JASC 5753

Service difficulty reports · 31,521

Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753'
  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 DHL2005784507Skin · gougedLT WING INBD FORE FLAP OUTBD END IS GOUGED BY LONG SCREW, WBL 240. FOUND AREA OUT OF LIMITS. REPAIRED IAW SRM.May 16, 2005 · N784DH · Boeing 727227SDR ABXA050137Attach Bracket · crackedLEFT INBOARD FLAP HINGE ATTACH BRACKET CRACKED IN TWO PLACES INSIDE FLAP. MOVED AND REPLACED LEFT INBOARD FLAP HINGE ATTACH BRACKET IAW DC-9 DWG 5914872.May 16, 2005 · N909AX · Doug DC932FSDR ASAA0580259Skin · gougedOKC - DURING C-CHECK, RIGHT WING INBOARD FLAP GOUGED OUTBOARD OF BUTT JOINT BOTTOM SURFACE. REMOVED DAMAGE, AND INSTALLED DOUBLER IN FLAP SKIN. (M)May 15, 2005 · N974AS · Doug DC983SDR DHL2005784504Skin · delaminatedLT INBD FORE FLAP IS DELAMINATED ON LOWER SURFACE, WBL 124. REMOVED LT I/B FORE FLAP IAW B727 MM 27-51-00. CUT OUT DELAMINATED AREA AND FABBED FILLER 2 INCH DIA AND DOUBLER AND BONDED REPAIR PARTS IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 3. REINSTALLED LMay 15, 2005 · N784DH · Boeing 727227SDR SWAA051415Wedge · delaminatedDURING SCHEDULED RON CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED MIDFLAP T/E WEDGE PER MM.May 15, 2005 · N504SW · Boeing 7375H4SDR 05FDEA01266Skin · damagedRT WING, INBD FLAP, EXTERIOR UPPER SURFACE MOST UPPER ABOUT 20 INCHES FROM INBD TO OUTBD, FOUND 1 EACH EXISTING REPAIR DOUBLER.May 13, 2005 · N576FE · Doug MD11SDR 05FDEA01248Flap Track · gougedRIGHT WING NR 5 FLAP TRACK OUTBOARD ROLLER TRACK HAS GOUGES IN BEND RADIUS OF TRACK. COMPLIED WITH EA 6-5720-88814 PT 1 AND RAS/DABRE/7005151/2005.May 12, 2005 · N403FE · Airbus A310203SDR SWAA051378Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.May 11, 2005 · N696SW · Boeing 7373T5SDR DHL2005741591Skin · delaminatedRT I/B FOREFLAP AT I/B HAS DELAMINATED AT CHAFE STRIP. REMOVED CHAFE STRIP ON UPPER IB SURFACE. CUT OUT DELAMINATED AREA AND EXTERNAL DOUBLER FROM 2024T3 .016 PO9001660. CLEANED, PREPPED, APPLIED PRIMER AND ADHESIVE TO REPAIR PARTS AND SURFACE. VACUUM BAGGEMay 7, 2005 · N741DH · Boeing 7272Q9SDR 05FDEA01220Skin · damagedDURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119.May 6, 2005 · N802FD · Airbus A310324SDR 05FDEA01218Flap · damagedDURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120.May 6, 2005 · N802FD · Airbus A310324SDR 05FDEA01215Fitting · crackedRIGHT WING O/B FLAP SECOND FLAP VANE TRACK FROM I/B UP-STOP FITTING FOUND CRACKED. CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01VOL II. CLASSIFIED AS MAJOR REPAIR PER GMM 6-1-100.May 6, 2005 · N576FE · Doug MD11SDR CA050505001Hinge · cracked(CAN) DURING A SCHEDULED INSPECTION, A CRACK WAS DETECTED VISUALLY, IN THE AFT, INNER MACHINED RADIUS OF THE RT FLAP OUTER HINGE, P.N: 25WF4402. MPI NDT DETECTED A SECOND CRACK IN THE OPPOSITE, FORWARD RADIUS. BOTH CRACKS RUN APPROXIMATELY 5.5 INCHES IN LENGMay 5, 2005 · Braero BAE125800ASDR AWXA200500609Skin · debondedDURING C-6 CHECK, THE RT OUTBOARD, AFT FLAP WAS FOUND TO BE DISBONDED ON THE LOWER SURFACE, APPROXIMATELY 6.54 INCHES FROM INBOARD END. FURTHER INSPECTION FOUND WATER IN HONEYCOMB STRUCTURE. DUE TO WATER IN HONEYCOMB STRUCTURE, MAINTENANCE REMOVED AND REPLACMay 5, 2005 · N335AW · Boeing 7373U3SDR AWXA200500607Skin · debondedDURING C-6 CHECK, THE LT INBOARD FOREFLAP WAS FOUND TO BE DISBONDED ON THE UPPER SURFACE, 36 INCHES FROM OUTBOARD END, LT WBL 146.275 TO LT WBL 148.275. MAINTENANCE REPAIRED DISBONDED AREA IAW B737-300 SRM 51-70-10-0, FIGURE 31.May 5, 2005 · N335AW · Boeing 7373U3SDR QXEA200500859Skin · damagedYYC - LEFT WING INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ-700 SRM 51-26-00-001-001-A01, 57-52-01-101-001-A01 AND SRM 51-25-01-001-001-A01.May 5, 2005 · N611QX · Cndair CL6002C10SDR AWXA200500550Skin · delaminatedMCN - MAJOR REPAIR - DURING C-14 CHECK THE UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED 12 INCHES FROM THE INBOARD END BETWEEN WBL 84 AND WBL 86. MAINTENANCE CUT OUT DAMAGE IN UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP; FABRICATED May 5, 2005 · N322AW · Boeing 7373G7SDR 05FDEA01210Hinge · crackedRIGHT WING NR 8 FLAP TRACK FAIRING AFT I/B END IS CRACKED AND FWD FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2.May 5, 2005 · N254FE · Boeing 727200SDR 05FDEA01206Flap Track · corrodedNR 2 FLAP TRACK REAR SPAR ATTACH AREA IS CORRODED. REPLACED NR 2 FLAP TRACK ON FED EX CARD 27X5706-03.May 4, 2005 · N264FE · Boeing 727200SDR 05FDEA01205Flap Track · corrodedLEFT WING NR 3 FLAP TRACK CORRODED AT SPOILER BEAM PAD. REPLACED NR 3 FLAP TRACK ON FED EX CARD 27X5705-03May 4, 2005 · N264FE · Boeing 727200SDR DHL2005807511Skin · dentedRT INBOARD FLAP FWD LWR PLATING HAS TWO DENTS OF 6 AND 5 STA XW 43.000 - 50.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-18-05, EO AST 050403 DATED 04-12-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST 050403. PERMay 3, 2005 · N807DH · Doug DC873FSDR DHL2005807510Skin · damagedRT OUTBOARD FLAP INTERIM REPAIR ON FWD UPPER PLATING, STA XF 227.000. PERFORMED MAJOR REPAIR. REMOVED ALL FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED SECTION IAW EO AST-050405. PERFORMED DETAIL VISUAL INSP OF AREA, FABRICATED NEWMay 3, 2005 · N807DH · Doug DC873FSDR CA050503008Support Bracket · cracked(CAN) ACCOMPLISHMENT INSTRUCTIONS, FOUND FLAP ACTUATOR SUPPORT BRACKET CRACKED. SERVICE KIT SK208-158 ORDERED AOG, WILL BE INSTALLED UPON RECEIPT.May 2, 2005 · Cessna 208BSDR QXEA200500932Bracket · wornYYC - RIGHT WING, OUTBOARD FLAP, INBOARD SIDE ROLLER GUIDE BRACKET WORN. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND SRM 51-42-21-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500938Skin · damagedYYC - RIGHT WING INBOARD FLAP HAS ROCK CHIPS ON LOWER FLAP INNER AREA. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 57-52-01-101-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500853Fitting · damagedYYC - LEFT OUTBOARD FLAP INBOARD GUIDE ROLLER FITTING DAMAGE AT TRAILING EDGE WING STATION 138.98. REPAIRED IAW CRJ-700 SRM 57-51-02-201-001-A01, 51-42-06-001-001-A01 AND 51-41-21-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500855Skin · damagedYYC - LEFT WING OUTBAORD FLAP UPPER SURFACE HAS RUBBED MARK AT MID SECTION. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND 51-25-00-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500860Vane · chafedYYC - LEFT INBOARD FLAP VANE INBOARD LEADING EDGE ACCESS PANEL 584ET HAS CHAFE MARK. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 57-52-02-001-A01, 51-25-16-001-001-A01 AND SRM 51-21-11-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR ABXA050114Structure · corrodedRIGHT FLAP NR 2 TRAILING EDGE SECTION HAD BULGING RIVETS ON THE LOWER SURFACE AT THE OUTBOARD AFT CORNER. REPAIRED AREA IAW DC-9 SRM.May 2, 2005 · N946AX · Doug DC931SDR AWXA200500551Skin · delaminatedMCN - MAJOR REPAIR - DURING C-14 CHECK THE UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED BETWEEN WBL 136 AND WBL 154. MAINTENANCE CUTOUT DAMAGE IN UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP FROM WBL 141.274 TO 154.275; FABRICATED A May 1, 2005 · N322AW · Boeing 7373G7SDR MALA050412Flap · damagedDURING C1, C2 INSPECTION IN YYC FOUND RT OB LEADING EDGE OB OF NR 4 FLAP TRACK THERE IS A TEMP REPAIR IAW EOA57099.Apr 30, 2005 · N503XJ · Bac AVRO146RJ85ASDR A6WA200540162Channel · crackedLEFT OUTBOARD FLAP T/E PUSHED FORWARD, .375 INCH WIDE BY .0625 INCH DEEP. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE. REMOVED CRACKED CHANNEL P/N 601R14538-3 AND INSTALLED SERVICEABLE CHANNEL P[/N 601R14538-3, IAW CRJ 200 SRM 51-25-01, 51-42-06, 51-42-10 AND Apr 30, 2005 · N451AW · Cndair CL6002B19SDR SWAA051285Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING T/E INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Apr 29, 2005 · N621SW · Boeing 7373H4SDR 05FDEA01172Rib · damagedRT WING I/B FLAP ASSY FOUND NEW FLAP SEGMENT ASSY RIB DAMAGED. DAMAGED AREA TRIMMED. REPAIR DOUBLER & FILLER FABRICATED AND INSTALLED AS PER SRM 57-00-01 FIG. 7 VOL I AND 51-35- 01 VOL II. MINOR REPAIR PER GMM 6-2-100.Apr 28, 2005 · N576FE · Doug MD11SDR DHL2005807505Skin · dentedRIGHT INBOARD FLAP AFT LWR PLATING HAS SEVERAL DENTS (STA XW 4.000 - 91.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING AND FASTENERS WITHIN REPAIR AREA IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICApr 27, 2005 · N807DH · Doug DC873FSDR SWAA051252Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Apr 27, 2005 · N648SW · Boeing 7373H4SDR QXEA200500724Bearing · corrodedPDX - PITTING NOTED ON LEFHAND NR 5 FLAP TRACK, OUTBOARD BEARING SURFACE -E-. REPAIRED IAW DHC-8-200 AMM TRASK 27-51-11-830-802 AND RD 8-57-889.Apr 27, 2005 · N346PH · Dhav DHC8202SDR CA050510005Bracket · torn(CAN) ON TUESDAY, APRIL 26, 2005 THIS AIRCRAFT SUFFERED A RIGHT HAND OUTBOARD FLAP FAILURE WHILE APPROACHING CYWG. THE CREW WERE ABLE TO MAINTAIN CONTROL OF THE AIRCRAFT AND LANDED WITHOUT FURTHER INCIDENT.ON EXIT FROM THE AIRCRAFT, THE CREW OBSERVED NR 1, 2 AApr 26, 2005 · Beech 200BEECHSDR 05FDEA01126Strap · crackedLEFT HAND WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP FOUND CRACKED ARB0029-509N. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.Apr 26, 2005 · N608FE · Doug MD11SDR QXEA200500840Flap · chafedPDX - LEFTHAND FLAP HAS CHAFE BACK OF FLAP BY NR 2 FLAP VANE ACCESS PANEL. REPAIRED IAW CRJ700 SRM 51-21-16 AND HORIZON AIR EA R-57-106.Apr 26, 2005 · N607QX · Cndair CL6002C10SDR ASAA0580220Skin · gougedDURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)Apr 25, 2005 · N958AS · Doug DC983SDR ASAA0580219Skin · dentedDURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M)Apr 25, 2005 · N958AS · Doug DC983SDR ASAA0580217Skin · delaminatedFOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M)Apr 25, 2005 · N958AS · Doug DC983SDR SWAA051215Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Apr 25, 2005 · N509SW · Boeing 7375H4SDR QXEA200500728Roller · corrodedPDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-C. REPAIRED IAW RD 8-57-988.Apr 20, 2005 · N346PH · Dhav DHC8202SDR QXEA200500727Roller · corrodedPDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-B. REPAIRED IAW RD 8-57-988.Apr 20, 2005 · N346PH · Dhav DHC8202SDR QXEA200500726Roller · corrodedPDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACE HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-D. REPAIRED IAW RD 8-57-988.Apr 20, 2005 · N346PH · Dhav DHC8202SDR QXEA200500725Roller · corrodedPDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK E. REPAIRED IAW RD 8-57-988.Apr 20, 2005 · N346PH · Dhav DHC8202SDR DHL2005741558Skin · chafedRT I/B FORFLAP CHAFED AT UPPER I/B END. REMOVED CHAFFED EXISTING DOUBLER FROM RT I/B FORE FLAP UPPER I/B END, CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGE IAW B727 SRM 57-50-1 FIG 3 57-50-2 FIG3 AND 51-40-20 FIGApr 19, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741506Skin · damagedIMPROPER REPAIR ON RT IB MID FLAP UPPER SURFACE WBL 100. REMOVED PREVIOUS REPAIR R/W I/B MID FLAP T/E WEDGE SURFACE AN CUTOUT DAMAGE AREA APPROX 4 1/4 INCH BY 9 1/4 INCH IAW B727 SRM 51-40-20 FIG 30. FABRICATED ONE SKIN REPLACEMENT APPROX 4 1/4" BY 9 1/4" AApr 19, 2005 · N741DH · Boeing 7272Q9
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