JASC 5753

Service difficulty reports · 31,515

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 2006UALA00541Track · separatedLEFT OUTBOARD FLAP DEFLECTION CONTROL TRACK HAS SEPARATED AT FWD END.Feb 21, 2006 · N644UA · Boeing 767322SDR UIEA200600007Support · crackedLEFT WING O/B MIDFLAP COVE PANEL CRACKED 18 INCHES LONG AT 3RD SUPPORT ARM I/B OF NR 1 CANOE.Feb 21, 2006 · N505MC · Boeing 7472D3BSDR UIEA200600009Support · crackedRIGHT WING OB MID FLAP COVE PANEL CRACKED AT 4TH SUPPORT ARM IB OB #8 CANOE APPROX 18" LONGFeb 21, 2006 · N505MC · Boeing 7472D3BSDR 06FDEA0802Hinge Fitting · crackedRT WING, OB FLAP IB HINGE FITTING AT MOST OB LOWER BOLT HOLE FOUND WITH CRACK INDICATION. REPLACED AS PER AMM 27-50-30-4. OTBD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.Feb 21, 2006 · N585FE · Doug MD11SDR UIEA200600008Panel · crackedL/W IB MIDFLAP COVE PANEL CRACKED AT PREVIOUS REPAIR- 4TH SUPPORT ARM FROM OB END.Feb 21, 2006 · N505MC · Boeing 7472D3BSDR SWAA060598Flap · delaminatedDURING SCHEDULED C3 CHECK, FOUND LH WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. R&R FLAP PER MM.Feb 20, 2006 · N301SW · Boeing 7373H4SDR 06FDEA0774Hinge · crackedLEFT HAND WING, OUTBOARD FLAP INBOARD HINGE AT MOST OUTBOARD LOWER BOLT HOLE FOUND WITH CRACK INDICATION. COMPLIED WITH FEDEX EA 1-5750-94604.Feb 20, 2006 · N585FE · Doug MD11SDR ASAA0640185Skin · puncturedTHE RT INBD MIDFLAP T/E IS PUNCTURED ON THE LWR SURFACE. REMOVED DAMAGED AREAS OF LWR SKIN FABRICATED AND INSTALLED TWO FILLERS AND TWO DOUBLERS IAW SRM 51 70 10 PARA 7 8 12 15 AND 20.Feb 19, 2006 · N755AS · Boeing 7374Q8SDR DHL2006760531Spar · crackedFOUND LT INBD MID-FLAP, REAR SPAR AT WBL 124, JUST BELOW INB AFT FLAP ACTUATION DRUM HAS CRACK. REMOVED DAMAGED AREA DIM.47" BY 2.25" ON L/H INBD MID FLAP LOWER, AND FAB NEW PART, MAT. BAC 1517-1367-6511, EXTRUSION, DIM 47" BY 2.25" IAW B727 SRM 57-50-1 AND IFeb 18, 2006 · N760AT · Boeing 7272B7SDR SWAA060575Skin · delaminatedDURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REPAIRED AFT FLAP PER SRM.Feb 18, 2006 · N680AA · Boeing 7373A4SDR 06FDEA0707Hinge Fitting · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING (ARC1991) OUTBOARD NR 3 BOLT HOLE FOUND CORROSION.Feb 17, 2006 · N615FE · Doug MD11SDR 06FDEA0706Hinge Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING AFT STRUT (ARC2128) FORWARD BOLT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FITTING AFT STRUT (ARC2128) FORWARD BOLT HOLE AS PER FEDEX EA 1-5750-90760.Feb 17, 2006 · N615FE · Doug MD11SDR SWAA060559Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Feb 16, 2006 · N653SW · Boeing 7373H4SDR 75883Safety Switch · failedAFTER TAKEOFF, CREW COULD NOT RETRACT THE FLAPS. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE THEN REMOVED AND REPLACED RIGHT FLAP SAFETY SWITCH. THE FLIGHT WAS A REPOSTION FROM ICT TO MCI, NO PAX ON BOARD.Feb 16, 2006 · N138YV · Beech 1900DSDR 06FDEA0687Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT, (ARC2126) AFT BOLT HOLE FOUND CORROSION.Feb 15, 2006 · N615FE · Doug MD11SDR 06FDEA0686Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT, (ARC2126) FORWARD BOLT HOLE FOUND CORROSION.Feb 15, 2006 · N615FE · Doug MD11SDR 06FDEA0674Flap Track · corrodedLEFT WING, NR 3 FLAP TRACK IS CORRODED AT THE SPOILER BEAM MOUNT AND THE MAIN MOUNT PADS. *S/D* REMOVED AND REPLACED CORRODED LT WING NR 3 FLAP TRACK IAW CARD 27X5705-01 AND CARD 27X5705-03.Feb 13, 2006 · N488FE · Boeing 727200SDR 06FDEA0655Flap Track · crackedRIGHT WING NR 6 FLAP TRACK CORRODED AT SPOILER BEAM PAD, MAIN MOUNTING PAD AND CRACKS EMMITTING FROM FAILSAFE BOLT HOLE. *S/D* REMOVED & REPLACED NR 6 FLAP TRACK PER FED EX CARD 27X5708-01 & 27X5708-03.Feb 13, 2006 · N488FE · Boeing 727200SDR 06FDEA0654Flap Track · corrodedNR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REPLACED PER CARD 27X5706-03.Feb 13, 2006 · N488FE · Boeing 727200SDR UPS06446217Panel · debondedINSPECTION TYPE:C RIGHT WING O/B AFT FLAP TOP PNL 688KT AFT EDGE MIDWAY AREA DEBONDED. DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.Feb 11, 2006 · N522UP · Boeing 747200SDR DJFA2006195Bolt · shearedDURING A SCHEDULED MAINTENANCE VISIT WHILE REMOVING THE FLAP ASSEMBLIES TO CONDUCT AN -A- LEVEL INSPECTION, IT WAS DISCOVERED THAT THE LEFT FLAP ACTUATOR MOUNTING BRACKET HAD A BOLT THAT WAS SHEARED OFF. THE BOLT WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TOFeb 11, 2006 · N457CW · Beech 400ASDR AWXA200600518Skin · crackedGYR - DURING C10 CHECK DISCOVERED THE LT OUTBOARD TRAILING EDGE FLAP HAD HAIRLINE CRACKS IN THE END POTTING COMPOUND. MAINTENANCE CLEANED AREA ON THE LT OUTBOARD TRAILING EDGE FLAP IAW AWA ER NR 19-2750-06075-RC1. FILLED INBOARD AND OUTBOARD EDGES ON THE LT Feb 10, 2006 · N906AW · Boeing 7572S7SDR 2006FA0000244Flap · crackedAIRCRAFT CAME IN FOR AN ANNUAL INSPECTION, DAMAGE TO THE FLAPS WERE FOUND DURING ROUTINE INSPECTION PROCESS. RT FLAP HAD CRACKS RADIATING OUT FROM RIVETS ON LOWER T/E SKIN, PLUS CRACKS RADIATING OUT FROM L/E SKIN, ON BOTTOM OF FLAP, IB OF MOUNTING BRACKET. DFeb 10, 2006 · N3533U · Cessna 172SSDR ASAA0640219Support · chafedRT OB FLAP I B ROLLER SUPPORT CHAFING. RT OB FLAP IB ROLLER SUPPORT REPLACED WITH NEW ONE IAW SRM 51 40 02 PARA 7A.Feb 10, 2006 · N799AS · Boeing 737490SDR 2006FA0000397Flap · damagedON DEC 4, 2005, THE RT FLAP JAMMED AT THE IB ATTACH ARMS IN ABOUT THE 20 DEGREE POSITION. FLAP MOTOR CONTINUED TO RUN FOR A SHORT PERIOD OF TIME, CAUSING SEVERE DAMAGE AND DISTORTION TO THE JAMMED FLAP, THE PILOT WAS ABLE TO LAND THE AIRPLANE WITHOUT FURTHERFeb 9, 2006 · N5464N · Cessna T182SDR QXEA200600504Arm · wornYYC - C3 LEFT HAND WING OUTBOARD FLAP, SIDE GUIDE ROLLER ARM AT FUSELAGE STATION 168.00, WORN ON ARM SECTION. REPAIRED IAW HORIZON AIR EA R-57-140, REO 670-57-53-035.Feb 9, 2006 · N607QX · Cndair CL6002C10SDR UPS06446216Panel · dentedINSPECTION TYPE:C RIGHT WING - I/B AFT FLAP UPPER O/B FLAP PANEL 678IT FOUND DENT MARK AT LOWER