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 UIEA2022021600140Floorbeam · damagedFWD CGO COMPT L/H O/B AT BS 740 FLOOR BEAM FOUND DAMAGED.(<P>FWD CARGO COMPT LH BS 740 LBL 47.25 FLOOR STRUCTURE CHORD REPAIR AS PER RI-53-65-15384 REV A.</P>)Feb 23, 2022 · N850GT · Boeing 74787UFSDR 2022F00054Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL Feb 23, 2022 · N519QS · Cessna 120SDR 2A6R2022022363004Deck Plate · corrodedTHE AFT CABIN FLOOR (PN: L533M1015104) AT APPROXIMATE FUSELAGE STATION 4,150MM TO 4,500MM BETWEEN LBL 130MM AND LBL 480MM WAS FOUND TO HAVE DENT AND DELAMINATION DAMAGE. THE DAMAGE WAS EXTENSIVE THROUGHOUT THIS AREA.Feb 23, 2022 · N135AN · Urocop EC135P2SDR 2A6R2022022363003Angle · corrodedTHE RIGHT-SIDE CENTER CONSOLE TO FLOOR ANGLE (PN: L311M1060235) AT APPROXIMATE FUSELAGE STATION 1,400MM TO 1,800MM WAS FOUND TO HAVE CORROSION DAMAGE. THE CORROSION DAMAGE IS ALONG THE LENGTH OF THE PART.Feb 23, 2022 · N135AN · Urocop EC135P2SDR 2A6R2022022363002None · noneTHE FORWARD LOWER SIDE OF THE FRAME 3 BULKHEAD AT FUSELAGE STATION 3,150MM, WATER LINE 1,480MM WAS FOUND TO HAVE CORROSION DAMAGE AT THE BOTTOM EDGE OF THE WEB. THE DAMAGE AREA IS ESTIMATED TO BE APPROXIMATELY 1.4” X 16.7” SPANWISE TOTAL.Feb 23, 2022 · N135AN · Urocop EC135P2SDR SWIA202265251None · crackedSUSPECTED CRACK- RH WING LOWER SKIN AFT OF SPAR 2, INBOARD OF RIB 3 (MARKED) (C-CHECK RO 3/30/2022) PERFORMED TEMPORARY REPAIR REF ETD2022-170-008295. SEE CONTINUATION CARD FOR WORK PERFORMED. - THIS REPAIR IS CONSIDERED TEMPORARY AS IT WILL REQUIRE A DFeb 22, 2022 · N603CZ · Emb ERJ170200LRSDR SWIA202264678None · crackedLH WINDSHIELD/WINDOW SIDE STRAP HOLE #26 HAS A CRACK IN THE STRUCTURAL SIDE POST P/N# 601R33223-1. (FILED - CLOSED) REMOVED AND REPLACED WITH NEW SIDE POST PN 601R33223-1 REF CRJ 900 SRM 51-42-21-001-001-A01.Feb 22, 2022 · N896SK · Cndair CL6002D24SDR R61A2022022800171Skin · damagedLIGHTNING STRIKE DAMAGE TO AFT AREA BETWEEN FR51 AND 52 STGR 1R AND 2R. REPAIRED IAW SRM 53-22-01 REPAIR 11P. MAJOR REPAIR. AC RETURNED TO SERVICE ON 2-26-22Feb 22, 2022 · N201JQ · Emb ERJ170200LRSDR R61A2022022800170Skin · damagedLIGHTNING STRIKE DAMAGE BETWEEN FR12-13 AND STGR 2L-3L. REPAIRED IAW ETD 2022-170-006903 MAJOR REPAIR. AC RETURNED TO SERVICE ON 2-26-22Feb 22, 2022 · N201JQ · Emb ERJ170200LRSDR CALA2022022200487Skin · puncturedFUSELAGE HAS GROUND DAMAGE AT STA 2174 BETWEEN STR 44R AND 45R. PUNCTURE DAMAGE MEASURES 9.75" LONG AND 4.5" WIDE. LOCKED C/W AVO9521 STEP 1A. OPEN HOLE HFEC INSP REF. NDT PT 6 51-00-02 PROC.1, C/W 1.B. COUNTERSUNK HOLE REF. NDT PT 6 53-00-01, AND C/W STEP 2C.Feb 22, 2022 · N792UA · Boeing 777222SDR CALA2022022200486Skin · puncturedFUSELAGE HAS GROUND DAMAGE AT STA 2174 BETWEEN STR 44R AND 45R. PUNCTURE DAMAGE MEASURES 9.75" LONG AND 4.5" WIDE. LOCKED C/W AVO9521 STEP 1A. OPEN HOLE HFEC INSP REF. NDT PT 6 51-00-02 PROC.1, C/W 1.B. COUNTERSUNK HOLE REF. NDT PT 6 53-00-01, AND C/W STEP 2C.Feb 22, 2022 · N792UA · Boeing 777222SDR FDEA202202210933Rivet · looseLOOSE RIVETS INSTALLED SCREWSFeb 21, 2022 · N126FE · Boeing 7673S2FSDR R612022F00004Doubler · corrodedFWD FUSELAGE FLOOR CORROSION FOUND ON L/H FLOOR DOUBLER BTWN FR 15-16.R&R FLOOR DOUBLER FR 15-16 IAW EMB 170 SRM 51-41-02.Feb 21, 2022 · N722YX · Emb ERJ170200LRSDR CALA2022022200478Angle · corrodedREF AMES ILN NRC 142584-0100-0035. BLENDED DAMAGE