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 CALA9802029Rib · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LT WING TIP RIB INSIDE OVAL ACCESS CUTOUT 8111. A REPAIR WAS ACCOMPLISHED IAW SRM 51-40-3, PAGE 3.Nov 3, 1998 · N59792 · Boeing 727232SDR AU981495Rib · cracked(AUS) LEFT WING RIB CRACKED ADJACENT TO THE MLG ATTACHMENT BRACKET. SUSPECT CAUSED BY HEAVY LANDING. PART TC: 1,598.Nov 3, 1998 · Grob G115CSDR ABXA9801128Rib · crackedLEFT WING LEADING EDGE RIB CRACKED STATION SFX 772.500. REPAIRED IAW ABX DWG K05056.Nov 2, 1998 · N823AX · Doug DC863SDR ABXA9801106Rib · crackedLEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS591.250. REPAIRED IAW SRM 51-1-20D.Oct 31, 1998 · N823AX · Doug DC863SDR ABXA9801105Rib · crackedLEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION FS 785. REPAIRED IAW DWG K05056.Oct 31, 1998 · N823AX · Doug DC863SDR DHL9980182CRib · crackedAT C-CHECK, LT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA STA 291.5 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE AND FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25.Oct 30, 1998 · N801DH · Doug DC873FSDR 98ZZZX4230Wing · crackedLEFT WING RIB WAS FOUND CRACKED AT STA 190.0. THIS LOCATION IS AT THE OUTBOARD HINGE LOCATION OF THE AILERON. THIS IS WHERE ALL THE BALANCE LEAD IS LOCATED. SUBMITTER SUGGESTED CAUSE AS FATIGUE DUE TO RIB FLEXING DURING TURBULENCE. AIRCRAFT IS USED FOR TRAOct 30, 1998 · N9343D · Cessna 172RGSDR DHL9980199CRib · crackedAT C-CHECK, RT WING CENTER LOWER INTERNAL AREA AT STA 300 FOUND CRACKD ON LOWER RIB. DRILLED TOP HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25.Oct 29, 1998 · N801DH · Doug DC873FSDR AU981501Rib · cracked(AUS) LEFT WING RIB CRACKED ADJACENT TO THE MLG ATTACHMENT BRACKET ON THE REAR END. SUSPECT CAUSED BY HEAVY LANDING. PART TC: 1,297.Oct 28, 1998 · Grob G115CSDR DHL9980181CRib · crackedAT C-CHECK, RT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA AT STA 291.5 FOUND CRACK IN LOWER RIB. STOP DRILLED AND FABRICATED REPAIR DOUBLER PER SRM 57-2-0, 6 X 1.25.Oct 24, 1998 · N801DH · Doug DC873FSDR UPS98828107Bulkhead Fitting · crackedINSPECTION TYPE-D, NR 3 MAIN TANK AT THE XRS 74 BULKHEAD STRINGER 51 AFT ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.Oct 21, 1998 · N779UP · Doug DC871FSDR UPS98828078Rib · crackedINSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT FITTING. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828076Rib · crackedINSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 797.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828063Rib · crackedINSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 585.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED L/E RIB IAW SRM 57-2-0 FIG 2.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828057Rib · crackedINSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 566.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828055Rib · crackedINSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 335.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828001Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828000Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB AT XFS822.5 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827999Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB AT 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827998Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB AT XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827997Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827996Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT AFT LWR END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827993Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98827992Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT XFS 760 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Oct 20, 1998 · N779UP · Doug DC871FSDR UPS98828062Rib · crackedINSPECTION TYPE-C, 3 RT WING LWR L/E RIB AT XFS 360.25 IS CRACKED BEYOND THE DOUBLER. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 19, 1998 · N779UP · Doug DC871FSDR UPS98828061Rib · crackedINSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 372.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.Oct 19, 1998 · N779UP · Doug DC871FSDR UPS98828059Rib · crackedINSPECTION TYPE-C, 3 RT WING L/E RIB AT XS 250.089 IS CRACKED 6 INCHES FWD OF THE SPAR. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.Oct 19, 1998 · N779UP · Doug DC871FSDR RRXA99979Rib · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE INTORADIOUS OF RIGHT WING L/E RIB AT STA= 540. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROVED TIMCO DER ENGIOct 19, 1998 · N964R · Doug DC863SDR DHL9980171CRib · crackedAT C-CHECK, RT WING O/B LEADING EDGE INTERIOR LOWER AREA AT STA 785 RIBS CRACKED. STOP DRILLED HOLE AND FABRICATED DOUBLER REPAIR 6 X 1/25 PER SRM 57-2-0.Oct 19, 1998 · N801DH · Doug DC873FSDR DHL9980198CRib · crackedAT C-CHECK, RT WING CENTER L/E LOWER INTERIOR AREA AT STA 347 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE, FABRICATED REPAIR DOUBLER PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-21, 6 X 1.25.Oct 18, 1998 · N801DH · Doug DC873FSDR MWEA981007Rib · crackedFOUND CRACK ON LEFT WING LEADING EDGE SECOND RIB OUTBOARD OF NUMBER 1 SLAT TRACK AT STATION 256.75. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.Oct 17, 1998 · N601ME · Doug MD88SDR DHL99801108Rib · crackedAT C-CHECK, LEFT WING LOWER INT AREA AT STA 337 HAS CRACK 12 INCHES LONG ON LOWER INT RIB WEB AREA. REMOVED CENTER L/E LEFT WING. REMOVED CRACKED LOWER DOUBLER FROM CENTER L/E AT 337. FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. INSTALLED DOUBLER PEROct 17, 1998 · N801DH · Doug DC873FSDR RRXA99983Rib · gougedDURING A MAINTENANCE VISIT, FOUND GOUGE IN RIB, L/W L/E AT STA= XFS= 540. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REOOct 15, 1998 · N964R · Doug DC863SDR UPS98827967Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XS 250.089 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871FSDR UPS98827965Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 385.25 IS CRACKED 16 FWD OF THE T/E. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871FSDR UPS98827964Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 691.250 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 13, 1998 · N729UP · Doug DC871FSDR UPS98828026Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA 691.25 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.Oct 11, 1998 · N729UP · Doug DC871FSDR UPS98827961Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 653.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Oct 11, 1998 · N729UP · Doug DC871FSDR P2EA98219Rib · crackedSJO - RIGHT WING NR 3 FUEL TANK RIB CRACKED IN AFT SECTION BETWEEN REAR SPAR AND STRINGER 2, WBL 135.5 DEFECT SIZE, LENGTH 1 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5 BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATEDOct 5, 1998 · N620PC · Boeing 737244SDR P2EA98200Rib · crackedSJO - LEFT WING NR 1 FUEL TANK RIB CRACKED AT WBL 135.5 IN AFT SECTION, BETWEEN REAR SPAR AND STRINGER 16. REPAIRED LEFT WING LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SB 737-57-1186 DATED APRIL 13, 1989 SECTION 3, PART 3, FIG 3. Oct 5, 1998 · N620PC · Boeing 737244SDR DHL9871524CRib · crackedAT C-CHECK, RIGHT WING TIP CRACK AT FWD UPPER EDGE. REMOVED AND REPLACED FWD RIB PER SRM 51-30-2. N/R 2064Oct 5, 1998 · N715DH · Boeing 727155CSDR DHL9871513CRib · corrodedAT C-CHECK, R/W LEADING EDGE INTERNAL STRUCTURE UPPER SURFACE RIB AT STA 246 HAS LOWER CHORD ANGLE CORRODED AT APPROX 8 FWD OF WING FRONT SPAR. REMOVED AND REINSTALLED LOWER CHORD ANGLE PER SRM 51-30-2, 23 INCHES LONG. N/R 2118Oct 5, 1998 · N715DH · Boeing 727155CSDR DHL9871525CRib · crackedAT C-CHECK, RIGHT WING FIXED L/E INTERIOR THE NR 6 SLAT I/B TRACK SUPPORT RIB AT FRONT SPAR IS CRACKED VERTICALLY AT THE ATTACH BOLTS. INSTALLED NEW ATTACH ANGLES AT RT LEADING EDGE I/B TRACK AT NR 6 SLAT PER SRM 57-20-1, 10 INCHES LONG.Oct 2, 1998 · N715DH · Boeing 727155CSDR UPS98827890Rib · crackedINSPECTION TYPE:C LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 597.5. REPAIRED IAW SRM 57-2-0.Sep 27, 1998 · N818UP · Doug DC873FSDR UPS98827886Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER AT STA XFS 578.75. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 27, 1998 · N818UP · Doug DC873FSDR UPS98827885Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 616.25. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 27, 1998 · N818UP · Doug DC873FSDR UPS98827884Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 610. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 27, 1998 · N818UP · Doug DC873FSDR UPS98827862Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 379.0. STOP DRILLED CRACKED AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 22, 1998 · N818UP · Doug DC873FSDR UPS98827861Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED AT AFT O/B FASTENER AT STA XOLDI 6.225. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Sep 22, 1998 · N818UP · Doug DC873FSDR CALA9801805Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING FIXED LEADING EDGE RIB BETWEEN XFS 1042 AND XFS 1192. THE RIB WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 57-21-00 FIGURE 8, 51-21-01 AND 51-31-01.Sep 17, 1998 · N14075 · Doug DC1030
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