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 AALA202201255036Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF WEB BENEATH AFT CARGO DOOR AT STA 800 AND STR 25R, MEASURING L=3.5 IN, W=1.5 IN, D=0.017 IN. REPLACED WEB WITH NEW IAW AARD 51-00-05-1.SDR CALA2021123002482Structure · crackedR/H FR35 STR30 HOLE #1,#4, #3, #2,PRODUCED CRACK INDICATIONS AT THE 6:00 POSITION 2ND LAYER. PER HAECO LCQ NR''S 9292019/20019, 9 292016/20016, 9292017/20017, 9292018/20018. GENERATED BY V061690 PERMANENT REPAIR ON THE FR 35 STR30RH HOLES #1-#4 PER PART 3 OF WSDR CALA2021122902481Angle · crackedL/H FR35 STR30 HOLE #1 PRODUCED CRACK INDICATIONS AT THE 2:00 PO SITION. HO,LE #3, #4. LH FORWARD PIT AFT OF FRAME 35 HOLES COMMO N TO ANGLE FITTING REMOVAL UPPER ROW 7TH AFT OF FRAME 35 INTERIO R SURFACE IS GOUGED JUST ABOVE THE HOLE AT 12:00. PER HAECO LCQ NSDR IXXA202112290003Pressure Deck · corrodedPRESSURE DECK AT FS 1263-1285 TO HAVE 2 SPOTS OF CORROSION.SDR DALA2024012401065Track · gougedSHIP 3261 DISC: COCKPIT R/H SIDE SLIDING WINDOW BOTTOM TRACK GOUGED AT FWD 2ND FASTENER. C/A: BLENDED DAMAGED AREA ON COCKPIT R/H SIDE SLIDING WINDOW BOTTOM TRACK IAW A320 SRM 53-11-12, EVALUATED AREA ORIGINAL MATERIAL THICKNESS 0.125" REMAINING MATERIAL 0.116SDR SWAA2022021056506Angle · crackedSUPPLEMENTAL INFORMATION: CABIN PASSENGER UPPER SECTION OF L1 DOOR INTERNAL AREA STA312 HAS CRACK ; / [01] REMOVED FASTENERS AND MADE CUT OUT OF CRACKED AREA AS PER B737-700 SRM 53-10-07-2R-1.; [02] VERIFIED STEP 1; [03] PERFORMED HFEC INSP ON REWORKED AREA. ISDR SWAA2022021056498Intercostal · crackedSUPPLEMENTAL INFORMATION: PASSENGER CABIN FWD WET AREA BETWEEN STA-312 AND STA-328 AT LBL-45; INTERCOSTAL WITH CRACK. DOT#208-104 ; / [01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN FS 312-328 LBL 45 IN REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIEDSDR SWAA2022020456549Rib · crackedABOVE FWD ENTRY DOOR FWD CORNER AT BS 312 THERE`S A CRACKED RIB. FABRICATED UPPER CHORD REPAIR IAW SRM 53-10-07-2R-1 REPAIR 1, TRIMMED OUT CRACK AREA IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKSSDR FDEA202112280168None · corrodedFOUND CORROSION ON FLOOR BEAM EXISTING REPAIR AT STA 1320 BETWEEN RBL24 TO RBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EO # F-5310-T0366466SDR FDEA202112280167Seat Track · corrodedFOUND CORROSION ON SEAT TRACK RBL 45 BETWEEN STA 1320 TO 1420 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED 2 EA SEAT TRACKS SECTION, 2 EA SPLICES , AND 1 EA STRAP PER SRM 53-00-52, REPAIR 1 FIG. 201, THIS REPAIR IS A PERMANENT CAT. A REPAIR, THE INSP. SDR FDEA202112280166Seat Track · corrodedFOUND CORROSION ON SEAT TRACK RBL 24 ON STA 1320 AND STA 