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 SWAA2023081471776Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 500D BTW STR 18R TO STR 19R LOWER FUSELAGE 2023-413018<[01] REPLACED SUPPORT BRACKET LOCATED BS 500D BTW STR 18R TO STR 19R LOWER FUSELAGE IAW B737 SRM 51-40-02 AND DWG 116A3010 REV: A . SEE INDIVIDUAL SIGN OFF BELOW.;[02] RSDR SWAA2023081471939Angle · brokenBROKEN T-ANGLE LOCATED BTW BS 530 TO BS 559 INTERNAL AREA OF ACCESS PANEL 192E CENTER SECTION LOWER FUSELAGE 2023-413021<[01] REPLACED T-ANGLE LOCATED BTW BS 530 TO BS 559 INTERNAL AREA OF ACCESS PANEL 192E CENTER SECTION LOWER FUSELAGE IAW B737-700 SRM 51-10-SDR FDEA202306261219Crossbeam · unknownEXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 66 BTW - Y953 ~ -Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPASDR REXA2022062700402Cleat · corrodedFLOOR BOARD SUPPORT ANGLE AT F.S.265 AND ATTACH ANGLE TO STGR 27 ARE CORRODED. REMOVED ATTACHMENT ANGLE AT FS.265 STRINGER 27. LOCATED, DRILLED AND INSTALLED ATTACHMENT ANGLE AT FS. 265 STRINGER 27 P/N: CC670-34228-3 IAW CRJ 900 SRM 15-40-11-001-001-A01 & 51-4SDR DXTA2023062689450Unknown · unknownFUSELAGE STRUCTURE: APPROXIMATE 3INCH GASH IN FUSELAGE AFT AND BELOW MAIN CABIN DOOR. HONEYCOMB EXPOSED. DISCOVERED ON PREFLIGHT. REPAIRED LH FORWARD AERODYNAMIC FAIRING IAW EWO-4661 REV. IR.SDR SWAA2023081471511Scuff Plate · crackedFOUND AFT CARGO COMPARTMENT CENTER SCUFF PLATE CRACKED AT FORWARD EDGE<[01] ACCOMPLISHED WELDING AT AFT CARGO DOOR CENTER SCUFF PLATE OUTSIDE BY J.L WELDNG VENDOR FAA REPAIR STATION # JLWR146K AS PER SRM 53-60-15-2R-1 AND BAC5975;[02] VERIFIED STEP 1.SDR REXA2022071000454Doubler · deformedDURING INCORPORATION OF SB 670-53-044 REV G, OVERSIZE FASTENERS FOUND @ STR 14L ON FS 202 BULKHEAD. (6 TOTAL FASTENERS) REPAIRED IAW MHIRJ REO # 690-53-11-1570 REV A DATED 2023-06-30.SDR SWAA2023081471322Web · crackedCRACK INDICATIONS FOUND(2EA) ON HORIZONTAL PRESSURE DECK WEB BTW RBL 40 TO RBL 47 ON BS 663 TO BS 675; CRACK LENGHT ARE AS FOLLOW: CRACK 1: 0.450 INCHES AND CRACK 2: 0.510 INCHES APPROX 2023-412963<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 2SDR FDEA202306241140Bracket · unknownAFT CGO COMP'T FWD BULKHEAD LH SUPPORT BRACKET CRACK AT Y 1959,Z-751 FR54 POSITION REMOVED CRACK BRACKET AND INSTALLED WITH NEW ONE.I.A.W A300-600F SRM 51-72-10-001. PAGE2SDR HNAA2023062600207Unknown · unknownLIGHTNING NEAR CAPT WINDOW
FACT 25JUN23 01:02 PHL PERFORMED LIGHTNING STRIKSDR SWI2023F00292Unknown · crackedFLIGHT COMPARTMENT R/H WINDSHIELD POST CRACKED (MARKED) (C-CHECK RO 8/31/2023) REMOVED DAMAGED RH WINDSHIELD POST AND LOCATED, DRILLED AND INSTALLED A NEW RH WINDSHIELD POST REF CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DRAWING 601R33007 REV U COMSDR AALA202309198597Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 LEFT. REPLACED CONTINUITY FITTING PER EA 345858.SDR AALA202309199587Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FRONT WINDSHIELD LEFT HAND FRAME LOWER RADIUS AT FR 3 AND Y0 LEFT. REPAIRED FRAME PER EA 345858.SDR SWIA20230622Unknown · crackedPAX DOOR FORMER FS347.25 IS CRACKED @ 4 EA FASTENER HOLES FOR PULLEY BRACKET (C-CHECK RO 8/16/2023) REPLACED PAX DOOR AFT FORMER REF CRJ-700 SRM 51-42-06-001-001-A01 REV 38 DATE JUL 25/2020, CRJ-700 SRM 51-42-21-001-001-A01 REV 38 DATE JUL 25/2020 AND SDR SWAA2023071170754Intercostal · crackedCRACKED INTERCOSTAL UPPER FLANGE BS 380-400 LBL 14 WL 208.