N741FD
Service difficulty reports · 198
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N741FD' AND registry_match = 'registration' 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 n_number = 'N741FD' AND registry_match = 'registration' 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 FDEA201007092450Floorboard · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 KK IS BROKEN. FABRICATED NEW FLOORBOARD 242 KK IAW DWG SRZ 25-005, REV "H".SDR FDEA201007092449Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD CORNER IS CRACKED AT FRAME 58; LBL 56. FABRICATED NEW MAIN CARGO FLOORBOARD AT FRAME 58, LBL 56 IAW DWG SRZ 25-005, REV "H".SDR FDEA201007092448Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD EAR IS CRACKED AT FRAME 57.2; LBL 97. FABRICATED NEW FLOOR PANEL AT FRAME 57.2, LBL 97 IAW DWG SRZ 25-005, REV "H".SDR FDEA201007092447Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 241 BF IS CRACKED FROM FRAME 31 TO FRAME 34. FABRICATED NEW MAIN CARGO FLOOR PANEL 241 BF IAW DWG SRZ 25-005, REV "H".SDR FDEA201007092457Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL 161 HF IS DENTED ON OVER 85 PERCENT OF THE TOP SURFACE. FABRICATED NEW FLOOR PANEL 161 HF IAW DWG SRZ 25-005, REV "H" AND 25-011, REV "C". REMOVED AND INSTALLED FLOOR PANEL 161 AF IAW AMM 53-10-35-4.SDR FDEA201007092451Floorboard · brokenMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 ZH IS BROKEN.SDR FDEA201007092446Floor Panel · puncturedBULK CARGO COMPARTMENT FLOOR PANEL NR 161 AF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL 161 AF IAW DWG SRZ 25-005, REV "H" AND 25-011, REV "C". REMOVED AND INSTALLED FLOOR PANEL 161 AF IAW AMM 53-10-35-4.SDR FDEA201007082418Stiffener · crackedLT WING T/E CAVITY UNDER PANEL 575 BB; UPPER PANEL SUPPORT IS CRACKED. RIB 6A-RIB 7. REMOVED CRACKED SUPPORT (STIFFENER) AND ADJACENT BRACKET IAW SRM 51-40-21, PARA 7. FABRICATED NEW STIFFENER IAW DWG A57241059 (-200). ALODINED AND PRIMED STIFFENER IAW SRSDR FDEA201007072385Web · crackedAFT CARGO COMPARTMENT DOOR CUTOUT FWD UPPER CLOSEOUT WEB IS CRACKED AT BS 60. REMOVED WEB IAW SRM 51-40-21, PARA 6. LOCATED AND DRILLED NEW WEB P/N A2557381120200 IAW SRM 51-40-44, PG 1. INSTALLED WEB IAW SRM 51-40- 21, PARA 7.SDR FDEA200902190588Strut · overservicedDURING TAKEOFF ROLL ACFT DRIFTED LEFT NWS UNRESPONSIVE REJECTED TAKEOFF AT 90 KTS. FOUND NOSE STRUT TO BE OVERSERVICED, SERVICED NOSE STRUT IAW MM 32-21-14-6. STEERING CHECK'S NORMAL AT THIS TIME. OK FOR SERVICE.SDR 08FDEA01374Splice · corrodedFOUND CORROSION ON SPLICE, C 72, P55-56 LT REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000017/2008 ISS C, APPROVED BY EA 6-5317-115240.SDR 08FDEA01361Fitting · corrodedFOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AND DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710-114882.SDR 08FDEA01360Fitting · corrodedFOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AND DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710-114882.SDR 08FDEA01356Web · damagedTHS - DURING INSTALLATION OF RT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLAING NEW WEB WITH LOCK FASTENERS DAN7-6 IAW RAS/CASA/6544/2008 ISS B, APPROVED BY EA 6-5514-117183.SDR 08FDEA01355Web · damagedTHS -DURING INSTALLATION OF LT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLING NEW WEB WITH LOCK FASTENERS DAN7-6 IAW RAS/CASA/6544/2008 IS B, APPROVED BY EA 6-5514-117183.SDR 08FDEA01354Attach Fitting · corrodedFOUND CORROSION IN PYLON NR 2 REAR ATTACH FITTING. REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLATING), APPROVED BY EA 6-5451-114851.SDR 08FDEA01353Attach Fitting · corrodedFOUND CORROSION IN PYLON