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 AALA202506196868Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND CONTINUITY FITTING RH SIDE WINDSHIELD. CRACK LE NGTH 0.200 INCH. VERTICAL DIRECTION. MAINTENANCE PERFORMED TIME LIMITED REPAIR ( REPLACED CONTINUITY FITTING) R/H SIDE WINDSHIELD LOCATED BTW FR1 TO FR3 AT LEVSDR AALA202506196913Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND CONTINUITY FITTING LH SIDE WINDSHIELD. CRACK LENGTH 0.200 INCH.VERTICAL DIRECTION. MAINTENANCE PERFORMED TIME LIMITED REPAIR ( REPLACED CONTINUITY FITTING) L/H SIDE WINDSHIELD LOCATED BTW FR1 TO FR3 AT LEVELSDR AALA202506196969Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION RH SIDE WINDSHIELD CENTER POST (LOWER BOLT). CRACK LENGTH 0.115 IN CRACK DIRECTION 7 OCLOCK. MAINTENANCE PERFORMED TIME LIMITED REPAIR OF MIRROR FITTING REPAIR RH AND HOLE B BUSH LOC ON CENTER WINDSHIELD FRAME SDR AALA202506191639Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION LH SIDE WINDSHIELD CENTER POST (LOWER BOLT). CRACK LENGTH 0.188 INCH. CRACK DIRECTION 3 O'CLOCK. MAINTENANCE PERFORMED TIME LIMITED REPAIR LH OF MIRROR FITTING REPAIR AND HOLE B BUSH LOC ON CENTER WINDSHIELD FRASDR DALA2025030501742Door Sill · corroded(LOG 0839105) DURING H-CHECK INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE AFT GALLEY DOOR LOWER MAIN SILL R/H INNER CHORD (PN 147A8540-30) AT BS 967 AND RBL 45. CORROSION REPAIRED PER ERA 624587-14.SDR LR7A2025030303735Riser Panel · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5323, FOUND LH FS477 BULKHEAD RISER PANEL CRACKED AT LBL67-LBL69, WL156-WL160. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0480.SDR LR7A2025030303734Tee Fitting · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5712, FOUND RH CENTER WING CWS174.3R VERTICAL SPLICE TEE CRACKED AT LOWER EDGE, FS517, WL269. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0421.SDR LR7A2025030303733Tee Fitting · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH CENTER WING CWS174.3L VERTICAL SPLICE TEE CRACKED AT LOWER EDGE, FS517, WL258. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0420.SDR LR7A2025030303731Angle · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC3211, FOUND LH MLG WHEEL WELL FS517 CHINE ANGLE CRACKED AT LBL61, WL142. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-27. NR# 0378.SDR LR7A2025030303719Chine · corrodedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS737.0E-FS817.0E CARGO FLOOR LH CHINE CAP AT TIEDOWN RING WELL CORRODED, LBL60, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0265. / PSE# 53-40-11, AD 2SDR SWIA202504280302Flange · corrodedCORROSION FOUND ON ATTACHING FLANGE OF INTERCOSTAL P/N SH670-32075-4 BETWEEN FS349-364 RIGHT OF STGR27. (29725888) (C-CHECK RO 04/26/2025)REMOVED AND REPLACED INTERCOSTAL BETWEEN FS349-364 RIGHT OF STGR27 P/N SH670-32075-4. REF. CRJ900 SRM 51-42-06-001-001-A0SDR IPXA2025031727544Angle · corrodedAPU INLET DOOR UPPER FWD CORNER ANGLE S-3R HAS CORROSION.REMOVE AND REPLACE 1 EACH S-3R CORNER SUPPORT ANGLE (P/N: 148N3141-6) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS.TREATED AND PRIMED ANGLE IAW SRM 51-20-01 P/N ALODINE11SDR R61A2025032300155Beam · corrodedDURING HEAVY CHECK MAINTENANCE FOUND AFT SERVICE DOOR LOWER BEAM REST HAS LEVEL 2 CORROSION. REPLACED SEAL REST IAW SRM 51-41-01SDR IPXA2025031727556Angle · corrodedAPU INLET DOOR LOWER ANGLE BETWEEN STA 1787.45 TO STA 1825.00 HAS CORROSION. INSTALLED 01EA ANGLE. IAW B757-200 SRM 51-40-02. RIVET P/N: MS20470AD6-10, BATCH: 0004366677. (24EA) PAINT P/N: PG-6-BR54K4Q, BATCH: 0004332931.PAINT CUP: 02-012-176. SEALANT: 04-001SDR IPXA2025031827619Angle · corrodedAPU INLET DOOR LOWER FWD CORNER ANGLE S-6R HAS CORROSION.REMOVED LOWER FWD ANGLE IAW B757-200PF SRM 51-40-02-0G-0.REMOVE AND REPLACE 1 EACH S-6R CORNER SUPPORT ANGLE (P/N: 148N3141-5) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTSDR CALA2025031002651Door Frame · crackedB757-52-3-0109 - CRACK ON FWD FRAME R2 DOOR UPPER GUIDE ARM CUTO UT. SFR FLAGGED. UPDATE INSPECTION ITEM ESFR ENTRY ALL