N730FD
Service difficulty reports · 213
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 = 'N730FD' 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 = 'N730FD' 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 FDEA201006031789Panel · damagedMLG WHEEL WELL KEEL BEAM BOX CAT WALK PANEL LOCATED AT THE CTR OF THE KEEL BEAM HAS THE FWD LT AND RT FASTENER HOLES DAMAGED. FABRICATED NEW MLG W/W KEEL BEAM CAT WALK PANEL 147 BF IAW DWG SRZ 25-005, REV "H". PART MARKED PANEL REF DWG SRZ 25-005, REV "H". SDR FDEA201006031788Panel · damagedBULK CARGO PIT SLANT PANEL 162 LW IS CRACKED AND PUNCTURED. FABRICATED NEW BULK CARGO PIT SLANT PANEL 162 LW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".SDR FDEA201006031787Panel · dentedBULK CARGO PIT SLANT PANEL 161LW HAS MULTIPLE DENTS. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 LW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".SDR FDEA201006031786Panel · dentedBULK CARGO PIT SLANT PANEL 161AW HAS MULTIPLE DENTS. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 AW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".SDR FDEA201006031785Panel · damagedBULK CARGO PIT SLANT PANEL 161GW HAS MULTIPLE DENTS AND IS DELAMINATED. FABRICATED PANEL 161 CW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".SDR FDEA201006031784Panel · damagedBULK CARGO PIT SLANT PANEL 161CW HAS MULTIPLE DENTS AND THE BACK IS CORRODED. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 CW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".SDR FDEA201006021766Shaft · corrodedRUDDER VARABLE STOP LEVER ATTACHMENT SHAFT IS CORRODED AND THE PLATING IS PEELING - RT SIDE. REMOVED RUDDER VARIABLE STOP UNIT IAW AMM 27-23-22-4. REMOVED SHAFT IAW CMM 27-23-22, PG 3010. REMOVED CORROSION FROM SHAFT IAW CMM 27-23-22. MEASURED WALL THICKNESDR FDEA201005281693Seal Depressor · corrodedAFT CARGO COMPT. LOWER DOOR SILL SEAL DEPRESSOR ABOVE NR 2 CARGO DOOR LOCK FITTING IS CORRODED. REMOVED SEAL DEPRESSOR IAW SRM 51-40-21, PARA 5. INSTALLED NEW SEAL DEPRESSOR PN A5397822421600 IAW SRM 51-40-21, PARA 5.SDR FDEA201005281692Profile · corrodedFWD.CARGO COMPARTMENT BALLMAT 131YG AFT PROFILE IS CORRODED. (PARTS RACK) REMOVED PROFILE IAW SRM 51-40-21 PARA 6 AND 51-72-10, LOCATED AND DRILLED IAW SRM 51-72-10, INSTALLED NEW PROFILE PN A2577186320600 PO 683083.1 IAW SRM 51-40-21 PARA 6,13 AND 51-72-10 ANSDR FDEA201005261697Flange · corrodedLOWER FUSELAGE FRESH WATER SERVICE PANEL CAVITY WATER QUANTITY GAGE FRAME, CORRODED FR 38.1 - FR 38.2, STGR. 45 - STGR. 47 REMOVED PRESSURE GAGE FLANGE IAW SRM 51-40-21, PARA 5, PG 7. RECEIVED EA NR 6-3810-136658. REMOVED CORROSION IAW SRM 51-74-10, PARA B SDR FDEA201005261696Flange · corrodedLOWER FUSELAGE FRESH WATER SERVICE PANEL CAVITY WATER PRESSURE GAGE FRAME CORRODED FR.38.1 - FR.38.2, STGR. 45 - STGR. 47. REMOVED PRESSURE GAGE FLANGE IAW SRM 51-40-21, PARA 5, PG 7. RECEIVED EA NR 6-3810-136658. REMOVED