JASC 5751

Service difficulty reports · 5,082

Reports filed under 5751 · Ailerons, 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 = '5751'
  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 SWIA201439829Skin · chafedRT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, BOTH SIDES OF OTBD HINGE. C-CHECK, BLENDED RT AILERON UPPER SKIN SHROUD IN 2EA LOCATIONS, BOTH SIDES OF OTBD HINGE IAW REO.Oct 18, 2014 · N866AS · Cndair CL6002B19SDR SWIA201439828Skin · chafedLEFT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, INBD OF INBD HINGE AND OTBD OF CENTER HINGE. C-CHECK, BLENDED THE LT AILERON UPPER SKIN SHROUD, 2EA, CHAFES, INBD OF INBD HINGE AND OT OTBD CENTER HINGE IAW REO.Oct 18, 2014 · N866AS · Cndair CL6002B19SDR SWIA201439810Skin · chafedRIGHT AILERON, L/E UNDER SHROUDS, CHAFED FROM WS 282.00- WS 353.00. C-CHECK, BLENDED OUT DAMAGE RT AILERON, L/E UNDER SHROUDS WS 282.00- WS 353.00 IAW REO.Oct 16, 2014 · N906SW · Cndair CL6002B19SDR CA141020005Spar · cracked(CAN) DURING THE COMPLETION OF A SCHEDULED MAINTENANCE INSPECTION CRACKS WERE DISCOVERED ON BOTH THE LT & RT AILERONS. EACH AILERON SPAR HAD CRACKS WHERE THE HINGE BRACKET ATTACHES TO THE AILERON. THE AILERON SPARS WERE REPLACED TO RECTIFY THIS DISCREPANCY.Oct 14, 2014 · Swrngn SA227ACSDR FDEA201410143150Skin · corrodedLEFT WING OTBD AILERON LOWER SURFACE SKIN PANEL HAS MILD CORROSION SPOTS. REMOVED CORROSION IAW SRM 57-10-00 VOL 1. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 V1 FIG 6 SHEET 1. WEIGHT & BALANCE COMPLIED WITH IAW SRM 57-50-00 PG 1.Oct 14, 2014 · N40061 · Doug MD1010FSDR IPXA2014102484696Skin · dentedINSPECTION D, LEFT WING INBD AILERON UPPER SURFACE OTBD SIDE MID AREA FOUND DENTED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 70.Oct 12, 2014 · N570UP · Boeing 74744AFSDR SWAA2014110433701Support Bracket · crackedLEFT WING AILERON OTBD HINGE TE PANEL SUPPORT BRACKET CRACKED. R & R BRACKET IAW DWG.Oct 6, 2014 · N969AT · Boeing 717200SDR FDEA201410062974Bracket · crackedLEFT AILERON OTBD HINGE PANEL BRACKET CRACKED REPAIRED LT AILERON OTBD HINGE PANEL BRACKET IAW EA 6-5750-T0312135. WINGS FLIGHT SURFACES FRONT SPAR LOWER DOUBLER BROKEN AT LT AILERON LOWER SURFACE LE MAJOR REPAIR IAW GMM 6-2-100.Oct 6, 2014 · N807FD · Airbus A310324SDR SWIA201439657Skin · chafedLEFT AILERON LOWER L/E SKIN CHAFED AT OTBD END. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN IAW REO.Oct 5, 2014 · N983CA · Cndair CL6002B19SDR SWIA201439661Skin · chafedRT AILERON PANEL 699AB IS CHAFED. DRILLED AND LOCATED NEW AILERON LOWER SKIN PANEL IAW REO.Oct 4, 2014 · N983CA · Cndair CL6002B19SDR SWIA201439656Skin · gougedGOUGE IN PANEL 599AB. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN 559AB IAW REO.Oct 4, 2014 · N983CA · Cndair CL6002B19SDR SWIA201439601Skin · chafedLT AILERON, INBD UPPER L/E SKIN CHAFED. C-CHECK, MEASURED REMAINING MATERIAL THICKNESS ON LT AILERON UPPER SKIN L/E IT WAS FOUND TO BE .064 IN NON CEM. MILLED AREA OUT OF .090 ORIGINAL THICKNESS . THE MATERIAL LOSS WAS .026 THAT WAS FOUND TO BE OUT OF LIMITS Sep 29, 2014 · N609SK · Cndair CL6002C10SDR SWIA201439557Shroud · chafedLEFT AILERON UPPER SKIN SHROUD CHAFED. C-CHECK, BLENDED CHAFE AREA IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439556Shroud · chafedLEFT AILERON LOWER SKIN SHROUD IS CHAFED. C-CHECK, BLENDED CHAFED AREA IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439555Shroud · chafedRIGHT AILERON LOWER SKIN SHROUD FROM A STA323.843 TO A STA329.875 IS CHAFED. C-CHECK, BLENDED CHAFED AREA ON RT AILERON LOWER SKIN SHROUD FROM A STA323.843 TO A STA329.875 IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439554Shroud · chafedRIGHT AILERON LOWER SKIN SHROUD IS CHAFED. C-CHECK, BLENDED CHAFED AREA IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439553Skin · chafedRIGHT AILERON UPPER SKIN SHOURD CHAFED, OTBD OF INBD HINGE TO OTBD EDGE. C-CHECK, BLENDED CHAFE ON RT AILERON UPPER SKIN SHROUD IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR FDEA201409262790Skin · corrodedLEFT WING INBD AILERON UPPER SURFACE SHOWS CORROSION. LT INBD AILERON R & R IAW N00135 & MM 27-10-01-4.Sep 26, 2014 · N564FE · Doug MD1010FSDR SWAA2014092932358Stiffener · crackedRIGHT WING AILERON 2ND HINGE STIFFENER CRACKED. R & R STIFFENER IAW SRM.Sep 25, 2014 · N609SW · Boeing 7373H4SDR ASOA2014101711442Bushing · deterioratedRIGHT AILERON INBD LUG AT INBD PCU ATTACHMENT POINT HAS MIGRATED BUSHING. REMOVED MIGRATED BUSHING, INSTALLED OVER SIZE BUSHING USING AMS5569 15-5PH H1000, PO 30012 MATERIAL IAW REO 601R-57-61-004, REV C AND DEVIATION, REO 601R-57-61-505, REV B. C/W ECTC REOSep 23, 2014 · N903EV · Cndair CL6002B19SDR SWAA2014100732718Angle · crackedRIGHT WING LOWER L ANGLE FOR AILERON WHIPPER PANEL CRACKED AT INBD END AT RSS 529. R & R L ANGLE IAW SRM & DWG.Sep 23, 2014 · N369SW · Boeing 7373H4SDR ASOA2014101611434Skin · chafedRT AILERON UPPER SKIN SHROUD IS CHAFED FROM CENTER FITTINGS OF AILERON TO INBD EDGE OF AILERON. DEEPEST DAMAGE MEASURING APPROX. .015". MAX DAMAGE ALLOWED .005". BLENDED TO A SMOOTH CONTOUR RT AILERON UPPER SKIN SHROUD FROM CENTER FITTINGS OF AILERON TO INBD Sep 21, 2014 · N903EV · Cndair CL6002B19SDR ASOA2014101311399Rub Strip · debondedLEFT AILERON TEFLON STRIP IS DISBONDED ON OTBD END. REPAIRED IAW REO 670-57-61-006-01, REV E.Sep 15, 2014 · N710EV · Cndair CL6002C10SDR HALA2014091500149Frame · crackedLT AILERON OTBD UPPER CONDUCTIVE FRAME WAS CRACKED. REMOVED DAMAGED CONDUCTIVE FRAME FROM TOP OF LT OTBD AILERON AND INSTALLED FABRICATED CONDUCTIVE FRAME ON TOP OF LT OTBD AILERON IAW 113T7110, REV N AND APPLIED DECORATIVE FINISH IAW AMM 51-21-10.Sep 15, 2014 · N583HA · Boeing 76733ASDR SWAA2014100732713Angle · crackedLEFT WING AILERON WHIPPER PANEL OTBD END ANGLE CRACKED AT LOWER FASTENER AT RSS 545. R & R ANGLE IAW SRM.Sep 11, 