JASC 5754

Service difficulty reports · 17,348

Reports filed under 5754 · Leading Edge Devices, 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 = '5754'
  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 QXEA9901991Skin · chafedYXX - LEFT-HAND WING OUTBOARD FLAP HAS CHAFING WEAR ON THE UPPER SURFACE OF THE FLAP AT YW225.00. REPAIRED IAW RD 57-1022.Sep 14, 1999 · N352PH · Dhav DHC8202SDR CALA9901213Slat · dentedINSPECTION FOUND RT WING 0 SLAT DENTED. REPAIRED SLAT IAW ECRA 5720-01170.Sep 14, 1999 · N93875 · Doug DC982SDR CALA9901210Skin · dentedINPECTION FOUND LEFT WING 0 SLAT DENTED. THE SLAT WAS REPAIRED IAW ECRA 5720-01120.Sep 14, 1999 · N93875 · Doug DC982SDR 99ZZZM669Skin · gougedRT WING INBOARD FLAP FOREFLAP LEADING EDGE GOUGED INBOARD OF INBOARD TRACK. FABRICATED REPAIR DOUBLER IAW SRM 57-50-4. INSTALLED REPAIR DOUBLER IAW SRM 57-50-4. (M)Sep 13, 1999 · N361KP · Boeing 727225SDR 99ZZZM668Skin · gougedRIGHT WING OUTBOARD FLAP FOREFLAP HAS GOUGE IN LEADING EDGE. FABRICATED REPAIR IAW SRM 57-50-4. INSTALLED REPAIR IAW SRM 57-50-4. (M)Sep 13, 1999 · N361KP · Boeing 727225SDR CALA9901197Fitting · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING NR 5 SLAT O/B FITTING. THE FITTING WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-30-2, 51-30-8, AND ECRA 5750-03276.Sep 12, 1999 · N93875 · Doug DC982SDR DHL99724008Bracket · brokenNR 1 KRUEGER FLAP INTRANSIT LIGHT ON DURING RETRACTION AT FLAPS 5 DEGREE. REMOVED AND REPLACED KRUEGER SWITCH ARM BRACKET PER MM 27-82-1, OPS CHECK OK.Sep 11, 1999 · N724DH · Boeing 727228SDR 20000515AP010Skin · tornFOUND LEFT WING NR 3 LEADING EDGE FLAP TORN AT TRAILING EDGE. BLENDED OUT DAMAGED AREA PER SRM 57-50-3. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-3 PAGE 10 AND 51-10-2 PAGE 1. (M)Sep 10, 1999 · N803MA · Boeing 727225SDR DL72S992011Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK O/B SIDE OF TRACK. REPAIR PER MM 57-20-21.Sep 10, 1999 · N416DA · Boeing 727232SDR AWXA9900303Spar · brokenCONDITION: C-CHECK SLAT DAMAGEDISCREPANCY: #3 SLAT LOWER AFT SPAR BROKEN OUT SECTION AT ACTUATORCORRECTIVE ACTION: REPAIRED PER AWA ER 3-57-55-38ARECOMMENDATION: CLOSESep 10, 1999 · N325AW · Boeing 737301SDR 2000ZZZX686Panel · corrodedLEFT OUTBOARD MOST UPPER SLOT DOOR BOTTOM INBOARD OF INBOARD ADJ SCREW HAS CORROSION XS 503.789. BLENDED OUT CORROSION, TREATED AND PRIMED. MAXIMUM UNDER CUT IN RIB IS DOWN .078 INCHES. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-Sep 10, 1999 · N812TC · Doug DC8F55SDR DL72E992185Rib · crackedAT HMV2, RIB CRACKED NR 7 L/E SLAT, NR 5 L/E SUPPORT RIB IS CRACKED AT UPPER LEG. REMOVED FASTENERS AND CLIPS, STOP DRILLED CRACK MM 57-54-00 FIG 809. REPAIRED PARTS PER SAME, INSTALLED DOUBLER PER 57-54-00.Sep 8, 1999 · N282WA · Boeing 727247SDR DL72E992172Rib · crackedAT HMV2, FOUND NR 4 L/E SUPPORT RIB IS CRACKED UPPER LEG. REMOVED FASTENERS AND CLIP, STOP DRILLED, FABRICATED DOUBLER REPAIR PER 57-54-00 FIG 809, AND INSTALLED PER SAME.Sep 8, 1999 · N282WA · Boeing 727247SDR DL72E992150Skin · crackedSKIN CRACKED UNDER FENCE NR 5 SLAT. REPAIRED AS PER MM 57-54-0.Sep 8, 1999 · N282WA · Boeing 727247SDR 99ZZZX3933Skin · crackedAPPROXIMATELY .6250 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING EDGE ABOVE NR 1 FLAP TRACK. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS AS WELL AS BENDING LOADS.Sep 8, 1999 · N803MA · Boeing 727225SDR 20000515AP009Skin · crackedFOUND LEFT INBOARD FORE FLAP LEADING EDGE HAS CUT AT CENTER SECTION. STOP DRILLED IAW SRM 57-50-4 HFEC, CRACK CONTAINED AT STOP DRILL PART 6 51-00-00, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4 AND 51-30-2 PAGE 4. (M)Sep 5, 1999 · N803MA · Boeing 727225SDR AT9900637Rib · gougedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND GOUGED ON THE LEADING EDGE NR 3 SLAT RIB AT XOS 288.193. BLEND OUT GOUGED AREA, TREAT, PRIMED, AND REFINISH IAW DC9 SRM 57-01-0 FIG 1, SHEET 3, 57-21-1 FIG 1, AND TIMCO EO NR 99-1238.Sep 5, 1999 · N866AT · Doug DC932SDR UPS99230592Rib · crackedINSPECTION TYPE:C NR 3 LE SLAT RIB CRACKED O/B SIDE OF I/B SLAT TRACK. RIB REPAIR CARRIED OUT IAW 57-30-3.Sep 2, 1999 · N926UP · Boeing 72731CSDR DL72W991954Angle · crackedNR 6 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED ANGLE PER M/M 57-20-21 PAGE 813.Sep 2, 1999 · N2809W · Boeing 727247SDR 2000ZZZX685Panel · corrodedOUTBOARD SLOT LEFT WING L/E HAS AREA OF EXFOLIATION XW 454. CUT OUT AREA OF EXFOLIATION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-13-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)Aug 30, 1999 · N812TC · Doug DC8F55SDR DL72S991897Angle · crackedREF SHIP 400 TPA LTR CHK C-1, NR 2 L/E SLAT ANTI-ICE T-DUCT CUT OUT ANGLE CRACKED. REPAIRED PER MM 57-54-0.Aug 25, 1999 · N400DA · Boeing 727232SDR 20000515AP048Structure · crackedAPPROX .625 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING ABOVE NR 1 FLAP TRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IW SRM 57-50-4 FIG 1. (M)Aug 23, 1999 · N803MA · Boeing 727225SDR CALA9901082Skin · corrodedINSPECTION FOUND LT WING NR 8 SLAT CORRODED ON LEADING EDGE AT TRACK. THE NR 8 SLAT WAS REMOVED AND REPLACED IAW MM 27-80-01.Aug 23, 1999 · N39081 · Doug DC1030SDR P2EA99268Angle · crackedSJO - RIGHT WING NR 6 SLAT INTERNAL ANGLE CRACKED. REPLACED ANGLE FROM SLAT STATION 385.36 TO 254.24 BY FABRICATION IAW SRM 51-10-01 PAGE 5 AND 51-30-02. (M)Aug 22, 1999 · N204AU · Boeing 737247SDR P2EA99276Skin · dentedSJO - LEFT WING NR 2 KRUEGER FLAP DENTED. REPAIRED IAW EO COO-3-57-511-99. (M)Aug 21, 1999 · N204AU · Boeing 737247SDR 20000515AP052Bracket · crackedOUTBOARD BRACKET HAS .015625 INCH VISIBLE CRACK AT OUTBOARD END BETWEEN BEND RADIUS AND BOLT HOLE WHERE NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. REMOVED FABRICATED AND INSTALLED