CORROSION IAW SRM 51-74-10, PARA B SDR FDEA201005261695Frame · crackedLT SIDE FR 40 CTR WING JOINT - MIDDLE HOLE HAS 2 CRACK INDICATIONS, BEGINNING APPROX .25 IN. FROM INBD FACE OF FR 40 TO APPROX .5 IN. INSIDE HOLE. APPEARS INDICATIONS ARE CONFINED TO FR 40 LAYER ONLY. INDICATIONS APPROX 8-9 O-CLOCK AS VIEWED FACING OTBD FRSDR FDEA201005251636Angle · corrodedAFT CARGO COMPARTMENT FWD LOWER CORNER DOOR SILL ANGLE SEAL DEPRESSOR IS CORRODED. R & R LOWER FWD CORNER SEAL DEPRESSOR, PO 682786.1 IAW SRM 51-72-10, PG 2 AND SRM 51-40-21, PARA 5. ALODINED AND PRIMED AREA IAW SRM 51-71-10, PG 1 AND PAINTED IAW SRM 51-75-10SDR FDEA201005251635Stringer · corrodedCORROSION ON FUSELAGE INTERNAL STRUCTURE BETWEEN FRAME 38.2 AND FRAME 39; BELOW THE OTBD HOT AIR VALVE. (STR 44R TO STR 44R) REMOVED CORRODED STRINGER IAW SRM 51-40-21, PARA 6 & 7. FABBED STRINGER AND COUPLING IAW SRM 53-10-14, FIG 201, PGS 203 / 204. ALSDR FDEA201005241622Skin · dentedR-1 DOOR LOWER FWD CORNER EXTERNAL SKIN IS DENTED/ BENT. MEASURED DEPTH OF DENT (D) D = 0.060. MEASURED LOCATION OF MAX DEPTH OF DENT, ADJACENT TO STIFFENER EDGE (A) A = 0.2. MAX ALLOWED DENT IS 2 PERCENT OF (A). DENT IS OUT OF LIMITS IAW SRM 52-10-0, FIG SDR FDEA201005241621Attach Angle · corrodedAVIONICS COMPARTMENT ATTACH ANGLE IS CRACKED AT FRAME 10; LBL 30. REMOVED ANGLE AND INSTALLED NEW ANGLE PN A5361235620100, PO 682607.3 IAW SRM 51-40-21, PARA 6 & 7.SDR FDEA201005241620Attach Angle · crackedAVIONICS COMPARTMENT ATTACH ANGLE IS CRACKED AT FRAME 10; RBL 30. REMOVED ANGLE AND INSTALLED NEW ANGLE PN A5361235620100, PO 682607.2 IAW SRM 51-40-21, PARA 6 & 7.SDR FDEA201005241623Floor Panel · damagedMAIN CABIN FLOOR PANEL 241 UF FABRICATED FLOOR PANEL 241 UF IAW DWG SRZ 25-005, REV "H".SDR FDEA201005211609Floor Panel · crackedMAIN CABIN FLOOR PANEL FROM FRAME 52 TO FRAME 54 IS CRACKED; PANEL 242 TG. FABRICATED MAIN CABIN FLOOR PANEL IAW DWG SRZ 25-005, REV "H". PO 679619.1SDR FDEA201005211608Floor Panel · damagedFWD CARGO COMPARTMENT FLOORBOARD 131RF HAS EDGE DAMAGE. REPAIRED WITH FILLER FWD CARGO COMPARTMENT FLOORBOARD 131 RF PER A300-600 SRM 53-10-20, FIG 201, PG 205.SDR FDEA201005211607Floor Panel · corrodedBULK CARGO COMPARTMENT FLOOR BOARD 161 HF TOP SURFACE IS CORRODED. REMOVED CORROSION, OUT OF LIMITS. ORIGINAL THICKNESS 0.063. REMOVED 0.025. REMAINING 0.038 FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. FABBED NEW TOP SKIN IAW DWG SRZ 25-011, REC "C". MATESDR FDEA201005211606Coupling · corrodedCORROSION ON FUSELAGE INTERNAL STRUCTURE AT THE END FITTING AND BASE OF FRAME 39, PRESSURE BULKHEAD BELOW THE INBD COLD AIR MANIFOLD CHECK VALVE. REMOVED PROFILE IAW SRM 51-40-21. REMOVED 2 EA COUPLINGS IAW SRM 51-40-21, PARA 6&7. REMOVED CORROSION IAW SRM SDR FDEA201005211605Support Angle · crackedAVIONICS COMPARTMENT BATTERY RACK LONGITUDINAL SUPPORT ANGLE IS CRACKED FROM FRAME 15 TO FRAME 17. REMOVED ALL ACFT BATTERIES IAW AMM 