JASC 5740

Service difficulty reports · 3,003

Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740'
  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 MWEA020507Stringer · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020494Stringer Clip · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020487Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTENDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION.Aug 13, 2002 · N800ME · Doug DC914SDR MWEA020486Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTENDING UNDER STRINGER 11. -- REMOVED CORRORION.Aug 13, 2002 · N800ME · Doug DC914SDR MWEA020480Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXTENDING UNDER STRINGERS 16 AND 17.Aug 13, 2002 · N800ME · Doug DC914SDR COOSDR020224Stiffener · crackedLEFT WING TRAILING EDGE AREA AT XRS407.000 CRACKED STIFFENER.Aug 1, 2002 · N602AL · Doug DC873FSDR UPS02438931Fitting · crackedINSPECTION TYPE:C, RIGHT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 8 HOLE CRACK FOUND APPROX 0.030 INCH, RUNNING I/B AND NR 3 HOLE CRACK FOUND AT FWD AND AFT DIRECTION. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPJul 17, 2002 · N677UP · Boeing 747123FSDR CA020715003Attach Angle · cracked(CAN) CRACK FOUND AT ATTACH FASTENER HOLE AT LOWER SPAR LOCATION DURING NDT REQUIRED BY AD 1997-07R2 WHOSE REQUIREMENTS ARE EVERY 415 FLIGHT HOURS OR 1500 WATER DROPS, WHICHEVER COMES FIRST. THIS AIRCRAFT HAD 1250 WATER DROPS SINCE THE LAST COMPLIANCE OF THIS Jul 12, 2002 · Cndair CL2151A10SDR UPS02438929Fitting · crackedINSPECTION TYPE: C, CRACK REVEALED AT RT OF BS 1241 REAR SPAR TO WING CENTER SECTION SPLICE FITTING SIGNAL INDICATION GREATER THAN 50 PERCENT FSH. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-F APPENJun 28, 2002 · N677UP · Boeing 747123FSDR ABXA020110Spar Cap · crackedRIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25.Jun 16, 2002 · N826AX · Doug DC863SDR UPS02238841Pin · corrodedINSPECTION TYPE:C+SI CORROSION ON RT WING FRONT SPAR BOTTLE PIN HEAD AFT FLANGE. BOTTLE PIN REPLACED IAW MM57-41-01.Jun 12, 2002 · N942UP · Boeing 72722CSDR S5248Fitting · corrodedRIGHT AFT WING ATTACMENT FITTING CORRODED,INSPECTED IAW PSB977 CORROSION MORE THAN SURFACE DEEP PITSJun 12, 2002 · N882TM · Piper PA32R300SDR ASAA0210124Fitting · crackedPAE - DURING SCHEDULED C-CHECK, FOUND LT MLG BEAM TO SPAR FITTING AT WING STATION 150-162 CRACKED. REPAIRED FITTING PER EA AND SERVICE BULLETING. (M)May 15, 2002 · N740AS · Boeing 737290CSDR ABXA010892Strap · brokenLOWER FRONT SPAR CAP, OUTBOARD OF #3 PYLON, #4 MAIN STRAP WAS BROKEN. REPLACED STRAP AND COMPLIED WITH REA #D857-43875.May 8, 2002 · N813AX · Doug DC863SDR KQ72002F00000Fitting · crackedDURING C5 AND C6 CHECK WITH FLAPS REMOVED FOR CPCP INSPECTION FOUND THE RT INBOARD FLAP INBOARD CARRIAGE AFT TRUNION BEARING SUPPORT CRACKED THROUGH INTIRE UPPER PART OF CASTING WHERE AFT BEARING SUPPORTS THE INBOARD FLAP CARRIAGE ASSEMBLY SPINDLE. THE FLAP CMay 1, 2002 · N727WF · Boeing 72723SDR 2002F00792Pin · corrodedAT C-CHECK, FOUND LEFT WING FORWARD BOTTLE PIN CORRODED. (M)Apr 24, 2002 · N8878Z · Boeing 727225SDR DHL2002807561FittingLT WING REAR SPAR AUX INTERIOR SHOWS A CRACKED FITTING 2 IN AT STA XW 80.000.REMOVED CRACKED FITTING PER SRM 51-3-0 PG 1.FABRICATED NEW FITTING (7075-T651).CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG1Apr 19, 2002 · N807DH · Doug DC873FSDR EIAA2002029Fitting · crackedMZJ - FOUND IN C-CHECK, LT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT T-FITING CRACKED AT THE NR 4 FLAP TRACK. INSTALLED NEW T-FITTING PER SRM 51-30-05. (M)Mar 30, 2002 · N479EV · Boeing 747132SDR