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"

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 UPS01834794Rib · crackedINSPECTION TYPE:C1&3, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 828.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Jan 25, 2001 · N701UP · Doug DC871FSDR UPS01834780Rib · crackedINSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 616.25, XFS 622.250. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 24, 2001 · N701UP · Doug DC871FSDR SWAA010248Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 & S-3. REPAIRED RIB LOWER CHORD PER ER.Jan 24, 2001 · N688SW · Boeing 7373Q8SDR UPS01834781Rib · crackedINSPECTION TYPE:C1&3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XFS 297.5, XFS 354. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 23, 2001 · N701UP · Doug DC871FSDR UPS01834777Rib · crackedINSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIBS ARE CRACKED AT FASTENER END AT XS442.185, XS448.581, XS467.323, XS478.897. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jan 23, 2001 · N701UP · Doug DC871FSDR DHL2001806559Rib · crackedC-CHECK - LT WING LE RIB UPPER PART CRACKED 1/2 INCH AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.Jan 18, 2001 · N806DH · Doug DC873FSDR CA010205024Rib · cracked(CAN) DURING THE 50 HOURS INSPECTION, THE RIB MEMBRANE LOCATED OUTSIDE THE MAIN LANDING GEAR (LT SIDE) WAS FOUND CRACKED AND DEFORMED.Jan 15, 2001 · Piper PA34200SDR RRXA003570Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING T/E REAR SPAR RIB AT STA XW 5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. --------CX--------Jan 5, 2001 · N801GP · Doug DC871FSDR 20010302AP001Bulkhead · crackedFOUND RIGHT WING INBOARD FLAP BELLCRANK BULKHEAD STA.54.75 CRACKED. CRACK WAS LOCATED LEFT LOWER CORNER OF BULKHEAD (LOOKING FWD) AND APPROX. 1.5 INCHES LONG. AIRCRAFT HAS ROBERTSON STOL KIT INSTALLED. SUSPECT HIGHER CABLE TENSIONS BECAUSE OF STOL KIT CONTRIBJan 3, 2001 · Cessna T210MSDR MALA010117Rib · crackedFOUND DURING C-CHECK, THE 3RD, 4TH, 5TH, 6TH AND 7TH RIB FROM INBOARD, CRACKED ON LEADING EDGE 611BR, REFER TO CELSIUS W/O 19193, TASK 6514.Dec 30, 2000 · N456XJ · Saab 340BSDR COMA0010428Shear Tie · crackedUPON COMPLIANCE 2C INSPECTION TASK 5720-651-01I THE RIGHT WING SKIN SUPPORT ON RIB 20 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.Dec 12, 2000 · N268CA · Emb EMB120RTSDR QXEA0003348Rib · chafedPDX- TOP SIDE OF RIB 5 IS CHAFED BY WIRES AFT OF CONNECTOR FOR UPPER CONNECTOR. REPAIRED IAW FOKKER SRM 55-01-01 AND 51-10-4.Nov 25, 2000 · N492US · Fokker F28MK4000SDR CALA0001796Rib · gougedINSPECTION FOUND LEFT WING O/B EDGE OF RIB GOUGED AT NR 15 SLAT TRACK CUTOUT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-30-2, 51-30-6, 51-30-4, 51-10-3, AND 51-30-5.Nov 17, 2000 · N14816 · Doug DC982SDR AALA20001877Rib · crackedTUL - FOUND UPPER CHORD RIB CRACKED 1.5 INCH ABOVE OUTBOARD AILERON INBOARD HINGE CASTING, WBL 499. REPLACED UPPER T-CHORD PER BOEING SERVICE BULLETIN 727-57-16F. (M)Nov 7, 2000 · N848AA · Boeing 727223SDR RRXA003640Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB IN RADIUS ON THE LT WING T/E, FLAPWELL BELOW #3 FLT SPOILER O/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Nov 5, 2000 · N603AL · Doug DC873FSDR SWAA002229Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WBL 135.0, BETWEEN S2 & S3. REPAIRED RIB ER 00-1172.Nov 3, 2000 · N657SW · Boeing 7373L9SDR 20001207SH013Rib · damagedDURING A HIDDEN DAMAGE INSP, LT WING ASSY PN 0523005-83 FOUND LIGHT DAMAGE TO MID L/E SKIN AND 1 NOSE RIB, UNAPPROVED REPAIR FOUND TO AFT INBD SPAR ASSY. ALMOST ALL NOSE RIBS IN WING FOUND DAMGED, 10 IN ALL. A T/E RIB WAS CUT BY A FLAP CONTROL CABLE. 