# Service difficulty reports: N750FD A list on [N750FD](https://openairdocs.org/aircraft/N750FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 6 · 260 reports - [SDR FDEA201910072506](https://openairdocs.org/sdr/FDEA201910072506.md): Rib · cracked · Oct 7, 2019 · N750FD · Airbus A300B4622R · Wing Main, Frame Structure > MDIS 750 57-10 0606 08OCT19 MEM OPEN U RH OUTBOARD SIDE OF RIB 5, EVIDENCE OF CRACK. COMPLIED WITH E.A. 6-5710-T0350686 PART 1 REV A, PART 2 AND PART 3 TEMPORARY REPAIR OF R/H WING RIB - [SDR FDEA2019101072506](https://openairdocs.org/sdr/FDEA2019101072506.md): Rib · cracked · Oct 7, 2019 · N750FD · Airbus A300B4622R · Wing, Rib/Bulkhead > RIGHT OUTBOARD SIDE OF RIB 5, EVIDENCE OF A CRACK. - [SDR FDEA201907031477](https://openairdocs.org/sdr/FDEA201907031477.md): Transmitter · cracked · Jul 3, 2019 · N750FD · Airbus A300B4622R · Hydraulic Pressure Sensor > BLUE RSVR LOW ON ECAM AT TOP OF DESCENT. FOUND CRACK IN BLUE SYSTEM PRESSURE TRANSMITTER HOUSING CAUSING HYDRAULIC LEAK. R&R BLUE SYSTEM PRESSURE TRANSMITTER IAW 29-12-12-04-0. LEAK AND OPS CK GOOD. - [SDR FDEA2019062091369](https://openairdocs.org/sdr/FDEA2019062091369.md): O-Ring · failed · Jun 19, 2019 · N750FD · Airbus A300B4622R · Hydraulic System, Main > CLIMBING APPROX FL180 GREEN SYS QTY WENT TO 0 RETURNED TO DEPARTURE FOR EMERGENCY LANDING, AFTER GEAR EXTENDED VIA GRAVITY EXTENSION AND AT 2000 GREEN QTY RETURNED TO NORMAL. TAXIED CLEAR OF RWY. VERIFIED GREEN SYSTEM HYDRAULIC QTY. WAS NOT DEPLETED COM - [SDR FDEA2018082192127](https://openairdocs.org/sdr/FDEA2018082192127.md): Flap · obstructed · Aug 19, 2018 · N750FD · Airbus A300B4622R · Trailing Edge Flap Control System > RIGHT WING INBOARD FLAP HAD A PANEL JAMMED IN THE FLAP. THE RT WING INNER OUTER FLAP DEFLECTOR WAS REMOVED AND REPAIRED ON WRI 57-50/8979. INSTALLED SERVICEABLE FLAP DEFLECTOR IAW AMM 27-54-41-04. OPS CHECKED GOOD IAW AMM 27-50-00-03. ACFTOK FOR SERVICE. - [SDR FDEA201806181539](https://openairdocs.org/sdr/FDEA201806181539.md): Sliding Window · out of adjust · Jun 18, 2018 · N750FD · Airbus A300B4622R · Flight Compartment Windows > F/O SLIDING WINDOW EXTREMELY HARD TO OPEN. FOUND F/O'S SLIDING WINDOW OUT OF ADJUSTMENT. RE-RIGGED F/O'S SLIDING WINDOW PER MM 56-12-00-04. OK FOR SERVICE. - [SDR FDEA201803010650](https://openairdocs.org/sdr/FDEA201803010650.md): Actuator · unknown · Mar 1, 2018 · N750FD · Airbus A300B4622R · Landing Gear Actuator > REMOVE AND REPLACE RT MLG BRACE STRUT ACTUATING CYLINDER DUE TO REPEAT LDG EXTENSION PROBLEMS. COMPLETED INSTALLATION AND TEST OF RT BRACE STRUT ACTUATING CYLINDER FROM PREVIOUSLY NOTED STEP E TO COMPLETION REF AMM 32-31-55-04 AND ALL CHECKS OK. - [SDR FDEA201803010560](https://openairdocs.org/sdr/FDEA201803010560.md): Uplock Actuator · faulty · Mar 1, 2018 · N750FD · Airbus A300B4622R · Landing Gear Actuator > UPON GEAR EXTENSION RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED, RED RIGHT GEAR UNLOCK LIGHT ILLUMINATED, FOLLOWED ECAM/QRH MANUAL GEAR EXTENSION 3 GREEN LIGHTS. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR AND RT MLG DRAG BRACE ACTUATING CYLINDER. COMPLETE - [SDR FDEA201802030299](https://openairdocs.org/sdr/FDEA201802030299.md): Uplock · failed · Feb 3, 2018 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension System > ON FINAL, WHEN GEAR SELECTED DOWN, THE RT MAIN GEAR DID NOT COME DOWN AND LOCK. WENT AROUND DID ECAM PROCEDURE FOR MANUAL GEAR EXTENTION. VERIFIED DOWN BY ALL 3 IND. STOPPED ON RWY DUE TO LACK OF NOSEWHEEL STEERING. AFTER FREE FALL EXTENSION.. PERFORMED - [SDR FDEA201711233299](https://openairdocs.org/sdr/FDEA201711233299.md): Sequence Valve · failed · Nov 23, 2017 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension System > DURING NORMAL GEAR EXTENSION, THE RIGHT MAIN GEAR ON SYS 1 AND 2, INDICATOR SHOWED RED UNLOCKED WITH THE AMBER DOOR LIGHT ILLUMINATED. SYSTEM 3 SHOWED NO LIGHT FOR RIGHT MAIN DOWN INDICATOR. THE GEAR WAS LOWERED WITH THE MANUAL GEAR EXTENSION AND ALL 3 GEA - [SDR FDEA201710273085](https://openairdocs.org/sdr/FDEA201710273085.md): Not Reported · malfunctioned · Oct 27, 2017 · N750FD · Airbus A300B4622R · Main Landing Gear > DURING GEAR EXTENSION RIGHT MAIN DID NOT EXTEND. GEAR DOOR DID OPEN, CONFIGURATION VERIFIED BY LAX TOWER. GRAVITY EXTENSION ACCOMPLISHED. PERFORMED NORMAL GEAR EXTENSION AND RETRACTION SEVERAL TIMES REF AMM AMM 32-31-00-05-09. OPS CHECKED GOOD, LEAK CHECK GOOD - [SDR FDEA201709152570](https://openairdocs.org/sdr/FDEA201709152570.md): Window · binding · Sep 15, 2017 · N750FD · Airbus A300B4622R · Flight Compartment Windows > FIRST OFFICER'S WINDOW EXTREMELY HARD TO OPEN WITH ZERO PRESSURE. LUBRICATED THE WINDOW IAW MM 12-22-56-00. WINDOW OPERATES NORMAL, NO BINDING IAW MM 56-12-00-04, AND M/M 25-13-21-4. - [SDR FDEA201706261764](https://openairdocs.org/sdr/FDEA201706261764.md): Skin · dented · Jun 26, 2017 · N750FD · Airbus A300B4622R · Ailerons > RT AILERON OTBD TRAILING EDGE, LOWER SURFACE HAS A DENT. REPAIRED IAW SRM 57-61-11, SRM 51-77-12, PARA 4B, FIG 218, AND EA 6-5750-T0333816. MAJOR REPAIR - [SDR FDEA201706161689](https://openairdocs.org/sdr/FDEA201706161689.md): Floor Panel · cracked · Jun 16, 2017 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 241HK IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CLASSIFIED AS A MAJOR REPAIR. - [SDR FDEA201706161688](https://openairdocs.org/sdr/FDEA201706161688.md): Floor Panel · cracked · Jun 16, 2017 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 251ZG HAS A BROKEN EDGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 CLASSIFIED AS A MAJOR REPAIR. - [SDR FDEA201706161685](https://openairdocs.org/sdr/FDEA201706161685.md): Floor Panel · cracked · Jun 16, 2017 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 242LK CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CLASSIFIED AS A MAJOR REPAIR. - [SDR FDEA201701290280](https://openairdocs.org/sdr/FDEA201701290280.md): Skin · punctured · Jan 29, 2017 · N750FD · Airbus A300B4622R · Trailing Edge Flaps > LEFT INBD FLAP HAS A PUNCTURE IN THE UPPER SURFACE APPROXIMATELY IN THE MIDDLE OF FLAP CAUSED BY LOOSE FASTENER FROM DROP DOWN PANEL IN FRONT OF PUNCTURE. REMOVED DAMAGE AND ACCOMPLISHED HFEC OF DAMAGE CUTOUT AREA. NO INDICATIONS NOTED IAW NTM PT6 51-10-08 - [SDR FDEA201610113545](https://openairdocs.org/sdr/FDEA201610113545.md): Nacelle · contaminated · Oct 11, 2016 · N750FD · Airbus A300F4622R · Nacelle/Pylon, Main Frame > DURING TAKE OFF, TOWER REPORTED SMOKE FROM THE NR 1 ENGINE. NO OTHER INDICATIONS OF FIRE. INSPECTED THE NR 1 ENGINE INTAKE AND EXHAUST. NO DAMAGE NOTED. OPENED COWLING AND INSPECTED FAN/CORE/EXHAUST SECTIONS. NO EVIDENCE OF FIRE FOUND. NO FLUID LEAKS FOUN - [SDR FDEA201608092846](https://openairdocs.org/sdr/FDEA201608092846.md): Hydraulic Line · leaking · Aug 9, 2016 · N750FD · Airbus A300B4622R · Hydraulic System, Main > GREEN HYDRAULIC LOW LEVEL ECAM WARNING DURING FLT. DROPPED