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 CALA2024081202190Fitting · crackedR/H AND L/H CONTINUITY FITTING CRACKEDPER HAECO LCQ N/R 9298153 /20153 GEN BY V934190 RMVD AND RPLD RH/LH CONTINUITY FITTINGS PER UNITED EC/RA 5311- 03248 AND AIRBUS DWG R53112919 ISSUE J BY MECH V075077 INSP BY V892442SDR DALA2024080907964Window Frame · cracked(LOG 0491404) FUSELAGE OPENING FRAME RH NO. 1 WINDOW FRAME UPPER CORNER CRACKED. REPAIRED PER ERA 619752-14AD.SDR DALA2024080907963Window Frame · corroded(LOG 0491395) CO-PILOT WINDOW FRAME #1 IS CRACKED IN UPPER O/B CORNER. REPAIRED PER ERA 619752-14.SDR DALA2024080907954Window Post · cracked(LOG 0491276) CAPTAIN'S #1 WINDOW O/B WINDOW POST HAS EVIDENCE OF CRACK. REMOVED DAMAGE AND REPAIRED #1 L/H WINDOW POST (CAPTAINS) PER ERA 618877-14AD REV ORIGINAL.SDR YENA2024080801100Beam · corrodedDURING HEAVY MAINTENANCE: AFTER OF AFT CARGO SEAL RESTS REMOVAL IN REF TO NRC 077, WAS FOUND CORROSION ON LOWER BEAM BTW FR77/80 AT AFT CA- RGO COMPARTMENT; REF TOMEX WO 2592, NR 00249, CORROSION ON LOWER BEAM BTW FR77/80 AT AFT CAR- GO COMPARTMENT WAS REMOVEDSDR IXXA2024080810Roller Tray · crackedALC ROLLER TRAY STA 1197-1263 LBL21-LBL23 CRACK AT END OF TRAYSDR KCSA202408081095Frame · corrodedMAIN DECK R/H FRAME EVIDENCE OF CORROSION STA 520 APPROX S-22 THROUGH S-26 LOCATION.SDR AALA202411203812Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD LEFT PASSENGER / CREW DOOR CUTOUT UPPER CORNER FRAME FASTENER HOLE AT FR 16 BETWEEN S7L AND S13L. REPAIRED FRAME PER EA 357795.SDR K11A2024090500282Door Frame · crackedFOUND CRACK INDICATION AT L-1 DOOR S-16 DOOR STOP LOWER FASTENER ROW MIDDLE HOLE.SDR REXA2024082700670Door Frame · crackedRH AFT OVERWING EXIT DOOR UPPER FORMER CRACKED AT AFT LUG REPAIRED IAW ENDEAVOR EA CRJ952-17122 REV.IR DATED 8/14/2024.SDR REXA2024082700669Door Frame · crackedLH FORWARD OVERWING EXIT DOOR UPPER FORMER CRACKED AT AFT LUG REPAIRED IAW ENDEAVOR EA CRJ952-17121 REV.IR DATED 8/14/2024.SDR VNAA202408070011Post · crackedRH WINDSHIELD SIDE POST IS CRACKED AT THE TOP. REMOVED AND REPLACED RH WINDSHIELD SIDE POST IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01."SDR DALA2024080907929Door Frame · corroded(LOG 0489058) CORROSION ON E&E BAY ACCESS DOOR SURROUND STRUCTURE LOWER CHORD AT STA 360 LBL 6. REMOVED DAMAGE AND REPAIRED E&E BAY ACCESS DOOR SURROUND STRUCTURE LOWER CHORD @STA. 360, LBL 6 PER ER/A 619503-14 REV ORIGINAL.SDR DALA2024080807913Window Frame · cracked(LOG 0489492) UPPER LH CORNER OF THE LH FLIGHT DECK WINDOW FRAME CRACKED. REPAIRED PER ERA 618877-14.SDR SWAA2024090523306Bear Strap · crackedCRACKED BEAR STRAP AT R1 DOOR JUST ABOVE SEAL DEPRESSOR; 3' BELOW FWD UPPER STOP FITTING. MARKED CORRECTION: CRACK FOUND ON FSD STUB FRAME.