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 SWAA071590Wedge · debondedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM.SDR HALA0700139Structure · damagedAIRCRAFT ARRIVED WITH IMPACT DAMAGE TO LEFT OUTBOARD FLAP. IMPACT LOCATION IS 48" OUTBOARD WBL 955.0 2.5 FT FWD OF TRAILING EDGE, 2 FT INBOARD OF FLAP CANOE. DIMENSIONS 5.5" IN LENGTH, 1/72" IN WIDTH AND 1/8" IN.DEPTH. ACCOMPLISHED INTERIM REPAIR PER HAL MSDR QXEA200700587Panel · chafedC3 OKC - FLAP PANEL 684EB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.SDR QXEA200700586Panel · chafedC3 OKC - FLAP PANEL 684ET CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.SDR QXEA200700585Panel · chafedC3 OKC - RIGHT FLAP PANEL 684GB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-25-16, 51-21-11.SDR DHL2007786523Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR NR 112916. LT OB FORE FLAP WAS FOUND TO HAVE A DEEP PUNTURE IN THE UPPER SURFACE WBL442. CUT OUT PUNTURE 1" DIA ON LT OB FORE FLAP UPPER SURFACE WBL442 AND APPLIED POTTING COMPOUND. FABRICATED DOUBLESDR 07FDEA01134Bullet · crackedNR 1 FLAP TRACK FAIRING ASSY BULLET IS CRACKED REMOVED AND REPLACED NR 1 FAIRING BULLET REF MM 27-31-031.SDR SWAA071563Flap · debondedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DISBONDED AT AFT EDGE. REPAIRED FLAP PER SRM & BAC DRAWING.SDR WRNA200700023Flap · delaminatedDURING B-CHECK, RIGHT INBOARD FORE FLAP WAS FOUND WITH DAMAGE, A 42 INCH LONG X 19 INCH WIDE PREVIOUS REPAIR, 45 INCHS FROM OUTBOARD END, DEPARTED FORE FLAP WITH 40% MATERIAL LOSS. ACCOMPLISHED REPAIR PER 747 SRM 51-40-12.SDR SWAA071521Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP UPPER OUTBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA071525Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.SDR SWAA071515Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR SWAA071507Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DISBONDED AT LOWER INBOARD END. REPAIRED FLAP PER SRM.SDR DHL2007786514Skin · debondedRIGHT WING, INBD FOREFLAP, UPPER SKIN INBD EDGE SHOWS INCORRECT PREVIOUS REPAIR. NR 4 LE FLAP, LE STA 130.7. REMOVED INCORRECT PREVIOUS FIBERGLASS REPAIR APPROX 1.5 IAW B727 SRM 51-40-22 FIG 3 AND APPLIED POTTING COMPOUND. FAB DOUBLER 4" BY 5", .016, 2024T3SDR SWAA071475Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED INBOARD UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.SDR 07FDEA01045Rib · damagedOLD REPAIR AT RIB 21 INNER FLAP LT. REPLACEMENT OF END RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-103333.SDR SWAA071459Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.SDR 07FDEA00987Vane · damagedCHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED.SDR 2007UALA00810Bolt · damagedLEFT WING, OUTBOARD FLAP, OUTBOARD FLAP DRIVE, FOREFLAP ATTACH FITTING, 3 OF 4 BOLTS MISSING, BROKEN, WITH FITTING SEPARATING FROM ITS MOUNTING POINT (4TH LOCK FASTENER IS LOOSE AND ABOUT TO SHEAR). [SUP 06-14-07] REMOVED AND REINSTALLED FITTING WITH OVERSISDR DL738070217Bolt · shearedLEFT WING O/B FLAP I/B FLAP TRACK FAIRING PUNCHED BY SHEARED AFT FLAP ACTUATING ROD. REPLACED