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.

SDR UALA2011071403572Unknown · damagedHAIL DAMAGE, WILL CONTINUE TO MAP OUT AND EVAL DAMAGE.Jul 14, 2011 · N448UA · Airbus A320232SDR UALA2011071403571Unknown · damagedA-C SUSTAINED HAIL STORM AT GATE. NEED TO PERFORM HAIL DAMAGE INSP.Jul 14, 2011 · N414UA · Airbus A320232SDR UALA2011071403569Unknown · damagedCREW REPORT: HEAVY HAIL ENCOUNTERED AT GATE.Jul 14, 2011 · N813UA · Airbus A319131SDR UALA2011071403568Unknown · damagedHAIL STRIKE DAMAGE.Jul 14, 2011 · N814UA · Airbus A319131SDR SWIA201126799Unknown · damaged(FLT 5622) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N975SW · Cndair CL6002B19SDR SWIA201126798Unknown · damaged(FLT 5599) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N973SW · Cndair CL6002B19SDR SWIA201126797Unknown · damaged(FLT 6515) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N961SW · Cndair CL6002B19SDR SWIA201126796Unknown · damaged(FLT 5573) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N959SW · Cndair CL6002B19SDR SWIA201126795Unknown · damaged(FLT 5574) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N958SW · Cndair CL6002B19SDR SWIA201126794Unknown · damagedFLT 5576, HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N937SW · Cndair CL6002B19SDR SWIA201126793Unknown · damagedFLT 5407, HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.Jul 13, 2011 · N923SW · Cndair CL6002B19SDR DXTA2011071104655Unknown · vibrationON APPROACH, AT 122 KNOTS, EXPERIENCED A VIBRATION AND ASSOCIATED LOW PITCH RUMBLE NOISE, SEEMED TO CHANGE WITH THROTTLE CHANGES. NOISE LASTED UNTIL TOUCHDOWN. RUMBLE COULD NOT BE HEARD ON TAXI IN. INSPECTED AIRFRAME AND BOTH ENGINES, RAN ENGINES AT ALL PJul 11, 2011 · N676QS · Cessna 560XLSDR ALGA063011194ALStructure · corrodedFUSELAGE SHELL ASSY LOWER FORWARD, MULTIPLE CORROSION SPOTS AND REPAIRS. REPLACED FUSELAGE SHELL ASSY LOWER FORWARD.Jun 30, 2011 · N194AL · Bell 206L4SDR IPXA1567982Unknown · dentedINSPECTION TYPE:C-1 AFT CARGO COMPARTMENT STA 1540 STR 22-23 R HAS DENT REPAIRED IAW SRM 53-00-07-2R-5 REPAIR 5 DETAIL 2 AND 53-30-07-2RJun 28, 2011 · N403UP · Boeing 75724APFSDR CHQA201100249Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE FORWARD SERVICE DOOR SILL. MAINTENANCE REPAIRED THE CABIN FLOOR STRUCTURE FORWARD SERVICE DOOR SILL IAW ETD2011-145/101400 WITH NO FURTHER DEFECTS NOTED. THE FINAL CORRECTIVE ACTION AND THE Jun 24, 2011 · N567RP · Emb EMB145LRSDR UIEA2011060400273Structure · damagedDURING LOADING OPERATIONS, ENGINE PALLET CAUSED DAMAGE TO FLOORBOARD PANELS BS1500 - BS1625, LBL 85.65 GOUGES/PUNCTURE DAMAGE (REF FIG 1). THE HOLE IS APPROX 30 INCHES LONG BY 2.5 IN. WIDE.Jun 4, 2011 · N409MC · Boeing 74747UFSDR 2011F00131Structure · crackedDURING NDT INSPECTION AT BS 291.5 ON SR 16, RT FORWARD GALLEY AREA FOUND CRACKED.Jun 1, 2011 · Boeing 