<[01] REMOVED AND REPLACED FWD SERVICE DOOR FWD UPPER STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG#141A8370 REV-C;[02] VERIFISDR SWAA2024082823152Beam · crackedR/H AC BAY LWR T CHORD CRACKED AT STA 663 RBL 42.<[01] DUPLICATE DISCREPANCY. SEE FAULT TTG8Q00V12TU FOR CHORD REPLACEMENT. MPM 52.02.05SDR DALA2024081107975Window Frame · crackedSHIP 3275 DISC: CRACK INDICATION FOUND ON WINDSHIELD FRAME LOWER CENTER POST RH SIDE, COCKPITS CRACK LENGTH IS 0.251 INCH. (AD 2020-17-03 /WORK CARD 5311-01 226-01. REQUESTING REPAIR DISPOSITION.REPAIR MUST BE ACCOMPLISHED PRIO R TO FURTHER FLIGHT). C/A: COMPLSDR DALA2024080807907Door Frame · corroded(LOG 0487699) UPON INSPECTION, CORROSION WAS DISCOVERED ON THE UPPER (INNER) SURFACE OF THE E&E BAY ACCESS DOOR SURROUND STRUCTURE CHORD AT BS 360, LBL 6. CORROSION REPAIRED PER ERA 619503-14.SDR JR2R20240806118Seal Rest · corrodedAFT CARGO DOOR LOWER SEAL DEPRESSOR LOWER LANDINGS CORRODED IN MULTIPLE PLACES. REPLACEDSDR SWAA2024082822842Beam · crackedRH LOWER BEAM CHORD RBL 40.875 CRACKED AT AFT ANGLE RADIUS AT STA 658 APPROX 0.60'<[01] LOCATED; DRILLED AND DEBURRED REPLACEMENT CHORD PER SRM 51-40-05.;[02] INSTALLED NEW NUT PLATES ON REPLACEMENT CHORD PER SRM 51-40-02.;[03] VERIFIED C/A #1 AND #2.;[04] REMSDR IPXA2024090690022Access Panel · corrodedWHEEL WELL, FRAME ACCESS PANEL 148ZC CORRODED. DOT 28-97. RO-28. INSTALLED PANEL ASSY P/N: A2551030700701, BATCH: 0004319687, IAW SRM 51-40-21 AT ZONE 100, WHEEL WELL RH SIDE. USED HARDWARE: NSA55184-1 (WASHER RETAINING), NSA55182-1B (GROMMET), NSA55181-22 (STSDR CALA2024080602170Deck Plate · damagedFLIGHT DECK FLOOR SKIN CREASE AT STA 259.5-5" LBL 3" REF AAR N/R 9893159 ACCOMPLISHED FLIGHT DECK FLOOR REPAIR AT STA 259.5IN AND LBL 3IN REF SRM 53-10-51-2R-2, FIG 203.SDR AALA202408054353Door Frame · damagedAIRCRAFT WAS GROUNDED: RAMP REPORTS DAMAGE TO EXTERNAL POWER ACCESS DOOR FRAME. ACCOMPLISHED PERMANENT REPAIR. PER SRM 53-10-15-2R.SDR CALA2024080502154Guide Fitting · damaged737-900ER LH MID CABIN DOOR PLUG, DOOR FRAME STRUCTURE AND UPPER GUIDE FITTINGS - INSPECTION - LH MID CABIN DOOR PLUG, UPPER AFT GUIDE TRACK FITTING IS CRACKED. REMOVED AND REPLACED L/H MID CABIN DOOR PLUG UPPER AFT GUIDE OPENED L/H MID CABIN EXIT DOOR PLUG FSDR CALA2024080502161Guide Fitting · cracked737-900ER LH MID CABIN DOOR PLUG, DOOR FRAME STRUCTURE AND UPPER GUIDE FITTINGS - INSPECTION - LH MID CABIN DOOR PLUG, UPPER AFT GUIDE TRACK FITTING IS CRACKED. REMOVED AND REPLACED L/H MID CABIN DOOR PLUG UPPER AFT GUIDE OPENED L/H MID CABIN EXIT