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 14; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPORT BS 380SDR IXXA2023070805Roller Tray · crackedDISCOVERED TWO CRACKS ON THE AFT CARGO ROLLER TRAY AT STA 1105 RBL 20.5. DAMAGES TRIMMED OUT TO 1.8" X 0.25" AND 1.7" X 0.26" CUTOUT AND INSTALLED REINFORCING DOUBLERSDR YENA2023062200697Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR STRUCTURE / FR 15-18 & Y=-202 TO Y=-302 AND FR 18-20 & Y= -203 TO Y=-303 / FWD. CABIN CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR SWAA2023072670423Depressor · crackedCRACK FWD SERVICE DOOR CUTOUT REVEAL LOCATED BS 294.5 BTW STR 8R TO STR 10R AT PASSENGER CABIN 2023-394780<[01] REPLACED DEPRESSOR (REVEAL) AND FASTENERS LOC. FWD SERVICE DOOR CUTOUT REVEAL LOCATED BS 294.5 BTW STR 8R TO STR 10R AT PASSENGER CABIN IAW B737-700SDR IPXA2023071338826Stringer · damagedFAULT: DURING INSPECTION ON EO-73926-JIC001 AN EXISTING REPAIR WAS FOUND AT STA 1300 LH S24-26L. ALTERNATE INSPECTION REQUIRED. WORK COMPLETEDSDR FDEA202306211093Support · corrodedFWD CARGO COMPT, AFT BULKHEAD, LOWER FLOOR BOARD SUPPORT STA RBL 10, HAS CORROSION ON VERTICAL LEG. INSTALLED TEE EXTRUSION AND REPAIR ANGLES AS REQUIRED. REF MD 11 SRM 53-00-00-2R FIGURE 208, SHEET 3, SRM 51-33-01-0G, DAC DWG ADA7667.SDR CALA2023062201975Stringer · corrodedSTRINGER 31R HAS EXFOLIATING CORROSION AT FR65 REQUIRES REPAIR/R EPLACE PER HAECO LCQ NR 9298009/28009 GENERATED BY V061673 REMOVED & REPLACED CORRODED STRINGER 31R @ FR65 IAW A320 SRM 51- 72-11-911-002 MECH V061673 INSP V921755SDR SWAA2023071161686Threshold · corrodedAFT CARGO BAY SUBTHRESHOLD IS CORRODED. CORROSION IS MEASURED FROM FWD EDGE OF PART AND IS MARKED ACCORDINGLY. (+8 TO+14); (+14 TO +16); (+17 TO+19); (+23 TO +25); (29 TO +32); (+33 TO +35)<[01] PARTIALLY STEPS 1;2;3.;[02] AFT CARGO BAY SUB THRESHOLD MUST BE RSDR SWAA2023071161703Threshold · corrodedAFT CARGO BAY SUB THRESHOLD CORRODED. CORROSION MEASURED FROMFWD EDGE AND IS MARKED ACCORDINGLY. (+36 TO +37); (+39); (+41 TO +42); (+44)<[01] REMOVED CORROSION ON AFT CARGO BAY SUBTHRESHOLD BETWEEN BS 827+12' RBL 28; WL.156 IAW SRM 51-10-02.<BR> MEASURE MAX. SDR SWAA2023071066727Angle · crackedCRACK ON ANGLE LOC. BETWEEN BS 380 TO BS 400. RBL10 FWD GALLEY PAX CABIN 2023-379081<[01] REPLACED ANGLE LOC. BETWEEN BS 380 TO BS 400. RBL10 FWD GALLEY PAX CABIN IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET 105 REV-. SEESDR SIMA20230620002Support Bracket · corrodedFR 81 STGR 28R FLOOR SUPPORT STABILIZER BRACKET CORRODED (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-RAR FR 81 STGR 28R FLOOR BOARD SUPPORT STABILIZER BRACKET IAW EMB 170 SRM 51-40-08SDR ASAA2023062043751Skin · corrodedCRACK FOUND ON THE LOWER SKIN OF THE LEFT-HAND HORIZONTAL STABILIZER AFT OF THE FWD SPAR, INBOARD OF STAB STA 138.70. APPROX 1 INCH LONG, BOTH ENDS MARKED. GROUNDED - YES. REPAIRED THE CRACK FOUND ON THE LOWER SKIN OF THE L/H HORIZ STAB I/B OF STAB STA 138.70 SDR ASAA2023062043748Fitting · corrodedAFT R/H PASSENGER DOOR CUTOUT AFT LOWER CORNER HAS CORROSION AT FR68. GROUNDED - YES. REMOVED AND REPLACED AFT R/H PASSENGER DOOR CUTOUT AFT LOWER CORNER FITTING AT FR68, STR 23R IAW A321 SRM 51-42-11.SDR ASAA2023062043641Fitting · corrodedAFT RH PASSENGER DOOR CUTOUT AFT LOWER CORNER HAS CORROSION AT FR68 GROUNDED - YES. REMOVED AND REPLACED AFT RH PASSENGER DOOR CUTOUT AFT LOWER CORNER FITTING AT FR68 IAW A321 SRM 51-42-11.SDR SWAA2023072860687Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 AT RBL 40. CRACK LENGTH:0.488' CRACK FOUND ON HORIONTAL PRESSURE DECK WEB STA 663 AT RBL 40. CRACK LENGTH:0.488'<[01] ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA 66SDR CALA2023062101972Beam · corrodedMAIN CABIN FLOOR BEAM UPPER SURFACE Y765 HAS A OUT OF LIMIT DENT AND CORROSION FR64 TO FR66 DOT 41-23 SEE LOG PAGE 4913899 FOR SIGNOFF.SDR DALA2023062105032Unknown · unknown(LOG 2824864) R/H SIDE HORIZONTAL STIFFENER CRACKED FWD. SIDE OF VAPOR BARRIER WEB RBL 6.12" - RBL 31. REMOVED R/H SIDE HORIZONTAL STIFFENER REF. BACDWG 111A1001 SHEET 116. ( CR 262129) DRILLED AND INSTALLED RH HORIZONTAL STIFFENER REF. BACDWG 111A1001 SHEET 1SDR AALA202306206189Door Frame · out of adjustAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED FORWARD LAVATORY DOOR JAMB. CHECKS OK.SDR SWAA2023081460415Stringer · crackedFWD CABIN WET AREA STRINGER CRACKED @ STA 294.5 S-8L MKD DOT<[01] ACCOMPLISHED STRINGER REPAIR AT LT FUSELAGE STRINGER 8-L FROM STA 286 TO STA 300 REF USED B737-7 SRM 53-00-03-2R-1 FIG 205 DETAIL A-A;[02] VERIFIED WORK STEPS ACCOMPLISHED FOR STRINGER REPAIR ATSDR SWAA2023071159999Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED; INCLUDNG ACROSS PREVIOUS WELD REPAIR<[01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PARTS DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT;[02] RECEIVED NEW SCUFF PLATE P/N654A0004-97 LOT#14934SDR SWAA2023071060142Angle · crackedCRACK ON ANGLE LOC. BETWEEN BS 380 TO BS 400 BL0 FWD GALLEY AREA 2023- 379035<[01] REPLACED ANGLE LOC. BETWEEN BS 380 TO BS 400 BL0 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 143A5400 SHEET 66 REV -.SEE INDIVIDUAL SIGN OFF BELOWSDR CALA2023061901917Stringer · unknownMAIN CABIN STRINGER 23RT HAS ENLONGATED HOLE FR 68-69 RT (A3NB-5 3-3-6187AFT) GENERATED AT HAECO LCQ PER NR 9292596 (22596) BY ME CH V052030 REMOVED & REPLACED RT SIDE STRINGER 23R BETWEEN FRAMES 68-69 IAW A319 SRM 51-72-11 ACCMP BY MECH V052030 INSP BY V91312SDR ASAA2023061743629Angle · corrodedACCESS DOOR 312AR FWD AT FUSELAGE FR71 AND DOOR JAMB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED DOOR JAMB ANGLE AT ACCESS DOOR 312AR AT FR71 IAW A320 SRM 51-42-11-001 REV 145.SDR R61A2023071200391Crossbeam · corrodedCROSSBEAM FR 14, RIGHT SIDE, HAS TWO AREAS OF CORROSION ON UPPER SURFACE. PERFORMED PERMANENT DOUBLER REPAIR ON CROSSBEAM 14. REF EMB SRM 53-00-10 /REPAIR 03P. SEE WIPS AND TASKS FOR WORK ACCOMPLISHEDSDR R61A2023071200390Crossbeam · corrodedCROSSBEAM FR 17, CENTER, HAS TWO AREAS OF CORROSION ON UPPER SURFACE. PERFORMED PERMANENT REPAIR BY CUTOUT AND L-ANGLE REPAIR ON CROSSBEAM FR 17 IN TWO EACH LOCATIONS IN ACCORDANCE WITH. REF SRM 53-00-10 REPAIR 03. SEE WIP'S AND TASKS