INSPECTIONS ACCOMPLISHED AT STENGINEERING IN PNS AS IAW B757-200 SRM 52-10-02 -2R-1 REPAIRED R2 DOOR FWD FRAME UPPER HINGE IAW B757-200 SRM SDR DALA2025030301632Repair · corrodedSHIP 6708 CORROSION ON PREVIOUS REPAIR DOUBLERS 2EA OF DECK PLATE BTW STA 1710-1720 BL0-RBL50 AND 1EA ON STA 1680 AND LBL10-LBL45 AT PASSENGER CABIN (W4). DOUBLERS 2EA OF DECK PLATE BTW STA 1710- 1720 BL0-RBL50 AND 1EA ON STA 1680 AND LBL10-LBL45 AT PASSENGESDR AALA202504242982Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON DOOR FRAME LOC. BTW FR67 TO FR68 AT LEVEL STG8 LH AFT GALLEY AREA, CRACK L=0.134 INCH.SDR AALA202504089626Lintel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON LINTEL LOC. BTW FR66 AND FR68 AT LEVEL STGR 8L UPPER FUSELAGE, MEASURE OF CRACK L= 0.135 IN. MAINTENANCE REPLACED LINTEL LOC. BTW FR66 AND FR68 AT LEVEL OF STGR 8L UPPER FUSELAGE, IAW A319 SRM 51-42-11-801 AND DWG D53480SDR SWAA2025040100172Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF USING BMS 4-17 TY6 LOT#1594495-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK4FA2417A/A; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2025SDR SIMA20250227001Doubler · corrodedSSI 53-23-018 WASTE DOOR CUTOUT INTERIOR SUPPORT CORRODED (LEVEL 2 CORROSION) REMOVED AND INSTALLED SERVICABLE WASTE DOOR CUTOUT INTERNALSUPPORT AND SHEAR CLIPS IAW EMB 170 SRM 51-40-08SDR IPXA2025031482551Strap · corrodedFAULT:STR ZONE 300 APU INLET DOOR AT STA 1787.45 FWD STRAP HAS CORROSION. REPLACE 1 EACH APU INLET FORWARD STRAP AT STA 1787.45 (P/N: 148N3138-20) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS. INSTALLED NUTPLATE ON STRAP AND ISDR YENA2025030300215Door Frame · crackedDURING HEAVY MAINTENANCE: MAIN CABIN L2 DOOR FRAME FR68 AT STOP FITTING #1 #3 HOLE HAS A CRACK; (RESOLVED ON W/O: 1355989 TASKCARD: NR-00006) REF GSO-HAECO WO# 169006 NR 32433. REPAIRED L/H FRAME 68 AT L-2 #1 STOP FITTING IAW A320 SRM 53-41-12-300-011. REVISIOSDR DALA2025022801568Threshold · fodSHIP 6812 1R DOOR "SLIDE" LIGHT DOESNT COME ON AFTER ARMING THE DOOR. CORRECTIVE ACTION: REMOVED DEBRIS FROM 1R DOOR THRESHOLD AREA. ALL OPS AND INDICATIONS NORMAL. (6346766)SDR FDEA202502270303Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR66, BETWEEN -Y953 AND -Y1456 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE FR66 BETWEEN -Y953 AND -Y1456 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS SDR FDEA202502270302Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR67, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS CASDR SWI2025F00738Window Frame · crackedCO-PILOT SIDE POST LWR OTBD HOLE CRACKED (C-CHECK RO 06/23/2025) INSTALLED NEW CO-PILOT SIDE WINDOW POST REF CRJ200 SRM 51-42-21 AND DWG# 601R33007 REV-U. CAL TOOL TORQUE SCREWDRIVER TUC9692 DUE 31-MAR-25 C/W 51-900-1003-SKYSDR SWIA202507210225Window Frame · crackedCOPILOTS UPPER WINDOW SUPPORT STRUCTURE HAS POSSIBLE CRACK (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW CO-PILOT WINDSHIELD POST UPPER FRAME P/N CC670-33470-4 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-0SDR SWAA2025032699648Strap · crackedCRACKED FASTENER HOLE FOUND AT LH BS639 STUB BEAM STRAP; AFT LOWER HOLE; O/B TITANIUM LAYER; PROPAGATING IN THE AFT DIRECTION.<[01] 'REFER TO EA 25-153-00450 WHICH IS ATTACHED TO FAULT TTG8Q00YVL59.';[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] TASK CARDSDR SWAA2025032699647Strap · crackedCRACKED FASTENER HOLE FOUND AT RH BS639 STUB BEAM STRAP; AFT LOWER HOLE; O/B TITANIUM LAYER; PROPAGATING IN THE AFT DIRECTION.