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 99T64R450EWARib · crackedFOUND DURING D-CHECK, CRACK IN RIB AT STATION XRS 178 MIDDLE AFT EDGE IN FLAP WELL LEFT WING. ROUTED OUT CRACK. FABRICATED REPAIR ANGLE AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 1/27/99. (M)Nov 22, 1999 · N605AL · Doug DC873FSDR AT9900858Rib · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FIVE CRACKS IN RIGHT WING OUTBOARD RIBS. STOP DRILLED CRACKS AND FABRICATED ANGLES IAW DC9 SRM 57-01 FIG 3, 51-10-03, AND 51-30-02.Nov 15, 1999 · N833AT · Doug DC932SDR 20000615AP012Rib · crackedDURING C-CHECK, FOUND TWO EACH 1 INCH CRACKS INSIDE LEFT WING FIXED L/E AT TOP AFT END OF NOSE RIB-SLAT STATION 0, SEEN FROM OUTBOARD SIDE. FABRICATED NEW RIB AND INSTALLED IAW 51-10-1, PAGE 4. (M)Nov 12, 1999 · N802EA · Boeing 727225SDR 20000615AP011Rib · crackedDURING C-CHECK, FOUND RIGHT WING FIXED L/E RIB AFT END HAS TWO .75 INCH CRACKS THROUGH BOLT HOLES WHERE IT MOUNTS TO FRONT SPAR. CUT OUT CRACK AREAS AT R/W L/E INTERIOR WEB STATION 130-599 IAW SRM 51-40-2 FIG 1. FABRICATED FILLER AND REPAIR DOUBLER AND INSTANov 12, 1999 · N802EA · Boeing 727225SDR 20000615AP006Rib · crackedDURING C-CHECK, FOUND RIGHT WING L/E RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)Nov 11, 1999 · N802EA · Boeing 727225SDR DL72E992465Rib · crackedACTUATOR RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.Nov 8, 1999 · N831WA · Boeing 727247SDR RRXA991678Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E OB OF NR 4 PYLON AT STA XFS 710, CRACKED SKIN IN 2 PLACES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 57-2-1 FNov 2, 1999 · N811AL · Doug DC871SDR RRXA991677Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIBS AT STA XFS 703.75, XFS 672.5, XFS 566.25, XFS 585, XFS 591.25, XF 603.75, XFS 622.5, XFS 635. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANDNov 2, 1999 · N811AL · Doug DC871SDR RRXA991676Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, CENTER L/E RIBS AT STA XFS 347.75 AND XFS 360.25. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS AND INST IAW DC8 SRM 53-2-0 FIG 1Nov 2, 1999 · N811AL · Doug DC871SDR RRXA991674Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPPER RIB AT END AT STA XS 442.185. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2.Nov 2, 1999 · N811AL · Doug DC871SDR RRXA991673Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPER RIBS AT FWD AT STA XS 484.895, XS 467.323, XFS 366.5, XFS 304, XF 322.75 AND XFS 379. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANov 2, 1999 · N811AL · Doug DC871SDR MWEA99748Rib · corrodedCORROSION AROUND FASTENERS AND ON TRACK, LOWER RIB TRACK AT STATION 446 AT LONGERONS 29 LEFT TO 28 LEFT. CORROSION OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER.Oct 28, 1999 · N202ME · Doug DC932SDR 20000505AP017Rib · crackedFOUND NR 1 INCH CRACK AT BOTTOM OF RIB NR 6 SLAT ADJACENT TO INBOARD SIDE OF ACTUATOR ROD END ATTACHMENT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 51-40-3. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR 20000505AP016Rib · crackedFOUND .5 INCH CRACK AT LEFT WING TRAILING EDGE RIB, FROM AFT END TO RIVET HOLE, JUST FORWARD OF OUTBOARD AILERON OUTBOARD HINGE AREA. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE, TREATED, PRIMED AND PAINTED. INSTALLED IAW 51-40-3. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR 20000502AP001Rib · crackedFOUND 1 INCH CRACK IN RIB ADJACENT TO CENTER FOREFLAP TRACK GUIDE, LEFT INBOARD MIDFLAP. REMOVED AND REPLACED FLAP ASSY WITH SERVICEABLE UNIT. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR ABXA9900826Rib · crackedDURING C-CHECK, FOUND RIGHT WING TRAILING EDGE PANEL INBOARD RIB CRACKED OUTBOARD OF MAIN LANDING GEAR. REPLACED RIB IAW DC9 SRM 51-30-2.Oct 26, 1999 · N928AX · Doug DC932SDR 99ZZZX4230Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK404-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES.Oct 25, 1999 · N5040Q · Cessna 402BSDR 99ZZZX4229Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK414-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES.Oct 25, 1999 · N5040Q · Cessna 402BSDR 99ZZZX4216Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-74. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT ASSOCIATED WITH THE CROct 25, 1999 · N5040Q · Cessna 402BSDR 99ZZZX4215Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-79. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT ASSOCIATED WITH THE CROct 25, 1999 · N5040Q · Cessna 402BSDR AALA991603Rib · crackedTUL - HFEC INDICATES CRACK IN RIB CHORD RADIUS INBOARD SIDE AT STATION 760R AT EDGE OF REPAIR DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SB 727-57-0112, DWG 65C33202 AND ESO 11697 DATED 10-20-99. (M)Oct 22, 1999 · N717AA · Boeing 727227SDR AALA991600Rib · crackedTUL - LEFT RIB CHORD CRACKED IN RADIUS UNDER DOUBLER STATION 760L. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SB 727-57-0112 DWG 65C3302 ESO 11697 DATED 10-20-99. (M)Oct 22, 1999 · N717AA · Boeing 727227SDR MWEA99706Rib · damagedRIGHT HAND TRAILING EDGE PANEL, AND RIB CAP DAMAGED ON OUTBOARD FLAP. MTC REMOVED AND REINSTALLED RIB.Oct 21, 1999 · N203ME · Doug DC932SDR MWEA99705Rib · damagedFIRST AND SECOND RIB OF THE RIGHT HAND WING TRAILING EDGE, INBOARD OF THE END CAP AND CHANNEL, DAMAGED. MTC REMOVED AND REPLACED FIRST AND SECOND RIB AS REQUIRED.Oct 21, 1999 · N203ME · Doug DC932SDR UPS99230878Shear Tie · corrodedINSPECTION TYPE:SI ,CORROSION (C57-571-01.01-02) R/W NR 3 FUEL CELL INTERNAL AFT LOWER SPAR CHORD AT WS 225-WS 229. REPAIRED PER ER 99-6094.Oct 7, 1999 · N951UP · Boeing 72725CSDR AU990995Rib · corroded(AUS) WING RIB CONTAINS EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE AND AT OTHER LOCATIONS ON THE RIB.Oct 7, 1999 · Socata TB10TOBAGOSDR AU990979Rib · corroded(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE. CORROSION ALSO EVIDENT IN OTHER AREAS OF THE RIB.Oct 7, 1999 · Socata TB10TOBAGOSDR AU990978Rib · corroded(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE. THE RIB IS THE ONE TO WHICH THE LANDING GEAR OLEO STRUT IS ATTACHED.Oct 7, 1999 · Socata TB10TOBAGOSDR UPS99830901Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Oct 3, 1999 · N814UP · Doug DC873FSDR 99T64R440EWARib · crackedLEFT WING T/E STA 261 FLAP WELL RIB CRACKED BELOW NR 4 SPOILER. CUT OUT CRACK. TREATED AND PRIMED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 2, 1999 · N8079U · Doug DC871SDR UPS99830834Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS340 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 29, 1999 · N718UP · Doug DC871FSDR MZZA99215Rib · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING INSPAR WS 738.5 RIB UPPER FLANGE ATTACHED TO UPPER STRINGER 12. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 57-10-05 FIG 5. (M)Sep 28, 1999 · N15781 · Boeing 727232SDR 99T64R467WEARib · crackedFOUND DURING D-CHECK. NR 2 STUB WING LEADING EDGE, 7 INCH CRACK TOP RIB STA 250.089. STOP DRILLED CRACK IAW DC-8 SRM 57-2-0. FABRICATED TWO DOUBLERS IAW DC-8 SRM 57-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20D AND Sep 23, 1999 · N8079U · Doug DC871SDR DLL19992182Rib · crackedTHE LEFT SIDE WING UPPER RIB CAP AT IWS 555 WAS FOUND CRACKED BETWEEN STRS 15 AND 16, DURING A ROUTINE INSPECTION OF THE RIB CAPS.Sep 21, 1999 · N768DL · Lkheed 10113853SDR UPS99830788Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 304.0 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830786Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 442.185 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830785Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 448.581 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830784Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT XS 454.976 WAS CRACKED AT THE AFT UPPER END. REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830782Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 297.5 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830781Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 735 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830779Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 835 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830777Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIB AT FS 335.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830769Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 841.250 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830766Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB ATV STA XFS 772.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830765Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 816.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830762Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 810 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830761Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 753.750 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830760Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 722.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830887Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT XILD O.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830851Rib · crackedINSPECTION TYPE:C123 LT WING L/E AT XS 250.089, ABOVE THE WIRE BUNDLES. THE RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Sep 15, 1999 · N718UP · Doug DC871F
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