1410 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED SEAT TRACK SECTION, 2 EA SPLICES , AND 1 EA STRAP PER SRM 53-00-52 REPAIR 1 , FIG 201, THIS REPAIR IS A PERMANENT CAT "A" REPAIR , THE INSP. GISDR IXXA202112280001Beam · corroded47487REA29 CORROSION AT STRINGER 38L STATION 720SDR SWAA2022011056447Angle · crackedA-125-02 - CRACK FOUND IN AC BAY; REAR BULKHEAD TO CENTER TANK LOWER SKIN ATTACH ANGLE; BS 663; RBL 11. CRACK NOTED VISUALLY; VERIFIED BY HFEC PART 6 51-00-00 P23 ; / [01] CUT OUT DAMAGED SECTION OF ANGLE IAW SRM 57-10-10-2R-5 STEP 4B FIG 202 SH 4 DETAIL B.; [SDR HALA2021122700202Door · damagedEMER EQ - DOOR - FOUND DENT/GOUGE BELOW LEADING EDGE OF 1R SERVICE DOOR. // EDDY CURRENT SHOWS NO CRACK. #8089 12/24/21. BLEND GOUGE PER SRM 53-01-01-1A-1. MEASURED BLEND: ADJ 0.024, MIN REM:0.017; M66 SUBMITTED. 12/24/2021 MECH:015816. #5178. REMEASURED BLENDSDR SWAA2022010355980Web · elongatedELONGATED HOLE DOOR CUTOUT WEB UPPER AREA LOCATED BETWEEN BS442 TO BS 490 AT FWD CARGO COMPARTMENT. REPLACED DOOR CUTOUT WEB UPPER AREA LOCATED FASTENERS IAW SRM 51-40-02 AND SRM 51-10-02 AND DWG 143A0081 SHEET 38 REV. B. REPLACED DOOR CUTOUT WEB UPPER IAW SSDR ASAA2021122437005Shroud · damagedWHILE AT GATE EXTERNAL POWER CORD SHORTED/SURGED CAUSING FIRE/EXCESSIVE HEAT DAMAGE TO EXTERNAL POWER RECEPTACLE SHROUD ASSY GROUNDED - YES. REPLACE EXTERNAL POWER RECEPTACLE SHROUD ASSY AND HARDWARE AS NEEDED IAW B737-700 SRM 51-40-02SDR ASAA2021122337212None · corrodedMAIN CABIN FLOOR PANEL SUPPORT BEAM ON RH SIDE AT APPROX Y-1292 HAS CORROSION ON UPPER SURFACE FROM FR 18- FR 20 (MARKED). DOT:W486 GROUNDED - YES. REMOVED CORROSION ORG .079, REMAINING .034 LOSS OF .045. FOUND OUT OF LIMITS IAW A320 SRM 53-11-14.REMOVE FLOSDR DXTA2021122754060None · defectiveFUSELAGE STRUCTURE: REPEAT WRITE-UP . LOUD HOWLING WITH VIBRATION FELT UNDER COCKPIT AREA . STARTED DURING CLIMBOUT THRU 2000 FEET AND STOPPED ONCE IN LEVEL CRUISE FLIGHT. HOWLING STARTED AGAIN DURING DECENT FROM 16000 FT DOWN TO 2000 FT. // SIGNOFF // ARRIVEDSDR SWAA2022020255901Web · corrodedCORROSION ON UPPER SURFACE OF CREASE BEAM WEB BS 787+5' WL 208 RBL 65. REMOVED CORROSION IAW SRM 53-60-13-1A-1 PARAGRAPH 2.B. ACCOMPLISHED VISUAL INSPECTION, NO DEFECTS OR CORROSION NOTED. UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00, PROCEDURE 2. RESDR V0XD20211228001Skin · dentedDENT ON FUSELAGE SKIN AT FS 1031 ON STGR 25R MEASURING 1.00"L X .5"W .031"D. CORRECTIVE ACCTION: REPAIRED AREA BY DRESSING BACK DENT AT FS 1031 ON STGR 25R TO .950"L X .475"W X .011"D AND FABRICATED DOUBLER REPAIR PARTS AND INSTALLED THEM AT FS 1031 AT STGR 2SDR UIEA2021122102484None · noneDENT PLUS REWORK ON FUSELAGE SKIN