ORIGINAL THICK NESS .090 REMOVED .045 OUT OF LIMITS IAW 757 SRM 53-00-51 FIG 10 1 DETAIL III REPLACED SUPPORT ANGLE PN 146N5300-77. V931851. REGUIRES SFRFeb 21, 2022 · N74856 · Boeing 757324SDR SWIA202265242None · corrodedCORROSION ON AFT WASTE WATER DRAIN MAST DOUBLER. (C-CHECK RO 3/30/2022) REMOVED AND REPLACED AFT WASTE WATER DRAIN MAST DOUBLER REF SRM 51-40-08. RESSTORED SURFACE PROTECTION REF SRM 51-23-06 AND CPM 51-25-00-901-001-AFeb 20, 2022 · N603CZ · Emb ERJ170200LRSDR R61A2022031000191Doubler · corrodedCNTR FUSELAGE III FLOOR STRUCTURE DOUBLER CORRODED AT FR 84, RBL12. R&R FLOOR DOUBLER AT FR 84, RBL12 IAW ERJ 175 SRM 51-41-01 AND 51-43-03.Feb 20, 2022 · N722YX · Emb ERJ170200LRSDR R61A2022031000190Beam · corrodedCNTR FUSELAGE III FLOOR STRUCTURE R/H BEAM CORRODED AT FR 87 PLUS 3, RBL 11. R&R FLOOR STRUCTURE AT R/H BEAM FR 87 PLUS 3 RBL11 IAW EMB 170 SRM 51-42-01 AND 54-43-01.Feb 20, 2022 · N722YX · Emb ERJ170200LRSDR R61A2022031000189Support Plate · corrodedCNTR FUSELAGE III FLOOR SUPPORT CORRODED AT FR89, RBL 38. R&R FLOOR SUPPORT AT FR 89, RBL 38 IAW ERJ 175 SRM 51-43-03, 51-42-01.Feb 20, 2022 · N722YX · Emb ERJ170200LRSDR R612022F00002Seat Track · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CENTER FUSELAGE III, AFT R/H SEAT TRACK IS CORRODED AT FR84, RBL 11. CENTER FUSELAGE III, CORRODED AFT R/H SEAT TRACK AT FR 84, RBL 11, REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-42-01 AND 51-43-02Feb 20, 2022 · N722YX · Emb ERJ170200LRSDR R612022F00001Doubler · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, FLOOR DOUBLER CORRODED AT FR 84, BL 12. CENTER FUSELAGE III, CORRODED FLOOR DOUBLER AT FR 84, RLB12, REMOVED AND REPLACED IAW EMBRAER 170/175 SRM 51-43-02.Feb 20, 2022 · N722YX · Emb ERJ170200LRSDR 2022F00060Damper · activeAFT LEFT SERVICE DOOR ASSIST PRESSURE LOW.Feb 20, 2022 · N193 · Airbus A300*SDR SWIA202265501None · corrodedMAIN AVIONICS BAY FS333.00 FRAME CORRODED BETWEEN STR 26L AND STR 25R (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW FS333.00 FROM STR 21L TO STR 20R, SPLICE REPAIR AND REINFORCING ANGLE SPLICE REF CRJ900 SRM 53-00-06-201-001-A03, CRJ900 SRM 51-42-06-Feb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265500None · corrodedMAIN AVIONICS BAY FS295.00 FRAME CORRODED BETWEEN STR 19L AND STR 20L (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED REPLACEMENT FS295.00 FRAME FROM STR18L TO STR20L REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31550 Feb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265499None · corrodedMAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED STR 22L FROM FS333.00 TO FS372.00 REF CRJ 900 SRM 53-00-03-201-001-A02, CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV-M. COMPLIED WITFeb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265498None · corrodedMAIN AVIONICS BAY STR 19L CLEAT AT FS295.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND REPLACED STR19L CLEAT AT FS295.00 REF. CRJ900 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020, AND DWG SH670-31550 REV G. COMPLIED WITH THE SKYWEST TASK CARD 51-9Feb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265497None · corrodedMAIN AVIONICS BAY STR 24L CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR24L SECTION FROM FS333.00 TO FS372.00 REF CRJ 900 SRM 53-00-03-201-001-A02, CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV-M. CFeb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265496None · corrodedMAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 23R FROM FS333.00 TO FS379.