JASC 5714

Service difficulty reports · 1,451

Reports filed under 5714 · Wing, Center Box, 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 = '5714'
  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 UPS04843266Web · crackedINSPECTION TYPE: C3, CENTER WING FS 700 LEFT CRACK IN WEB EXTENDED PAST REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGED WEB. FABRICATED WEB & SPLICE DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0.Sep 5, 2004 · N772UP · Doug DC871FSDR COOSDR040018Plate · corrodedLT WING, FRONT SPAR LOWER CHORD PLATE FROM FSS 731 TO FSS 759, WITH CORROSION.Aug 17, 2004 · N994AJ · Boeing 727233SDR UPS04443118Shear Tie · crackedINSPECTION TYPE:C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 75. SHEAR TIE REPLACED IAW SRM 51-10-01 P8.Aug 17, 2004 · N520UP · Boeing 747200SDR UPS04443117Shear Tie · crackedINSPECTION TYPE: C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 35. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 P. 8.Aug 17, 2004 · N520UP · Boeing 747200SDR UPS04443116Shear Tie · crackedINSPECTION TYPE: C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT LBL 65. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8.Aug 17, 2004 · N520UP · Boeing 747200SDR UPS04443115Shear Tie · crackedINSPECTION TYPE:C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT RBL 80 IN. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 PG8.Aug 17, 2004 · N520UP · Boeing 747200SDR UPS04443114Shear Tie · crackedINSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 10 IN. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8.Aug 17, 2004 · N520UP · Boeing 747200SDR UPS04443113Shear Tie · crackedINSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 35 INCH CTR TANK FRONT SPAR UPPER CHORD, SHEAR TIE REPLACED AT LBL 35 INCH IAW SRM 51-10-01 PG 8.Aug 17, 2004 · N520UP · Boeing 747200SDR 04FDEA02347Fitting · crackedCRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING. REMOVED DAMAGED FITTING IAW DC10 SRM 51-33-01 VOL II. NEW FITTING FABBED ON FEDEX CARD N00880. LOCATED AND DRILLED FITTING IAW DC10 SRM 51Aug 2, 2004 · N68058 · Doug DC1010FSDR SWAA042167Fitting · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT AND RT CENTER SECTION FITTINGS ABOVE CENTER TANK RT AND LT BS 616, CRACKED. REPAIRED FITTINGS PER T1-153-018.Jul 29, 2004 · N326SW · Boeing 7373H4SDR LR7A04079Panel · crackedDURING SCHEDULED C-5 INSPECTION IAW HSP57141 FOUND RT CTR WING LOWER SURFACE NR 3 PANEL CRACKED APPROX. 3.0 IN. AT FS 597, CWS 62R AND NR 24 CW STRINGER CRACKED APPROX 14 IN. SAME LOCATION. REPAIRED IAW LAC MEA 382-57-04-051 AND LOCKHEED SES GLD-1720 TN 0034,Jul 16, 2004 · N403LC · Lkheed 382GSDR LR7A04078Panel · crackedDURING SCHEDULED C-5 INSPECTION, IAW SB382-57-55R1 PARA 1.B.3. HFEC FOUND FS 564 RT CENTER WING NR 2 PANEL LOWER SURFACE CRACKED APPROX .280 IN. AT CWS 63R. REPAIRED IAW LAC MEA 382-57-04-050 AND LOCKHEED SES GLD-1720 TN 0033, DWG SK382-57-278. DRC 2189.Jul 16, 2004 · N403LC · Lkheed 382GSDR 04FDEA02043Support Fitting · corrodedCENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT FS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.Jul 10, 2004 · N245FE · Boeing 727200SDR 04FDEA02042Support Fitting · corrodedCENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT BS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1.Jul 10, 2004 · N245FE · Boeing 727200SDR ASOA04475Rib · crackedDURING A C-CHECK IN MCN, THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 IAW ASA EO 600-57-039A. (M)Jun 30, 2004 · N844AS · Cndair CL6002B19SDR C1HA200478003Skin · corrodedCENTER WING LOWER SKIN IS CORRODED ON RT SIDE AT STA 535. REPAIRED IAW EO-727-57-10-01.Jun 22, 2004 · N678MG · Boeing 727225SDR C7WA200400028Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232SDR LR7A04059Web · crackedDURING SCHEDULED B3 INSPECTION NR 02/REP/51/2 REPAIR ACCOMPLISHMENT FOUND CENTER WING FWD BEAM WEB CRACKED .75 IN AT 2 EA. FASTENER HOLES AT CWS 72R, FS 517, WL 258 AND 282. REPAIRED IAW LAC MEA 382-57-04-041 AND SRM SMP 583 57-30-22. NR 0124.May 26, 2004 · N401LC · Lkheed 382GSDR AUS20040355Stringer · corroded(AUS) WING CENTER SECTION EXTERNAL LOWER SURFACE Z SECTION STRINGERS CONTAINED LEVEL 3 CORROSION.May 6, 2004 · Fokker F28MK0100SDR ASAA0440112Support · corrodedGYR - FOUND LEFT AC BAY HEAT EXCHANGER DUCT MOUNTING FLANGE CORRODED AT APPROX BS 580 LBL 36. REPAIRED LEFT CENTER WING SUPPORT WEB AT STATION 587 PER EA NR 5710-01104. (M)May 4, 2004 · N776AS · Boeing 7374Q8SDR 04FDEA00884Skin · corrodedEXFOLIATING CORROSION ON TOP OF CENTER WING AT STA 1331, LBL 97.0 ON AN AREA OF APPROXIMATELY 6 X 8 INCH. REMOVED ALL EVIDENCE OF CORROSION. INSTALLED FILLERS AND DOUBLERS AS PER EA 8-5730-74212-WING UPPER AFT SKIN PANEL, CENTER BOX-CORROSION.Apr 8, 2004 · N310FE · Doug DC1030SDR CA040408005Pump · failed(CAN) INCONSISTENCIES IN FUEL PRESSURE, FUEL PRESSURE WAS CHECKED AND FOUND THAT THE LOW SIDE OF THE ELECTRIC FUEL PUMP WAS NEAR NIL. HIGH SIDE WAS 5.5. THE FUEL PUMP FAILURE IS BELIEVED TO BE CAUSED BY THE AIRCRAFT BEING OUT OF SERVICE FOR LONG PERIOD OF TIMEApr 2, 2004 · Diamon DA20C1SDR UIEA200400010Skin · corrodedDURING D-CHECK AT SIN, CENTER WING TANK, LOWER SKIN ABOVE NR 1 ACM FOUND CORRODED. LEVEL 1. CORROSION WAS BLENDED OUT WITH A MACHINED FINISH. THE BLENDED AREA WAS HFEC INSPECTED AND FLAP/SHOP PEENED. ALODINE PRIMER AND BMS 3-23 CORROSION INHIBITING COMPOUNFeb 5, 2004 · N517MC · Boeing 747243BSDR 04FDEA00173Structure · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235 RT X =30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RT X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKJan 16, 2004 · N604FE · Doug MD11SDR DHL2003807528Fitting · crackedMAIN CARGO COMPT CENTER WING FITTING CRACKED 1.500 AT STA 760.000 LBL-24. REMOVED AND REPLACED CRACKED FITTING ON MAIN CARGO COMPT CENTER WING, STA 760.000, LBL-24 IAW SRM 51-3-0 PG 1.Oct 22, 2003 · N807DH · Doug DC873FSDR UPS03841524Splice · corrodedINSPECTION TYPE: C2, CENTER WING TANK UPPER REAR SPAR CAP SPLICE/ANGLE REPAIR FILLER SPACER IS CORRODED BEYOND