DOOR PLUG FSDR SWAA2024091022950Panel · corrodedP15 REFUEL PANEL FACEPLATE HAS MULTIPLE CORROSION SPOTS<[01] REMOVED AND REPLACED P15 REFUEL PANEL FACE PLATE I/A/W BOEING AMM 28-21-00-000-801 & 28-21-00-400-801; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1SDR AALA2024081509386Splice · damagedAIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA LOWER OUTBOARD SPLICE HAS ELONGATED HOLE AT FR 64 AND +Y765. REPLACED SPLICE PER SRM 51-72-11.SDR SWAA2024080922095Drain Mast · corrodedINTERGRANULAR CORROSION ON AFT DRAIN MAST APPROX. STA 1000 BETWEEN S-24L & 25L<[01] C/W EA 24-153-02124;[02] VERIFIED REPAIR PER EA 24-153-02124-WIP1 TTG8Q00V07QE; EA 24-153-02124-WIP2 TTG8Q00V0QTW AND EA 24-153-02124 FINAL TTG8Q00V18WP.SDR DALA2024080807915Window Frame · cracked(LOG 6210954) R3 WINDOW FRAME CRACKED. PERMANENT REPAIR TO BE COMPLETED PER ERA 619933-14.SDR JR2R20240803190Beam · corrodedAFT CARGO DOOR SURROUND STRUCTURE LOWER BEAM CORRODED. REPLACEDSDR JR2R20240803126Seal Rest · corrodedFWD CARGO DOOR LOWER SEAL DEPRESSOR LOWER LANDING CORRODED. REPLACEDSDR IPXA2024082267447Door Frame · scratchedCREW DOOR FRAME, UPPER EXTERNAL SURFACE WITH SCRATCHES. PRIMED & PAINTED AT Z831, CREW DOOR FRAME, UPPER EXTERNAL SURFACE. IAW 51-21-10 USING 4OZ PRIMER 02-013-8, BATCH # 4263188 AND WHITE PAINT PG6-W2K4Q, BATCH #415963, CUP #02-012-176.SDR IPXA2024081367429Door Frame · damaged**SDR FILED OPEN**FAULT - STR - Z831 - CREW DOOR, UPPER INTERNAL SURFACE WITH SCRATCHES. DOT 73-049. (MOYA-73) APPROVED.SDR IPXA2024081367447Door Frame · damaged**SDR FILED OPEN**FAULT - STR - Z831 - CREW DOOR FRAME, UPPER EXTERNAL SURFACE WITH SCRATCHES. DOT 73-050 (MOYA-73) APPROVED.SDR IPXA2024080566971Door Frame · gougedCREW DOOR CUTOUT, AFT MID AREA WITH GOUGE. DOT 73-045 (MOYA-73) APPROVED.SDR CALA2024080502153Crease Beam · corrodedB737-53-3-0736: MAIN CABIN R/H SIDE CREASE BEAM INNER CHORD UPPER SURFACE IS CORRODED BETWEEN STA 787 AND 807. TRANSCRIBED FROM HAECO GSO NRC 9288511. REPAIRED CREASE BE33AM INNER CHORD FORM STA 787 TO STA 867 IAW UAL EC/RA 5360-01845 REV-. HAECO GSO MECH V8SDR AALA202410289648Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE FASTENER HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 357058SDR SWAA2024082821316Shield · corrodedFORWARD CARGO DOOR CUTOUT; AFT SHIELD (SIDEPATE) STA. 492-500A HAS CORROSION AT NUTPLATE HOLES.