DHL2002705543Support FittingUPON COMPLYING WITH VISUAL INSP OF LEFT WING, FOUND # 4 SPOILER ACTUATOR SUPPORT BRKT BOTTOM LEG CRACKED AND INBD AFT SPAR MOUNT ANGLE CRACKED AT LOWER END.Mar 27, 2002 · N705DH · Boeing 72722CSDR DHL2002807558FittingDURING C CHECK, FOUND L/H INBD FLAP WELL FITTING WITH CRACK IN IT AT STA XW 70.000.REMOVED DAMAGED FITTING AT STA. 70.000 PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG 1.Mar 12, 2002 · N807DH · Doug DC873FSDR COOSDR02025Fitting · corrodedRT WING, TRAINLING EDGE AT WS383.5, FITTING CORRODED.Mar 1, 2002 · N199AJ · Boeing 7272F9SDR CA020304001Fitting · cracked(CAN) INSPECTION REVEALED A SMALL CRACK IN THE WEB WHERE IT JOINS THE LOWER RIGHT BOLT HOLE.THE CRACK RUNS PERPENDICULAR TO THE WEB.PART TIME IS UNKNOWN, TIME GIVEN IS AIRFRAME TIME.Feb 27, 2002 · Piper PA31350SDR USAA020068Fitting · crackedPIT - FOUND LEFT MLG BEAM SUPPORT FITTING 1 INCH LONG VERTICAL CRACK, TOP INBOARD FASTENER FROM BEAM PIN SLOT TO FTG EDGE. REPLACED FITTING PER BOEING SB 737-57-1216 REV 2 DATED 5/6/99 AND EA 73242. (M)Jan 23, 2002 · N391US · Boeing 7373B7SDR ABXA010738Fitting · crackedRIGHT WING AUX SPAR, LOWER "L" ANGLE, WAS CRACKED APPROXIMATELY 10 INCHES LONG AT XRS 47. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-1-8 AND 51-1-20D.Jan 23, 2002 · N847AX · Doug DC861SDR 2002F00044Attach Bolt · wornRIGHT FORWARD LOWER WING ATTACH BOLT WORN WHICH ALLOWED MOVEMENT BETWEEN RIGHT LOWER WING AND FUSELAGE ATTACH FITTINGS. THIS CONDITION WAS DETECTED AUDIBLY WHILE TAXING WITH A FULL FUEL LOAD.Jan 22, 2002 · N913RC · Cessna 500CESSNASDR AWXA200200087Attach Fitting · chafedDURING C-13 CHECK DAMAGE WAS FOUND TO THE LT WING NR 2 L/E SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 2 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.Jan 13, 2002 · N331AW · Boeing 737317SDR UPS02237448Pin · corrodedINSPECTION TYPE:C+SI LEFT BS 740 TERMINAL PIN IS CORRODED IN AREA UNDERNEATH HEAD, AND PIN RETAINING BOLT HAS PITTING CORROSION. LEFT BS 740 TERMINAL PIN AND RETAINING BOLT REPLACED IAW MM 57-41-04.Jan 12, 2002 · N940UP · Boeing 727185CSDR 0200063215Fitting · corrodedDuring "M" check found corrosion in three holes of inner rear spar anchorage fitting. Repaired per EA 32-184839.Jan 9, 2002 · N315US · Airbus A320211SDR AWXA200200086Attach Fitting · damagedDURING C-13 CHECK DAMAGE WAS FOUND TO THE RT WING NR 5 SLAT ACTUATOR ATTACH RIB WS 189. MAINTENANCE DRESSED OUT DAMAGE TO NR 5 SLAT ACTUATOR ATTACH RIB, FABRICATED REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIRS. SLAT REMOVED AND REINSTALLED.Jan 7, 2002 · N331AW · Boeing 737317SDR MWEA030040Doubler · crackedLEFT WING LEADING EDGE INTERNAL DOUBLER IS CRACKED AT STATION XIS 194 -- REMOVED, FABRICATED AND INSTALLED INTERNAL DOUBLER.Jan 7, 2002 · N803ME · Doug DC981SDR F3LA200100138Bushing · corrodedDURING C-1 CHECK, INSPECTION REPORTED ALL BUSHINGS CORRODED ON RT WING SWING LINK ASSY. REPLACED RT WING SWING LINK ASSY PER BOEING DRAWING 65-82770 AND MM 57-15-0, STEP 5E.Dec 15, 2001 · N270FL · Boeing 7372L9SDR FGQ2001F00000Fitting · corrodedINSPECTION OF LEFT WING ASSEMBLY REVEALED SEVERE EXFOLIATION CORROSION OF WING ATTACH FITTING (FWD) EXTENDING, APPROXIMATELY 18 INCHES OUTBOARD WING SKIN WAS LIFTED UP FROM SPAR.Dec 1, 2001 · N3562Y · Cessna 182FSDR 0104839855Fitting · corrodedDuring Mck in DHN, the LH MLG fitting side brace lug was found with corrosion on the forward and aft faces. Repaired per EA 98-186771.Nov 27, 2001 · N764NC · Doug DC951SDR DL73K011796Track · corrodedTHE REAR ENGINE MOUNT ATTACH HOLES ON THE #2 AND #3 TE O/B FLAP TRACKS WERE FOUND CORRODED. THE