JASC 5711

Service difficulty reports · 5,587

Reports filed under 5711 · Wing Spar, 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 = '5711'
  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 COOSDR030070Spar · corrodedLT WING, FRONT SPAR LOWER CHORD PLATE, LOWER SURFACE CORRODED, BETWEEN SS 130.250 AND SS 143.750.Jan 1, 2004 · N79745 · Boeing 727224SDR COOSDR030057Spar · crackedRT WING, REAR SPAR LOWER CHORD SECTION, FROM WBL 113 INCHES TO WBL 130 INCH OB SPLICE PN 65-50821-142.Jan 1, 2004 · N767TW · Boeing 737200SDR TSAA0457016Spar · corrodedDISCOVERED CORROSION AT WBL 349 AND 503 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED ARE PER SRM 57-30-1, FIGURE 1A AND 1B INSTRUCTIONS. FABRICATED AN .020 INCH THICK EXTERNAL REPAIR DOUBLER FROM 7075-T6 SHEET. CLEAN ANDDec 20, 2003 · N820AL · Boeing 737230SDR TSAA0457015Spar · corrodedDISCOVERED CORROSION AT WBL 245, 254, 336, AND 341 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED AREA PER SRM 57-30-1, FIGURES 1A AND 1B INSTRUCTIONS. REMOVED FASTENERS IN THE BLEND OUT AREA. INSTALLED HI-LOCKS WET WITH BDec 20, 2003 · N820AL · Boeing 737230SDR AUS20031280Spar · corroded(AUS) LT WING REAR SPAR CORRODED. FOUND DURING INSPECTION IAW AD/PA28/40A.Dec 18, 2003 · Piper PA28180SDR AUS20031278Spar · corroded(AUS) RT WING REAR SPAR CORRODED. FOUND DURING INSPECTION IAW AD/PA28/40A.Dec 18, 2003 · Piper PA28180SDR QXEA200301599Spar · chafedPDX- RIGHT HAND LEADING EDGE LOWER FORWARD SPAR HAS CHAFE DAMAGE AT INBOARD END, 3 INCHES LONG AT WING STATION YW57.000. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-20-26.Dec 18, 2003 · N353PH · Dhav DHC8202SDR AUS20031334Doubler · corroded(AUS) WING SPAR DOUBLERS PN 68-1.4009-3 AND PN 68-1.4009-4 CONTAINED A SMALL AMOUNT OF CORROSION. DOUBLERS ARE LOCATED IN AREA BEHIND ENGINES AND ENGINE FIREWALLS.Dec 15, 2003 · Parten P68BSDR 2003FA0001255Spar · corrodedLEFT FRONT SPAR SHOWS EXFOLIATION CORROSION ABOUT 12 INCHES FROM ROOT. HAD BEEN INSPECTED AND COATED WITH PRIMER, THEN SIGNED OFF AS AIRWORTHY. THIS CORROSION APPEARED TO BE 75 PERCENT THROUGH BOTTOM SPAR FLANGE.Dec 8, 2003 · N94107 · Univar 415CSDR ARWA20031204Spar · crackedDURING ACCOMPLISHMENT OF RB 17284 SB 57-090 INSPECTION. LEFT WING FRONT SPAR XFS 517 & XFS 518, LOWER CAP HOLES (2 EACH) WITH CRACKS.Dec 6, 2003 · N810BN · Doug DC862SDR CA031127003Attach Fitting · cracked(CAN) DURING AN UNSCHEDULED INSPECTION A SMALL CRACK WAS FOUND IN THE UPPER FORWARD WING ATTACH FITTING, THE CRACK WAS APPROXIMATELY .0625 OF AN INCH LONG STARTING AT THE TOOLING HOLE HEADING TOWARD THE TUB. THE AIRCRAFT IS GROUNDED WAITING FOR WING SPAR REPLNov 25, 2003 · Beech A100SDR AUS20031202Spar · corroded(AUS) RT WING SPAR ANGLE CONTAINED INTERGRANNULAR CORROSION IN AREA WHERE IT PASSES THROUGH THE FUEL TANK CAVITY.Nov 24, 2003 · Cessna 152SDR CALA0300653Spar · corrodedINSPECTION FOUND RT WING FORWARD SPAR CORRODED AT STA XRS 258-335. REPAIRED IAW ECRA 5731-01040.Nov 20, 2003 · N18835 · Doug DC982SDR 2003FA0001175Spar · crackedCRACKED WING SPAR WEB AT ATTACHMENT FOR RECIPROCATING FUEL PUMP ASSOCIATED WITH FLINT WING TIP AUXILIARY FUEL SYSTEM. VIBRATION ASSOCIATED WITH FUEL PUMP OPERATION CAUSES THIN SPAR WEB (.025 INCH) TO FLEX AND CRACK AT OUTSIDE RADIUS OF ATTACHMENT HARDWARE.Nov 17, 2003 · N7568N · Cessna T210NSDR DHL2003802504Frame · crackedLEFT WING L/E FORMER CRACKED 0.500 AT STA 797.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10.Nov 10, 2003 · N802DH · Doug DC873SDR DHL2003802502Frame · crackedLT WING L/E FRAME CRACKED 0.500 STA XFS 772.500. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10.Nov 7, 2003 · N802DH · Doug DC873SDR TIM2003F00002Fitting · crackedFITTING FOUND TO BE CRACKED DURING STRUCTURAL INSPECTION. (CNTRL NR 82)Nov 5, 2003 · N950AA · Beech B99SDR DHL2003742514Frame · crackedDURING C-CHECK, RT WING L/E 130 INT FRAME IS CRACKED ON LOWER SKIN ATTACH ANGLE. STOP DRILL IAW B-727 SRM 51-10-1. REMOVED FASTENERS ON RT WING BL 92 INT FRAME VERT STIFFENER IAW B-727 SRM 51-30-2. FABRICATED DOUBLER FROM 7075 T6 .040 PO 900226 DIM 4.625 INov 4, 2003 · N742DH · Boeing 727225SDR AUS20031164Spar · corroded(AUS) LT AND RT MAIN WING SPARS CORRODED ON REAR FACE. SPAR PN TB20-11-003-100 AND PN TB20-11-003-101.Nov 3, 2003 · Socata TB20TRINIDADSDR 2003FA0001157Spar · crackedANNUAL INSPECTION. PERFORMED AD2001-25-02R1. NOTED CRACK ON LEFT/AFT WING SPAR. CRACK IS ON WOOD SPAR OUTBOARD OF LIFT STRUT ATTACH POINT. AIRCRAFT TT 6517.08. SPAR ORIGIN UNKNOWN. NOTED PREVIOUS SPAR REPAIR IN DIFFERENT LOCATION DATED 1979. RECOMMEND ANov 1, 2003 · N84670 · Bbavia 7ACSDR 2003FA0001127Spar Cap · corrodedWHEN PERFORMING INSPECTION REQUIRED BY PARAGRAPH (A)OF AD94-18-04 R1 FOUND SEVERE INTERGRANULAR CORROSION IN BOTH LT AND RT LOWER SPAR CAPS. CORROSION WAS LOCATED 6 INCHES FROM INBOARD END OF LOWER SPAR CAP TO 18 INCHES FROM INBOARD END. CORROSION HAS PENETRATNov 1, 2003 · N99734 · Univar 415CSDR L2498Spar Cap · corrodedDURING A ROUTINE INSPECTION SOME PAINT BLISTERING WAS NOTICED ALONG THE LT AFT SPAR UPPER CAP IN THE THE EXPOSED AREA OF THE LT WHEEL WELL. FURTHER INVESTIGATION REVEALED THAT THE SPAR CAP HAD SEVERE EXFOLIATION TYPE CORROSION AND WAS CAUSING THE SPAR CAP TO FOct 31, 2003 · N84LJ · Cessna 441SDR U2R2004F00000Spar Cap · crackedDURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.Oct 29, 2003 · N921R · Doug DC863FSDR U2RB102903Spar Cap · crackedDURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITIOOct 29, 2003 · N921R · Doug DC863FSDR AUS20031085Support · corroded(AUS) LT WING SPAR SUPPORT CORRODED.Oct 28, 2003 · Cessna 402CSDR AUS20031084Spar Cap · corroded(AUS) LT WING LOWER SPAR CAP CORRODED IN AREA IN FRONT OF AILERON.Oct 28, 2003 · Cessna 402CSDR AUS20031083Spar Cap · corroded(AUS) RT