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 SWAA2022020969812None · bentSTRINGER CLIP BENT BS480 STR24L / STRINGER CLIP BENT AT B.S 480 STR 24L 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'SDR SWAA2022020935546Angle · corroded***CORROSION***FWD CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT ANGLE HAS CORROSIO N IN MULTIPLE PLACES AT STA.490 TO 500I / AFTER EVALUATION OF CORROSION DAMAGE ON THE FWD CARGO L/H FLOOR TO SIDEWALL SUPPORT STA 490-500I; FOUND TO BE OUT OF LIMITS DUE TO CSDR FDEA201802200433Door Frame · wornMAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FOR COMPLY WITH EA 1-5310-T0338478 REV NO. POS P1. REAMED HOLE ON THE FIRST TWO LUGS ON THE FWD A/C FUSELAGE SIDE HINGE FITTING OVER THE CMM REPAIR LIMITS OF .462. NE DIAMETER OF LUGS BORE IS .470, SDR SWAA2022020969813None · bentSTRINGER CLIP BENT BS480 STR 23L / STRINGER CLIP BENT AT B.S480 STR 23L'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'SDR DALA2018021901030Door Frame · corrodedCORROSION ON THE L2 AFT DOOR FRAME, BS 729.6, STRINGERS 19L - 20L, THE DOOR FRAME WAS FOUND TO BE OUT OF LIMITS WITH 100% MATERIAL LOSS. REPAIRED THE DOOR FRAME IAW ERA 556482-14, REV ORIGINAL.SDR SWAA2022020835544Angle · corroded***CORROSION*** L/H FLOOR TO SIDEWALL SUPPORT ANGLE HAS CORROSION IN MULTIPLE PACES IN THE AFT CARGO COMPARTMENT AT STA. 727W TO 847 / CORROSION ON LH FLOOR TO SIDEWALL SUPPORT ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED FLOOR TO SIDSDR SWAA2022020835545Angle · corroded***CORROSION*** R/H FLOOR TO SIDEWALL SUPPORT ANGLE HAS CORROSION IN MULTIPLE PLACES AT STA.727W+10 TO 767 / REMOVED CORROSION IN AN AREA OF 1.3'W X 1'L X .018'D ORIGINAL THICKNESS WAS .040 MAX ALLOWABLE REMOVAL IS .004' FOUND TO BE OUT OF LIMITS IAW SRM 53-00SDR IPXA2018030427106Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR R61A201803010262Crossbeam · corrodedFWD FUSELAGE WET AREA FRAME 17 IN FRONT OF SERVICE DOOR RIGHT SIDE CORRODE. FOUND CORROSION TO BE GREATER THAN 10 % OUT OF LIMITS, CUT OUT DAMAGED PORTION, FABRICATED AND TRIMMED TO SIZE EXTRUSION AND FILLER REPAIR, INSTALLED NEW EXTRUSION AND FILLER IAW SSDR R61A201803010260Crossbeam · corrodedCORROSION FOUND AT CENTER OF FORWARD FUSELAGE FRAME 14 CROSSBEAM. REPAIRED THE CROSSBEAM IAW SRM 53-00-10.SDR R61A201803010257Beam · corrodedCORROSION ON THE L2 DOOR LOWER BEAM UNDER FWD ESCAPE SLIDE FITTING. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-08.SDR R61A201803010255Beam · corrodedAFT WET AREA LT BEAM AFT OF FRAME 90 IS CORRODED. COMPLIED WITH ETD2018-170-020644, INSTALLED A DOUBLER AND FILLER.SDR R61A201803010251Beam · corrodedAFT WET AREA LT BEAM AT FRAME 87 IS CORRODED. PERFORMED A DOUBLER, FILLER REPAIR IAW SRM 53-23-10.SDR R61A201803010248Beam · corrodedAFT WET AREA RT BEAM AT FRAME 87 IS CORRODED. PERFORMED DOUBLER/FILLER REPAIR IAW SRM 53-23-10.SDR ASOA201802167015Structure · crackedDURING A C-CHECK INSPECTION, FOUND THE LATERAL FRAME ABOVE THE FIRST OFFICER`S WINDSHIELD SIDE POST WAS CRACKED. REPAIRED