737200SDR FDEA201105272010Floorbeam · crackedAFT FUSELAGE FR66 FLOOR BEAM CRACKED AT VERTICAL STIFFENER BETWEEN SEAT TRACK 3 AND 4L.May 27, 2011 · N654FE · Airbus A300F4605RSDR DALA1503679228Rail · corrodedCORROSION ON 2 LT GUIDE RAILS OF AFT PASSENGER COMPARTMENT FROM BS 1184 - 1288. SRM 53-40-01, VOL 1, FIG 6, REPAIR IAW SRM 53-40-01,May 26, 2011 · N928DN · Doug MD9030SDR DALA1135299866Structure · chafedAFT ACC COMPT STA 1190 L17R HOLE CHAFED IN FR OB OF VALVE. CUT OUT DAMAGED AREA 2.5 INCH BY 1 INCH. NO DEFECTS PER NDT SPM 06-10-01.001. FIB FILLER FROM PART NR 9958233-27 AND DOUBLERS FROM.063 7075-T6 PART NR SR09530035-25. INSTALLED YAW DC9 SUM 5304 FIG May 18, 2011 · N775NC · Doug DC951SDR UALA2011041101727Unknown · corrodedSTATION 1701 THRU 1720 HAS SURFACE CORROSION IN 2 PLACES. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION 2 AREAS FOUND TO BE OUT OF LIMITS STA 1704.5 AND 1708.5 RBL 50. PERFORMED HFEC OF FASTENER HOLES AND DECK PLATE NO DEFECTS NOTED. FABRICATED AND INSTALLEApr 10, 2011 · N561UA · Boeing 757222SDR ASOA201100670Structure · crackedCRACK INDICATION NOTED AT FS 559, RBL 9, WL 54.10 IN CHEM-MILL APPRO .100" LENGTH 50 PERCENT FULL SCREEN HEIGHT, FAILED NDT. REPAIRED IAW REO 601R-53-41-609 REV B.Mar 31, 2011 · N917EV · Cndair CL6002B19SDR ASOA201100654Bulkhead · crackedCONTINUATION FS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CLIP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. INSTALLED LT CAP ANGLE AND SPLICE IAW REO 601R-53-41-260. INSTALLED REPAIR PARTS ON LMar 29, 2011 · N914EV · Cndair CL6002B19SDR ASOA201100559Unknown · corrodedCORROSION ON RBL 9 AT FS 559+96 FLOORBEAM. TRIMMED OUT FLOORBEAM IAW SRM 53-00-43, PG 201. PERFORMED EDDY CURRENT INSPECTION, NO INDICATIONS FOUND. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW SRM 53-00-43.Mar 23, 2011 · N881AS · Cndair CL6002B19SDR ASOA201100502Unknown · corrodedBOTH SEGMENTS OF RBL 9.0 IN CARGO BAY HAVE CORROSION AND PREVIOUS CORROSION REPAIRS. REMOVED SEAT RAILS ON RBL 8 IN CARGO BAY IAW SRM 51-40-11, AMM 53-01-11-946-003 AND DWG 601R38312. FABRICATED NEW SEAT TRACK SEGMENTS IN CARGO BAY. FABRICATED NEW SEAT TRACMar 16, 2011 · N849AS · Cndair CL6002B19SDR U2RA486DHN010Mount · corrodedMAIN CABIN CTR GALLEY MOUNT STA 1685, BL 0 CORROSION.Mar 2, 2011 · N763CA · Boeing 7572Y0SDR U2RA486DHN007Floor Support · corrodedAFT CARGO, STA. 1340-1360, RBL 8,FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES.Mar 1, 2011 · N763CA · Boeing 7572Y0SDR FDEA201102280793Tube · missingPFM 1C CHECK FOUND HOSE TUBE WAS MISSING AT FR38-FR40 OF LEFT WALL OF M/D COMPLIED WITH EA 6-2610-149002 AND CHECK CONDITION IS NORMAL IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Feb 28, 2011 · N743FD · Airbus A300B4622RSDR DALA1114351805Panel · missingPANEL 149AL MISSING FROM AIRCRAFT, INSTALLING ERA 490445-14.Feb 28, 