4 SKINNov 2, 2000 · N7122G · Cessna 172KSDR 20001109SH011Rib · crackedDURING A PHASE INSPECTION, FOUND A 1.1 INCH CRACK IN LEFT WING CANTED RIB. CRACK STARTING AFT OF THE FORWARD SPAR AND EXTENDED AFT ALONG THE RIB RADIUS. SUBMITTER STATED CESSNA NO LONGER WILL ALLOW STOP DRILLING OF THIS CRACK, SO THE RIB WAS REPLACED. (X)Oct 30, 2000 · N185GA · Cessna 441SDR DHL200080760CRib · crackedAT C-CK; LT WING CTR L/E RIB CRACKED AT STA XW 408 UPPER PART. REMOVED CRACKED RIB IAW SRM 51-1-20D, PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW RIB IAW SRM 51-1-20D, PG 9. REF: N/R 1974.Oct 25, 2000 · N807DH · Doug DC873SDR DHL200080754CRib · crackedAT C-CK; LT WING CTR L/E RIB CRACKED AT STA XW 408 UPPER PART. REMOVED CRACKED RIB IAW SRM 51-1-20D, PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2. INSTALLED NEW RIB IAW SRM 51-1-20D, PG 9. REF: N/R 1974.Oct 25, 2000 · N807DH · Doug DC873SDR 20001109SH024Rib · crackedDURING A PHASE INSPECTION, FOUND THE CRACK IN THE RIGHT CANTED RIB HAD PROGRESSED BEYOND THE PREVIOUSLY INSTALLED STOP DRILLS. AIRCRAFT WAS RETURNED TO THE OPERATOR WITH A ''FERRY PERMIT'' FOR REPAIR. (X)Oct 20, 2000 · N445AE · Cessna 441SDR 20001109SH012Rib · crackedDURING A PHASE INSPECTION, FOUND A .9 INCH CRACK IN RIGHT WING CANTED RIB TOP CAP. CRACK STARTS AFT OF FORWARD SPAR AND EXTENDS AFT. FOR MANY YEARS, CESSNA HAS ALLOWED THESE CRACKS TO BE STOP DRILLED, BUT NO LONGER WILL ACCEPT THIS REPAIR. NO PARTS ARE AVAIOct 20, 2000 · N185GA · Cessna 441SDR SWAA001986Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING INTERNAL RIB CRACKED AT WBL 135.5, BETWEEN STR S-2 & S-3. REPAIRED RIB PER ER 00-1051A.Oct 10, 2000 · N316SW · Boeing 7373H4SDR UPS00434235Rib · crackedINSPECTION TYPE:C, RT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1246.35. REPAIR CARRIED OUT IAW Q/NOTE 61/00.Oct 9, 2000 · N675UP · Boeing 747123SDR UPS00434237Rib · crackedINSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1318.65. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.Oct 9, 2000 · N675UP · Boeing 747123SDR UPS00434236Rib · crackedINSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1277.15. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.Oct 9, 2000 · N675UP · Boeing 747123SDR UPS00833849Rib · crackedINSPECTION TYPE:C1, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 310.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 2, 2000 · N779UP · Doug DC871FSDR QXEA0002775Rib · corrodedPDX- CORROSION AT END RIB 1825, 28 INCHES AFT OF FORWARD SPAR ACCESS THRU 72A. REPAIRED IAW FOKKER SRM 51-30-02 AND 28-11-0.Sep 22, 2000 · N499US · Fokker F28MK4000SDR DL72W001862Rib · crackedTHE BL 70.5 RIB CHORDS ON THE LT & RT WINGS WERE FOUND WITH TYPICAL FASTENER HOLE CRACKS IN THE VERTICAL FLANGE OF THE CHORDS AT FS 760.95. THE CRACKS ARE THE FWD FASTENER HOLE OF EACH CHORD AND ARE TYPICAL OF BAC S/B 727-57-0112. THE CRACKS WERE REMOVED BY Sep 22, 2000 · N296WA · Boeing 727247SDR MALA000625Rib · crackedFOUND DURING C-CHECK, 3 RIBS CRACKED ON LEADING EDGE PANEL 611BR. REFER TO CELSIUS TASK CARD 6506, W/O18843. MAINTENANCE REMOVED CRACKED SECTION OF 3 CRACKED RIBS IAW SRM 57-10-30. NDT PERF FVNDT006EC NO CRACKS NOTED. FABRICATED 3 REPAIR ANGLES AND SHIMS ISep 20, 2000 · N416XJ · Saab 340BSDR EIA2000283Rib · damagedEAC-MZJ - FOUND DURING C6 CHECK, PREVIOUSLY BLENDED AREA ON RIGHT WING LEADING EDGE RIB. REPAIRED PREVIOUSLY BLENDED AREA ON RT WING LEADING EDGE RIB AT XOS 238.581. BLENDED FURTHER TO 63 RMS FINISH PER ECRA 944-57-045-2. (M)Sep 18, 2000 · N944F · Doug DC933FSDR 20001103SH029Rib · damagedDURING C-CHECK, FOUND PREVIOUS BLENDED AREA, RIGHT WING, LEADING EDGE RIB. (X)Sep 18, 