOSED) REMOVED DAMAGED INTERCOSTAL PN CC670-33194-7. FABRICATED NEW INTERCOSTAL SAME AS ORIGINAL REF CRJ 700 SRM 51-24-21-001-001-A01 AND DWG CC670-3SDR JJBA20220919019None · noneAFT FUSELAGE SKIN HAS CORROSION WHERE RADIO ALTIMETER RECEIVER ANTENNA #2 IS LOCATED. REPAIRED SKIN AT RAR #2 ANTENNA LOCATIONSDR GTIA2022080436572None · none"DESCENDING THROUGH 4,000 FT LOW POWER SETTING CABIN ODOR. MILDEW / MUSTY ISOLATED TO PACK #1-REF TSM 05-50-00-810-831-A PERFORMED GVI OF APU IAW AMM 49-00-00 NO LEAKS OR DEFECTS NOTED. PERFORMED GVI OF ENG #1 AND ENG #2 FOUND NO VISIBLE SIGNS OF LEAKS OR ANY SDR GTIA2022080436568None · corrodedDURING CHECK FOUND CORROSION AT STRAP BUTT CROSS AT FRAME 47-51 STR 41-42 LH RAF 2935796-01 OPEN SDR ITEM -VERIFIED NR # 5001171997-0050 AND TC # 1003784507-0010. REPAIR WAS PERFORMED AS PER SPIRIT EO 5341-2244 REV.00.SDR GTIA2022080436565None · damagedTHRESHOLD PANEL 261LG FOUND DAMAGE RAF 2935795-02 OPENED.-VERIFIED NR # 5001171840-0030 AND TC # 1003784506-0010. REPAIR WAS PERFORMED AS PER SPIRIT EO 5342-2243 REV.00.SDR FXGA20220802221None · noneFUSELAGE STRINGER REPAIR AT F/STA -38, STRINGER 14R. TO REPAIR A CRACKED STRINGER BEHIND #4 FIRE BOTTLE, STRINGER 14R, F/STA -38. PERFORM STRINGER REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.SDR YENA2022082400815None · failedFLT# 1373, EWR-LAX. 'CREW REPORTS SPARK AT SIDEWALL FLOOR AREA AT SEAT 1A ( LIVE TV4 (COMPONENTS)); TERMINATED DISCONNECT IAW A321 AMM EA# 3433, MINT SEAT OPS CHECK GOOD. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. REMOVED AND REPLACED ZONE 7 CIRCUIT BREAKER SDR JJBA20220824026None · noneSUSPECTED CRACK FOUND ON L/H OMEGA BEAM #1 AT FR 23 ON FLOOR STRUCTURE AREA BEAM REPAIRED WITH A DOUBLERSDR YENA2022080500749None · noneFLT#1470, CHS-LGA. 'DIRTY SOCK SMELL BELOW 10000 FT. ISOLATED BY TURNING PACK #1 OFF AS SMELL WAS MOSTLY CONTAINED IN COCKPIT & FWD CABIN SMELL IMPROVED BUT STILL PRESENT; C/W INFO NOTICE 2017-T15 SECTION (A) ISOLATED FAULT TO TYPE 10, 1C TSM 05-50-00-810-831-SDR JR2R8573138Doubler · corrodedFWD LH FLOOR DOUBLER CORRODEDSDR 2022FA0000521Compressor Blade · failedAIRCRAFT DEPARTED KHLN JULY 31 2022 AROUND 9:55 AM MDT CLIMBING THROUGH 25,000FT PILOT REPORTED LOUD BANG FROM #2 ENGINE AND THEN THE ENGINE ROLLED BACK AND SHUTDOWN. THEY THEN TURNED BACK AROUND AND LANDED AT KHLN.SDR IXXA2022083102None · corrodedLEFT WHEEL WELL UPPER SURFACE OFF REAR SPAR FITTING WHERE THE DOG BONE FITTING ATTACHES TO REAR SPAR FITTING CORROSION UNDER HARDWARE BOLT.SDR A6WA202207308302None · gougedR/H EXTERNAL SKIN HAS 5 EACH GOUGES BENEATH APU EXHAUST SHIELD AT FS 640+12 TO FS 672+6 & S15R. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 53-00-31 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED DAMAGE SDR ABXA2023050878Unknown · corrodedDURING AIRCRAFT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL UPPER OUTER CHORD(143T8204-1). THE 2 AREAS OF CORROSION ARE LOCATED AT STA 566 AND STA 610. AREA 1 AT STA 566- ORIGINAL MATERIAL .200 INCH, MATERIAL LOSS OF .0SDR A6WA202207298240Floor Skin · corrodedFLOOR BEAM LBL9 HAS CORROSION ALONG EDGES IN SEVERAL AREAS FROM FS559+16 TO FS559+80 ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW LBL 9 FLOOR BEAM CAP BETWEEN FS 559.00+10 AND FS 569 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-- 22, REO 601R-5
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