N748FD
Service difficulty reports · 211
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 = 'N748FD' 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 = 'N748FD' 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 FDEA201006222113Computer · malfunctionedCHECKED FUEL GAUGES. 2900 NR SPLIT BETWEEN LT INNER AND RT INNER (4.42 L VS 1.9 R) DIFFERENCE INCREASED RAPIDLY TO 2800 NR WITHIN 2 MINUTES. DECLARED EMERGENCY FOR POSSIBLE FUEL LEAK AND DIVERTED. OPEN XFEED TO MAINTAIN FUEL BALANCE. TOTAL BURN IN 35 MINUTSDR FDEA201004251358Actuator · malfunctionedON GEAR RETRACTION, HAD LANDING GEAR NOT UP AND LOCKED INDICATION ON FWD PANEL AND OVERHEAD PANEL. RETURNED TO DEPARTURE AND LANDED. FOUND UNIVERSAL BINDING AND UPLOCK FREE FALL RETURN SPRING TENSION WEAK. REMOVED AND REPLACED RT MAIN GEAR UPLOCK ACTUATOR ANSDR FDEA201004251357Sequence Valve · malfunctionedAFTER TAKEOFF, RT MLG DOOR LIGHT REMAINED ON. PUT MLG DOWN, RETURNED TO PIT. RELEASED FOR SERVICE IAW MEL: 32-61-01-C CATEGORY: B EXPIRATION: 28APR10 "MEL 32-61-01-C: RT MLG DOOR INDICATORS SYS NR 1 - INOP." TESTED RT MLG DOOR IAW MM 21-31-00-5 GROUND OSDR FDEA200905181707Skin · dentedDURING ACFT POLISH OF LOWER FUSELAGE BELLY FOUND 1 EA DENT WITH FILLER BELOW FWD CARGO ENTRY DOOR BETWEEN FR 23 AND FR 24,R/H STRINGER 43 AND 44. AFTER REMOVAL OF DENT FILLER DENT MEASURED OUT OF LIMITS IAW A300 -600 FRIEGHTER SRM 53-13-12,FIG 103. CUT OUTSDR FDEA200903050852O-Ring · pinchedECAM GAVE BLUE HYD RES LOW QTY. FOLLOWED ECAM AND TURNED OFF BLUE HYD PUMP. CHECKED QRH RED TABS MISC SECTION FOR GUIDANCE. CONT TO KLAX. A/C DIVERTED FROM SNA TO LAX. FOUND BLUE SYSTEM SERVO CONTROL PRESSURE SWITCH 17CB O-RING PINCHED/LEAKING. REMOVED ASDR 08FDEA02203Indication Sys · malfunctionedLEFT ECAM INDICATED GREEN SYS HYD RESVR LO LEVEL ON DESCENT. GREEN SYS HYD OVERHEAD PANEL GAUGE INDICATED BOTTOM OF YELLOW ARC. RT ECAM HYD POINTER INDICATED BOTTOM OF YELLOW ARC. AFTER COMPLETING HYD RSVR LO LEVEL PROC AND L/G GRAVITY EXT PROC, GREEN SYS QSDR 07FDEA01191Rib · mismanufacturedEDGE MARGIN TO SHORT FOR TEMPORARY REPAIR ON RIB 5 IAW DR 426 REPAIR PERFORMED BY INSTALLATION ADDITIONAL FASTENER IAW EA 6-5710-108975 AND RAS/BAE/1004080/2006 A.SDR 07FDEA01177Angle · crackedCRACKS IN SEALING ANGLE AND AFT SPLICE, RT, FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-5002 PART 4 REPAIR PERFORMED BY SEALING ANGLE REPLACEMENT IAW DRAWING R571-50404, APPROVED BY EO 5-5710-7-5002.SDR 07FDEA01176Frame · damagedMISDRILLED HOLE AT FRAME 13A DURING ACCOMPLISHMENT OF DR 179. REPAIR PERFORMED BY REAM UP AND COLD WORKING IAW EA 6-5312-106395 A AND RAS/AS/010/2007 ISS. CSDR 07FDEA01161Shroud · corrodedFOUND CORROSION FINDING ON RT WING OUTER SHROUD BOX RIB 25-29 