LIMITS AT RBL 43 AT STA 857. REMOVED, FABRICATED AND REPLACED SPLICE IAW SRM 53-2-5 FIG 12.Oct 22, 2003 · N867UP · Doug DC873FSDR ABXA030378Support Fitting · corrodedCORROSION ON UPPER CHORD OF CENTER WING REAR SPAR AT PRESSURE BULKHEAD F.S. 855, LEFT BUTT LINE 11 - 21. REMOVED AND INSTALLED BLOWOUT PANEL 3 EA. VERTICAL STIFFENERS, WEB ATTACH ANGLE, DOUBLER, FITTING AND SHEAR WEB ATTACH ANGLE IAW DC-8 SRM 51-30-0 AND 51-1-Oct 1, 2003 · N853AX · Doug DC861SDR GTIA030822Angle · crackedFOUND WEB ANGLE ATTACHMENT STATION 864 OVER CENTER WING TANK CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M)Sep 30, 2003 · N820NK · Doug DC982SDR SWAA031918Beam · crackedDURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL BEAM CRACKED, BS 663, BL 0. REPAIRED BEAM PER SWA EA.Aug 27, 2003 · N672SW · Boeing 7373Q8SDR LR7A03071Web · crackedDURING SCHEDULED C5 INSPECTION NR 2109 ACCOMPLISHMENT FOUND RT CENTER WING AFT BEAM WEB CRACKED APPROX 2.0 INCHES AT CWS 22, WL 280. REPAIRED IAW SRM SMP 583 57-30-25 AND LAC MEA 382-57-03-054. NR 2143.Jul 25, 2003 · N401LC · Lkheed 382GSDR EIA2003099Skin · corrodedUPON REMOVAL OF FASTENERS FOR ADJACENT S/M REPAIR, CENTER TANK UPPER AFT SKIN PANEL WAS FOUND CORRODED AT STA 1237, RBL 37 UNDERNEATH LONGITUDINAL FLOORBEAM LOWER CHORD. DAMAGED AREA REPAIRED PER ECRA 485-57-154-2.Jul 25, 2003 · N485EV · Boeing 747212BSDR DL76L030597Rib · gougedLOWER STRUCTURAL DAMAGE REPAIR THE LOWER STRUCTURE OF THE LBL 62.05 LOWER BEAM OF THE CENTER WING WAS BADLY GOUGE TO A BLOWN DUCT FROM FS 915-919. THE DAMAGED SECTION OF CHORD WAS CUT AND REMOVED. A NEW SECTION OF STRUCTURE WAS SPLICED IN WITH STEEL REPAIR AJun 28, 2003 · N196DN · Boeing 767332SDR DHL2003604584Access Door · corrodedLT C/W AUX TANK - PERFORM ANTI-CORROSION TREATMENT TO LT 5056 ACCESS DOOR. REMOVED CORROSION ON LT 5056 ACCESS DOOR IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075Jun 10, 2003 · N604AL · Doug DC873FSDR QXEA200300720Flange · chafedPDX - TRAILING WING BOX UPPER FLANGE HAS CHAFES FROM YW43L TO YW43R. REPAIRED IAW RD 8/4-53-451.Jun 4, 2003 · N408QX · Bombdr DHC8401SDR 03FDEA00819Skin · corrodedMAIN CARGO-CORROSION FOUND AT STA 1371 LBL 85 AT REAR SPAR TOP OF FUEL TANK. WILL NEED TO HAVE FASTENERS REMOVED. ** S/D ** CLOSING ACTION: ACCOMPLISHED REPAIR - CENTER WING - UPPER SKIN CORROSION - PER EA 8-5710-69306.May 27, 2003 · N68059 · Doug DC1010SDR UPS03840758Fitting · crackedINSPECTION TYPE: C1, LT STA 980 FITTING IS CRACKED NEXT TO FUSELAGE ON WING BOX. REMOVED AND REPLACED FITTING IAW DWG 4647365 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871FSDR 2003FA0000529Skin · crackedDURING ANNUAL (SPECIAL) INSPECTION CRACKS IN THE WING CENTER BOX PLANK NR 1 AND NR 3 WERE FOUND EMITTING FROM THE INTERNAL WEEP HOLES LOCATED NTHE INTERNAL PLANK RISERS. CRACK IN NR 1 PLANK, RT SIDE WAS ABOUT 3 INCHES LONG AND A 1 INCH CRACK IN SAME PLANK ON Apr 14, 2003 · N925AU · Lkheed P3ASDR P5CA0300818Skin · corrodedLEVEL 1 CORROSION - WING CENTER SECTION UPPER SKIN REAR SPAR LBL 98.58. REPAIRED