JASC 5712

Service difficulty reports · 6,970

Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712'
  ORDER BY difficulty_date DESC"

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SDR 58392816RRib · crackedINSPECTION OF AIRCRAFT IN MAINT HANGAR REVEALED TWO INCH CRACK ON LT WING AT APPROX WS 49.25, AROUND SINGLE RIVET, SKIN HAD BULGED AROUND RIVET AND CRACKED FORE AND AFT. INSPECTION IN WHEEL WELL SHOWED THAT RIVETS ATTACHING FLANGE TO FALSE REAR SPAR AND RIB TOMar 19, 2001 · N2816R · Piper PA28R200SDR DHL2001806570Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 860. PERFORMED STOP DRILL AND FABRICATED DOUBLERS IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873FSDR DHL2001806569Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8, PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 13, 2001 · N806DH · Doug DC873FSDR DHL2001806566Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1/2 INCH CRACK AT STA XFS 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 PAGE 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 9/10. STATUS-CLOSEDMar 13, 2001 · N806DH · Doug DC873FSDR DHL2001806563Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1 INCH CRACK AT STA XFS 766.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 PAGES 9. 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10. STATUS-CLOSMar 13, 2001 · N806DH · Doug DC873FSDR DHL2001806555Rib · crackedC-CHECK - WING LE RIB UPPER PART 1 INCH CRACK AT STA 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 P1, 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLERS IAW SRM 57-2-0 PAGE 10. STATUS-CLOSEDMar 13, 2001 · N806DH · Doug DC873FSDR AWXA0001494Rib · crackedLT WING L/E RIB CRACKED IN RADIUS, I/B OF NR 1 PYLON WBL 183.4. STOP DRILLED CRACK; FORMED, DRILLED AND INSTALLED REPAIR ANGLES IAW SRM 51-40-3 FIG 1.Mar 13, 2001 · N179AW · Boeing 737277SDR EIA2001192Rib · crackedHKG-HAECO - FOUND LT WING SURGE TANK WS 1516 UPPER RIB STRINGER 6 AFT BOLT HOLE CRACKED. REPAIRED UPPER RIB CHORD PER SRM 57-10-05 FIG 4. (M)Mar 12, 2001 · N471EV · Boeing 747273CSDR DHL2001806573Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 660. PERFORMED STOP DRILL AND FAVRICATE REINFORCING ANGLE IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873FSDR DHL2001806568Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873FSDR DHL2001806558Rib · crackedC-CHECK - LT WING LE RIB 1 INCH CRACK AT UPPER PART STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 12, 2001 · N806DH · Doug DC873FSDR DHL2001806637Rib · crackedC-CHECK, LT WING L/E RIB LWR PORT .5 INCH CRACK AT STA XFS 642 - 250.Mar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806609Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 747.000. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INBSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATMar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806580Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 041.950.PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806579Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 841.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806578Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 822.950. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806576Rib · crackedC-CHECK, LT WING L/E RIB LOWER PART HAS A 1/2 INCH CRACK AT STA XFS 803.750.PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CMar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806567Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Mar 11, 2001 · N806DH · Doug DC873FSDR DHL2001806556Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG2. STATUS-CLOSEDMar 11, 2001 · N806DH · Doug DC873FSDR IXXA0100047SRib · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE LOWER RIB OUTBOARD ACCESS PANEL 518. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUALMar 8, 2001 · N820BX · Doug DC871FSDR IXXA0100044SRib · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE RIB BETWEEN ACCESS PANELS 519A AND 519B. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERINGMar 8, 2001 · N820BX · Doug DC871FSDR IXXA0100043SRib · gougedDURING ROUTINE C CHECK INSPECTION, A GOUGE WAS DETECTED ON THE LEFT WING LEADING EDGE RIB AT STATION XFS 445. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-17Mar 8, 2001 · N820BX · Doug DC871FSDR SWAA010659Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT AND RT WING RIB LOWER CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 AND 3. REPAIRED LOWER CHORDS PER BFG ER''S.Mar 5, 2001 · N672SW · Boeing 7373Q8SDR AU010166Rib · cracked(AUS) LT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 76.2MM (3IN).Feb 26, 2001 · Swrngn SA227ACSDR AU010165Rib · cracked(AUS) RT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 203.2MM (8IN).Feb 26, 2001 · Swrngn SA227ACSDR UPS01835150Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 747.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835149Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 785. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835148Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 816.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835147Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 778.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835146Rib · crackedINSPECTION TYPE:C2,3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XS 491.193, XS 503.789. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835145Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIBS ARE CRACKED AT XFS 647.5, 672.5, 685, AND 697.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835144Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835143Rib · crackedINSPECTION TYPE:C2,3 RIGHT WING L/E RIB IS CRACKED AT XFS 597.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835109Rib · crackedINSPECTION TYPE:C2/3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 310.25 AND XFS 335.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR UPS01835108Rib · crackedINSPECTION TYPE:C2/3, LEFT WING CENTER L/E LOWER RIB IS CRACKED AT XW 461.372. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Feb 23, 2001 · N811UP · Doug DC873FSDR SWAA010514Rib · crackedDURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH CRACK IN LT WING LOWER RIB CHORD, WBL 135.5, AFT END, STRINGER 3. REPAIRED LOWER CHORD PER SWA RA.Feb 20, 2001 · N664WN · Boeing 7373Y0SDR 2001F00630Rib · crackedTUL - FOUND BS 760.95 RIGHT RIB CHORD HFEC INDICATED CRACK ON VERTICAL LEG STOPPING AT TOP OF RADIUS. ACCOMPLISHED RIB CHORD REPAIR PER ESO 11697 (DATED 2-14-01), SB 727-57-0112 PART IV, LARGE REPAIR, DWG 65C33202. (M)Feb 15, 2001 · N879AA · Boeing 727223SDR 0103389992Rib · crackedDuring H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959.Feb 13, 2001 · N8960E · Doug DC931SDR 0103399992Rib · crackedDuring H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959.Feb 13, 2001 · N8960E · Doug DC931SDR UPS01835165Rib · crackedINSPECTION TYPE:C1/3, RIGHT O/B FIXED L/E HAS CRACK ON L/E OF MATING SURFACE AT FASTENER ATTACH HOLES. FABBED NEW -8 ANGLE AND -11 DOUBLER IAW DAC DWG 9753297, LOCATED AND DRILLED NEW -4 RIB IAW DC-8 SRM 51-1-24. INSTALLED -8 ANGLE, -11 DOUBLER & -4 RIB IAW Feb 6, 2001 · N810UP · Doug DC873FSDR MWEA010130Rib · corrodedRIGHT WING RIB STATION 69 WEB AND LOWER T-EXTRUSION HAS AREAS OF MODERATE CORROSION FROM AFT SPAR TO STRINGER 17. REMOVED AND REPLACED T-CORD.Jan 29, 2001 · N207ME · Doug DC932SDR UPS01834811Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 360. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 28, 2001 · N701UP · Doug DC871FSDR UPS01834793Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 27, 2001 · N701UP · Doug DC871FSDR UPS01834792Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 741.250. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 27, 2001 · N701UP · Doug DC871FSDR UPS01834791Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 27, 2001 · N701UP · Doug DC871FSDR UPS01834838Rib · crackedINSPECTION TYPE:C1&3, LEFT NR 2 STUBWING HAS UPPER RIB CRACKED AT XILD .7095. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871FSDR UPS01834833Rib · crackedINSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871FSDR UPS01834797Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XOLDI 6.225, XS 435.78, XS 442.185, XS 448.581, XS 466.651. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871FSDR UPS01834796Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 835, XFS 828.75, XFS 822.5, XFS 816.25, XFS 803.75, XFS 797.5, XFS 785, XFS 766.25. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871FSDR UPS01834795Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25, XFS 641.25, XFS 653.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871F
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