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"

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SDR DHL9970302CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD SUPPORT WS 498.08 PER SRM 51-30-2, 51-10-1 PAR 4 N/R 2045.Jul 20, 1999 · N703DH · Boeing 72730CSDR AU990891Angle · corroded(AUS) LEFT WING SPAR UPPER REAR SPAR CAP ANGLE CORRODED. AN ATTEMPT HAD BEEN MADE TO HIDE THE CORROSION USING MASKING TAPE AND PAINT.Jul 20, 1999 · Beech 58SDR DL72S991626Angle · crackedNR 5 SLAT LOWER COVE ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812.Jul 19, 1999 · N404DA · Boeing 727232SDR QXEA9901474Web · crackedPDX - BL245R AND Z STRINGER 2.02 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298.Jul 18, 1999 · N490US · Fokker F28MK4000SDR QXEA9901473Web · crackedPDX - BL245R AND Z STRINGER 2.01 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298.Jul 18, 1999 · N490US · Fokker F28MK4000SDR QXEA9901472Web · crackedPDX - BL245L AND Z STRINGER 2.02 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW EA 4-57-298.Jul 18, 1999 · N490US · Fokker F28MK4000SDR QXEA9901471Web · crackedPDX - BL245L AND Z STRINGER 2.01 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298.Jul 18, 1999 · N490US · Fokker F28MK4000SDR 99ZZZX2977Bracket · brokeUPPER RIGHT AILERON PULLEY BRACKET BROKEN IN-FLIGHT ABOUT 2 MINUTES AFTER TAKEOFF. AIRPLANE WAS FLOWN RUDDER ONLY BACK TO AIRPORT. NO DAMAGE OR INJURIES.Jul 18, 1999 · N77310 · Cessna 140SDR QXEA9901580Angle · crackedPDX - RIGHT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11.Jul 17, 1999 · N821PH · Dhav DHC8102SDR DHL9970306CTip · crackedAT C CHECK, LEFT WING TIP AFT O/B EDGE AREA CRACKED IN TWO PLACES. REMOVED LEFT WING TIP OUTBOARD EDGE FOR REPAIR IAW SRM 51-30-2. STOP DRILLED CRACK AT TWO PLACES IAW SRM 51-10-1, PERFORMED HFEC IAW NDT PART 68-00-00 FIG 4. NO CRACKS NOTED BEYOND STOP DRILJul 17, 1999 · N703DH · Boeing 72730CSDR UPS99830235Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LOWER SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21 AND 51-1-20D.Jul 16, 1999 · N866UP · Doug DC873FSDR UF6A990745Angle · crackedSBN - LEFT MODULE 7 HAS INTERNAL CRACK. MAINTENANCE REPAIRED CRACKED IAW BAE ATP SRM 51-60-01, FIG 2. (M)Jul 16, 1999 · N859AW · Bag ATPSDR QXEA9901586Angle · crackedPDX - LEFT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11.Jul 16, 1999 · N821PH · Dhav DHC8102SDR DHL9970303CFairing · crackedAT C CHECK, LEFT WING NR 1 MOVABLE FAIRING GOUGED AT PREVIOUS REPAIR INNER SECTION. REMOVED PAINT FROM REPAIR AREA, REPLACED PREVIOUS REPAIR (5 BY 12) PER SRM 57-20-2 AND SRM 51-40-2, ALODINED AND REPRIMED PER SRM 51-10-2, N/R 1103.Jul 16, 1999 · N703DH · Boeing 72730CSDR AU990751Angle · corroded(AUS) RIGHT WING SPAR CAP TOP ANGLE CONTAINED INTERGRANNULAR CORROSION IN THE AREA FROM WS 76 TO WS 118.Jul 16, 1999 · Cessna 182FSDR QXEA9901518Strut · chafedPDX - LEFT STUBWING ENGINE THRUST STRUT IS CHAFFED ON TOP ABOUT MID POINT BY THE FORWARD BLEED AIR LINE. REPAIRED IAW HORIZON AIR EA 4-71-128.Jul 14, 1999 · N490US · Fokker F28MK4000SDR TWRA9928Fasteners · failedLEFT WING UPPER WEB TO CHORD FASTENERS SHEARED (ONE EACH) AT FS 636.84 AND (3 EACH) AT FS 655.75, AND FS 646.07. LOWER WEB TO CHORD FASTENERS SHEARED (23 EACH) FS 618.96 TO FS 661.37. REPLACED RIVETS IAW AD 98-15-21 AND SB 57A22266 REV 5. (X)Jul 13, 1999 · N602FF · Boeing 747124SDR TWRA9927Fasteners · crackedRIGHT WING WEB TO CHORD UPPER FASTENERS CRACKED (2 EACH) AT FS 636.84 AND FS 646.07. LOWER WEB TO CHORD FASTENERS CRACKED (ONE EACH) AT FS 636.84 AND FS 