JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 YENA2023112901476Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT POCKET LH SIDE, LOWER INBOARD RADIUS, CRACK LENGTH IS 0.170 INCH APPROX, IN COCKPIT (1 EA); ACCOMPLISHED THE REPAIR OF THE CRACKS FOUND AT THE WINDSHIELD FRAME SDR YENA2023112901475Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT (1 EA); REF AEROMAN NR 2023-556993 WO 2023 275/1, ACCOMPLISHED THE REPAIR OF THE CSDR YENA2023112901465Pressure Panel · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LH & RH SIDES / PRESSURE PANEL ATTACHMENT HOLES / SB A320-53-1263 ACCOMPLISHMENT AND CRACK DAMAGE. PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023112901464Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER ATTACHMENT AREA AND CONTINUITY FITTING / CRACKS - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR AALA202403123297Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST LOWER ATTACHMENT UPPER RADIUS BETWEEN FR 1 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 349770.SDR AALA202403085318Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK RIGHT HAND LATERAL POST WINDSHIELD FRAME LOWER ATTACHMENT BETWEEN FR 1 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 349770.SDR AALA202403053246Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CONTINUITY FITTING LOWER ATTACHMENT AREA ON THE LEFT-HAND SIDE. PERFORMED TIME REPAIR (REPLACED CONTINUITY FITTING LEFT-HAND SIDE LOCATED BETWEEN FR 1 TO FR 2 AND LEVEL OF Y0 PER EA 349770SDR AALA202403054362Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CONTINUITY FITTING LOWER ATTACHMENT AREA RIGHT-HAND SIDE. PERFORMED TIME LIMITED REPAIR (REPLACED CONTINUITY FITTING) RIGHT-HAND SIDE LOCATED BETWEEN FR 1 TO FR 2 AND LEVEL OF Y0 IAW EA349770SDR SIMA202312184001Seal Rest · corrodedSSI 53-21-009 ? FWD CARGO DOOR CUTOUT LOWER AFT CORNER SEAL DEPRESSOR CORRODED (LEVEL 2 CORROSION). -C/A-REMOVED AND REPLACED FWD CARGO DOOR CUTOUT LOWER AFT CORNER SEAL DEPRESSOR IAW EMB 170 SRM 51-40-02. SSI 53-21-009 ? FWD CARGO DOOR CUTOUT LOWER AFT CORNERSDR DALA2023112709708Unknown · unknown(LOG 0080246) WINDOWS / FLIGHT COMPARTMENT / RH NO. 1, NO. 2 AND NO. 3 WINDOW FRAME FWD UPPER CORNER HAS CORROSION. REPAIRED PER ERA 611542-14.SDR AALA202312123763Pressure Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE PLATE FASTENER HOLE BETWEEN FR 42 AND FR 43 AT S24R. REPLACED PRESSURE PLATE PER SRM 51-42-11.SDR DALA2023112709721Unknown · unknownCRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00706: CRACK ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT INNER SKIN WAS REPAIRED PER ER/A 613654-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6SDR DALA2023112409674Unknown · unknownSHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563226-14AD. (0078980)SDR DALA2023112409673Unknown · unknownSHIP 3119 CRACK HAS BEEN NOTICED IN UPPER AREA OF FR20 LHS, EXISTING REPAIR ON HOLE 5. CORRECTIVE ACTION: REPAIRED PER ER/A 563224-14AD. (0078904)SDR DALA2023112409670Unknown · unknownSHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079068)SDR DALA2023112409669Unknown · unknownSHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA FROM UPPER TENSION BOLT, RH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079050)SDR DALA2023112409668Unknown · unknownSHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, FROM UPPER TENSION