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 A6WA200740015Nut Clip · crackedRIGHT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-58 CRACKED APPROX .3 INCHES LONG INBOARD SIDE RBL 9.0. MAINTENANCE REMOVED CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD REPAIRSDR 06FDEA04384Flange · corrodedAPU AIR INLET SOUND SUPPRESSOR AND MOUNTING FLANGE IN WHEEL WELL HAVE CORROSION ON MATING SURFACE. BLENDED FORWARD, AFT AND INTERCOSTAL HFEC FOR MATERIAL LOSS, FORWARD STIFFENER AND INTERCOSTAL BEYOND LIMITS, AFT STIFFENER, REPAIRED PER EA NR 7-5310-99309. RSDR DXTA200601797Unknown · vibrationON CLIMBOUT PASSING THROUGH FL 190 AT 280 KTS GOT VERY PRONOUNCED VIBRATION. VIBRATION CONTINUED UNTILL LANDING BACK IN CMH. JACKED AIRCRAFT AND CYCLED GEAR. INSPECTED GEAR AND DOORS, FLIGHT CONTROLS AND EXTERNAL DOORS. FOUND LOCK ON EXTERNAL LAV SERVICE DOORSDR SIMA200631707Structure · vibrationON DESCENT AT 250 KNOTS, NO ICING CONDITION AND GEAR UP. STRONG VIBRATION IN AIRFRAME WAS FELT. VIBRATION NOT FELT IN THE CONTROLS. APPEARS TO BE MORE PROMINENT ON THE RIGHT SIDE AFT OF THE FLIGHT DECK. SPEED REDUCED TO 200 KNOTS, VIBRATION GOES AWAY. PERSDR TRAX200601105Doubler · unknownRIGHT FS 640 DOUBLER SUSPECT CRACKED, REF EO600-53-69 0002. REPAIRED IAW ASA EO 600-53-81 REPSDR 06FDEA04208Unknown · crackedLOWER FWD CARGO COMPT 2 CRACKS 1" LONG ON CAP AT L35 LT & AT L39 LT AT STA 595. ACCOMPLISHED EA NR 8-5310-96117.SDR TRAX200601087Unknown · crackedSUSPECT CRACK AT RIGHT FS 640 STRINGER 14 FWD RADIUS.SDR QXEA200603389Fastener · corrodedPDX C4 - SEVERAL RIVET BUCK TAILS HAVE CORROSION IN BETWEEN STATIONX 43650. - 445.50 ALONG STRINGER 31R IN CABIN UNDERFLOOR. REPAIRED IAW DHC-8-200 SRM 51-20-26 AND SRM 51-40-11.SDR 2006UALA02157Unknown · vibrationAIRFRAME VIBRATION ON CLB AT FL250-340 .78 MACH. LIGHT VERTICAL VIBRATION FELT THRU THE FLOOR, NOSE TO TAIL AT 327 KNOTS, 78 MACH ON CLIMB FROM FL 250 -340. NO ENGINE VIBRATION. CONTROL INPUT DID NOT STOP VIBRATION. FOUND 10" PIECE OF WING TO BODY FAIRING SDR TRAX200600968Intercostal · crackedFOUND RT SIDE FS 484 INTERCOSTAL CRACKED AT RBL 36.00 (MARKED).SDR DU4R2006654Threshold · corrodedAFT CARGO THRESHOLD BLENDED (SILL AREA) STILL SHOWS EVIDENCE OF CORROSION. FWD AND AFT HORIZ FLANGES BLENDED OUT OF LIMITS IAW DC-9/SRM MD-88 SRM 53-05 FIG 63. FABRICATED AND INSTALLED DOUBLER REPAIR FROM 6AL-4V.040 TITANIUM IAW DC-9/MD-88 SRM 53-05D FIG 63 SDR SIMA200629202Structure · vibrationRUDDER PEDALS AND CONTROL COLUMN VIBRATION FELT AFTER A CLUNK NOISE ON RIGHT SIDE OF THE AIRCRAFT. VIBRATION FELT MOSTLY ON RIGHT CONTROL COLUMN AND ON FLOORBOARD ALONG THE AIRCRAFT. WALK AROUND REVEALED NO VISIBLE DAMAGE. FLIGHT DIVERTED TO BNA. COMPLIED SDR 06FDEA03605Structure · vibrationIN CLIMB THRU FL190 (300 KNOTS) A-FRAME BUFFET. CYCLED SPEED BRAKE (NO HELP). DISCONNECTED A/P AND SLOWED TO 280 KNTS WITH CONTINUAL BUFFET. AT FL 240 A-FRAME BUFFET STOPPED, VIBRATION IN NR 1 THROTTLE.SDR 2006FA0001086Support · corrodedDURING ANNUAL INSPECTION PEDAL SUPPORT WAS FOUND WITH CORROSION ON LOWER BOLT PADS BEYOND REPAIRABLE LIMITS. REPLACED SUPPORT BRACKET WITH SERVICEABLE PART. (K)SDR CA061011005Access Panel · missing(CAN) UPON AIRCRAFT ARRIVAL, DURING WALK AROUND INSPECTION, FOUND THE FWD CARGO DOOR LOWER FWD ACCESS