FOR WORK PERFORMED.SDR SWAA2023071159809Angle · crackedMAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 RBL 10' CRACKED<[01] REMOVED MAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 RBL IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED MAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 RBL IAW SRM 51-40-05-0G-0 AND DWG 143SDR SWAA2023071059773Web · crackedCRACK WEB LOCATED FLOOR STRUCTURE BS 294.5 BL0 AND WL 208.1 AT FWD GALLEY AREA 2023-378962<[01] REPLACED WEB LOCATED FLOOR STRUCTURE BS 277 TO BS 294.5 BL0 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20SDR SWAA2023071060123Web · crackedCRACK WEB LOCATED FLOOR STRUCTURE AT BS 312 TO BS 328 RBL 32 AND WL 208.1 AT FWD GALLEY AREA. 2023-378963<[01] REPLACED WEB LOCATED FLOOR STRUCTURE AT BS 312 TO BS 328 RBL 32 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWSDR SWAA2023071060125Web · crackedCRACK WEB LOCATED FLOOR STRUCTURE AT BS 312 TO BS 328 LBL 45 AND WL 208.1 AT FWD GALLEY AREA 2023-378964<[01] REPLACED WEB LOCATED FLOOR STRUCTURE AT BS 312 TO BS 328 LBL 45 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWGSDR SWAA2023071060120Angle · crackedCRACK ON ANGLE LOCATED BTW BS 907 TO BS 927 INTERNAL STRUCTURE AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2023-378967<[01] REPLACED ANGLE LOCATED ON 907 TO BS 927 INTERNAL STRUCTURE AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM SDR SWAA2023071060132Track · crackedCRACK ON CARGO TRACK LOCATED RBL 13.84 BS 727E AT AFT CARGO COMPARTMENT 2023-378975<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] PERFORMED PERMANENT REPAIR ON CARGO TRACK LOCATED RBL 13.84 BETWEEN BS 727D TSDR SWAA2023071060126Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 727B TO BS 767 STR 25R RBL 22 AND WL 156 AFT CARGO COMPARTMENT 2023-378972<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 221859911; DUE DATE: 07 NOV 23;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 STR 25R RBL SDR SWAA2023071060127Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 727A TO BS 787 STR 25L LBL 22 AND WL 156 AFT CARGO COMPARTMENT 2023-378974<[01] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130066401; CAL DUE DATE: 21-SEP-23;[02] REPLACED SUPPORT ZEE SECTION LOCATED BTW BS 727+4 SDR SWAA2023081459503Support Bracket · crackedFWD CARGO COMPARTMENT L/H FLOOR SUPPORT BRACKET CRACKED UNDER Z CHANNEL S-26L STA 500A MKD DOT<[01] REMOVED L/H FLOOR SUPPORT BRACKET AT FWD CARGO COMP UNDER Z CHANNEL S-26L STA 500A PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACESDR SWAA2023081459504Support Bracket · crackedFWD CARGO COMPARTMENT L/H 2EA SUPPORT BRACKETS CRACKED @ S-26L STA 500C FWD & AFT OF SUPPORT FRAME MKD DOTS<[01] REMOVED L/H 2EA SUPPORT BRACKETS AT FWD CARGO COMP S-26L STA 500C FWD & AFT OF SUPPORT FRAME PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[SDR SWAA2023081459509Vapor Barrier · crackedLOWER FUSELAGE CENTER WING BULKHEAD R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED AT RBL 40 STA 663.75<[01] OK TO INSTALL NEW VAPOR BARRIER UPPER CHORD ATTACHED ANGLE.;[02] REMOVED; FABRICATED AND INSTALLED NEW R/H VAPOR BARRIER UPPER CHORD ATTACHED ANG
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