WING LOWER SPAR CAP CORRODED IN AREA IN FRONT OF AILERON.Oct 28, 2003 · Cessna 402CSDR GAIA03121STStiffener · crackedDURING C-CHECK INSPECTION FOUND RIGHT WING FRONT SPAR VERTICAL STIFFENER CRACKED AT WBL 90.5. REF FASI N/R NR 61293. INSTALLED DOUBLER REPAIR 7075-T6 .063 5.5 INCH BY 2.5 INCH IAW B727 SRM 57-10-2 AND 51-40-3 FIG 3. (M)Oct 24, 2003 · N1269Y · Boeing 727243SDR UPS03841611Fitting · crackedINSPECTION TYPE: C3, ATTACH FITTING AT XRS 624.000 REAR SPAR CRACKED. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001. CRACK NOTED. REMOVED AILERON SUPPORT FITTING CRACKED ATTACH FITTING AND MOUNTING STUD IAW DC8 SRM 51-1-20 AND 51-3-0. LOCATED AND DRILLED ATTACOct 22, 2003 · N852UP · Doug DC873FSDR EIA2003130Spar · corrodedRT WING UPPERCHORD OF FIX TRAILING EDGE PANEL SUPPORT BEAM SPAR APPROX WBL 235.2-445 CORRODED. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-57-184-2Oct 20, 2003 · N482EV · Boeing 747212BSDR CA031106005Spar Cap · cracked(CAN) DURING ACCOMPLISHMENT OF AD CF-92-26R1, THE ULTRASONIC INSPECTION WAS BEING COMPLETED IAW SB 215-A454. CRACKS WERE DETECTED ON THE LOWER RT AND LOWER LT SPAR CAPS. THE AIRCRAFT WILL BE REPAIRED IAW MFG REO PRIOR TO BEING TO RETURNED TO SERVICE.Oct 15, 2003 · Cndair CL2151A10SDR AUS20031067Spar Cap · corroded(AUS) RT WING MAIN SPAR LOWER SPAR CAP CORRODED. MICROBIOLOGICAL GROWTH FOUND ON INSIDE OF FUEL ACCESS PANELS 621BB AND 521BB AND 521CB.Oct 15, 2003 · Reims F406SDR AK62004F00002Spar Cap · corrodedDURING AN ATTEMPT TO REPAIR CORROSION AROUND THE LT WING FLAP BELLCRANK, LOCATED IN THE EXHAUST GAS TRAIL ON LOWER SIDE OF WING. DISCOVERED SEVERE INTERGRANULAR CORROSION ON LOWER SPAR CAP (JUST OB OF FACTORY SPLICE PLATE).Oct 14, 2003 · N777TS · Cessna 421BSDR FEF200300003Spar Cap · corrodedDURING THE C7 CHECK, PERFORMING THE TASK NR 0805, AND LOCAL CORROSION WAS FOUND AT RT LOWER SPAR CAP. XRS262~XRS267 L=5" W=1.2" D=0.8" ACTION TAKEN: REQUEST MFG ASSISTANCE FOR PERMANENT REPAIR AND IAW MFG RESPONSE REPAIR THE CORROSION. MANUFACTURER OFFEREOct 10, 2003 · Doug DC982SDR 2003FA0001075Spar Cap · corrodedRT WING REPLACED. EXISTING WING HAD EXFOLIATION CORROSION IN BOTTOM SPAR CAP AT INBOARD REAR OF FUEL TANK. THERE IS NO ACCEPTABLE REPAIR. CORROSION IS VISIBLE ONLY WHEN FUEL TANK IS REMOVED.Oct 9, 2003 · N4606R · Piper PA28140SDR 2003UALA00766Spar · crackedLT WING SPAR UPPER CHORD CRACKED AT MLG BEAM SUPPORT FITTING. MAJOR REPAIR ACCOMPLISHED. SPLICED NEW CHORD.Oct 9, 2003 · N371UA · Boeing 737322SDR 2004FA0000177Spar Cap · crackedDURING COMPLIANCE OF AD, INSPECTION, A CRACK WAS DISCOVERED IN THE LOWER WING SPAR CAP.Oct 8, 2003 · N502SE · Beech C90SDR 2003FA0001030Spar Cap · crackedDURING COMPLIANCE OF RAYTHEON AD 89-25-10, WING SPAR INSPECTION, A CRACK WAS DISCOVERED IN THE RIGHT WING LOWER WING SPAR CAP.Oct 8, 2003 · N502SE · Beech C90SDR DHL2003807504Frame · crackedRIGHT WING CENTER L/E LOWER PART FORMER CRACKED 0.500 AT XFS 316.