BETWEEN STA 282 AND STGR 19 / 20LH(<P>EVALUATED AREA PER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL III, HOWEVER IT WAS FOUND OUT OF LIMITS AND FOR SUCH REASON MXA CONTACTED TO BOEING PER SR# 3-5178994812 (LEAVE IN "AS IS" CONDITSDR GTIA2021122336187Panel · dentedFOUND DENT AT FR 23+18" AT STR 42R REF HAECO NR 44150 RAF 01 OPENED-REPAIRED DENTED AREA ON FUSELAGE SKIN FR 23 + 18" STR 42R Y-175 IAW A319 REO L23549 AIRBUS OEM MESSAGE SR 81002501 REF RDAF # 81002501/003/2021#ASDR GTIA2021122336186Unknown · dented3 DENTS ON FR 2-3 STRINGERS 30R-34R. REF HAECO INCOMING NRI-00001. RAF 01 OPENED-REPAIRED IAW A319 SRM 53-11-11-300-075 CAT B REPAIR. REQUIRES REINSP AT 60,000FC 100,000FH FROM EMBODIMENT PER SRI 53-11-11-205-055SDR ASAA2021122237211None · corrodedR1 DOOR LOWER THRESHOLD BEAM HAS CORROSION AT GIRT BAR FITTING STUDS, FR20 (MARKED) DOT:T544 GROUNDED - YES. BLENDED AREA AND REMOVED CORROSION, LOWEST REMAINING THICKNESS IS .165Ï¿½ FOUND WITHIN LIMITS IAW AIRBUS A320 SRM 53-11-14DOT REMOVED TOOLING T84SDR ASAA2021122237122None · corrodedL1 DOOR LOWER THRESHOLD BEAM HAS A LIGHT CORROSION AT GIRT BAR FITTING STUD, FR16 (MARKED)DOT:T545 GROUNDED - YES. REMOVED CORROSION ON 2EA AREAS, LOCATION 1 IS 1.93Ï¿½ LENGTH 1.00Ï¿½ WIDTH. AND .173Ï¿½ REMAINING LOCATION 2 IS 1.75Ï¿½ LENGTH, 1.15Ï¿½ WIDTSDR ASAA2021122237455Beam · corrodedR1 DOOR LOWER THRESHOLD BEAM HAS CORROSION AT GIRT BAR FITTING STUDS, FR16 (MARKED). DOT:T543 GROUNDED - YES. REMOVED AND REPLACED R1 DOOR LOWER SILL IAW ALASKA EA # A320-53EA-01286 AND AIRBUS A320 SRM 51-42-11. DOT REMOVED TOOLING T8492USDR SWAA2022020255753Barrier · crackedBS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 8 WL 160. CUT AND REMOVED THE DAMAGE IAW SRM 57-10-10-2R-5, REPAIR 5, DETAIL B. HFEC ROTARY INSPECTED ALL INITIAL FASTENER HOLES IN THE REPAIR AREA IAW NDT PART 6 51-00-00 PROCEDURE 16. NO CRACKS FOUND.SDR SIMA20211222004None · noneDISCREPANCY: 53-10 FUSELAGEFUSELAGE MAIN, STRUCTURE - REF: AML 4741171 ITEM 1 DENT ON RH FUSELAGE BETWEEN FR 06-07 AND STR 13-14 UNDER FO DV WINDOW AND BEHIND RH SMART PROBE AND RVSM AREA "MAJOR REPAIR"-C/A-PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM FUSDR YENA2022021600065Door Frame · corrodedDURING HEAVY MAINTENANCE, "FROM TOMX NR 00300, INITIAL INSPECTION: ""CPCP FINDING"" CORROSION IN FASTENER PERIPHERY LOCATED OVER MACHINED BEAM BETWEEN STRG 27R/28R AND FR 77 IN AFT CARGO DOOR CUTOUT STRUCTURE" ; "FROM TOMX NR 00300, INITIAL INSPECTION: ""CPCP SDR YENA2022021600064Door Frame · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE; "ALL WORK ACCOMPLISHED REF TOMX NR 00301 MIDDLE SEAL REST IN LOWER EDGE OF AFT CARGO DOOR CUTOUT STRUCTURE WAS REPLACED