JASC 5744
Service difficulty reports · 2,731
Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 = '5744' 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.
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 = '5744' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AU000321Hinge · corroded(AUS) RT AILERON INBOARD HINGE CORRODED.SDR UPS00231979Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.SDR UPS00231978Hinge · corrodedINSPECTION TYPE:C, CORROSION (C57-581-01.00-01) ON LOWER SURFACE OF LEFT O/B AILERON O/B HINGE FITTING AROUND FASTENER HOLES. REMOVED AND REPLACED HINGE PER SRM 51-30-2.SDR 00FDEA00125Hinge · crackedLEFT WING OTBD ATTACH FITTING (HINGE HALF) FOR THE INBD AILERON IS CRACKED. REMOVED AND REPLACED PER IAW SRM 51 -30-2.SDR CA000203014Hinge · cracked(CAN) DURING SCHEDULED MAINTENANCE, THE AILERON OUTBOARD HINGE MOUNTING BRACKET WAS FOUND CRACKED HALF WAY THROUGH THE CENTER LUG.SDR TWAA9916006Fitting · crackedDURING OP 16 MAINT CHECK, THE RT WING I/B FLAP HINGE CASTING AREA XRS 164, I/B LOWER HOLE IN REAR SPAR HAD 2 CRACKS APPROXIMATELY 1.25 AND .5 INCH LONG. CRACKS WERE STOP DRILLED AND NDT CHECKED FOR CRACK CONTAINMENT. DOUBLERS WERE INSTALLED PER DOUGLAS DRAWISDR TWAA9916005Fitting · crackedDURING OP 16 MAINT CHECK ON RT WING THE I/B FLAP HINGE CASTING AREA XRS 164 HAD LOWER O/B HOLE CRACKED AT 12 O'CLOCK POSITION. CRACK WAS STOP DRILLED AND NDT CHECKED FOR CRACK CONTAINMENT. DOUBLERS INSTALLED PER DOUGLAS DRAWING JO 60271.SDR ABXA9900683Hinge · crackedDURING C-CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING CRACKED AT SPAR MOUNT HOLE. REPLACED HINGE IAW DACO DWG 5910515.SDR ABXA9900554Fitting · corrodedDURING C-CHECK, FOUND LEFT WING SPOILER OUTBOARD ATTACH FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR UPS99229688Fitting · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 2 FLAP TRACK FWD ATTACH WING FITTING. REWORK OUT OF LIMITS PER BOEING DWG 65-32733. REPLACED WITH NEW ITEM.SDR TWAA9907510Casting · crackedDURING OP 16 MAINT CHECK, FOUND LT WING REAR SPAR I/B FLAP ATTACH CASTING HAD CRACK INDICATION AT LOWER O/B HOLE AT 8 O'CLOCK AND LOWER I/B HOLE AT 5:30 AND 6:00 O'CLOCK POSITIONS. REPAIRED PER MC8-AD-34 AND DRAWING JO60271M.SDR UPS99229626Hinge · crackedINSPECTION TYPE:C, RIGHT O/B AILERON HINGE CASTING CRACKED AT WS 68605 APPROX (I/B CASTING I/B BALANCE BAY). REPLACED CASTING IAW DRG 65-19260.SDR TWAA9906902Casting · crackedDURING OP 16 MAINT CHECK, FOUND RT WING T/E REAR SPAR CENTER FLAP ATTACH CASTING HOLES LINER O/B HOLE AT 6 O'CLOCK POSITION WITH CRACK INDICATION. FIFTEEN PERCENT THICKNESS GROUND OUT AND CRACK WAS GONE. REPAIRED REAR SPAR AREA PER DOUGLAS SERVICE REWORK DRASDR CA990420032Lug · cracked(CAN) FLIGHT CREW REPORTED .8 DEGREES RIGHT WING DOWN REQUIRED. INITIAL REWORK OF LE FLAP DID NOT CORRECT PROBLEM. FURTHER INVESTIGATION REVEALED EXCESSIVE BACKLASH IN THE LT AILERON. EXAMINATION OF AILERON ATTACHMENT POINTS REVEALED CRACKING AND SEPARATIONSDR UPS99829569Fitting · crackedINSPECTION TYPE:C2, RT WING FLAP HINGE SUPPORT FITTING I/B SIDE GAVE CRACK INDICATION. REPLACED BRACKET.SDR AALA990376Casting · corrodedTUL - INBOARD AILERON QUAD MOUNT CASTING CORRODED ON CASTING AND AROUND BEARING BORES. REMOVED AND REPLACED CORRODED CASTING PER SRM 51-10-1 PAGE 4. (M)SDR UPS99228757Fitting · corrodedINSPECTION TYPE-C, NR 4 FLAP TRACK FORWARD MOUNT FITTING HAS CORROSION IN MOUNT HOLE BORES. NR 4 FLAP TRACK FITTING WAS REPLACED IAW OHM 20-50-01 PG 1 PARA 2 AND TABLE 1 AND M/M 27-51-31 PARA D8, ON NRC 879844.SDR CALA9900173Fitting · brokenINSPECTION FOUND RT O/B AILERON TAB SUPPORT FITTING (SECOND FROM O/B END) BROKEN OFF INSIDE AILERON. THE TAB SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-2.SDR 99ZZZX936Flap Track · wornFOUND BOTH LT AND RT INBOARD FLAP TRACK WORN BY FLAP ROLLERS INTO SIDE OF TRACK. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED. FOURTH PAIR OF TRACKS IN LAST 5 INSPECTIONS (3 MONTHS) 2 PAIR WERE REPAIRABLE, THE OTHERS WERE REPLACED. THE 5TH HAD LESS THANSDR 99ZZZX935Flap Track · wornFOUND BOTH LT AND RT INBOARD FLAP TRACK WORN BY FLAP ROLLERS INTO SIDE OF TRACK. CANNOT BE PROPERLY DETECTED WITH FLAP INSTALLED. FOURTH PAIR OF TRACKS IN LAST 5 INSPECTIONS (3 MONTHS) 2 PAIR WERE REPAIRABLE, THE OTHERS WERE REPLACED. THE 5TH HAD LESS THANSDR LR7A9841Fitting · crackedDURING ROUTINE MAINT, THE LT OWS 241 FLAP TRACK ATTACH FITTING WAS DISCOVERED CRACKED. REMOVED AND REPLACED FITTING IAW SMP 583 51-10 PARA G, AND 57-10-04.SDR DHL9872004DBracket · crackedAT D CHECK, RT WING TRAILING EDGE FALSE SPAR VERTICAL ATTACH BRACKED FOR THE NR 5 FLAP TRACK IS CRACKED. REPLACED BRACKET PER SRM 51-30-2 N/R 2891.SDR DHL9872033DFitting · crackedAT D CHECK, RT AILERON CENTER SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER MM 27-10-01, N/R 2830.SDR CALA9801979Fitting · corrodedINSPECTION FOUND NR 4 FLAP TRACK ATTACH FITTING CORRODED. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01862 AND MM 32-11-51.SDR DHL9880416CFitting · crackedAT D-CHECK, LEFT WING I/B FLAP HINGE SUPPORT FITTING AT STA 97. FOUND 2 CRACKS IN FWD AND DRIVE LINK ATTACHING HOLES. REAMED HOLES .0312 OVERSIZE. HFEC, OUT OF LIMITS. REPLACED FITTING PER SRM 51-1-21. N/R 679SDR AALA981543Bracket · corrodedTUL - FOUND CORROSION IN ONE OF ATTACH BORES TO WRAP AROUND PULLEY BRACKET (RT WING). ENLARGED BORE TO ACCEPT .030 INCH WALL SLEEVE BUSHING NOT EXCEEDING .4340. FABRICATED BUSHING AS PER DC10 SRM FOR SLAT ATTACH LUGS. INSTALLED BUSHING .4345. WET WITH PRIMSDR CALA9801413Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9801412Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9801411Bracket · crackedINSPECTION FOUND A 1 CRACK IN RT NR 5 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET AT UPPER OUTBOARD LEADING EDGE. THE MOUNT BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR P2EA98147Fitting · crackedSJO - C-CHECK ITEM - OUTBOARD SUPPORT FITTING RT WING SPOILER NR 5 CRACKED. DEFECT SIZE L = 2.5 INCHES. REPLACED NR 5 GROUND SPOILER OUTBOARD HINGE PER SRM 51-10-1 PAGE 5. FABRICATED FITTING PER COOPESA E.O. COO3-57-377-98 DATED DOCUMENTED ON FAA FORM 8110-SDR AU981210Fitting · cracked(AUS) LEFT WING DEFLECTION CONTROL SUPPORT FITTING LOWER ATTACHMENT LUG FRACTURED THROUGH THE BEARING HOUSING. FITTING IS LOCATED AT WS 906.20. PART TC: 41,421.SDR TWAA9812016Casting · crackedDURING OP 15 MAINT CHECK, FOUND 1 INCH CRACK ON RT WING T/E FLAP O/B HINGE CASTING, O/B UPPER ATTACH FLANGE. REPLACED CRACKED FRAME WITH PART NR 165489. INSTALLED FASTENERS PER SRM 51-30-2.SDR TWAA9812015Casting · crackedDURING OP 15 MAINT CHECK, FOUND CRACK ON RT WING T/E FLAP O/B HINGE CASTING, I/B UPPER ATTACH FRAME. REPLACED CRACKED FRAME WITH NEW FRAME AND INSTALLED FASTENERS PER SRM 51-30-2.SDR TWAA9810613Casting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING, THE CENTER AND INBD FWD FLAP HINGE CASTING HAD BADLY PITTED MOUNT HOLES. INSTALLED NEW FLAP HINGE CASTING PER MM 57-40-01, PG 201 TO PG 205. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR B4MR98040Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND NR 13 SPOILER ACTUATOR / FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 546. REMOVED AND REPLACED BRACKET IAW AIA EDR NR B205594 AND B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57-581-03. NON-ROUTINE TASDR B4MR98031Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND NR 3 SPOILER ACTUATOR/FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 515. REMOVED AND REPLACED BRACKET IAW AIA EDR NR B2-05594 AND IAW B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57-581-03. NON-ROUTINESDR AALA981171Bracket · corrodedTUL - CORROSION IN 2 EACH BOLT HOLES AND ON FACE OF OUTBOARD FLAP, OUTBOARD HINGE BRACKET SIDE LOAD SUPPORT BOSS. RE-WORKED OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD SUPPORT BOSS BORES PER CMM 57-44-09 AND ESO'S 7327 AND 7349 DATED 6-10-98. TST: 96,680.24 HOURSSDR 98ZZZX2557Mount · crackedCRACK IN AIRFRAME ACROSS AREA WHERE FLAP HINGE BRACKET BOLTS ON. FOUND ON RT WING, OUTBOARD FLAP SEGMENT, INBOARD MOUNT. CRACK VISABLE WITH NAKED EYE. CRACK 1.25 INCHES LONG, BOTH DOUBLER AND SKIN. TOTAL TIME AIRFRAME: APPROXIMATELY 6,805.4 HOURS.SDR DL72S981112Fitting · corrodedNR 4 FLAP TRACK FWD ATTACH FITTING LARGE HOLE HAS CORROSION IN HOLE. REPAIRED PER M/M 57-42-0.SDR AU980555Screw · improper part(AUS) INCORRECT HARDWARE WAS USED TO FIT THE AILERONS TO THE AIRCRAFT FOLLOWING PAINTING. INCORRECT TYPE P/N AN526C1032R SCREWS WERE USED INSTEAD OF THE CORRECT P/N MS20365-1-10 SCREWS. UNAPPROVED PART.SDR C2XA98IA157Fitting · elongatedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 5 LUG FITTING FOR FLAP HINGE, FASTENER HOLE ELONGATED. MAINTENANCE REPAIRED THE WING LUG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5750-01112. THE AIRCRAFT WAS APPROVED FOR RSDR UPS98826820Fitting · crackedINSPECTION TYPE-C, LT WING NR 4 FLAP HINGE ACTUATOR MOUNT FITTING IS CRACKED. REMOVED AND REPLACED CANOE FITTING IAW MM 27-51-00.SDR RAAA98B1034Fitting · crackedDURING SCHEDULED C1 CHECK PER CARD C-22004, FOUND RT WS 440 NR 11 SPOILER INBD DOWN STOP FITTING CRACKED AT STOP PAD. REPLACED FITTING PER SRM 51-10-1. M-54 NR 132.SDR RAAA98B1029Fitting · crackedDURING SCHEDULED C1 CHECK PER CARD C-22004, FOUND RT WS 343 NR 10 SPOILER CENTER HINGE BEARING FITTING CRACKED APPROX .75 INCH AT UPPER OUTBD MOUNT BOLT HOLE. REPLACED FITTING PER SRM 51-10-1, PG 4 AND 51-30-2, PG 8 AND 14. M-54 NR 130.SDR UPS98826819Fitting · crackedINSPECTION TYPE-C, THE RT WING FLAP HINGE SUPPORT FITTING AT STA XF 409.6673, INBOARD SIDE HAS A CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR CA980525009Hinge · loose(CAN) DURING INSPECTION OF LEFT ELEVATOR OUTBOARD HINGE PIN BRACKET, A LIGHT BLACK STAIN WAS NOTED ALONG THE INBOARD EDGE. BORESCOPE INSPECTION OF INTERNAL STRUCTURE FOUND THAT TWO RIVETS THAT ATTACH THE FITTING TO THE REAR SPAR WERE LOOSE.SDR TWAA9807702Hinge Fitting · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING EYEBROW CRACK INDICATION AT LOWER OUTBOARD MOUNT HOLE FOR FLAP IDLER HINGE. INSTALLED REPAIR PER ROD SKETCH 95-12-06-18, AND ARA 10991. (M)SDR TWAA9806414Casting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE REAR SPAR NR 2 FLAP HINGE CASTING, UPPER INBD AND OTBD MOUNT HOLES WITH CORROSION ABOVE HOLES. REMOVED CORROSION. STOP DRILLED CRACK WITH .25 INCH. INSTALLED FILLER IN BLENDED OUT AREA. INSTALLED DOUBLSDR TWAA9807312Block · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INSIDE FLAP OUTBOARD FLAP HINGE TO FORWARD MOUNT BOLT, RT AND LT SIDE MOUNT WEBS CRACKED OUT FROM BOLT HOLES. REPLACED MOUNT BLOCK PER STANDARD PRACTICES AND SRM 51-01. (M)SDR AALA980723Post · corrodedTUL - RIGHT INBOARD FLAP TRACK NR 1 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5. REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED/PAINTED, SRM 51-21-01, VOL II. TST: 91,033.07 HOURS. CYCLES: 18,
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