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 JJBA20211101006None · noneCF1, BTW FR 13-14 AND BTW STR 10R-11R, SKIN DAMAGED DURING RIVET REPLACEMENT. BTW FR 13-14 AND BTW STR 10-11 RH REPAIR ON SKIN PERFORMEDSDR MASA20211105533Doubler · corrodedDOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEECT LSDR CALA2021110302020Beam · corrodedB767-53-3-0172 CABIN STA 303 LBL 13 TO 53 FLOOR BEAM FOUND CORROSION TRANSFER REF. NON-ROUTINE LP 9131181 AND ORIGINATED BY EMP NO. V897790 CABIN STA 303 LBL 3" TO LBL 66" FLOOR BEAM REPAIRED AS PER SRM 53-00-51-2R-1 REPAIR 1 FIG 201 ATTACH FORM 44.0008 ITEM 1SDR MASA20211102523Doubler · corrodedDOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEFECT SDR 2A6D2021110109701Frame · gougedDAMAGE WAS NOTED TO THE RH X1790.15 FRAME (PN: 350A21-1368.23) IN THE FORM OF CHAFES NEAR THE TOP FLANGE. THE CHAFES WERE MEASURED TO BE APPROXIMATELY 0.10” X 0.20” AND 0.007” DEEP, AS WELL AS 0.10” X 0.10” AND 0.003” DEEP.SDR IPXA2021110175500Beam · noneINSPECTION TYPE:SEG31 EA FASTENER HOLE AT STA 1681 LBL 39.5, COMMON TO DECK PLATE AND FLOOR BEAM HAS CORROSION.REPAIRED PER UPS EO B757-5310-82015-A AND VT MAE EA 757-5360-27-A2727 REV-.SDR CALA2021110102017Windshear Sys · noneRTO DUE WINDSHEAR AT 96 KTS REVIEWED PARAMETERS IAW 05-51-07-210-801. NO MTC ACTION REQUIREDSDR 2021FA0000335Servo · failedGARMIN GSA28 PITCH TRIM SERVO FAILED AFTER APPROXIMATELY EIGHTEEN MONTHS / 68 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED "SERVO HARDWARE FAULT" AND RED "PTRIM" FLAG DURING FLIGHT, AND ELECTRIC PITCH TRIM BECAME INOPERATIVE. THE SERVO DISPLAYED A "RED" SDR 2022FA0000072Hose · noneTHE PROPELLER IS DE-ICED BY TKS FLUID BY MEANS OF A SLINGER RING, A HOSE AND A SPRAY NOZZLE. THE AIRCRAFT/ENGINE/PROPELLER HAD ONLY 336.6 HOURS TOTAL TIME. ALL 4 HOSES ON THE PROPELLER WERE BADLY CRACKED ALMOST IN TWO PIECES AND NEEDED REPLACEMENT.SDR HNAA2021112900582None · noneCORRECTION TO DUPLICATE UNIQUE CONTROL NUMBER - E887876 - CARGO DOOR CUT-OUT FR 65 SHEAR CLIP CORRODED .... REPAIRED CARGO DOOR CUT OUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04-RE FIGURE 212 AND EO1-53-21-0317SDR HNAA2021112900570None · noneE887314 - LAV BUCKET EXTERNAL SURFACE CORRODED AROUND WASTE DRAIN VALVE MARKED ... REMOVED, PREPPED AND INSTALLED SERVICEABLE LAV ( BUCKET) CUP IAW EMB 145 SRM 51-40-02SDR 2021FA0000338Battery · failedGARMIN G5 FLIGHT INSTRUMENT BACKUP BATTERY FAILED AFTER APPROXIMATELY FOUR MONTHS / 16 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED "1%" BATTERY CHARGE STATUS AFTER NOT HAVING USED THE INSTRUMENT ON BACKUP POWER. BATTERY WOULD NOT CHARGE ABOVE 1%. "BATTESDR QMLA2021111020060Frame · noneFOUND DAMAGE ON RIB STRUCTURE WHERE THE HEAT/ DEMIST LINE IS SECURED TO THE RIB.SDR