<[01] REMOVED CORROSION PER SRM.51-10-02 ; (MATERIAL REMOVED 0.040 ) FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1 ; REMOVED AND REPLACED PART #143A8126Y38ATSMRO PSDR YENA2024080601079Window Post · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTRAL LOWER NODE LH SIDE. CRACK LENGTH 0.5 IN AND DIRECTION 5 OCLOCK; (RESOLVED ON W/O: 1275940 TASKCARD: NR-00054) PERFORMED REPAIR AT WINDSHIELD CENTRAL LOWER NODE LH SIDE UAW EC NO. A24-909-01SDR YENA2024080601078Window Post · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTRAL LOWER NODE RH SIDE. CRACK LENGTH 0.125 INCH AND DIRECTION 7 OCLOCK; (RESOLVED ON W/O: 1275940 TASKCARD: NR-00055) PERFORMED REPAIR AT WINDSHIELD CENTRAL LOWER NODE RH SIDE IAW EC NO. A24-90SDR YENA2024080601073Post · crackedDURING CURRENT CHECK, AEM REPORTED CRACKS ON THE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT ON BOTH SIDES OF AREAS C & D. DAMAGE REMOVED BY FOLLOWING CRACK ASSESSMENT GUIDELINES, REF /3/, FOR BOTH AREAS. AIRBUS WAS CONTACTED FOR ASSESSMENT AND DETERMINESDR DALA2024080507775Beam · corroded(LOG 0479206) CORROSION ON BEAM STA 294.3 RBL 14 AT W1. BEAM STA 294.3 RBL 14 AT W1. WAS REPAIRED PER B737-800 SRM 53-10-51-2R.SDR CALA2024080502155Window Frame · crackedAFTER NDT INSPECTION PER EA 5310-04554 REV C OP 007 CRACKS FOUND AT LH #1 WINDOW FRAME (REF: AAR NR 100013256) ECRA 5610-01552. DIP PER ABOVE REQUIREMENTS, NOTE: AIRCRAFT CURRENTLY HAS 15458 TC (49900-15458 = 34442) (50000- 15458 = 34542) WORK PERFORMED IAW EASDR AALA202408017405Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR (ZONE 841) BEAM FROM STA 311 TO STA 345. REPLACED BEAM PER 52-10-02-01 PROCEDURE 1 AND CMM 52-41-05.SDR DALA2024080107692Pintle Pin · gougedSHIP 3309 L/H MLG WHEEL WELL. 3EA GOUGES FOUND AT REAR PINTLE PIN FITTING BETWEEN THE FORWARD AND AFT LUG. CORRECTIVE ACTION: REPAIRED PER A330 SRM 57-26-13. (0478048)SDR DALA2024080107691Support Rib · gougedSHIP 3309 R/H MLG WHEEL WELL. GOUGE FOUND ON GEAR SUPPORT RIB 6, AT REAR PINTLE-PIN FITTING ON FORWARD LUG, AFT FACE. CORRECTIVE ACTION: REPAIRED PER A330 SRM 57-26-13. (0478044)SDR DALA2024080107690Support Rib · gougedSHIP 3309 R/H MLG WHEEL WELL. GOUGE FOUND ON GEAR SUPPORT RIB 6, AT REAR PINTLE-PIN FITTING BETWEEN THE FORWARD AND AFT LUG. CORRECTIVE ACTION: REPAIRED PER A330 SRM 57-26-13. (0478047)SDR IXXA2024080102Roller Tray · corrodedROLLER TRAY CORRODEDSDR SWAA2024090920673Angle · crackedCRACK BRACKET ANGLE LOCATED UPPER FUSELAGE AT STA 1016 AT VERTICAL STABILIZER 2024-473131<[01] REPLACED BRACKET ANGLE AND FASTENERS LOCATED UPPER FUSELAGE AT STA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 176A7101; SHEETSDR DALA2024080107696Door Frame · crackedSHIP 3170 FUSELAGE FRAME/FORMERS FR16 RH AT DOOR STOP 7 LEVEL DOUBLE JOGGLE AREA HOLES #7, #8 & #B CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 593334-14AD. (0476505)
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