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 AALA202006049014Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE. FLIGHT DECK RIGHT HAND LATERAL WINDOW CUT OUT FRAME CRACKED AT FR 4 AT THE LOWER VERTICAL STIFFENER ATTACHMENT POINT. REPAIRED FRAME PER EO 5319Y021-002.SDR SWIA2020080751655Structure · corroded* A BAY - AFT OF FS 280 - STGR'S 18 - 21L- JOINT PLATE CORRODED. REMOVED CORROSION FROM FS280 JOINT PLATE BETWEEN STGRS 18L - 21L, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS REF REO.SDR SWIA2020080751648Structure · corroded* THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION REF CRJ700 SRM FROM THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 AT MULTIPLE LOCATIONS OF CORROSION. FOUND MULTIPLE ESDR SWIA202051647Crossbeam · corroded* THE CROSSBEAM CAP AT BS 333, LBL 27 HAD CORROSION. PERFORMED A REPAIR TO THE CROSSBEAM IAW REO. COMPLIED WITH TASK CARD.SDR IPXA2020061756698Frame · crackedINSPECTION TYPE: 2C, FWD AVIONICS COMPARTMENT LT TRANSVERS FRAME AT BS 469 WAS CRACKED. REPAIRED CRACKED FWD AVIONICS COMPARTMENT LT TRANSVERS FRAME AT BS 469.173 CANT & X=60 IAW SRM 53-10-07, REPAIR 1, FIGURE 201. MAJOR.SDR FDEA2020061011098Crease Beam · corrodedMAIN DECK STA 1605 RBL64.20 CREASE BEAM CORRODED. REMOVED CORROSION FROM MAIN DECK CREASE BEAM STA 1605 RBL 64.20, EVALUATED AREA FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL .070 REMAINING .020, REPIARED AREA OF CREASE BEAM PER SRM 53-00-13-2R REPAIR 1 FIG 2SDR FDEA2020060111098Crease Beam · corrodedMAIN DECK STATION 1605, RBL 64.20 CREASE BEAM CORRODED.SDR SWAA2020062988382Stub Frame · corrodedE/E COMPARTMENT BS 319, STRINGER 23L, STUB FRAME FWD LOWER END HAD CORROSION. REMOVED CORROSION, ORIG 'T' .040', REMAINING .033', LOSS OF .007' . FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE STUB FRAME. APPLIED CIC TO AREA IAW SRM 51-10-02-0G-0; 53-SDR SWAA2020062988383Stub Frame · corrodedE/E COMPARTMENT STA 319 S-23L L-CHORD HAS A SPOT OF CORROSION AT FWD SIDE OF STUB FRAME. REMOVED CORROSION FROM STR23L CHORD PN 141A8240-37 FOUND ORIG T .100' LOSS .042' REMAINING .058' TO BE OUT OF LIMITS IAW SRM 53-20-15-1A-1 REPAIRED CHORD IAW EA 200428 RSDR IPXA2020072057978Structure · corrodedINSPECTION TYPE:3C, CENTER TO AFT CARGO FLOOR BULKHEAD UPPER STRUCTURE WAS CORRODED AROUND FASTENER HOLES, ENTIRE LENGTH FROM LT TO RT AT BS 1841. REMOVED THE BULKHEAD CHORD, FABRICATED AND INSTALLED IN MID TO AFT CARGO IAW DWG AGA7170.SDR SWAA2020062987809Crease Beam · corrodedCORROSION ON L1 CREASE BEAM VERTICAL FLANGE AT BS 303.9, LBL 56, WL 209. REMOVED AND REPLACED L1 CREASE BEAM FROM BS 270 - 360 IAW SRM 53-10-15-01, SRM 51-10-02-0G, SRM 53-10-15-1A, SRM 51-40-02-0G, DRAWING 141A8110, REV A, SRM 51-40-05-0G, AMM 51-21-9SDR FY4Y2020009085006Support Angle · corrodedCORROSION WAS FOUND BETWEEN WING CENTER SECTION UPPER PANEL AND PRESSURE WEB SUPPORT ANGLE 65-82682-1 AT EACH BAY (FROM LBL 70 ~ RBL 70).SDR SWAA2020062987162Door Frame · crackedFORWARD CABIN, SERVICE DOOR FRAME WAS CRACKED AT TOP END. REPLACED THE