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 FDEA202010042414Crease Beam · corrodedMAIN DECK BETWEEN STA 1020-1040 RT CREASE BEAM CORRODED. REMOVED CORROSION AT CREASE BEAM STA 1020-1040 RT SIDE, IAW B 757 SRM 51-10-02-OG, ORIGINAL MAT .070", MINIMUN REMAINING .022". MAT LOSS .048" FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG SDR 2020F00421Doubler · crackedCRACK DAMAGE REPAIR OF NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS, FS 75. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020 WITH FAA FORM 8100-9 DATED 06/01/2020.SDR FDEA202010032401Doubler · out of alignmentWHILE ACCOMPLISHING E.O. #G-5310-E0332629 H P6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES BETWEEN BODY STATION 993 TO BODY STATION 1008. BETWEEN STRINGER S35R TO STRINGER S36R. MISALIGNSDR DALA2020100503279Pressure Deck · crackedRIGHT SIDE FR 35/36 PRESSURE FLOOR PANEL HOLE NR 6 & 7 HAVE HFEC CRACK INDICATIONS. CORRECTIVE ACTION: REPAIRED PER AMDS NR 5311-01171-04B.SDR SWAA2021080320100Pressure Deck · damagedFLIGHT DECK FLOOR @ BS 260 DAMAGED. / CUTOUT DAMAGED AREA AT FLIGHT DEECK FLOOR BS 260 AND INSTALLED REPAIR AS PER EA NO. 1-A53-33179 REV1.SDR SWIA202053853Window Frame · corrodedLT CABIN WINDOW BETWEEN FS 517.00 TO 533.00 HAS CORRODED HARDWARE. C-CHECK RO 11/3/2020. REMOVED AND REPLACED CORRODED HARDWARE ON LT CABIN WINDOW BETWEEN FS 517.00 AND 533.00, REF CRJ-700 AMM. TUC 7824 CAL DUE 30 JUN 21.SDR SWIA202053820Web · corrodedLT FS 280 WEB HAS BULGE WITH EVIDENCE OF INTERNAL EXFOLIATION CORROSION AT INBOARD EDGE/FLOOR LEVEL. C-CHECK RO 11/3/2020. REPLACED CORRODED LT 280 WEB INBOARD EDGE AT FLOOR LEVEL WITH A SERVICEABLE UNIT/SPLICE REPAIR, REF CRJ-700. COMPLIED WITH TASK CARD, SDR SWIA202053819Window Post · crackedFLIGHT COMPARTMENT: RT WINDOW SIDE POST LOWER AFT SILL BRACKET HAS EVIDENCE OF CRACK IN RADIUS. C-CHECK RO 11/3/2020. FLIGHT COMPARMENT: RT WINDOW SIDE POST LOWER AFT SILL BRACKET REPLACED, REF CRJ700 SRM & DRAWING. COMPLIED WITH TASK CARD.SDR SWIA202053818Window Post · crackedFLIGHT COMPARTMENT: LT WINDOW SIDE POST LOWER AFT SILL BRACKET HAS EVIDENCE OF CRACK IN RADIUS. C-CHECK RO 11/3/2020. REMOVED AND REPLACED FLIGHT COMPARTMENT: LT WINDOW SIDE POST LOWER AFT SILL BRACKET, REF CRJ-700 SRM AND DWG. COMPLIED WITH ST CARD STRUCTUSDR ASAA2020100233471Window Post · crackedLT NR 1 WINDOW POST CRACKED UPPER OUTBOARD CORNER. GROUNDED-YES. WORK ACCOMPLISHED ON 1018763 2000-0184, SB737-53-1336-NG-1L FOR TRACKING PURPOSES ONLY.SDR IPXA2020102361593Door Frame · crackedINSPECTION TYPE: 2C L-3 DOOR JAMB INNER SKIN IS CRACKED BETWEEN STA 1256.75 & 1250.75 AND BETWEEN DOOR STOPS 6 & 7. REPAIRED CRACKED L-3 DOOR JAMB INNER SKIN BETWEEN STA XOS 1256.75 & 1250.75 AND BETWEEN DOOR STOPS 6 & 7, IAW VT-SAA EA 011-5310-01-A8611 REV ISDR SWIA202053223Beam · corrodedCORROSION ON FWD PAX DOOR THRESHOLD BEAM AFT GIRT BAR FITTING CUTOUT. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FWD PAX DOOR THRESHOLD BEAM WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE IN WEIGHT AND BALANCE, REF EMB175 SRM.SDR DALA2020100503293Door Frame · corrodedDURING INSPECTION FOUND CORROSION ON LAV G DOOR OPENING LOWER FRAME. REPAIRED PER ERA 582489-14TR REV O.SDR DALA2020100503292Door Frame · corrodedDURING INSPECTION FOUND CORROSION ON LAV E DOOR OPENING LOWER FRAME. REPAIRED PER ERA 582489-14TR REV O.SDR DALA2020100503291Door Frame · corrodedDURING INSPECTION FOUND CORROSION ON LAV D DOOR OPENING LOWER FRAME. REPAIRED PER ERA 582489-14TR REV O.SDR DALA2020100503290Door Frame · corrodedDURING INSPECTION FOUND CORROSION ON LAV A DOOR OPENING LOWER FRAME. REPAIRED PER ERA 582489-14TR REV O.SDR R61A2020100200678Crossbeam · corrodedWHILE IN HEAVY CHECK CORROSION ON FR 17 CROSSBEAM BETWEEN LT AND RT SEAT TRACK & OUTBOARD OF RT SEAT TRACK. REPAIRED BY CUTOUT, USING FILLER, DOUBLERS PER SRM 53-00-10/R3 FIG 203.SDR SWAA2021081621619Door Frame · deterioratedDETERIORATED ENTRY DOOR CUT OUT UPPER FLAPER AT FWD GALLEY AREA / REPLACED ENTRY DOOR CUT OUT UPPER FLAPPER AT FWD GALLEY AREA IAW AMM 52-11-00-420-801 TOOL USED TORQUE P/N QD150 S/N 0612058997 DUE DATE 27-MAY-21SDR FDEA202010012384Frame · crackedHFEC SURFACE INDICATION OF DEFECT(CRACK)NOTED AND MARKED IN RED SHARPIE ON FUSELAGE MAIN FRAME 1640RIGHT HAND SIDE INNER CHORD FWD RETURN FLANGE RADIUS INLINE WITH STRINGER 14R. INDICATION RUNS FROM EDGE OF FLANGE UNDER STRAP TO SINGLE FASTENER ATTACHED SDR V0XD20200510052Window Post · crackedRT WINDSHIELD TO SIDE WINDOW POST CRACKED AT TOP BARREL NUT. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2302.SDR 2020F00420Doubler · crackedREPAIR TO NOSE LANDING GEAR WHEEL WELL CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. WITH FAA FORM 8100-9 DATED 06/01/2020.SDR SWIA202053809Door Frame · corrodedPAX DOOR-DOOR FRAME CORRODED, AS MARKED UNDER PANEL 832 FL. C-CHECK RO 11/3/2020. INSTALLED NEW PAX DOOR FORMER PN 601R318031-5, REF DRAWING CRJ700 SRM. LEAK CHECK IS GOOD. SEE CONTINUATION FOR DETAILS.SDR IPXA2020102261558Beam · crackedINSPECTION TYPE: 2C FWD LOWER CARGO HORIZONTAL BEAM IS CRACKED AT STA 6-73 ABOVE LONGERON 44R. REMOVED AND REPLACED CRACKED FWD LOWER CARGO HORIZONTAL BEAM AT STA 6-73 ABOVE LONGERON 44R, IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)SDR SWIA202053441Lintel · damagedCOMPLY WITH REO 670-53-21-493 REV-D DATED 2015-07-10 FOR SB 670BA-53-040. SEE JOB-71032965 OP-74 MXTRANS-21556987. C-CHECK RO 10/17/2020. COMPLIED WITH REO REPAIR TO PAX DOOR LINTEL (STG 3L) BETWEEN FS 280 AND FS 295 FOR SB SEE JOB-71032965 OP-74 MX TRANS-2SDR AALA202010059014Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF CENTER FITTING BETWEEN FR66 AND FR68 AT STR 23L, MEASURING L=3.940 IN, W=0.540 IN, D=0.018 IN. REPLACED CENTER FITTING WITH NEW IAW A321 SRM 51-42-11-801 AND DRAWING D53480505.SDR ASAA2020093033231Window Post · crackedLT NR 1 WINDOW POST IS CRACKED UPPER OUTBOARD CORNER MARKED. GROUNDED-YES. REPAIRED LT NR 1 WINDOW