2014 · N369SW · Boeing 7373H4SDR SWIA201439379Skin · chafedLEFT WING AILERON LOWER OTBD SKIN SHROUD HAS CHAFE DAMAGE. REPAIRED THE LT AILERON LOWER SKIN SHROUD IAW REO.Sep 6, 2014 · N947SW · Cndair CL6002B19SDR SWIA201439378Skin · chafedRIGHT WING AILERON UPPER SKIN SHROUD HAS CHAFE DAMAGE. BLENDED OUT THE CHAFE AND FOUND TO BE WITHIN LIMITS IAW REO.Sep 6, 2014 · N947SW · Cndair CL6002B19SDR SWIA201439305Skin · chafedRIGHT AILERON CHAFED. REMOVED DAMAGE FROM LT AILERON TOPSIDE IAW SRM AND FOUND TO BE WITHIN LIMITS AND RESTORED FINISH IAW REO.Sep 4, 2014 · N817SK · Cndair CL6002D24SDR ASOA20140830267Bracket · wornDURING C-CHECK, THE RT AILERON PCA BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 30, 2014 · N14977 · Emb EMB145LRSDR FDEA201408292359Skin · chafedRIGHT INBD AILERON LE SKIN LOWER SURFACE, ENTIRE LENGTH HAS CHAFED. R & R SKIN PN ARC1286-6 IAW SRM 51-31-01. FABRICATED SKIN ON STAM TRAVELER T14 1086055. TRACKED ON EA 8-5730-T0310879, RSC TRACKING ONLY. MAJOR REPAIR.Aug 29, 2014 · N567FE · Doug MD1010FSDR FDEA201408282344Skin · chafedRIGHT INBD AILERON INBD LOWER LE SKIN HAS CHAFED. FOUND SKIN TO BE OUT OF LIMITS, ORIGINAL MATERIAL .040 INCHES, MATERIAL REMAINING .027 INCHES, MATERIAL LOSS .013 INCHES IAW SRM 57-00-01 FIG 1A SHEET 3. REMOVED INBD AILERON INBD LOWER LE IAW SRM 51-31-01. Aug 28, 2014 · N567FE · Doug MD1010FSDR CHQA20140827260Fitting · damagedDURING INSPECTION THE LT AILERON PCA OTBD FITTING WAS FOUND TO HAVE AN ENLARGED HOLE. THE LT AILERON PCA OTBD FITTING WAS REPLACED IAW SRM 51-40-02.Aug 27, 2014 · N295SK · Emb EMB135KLSDR SWIA201439330Skin · chafedRIGHT AILERON UPPER L/E SKIN CHAFED IN MULTIPLE AREAS. REPAIRED AILERON UPPER SKIN IAW REO.Aug 26, 2014 · N952SW · Cndair CL6002B19SDR SWIA201439329Skin · chafedLT AILERON UPPER L/E SKIN CHAFED AT MULTIPLE AREAS. REPAIRED AILERON UPPER SKIN IAW REO.Aug 26, 2014 · N952SW · Cndair CL6002B19SDR ASOA20140823260Attach Bracket · wornDURING C-CHECK, THE LT AILERON PCA ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5760-01044 REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 23, 2014 · N12563 · Emb EMB145LRSDR REXA2014081900769Access Panel · chafedRIGHT AILERON ACCESS PANEL 699AB CHAFED. REPAIRED IAW SRM 57-60-00.Aug 17, 2014 · N800AY · Cndair CL6002B19SDR FDEA201408132158Panel · delaminatedON WALK AROUND FOUND LT OTBD AILERON UPPER WING CLOSE OUT PANEL DELAMINATED & BROKE AWAY FROM ACFT. INSTALLED NEW PANEL IAW SRM 51-31-01.Aug 13, 2014 · N576FE · Doug MD11FSDR SWAA2014090931725Skin · delaminatedRIGHT WING AILERON LOWER SURFACE DELAMINATED. R & R AILERON IAW AMM.Aug 11, 2014 · N396SW · Boeing 7373H4SDR IPXA2014082784084Stiffener · corrodedINSPECTION 10S2, LT AILERON UPPER OTBD PANEL T/E SURFACE IS BULGED. ACCOMPLISHED STIFFNER, REPLACEMENT IAW FINAL EA 757-27-A2140 AND EO 5750-55303-A AT LT WING UPPER AILERON PANEL. CLASSIFIED AS MINOR REPAIR.Aug 7, 2014 · N455UP · Boeing 