24-31-11-4. REMOVED DRIP COVER SUPPORT WITH DRIP COVER IAW SRM 51-40-21, PARA 5, PG 7. REMOVED SUPPORT ANGLE IAW SRM 51-40-2SDR FDEA201005171557Fitting · crackedMAIN CABIN UNDER FLOOR PANEL FLOOR SUPPORT FITTING IS CRACKED AT FRAME 49, RBL 57. REPLACED FLOOR SUPPORT LINK IAW SRM 51-72-10, PGS 1-4.SDR FDEA201005171556Support Fitting · crackedMAIN CABIN LT SIDE UNDER FLOOR SUPPORT FITTING IS CRACKED AT FRAME 48, LBL 57. REMOVED CRACKED LINK AND INSTALLED NEW LINK IAW SRM 51-72-10, PARA 6, PG 2.SDR FDEA201005171555Support Fitting · crackedMAIN CABIN LT SIDE UNDER FLOOR SUPPORT FITTING IS CRACKED AT FRAME 49, LBL 57. REMOVED CRACKED LINK AND INSTALLED NEW LINK IAW SRM 51-72-10, PARA 6, PG 2.SDR FDEA201005171553Skin · damagedRT WING, (2) HOLES INBD OF RIB 9 SKIN PANEL THAT ARE COMMON TO THE ATTACH ANGLE SHOW CRACK INDICATIONS IN THE FWD AND AFT DIRECTIONS. PERFORMED REPAIR IAW DWG R57340199, EA 6-5710-136653.SDR FDEA201005171552Skin · crackedLT WING T/E AREA BOTTOM SKIN IS CRACKED FROM RIB 8 TO RIB 9. PERFORMED REPAIR IAW DWG R57340199, EA 6-5710-136653.SDR FDEA201004061076Outflow Valve · malfunctionedDURING CLIMB OUT,PASSING ABOUT FL280,RECEIVED RT CABIN DOOR WARNING LIGHT,AFTER PUSHING DOOR HANDLE THE DOOR WARNING LIGHT WENT OUT,BUT THE CABIN PRESSURE CONTINUED TO CLIMB TO 10,000,RESULTING IN A CABIN PRESS WARNING. PERFORMED BITE TEST OF NR 2 CABIN SDR FDEA201003240974Probe · odorSHORTLY AFTER TO F/O'S TAT FAULTED THERE IS A FAINT BURNING SMELL. RELEASED FOR SERVICE IAW MEL: 30-31-05-B, CATEGORY: C EXPIRATION: 03APR10 "MEL 30-31-05-B: F/O TAT PROBE HEAT- INOP. OBSERVE TAT ON ECAM MEMO PAGE." ITEM CURRENTLY HAS MEL ISSUED. DURING TROSDR FDEA201002180454Seal · dislodgedON TAKEOFF, CAPT'S WINDOW WAS VERY LOUD. SOUNDS LIKE NOT SEALED. ON INSP FOUND SEAL PROTRUDING FROM BOTTOM EDGE OF WINDOW FRAME INSPECTED SEAL FOR CUTS NONE NOTED. INSPECTED WINDOW FRAME FOR DEBRIS NONE NOTED SUSPECT SEAL WAS PINCHED AT DOOR CLOSING. REASDR FDEA200904131287Gearbox · malfunctionedON APPROACH, LOWERED FLAP HANDLE TO 15/20, RECIEVED ECAM ALERT " FLAPS SYS 1&2 FAULT" RECYCLED TO 15/15 & FAULT CLEARED. FLAPS FAULTED AGAIN WHEN LOWERED TO 15/20. FLAP POSITION APPROX 19 DEG. POSITIONED FLAPS TO 15/15 PER QRH. ON APPROACH WHEN HANDLE AT 3SDR FDEA200903271095Controller · failedON FINAL WHEN MOVING FROM FLAP 20 TO FLAP 40 THE FLAPS STUCK AT 20. RECYCLE WITH NO HELP. LANDED WITH FLAPS 30/20. REMOVED AND REPLACED NR 1 SFCC IN REF TO MM 27-51-18-4 , CYCLED SLAT/FLAPS NO FAULTS NOTED, OK FOR SERVICE.SDR FDEA200812215255Autothrottle Sys · malfunctionedABORTED T/O DUE TO LARGE SPLIT IN THROTTLE LEVERS ( APROX 2 KNOBS WIDTH) NORMAL ACCELERATION ON NR 1. NR 2 LAGGED BEHIND WITH ENG INDICATORS ON NR 2 ALSO SLOW AND BEHIND NR 1. ABORTED T/O AT APPROX 60 KTS. RETURNED FOR TAKEOFF THIS TIME WITH TOGA ENGAGED. THSDR 08FDEA03856Cabin Pressure · failedSHORTLY AFTER TAKEOFF CABIN PRESS 1 AND 2 FAILED. MANUAL PRESSURE