PANEL, FIN811AR, MISSING. MOUNTING HARDWARE, FASTENERS AND LANYARDS WERE STILL ATTACHED TO THE CARGO DOOR. DOOR WAS INSPECTED AND NO FURTHER DAMAGE WAS NOTICESDR 2006UALA01841Crease Beam · corrodedSTA 395 RT SIDE CREASE BEAM WEB CORRODED RBL 54 WL 207. MAJOR REPAIR: REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-02.SDR CA060818002Washer · damaged(CAN) THE -4 WASHER IS NOT CUT TO FIT THE BOLT AT THE SHANK, CAUSING FRETTING AND CORROSION ON THE SHANK RADIUS UNDER THE BOLT HEAD. (TC NR 20060818002)SDR PIDR2006010Repair · improperEXISTING REPAIR AT BS887 AND STR25RT NOT IN COMPLIANCE WITH THE SRM. REPLACED EXISTING REPAIR IAW SRM 53-00-01 REPAIR 31.SDR 06FDEA2590Structure · crackedCOCKPIT FLOOR AREA AT RIGHT OBS SEAT LOCATION, CUTOUT FOUND WITH CRACKS ALONG CIRCUMFERENCE.SDR 2006UALA01326Structure · vibrationRETURNED TO THE FIELD TWICE DUE TO AN AIRFRAME VIBRATION. PEFORMED VIBRATION CHECK AND FOUND LEFT PACK EXHAUST DOOR LINKAGE BROKEN. REPLACED LINKAGE. INFORMED CREW FOR MONITORING THIS PROBLEM FOR FUTURE EVALUATION.SDR AMTA200600379Pin · corrodedDURING ACCOMPLISHMENT OF EO, FOUND THE LT SIDE PINS (5) CORRODED OR WORN AND FOUND THE RT SIDE PINS (4) CORRODED OR WORN. REMOVED AND REPLACED ALL 10 MOUNT PIN IAW EO. (K)SDR TRAX200600229Clip · crackedRT I/B CLIP CRACKED AT F.S. 484. REMOVED CRACKED CLIP AT RT I/ B BS 484 FABRICATED NEW SERVICEABLE CLIP USING .063 2024-T3 PO 3580. ALODINED, PRIMED AND PAINTED IAW CRJ SRM 51-21-11 AND 51-25-00, INSTALLED CLIP ALL WORK DONE IAW REO 601R-53-41-059.(CLOSED)SDR TRAX200600194Structure · crackedFOUND CRACK AT RBL 9 FS 559.00, RESOLVED ON W/O: 24018 TASKCARD: N/R-00406. PERFORMED ET INSPECTION IN SUSPECT CRACK IAW NDT CRJ 200 NDT MANUAL PART 1 CHAPTER 51-20-06. NO DEFECTS NOTED.SDR TRAX200600198Structure · crackedAEB RT STA 640 POSSIBLY CRACKED.SDR SIMA200612501Skin · vibratesDURING CLIMB HEARD A LOUD POPPING SOUND AT 16,100 AND 30,500. ON DESCENT INTO CVG, SOUND AGAIN AT ALTITUDES 26,000, 18,000, 13,400, 10900, 6,700, 4,400, AND 3,200. INSPECTED AND FERRIED AIRCRAFT TO SAW FOR REPAIR. REPAIRED OIL CANNING OF SKIN BETWEEN FRAMESSDR IXXA06RNG025SSkin · misrepairedDURING ROUTINE C CHECK, AN IMPROPER REPAIR ON SKIN AT STATION 479, LONGERON 28-RIGHT. DAMAGED SKIN SECTION WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-055 AND SRM 53-2-5 FIGURE 14A. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR GLBA20060734Structure · corrodedCORROSION FOUND DURING STRUCTURAL INSPECTION, STA 220-288 AND STR 13L-16L, PENDING REPAIR.SDR EIA2006099Unknown · lightning strikeFOUND LIGHTNING STRIKE BS 420 - 440 STR 0 1R HAS BLIND RIVET INSTALLED. FABBED AND INSTALLED CAT A REPAIR PER B747 SRM 53-30-03 FIG 4B.SDR TSAA0653021Spar · corrodedCORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-301. REMOVED CORROSION AND INSTALLED REPAIR FILLER IAM ALOHA'S ECO 3560. FAA 8100.9 RECEIVED.SDR MALA060178Panel · corrodedRT WRAP AROUND PANEL, P/N 7253710-243 IS CORRODED OUT OF LIMITS AND HAS BEEN REMOVED AND REPLACED WITH A NEW PART IAW SRM 51-40-21. REF: EAMS WORK ORDER 213643 TASK 1528.SDR SWAA060788Structure · crackedDURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 184, RBL 5.7, WL 184. REPAIRED CHORD PER EA & SRM.SDR SIMA200606913Web · corrodedRT WEB AT STA 280 WAS FOUND CORRODED. PERFORMED CUT OUT OF WEB TO REMOVE