SURFACE. DENT AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-22 FIG 3.Feb 9, 2006 · N522UP · Boeing 747200SDR SWAA060512Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Feb 9, 2006 · N658SW · Boeing 7373L9SDR 06FDEA0609Stop Fitting · crackedSNRM N0754: RIGHT HAND WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED.Feb 9, 2006 · N615FE · Doug MD11SDR UPS06446322Support · crackedINSPECTION TYPE:C RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT O/B AREA CRACKED, CRACK LENGTH 12 INCHES. RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 3.Feb 8, 2006 · N522UP · Boeing 747200SDR UPS06446306Access Panel · corrodedL/W O/B AFT FLAP ACCESS PANEL NR 588KT AFT SUPPORT I/B AREA CORROSION CRACK REVEALED. CORROSION BLEND OUT 0.055" BY 1" BY 3" EXCEED SRM 57-50-01 FIG 3. LIMIT AFT SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 4 AND HFEC INSP C/OUT AS PER NTM PART6 51-00-0 FIG 4. Feb 8, 2006 · N522UP · Boeing 747200SDR UPS06446294Flap Track · chafedO/B MID FLAP I/B SLIDE TRACK I/B WEB AFT AREA DEEP CHAFING REVEALED. RHW O/B MID FLAP O/B SLIDE TRACK I/B WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Feb 8, 2006 · N522UP · Boeing 747200SDR AWXA200600338Skin · debondedMCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT OUTBOARD AFT FLAP AT THE INBOARD END, FROM WS 230.68L TO WS 239.68L. MAINTENANCE REMOVED DISBOND AREA FROM THE LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2RFeb 8, 2006 · N173AW · Boeing 73733ASDR ASAA0640135Support · chafedRT OUTBD FLAP INBD ROLLER SUPPORT CHAFING. RT OUTBD FLAP INBD ROLLER SUPPORT REPLACED WITH NEW PART PER SRM 51 40 02 PARA A7A.Feb 8, 2006 · N799AS · Boeing 737490SDR ASAA0640150Skin · debondedREPAIR ON UPPER SURFACE OF RT IB TE FLAP IS DISBONDED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51 70 10.Feb 8, 2006 · N769AS · Boeing 7374Q8SDR ASAA0640149Skin · dentedLT IB FORE FLAP DENTED 5 INCHES FROM TE AND 15 INCHES FROM IB END ON LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51 70 10.Feb 8, 2006 · N769AS · Boeing 7374Q8SDR DHL2006753516Skin · delaminatedFOUND LEFT O/B FOREFLAP CTR T/E IS DELAMINATED AT WBL 400. CUT OUT DELAMINATED AREA ON LEFT O/B FOREFLAP, LWR SURFACE, APPROX 2" X 5". REMOVED CORRODED CORE, APPROX 2" X 5", FABRICATED FILLER APPROX 2" X 5" AND DOUBLER APPROX 3.5" X 8" FROM 2024-T3 .016 PO 9Feb 7, 2006 · N753DH · Boeing 727223SDR UPS06446218Panel · debondedINSPECTION TYPE:C RIGHT WING - I/B AFT FLAP I/B LWR FIXED PANEL FOUND DEBOND AT PANEL I/B PORTION (AFTER PANEL REMOVAL). DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.Feb 7, 2006 · N522UP · Boeing 747200SDR AWXA200600337Skin · debondedMCN - DURING C22 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT OUTBOARD FORE FLAP, 93 INCHES FROM THE INBOARD END, FROM WS 290.69L TO WS 296.69L. MAINTENANCE REMOVED DISBOND AREA FROM THE LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2RFeb 7, 2006 · N173AW · Boeing 73733ASDR AWXA200600336Skin · debondedMCN - DURING C22 CHECK DISCOVERED DISBOND ARE ON THE LOWER SURFACE OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, 32 INCHES FROM THE INBOARD END, FROM WS 101.75R TO WS 109.25R. MAINTENANCE REMOVED DISBOND AREA FROM THE RT INBOARD MID FLAP IAW BOEING 737-300 Feb 7, 2006 · N173AW · Boeing 73733ASDR 06FDEA0571Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON LT INBOARD FOREFLAP LEADING EDGE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-4 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERFeb 7, 2006 · N487FE · Boeing 727200SDR DHL2006753515Skin · delaminatedFOUND LEFT O/B FOREFLAP O/B END LOWER SURFACE WBL 485 IS DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIRS ON LEFT O/B FLAP, APPROX 4" X 4" AND 4.5" X 5". FABRICATED FILLERS 4.5" X 5" AND 4" X 4" AND DOUBLERS 6.5" X 6.5" AND 5.5 X 5.5" FROM 2024-T3 .016 PO 9Feb 6, 2006 · N753DH · Boeing 727223SDR UPS06446373Support Tube · corrodedRHW I/B FORE FLAP I/B LEVER SUPPORT TUBE FOUND CORRODED AT FWD FACE INSIDE THE FORE FLAP, EXFOLIATION CORROSION. SUPPORT TUBE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 6, 2006 · N522UP · Boeing 747200SDR AWXA200600228Skin · crackedPHX - DURING INSPECTION DISCOVERED RT OUTBOARD MID-FLAP LEADING EDGE SKIN CRACKED, JUST INBOARD OF CARRIAGE, ON THE EDGE OF CUTOUT. NO CRACKS ARE ALLOWED PER BOEING 737-300 SRM 57-53-01. MAINTENANCE BLENDED CRACK OUT ON MID FLAP. FABRICATED FILLER AND DOUBLFeb 6, 2006 · N154AW · Boeing 7373G7SDR 06FDEA0545Skin · crackedRT WING OUTBOARD FLAP CRACK 1,5" LONG AND NR 20 FASTENERS U/S ON UPPER SKIN AT STA XOF 542. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 85 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163355/N00355 AND IAW SRM 57-10-00 FIG 85 VOL 1.Feb 6, 2006 · N68056 · Doug DC1010SDR 06FDEA0543Skin · damagedRIGHT WING LOWER SURFACE OUTBOARD FLAP FOUND REPAIR AT TRAILING EDGE SECTION AT APPROX STA XOS 470. SCRAPED DOUBLER OF EXISTING EA REMOVED DAMAGED SECTION OF SKIN AND REPAIRED IAW SRM 57-10-00 FIG 7 SHT 3 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER F163850Feb 6, 2006 · N68056 · Doug DC1010SDR SWAA060451Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Feb 6, 2006 · N397SW · Boeing 7373H4SDR SWAA060450Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RIGHT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Feb 6, 2006 · N397SW · Boeing 7373H4SDR QXEA200600436Skin · chafedPDX - OUTBOARD FLAP UPPER SURFACE CHAFED ON PLATE BETWEEN STA YW194.0 AND YW263.019. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05, TASK 57-52-30-320-801. NDTM PART 6, 51-00-02, NDTM PART 1, 51-00-04, HORIZON EA 6-57-340, TASK 51-18-00-800-808, SRM 51-25-10, SRFeb 5, 2006 · N404QX · Bombdr DHC8402SDR UPS06446214Panel · chafedINSPECTION TYPE:C LHW, O/B AFT FLAP UPPER CENTER FLAP PANEL NR 588JT FOUND CHAFE MARKS. CHAFED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.Feb 4, 2006 · N522UP · Boeing 747200
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