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 IPXA1666677Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR AT STA 785.9, RBL 10.94 VERTICAL STIFFENER FOUND CRACKED. VERTICAL STIFFENER REPAIRED IAW SRM 57-10-10-2R2. REPAIR 2, FIG 201, REV 49 JUST AT STA 785.9, RBL 10.94 ORG MAT'L BAC1518-912-2024T3511 CRACK LESDR IPXA1666676Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT CTR TANK FRONT SPAR AT STA 785.9, RBL 32.94 VERTICAL STIFFENER FOUND CRACKED. VERT STIFFENER REPAIRED IAW SRM 57-10-10-2R2. REPAIR 2, FIG 201, REV 49 AT STA 785.9, RBL 32.94 ORG MAT'L BAC1518-749-2024T3511 CRACK LENGTH IS SDR USAA2011060600009Strut · corrodedSAL - S4 - CORROSION ON INTERNAL CAVITY OF INTERCONNECTING STRUT AT RIGHT WING AT WS 486 RIB 9. REPLACED INTERCONNECTING STRUT AT RIGHT WING AT WS 486 RIB 9 IAW A319 AMM 27-51-44.SDR WRLA20110506479Spacer · crackedCRACK: LT WINGLET AFT FITTING SPACER PN: ARB7602-3 CRACK, NRC U05087 ISSUED.SDR WRLA20110506477Fitting · crackedRT LOWER WINGLET FWD FITTING CRACKED.SDR MASA2011050602628Bolt · looseFUEL LK LEFT WING; TIGHTENED LOOSE BOLT AT LEFT I/B FLAP HINGE BOX, O/B FWD FITTING.SDR SWAA113345Structure · crackedDURING SCHEDULED 22Y CHECK, FOUND CRACK FUEL TANK OF RIGHT WING, LWR CHORD, WBL 135.50, STR 2 TO STR 3. REPAIRED PER DOC.SDR FDEA201104231593Fairing · missingAFTER FLIGHT, A FAIRING WAS DISCOVERED MISSING ON LT WING, UNDERSIDE, OTBD OF AFT PART OF THE ENGINE PYLON. NEW FAIRING INSTALLED AS PER AMM 57-20-35 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112SDR UALA2011042101937Heat Shield · damagedHEAT SHIELD HAS DAMAGE. REPLACED HEAT SHIELD PER MM.SDR EE4Y1104008Plate · crackedRT WING T/E AT XCW 47.45 DEBRIS DEFLECTOR PLATE CRACKED. REPLACED THE PART.SDR NOCA20110112001Angle · crackedSUPPORT CAP CRACKED LEFT WING L/E CAVITY LES 550.10. REMOVED LOWER CHORD P/N 114T2207-5 AND LOWER NUT PLATE ANGLE DRILLED UP NEW ANGLE AND PRIMED. INSTALLED NEW ANGLE AS DRAWING 114T2207 AND PER SRM 57-41-04.SDR LR7A2011041900189Angle · crackedDURING SCHEDULED C-9 CHECK, FOUND RT UPPER CW NR 7 STRINGER SPLICE ANGLE LAYER CRACK AT CWS217. REPAIR ACCOMPLISHED BY REPLACING ANGLE IAW LOCKHEED SMP583 CHAP 51-60 & 51-70.SDR KGBR20110411337Structure · corrodedLEFT WING, CENTER SECTION, AREAS OF TRAILING EDGE OVER FLAP REMOVED, WS 1963-2200 AND WS 3296-3497, SAME AREAS HAVE SEVERE CORROSION (LEVEL 2).SDR V0XR201104060016Strip · cracked(V0XR) RT INBOARD LEADING EDGE WING-BODY ATTACHMENT IS CRACKED. REMOVED AND REPLACED RIB STRIP. W/C 6039SDR V0XR201104060015Attach Angle · broken(V0XR) LT LOWER NR 4 WING FAIRING ATTACHMENT ANGLE IS BROKEN. REMOVED AND REPLACED ANGLE. W/C 5064SDR NOCA03711Flange · wornFLANGE WORN NR 1 ENGINE INBD SIDE OF PYLON ACCESS PLATE 416BR CUT OUT FLANGE 5 O'CLOCK POSITION WORN GOUGED. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT TO CHECK FOR CRACKS NO DEFECTS FABRICATE FILLERS THICKNESS AND PROFILE TO MATCH DOUBLER CUTOUTS CHEM-FILM TRESDR U2RA227DHN042Angle · corrodedINBD LANDING FOR WING ACCESS PANEL NR 611JB HAS CORROSION AT FWD SECTION.SDR ASAA1149488Angle · chafedRIGHT WING TRAILING EDGE UPPER ANGLE I/B OF AILERON IS CHAFED. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 57 51 90 AND SRM 51 40 02.SDR NOCA03411Angle · crackedLEFT WING STA 550 NR 4 SLAT INBD OF INBD TRACK ANGLE CRACKED. REMOVED OLD ANGLE PER SRM 51-10-02. DRILLED UP NEW ANGLE AND INSTALLED AS PER SRM 51-20-05.SDR NOCA03211Angle · crackedLT WING STA 500 UNDER SLAT NR 5 OUTBOARD SIDE OF OUTBOARDD TRACK ANGLE CRACKED. REMOVED AND DRILLED REPLACMENT ANGLE AS PER SRM 51-10-22.SDR NOCA02911Angle · crackedANGLE CRACKED, WING FIXED L/E AT NR 5 SLAT O/B DRIVE ROD CUTOUT. REMOVED ANGLE AND DRILLED UP REPLACMENT ANGLE AS PER SRM 51-10-02. REPLACED ANGLE AS PER SRM 51-10-02.SDR C2XA11TY037Structure · damagedTYS - A/C WAS EN ROUTE TO BNA FROM EWR WHEN LIGHTNING STRUCK THE A/C. THE A/C LANDING AT BNA WITHOUT ANY INCIDENT. MAINTENANCE COMPLIED WITH TASKCARD 6232012, WHICH IS THE LIGHTNING STRIKE TASKCARD. THE A/C WAS THEN FERRIED TO TYS WHERE MAINTENANCE REMOVED ASDR ASAA1179326Support Beam · crackedLEFT WING PANEL 551GB SUPPORT BEAM CRACKED. REMOVED AND REPLACED SUPPORT BEAM IAW B737 700 SRM 51 40 02 AND BOEING DWG 115A2714.SDR ASAA1179325Plate · crackedLEFT WING LOWER TRAILING EDGE WIGGLE PLATE IS CRACKED AT RSS270. REMOVED AND REPLACED WIGGLE PLATE IAW B737 700 SRM 51 40 02, 51 30 01, 51 40 05, B737 700 AMM 51 21 99 300 801 BOEING DWG 115A2782 115A2793.SDR HNAA2011042400092Plate · crackedLADDER PLATE CRACKED AT RT WING STATION YW139.00. CRACKED SECTION OF LADDER PLATE, CUT AND REMOVED AS REQUIRED. WORK DONE IAW RD8-57-2375. EDDY CURRENT AND ULTRASONIC INSP, REQUIRED ON CUTOUT LOCATION, NO CRACKS NOTED, NO DEBOND DETECTED IAW RD 8-57-2375.SDR HNAA2011041200076Plate · crackedLADDER PLATE CRACKED AT RT WING STA YW139.00. REPAIRED CTR WING LADDER PLATE AT YW139.00 AND STR 6 IAW RE8-57-5044.SDR HNAA2011042400094Panel · corrodedCORROSION FOUND ON PANEL 623AT AND WING LADDER PLATE. REMOVED CORROSION FROM PANEL 623AT AND WING LADDER PLATE. BOTH ARE FOUND TO BE WITHIN LIMITS IAW -8-300 SRM CHAPTER 57-00-16. ALODINE IAW CHAPTER 51-20-16.SDR HNAA2011042400088Panel · corrodedCORROSION FOUND ON PANEL 523AT AND WING LADDER PLATE. REMOVED CORROSION FROM PANEL 523AT AND WING LADDER PLATE IAW RD8-57-455. NDT IAW RD8-57-455. NO CRACKS NOTED.SDR COEA2011031446805Panel · corrodedHEAVY CK COE / LEVEL 2 CORROSION: PANEL 623GT HAS LEVEL 2 CORROSION. REMOVED AND REPLACED PANEL PER ATR SRM.SDR ASAA1149268Angle · crackedLEFT WING STIFFENER JUST FORWARD OF THE NR 2 AILERON HINGE IS CRACKED APPROX RSS543. REMOVED AND REPLACED STIFFENER IAW B737 400 SRM 51 40 02.SDR COEA2011031445805Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: RIGHT WING ACCESS DOOR CUTOUT FOR PANEL 622CT CUT OUT HAS CORROSION (LENGTH 2.3", WIDTH .260", DEPTH .034"). REWORKED AREA IAW ATR STRUCTURAL REPAIR INSTRUCTIONS AND SRAS DO/TS-1529/05, 3169 ISSUE C.SDR COEA2011031444805Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: WING CUTOUT FOR PANEL 521DT HAS AREAS OF LEVEL 2 CORROSION (LENGTH 7.5", WIDTH 5.55", DEPTH .010"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS DO/TS-1529/05, 3169 ISSUE C.SDR A6WA201140245Track · mislocatedFOUND TRACK RIVET AT LT OTBD L/E LOCATION TOO CLOSE TO SCREW HOLE. REPAIRED IAW REO 601R-57-41-747.SDR ASOA201100477Support Bracket · crackedSUPPORT BRACKET BETWEEN LT WING INBD AND CTR L/E'S IS CRACKED ON OTBD UPPER CORNER. R & R SUPPORT BRACKET BETWEEN LT WING INBD AND CENTER L/E'S IAW SRM 51-41-02 AND 51-45-00.SDR COEA2011031142805Web · crackedHEAVY CK COE / MAJOR REPAIR: LT WING LEADING EDGE PANEL 514 INNER TWO WEBS ARE CRACKED UPPER INBOARD AREA. REPAIRED PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS DO/TS-420/11-6253.SDR ZZDA2011306Attach Angle · corrodedRIGHT WING LOWER T/E PANEL, FWD OF MLG SIDE BRACE ATTACH ANGLE, CORROSION. ACCOMPLISHED ATTACH ANGLE REPLACEMENT PER B717 SRM 51-70-11 REPAIR 1.SDR USAA2011031191026Skate Angle · wornCLT - Q5 - MAJOR REPAIR - LEFT WING LOWER SURFACE SKATE ANGLE HAS 7 WORKING FASTENERS JUST INBOARD OF PYLON AT WBL 183. REPLACED LEFT WING LOWER SURFACE SKATE ANGLE IAW TYPICAL REPAIR 737-5740-10-0301 PART B.SDR SIMA201106705Attach Angle · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE, SECOND ONE AFT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW ATTACH ANGLE IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASAA1159146Bracket · crackedLEFT WING TRAILING EDGE VERTICAL WEB CRACKED ON FORWARD SIDE AT FASTENER HOLES. REMOVED AND REPLACED CRACKED BRACKET IAW B737 700 SRM 51 40 02. NO DAMAGE TO WEB.SDR FDEA201103030841Angle · corrodedLEFT WING REAR SPAR ATTACHMENT, VERTICAL ZEE ANGLE IS CORRODED AT BOTTOM WBL 85, REMOVED CORRODED SECTION OF ZEE ANGLE IAW SRM REV 103 51-10-1. FABRICATED FILLER, 2 REPAIR DOUBLERS AND 2 SHIMS IAW SRM 51-40-4 FIG 1. INSTALLED REPAIR PARTS ON LT WING REAR SPSDR IPXA1M65421Angle · crackedINSPECTION TYPE:3C, IN LT WING L/E COMPARTMENTAT XOS 792, FWD AREA, ANGLE IS CRACKED. FABRICATED AND INSTALLED REPAIR AT XOS792 LT WING L/E REF EO MD11-5720-41805-A AND STA, SA, EA 011-5720-01-A2942.SDR FDEA201103010803Support Angle · crackedRT WING T/E AREA 1 EA SUPPORT ANGLE CRACKED POSITION UNDER NR 3 SPOILER INBD SIDE. REMOVED DAMAGED ANGLE AND MADE REPAIR PART OF ANGLE IAW DWG A57240073 PN A57240073201. INSTALLED NEW SUPPORT ANGLE WITH FASTENERS IAW SRM 57-51-11 AND 51-72-10.SDR FDEA201103010802Support Angle · crackedLT WING UPPER T/E FIXED PANEL 1EA SUPPORT ANGLE GOT CRACKED AT NR 4 SPOILER OTBD HINGE. REMOVED DAMAGED ANGLE AND MADE REPAIR PART OF ANGLE IAW DWG A57240194 PN A57240194201. INSTALLED NEW PART OF ANGLE WITH FASTENERS IAW AB6 SRM 57-51-11 AND 51-72-10.SDR FDEA201103010801Support Bracket · crackedRT WING T/E AREA 1EA SUPPORT BRACKET CRACKED POSITION UNDER NR 3 SPOILER INBD SIDE. REMOVED DAMAGED BRACKET AND MADE REPAIR PART OF BRACKET IAW DWG A57240071, PN A57240071-201. INSTALLED NEW BRACKET WITH FASTENERS IAW SRM 57-51-11 AND 51-72-10.SDR IPXA1M65385Beam · chafedINSPECTION TYPE:3C, LT WING T/E INBD BEAM CAP FWD FLANGE CHAFING INTERM REPAIR TRANSFERRED FROM LOG PAGE 615637. DEF 438237 ACCOMPLISHED REPAIR IAW EO MD11-5720-40406-D.SDR ASAA1149337Panel · damagedRIGHT TRAILING EDGE CLOSE OUT PANEL IS CHAFED AND DENTED. FABRICATED REPLACEMENT PANEL AND INSTALLED IAW B737 400 SRM 51 40 05.SDR FDEA201102220674Panel · corrodedLT WHEEL WELL SLANT PANEL HAS SURFACE CORROSION ALONG THE LOWER EDGE IN SEVERAL AREAS. R & R LOWER SECTION OF SEAL RETAINER, REF SRM 51-35-01 AND 51-33-01.SDR FDEA201102220673Angle · corrodedLT WHEEL WELL SLANT PANEL INBD VERTICAL "L" ANGLE IS CORRODED AT LWR EDGE. R & R "L" ANGLE, REF SRM 51-35-01.SDR COEA2011022231805Structure · corrodedHEAVY CHECK / COE / LEVEL 2 CORROSION / MAJOR REPAIR: REMOVABLE WING CUTOUT FOR PANEL 522CT HAS CORROSION (LENGTH 7.5", WIDTH 5.55", DEPTH .015"). REPAIR PER STRUCTURE REPAIR INSTRUCTIONS FROM ATR.SDR COEA2011022230805Panel · corrodedHEAVY CHECK / COE / LEVEL 2 CORROSION: PANEL 523GT MATTING FLANGE HAS CORROSION (LENGTH 11.85", WIDTH 7.85", DEPTH .012"). REMOVED AND REPLACED PANEL WITH OEM PART IAW ATR72 SRM.
Back to JASC 5720