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.

SDR FDEA201810313068Rib · crackedRT WING CENTER FLAP RIB 26 HAS TWO CRACKS AT TOP SKIN ATTACHMENT, 6TH FASTENER AND 12TH FASTENER FWD OF REAR SPAR. REPAIRED 2 CRACKS BETWEEN STR 2.7 AND 2.8 IAW SRM 57-50-00, FIG 201, SEE RSC TRACKING EA 6-5750-T0343180 PT1, WRI 57502376. REPAIR IS CLASSIFIED Oct 31, 2018 · N748FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA2018102973031Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL 252XG WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Oct 27, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2018102973030Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 242KF WAS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Oct 27, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2018102973029Web · bentTAIL COMPARTMENT BETWEEN FRAMES 86 AND 87, STRINGER 23R, WEB AND STRAP ARE BENT. FABRICATED THE WEB AND STRAP IAW SRM 53-19-18, AND SRM 51-31-00. REMOVED AND REPLACED THE WEB AND STRAP IAW SRM 51-40-21. MAJOR REPAIR.Oct 27, 2018 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201810232986Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 231HG BROKEN. FABRICATED FLOOR PANEL 231HG IAW SRZ-25-005 ON T18/1373260. INSTALLED ON WORK CARD E-6-5321-E0339394 A PT4. REPAIR CAT "A" MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810232985Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 252UH BROKEN. FABRICATED FLOOR PANEL 252UH IAW SRZ-25-005 ON T18/1373247. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810232984Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 252WG BROKEN. FABRICATED FLOOR PANEL 252WG IAW SRZ-25-005 ON T18/1373244. INSTALLED ON WORK CARD 250-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810232982Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 242WJ BROKEN. FABRICATED FLOOR PANEL 242WJ IAW SRZ-25-005 ON T18/1373250. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810232980Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 242XJ BROKEN. FABRICATED FLOOR PANEL 242XJ IAW SRZ-25-005 ON T18/1373258. INSTALLED ON WORK CARD 240-FL-FIT. REPAIR CAT "A" MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810232979Floor Panel · brokenMAIN CARGO DECK FLOOR PANEL 252JK BROKEN. FABRICATED FLOOR PANEL 252JK IAW SRZ-25-005 ON T18/1373252. INSTALLED ON WORK CARD 250-FL-FIT. MAJOR REPAIR.Oct 23, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810182943Floor Panel · brokenMCD FLOOR PANEL 252XK BROKEN. FABRICATED FLOOR PANEL 242XK ON T18/1372105 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Oct 18, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810182942Floor Panel · brokenMCD FLOOR PANEL 251SK BROKEN. FABRICATED FLOOR PANEL 241SK ON T18/1372103 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Oct 18, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810182941Floor Panel · brokenMCD FLOOR PANEL 251XF BROKEN. FABRICATED FLOOR PANEL 241XF ON T18/1372104 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Oct 18, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810182940Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 241LK HAS DAMAGED CORNER SECTION. FABRICATED FLOOR PANEL 241LK ON T18/1372165 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Oct 18, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810182939Floor Panel · brokenCABIN FLOOR PANEL 241HK HAS BROKEN CORNER. FABRICATED FLOOR PANEL 241HK ON T18/1372172 IAW SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Oct 18, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201810152885Floor Panel · delaminatedCOURIER FLOOR PANEL 221PF DELAMINATED. FLOOR PANEL 221PF FABRICATED ON T18/1371843. CLASSIFIED AS A CAT "A" MAJOR REPAIR IAW SRZ-25-005.Oct 15, 2018 · N748FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201809272718Control Unit · faultyDURING CLIMB OUT FROM KMEM, ENG 1 LOOP B FAULTED. PER FLT CREW THE ENG 1 B LOOP FAULT LIGHT FLICKERED ON AND OFF MULTIPLE TIMES THEN WOULD FAULT AND GO OUT AGAIN. THEN FAULTED AND STAYED FAULTED. THE LOOP TESTED GOOD ON THE GROUND AND WOULD NOT FAULT. PERFORMESep 27, 2018 · N748FD · Airbus A300B4622R · Fire DetectionSDR FDEA201803170724Slide · malfunctionedDURING BLOCK IN, NOTICED THE RIGHT CABIN DOOR SLIDE SHOWED DISARMED