LT O/B FLAP BELLCRANK BOTH AFT FLAP PUSHRODS AND FL FAIRING. REPLACED RODS P/N 113A3920-5, P/N 113A3920-7. BELLCRANK 113A3910-3 AND FAIRING 113A9250-13. REPLACED SDR SWAA071413Skin · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REPAIRED FLAP PER SRM.SDR DHL2007786522Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF. ASTAR NR 080502. LT WING IB MID FLAP LOWER TE CHORD WBL100-134 HAS 5 CRACKS ON 3 CUTOUTS. REMOVED LT IB MID FLAP LOWER ACCESS PANEL FOR ACCESS IAW B727 SRM 51-30-2. FABRICATED REPAIR, MATERIAL USED ANGLE EXTSDR DHL2007786521Structure · crackedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES REF ASTAR NR 080528. RT WING IB MID FLAP LOWER CHORD AT WBL135 SHOWS CRACK. REMOVED R/WING IB MID FLAP LOWER PANEL AND LOWER AFT CHORD WBL135 AS REQ IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM BAC1503-100046 7075T6SDR DHL2007786517Skin · debondedLEFT OUTBD FOREFLAP WBL 305, HAS T/E DISBONDING. CUT OUT DAMAGED AREA APPROX 2 BY 6 ON LT OUTBD FOREFLAP WBL 305 IAW B727 SRM 51-40-20. FABRICATED FILLER .016 BY 2 BY 6 AND DOUBLER, .016 3.50 BY 8.50 FROM 2024T3 IAW B727 SRM 53-10-4, FIG 13. BONDED FILLER ASDR ARWA20070303Support · chafedDURING "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP "A" SUPPORT IN FLAP WELL CHAFED. BLEND-OUT AREA FOUND WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8.SDR 07FDEA00855Skin · crackedFOUND 3 CRACKS AND LOOSE RIVETS ON SKIN OF OUTBOARD FLAP LT WING LWR AND UPPER SURFACE BETWEEN STA XOF 533 & XOF 462. CUT OUT DAMAGED AREA IAW SRM 57-10-00 FIG 85 VOL 1. FOUND ON "C" 2 CRACKS 1" LONG AND .25" LONG. REMOVED TO GAIN ACCESS T/E PROFIL UP AND LSDR 07FDEA00829Skin · delaminatedOLD DELAMINATION REPAIR ON INBOARD FLAP RT UPPER SURFACE AT TRAILING EDGE. REPAIR PERFORMED BY REPLACING THE EXISTING REPAIR IAW SRM 57-53-12/FIG 209 APPROVED BY EA 6-5752-103367 AND RAS/DABRE/7007093/2006 ISSUE "A".SDR 07FDEA00826Skin · delaminatedDELAMINATION ON OLD DOUBLER REPAIR, LT INBOARD FLAP, AFT OF TRACK NR 2. REPAIR PERFORMED BY REMOVING THE EXISTING REPAIR AN INSTALL SRM REPAIR PER 57-53-12, FIG 209. APPROVED BY EA 6-5752-103366 AND RAS/DABRE/7007096/2006 ISSUE "A".SDR QXEA200700429Flap Track · corrodedC4 PDX - FLAP TRACK NR 5 ON LEFT WING HAS PITTING ON OUTBOARD SIDE ON TRACK E. REPAIRED IAW EA 2-57-217A AND DHC-8 TASK 27-51-11-830-801.SDR QXEA200700428Flap Track · corrodedC4 PDX - FLAP TRACK 4 ON LEFT WING HAS PITTING ON OUTBOARD SIDE ON TRACK E. REPAIRED IAW EA 2-57-216A AND DHC-9 TASK 27-51-11-830-801.SDR QXEA200700427Flap Track · corrodedC4 PDX - FLAP TRACK 4 ON LEFT WING HAS PITTING THE FULL LENGTH OF ROLLER TRAVEL ON TRACK E ON INBOARD SIDE. REPAIRED IAW DHC-8 AMM 27-51-11-830-801.SDR 07FDEA00834Slat Track · corrodedFOUND CORROSION ON SLAT TRACK NR 7 INBOARD AT INNER LOWER SKIN. REPAIR PERFORMED IAW EA 6-5720-103412.SDR 07FDEA00831Support Bracket · crackedNR 2 FLAP TRACK AFT SUPPORT BRACKET IS CRACKED OTBD AFT END. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.SDR ARWA20070302Fitting · gougedDURING AN "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND, LT INBD FLAP I/B THE UNIT FITTING WAS TWO GOUGES. BLEND-OUT AREAS, FOUND WITHIN LIMITS PER BOEING MESSAGE 1-301363052-8.SDR AWXA200700369Strut · corrodedSAL - FOUND CORROSION ON RIGHT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING HOLE, WS 3758/RIB 7. REPLACED RIGHT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING, WS 3758/RIB 7 IAW A320 SRM 51-72-11.SDR SWAA071366Flap · delaminatedDURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD MIDFLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED LEFT WING INBOARD MIDFLAP PER MM.SDR UPS07M49674Hinge · corrodedINSPECTION TYPE:C RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT PIN ATTACHMENT HOLE SPOT FACE FOUND CORRODED. RIGHT WING AFT O/B FLAP I/B HINGE PIVOT I/B BORE BUSHING & SPOTFACE CORROSION REMOVED & FOUND EXCESS LIMIT AS PER CMM 57-52-04 PG 621-22 REV.57SDR AWXA200700452Skin · delaminatedMCN - RIGHT WING OUTBOARD FLAP UPPER SURFACE DELAMINATED, WS 316.45 - WS 326.45. REPAIRED RIGHT WING OUTBOARD FLAP UPPER SURFACE, WS 316.45 - WS 326.45 IAW B737-300 SRM 51-70-10-2R4 FIGURE 203.SDR 07FDEA00728Vane · delaminatedRIGHT HAND WING - INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED COMPLIED WITH FEDEX EA 1-5750-109837, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00727Vane · delaminatedLEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. (SUPPLEMENTAL 28 MARCH 07) COMPLIED WITH FEDEX EA 1-5750-105636, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR PIDA07013Fairing · damagedDURING INSPECTION, FOUND CORROSION ON LOWER SURFACE OF LEFT WING AT THE FORWARD ATTACH POINT FOR THE I/B FLAP TRACK FAIRING (WING STA 285.65). REPAIRED PER BOEING MESSAGES 1-281963543-1 AND 1-281963543-9 WITH FAA DOA APPROVED 8100-9 DATED 3-6-2007.SDR ASAA0741506Skin · dentedTHE LEFT I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS. PREPARED FORE FLAP ASSY LWR SURFACE FOR BONDING FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.SDR SWAA071288Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA071289Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR DL738070194Skin · delaminatedA BLOWN TIRE CAUSED LARGE DAMAGE TO THE LOWER SKIN AND CORE OF THE INBD AFT FLAP. REPAIRED PER DELTA ERA 460616-14.SDR 07FDEA00700Skin · delaminatedOUTB FLAP RT, DELAMINATION FOUND ON THE INBD AREA, INNER SKIN SURFACE REPAIRED PER FEDEX ENG AUTH 6-5710-106684. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR SWAA071267Structure · delaminatedDURING SCHEDULED C3 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT UPPER INBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA071241Structure · delaminatedDURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.SDR QXEA200700338Skin · unknownC4 PDX - FOUND LEFT OUTBOARD FLAP UPPER INBOARD SURFACE HAS CHAFE ON PREVIOUS REPAIR. REPAIRED IAW SRM 51-20-91, 51-20-11, AND RD8-57-1734.SDR 07FDEA00653Skin · misrepairedFOUND REPAIR AT LT WING INBD FOREFLAP LE SKIN 21" FROM IB END (EXTERNAL REPAIR). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR, FOUND NOT TO CONFORM TO SRM 57-50-4 FIG 1. RE
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