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 DALA2023090707328Unknown · unknown(LOG 2954285) CAPTAINS UPPER O/B CORNER OF WINDOW FRAME IS CRACKED. REPAIRED PER PRI 611573-14 REV 1 AND ER/A 611573-14 REV ORIGINAL.SDR DALA2023090707329Failsafe · corroded(LOG 2954806) CORROSION AT AFT CARGO COMPARTMENT DOOR SURROUND FAIL SAFE STRAP AT STA 794 APPROX RBL 25 WL 159. C/W ER/A 610890-14 REV ORIGINAL.SDR CALA2023090502709Frame · crackedUPON REMOVAL OF R2 DOOR SILL FR 67 FRAME SEGMENT (STRAP) WAS FOUND TO HAVE CRACK ON UPPER I/B REDIUS. GEN BY V061616 ON HAECO LC Q NR 9290815/40815 REMOVED AND REPLACED FRAME SEGMENT STRAP AT FRAME 67 IAW A319 SR M 51-72-11 P 1&2 ACMP BY V052030 INSP BY V07988SDR DALA2023090407172Unknown · unknownSHIP 3126 CRACK INDICATION FOUND ON LH CONTINUITY FITTING LOCATED ON WINDSHIELD CENTER LOWER NODE AT FR 2. CORRECTIVE ACTION: COMPLIED WITH ER/A 610569-14AD. (2951315)SDR DALA2023090407171Unknown · unknownSHIP 3126 CRACK INDICATION FOUND ON RH CONTINUITY FITTING LOCATED ON WINDSHIELD CENTER LOWER NODE AT FR 2. CORRECTIVE ACTION: COMPLIED WITH ER/A 610569-14AD. (2951293)SDR AALA202312060565Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND SIDE WINDSHIELD FRAME UPPER RADIUS AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 347848.SDR AALA202312068664Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLIGHT DECK WINDSHIELD CENTER POST RIGHT HAND SIDE WINDSHIELD FRAME UPPER RADIUS AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 347848.SDR AALA202311249598Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347848.SDR AALA202311243615Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347848SDR SWAA2023100596757Pressure Deck · debondedLEFT HAND PRESSURE DECK WEB (P/N144A7732-3) IS DISBONDED.<[01] DRILLED PRESSURE FLOOR WEB P/N: 654A0004-1743 IAW BOEING B737 SRM 51-40-05-0G-0 AND DWG 144A7730 REV. A.;[02] REMOVED AND REPLACED WEB ON SHELF IAW DWG 144A7730 REV. A;[03] VERIFIED STEPS 1 & 2;[04SDR AALA202309065377Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB LOCATED AT BS 663 AND RBL 31.83. REPAIRED WEB PER SRM 57-10-10-2R-3.SDR JR2R20230902585Doubler · corrodedDOUBLER AT FR89 RBL11 CORRODEDSDR JR2R20230902583Doubler · corrodedDOUBLER IN THE CENTER OF FR90 CORRODEDSDR JR2R202309020884Floor Support · corrodedFLOOR SUPPORT FITTING AT FR84 RBL13 CORRODEDSDR AALA202311079998Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347841.SDR AALA202311076502Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST UPPER RADIUS AREA AT FR 2 AND Y0. REPAIRED FRAME PER EA 347841.SDR AALA202311072992Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST UPPER TENSION BOLT AREA AT FR 2 AND Y0. REPAIRED FRAME PER EA 347841.SDR IPXA2023092894281Doubler · dentedINSPECTION TYPE:1C*MAJOR REPAIR* RH FUSELAGE DENT AT FRAME 11 3 O'CLOCK POSITION.WORKED PER UPS RCD 297600SDR AALA202311014270Stop Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED #1 DOOR STOP INBOARD LOWER FASTENER HOLE AT FR 68 AND S22R. REPAIRED DOR STOP PER SRM 53-41-12-300-011.SDR CALA2023090402680Window Frame · crackedWINDSHIELD LH AND RH CONTINUITY FITTINGS HAVE CRACK INDICATION A PPROX.. 400 INCH OUT FROM CENTER POST. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" (AD RELEATED SUPPORT TAS K (AD 2020-17-03) GENERATED AT HAECO LCQ PER NR 9296319(20319) A NSDR DALA2023090107154Unknown · unknown(LOG 2944766) WHILE OVERNIGHT IN MIA, THE AIRCRAFT EXPERIENCED GROUND DAMAGE RESULTING IN A DENT AND GOUGE DAMAGE COMMON TO THE FWD CARGO DOOR SURROUND SKIN, (P/N: 143A3232-7), BEARSTRAP (143A3254-2), EXISTING REPAIR, AND BULLNOSE CHORD. MAINTENANCE REPAIRED DSDR YENA2023090101015Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE CROSS BEAM X=3301.3 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR SWI2023F00454Unknown · dentedFLIGHT COMPARTMENT FLOOR DENTED/GOUGED BETWEEN COPILOT SEAT TRACKS (C-CHECK RO 11/4/2023) REPAIRED FLIGHT COMPARTMENT FLOOR BETWEEN COPILOT SEAT TRACKS IAW REO 670-53-11-1881 REV. -- DATED 2023-09-08 STEPS 1 THROUGH 11. COMPLIED WITH TASK CARD 51-900-1002-SDR SWAA2023092694709Pressure Deck · crackedHORIZONTAL PRESSURE DECK CRACKED BS664.5; WL 202; LBL52 APPROX 1 INCH IN LENGTH. MARKED WITH BLACK SHARPIE.<[01] REPAIRED HORIZONTAL BEADED PRESSURE DECK WEB BETWEEN STA 663.75 TO 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2. FIG. 203.;[02] VERIFIED CORRECTIVE ASDR DALA2023090107141Unknown · unknown(LOG 4643646) CAPT UPPER RT CORNER OF WINDOW CRACKED. MAINTENANCE REPAIRED PER ERA 611575-14.SDR DU4R202308310030Fitting · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AD RELATED TASK, EASA AD 2020-0005, RIGHT WINDSHIELD FRAME, LOWER CENTER POST, CONTINUNITY FITTING HAS A CRACK INDICATION AT 1.125 INCH FROM THE LEFT OF CENTER. S/O 339001 N/R 28420SDR DU4R202308310029Fitting · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AD RELATED TASK, EASA AD 2020-0005, LEFT WINDSHIELD FRAME, LOWER CENTER POST, CONTINUNITY FITTING HAS A CRACK INDICATION AT 1.125 INCH FROM THE LEFT OF CENTER. S/O 339001 N/R 28419SDR DALA2023083107105Unknown · unknown(LOG 2941011) L/H AFT FIXED WINDOW FRAME CRACKED ON FWD SIDE LOWER CORNER #3 WINDOW. MAINTENANCE REPAIRED PER ERA 611576-14.SDR DALA2023083107104Unknown · unknown(LOG 2940944) WHILE CLEANING FLIGHT DECK WINDOWS CRACK F/O'S WINDOW UPPER RIGHT CORNER. MAINTENANCE REPAIRED PER ERA 611576-14.SDR DALA2023083107106Unknown · unknown(LOG 2940939) CAPT UPPER RT CORNER OF WINDOW FRAME CRACKED. MAINTENANCE REPAIRED PER ERA 611575-14.SDR DALA2023083107097Unknown · unknown(LOG 2941297) CRACK FOUND IN THE LH #1 WINDOW FRAME IN FLIGHT COMPARTMENT. MAINTENANCE REPAIRED PER ERA 611573-14.SDR DALA2023083107096Unknown · unknown(LOG 4643647) L/H AFT FIXED WINDOW FRAME CRACKED ON FWD SIDE LOWER CORNER #3 WINDOW. MAINTENANCE REPAIRED PER ERA 611584-14.SDR UIEA2023082900800Unknown · unknownDURING GROUND OPS, LOADING TO FWD FUESLAGE WAS DAMAGED BY LOADER. APPROX 47 INCHES LONG, GOUGE 12 INCHES AFT OF FWD CARGO DOOR, BODY STATIONS 670-700, STRINGERS 30R-36R.(<P>PERFORMED HFEC, BOLT HOLE AND ULTRASOUND THICKNESS INSPECTION AT DAMAGE AREA FWD OF CARSDR AALA202311139634Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347615.SDR AALA202311130161Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 347615.SDR HNAA2023101000351Unknown · unknownE993556 ; INTERNAL DOUBLER IS CORRODED BETWEEN FRAMES 62-62A STRINGERS 19L-20L. : FABRICATED AND INSTALLED SERVICEABLE INTERNAL DOUBLER FOR INSTALLATION BTW FR 62-62A STGR19L-20L IAW ETD# ETD2023-145-023886 AND EO1-53-23-0290SDR IPXA2023091848102Frame · unknownMAJOR REPAIR FAULT: AFT CARGO RH FRAME STA 1280 HAS A PREVIOUS REPAIR AT STR 25R ACCOMPLISHED REPAIR IAW