BOLT, LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079046)SDR HNAA2023122800510Unknown · unknown53-2077 CORROSION ON BAG DOOR LOWER CUT-OUT LOWER BEAMSDR SWAA2023122124234Door Frame · crackedMAIN CABIN LH STA 303.9 INNER CHORD CRACK<[01] REMOVED AND REPLACED INNER CHORD AT MAIN CABIN L1 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1SDR SWAA2023122124236Intercostal · crackedMAIN CABIN BL 0' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND BOEING AIRCRAFT DWG # 143A5400.;[02] VERIFIED STEP 1SDR SWAA2023122124458Support Angle · corrodedMAIN CABIN FWD WET AREA INNER CHORD SUPPORT ANGLE LBL 60' BETWEEN STA 294.5-328 UPPER SURFACE CORROSION<[01] REMOVED AND REPLACED SUPPORT ANGLE AT MAIN CABIN FWD WET AREA INNER CHORD LBL 60' BETWEEN STA 309 TO 343 SRM 51-40-02-0G-0 AND DWG141A8110;[02] VERIFIESDR CALA2023112703485Door Frame · crackedLT AFT EMERGENCY EXIT HATCH CRACKED. REMOVED AND REPLACED FWD FRAME SEGMENT ON L/H AFT EMERGENCY HATC H IAW A320 SRM 51-72-11-911-001.SDR JAPA2023112200771Deck Plate · crackedCRACK IN THE BOTTOM ENGINE DECK WHERE THE AIR-CONDITIONING LINES COME THROUGH. REPAIR MADE WITH BELL DATA.SDR HNAA2023121900487Unknown · unknownE010216 ACCOMPLISH FCD1-53-23-0180, FUSELAGE WINDOW PILLAR REINFORCMENT. ACCOMPLISHED PIEDMONT AIRLINES FCD1-53-23-0180SDR MASA20231127006Window Frame · damagedCAPTAIN SIDE WINDSHIELD FRAME DAMAGED FURING NUTPLATE REPAIR. LH COCKPIT WINDSHIELD FRAME 3 MISDRILLED RIVET HOLES AND SCRATCHED. REPAIRED PER RO# E175-53-4577.SDR DU4R202311010056Pressure Panel · corrodedCOMPLY WITH SB A319-53-1263 COL WORKING OF ATTACHMENT HOLES ON THE PRESSURE PANEL.SDR UIEA2023112000962Unknown · unknownCORROSION - FOUND LH BLG INBD LWR BEARINGS CAP CORROSION(<P>1) REMOVED THE CORROSTION AREA IAW SRM 53-40-90-2R-1 REV 56. 2) REPAIR CORROSION DAMAGES ON THE CAP FITTING IAW EI T2023A32M-3095 REV 1. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023112000963Unknown · unknownCORROSION - FOUND RH BLG INBD LWR BEARING CAP CORROSION(<P>1) REMOVED THE CORROSION AREA IAW SRM 53-40-90-2R-1 REV 56. 2) REPAIR CORROSION DAMAGED ON THE CAP FITTING IAW EI T2023A32M-3095 REV 1 & EI ATTACHED TO W/O 8888188. 3) CONDITION CHECK NORMAL AND JOB COSDR SIMA20231120001Crossbeam · corrodedCTR FUSELAGE 3 CROSSBEAM AT FR84 HAS CORROSION ON LH SIDE (LEVEL 2 CORROSION) (MAJOR REPAIR).-C/A-PERFORMED REPAIR OF CTR FUSELAGE 3 CROSSBEAM AT FR 84 IAW ENVOY ERS-EJ-53MR-4904SDR YENA2023112201450Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CORROSION IN CROSS BEAM AND SPLICE LOCATED BETWEEN Y= -300.0/+300.0 AND FR 11 AT COCKPIT FLOOR STRUCTURE; (RESOLVED ON W/O: 1269682 TASKCARD: NR-00008 ) REF TOMX WO 2384 NR 00136: CORROSION IN CROSS BEAM AND SPLICESDR DALA2023112009551Unknown · unknownSHIP 3119 FR35 PRESSURE BH ATTACHMENTS A CRACK 2.0" LONG WAS FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7 IN LHS FR35 BH AT LEVEL OF STR30. CORRECTIVE ACTION: COMPLIED WITH ERA 612601-31. (0073402)SDR SWI2024F00024Lintel · wornPASSENGER DOOR SURROUND LINTEL HAS WORN AREA (C-CHECK RO 1/24/2024) REMOVED WORN AREA ON THE PAX DOOR SURROUND LINTEL AND FOUND OUT OF LIMITS PER CRJ700SRM 53-21-23-101-001-A01. RECEIVED AND COMPLIED WITH REO 670-53-21-2345 REV -- DATED 2023-12-01 BY REMOVSDR SIMA2024010318001Skin Panel · dentedFUSELAGE SKIN DENT BTW FR 1-2 AND STR 6R-18R.