TO BELOW RED DOT. IMMEDIATELY ON ALERT WITH SOME FLUID INDICATION, TURNED OFF BOTH GREEN HYD PUMPS. EVENTUALLY FLUID DROPPED TO ALMOST ZERO. REMOVAL, INSTALLATION OF NR 2 ENGINE CASE DRAIN HYD TU - [SDR FDEA201605201688](https://openairdocs.org/sdr/FDEA201605201688.md): Pump · worn · May 20, 2016 · N750FD · Airbus A300B4622R · Hydraulic Pump (Electric/Engine), Main > ON TAKEOFF ROLL, GOT YELLOW SYS, TURNED OFF PUMP, LOW PRESS. REJECTED TAKEOFF. INFO ONLY, YELLOW SYS LOW PRESS WARNING COMES BACK WHILE CYCLING FLIGHT CONTROLS. R & R YELLOW SYS ENG DRIVEN PUMP & OPERATIONS CHECKED GOOD IAW MM 29-11-32-04-01. DRY MOTOR NR - [SDR FDEA201511283810](https://openairdocs.org/sdr/FDEA201511283810.md): Connector · dirty · Nov 28, 2015 · N750FD · Airbus A300B4622R · Hydraulic Power System Wiring > ON TAKEOFF ROLL, 80 KNOTS, YELLOW HYD SYS LO LEVEL ECAM ANNUNCIATED. SPOILER FAULTS ON SPOILER 3 & 2, 5. RTO, SERVICED YELLOW SYS HYD IAW AMM 12-12-29-00. VERIFIED HEAD PRESS, RAN NR 2 ENG IAW JRH. ALL PARAMETERS NORMAL. RECHECKED HYD SERVICING AFTER RUN - [SDR FDEA201504031146](https://openairdocs.org/sdr/FDEA201504031146.md): Engine · leaking · Apr 3, 2015 · N750FD · Airbus A300B4622R · Engine (Turbine/Turboprop) > GOT MIN EQUIPMENT BAY SMOKE WARNING IN FLIGHT, APPROX 16000 FEET COMPLIED WITH ECAM. ORH SAW HAZY LIGHT SMOKE AT ENG INSTRUMENT PANEL. RAN AVIONICS SMOKE CHECKLIST LANDED UNEVENTFULLY. PREFORMED CRUISE POWER ENG RUN IAW JRH, CONFIRMED OIL SMELL COMING FROM - [SDR FDEA201502040424](https://openairdocs.org/sdr/FDEA201502040424.md): Web · gouged · Feb 4, 2015 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous Structure > THIS COMPARTMENT LT DOOR, 313AL, CUT OUT BUCKLED WITH GOUGE. LOCATED OTBD IN FROM FWD CORNER. REMOVED DAMAGED WEB, INSTALLED NEW WEB & 2 EA INTERCOSTAL AFT THS COMPARTMENT LT DOOR CUT OUT IAW SRM 51-40-21. FABRICATED ON T15 1115998. MAJOR REPAIR. - [SDR FDEA201501270306](https://openairdocs.org/sdr/FDEA201501270306.md): Stringer · corroded · Jan 27, 2015 · N750FD · Airbus A300B4622R · Fuselage Main, Structure > FUSELAGE EXTERNAL STRINGER BELOW VERT STAB AT LT MIDDLE FIN TO FUSELAGE FITTING IS CORRODED. R & R ON FUSELAGE EXTERNAL STRINGER 3L BELOW VERT STAB IAW 51-40-21. REMOVED CORROSION AT STRINGER 3L, ORIGINAL THICKNESS.155 AFT REWORK MATERIAL LOSS IS.040. FOU - [SDR FDEA201501240292](https://openairdocs.org/sdr/FDEA201501240292.md): Fitting · corroded · Jan 24, 2015 · N750FD · Airbus A300B4622R · Wing, Landing Gear Attach Fittings > RIGHT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES. REPAIRED IAW DWG R57240425 REV D & EA 6-5710-T0314932. MAJOR REPAIR. - [SDR FDEA201501170219](https://openairdocs.org/sdr/FDEA201501170219.md): Floor Panel · cracked · Jan 17, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > COURIER AREA FLOOR PANEL 222NF IS CRACKED. FABRICATED COURIER AREA FLOOR PANEL 222NF IAW SRZ-25-005 REV K ON T14 1113353 CAT A MAJOR REPAIR. - [SDR FDEA201501160202](https://openairdocs.org/sdr/FDEA201501160202.md): Seat Track · corroded · Jan 16, 2015 · N750FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK YD 37.52 HAS CORROSION FROM FRAME 11 - 17 IN SEVERAL AREAS. R & R SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR. - [SDR FDEA201501160201](https://openairdocs.org/sdr/FDEA201501160201.md): Floor Support · gouged · Jan 16, 2015 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous Structure > COURIER AREA, CENTERLINE FLOOR SUPPORT IS GOUGED ON UPPER SURFACE