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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS07M50364Skin · damagedINSPECTION TYPE:C RIGHT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO REPLACE DUE TO BADLY PITTED. RIGHT WING I/B FLAP LOWER SURFACE I/B SEGMENT LOWER SKIN REMOVED PER SRM 51-31-01 V2 R38. NEW SKIN FAB PER BOEING DRAWING ARC2736 REV B. NEW SKIN HOLES PICKSDR 2007FA0000506Skin · crackedBOTH FLAPS CRACKED AT ACTUATOR ATTACH POINT. LT FLAP SKIN AND RIB CRACKED. RT FLAP RIB CRACKED. RIGGING WAS OK, PROBABLY AN OPERATOR INDUCED PROBLEM. BELIEVE THE FLAPS HAVE BEEN LOWERED AT TOO HIGH AN AIRSPEED. (K)SDR QXEA200700837Fitting · damagedC4 PDX - LEFT OUTBOARD FLAP FORWARD INBOARD AND OUTBOARD MOUNT FITTINGS TO NR 4 CARRIAGE, HAVE FLAT SPOTS WORN ON ENDS. REPAIRED IAW RD8/4-57-228.SDR SWAA072503Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR 07FDEA01837Flap Track · corrodedLT WING TE IB FLAP OB TRACK IS CORRODED AT FWD END AND SPOILER SPPT ATTACH POINT LT WING INBD T/E FLAP OUTBD (NR3) FLAP TRACK REPLACED ON FED EX W/C 27X5705-03.SDR DHL2007788525Skin · gougedWHILE AT C CHECK AT FLIGHTSTAR, RT I/B FORE FLAP I/B UPPER SURFACE GOUGED. REMOVED DAMAGED AREA 5" DIA CLEANED AND PREPPED REPAIR AREA, FABRICATED FILLER 5" AND DOUBLER 8" FROM .016" 2024-T3 PO NR 9003189 ALODINED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRSDR DHL2007740506Skin · delaminatedLT I/B MID FLAP UPPER SURFACE DELAM 36" FROM O/B END. REMOVED DAMAGED AREA APPROX 6 3/4" BY 4" BY 4 1/4" CLEANED AN PREPPED AREA TO BOND, FABBED FILLER (6 3/4"X 4 1/4") AND FILLER 2 EACH 3" BY 4 1/4" FROM .016 7075-T6 PO NR 9003988, ANODIZED, PRIMED AN APPLIESDR HALA0700223Structure · dentedDENT IN LEFT WING INBOARD AFT FLAP, 6" INBOARD OF THE NUMBER 3 FLAP FAIRING. DENT IS OUT OF LIMITS PER SRM 51-70-10. REPAIRED LT WING I/B AFT FLAP, USING METAL TO METAL HOT BOND METHOD IAW SRM 57-53-01, AND SRM 51-70-2R.SDR 07FDEA01819Flap Track · corrodedLEFT WING TE OB FLAP OB TRACK IS CORRODED AT AFT ATTACH POINT. TRACK ASSEMBLY REPLACED ON FED EX W/C 27X5707-01 REF MM 27-51-031-4.SDR YNTA200728101Yoke · corrodedON APPROACH THE FLAP SYSTEM FAILED TO EXTEND PAST 15 DEGREES AND THEN BECAME STUCK AT 15 DEGREES. TRIED TO SET FLAPS TO 25 DEGREES AND FLAPS DID NOT MOVE, RESET FOR 15 DEGREES AND THEN UP TO 0 DEGREES WITH NO MOVEMENT. RESELECTED FLAPS TO 15-DEGREE POSITION. LSDR 07FDEA01783Wedge · delaminatedRIGHT WING OUTBOARD FLAP INBOARD WEDGE TRAILING EDGE UPPER SURFACE FOUND DELAMINATED RIGHT WING OUTBOARD FLAP INBOARD WEDGE REMOVED AND REPLACED AS PER AMM 20-50-02, P/N ON: ARC4363-2, S/N ON: 177679-9.SDR 07FDEA01777Support Fitting · crackedLT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. LT WING OUTBD FLAP ASSY REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. LT OUTBD FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805, FOUND SATIS.SDR USAA070380Skin · crackedLEFT OUTBOARD MID FLAP L/E SKIN AT INBOARD FORE FLAP OPENING HAS CRACK. INSTALLED SPLICE PLATE & FILLER PER SRM 57-53-01 REP 7, DEFECT SIZE: 2 INCHES.SDR USAA070373Skin · chafedINBOARD LEADING EDGE OF LEFT OUTBOARD MIDFLAP CHAFED. INSTALLED DOUBLER PER SRM 53-01, DEFECT SIZE: 1 X 2 INCH.SDR MASA200700291Rib · damagedDAMAGE TO RT I/B FLAP RIB FLAP. REPAIRED LT I/B FLAP RIB FLAP.SDR QXEA200700806Flap Track · damagedC4 PDX - RIGHT WING FLAP TRACK NR 4 AT YW 281.019 HAS TUNGSTEN CARBIDE COATING MISSING INBOARD SURFACE 23" AFT