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT Oct 7, 2003 · N807DH · Doug DC873FSDR DHL2003807505Frame · crackedRIGHT WING CTR L/E UPPER FORMER 0.250 CRACK AT STA XFS 297.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT WING COct 7, 2003 · N807DH · Doug DC873FSDR 03FDEA01781Spar · corrodedRIGHT WING - REAR SPAR UPPER SURFACE O/B OF O/B AILERON FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5710-74238 - WINGS, BASIC STRUCTURE - RIGHT REAR SPAR UPPER SURFACE CORROSION - XORS 1044.800.Oct 7, 2003 · N614FE · Doug MD11SDR ABXA030396Spar Cap · crackedCRACK ON UPPER SPAR CAP REAR SPAR XCW '0' TO XCW '10' RIGHT. REPAIRED AREA IAW DC-9 SRM.Oct 6, 2003 · N947AX · Doug DC931SDR AAL2004F00004Spar Cap · damagedRT WING REAR SPAR LOWER CAP DAMAGED (GROUND DAMAGE). INSTALLED SERVICEABLE LOWER CAP DOUBLER AND FILLER IAW ESO 80559.Oct 3, 2003 · N411AA · Doug DC982SDR GAIA03119STStiffener · crackedDURING C-CHECK INSPECTION, FOUND RIGHT WING FRONT SPAR VERTICAL STIFFENER CRACKED JUST OUTBOARD OF NR 6 SLAT INBOARD TRACK CAVITY. REF FASI N/R NR 61212, REPLACED STIFFENER BAC 1505-29D63 PO NR 314624 IAW B727 SRM 51-30-2. (M)Oct 3, 2003 · N1269Y · Boeing 727243SDR CA031022010Spar · cracked(CAN) CRACKED AT BOLT HOLES AT SPAR ATTACHMENT.Oct 3, 2003 · Piper PA23250SDR CA031010001Spar Cap · cracked(CAN) A CRACK WAS FOUND IN THE RT LOWER SPAR CAP HORIZONTAL FLANGE AT STATION 117.0 BL.THE CRACK EXTENDED FROM THE RIVET HOLE AFT TO THE EDGE OF THE FLANGE, AND FORWARD JUST SHY OF THE FLANGE RADIUS (OF THE VERTICAL LEG).THE CRACK WAS NOTICED ON A PREFLIGHT INOct 2, 2003 · Beech 1900DSDR BDJ2003F00001Spar · crackedOWNER REQUESTED AN INSPECTION IAW AD2000-25-02R1 WOOD SPAR INSPECTION. INSPECTION REVEALED THAT ALL INSPECTION HOLES HAD NOT BEEN ADDED IAW SL406 REV. A. UPPER FRONT SPAR HOLES WERE CUT AND CONVERED WITH DUCT TAPE, RT FRONT SPAR HAD OPEN CRACK AT BUTT EXTENDSep 29, 2003 · N2205E · Bbavia 7ACSDR BDJ2003F00000Spar · crackedOWNER REQUESTED AN INSPECTION IAW AD 2000-25-02R1, WOOD SPAR INSPECTION. INSPECTION REVEALED ADDITION INSPECTION. HOLES WERE NOT ADDED IAW LS406, REV A, RT REAR SPAR HAD AN OPEN CRACK AT THE BUTT INTO THE SPAR ATTACH PLATE BOLT HOLE, SPAR SEPARATING AT THE Sep 29, 2003 · N2205E · Bbavia 7ACSDR CA031015012Spar · cracked(CAN) RT WING AFT SPAR FOUND CRACKED AT AFT WING ATTACH POINT. 1 INCH CRACK LOCATED FROM INBOARD END OF AFT SPAR P/N 0426400-32 JUST BELOW SPAR REINFORCEMENT CRACK EXTENDS ALONG THE LENGTH OF THE SPAR 1 INCH. WING REMOVED FOR REPAIR.Sep 25, 2003 · Cessna 152SDR QXEA200301175Spar Cap · chafedRIGHT WING LOWER SPAR CAP IS CHAFED WHERE INBOARD END OF 611AR CONTACTS LOWER SPAR CAP. REPAIRED IAW DHC-8 SRM 51-00-06, 51-40-11, 51-20-16, 51-20-36 AND RD 8-57-811.Sep 21, 2003 · N348PH · Dhav DHC8202
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