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 P5CA9700318Flange · corrodedLEVEL 1 CORROSION AND EXFOLIATION AT PANEL MOUNTING FLANGE ON LEFT WING UPPER LEADING EDGE OUTBOARD OF NR 2 PYLON. REMOVED CORROSION, BLENDED, AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.Feb 19, 1997 · N859FT · Boeing 747123SDR P5CA9700313Wing Tip · separatedSEPARATED SKIN ON RIGHT WING TIP ADJACENT TO ANTENNA. REPAIRED PER BAC SRM 51-40-09 AND PAINTED PER BAC SRM 51-24-11.Feb 19, 1997 · N859FT · Boeing 747123SDR UPS97822285Angle · crackedLT AFT, LT CORNER CENTER WING ANGLE TO FUSELAGE FITTING CRACKED BS 980. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-1-20D AND DWG 4647365.Feb 17, 1997 · N748UP · Doug DC871FSDR RRXA97049Stringer Clip · crackedDURING C-CHECK, FOUND CRACK ON STRINGER CLIP ON RIGHT WING AT, XRS 22.730 AND BETWEEN STRINGERS 1R AND 2R. NEITHER REPLACEMENT PART NOR BLANK FORGING AVAILABLE FROM ACFT MFR. FABRICATED AND INSTALLED NEW CLIP IAW TIMCO REO-02751 DTD 2/11/97 AND FAA-DER APPROFeb 17, 1997 · N105WP · Doug DC873SDR UPS97822200Doubler · crackedINSPECTION TYPE:D, RT WING L/E SECTION, BETWEEN PYLONS, HAS A 17 INCH CRACK AT LWR INTERNAL DOUBLER AT MIDDLE OF SECTION (LWR). REMOVED INTERNAL DOUBLER, FABRICATED REPLACEMENT SPLICE STRAP IAW SRM51-3-1. INSTALLED SPLICE STRAP IAW SRM 51-1-20 AND 51-1-21.Feb 15, 1997 · N748UP · Doug DC871FSDR CA970227005Fitting · cracked(CAN) DURING REPAIR FOR WING BOLT COVER, VISUAL INDICATION SHOWED A SCRATCH. FURTHER INSPECTION FOUND A CRACK EXTENDING FROM THE BOLT HOLE COUNTER BORE. AIRCRAFT TT: 30,367 HOURS.Feb 15, 1997 · Beech 99SDR VJ970101T-Cap · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XW 58.768 BETWEEN STRINGER 16-17 T-CAP IS CORRODED. XW 58-768 LEFT MAIN TANK BETWEEN STRINGER 16-17 T-CAP CORROSION COMPLIED WITH IAW AERO EO 97-475 REV IFeb 13, 1997 · N919VV · Doug DC932SDR VJ970100T-Cap · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XW 58.768 BETWEEN STRINGER 15-16 T-CAP IS CORRODED. XW 58.768 LEFT MAIN TANK BETWEEN STRINGER 15-16 T-CAP CORROSION COMPLIED WITH IAW EO 97-475 REV IR DATFeb 13, 1997 · N919VV · Doug DC932SDR VJ970099T-Cap · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK XW 58.768 BETWEEN STRINGER 14-15 T-CAP IS CORRODED. XW 58-768 LEFT MAIN TANK BETWEEN STRINGER 14-15 T-CAP CORROSION COMPLIED WITH IAW EO 97-475 REV IR DATFeb 13, 1997 · N919VV · Doug DC932SDR VJ970098T-Cap · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE XW 58.768 BETWEEN STRINGER 13-14 T-CAP IS CORRODED. XW 58-768 LEFT WING TANK BETWEEN STRINGER 13-14 T-CAP CORROSION COMPLIED WITH IAW EO 97-475 REV IR DATED 02-14-07. (Feb 13, 1997 · N919VV · Doug DC932SDR VJ970096T-Cap · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT WING TANK XW 58.768 BETWEEN STRINGER 11-12 T-CAP IS CORRODED. XW 58-768 LEFT WING TANK BETWEEN STRINGER 11-12 T-CAP CORROSION COMPLIED WIHT IAW EO 97-475 REV IR DATFeb 13, 1997 · N919VV · Doug DC932SDR VJ970086Clip · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND, THE LEFT MAIN TANK STRINGER CLIP AT XRS 111.5 STRINGER 12-13 IS CORRODED. REMOVED CLIP CORRODED BEYOND 20 