2000 · N944F · Doug DC933FSDR 20001120SH049Structure · corrodedLEFT LEADING EDGE WING RIB SUPPORT STA 822.5 HAD CORRODED BORES. REPAIRED PER ECRA 621-57-006. (X)Sep 15, 2000 · N621FF · Boeing 747259BSDR ABXA000487Rib · crackedCRACKS ON WING LEADING EDGE. REPAIRED IAW ABX REA 657-37420MR.Sep 13, 2000 · N788AX · Boeing 767281SDR RAAA00B2045Rib · crackedDURING INSPECTION OF AD88-17-06, LT WING FOUND CRACK IN WING RIB, LOWER NR 6 STRINGER ATTACH POINT, CRACK IN RADIUS OF RIB. REPAIRED IAW B727 SRM 57-10-05 M-54 NR 1.Sep 12, 2000 · N832RV · Boeing 72722CSDR DL72W001711Rib · crackedTHE UPPER RIB CHORD ON THE RT WING AT FS 760.95 AND RBL 70.85 WAS FOUND WITH A CRACK IN THE VERTICAL FLANGE OF THE CHORD. THE FLANGE WAS TRIMMED AWAY TO REMOVE THE CRACK AND REPAIRED WITH A REPAIR ANGLE MODIFICATION PER BAC S/B 727- 57-0112 AND ER/A 378263-1Sep 6, 2000 · N297WA · Boeing 727247SDR UPS00833720Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT FASTENER END AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833719Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT FASTENER END AT XFS 347.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833717Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 566.25, 610, 628.75 AT FASTENER END. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833715Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 803.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833713Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XS 478.897, XFS 372.75, XFS 379 AT FASTENER END. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Sep 1, 2000 · N729UP · Doug DC871FSDR UPS00833711Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT STA XFS 653.750. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Aug 31, 2000 · N729UP · Doug DC871FSDR RRXA003189Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RIGHT O/B LEADING EDGE AT STA XFS 841, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 28, 2000 · N957R · Doug DC863FSDR MALA000522Rib · crackedFOUND DURING C-CHECK, LT LEADING EDGE 511BL HAS 1 CRACKED RIB 5TH FROM OUTBOARD LOWER END. MAINTENANCE CUT OUT CRACKED RIB IAW SRM 57-10-30. FABRICATED REPAIR DOUBLER FROM 2024T3-050 AND FILLER FROM 2024T3.025 IAW SRM 57-10-30. ALODINED AND PRIMED IAW SRM 5Aug 11, 2000 · N446XJ · Saab 340BSDR DHL200080578CRib · crackedRIGHT WING L/E INTERIOR UPPER RIB CRACK AT STA XFS 693.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE.Aug 10, 2000 · N805DH · Doug DC873FSDR DHL200080576CRib · crackedRIGHT WING L/E INTERIOR UPPER RIB CRACK .5 INCH AT STA XFS 727.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.Aug 10, 2000 · N805DH · Doug DC873FSDR DHL200080575CRib · crackedRIGHT WING L/E INTERIOR UPPER RIB CRACKED .5 INCH AT STA XFS 717.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.Aug 10, 2000 · N805DH · Doug DC873FSDR DHL200080570CRib · crackedRIGHT WING L/E INTERIOR UPPER RIB CRACK .5 INCH AT STA XFS 752.000. STOP DRILLED PER SRM 57-2-5. FABRICATED REINFORCING ANGLE PER SRM 57-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.Aug 3, 2000 · N805DH · Doug DC873FSDR CALA0001197Rib · crackedINSPECTION FOUND A CRACK IN RT WING LEADING EDGE O/B RIB AT WS XRS 267-295. REPAIR ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-05 AND 57-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-05, EA 9-5720-2-A0742, AND ECRAug 2, 2000 · N33817 · Doug DC982SDR CALA0001195Rib · crackedINSPECTION FOUND RT WING LEADING EDGE I/B RIB AND DOUBLER CRACKED AT WS XRS 267-295. THE RIB WAS REMOVED AND TWO REPAIR DOUBLERS WERE INSTALLED IAW EA 9-5721-2-A0744 AND ECRA 5720-01810.Aug 2, 2000 · N33817 · Doug DC982
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