NR 1 REAR ATTACH FITTING REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLATING), APPROVED BY EA 6-5451-114851.SDR 08FDEA01352Spar · crackedFOUND CRACKS IN CENTER SPAR WEB VARIOUS LOCATION (HOLE 2, 3, 5, 7) REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING A BUSH IN HOLE 5 IAW RAS057091/022/2007 ISS A, APPROVED BY EA 6-5710-114861.SDR 08FDEA01346Skin · corrodedCORROSION FINDINGS ON EXISTING REPAIR BETWEEN RIB 7-8, AFT OF REAR SPAR LT WING BOTTOM SKIN REPAIR PERFORMED BY RENEWING DOUBLER REPAIR, BLEND OUT CORROSION IAW RAS/BAE/1006289/2008 ISS A, APPROVED BY EA 6-5720-114855.SDR 08FDEA01345Skin · damagedANTI-ROTATING DEVICE CAN NOT BE INSTALLED IAW SB 29-6057 ON LT WING HOLE NR 2 AND NR 4. REPAIR PERFORMED BY ADDITIONAL DRILLING HOLE FOR SECOND FASTENER AND CUTTING ANTI ROTATING DEVICE IAW, TA-SEE53-2008-226024-1, APPROVED BY AND EA 6-2910-115253.SDR 08FDEA01344Skin · wornFOUND ON LT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY RAS/BAE/1006287/2008 ISS A AND EA 6-2910-115253.SDR 08FDEA01343Skin · wornFOUND ON RT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY TA-SEE53-2008-226024-1 AND EA 6-2910-115253.SDR 08FDEA01342Attach Fitting · corrodedCORROSION FINDINGS ON RT ASA ACTUATOR ATTACH FITTING UNDER BUSHING IN OUTER LUG REPAIR PERFORMED BY INCREASING THE HOLE DIAMETER, NDT FOR CRACK FREE AND INSTALLING A BUSH PER DRAWING A576-61546-200 AND A576-61024 IAW RAS/FOK/067/2008 ISS A, APPROVED BY EA 6-57SDR 08FDEA01341Skin · corrodedFOUND ON LT OUTER WING CORROSION ON SKIN INSIDE AROUND HYDRAULIC FITTING HOLES 3 AND 4. REPAIR PERFORMED BY BLEND OUT CORROSION, REPAIR IAW. DRAWING R571-50532 AND INSTALLING A RETAINING PLATE IAW RAS/BAE/1006804/2008 ISS A, APPROVED BY EA 6-5720-117167.SDR 08FDEA01329Skin · damagedFOUND OLD DOUBLER REPAIR ON SLAT NR 1 RT LOWER SKIN BETWEEN TRACK 3 AND RIB 20 WITHOUT DOCUMENTATION. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A DOUBLER IAW RAS/FOK/004/2008 ISS D, APPROVED BY EA 6-5742-114858.SDR 08FDEA01328Skin · chafedFOUND CHAFING MARK ON SLAT NR 1 RT LOWER SKIN. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW RAS/FOK/004/2008 ISS D, APPROVED BY EA 6-5742-114858.SDR 08FDEA01327Skin · damagedFOUND 2 DEEP NICKS ON SLAT NR 1 LT LOWER SKIN, INNER RIB 18. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A DOUBLER IAW RAS/FOK/003/2008, APPROVED BY EA 6-5742-114860.SDR 08FDEA01326Skin · dentedFOUND CHAFING MARK ON SLAT NR 1 LT LOWER SKIN, INNER RIB 20-22. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW RAS/FOK/003/2008, APPROVED BY EA 6-5742-114860.SDR 08FDEA01325Skin · crackedCRACKS FOUND ON PYLON NR 2 AFT FAIRING FWD SKIN PANEL REPAIR PERFORMED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER IAW, RAS/ROHR/0162/2008 , APPROVED BY EA 6-5455-115264.SDR 08FDEA01324Skin · misrepairedIT EXISTS AN OLD RAS/BAE 310/97 FOR A FOLDING NOSE REPAIR ON SLAT NR 1 RT. THE EXISTING REPAIR ARE NOT PERFORMED IAW RAS. REPAIR PERFORMED BY PERFORMING SB A300-57-6067 ON SLAT NR 1 FOLDING NOSE, APPROVED BY EA 6-5742-117181.SDR 08FDEA01323Skin · misrepairedIT EXISTS AN OLD RAS/BAE.310/97 FOR A FOLDING NOSE REPAIR ON SLAT NR 1 LT. THE EXISTING REPAIR ARE NOT PERFORMED IAW RAS REPAIR PERFORMED BY PERFORMING SB A300-57-6067 ON SLAT NR 1 FOLDING NOSE, APPROVED BY EA 6-5742-117181.SDR 08FDEA01322Skin · dentedFOUND A DENT WITH TOOLING MARK BETWEEN C42-43, P10-11 LT REPAIR PERFORMED BY CUT OFF AFFECTED SKIN PART AND INSTALLING A INTERNAL DOUBLER IAW DRAWING R539-71110 AND SRM 53-10-14 FIG.201, APPROVED BY RAS/EFW/9000012/2008 ISS B AND EA 6-5315-114872.SDR 08FDEA01288Skin · crackedSPOILER NR 3 LT WAS DAMAGED (CRACKED AND DELAMINATED) AT