*(MAJOR REPAIR) -C/A-ACCOMPLISHED PERMANENT REPAIR OF FUSELAGE SKIN DENT BTW FR 1-2 AND STGR 17R-18R IAW ERS-EJ-53MR-4933.SDR WX0A1900010031903Unknown · unknown(MAJOR REPAIR) CORROSION FOUND ON BULK CARGO LOWER SILL BEAM FASTENER HOLES / ON BULK CARGO LOWER SILL BEAM, FASTENERS HOLES PERMANENTLY REPAIRED AS PER SRM 53-41-49-300-003 REV. 146, REPAIR CATEGORY B, WITH REPEAT INSPECTION REQUIREMENT LISTED SRI53-41-49-205SDR DALA2023112009550Unknown · unknownSHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071632)SDR DALA2023112009549Unknown · unknownSHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071624)SDR DALA2023112009548Unknown · unknownSHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071606)SDR IXXA20231118001Failsafe · corrodedCORROSION ON FAILSAFE STRAP IN FLC DOOR CUTOUTSDR F3LA2023120100219Door Seal · corrodedDISCREPANCY: REFERENCE NR 5001278732-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH DOOR SILL BEAM NUT PLATE HOLE ALONG FRAME 68 REQUIRES REPAIR AS PER A320 NEO SRM TASK 53-41-15-300-001 REV. 38. REPAIRED LH DOOR SILL BEAM SDR R61A2023112700648Seal Rest · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO DOOR SURROUND, FWD SEAL REST CORRODED FR24 STR25L. REPLACED CARGO DOOR SURROUND FWD CARGO SEAL REST IAW AMM 20-10-01.SDR DU4R2023110052Pressure Panel · crackedDURING INSPECTION AT HAECO LAKE CITY, FLORIDA THE R/H FR 35-36 PRESSURE PANEL HOLE # 26 WAS FOUND CRACKED AT THE 12 O'CLOCK POSITION IN THE PRESSURE DECK PANEL.SDR DU4R2023110051Pressure Panel · crackedDURING INSPECTION AT HAECO LAKE CITY, FLORIDA THE R/H FR 35-36 PRESSURE PANEL HOLE # 23 WAS FOUND CRACKED AT THE 5 O'CLOCK POSITION IN THE PRESSURE DECK PANEL.SDR DU4R2023110050Pressure Panel · crackedDURING INSPECTION AT HAECO LAKE CITY, FLORIDA THE R/H FR 35-36 PRESSURE PANEL HOLE # 22 WAS FOUND CRACKED AT THE 11 O'CLOCK POSITION IN THE PRESSURE DECK PANEL.SDR DU4R2023110049Pressure Panel · crackedDURING INSPECTION AT HAECO LAKE CITY, FLORIDA THE R/H FR 35-36 PRESSURE PANEL HOLE # 20 WAS FOUND CRACKED AT THE 5 O'CLOCK POSITION IN THE PRESSURE DECK PANEL.SDR DU4R2023110048Pressure Panel · crackedDURING INSPECTION AT HAECO LAKE CITY, FLORIDA THE R/H 35-36 PRESSURE PANEL HOLE # 7 WAS FOUND CRACKED AT THE 5 O'CLOCK POSITION IN THE FITTING.SDR DU4R2023110047Pressure Panel · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H FR 35 - 36 PRESSURE PANEL HOLE # 6 IS CRACKED AT THE 12 O'CLOCK POSITION IN THE FITTING.SDR HNAA2023112000421Unknown · unknownBIRD STRIKE TO NOSE AND R/H FUSELAGE. CLEANED AREA AND INSPECTED A/C IAW AMM 05-50-08. FOUND 2 DENTS ON FUSELAGE AND RADOME LATCH DAMAGED. REPAIRED DENTS IAW EO1-53-23-0396. R&R'D LATCH IAW AMM 53-11-01-820-801-ASDR JR2R20231118148Beam · corrodedRH AFT LONG BEAM CORRODED BETWEEN FR87 AND FR88 AT RBL11. FOUND TO BE OUT OF LIMITS. REPAIRED BEAMSDR SWIA2024012631116Window Post · cracked* CO-PILOT'S WINDSHIELD SIDE POST, LOWER ANGLE BELOW BOTTOM OF WINDSHIELD SILL IS CRACKED, MARKED. (C-CHECK RO 1/24/2024) INSTALLED NEW FRAME SECTION P/N 601R34032-22. REF: CRJ200 SRM 51-42-06 AND DWG 601R34032, REV: V. NO LEAKS NOTED. COMPLIED WITH TASK CSDR SWAA2023121221908Pressure Deck · crackedRH HORIZONTAL PRESSURE DECK HAS TWO CRACKS. 1) BS 664.5 RBL 40.5 WL 202 AND 2) BS 672.5 RBL 41.5 WL 202. FOUND ON HFEC INSPECTION.<[01] REPAIRED R/H BEADED PRESSURE DECK WEB BETWEEN STA 663.75 AND STA 675 RBL 30 TO RBL 62 PER SRM 53-40-51-2R-2 REPAIR 2 FIG. 20
Back to JASC 5310