BETWEEN FRAME 11 & 12. R & R FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR. - [SDR FDEA201501150177](https://openairdocs.org/sdr/FDEA201501150177.md): Floorbeam · corroded · Jan 15, 2015 · N750FD · Airbus A300B4622R · Fuselage Main, Floor Beam > COURIER AREA, FLOORBEAM YC HAS CORROSION IN 3 PLACES BETWEEN FRAME 11 & 12 ON TOP SURFACE T CAP CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15 L=1.0" W=1.0" D= 100%. R & R T CAP IAW SRM 51-40-21 CAT A MAJOR REPAIR. - [SDR FDEA201501140162](https://openairdocs.org/sdr/FDEA201501140162.md): Floor Panel · damaged · Jan 14, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > BULK CARGO COMPARTMENT FLOOR PANEL 171CF IS DAMAGED & BROKEN ON EDGE OF PANEL. FLOOR PANEL 171CF FABRICATED ON T15 1114494, REPAIR CLASSIFIED CAT A MAJOR. - [SDR FDEA201501120122](https://openairdocs.org/sdr/FDEA201501120122.md): Seat Track · gouged · Jan 12, 2015 · N750FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK BETWEEN FRAME 57 & 57.2 SEAT TRACK -Y450 HAS GOUGE. R & R SEAT TRACK SECTION -Y450 BETWEEN FRAME 57 TO 57.2, PN A53274005SF BATCH 0002120270 IAW SRM 53-10-16. MAJOR REPAIR. - [SDR FDEA201501120121](https://openairdocs.org/sdr/FDEA201501120121.md): Floor Panel · damaged · Jan 12, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FLOOR PANEL 161AF DAMAGED. FLOOR PANEL 161AF FABRICATED ON T14 111858 IAW DWG SRZ 25-0. REPAIR CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501120120](https://openairdocs.org/sdr/FDEA201501120120.md): Floor Panel · damaged · Jan 12, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FLOOR PANEL 161BF DAMAGED. FLOOR PANEL 161BF FABRICATED ON T14 111859 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501120119](https://openairdocs.org/sdr/FDEA201501120119.md): Floor Panel · cracked · Jan 12, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > AFT CARGO FLOOR PANEL 151UF IS CRACKED AT CORNER FLOOR PANEL 151UF. FABRICATED ON T14 1114496 IAW DWG SRZ25-005. CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501080095](https://openairdocs.org/sdr/FDEA201501080095.md): Floor Panel · damaged · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > PANEL 152HF IN AFT PIT PUNCTURED. FLOOR PANEL 152HF FABRICATED ON T14 1111933 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501080094](https://openairdocs.org/sdr/FDEA201501080094.md): Floor Panel · damaged · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > PANEL 152QF IN AFT PIT PUNCTURED. FLOOR PANEL 152GF FABRICATED ON T14 1111934 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501080093](https://openairdocs.org/sdr/FDEA201501080093.md): Floor Panel · damaged · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > COURIER COMPARTMENT FLOOR PANEL 221MF HAS EDGE DAMAGE & IS MISSING ONE INSERT. FLOOR PANEL 221MF FABRICATED ON T14 143354 IAW DWG SRZ 25-005. CAT A CLASSIFIED MAJOR. - [SDR FDEA201501080091](https://openairdocs.org/sdr/FDEA201501080091.md): Floor Panel · cracked · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231BH IS CRACKED. FLOOR PANEL 231BH FABRICATED ON T14 1111397 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501080090](https://openairdocs.org/sdr/FDEA201501080090.md): Floor Panel · cracked · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 241AK IS CRACKED. FLOOR PANEL 241AK FABRICATED ON T14 1111592 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501080089](https://openairdocs.org/sdr/FDEA201501080089.md): Floor Panel · delaminated · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 242XK IS DELAMINATED ON THE LOWER SURFACE. FLOOR PANEL 242XK FABRICATED ON T14 1111593 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201501080088](https://openairdocs.org/sdr/FDEA201501080088.md): Floor Panel · cracked · Jan 8, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > COURIER AREA FLOOR PANEL 221PF HAS 5 INCH LONG CRACK AT THE RT CUT OUT. FABRICATED NEW FLOOR ON T14 1113599 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201501070058](https://openairdocs.org/sdr/FDEA201501070058.md): Floor Panel · cracked · Jan 7, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CARGO DECK FLOOR PANEL 241RJ IS CRACKED AT RT END OF THE CUT OUT. FABRICATED NEW FLOOR PANEL 241RJ ON T14 1113601 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201501070054](https://openairdocs.org/sdr/FDEA201501070054.md): Floor Panel · cracked · Jan 7, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FORWARD PIT FLOOR PANEL 131 HG IS CRACKED. FABRICATED NEW FLOOR PANEL 131HG ON T14 1111506 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201501070053](https://openairdocs.org/sdr/FDEA201501070053.md): Floor Panel · damaged · Jan 7, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FORWARD CARGO COMPARTMENT FLOOR PANEL 131QF, HONEYCOMB MATERIAL IS DAMAGED AT SEVERAL LOCATIONS AROUND THE PANEL EDGES. FABRICATED NEW FLOOR PANEL 131QF ON T 141113602 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. - [SDR FDEA201501070052](https://openairdocs.org/sdr/FDEA201501070052.md): Floor Panel · damaged · Jan 7, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FLOOR PANEL 251VF DAMAGED. FLOOR PANEL 251VF FABRICATED ON T14 1111616 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR. - [SDR FDEA201501070050](https://openairdocs.org/sdr/FDEA201501070050.md): Floor Panel · damaged · Jan 7, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > FLOOR PANEL 251WH DAMAGED. FLOOR PANEL 251WH FABRICATED ON T14 1111615 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS A CAT A MAJOR. - [SDR FDEA201501020005](https://openairdocs.org/sdr/FDEA201501020005.md): Floor Panel · cracked · Jan 2, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231FF IS CRACKED. FLOOR PANEL 231FF FABRICATED T14 111598 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR. - [SDR FDEA201501020004](https://openairdocs.org/sdr/FDEA201501020004.md): Floor Panel · damaged · Jan 2, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231EF HAS TWO EACH PUNCTURES. FLOOR PANEL 231EF FABRICATED T14 1111400 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR. - [SDR FDEA201501020003](https://openairdocs.org/sdr/FDEA201501020003.md): Floor Panel · damaged · Jan 2, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 232DF HAS A PUNCTURE. FLOOR PANEL 232 DF FABRICATED T14 1111597 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR. - [SDR FDEA201501020002](https://openairdocs.org/sdr/FDEA201501020002.md): Floor Panel · delaminated · Jan 2, 2015 · N750FD · Airbus A300B4622R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 232HG HAS A PUNCTURE & DELAMINATION. FLOOR PANEL 232HG FABRICATED T14 1111599 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR. Next page: https://openairdocs.org/aircraft/N750FD/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N750FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N750FD/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.