JASC 5310
Service difficulty reports · 38,548
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 DALA2014112206314Door Frame · corrodedCORROSION ON LOWER STRUCTURE OF CARGO DOOR FRAME BS 1155-1212 AND LONG 28R. NEW SPACER WAS INSTALLED IAW SRM 53-05, FIG 123 AND 51-30-5.SDR USAR201411260003Door Frame · cracked(BP069) PRESSURIZATION LEAKAGE, ENTRANCE DOOR, FATIGUE CRACK FOUND ON THE UPPER AFT CORNER CLOSURE.SDR USAR201411260002Door Frame · cracked(BP069) PRESSURIZATION LEAKAGE, ENTRANCE DOOR, FATIGUE CRACK FOUND ON THE UPPER FORWARD CORNER CLOSURE.SDR USAR201411260001Door Frame · cracked(BP069) PRESSURIZATION LEAKAGE, ENTRANCE DOOR. FATIGUE CRACK FOUND ON THE LOWER CORNER CLOSURE.SDR DALA2014112806285Crease Beam · corrodedMAIN CABIN CREASEBEAM CORRODED BETWEEN BS 1140-1160 RT SIDE, OUT OF LIMITS, FABRICATED REPAIR AND INSTALLED.SDR UHLA2014111900824Finger Doubler · corrodedCORROSION FOUND ON FWD CARGO AFT FINGER DOUBLER. REPAIRED THE AFT FINGER DOUBLER IAW ETD 2014-170-095748.SDR UHLA2014111900814Splice · corrodedCORROSION FOUND ON LEFT SHEAR PLATE TO FUSELAGE SPLICE PLATE. R & R THE SPLICE FRAMES 86-87.SDR SWAA2014120134535Window Frame · crackedRIGHT NR 1 FLIGHT DECK WINDOW FRAME TOP OTBD CORNER CRACKED. R & R FRAME IAW ACO.SDR SWAA2014120134534Window Frame · crackedRIGHT NR 1 FLIGHT DECK WINDOW FRAME TOP OTBD CORNER CRACKED. R & R FRAME IAW ACO.SDR SWAA2014120934871Window Frame · crackedLEFT NR 1 WINDOW FRAME CRACKED. REPAIRED WINDOW IAW EA.SDR ASAA2014111809865Window Frame · crackedCOCKPIT L1 WINDOW OTBD UPPER CORNER FRAME IS CRACKED. ACFT GROUNDED. REPAIR OF WINDOW FRAME ACCOMPLISHED ON SB737-53-1336NG800-1, OPS 9955. .SDR ASAA2014111809864Window Frame · crackedFLIGHT DECK R1 WINDOW FRAME UPPER OTBD CORNER HAS A CRACK. ACFT GROUNDED. REPAIR OF WINDOW FRAME ACCOMPLISHED ON SB737-53-1336NG800-4.SDR USAR201411210001Door Frame · cracked(BL094) PRESSURIZATION LEAKAGE: FATIGUE CRACK FOUND ON THE UPPER FORWARD CORNER CLOSURE.SDR DALA2014111806143Crossbeam · damagedAFTER REMOVE PROFILE WAS FOUND ELONGATED HOLES ON CROSSBEAM LOCATED AT LEVEL OF FRAME 56 AND BETWEEN STR 42R TO STR 38L IN AFT CARGO COMPARTMENT. REPLACED CROSSBEAM IAW SRM 51-72-11 AND DWG D534-70320.SDR QXEA2014120100954Door Frame · corrodedEMERGENCY EXIT DOOR SURROUND STRUCTURE HAS CORRODED GUSSET AT STA X88.200, PN 85329446-115. REMOVED GUSSET, PN 85329446-115, REF SRM 51-42-15 5.G. 1THRU 2 D & 51-42-05 4.E.1 THRU 8). LOCATED & DRILLED NEW GUSSET, PN 85329446-115 IAW SRM 51-40-07. INSTALLESDR DALA2014111906304Beam · corrodedCORROSION ON SEVERAL POINTS OF DOOR FRAME LOWER BEAM BS 660-678 IN THE MID CARGO BAY. THE DOOR FRAME BEAM WAS REPAIRED IAW SRM 53-05, FIG 123 AND ER/A 530126-14, REV ORIGINAL,SDR DALA2014111906303Beam · corrodedCORROSION ON REPAIR DOUBLERS OF DOOR FRAME LOWER BEAM IN THE MID CARGO BAY. BEAM REPAIRED IAW SRM 53-05, FIG 123 AND ER/A 530126-14, REV ORIG.SDR DALA2014111806142Door Frame · crackedDURING INSPECTION, FOUND CRACK ON E/E BAY DOOR FRAME. REPLACED IAW SRM A320 51-72-11 AND DWG D52279040.SDR DALA2014111806141Door Frame · crackedDURING INSPECTION, FOUND CRACK ON E/E BAY DOOR FRAME. REPLACED IAW SRM A320 51-72-11 AND DWG D52279040.SDR DALA2014111806140Door Frame · crackedDURING INSPECTION, FOUND