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 UPS99829969Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN I/B AT W/S 74.000 REAR SPAR HAS FWD AND AFT FITTINGS CRACKED. REMOVED AND REPLACED FITTINGS W/SERVICABLE PART IAW DAC DWG 5613423 AND DC8 SRM 51-1-20D.Jun 15, 1999 · N807UP · Doug DC873FSDR UPS99829968Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN IB AT FS 74 REAR SPAR HAS TWO CRACKED FITTINGS. REMOVED AND REPLACED END FITTING IAW UPS DC8 SRM 51-2-20D AND DWG 3704 841.Jun 15, 1999 · N807UP · Doug DC873FSDR UPS99230004Fitting · crackedINSPECTION TYPE:C&SI, CRACK INDICATION IN WING CENTER SECTION RT WING TERMINAL FITTING, LWR O/B FASTENER HOLE, BS 870. REPAIRED IAW SMRO EO 99416RI UPS EO NR B727-5710-11557-A.Jun 15, 1999 · N927UP · Boeing 72731CSDR GTIA9900885Trap Fitting · defectiveMHV - ULTRASONIC INPECTION SHOWS AN INDICATION OF A DEFECT ON THE INBOARD SIDE OF THE INBOARD VETICAL BOLT ON THE LEFT REAR SPAR TO TRAPEZOIDAL FITTING. REPLACED TRAP FITTING PER S/B NR 57-129 JACKED AND SHORED A/C. REMOVED AND REPLACED AILERON CABLE MIXER FJun 15, 1999 · N13512 · Doug DC932SDR AT9900477Bracket · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND PULLEY BRACKET ON LEFT WING REAR SPAR AT XRS 398 CORRODED. REMOVED AND REPLACED PULLEY BRACKET, RETENSION TRIM CABLES AND TRAVEL CHECK GOOD IAW DC9 MM 27-10-0.Jun 13, 1999 · N867AT · Doug DC932SDR HNAA9900085Angle · crackedAFT LEFT CLOSING ANGLE IS CRACKED. REMOVED AND REPLACED CLOSING ANGLE.Jun 11, 1999 · N914HA · Dhav DHC8102SDR 99FDEA00216Chord · corrodedNR 799 WHILE WORKING NR 246 FOUND WING CTR SECTION LWR CHORD AT BS 870, RBL 16 TO RBL 55 TO BE CORRODED.Jun 11, 1999 · N511FE · Boeing 72725SDR 99FDEA00215Web · corrodedNR 634 WHILE WORKING NR 246 FOUND BS 870 WING CTR SECTION AFT VERTICAL WEB TO BE CORRODED BEYOND LIMITS.Jun 11, 1999 · N511FE · Boeing 72725SDR 99FDEA00214Chord · corrodedNR 246 CORROSION (C53-132-02(1)) BETWEEN BS 870 UPPER CHORD AND 870 WEB AT LBL 41.Jun 11, 1999 · N511FE · Boeing 72725SDR QXEA9901282Mount · loosePDX - LEFT WING CANOE 81CE FORWARD MOUNT IS LOOSE. REPAIRED IAW HORIZON AIR EA 4-57-278.Jun 9, 1999 · N493US · Fokker F28MK4000SDR MZZA99119Stiffener · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)Jun 8, 1999 · N15790 · Boeing 727232SDR GAIA9967Angle · corrodedFOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. RIGHT WING STATION 525, REAR SPAR STIFFENER ANGLE HAS CORROSION AT NR 12 SPOILER ACTUATOR OUTBOARD FLANGE. REMOVED AND REPLACED STIFFENER ANGLE IAW B727 SRM 51-30-02. SEALED FASTENEJun 8, 1999 · N6833 · Boeing 727223SDR GAIA9966Beam · corrodedFOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. CORROSION ON RIGHT WALKING BEAM FORWARD OF THE NR 8 SPOILER ACTUATOR. REWORKED RIGHT WALKING BEAM IAW, AMERICAN INTERNATIONAL AIRWAYS, ENGINEERING DEVIATION REQUEST B2-06492. FLAP PJun 8, 1999 · N6833 · Boeing 727223SDR UPS99229991Stiffener · corrodedINSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT STIFFENER BETWEEN UPPER & LWR WING CENTER SECTION SPAR CHORDS RBL 45. STIFFENER REPLACED IAW DRAWING 65-16202.Jun 7, 1999 · N927UP · Boeing 72731CSDR A6WA9900066Fastener · damagedPERFORMED RIL HC571H9033 LEFT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H9033 TO LEFT RIB 2 JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR A6WA9900065Fastener · damagedPERFORMED RIL HC571H9033 LEFT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H9033 TO ABOVE LEFT RIB 2 JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR A6WA9900064Fastener · damagedPERFORMED RIL HC571H9033 LT CENTER TANK RIB 0 JO-BOLTS. C/W RIL HC571H9033 TO LEFT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR A6WA9900063Fasteners · damagedPERFORMED RIL HC571H9033 RT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H0933 RT WING SIDE OF RIB 2 JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR A6WA9900062Fastener · damagedPERFORMED RIL HC571H9033 ON RT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H0933 RT RIB 2 CENTER TANK SIDE JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR A6WA9900061Fastener · damagedPERFORMED RIL HC571H9033, RT RIB 0 JO BOLTS. C/W RIL - HC571H9033 TO RT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)Jun 7, 1999 · N179US · Bag BAE146200ASDR CALA9900638Support · corrodedINSPECTION FOUND LT AND RT MLG A FRAME SUPPORT BEAM BOLT HOLES CORRODED. THE SUPPORT BEAM WAS REPAIRED IAW SRM 57-20-00, PAGE 104.Jun 4, 1999 · N83071 · Doug DC1030SDR DL72S991243Chord · damagedINSPECTIONS PER 4-58560-12AD, FOUND 4 FASTENER HOLES WITH TOOLING DAMAGE. NO CRACK INDICATIONS WERE NOTED. REPAIRED PER ERA 333191-14AD, REV A.Jun 3, 1999 · N521DA · Boeing 727232SDR RRXA991130Fastener · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, FASTENER DAMAGED INSIDE NR 4 ALT FUEL TANK BY NR 4 PYLON AT XW 463 STR 58 LOWER SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. FASTENER OK AS IS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETJun 2, 1999 · N606AL · Doug DC873FSDR RRXA991104Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 2 STUB WING, 9.75 LEFT WING NR 2 STUB WING I/B FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSJun 2, 1999 · N606AL · Doug DC873FSDR CALA9900614Angle · crackedINSPECTION FOUND A .3125 INCH CRACK IN DOUBLER ANGLE AT RT WING FRONT SPAR WBL 92. THE ANGLE AND STIFFENER WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, FIGURE 4.Jun 2, 1999 · N79749 · Boeing 727224SDR AWXA9900341Angle · crackedC-CHECK, .75 INCH CRACK ON UPPER ANGLE OF LT WING L/E RIB I/B SIDE OF NR 1 ENG PYLON. FABRICATED AND INSTALLED REPAIR PART AT WING STA 185.5 IAW 51-30-00, MATERIAL 2024-0 .063 HEAT TREATED TO 2024-T4.Jun 2, 1999 · N141AW · Boeing 7372M8SDR 99T64R267ARNutplate · missingNR 288 - TWO EACH, CHANNEL NUTPLATES AND SCREWS MISSING LT INBOARD L/E FUEL TANK XRS 64-XFS 14. INSTALLED NAS-1670-4 BLIND FASTENERS PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Jun 2, 1999 · N1808E · Doug DC862SDR UPS99229703Stiffener · corrodedINSPECTION TYPE:SI, CORROSION AND POPPED FASTENER ON BS 870, BL 0 STIFFENER WING CENTER SECTION. REMOVED AND REPLACED STIFFENER PER SRM 51-30-02.Jun 1, 1999 · N946UP · Boeing 72725CSDR 99UAL900299Bolts · looseRIGHT WING LANDING GEAR BEAM OUTBOARD END GATE FITTING SUPPORT ASSEMBLY (P/N 65B08186-30) SHOWED SIGNS OF MOVEMENT DUE TO BROKEN SEALANT. INSPECTION REVEALED TWO UPPER BOLTS (P/N BACB30US10K54) AND LOWER BOLTS (P/N BACB30PE10C45W) WERE LOOSE. THE BOLTS ATTACJun 1, 1999 · N172UA · Boeing 747422SDR 99FDEA00201Chord · corrodedNR 3 FUEL CELL (NR 2 TANK) BULGED WEB AND POPPED FASTENERS UPPER CHORD BS 870. REMOVED AND REPLACED PER EA 7-5710-43038A, DATED 5/24/99.Jun 1, 1999 · N149FE · Boeing 72722SDR CALA9900643Beam · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING TRAILING EDGE PANEL FITTING BEAM AT STA XORS 299. A REPAIR WAS PERFORMED IAW SRM 57-00-01.May 28, 1999 · N13066 · Doug DC1030SDR CALA9900640Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD AFT FITTING ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-30-00.May 