N740FD
Service difficulty reports · 156
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 = 'N740FD' 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 = 'N740FD' 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 FDEA200903030834Skin · delaminatedRIGHT WING UPPER SKIN EXTERIOR SURFACE T/E AREA HAS COMPOSITE LAYERS PEELING BETWEEN RIB 1 AND RIB 2. REPAIRED THE RIGHT WING UPPER SKIN BY REMOVING THE DAMAGE, POTTING THE PANEL AND THE HONEY COMB CORE. APPLYING FIBERGLASS OVERLAYS AND CURING IAW A300-600 SSDR FDEA200903030814Retainer · gougedNR 2 ENGINE OTBD T/R NR 2 BLOCKER DOOR REQUIRES REMOVAL OF NEW DOOR TO INSTALL ORIGINAL DOOR PER CUSTOMER REQUEST. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923. REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-SDR FDEA200903020808Intercostal · crackedINTERCOSTAL FLANGE FROM FRAME 86 - FRAME 87, STRINGER 36 IS CRACKED. REMOVED CRACKED FLANGE IAW SRM 51-40-21, PARA 7. LOCATED AND DRILLED NEW FLANGE IAW SRM 51-40-44, PG 1. ALODINED AND PRIMED IAW AMM 51-23-10-0 PARA 1. INSTALLED NEW FLANGE IAW SRM 51-40-2SDR FDEA200903020805Spar · damagedRIGHT INBD FLAP LEADING EDGE SPAR WEB HAS MISDRILLED HOLES ( 2 PLACES ). REMOVED & REPLACED STRUCTURE AS NECESSARY TO GAIN ACCESS TO THE DAMAGED AREA IAW SRM 51-40-21; PG 1; PG 7 AND PG 133. COMPILED WITH E.A. 6-5750-127919 PG 1 & PG 2.SDR FDEA200903020807Duct · crackedLEFT PACK LOWER DUCT FROM THE HEAT EXCHANGER TO THE ACM HAS A CRACK APPROX 1.5 INCH LONG. REMOVED DUCT ASSY AS REQUIRED REF A300-600 AMM 21-51-32. PERFORMED WELD REPAIR REF DRM, PARA 4-C. ACCOMPLISHED FPI REF NTM 51-90-00 PT9 PER EA 6-2150-127942 "AIR CONDSDR FDEA200903020804Retainer · gougedNR 2 ENGINE OTBD T/R 5TH FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923 "EXHAUST SYSTEM - NR 2 ENGINE OTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMM 78-32-1SDR FDEA200903020803Retainer · gougedNR 2 ENGINE OTBD T/R 4TH FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923 "EXHAUST SYSTEM - NR 2 ENGINE OTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMM 78-32-1SDR FDEA200903020802Retainer · gougedNR 2 ENGINE O/B T/R 3RD FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW E.A. 6-7830-127923 " EHHAUST SYSTEM - NR 2 ENGINE OUTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMSDR FDEA200903020801Blocker Door · gougedNR 2 ENGINE OTBD T/R UPPER BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923. REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.SDR FDEA200903020806Skin · crackedTHE RIGHT INBD FLAP SKIN A57960007001 REMOVED ON E 6-5750-7-5003 PT 2 HAS A CRACK AT THE AFT END. COMPLIED WITH EA 6-5720-127917.SDR FDEA200903020800Panel · wornTHE OTBD CORNER UPPER SURFACE IS WORN AT LEFT WING 2ND FROM INBD TRAILING EDGE DROP DOWN PANEL NR 572 CB. REPAIRED OTBD FWD UPPER CORNER OF THE PANEL BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND RESDR FDEA200903020799Panel · delaminatedFOIL IS DISBONDED ON THE UPPER SURFACE OF THE 2ND PANEL FROM INBD, LEFT WING DROP DOWN TRAILING EDGE PANEL NR 572 CB. REPAIRED FLAP DIFFUSER PANEL INNER SKIN BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACSDR FDEA200903020798Panel · delaminatedLEFT WING TRAILING EDGE PANEL NR 572 GB HAS THE TOP LAMINATE PEELING. REPAIRED PANEL NR 572 GB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW DWG SR 27-53-011 AND EA 6-5720-127921.SDR FDEA200903020797Panel · delaminatedLEFT WING TRAILING PANEL NR 572 LB HAS THE TOP SURFACE LAMINATE PEELED. REPAIRED PANEL NR 572 LB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW FEDEX DWG SR 27-53-011 AND FEDEX EA 6-5SDR FDEA200902190589Seat Track · gougedMAIN CARGO DECK SEAT TRACK IS GOUGED BETWEEN FRAME 60 AND FRAME 61, LBL 37.5. REMOVED FLOORBOARD IAW SRM 51-40-20, PG 5. REMOVED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201. LOCATED AND DRILLED NEW SEAT TRACK SECTION P/N A53274005202000, PO 633379.1 AND NESDR FDEA200902170563Rib · damagedWHILE PEFORMING EA 6-5750-5000 PT3 "WINGS - INBD FLAP NOSE RIB 7 REPLACEMENT LT"; SEVERAL HOLES WERE FOUND TO BE ELONGATED. COMPLIED WITH EA 6-5750-127920.SDR FDEA200902170562Attach Bracket · brokenFAIRING 632 BB RIGHT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916.SDR FDEA200902170561Attach Bracket · brokenFAIRING 635 BB LEFT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916. NO FURTHER ACTION IS REQUIRED.SDR FDEA200902170560Attach Bracket · brokenFAIRING 636 BB LEFT AND RIGHT AFT ATTACH BRACKETS, SAFETY WIRE ATTACH POINTS ARE BROKEN. COMPLIED WITH E.A. 6-5750-127916.SDR FDEA200902160553Skin · gougedFUSELAGE EXTERNAL SKIN HAS A GOUGE AT FRAME 20, S39R. REMOVED GOUGE IAW SRM 51-73-10 AND IS FOUND TO BE OUT OF LIMITS IAW SRM 50-10-00. CUTOUT DAMAGE IAW SRM 53-10-12. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED FILLER & DOUSDR 07FDEA00509Skin · crackedFOUND CORROSION ON BOTTOM SKIN, MLG REINFORCING PLATE RT WING. NDT DETECTED A CRACK IN HOLE NR 552. REPAIR WAS PERFORMED IAW RAS/BAE/1003853/2006 ISS.: A AND EA 6-5720-103395.SDR 07FDEA00494Structure · damagedDAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305. HOLES H/I ON LT AND L/K ON RT. REPAIR WAS PERFORMED IAW RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.SDR 07FDEA00493Structure · damagedDAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, HOLES L/U/I/K ON LT AND K ON RT. REPAIR WAS PERFORMED IAW. RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.SDR 07FDEA00491Repair · unknownFOUND OLD REPAIR BY INSTALLATION OVERSIZE FASTENERS, HOLE 2 LT, 187 RT AND 165 RT. REPAIR VERIFICATION OF OVERSIZED FASTENERS IAW RAS 033237/017/2004 ISSUE: A AND EA 6-5710-106363.SDR 07FDEA00486Skin · corrodedOLD REPAIR ON LT SLAT NR 3 LEADING EDGE, BY AN EXTERNAL PATCH, FASTENERS WERE CORRODED AND SOME HOLE DIAMETERS ARE OVERSIZE. REPAIR WAS PERFORMED IAW TD FOK/308/2006 ISSUE A BY EA 6-5744-106357.SDR 07FDEA00485Skin · misrepairedFOUND OLD CORROSION REPAIR ON UPPER WING SKIN LT, CLOSED TO RIB 5. REPAIR WAS VERIEFIED IAW RAS/BAE/0937/2004 ISSUE B AND CAL EO AB6-57-00-0057R1. THE REPAIR DIDN'T CORRESPOND WITH THE DOCUMENTS. THE REPAIR WAS ACCOMPLISHED IN THE FOLLOW DR 456.SDR 07FDEA00482Fitting · corrodedFOUND CORROSION ON CORNER FITTING C63, P43 LT AND ON CROSSBEAM C61, P45 LT AND C58, P47 RT. REPAIR WAS PERFORMED BY REPLACE A NEW FITTING IAW SRM 51-72-10 AND SRM 53-17-15, FIG 5. CROSSBEAM REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 208 SEE ALSO SRM 53-16-15 SDR 07FDEA00481Plate · damagedFOUND OLD REPAIR ON REAR CARGO DOOR SEALING PLATE C60-C60A IN FUSELAGE ABOVE DOOR. OLD REPAIR WAS VERIFICATION THAT IT IS PERFORMED IAW RAS DA/HAM-1083/98 ISSUE B.SDR 07FDEA00460Panel · crackedFOUND CRACK AT PYLON NR 2 RT ON AREA AT LOWER SIDE PANEL AT RIB 18 INBOARD. REPAIR WAS PERFORMED IAW RAS 048245/005/2006 ISSUE: A AND EA 6-5451-103394.SDR 07FDEA00457Stringer · corrodedCORROSION ON MILLED STRINGER P56 RT/LT BETWEEN C76/77 AND ON OUTER SKIN BETWEEN C76/77, FOUND AFTER REMOVING TAIL BUMPER. REPAIR WAS PERFORMED IAW RAS/DATLS/0003476/2006 ISSUE: B AND EA 6-5318-103383.SDR 07FDEA00455Skin · corrodedAFTER REMOVAL OF AN OLD FLUSH DOUBLER BETWEEN C70/71, P45/46 RT, AN OLD CORRODED REWORKED AREA WAS FOUND AT INNER SKIN SHEET. REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 229 