PER SRM 51-10-01.Apr 10, 2003 · N920FT · Boeing 747249FSDR LR7A03027Stiffener · crackedDURING SCHEDULED C4 INSPECTION PER JOB CARD HST5710 FOUND LT FRONT BEAM WEB T-SPLICE STIFFENER CRACKED 1.0 INCH AT CWS 175, FS 517, WL 270. T-SPLICE STIFFENER REPLACED IAW SRM SMP 583 57-40-04. NR 2179.Mar 13, 2003 · N403LC · Lkheed 382GSDR AUS20030237Stiffener · corroded(AUS) LT WING CENTER SECTION SUPPORT BEAM STIFFENER CONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW J3-CA53-0129.Feb 28, 2003 · Boeing 737377SDR AUS20030238Web · corroded(AUS) LT WING CENTRE SECTION SUPPORT BEAM WEB CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN THE HEAT EXCHANGER CUTOUTS. AREA OF CORROSION 6.3MM (0.250IN) IN DIAMETER BY 0.508MM (0.020IN) DEEP.FOUND DURING INSPECTION IAW J3-CA53-0129.Feb 27, 2003 · Boeing 737377SDR DHL2003804906Panel · delaminatedLT WING - NR 728 CTR WING LOWER PANEL INNER SKIN DELAMINATED, STA 779.000 - STA 810.000. REMOVED AND REPLACED CTR WING LWR PANEL NR 728 IAW SRM 51-3-0 PG 1.Feb 15, 2003 · N804DH · Doug DC873FSDR BLAI200200001Rib · corrodedDURING REFURBISHMENT OF THE WING CENTER SECTION WING WALKWAY BOXES, AN INSPECTION WAS CONDUCTED TO COMPLY WITH AD 2002-26-02. LOWER SKINS OF THE WALKWAY BOXES HAD BEEN REMOVED TO PROVIDE ACCESS FOR REFURBISHMENT, THIS PROVIDED UNIMPEDED ACCESS TO THE ENTIRE CEJan 3, 2003 · N99997 · Univar 415DSDR EIAA2002127Structure · corrodedMZJ - FOUND MAIN DECK WING CENTER SECTION BODY STATION 1080 BBL 94L CORROSION. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 480-57-121-2. (M)Nov 8, 2002 · N480EV · Boeing 747121SDR SWAA022425Beam · crackedDURING SCHEDULED 1/4D CHECK, FOUND TRANSVERSE BEAM CRACKED (2 EA) AT BS 706, BL O AND LBL 25. REPAIRED TRANSVERSE BEAM PER SWA EA.Oct 15, 2002 · Boeing 7372H4SDR UPS02239756Stiffener · corrodedBULGING EVIDENT ON WING CENTER SECTION REAR SPAR WEB AT BS 870, 3RD VERTICAL STIFFENER FROM LEFT SIDE. CORROSION FOUND ON VERTICAL STIFFENER AT LBL 24.70. STIFFENER REPLACED IAW SRM 51-30-2 AND DRAWING 65-16202.Sep 19, 2002 · N930UP · Boeing 72722CSDR DL76S020889Stiffener · crackedCRACKS WERE FOUND IN THE LBL 10 VERTICAL STIFFENER OF THE CENTER SECTION FRONT SPAR, IN THE WEB OF THE STIFFENER AT THE OVERWING FLOORBEAM TO STIFFENER JOINT. A SPLICE REPAIR WAS ACCOMPLISHED.Jul 27, 2002 · N116DL · Boeing 767332SDR 2002F00735Fitting · crackedAT C-CHECK, FOUND UPPER T-FITTING CRACKED, ON CENTER WING FUEL TANK FRONT SPAR, STATION 760, LBL 25. (M)May 31, 2002 · N7635U · Boeing 727222SDR 2002F00734Fitting · crackedAT C-CHECK, FOUND CENTER WING FUEL TANK FRONT SPAR UPPER FITTING CRACKED, AT STATION 740, LBL 45. (M)May 31, 2002 · N7635U · Boeing 727222SDR UPS02438268Fitting · crackedINSPECTION TYPE:C CRACK REVEAL ON THE FASTENER HOLE OF THE FITTING INSIDE WING CENTER TANK COMMON TO LT SIDE BATHTUB FITTING RUNNING UPWARD APPROX .125" LONG. LT SIDE STA 983 S38L INSIDE DRY BAY BATHTUB DRAG FITTING REPLACED AS PER SRM 51-30-02.Apr 23, 2002 · N676UP · Boeing 747123
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