JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 05FDEA01197Retainer · crackedNR 3 SLAT INBOARD MOLDED SEAL RETAINER CRACKED ON SEVERAL AREAS. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.SDR USAA050576Skin · debondedCLT - NR 6 SLAT SKIN DISBOND 6 INCHES, INBOARD EDGE OF THE WEDGE. R & R DAMAGED SKIN AND CORE IAW TR 57-42-04 AND 51-30-03. (M)SDR USAA050572Skin · damagedCLT - PREVIOUS REPAIR OF NR 5 SLAT, RT WING NR 5 SLAT 7 INCH BY 8 INCH AT OUTBOARD END. REPAIR PCW IAW SRM 57-43-01. (M)SDR 05FDEA01183Support Angle · crackedLEFT WING KRUEGER FLAP SUPPORT ANGLE ON WEB IS CRACKED REF N00164. REMOVED DAMAGE AREA, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR IAW SRM 51-71-40.SDR 05FDEA01180Panel · crackedOUTBOARD LANDING LEADING EDGE SLAT INBOARD PANEL 523BB NEXT TO PYLON LANDING IS CRACKED ON CORNER REF N00643. REMOVED AND FABRICATED & INSTALLED NEW LANDING IAW DRW A57248771 AND SRM 51-40-21.SDR AWXA200500582Wedge · delaminatedMCN- FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 5 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT ASDR AWXA200500581Wedge · delaminatedMCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 4 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 4 SLAT SDR AWXA200500579Wedge · delaminatedMCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 6 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT SDR ASAA0580216Rib · crackedDURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M)SDR USAA050543Skin · crackedCLT - FOUND SKIN CRACKED .125 INCH, NR 6 SLAT AFT ROW OF RIVETS AT NR 6 SLAT INBOARD AUX TRACK. INSTALLED DOUBLER, SDA UPDATED IAW SRM 57-43-01 FIG 206. (M)SDR 05FDEA01064Vane · chafedRIGHT FLAP VANE LEADING EDGE HAS 2 CHAFED AREAS. REMOVED RT WING FLAP VANE IAW A310-200 AMM 27-50-15-4. COMPLIED WITH EA 6-5750-87216. INSTALLED RT FLAP VANE IAW A310-200 AMM 27-50-15-4. OPS CHECKED GOOD IAW A310-200 AMM 27-54-00-5.SDR 05FDEA01049Skin · chafedLEFT WING: LEADING EDGE SLAT NR 1 INBOARD AREA LOWER SURFACE FOUND WITH CHAFFING MARK ABOVE SLAT TRACK NR 1. (OPEN)SDR DHL2005741544Skin · dentedDENT WAS EVALUATED AND FOUND BEYOND ALLOWABLE LIMITS IAW B727 SRM 57-50-1 FIG 2. REPAIRED IAW SRM.SDR DHL2005741543Skin · dentedFOUND DENT TO BE OUT OF LIMITS ON NR 5 SLAT L/E SKIN WS 330- 357 IAW B727 SRM 57-50-1 FIG 2. REPAIRED IAW SRM.SDR 05FDEA01041Skin · puncturedLT WING, PUNCTURED LEADING EDGE SLAT NR 6 AFT FACE SKIN. REPAIRED PER SRM 57-10-00 VOLUME I, FIGURE 1.SDR DHL2005783510Skin · misrepairedACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON NR 2 SLAT AT WS600 PER ASTAR JC FCD500001-018-B. PREVIOUS REPAIR FOUND TO BE NON-COMPLAINT IAW 727 SRM 57-50-3 FIG 1. FABRICATED DOUBLER USING 2024T3 .080 PO NR 9002012 DIM. 9 1/2" BY 7 3/4" IAW B727 SRM 57-50-SDR DHL2005741546Rib · chafedNR 1 SLAT ACTUATOR ROD END BOLT CHAFING AGAINST I/B SLAT RIB. REMOVED DAMAGED I/B RIB IAW B727 SRM 51-30-2. DRILLED, TREATED, PRIMED RIB AND AREA IAW B727 SRM 51-30-2 AND 51-10-2. INSTALLED I/B RIB IAW B727 SRM 51-30-2 PO 5096329 P/N 65-17327-3.SDR DHL2005741547Rib · crackedNR 4 SLAT I/B & O/B ROD END ATTACH RIBS CRACKED. REMOVED DAMAGED PARTS AND INSTALLED NEW IAW B727 SRM 51-30-2, AREA NR 4 SLAT I/B & O/B ROD END ATTACH RIBS. P/N 65-17276U11, PO 5079120 AND P/N 65-17276-9, PO 5079118.SDR DHL2005741508Skin · dentedNR 3 SLAT EXTERIOR SKIN DENTED WS 500-519. CUTOUT DAMAGED SKIN (20" BY 19") AN DAMAGED HEAT SHIELD (16" BY 9"). FABRICATED REPAIR PARTS, SKIN 2024-T3, PO NR 9002235(20: X 19") HEAT SHIELD- 2024-T3 .025, PO NR 9001660 (16' BY 9"). SPLICES (2 EA) 2024-T3,.090SDR DHL2005740501Rib · crackedNR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INBD AND OUTBD RIBS CRACKED NDT CONFIRMED. REMOVED AND REINSTALLED NR 5 SLAT PER 727 MM 27-81-11. OPS CHECKED OK IAW B727 MM 27-81-00. FAB Z NEW RIBS FROM 2024T3 .0140 PO NR 9002012 SIZE 15 1/8" BY 5 1/8" IAW B727 SSDR DHL2005782572Attach Fitting · crackedNR 5 SLAT ACTUATOR ATTACH POINT IS CRACKED INSIDE SLAT. DISCONNECTED NR 5 SLAT ACTUATOR FOR ACCESS IAW 727 MM 27-81-22. OPENED SLAT INNER SKIN IAW 727 SRM 51-30-2. REMOVED DAMAGED PART AND FABBED FROM 2024T3 .071 PO 9001978 DIM 12 X 4.5 INCH IAW 727 SRM 57-SDR QXEA200500758Panel · chafedYYC - LEFT WING INBOARD FLAP VANE LEADING EDGE PANEL HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01, 51-21-11-001-001-A01, AND 51-25-01-001-001-A01.SDR SWAA051028Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT INBOARD & OUTBOARD AUX TRACK CUTOUTS CRACKED. REPAIRED SLAT PER SWA EA & SRM.SDR C1HA200595002Skin · crackedLEFT WING - L/E NR 3 SLAT AT O/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 NDT VERIFIESDR C1HA200595001Skin · crackedLEFT WING - L/E NR 3 SLAT AT I/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 REQUEST NDTSDR AWXA200500488Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 54 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 46.6 TO SS 63.3; FABRICATED A CORE FILLER AND SDR AWXA200500487Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 84 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 74.5 TO SS 94.4; FABRICATED A CORE FILLER AND SDR AWXA200500464Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 2 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT OUTBOARD END BETWEEN SLAT STA 250.9 AND SLAT STA 254.4 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 2 SLAT WEDGE FROM SS 2SDR AWXA200500463Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 1 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT SLAT STA 348 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 1 SLAT WEDGE FROM SS 343 TO SS 350 LT; FABRICATED A CORE FILLER SDR AWXA200500462Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 4 SLAT WEDGE WAS DELAMINATED AT THE BOTTOM OUTBOARD END BETWEEN SLAT STA 120-124 RT. MAINTENANCE REMOVED DAMAGE IN LOWER SURFACE SKIN OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLASDR 2005UALA00278Skin · delaminatedSLAT NR 6 TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT. LEADING EDGE PANELS DAMAGED AFT OF THE NR 6 SLAT. DELAMINATION OF SLAT'S TRAILING WEDGE (INDUSTRY PROBLEM). WEDGE DAMAGED LEADING EDGE PANELS PRIOR TO DEPARTURE. NEW NR 6 LEADING EDGE SLAT INSTALLED. LESDR 05FDEA00777Fitting · crackedLT WING O/B FLAP HAS CRACK ON STRUCTURE AT STOP BOLT. LT WING O/B FLAP CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERRED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01 VOL II. MAJOR CLASSIFICATION AS PER GMM 6-2-100.SDR USAA050571Structure · damagedCLT - FOUND NR 1 SLAT, NR 1 SLAT LOWER NOSE SURFACE T/E AT AFT ROW OF FASTENERS. REPAIR PCW IAW SRM 57-43-01. (M)SDR USAA050476Skin · delaminatedPIT - FOUND NR 4 SLAT DELAMINATED 3 INCH BY 6 INCH AREA, NR 4 SLAT UPPER INBOARD CORNER. BOEING SRM REPAIR 17 PER 51-70-10. (M)SDR AWXA200500478Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER AND LOWER SURFACE OF NR 4 SLAT WEDGE DELAMINATED AT SS 59 RT. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT WEDGE FROM SS 57 TO SS 61 RT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B73SDR QXEA200500566Slat · gougedYYC - LEFTHAND WING LEADING EDGE SLAT NR 1 TRAILING EDGE IS GOUGED AT SS60. REPAIRED IAW HORIZON AIR EA R-57-100 AND REO 690-57-42-001.SDR DHL2005740522Skin · dentedNR 1 SLAT EXTERNAL SKIN DENTED AT W STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS. CUTOUT DAMAGED AREA FROM EXT SKIN 3.25 INCH BY 3.125 INCH, TRIMMED OUT SKIN AND ACCESS TO DOUBLER IAW SRM. FAB PARTS FILLER 3 .125 INCH BY 3.0625 MAT 2024 2024 T3SDR DHL2005740012Rib · crackedNR 4 SLAT CRACKED AT ACTUATOR I/B RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727MM 27-81-11, REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2, FABRICATED NEW RIBS I/B AND O/B MAT USED 2024T3 .040SDR DHL200574011Skin · damagedNR 1 SLAT EXTERNAL SKIN DENTED AT WING STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS IAW B727 SRM 51-30-2 CUT OUT DAMAGE AREA FROM SKIN. TRIMMED OUT SKIN TO ACCESS DOUBLER IAW B727 SRM 57-30-3. FABBED FILLER. DOUBLER 3 PIECES IAW B727 SRM 57-50SDR DHL2005740010Rib · damagedNR 4 SLAT CRACKED AT ACTUATOR IB RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727 MM 27-81-11. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2. FABRICATED NEW RIBS IB AND OB MAT USED 2024T3 .04SDR SWAA050903Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0540195Skin · delaminatedRT NR 5 SLAT IB T/E IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)SDR DHL2005782562Skin · dentedNR 2 LE SLAT EXTERNAL SKIN HAS DENT WS 684.3 (AREA MARKED). DENT AT WS 684.3 ON NR 2 SLAT SKIN OUT OF LIMITS A.9/Y.032=28.1 IAW B727 SRM 57-50-1 FIG 1. CUT OUT DAMAGE AREA SIZE 1" BY 1" IAW B727 SRM 57-50-1. FABRICATED DOUBLER REPAIR USING 2024T3 .080 PO NRSDR UIEA200500025Skin · crackedDURING INSPECTION, NR 16 KRUEGER FLAP, FOUND CRACK AT PANEL ATTACH FASTENER HOLE. TRIMMED OUT AFFECTED SPAR SEGMENT. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDIION. INSTALLED REPAIR FILLER AND ALUMINUM REPAIR ANGLE WITH ADDITIONAL FASTENERS. REFINISDR ASAA0540184Wedge · delaminatedOKC - FOUND LEFT WING NR 2 L/E NR 2 SLAT T/E WEDGE IS DELAMINATED AT OUTBOARD END AND EDGE POTTING DETERIORATED AT THE INBOARD END. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M)SDR ASAA0540182Wedge · delaminatedOKC - FOUND RIGHT WING NR 4 L/E SLAT INBOARD SIDE OF TRAILING EDGE WEDGE HAS SLIGHT DELAMINATION AND INBOARD AND OUTBOARD EDGE POTTING IS DETERIORATED. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M)SDR USAA050482Skin · damagedBFM - FOUND SLAT WITH DAMAGED AREA, 9 INCHES LONG BY 3.75 INCH WIDE BY .380 INCHES DEEP, RT NR 5 SLAT L/E. CUT OUT DAMAGE AND INSTALLED NOSE SKIN REPAIR PER SRM 57-40-00 FIG 204, SHT 3 AND EA 96392. (M)SDR DHL2005782545Skin · crackedNR 6 SLAT IB TRACK SEAL CUTOUT CRACKED WS474 R/W L/E. REMOVED NR 6 SLAT ASSY TO FROM IAW B727 W/W 27-81-41. REMOVED FASTENERS AT NR 6 SLAT I/B TRACK SEAL WS 474 R/W L/E FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILL CRACK IAW B727 SRM 51-10-1. HFEC INSP PER NSDR DHL2005782541Skin · dentedDENT ON NR 8 SLAT EXTERNAL SKIN (MARKED). CUT OUT DAMAGE AREA SIZE 1 INCH BY 1 1/2 INCH IAW B727 SRM 57-50-1 FIG 2. FABRICATED DOUBLER REPAIR USING 2024 T3 .080 PO NR 90020125126 DIMENSIONS 6" BY 5" IAW B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. ALODINE AND SDR DHL2005782540Skin · dented4 DENTS ON NR 7 SLAT EXTERNAL SKIN (MARKED). MEASURED 4 DENTS ON NR 7 SLAT IAW B727 SRM 53-30-1 FIG 1 AND FOUND 3 MOST INBOARD DENTS WITHIN LIMITS, A.4/Y.013=30.7, A.2/Y.003=66.6, A.2/Y.002=100 AND OUTBOARD DENT OUT OF LIMITS A.4/Y.O41=9.7. CUT OUT DAMAGED A
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