<[01] 'REFER TO EA 25-153-00450 WHICH IS ATTACHED TO FAULT TTG8Q00YVL59.';[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] TASK CARDSDR DALA2025030201586Stanchion · cracked(LOG 0829147) DURING INSPECTION, A CRACK WAS FOUND RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAMES OF THE LH (P/N 141A8811-3) AND/OR RH (P/N 141A8811-4) NO. 1 DECK WINDOWS.REPAIRED PER ERA 619132-14.SDR DALA2025030201585Window Frame · cracked(LOG 0829143) CRACK INDICATION FOUND ON THE INNER CORNER RADIUS AND ON THE INTERNAL SURFACE OF RADIUS AREA OF THE NO 1 LH WINDOW FRAME. PERFORMED PERMANENT REPAIR ON N1 LH WINDOW FRAME AS PER ER/A 619132-14ADTR.SDR AALA202502281991Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL PLATE JUST AFT OF THE FORWARD GIRT BAR FITTING AT FR 66 AND S23L. REPAIRED SILL PLATE PER SRM 53-41-14-283-002.SDR N6WA2025022605Door Frame · corrodedLOWER LH PAX DOOR POST AT FS280.00 CORRODED. PERFORMED REPAIR ON LH LOWER DOOR POST AT FS280.00 IAW EO- C550-53MR-053.SDR AALA202502267258Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND WINDSHIELD CENTER POST AREA AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 360681.SDR SWAA2025032698984Pressure Deck · crackedA177-001 HORIZONTAL PRESSURE DECK WEB STA 665; RBL 43; WL 202 HAS A .50' CRACK IN WEB. VERIFIED WITH HFEC AND MARKED ENDS IN BLACK.<[01] 04 - REPAIRED HORIZONTAL PRESSURE DECK WEB BETWEEN RBL 38.5 TO RBL 60 AND BETWEEN STA 663.75 TO STA 675PER [SRM 53-40-51-2RSDR AALA202502266315Window Frame · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND WINDSHIELD FRAME CENTER POST AREA AT FR 2 AND Y0 NEEDS TO BE MODIFIED (MIRROR FITTING / POCKET MACHINING) PER EA 360681. MODIFISDR AALA202504258159Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLES AT FR 36 BETWEEN -Y1292 AND -Y1523. REPAIRED PRESSURE DECK MEMBRANE PER EA 362547.SDR SWI2025F00474Stop Fitting · groovedAFT CARGO DOOR OPENING ON FS574.00 UPPER AND LOWER STOPS GROOVED. (C-CHECK RO 04/17/2025) REMOVED DAMAGE AT AFT CARGO DOOR OPENING ON FS574.00 UPPER AND LOWER STOPS,. FOUND OUT OF LIMITS. REPAIRED PER REO 601R-53-61-8306, REV --, 2025-03-17. FITS AND CLEARANCESDR AALA202502284467Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BEAM AT FR 66 AND S23L. REPAIRED SILL BEAM PER SRM 53-41-14-283-002.SDR YENA2025022500208Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) (ON DOOR STOP FITTING 7 HOLE 1 FR16LH. LENGTH 0.100 INCH. CRACK DIRECTION 9 O’CLOCK ); REF AEROMAN NR 2025 – 29477, W/O: 2025 13/1 PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LSDR YENA2025022500207Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 1 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 3 O’CLOCK; REF AEROMAN W/O: 2025 13 / 1, NR 29476, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DOSDR YENA2025022500206Door Frame · crackedDURING HEAVY MAINTENANCE:CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 3 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 6 O’CLOCK.; REF AEROMAN W/O: 2025 13 / 1, NR 29478, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DOSDR YENA2025022500202Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND DOOR STOP 1 HOLE H3 FR68LH. CRACK DIRECTION 11 OCLOCK . CRACK LENGTH 0.100 INCH; REF AEROMAN WO 2025 13/1 NR 2025-29474; ACCOMPLISHED THE REPAIR OF THE CRACK DAMAGE FOUND ON THE REAR FUSELAGE FR68 LHS ( NEAR STRSDR YENA2025022500201Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC UPPER CORNER .CRACK DIRECTION 1 O'CLOCK. CRACK LENGTH 0.250 INCH.REF AEROMAN WO 2025 13/1 NR 2025-29453; ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACK DAMAGE ON THE LH WINDSHISDR YENA2025022500200Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC LOWER CORNER .CRACK DIRECTION 5 O'CLOCK. CRACK LENGTH 0.500 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29454; ACCOMPLISHED THE PSDR YENA2025022500199Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND CONTINUITY FITTING WINDSHIELD RH SIDE . CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29455; ACCOMPLISHED THE PERMANENT RSDR YENA2025022500195Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2025022500194Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH AND STGR 22 / DOOR STOP FITTING #1 / LOWER INBD HOLE / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)SDR SIMA202503262001Doubler · corrodedCOCKPIT FLOOR STRUCTURE UPPER SURFACE CORRODED BETWEEN FRAMES 11-12, ON CO-PILOTS SIDE INBD SEAT TRACK BEAM. (MAJOR REPAIR) REPAIRED COCKPIT FLOOR STRUCTURE UPPER SURFACE BETWEEN FRAMES 11-12 ON CO-PILOTS SIDE INBD SEAT TRACK BEAM IAW ERS-EM-53MR-5156
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