CRACK ON DOOR FRAME OF E/E DOOR. REPLACED THE DOOR FRAMES IAW SRM 51-72-11 AND DWG D52279040.SDR ASOA2014120911856Fitting · corrodedCORROSION ON LT SIDE OF NOSE JACK FITTING SUPPORT BS 365.280. FOUND AREAS TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-101-001-A01, NEW SERVICEABLE SUPPORT TO BE INSTALLED. REMOVED CORRODED SUPPORT FITTING, INTERCOSTAL, IAW SRM 51-42-06-001-001-A01 & 51-42-21SDR ASOA2014120511830Structure · corrodedCORROSION ON CIRCUMFERENTIAL JOINT FS280-282.86 BETWEEN STR 26 R-25R. REMOVED CORROSION AT STA 280 STRG25L-27 IAW SRM 51-21-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORROSION FROM CIRCUMFERENTIAL JOINT AT FS280-282-.SDR QXEA2014120100952Door Frame · corrodedEMERGENCY EXIT DOOR SURROUNDING STRUCTURE HAS CORRODED RIB AT STA X71.300, PN 85329513-101. EVALUATED THE EMERGENCY EXIT DOOR SURROUND RIB EDGE, PN 85329513-101 AFTER REMOVAL OF MODERATE CORROSION WITH LIGHT PITTING. ORIGINAL MATERIAL THICKNESS IS 0.063", RESDR QXEA2014120100951Door Frame · corrodedEMERGENCY EXIT DOOR SURROUNDING STRUCTURE HAS CORRODED RIB AT STA X94.800, PN 85329513-102. EVALUATED THE EMERGENCY EXIT DOOR SURROUND RIB EDGE, PN 85329513-102 AFTER REMOVAL OF LIGHT SURFACE CORROSION, NO PITTING FOUND. ORIGINAL MATERIAL THICKNESS IS 0.063"SDR ASAA2014111409821Support · corrodedFWD CARGO BAY AFT BULKHEAD LT SUPPORT RAIL IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, CORROSION IS EXFOLIATED IAW SRM 53-00-53. REMOVED SUPPORT RAIL ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT RAIL ANGLE IAW SRM 51-SDR SWAA2014120434669Window Frame · crackedRIGHT NR 1 FLIGHT DECK WINDOW CRACKED. R & R FRAME IAW AMM.SDR SWIA201440281Structure · damagedUPON REMOVAL OF FASTENERS FOR CORROSION REMOVAL FOUND ONE HOLE ELONGATED LOCATED ON LOWER AFT FUSELAGE, BS 559.47, RIGHT OF STR 27. REPAIRED.SDR DALA2014111506182Beam · corrodedCORROSION ON BEAM BETWEEN BS 1220-1231 AND LONGERON 28R AT AFT CARGO BAY. CORROSION REMOVED, AREAS TREATED AND PAINTED, CIC WAS APPLIED IAW SRM 51-10-3, PAR. 26, 21, 14 AND 38.SDR ASOA20141114335Door Frame · corrodedDURING C-CHECK CARGO DOOR FWD FRAME CORRODED. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR FWD FRAME IAW SRM 51-40-02 AND EC5230-01349. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20141114334VDoor Frame · corrodedDURING C-CHECK, CARGO DOOR AFT FRAME CORRODED, LOCAL LEVEL 2 AT NUTPLATE. MAINTENANCE PERFORMED REPAIR OF CARGO DOOR AFT FRAME AT NUTPLATE IAW EC5230-01349 UP TO AND INCLUDING FINAL STEP 2.1,2.7. INSTALLED REPAIR IAW SRM 51-40-02. THE ACFT WAS APPROVED FORSDR SWAA2014112634501Crease Beam · corrodedRIGHT CREASE BEAM CORRODED AT STATION 950 TO 990, WL 208. REPAIRED CREASE BEAM IAW SRM.SDR CALA2014111492702Crease Beam · corrodedCORROSION ON GUARD AT CREASE BEAM STATION 287.0 RBL 81. R & R NEW CREASE BEAM AT BS 287.0 RBL 81 IAW SRM 51-40-02 PAR 7 FIG 1 DUE TO 100 PERCENT MAT LOSS PN 141T8310-410 PO 435783.1.SDR DALA2014111306112Vertical Beam · corrodedCORROSION ON VERTICAL BEAM, LT SIDE OF NOSE WHEEL WELL STRUCTURE AT ATTACHMENT TO BS 377.7, FRAME, LOWER END OF VERTICAL BEAM, FOUND OUT OF LIMITS IAW SRM. INSTALLED NEW BEAM IAW DWG 141N9940, REV C.SDR ERAA201411120069Window Frame · corrodedCORROSION REMOVAL NOT