IAW ETD 2018-145-016753.SDR DALA2018021600935Door Frame · delaminatedFOUND SEVERE DELAM CORROSION. AFT RT CORNER OF AFT LAV SVC DOOR FRAME. COMPLIED WITH ERA 482821-14 REV A. RECEIVED FINAL ERA 48281-14 REV A. COMPARED TO PRI 482821-14 REV A. REV 2. PRI MATCHES ERA.SDR SWAA2022021022978Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 277-294; R.B.L. 2; W.L. 208. / REMOVED AND REPLACED INTERCOSTAL AT BS 277-294; RBL 2 WL 208 PER SRM 51-40-02 AND DWG # 141A5400SDR SWAA2022021022979Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 312-328; R.B.L. 33; W.L. 208. / REMOVED AND REPLACED INTERCOSTAL BS 312-328; RBL 33; WL 208 IAW SRM 51-40-02 AND DWG # 141A5400.SDR SWAA2022021022980Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 312-328; L.B.L. 47; W.L. 208. / REMOVED AND REPLACED INTERCOSTAL AT BS 312-328; LBL 47; WL 208. PER SRM 51-40-02 AND DWG # 141A5400SDR DALA2018021600992Box Beam · crackedRT SIDE BOX BEAM, HFEC FOUND TWO AFT 1/4 INCH FASTENER HOLES WITH CRACK INDICATIONS IN BOX BEAM FLANGE. REPAIRED IAW AMDS 5310-01450-04B.SDR UIEA2018021400218Structure · damagedDURING POST FLIGHT WALK AROUND INSPECTION, MX FOUND DAMAGE ON AFT FUSELAGE FWD OF APU AREA. REPAIRED IAW EO 6753A652, REVISION 1, PART 2.SDR IPXA2018021526553Floorbeam · crackedMAIN CABIN FLOORBEAM AT FRAME 79, Y1580 FOUND CRACKED. REPAIRED IAW EO A300-5310-67272-A.SDR ABXR2018021400135Fitting · corrodedUPPER CARGO RBL 77 TO RBL 88, PRESSURE DECK FITTING CORROD AT BS 955.SDR 7C7A2018021400367Window Frame · corrodedCORROSION DAMAGE LOWER RT CORNER OF CO-PILOT WINDSHIELD FRAME, BLENDED AND REPAIRED IAW RD 8-53-15558 AND ECO 008.56-18.01.SDR AALA201802229023Beam · corrodedCORROSION FOUND ON LAV L74 AFT MOUNT AREA ON INBOARD AUXILIARY BEAM. REPLACED AUXILIARY BEAM IAW SRM 51-42-11.SDR AALA201802209014Doubler · corrodedCORROSION FOUND ON THE DOUBLER CONNECTOR LOCATED AT FRAME 11, Y=+25.4. REPLACED CONNECTOR IAW DWG 170-13808-001, DWG 170-00825-503, & SRM.SDR CALA2018021600632Failsafe · crackedBS 955 RT FAILSAFE STRAP FOUND CRACKED. THE FAILSAFE WAS REPAIRED IAW EA 5340-01478, REV C, OP 04.SDR AALA201802149014Stop Fitting · wornWEAR ON THE STOP FITTING ON THE DOOR CUT OUT, FRAME 26 + 5 INCHES IN THE FORWARD CARGO BAY. REPLACED THE STOP FITTING IAW SRM 51-72-11, AND D53231761.SDR UIEA2018021400220Step · crackedMID CREW ACCESS LADDER THREAD ASSY, NR 5 STEP FOUND CRACKED. REPAIRED IAW RI-25-50-12454, REV A.SDR SWIA201844411Doubler · corrodedDOUBLER AT SERVICE DOOR FRAME BS 349, STRINGER 18R AND DOUBLER AND LOWER FRAME BRACKET AT BS 319.7, STRINGER 18R CORRODED. REPLACED THE DOOR FRAME BRACKETS AND RESTORED FINISH TO DOUBLERS IAW SRM.SDR ABXA20180211015Door Frame · corrodedCORROSION ON THE AFT DOOR FRAME WEB OF THE FORWARD LOWER CARGO DOOR. THE WEB WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20180211013Door Frame · corrodedCORROSION ON FORWARD DOOR FRAME OF FORWARD LOWER CARGO DOOR UNDER FORWARD LOWER STOP. THE DOOR FRAME WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR AALA201803079034Fitting · crackedCRACK INDICATATION ON WINDHSIELD CENTER POST CONTINUITY FITTING, RIGHT LOWER ATTACHEMENT. BETWEEN FRAMES 1 & 2, BL 0. REPLACED THE FITTING IAW EA 277567.SDR AALA201803079028Fitting · crackedCRACK INDICATION ON WINDSHIELD CENTER POST CONTINUITY FITTING, LEFT LOWER ATTACHMENT AREA IN COCKPIT. PERFORMED A PERMANENT REPAIR ON THE CENTER POST, THE CONTINUITY FITTING WAS REPLACED IAW EA 277567.SDR DALA2018021600979Grill · corrodedCORROSION ON FRAME GRILL R1. THE FRAME GRILL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG.201.SDR ASAA2018020923530Window Frame · crackedMAJOR REPAIR ON RT NR 3 WINDOW FRAME REPAIR. GROUNDED - YES. C/W SDR AND MAJOR REPAIR TRACKING ONLY FOR T/C SB737-2345-NG-1R.SDR DALA2018020900805Failsafe · crackedDURING UT INSPECTION, FOUND A CRACK INDICATION ON THE RT BS 955 FAILSAFE STRAP. THE FAILSAFE WAS REPAIRED.SDR SCNA20180208040Post · crackedDURING NDT INSPECTION OF RT NR 1 FLIGHT DECK WINDOW, FOUND CRACK INDICATION AT UPPER OUTBD CORNER, MARKED. REPAIRED RT NR 1 FLIGHT DECK WINDOW POST.SDR SCNA20180208039Post · crackedDURING NDT INSPECTION OF LT NR 1 FLIGHT DECK WINDOW, FOUND CRACK INDICATION AT UPPER OUTBD CORNER, MARKED. REPAIRED LT NR 1 FLIGHT DECK WINDOW POST.SDR DALA2018020800804Failsafe · crackedDURING A HFEC OPEN HOLE INSPECTION, FOUND A CRACK AT BS 955, ON THE FAIL SAFE STRAP. THE FAIL SAFE WAS REPAIRED IAW AD 2012-09-04.SDR SWAA2018022219999Web · corrodedAFT CARGO BAY DOOR THRESHOLD SUB WEB CORRODED BETWEEN BS 794 TO BS 847, UPPER SURFACE. R&R SUB WEB IAW SRM & DWG.SDR VNAA2018020799907Web · corrodedRIGHT, BS 280 LOWER WEB FOUND TO BE CORRODED BEYOND LIMITS IAW REO 670-53-11-052, REV A. REMOVED AND REPLACED THE WEB IAW SRM 53-11-10-201-004-A01.SDR SWAA2018030720268Beam · crackedR1 DOOR CUTOUT UPPER FORWARD STUB BEAM FRAME CRACKED. R & R THE STUB BEAM IAW SRM AND DWG.SDR QXEA2018020700040Flange · crackedPILOTS BULKHEAD KICKPLATE FLANGE CRACKED. THE KICKPLATE FLANGE WAS REPAIRED IAW SRM 53-10-25.SDR C77A20180206001Crossbeam · corrodedINSPECTION DISCOVERED THE FORWARD FRAME 14 CROSSBEAM, CORRODED. REPAIRED THE CROSSBEAM IAW DRAWING AND SRM.SDR QMLA2018020518013Angle · crackedDURING A 12 MONTH INSPECTION, FOUND A CRACK APPROX 1.5 INCHES LONG ON THE RT FORWARD MAIN GEARBOX DECK AT THE TRANSITION TO THE CABIN ROOF ABOVE THE NR 4 BULKHEAD. THE CRACK IS LOCATED IN THE RADIUS OF THE DOUBLER THAT MAKES THE TRASITION. REPAIRED IAW SRM 51SDR SWAA2018022019878Crease Beam · corrodedLT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747. R&R WEB IAW DWG AND SRM.SDR SWAA2018021919736Stub Frame · crackedR1 DOORWAY STUB FRAME CRACKED AT BS 295, STRINGER 17R. R & R THE STUB FRAME IAW SRM.SDR DALA2018020400644Pan · crackedCRACK ON RING PAN AFT LOWER CORNER BS 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R-1, FIG 202.SDR DALA2018020400643Pan · crackedCRACK ON RING PAN FWD LOWER CORNER BS 446 . REPAIRED PER B717 SRM 56-20-02-2R-1 FIG 202 . LONG CRACK 0.100" INCH. (LP #0410120)
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