POST, IAW ALASKA AIRLINES TASK CARD SB737-53-1336-NG-2L. WORK ACCOMPLISHED ON ALASKA AIRLINES TASK CARD SB737-53-1336-NG-2L, 1018825 2000-0172.SDR FDEA202009292351Flange · crackedDURING ULTRASONIC INSPECTION AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON RIGHT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY RIGHT BUTT LINE 82 ASDR FDEA202009292350Flange · crackedDURING ULTRASONIC INSPECTION AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON LEFT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY LEFT BUTT LINE 82 ANDSDR SWAA2020101520568Floor Skin · dentedFLIGHT DECK FLOOR HAS SEVERAL DENTS STA 260, LBL10 TO RBL 4, WL 208. REPAIRED FLIGHT DECK FLOOR WEB STA 260, AS PER EA 1-A53-33179 REV 1.SDR SWAA2020101419419Structure · crackedCENTER WING BOX STA 663 LOWER CHORD FWD SIDE IS CRACKED AT RBL 7' / CENTER WING BOX STA 663 LOWER CHORD FWD SIDE AT RBL 7; CUTOUT DAMAGED ANGLE. INSTALLED NEW REPAIR ANGLES; CAP SEALED AND FILLET SEALED REPAIR IAW SRM 57-10-10-2R-5. LEAK CHECKED REPAIR AREA; NSDR HALA2020092903138Beam · cracked492 C CHECK. SMALL CRACKS ON THE MED NR 6 BEAM (P/N: 9955757-503) AT/NEAR THE BAYONET CRANK FITTING BOLT HOLE. REPAIRED MED NR 6 BEAM, PER E105-B10650-PERM 08/17/2020.SDR HALA2020092903137Structure · corroded492 C CHECK. SM S/C AROUND STA 974 AND LONG 30 (M). REMOVED CORROSION, PER B717SRM 51-10-04-OG-O. FOUND TO BE BEYOND LIMITS, PER SRM 53-00-090-1A 0 FIG 103 M66 SUBMITTED. PENDING INSTALLATION OF FASTENERS TREAT PRIME AND PAINT POST REPAIR. INSTALLED LOCK SDR HALA2020092903136Former · corroded492 C CHECK. CORROSION UNDERNEATH BONDING WIRE ON LEFT FILLET FORMER 4TH BACK FROM FWD (M). REMOVED CORROSION, PER SRM 51-10-04. FOUND TO BE OUT OF LIMITS. M66 SUBMITTED. CORROSION BLEND ON THE WING TO FUSELAGE FILLET FORMER AT Y=636 SURFACE CORROSIOSDR HALA2020092903134Frame · corroded492 C CHECK. CORROSION DISCOVERED ON THE STA 1098.868 FRAME TEE (PN 9971144-61) AT L-28L. THE CORROSION WAS MECHANICALLY REMOVED WITH MORE THAN 50% MATERIAL LOST IN THE VERTICAL FLANGE AND PITTING CORROSION 100% THROUGH THE AFT HORIZONTAL FLANGE. INSTALLED SDR FDEA202009272563Support Beam · crackedCRACK INDICATION ON INTERNAL STRUCTURE IN OPEN HOLES 3 E/A ON DOOR ACTUATOR SUPPORT BEAM IN FWD CARGO COMPARTMENT. CRACKS LOCATIONS ARE: CRACK HOLE 1 LOCATION FR 22 MORE 2.5 INCH; CRACK HOLE 2 LOCATION FR 22 MORE 7.5 INCH; CRACK HOLE 4 LOCATION FR 22 MORE 18.SDR SIMA20200926003Door Frame · corrodedRT OVERWING EXIT LOWER EDGE IS CORRODED AROUND AND UNDER FWD AND AFT BLACK TEFLON PADS. C/A: REMOVED AND REPLACED RT OVERWING EXIT LOWER PROFILE, IAW EMB 145 SRM 51-10-02.SDR UIEA2020092802101Structure · crackedCRACKED CHORD. REPAIRED CHORD, IAW B767 SRM 51-70-12.SDR UIEA2020092802109Structure · corrodedCORROSION FOUND BETWEEN 1375 AND 1417 S35R-36R. BLENDED CORROSION AND REPAIRED, IAW AMES DOC 47416 REA 13.SDR UIEA2020092802111Tee Fitting · corrodedLT WHEEL WELL STA 955 LBL 97 "T" FITTING HAS CORRSION ON RACK AFT OF