PERCENT LIMIT, DRILLED AND DEBURRED NEW CLIP IAW DC-9 SRM 51-10-4. Feb 13, 1997 · N919VV · Doug DC932SDR VJ970069Clip · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND LEFT WING INTERNAL, CORROSION ON CLIP STATION 58 ON FRONT SPAR. REMOVED CORRODED CLIPS, ORDERED, DRILLED AND DEBURRED, TREATED AND PRIMED AND INSTALLED NEW CLIPS IAW DC-9 SRMFeb 13, 1997 · N922VV · Doug DC932SDR VJ970068Shear Clip · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND RIGHT WING SHEAR CLIP AT REAR SPAR STATION 111 IS CRACKED. FABRICATED AND INSTALLED NEW SHEAR CLIP IAW DOUGLAS DRAWING NR 4912005 AND DC-9 SRM 51-10-4, 51-22-1, 51-20-0, AND Feb 12, 1997 · N922VV · Doug DC932SDR UPS97822203Angle · crackedINSPECTION TYPE:D, LT WING INBD L/E INBD UPPER AFT L/E ATTACH ANGLE CRACKED APPROX 4.75. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER DWG 5769646 AND SRM 51-3-0 AND 53-8-1.Feb 12, 1997 · N748UP · Doug DC871FSDR 97FDEA00115Beam · corrodedNR 0674 12, CORROSION IN GEAR BEAM AT O/B BOLT HOLE NR 4 FLAP TRACK ATTACH HOLE. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED NEW BUSHING AND SPECIAL WASHER PER EA 7-5710-28983 DATED 2/10/97.Feb 12, 1997 · N241FE · Boeing 727277SDR 97FDEA00114Beam · corrodedNR 0673 011, CORROSION IN I/B HOLE IN GEAR BEAM FOR NR 4 FLAP TRACK ATTACH. REMOVED CORROSION, EDDY CHECKED HOLE, INSTALLED BUSHING PER EA 7-5710-28983 DATED 2/10/97.Feb 12, 1997 · N241FE · Boeing 727277SDR CALA9700240Doubler · corrodedINSPECTION FOUND LT WING INBOARD WING UPPER SURFACE EXTERNAL DOUBLER CORRODED AND DELAMINATED AT STA 264. THE DOUBLER WAS REMOVED, A REPAIR PART WAS FABRICATED AND INSTALLED IAW SRM 57-31-01, 51-21-01, AND 51-31-01.Feb 8, 1997 · N68041 · Doug DC1010SDR ABXA9701462Bracket · crackedFITTING CRACKED INSIDE PANEL 1547A, LEFT FLAP. REPLACED BRACKET IAW DC-9 SRM 51-30-5.Feb 8, 1997 · N952AX · Doug DC941SDR 97ZZZM614Chord · corrodedRIGHT WING T/E LOWER CHORD CORRODED AT INBOARD FLAP OUTBOARD TRACK ATTACH POINT ON LOWER SURFACE AND INSIDE OUTBOARD ATTACH HOLE. REMOVED LIGHT SURFACE CORROISON (.001) IN LIMITS IAW SRM 51-10-6 AND MM 51-21-51. FABRICATED BUSHINGS ON OUTBOARD HOLE PER EO 97Feb 8, 1997 · N467AT · Boeing 7372T4SDR 97ZZZM612Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARDTRACK AFT MOUNT IS CORRODED. REMOVED TWO BUSHINGS FROM LEFT OUTBOARD FLAP INBOARD TRACK FITTING OUTBOARD HOLE AND OUTBOARD TRACK FITTING OUTBOARD HOLE. REMOVED CORROSION BY REAMING HOLES TWO EACH. NDT INSPECTED, NO CRACKS, NOFeb 8, 1997 · N467AT · Boeing 7372T4SDR 97ZZZM608Fitting · pittedRIGHT WING SPAR OUTBOARD FLAP INBOARD TRACK MOUNTING RIGHT HOLW I/D HAS PITTING. REMOVED CORROSION BY REMOVING BUSHINGS FROM RIGHT REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT AND OUTBOARD TRACK MOUNT. REAMED HOLES TO REMOVE CORROSION. NDT INSPECTED, NO CORRFeb 8, 1997 · N467AT · Boeing 7372T4SDR 97ZZZM607Chord · corrodedRIGHT WING T/E LOWER CHORD CORRODED AT INBOARD FLAP OUTBOARD TRACK ATTACH POINT ON LOWER SURFACE AND INSIDE ATTACH HOLE. REMOVED LIGHT SURFACE CORROSION (.001) IN LIMITS IAW SRM 51-10-6 AND MM 51-21-51. FABRICATED BUSHINGS ON OUTBOARD HOLE PER EO 