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS. A.SDR 07FDEA01160Skin · corrodedFOUND CORROSION FINDINGS ON RT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS.A.SDR 07FDEA01156Frame · crackedCRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5710-7-3305 REV C1, SB A300-57-6050 REV 3-AD 2005-23-08 REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW EA 6-5710-106435 AND RAS/049856/032/2007 ISS. ASDR 07FDEA01155Spar · crackedCRACK AND BEND ON LT SIDE OF THE CENTER SPAR REINFORCING ANGLE REPAIR PERFORMED BY TRIM OUT IAW EA 6-5511-106378 AND RAS/CASA/5355/2007 ISS A.SDR 07FDEA01142Skin · corrodedCORROSION SPOTS ON OUTER SHROUD BOX AND TOP SKIN REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. ASDR 07FDEA01141Skin · corrodedCORROSION SPOTS ON LT WING TOP SKIN RIB 1-25 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106376 AND RAS/BAE/1004287/2007 ISS. A.SDR 07FDEA01140Rib · crackedCRACK WAS FOUND ON MLG RIB 5 RT WING INTERIM REPAIR PERFORMED IAW, DRAWING R572-40265 AND APPROVED BY EA 6-5710-108975 AND RAS/BAE/1004080/2006 ISS.ASDR 07FDEA01139Structure · damagedDAMAGE ON SPOILER NR 4 LT REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY EA 6-5770-106440 REV A AND RAS/DABRE/7007420/2007 ISS. ASDR 07FDEA01138Angle · corrodedCORROSION AND CRACK FINDINGS DURING SEALING ANGLE INSTALLATION- EO 6-5710-7-5002- SB A300-57-6033 REV 1- SBA300-57-6027 REV 6- AD 98-18-02 AND AD 2006-07-07 REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106433 AND RAS/BAE/1004205/2007 ISS. A.SDR 07FDEA01136Angle · corrodedCORROSION AND CRACK FINDINGS IN HOLES DURING SEALING ANGLES INSTALLATION-EO 6-5710-7-5002-SB A300-57-6033 REV 01-SB A300-57-6-27 REV 6- AD98-18-02 AND AD 2006-07-07. REPAIR PERFORMED BY REAM UP AND SEALING ANGLE REPLACEMENT IAW EA 6-5720-106433 AND RAS/BAE/10SDR 07FDEA01130Fitting · corrodedCORROSION ON AFT BEAM (RIB 8) OF PYLON NR 1, REPAIR WAS PERFORMED BY OVERSIZING IAW EA 6-5451-106439 AND RAS/050001/005/2007 ISS.ASDR 07FDEA01105Gusset · corrodedFUSELAGE NOSE SECTION-CORROSION ON FWD PAX DOOR FRAME AREA, RT LOWER CORNER, GUSSET A536-11517-205 REPAIR PERFORMED BY REPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.BSDR 07FDEA01107Splice · crackedCRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017, SB A300-53-6123 REV 2, AD2004-20-14, SPLICE FITTING C47 RT REPAIR PERFORMED BY REPLACEMENT OF FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS/033769/043/2004 ISS.A,SDR 07FDEA01106Splice · crackedCRACKS FOUND DURING EMBODIMENT OF EO 6-5310-7-5017-SB A300-53-6123 REV 2-AD2004-20-14, ON SPLICE FITTING C47 LT REPAIR WAS PERFORMED BY REPLACEMENT OF SPLICE FITTING AND REAM UP IAW EA 6-5315-106436 AND RAS /033769/043/2004 ISS.ASDR 07FDEA01104Gusset · corrodedFUSELAGE NOSE SECTION, CORROSION