# Service difficulty reports: N748FD

A list on [N748FD](https://openairdocs.org/aircraft/N748FD.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 5 · 211 reports

- [SDR FDEA202607291057](https://openairdocs.org/sdr/FDEA202607291057.md): Shear Pin · damaged · Jul 29, 2026 · N748FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > WHILE PERFORMING FREE FALL CHECK, FOUND "NLG" FREE FALL QUADRANT 3 TO MOVE MORE ON SHAFT THAN ADJACTENT MLG FREE FALL QUADRANT 1 DOES ON SHAFT. INSTALLED BUSHING & SHEAR PIN INTO NLG FREE FALL AMM 32-33-00-05, EA 6-3230-T0388190A, COMPLETED OPS CHECK OF LA
- [SDR FDEA202607220985](https://openairdocs.org/sdr/FDEA202607220985.md): Uplock · leaking · Jul 22, 2026 · N748FD · Airbus A300B4622R · Hydraulic System, Main
  > GREEN HYD RSVR LO LEVEL ECAM ON DEPARTURE. QUANTITY WAS AT ORANGE DOT IN YELLOW BAND. COMPLIED WITH ECAM/QRH. CAPTAIN REPORTED THE ALTERNATE GEAR EXTENSION PROCEDURE WAS USED AS DIRECTED BY RED TABS. RESTORE THE GEAR IAW AMM 32-33-00-02-0. REMOVED AND RE
- [SDR FDEA202606180772](https://openairdocs.org/sdr/FDEA202606180772.md): Slide · fouled · Jun 18, 2026 · N748FD · Airbus A300B4622R · Escape Slide
  > PER CREW DEBRIEF, R1 DOOR SLIDE HANDLE HARD TO ARM/DISARM, DOOR OPENING/CLOSING AND LATCHING NOT AFFECTED, DOOR OPERATES NORMAL. RELEASED FOR SERVICE IAW MEL: 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 25-61
- [SDR FDEA202602210249](https://openairdocs.org/sdr/FDEA202602210249.md): Girt Bar · unsecure · Feb 21, 2026 · N748FD · Airbus A300B4622R · Emergency Equipment
  > R1 DOOR SLIDE WOULD NOT DISARM. PBI RELEASED FOR SERVICE PER MEL: 52-11-01-01 CATEGORY C. CREW ENTRY DOOR ESCAPE SLIDE R1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." MEL: 52-11-01-001 OK FOR SERVICE. AMM: 12-22-52-00-01, AMM: 25-61-22-04-02, AMM: 52
- [SDR FDEA202602190236](https://openairdocs.org/sdr/FDEA202602190236.md): Bottle · leaking · Feb 19, 2026 · N748FD · Airbus A300B4622R · Passenger/Crew Doors
  > R1 DOOR ASSIST BOTTLE REQUIRES DIAPHRAGM REPLACEMENT AND SERVICE PER AMM 52_10_14_03_10. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE DIAPHRAGM. SERVICED NITROGEN TO PLACARD ONBOARD. NO LEAK NOTED. CHECKS GOOD. OKAY FOR SERVICE.
- [SDR FDEA202602130237](https://openairdocs.org/sdr/FDEA202602130237.md): Bottle · damaged · Feb 13, 2026 · N748FD · Airbus A300B4622R · Passenger/Crew Doors
  > FOUND ON SERVICE CHECK L 1 EMERGENCY OPERATION CYLINDER LOW PER SERVICE CHART. AMM: 52-10-14-03-10 SERVICED L 1 EMERGENCY OPERATION CYLINDER PER REF.
- [SDR FDEA202602050136](https://openairdocs.org/sdr/FDEA202602050136.md): Gearbox · failed · Feb 5, 2026 · N748FD · Airbus A300B4622R · Engine Thrust Reverser
  > ON DEPARTURE, NR 1 ENG REV UNLOCK. RAN QRH, DECLARED EMERGENCY AND RETURNED TO ORF WITHOUT INCIDENT. AMM 78-31-35-04, AMM 78-32-11-05 IAW MOCC REQ (MTSI#78-31/9965) REPLACE ENG 1 SPLITTER GEARBOX. R & R ENG 1 SPLITTER GEARBOX. OPS CK OK. R & R SPLITTER
- [SDR FDEA202601110022](https://openairdocs.org/sdr/FDEA202601110022.md): Apu · leaking · Jan 11, 2026 · N748FD · Airbus A300B4622R · Air Distribution System
  > PRIOR TO PUSHBACK, WITH ALL DOORS CLOSED EXCEPT CREW ENTRANCE DOOR, RECEIVED AN ECAM ALERT FOR MAIN DECK CARGO SMOKE DETECTED MID & EXPERIENCED SMOKE IN COCKPIT FROM GASPERS. SMOKE ON SET RAPID & HIGHLY CONCENTRATED. SMOKE CLEARLY VISIBLE IN COCKPIT, AP
- [SDR FDEA202508111420](https://openairdocs.org/sdr/FDEA202508111420.md): Skin · contaminated · Aug 11, 2025 · N748FD · Airbus A300B4622R · Elevator, Plate/Skin
  > EMPENNAGE - RH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER13) REPAIRED EMPENNAGE RH ELEVATOR UPPER L/E ER13 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE
- [SDR FDEA202508111419](https://openairdocs.org/sdr/FDEA202508111419.md): Skin · contaminated · Aug 11, 2025 · N748FD · Airbus A300B4622R · Elevator, Plate/Skin
  > EMPENNAGE - LH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER2) REPAIRED EMPENNAGE LH ELEVATOR UPPER L/E ER2 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE FO
- [SDR FDEA202508011359](https://openairdocs.org/sdr/FDEA202508011359.md): Longeron · cracked · Aug 1, 2025 · N748FD · Airbus A300B4622R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4EA FASTENER HOLES REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE PT1 BETWEEN FR22 AND FR25 4EA CRACKED FASTENER HOLES PER EA 6-5230-T0384376, MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202507251336](https://openairdocs.org/sdr/FDEA202507251336.md): Skin · delaminated · Jul 25, 2025 · N748FD · Airbus A300B4622R · Spoilers
  > LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)30MM*18MM, DEPTH: 2.32MM (2) 82MM*39MM, DEPTH: 1.98MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR DELAMINATED SKIN. MAJOR RE
- [SDR FDEA202507251335](https://openairdocs.org/sdr/FDEA202507251335.md): Skin · delaminated · Jul 25, 2025 · N748FD · Airbus A300B4622R · Spoilers
  > LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)30MM*11MM, DEPTH: 1.60MM (2)150MM*15MM, DEPTH: 1.81MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKI
- [SDR FDEA202507251334](https://openairdocs.org/sdr/FDEA202507251334.md): Skin · delaminated · Jul 25, 2025 · N748FD · Airbus A300B4622R · Spoilers
  > LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)40MM*16MM, DEPTH: 1.76MM (2)30MM*22MM, DEPTH: 1.83MM COMPLIED WITH EA 6-5750-T0384250 REPAIRED LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKIN
- [SDR FDEA202507251333](https://openairdocs.org/sdr/FDEA202507251333.md): Skin · delaminated · Jul 25, 2025 · N748FD · