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.

SDR QXEA0100622Attach Angle · crackedYYC- LEFT HAND WING INBOARD TRAILING EDGE UPPER ATTACH ANGLE TO 5280 BEAM IS CRACKED. REPAIRED IAW FOKKER SRM 51-32-01, 51-32-01 AND 51-35-02.Apr 5, 2001 · N493US · Fokker F28MK4000SDR QXEA0100485Attach Angle · gougedPDX- LEFT HAND WING STATION YW171.40 FORWARD SURFACE OF FRONT SPAR HAS GOUGE WORK ON ATTACHING ANGLE TO NACELLE. REPAIRED IAW DHC-8 SRM 51-20-00, 51-20-11, 51-00-06, 51-20-16 AND 51-20-36.Apr 5, 2001 · N346PH · Dhav DHC8202SDR MWEA010245Splice · gougedCENTER TANK STRINGER NR 11 FORWARD SPLICE HAS 2 EA. HOLES WITH DEEP GOUGES. FABRICATED AND INSTALLED SPLICE.Apr 5, 2001 · N800ME · Doug DC914SDR CALA0100280Stiffener · gougedINSPECTION FOUND VERTICAL T-SUPPORT (STIFFENER) ON AFT SPAR JUST I/B OF MLG SUPPORT BEAM O/B FITTING GOUGED AT WS 133. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-5 AND 51-40-6.Apr 5, 2001 · N19357 · Boeing 7373T0SDR ABXA010172Fitting · crackedRIGHT WING JACK POINT CRACKED AT XRS 139.Apr 3, 2001 · N828AX · Doug DC863SDR SROM200100019Fitting · corrodedDURING C CHECK INSPECTION, FOUND CORROSION ON ATTACH FITTING. REPLACED FITTING PER MM 57-15-50.Apr 3, 2001 · N733AR · Boeing 737205SDR DL72L010541Stiffener · crackedIB SPAR STIFFENER IS CRACKED AT NR 2 SLAT IB TRACK. REPAIR PER M/M 57-20-021-8Apr 2, 2001 · N512DA · Boeing 727232SDR MWEA010504Clip · crackedFOUND CLIP CRACKED AT XRS 111.5, STRINGER 21-22 OUTBOARD. -- FABRICATED SHEAR TIE, LOCATED, DRILLED AND INSTALLED CLIP.Apr 2, 2001 · N800ME · Doug DC914SDR UPS01835598Angle · crackedINSPECTION TYPE:C2,3 LEFT WING L/E. ATTACH ANGLE IS CRACKED AT XW454. REMOVED, FABRICATED, AND REPLACED ANGLE I.A.W. DWG. 9753297,AND SRM. 51-1-20D,51-1-21Mar 31, 2001 · N797UP · Doug DC871FSDR SWAA010995Stiffener · crackedDURING SCHEDULED RON CHECK, FOUND WING CENTER SECTION REAR SPAR ZEE STIFFENER CRACKED AT LBL 6.15. REPAIRED STIFFENER PER SWA RA.Mar 31, 2001 · N303SW · Boeing 7373H4SDR AU010315Bracket · cracked(AUS) FORWARD SPAR ATTACHMENT BRACKET LOCATED AT STN104.6 CRACKED ONFORWARD AND REAR SIDES.Mar 30, 2001 · Piper PA31350SDR AU010314Bracket · cracked(AUS) FORWARD SPAR ATTACHMENT BRACKET LOCATED AT STN 104.6 CRACKED ONFORWARD AND REAR SIDES.Mar 30, 2001 · Piper PA31350SDR DL76S010536Stiffener · crackedTHE WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER LOCATED AT LBL 10.94 WAS FOUND CRACKED AT ITS TOP END. THE DAMAGE WAS IN THE WEB OF THE STIFFENER AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT.Mar 28, 2001 · N128DL · Boeing 767332SDR MWEA010426Bracket · chafedRIGHT WING UPPER FILLET SUPPORT BRACKET IS CHAFFING, STATION 585. -- BLENDED CHAFE AREA, FABRICATED AND INSTALLED DOUBLER, INSTALLED CHAFE STRIP AND FILLET BRACKET.Mar 27, 2001 · N800ME · Doug DC914SDR RRXA10764Stringer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING STR.53 AT STA. 495 AND AFT HORZ. LEG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O. #01-Mar 26, 2001 · N8091U · Doug DC871FSDR RRXA10763Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE DAMAGE TO LT. WING CANOE FITTING AT STA.340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/23/01Mar 26, 2001 · N8091U · Doug DC871FSDR SWAA010901Fitting · wornDURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM FWD ATTACH FITTING ON REAR SPAR WORN AT WBL 135.505. REMOVED AND REPLACED BEAM FITTING PER MM.Mar 24, 2001 · N693SW · Boeing 737317SDR USAA010407Bracket · crackedPIT - FOUND BRACKET CRACKED .375 INCH, 14 INCHES INBOARD OF ENGINE PYLON LEFT WING REAR SPAR. REPAIRED PER 2024-T3 DWG NR 69-43586-7 SH 26 ZONE B6 PER SRM 57-20-10 PAGE 10. (M)Mar 20, 2001 · N587US · Boeing 737301SDR 2001UALA00308Web · crackedLEFT WING TRAILING EDGE VERTICAL SUPPORT WEB HAS CRACK WBL 249.3, INBOARD SIDE OF INBOARD AILERON.Mar 20, 2001 · N7446U · Boeing 727222SDR AWXA0001507Fitting · damagedLEFT FR 40 INNER FITTING FOUND DAMAGED. REPAIRED IAW AWA ER 26-5711-01072-JS5.Mar 19, 2001 · N620AW · Airbus A320231SDR ABXA010151Fitting · crackedTHE RIGHT WING LOWER FORWARD TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-2-7.Mar 13, 2001 · N814AX · Doug DC863FSDR EIA2001188Web · crackedHKG-HAECO - FOUND LT WING NR 2 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED BETWEEN WS 440-469. TRIMMED CRACKED AREA, NDT INSPECTED, REPAIRED WEB PER SRM 57-10-06 FIG 5. (M)Mar 12, 2001 · N471EV · Boeing 747273CSDR EIA2001189Web · crackedHKG-HAECO - LT WING NR 2 MAIN TANK MID SPAR UPPER WEB FASTENER EDGE CRACKED FROM WS 382-411. TRIMMED OFF CRACKED AREA, NDT INSPECTED, INSTLALED FREEZE PLUG AND REPAIRED MID SPAR WEB PER SRM 57-10-06. (M)Mar 12, 2001 · N471EV · Boeing 747273CSDR EIA2001190Web · crackedHKG-HAECO - FOUND LT WING NR 2 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED FROM WS 150-353. TRIMMED OFF CRACKED AREA, NDT INSPECTED, INSTALLED FREEZE PLUG AND REPAIRED MID SPAR WEB PER SRM 57-10-06. (M)Mar 12, 2001 · N471EV · Boeing 747273CSDR EIA2001191Web · crackedHKG-HAECO - FOUND RT WING NR 3 MAIN TANK MID SPAR UPPER WEB 1 FASTENER EDGE CRACKED FROM WS 382-411. TRIMMED OFF CRACKED AREA, NDT INSPECTED, INSTALLED FREEZE PLUG AND REPAIRED MID SPAR WEB PER RM 571-0-06. (M)Mar 12, 2001 · N471EV · Boeing 747273CSDR COMA0110077Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110076Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110075Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRCTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110064Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110060Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110058Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.Mar 12, 2001 · N462CA · Emb EMB120RTSDR COMA0110057Support · crackedDURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3813-1, REV IR, 11-5-00.Mar 12, 2001 · N462CA · Emb EMB120RTSDR CA010402006Fitting · cracked(CAN) THE PART WAS CRACKED TWO-THIRDS OF THE CIRCUMFERENCE AROUND THE RAISED BOSS (CASTING) NEAR THE RADIUS. THE TOP END FITTING WAS REPLACED IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND CHECKED - SERVICEABLE.Mar 9, 2001 · Dhav DHC8102SDR SIMA06622Link · unserviceableSAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED THE LEFT FORWARD LOWER WING TO FUSELAGE JUNTION ROD (DOG BONE) HAD AN EXCESSIVELY TIGHT BEARING AND PITTED BUSHING. MAINTENANCE REMOVED AND REPLACED THE JUNCTION ROD IAW JIC 57-15-21-RAI-10000-006. AIRCRAFT Mar 7, 2001 · N314AM · Aerosp ATR42300SDR SWAA010662Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LT WING STABILIZER BEAM FITTING CORRODED ON REAR SPAR CHORD. REMOVED AND REPLACED BEAM FITTING PER MM.Mar 5, 2001 · N672SW · Boeing 7373Q8SDR GAIA01066STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYDRAULIC LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 386 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 386 IAW B727 SRM 51-30-2 AND 51-30-5. P/N 65-17209Feb 28, 2001 · N281KH · Boeing 7272J0SDR GAIA01065STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYD LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 396 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 396 YAW B727 SRM 51-30-2 AND 51-30-5 P/N 65-17210-27. TFeb 28, 2001 · N281KH · Boeing 7272J0SDR GAIA01064STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING L/E WS 390 HAS CORROSION ON FORWARD SPAR STIFFENER. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 390 LEFT 390 IAW B727 SRM 57-10-2 FIG 3 AND 51-30-2. MATERIAL STIFFENER BAC 1517-1Feb 28, 2001 · N281KH · Boeing 7272J0SDR DHL2001747538Support · corrodedD-CHECK, RT WING L/E LOWER INBOARD FAIRING SUPPORT HAS LIGHT CORROSION IN END OF SUPPORT. REMOVED PART IAW SRM 51-30-2.Feb 27, 2001 · N747DH · Boeing 727224SDR DL76S010351Web · crackedDAMAGE FOUND IN WEB OF THE LBL VERTICAL STIFFENER ON THE CENTER SECTION FRONT SPAR AT THE OVERWING FLOORBEAM TO VERTICAL STIFFENER JOINT. CRACKED PORTION OF WEB WILL BE REMOVED AND REPAIRED BY SPLICING IN NEW SECTION OF STIFFENER. ER/A 397281-14.Feb 26, 2001 · N125DL · Boeing 767332SDR 20010410AP006Cuff · corrodedTHE STAINLESS STEEL CUFFS ARE ONLY ON THE RT WING STUTS AND THEY PROVIDE PROTECTION FOR THE STRUT WHEN OPENING/CLOSING THE CABIN DOOR. THESE CUFFS ARE NOT BONDED TO THE WING STRUT BUT ARE WRAPPED AROUND THE STRUT AND CRIMPED IN PLACE. WHEN THE CUFFS WERE REMOVFeb 23, 2001 · N36259 · Howard DGA15PSDR DHL2001747534Stiffener · corrodedD-CHECK, RT WING FWD SPAR STIFFENER HAS LIGHT CORROSION UNDERNEATH PRIMER, JUST OUTBOARD OF NR 5 FLAP ACTUATOR.Feb 22, 2001 · N747DH · Boeing 727224SDR DHL2001747532Stiffener · corrodedC-CHECK, RT WING FWD UPPER AND LOWER SPAR STIFFENERS, RT & LT OF NR 5 L/E FLAP ACTUATOR HAVE MED CORROSION.Feb 22, 2001 · N747DH · Boeing 727224SDR 20010323CW012Angle · crackedWHILE INSPECTING FOR FUEL LEAKS A CRACK APPROXIMATELY 2.5 INCHES IN LENGTH WAS FOUND IN THE LEFT CANTED RIB, JUST AFT OF THE FORWARD SPAR, BELOW THE TOP SKIN. RECOMMEND REPLACEMENT OF THE ANGLE.Feb 19, 2001 · N926ES · Cessna 425SDR UPS01235233Stiffener · corrodedINSPECTION TYPE:C+SI, WHILE REMOVING CORROSION FROM NR 3 FLAP TRACK TO AUX SPAR MOUNT HOLES THE STIFFENER ABOVE MOUNT RIVETED TO THE AUX SPAR WAS FOUND TO HAVE EXCESSIVE CORROSION IN BARREL NUT HOLE. STIFFENER REPLACED IAW SRM 51-30-00 AND DRAWING 65-16216.Feb 19, 2001 · N941UP · Boeing 72722CSDR RRXA10802Clip · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACCESS HOLE 505D AND BETWEEN STRINGER 68 & 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AFeb 15, 2001 · N801GP · Doug DC871FSDR RRXA10751Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 4 STUB WING I/B LWR. FRONT SPAR L/E SHIM PLATE AT I/B LWR. FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.0Feb 15, 2001 · N8091U · Doug DC871FSDR RRXA10750Shim · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 STUB WING I/B LWR. FRONT SPAR L/E SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01Feb 15, 2001 · N8091U · Doug DC871FSDR RRXA10798Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #3 PYLON WING L/E BULLNOSE AT STA. XS220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-24 AND DC-8 SRM 51-1-21 AND Feb 9, 2001 · N801GP · Doug DC871FSDR RRXA10787Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING L/E AT STA. XW485.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8Feb 9, 2001 · N801GP · Doug DC871F
Back to JASC 5720