DOOR FRAMEIAW AIPC 25-21-35-92 A.SDR SWIA2020080751706Stop Fitting · chafedTHE MAIN AVIONICS BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD RT STOP FITTING WAS CHAFED. NO DAMAGE ALLOWED TO THE STOP FITTING. REMOVED AND REPLACED THE STOP FITTING IAW SRM AND AMM.SDR SWIA2020080751705Stop Fitting · chafedTHE MAIN AVIONICS BAY DOOR EXTERNAL FUSELAGE SURROUND FWD LT STOP FITTING WAS CHAFED. NO DAMAGE ALLOWED TO THE STOP FITTING. REMOVED THE STOP FITTING. LOCATED AND DRILLED A NEW FITTING IAW SRM. INSTALLED THE NEW FITTING IAW AMM.SDR AALA2020061529005Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE; CRACK INDICATIONS AT FASTENER HOLES #4 AND #8 FROM OUTBOARD END ON FLOOR PRESSURE DECK PANEL AT FR 36 LEFT SIDE. REPAIRED FLOOR PRESSURE DECK PANEL PER EA 306005A AND EO 5316Y209.SDR AALA2020060219010Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK INDICATIONS AT FASTENER HOLES NR 6, 8 & 9 FROM OUTBOARD END FLOOR OF PRESSURE DECK PANEL AT RIGHT HAND FR36. REPAIRED FASTENER HOLES ON FLOOR PRESSURE DECK PANEL PER EO 5316Y209.SDR FDEA2020052961051Window Frame · gougedCAPTAIN'S WINDSHIELD FRAME WORK AT LOWER INBD SIDE, FASTENER HOLE GOUGED. ACCOMPLISHED REPAIR IAW EA 6-5310-T0353313. MAJOR REPAIR CAT C REPAIR. FUSELAGE, MAIN FRAME AND WINDSHIELD CENTER POST HOLE DOUBLE DRILLED CRACK INDICATION INTERIM REPAIR.SDR AALA2020052989012Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: SUSPECTED CRACK ON FLIGHT DECK R1 WINDOW CUT OUT UPPER OUT BOARD CORNER WINDOW FRAME AT BS 219.8 AND RBL 30 ON WINDOW POST C - D. REPAIRED WINDOW FRAME PER EA 305869.SDR AALA2020052989011Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: SUSPECTED CRACK ON FLIGHT DECK L1 WINDOW CUT OUT UPPER OUT BOARD CORNER WINDOW FRAME AT BS 219.8 AND LBL 30 ON WINDOW POST C - D . REPAIRED WINDOW FRAME PER EA 305869.SDR IPXA2020062436898Web · crackedINSPECTION TYPE:3C, UPPER CARGO COMPARTMENT L-3 DOOR FWD JAMB TORQUE BOX WEB IS CRACKED BETWEEN STA 1250 - 1256REPAIRED CRACKED L3 DOOR FWD JAMB TORQUE BOX WEB BETWEEN STA 1250-1256 IAW SRM 53-40-15 REPAIR 3 FIG 201 REV 66. (MAJOR)SDR IPXA2020061556514Door Frame · corrodedINSPECTION TYPE:4C MAIN CABIN L3 DOOR FWD JAMB HAS CORROSION IN 3 PLACES. REPAIRED MAIN CABIN L3 DOOR FWD JAMB CORROSION IAW EA 011-5340-01-A8327 REV IR AND EO MD11-5340-76829-A. (MINOR)SDR IPXA2020061556513Door Frame · corrodedINSPECTION TYPE:4C MAIN CABIN R3 DOOR AFT JAMB HAS CORROSION IN 2 PLACES. REPAIRED MAIN CABIN R3 DOOR AFT JAMB CORROSION IAW EA 011-5340-01-A8326 REV IR AND EO MD11-5340-76828-A. (MINOR)SDR IPXA2020062256822Door Frame · crackedINSPECTION TYPE:3C MAIN CABIN FLOOR R3 DOOR SURROUND FWD LOWER LIGHTNING HOLE HAS A CRACK. REPAIRED CRACKED R3 DOOR JAMB SKIN BETWEEN STA 1250-1256 IAW SRM 53-40-15 REPAIR 3 FIG 201. (MAJOR)SDR SWAA2021060280113Panel · crackedL/H MLG WHEEL WELL HAS A 9' CRACK JUST OUTBOARD OF 'A' SYSTEM RETURN FILTER. / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2.SDR SWIA2020062351142Beam · corrodedFS280 BEAM BETWEEN LBL 12 - RBL 12 IS CORRODED ON TOP AND