97-457 AND Feb 8, 1997 · N467AT · Boeing 7372T4SDR CALA9700176Angle · crackedINSPECTION FOUND A 2.5 INCH CRACK IN RIB LOWER CHORD ANGLE AT S3 IN FUEL ACCESS PANEL 7202 AT LT WING FUEL TANK, WBL 135.5. THE CRACKED AREA WAS REMOVED, A REPAIR TEE WAS INSTALLED IAW BOEING SERVICE BULLETIN 737-57-1186 AND REPAIR ENGINEERING ORDER NUMBER 02Feb 5, 1997 · N14233 · Boeing 737217SDR DL72S970213Stiffener · crackedFOUND DURING F-1 LETTER CHECK, I/B SPAR STIFFENER CRACKED AT NR 3 L/E SLAT O/B TRACK. REPAIRED PER M/M 57-20-21.Feb 4, 1997 · N475DA · Boeing 727232SDR DL72S970212Fitting · chafedFOUND ON F1 LETTER CK, MLG CHAFING FWD SIDE OF AUX SPAR. REPAIRED PER MM 57-43-0.Feb 4, 1997 · N475DA · Boeing 727232SDR ABXA9700554Angle · crackedDURING C-CHECK, THE LT WING LEADING EDGE SPLICE ANGLE OUTBOARD OF NR 6 SLAT TRACK WAS FOUND CRACKED. THE SPLICE WAS REPLACED IAW DC9 SRM 51-30-2.Feb 4, 1997 · N946AX · Doug DC931SDR AU970067Bracket · cracked(AUS) LH WING TIP TANK ATTACHMENT BRACKET CRACKED IN AREA OF TOP REAR RADIUSFeb 3, 1997 · Cessna 310RSDR ABXA9700587Doubler · crackedDURING C-INSPECTION, FOUND THE RIGHT WING LEADING EDGE SKIN SEAM DOUBLER AND ATTACH ANGLE AT WS 267 CRACKED. REPLACED LEADING EDGE SEAM DOUBLER IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Feb 3, 1997 · N949AX · Doug DC931SDR UPS97521925Cover · crackedFOUND 1.375 INCH CRACK IN NOSE GAP COVER ASSY, LEFT SIDE ON INBD SIDE OF ASSY BOTTOM OF LEADING EDGE. INSTALLED REPAIR TO LT WING FIXED L/E PER EO B757-5740-9005A.Feb 2, 1997 · N415UP · Boeing 75724APFSDR 9702299958Fitting · crackedDURING H-CHECK, FOUND CRACK IN RIB TO STRINGER ATTACH FITTING AT STR 23, RIB XRS 91.0, RIGHT WING. REPLACED PER SRM 51-30-5.Feb 2, 1997 · N917RW · Doug DC931SDR UPS97822188Extrusion · crackedINSPECTION C-CHECK, RT WING LE OUTBOARD, OUTBOARD SIDE UNDER SLOTED DOOR EXTRUSION, CRACKED. FABRICATED REPAIR DOUBLER SHIM. REPLACEMENT ANGLE IAW REO 02750. ALODINED AND PRIMED IAW DC8 SRM 51-1-8D. INSTALLED REPAIR DOUBLER AND SHIM IAW REO 02750 AND INSTAJan 31, 1997 · N708UP · Doug DC871FSDR AALA970268Spar Chord · corrodedTUL - FOUND CORROSION FORWARD SPAR LOWER CHORD FSS 385, BELOW FUEL SHUTOFF. REMOVED CORROSION, REPAIRED LOWER SPAR CHORD PER ESO 11697, DATED 7-19-95. (M)Jan 30, 1997 · N894AA · Boeing 727223SDR 97ZZZX1570Frame · crackedLEFT WING STA 25 FRAME CRACKED UPPER 'Z'.Jan 28, 1997 · N582P · Cvac 440SDR 97ZZZX1565Shroud · crackedCRACK IN INNER SHROUD RT OTBD L/E STA 290.Jan 28, 1997 · N582P · Cvac 440SDR AALA970298Support · corrodedAFW - NR 1 FLAP TRACK FORWARD SUPPORT HAS CORROSION. REPAIRED PER MRB 727-0022. (M)Jan 27, 1997 · N716AA · Boeing 727227SDR UPS97822060Doubler · crackedINSPECTION TYPE-C, LT AILERON TAB LOCK-OUT CYLINDER ACCESS PANEL LAND, MATING SURFACE HAS 2 CRACKS. CUT OUT DAMAGED AREA OF INNER DOUBLER, FABRICATED AND INSTALLED REPAIR IAW DHC SK-806-413 REF UPS ENRG FILE NR DC8-57-0752.Jan 25, 1997 · N806UP · Doug DC873FSDR CALA9700124Mount Tang · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD VENT BOX AFT MOUNT TANG WHERE IT MOUNTS TO TOP OF RIB AT W.S. 686.50, LEFT WING FUEL TANK ACCESS CUT OUT NR 7218. A