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 CALA9900135Panel · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 4 SLAT CLOSURE PANEL. THE PANEL WAS REPAIRED IAW SRM 51-70-05.Feb 12, 1999 · N17104 · Boeing 757224SDR 99ZZZX1303Panel · corrodedDURING A C-CHECK, CORROSION NOTED ON LT SLAT PANEL NR 6205.Feb 12, 1999 · N906PG · Boeing 727281SDR UPS99228986Hinge · corrodedINSPECTION TYPE-D, NR 1 LE FLAP MIDDLE MOUNTING CASTING HINGE CORRODED. REPLACED CASTING HINGE IAW DRAWING NR 65-18533.Feb 11, 1999 · N923UP · Boeing 72731CSDR CALA9900129Panel · crackedINSPECTION FOUND A 1 CRACK IN LT WING NR 3 SLAT PANEL AT FASTENER I/B OF SLAT ACTUATOR. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C30133.Feb 11, 1999 · N17329 · Boeing 7373T0SDR AU990430Wedge · disbonded(AUS) LEADING EDGE SLAT T/E WEDGES DISBONDED IN FOLLOWING AREAS: 1. NR 3 SLAT UPPER SURFACE DISBONDED AT OUTBOARD END 45 MM (1.771 INCH) FROM T/E . AREA OF DISBOND 50 MM BY 45 MM (1.968 INCH BY 1.771 INCH). 2. NR 4 SLAT UPPER SURFACE DISBONDED 1440 MM (Feb 11, 1999 · Boeing 767216SDR 99ZZZX1310Angle · corrodedDURING A C-CHECK, CORROSION NOTED ON NR 6 LEADING EDGE SLAT INBOARD SLAT TRACK LOWER ATTACH ANGLE.Feb 11, 1999 · N906PG · Boeing 727281SDR TWAA9902302Skin · delaminatedDURING CHECK-C, MAINTENANCE FOUND NR 5 L/E SLAT INBD TOP DELAMINATED 3 INCH BY 3 INCH. REMOVED DELAMINATED SKIN AND INSTALLED FILLER AND METAL HOT BOND REPAIR PER SRM 51-70-10.Feb 7, 1999 · N650TW · Boeing 767205SDR UPS99228753Rib · corrodedINSPECTION TYPE-C, CORROSION (C57-562-01.00-01) LT WING NR 1 K-FLAP CORRODED AROUND BONDING JUMPER BOLT HOLE ON BOTH SIDES OF RIB. CORROSION OUT OF LIMITS. REMOVED AND INSTALLED NEW K-FLAP. WORK DONE IAW SRM 57-50-1, MM 27-81-01.Feb 3, 1999 · N948UP · Boeing 72725CSDR SWAA990214Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT HAD A CRACK, STOP DRILL AT OUTBOARD AUX TRACK CUTOUT PAST STOP DRILL. REPAIRED CRACK PER RA NR 1-257-0063.Feb 3, 1999 · Boeing 7372H4SDR SWAA990210Skin · crackedDURING SCHEDULED BC1 CHECK, FOUND A .125 INCH CRACK IN NR 6 SLAT LOWER T/E SKIN 18 INCHES FROM ACTUATOR. REPAIRED PER SWA RA 1-357-0634.Feb 3, 1999 · N333SW · Boeing 7373H4SDR DHL9974012CAngle · crackedAT C CHECK, INNER STRUCTURE SUPPORT ANGLE IS CRACKED AT NR 2 L/E SLAT INNER NOSE BETWEEN L/E SLAT ACTUATOR AND ANTI-ICE DUCT. STOP DRILLED CRACK, HFEC STOP DRILL. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 BY 1 BY 17.5, N/R 1090.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR DHL9974009CFence · erodedAT C CHECK, NR 5 SLAT AERODYNAMIC FENCE ERODED IN SEVERAL AREAS. INSTALLED FILLER REPAIR PER SRM 51-40-1, 9 BY 3, N/R 2030.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR DHL9974008CShield · delaminatedAT C CHECK, NR 5 SLAT AERODYNAMIC FENCE LEADING EDGE METAL SHIELD DELAMINATING. INSTALLED BONDING REPAIR PER SRM 51-20-3, 6 BY 3, N/R 2029.Feb 3, 1999 · N740DH · Boeing 7272Q9SDR CALA9900098Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01.Jan 30, 1999 · N37077 · Doug DC1030SDR UPS99228558Skin · corrodedINSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLAP PER MM 27-81-01 AND ADJUST/TEST PER 727 MM 27-81-00.Jan 27, 1999 · N933UP · Boeing 72725CSDR DL72K990329Angle · crackedTHE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION 20 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY INSTALLING A DOUBLER AND NEW SECTION OF ANGLE.Jan 27, 1999 · N526DA · Boeing 727232SDR UPS99228639Rib · crackedINSPECTION TYPE-C, NR 6 L/E SLAT CRACK IN RIB 6 