SHEET 1 AND SRM 53-10-14, FIG 201 SHEET 1, APPROVED BY EA 6-5317-106349.SDR 07FDEA00378Door · dentedDENT ON RT MAIN LANDING GEAR DOOR. REPAIR WAS PERFORMED IAW RAS 048387/0082006 ISSUE: A, APPROVED BY EA 6-5281-103396.SDR 07FDEA00377Skin · damagedON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS/BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392.SDR 07FDEA00376Door · delaminatedTHE FWD LOWER CORNER OF THE RT NOSE LANDING GEAR DOOR WAS DAMAGED. REPAIR WAS PERFORMED IAW RAS/CASA/5273/2007 ISSUE: A, APPROVED BY EA 6-5282-106412.SDR 07FDEA00361Web · dentedWEB PLATES OF BULK CARGO DOOR TORSION BOX FWD AND AFT C68 BETWEEN P33 AND P36 RH DENTED AND SCRATCHED. REPAIR WAS PERFORMED BY DRESSED BACK DENTS AND REWORK OF AFFECTED WEB PLATES IAW RAS/DAHAM/4021476/2006 AND EA 6-5317-106348.SDR 07FDEA00285Crossbeam · corrodedFOUND CROSS BEAM ATTACHMENT PROFILE (SRM 53-17-15 FIG.10 ITEM 455) AT C61 RT CORRODED REPLACEMENT OF RELATED PART WAS PERFORMED IAW SRM 51-72-10.SDR 07FDEA00284Plate · chafedFOUND CHAFING MARKS ON TORSION PLATE C86 RT. REPLACEMENT WAS PERFORMED IAW SRM 51-72-10.SDR 07FDEA00283Skin · corrodedFOUND CORROSION ON INNER SKIN BETWEEN C55/56 BETWEEN STRINGER 55/56 RT AND 55/56 LT, AND CORROSION ON STRINGER 45 RT BETWEEN C57.3-58 AND STRINGER 51 LT BETWEEN C57.3-58. REPAIR WAS PERFORMED IAW RAS/DATLS/0003480/2006 ISS.A (CORROSION REWORK), APPROVED BY EA SDR 07FDEA00282Stringer · corrodedFOUND CORROSION ON STRINGER P55 LT BETWEEN C69-C70. REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201.SDR 07FDEA00281Bulkhead · damagedTOOLING MARKS FOUND ON AFT PRESSURE BULKHEAD AT ME15, C80/82. REPAIR WAS PERFORMED IAW RAS/DAHAM/4021516/2006 ISS. A (BLEND OUT, FASTENER REPLACEMENT), APPROVED BY EA 6-5319-103386.SDR 07FDEA00280Skin · damagedFOUND SEVERAL SCRUB MARKS ON SKIN PANEL BETWEEN C56-C57, P34-P35 LT AND RT. REPAIR WAS PERFORMED IAW RAS/DATLS/0003483/2006 ISS. A (BLEND OUT), APPROVED BY EA 6-5316-103385.SDR 07FDEA00279Sill · corrodedFOUND CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM A539-73085-210 BETWEEN C 59-63 REPAIR WAS PERFORMED IAW RAS/DATLS/0003479/2006 ISS.A (FLANGE REPAIR AND CORROSION REWORK), APPROVED BY EA 6-5317-103384.SDR 07FDEA00278Beam · corrodedDURING KRUEGER FLAP INSTALLATION, RT WING, FOUND BEAM A535-10218-201 CORRODED REPLACEMENT OF CORRODED BEAM IAW SRM 57-45-11.SDR 07FDEA00277Attach Fitting · corrodedFOUND CORRODED CLIP AT C35 BETWEEN P43-44 LT AND STRINGER P 44 BETWEEN C35-C36, LT CORROSION REPAIR WAS PERFORMED BY REPLACEMENT OF CLIP IAW SRM 51-72-10 AND STRINGER REPAIR IAW SRM 53-10-14 FIG 201.SDR 07FDEA00276Stringer · corrodedFOUND STRINGER P50 LT AT C70 CORRODED STRINGER REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201.SDR 07FDEA00275Sill · corrodedANGLE BRACKET AT DOOR SILL C24A-25 IS DAMAGED AND CORRODED PART WAS REPLACED IAW SRM 51-72-10.SDR 07FDEA00274Stringer · corrodedSTRINGER P50 LT BETWEEN C72 AND C73 CORRODED AND CONNECTION SECTION AT C72, P50 LT CORRODED STRINGER REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201 AND REPLACEMENT OF CORRODED CONNECTING SECTION WAS PERFORMED IAW SRM 51-72-10.SDR 07FDEA00273Crossbeam · noneOLD REPAIRS ON CROSSBEAM C60 WITHOUT ANY OLD RECORDS CROSSBEAM WAS REPLACED BY NEW PART IAW SRM 51-72-10.SDR 07FDEA00272Crossbeam · corrodedFOUND CROSSBEAM ATTACHMENT PROFILE IS CORRODED ON C67 RT REPLACEMENT OF CORRODED PART IAW SRM 51-72-10.SDR 07FDEA00271Stringer · corrodedFOUND CORRODED STRINGER P46RH, C60-C60A REPAIR WAS PERFORMED IAW RAS/DATLS/0003135/2006 ISS.A, STRINGER SPLICE REPAIR WITH DWR 17 R539 70094B), APPROVED ALSO BY EA 6-5317-106347.
Back to N740FD