LT WHEEL WELL. CORRODED "T" ANGLE FOUND TO BE OUT OF LIMITS, IAW SB 767 53A0100 STEP 9. INSTALLED NEW ANGLE ON EO NR 6753A070 STEP NR 11.SDR UIEA2020092802112Failsafe · crackedLT FAIL SAFE STRAP AT STA 955 LOWER FASTENER HOLE CRACKED. PERFORMED CUT OUT OF FAILSAFE STRAP, IAW BSB SB 53-A0100 FIG 15 + ATLAS 6753A070 (EO).SDR UIEA2020092802113Failsafe · cracked2 EA LOWER BOLT HOLES CRACKED ON RT FAIL SAFE STRAP STA 955 RBL 98. PERFORMED CUT OUT ON FAIL SAFE STRAP, IAW SB 53-A0100 FIG 15 AND ATLAS EO 6753A070.SDR SWIA202053942Bracket · corrodedPAX DOOR SURROUND STRUCTURE BRACKET CONNECTORS FWD AND AFT CORRODED BETWEEN FS 319.70 ND FS 333 AND BETWEEN STGR 17L AND STGR 18L. C-CHECK RO 11/11/2020. REMOVED FWD AND AFT CONNECTOR BRACKETS, IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED NEW SDR SWIA202053925Fitting · crackedWINDSHIELD CENTER POST LOWER FITTING IS CRACKED FROM THE LOWER VERTICAL EDGE TO THE FIRST LOWER FASTENER HOLE ON THE RT & LT SIDES. FAIL DETAILED VISUAL INSPECTION. C-CHECK RO 11/11/2020. REMOVED AND REPLACED WINDSHIELD CENTER POST RT AND LT LOWER FITTING FSDR JJBA20200924008Structure · corrodedCORROSION AROUND A/C DATA PLATE LOCATED AT AFT EXTERIOR OF A/C. PERFORMED HFEC INSPECTION OF SKIN CUTOUT AT DATA PLATE AREA. NO INDICATIONS NOTED. PERFORMED CUT OUT AFFECTED AREA AND REMOVED DATA PLATED. FABRICATED DOUBLER, FILLER AND APPLIED CHEMICAL CONVSDR SWIA202053882Door Frame · damagedFOUND PAX DOOR FRAME ON FWD SIDE TO HAVE MULTIPLE OVERSIZED HOLES. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR FWD FRAME, IAW CRK 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORKSDR AALA202010269025Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION OF RT TRANSITION PANEL BETWEEN STA 727 AND STA 867 AT STR 25R, MEASURING L=1.0 IN, W=0.5 IN, D=0.038 IN. REPLACED TRANSITION PANEL WITH NEW, IAW SRM 53-00-53-2R-6.SDR SWAA2020102320997Flange · crackedCRACK GROUND SERVICE DOOR 114AR INTERNAL FLANGE AROUND CUT OUT AT LOWER FUSELAGE. PERFORMED REPAIR GROUND SERVICE DOOR 114AR INTERNAL FLANGE AROUND CUT OUT AT LOWER FUSELAGE, IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204.SDR FDEA202009222290Support Beam · crackedAFT CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR61-FR62 Y-1456 - Y-1959 FOUND 2EA CRACKS AS MARKED REPLACED AFT CARGO DOOR ACTUATOR CRACKED SUPPORT BEAM BETWEEN FR61-FR62 Y- 1456 - Y-1959 PER A300-600F SRM51-40-21. INSTALLED THE AFT CARGO DOOR ACTUATOR AND SDR SWAA2020101419694Pressure Deck · crackedFOUND 663 HORIZONTAL PRESSURE DECK TO BE CRACKED AT FWD O/B CORNER OF BEAD AT BS 664 RBL 41 WL 200. / REMOVED DAMAGED SECTION OF 663 HORIZONTAL PRESSURE DECK AT BS. 664 RBL 41 WL 200; AND REPAIRED PER SRM 53-40-51-2R-2.SDR SWAA2020101318514Floor Skin · dentedCOCKPIT FLOOR DENTED AT STA 260 AT 2ND OBSERVER SEAT INBOARD LEG. ACCOMPLISHED PERMANENT REPAIR ON COCKPIT FLOOR WEB AT STA 260 BETWEEN LBL 20 & RBL 5, PER EA 1-A53--33179.
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