WORKED OK. TROUBLESHOT REF TSM 21-31-00. PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM REF MM 21-31-00-5. OPS CHECK NORMAL. NO DEFECTS NOTED.SDR 08FDEA01437Skin · wornHYDRAULIC LINES IN WING WORN OUT. REPAIR PERFORMED IAW SB 29-6057 (INSTALLATION OF ANTI-ROTATING DEVICES) ON BOTH WINGS, RIB 8-9.SDR 08FDEA01436Skin · wornSEVERAL HOLES ELONGATED ON LT WING BOTTOM SKIN AND SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (REAM UP AND BUSHING INSTALLATION) IAW RAS/BAE/1006453/2008 ISS A, APPROVED BY EA 6-2910-115254.SDR 08FDEA01412Spar · crackedFOUND CRACK ON PYLON LOWER SPAR CENTER STIFFENER RIB 10 REPAIR PERFORMED IAW, DRAWING R546-10340 AND SB 54-6019, APPROVED BY RAS/AS/0029/2008 ISS A AND EA 6-5450-117165.SDR 08FDEA01410Skin · dentedFOUND DENTS ON LEADING EDGE SLAT NR 3 RT FLUSH DOUBLER REPAIR PERFORMED IAW RAS/FOK/022/2008, APPROVED BY EA 6-5744-115245.SDR 08FDEA01405Fitting · damagedFOUND ON C 47 LOWER JUNCTION FITTING ON SEVERAL HOLES (HOLE 3, 4, 5, 36, 40, 42, 160, 165, 169) DAMAGES REPAIR PERFORMED BY OVERSIZING THE HOLES, COLD WORKING AND INSTALLING BUSHES IF NECESSARY IAW RAS 70503594/042/2008, APPROVED BY EA 6-5710-115255.SDR 08FDEA01403Fitting · damagedFOUND ON C 47 LOWER JUNCTION FITTING ON SEVERAL HOLES (HOLE 8, 5, 6, 41, 161) DAMAGES REPAIR PERFORMED BY OVERSIZING THE HOLES, COLD WORKING AND INSTALLING BUSHES IF NECESSARY IAW RAS 70503594/042/2008, APPROVED BY EA 6-5710-115255.SDR 08FDEA01402Skin · dentedFOUND DENTS ON SLAT NR 3 RT ON LEADING EDGE, RIB 34-35. REPAIR PERFORMED BY INSTALLATION OF A FLUSH DOUBLER IAW RAS/FOK/022/2008 ISS A, APPROVED BY EA 6-5744-115245.SDR 08FDEA01378Rib · damagedFOLDING SLAT NR 1 RT , FOUND MISDRILLED HOLE DURING EMBODIMENT OF SB 57-6067 REPAIR PERFORMED DURING EMBODIMENT OF SB 57-6067 BY INSTALLING OVERSIZED BLIND RIVET AND 4,00MM RIVETS IN OFFSET HOLES IAW RAS/BAE/1006919/2008 ISS A, APPROVED BY EA 6-5742-115256.SDR 08FDEA01377Panel · crackedFOLDING NOSE SLAT NR 1 LT WITH CRACK FINDINGS REPAIR PERFORMED BY PERFORMING SB 57-6067 (INNER PAN REPLACEMENT).SDR 08FDEA01373Spoiler Panel · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 4 LT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51.SDR 08FDEA01372Spoiler Panel · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 3 LT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51.SDR 08FDEA01371Spoiler Panel · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 5 RT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-53.SDR 08FDEA01370Spoiler Panel · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 4 RT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51.SDR 08FDEA01369Skin · delaminatedFOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51.SDR 08FDEA01357Skin · delaminatedDELAMINATION OUT OF LIMIT FOUND ON SPOILER NR 5 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53 PB 400.
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