EVCA102921Angle · crackedDOING A VISUAL INSPECTION FOUND THE RH 145 BULKHEAD UPPER ANGLE CRACKED AROUND FASTENERS.SDR CALA2021110102007Skin · noneLIGHTING STRIKE INSPECTION C/W REF AMM 05-51-19/201 , NOTED LIGHTING STRIKE AT STA 285 , STRINGER 1-2 RH , REF LOG PG. 7310533 . TAPE APPLIED AT LOCATION . OF ALL INITIAL FASTENER HOLES REF 737 NDT PART 6, 51-00-00, OF ALL INITIAL FASTENER HOLES REF 737 NDT PSDR FDEA202110292660None · noneMAIN EQUIPMENT CENTER CEILING, RIGHT SIDE MAIN CABIN FLOOR STRUCTURE STA 410 RBL 25 ANGLE SUPPORT IS CRACKED ACCOMPLISHED FEDEX EA # F-5310-T0364861 FUSELAGE - SEAT TRACK SUPPORT - STA 410, RBL 24.75, CRACK, PERMANENT REPAIRSDR SWIA202165302None · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54980-670-53-51-156 N715SKMXCODEID50027-PR - GOUGE DAMAGE TO LOWER FUSELAGE SKIN BETWEEN FS969.00 AND FS977.00 AT STRG 27 MEASURING 1" LENGTH X 0.7" WIDTH X .020" DEPTH. PERFORMED TEMPORARY REPAIR IAW REO 670-53-51-156SDR R61A2021111900917Beam · corrodedPASSENGER CABIN FLOOR STRUCTURE FR 14 CROSSBEAM HAS 3 AREAS OF CORROSION AT RH OUTBOARD SIDE.REPAIRED PASSENGER CABIN FLOOR STRUCTURE FR 14 CROSSBEAM AS REQUIRED AT RH OUTBOARD SIDE REF SRM 53-00-10/REPAIR 03P REF TO WIP# 1-24 AND TASK # 1-4 FOR WORK ACCOMPLISSDR V6NA2021102901Web · crackedDURING SCHEDULED INSPECTION, DISCOVERED TWO INCH CRACK RUNNING LONGITUDINALLY ON RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL THROUGH EXISTING FASTENER HOLE. CRACK LOCATION WAS OUTSIDE THE PRESSURE VESSEL. DAMAGE AREA WAS REMOVED AND ALUMINUM FLUSH PATCH INSTALLSDR CALA2021102901996Skin · damagedA3NB-51-4-6001 SEQ. 2328 REPAIR FUSELAGE OUTER SKIN AT FR70-71 STRG 30R-32R REQUIRES REPAIR RECORD BEFORE FUTHER FLIGHT. EVALUATE AND TAKE FURTHER ACTION. THICKNESS BTW 1.2 AND 4.00MM. DVI PERFORMED AS PER NTM 51-90-00 BETWEEN 1.2 MM (0.047 IN) AND 4.0 MM (0.1SDR SWIA202164804None · crackedFORWARD FUSELAGE LEFT WINDSHIELD SUPPORT POST BETWEEN PILOT'S SIDE WINDSLIELD AND FORWARD WINDSHIELD IS CRACKED. (C-CHECK RO 3/10/2022) REMOVED CRACKED PILOT SIDE WINDOW SUPPORT POST AND REPLACED WITH NEW SUPPORT POST. REF. CRJ700 SRM 53-11-35, 51-40-11SDR IXXA2021122307Stringer Clip · crackedSTRINGER H-CLIP ON STR 36L AT STA 632 IS CRACKEDSDR 2021F00375None · leakingRIGHT ENGINE IDG PAD DRAIN WITH OIL LEAK. DURING TRANSIT CHECK, IT WAS A DETECTED AN OIL LEAK ON RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION AT RIGHT ENGINE, DETECTING AN OIL LEAK ON IDG PAD DRAIN OF 20 DROPS PER MINUTE; SO THE SEALOL SEAL ASSEMBLSDR HNAA2021112900581None · noneE887876 - CARGO DOOR CUT-OUT FR 65 SHEAR CLIP CORRODED .... REPAIRED CARGO DOOR CUT OUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04-RE FIGURE 212 AND EO1-53-21-0317SDR HNAA2021112900580None · noneE887870 - SHEAR CLIP AT FR 65 BETWEEN STRGS 21R-20R CORRODED ... REMOVED AND REPLACED SHEAR CLIP AT FR 65 BETWEEN STRGS 21R-20R IAW EMB 145 SRM 51-40-02.SDR HNAA2021112900577None · noneE887864 - CARGO DOOR LWR CUT-OUT FLOOR SILL CORRODED ... REMOVED AND REPLACED CARGO DOOR CUT- OUT LOWER FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR HNAA2021112900576None · noneE887863 - RH #4 CARGO FLOOR SILL CORRODED .... RAR RH #4 CARGO FLOOR SILL IAW EMB145 SRM 51-40-02SDR HNAA2021112900575None · noneE887860 - RH #1 CARGO FLOOR SILL CORRODED ... REMOVED AND INSTALLED NEW RH #1 CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR HNAA2021112900574None · noneE887858 - LH #2 CARGO FLOOR SILL CORRODED .... UPON FURTHER INVESTIGATION FOUND DAMAGE ON THE LH #2 CARGO FLOOR SILL TO BE OUT OF LIMITS IAW EMB 145 SRM 51-31-10-AD. REMOVED AND REPLACED LH #2 CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR R61A2021111900918Beam · corroded4 CROSSBEAM IS CORRODED IN TWO LOCATIONS OUTBOARD OF RH SEAT TRACK BEAM AS MARK CUT OUT DAMAGE, FABRICATED AND INSTALLED 'L'' ANGLE REPAIR AT CROSSBEAM FRAME 84 OUTBOARD OF RH SEAT TRACK BEAM REFER ETD2021-170-036002. RESTORED SURFACE PROTECTION TO REWORKED ARSDR R61A2021111900916Beam · corrodedFR 17 CROSSBEAM HAS SEVERAL AREAS OF CORROSION INBOARD AND OUTBOARD OF RH SEAT TRACK BEAM. REPAIRED CROSSBEAM FRAME 17 INBOARD AND OUTBOARD OF RH SEAT TRACK BEAM REFER SRM 53-00-10/REPAIR 03P. RESTORED SURFACE PROTECTION TO REWORKED AREA REFER SRM 51-23-06, CSDR 2021FA0000301None · noneAIRCRAFT REPORTED INTERMITTENT ELECTRICAL FAILURES AND OTHER SHOPS HAD REPLACED ALTERNATOR, REGULATOR, AND ALTERNATOR INOP SENSOR WITH NO HELP. FOUND WIRE ON FIELD TERMINAL OF ALTERNATOR SWITCH IN INSTRUMENT PANEL WAS 2 1/2 TURNS LOOSE CAUSING INTERMITTENT CONSDR 2021FA0000300Pitot Head · arcedPITOT HEAT FAIL CAS MESSAGE CAME ON WHEN PITOT HEAT WAS TURNED ON. FOUND PITOT MAST AFT HEATING ELEMENT WIRES WERE INSTALLED AND TY-WRAPPED IN JUST A WAY THAT THEY SHORTED ON THE PITOT HEAT ELEMENT CASE. THIS CAUSED THE ELEMENT TO FAIL BUT ALSO CAUSED PITOT ANSDR MASA20211027521Stringer · corrodedCORROSION STRINGER 26R BETWEEN FS280 AND FS295 IN MAIN AVIONICS BAY|R&R STRINGER 26RSDR 2021FA0000002None · noneSOME PROBLEM TEXTSDR IXXA2021122309Stringer Splice · corrodedFACTORY STRINGER SPLICE AT STA 1285, S39L IS CORRODEDSDR HNAA2021112900578None · noneE887865 - FR 66 CRACKED AT STRG 16R .... REMOVED, FABRICATED AND INSTALLED FABRICATED FR-66 SPLICE "U" SHAPE DOUBLER REPAIR AT STRG 16R IAW EMB 145 SRM 53-00-04-RE FIGURE 201 AND EO1-53-21-0318SDR JJBA20211026002None · noneDENT FOUND ON EXTERNAL SKIN BTW FR 79-80 AND BTW STR 11LH - 12LH. ON LH REAR FUSE 2 SKIN, AFTER INVESTIGATION, DENT IS LOCATED BTW FR80-81 AND BTW STR 11L-13L. DENT