ON FWD PAX DOOR FRAME AREA C14 UPPER CORNER LT, GUSSET A536-11511-204. REPAIR PERFORMED BY REPLACEMENT OF GUSSET AND REWORK IAW EA 6-5312-106395 AND RAS/AS/010/2007 ISS.B.SDR 07FDEA01049Cover Plate · chafedOLD TOOLING MARK ON COVER PLATE AT DOOR NR 4 RT. REPAIR PERFORMED BY REWORK AND HFEC INSPECTION IAW EA6-5318-106393 AND RAS/DAHAM/4021668/2006 ISSUE "A".SDR 07FDEA01048Cover Plate · chafedTORSION BOX COVER PLATE MARKS AT EMERGENCY EXIT DOOR RT. REWORK WAS PERFORMED BY BLEND OUT, HFEC INSPECTION AND FLAP PEENING IAW EA 6-5316-106394 AND RAS/DATLS/0003542/2006 ISSUE "A".SDR 07FDEA01047Hinge Fitting · corrodedFOUND CORROSION ON RUDDER HINGE FITTINGS NR 5, NR 6 AND NR7 (A554-71605-200, A554-71606-200, A554-71617-000) CORROSION REWORK AND HFEC INSPECTION IAW EA 6-5546-106387, APPROVED BY RAS/DAHAM/4021625/2006 ISSUE "B".SDR 07FDEA00999Skin · damagedPYLON SUPPORT BRACKET AND BOTTOM WING SKIN (LT WING), ELONGATED HOLES REPAIR WAS PERFORMED IAW DRAWING R571-50532 REV A, APPROVED BY EA 6-5720-106407 AND RAS/BAE/1004134/2007 ISS A.SDR 07FDEA01000Flange · damagedREPAIR DEFORMATION AND TOOL MARKS ON C74 OUTER FLANGE AT P26 LT AND RT REPAIR WAS PERFORMED BY REWORK TO SMOOTH CONTOUR ON THE OUTER FLANGE IAW EA 6-5318-106420 AND RAS/DATLS/0003545/2007 ISS. ASDR 07FDEA00998Doubler · damagedOLD GRINDING MARK AT INTERNAL DOUBLER, C70-71, P48-49 LHS REPAIR WAS PERFORMED BY BLEND OUT THE DAMAGE IAW EA 6-5317-106396 AND RAS/DAHAM/ 4021674/2006 ISS. A.SDR 07FDEA00997Skin Panel · corrodedCORROSION ON FUSELAGE UPPER SKIN PANEL C78-85, P4RH AND P7 LT REPAIR WAS PERFORMED BY REWORK IN SMOOTH CONTOUR AND FLAP PEENING IAW EA 6-5319-106398 AND RAS/DAHAM/4021681/2006 ISS. BSDR 07FDEA00993Angle · crackedCRACK FINDINGS IN ANGLE (HOLE 11, 13, 42, 45, 160, 180, 191, ALL LT SIDE) DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, SB A300-57-6050 REV.03, AD 2005-23-08 REPAIR WAS PERFORMED BY REAM OUT, OVERSIZING AND COLD WORKING IAW EA 6-5710-106435 AND RAS/049856/032/SDR 07FDEA00992Sill · corrodedCORROSION ON SILL BEAM C59-63A, RT REPAIR WAS PERFORMED BY CUT OUT AT C60 AND C63 IAW SRM 53-17-18 AND REWORK AT SILL BEAM EDGE IAW EA 6-5317-106399 AND RAS/DAHAM/4021663/2006 ISS. ASDR 07FDEA00864Skin · corrodedBOTTOM SKIN REWORK CAUSED BY CORROSION AT RIB 8, P19, RT OUTER WING REPAIR WAS PERFORMED IAW EA 6-5721-106402 AND RAS/BAE/1004132/2007 ISS A (BLEND OUT CORROSION, FASTENER REPLACEMENT.SDR 07FDEA00854Rib · crackedFOLDING NOSE LT INTERNAL RIB CRACKED. REPAIR WAS PERFORMED IAW EA 6-5710-106358 AND SB A300-57-6067.SDR 07FDEA00852Skin · corrodedLT WING TIP, CORROSION UNDER ONE STATIC DISCHARGER AND CRACK ON NAVIGATION LIGHT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5730-106400 AND RAS/FOK/004/2007 ISSUE "A".SDR 