BETWEEN THE COCKPIT AFT FLOOR SUPPORT ANGLE AND BEAM. (C-CHECK) RO 6/21/2020 REPAIRED CORROSION ON THE FS 280 BEAM, BETWEEN LBL12 TO RBL12 REF SRM, DWG. RESTORED FINISH AND APPLIED CIC TO REPAIR AREA SDR FDEA2020052621034Window Frame · gougedCAPT'S WINDSHIELD FRAMEWORK AT LOWER INBD SIDE, FASTENER HOLE GOUGED. ACCOMPLISHED REPAIR PER EA 6-5310-T0353313. MAJOR REPAIR CAT "C" REPAIR. FUSELAGE - MAINFRAME - WINDSHIELD CENTER POST HOLE DOUBLE DRILLED / CRACK INDICATION. INTERIM REPAIR.SDR KCSA202005221068Stop Fitting · crackedSTA 800 FWD DOOR STOP ASSEMBLY WEB CRACKED JUST BELOW STR 24RSDR KCSA202005221067Stop Fitting · crackedSTA 800 FWD DOOR STOP ASSEMBLY WEB CRACKED JUST BELOW STR 24LSDR IPXA2020052255639Structure · corrodedINSPECTION TYPE:SEGMCD FWD CARGO LIGHT ASSY RUSTY, FR 34-35 NUTPLATES AT CROSSBEAM 20LBL-20RBL RUSTYREMOVED CORROSION FOUND CROSSBEAM ASSY OUT OF LIMITS IAW SRM 53-10-15 FIG 105. FABRICATED ANGLE AND INSTALLED ON T/201495032 AND SRM 51-40-21.SDR AALA2020052659001Crossbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT CROSS BEAM AT FR 53 BETWEEN S38L AND S38R. REPLACED CROSS BEAM PER SRM 51-72-11.SDR CALA2020052200988Fitting · crackedBS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 15.04 CRACKED. REMOVED AND REPLACED AT BS 540 SPAR ANGLE AT LBL 15.04 CRACKED.SDR CALA2020052200987Fitting · crackedBS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 6.01 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT LBL 6.01.SDR CALA2020052200986Fitting · crackedB737-53-3-0716 STA 540 WING CENTER SECTION UPPER FRONT SPAR AT RBL 15.04 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 15.04.SDR CALA2020052200985Fitting · crackedBS 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 6.01 CRACKED. REMOVED AND REPLACED AT STA 540 WING CENTER SECTION UPPER FRONT SPAR ANGLE AT RBL 6.01.SDR VNAA2020052099921Drag Angle · cracked670-52-11-1135 (PERM REPAIR - TEMPORARY REPAIR TO PASSENGER DOOR STAIR AFT DRAG ANGLE AND AFT SIDE PANEL) COMPLY WITH PERM REPAIR PER REO INSTRUCTIONS. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE AFT WEB DRAG ANGLE, IAW CRJ700 SRM 51-40-11-001-001-A01.SDR GTIA2020052035181Window Frame · damagedRH WINDSHIELD FRAME DAMAGED RAF # 250456801.-PERFORMED PERMANENT REPAIR FOR ALL WORK PERFORMED REWF TO LTPR DO 5000999744-0010/1003177290-0010 SPIRIT EO 5311-2038. REPAIR IS CAT A PERMANENT NO RE-INSPECTION RQRD REF RDAS 80784402-003-2020SDR GTIA2020051935178Window Post · crackedRAF #2504561-2 ENTERED FOUND LH WINDSHIELD CENTER POST CRACKED.SEE NR ITEM 5000996328-0010-BOTH CONTINUITY FITTINES REPLACED. FOR ALL WORK PERFORMED PLEASE REF TO LTPR 5000996328-0010 10033173811-0010 AND SPIRIT AIRLINES EO 5311-2027SDR SWAA2021080580688Beam · crackedCRACK INDICATION ON RADIUS NEAR OF THE FIRST HOLE FROM INBOARD SIDE OF 141A6536-15 BEAM #5 AT SERVICE DOOR / REPLACED BEAM #5 AND FASTENERS ON FWD SERVICE DOOR INTERNAL AREA IAW SRM 737-700;51-40-02;51-10-02 STEP 9 AND DRAWING #141A6516 AND 141A6535 AND DOC NUSDR SWAA2021060277769Vapor Barrier · crackedRIGHT