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 DHL2003804549Fitting · crackedRT ZEE PAN WING ZEE PAN FITTING CRACKED 2.00STA. XW 223.000 CORR: REMOVED FITTING ZEE PAN(CRACKED CONDITION)IAW SRM51-3-0 PG. 1 CLEANED , TREATED, & PRIMED AREA IAW SRM51-1-8B , INSTALLED NEW FITTING ZEE PAN ON RH WING L/E , STA. XW 233.000 IAW SRM51-3-0 PG. 1Feb 6, 2003 · N804DH · Doug DC873FSDR AUS20030093Lift Strut · out of adjust(AUS) WING LIFT STRUTS (4OFF) PNO 2200E AND PNO 2201E OUT OF ADJUSTMENT RESULTING IN THE MAINPLANES NOT BEING SYMMETRICAL WITH THE FUSELAGE. LIFT STRUTS HAD BEEN FITTED ON 10 MAY 1996 IAW AD/ML-M7/2.Jan 31, 2003 · Maule MX7180SDR IXXA060515SWeb · gougedDURING ROUTINE C CHECK, FOUND LEFT MAIN LANDING GREA STRUT CUTOUT AFT VERTICAL WEB GOUGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 51-1-21, 51-1-8, AND DOUGLAS DRAWING 5651221.Jan 21, 2003 · N820BX · Doug DC871FSDR 2003F00100Bracket · crackedSTRUCTURAL FAILURE (SUPPORT ASSY- FLAP ACTUATOR) PILOT REPORTED FLAPS SELECTED TO 10 DEG, FLAPS OPERATED TO 10 DEG, AT THE NEXT FLAP SELECTION THE FLAP CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE Jan 20, 2003 · N1276P · Cessna 208BSDR P5CA0300724Stiffener · corrodedCORROSION LEVEL 1 FOUND R/H WING LEADING EDGE FRONT SPAR "L" STIFFENER AT FSSI 1435 LOWER PORTION. REPAIR CARRIED OUT IAW SRM 51-30-02.Jan 12, 2003 · N922FT · Boeing 7472U3BSDR P5CA0300723Stiffener · corrodedCORROSION LEVEL 1 FOUND LEADING EDGE TOP PANEL SUPPORT RIB AT STA. FSS 1336.00, "L" ANGLE STIFFENER TO FRONT SPAR. "L" ANGLE REPAIR CARRIED OUT AS PER SRM 51-30-02.Jan 12, 2003 · N922FT · Boeing 7472U3BSDR QXEA0300097Channel · corrodedPDX- LEFT HAND WING LOWER STATION 2230 RIB 'U' CHANNEL HAS EXFOLIATION CORROSION ON THE INTERIOR INBOARD RADIUS AT STRINGER 2.14 APPROXIMATELY .35 INCHES LONG. REPAIRED IAW FOKKER SRM 57-01-01.Jan 11, 2003 · N497US · Fokker F28MK4000SDR QXEA0300096Channel · corrodedPDX- LEFT HAND WING LOWER STATION 2230 RIB 'U' CHANNEL HAS EXFOLIATION CORROSION ON THE INTERIOR AT STRINGER 2.13 APPROXIMATELY .5 INCHES LONG. REPAIRED IAW FOKKER SRM 57-01-01.Jan 11, 2003 · N497US · Fokker F28MK4000SDR ASAA0380021Bracket · chafedOKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE PANEL 1248C BRACKET IS CHAFED. REPLACED CHAFED AREAS OF BRACKET PER SRM 51-10-2 AND 51-30-2. (M)Jan 4, 2003 · N972AS · Doug DC983SDR ASAA0380008Support · crackedOKC - FOUND DURING 30K CHECK, RIGHT WING TRAILING EDGE INNER SUPPORT FORMER CRACKED AT FORWARD EDGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-10-2, 51-10-4, AND 51-30-2. (M)Jan 3, 2003 · N972AS · Doug DC983SDR AUS20030304Stiffener · corroded(AUS) FORWARD SPAR LEADING EDGE VERTICAL STIFFENER CONTAINED LEVEL 2CORROSION LOCATED AT STN236. FOUND DURING CPCP INSPECTION IAW C57-562-02.Jan 2, 2003 · Boeing 727277SDR SROM200200027Gusset · gougedDURING C CHECK INSPECTION FOUND NUMBER TWO FIXED FAIRING NR 3 RIB GUSSET GOUGED. REMOVED, FABRICATED AND INSTALLED # 3 RI GUSSET PER SRM 54-30-1 & 51-30-2. MINOR REPAIR.Dec 17, 