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 RRXA000628Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 641.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-32-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000627Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 635.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000626Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 622.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000625Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 616.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000624Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 591.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000623Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 610.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000622Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 603.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR DHL200080308CRib · crackedAT C-CHECK, LT WING INTERCOL 9 RIBS CRACKED .5 INCH IN BETWEEN NR 518E AND 518C ACCESS PANELS. FABRICATED DOUBLER PER SRM 57-2-0 PAGE 9-10. INSTALLED DOUBLER PER SRM 51-2-0 PAGE 6-10. WORK ACCOMP ON NONE ROUTINE WORK CARD 1171.Jan 22, 2000 · N803DH · Doug DC873FSDR ASOA00010Rib · crackedDURING C-CHECK, FOUND RT WING RIB NR 20 SECOND CLEAT FROM THE FRONT CRACKED. MAINTENANCE REPLACED CRACKED CLEAT IAW EMB 120 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (X)Jan 22, 2000 · N273AS · Emb EMB120RTSDR UPS00831574Rib · damagedINSPECTION TYPE:C1 RIGHT WING L/E RIB AT XW 257.5 IS DAMAGED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5769517, AND SRM 51-1-20D.Jan 19, 2000 · N703UP · Doug DC871FSDR RRXA000050Rib · crackDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT L/E CENTER SECTION AT STA XFS 310 LWR RIB. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 18, 2000 · N792FT · Doug DC873FSDR UPS00831402Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E AT STA XFS616.250, THE LOWER L/E RIB FWD OF ACCESS PANEL OPENING HAS A 3 INCH CRACK. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 12, 2000 · N703UP · Doug DC871FSDR UPS00831371Rib · crackedINSPECTION TYPE:C1 LT WING L/E AT STA XFS329.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 12, 2000 · N703UP · Doug DC871FSDR UPS00831349Rib · crackedINSPECTION TYPE:C1, LEFT WING L/E AT STA XFS297..500, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 12, 2000 · N703UP · Doug DC871FSDR UPS00831441Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E AT XFS304 UPPER RIB IS CRACKED STOP DRILLED CRACK AND REPAIRED I.A.W. SRM 57-2-0 FIG. 2Jan 11, 2000 · N703UP · Doug DC871FSDR UPS00831417Rib · crackedINSPECTION TYPE:C1, RT WING L/E AT STA XFS 448.581, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 11, 2000 · N703UP · Doug DC871FSDR UPS00831373Rib · crackedINSPECTION TYPE:C1 RT WING L/E AT STA XS408.3434, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 11, 2000 · N703UP · Doug DC871FSDR UPS00831372Rib · crackedINSPECTION TYPE:C1 RT WING L/E AT STA XS442.185, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 11, 2000 · N703UP · Doug DC871FSDR UPS00831366Rib · crackedINSPECTION TYPE:C1, RT WING L/E AT STA XOLDI6.225, THE LOWER L/E RIB IS CRACKED AT THE AFT END. REPAIRED AREA IAW SRM 57-2-0 FIG 2.Jan 11, 2000 · N703UP · Doug DC871FSDR 2000UALA00017Rib · crackedDURING INSPECTION PER SB 727-57-0112 AS MANDATED BY AD94-07-08 ON THE LBL 70.5 RIB CHORD AT STATION 760.95, TWO CRACKED FASTENER HOLES WERE FOUND. CAUSE WAS FATIGUE. BOTH HOLES WERE OVERSIZED UNTIL THE CRACKS WERE ELIMINATED AND OVERSIZED FASTENERS INSTALLEDJan 10, 2000 · N7463U · Boeing 727222SDR UPS00831374Rib · crackedINSPECTION TYPE:C1 RT WING L/E ATV STA XFS335.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED AREA IAW SRM 57-2-0 FIG 2 AND 57-3-1.Jan 10, 2000 · N703UP · Doug DC871FSDR UPS00831358Rib · crackedINSPECTION TYPE:C123 LEFT WING CTR L/E SECTION IB END UPPER RIB CRACK ON INTERIOR. STOP DRILLED CRACKED RIB VERIFICATION OF REPAIR IAW 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALL REPAIR PER SRM 57-2-0 AND 51-1-2 0.Jan 10, 2000 · N752UP · Doug DC871FSDR UPS00831375Rib · crackedINSPECTION TYPE:C1 RT WING L/E AT STA. XFS622.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831370Rib · crackedINSPECTION TYPE:C1 RT WING L/E AT STA XOLDI 6.225, THE UPPER L/E RIB IS CRACKED AT MID-SPAN. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831369Rib · crackedINSPECTION TYPE:C1, RT/H WING L/E AT STA XFS635..00, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831368Rib · crackedINSPECTION TYPE:C1, RT WING L/E AT STA XFS791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831367Rib · crackedINSPECTION TYPE:C1 RT WING L/E AT STA XFS797.500, THE L/E RIB IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR UPS00831352Rib · crackedINSPECTION TYPE:C1, LT WING L/E RIB AT STA XFS591.25 IS CRACKED AT THE UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 9, 2000 · N703UP · Doug DC871FSDR CA000720002Rib · loose(CAN) EXCESSIVE LOOSENESS BETWEEN THE TWO HALVES OF THE FLAP AT THE CENTER HINGE ARM POSITION. THE RIBS ON EITHER SIDE OF THE HINGE ARM ARE ASSEMBLED TO THE ARM BY THE USE OF LONG MS20470AD5 SOLID RIVETS. IT WOULD APPEAR THAT THERE HAS BEEN SOME WORKING BETWEJan 6, 2000 · Dhav DHC6300SDR UPS00831296Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 347.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Jan 2, 2000 · N702UP · Doug DC871FSDR UPS00831295Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 347.75, 354, AND 391.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.Jan 2, 2000 · N702UP · Doug DC871FSDR UPS00831285Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 635 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACKED AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Jan 2, 2000 · N702UP · Doug DC871FSDR UPS00831294Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 336 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 31, 1999 · N702UP · Doug DC871FSDR UPS00831308Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831307Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831306Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831293Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831291Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 297 AND 304 ARE CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831289Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 360.25 AND 366.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831280Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831278Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR UPS00831276Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 597.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.Dec 28, 1999 · N702UP · Doug DC871FSDR AT9900918Rib · crackedFOUND LEFT WING OUTBOARD TRAILING EDGE INSIDE RIB NR 2 TOP AND BOTTOM CRACKED. INSTALLED DOUBLERS ON TOP AND BOTTOM OF NR 2 RIB.Dec 23, 1999 · N834AT · Doug DC932SDR A6WA0000005Rib · crackedRIGHT WING TIP FALSE RIB HAS A CRACK. REPAIRED ASSY PER ABOVE IAW AW-57-02-9412-06. (M)Dec 13, 1999 · N292UE · Bag BAE146200ASDR P2EA99352Rib · crackedSJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51-10-1 PAGE 5. (M)Dec 1, 1999 · N219US · Boeing 737281SDR TWAA9917504Rib · crackedDURING OP 16 MAINT CHECK, FOUND ON THE RT WING A CRACK APPROXIMATELY 1 IN LONG WAS FOUND IN REPAIR DOUBLER OF WING L.E. RIB, 13 IN OTBD OF INBD END OF NUMBER 4 SLAT. INSTALLED NEW DOUBLER AND SHIM PER SRM 57-06A, FIG 5, SHEET 1 AND 4.Nov 30, 1999 · N925L · Doug DC932SDR CA991210022Bracket · cracked(CAN) THE CRACK WAS CREATED BY THE ATTACHMENT OF THE BRACKET ONTO THE RIB WITH AN AN3-4A BOLT.Nov 29, 1999 · Piper PA28140SDR GAIA99200Rib · damagedRIGHT WING DAMAGED AT RIB LOWER FLANGE STA 686.5 AND STR 6. REPLACED FLANGE AT LOWER RIGHT WING RIB, STA 686.5, STR 6 IAW SRM 51-30-2. REF: N/R 2448. (X)Nov 23, 1999 · N916PG · Boeing 727287SDR AALA991785Rib · crackedTUL - LEFT 760.95 RIB CHORD ANGLE CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR KIT PER SB 57-0112. TST: 63,311 HOURS. CYCLES, 40,510. (X)Nov 23, 1999 · N848AA · Boeing 727223SDR RRXA000298Rib · crackedDURING A MAINTENANCE VISIT FOUND LEFT WING, FLAP WELL, RIB CRACKED AT XRS 178. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-18Nov 22, 1999 · N605AL · Doug DC873F
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