JASC 5753

Service difficulty reports · 31,513

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 SWIA201642705Skin · dentedDENT LOCATED APPROXIMATELY AT FLAP STATION 87.8 ON LT INBOARD FLAP LOWER CENTRAL AFT. PERFORMED THE REPAIR IAW SRM.Sep 26, 2016 · N752SK · Cndair CL6002C10SDR DALA2016092706887Skin · puncturedPUNCTURED LOWER SKIN ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING. DUE TO EXCESSIVE DAMAGE ON OUTER VANE GUIDE OF OTBD FLAP AT RT WING WAS REPLACED IAW IPC 27-50-04-01A.Sep 26, 2016 · N907DE · Doug MD88SDR ASOA201609240745Skin · dentedMCN DURING C CHECK INSPECTION, THE RT INBD FLAP IS DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV.THIS IS A MAJOR REPAIR. ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 24, 2016 · N710EV · Cndair CL6002C10SDR SWAA2016100308369Angle · crackedRT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED AT WBL 185. R&R ANGLE IAW SRM AND DWG.Sep 24, 2016 · N603SW · Boeing 7373H4SDR TSAA20161202039Skin · delaminatedRIGHT HAND INBOARD TRAILING EDGE AFT FLAP DELAMINATED ALONG AFT EDGE ON LOWER SURFACE. REPAIRED IAW SRM, REV 111, 51-70-10, REPAIR 4, PAGE 214, FIGURE 202, ITEM H.Sep 23, 2016 · N361NC · Boeing 737301SDR SWAA2016092708213Skin · crackedLEFT WING NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN IAW SRM.Sep 23, 2016 · N748SW · Boeing 7377H4SDR DALA2016092406823Skin · crackedDAMAGE TO CRACKED UPPER SKIN, FORWARD OTBD STUD AREA, AT LT OTBD FLAP MID GUIDE VANE. LEFT OTBD FLAP MID GUIDE VANE WAS REPAIRED BY ER/A 550294-14, REV ORIGINAL.Sep 23, 2016 · N906DE · Doug MD88SDR A6WA201644359Skin · dentedRIGHT INBOARD FLAP LOWER SKIN HAS DENT AT WS 74.0.Sep 23, 2016 · N421ZW · Cndair CL6002B19SDR FDEA201609223349Skin · dentedLEFT INBD AFT FLAP LOWER SURFACE HAS A DENT AT RIB 17. REPAIRED THE FLAP SKIN IAW SRM 57-50-00.Sep 22, 2016 · N653FE · Airbus A300F4605RSDR FDEA201609223346Rib · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND OUTER FLAP RIB 3 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0328395 PT1 MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223345Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.2 AND 2.3. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223344Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223343Stiffener · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 21 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328403 PT1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223342Stiffener · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223341Stiffener · crackedRIGHT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328403 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223340Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 19 UPPER STIFFENER CRACKED, BETWEEN STRINGERS 2.1 AND 2.2. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223339Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 27 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223338Stiffener · crackedLEFT WING CENTER FLAP TOP SKIN AND RIB FLANGE, FOUND FLAP RIB 17 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223337Stiffener · crackedLEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 26 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR FDEA201609223336Stiffener · crackedLEFT WING FLAPS INTERNAL STRUCTURE, FOUND CENTER FLAP RIB 11 UPPER STIFFENER CRACKED, BETWEEN STRINGER 2.1 AND REAR SPAR. REPAIRED IAW EA 6-5750-T0328396 PT1. MAJOR REPAIR IAW GMM 6-2-100.Sep 22, 2016 · N652FE · Airbus A300F4605RSDR DALA2016092206773Skin · wornINITIAL: WEAR ON OTBD EDGE UPPER SKIN OF OUTBD VANE GUIDE ON INBD FLAP AT RT WING. RT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007, CARD 2000-8149-02 AND SRM 57-03D, PARA 11, FIG 11.Sep 21, 2016 · N907DE · Doug MD88SDR IPXA2016092608669Skin · dentedINSPECTION TYPE:1C, LEFT WING CENTER FLAP OTBD LE DENTED OUT OF LIMITS. REPAIR IAW SRM 57-50-00 PARA 4H FIG 208(SHEET 2).Sep 20, 2016 · N159UP · Airbus A300F4622RSDR IPXA2016092708701Skin · dentedINSPECTION TYPE: 1C, LEFT WING CENTER FLAP OTBD LE SKIN DENTED OUT OF LIMITS. REPAIR IAW SRM 57-50-00 PARA 4H FIG 208 (SHEET 2).Sep 20, 2016 · N159UP · Airbus A300F4622RSDR FDEA201609203314Wedge · delaminatedRIGHT WING OTBD FLAP INBD TRAILING EDGE WEDGE DELAMINATED. WEDGE REPAIRED AND SMOOTHED AS PER SRM 57-50-80 REPAIR 1 PARA 4A1B. REFER TO WR1 57504399 FOR WORK DETAIL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 20, 2016 · N617FE · Doug MD11FSDR AALA201609299002Skin · chafedAIRCRAFT IN BASE MAINTENANCE. RIGHT HAND WING INBOARD AFT FLAP UPPER SKIN CHAFED BETWEEN RIB 1A-2. REPAIRED AFT FLAP UPPER SKIN PER EA 263550.Sep 19, 2016 · N945UW · Emb ERJ190100IGWSDR DALA2016092006734Doubler · wornINITIAL: CM WORN UPPER PREVIOUS DOUBLER REPAIR ON OUTBD GUIDE VANE INBD FLAP OUTBD SECTION AT LT WING. LT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW A/C 9007 CARD 2000-8149-01, JOB 000-0014 AND SRM 57-03D, PARA 11, FIGURE 11.Sep 19, 2016 · N907DE · Doug MD88SDR FDEA201609183307Hinge · corrodedRIGHT WING OTBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328400 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609183304Hinge · corrodedLEFT WING OTBD FLAP INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328382, PART 1, STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-1Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609183303Hinge · corrodedLEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609183302Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75300C P5, STEP 1A & STEP 1C. CLASSIFIED AS MAJOR IAW GMM 6-2Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609183301Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 2 & STEP 4. REPAIR CLASSIFIED AS MAJOR IAW GMM Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609183300Hinge · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-75312C PART 5 STEP 4 & STEP 4.Sep 18, 2016 · N617FE · Doug MD11FSDR FDEA201609163285Vane · puncturedRIGHT INBD FLAP VANE HAS PUNCTURE DAMAGE ON BOTTOM SIDE. REPAIRED IAW SRM 51-71-00, VOL II.Sep 16, 2016 · N562FE · Doug MD1010FSDR FDEA201609153266Skin · dentedLEFT INBD MAIN FLAP LOWER SURFACE APPX 10 INCHES FROM INBD EDGE AND 3 INCHES ABOVE T/E WEDGE DENTED. REPAIRED LT INBD MAIN FLAP LOWER SURFACE BY HOT-BONDING NEW CORE & DOUBLER IAW SRM 57-53-01, FIG 1 & SRM 51-70-10-2R. REPAIR NR 3 AND SRM 51-70-10-2R REPAIRSep 15, 2016 · N798FD · Boeing 757222SDR IPXA2016100408941Panel · corrodedINSPECTION TYPE: 3C, RT INBD FLAP HINGE FAIRING OB SIDE PANEL LANDING CORRODED BEYOND ALLOWABLE LIMTS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PANEL LANDING IAW DWG ARC2540 AND SRM 51-35-02.Sep 14, 2016 · N258UP · Doug MD11FSDR SWIA201642659Vane · chafedRIGHT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.Sep 14, 2016 · N956SW · Cndair CL6002B19SDR SWIA201642658Vane · chafedRIGHT INBOARD FLAP INBOARD VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.Sep 14, 2016 · N956SW · Cndair CL6002B19SDR SWIA201642657Vane · chafedRIGHT INBOARD FLAP CENTER VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.Sep 14, 2016 · N956SW · Cndair CL6002B19SDR 2016FA0000455Flap Track · brokenRIGHT FLAP OUTBOARD FLAP TRACK ASSEMBLY BROKEN. FLAPS WERE MOVED FROM 20 DEGREES TO FULL EXTENSION. MOMENTS UPON REACHING AND STOPPING AT FULL EXTENSION, A LOUD "BANG" WAS HEARD (APPROX 200FT AGL). PILOT LOOKED RIGHT AND SAW BROKEN PART PROTRUDING FROM WING. ASep 14, 2016 · N10100 · Cessna 182TSDR IPXA2016100609005Strap · corrodedINSPECTION TYPE:3C, LT INBD FLAP HINGE FAIRING IB SIDE SUPPORT STRAP CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT STRAP IAW DWG ARC2540 AND SRM 51-31-01.Sep 13, 2016 · N258UP · Doug MD11FSDR DALA2016091306601Skin · delaminatedAWR HIDDEN DAMAGE: DELAMINATION UPPER SKIN OF OTBD VANE GUIDE ON INBD FLAP AT RT WING. DAMAGE AREA WAS REPAIR IAW SRM 57-03D, P11, FIG 11 AND JIC OPN 1031.Sep 13, 2016 · N907DE · Doug MD88SDR TSAA20161115021Attach Bracket · corrodedRIGHT HAND INBOARD TRAILING EDGE FORE FLAP, CENTER ATTACH BRACKET, AFT BORE AND FACES FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CENTER ATTACH BRACKET IAW CMM 57-53-24, REVISION 51.Sep 12, 2016 · N361NC · Boeing 737301SDR IPXA2016092908759Skin · delaminatedINSPECTION TYPE:3C, LT IB FLAP VANE LOWER SURFACE AREA OF DELAM STA XIFH 197. REPAIRED NOTED DELAMINATION ON LT IB FLAP VANE PER SRM 57-50-80 REPAIR 2 FIG 201 (MAJOR)Sep 12, 2016 · N258UP · Doug MD11FSDR IPXA2016092908757Skin · chafedINSPECTION TYPE:3C, RT IB FLAP VANE UPPER SURFACE CHAFE DAMAGE STA XIFH267. REPAIRED NOTED CHAFE DAMAGE PER SRM 57-50-80 REPAIR 2 FIG 201 (MAJOR)Sep 12, 2016 · N258UP · Doug MD11FSDR A6WA201644320Skin · gougedRIGHT WING INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH GOUGES, PITTING AND DENTS FROM DEBRIS.Sep 11, 2016 · N414ZW · Cndair CL6002B19SDR A6WA201644321Skin · damagedLEFT WING INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH GOUGES PITTING AND DENTS FROM DEBRIS.Sep 11, 2016 · N414ZW · Cndair CL6002B19SDR SWIA201642648Vane · chafedRIGHT FLAP VANE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE OTBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19SDR SWIA201642647Vane · chafedRIGHT FLAP VANE CENTER OF LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CENTER LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19SDR SWIA201642646Vane · chafedRIGHT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE INBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19SDR SWIA201642645Vane · chafedLEFT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED LT FLAP VANE INBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19
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