IS OUT OF LIMITS. PAINT STRIPPED FOR INVESTIGATION AT DENT LOCATION. DENT ON EXTERNAL SKIN BTW SDR JJBA20211026001None · noneCRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. LH FRAME 59 REPAIR FRAME SEGMENT AND SPLICE FABRICATED. LH FRAME 59 REPAIR PERFORMED BTW STR 14L-18L WITH NEW FABRICATED FRAME SEGMENT AND SPLICE.SDR MASA20220329149None · corrodedCORROSION ON LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN
LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN WAS REPLACED PER AMM 53-00-49SDR MASA20220329148None · corrodedCORROSION ON RIGHT FLOOR SEAT RAIL FS349-FS485 BL 9.0 AT PAX CABIN | FLOOR SEAT RAIL FS349-FS485 BL 9.0 AT PAX CABIN WAS REPLACED PER CRJ-900 SRM 53- 00-49.SDR HNAA2021112900579None · noneE887868 - FR 69 DAMAGED FROM CHAFING BETWEEN STRGS 18L-19L .... PREPPRED, FABRICATED AND INSTALLED SERVICEABLE REPAIR INTERNAL DOUBLER AND FILLER FOR FR 69 BETWEEN STRGS 18L-19L IAW ETD2021-145-037110 AND EO1-53-21-0319SDR SWIA202162173None · noneTRANSFER FROM EAML 763411 : QTY 07 MIS-DRILLED HOLES RH H/STAB LOWER SKIN O/B RIB NO 9. REF REO601R-55-11-699 DATED 2021-10-22 REV -- (FLIGHT 5459 - FILED CLOSED) REPAIRED MIS-DRILLED HOLES IN RH HORZONTAL STAB LOWER SKIN BETWEEN RIB #7 - RIB #9 AND F/SPARSDR EVCA102521Ring · crackedUPPER LH ATTACHMENT FITTING ON TAILBOOM RING IS CRACKEDSDR 2A6R2021102562004Frame · corrodedDAMAGE TO FRAME 1 (PN: L533M1011212) IN THE FORM OF EXTENSIVE CORROSION ACROSS THE LOWER FLANGESDR CALA2021102501966None · corrodedAFT CARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 58- 59 STR 43LH HAS CORROSION. PER HAECO LCQ NR 9296565/30565 GENERA TED BY V061595 REPAIRED AFT CARGO STRINGER SPLICE AT FR 58-59 STR 43L/H IAW 320 CORRECTING DIP LIMITS TO THE FOLLOWING 60,000FC / SDR CALA2021102501964None · corrodedAFT CARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 56- 57 STR 41LH HAS CORROSION. REPAIR EMBODIMENT IAW SRI 53-00-13-205-001 TABLE 006.ALL WORK AC COMPLISHED ON HAECO NR 9296564. REMOVED AND REPLACED STRINGER REPAIR DOUBLER IN AFT CARGO AREA F R 56-5SDR IXXA2021123005Ball Mat · crackedALC CENTER BALL MATT CRACKED ON LOWER SURFACE AT BALL FITTINGSDR SWIA202163186None · corrodedCORROSION ON GALLEY SERVICE DOOR ATTACH ANGLE TO INNER STRAP AT FS 319.00, STR 17R. (C CHECK RO 12-19-21) REPLACED ATTACH ANGLE AT FS 319.00 STGR 17R REF. CRJ700 SRM 51-42-06-001-001-A01 / COMPLIED WITH TASK CARD 51-900-1002-SKYSDR A6WA202112178029Skin · dentedAIRCRAFT LOWER BELLY SKIN EXTERIOR HAS 3 EACH DENTS AT FS 654.50+10-FS 654.50+16 AND S25R+1 S26L+4. DENT DIMENSIONS ARE AS FOLLOW: (P1) = FS654.50+12 & S26L+4 = .500"L X .455"W X .016"D (P2) = FS654.50+10 & S26R+4 = .550"L X .450"W X .007"D (P3) = FS654.50+16
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