JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous 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 = '5720' 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 = '5720' 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 CALA9802094Angle · crackedINSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED IAW SRM 51-30-2, PAGE 3 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-2, PAGE 12 AND 51-30-2 SDR CALA9802093Stiffener · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR ABXA9801147Fitting · crackedDURING C-CHECK, FOUND CENTER WING FORWARD SPAR ATTACH FITTING AT STATION 600 AND LONGERON 24R CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR DL72S982401Tip · damagedFLAP FAIRING RT WING TIP DAMAGED ON LANDING. FOUND ON INSP RT O/B AILERON AND TAB DAMAGED, NR 4 AFT FLAP AND FAIRING DAMAGED, RT WING TIP DAMAGED O/B EDGE. REPAIRED ALL.SDR CKSA98683Chord · corrodedLOWER T-CHORD OF WEB AT ZONE 500, OLES 1185 LT WING, SEVERE EXFOLIATED CORROSION EXISTS AT NOTED LOCATION MEASURES 12.0 X 1.5. REPAIRED IAW BOEING ASA CKF-EXW-121 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENSDR P2EA98280Web · crackedSJO - WEB CRACKED AT BS 663.75, RBL 0, WL 206. DEFECT SIZE LENGTH 1.5 INCH. REPAIRED CENTER WING BOX, FLOORBEAM UPPER CHORD BETWEEN BS 650 AND BS 675, BL 0 PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991, SECTION III FIG 4. (M)SDR RRXA98568Splice · misdrilledDURING MAINTENANCE VISIT, FOUND SPLICE WITH DRILL DAMAGE ON LT WING L/E AT STA XW 257. REMOVED DAMAGED SPLICE, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05507 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98565Angle · chafedDURING MAINTENANCE VISIT FOUND ANGLE CHAFED EXCEEDING ALLOWABLE LIMITS ON LEFT WING INBOARD T/E STRUCTURE AT WING STA XWS-12. REPLACED ANGLE IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05479 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR DHL9980180CDoubler · damagedAT C-CHECK, LEFT WING CENTER LEADING EDGE O/B AREA AT STA 456 FOUND DAMAGED ON SLOT L/E SIDE. TRIMMED DAMAGED I/B EDGE OF OUTER PLATING OF LEFT WING EXTENDED L/E. REMOVED DAMAGED INNER DOUBLER, FABRICATED REPAIR DOUBLER AND FILLER PER EO 18R5761050.SDR CALA9802076Cover · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER T/E HINGE COVER OF NR 3 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-20-1 AND 51-30-2, PARAGRAPH 7.SDR ASAA9880242Support · gougedLCQ - DURING 30K CHECK, GOUGES WERE FOUND ON LEFT WING NR 0 L/E SLAT OUTBOARD SUPPORT. REPAIRED IAW ASA EA 5740-01149. (M)SDR DHL9980172CBracket · crackedAT C-CHECK, LEFT WING O/B UPPER INTERIOR AREA AT STA 603 PNEUMATIC DUCT SUPPORT HOUSING IS CRACKED. REMOVED DAMAGED HOUSING BRACKET, FABRICATED NEW AND INSTALLED PER SRM 51-1-21, 4 X 6.SDR QXEA9801895Strap · gougedPDX - LEFT WING ROOT/CENTER WING LOWER SKIN JOINT STRAP GOUGED .045 DEEP AT WING STATION 1700 FUSELAGE STATION 11500. REPAIRED IAW HORIZON AIR EA 4-57-137 AND FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH C.SDR EISA98255Mount · crackedDURING ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED NR 8 SLAT ACTUATOR ATTACH MOUNT CRACKED. REPLACED NR 8 SLAT PER MM 27-33-11. (M)SDR DHL9980177CAngle · crackedAT C-CHECK, LEFT WING TRAILING EDGE I/B LOWER AREA STA XW 5, FOUND CRACKED ANGLE BEHIND WEB PANEL JUST ABOVE I/B FLAP. STOP DRILLED CRACK 25 AND FABRICATED REPAIR DOUBLER PER SRM 53-2-3, 6 X 2. INSTALLED PER SRM 53-2-0.SDR CALA9802063Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN SPAR ATTACH ANGLE OF RT WING LEADING EDGE RIB AT WS 115. THE CRACK WAS STOP DRILLED IAW SRM 51-40-3. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9802062Chord · corrodedINSPECTION FOUND RT WING LOWER CHORD CORRODED AT WS 645 TO 636. THE CORROSION WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2, PAGE 14, 51-10-2, PAGE 4 AND 51-30-10 PAGE 1.SDR DHL9980191CStiffener · crackedAT C-CHECK, LEFT WING CENTER L/E INTERIOR MID UPPER SECTION FOUND 2 INCH CRACK ON STRUCTURAL STIFFENER. REMOVED CRACKED ANGLE, FABRICATED ANGLE PER SRM 51-1-8, 2 X 1.75. INSTALLED PER SRM 51-1-2.SDR 98ZZZX4623Bottle Pin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LEFT FRONT SPAR WING TO BODY BOTTLE PIN.SDR 98ZZZX4622Bottle Pin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RIGHT FRONT SPAR WING TO BODY BOTTLE PIN.SDR MWEA981045Doubler · corrodedLEFT WING TOP TRUNNION FITTING DOUBLER WAS FOUND CRACKED. REMOVED CRACKED AREA AND INSTALLED AERODYNAMIC FILLER.SDR DL72S982324Angle · crackedLWR CHORD ANGLE 1 INCH CRACK AT FWD END BELOW NR 8 SPOILER ACTUATOR. REPAIRED PER M/M 57-20-22 FIG 806.SDR DHL9980163CSupport · crackedAT C-CHECK, WING CENTER LOWER FUSELAGE RT LOWER AREA APPROX FS 822 AT RT OF FUEL DRAIN VALVE FOUND CRACK ON ANGLE SUPPORTS. REMOVED DAMAGED ANGLE SUPPORTS, FABRICATED AND INSTALLED PER SRM 51-1-20, 5.5 X 1 X 1.SDR P2EA98246Fitting · damagedSJO - INTERNAL FITTING FOUND OUT OF LIMITS AT RT WING FRONT SPAR SECTION AS FSS 432. REPLACED RIGHT WING FRONT SPAR FITTING AT FSS 432 SRM 51-10-1 PAGE 5. (M)SDR DHL9980193CBracket · crackedAT C-CHECK, LEFT WING L/E SPAR AT XRS 456 CONDUIT BRACKET CRACKED. REMOVED AND FABRICATED BRACKET AND INSTALLED PER SRM 51-1-21, 2 X 1.SDR 98ZZZX4275Bolt · corrodedDURING A C-CHECK, CORROSION NOTED ON LEFT FORWARD WING BODY TERMINAL PIN BEARING LUG BOLT.SDR CALA9802041Doubler · crackedINSPECTION FOUND A 2.7 INCH CRACK AND DELAMINATION ON RT WING MLG SUPPORT DOUBLER. THE CRACKED AND DELAMINATED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLER AND FILLER IAW SRM 53-45-01, FIGURE 1, 51-21-01, AND ECRA 5730-01595.SDR 98ZZZX4293Web · corrodedDURING A C-CHECK, CORROSION NOTED ON RIGHT WING WBL: 203, BOTTOM WEB REAR SPARSDR UPS98828159Doubler · crackedINSPECTION TYPE-C3, RT WING L/E LWR SKIN AT XFS 598.375 THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.SDR DHL9872030DAngle · brokenAT D CHECK, L/W FALSE SPAR LOWER COVE PANEL HAS 2 EACH BROKEN SUPPORT ANGLE. REPLACED ANGLES PER SRM 51-30-02, N/R 1938.SDR UPS98828108Angle · crackedINSPECTION TYPE-D, VERTICAL ATTACHMENT ANGLE ON THE I/B SIDE OF THE NR 1 STUB WING CRACKED IN RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9753297.SDR CALA9802019Stiffener · corrodedINSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2.SDR CALA9802015Chord · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD AT WBL 135.2. THE CRACKED AREA WAS CUT OUT AND SPLICE ANGLE AND