2002 · N736BP · Boeing 737205SDR SROM200200026Gusset · gougedDURING C CHECK INSPECTION FOUND NUMBER ONE O/B FIXED FAIRING UPPER AFT GUSSET GOUGED. REMOVED, FABRICATED AND INSTALLED GUSSET PER SRM 54-10-2 & 51-30-2. MINOR REPAIR.Dec 17, 2002 · N736BP · Boeing 737205SDR ASAA0240242Angle · crackedPAE - DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE HAS A CRACKED ANGLE AT RSS 545. REPAIRED IAW SRM. (M)Dec 14, 2002 · N764AS · Boeing 7374Q8SDR UPS02239970Angle · corrodedINSPECTION TYPE:C SMALL AREA OF CORROSION NOTED IN R/H WING T/E STRUCTURE WS 383, ANGL E BETWEEN SUPPORT WEB & UPPER T/E SKIN REMOVED FASTNERS FROM CORRODED AREA AS PER SRM 51-30-02 & CUT AND TR IMMED ANGLE AS PER SRM 51-20-00. FABRICATED REPAIR PARTS IAW Dec 6, 2002 · N906UP · Boeing 72730CSDR QXEA0202040Support Bracket · crackedPDX - RIGHT WING UPPER FRONT SPAR LEADING EDGE 611AR SUPPORT BRACKET NEAR NACELLE CRACKED. REPAIRED IAW RD 8-57-078.Nov 29, 2002 · N365PH · Dhav DHC8202SDR QXEA0202039Support Bracket · crackedPDX - RIGHT WING FRONT SPAR LEADING EDGE SUPPORT BRACKET CRACKED. LONG BRACKET FOR 611AR NEAR NACELLE. REPLACED IAW RD 8-57-078.Nov 29, 2002 · N365PH · Dhav DHC8202SDR 02FDEA00875Support · crackedLT WING L/E WING SUPPORT FOUND CRACKED AT NR 16 SLAT TRACK.Nov 26, 2002 · N587FE · Doug MD11SDR CALA0200558Stiffener · crackedINSPECTION FOUND A 7" CRACK IN STIFFENER AT I/B SIDE OF WEB, L/H WING STA 453. REPAIRED IAW ECRA 5713-01000.Nov 22, 2002 · N14336 · Boeing 7373T0SDR ASAA0240223Angle · crackedDURING SI CHECK, FOUND ANGLE CRACKED ON LEFT WING TRAILING EDGE. REPAIRED IAW EA. (M)Nov 21, 2002 · N784AS · Boeing 7374Q8SDR ASAA0240196Support · damagedDURING SI CHECKED, FOUND LEFT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 RIGHT AND BS 729. REPAIRED IAW SRM. (M)Nov 13, 2002 · N784AS · Boeing 7374Q8SDR ASAA0240195Support · damagedPAE - DURING SI CHECKED, FOUND RIGHT WING UPPER TRAILING EDGE PANEL SUPPORT HAS FASTENER HOLE ELONGATED AT WBL 70 AT BS 729. REPAIRED IAW SRM. (M)Nov 13, 2002 · N784AS · Boeing 7374Q8SDR ASAA0240193Support · chafedPAE - DURING SI CHECKED, FOUND RIGHT WING TRAILING EDGE PANEL SUPPORT IS CHAFED ABOVE PYLON CUTOUT. REPAIRED IAW SRM. (M)Nov 13, 2002 · N784AS · Boeing 7374Q8SDR UPS02439870Stiffener · corrodedA STIFFENER CORRODED CENTER SECTION REAR SPAR. LBS. 85.6 HAS CORROSION. APPROX. 11 INCHES LONG. NEXT TO FUEL PUMP APERATURE. REMOVED VERTICAL STIFFNER PER SRM 51 30 02 39550/ INSTALLED NEW STIFFNER PER SRM 51 10 01 REPLACEMENT OF PART. REF LOG 914476 ITEM Nov 3, 2002 · N672UP · Boeing 747123SDR CALA0200515Angle · crackedSUPPORT ANGLE CRACKED TWO PLACES FORWARD OF NR 3 FLAP TRACK FAIRING. REPLACED SUPPORT COLLAR ANGLE PER SRM 51-40-02.Oct 29, 2002 · N39343 · Boeing 7373T0SDR CALA0200514Stiffener · wornHOCKEY STICK WORN IB EDGE OF NR 3 FLAP TRACK FAIRING. REPLACED HOCKEY STICK IB EDGE OF NR 3 FLAP TRACK FAIRING PER SRM 51-40-02.Oct 29, 2002 · N39343 · Boeing 7373T0SDR ASAA0210259Support · crackedPAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FOR