O/B OF FLAP ACTUATOR. AREA REPAIRED IAW SRM 57-50-03 FIG 9.Jan 22, 1999 · N917UP · Boeing 72730CSDR UPS99228625Skin · crackedINSPECTION TYPE:C NR 3 LE KRUEGER FLAP HAS CRACK ON ANTI-ICE SKIN. CRACK STOP DRILLED IAW SRM 51-10-1.Jan 22, 1999 · N917UP · Boeing 72730CSDR TWAA9901402Seal · damagedDURING CHECK-C, FOUND THE INBD END OF THE NR 2 LE SLAT, LOWER AFT SEAL, REPAIR DELAMINATING ON UPPER SIDE. BONDED SURFACES WITH 150 DEGREE CURE RESIN PER SRM 51-70-06, FIG 11.Jan 22, 1999 · N605TW · Boeing 767231SDR DL72L990154Stiffener · crackedCHK D-1, O/B SPAR STIFFENER CRACKED, NR 6 L/E SLAT O/B TRACK BOX. REPLACED PER MM 57-20-21.Jan 22, 1999 · N514DA · Boeing 727232SDR TWAA9901603Skin · damagedDURING CHECK-C MAINT, ON LT WING THE NR 1 LE SLAT LOWER SURFACE, O/B END HAD HOLE. INSTALLED 2 INCH BY 2 IN METAL TO METAL HOT BOND PER SRM 51-70-10.Jan 20, 1999 · N605TW · Boeing 767231SDR 99ZZZX1844Spar · damagedUPON REMOVAL OF AN UNSERVICEABLE LEADING EDGE SKIN REPAIR, DISCOVERED THE LOWER SPAR HAD BEEN SEVERELY DAMAGED BY IMPACT. THE SPAR HAD BEEN CUT IN SEVEN LOCATIONS IN AN ATTEMPT TO STRAIGHTEN THE SPAR, AND A DOUBLER WAS THEN INSTALLED. THE DOUBLER DOES NOT COJan 20, 1999SDR TWAA9901009Skin · damagedNR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED PER SRM 51-70-10, PAGE 26, FIG 10. CHECK-C 10-28-98 LAX.Jan 18, 1999 · N608TW · Boeing 767231SDR TWAA9901401Skin · damagedTHE NR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED BY SRM 51-70-10, PAGE 26 FIG 10. CHECK-C 10-28-98 LAX.Jan 15, 1999 · N650TW · Boeing 767205SDR SWAA990118Skin · crackedDURING SCHEDULED D-CHECK, FOUND NR 5 SLAT LOWER T/E SKIN LOWER SURFACE CRACKED AT FASTENER LOCATION 39 INCHES FROM I/B END. REPAIRED PER TRAMCO EWO 98-1191.Jan 15, 1999 · Boeing 7372H4SDR AU990037Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND WITH DISBONDED AREAS ON A TOTAL OF SEVEN SLATS. FOUND DURING VISUAL AND ULTRASONIC INSPECTIONS IAW BOEING ALERT SB 767-57A0039.Jan 13, 1999 · Boeing 767204SDR DL72S990065Skin · cracked4.5 INCH CRACK IN NR 8 SLAT COVE SKIN ANGLE AT O/B UPSTOP PAD. REPAIR PER MM 57-54-0 PG 816.Jan 11, 1999 · N519DA · Boeing 727232SDR SWAA990069Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER SKIN IS CRACKED 15 O/B OF O/B ACTUATOR STOP PAD 1 LONG. REPAIRED PER SWA RA 1-357-0616.Jan 10, 1999 · N685SW · Boeing 7373Q8SDR CALA9900057Bracket · crackedBRACKET HAS .3125 INCH CRACK AT INBOARD SIDE AT LEFT WING NR 1 SLAT WHERE INBOARD TRACK MOUNTS TO LOWER SKIN. REMOVED AND REPLACED CRACKED BRACKET PER SRM 51-30-2.Jan 9, 1999 · N33785 · Boeing 727232SDR UPS99228616Rib · crackedINSPECTION TYPE-SI, NR 4 SLAT O/B ACTUATOR RIB IS CRACKED. REMOVED AND REPLACED NR 4 SLAT WORK ACCOMPLISH ON NRC 838733.Jan 8, 1999 · N949UP · Boeing 72725CSDR UPS99228449Web · crackedINSPECTION TYPE-C, LT WING NR 4 LE SLAT AND ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW SRM 57-50-3.Jan 8, 1999 · N944UP · Boeing 72722CSDR UPS99228628Rib · crackedINSPECTION TYPE:SI NR 2 SLAT I/B TRACK I/B MOUNTING BRACKET SUPPORT RIB IS CRACKED. REPLACE NR 2 SLAT PER MM 27-81-11.Jan 7, 1999 · N949UP · Boeing 72725CSDR UPS99228364Skin · damagedINSPECTION TYPE:C BLEND OUT ON TE OF NR 5 LE SLAT RT WING. DAMAGE REPAIRED IAW SRM 57-50-3.Jan 7, 1999 · N944UP · Boeing 72722CSDR DL76G990040Skin · delaminatedTHE UPPER SKIN OF THE NR 3 SLAT T/E WEDGE WAS FOUND WITH A 6 X 13.5 DELAMINATED REPAIR. THE REPAIR WAS REMOVED, ALL DELAMINATION TO THE SKIN TRIMMED AWAY AND THEN REPAIRED PER B767 SRM 57-43-02. THE REPAIR