OF REAR SPAR. REPAIRED IAW RD8/4-57-792.SDR AWXA200700625Skin · delaminatedMCN - RIGHT WING INBOARD FLAP TRAILING EDGE IS DELAMINATED, MAIN FLAP STATION 120, MAIN FLAP STATION 124. REPAIRED IAW B757-200 SRM 51-70-04.SDR QXEA200700853Skin · gougedC4 OKC - LEFT WING, INBOARD FLAP, MIDDLE INBOARD VANE SPRING ACTUATOR AREA HAS A GOUGE IN THE SKIN. REPAIRED IAW SRM 51-12-00, 57-52-01.SDR QXEA200700814Skin · chafedC4 PDX - RIGHT WING OUTBOARD FLAP UPPER SURFACE HAS A CHAFE IN SKIN FROM WING TRAILING EDGE SEAL LOCATED AT YW 211 TO YW 264. REPAIRED IAW SRM 51-21-10, 51-25-10, 57-52-30.SDR DL76L091889Collar · damagedWING T/E- INBD FLAP- MAIN FLAP - COLLAR FITTING REPAIR IAW 01-073591-12 ME12 LT AND ME13 RT , EO 01-073591-12 ME12 LT AND ME13 RT.SDR UPS07M50400Stop Fitting · crackedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP STOP FITTING FOUND CRACK (VANE TRACK NR 4 FROM I/B VICINITY) LEFT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30R.55. LEFT WING O/B FLAP I/B & O/B CARRIAGE ROLLERS ASSY REMOVED PER CMM 57-52-04 R.58.SDR UPS07M50384Stop Fitting · crackedINSPECTION TYPE:C RIGHT O/B TRAILING EDGE FLAP STOP FITTING SUSPECTED CRACK (VANE TRACK NR 4 FROM I/B). RIGHT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30 R55. HFEC INSP C/OUT PER DA DACNDTSPM R.13 PART 06-10-01-001 ON STOP FITTING FOUND CRACK. SDR SWAA072392Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA01764Skin · delaminatedRT FOREFLAP I/B END LOWER SURFACE AND EDGE ARE DELAMINATED REPAIRED DELAMINATION ON I/B END LOWER SURFACE OF FOREFLAP REF SRM51-40-20. TAP TEST GOOD, PRIMED AND PAINTED REPAIR AREA REF M/M 51-40-20-151-7 COOK TICKET ATTACHED.SDR UPS07649785Flap · damagedDAMAGE TO RIGHT O/B FLAP. DENTS AND DELAMINATION BEYOND SRM LIMIT. [SUP 05-14-07] ACCOMPLISHED STEPS 1 THRU 5A AND STEP 5B ON DENT 2 ONLY PER EO B767-5750-25812-A, PARAGRAPH 6A. ACCOMPLISHED INTERIM REPAIRS TO REMAINING AREAS PER EO B767-5750-26812A. REPEATSDR QXEA200700849Support · wornC4 OKC - RIGHT WING, OUTBOARD FLAPS, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-01, 51-12-00.SDR QXEA200700850Skin · chafedC4 OKC - RIGHT FLAP PANEL 684AB CHAFED. REPAIRED IAW SRM 51-12-00, 51-21-11.SDR DHL2007788528Skin · dentedWHILE IN "C" CHECK, 3 DENTS ON R/W I/B AFT FLAP UPPER SURFACE 31", 55", AND 82" FROM I/B END. EVALUATED 3 DENTS AT 31" A=1.5, Y=.032, A/Y=46.37. 55" A=1.5", Y=.038, A/Y=39.47. 82" A=1.8, Y=.028, A/Y=64.28. AREA FOUND WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1.SDR DLM88070551Vane · delaminatedINADEQUATE REPAIR AND DELAMINATION ON RT INNER FLAP INNER VANE. FILLER, DOUBLER REPAIR WERE FABRICATED IAW SRM 57-03D PAR 8A FIG 9A ( SHEET 1 AND 2 ) RT INNER FLAP INNER VANE WAS REPAIRED IAW SRM 57-03 PAR 8A FIG 9A SHEET 1 AND 2 (AMX 200202768).SDR DLM88070550Vane · dentedEROSION AND DELAMINATION ON LOWER SURFACE DENTS ON UPPER SURFACE OF LT INNER FLAP OUTBD VANE. DOUBLER, FILLER REPAIR BONDING WAS DONE IAW SRM 51-70-2D PARA H. REPAIRED IAW SRM 57-03D PARA 8A FIG 9A.SDR DLM88070509Vane · delaminatedDELAMINATION AT LOWER SURFACE ON RT WING INBOARD FLAP VANE BETWEEN STATIONXCW=79.00 AND XCW=104.500. AMX PERFORMED PERMANENT REPAIR PER SRM 57-03 FIG 9A.SDR DLM88070508Vane · delaminatedEROSION AND DELAMINATION ON LOWER SURFACE, DENTS ON UPPER SURFACE OF LT INNER FLAP O/B VANE. AEROMEXICO PERFORMED PERMANENT REPAIR FOR THE DAMAGED SKIN PORTION IAW MD-80 SRM 57-03 FIG 9A (DELTA AIRLINES SRM CHAPTER 57-03D