PERMISSIBLE AT THIS LOCATION IAW RD8-53-6323 FOR CABIN WINDOW FRAMESDR SWIA201440257Rib · gougedREAR PRESSURE BULKHEAD FORWARD FACE UPPER RIB BETWEEN DOOR TRACK AND FUSELAGE GOUGED. C-CHECK, RO 11/30/14, REPAIRED SUPPORT BRACKET, RIB, PN 601R36008-175 ON FS 621 BULKHEAD LT SIDE REF REO. ALL STEP COMPLIED WITH.SDR SWAA2014121535021Window Frame · crackedFLIGHT DECK LT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW ACO.SDR SWAA2014121535020Window Frame · crackedFLIGHT DECK RT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW ACO.SDR SWIA201440078Structure · crackedAFT CARGO BAY AT BS 605 HAS A CRACK AT CARGO DOOR. PERFORMED CUT OUT OF DAMAGED AREA ON FLOOR LANDING PLATE AT FS 605.0, REF REO. PERFORMED ET INSP ON REWORKED AREA AND UNDERLAYING STRUCTURE IAW REO. NO DEFECTS NOTED, BTAC NDT-9, TOUCHED UP REWORKED AREA RSDR R61A201411101176Rib · crackedDURING HEAVY CHECK, LT RIB 52 INBD RIB WEB CRACKED ON BOTTOM SIDE. MX R & R IAW SRM 57-42-01. REFERENCE NRWC FOR WORK DETAILS. PN 170-24656-003, RIB.SDR ASOA2014111311637Structure · damagedDAMAGE NOTED ON REPAIR MADE TO UPPER LT WING ROOT. COMPLIED WITH GREO 601R-53-41-341SDR USAR201411130004Structure · cracked(BL064) UPON INSPECTION OF THE ENTRY DOOR CLOSURE AREA, CARGO DOOR, A FATIGUE CRACK WAS NOTED ON THE AFT LOWER PORTION OF THE SILL AREA.SDR SWIA201440069Floor Skin · crackedTRU BAY FLOOR SKIN IS CRACKED AT BS 193. REPAIRED TRU BAY FLOOR SKIN IAW REO.SDR DALA2014111006043Door Frame · crackedDURING INSPECTION, FOUND LT OVERWING FRAME AT BS 674 CRACKED. R & R LT OVERWING FRAME IAW AMDS WC NR 5310-01436-03A.SDR R61A201411091167Fastener · corrodedDURING HEAVY CHECK, 9 FASTENERS ON OTBD SIDE OF STR 28R BETWEEN FRAMES 88-89 NEXT TO WASTE BOX ARE CORRODED. MX R & R 9 FASTENERS ON OTBD SIDE OF STR 28R BETWEEN FRAMES 88-89 NEXT TO WASTE BOX IAW SRM 51-41-02.SDR SWAA2014120434668Window Frame · crackedRIGHT NR 1 FLIGHT DECK WINDOW FRAME UPPER OTBD EDGE CUT OUT CRACKED. R & R FRAME IAW ACO.SDR SWIA201440031Pressure Deck · crackedPRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND LBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.SDR R61A201411081165Doubler · corrodedDURING HEAVY CHECK, INTERNAL DOUBLER AT WATER SERVICE PANEL UNDER AFT LAV FLOOR IS CORRODED. MAINTENANCE COMPLIED WITH SB R170EO-53-10-00-0020, REMOVED AND DISCARDED POTABLE WATER PANEL INTERNAL DOUBLERS.SDR DALA2014110906010Door Frame · crackedDURING OVERWING FRAME INSPECTION IAW AD 14-05-22/SB 717-53A0034, THE LT OVERWING FRAME WAS FOUND TO BE CRACKED AND REQUIRED REPLACEMENT. DURING REMOVAL OF THE FRAME, IT WAS FOUND THAT LONGERON 11L AFT MOST END INTERFERES WITH REMOVAL OF THE STA 674 LT FRAME, SDR CA150508014Reinforcement · cracked(CAN) CRACK FOUND ON RT REINFORCEMENT PLATE, STEEL. BULKHEAD UNDER THE REINFORCEMENT PLATE CRACKED AS WELL. CAUSE UNKNOWN BUT MANY CYCLES DONE IN THE LAST 20 YEARS BECAUSE OF GLIDER TOWING.SDR CA150508013Reinforcement · cracked(CAN) FOUR CRACKS FOUND IN 4 REINFORCEMENT PLATES, STEEL, RT & LT, FWD & AFT OF LANDING GEAR BULKHEAD ASSEMBLY. BULKHEAD UNDER THE REINFORCEMENT PLATES CRACKED AS WELL. CAUSES UNKNOWN BUT MANY CYCLES DONE IN THE LAST 20 YEARS BECAUSE OF GLIDER TOWING.
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