PSDR SWAA2022020754968Strap · corrodedCORROSION AT AFT WET AREA FLOOR WEB SUPPORT STRAP LBL-3 STA 1016 MKD DOT-001 ; / [01] REMOVED FASTENERS FOR ACCESS 2EA AS PER REF B737-700 SRM 51-40-02-0G-0;[08] VERIFIED STEPS 6 AND 7. OK TO INSTALL NEW STRAP.; [09] INSTALLED NEW STRAP P/N: 147A5620-3 AT AFT SDR SWAA2022020255053Doubler · crackedCRACK IN FWD GALLEY DOOR BEAR STRAP BS 294, S8R & 9R. CRACK IS APPROX .5 INCHES LONG PROPAGATING FROM FASTENER HOLE. CUT & REMOVED PART OF BEAR STRAP 2.3'LX1.0W IAW SRM 53-10-01-2R-6, REPAIR 6. ACCOMPLISHED HFEC INSPECTION IAW NDTM D6-37239 PART 6, 51-00-00SDR MASA20211221642None · noneTHE PASSENGER DOOR FWD SEAL STRIKER WAS FOUND BENT COMMON TO THE OUTBOARD FLANGE OF THE STRIKER. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-23-001-001-A01, FIG 53-21-23-995-818 ITEM 1388 (REV. 38 DATED JUL. 25, 2020).SDR 2022F00109Stringer · crackedPASSENGER DORR LINTEL STRINGER IS CRACKED AT F.S. 280.00. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED THE PASSENGER DOOR LINTEL STGR AT F.S. 280.00 IW BOMBARDIER SB 670BA-53-040 REV. C DATED SEPT 20/2012 AND BOMBARDIER REO 670-53-21-493 REV. D DARED 2SDR V0XD20211221002Lintel · crackedPASSENGER DOOR LINTEL STRINGER IS CRACKED AT F.S. 280.00. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED THE PASSENGER DOOR LINTEL STGR AT F.S. 280.00 IWW BOMBARDIER SB 670BA-53-040 REV. C DATED SEPT 20/2012 AND BOMBARDIER REO 670-53-21-493 REV. D DARED SDR CALA2021122002416Line · leakingREF LOGPAGE 7616396. WITHIN 7 DAYS ACCOMPLISH EC/RA 2011-01000, CARGO COMPARTMENT SPILL, SECTION 2.B. IN-DEPTH CLEANUP, IN THE APPROXIMATE AREA FROM BODY STATION FR-24 TO BODY STATION FR-35. BETWEEN STRINGER 41RH AND STRINGER 41LH. FWD CARGO PIT. UNDER POTABLSDR AALA202112219944Frame · damagedAIRCRAFT IN BASE MAINTENANCE: FASTENER HOLE OVERSIZED TO 0.2885" ON FRAME AT INBOARD TRANSITION ATTACH POINT AT STA 807 AND STR 25L. ACCOMPLISHED TIME LIMITED STRAP REPAIR IAW EA332659.SDR SWAA2022011254858Web · corrodedAFT CARGO THRESHOLD WEB HAS AREAS OF CORROSION AT FASTENER HOLE NUT PLATES; UPPER AND LOWER SURFACES. STATION 807-814 WL 156 AND RBL 25. ; / [01] REMOVED 3EA NUT PLATES TO FOM IAW B-737 SRM 51-40-02.; [02] DAMAGE REMOVED IAW B-737 SRM 51-10-02-0G-0. 10X MAG LESDR 2022F00107None · corrodedFALSE FLANGE AT F.S. 310 BETWEEN STGR 26R AND 24R IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGE AND REPAIRED THE FALSE FLANGE (PN: S1710-3) IAW BOMBARDIER REO 670-53-21-1281 REV. -- DATED 2016-04-11.SDR VNAA202201029996Flange · corrodedFALSE FLANGE AT F.S. 310 BETWEEN STGR 26R AND 24R IS CORRODED. CORRECTIVE ACTION: REMOVED AND DAMAGE AND REPAIRED THE FALSE FLANGE (P/N S1710-3) I/A/W BOMBARDIER REO 