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 SWIA200413939Rib · crackedRIB ATTACH ANGLE CRACKED ON RIGHT WING, RIB 21, TOP SURFACE OF RIB, BETWEEN STRINGERS 3 AND 4. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PART IAW EMB 120 SRM 51-25-00, 51-40-00, 51-30-01, 51-40-01, 51-40-02, 51-40-05 AND REF 57-20-07 FIG 6 ITEM 90.Aug 23, 2004 · N196SW · Emb EMB120ERSDR SWIA200413938Rib · crackedLEFT WING FORWARD RIB 17 CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1 AND 51-12-02.Aug 23, 2004 · N196SW · Emb EMB120ERSDR SWIA200413937Rib · crackedLEFT WING FORWARD RIB 21 IS CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-12-02 & 57-20-07 FIG 203.Aug 23, 2004 · N196SW · Emb EMB120ERSDR ASOA04602Rib · crackedDURING A C-CHECK IN MCN, THE RT MLG WW BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046. (M)Aug 15, 2004 · N878AS · Cndair CL6002B19SDR ASOA04532Rib · crackedDURING A C-CHECK IN YUL, LEADING EDGE RIBS 6 AND 7 AT THE RIGHT INBOARD FLAP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED LEADING EDGE RIBS 6 AND 7 AT THE RIHT INBOARD FLAP IAW SRM 51-25-03 AND 51-25-01. (M)Jul 27, 2004 · N533AS · Aerosp ATR72212SDR 04FDEA02151Rib · crackedLEFT WING I/B LEADING EDGE ACCESS PANEL 516FE RIB WITH CRACK. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01.Jul 22, 2004 · N326FE · Doug DC1030SDR 04FDEA02150Rib · crackedRIGHT WING I/B LEADING EDGE ACCESS PANEL 616ET SEVERAL RIBS CRACKED. REMOVED CRACKED RIBS AND REPLACED WITH NEW RIBS IAW SRM 51-31-01. PAINTED IAW SRM 51-23-01.Jul 22, 2004 · N326FE · Doug DC1030SDR 04FDEA02098Rib · damagedC/W EA 8-5750-80579 WINGS RT INBOARD FLAP VANE TRACK OVERSIZE HOLE REPAIR AT XIFH 216.3 (P/N ARC2966). COMPLIED WITH EA 8-5750-80579.Jul 17, 2004 · N359FE · Doug MD11SDR SWIA200413896Rib · crackedLEFT WING AT RIB 8 WING TO WEB CLIP IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED SUPPORT BRACKET IAW SRM 51-25-00, 51-40-00.Jul 16, 2004 · N186SW · Emb EMB120ERSDR IXXA060447SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING AUXILIARY TANK RIB CRACKED AT STATION XFS20. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862FSDR UPS04842864Rib · crackedINSPECTION TYPE: C1, RIGHT WING LEADING EDGE LOWER RIB IS CRACKED AT FASTENER HOLE AT XFS 601. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Jul 13, 2004 · N802UP · Doug DC873FSDR IXXA060409SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS384. REPAIRED PER ALL APPLICABLE DATA.Jul 3, 2004 · N41CX · Doug DC862FSDR UPS04842699Rib · crackedINSPECTION TYPE: C-3, RT CENTER L/E HAS CRACKED RIB AT APPROX STA 304.600. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-211. MAT ID FOR REPAIR ANGLE BAC 1503-100147 EXTRUSION 7075-T6 PO 437138. STOP DRILLED CRACKED. LOCATED, DRILLED & DEBURRED REPAIR ANGLE. Jul 2, 2004 · N803UP · Doug DC873FSDR UPS04842698Rib · crackedINSPECTION TYPE: C-3, RT CENTER 4E HAS CRACKED RIB AT APPROX STA 448.00. REMOVED FASTENERS IN REPAIR AREA RT CENTER L/E AT STA 448.00 & STOP DRILL CRACK. MAT ID FOR REPAIR ANGLE 9751065-33 EXTRUSION 7075-T6 PO 387706. PERFORMED HFEC IAW MD NDT SPM 06-10-01.Jul 2, 2004 · N803UP · Doug DC873FSDR 04FDEA01911Rib · gougedCOMPLY WITH EA 8-5750-79543 WINGS RT FIXED LEADING EDGE SLAT RIB TRACK RIB GOUGE REPAIR XOS 427.4. COMPLIED WITH EA 8-5740-79543.Jul 2, 2004 · N398FE · Doug MD1010FSDR UPS04842697Rib · crackedINSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IAW DAC NTSPM 06 10-01Jul 1, 2004 · N803UP · Doug DC873FSDR UPS04842696Rib · crackedINSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM NDT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REPAIR ANGLE 7075-T6 .0Jul 1, 2004 · N803UP · Doug DC873FSDR 04FDEA01897Rib · crackedRIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING CRACKED. RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.Jun 30, 2004 · N606FE · Doug MD11SDR 04FDEA01870Rib · gougedACCOMPLISH EA 8-5710-78226, WINGS REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1086-1. COMPLIED WITH EA 8-5710-78226.Jun 28, 2004 · N387FE · Doug DC1010SDR DHL2004804505Rib · crackedRT WING CTR. LE UPPER FORMER CRACKED 0.500, XFS 347.750. CORR.: REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Jun 27, 2004 · N804DH · Doug DC873FSDR DHL2004804504Rib · crackedITEM REF. NR. 1514: RT WING CTR. LE UPPER FORMER CRACKED 0.500 AT XFS 354.000. REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED TREATED AND PRIMED ANGLE DOJun 27, 2004 · N804DH · Doug DC873FSDR 04FDEA01843Rib · gougedLT FIXED LEADING EDGE SLAT TRACK RIB GAUGE REPAIR XOS 427.4. COMPLIED WITH FED EX EA 8-5740-79537, LT FIXED LEADING EDGE SLAT TRACK RIB GOUGE REPAIR XOS 477.41.Jun 22, 2004 · N387FE · Doug DC1010SDR 04FDEA01835Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORRODED. RIGHT HAND WING, OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIGINAL HOLE SIZE DIA 0.3125 INCH FINAL HOLE SIZE DIA 0.375 INCH REJun 21, 2004 · N587FE · Doug MD11FSDR UPS04842662Rib · gougedINSPECTION TYPE: C-3, RT WING OUT BOUND L/E INBOARD END RIB HAS DEEP GOUGE. BLENDED GOUGE AREA, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB DOUBLER REPAIR IAW DC8 SRM 57-2-0 AND 51-1-4. LOCATED & DRILLED DOUBLER IAW DC8 SRM 51-1-24 & 51-2-0. ALODINJun 17, 2004 · N803UP · Doug DC873FSDR UPS04842660Rib · chafedINSPECTION TYPE: C-3, RIGHT WING LEADING EDGE INTERIOR RIB CHAFED ABOVE PNEUMATIC SHUT OFF VALVE. INSTALLED REPAIR DOUBLER IAW 57-2-0.Jun 15, 2004 · N803UP · Doug DC873FSDR IXXA060433SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE RIB CRACKED AT STATION XW36. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862SDR IXXA060162SRib · gougedDURING ROUTINE C-CHECK, FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SJun 11, 2004 · N605AL · Doug DC873FSDR IXXA060397SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS842. REPAIRED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR IXXA060396SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS780. REPLACED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR 05FDEA00014Rib · crackedWING - LT WING RIB XORS 372 UPPER CAP CRACKED. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-78165.Jun 10, 2004 · N565FE · Doug MD1010FSDR IXXA060427SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE CAVITY LOWER RIB CORRODED AND CRACKED AT STATION XFS360.25. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862FSDR IXXA060425SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS773. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862FSDR 04FDEA01539Rib · wornCOMPLY WITH EA 8-5710-77424 WINGS - REWORK OF RIGHT NR 7 SLAT TRACK OUTBOARD RIB ARB1868. COMPLIED WITH EA 8-5710-77434.May 29, 2004 · N68051 · Doug DC1010SDR 04FDEA01387Rib · damagedCOMPLY WITH EA 7-5720-77412 WING - SPOILER DOWN STOP RIB REPAIR. COMPLIED WITH EA 7-5720-77412. WORKED IN CONJUNCTION WITH EA 7-5720-77423.May 21, 2004 · N241FE · Boeing 727200SDR 04FDEA01384Rib · crackedMAJOR REPAIR DURING C-CHECK, PASSENGER TO FREIGHTER CONFIG, FOUND RIB XCW/81 BETWEEN LONGERON 21 AND 22, UPPER CORD RADIUS HAS .5 INCH CRACK CENTER WING RIB. REPAIRED AREA WITH A FAB ANGLE, PER EA 8-5710-70141.May 21, 2004 · N559FE · Doug DC1010SDR 04FDEA01383Panel · crackedMAJOR REPAIR DURING C-CHECK, AND PASSENGER TO FREIGHTER CONFIG BY ULTRASONIC INSPECTION, FOUND 1 PANEL CRACKED ON THE HORIZONTAL STABILIZER. P/N REMOVED ALC7204-1. REMOVE AND REPLACE PANEL WITH P/N ALC7204-501N PER EA 8-5510-70126.May 21, 2004 · N559FE · Doug DC1010SDR ASOA04348Rib · crackedDURING C-CHECK INSPECTION, THE RT MLG BATT RIB WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED MLG BATT RIB IAW EO 600570039A AND 600570042.May 14, 2004 · N838AS · Cndair CL6002B19SDR WVE2004F00015Rib · crackedRT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)May 10, 2004 · N597SW · Cndair CL6002B19SDR WVE2004F00014Rib · crackedLEFT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE; STRESS. RECOMMENDATION: REPAIR IAW MFG REPAIR EO. (EA09200402314)May 10, 2004 · N597SW · Cndair CL6002B19SDR 04FDEA01168Rib · crackedLT WING SLAT TRACK 16 I/B RIB FOUND CRACKED. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II & INSTALLED NEW RIB AT LT WING SLAT TRACK NR 16 AS PER SRM 51-33-01 VOL II.May 7, 2004 · N597FE · Doug MD11SDR SWIA200413495Rib · wornRIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1.May 6, 2004 · N187SW · Emb EMB120ERSDR SWIA200413493Rib · crackedRIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLACED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2.May 6, 2004 · N187SW · Emb EMB120ERSDR SWIA200413492Rib · crackedRIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 REPLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00.May 6, 2004 · N187SW · Emb EMB120ERSDR ASOA04342Rib · crackedDURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MLG BATT RIB ASSEMBLIES AT WS 53.60 IAW EO60057039A.May 6, 2004 · N856AS · Cndair CL6002B19SDR ASO2004F00016Rib · crackedDURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO.May 6, 2004 · N856AS · Cndair CL6002B19SDR ASOA4342Rib · crackedDURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO.May 6, 2004 · N856AS · Cndair CL6002B19SDR UPS04842422Rib · crackedINSPECTION TYPE: C1 LT WING LE UPPER RIB IS CRACKED AT XFS 641. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2May 4, 2004 · N730UP · Doug DC871FSDR UPS04842370Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 603. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.May 4, 2004 · N730UP · Doug DC871FSDR UPS04842369Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 358. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.May 4, 2004 · N730UP · Doug DC871FSDR UPS04842367Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.May 4, 2004 · N730UP · Doug DC871F
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