646.07. REPLACED RIVETS IAW AD 98-15-21 AND SB 57A22266 REV 5. (X)Jul 13, 1999 · N602FF · Boeing 747124SDR HNAA9900095Cover · leakingFUEL BOOST PUMP COVER HAS RUNNING LEAK. REPAIRED IAW EO8-57-99-730 & EO8-57-99-732. THIS HA-300 COVERS LEAK CHECK ONLY.Jul 9, 1999 · N937HA · Dhav DHC8102SDR USAA990691Doubler · crackedPIT - PILOT REPORT INDICATED OUTBOARD LEG COMPLETELY CRACKED OFF. INBOARD LEG 2.50 INCH CRACK AT PANEL ATTACH DOUBLER AT BOTH FORWARD EXTENDING LEGS BETWEEN RIBS 23 AND 24, LT WING. MANUFACTURED NEW DOUBLER 2024-T3 0.063 INCH PER SRM 57-51-26 FIG 9. (X)Jul 7, 1999 · N711UW · Airbus A319112SDR USAA990689Angle · crackedPIT - PILOT REPORT INDICATED 3 INCH CRACK, PIECE MISSING AT INBOARD ATTACH ANGLE FOR PANEL 575AT LEFT WING. MANUFACTURED NEW ANGLE OF 2024-TE 0.063 INCH PER DWG D575-41499. (X)Jul 7, 1999 · N711UW · Airbus A319112SDR DL72S991547Angle · crackedANGLE CRACKED APPROX 3 INCHES AND FASTENERS SHEARED AT FWD SIDE OF NR 7 SPOILER ACTUATOR CASTING. REPAIRED ANGLE PER M/M 57-20-22 PG 809 PER ERA 367745-14 REF NR 64.Jul 7, 1999 · N8890Z · Boeing 727225SDR AALA991009Angle · damagedTUL - ACCOMPLISH PERMANENT REPAIR TO LEFT WING ROOT PICK UP ANGLE. INSTALLED PERMANENT REPAIR TO LT WING ROOT PICK UP ANGLE PER ESO 3095, DATED 7-6-99. (M)Jul 7, 1999 · N11060 · Airbus A300B4605RSDR 99ZZZX3465Beam · brokenPIT - PILOT REPORT INDICATED 12 INCH SECTION BROKEN OFF BEAM ASSEMBLY, TIE, ATTACHED TO PANEL 575AT LEFT WING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (X)Jul 7, 1999 · N711UW · Airbus A319112SDR EIA990220Shear Tie · crackedHKG - DURING C/D CHECK, RIGHT WING, WS 469 RIB UPPER CHORD BETWEEN FRONT SPAR AND STRINGER 30, SHEAR TIE CRACKED. SHEAR TIE FITTING REPAIRED PER SRM 57-10-05 FIG 7. (M)Jul 6, 1999 · N481EV · Boeing 747132SDR DL72S991522Stiffener · crackedREF SHIP 497 TPA LTR CHK D-1, NR 7 SLAT I/B TRACK I/B L/E SPAR STIFFENER CRACKED. REPLACED STIFFENER PER MM 57-20-21.Jul 6, 1999 · N497DA · Boeing 727232SDR CALA9900781Support · crackedINSPECTION FOUND LT FLAP FIXED VANE SUPPORT WORN WITH A .25 INCH CRACK AT STA XFLS 171. THE FIXED SUPPORT WAS REPLACED IAW MM 27-51-3, PAGE 201.Jul 6, 1999 · N17533 · Doug DC932SDR UPS99830204Clip · crackedINSPECTION TYPE:C123, RT WING L/E, ABOVE THE NR 3 PYLON, APPROX STA XFS 267, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.Jul 5, 1999 · N874UP · Doug DC873FSDR UPS99830203Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.Jul 5, 1999 · N874UP · Doug DC873FSDR UPS99830200Doubler · crackedINSPECTION TYPE:C123, RT WING L/E AT XFS 597.5, THE SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.Jul 4, 1999 · N874UP · Doug DC873FSDR UPS99830197Doubler · crackedINSPECTION TYPE:C123, NR 3 MAIN TANK INBD AFT ACCESS PANEL LAND IS CRACKED AT 2 FASTENER HOLES, (ACCESS PANEL 505F). CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 36.Jul 4, 1999 · N874UP · Doug DC873FSDR RRXA991365Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, INTERCOSTAL TOP CUP BETWEEN LEFT WING NR 2 AND NR 3 SPOILERS AT STA XW 129. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW Jul 3, 1999 · N8091U · Doug DC871FSDR UPS99830088Doubler · crackedINSPECTION TYPE:C2 R/W L/E DOUBLER CRACKED JUST ABOVE NR 4 PYLON. FABRICATED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-1A AND 51-1-20D.Jul 1, 1999 · N809UP · Doug DC873FSDR HNAA9900096Ring · corrodedAREA WHERE ANTI-FRET RING RESTS AGAINST WITH CLAMP RING HAS SIGNS OF CORROSION APPROX DEPTH .005 - .008. REPAIRED IAW EO8-57-99-732.Jul 1, 1999 · N937HA · Dhav DHC8102SDR 9903021145Doubler · crackedDURING M CHECK, FOUND CRACK ON RIGHT WING FIXED LEADING EDGE AT XORS 593 TO 629.3. REPAIRED PER EA 11-168615.Jun 30, 1999 · N145US · Doug DC1040SDR DL72S991469Angle · crackedVERTICAL SPAR STIFFENER CRACKED NR 3 L/E SLAT I/B SIDE OF I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 PG 813.Jun 29, 1999 · N483DA · Boeing 727232SDR AT9900483Clip · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THREE OUTBOARD STRINGER CLIPS CORRODED ON LEFT WING AT XRS 111.5 BETWEEN 11-12, 12-13, AND 13-14 STRINGERS. REMOVED AND REPLACED CLIPS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED NEW CLIPS IAW DC9 SRM Jun 29, 1999 · N845AT · Doug DC932SDR UPS99830039Doubler · crackedINSPECTION TYPE:C2 RT WING L/E AT XFS 372, THE LIFT TRANSDUCER DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769589 AND SRM 51-1-21.Jun 25, 1999 · N750UP · Doug DC871FSDR EIA990197Fitting · crackedHKG - DURING C/D CHECK, LEFT WING WS 670 FRONT SPAR VERTICAL SUPPORT FITTING HAS 2 FASTENER HOLES CRACKED. RIB FITTING REPLACED IAW SB 747-57A2273 FIG 5. (M)Jun 25, 1999 · N481EV · Boeing 747132SDR DHL9970242CBracket · crackedC-CHECK, RT WING T/E COVE PNL SUPPORT BRACKET CRACK AT FASTENER HOLE, I/B END OF NR 11 SPOILER PNL AND BELOW. REPLACED BRACKET AT I/B END OR NR 11 SPOILER PNL AS PER B77 SRM 51-10-1 PAR 4 AND 51-30-2. N/R 2083.Jun 23, 1999 · N702DH · Boeing 72730CSDR DHL9970229CSupport · crackedC CHECK, RT WING L/E STRUCTURE, CEILING CROSS SUPPORT CRACKED AT O/B END, L/E STA 130.7. REMOVED UNSERVICEABLE CROSS SUPPORT AND REPLACED WITH NEW EXTRUSION ANGLE AS PER B727 CHAP 51-30-2 MAT USED 7075-T6 .75 BY3.75 BY X 16 LOT NR 354192 PO NR 831451. ALODINJun 23, 1999 · N702DH · Boeing 72730CSDR DHL9970222CSupport · crackedC CHECK, RT WING L/E STRUCTURE WBL 92.8 VERT SUPPORT CRACKED AT BOTTOM WITH SEVERAL STOP DRILLED HOLES. CUT OUT DAMAGED SECTON, INSTALLED ANGLE REPAIR 1 BY 1.5 BY 7 PER SRM 51-40-3, N/R 2055.Jun 23, 1999 · N702DH · Boeing 72730CSDR CALA9900790Bolt · brokenINSPECTION FOUND TRAPEZOIDAL PANEL BOLT IN RT MLG WHEEL WELL BROKEN AT STA 1370. THE BOLT WAS REPLACED IAW MM 20-50-02.Jun 23, 1999 · N17085 · Doug DC1030SDR CALA9900789Strap · crackedINSPECTION FOUND A 1.5 CRACK IN RT WING LOWER SKIN LEADING EDGE STRAP BETWEEN STA XORS 433 AND XORS 455. A NEW STRAP WAS INSTALLED IAW DRAWING ARB2935 AND SRM 51-31-01.Jun 19, 1999 · N17085 · Doug DC1030SDR CALA9900787Strap · crackedINSPECTION FOUND A 2 INCH EFTACK IN LEFT WING LEADING EDGE STRIP AT STA XORS 455 AND XORS 506. REPAIRED IAW DRAWING 2933 AND SRM 51-30-00.Jun 19, 1999 · N17085 · Doug DC1030SDR UPS99830034Doubler · crackedINSPECTION TYPE:C2 RT WING L/E AT XFS 598, THE INNER DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.Jun 18, 1999 · N750UP · Doug DC871FSDR UPS99829978Fitting · crackedINSPECTION TYPE:C-1, STRINGER-51 NR 2 MAIN O/B AT WS 74.00 REAR SPAR HAS FWD FITTING CRACKED. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.Jun 18, 1999 · N807UP · Doug DC873FSDR UPS99830030Doubler · crackedINSPECTION TYPE:C2 LT WING L/E LWR SKIN, INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.Jun 17, 1999 · N750UP · Doug DC871FSDR TSAA9957314Fitting · corrosionRIGHT WING FRONT SPAR WEB CORROSION AT FSS 435. REPAIRED IAW ECO 2970. (M)Jun 17, 1999 · N804AL · Boeing 7372Q9SDR UPS99829970Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 2 MAIN O/B AT W/S 74.000 REAR SPAR HAS AFT FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW DAC DAW 5613423 AND DC8 SRM 51-1-20 D.Jun 15, 1999 · N807UP · Doug DC873F
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