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG:SH690-31350 REV M. COMPLIED WITH TASK CARD 51-900-1002-SKY. LFeb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265495None · corrodedMAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED STINGER 21R FROM FS333.00 TO FS 379.00 REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV-M. COMPLIED WITH TASK CARD 51-900-1002-SKY.Feb 19, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265494None · corrodedMAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 4/25/2022) NO CORROSION DAMAGE NOTED FROM FS352.00 TO FS364.00 ON STR 24R. / REMOVED AND INSTALLED NEW STR 24R SECTION FROM FS333.00 TO FS352.00 AND NEW REPAIR REF CRJ900 SRM 5Feb 19, 2022 · N549CA · Cndair CL6002D24SDR R61A2022030800179Shear Panel · damagedSHEAR CLIP ON FRAME 89 BETWEEN STRINGERS 25R-27R HAS TOOLING DAMAGE. REMOVED AND REPLACED DAMAGED SHEAR CLIP ON FRAME 89 BETWEEN STRINGERS 25R-27R REF SRM 51-40-08.Feb 19, 2022 · Emb ERJ170200LRSDR R61A2022030800178Shear Panel · damagedSHEAR CLIP ON FRAME 89 BETWEEN STRINGERS 23R-25R HAS TOOLING DAMAGE. REMOVED AND REPLACED DAMAGED SHEAR CLIP ON FRAME 89 BETWEEN STRINGERS 23R-25R. REF SRM 51-40-08Feb 19, 2022 · Emb ERJ170200LRSDR CALA2022022100464Skin · damagedAIRCRAFR DAMAGE,LEFT SIDE, BELOW THE 14TH WINDOW, 7:00 POSITION, DAMAGE OUTER SKIN 10 INCH BY 4 INCH VERIFIED PER AVO 5900 PART A. STEPS 1 THRU 6. OK TO CONTINUE. PER AVO 5900 COMPLIED WITH PART A. STEPS 1 THRU 6. PER AVO9500 PART A STEP 7 HFEC CW ON CUTOUT RFeb 19, 2022 · N76062 · Boeing 767424ERSDR COEA2022032509801Floorbeam · corrodedWO 232458 NR 100012 HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 41 HAS LEVEL 2 CORROSION ON THE LOWER FLANGE, UPPER SURFACE. CORRECTIVE ACTION: REPLACED FLOORBEAM WITH NEW IAW SRM.Feb 18, 2022 · N801FX · Aerosp ATR72212SDR COEA2022032408801Floorbeam · corrodedWO 232458 NR 100017 HEAVY CHECK COE/MAJOR REPAIR: FRAME 33 FLOORBEAM HAS LEVEL 2 CORROSION BETWEEN THE LH SEAT TRACKS. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0155563_01...18727 ISSUE A, DATED 3/17/2022.Feb 18, 2022 · N801FX · Aerosp ATR72212SDR COEA2022032407801Stringer · corrodedWO 232458 NR 100044 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 15R FRAMES 39-40 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0155958_01...18752 ISSUE A, DATED 3/17/2022.Feb 18, 2022 · N801FX · Aerosp ATR72212SDR COEA2022032406801Stringer · corrodedWO 232458 NR 100027 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 17L HAS LEVEL 2 CORROSION FRAMES 35-36. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0155584_01...18751 ISSUE A, DATED 3/17/2022.Feb 18, 2022 · N801FX · Aerosp ATR72212SDR COEA2022032401801Angle · corrodedWO 232458 NR 100026 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 17L INTERCOSTAL CHORD ANGLE BETWEEN FRAMES 38-39 HAS LEVEL 2 CORROSION ON BOTTOM SURFACE OF FLANGE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0155768_01...18749 ISSUE A, DATED 3/17/2022.Feb 18, 2022 · N801FX · Aerosp ATR72212SDR CALA2022022100454Stringer · crackedAD 2019-11-02 SUPPORT TASK EA 5310-06900 OP4 REV D FUSELAGE BS 1035 R/H BUILT-UP UNDERWING LONGERON FOUND 1EA CRACK AT FIRST LAYER (COUNT