JASC 5714
Service difficulty reports · 1,451
Reports filed under 5714 · Wing, Center Box, 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 = '5714' 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 = '5714' 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 UPS02438338Spar · crackedINSPECTION TYPE:C RT BS 990 FRONT SPAR WEB ONE EACH FASTENER HOLE COMMON TO BATH TUB FITTING CRACK REVEALED AT FRONT SPAR WEB LAYER FOR DETAIL PLS REFER ATTACHED SKETCH. RT BS 990 FRONT SPAR WEB CRACKED HOLE OVERSIZED TO 0.660" AND FREEZE PLUG INSTALLED AND DSDR UPS02438307Skin · corrodedINSPECTION TYPE:C M/D - WING CENTER SECTION SURFACE FOUND CORRODED. WING CENTER SECTION CORRODED SKIN REPAIRED AT BS 1220 LBL 97 AS PER RS R57-14-34799.SDR EIA2002018Structure · corrodedMZJ-EAC - FOUND CORROSION AT STATION 1238, RBL 2, ON CENTER WING TANK SKIN. REPAIRED PER ECRA 482-57-149-2. (M)SDR EIA2002005Spar · corrodedMZJ - FOUND CORROSION ON REAR SPAR WEB OF WING CENTER SECTION BS 1241 BULKHEAD FITTING. CORROSION REMOVED AND WORK ACCOMPLISHED PER SB 747-57-2263/EO 57--747-1544-99 (A).SDR UPS02437413Structure · corrodedINSPECTION TYPE:SP CENTER WING BOX UPPER SKIN HAS EXFOLIATION CORROSION APPROX 4 INCHES IN DIAMETER STA 1110, RBL 104. REPAIRED AREA IAW ENGINEERING FILE 747-57-20016.SDR UPS02437412Angle · crackedINSPECTION TYPE:SP STA 1140 ON RT SIDE UNDERNEATH SECOND FLOOR PNL, I/B AND BENEATH DUCTING A 2 INCH CRACK WAS FOUND AND CORROSION ON CTR WING BOX.SDR ASAA0210027Web · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND WING CENTER SECTION UPPER SKIN AT BS 565-569, LEFT BUTTOCK LINE 53 CORRODED. REPAIRED PER EA. (M)SDR 2002F00172Angle · crackedFOUND CENTERWING FRONT SPAR SUPPORT ANGLE IS CRACKED AT BS 538 RBL 8. (M)SDR DHL2001801547Angle · crackedCENTER WING BEAM LOWER SUPPORT ANGLE CRACKED 1 INCH AT STA 683 XCW 23 R. REMOVED CRACKED SUPPORT ANGLE PER SRM 51-1-20 PG 21. FABRICATED NEW SUPPORT ANGLE PER SRM 53-2-0 PG 1-2. INSTALLED NEW SUPPORT ANGLE PER SRM 51-1-20 PG 9.SDR DHL2001801556Fitting · crackedCTR WING (MAIN CARGO COMPT) FITTING CRACKED 1 IN AT STA 381.000 XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AERA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-120D PG 9.SDR DHL2001801559FittingCENTER WING (MAIN CARGO COMPT)FITTING CRACKED 1 IN AT STA 759.000, XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.SDR DHL2001801557FittingCENTER WING FITTING CRACKED AT STA 717.XCW 23 L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PERSRM 51-1-20D PG 9.SDR QXEA0101649Web · crackedPDX - CENTER WING FORWARD WING BOX AT STATION YW02.858 AND X374.500 THERE IS A CRACK IN THE WEB. REPAIRED IAW RD 8-53-5437.SDR DHL2001727594Spar · damagedON "C" CHECK DISCREPANCY. WING CENTER SECTION AFT. SPAR LOWER CHORD APPROX. 15 RBL. RIVET HEAD BROKEN ON VERTICAL LEG OF CHORD.SDR 2001F00409Clip · crackedWING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP (SMALL ANGLE) CRACKED AT BS 870 AND BBL 0. REMOVED AND REPLACED ATTACH CLIP IN WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD BS 870 AND BBL 0 AS PER B727 SRM 51-30-2. (M)SDR DL73K011140Doubler · crackedINSPECTION OF THE LONGITUDINAL FLOORBEAM AT RBL 24 ABOVE THE CENTER WING BOX REVEALED A CRACK IN THE REINFORCING DOUBLER OF THE BEAM WEB AT FS 678 ADJACENT TO A CABLE CUTOUT.SDR AWXA0002055Angle · crackedD: Cabin center wing box area lower attach angle cracked STA 674 RBL 45C: Repaired cabin center wing box area lower attach angle B.L 45R BS 674 IAW ER 155715-01200 OL3SDR MWEA010783Fitting · crackedCENTER WING FORWARD SPAR LOWER ATTACH FITTINGS TO PRESSURE BULKHEAD WEB AND FUSELAGE SKIN IS CRACKED IN RADIUS. FUSELAGE STATION 606 ABOVE LONGERON 24 LEFT. REMOVED CRACKED FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING.SDR 01FDEA00344Web · corrodedDURING ROUTINE INSP CTR WING BOX FOUND CORRODED AT BS 870 NEXT TO LWR SPAR CHORD. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5710-57245.SDR 01FDEA00343Angle · corrodedDURING ROUTINE INSP CTR WING BOX AFT SPAR LWR CHORD ANGLE FOUND CORRODED. R&R PER 727 SRM 57-10-1 FIG 3, 51-10-2.SDR ABXA010201Angle · corrodedAN L-ANGLE AT FS 637 LBL 44 THROUGH LBL 54 WAS CORRODED ON THE UPPER SIDE OF THE CENTER FUEL TANK PANEL. MAINTENANCE REPAIRED THE AREA IAW DC-9 SRM 51-30-1, 51-30-5 AND DOUGLAS DRAWING 5910464.SDR DHL2001705511Stiffener · corrodedAT C-CHECK- WING CENTER SECTION STA 870 WEB VERTICAL STIFFENER AT BL 0 HAS CORROSION. REMOVED WEB VERTICAL STIFFENER AT WING CENTER SECTION FOR REPLACEMENT AS PER B727 SRM 51-30-2. INSTALLED NEW VERTICAL STIFFENER AT CENTER SECTION BS 870 BL 0 AS PER B727 SRSDR 01FDEA00245Stiffener · corrodedDURING ROUTINE INSP THE VERTICAL STIFFENER AT LBL 14 ON THE AFT SIDE OF THE CTR WING TANK FOUND CORRODED 2 IN FROM TOP OF THE STIFFENER.SDR UPS01235623Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND LBL 13 WEB AS PER B 7SDR UPS01235622Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOWER CENTER WING AT BSSDR UPS01235621Web · crackedINSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WEB LOWER CENTER WING SDR C2XA01IA157Structure · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE STRUCTURE AT FRAME 29A LEFT IN THE WING BOX WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRUCTURE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA156Structure · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE STRUCTURE IN THE WING BOX AT FRAME 29A RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRUCTURE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA150Intercostal · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE WING BOX INTERCOSTAL AT STRINGER 1 LEFT WAS FOUND TO BE CRACKED BETWEEN FRAMES 23 & 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED INTERCOSTAL IN ACCORDANCE WITH ATR42-320 SRM 51-25-01, AND THE AIRCRSDR UPS01235254Stiffener · corrodedINSPECTION TYPE:C+SI, ON REMOVAL OF CENTER SECTION REAR SPAR UPPER CHORD SEVERAL STIFFENERS FOUND DAMAGED AND CORRODED. REPLACED STIFFENERS IAW 51-30-02 AND DWG 65C21531.SDR UPS01235263Structure · crackedINSPECTION TYPE:C+SI, X-RAY REPORTS SUSPECT CRACKS AND CORROSION IN WING CENTER SECTION AT WBL 70.5 UPPER RT AREA AT BS 870. REPAIRED IAW SMRO EO 2001-006-016.SDR UPS01234894Frame · corrodedINSPECTION TYPE:C, RIVET POPPED AND EVIDENCE OF CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870. REPAIR CARRIED OUT IAW SRM 51-30-02 & SRM 51-20-4 AND DRAWING 65C215 66.SDR G2L2001F00000Angle · crackedDURING VISUAL INSPECTION PERFORMED IN CONJUNCTION WITH FUEL TANK SEALING ON B707 AIRCRAFT, TWELVE(12) SUPPORT ANGLES WERE DISCOVERED CRACKED AT THE TOP OF THE WING CENTER SECTION ATTACH. FRONT SPAR STIFFENERS AT FS 600K, WL195, R/L BL 7,13,20,28,35,42. SIMILSDR USAA002144Structure · crackedCLT - FOUND T-CAP AND WEB CRACKED 6 INCHES, STATION 663, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M)SDR LR7A00211Fitting · crackedDURING SCHEDULED C2 CHECK PER JOB CARD HST5713, FOUND RT CENTER WING LWR RAINBOW WING JOINT FITTING CRACKED AT THE 6TH HOLE FROM THE FWD EDGE, CWS 220. REPLACED FITTING IAW LAC MEA 382-57-00-137.SDR DHL200080733CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 4 FITTING CRACKED 1 INCH AT STA 680.000 BL -0. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PG 9. REF: N/R 1611.SDR DHL200080731CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 5 FITTING CRACKED 1 INCH AT STA 759.000 BL 24R. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PG 9. REF: N/R 1620.SDR DHL200080730CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 3 FITTING CRACKED 2 INCHES AT STA 781.500 BL 24L. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA IAW 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PG 9. REF: N/R 1619.SDR DHL200080703CFitting · crackedWING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 5 FITTING CRACKED 1 INCH AT STA 717.750 BL 24R. REMOVED CRACKED FITTING AT STA 717.750 BL 24R, CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING PER SRM 51-1-20 PAGE 9.SDR DHL200080743CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 5 FITTING CRACKED 1 INCH AT STA 742.250 BL 24R. REMOVED CRACKED FITTING IAW SRM 51-1-20D, PG 21, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20SDR SWAA001792Beam · corrodedDURING SCHEDULED D-CHECK, FOUND CORROSION ON RT WING MLG SUPPORT BEAM LOWER SURFACE AROUND HOLES 12 & 21. REPAIRED BEAM PER ER 00-1020.SDR CA010912004Frame · cracked(CAN) WHILE HAVING NDT PERFORMED TO COMPLY WITH AD CF-97-07 REV.2, WING TO FUSELAGE FRAME ANGLE INSPECTION, THE LT FRONT OUT BOARD ANGLE WAS FOUND CRACKED. ANGLE WAS REPAIRED IN ACCORDANCE WITH DRAWING 215-53-10-54 PAGES 2,3 & 6. THE AIRCRAFT HAD ACCUMULATED ASDR AU000550Drain Line · blocked(AUS) WING CENTRE SECTION CAVITY DRAIN BLOCKED BY WAX BUILDUP. LARGEAMOUNTS OF DEBRIS FOUND IN AREA. FOUND DURING INSPECTION IAWAD/B747/71.SDR 00FDEA00436Splice · corrodedDURING ROUTINE INSP, THE CENTER WING AFT UPPER SPAR SPLICE AT BS 870, RBL 70.5 FND CORRODED BEYOND ALLOWED LIMITS. R&R PER IAW SRM 51-30-2.SDR UPS00433289Skin · corrodedINSPECTION TYPE:C, RT WING L/E BULGING ON L/E LOWER FALSE WORK PANEL AT OLES 1430 AND 1532. REPAIRED IAW QUERY NOTE 13 /2000 AND SRM 57-30-03 FIG 9. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER.SDR LR7A00121Attach Angle · crackedDURING SCHEDULED C2 INSPECTION, FOUND CENTER WING RT AFT MINOR BOLT ATTACH ANGLE CRACKED IN LOWER RADIUS AT RH CWS 220.0. REPAIRED IAW SRM SMP 583-57-30-23. NR 39336.SDR UPS00832583Cap · crackedINSPECTION TYPE:C-2, STA 857 CENTER WING TANK UPPER CHORD CRACKED AND CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW SPAR CAP IAW SRM 51-1-20D & 51-1-21.SDR UPS00432861Frame · corrodedINSPECTION TYPE:C, CORROSION ON RT WING LWR SKIN IN SPAR EXTENSION AT FS 770. CORROSION CLEANED UP, FILLER FABRICATED AND FITTED PER Q/NOTE 18/00.SDR UPS00432860Frame · corrodedINSPECTION TYPE:C, CORROSION ON LWR WING SKIN AT FS 790 UNDER LWR CHORD. CORROSION BLENDED OUT, FILLER FABRICATED AND FITTED REFERENCE Q/NOTE 18/00.SDR ABXA000249Tank · corrodedDURING D-CHECK, FOUND AFT EDGE OF UPPER CENTER TANK PLATING CORRODED AT STATION XCW 20. REPAIRED IAW ABX REA D957-36744.
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