28, 1999 · N13066 · Doug DC1030SDR SWAA990935Beam · corrodedDURING SCHEDULED TRANSITION CHECK, FOUND LT MAIN LANDING GEAR STABILIZER BEAM CORRODED ARROUND LUGS. REMOVED AND REPLACED BEAM PER MM.May 27, 1999 · N308SA · Boeing 7373Y0SDR ABXA9900547Skin · delaminatedRIGHT WING VANE, LOWER LEADING EDGE SKIN WAS 20 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM.May 27, 1999 · N843AX · Doug DC861SDR ABXA9900546Skin · delaminatedLEFT WING VANE, LOWER SURFACE WAS 90 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM.May 27, 1999 · N843AX · Doug DC861SDR UPS99829828Angle · crackedINSPECTION TYPE:C1, LT CENTER LEADING EDGE O/B VERTICAL ATTACH ANGLE AT I/B SIDE OF NR 1 STUB WING AT STA XS 520.00 IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297.May 26, 1999 · N705UP · Doug DC871FSDR DHL9970501CAngle · crackedAT C-CHECK, RT WING L/E CAVITY FS 115 VERTICAL ANGLE CRACKED. CUT OUT DAMAGE, HFEC, INSTALLED ANGLE REPAIR 9 BY 2 PER SRM 51-40-3, N/R 2058.May 25, 1999 · N705DH · Boeing 72722CSDR UPS99229924Bracket · crackedINSPECTION TYPE: C & SI, LT WING TIP LENS ATTACH BRACKET AFT LWR END CRACKED. REPLACED BRACKET IAW SRM 51-30-2.May 24, 1999 · N927UP · Boeing 72731CSDR ABXA9900521Frame · crackedFRAME CRACKED AT STATION XFS 145.00 UPPER TOP CORNER OF AUX TANK, RIGHT WING. REPAIRED IAW DC8 SRM 57-3-3 AND 57-2-0.May 22, 1999 · N816AX · Doug DC863SDR AT9900530Jamb · gougedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND MAIN RE-FUELING POINT AT LOWER WING SKIN WORN THROUGH WHERE LATCH FOR FUEL DOOR MATES TO LOWER SKIN. FABRICATED FITTINGS. DRILLED, DEBURRED AND COUNTERSUNK HOLES IN FITTINGS. INSTALLED FITTINGS IAW May 21, 1999 · N805AT · Doug DC932SDR ABXA9900378Vane · delaminatedDURING C-CHECK, FOUND RIGHT INBOARD FLAP FIXED VANE DELAMINATED. REPLACED FLAP FIXED VANE IAW DC9 MM 27-50.May 21, 1999 · N963AX · Doug DC941SDR ABXA9900543Slot Vane · corrodedLEFT WING INBOARD SLOT VANE HAD HEAVY CORROSION. REPAIRED IAW DC8 SRM 57-3-1.May 15, 1999 · N816AX · Doug DC863SDR UPS99229789Fitting · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH WING FITTING. CORROSION OUT OF LIMITS PER BOEING DWG 65-32733, PART REPLACED WITH NEW ITEM PER SRM 51-30-02 AND DWG 65-17357.May 13, 1999 · N946UP · Boeing 72725CSDR DL72S991021Fitting · corrodedDURING RTN INSP OF THE RT MLG BEAM FWD SUPPORT FITTING, CORROSION WAS FOUND ON THE INNER SURFACE OF THE MLG ATTACHMENT BOLT BORE. FINAL DIAMETER OF 1.875 WAS NEEDED TO REMOVE ALL DAMAGE. REPAIRED PER ERA 333106-14, REV A.May 10, 1999 · N8873Z · Boeing 727225SDR A6WA9900054Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8. (X)May 7, 1999 · N463AP · Bag BAE146100ASDR A6WA9900053Stiffener · crackedRIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8 IAW BAE FAX DJR/RJ0630-98. (X)May 7, 1999 · N463AP · Bag BAE146100ASDR A6WA9900052Stiffener · crackedRIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 3 AND 4. (X)May 7, 1999 · N463AP · Bag BAE146100ASDR A6WA9900051Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 8 AND 9. (X)May 7, 1999 · N463AP · Bag BAE146100ASDR 17WA9900050Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAILING EDGE STIFFENER BETWEEN RIBS 8 AND 9 IAW BAE FAX DJR/RJ0630-98. (X)May 7, 1999 · N463AP · Bag BAE146100ASDR EIAA990124Fitting · corrodedMZJ - DURING C-CHECK, THE RIGHT MLG FITTING BRACE ATTACH LUG FACE WAS FOUND CORRODED. REPAIRED PER ECRA NR 942-57-003-2. (X)May 5, 1999 · N942F · Doug DC933F
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