670-21-1281 REV. -- DATED 2016-04-11.SDR CALA2021122002406None · noneSTATION 1016 PRESSURE BULKHEAD, BETWEEN STR:1R AND 2R. WL 299.5. DOME WEB, "OIL CANNED" CONDITION FOUND. LENGTH 8", WIDTH5" DEPTH 0.1515" REPAIRED APB PER SRM 53-80-08 REPAIR 12 PERFORMED INTERIM REPAIR TO OILCANNING LOCATED AT PRESS BULKHEAD TOMC-APPROVAL FROSDR AALA202112174878Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ANGLE AT STA 663 AND RBL 43, MEASURING L=0.5 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR IAW SRM 57-10-10-2R AND EA332269.SDR SWAA2022012753775Shear Web · corrodedCORROSION ON UPPER SURFACE OF WEB AT STA 987 RBL 33. (MARKED) ; / [01] REMOVED DAMAGE PER SRM 51-10-02. NO DAMAGE IS ALLOWED ON SHEAR WEB IAW SRM 53-70-51-1A-1. WEB IS OUT OF LIMITS.; [02] REPAIRED PER TASK CARD #TTG800A0UMP AND REFERENCE TSR # 2021008523.; [0SDR AALA202201259946Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF RH TRANSITION PANEL BETWEEN STA 500A AND STA 500I AT RBL 24, MEASURING L=1.0 IN, W=1.0 IN, D=0.007 IN. REPLACED TRANSITION PANEL WITH NEW IAW SRM 53-00-53.SDR AALA202112218413Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF STRINGER CHORD AT STA 315 AND STR 23L. ACCOMPLISHED TIME LIMITED STRAP REPAIR IAW EA332428.SDR V0XD20211220001Angle · corrodedSTRINGER 26R BETWEEN F.S. 333 AND F.S.349 THE JOINT SPLICE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE JOINT SPLICE(PN; N126-3999) ON STGR 26R BETWEEN F.S. 333 AND F.S. 349 IAW CTJ 700 SRM 51-42-06-001-001-A01 AND 53-21-08-01-002.SDR CALA2021121702378Stringer · corrodedAFT CARGO PIT STRINGER 41RT BETWEEN FRAME 61-62 HAS CORROSION O N VERTICAL FLANGE (SUPPORT TASK) GENERATED BY V052030 AT HAECO L CQ PER NR 9294337 (22337) REMOVED AND REPLACED STRINGER 41RT AFT CARGO. IAW A320 SRM 51-72 -11. PERFORMED BY V052030 INSP BY V06133SDR CALA2021121702377Stringer · corrodedAFT CARGO PIT STRINGER 42 LEFT HAS CORROSION AT FRAME 57LT AND F R59 LEFT (SUPPORT TASK) GENERATED BY V052030 @HAECO LCQ PER NR 9 294340 (22340) REMOVED AND REPLACED STRINGER 42L IN AFT CARGO. IAW A320 SRM 51- 72-11. PERFORMED BY V052030 INSP BY V061334SDR SWAA2022011053103Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS774 RBL20. MARKED. ; / [01] REMOVED CORROSION ON WEB AT BS 774; RBL20; WL 156 PER SRM51-10-02-0G-0 MEASURE L=3.3'X W=1.1'X D=0.002' MAX. MAT LOSS IS 0.002'; REMAINING THICKNESS IS 0.048'; ORIGINAL THICKNESS IS 0.050' WAS FOUSDR ASAA2021121236957None · corrodedFWD PIT DOOR CUTOUT LOWER SILL WEB HAS CORROSION. DOT: AP377-001. GROUNDED - YES. REMOVED AND REPLACED FWD PIT DOOR CUTOUT LWR SILL WEB IAW B737-900 SRM 51-40-02-0G-0W: 6 O: .045 R: .037 L: 12 D: .008.
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