FIG 9A)SDR QXEA200700848Skin · damagedC4 OKC - PANEL 684ET HAS WEAR MARK ON LEADING EDGE. REPAIRED IAW SRM 55-00-00, 51-12-00.SDR DHL2007788517Skin · crackedRT IB AFT FLAP IS CRACKED 3 PLACES. CUT OUT 3 CRACKED AREAS ON RT IB AFT FLAP UPPER SKIN (1) 1.2" DIA. (2) 1" DIA (3) 1.8" DIA. CUTOUT 2 DELAMINATED AREAS ON LOWER SKIN (1) 8" BY 8" (2) 8 1/2" BY 23". FABRICATED UPPER DOUBLERS (1) 4.2" DIA (2) 4" DIA. (3) 4SDR DLM88070523Skin · dentedDENTS ON LOWER SKIN OF LT INNER FLAP STA XW-49. REPAIRED PER ERA 461313-14 REV O.SDR SWAA072356Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR USAA070367Wedge · wornWEAR MARKS LEFT INBOAD MID FLAP TRAILING EDGE WEDGE, UNDERSIDE 34 INCHES FROM I/B END. INSTALLED BONDED REPAIR DOUBLER PER EA 98647, DEFECT SIZE: 6 INCHES.SDR DL76L091978Fitting · unknownWING T/E INBD FLAP - MAIN FLAP - COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13 C/W EO 01-073591-12 ME12 AND ME13.SDR USAA070357Wedge · damagedLT I/B TE FLAP WEDGE. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER PER EA 98647. DEFECT SIZE: 3" DIA.SDR DHL2007788511Skin · delaminatedLEFT WING INBD FORE FLAP, LWBL 74 UPPER SURFACE DELAMINATED AT EXISTING REPAIR. REMOVED DELAMINATED AREA 2.5" BY 7" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 10" BY 5.7" AND FILLER 2.5" BY 7" FROM .016, 2024T3, SDR 07FDEA01690Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.656". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875, SDR 07FDEA01689Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE FORWARD FITTING INBOARD CENTER HOLE FOUND WITH CORROSION DURING ACCOMPLISHMENT OF EO 1-5750-7-5008. ORIGINAL HOLE DIAMETER = 0.580"; FINAL HOLE DIAMETER = 0.657". [SUP 05-14-07] COMPLIED WITH FEDEX EA 1-5750-109875,SDR 07FDEA01688Skin · delaminatedRIGHT WING OUTBOARD FLAP CENTER TRAILING EDGE LOWER SURFACE FOUND DELAMINATED 4" BY 4" (LENGTH X WIDTH). [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 20-50-02.SDR 07FDEA01687Skin · delaminatedRIGHT WING, OUTBOARD FLAP INBOARD TRAILING EDGE UPPER SURFACE FOUND DELAMINATED 5" BY 7" (LENGTH X WIDTH). REMOVED AND REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR TRAX200700600Angle · damagedETNRTC 500-13, AT WS 178 OUTB'D FLAP ANGLE ON THE FLAP AFT SIDE ANGLE CRACKED. [SUP 05-15-07] AFTER FURTHER INVESTIGATION HOLE WAS FOUND TO BE DOUBLE HOLED THRERFORE WAS RWORKED TO INSTALL OVERSIZE FASTENER IAW SRM 51 42 20 , 51 42 06.SDR ASAA0741628Skin · puncturedTHE IB FORE FLAP IS PUNCTURED NEAR THE CENTER TRACK. REMOVED THE DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.SDR ASAA0741627Skin · chafedTHE RT OB MID FLAP IS CHAFED ON AN EXITING LE DOUBLER AT THE IB END. REMOVED THE EXITING REPAIR DOUBLER FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57 53 01 FIG 201 REPAIR 8.SDR ASAA0741623Doubler · chafedRT IB FORE FLAP CHAFED ON AN EXITING REPAIR DOUBLER ON THE UPPER SIDE. REMOVED THE EXITING REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED A REPLACEMENT DOUBLER AND FILLER IAW SRM 51 70 10 PARA 7 8 11 15 18 AND 20.SDR ASAA0741622Skin · dentedLT IB FOR FLAP DENTED OUT OF LIMITS NEAR CENTER TRACK. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51 70 10 PARA 8 11 15 18 AND 20.SDR UPS07M49847Fitting · crackedINSPECTION TYPE:4C LEFT I/B SLAT FITTING BETWEEN NR 7 & 8 SLAT IS CRACKED. REMOVED AND REPLACED FITTING IAW MD-11 SRM 51-33-01 AND 51-35-01.
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