EO-88073-REQ 1 AND VT-MAE EA 757-5360-27-A3342, REV.SDR CALA2023083002669Crease Beam · corroded(B737-53-3-3568) MAIN CABIN, CREASE BEAM SHEAR WEB HAS CORROSION ON UPPER SURFACE FROM STA 670-685 RBL 68, TRANSCRIBED FROM HAEC O GSO N/R 9288654 REMOVED CORROSION, ORIGINAL THICKNESS .040" MATERIAL LOSS .008", V894900 INSP QC194 REMANING THICKNESS .032". FOUSDR R61A2023082700456Crossbeam · corrodedDURING HEAVY CHECK, FWD FUSE FR17 RBL12 FOUND TO HAVE CORROSION ON CROSSBEAM.: FWD FUSE FR17 RBL12 FOUND TO HAVE CORROSION ON CROSSBEAM REPAIRED IAW EMBRAER 170-175 SRM 53-00-10 R03.SDR DALA2023082907019Unknown · unknown(LOG 4917828) L1 WINDOW FRAME CRACK. INSTALLED DOUBLER PER STEP 6 OF PRI 611601-14 REV 1.SDR CALA2023082802639Door Frame · crackedEMERGENCY EXITS INTERNAL STRUCTURE, L/H FWD HATCH Z833, FWD LOAD TRASMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES,MULT IPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9 296232 (20232) BY MECH V920443 REMOVED AND REPLACED L/H FWD HATCH, SDR SWAA2023091493100Pressure Deck · crackedHORIZONTAL PRESSURE DECK IS CRACKED AT BS 665 LBL 33 WL202. APPROX 1 INCH IN LENGTH. FOUND ON HFEC INSPECTION. MARKED ENDS OF CRACK.<[01] SRM 53-40-51-2R-2 REPAIR 2 IS APPLICABLE;[02] CUT AND REMOVED THE DAMAGED PART OF THE WEB PER SRM 53-40-51-2R-2 FIGURE 203SDR 2A6D20230824003Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE FIRST CHAFE AREA MEASURES APPROXIMATELY: 0.014" DEEP, 3/8" LONG AND 1/4" WIDE. THE SECOND CHAFE AREA MEASURES APPROXIMATELY 0.007” DEEP, 3/8” WIDE AND 2.5” LONG.SDR SWIA20230823Unknown · crackedSUSPECTED CRACK FOUND ON UPPER BARREL NUT ON PILOTS SIDE WINDOW POST. (C-CHECK RO 10/4/2023) REMOVED AND INSTALLED NEW PILOT SIDE WINDOW POST REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG 601R33007 REV U.COMPLIED WITH THA TASK 51-900-1002-SKYSDR ASAA2023082246615Beam · corrodedDOOR SILL AT FR68 HAS CORROSION GROUNDED - YES. REMOVED CORROSION FROM L2 DOOR SIL AT FR68, REMOVED 0.032", ORIGINAL MATERIAL 0.063", REMAINING MATERIAL 0.031" FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-41-14-283-002. "MAJOR REPAIR ACCCOMPLISHED- LH FUSELAGE AFSDR SWAA2023092192640Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT RBL 41' BETWEEN STA 380-400<[01] REMOVED AND REPLACED ANGLE AT MAIN CABIN RBL 41'' STA 380TO 400 DWG 43A5400 AN SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023092192641Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT RBL 10' BETWEEN STA 380-400<[01] REMOVED AND REPLACED NEW UPPER ANGLE AT MAIN CABIN INTERCOSTAL AT RBL 10' BETWEEN STA 380 TO 400 AND TREATED & PRIMER ALL FASTENERS HOLES AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG # 143A5400;5SDR AALA202309194221Pressure Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND PRESSURE PLATE AT FR 42 BETWEEN -Y1292 AND -Y1650. REPLACED PRESSURE PLATE PER SRM 51-42-11.SDR AALA202309192841Pressure Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND PRESSURE PLATE AT FR 42 BETWEEN +Y1292 AND +Y1650. REPLACED PRESSURE PLATE PER SRM 51-42-11.SDR SWAA2023091592555Intercostal · crackedCRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] UPDATED MEASUREMENT TABLE.;[02] ACCOMPLISHED STEPS 1 AND 2.;[03] REMOVED AND REPLACE CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 141A5400.
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