JASC 5750

Service difficulty reports · 1,158

Reports filed under 5750 · Wing, Control Surfaces, 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 = '5750'
  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 SWIA200923328Flap · obstructedWHEN FLAPS 45° ARE DEPLOYED AIRCRAFT ROLLS TO THE RIGHT. (FLT 4740) REMOVED EXCESSIVE SEALANT ALONG RIGHT FLAPS.Dec 27, 2009 · N864AS · Cndair CL6002B19SDR ASAA0947157Panel · chafedPANEL 9220 LOWER SURFACE IS CHAFED. FABRICATED PANEL.Dec 18, 2009 · N784AS · Boeing 7374Q8SDR ASAA0996827Fairing · crackedFAIRING 542BB HAS CRACK IN THE FORWARD LOWER EDGE BAND. REPAIRED CRACK IN THE EDGE BAND.Oct 20, 2009 · N323AS · Boeing 737990SDR ASAA0996804Support Angle · chafedUPPER T/E PANEL SUPPORT ANGLE COMMON TO PROGRAM ROLLER FITTING IS CHAFED. REMOVED AND REPLACED SUPPORT ANGLE.Oct 18, 2009 · N323AS · Boeing 737990SDR FDEA200907202677Shroud · damagedDAMAGE AT SHROUD BOX DEFLECTORS LT SIDE. DAMAGE REPAIRED IN ACCORDANCE WITH SRM 51-77-10/ PARA 2M (2) (E); 51-77-12 /201/PARA 3 I; 57-41-12 /201/PARA 5B/5C AND 51-75-10 AS WELL AS TD/J1/S1/10227/2009 ISSUE B AND EA 6-5750-131261Jul 20, 2009 · N751FD · Airbus A300B4622RSDR C2XA09TY124Bushing · migratedDURING C-CHECK, A MIGRATED HAT BUSHING WAS FOUND ON THE LT AILERON OTBD PCA FITTING INBD LUG. THE AILERON PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-01177C. ACFT STILL IN C-CHECK.Jun 23, 2009 · N17115 · Emb EMB145XRSDR FDEA200906142086Support Bracket · crackedLT OTBD T/E MAIN FLAP PN 113N3003-13, SN CA-0206 OTBD CLOSURE RIB AREA AT WBL 561.0 AFT BRACKET WITH RIVET HOLE FOUND CRACKED. EVALUATE AND RECTIFY AS REQUIRED. LT OTBD T/E FLAP OTBD CLOSURE RIB AREA, WBL 561.0 AFT CRACK SUPPORT BRACKET REMOVED AND REPLACEDJun 14, 2009 · N933FD · Boeing 75721BSDR IPXA09M55866Wedge · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-007 LHW INBD AILERON TRAILING WEDGE STA XIA 312.342 SECTION REPAIR NEED VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-007 DOES NOT CORRELATE TO SRM 57-20-00, FIG3, VOLI, REV40. EXISTING REPAIR WEDGEApr 23, 2009 · N285UP · Doug MD11FSDR IPXA09B55842Seal · damagedINSPECTION TYPE:D DMI C397322 RT WING MISSING MID - FLAP T/E FLAP TO FUSELAGE SEAL. ORIGINAL COMPRESSION SEAL ASSY BETWEEN FROM CUSTOMER. VISUAL INSP PERFORMED SUPPORT TUBES FOUND WORN AND SUPPORT WEB CRACK FOUND. SUPPORT TUBES REPLACED AS PER SRM 57-52-01.Apr 20, 2009 · N578UP · Boeing 74745ESDR FDEA200903301101Skin · misrepairedRIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING DOUBLER REPAIR FOUND AT LEADING EDGE STA XIA 328. RIGHT WING, INBOARD AILERON ASSY UPPER SURFACE, EXISTING REPAIR FOUND NOT IN ACCORDANCE WITH SRM REPAIR. RIGHT WING INBOARD AILERON ASSY UPPER SURFACE Mar 30, 2009 · N588FE · Doug MD11FSDR C2XA09TY019Bonding Strap · corrodedPANEL 191 WAS FOUND CORRODED AND MX R&R THE BONDING STRIP IAW EMB EC 5750-01315, ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.Jan 19, 2009 · N16951 · Emb EMB145LRSDR C2XA09TY018Panel · corrodedPANEL 192AL WAS FOUND CORRODED AND MX R&R THE PLATE IAW EMB EC 5750-01315. ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.Jan 19, 2009 · N16951 · Emb EMB145LRSDR C2XA09TY015Bonding Strap · corrodedPANEL 192 WAS FOUND WITH A CORRODED BONDING STRAP AND MX R&R THE PLATE IAW EMN EC 5750-01315. ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.Jan 19, 2009 · N16951 · Emb EMB145LRSDR C2XA09TY014Bonding Strap · corrodedPANEL 193 BONDING STRIP WAS FOUND CORRODED AND MX R&R 193 BONDING PLATE IAW EMB EC 5750-01315. ACFT WILL BE RELEASED TO SERVICE AFTER THE C-CHECK IS COMPLIED WITH.Jan 19, 2009 · N16951 · Emb EMB145LRSDR UPS09854388Doubler · chafedINSPECTION TYPE:P PREVIOUS REPAIR PER EO DC8-5750-29802-A REPAIR DOUBLER HAS CHAFING DAMAGE AT XF STATION 227. REPAIR PER EO DC8-5750-29802.Jan 16, 2009 · N810UP · Doug DC873FSDR C2XA09TY006Panel · damagedPANEL 193 HAS DAMAGE, SCREW HOLES. REPAIRED IAW EC5750-01315.Jan 3, 2009 · N16954 · Emb EMB145LRSDR ASAA0842519Torque Shaft · bindingFLAPS WOULD NOT EXTEND BEYOND 9 + 1. FLAPS WERE SYMMETRICAL BUT DID NOT AGREE WITH FLAP HANDLE COMMAND TO 15DEGS. FLAP WOULD NOT MOVE USING "ALT FLAPS". OPS FROM QRC EMERGENCY DECLARED. DIVERTED TO KTN. FOUND LT WING INBD FLAP MID FLAP TORQUE SHAFT DOOR BJan 21, 2008 · N762AS · Boeing 7374Q8SDR ASAA0792308Support · crackedRT WING FIXED TRAILING EDGE AFT OF NACELLE CENTER SUPPORT IS CRACKED WS 278.5 (FWD AND AFT) RT WING FIXED TRAILING EDGE AFT OF NACELLE FWD AND AFT CENTER WEB SUPPORTS REPLACED IAW 737 900 SRM 51 40 02.Nov 24, 2007 · N302AS · Boeing 737990SDR ASAA0792307Support · crackedLT FIXED TRAILING EDGE AFT OF NACELLE CENTER SUPPORT IS CRACKED WS 278.5 LT WING FIXED TRAILING EDGE AFT OF NACELLE CENTER SUPPORT WEB REPLACED IAW B737 900 SRM 51 40 02.Nov 24, 2007 · N302AS · Boeing 737990SDR 07FDEA04308Skin · damagedOLD REPAIR ON RT OUTER FLAP TRAILING EDGE AT INBD SIDE, LOWER SKIN AND END RIB IN BAD CONDITION WITH SEVERAL DAMAGES. REPAIR PERFORMED BY REPLACEMENT OF UPPER SKIN PANEL, RESTORING CONDITION OF TD FOK/010/2005 ISSUE A AND REPLACEMENT OF RIVETS IN LOWER SKIN PSep 26, 2007 · N724FD · Airbus A300B4622RSDR 07FDEA03490Skin · dentedLT ALL SPEED AILERON LOWER SKIN, DENTS IN TRAILING EDGE HONEYCOMB AREA. REPAIR PERFORMED BY CUT OUT DENTED SKIN AND APPLY WITH EXTERNAL PATCHES IAW EA 6-5761-95884 AND RAS/FOK/199/2005 ISSUE B.Sep 10, 2007 · N728FD · Airbus A300B4622RSDR 07FDEA03218Skin · misrepairedOLD FLUSH DOUBLER REPAIR FOUND ON LT SLAT NR 1 AT UPPER SURFACE BETWEEN RIB 8-10. INVALID REPAIR AS PER SRM 57-42-11/FIG 202 WHICH IS ONLY VALID FOR INBOARD OF RIB 19, STRG 1.3 AND 1.4. REPAIR PERFORMED IAW TD FOK/055/2008 ISSUE: D, APPROVED BY EA 6-5742-991Aug 29, 2007 · N725FD · Airbus A300B4622RSDR 07FDEA03205Skin · delaminatedFOUND TWO DELAMINATED AREAS ON BOTTOM SKIN TRAILING EDGE OF LT SPOILER NR 1. DELAMINATION REPAIRS PERFORMED IAW SRM 57-71-11/PG 201/PARA 10, APPROVED BY EA 6-5770-101551.Aug 29, 2007 · N725FD · Airbus A300B4622RSDR 07FDEA02179Vane · noneWING LT, FLAP INBD, PREVIOUS REPAIR FOUND LOCATED ON FLAP VANE UPPER SKIN IN BETWEEN RIB 17-18. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO FEDEX ENGINEERING AUTHORIZJun 18, 2007 · N452FE · Airbus A310222SDR 07FDEA02174Skin · unknownOLD REPAIR (FLUSH DOUBLER) REPAIR ON RT OUTBOARD SLAT NR 3 JACK RIB 6 NOT CONFORM TO SRM (FILLER MATERIAL, RIVET PITCH, USED FASTENER). REPAIR PERFORMED BY NEW FLUSH REPAIR, APPROVED BY EA 6-5744-103280 REV A AND RAS/FOK/213/2006 ISS. C.Jun 18, 2007 · N726FD · Airbus A300B4622RSDR 07FDEA02145Flap · noneWING RT, FLAP INBOARD, PREVIOUS FLUSH REPAIR LOCATED ON FLAP VANE LEADING EDGE BETWEEN RIB 6 - 8. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR CONFORMS TO EXISTING FEDEX EA 6Jun 15, 2007 · N452FE · Airbus A310222SDR 07FDEA02144Flap · noneLT WING, KRUEGER FLAP, PREVIOUS PATCH REPAIR FOUND LOCATED ON KRUEGER FLAP BETWEEN RIB 2A AND RIB3, WS 67. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX Jun 15, 2007 · N452FE · Airbus A310222SDR 2007FA0000403Control Cable · chafedDURING PREFLIGHT INSPECTION, FOUND FLAP CONTROL CABLES CHAFING ON THE FLAP TRACK. DEPTH OF INTERFERENCE BETWEEN CABLE AND TRACK WAS ABOUT THE DIAMETER OF THE CABLE.May 22, 2007 · Sympho SA160SDR QXEA200603286Panel · wornC3 OKC - PANEL 684CB WORN BARE METAL AT CUTOUT. REPAIRED IAW SRM 57-41-01, 51-21-16.Dec 5, 2006 · N609QX · Cndair CL6002C10SDR QXEA200603285Panel · wornC3 OKC - FOUND PANEL 684AB WORN BARE METAL AT CUTOUT. REPAIRED IAW SRM 57-41-01, 51-21-16.Dec 5, 2006 · N609QX · Cndair CL6002C10SDR QXEA200603284Panel · wornC3 OKC - PANEL 684JB WORN BARE METAL AT CUTOUT. REPAIRED IAW SRM 57-41-01, 51-21-16.Dec 5, 2006 · N609QX · Cndair CL6002C10SDR QXEA200603283Panel · wornC3 OKC - PANEL 684LB WORN BARE METAL AT CUTOUT. REPAIRED IAW SRM 57-41-01, 51-21-16.Dec 5, 2006 · N609QX · Cndair CL6002C10SDR QXEA200603100Hinge · unknownC3 YYC - REPAIR OR REPLACE LEFT OUTBOARD MFS HINGE. REPAIRED IAW CRJ MM 27-54-20, 57-73-27.Nov 20, 2006 · N613QX · Cndair CL6002C10SDR QXEA200603405Panel · damagedPDX C3 - LEFT WING FLAP CANOE PANELS 526AB AND 527AB BULB SEALS DAMAGED. REPAIRED IAW Q400 SRM 51-42-05.Oct 16, 2006 · N414QX · Bombdr DHC8402SDR QXEA200602628Bracket · damagedC3 PDX - RIGHT WING SHROUD BRACKET AT STATION WING 140.0 HAS ELONGATED FASTENER HOLE. REPAIRED IAW REO 670-57-51-106 AND SRM 51-21-16.Sep 26, 2006 · N608QX · Cndair CL6002C10SDR SWIA200617102Angle · crackedRT BATT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 57-61-046.Jul 9, 2006 · N459SW · Cndair CL6002B19SDR QXEA200601244Panel · chafedPDX - C3 CHAFING ON PANEL 684GB. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.Apr 30, 2006 · N604QX · Cndair CL6002C10SDR UPS06446040Panel · blisteredINSPECTION TYPE:C RHW - IB MID FLAP LWR FLAP FOUND BULGED UP AT 95 INCHES - 135 INCHES FROM IB SIDE AS MARKED. TIME LIMITED REPAIR ACCOMPLISHED IAW HX RS NR R-57-55-35418 AND UPS EO NR B747-5750-23648-A.Dec 31, 2005 · N520UP · Boeing 747200SDR AU510001907Indicator · faulty(AUS) TRAILING EDGE FLAP ASSYMETRY. FLAPS RECYCLED AND OPERATED NORMALLY. INVESTIGATION CONTINUING. (CASA NR 510001907)Dec 12, 2005 · Boeing 737476SDR QXEA200500950Shroud · crackedPDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD INBOARD RIVET AT SIXTH BRACKET HAS CRACK AT AFT INBOARD. REPAIRED IAW RD 8/4-57-261.May 14, 2005 · N412QX · Bombdr DHC8401SDR 05FDEA00413Support · corrodedCOMPLY WITH EA 8-5750-55448 WINGS - FLAP VANE SUPPORT CORROSION REWORK LT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-55448.Mar 8, 2005 · N369FE · Doug DC1010SDR DHL2004764009Connector · mispinnedNR 3 LED WOULD NOT RETRACT ON DEPARTURE ACCOMPLISHED ABNORMAL PROCEDURE LED WOULD NOT RETRACT ON SECOND ATTEMPT, NR 3 SLAT. SWAPPED PINS 1 AND 3, 2 AND 4 ON NR 3 SLAT ACTUATOR IAW B727 MM 27-82-11 PAGE 101. OPS CKS GOOD.Aug 31, 2004 · N764AT · Boeing 727264SDR DL757040421Skin · delaminatedACCOMPLISHED METAL BOND REPAIR TO UPPER INBOARD SKIN ON THE NUMBER 4 SLAT.May 10, 2004 · N662DN · Boeing 757232SDR CA040428002Fairing · lightning strike(CAN) LIGHTNING STIKE ON APPROACH INTO AIRPORT. LIGHTNING ENTERED LT SIDE OF WEATHER RADAR. NO OBVIOUS EFFECT TO AIRCRAFT SYSTEMApr 27, 2004 · Cndair CL6002D24SDR UIEA200400051Bushing · worn(D) CHECK, DURING SCHEDULE MAINTENANCE, NR 8 MOVEABLE CANOE AFT SECTION SECONDARY DOOR ASSEMBLY LOWER BEARING FOUND MIGRATED. THE LUG BORES ARE OVERSIZED TO 0.7827 INCH DIAMETER TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE. AN ALUMINUM REApr 15, 2004 · N522MC · Boeing 7472D7BSDR 03FDEA02343Bracket · crackedLT WING O/B FLAP I/B HINGE (WING SIDE) FAIRING SUPPORT FWD I/B BRACKET FOUND CRACKED. REMOVED & REPLACED AS PER AMM 20-50-02.Dec 29, 2003 · N621FE · Doug MD11SDR 03FDEA02344Bracket · crackedLEFT WING I/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT BRACKET (TOP OF ACTUATOR) FOUND CRACKED. REMOVED & INSTALLED NEW BRACKET AS PER CMM 20-50-02.Dec 29, 2003 · N621FE · Doug MD11SDR 03FDEA02018Hinge · corrodedLEFT O/B FLAP, FOUND O/B HINGE ACTUATOR HOLE NR 2 O/B UNFLANGE SIDE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74255 - WINGS - LEFT AND RIGHT OUTBOARD FLAP -OUTBOARD HINGE BRACKET BORE CORRODED.Dec 3, 2003 · N583FE · Doug MD11SDR 2004FA0000252Aileron · mislocatedFOUND RIVET IN AILERON LEADING EDGE HAD CAUGHT CORNER OF RIB INSTEAD OF THROUGH CENTER OF RIB. CONDITION IN BOTH LEFT AND RIGHT AILERONS AT WS123. REPAIRED CONDITION IAW MFG LETTER OF INSTRUCTION.Nov 6, 2003 · N354C · Aviat A1BSDR 2003FA0000723Control Cable · brokenPILOT REPORTED WHEN SETTING FLAP SELECTOR TO 15 DEGREES, INDICATOR STAYED A (0), RIGHT FLAP EXTENDED TO 30 DEGREES AND LEFT FLAP STAYED IN THE UP POSITION AND CIRCUIT BREAKER POPPED. ON FURTHER INVESTIGATION FOUND THAT FLAP CABLE WAS BROKEN WERE IT CONNECTS TJun 17, 2003 · N5581T · Beech F33A
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