WALKING BEAM AT LEFT WING REAR SPAR STATION 201.85, CRACKED. REMOVED AND REPLACED SUPPORT FOR WALKING BEAM PER MANUFACTURER'S DRAWING. (M)Oct 28, 2002 · N743AS · Boeing 737210CSDR GAIA02137STWeb · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE WEB AT WING STATION 130.7 UPPER CHORD IS CRACKED ABOUT 10 INCHES LONG. REPAIRED ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225SDR GAIA02136STStiffener · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING FRONT SPAR AT FSS 106.8 VERTICAL STIFFENER IS CRACKED AT THE FORWARD END. REPAIR ACCOMPLISHED IAW BOEING 727 SRM 57-30-4, FIGURE 7. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225SDR ASAA0280412Strap · crackedOKC - FOUND 30K CHECK, RIGHT WING LEADING EDGE SPLICE STRAP IS CRACKED AT STATION XRS 164, XFS 299. REPLACED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M)Oct 21, 2002 · N976AS · Doug DC983SDR UPS02839882Fitting · crackedINSPECTION TYPE:C-2 LT WING STR 51, O/B FWD STRINGER END FITTING IS CRACKED. RECEIVED NEW FITTING LOCATED & DRILLED FITTING IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.Oct 21, 2002 · N798UP · Doug DC871FSDR UPS02839881Fitting · crackedINSPECTION TYPE:C-2 LT WING STR 51 I/B END, STR END FITTING CRACKED. RECEIVED NEW FITTING LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-3-0 & 51-1-20D.Oct 18, 2002 · N798UP · Doug DC871FSDR SWAA022503Casting · crackedDURING SCHEDULED C4 CHECK, FOUND BOTH LT/RT WING FLAP CASTING CRACKED (BETWEEN FLAP AND AILERON) OTBD OF OTBD FLAP. REPAIRED CASTINGS PER SWA EA.Oct 18, 2002 · N712SW · Boeing 7377H4SDR DHL2002720520Structure · corrodedDURING C CHECK, T/E FALSE SPAR UPPER BEAM IS CORRODED AFT. OF RT MLG AFT. TRUNNION. REPAIRED IAW SRM.Oct 11, 2002 · N720DH · Boeing 727228SDR AALA20021532Casting · gougedTUL - FOUND LEADING EDGE SLAT CABLE PULLEY CUT GROOVE IN NR 1 SLAT CASTING INBOARD SIDE FORWARD SIDE OF CASTING RT WING. BLENDED GOUGE AND INSTALLED DOUBLER PER ESO 80559. (M)Oct 10, 2002 · N553AA · Doug DC982SDR MV52002F00005Bracket · crackedLT WING OUTBOARD FLAP INBOARD ATTACHMENT TO THE WING HAD A CRACK IN THE BRACKET ON THE WING LOWER AFT BOLT. CRACK WAS ONE INCH LONG IN A FORWARD AND AFT DIRECTION.Oct 8, 2002 · N2VA · Gulstm 695BSDR AWXA200201006Stiffener · crackedDURING C-17 CHECK A 1 3/4 INCH CRACK WAS FOUND ON THE LOWER AFT END OF STIFFENER AT LT WING NR 3 FLAP FAIRING, WS 184.40 TO WS 191.00. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT WS 184.40 TO WS 191.00, FABRICATED A NEW REPLACEMENT STIFFENER, AND INSTALLED ROct 7, 2002 · N324AW · Boeing 737301SDR DHL2002720529Stiffener · crackedDURING C CHECK, VERTICAL STIFFENER IS CRACKED ON LEFT WING FRONT SPAR, LOWER END. LWS 130. REPAIRED IAW SRM.Oct 6, 2002 · N720DH · Boeing 727228SDR AWXA200201002Support · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 3" CRACK WAS FOUND ON THE INTERCOASTAL FOR AFT CARGO COMPARTMENT DOOR LATCH SUPPORT, BS 787. MAINTENANCE REMOVED THE CRACKED AFT CARGO COMPARTMENT DOOR LATCH SUPPORT AT BS 787, FABRICATED A NEW REPLACEMENT SUPPORT, AND Oct 5, 2002 · N324AW · Boeing 737301SDR SWIA200211379Clip · crackedRIGHT FUEL CELL RIB NR 15, 3RD CLIP FROM FORWARD (LONGER CENTER CLIP) CRACKED AT FORWARD END. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED CLIP IAW SRM 51-40-02.Oct 3, 2002 · N585SW · Emb EMB120ERSDR AWXA200201000Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/2" CRACK WAS FOUND ON THE L/H UPPER WING PANEL ATTACH ANGLE OUTBOARD OF THE PYLON, WS 204.40. MAINTENANCE REMOVED CRACKED L/H UPPER WING PANEL ATTACH ANGLE AT WS 204.40, FABRICATED A NEW REPLACEMENT ATTACH ANGLE, ANOct 3, 2002 · N324AW · Boeing 737301SDR AWXA200200990Angle · crackedMCN - MAJOR REPAIR - DURING C-12 CHECK A 1/4" CRACK WAS FOUND ON LOWER SURFACE L/H WING CLOSE OUT WEB SUPPORT ANGLE 33" OUTBOARD OF THE INBOARD END OF AILERON, WS 538. MAINTENANCE REMOVED THE DAMAGED ANGLE FROM CLOSE OUT WEB WS 538, FABRICATED A NEW REPLACEMENOct 1, 2002 · N322AW · Boeing 7373G7SDR QXEA0201667Stiffener · gougedPDX - GOUGE AND POSSIBLE CRACK ON RT CONTROL CABLE PULLEY BRACKET STIFFNER AFT OF RT BLEED AIR LINE SHROUD COUPLING UNDER PANEL 261JT, STATION X381. REPAIRED IAW DHC-8 SRM 51-20-11 AND MM 20-32-02, TASKJ 20-32-02-390-801 AND MM TASK 20-34-08-400-801.Sep 30, 2002 · N368PH · Dhav DHC8202SDR DHL2002803516Doubler · crackedLT WING CENTER L/E INNER DOUBLER AT STA XFS 435.000 WITH 2 INCH CRACK IN IT. REMOVED DAMAGED DOUBLER PER SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075.T6 AL0.080) PER SRM57-2-0 FIG 2. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 5Sep 27, 2002 · N803DH · Doug DC873SDR DHL2002803529Doubler · brokenLT WING CENTER L/E INTERNAL PART SHOWS DOUBLER BROKEN (2IN) AT XFS 521.250. REMOVED DAMAGED DOUBLER PER SRM 57-2-0 FIG 2. FABRICATED NEW DOUBLER (7075T6AL0.050) PER SRM 57-2-0. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 ANDSep 26, 2002 · N803DH · Doug DC873SDR 2002UALA01490Stiffener · gougedLEFT HAND WING S12 Z STIFFENER GOUGED ON EDGE OF LOWER FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE.Sep 25, 2002 · N945UA · Boeing 737522SDR DHL2002803518Pan · crackedRT WING L/E PAN UPPER PART CRACKED 2 INCH, XFS 327.000. REMOVED ZEE PAN PER SRM 51 1 20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN FITTING PER SRM 51-1-20D PG 9.Sep 24, 2002 · N803DH · Doug DC873SDR QXEA0201559Bracket · crackedPDX - LEFT HAND LEADING EDGE 511AL MOUNTING BRACKETS CRACKED, TOP AND BOTTOM. REPAIRED IAW DHC-8 MM 51-11-00.Sep 24, 2002 · N368PH · Dhav DHC8202SDR QXEA0201568Bracket · crackedPDX - RIGHT HAND LEADING EDGE 611AR MOUNTING BRACKETS CRACKED AT TOP AND BOTTOM. REPAIRED IAW D8 MM 51-11-00.Sep 24, 2002 · N368PH · Dhav DHC8202SDR USAASB02177Seal · tornDURING CLIMB OUT, ENROUTE, AIRCRAFT DEVELOPED A MODERATE LATERAL AIRFRAME VIBRATION. VIBRATION OCCURRED AT ALL SPEEDS BETWEEN 235 AND 335 KNOTS, WITH OR WITHOUT AUTOPILOT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARSep 22, 2002 · N433US · Boeing 7374B7
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