07FDEA00810Skin · inoperativeELONGATED HOLES IN PYLON SUPPORT BRACKET AND BOTTOM SKIN, RT WING. REPAIR PERFORMED IAW AI-INSTRUCTION: R571-50532 ISSUE "A" AND EA 6-5720-106407.SDR 07FDEA00743Crossbeam · corrodedFOUND CORROSION ON CROSSBEAMS C56 AND C58. PARTS REPLACED IAW SRM 71-52-10.SDR 07FDEA00742Stringer Clip · corrodedFOUND CLIP AT FRAME 22 AD HEAVY CORRODED. NEW PART INSTALLED IAW SRM 51-72-10.SDR 07FDEA00741Structure · corrodedSOME PARTS IN KRUEGER FLAP AREA AT FWD FAIRING HEAVY CORRODED, PARTS REPLACED IAW SRM 57-45-11, KEEL BEAM PN A535-10215-201, BRACKET A535-10219-201 AND FITTING A535-10561-201.SDR 07FDEA00679Skin · corrodedFOUND CORROSION AROUND TWO FASTENERS BETWEEN RIB 7-8 AT STRINGER 19 ON RT WING BOTTOM SKIN. REPAIR WAS PERFORMED IAW EA 6-5721-106402, APPROVED BY RAS/BAE/1004132/2007.SDR 07FDEA00677Hinge Fitting · corrodedFOUND CORROSION INSIDE OF FORK ON RUDDER HINGE FITTING NR 5, NR 6 AND NR 7. REPAIR WAS PERFORMED IAW EA 6-5546-106387 INCLUDES REPAIR REF.: TD/K4/S1/21625/2006/A AND IS APPROVED BY RAS/DAHAM/4021625/2008 ISS B.SDR 07FDEA00675Latch · corrodedFOUND CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR WAS PERFORMED IAW SRM 53-13-13, FIG 204, SHEET 1, 2.SDR 07FDEA00674Beam · corrodedCORROSION AT ATTACHMENT HOLES ON SILL BEAM BETWEEN C25 AND 25A AT FWD CARGO DOOR. REPAIR WAS PERFORMED IAW TD/K7/S1/07372/2006 ISS A AND EA 6-5313-106401 AND IS APPROVED BY RAS/DABRE/7007372/2006 ISS A.SDR 07FDEA00673Skin · damagedOLD GRINDING MARK BETWEEN C70-71, P48-49 LT. REPAIR WAS PERFORMED IAW TD/K4/S1/21674/2006 ISS A, APPROVED BY RAS/DAHAM/4021674/2006 ISS A.SDR 07FDEA00672Longeron · corrodedFOUND CORROSION ON FLOOR SUPPORT STRUCTURE IN SEC 12. THE AFFECTED PARTS ARE SHOWN IN SRM 53-12-15 FIG.19, SHEET 3: ITEM 190,200 AND 275. REPAIR WAS PERFORMED IAW SRM 53-12-15, FIG 207 (ITEM 190 / 200) AND BY REPLACE A NEW PART IAW SRM 51-72-10 (ITEM 275).SDR 07FDEA00671Crossbeam · corrodedFOUND CORROSION ON CROSSBEAM C67 RT. REPAIR WAS PERFORMED IAW SRM 53-10-15, FIG 207.SDR 07FDEA00629Fitting · corrodedFOUND CORROSION AT C54, TRACK 5, LT AND RT REPAIR WAS PERFORMED IAW EA 6-5315-106393 AND RAS/049222/.008/2006 ISS A, LT INSTALL FITTING P/N A538-13311, RT INSTALL COUNTRSINK BUSH.SDR 07FDEA00527Skin · corrodedFOUND CORROSION ON SKIN PANEL BETWEEN C77-87, P3-6 RT AND C78-86, P3-6 LT. REPAIR PERFORMED BY REMOVE CORROSION IAW SRM51-74-10, SRM 53-19-12/FIG 1.SDR 07FDEA00359Bracket · corrodedCORRODED BRACKET UNDER PRESSURE MEMBRANE AT TRACK 5 LT C54. CORRODED HOLE AFTER COUNTERSINK OF PRESSURE MEMBRANE AT TRACK 5 RT, C54. REPAIR WAS PERFORMED BY INSTALLING FITTING P/N A538-13311-201-EF ON LHS AND INSTALLING A COUNTERSUNK BUSH IN THE AFFECTED HOL
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