STRAPS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, ECRA 5740-01866.SDR P5CA9801584Fitting · crackedLEFT WING FLYING PANEL CRACKED FWD LEFT ATTACH FITTING. REMOVED AND REPLACED LT FLYING PANEL IAW SRM 51-10-01, RIG CHECKED GOOD IAW MM 57-20-01.SDR SWAA982683Angle · wornDURING SCHEDULED 1/4D CHECK, FOUND WORN SPOTS ON VERTICAL ANGLE JUST AFT OF LEFT GEAR CENTER DOOR FRAME. REMOVED AND REPLACED ANGLE PER BOEING SRM.SDR ABXA9801153Angle · crackedRIGHT WING LEADING EDGE, INBOARD OF STATION XW454 RIB, VERTICAL ANGLE CRACKED AT LOWER END. REPAIRED IAW DC8 SRM 51-1-21, 51-3-0 AND DWG 9755297.SDR GAIA9898Fitting · damagedDURING ROUTINE HEAVY CHECK, INSPECTION FOUND TWO PILOT HOLES ELONGATED, LOCATED AT RT MLG WHEEL WELL AREA. THE HOLES WHERE REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 57-98515-2. THE AIRCRAFT WAS THEN RETURN TO SERVICE (M)SDR DHL9980188CAngle · crackedAT C-CHECK, LT WING LEADING EDGE INTERIOR UPPER O/B AREA AT XFS 520 FOUND CRACKED. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-21.SDR DHL9980187CAngle · crackedAT C-CHECK, LT CENTER WING LEADING EDGE UPPER O/B AREA STA XFS 520 FOUND CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PER SRM 51-1-21.SDR CALA9802000Angle · crackedINSPECTION FOUND LOWER LEADING EDGE TO RIB SUPPORT ANGLE CRACKED AROUND EIGHT BOLT HEADS INSIDE L/H WING LEADING EDGE AT OUTBOARD SIDE OF RIB, FSS 121. THE RIB SUPPORT ANGLE WAS REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-1, AND 51-10-SDR DHL9980186CAngle · crackedAT C-CHECK, RT WING T/E INTERIOR AREA AT STA 463 JUST ABOVE NR 4 PYLON ON I/B SIDE FOUND CRACK ON VERTICAL ANGLE. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-1-21.SDR DHL9980185CShim · crackedAT C-CHECK, RT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 4 PYLON ON LT SIDE FOUND BROKEN SHIM ON LOWER SPAR MATING AREA. REMOVED AND FABRICATED LOWER SHIM PER SRM 51-1-21.SDR DHL9980184CAngle · crackedAT C-CHECK, LEFT WING L/E INTERIOR AREA AT STA 463 JUST ABOVE NR 1 PYLON ON I/B SIDE FOUND CRACKED ANGLE SUPPORT. FABRICATED ANGLE PER SRM 57-3-2.SDR DHL9980183CShim · crackedAT C-CHECK, LT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 1 PYLON LT SIDE FOUND BROKEN SHIM. TRIMMED AREA, WITHIN LIMITS.SDR ABXA9801067Doubler · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRED IAW ABX REA D957-25131MR.SDR VJ9800618Vane · corrodedLT WING CENTER FIXED VANE FLAP L/E CORRODED. REPLACED FIXED VANE IAW DC9 MM 27-51-3. FIT AND FAIRED, OPS CHECKED GOOD IAW DC9 MM 27-51-3.SDR UPS98828060Doubler · crackedINSPECTION TYPE-C, 3 RT WING L/E LWR SKIN AT XFS 570.75, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.SDR P2EA98185Fitting · crackedSJO - RIGHT WING SPAR FITTING CRACKED AT FSS 525, DEFECT SIZE LENGTH=1 INCH. REPLACED FRONT SPAR FITTING PER SRM 51-10-01 PAGES 5 AND SRM 51-30-2. (M)SDR UPS98828155Fitting · crackedINSPECTION TYPE-C, 3 RT WING T/E, THE WING JACK POINT FITTING IS CRACKED AT THE UPPER END. REMOVED AND REPLACED THE WING JACK POINT FITTING IAW SRM 51-1-20D AND 51-3-0.SDR UPS98828058Angle · crackedINSPECTION TYPE-C, 3 RT WING L/E RIB AT XW 256, ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 9753294 AND SRM 51-1-20D.
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