DAMAGE. PREPARED SECTION FROM NEW WEB. FABRICATED A WEB SPLICE. REPAIR DONE IAW REO. (K)SDR ASOA06279Sill · corrodedDURING A C-CHECK, THE FLOOR SILL, AROUND THE NUT PLATE HOLE AT FS 529.00 AND 36 LBL, WAS FOUND TO BE CORRODED. MRR WILL REMAIN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)SDR ASOA06274Structure · crackedDURING C-CHECK, STATION 202, NEAR THE PARKING BRAKE CABLE, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K)SDR SIMA200606201Web · corrodedDURING 2C CHECK OF AIRCRAFT, THE RT LOWER WEB AT FS 280 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A SECTION OF BEW FOR REPAIR, FABRICATED A SLICE PLATE. REPAIR DONE IAW REO. (K)SDR QXEA200600557Unknown · damagedYYC - C3 FUSELAGE INTERIOR HAS TOOL MARK ON INNER RADIUS OF CHANNEL BELOW WINDOW AT FUSELAGE STATION 985, STRINGER 12R. REPAIRED IAW REO 670-53-51-011 AND HORIZON AIR EA R-53-437.SDR ASAA05040087Skin · lightning strikeYXX- LIGHTING STRIKE FOUND AT BSTA 340 BETWEEN STR 21 AND 22 RT. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01, FIG 201.SDR ASAA05400081Skin · lightning strikeYXX- LIGHTING STRIKE AT BS 360, STR 22R. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201 REPAIR 19.SDR 0080Skin · lightning strikeLIGHTING STRIKE AT BSTA 320 BETWEEN STRINGER 21R AND 22R. LIGHTING STRIKE REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 19.SDR 2006UALA00161Rivet · crackedFOUND 5 EA CONFIRMED CRACKED RIVETS AROUND PERIMETER OF 1 LT, 2 LT, 3 LT & 5 LT FLIGHT DECK WINDOWS. REPLACED CRACKED RIVETS PER SRM 51-40-02.SDR ASOA06157Access Panel · crackedDURING C-CHECK, THE LOWER RT ENGINE BEAM ACCESS PANEL, IB FORWARD CORNER, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER RT ENGINE BEAM ACCESS PANEL, IB FWD CORNER, IAW EO. (K)SDR 2006UALA00154Rivet · crackedCRACKED RIVET HEADS FOUND REPLACED CRACKED RIVETS PER SRM 51-40-02.SDR 2006UALA00096Fastener · crackedNR 1R, 2R, 3R & 4R FLIGHT DECK WINDOWS HAVE 4EA, 11EA, 18EA & 4EA CRACKED RIVETS RESPECTIVELY AROUND THE PERIMETER OF THE WINDOWS & FRAME ON EXTERNAL SKIN. REPLACED CRACKED RIVETS ON EXTERIOR OF AIRCRAFT AT PERIMETER OF WINDOWS REF SRM 51-40-02.SDR ASOA06045Unknown · corrodedDURING A C-CHECK IN MCN, FOUND CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 557, RBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 557, RBL 42, IAW REO. (K)SDR ASOA06048Unknown · corrodedDURING A C-CHECK IN MCN, CORROSION FOUND AROUND THE NUT PLATE AT FS 441, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 441, LBL 42, IAW REO. (K)SDR ASOA06020Doubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS425, RBL 39. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)SDR 05FDEA04323Repair · noneEXTERNAL DOUBLER REPAIR FROM STA 2007 TO STA 2018 BETWEEN LONG 41 AND 48 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.SDR 05FDEA04322Repair · unknownEXTERNAL DOUBLER REPAIR AT STA 1227 BETWEEN LONG 40 AND 41 RT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.SDR 05FDEA04321Repair · unknownEXTERNAL DOUBLER REPAIR FROM STA 1511 TO STA 1520 BETWEEN LONG 52 AND 51 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.SDR 05FDEA04283Repair · unknownMAIN CABIN R-3 FWD DOOR JAMB HAS AN EXTERNAL DOUBLER REPAIR BOTTOM PART STA 1256 DIM 7" BY 9.75". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.
Back to JASC 5300