EVEN THOUGH THE LEVER WAS IN ARMED POSITION. PERFORMED OPS TEST OF THE R1 DOOR SLIDE ECAM MESSAGE IAW MM 52-73-13-05-09, OPS TESTED NORMAL.Mar 17, 2018 · N748FD · Airbus A300B4622R · Escape SlideSDR FDEA201712083345Trim System · no testWITH STAB TRIM SET AT 2.5 DEGREES THE TAKE OFF CONFIGURAION TEST FAILED WHEN CHECKED ON TAXI OUT. WE CONFIRMED THE TRIM WAS CORRECT AND WAS SET ACCORDING TO APS. ECAM HAD INDICATED OUT OF TO RANGE AS REASON FOR FAILURE. WE RESET TRIM SETTING, VERIFIED THDec 8, 2017 · N748FD · Airbus A300B4622R · Stabilizer Control SystemSDR FDEA201705231488Handle · unsecureR1 DOOR INDICATED UNLOCKED WHILE CLIMBING THROUGH APPROX 4000 FEET. PRESSURIZATION INDICATED NORMAL. FOUND THE DOOR CONTROL HANDLE NOT FULLY IN LOCKED POSITION AND LOUD SQUEAL COMING FROM AROUND THE DOOR FRAME. PUSHED DOOR HANDLE DOWN IAW QRH AND DOOR INMay 23, 2017 · N748FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA201604221337Spar · crackedRIGHT PYLON RIB 18-19, AFT FAIRING UPPER SPAR CRACKED AT OTBD SIDE, APPROX 3.0 INCHES IN LENGTH.Apr 22, 2016 · N748FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201604221336Stiffener · crackedRIGHT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10 FOUND CRACK. COMPLIED WITH EA 6-5450-T0324904 PT 1. REPAIRED RT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10. THIS REPAIR WAS CATEGORY C. REPAIR LIFE LIMITATION 6 MONTHS. LIFE LIMITATION MAYBEApr 22, 2016 · N748FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201604221335Stiffener · crackedLEFT PYLON LOWER SPAR CTR STIFFENER, BETWEEN RIB 9 & 10 FOUND CRACK. COMPLIED WITH EA 6-5450-T0324873 PT 1, REPAIRED LT PYLON LOWER SPAR CENTER STIFFENER. THIS REPAIR WAS CATEGORY C. REPAIR LIFE LIMITATION 6 MONTHS. LIFE LIMITATION MAY BE FURTHER EXTENDED Apr 22, 2016 · N748FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201604181244Web · crackedCENTER MAIN DECK UNDER FLOOR, FRAME 47, BETWEEN Y953 & Y1456, VERTICAL WEB CRACKED. REPLACED THE VERTICAL WEB, CTR MAIN DECK UNDER FLOOR IAW SRM 51-40-21. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 18, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604151236Web · crackedCENTER MAIN DECK UNDER FLOOR FRAME 47, BETWEEN Y-953 & Y-1456, VERTICAL WEB CRACKED. REPAIRED THE VERTICAL WEB IAW SRM 53-15-15 FIG 201 SHEET 2. THE REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100. THE FIRST INSPECTION THRESHOLD WAS 24000 FCApr 15, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604131200Floor Support · corrodedMAIN DECK CARGO COMPARTMENT, FRAME 11 - 13A, Y953, FLOOR SUPPORT CORRODED. REPLACED THE MDCC FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR WAS CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.Apr 13, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604131199Floor Support · corrodedMAIN DECK CARGO COMPARTMENT, FRAME 11 - 13A, Y730, FLOOR SUPPORT CORRODED. REPLACED THE MDCC FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR WAS CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.Apr 13, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604121190Floor Support · corrodedBULK CARGO COMPARTMENT, FRAME 66 - 69, Y805, FLOOR SUPPORT CORRODED. REPLACED THE BULK CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-40-21. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.Apr 12, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604121189Floor Support · corrodedBULK CARGO COMPARTMENT, FRAME 66 - 69, Y140, FLOOR SUPPORT CORRODED. REPLACED THE BULK CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-40-21. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.Apr 12, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201604121188Crossbeam · corrodedAFT CARGO COMPARTMENT FRAME 63, BETWEEN Y805 & Y1470, FLOOR CROSSBEAM CORRODED. REPAIRED THE TOP CAP OF FLOOR CROSSBEAM IAW SRM 53-10-15 FIGURE 207. THIS REPAIR WAS CATEGORY A. MAJOR REPAIR IAW MM 6-2-100.Apr 12, 2016 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201510093161Tachometer · faultyAFTER LANDING ON 15R & CLEARING RUNWAY, BRAKE TEMPS APPEARED TO BE CLIMBING NORMALLY, NO BRAKES FANS, AFTER TAXING FOR A WHILE MOST BRAKE TEMPS WERE BELOW 200 DEGREES. ONE ON THE LT SIDE CLIMBED TO MAX 280 DEGREES. NR 3 BRAKE KEPT CLIMBING. RT SIDE BRAKES WOct 9, 2015 · N748FD · Airbus A300B4622R · Landing Gear Brake SystemSDR FDEA201510093153Brake Assy · failedAFTER LANDING, BRAKE TEMPS APPEARED TO BE CLIMBING NORMALLY, NO BRAKES FANS. AFTER TAXING FOR A WHILE MOST BRAKE TEMPS WERE BELOW 200 DEGREES, ONE ON THE LT SIDE CLIMBED TO MAX 280 DEGREES. NR 3 BRAKE KEPT CLIMBING., RT SIDE BRAKES WHERE NOT USED AFTER 285 DOct 9, 2015 · N748FD · Airbus A300B4622R · Landing Gear Brake SystemSDR FDEA201410153158Warning System · activatedWE HAD A VIOLENT BANG WITH THE GEAR WARNING ON THE RT MAIN GEAR DOOR WITH OVERSPEED WARNING, NO OTHER INDICATIONS. NORMAL GEAR EXTENSION AT LANDING ON TOUCHDOWN WE COULD FEEL THE RUMBLE OF POSSIBLE TIRE FAIL. QRH FOR GEAR DOOR WAS COMPLETED. DOOR WAS INSTALOct 15, 2014 · N748FD · Airbus A300B4622R · Landing Gear Position and WarningSDR FDEA201408272334Fitting · corrodedRIGHT RIB 5 MLG FITTING HAS CORROSION IN BORE AT FWD LUG. COMPLIED WITH EA 6-5710-T0310821 P2 BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.Aug 27, 2014 · N748FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201408272333Fitting · corrodedLEFT MLG RIB 5 FITTING FWD LUG HAS CORROSION IN BORE, FWD FACE & AFT FACE. COMPLIED WITH EA 6-5710-T0310821 P1 BASIC WINGS STRUCTURE LT & RT RIB 5 CORROSION.Aug 27, 2014 · N748FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201404040645Frame · crackedMAIN DECK FRAME 47, STRINGER 24 - 26 RT N HOLE FOUND CRACKED. REPAIRED, MAJOR REPAIR IAW 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201404040652Attach Angle · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH ANGLE AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040651Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040650Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW FEDEX GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040649Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040648Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040647Attach Fitting · crackedRIGHT FUSELAGE TO CENTERR WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage, Wing Attach FittingsSDR FDEA201404040646Frame · crackedRIGHT FUSELAGE TO CENTER WING BOX FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 4, 2014 · N748FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201404020619Frame · crackedCRACK FOUND IN CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.Apr 2, 2014 · N748FD · Airbus A300B4622R · Wing Main, Frame StructureSDR FDEA201404020618Frame · crackedCRACK FOUND IN THE CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.Apr 2, 2014 · N748FD · Airbus A300B4622R · Wing Main, Frame StructureSDR FDEA201404020617Frame · crackedCRACK FOUND IN THE LT CENTER WING JOINT AT FRAME 40. REPAIRED IAW EA 6-5710-T0307352 PT1. MAJOR REPAIR IAW GMM 6-2-100.Apr 2, 2014 · N748FD · Airbus A300B4622R · Wing SparSDR FDEA201312102951Transmitter · inoperativeGREEN HYD QTY DECREASED DURING FLIGHT UNTIL LOW QTY ECAM WARNING. DECLARED EMERGENCY, FOLLOWED QRH MANUAL GEAR EXTENTION HYD FAILURE REQ TOW IN. PRESS REMAINED NORMAL UNTIL QTY LOW INDICATION, VERY SLOW QTY LOSS ABOUT 2 HRS INTO FLIGHT WHEN INDICATION OCCURRDec 10, 2013 · N748FD · Airbus A300B4622R · Hydraulic Quantity SensorSDR FDEA201305211054Electrical Sys · malfunctionedDURING CLIMB, RECEIVED A PARTIAL POWER LOSS. ALL INSTRUMENTS ON F/O'S SIDE. RT ECAM, RT FMS AND RT IDC 900 WERE LOST. FOUND TR2 FAULTED ON MAINT PANEL. R & R TR2 (2PU) IAW MM 24-32-11-04. OPS TEST NORMAL IAW MM 24-32-00-05. OK FOR SERVICE.May 21, 2013 · N748FD · Airbus A300B4622R · AC Power Distribution SystemSDR FDEA201202160596Line · shearedIMMEDIATELY AFTER TAKEOFF, ECAM YELLOW LOW PRESSURE. LOW YELLOW QUANITY. FOUND LT AILERON YELLOW SYS SERVO CONTROL HYD LINE RUPTURED. R & R HYD LINE, (PN A27142012), REF MM 27-14-12-04. SERVICED YELLOW HYD SYS IAW MM 12-12-29-0. LEAK CK GOOD. ENGINE PUMFeb 16, 2012 · N748FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201111194983Skin · dentedLT WING ALL SPEED AILERON LOWER SURFACE T/E HAS 2 EA DENTS WITH DELAMINATION 10 IN FROM OFF CENTER T/E DEFECTS MEASURE 1.5 X 1.0 X 0.003 AND 1.0 X 1.5 X 0.002. REPAIRED LT WING AILERON LOWER T/E SURFACE BY CUTTING OUT DAMAGE AND APPLYING FILLER AND DOUBLER Nov 19, 2011 · N748FD · Airbus A300B4622R · Ailerons
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