REPAIR WAS INSTALLED IAW EA 5762-01050.Jan 23, 1997 · N79754 · Boeing 727227SDR CALA9700122Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN ANGLE AT RT WING LEADING EDGE RIB, SLAT STA ZERO. A NEW ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-1.Jan 23, 1997 · N79754 · Boeing 727227SDR UPS97821869Angle · crackedINSPECTION TYPE: C. LT WING SECTION BETWEEN PYLONS AT CENTER AFT OF PART HAS L/E RIB SUPPORT ANGLE CRACKED ON LOWER AFT END. STOP DRILLED CRACK AND INSTALLED REPAIR IAW 57-2-0.Jan 22, 1997 · N706UP · Doug DC871FSDR UPS97821936Doubler · crackedINSPECTION TYPE-C, RT WING L/E INTERNAL LOWER DOUBLER AND STRAP CRACKED AT RIB XFS435. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND STRAP AND INSTALLED IAW SRM 51-1-21.Jan 21, 1997 · N706UP · Doug DC871FSDR TWAA9805603Doubler · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DOUBLER CRACKED AT RE-FUELING PANEL DOOR FRAME. REPLACED DOUBLER PER SRM 51-01 PAGE 1 ITEM 2. (X)Jan 21, 1997 · N909TW · Doug DC982SDR P5CA9700183Cover · corrodedNR 3 PYLON TO WING GAP COVER ERODED AT FWD END. SANDED AND CLEANED, APPLIED FILLER AND OVERLAYS IAW SRM 51-40-09.Jan 21, 1997 · N858FT · Boeing 747123SDR P5CA9700175Stiffener · damageSTIFFENER GOUGED AT WS 1020 FWD SPAR I/B OF NR 4 PYLON AS VEIWED FROM SLAT CAVITY. BLENDED DAMAGE AND TREATED IAW SRM 57-10-01 AND 51-10-02 ORG MAT .125 AFTER REWORK .114 WITHIN LIMITS IAW SRM 57-10-01 FIG 1.Jan 21, 1997 · N858FT · Boeing 747123SDR EISA97017Vent Box · crackedRIGHT WING VENT BOX CRACKED AT WS 686. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-4. (M)Jan 21, 1997 · N6839 · Boeing 727223SDR DHL9774108CFalse Spar · crackedAT C-CHECK, FALSE SPAR WEB CRACKED AFT SIDE ABOVE NR 4 FLAP TRACK. REMOVED FASTENERS IN WEB, STOP DRILL CRACK, ACCOMPLISHED HFEC, NO CRACKS NOTED. INSTALLED WEB REPAIR PER SRM 51-40-2, 4.5 BY 3.5.Jan 21, 1997 · N741DH · Boeing 7272Q9SDR 97ZZZX539Fitting · crackedDURING INVESTIGATION OF FATAL ACCIDENT (MIA97FA047), THE LEFT FORWARD LIFT STRUT TO WING SPAR FITTING WAS FOUND CRCKED IN 2 PLACES AT THE OUTBOARD WELD TERMINALS. ONE CRACK CROSSED THE FITTING FLANGE AND PROGRESSED .3750 INCH VERTICALLY ON THE WEB OF THE FITTJan 17, 1997 · N7596F · Bbavia 7GCBCSDR 97ZZZM228Trap Panel · crackedDTW - ULTRASONIC AND EDDY CURRENT INDICATION CRACK EMANATING FROM NR 9 ATTACH HOLE IN UPPER AFT HORIZONTAL FLANGE OF LT TRAP PANEL. CRACK LENGTH APPROX 1 INCH. REPAIR ACCOMPLISHED IAW SB 53-182 AND DOUGLAS STRUCTURAL REPAIR MANUAL (SRM) 57-09 FIGURE 7A AND EJan 17, 1997 · N934ML · Doug DC931SDR 97ZZZM227Trap Panel · crackedLEFT TRAP PANEL HAS CRACK INDICATIONS ALONG UPPER HORIZONTAL FLANGE BETWEEN AFT ATTACH BOLTS 3-4 AND 7-8 AND FORWARD BOLTS A-B AND AFT OF D. REF DC-9 SRM CHAPTER 57-09, FIG 6, SHEET 4. REPAIRED CRACKED PORTION OF LT FORWARD TRAP PANEL IAW DC-9 SRM 57-09, FIGJan 17, 1997 · N12536 · Doug DC932SDR UPS97221921Gear Beam · corrodedINPECTION TYPE-D, SUSPECT CORROSION IN FLAP ATTACH HOLES OF LT LANDING GEAR BEAM. REPAIRED IAW SRS EO 97-02-021, UPS FILE NR 727-57-1782.Jan 16, 1997 · N945UP · Boeing 72722C
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