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 751003Fitting · shearedLOUD THUMP HEARD WHEN MOVING FLAPS FROM 10 TO 20 DEGREES. INSPECTED AIRCRAFT AND FOUND RT INBD TRAILING EDGE FORE-FLAP FITTING SHEARED AND OTHER COMPONENTS IN THE AREA DAMAGED. REMOVED AND REPLACED FORE-FLAP, 2 EACH RIBS, RT INBD AILERON AND PERFORMED A FLAPSDR 07FDEA01667Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.SDR 07FDEA01666Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.SDR 07FDEA01664Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 1 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.SDR 07FDEA01663Strut · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT (P/N: ARC2126) FWD AND AFT HOLE FOUND CORRODED. [SUP 05-15-07] COMPLIED WITH FEDEX E.A. 1-5750-111092.SDR 07FDEA01662Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORRODED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. COMPLY WITH FEDEX EA 1-5710-111094. REPAIR CSDR 07FDEA01661Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 2 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.SDR DHL2007788512Skin · delaminatedLEFT WING, INBD FORE FLAP LOWER SURFACE DELAMINATED AT LWBL 125. CUT OUT DELAMINATED AREA 8.4" BY 9.4" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3 AND 51-40-24, FIG 1. FABRICATED DOUBLER 10" BY 12.4" AND FILLER 8.4" BY 9.4" FROM .016SDR HALA0700200Skin · dentedRIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS RAVEL DAMAGE INBOARD END TO 74 INCHES OUTBOARD,TRAILING EDGE FORWARD 16 INCHES. REPAIRED PER 767 SRM 51-70-01-06-0.SDR HALA0700201Skin · dentedRIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS GRAVEL DAMAGE 38 INCHES INBOARD OF OUTBOARD FAIRING 15 INCHES FORWARD OF TRAILING EDGE. REPAIRED PER STRM 51-70-01-06-0.SDR HALA0700202Skin · dentedRIGHT WING INBOARD AFT FLAP LOWER SURFACE HAS GRAVEL DAMAGE 27 INCHES INBOARD OF OUTBOARD END 16 INCHES FORWARD OF TRAILING EDGE. REPAIRED PER 767 SRM 51-70-01-06 -0.SDR SWAA072079Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD LOWER END. REMOVED AND REPLACE FLAP PER MM.SDR DL76L100222Fitting · 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 LT AND ME13 RT.SDR UIEA200700211Structure · damagedRIGHT OUTBOARD AFT FLAP HAS A NICK IN THE TRAILING EDGE AS MARKED 0.25" BY 0.25". REPAIRED IAW XEO- 57-042307-2.SDR UIEA200700209Panel · dentedLT O/B AFT FLAP HAS UPPER ALUMINUM HONEYCOMB PANEL DENTS. REPAIRED IAW XEO- 57-042307-3.SDR NOCA08707Skin · corrodedLEVEL 1 CORROSION ON I/B FWD FLAP UPPER SKIN 18 - 36 INCHES I/B END 15 INCHES FROM T/E. REMOVED AND BLENDED OUT CORROSION PER 57-53-01, ALODINED AND PRIMERED AND PAINTED PER SRM 51-20-01.SDR SWAA072048Structure · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP CRACKED AT LOWER OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA01597Vane · misrepairedLEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND WITH EXISTING REPAIR WHICH IS NOT COVERED BY SRM. [SUP 05-16-07] REMOVED AND REPLACED AS PER AMM 27-50-22-04. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-05. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01596Vane · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR MALA070056Structure · damagedTHE RT FLAP, P/N 7257800-574, S/N 1326, IS DAMAGED APPROXIMATELY 4.0" FROM THE AFT EDGE AND 2.6' FROM THE INBOARD END OF THE PART. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S57060. REF: EAMS WORK ORDER 216293 TASK 6501.SDR UPS07M50116Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B AFT HINGE LOWER BORE (02EA) FOUND RUSTY. RT AFT O/B FLAP I/B HINGE PIVOT I/B AND O/B BORE BUSHING REMOVED. SPOT FACE CORROSION REMOVED FOUND EXCEED LIMIT. FPI C/OUT ON REWORK AREA FOUND NO CORROSION AND NO CRACK. REWORK ARSDR DHL2007788514Skin · delaminatedLEFT WING, INBD FORE FLAP, LOWER SURFACE NEAR TRACK FITTING, LWBL 90, AREA DELAMINATED. CUT OUT DELAMINATED AREA 13" BY 15.5" FABRICATED FILLER, 13" BY 15.5" AND DOUBLER, TWO EACH, 3" BY 15.5" FROM .016, 2024T3. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAWSDR DHL2007788501Skin · gougedRIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20,PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PRSDR DHL2008788501Skin · gougedRIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PSDR 07FDEA01559Flap · dentedSEVERAL DAMAGES (DENTS, CORRODED CORE) ON RT INBOARD FLAP AT LOWER AND UPPER SURFACE BETWEEN RIB2-9. REPAIR PERFORMED IAW SRM 57-53-12/FIG 208/209, APPROVED BY EA 6-5753-99189 AND RAS/DABRE/7006468/2006 ISSUE "B".SDR UPS07M49869Mount · corrodedINSPECTION TYPE:C LEFT WING I/B FLAP I/B ACTUATOR ENCLOSURE, UPPER AFT LARGE ROLLER BEARING MO MOUNTING FOUND CORRODED. I/B & O/B BUSHINGS MOUNT ELONG HOLE EXCEED LIMIT. I/B HOLE MATL REMOVED 0.0 06" O/B HOLE MATL REMOVED 0.015". MAX ALLOW DIA 1.000". FPE CSDR SWIA200718164Structure · damagedBIRD STRIKE TO LEFT INBOARD FLAP ON APPROACH INTO YWG. REPLACED LEFT INBOARD FLAP INBOARD LEADING EDGE PER 57-52-01.SDR ASAA0771607Flap Track · wornLT INBD AFT FLAP OTBD TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16.SDR ASAA0771606Flap Track · wornRT INBD AFT FLAP OTBD TRACK HAS AREA OF WORN PLATING REPLACED FLAP TRACK IAW AMM 27 51 16.SDR ASAA0771605Flap Track · wornRT INBD AFT FLAP TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16.SDR 07FDEA01534Skin · gougedLT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGED PART REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED DOUBLER REF; DC/MD10-10 SRM 57-10-00 VOL1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLED DOUBLER REF; DC/MDSDR 07FDEA01533Skin · gougedLT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGE REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED REPAIR DOUBLER. [SUP 04-30-07] REF; DC/MD10 -10 SRM 57-10-00 VOL 1. ALODINED AND PRIMED REF; DC/MD10-10 SRM 51-21-01 VOL 11. INSTALLESDR DHL2007788506Skin · gougedLEFT W/S 464, OUTBD FOREFLAP, INBD L/E AT PREVIOUS REPAIR DOUBLER GOUGED. REMOVED GOUGED DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 5" BY 6" BY .063 FROM 2024T3 AND FILLER 2.20" BY 1.90" BY .063 FROM 2024T3 IAW B727 SRM 57-50-4, FIG 4. TREATED SDR CA070803001Flap Track · separated(CAN) DURING HARD MANEUVERING WITH FLAPS DOWN, A LOUD BANG WAS HEARD BY THE PILOTS WHO NOTICED THE LT FLAP BEING PUSHED BACK AT A STRANGE ANGLE. THE FLAPS WERE LEFT IN THE DOWN POSITION AND THE AIRCRAFT WAS RETURNED WITHOUT INCIDENT. UPON INVESTIGATION THE LSDR CA070426005Seal · missing(CAN) AFTER 30 MINS