BRACKET IAW SRM''S 51-30-1 PAGE 1, 51-20-1 FIG 7, 51-30-2 PAGE 6. (M)Aug 20, 1999 · N803MA · Boeing 727225SDR 20000515AP045Bracket · crackedBOTH SUPPORT BRACKETS CRACKED .25 INCH AT BOTTOM OF NR 3 SLAT OUTBOARD TRACK WHERE IT ATTACHES TO THE LOWER SKIN EXTENSION. REMOVED FABRIATED AND INSTALLED 2 SUPPORT BRACKETS IAW SRMS 51-20-1 FIG 7, 51-20-2 PAGE 7, 51-30-2 PAGE 1. (M)Aug 20, 1999 · N803MA · Boeing 727225SDR 20000515AP044Angle · crackedAPPROX TWO 2.25 INCH CRACKS AT NR 1 LEADING EDGE SLAT CHORD WHERE OUTBOARD AND INBOARD UPSTOP PAD MOUNTS. REMOVED AND FABRICATED NEW SLAT CHORD AND INSTALLED IAW SRM 51-10-2 PAGE 4, 51-20-1 FIG 7, 51-30-2 PAGE 1. (M)Aug 20, 1999 · N803MA · Boeing 727225SDR 20000515AP032Angle · crackedFOUND APPROX 2.5 INCH CRACK AT RIGHT WING NR 6 SLAT LOWER CHORD WHERE INBOARD UPSTOP MOUNTS. REMOVED DAMAGE AREA IAW SRM 51-40-3 PAGE 3. FABRICATED PARTS AND SPLICE IAW SRM 51-40-2 AND INSTALLED REPAIR IAW SRM 51-40-3 PAGE 3. (M)Aug 19, 1999 · N803MA · Boeing 727225SDR 20000515AP046Rib · crackedFOUND 1.75 INCH CRACK AT OUTBOARD SIDE LEFT WING FIXED LEADING EDGE RIB AT UPER AFT END THROUGH TWO BOLT HOLES WS 330. REMOVED RIB. FABRICATED AND INSTALLED RIB REPAIR IAW SRM 51-20-1 PAGE 18. (M)Aug 17, 1999 · N803MA · Boeing 727225SDR AWXA9900265Skin · wornC-CHECK, WEAR MARK IN UPPER SURFACE OF LT O/B FOREFLAP MID SECTION. REMOVED FOREFLAP, REPAIRED PER ER 3-57-52-162, REINSTALLED FOREFLAP AND OPERATIONALLY CHECKED OK PER AWA T/C R3M27002.Aug 17, 1999 · N325AW · Boeing 737301SDR 20000515AP043Skin · crackedFOUND .3125 INCH CRACK AT LT WING FIXED LE CUTOUT ABOVE NR 4 SLAT INBOARD TRACK AREA. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW SRM 57-30-4 PAGE 7. (M)Aug 14, 1999 · N803MA · Boeing 727225SDR MALA976546Strap · brokenDURING HEAVY CHECK INSPECTION FOUND CENTER HINGE FLAP STRAP BROKEN AD 990417-01. MAINTENANCE REMOVED AND REPLACED STRAP IAW EO AD 990417-02.Aug 13, 1999 · N46XJ · Saab SF340ASDR UPS99230445Skin · crackedINSPECTION TYPE:C, NR 3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED IAW EO B727-5750-3082.Aug 10, 1999 · N941UP · Boeing 72722CSDR UPS99230444Skin · crackedINSPECTION TYPE:C, NR 3 L/E FLAP ANTI-ICE SKIN CRACKED AT UPPER FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED IAW EO B727-5750-3082.Aug 10, 1999 · N941UP · Boeing 72722CSDR DL72L991929Rib · crackedAT HMV2, FOUND NR 6 L/E SLAT 10TH RIB FROM I/B END IS CRACKED IN TWO PLACES. REMOVED RIB, FABBED NEW PER SRM 51-00 AND INSTALLED.Aug 9, 1999 · N501DA · Boeing 727232SDR SWAA991311Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER AFT INBOARD CORNER. REPAIRED SLAT PER SRM.Aug 6, 1999 · N511SW · Boeing 7375H4SDR UPS99230364Rib · crackedINSPECTION TYPE:C WHILE WORKING CUSTOMER CARD #934321 FOUND CRACKED RIB IN NR 4 SLAT, 3RD RIB I/B OF O/B SLAT TRACK WHERE RIB ATTACHES TO LOWER AFT CHORD. REMOVED CRACKED RIB AND INSTALLED NEW