BORES WERE OVERSIZED TO .939" AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 13, 2001 · N321DL · Boeing 737232SDR ABXA010643Fitting · damagedDURING THE SIDE LINK FITTING REPLACEMENT ON THE RIGHT WING, DISCOVERED THAT TWO EXISTING ATTACHMENT HOLES WERE ALREADY SECOND OVERSIZED, WHILE SERVICE BULLETIN ALLOWED THE HOLES TO BE ENLARGED (AFTER COLDWORK) TO A MAXIMUM OF SECOND OVERSIZE. ONE OF THE HOLESSep 30, 2001 · N791AX · Boeing 767281SDR UPS01237075Splice Plate · crackedINSPECTION TYPE:C RIGHT MAIN W/W CENTER SPLICE PLATE CRACKED AT STR 18A RT. STA 935 STOP DRILLED END OF CRACK IAW B727 SRM 51-10-1. INSTALLED REPAIR IAW EO B727-5330-3815A ON FUSELAGE SKIN BS 935 STR 18A R/H SIDE.Sep 19, 2001 · N938UP · Boeing 727173CSDR UPS01237072Splice Plate · crackedINSPECTION TYPE:C LEFT MAIN WHEEL WELL CENTER SPLICE PLATE, CRACK AT STR 18 ALT BS935 STOP DRILED END OF CRACK IAW B727 SRM 51-10-10, INSTALLED REPAIR STR 18 ALT SIDE FUSELAGE SKIN IAW B727 EO B727-5330-3815A.Sep 19, 2001 · N938UP · Boeing 727173CSDR 2002F00861Attach Fitting · crackedWING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP, SMALL ANGLE, CRACKED AT BS 870 AND BBL 0. (M)Aug 22, 2001 · N356QS · Boeing 72721SDR QXEA0101315Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW195. REPAIRED IAW DHC-8 RD8-57-1675, RM 51-20-16, AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101314Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE AT YW288. REPAIRED IAW DHC-8 RD8-57-1675, SRM 51-20-36, AND SRM 51-20-16.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101313Flange · gougedPDX-GOUGES ON TOP SURFACES OF RIGHT WING LEADING EDGE FLANGE AT YW202. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-16 AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101312Flange · gougedPDX-GOUGES ON TOP SURFACE RIGHT WING LEADING EDGE FLANGE AT YW315. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101311Flange · gougedPDX-GOUGES ON TOP SURFACEOF RIGHT WING LEADING EDGE FLANGE AT YW297. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101310Flange · gougedPDX-GOUGES ON TOP SURFACE OF RIGHT WING LEADING EDGE FLANGE FROM YW321 TO YW326. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR QXEA0101308Flange · gougedPDX-GOUGES ON TOP SURFACE OF LEADING EDGE FLANGE AT RIGHT WING STATION YW376. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36.Aug 3, 2001 · N349PH · Dhav DHC8202SDR MWEA011078Rib · crackedLEFT WING #3 SLAT DRIVER OUTBOARD FITTING HAS A SMALL 1/8" CRACK ACROSS THE SIDE TO SIDE GUIDE ROLLER LOBE. -- REMOVED CRACKED RIB, LOCATED BOTH INBOARD AND OUTBOARD FITTING, INSTALLED RIB.Jul 30, 2001 · N202ME · Doug DC932SDR MWEA011054Skin · crackedNUMEROUS CRACKS ON LEFT WING UPPER AND LOWER INNER SKIN OF #2 LEADING EDGE, BETWEEN STATIONS XFS 202.400 - 299.939. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS.Jul 17, 2001 · N700ME · Doug DC914SDR AUS20010642Bolt · corroded(AUS) LOWER RH SIDE STRUT LOWER BOLT SEIZED. FOLLOWING BOLT REMOVAL ITWAS FOUND TO BE VERY RUSTED AND PITTED.Jun 14, 2001 · Bbavia 7GCAASDR 0104379971Skin · crackedDuring A H Ck inATL, a crack was found in the lower skin of the LH inbd slat at station Xis =136.42. Stopped drilled and doubler installed 2014-t6 AL. Repaired per EA 99-181273Jun 12, 2001 · N9335 · Doug DC931SDR CA010625017Bracket · cracked(CAN) AILERON SUPPORT BRACKET AT BOLT HOLE WERE FOUND CRACKED WITH THE RIGHT HAN D PART COMPLETLY BROKEN AS PER PHOTO. SUSPECT CAUSE-CONTROLS NOT SECURED BUT ALLOWED TOFLOP AROUND DURING WINDY CONDITIONS, PROBABLY OVER A PERIOD OF TIME._P/N'S 62102-000(LEFT) 6Jun 5, 2001 · Piper PA28140
Back to JASC 5740