FROM I/B) PLEASE PRINT AND ACCOMPLISHED EA 5310- 06900 OP 4 TRANSFER REF. NON-ROUTINE HX NRC WO.535988 AND ORIGINATED BY EFeb 18, 2022 · N78001 · Boeing 777224SDR CALA2022022100453Skin · damagedDAMAGE (HOLE) ON RT SIDE OF FUSELAGE, JUST AFT OF STATION 368, AND BETWEEN STRINGERS S-5 AND STRINGER S-6. DAMAGE MEASURES 5" X 2" TRANSFER REF HX WO 552872 AND ORIGINATED BY EMP V913166 AT INTERVALS NOT TO EXCEED 11400 PTC THEREAFTER... ACCOMPLISH INSPECTIONSFeb 18, 2022 · N669UA · Boeing 767322SDR CALA2022022100450Joint · corrodedA3NB-53-3-6105 FORWARD CARGO STRG 42R HAS CORROSION BETWEEN FR 3 3 AND FR 34. (DOT 38-82)() REMOVED AND INSTALLED SPLICE, STRG 42R BETWEEN FR33 AND FR34 IAW A320-200, SRM 51-42-11/001 AND APPLIED TREAT AND PRIME IAW A320 -200, SRM 51-21-11/001. ATTACHED 44-000Feb 18, 2022 · N433UA · Airbus A320232SDR SWIA202265492None · corrodedFWD CARGO FITTING AT FS565.00 BETWEEN STGR27 AND STGR26L IS CORRODED BEYOND LIMITS, REPLACEMENT REQUIRED (C-CHECK RO 4/25/2022) REMOVED AND REPLACED CARGO FITTING AT FS565 STGR 26L-27 REF. CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-Feb 17, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265491None · corrodedMAIN AVIONICS BAY FS349.00 FRAME CORRODED BETWEEN STR 26L AND STR 26R (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW FRAME SECTION FROM FS349.00 TO STR 23L TO STR 24R REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG: SH690-31350 REV-M. COMPLIED WITH TASK CFeb 17, 2022 · N549CA · Cndair CL6002D24SDR SWIA202265254None · elongatedRH AFT WINDSCREEN UPPER OUTBD FUSELAGE SUPPORT HAS ELONGATED HOLE FR 84-85 STR 5R (C-CHECK RO 3/30/2022) REMOVED AND REPLACED RH AFT WINDSCREEN UPPER OUTBD FUSELAGE SUPPORT FR 84-85 STR 5R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. Feb 17, 2022 · N603CZ · Emb ERJ170200LRSDR SWIA202265253None · elongatedRH AFT WINDSCREEN UPPER INBD FUSELAGE SUPPORT HAS ELONGATED HOLE FR 84-85 STR 2R (C-CHECK RO 3/30/2022) REMOVED AND REPLACED RH AFT WINDSCREEN UPPER INBD FUSELAGE SUPPORT REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.Feb 17, 2022 · N603CZ · Emb ERJ170200LRSDR SWIA202265252None · elongatedLH WINDSCREEN UPPER OUTBD FUSELAGE MOUNT BRACKET HAS ELONGATED HOLE (C-CHECK RO 3/30/2022) REMOVED AND REPLACED LH WINDSCREEN UPPER OUTBD FUSELAGE MOUNT BRACKET REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. APPLIED Feb 17, 2022 · N603CZ · Emb ERJ170200LRSDR 2022F00062None · noneFADEC CRTL DEGRADED. FADEC NO DISPATCH.Feb 17, 2022 · N26VJ · Cirrus SF50SDR JR2R20220217919Plate · damagedWASTE BOX UPPER PLATE HAS DOUBLE DRILLED HOLE ON FWD SIDEFeb 17, 2022 · N922FJ · Cndair CL6002D24SDR JJBA20220216019Not Reported · not reportedCORROSION ON THE OMEGA BEAM AT MULTIPLE PLACES FROM FRAME 22 TO 31 STRINGER 19R Y = 479.0. REMOVED AND REPLACED OMEGA BEAM FROM FR22 - FR31Feb 16, 2022 · N11199 · Emb EMB145XRSDR JJBA20220216012Not Reported · not reportedSIGNS OF CORROSION AT MULTIPLE LOCATIONS ON GUSSET OF OMEGA BEAM Y=0 FROM FR61 TO FR71. REMOVED AND REPLACED GUSSET OF OMEGA BEAM Y=0 FROM FR61 TO FR71Feb 16, 2022 · N13202 · Emb EMB145XRSDR JJBA20220216011Not Reported · not reportedPOSSIBLE CORROSION LAV CARGO LATERAL FLOOR SUPPORT FR 59-61+4 STR 17L OMEGA BEAM Y=479 GUSSET. REMOVED DAMAGE D GUSSET AND INSTALLED NEW GUSSET.Feb 16, 2022 · N13202 · Emb EMB145XR
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