RIB PER SRM 51-30-2.Aug 5, 1999 · N935UP · Boeing 7271A7CSDR UPS99230299Rib · crackedINSPECTION TYPE:C, CRACKED RIB IN NR 4 SLAT, 2ND RIB I/B OF O/B SLAT TRACK WHERE RIB ATTACHES TO LOWER AFT CHORD. REMOVED AND REPLACED RIB PER SRM 51-30-7.Aug 5, 1999 · N935UP · Boeing 7271A7CSDR TSAA9957379Skin · inoperativeNR 1 LEADING EDGE SLAT L/E SKIN HAS 3 CLOSE DENTS 14.5 INCHES INBOARD OF SLAT OUTBOARD EDGE. HFEC REVEALED NO CRACKS AT DENTS. THREE DENTS LOCALIZED WITHIN 2 INCH AREA WITH DEEPEST POINT .067 INCH DEEP. PER SRM 57-50-1 FIG 2, DENT IS OUT OF LIMITS. REMOVEDAug 5, 1999 · N808AL · Boeing 7372T4SDR CALA9900936Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING NR 7 SLAT LOWER CHORD. THE LOWER CHORD ANGLE WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2.Aug 2, 1999 · N79748 · Boeing 727224SDR CALA9900930Bracket · gougedINSPECTION FOUND A GOUGE IN LT WING SLAT NR 0 O/B END AFT ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 27-80-01.Aug 1, 1999 · N83872 · Doug DC982SDR UPS99230754Mounting Lug · corrodedINSPECTION TYPE:C, (CORROSION C57-562-01.00-02) CORROSION ON NR 6 K-FLAP INBOARD MOUNT LUG UPPER BOLT. REMOVED NR 6 K-FLAP PER MM 27-81-01. NR 6 K-FLAP CORROSION OUT OF LIMITS PER SRM ADDENDUM EO B727-5750-5542. REPLACED K-FLAP PER MM 27-81-01.Jul 30, 1999 · N935UP · Boeing 7271A7CSDR AT9900581Skin · corrodedDURING SCHEDULED INSPECTION AT TIMCO, FOUND RT WING LEADING EDGE INBOARD FLAP SURFACE HAS SURFACE CORROSION. REMOVED CORROSION, DYE PENETRANT AND HFEC INSPECTION. NO RELEVANT INDICATIONS. ALODINED, PRIMED IAW DC9 SRM 51-10-3 AND TIMCO EO NR 99-1192.Jul 30, 1999 · N832AT · Doug DC932SDR USAA990787Skin · crackedCLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)Jul 29, 1999 · N338US · Boeing 737301SDR DHL9970328CBolts · crackedAT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074.Jul 27, 1999 · N703DH · Boeing 72730CSDR CALA9900873Rib · crackedINSPECTION FOUND A 0.085 CRACK AT FASTENER HOLE OF LT O/B NR 5 SLAT SEAL RETAINING RIB. THE RIB WAS REMOVED IAW SRM 51-30-0. THE RIB WAS REPAIRED AND REINSTALLED IAW SRM 51-30-0, ECRA 5750-03253, AND EA 9-2780-2-AO467.Jul 27, 1999 · N16806 · Doug DC982SDR DL72W991680Bracket · crackedFOUND ON F-1 LETTER CK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED OUTBOARD END. REPAIRED PER MM 57-20-0.Jul 26, 1999 · N2811W · Boeing 727247SDR DL72S991676Rib · damagedLWR AFT EXTERNAL SKIN OPENED UP TO FACILITATE REPAIR OF NR 6 RIB. REPAIRED SKIN PER SRM 57-54-0 FIG 801.Jul 25, 1999 · N527DA · Boeing 727232SDR AT9900580Skin · punctureDURING SCHEDULED INSPECTION AT TIMCO, FOUND TEMPORARY REPAIR OF POSSIBLE PUNCTURE OF RT WING LEADING EDGE NEAR FUELING DOOR. REMOVED RT NR 3 SLAT. INSPECTED PER DC9 NDT SRM. NO NEW CRACKS FOUND. REMOVED INSIDE SKIN PER SRM 57-09. FABRICATED REPAIR DOUBLERJul 25, 1999 · N832AT · Doug DC932
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