INTO FLIGHT, CREW REPORT AILERON MISMATCH, AP DISCONNECTED AND AILERON STUCK. PILOT USED FORCE TO RELEASE AILERONS. REST OF FLT SYSTEM, OPS NORMAL. THIS WAS THE FIRST FLT OF THE DAY AND THE TEMP AT FL250 WAS -45 DEG C. FOUND RT FLAP SEASDR DALA1108510173Fitting · damagedFLAP COLLAR FITTING REPLACED IAW EA 01-073591-12, ME12, ME13, ME20, ME21.SDR DHL2007788509Skin · crackedLEFT INBD MID FLAP LWBL 85-100, LOWER T/E CHORD CRACKED THREE PLACES ON CUTOUTS. CUTOUT DAMAGE AREA 46.625" BY 2" IAW B727 SRM 51-40-3, FIG 1. FABRICATED NEW ANGLE FROM BAC1503-100046-7075T6, 46.625" BY 2" AND TWO EACH SPLICES FROM BAC 1503-100046-7075T6, 7.SDR DHL2007788504Skin · debondedLEFT INBD AFT FLAP, UPPER SURFACE LWBL 244, UPPER SURFACE CRACKED AND DISBONDED. REMOVED DAMAGED AREA 12.5" BY 15", CLEANED, PREPPED AREA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 3" BY 15" AND SKIN 12.5" BY 15" FROM 7075T6, .012, PRIMED, APPLISDR SWAA071911Flap · crackedDURING SCHEDULED 22Y CHECK, FOUND LEFT WING INBOARD FORE FLAP CRACKED AT LOWER AFT END. REPAIRED FLAP PER SRM.SDR SWAA071897Flap · delaminatedDURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA071918Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LEFT WING OUTBOARD AFT FLAP DELAMINATED UPPER INBOARD SURFACE. REPAIRED FLAP PER SRM.SDR 07FDEA01512Skin · damagedDURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT RT WING INBOARD FLAP UPPER SIDE WITH EXISTING REPAIR STA XIFH 219.550 REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 85.SDR QXEA200700677Flap Track · corrodedC5 PDX - RIGHT WING NR 5 FLAP TRACK INBOARD SIDE LOAD ROLLER TRACK SURFACE HAS SURFACE RUST FORMING. REPAIRED IAW RD8-57-989.SDR QXEA200700667Flap Track · corrodedC5 PDX - LEFT FLAP TRACK NR 5 HAS SURFACE CORROSION ON THE UNDERSIDE OF THE TOP OUTBOARD TRACK JUST FORWARD OF THE ROLLER CONTACT AREA AND ON THE FORWARD PORTION OF THE OUTBOARD SIDE ROLLER TRACK. REPAIRED IAW RD8-57-989.SDR QXEA200700668Flap Track · corrodedC5 PDX - FOUND LEFT FLAP TRACK NR 4 HAS SPOTS OF CORROSION ON MOST SURFACES, ESPECIALLY IN THE ROLLER TRACK AREA. REPAIRED IAW RD8-57-988.SDR DLM88070468Skin · damagedLT INBOARD FLAP LOWER SKIN REPAIR BETWEEN STA XW=47 AND XIFO=64.7248 - TEMPORARY REPAIR INSTALLED. TEMPORARY REPAIR REMOVED, DAMAGED SKIN TRIMMED OUT AND NEW SECTION WAS SPLICED PER AM REPAIR DWG AMR0957194 R01 DATED 14MAR07 AND ERA 460139-14.SDR 07FDEA01496Vane · chafedCHAFING MARKS AT INBOARD FLAP VANE, RHS. REPAIR WAS PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5752-101309 AND RAS/DABRE/7006736/2006 ISSUE "A".SDR ASAA0741576Skin · chafedTHE LEFT WING OUTBOARD FORE FLAP IS CHAFED ON AN EXISTING LEADING EDGE REPAIR AT THE INBOARD END. REMOVED THE EXISTING SKIN REPAIR DOUBLER IAW SRM 57-53-01 FIG 201.SDR ASAA0741575Skin · dentedTHE RIGHT INBOARD FORE FLAP IS DENTED ON THE LWR INBOARD SIDE. PREPARED THE DAMAGED SURFACE OF THE LWR SKIN FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.SDR ASAA0741574Skin · puncturedTHE LEFT WING INBOARD FORE FLAP IS PUNCTURED ON THE LWR SURFACE 4 INCHES FROM THE TRAILING EDGE AND 20 INCHES FROM THE INBOARD SIDE. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8,
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