WAS DOCUMENTED PER ER/A 366432-14.Jan 7, 1999 · N153DL · Boeing 7673P6SDR DL72L990039Skin · crackedNR 7 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.Jan 7, 1999 · N505DA · Boeing 727232SDR P2EA99025Rib · crackedSJO - LEADING EDGE FSS 594, NR 1 SLAT OUTBOARD MAIN TRACK, RIB CRACKED. DEFECT SIZE, LENGTH .0125 INCH. REPLACED RIB AT FSS 594 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Jan 6, 1999 · N209US · Boeing 737222SDR DL72S990031Bracket · crackedLTR CHK D-2 1/6/99, CRACK IN UPPER O/B RADIUS NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-20-21.Jan 6, 1999 · N484DA · Boeing 727232SDR DL72L990013Frame · crackedA .25 INCH VISIBLE CRACK LOWER FWD CORNER NR 5 FLAP ACT MOUNT BOX I/B FRAME. REPAIRED PER MM 57-20-21.Jan 4, 1999 · N510DA · Boeing 72723SDR 98FDEA00760Skin · damagedON WALKAROUND FOUND LT NR 1 L/E SLAT INBD FAIRING MISSING. ALSO, DAMAGE TO L/E SLAT ASSY. *S/D* REPLACED NR 1 L/E SLAT (LT) ASSY WITH FAIRING PER MM 27-80-01-4.Dec 22, 1998 · N320FE · Doug DC1030FSDR DL72W982645Rib · crackedFOUND DURING MV2/F-1 LETTER CHECK, .75 INCH CRACK AT NR 2 SLAT NOSE RIB O/B SIDE OF ACTUATOR AT AFT LWR CORNER. REPAIRED PER M/M 57-54-0.Dec 15, 1998 · N2807W · Boeing 727247SDR CALA9802176Rib · crackedINSPECTION FOUND A 4 INCH CRACK IN NR 2 SLAT RIB. THE RIB WAS REPLACED IAW MM 27-80-01, PAGE 402B AND 601 AND SRM 51-31-01.Dec 14, 1998 · N68047 · Doug DC1010SDR DL72S982549Rib · crackedLTR CHK B-1 12-11-98, NR 5 L/E SLAT I/B ACTUATOR NOSE RIB CRACKED. REPAIRED PER MM 57-54-0.Dec 11, 1998 · N404DA · Boeing 727232SDR P2EA98279Bolt · looseMDW - FLT 418 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. AT FLAPS 1 RECEIVED UNCOMMANDED ROLL. POST FLIGHT REVEALS LOOSE, LEADING EDGE SLAT. FOUND NR 4 SLAT, INBOARD AUX TRACK ADJUSTMENT BOLT LOOSE. REPLACED BUSHING AND TIGHTENED BOLT PER MM 27-81-21, SLADec 9, 1998 · N620PC · Boeing 737244SDR EISA98309Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 8 SLAT WAS FOUND CRACKED AT MOST OUTBOARD RIB. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-3. (M)Dec 9, 1998 · N275WC · Boeing 727277SDR CALA9802156Stiffener · corrodedINSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.Dec 9, 1998 · N17407 · Boeing 727243SDR EISA98312Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 2 SLAT WAS DISCOVERED CRACKED AT THIRD RIB FROM INBOARD END. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)Dec 8, 1998 · N275WC · Boeing 727277SDR EISA98311Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 3 SLAT WAS FOUND CRACKED AT 2ND AND 7TH RIBS FROM OUTBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)Dec 8, 1998 · N275WC · Boeing 727277SDR EISA98310Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 5 SLAT WAS FOUND CRACKED AT NR 5 AND NR 9 RIBS FROM INBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 51-50-2 AND INSTALLED PER SRM 57-20-3. (M)Dec 8, 1998 · N275WC · Boeing 727277SDR TWAA9819808Rib · crackedDURING OP 15 MAINT CHECK, FOUND A 4 INCH CRACK IN LT WING L/E BULLNOSE RIB, I/B END OF NR 4 SLAT ACTUATOR, LT WING STA 565. INSTALLED NEW RIB (P/N 114T2512-7). INSTALLED WITH RIVETS AND HI-LOKS.Dec 7, 1998 · N606TW · Boeing 767231SDR 98UAL900593Slat · damagedLEADING EDGE SLAT NR 6 DID NOT RETRACT. VERIFIED FULL DOWN BY VISUAL CHECK. POSSIBLE BIRD STRIKE ON DEPARTURE FROM SMF. DIVERTED TO SFO. *S/D* SLAT DAMAGED BY BIRD STRIKE. REPLACED NR 6 SLAT, SYSTEM OPERATIONALLY CHECKED OK.Dec 5, 1998 · N7264U · Boeing 727222
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