75724APFSDR 2014FA0000469Hinge · looseTWO OF THE THREE AILERON HINGES ARE LOOSE, SPECIFICALLY THE 1 WHERE THE SPADES ARE MOUNTED. BOTH AILERONS ARE AFFECTED. EACH AILERON IS ATTACHED BY 3 HINGES AND 2 OF THEM MOVE DUE TO THE BOLTS BEING LOOSE.Aug 7, 2014 · Amtr EA230SDR ASOA2014082911148Rub Strip · unsecureLT AILERON L/B PHENOLIC RUB STRIP UNSECURE. REPAIRED IAW REO 601R-57-61-503 PERMANENT REPAIR.Aug 5, 2014 · N917EV · Cndair CL6002B19SDR A6WA201441848Skin · damagedCOMPLIED WITH AWAC CARD 4DMI17327 REPAIR LT OTBD FLAP LOWER SKIN.Jul 29, 2014 · N448AW · Cndair CL6002B19SDR IXXA140708ILN020SStop Fitting · corrodedOUTBOARD AILERON AT GND STOP ON AIRPLANE GND POINT SIDE CORRODED. OTBD AILERON FITTING R & R IAW SRM 51-40-02.Jul 18, 2014 · N791AX · Boeing 767281SDR FDEA201407171838Skin · damagedFLIGHT CONTROLS LT INBD AILERON LOWER SKIN DAMAGE. COMPLY WITH EA 8-2710-T0308548 REV NO POS P3. THIS WRITE UP IS A WORK RELEASE ITEM SEQ 000669 WRI 27104334. NO NON-ROUTINE WAS GENERATED. REPAIRED LT INBD AILERON LOWER SKIN IAW SRM 57-10-00 FIG 85 & EA 27Jul 17, 2014 · N368FE · Doug MD1010FSDR FDEA201407151778Skin · delaminatedRIGHT WING AILERON UPPER SURFACE HAS ONE DENT 5.5 INCHES FROM AFT SIDE & 6 INCHES FROM INBD SIDE. IAW NTM 51-10-08 CHECK FOR CRACK & NO CRACK FOUND. TAP TEST INSPECT THE DENT & FOUND DELAMINATION 20MMX20MM IAW SRM 57-61-11 & SRM 51-77-12 PARA 4 D REMOVE THE Jul 15, 2014 · N682FE · Airbus A300F4605RSDR FDEA201407141770Rib · damagedRIGHT OTBD AILERON OTBD END OF TE WEDGE X948 DISBONDED & LOOSE. REMOVED TE CLOSE OUT RIB IAW SRM 51-31-01. FABRICATED NEW CLOSE OUT RIB ON T14 1079273. INSTALLED NEW CLOSE OUT RIB IAW SRM 51-35-01. BROKEN CLOSE OUT RIB CAUSED THE APPEARANCE OF DELAMINATIONJul 14, 2014 · N315FE · Doug MD1030FSDR SWIA201438938Skin · chafedLEFT WING AILERON PANEL 599BB IS CHAFED. C-CHECK, BLENDED PANEL 599BB IAW REO.Jul 13, 2014 · N910SW · Cndair CL6002B19SDR ASOA2014080611025Rub Strip · deterioratedLT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. COMPLIED WITH EC/TC, REO 670-57-61-006 PERMANENT REPAIR. COMPLIED WITH REO 670-57-61-006, REV D OF PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC REO 670-57-61-006-01.Jul 12, 2014 · N741EV · Cndair CL6002C10SDR ASOA2014080611024Rub Strip · deterioratedRT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. PERMANENT REPAIR TO RT AILERON OTBD RUB STRIP IAW SRM 51-22-00. COMPLIED WITH REO 670-57-61-006, REV D FOR PERMANAENT REPAIR TO RT AILERON RUB STRIP.Jul 12, 2014 · N741EV · Cndair CL6002C10SDR FDEA201407102018Skin · dentedALL SPEED AILERON UPPER SURFACE HAS DENT LOCATION 2 INCHES OTBD OF OUTER HINGE LT WING. DENT ON OTBD UPPER SURFACE OF LT WING ALL SPEED AILERON WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11. PERFORMED HFEC WITH NO INDICATIONS IAW NTM 51-10-08 TOOL NR TR 179Jul 10, 2014 · N685FE · Airbus A300F4605R
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