HAND MAIN LANDING GEAR FORWARD BULKHEAD AT B.S. 540 VAPOR BARRIER CRACKED IN TWO (2) LOCATIONS.PERFORMED INTERIM REPAIR PER REPAIR 57 EA-07683 FOR FURTHER CORRECTIVE ACTION REF 943 & #V005123REPETITVE ACTION REQUIRED:REMOVE ALUM FOIL TAPE AND PERFORM DETSDR SWIA2020060950972Stop Fitting · chafedTHE AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING IS CHAFED. (C-CHECK) RO 4/27/2020 REPLACED AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING REF SRM TUC4200 DUE:30-SEP-20 SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA2020060950971Stop Fitting · chafedTHE AVIONICS BAY DOOR CUTOUT SURROUND FWD LT STOP FITTING IS CHAFFED. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT LIMITS REF SRM. REMOVED AND REPLACED NEW AVIONICS BAY DOOR CUTOUT SORROUND FWD LT STOP FITTING. REF SRM.SDR AALA2020051329008Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK R1 WINDOW CUT OUT UPPER OUTBOARD CORNER C-D WINDOW POST FRAME CRACK SUSPECTED AT BS 219.8 AND RBL 30. UPON ADDITIONAL EVALAUATION NO CRACK WAS FOUND AND PREVENTATIVE MODIFICATION DOUBLER WAS INSTALLED PER EA 304963 ANDSDR AALA2020051329007Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK L1 WINDOW CUT OUT UPPER OUTBOARD CORNER C-D WINDOW POST FRAME CRACK SUSPECTED AT BS 219.8 AND LBL 30. UPON ADDITIONAL EVALAUATION NO CRACK WAS FOUND AND PREVENTATIVE MODIFICATION DOUBLER WAS INSTALLED PER EA 304961 ANDSDR AALA2020050769010Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK, RIGHT HAND #3 WINDOW CUT OUT E-F WINDOW POST FRAME #2 FASTENER HOLE CRACKED AT BS 196.5. REPAIRED WINDOW POST PER EA 304965.SDR AALA2020050769008Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK, LEFT HAND #3 WINDOW CUT OUT E-F WINDOW POST FRAME #2 FASTENER HOLE CRACKED AT BS 196.5. REPAIRED WINDOW POST PER EA 304965.SDR VNAA202005069992Former · corrodedPAX DOOR FWD FORMER AND SKIN IS CORRODED INSIDE ACCESS PANEL CUTOUT 832FL. RECEIVED NEW SERVICEABLE PAX DOOR FORMER PN:601R318031-5 LOCATED AND DRILLED UP FORMER IAW CRJ700 SRM 51-40-11-001-001-A01 REV-37 DATED AUG 15,2019.INSTALLED PAX DOOR FWD FORMER IAW SDR CALA2020051700964Pressure Panel · damagedRH FRAME 35-36 PRESSURE PANEL HOLE #''S 4, 5, 7, 9, 11, 19, 22, 25, 26, 28 & 60 REPAIRED IAW EC/RA 5331-02674. PLACE ON DIP TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5331-02674 ON OR BEFORE NOVEMBER 4, 2020. PLANNING TO CONTACT ENGINEERING AFTER OCSDR CALA2020050900932Pressure Panel · damagedLHS FRAME 35-36 PRESSURE PANEL HOLE #''S 4-11, 22, 27, 28, 35, 45 AND HOLE AT LONGITUDINAL BEAM AT Y+765 REPAIRED IAW EC/RA 5331-02673. PLACED ON DIP TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5331-02673 ON OR BEFORE NOVEMBER 4, 2020. PLANNING TO COSDR SWAA2021041575107Web · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L 31; W.L. 154. ACCESS AS REQUIRED . AND REINSTALL. / REMOVED AND REINSTALLED VAPOR BARRIER WEB BS 663 AT L.B.L 31; W.L 154 PER SRM 51-40-02; REF DWG; 111A1000; 149A7216; AND 111A1151; 111A1001 AND AMM 53-51-
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