2011 · N829MH · Boeing 767432ERSDR FOTR2101904027Skin · damagedEVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 296 BETWEEN STRINGER 26-25 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 296 BETWEEN STRINGER 26-25 LT IAW SRM 51-30-2. HFEC AREA IAW NDTM 51-00-00 FIGURE 23 PART 6 WITH NO DEFECTS NOTEFeb 25, 2011 · N815EA · Boeing 727225SDR EE4Y20110109Longeron · corrodedDURING THE INSP FOUND THE LONG 30 CORRODED FROM 1147 TO 1201 IN SEVERAL PARTS.Feb 15, 2011 · N573SH · Doug DC982SDR QXEA2011011800034Diaphragm · crackedC6 CHECK - FOUND A CRACK ON LT DIAPHRAGM UNDER PANEL 195DL AT FS 909. FOUND CRACK TO BE 1" LONG, SENT REQUEST TO MFG. RECEIVED REO 670-53-82-413. COMPLIED WITH REPAIR IAW REO 670-53-82-413.Jan 14, 2011 · N603QX · Cndair CL6002C10SDR IXXA11SMN001SFastener · improper partDURING ROUTINE C-CHECK INSP, FOUND CHERRY MAX RIVETS USED IN REPAIR AT STATION ES 1360-1380. REMOVED FASTENERS FROM REPAIRED AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FINGER DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEJan 13, 2011 · N799AL · Doug DC862FSDR UIEA2010122200212Unknown · misrepairedDEVIATION DURING PERFORM EO NR 4421A060, SHORT EDGE MARGIN INTERFERENCE OVERSIZE HOLE. (IAW EI NR T2010A21B-3142, REV 00 AND REV 01.)Dec 22, 2010 · N747BC · Boeing 7474J6SDR ASOA201001971Frame · corrodedFS 349 FRAME CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. LOCATED, DRILLED AND DEBURRED & INSTALLED NEW FRAME IAW SRM 51-42-06.Dec 15, 2010 · N882AS · Cndair CL6002B19SDR ASOA201001970Unknown · corrodedFS 333 BOTTOM SECTOR IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. R & R FRAME IAW SRM 51-42-06 & 51-42-21, PN 601R32004-55.Dec 15, 2010 · N882AS · Cndair CL6002B19SDR QXEA2010121000858Unknown · corrodedC5 CHECK - BLENDED CORROSION IAW SRM 53-20-31. REMAINING MATERIAL .062 REF NTM 51-00-02-250-801 FOUND TO BE WITHIN LIMITS IAW SRM 53-20-31-02-01 LESS THAN .002 MATERIAL LOSS IAW SRM 51-20-31 ORIGINAL MAT .063. ALODINED AND PRIMED IAW 51-21-10 AND 51-25-10. CDec 7, 2010 · N424QX · Bombdr DHC8402SDR FOTR2019813832Frame · damagedREMOVAL OF GILLINER ATTACH ANGLE ON LT SIDE OF FUSELAGE AT TOP OF WINDOW LEVEL REVEALED DOUBLE DRILL HOLES IN FRAME AT FS 720D. CUT DAMAGED AREA DIM. .800" X .800" AT STA 720D FAB NEW REPAIR PARTS 2EA ANGLES FROM 7075-0 PO 90010396 DIM. 13.2500" X 3". LOCATEDNov 26, 2010 · N713AA · Boeing 727223SDR FOTR2019813583Intercostal · damagedBS 950E-950F INTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 AFT CARGO. REMOVED INTERCOSTAL AT STA 950E-950F RBL4 IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .040". PO 9009608. IAW SRM 53-10-2. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED INTERCOSTANov 17, 2010 · N713AA · Boeing 727223SDR QMLRMD7271Support Angle · burredFLOOR NUTPLATE CAME LOOSE WHILE INSTALLING A SCREW AND DAMAGED THE SUPPORT RIB. DURING THE INSTALLATION OF A LITTER LOADING ATTACHMENT SCREW INTO A NUTPLATE IN FLOOR IN CABIN AREA, LT SIDE OF ACFT, RIVETS RETAINING THE NUTPLATE SHEARED. THE NUTPLATE SUBSEQUENov 16, 2010 · N808LF · Snias AS350B3SDR IXXA10SMN109SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT SECTION FLOOR LONGERON 36 CORRODED AT STA 1690.000 - 1725.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON AND STRAPS. CLEANED, TREATED, PRIMED ARENov 10, 2010 · N602AL · Doug DC873FSDR RMXA102820100706Structure · crackedDURING SCHEDULED INSP, A 1.5" LONG CRACK WAS DISCOVERED ON THE COMPOSITE LT CLAMSHELL DOOR. THE CRACK IS AT THE OPENING FOR THE LOCKING PIN TO SECURE THE DOORS TOGETHER NEXT TO THE UPPER LATCH ASSY, TERMED ALIGNMENT CONE BY THE MFG. THE DAMAGED AREA WAS SANDEOct 28, 2010 · N135CM · Urocop EC135P2SDR C2XA10SH349Beam · corrodedSHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLANGE AT FRAME 54-59 IAW EMB-145 EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ERSDR HALA2010101100498Structure · corrodedLEVEL 2 CORROSION, ON UPPER CHORD, STA 347 BETWEEN LBL 33 TO LBL 55. BLENDED OUTSIDE LIMITS, IAW SRM 53-00-51-1A-1, REV 84. DAMAGED SECTION R & R IAW SRM 53-00-51, REPAIR 1.Oct 11, 2010 · N585HA · Boeing 7673G5SDR ASOA201001501Floor Support · crackedFS 484, RBL 27 FLOOR SUPPORT ANGLE CRACKED. R & R FS 484, RBL 27, FLOOR SUPPORT CLIP PN 601R31171-9 IAW SRM 51-42-06 AND 51-42-21.Oct 5, 2010 · N905EV · Cndair CL6002B19SDR HALA2010092000483Mount · corrodedLEVEL 2 CORROSION ON GALLEY FEET MOUNTS AT STA 1588, LBL76,STA.1592 LBL45, AND RBL 45, STA.1614, RBL45. R & R FEET IAW SRM 51-10-02, REV 84.Sep 20, 2010 · N586HA · Boeing 7673G5SDR CA101005001Cell · failed(CAN) THE AIRCRAFT WAS PERFORMING AERIAL FERTILIZATION OPERATIONS. THE HYDRAULIC LOAD CELL THAT IS ATTACHED TO THE CARGO HOOK FAILED INTERNALLY. THIS FAILURE ALLOWED THE HOOK TO ROTATE APPROXIMATELY 90 DEGREES WHICH IN TURN CAUSED THE MANUAL RELEASE CABLE TOSep 18, 2010 · Aerosp SA315BSDR UALA2010082603164Unknown · vibrationAIRFRAME VIBRATION DURING CLIMB FL300 - FL360..78M. CAN DAMPEN WITH RIGHT RUDDER. REPLACED BLUE SYSTEM RUDDER SERVO. TROUBLESHOOTING ACP'D.Aug 26, 2010 · N494UA · Airbus A320232SDR ASOA201001025Bulkhead · crackedTHE 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE FEED THRU HOLE AT 9:00. CUTOUT DAMAGE AND FABRICATED DOUBLER IAW REO 601R-53-11-563 STEP 1,2 & 5. C/W STEP 3 OF REO 601R-53-11-563. PERFORMED EDDY CURRENT OF FS 202.73 BULKHEAD CUTLINE IAW NDTM 51-20-06. NJul 21, 2010 · N682BR · Cndair CL6002B19SDR CA100609008Rod · mismanufacturedQTY 4 RODS WERE MFG WITH A FASTENER MISSING, FROM 1 ROD END IAW THE DWG. MFG IS CURRENTLY INVESTIGATING THE CONFIGURATION OF 2 PUSH RODS INSTALLED ON THIS ACFT TO DETERMINE IF FURTHER ACTION IS REQUIRED. 2 ARE BEING RETURNED FOR REWORK.Jun 7, 2010 · Dhav DHC6
Back to JASC 5300