N732FD
Service difficulty reports · 157
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 = 'N732FD' 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 = 'N732FD' 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 FDEA201206222300Control Panel · failedDURING TAXI OUT, DETECTED AN ACID ODOR (CHEMICAL). RETURNED TO RAMP AND SMOKE DETECTED COMING FROM CENTER CONSOLE BETWEEN RADAR AND ECAM PANEL. FIRE DEPT DETECTED A VERY SMALL HOT SPOT ON RADOME. DISPLACED ECAM CONTROL PANEL AND BOTH IDC'S, INSPECTED WIRESDR FDEA201204061329Valve · failedAT LEVEL OFF, NOTED LEFT OUTER FUEL QUANITY INDICATING LESS THAN THE RT OUTER. LT OUTER TANK FUEL QUANTITY CONTINUED TO DECREASE AT A STEADY RATE. FUEL USED AND STARTING FUEL COMPARISON SHOWED THE CORRECT TOTAL FUEL REMAINING. DIVERTED, ON LANDING LT OUTER QSDR FDEA201203271135Fitting · bentFR47, S24R TO S26R FWD FRAME FITTING UPPER SECTION CHAFED NEAR FASTENER HOLE. COMPLIED WITH EA 6-5710-158251.SDR FDEA201203271134Fitting · damagedFRAME 47 RT SPLICE FITTING (S-24R TO S-26R) HOLE "N" FOUND DAMAGE. COMPLIED WITH EA 6-5710-18255SDR FDEA201203271133Fitting · bentFRAME 47 RT FITTING S-24R TO S-26R. FOUND DAMAGE NEAR HOLE "N" AND HOLE "N" WAS DAMAGE. COMPLIED WITH EA 6-5710-158255.SDR FDEA201203241089Rib · crackedCRACK WAS FOUND AT THE RECUT SPOT FACE HOLE 47 (LT & RT) OF MLG RIB NR 5. COMPLY WITH EA 6-5710-158246.SDR FDEA201203231069Frame · gougedFR47 FRAME FITTING FOUND GOUGE DAMAGE AT THE MACHINE MILL EDGE B/W STR 24L-STR 25L. COMPLIED WITH EO.SDR FDEA201203080817Skin · corrodedLT WING LOWER SKIN DOUBLER EXTERIOR SURFACE CORRODED AT MLG RIB NR 5 LOCATION. REPAIRED IAW EA 6-5730-158253.SDR FDEA201106092172Blades · damagedON CLIMBOUT, HEARD VERY LOUD BANG, ACFT YAWED RT AND NR 2 ENGINE SPOOLED DOWN, NO RED ECAM. NR2 ENG FLUCUATED AT IDLE WITH HIGH EGT FOR ABOUT 30 SECS. ECAM SHOWED NR2 OVERLIMIT BUT GAUGES DID NOT SHOW ANY. ENGINE STABILIZED AT IDLE, LT IT RUNNING THERE, ALOSDR FDEA201007152569Wire Harness · failedON CLIMB OUT PASSING FL 290, NR 2 ENGINE EGT COMPLETELY FAILED ( BOTH DIGITIAL AND ANALOG ) WITH - 2 PERCENT N1 AND N2 FLUX WITH - 200 POUNDS FUEL FLOW FLUX. UPON LANDING AT MEM - BOTH EGT'S WORKED NORMAL. R & R NR 2 ENG LOWER AND UPPER EGT HARNESSES IAW ASDR FDEA201007152515Indicator · failedENROUTE CAPT NOTICED NR2 EGT POINTER BELOW THE ZERO POSITION. DIGITAL READOUT SHOWED (4) GREEN DASHES. R & R NR2 EGT INDICATOR IAW MM 77-21-21-04-0. OPS CHECK GOOD, RAN NR2 ENGINE IAW JRH CHAP 5, ALL INDICATIONS GOOD. ACFT OK TO CONTNIUE FOR SERVICE.SDR FDEA200906031908Engine · leakingON TAKEOFF ROLL JUMP SEATERS DETECTED AN OIL ODOR AND SAW HAZY SMOKE. NOT ELECTRICAL, BUT IRRITATING. DURING CLIMB AND RETURNED TO MEM, ODOR DISSAPATED. 15 INCH OIL PUDDLE UNDER NR 2 ENGINE. COMPLETED INSTALLATION OF NR 2 ENGINE REF WORK CARD 64T0712-2, SDR FDEA200905121637Pressure Switch · failedAT 80KTS ON TAKEOFF RECEIVED NR 2 ENG OIL CLOG ECAM REJECTED TAKEOFF RETURN TO GATE AS SOON AS THROTTLES CLOSED WARNING CEASED. ENG 2 OIL CLOG ON START BUT CEASED W/IN 3 MINS. ACN RELEASED FOR SERVICE PER MEL/CDL: 79-35-01, CATEGORY: B EXPIRATION: 16MAY09 SDR 07FDEA03286Skin Panel · wornELONGATED HOLES ON PYLON NR 1 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 LT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.SDR 07FDEA03285Skin Panel · wornELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.SDR 07FDEA03284Skin Panel · wornELONGATED HOLES ON PYLON NR 2 SUPPORT BRACKET AND LOWER WING SKIN, RIB 7-8 RT. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF FREEZE PLUGS IAW EA 6-2900-106507 AND RAS/BAE/1005210/2007 ISSUE A.SDR 07FDEA03176Frame · corrodedHEAVY CORROSION FOUND ON FRAME 92 AT SEVERAL ANGLE SECTIONS, STRG 14 RT TO 17 LT. REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SRM 51-72-10.SDR 07FDEA03070Fitting · corrodedCORROSION AT FRAME 91 LOWER HIP FITTING RT, LOWER ATTACHMENT LUG REPAIR PERFORMED BY CORROSION REMOVAL AND INSTALLING BUSHING IAW EA 6-5319-112489 AND RAS/DAHAM/022566/2007 ISS D.SDR 07FDEA03045Angle · damagedDAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47 RHS. REPAIR PERFORMED BY OVERSIZING THE HOLES AND CUT OUT THE EXTERNAL FITTING IAW EA 6-5710-112481 AND RAS/053362014/2007 ISS "A".SDR 07FDEA03044Angle · damagedDAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-112481 AND RAS/013359/011/2001 ISS "A" AND RAS/053362014/2007 ISS "A".SDR 07FDEA02978Beam · corrodedAFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT C67-69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERCENT. BEAM SECTION: A539-730057-202 REPAIR PERFORMED BY REPLACEMENT OF BEAM SECTION IAW SRM 51-72-10.SDR 07FDEA02977Structure · corrodedAFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT 69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERCENT. REPAIR PERFORMED BY REPLACEMENT OFF MENTIONED PART IAW SRM 51-72-10.SDR 07FDEA02934Frame · corrodedCORROSION FOUND ON FRAME WEB PLATE ON C92, P15-17 RT REPAIR PERFORMED BY CUT THE WEB AND INSTALL A FILLER AND AN ANGLE IAW EA 6-5319-112477 AND RAS/DAHAM/22468/2007 ISS B.SDR 07FDEA02932Profile · corrodedCORROSION ON STRINGER P56 LHM C76-77, REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10 AND OVERSIZING RIVET HOLES IAW EA 6-5318-106512 A AND RAS/DATLS/0003775/2007 ISS B.SDR 07FDEA02931Skin · corrodedRT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON LOWER SKIN REPAIR PERFORMED BY BLEND OUT THE COROSION IAW SRM 51-74-10, APPROVED BY EA 6-57820-112490 AND RAS/BAE/1005335/2007 ISS A.SDR 07FDEA02930Skin · corrodedLT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON WING SKIN REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10, APPROVED BY EA 6-5720-112490 AND RAS/BAE/100535/2007 ISS A.SDR 07FDEA02928Stringer · crackedCRACKED STRINGER P 9 RT, C97-100 STRINGER REPAIR PERFORMED BY SPLICING IAW. EA 6-5319-106510 AND RAS/DAHAM/4022477/2007 ISS A.SDR 07FDEA02927Frame · crackedCRACKED FRAME SEGMENT (A539-89388-201) ON C98 WITH CRACKED FIREWALL (P/N A539-89596-000). REPAIR PERFORMED BY REPLACEMENT OF DAMAGED PART ON FRAME SECTION C98 AT P10 AND DOUBLER INSTALLATION ON FIREWALL, APPROVED BY EA 6-5319-106510 AND RAS/DAHAM/4022477/2007SDR 07FDEA02926Skin Panel · corrodedCORROSION ON SKIN PANEL C54, P56-57 REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5315-112494 AND RAS/053735/004/2007 ISS A.SDR 07FDEA02895Stringer · corrodedCORROSION FOUND ON P56 RT, C57.2-57.3 STRINGER REPAIR (CORROSION BLEND OUT AND COUPLING REPAIR) PERFORMED IAW EA 6-5316-112484 A AND RAS/DATLS/0003790/2007 ISS B.SDR 07FDEA02894Fairing · corrodedCORROSION FOUND ON APU EXHAUST ACCESS FAIRING C103A DOUBLER REPAIR PERFORMED IAW EA 6-5319-112491 AND RAS/DATLS/0003798/2007 ISS A.SDR 07FDEA02893Spar · crackedCRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT, RELATED P/N WEB A571-10431-200, HOLE C, D IAW SB 53-242. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A.SDR 07FDEA02892Spar · crackedCRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT (RELATED P/N TEE A571-10122-200, HOLE C, D IAW SB 53-242). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A.SDR 07FDEA02891Splice · crackedCRACKS FOUND ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 RT IN SEVERAL HOLES (B, D, K, M, A3). REPAIR PEROFRMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5315-106505 AND RAS/053356/009/2007 ISS A.SDR 07FDEA02890Splice · crackedCRACKS IN SEVERAL HOLES ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 LT, (HOLE G ,I ,L , M, A3, A4 ,A5 ,A6 , A7, A8). REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5315-106504 AND RAS/053351/014/2007 ISS A.SDR 07FDEA02849Skin · corrodedCORROSION ON SKIN AT C101-102, P17-20 RT REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10, APPROVED BY EA 6-5319-106509 AND RAS/DAHAM/4022473/2007 ISS B.SDR 07FDEA02848Sill · corrodedCORROSION SPOTS ON SILL BEAM C20 AND C25A REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALL A BUSH IN C 20 AND A MACHINED ANGLE IN C25 A IAW EA 6-5313-106503 AND RAS/DABRE/7007983/2007 ISS A.SDR 07FDEA02847Stringer · corrodedCORROSION SPOT ON STRINGER P52 RT, C62-63, REPAIR PERFORMED BY REWORK OF THE AREA IAW EA 6-5317-112485 AND RAS/DATLS/0003791/2007 ISS A.SDR 07FDEA02846Web · corrodedCORROSION ON WEB C63, P49-50 LT OUT OF LIMIT REPAIR PERFORMED BY CORROSION REMOVAL IAW SRM 51-74-10, APPROVED BY EA 6-5317-112487 AND RAS/DATLS/0003810/2007 ISS A.SDR 07FDEA02845Floorbeam · misrepairedOLD SPLICE REPAIR ON TOP CAP BEAM C 33 , -Y140-805 IN FWD CARGO COMPARTMENT NOT CONFORM TO SRM. REPAIR RENEWED IAW, SRM 53-10-15 FIG 207.SDR 07FDEA02843Doubler · crackedDOUBLER CRACKED AT FIRE WALL C95 REPAIR PERFORMED BY DOUBLER INSTALLATION, APPROVED BY EA 6-5319-112476 AND RAS/DATLS/0003777/2007 ISS A.SDR 07FDEA02842Skin · chafedSLAT NR 2 LT WITH CHAFING MARKS ON UPPER SKIN AT NOSE SECTION. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW EA 6-5743-112493 AND RAS/FOK/177/2007 ISS A .SDR 07FDEA02841Fitting · corrodedPYLON NR 1 LOWER FITTING WITH CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-106504SDR 07FDEA02840Fitting · corrodedPYLON NR 2 LOWER FITTING CORROSION IN BEARING HOLE REPAIR PERFORMED BY SB A300-54-6018, APPROVED BY EA 6-5451-106505.SDR 07FDEA02821Skin Panel · crackedSKIN PANEL UNDER ANTI CHAFING PLATE FR 92 - FR 95 CRACKED AND IN SOME SMALL AREAS CORRODED STRUCTURE REPAIR IN ACCORDANCE WITH EA 6-5319-106511 AND RAS /DAHAM/4022481/2007 PERFORMED.SDR 07FDEA02725Fitting · damagedELONGATED HOLE (DIA 6,6MM), FOUND IN CORNER FITTING (P/N: A537-73644-203) AT C31, P'40-41, RT. REPAIR PERFORMED BY INSTALLING A BUSHING (RE0016-202, DIA. 8MM) IAW EFW CONCESSION DD-0713005.SDR 07FDEA02720Skin · corrodedTWO CORROSION SPOTS AT INTERNAL SKIN IN THE AREA OF C69, P'47 RHS. HEAVY CORROSION AT CONNECTING SECTION AT C67, P'48 RHS (P/N: A539-78339-200 AND A539-78339-200-90). REPAIR PERFORMED BY BLEND OUT CORROSION SPOTS AT INTERNAL SKIN IAW SRM 51-74-10, IN LIMIT. SDR 07FDEA02717Sill · corrodedCORROSION FOUND ON AFT CARGO DOOR SILL BEAM UPPER FLANGE BETWEEN C59-59A, RT. REPAIR PERFORMED BY REWORK, EXCEEDING LIMIT AND IS APPROVED BY RAS/DATLS/0003788/2007 ISSUE "A" AND EA 6-5317-112483.SDR 07FDEA02714Frame · damagedFOUND MISDRILLED HOLE AT C40, P'13, RHS. REPAIR PERFORMED BY INSTALLING FASTENER DAN6-8-12Y WITH TRANSITION FIT AND USING RADIUS FILLER IAW RAS/DAHAM/4022410/2007 ISSUE "B" AND EA 6-5315-106497.SDR 07FDEA02713Skin Panel · damagedFOUR OVERSIZED HOLES (DIA. 4.8MM) FOUND AT C74, P'39-43, RHS. THE ORIGINAL RIVET SIZE IS 4.0MM. REPAIR PERFORMED PER INSTALLING FASTENERS NAS1241D6 IAW SRM 51-40-20 (-21), RAS/DAHAM/4022495/2007 ISSUE "A" AND EA 6-5318-112475.
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