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 ASAA0480278Floor Panel · delaminatedOKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 1309-1361. REPLACED FLOOR PANEL PER SRM 53-05. (M)SDR ASAA0480219Floorboard · delaminatedFOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION LEFT 1155 TO 1250 DELAMINATED AND NUMEROUS INSERTS CORRODED, AND BROKEN WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANELS IAW MD80 SRM 53-05. (M)SDR DXTA200400174Structure · noisyCLIMBING THROUGH 12,000 FT AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWED DOWN BELOW 250 KNOTS THEN THE PROBLEM STOPPED, RE-ACCELERATED IT HAPPENED AGAIN. LOWERED THE GEAR NORMALLY AND DIVERTED TO ACY. - ITEM IS SDR C2XA04SH174Buttstrap · corrodedSHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR MALA040142Structure · vibrationDURING FLT, VIBRATION FELT IN CONTROL COLUMN. HIGH FREQUENCY VIBRATION STILL FELT AT 250 KTS-270 KTS. VIBRATION MOST PRONOUNCED WHEN BANKING LEFT; ESPECIALLY WHEN RIGHT BANK ESTABLISHED, THEN LEFT CONTROL (ROLL) INPUT ENTERED. AIR RETURN TO MEM. WHILE REDUSDR C2XA03SH354Sill · corrodedDURING C CHECK THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA03448Skin · crackedDURING A C-CHECK IN MCN, THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 IAW ASA EO 600-53-0122. (M)SDR ASOA03430Angle · crackedDURING A C-CHECK IN MCN, THE FLOORBEAM VERTICAL ANGLES AT FS 484, LBL AND RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM VERTICAL ANGLES AT FS 484, LBL AND RBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M)SDR USAA030191Skin · crackedFOUND SKIN CRACKED .125 INCH, UPPER HINGE CUTOUT OF AFT ENTRY DOOR OPENING. BLENDED DAMAGE PER SRM 53-00-01. (M)SDR 2003F00580Panel · departedAIRCRAFT LOST NOSE PANEL ON TAKEOFF DURNG A PART 91 FLIGHT AIRCRAFT RETURNED TO BASE. UPON RECOVERY INSPECTION, FOUND THAT NOSE PANEL WAS LEFT UNFASTENED BY MAINTENANCE PERSONEL. (M)SDR HEEA088481Horn · damagedMECHANICAL DAMAGE INSIDE OF HORN BEYOND LIMITS. SCRAPPED.SDR ASOA03294Frame · crackedDUIRNG A C-CHECK IN MCN, THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 IAW ASA EO 600-53-0067A. (M)SDR USAA030055Intercostal · corrodedFOUND INTERCOSTAL CHANNEL AT STATION 396 RBL 59, WITH 1 INCH AREA OF CORROSION. FABRICATED PART FROM EXTRUSION PER BOEING DWG 14IN5161 AND SRM 51-10-0. CORROSION LEVEL 1, TASK NR C53-221 AND 222 -02, 03. (M)SDR GTIA030429Skin · dentedFOUND DENT AT FS 360 BETWEEN LONGERONS 19 AND 20R. DENT IS WITHIN ONE INCH OF STRUCTURE AND REQUIRES REPAIR. FABRICATED 1 DOUBLER. INSTALLED 1 DOUBLER REPAIR. (M)SDR USAA030072Stringer Clip · crackedPIT - FOUND CLIP CRACKED 1 INCH, STATION 360 STRIGNER 11R. INSTALLED FABRICATED CLIP PER SRM 51-40-02. (M)SDR USAA030049Clip · crackedPIT - FOUND STRINGER ATTACH CLIP CRACKED .25 INCH, STATION 578, S4R. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. (M)SDR ASAA02401DDSkin · chafedDURING C-CHECK, FOUND SKIN HAS AREAS OF CHAFING DAMAGE AT THE LEFT AFT LOWER SLIDE SEAL AT BS 1154. REPAIRED IAW SRM. (M)SDR C2XA03SH060Sill · corrodedSHV DURING C CHECK THE RIGHT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED REPAIR ON AFFECTED SILL IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ASAA024015AFrame · corrodedPAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 727E RBL 8-12 AND WL 148. REPAIRED IAW SRM. (M)SDR VNAA0303021Seal · failedDURING CLIMB OUT, THE CREW HEARD A THUMPING NOISE FROM THE UPPER RIGHT SIDE OF THE AIRCRAFT AND RETURNED TO DAY. MAINTENANCE INSPECTED AND TRIMMED THE UPPER FUSELAGE FAIRING SEAL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. FLIGHT 4192 THE LEFT WISDR C2XA03SH058Track · corrodedSHV DURING C CHECK LEFT UPPER SEAT TRACK NUMBER 3 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED TRACK IAW EMB 135 AMM 53-01-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH054Track · corrodedSHV DURING C CHECK LEFT HAND UPPER SEAT TRACK NUMBER 4 WHERE FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED TRACK IAW EMB 135 AMM 53-01-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ASAA0240134AFloor Support · corrodedPAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 860, RBL 8 AND WL 148. REPAIRED IAW SRM. (M)SDR C2XA03SH051Stringer · gougedSHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 TO 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH045Stringer · gougedSHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 TO 53. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICSDR C2XA03SH047Bracket · corrodedSHV DURING C CHECK CORROSION WAS FOUND ON PULLEY BRACKETS BETWEEN FRAMES 67 TO 68, BETWEEN STRINGERS 21 LEFT AND 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH044Stringer · corrodedSHV DURING C CHECK STRINGER 21 RIGHT WAS FOUND TO HAVE CORROSION BETWEEN SPLICES AT FRAMES 52 TO 53 AND FRAMES 60 TO 61. MAINTENANCE REMOVED AND REPLACED AFFECTED STRINGER IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH38Clip · corrodedSHV DURING C CHECK CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 20R AND 19R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH41Sill · corrodedSHV- DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 AND 23. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01089. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICESDR C2XA03SH40Skin · corrodedSHV DURING C CHECK CORROSION WAS FOUND ON THE CABIN UNDERFLOOR SKIN BETWEEN FRAMES 50 AND 61. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH36Skin · corrodedSHV DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 61 AND 65 AT STRINGERS 21L TO 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234 AND EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICSDR C2XA03SH35Skin · corrodedSHV DURING C CHECK CORROSION WAS FOUND ALONG CARGO FLOOR SKIN BETWEEN FRAMES 65 TO 68 AT STRINGERS 21L AND 2OR. MAINTENANCE REMOVED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH034Skin · corrodedSHV- DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 68 AND 73 AT STRINGERS 21L AND 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR EIA2003032StringerStringer 22L at BS 544 Corroded. CORRECTIVE ACTION: Repaired er ECRA 481-53-178-2. Removed corrosion per B747 SRM 51-10-02SDR EIA2003028IntercostalNose W.W. STA 300-320, Intercostal at LBL 10 Cracked. CORRECTIVE ACION: Removed and replaced Intercostal @ STA 300-320 per ECRA 481-53-170-2 & SRM B747 51-10-06, Pgs 1-30SDR EIA2003027IntercostalTop Side of