INBOARD AND OUTBOARD END DURING DELIVERY. REPAIR PERFORMED BY REMOVING OF DAMAGED TOP SKIN PLIES AND REPAIR AS PER SRM 57-72-11 FIG 205, APPROVED BYB RAS/BABRE/7009341/2008 ISS A AND EA 6-5772-117182.SDR 08FDEA01287Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 3 LT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276151.SDR 08FDEA01286Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 5 LT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276153.SDR 08FDEA01285Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 4 RT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276151.SDR 08FDEA01284Skin · delaminatedFOUND DELAMINATION ON SPOILER NR 5 RT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276153.SDR 08FDEA01282Doubler · corrodedFOUND CORROSION ON ANTENNA DOUBLER NEAR C 65, P56-57 LT. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK AND FLAP PENNING IAW RAS/EFW/9000031/2008 ISS A, APPROVED BY EA 6-5317-117175.SDR 08FDEA01267Plate · delaminatedFOUND ON RUDDER LIGHTNING PLATE CORRODED AND DISBONDED. REPAIR PERFORMED BY LAMINATING AND INSTALLING A NEW LIGHTNING PLATE IAW RAS/DAHAM/4024036/2007 ISS A, APPROVED BY EA 6-5540-114862.SDR 08FDEA01266Plate · delaminatedFOUND ON RUDDER LIGHTNING PLATE CORRODED AND DISBONDED. REPAIR PERFORMED LAMINATING AND INSTALLING A NEW LIGHTNING PLATE IAW RAS/DAHAM/4024036/2007 ISSA, APPROVED BY EA 6-5540-114862.SDR 08FDEA01259Beam · damagedON AFT CARGO DOOR SILL BEAM A HOLE WAS MISDRILLED, AT C 59-59A. REPAIR PERFORMED BY FREEZE PLUG INSTALLATION WITH SHOULDERED BUSHING IAW. RAS/9000023/2008 ISS. A, APPROVED BY EA 6-5317-115265.SDR 08FDEA01257Spar · damagedFOUND OVERSIZED HOLE ON PYLON NR 2 LOWER SPAR, BETWEEN RIB 12-18. REPAIR PERFORMED BY BORING THE HOLE TO 21,5 MM, FREEZE INSTALLATION OF SHOULDERED BUSH IAW RAS 70503539/004/2008 AND REPAIR DRAWING R546-10338, APPROVED BY EA 6-5451-114870.SDR 08FDEA01254Skin · damagedFOUND IMPACT/TOOLING MARKS ON SKIN AT STRINGER 4 RT, C 83-84. REPAIR PERFORMED BY REWORK OF DAMAGE TO SMOOTH CONTOUR, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000016/2008 ISS A, APPROVED BY EA 6-5319-114883.SDR 08FDEA01252Stringer · corrodedFOUND CORROSION AT STRINGER 56LT, P54.3-57.2. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000014/2008 ISS A, APPROVED BY EA 6-5316-114880.SDR 08FDEA01251Stringer · corrodedFOUND CORROSION ON STRINGER P 56 LT, C 76-78. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000015/2008 ISS A, APPROVED BY EA 6-5318-114879.SDR 08FDEA01207Stringer · chafedFOUND VENT TANK CHAFING MARKS AROUND NACA OPENING (INBOARD RIB 28, STRINGER 17A AND REAR STIFFENER) ON LT WING. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND NDT FOR CRACK FREE IAW RAS/BAE/1006860/2008 ISS A, APPROVED BY EA 6-5720-117169.SDR 08FDEA01146Rib · damagedDURING SB 28-6028 EMBODIMENT, 2 HOLES WERE MIS-DRILLED IN RIB 2 AFT WEB, BOTH WINGS. REPAIR PERFORMED BY INSTALLATION OF RIVETS TO FILL MIS-DRILLED HOLES, WITH REMAINING ACTIONS AS PER SB, ALL IAW EA6-5720-115257 AND RAS/BAE/1006544/2008 ISSUE A.SDR 08FDEA01076Fitting · corrodedFOUND CORROSION ON FITTING AT KRUEGER FLAP AREA LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA01075Skin · corrodedFOUND CORROSION ON BOTTOM SKIN AT RIB 4 REAR SPAR AREA. REPAIR PERFORMED BY REWORK OF CORRODED AREA IAW RAS/BAE/1006318/2008, APPROVED BY EA 6-5720-114866.SDR 08FDEA01074Skin · corrodedFOUND OLD CORROSION REPAIR UNDER STATIC DISCHARGER, LT WING TIP WITHOUT DOCUMENTATION REPAIR PERFORMED BY BLEND OUT CORROSION AND INSTALLING A REPAIR PATCH IAW RAS/FOK/016/2008 ISS A, APPROVED BY EA 6-5730-114884.
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