W.W. (Nose) between STA 260-280 Intercostal at LBL 20 cracked. CORRECTIVE ACTION: Removed and Replaced per ECRA 481-53-170-2, B747 51-30-02, Pgs 1-3, & 21-32. Installed per B747 SRM 51-30-02 5-9 & 38-60, plus 51-10-06, Pgs 1-30SDR EIA2003026StrapFuselage Right Side Interior, Corrosion along skin longitudinal splices to stringer 12, STA 1740-2240. CORRECTIVE ACTION: Repaired per ECRA 481-53-169-2 Rev A. Removed corrosion per B747 SRM 51-10-01, pgs 13 & 14. Fab'd and installed quadrupler strap SDR EIA2003025StrapStringer 46L corroded under frame at B.S. 1700 (AFT PIT). CORECTIVE ACTION: Repaired per ECRA # 481-53-158-2 Rev A. Fab'd Strap (M) per ECRA. Installed per B747 SRM 51-30-02, Pgs 57-58-58BSDR EIA2003047Skin PanelGOUGH AFT OF MAIN CARGO DOOR CORRECTIVE ACTION: CLASS I REPAIR INSTALLED ON L/H FUSELAGE STA 447.5 to STA 457.5, from LONGERON 16L-17L (DOUBLER) PER DC9 SRM 53-04 Pg 60 & DC9 SRM 51-30-5, Pgs 1-30. REPETITIVE INSPECTION REQUIRED PER DC9 SRM 53-04, FIG 12BSDR EIA2003044StrapSTA 1581.5, THERE ARE TWO MIS-DRILLED HOLES IN HE LAP SKIN AT STRINER 19R. CORRECTIVE ACTION: NDT HOLES, INSTALL FREEZE PLUGS, FAB'D AND INSTALLED REPAIR STRAP PER ECRA 481-53-187-2 Rev A.SDR EIA2003043StringerLAP @ STA 2280 to 2340, RIGHT SIDE, STRINGER 12, HAS CORROSION LIFTING SEALANT. CORRECTIVE ACTION: REPAIRED STRINGER 12, FAB'D DOUBLER, PRIMED AND SEALED PER B747 SRM 53-30-03, FIG 18, & 53-30-02, FIG 2. REST OF LAP PER EO 53-747-1047-90 Rev B.SDR EIA2003042StringerAT STA 1416, CENTER OF STRINGER 19R, THERE IS (1) MIS-DRILLED HOLE IN LAP SKIN. CORRECTIVE ACTION: REPAIRED PER ECRA 481-53-187-2, PART 5. INSTALLED STRINGER TEE PER SRM 51-30-02, Pg 5-58.SDR EIA2003041FastenerIMPROPER FASTENER ON LAP SEAM AT BS 755 AND STRINGER 44R, ON R/H SIDE OF FUSELAGE NEXT TO REPAIRED AREA. CORRECTIVE ACTION: REPAIRED IMROPER FASTENER ON LAP SEAM AT BS 755, STRINGER 44R PER ECRA 481-53-179-2 Rev ASDR EIA2003040AngleMAIN DECK STA 1168, BBL35R, WL 19.6, CENTER TANK ANGLE HAS CRACK. CORRECTIVE ACTION: REMOVED DAMAGE, NDT AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-172-2SDR EIA2003039IntercostalTOP SIDE OF NOSE WHEEL WELL BETWEEN STA 260 & 280, INTERCOSTAL AT RBL20 CRACKED. CORRECTIVE ACTION: REMOVED & REPLACED INTERCOSTAL @ STA 260-280, PER ECRA 481-53-170-2 Rev ASDR EIA2003038Skin PanelLEFT WING WHEEL WELL, UPPER FOWARD RIGHT CORNER, BS 1241, LBL6-LBL175, CORROSION ON OUTER SKIRT CORECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECT AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-68-2SDR EIA2003016BeltframeFwd. Cargo Pit, R/H structure frame at STA 540, RBL 60", has a crack as marked. CORRECTIVE ACTION: Repaired as per ECRA 481-53-167-2SDR EIA2003037StringerAT STATION 1601, ABOUT 3 INCHES ABOVE STRINGER 19R, THERE IS ONE (1) MIS-DRILLED HOLE CORRECTIVE ACTION: NDT HOLE, FAB'D AND INSTALLED REPAIR PARTS PER ECRA 481-53-187-2 Rev A.SDR EIA2003024StrapLap repairs from STA 1960-2180 at Stringer 19L requires additional strap. CORECTIVE ACTION: Installed external strap per ECRA 481-53-169-2 Rev ASDR EIA2003019StrapLap repairs from STA 1770-1960 at Stringer 12R reguires an additional strap. CORRECTIVE ACTION: Installed external strap per ECRA 481-53-169-2 Rev A
Back to JASC 5300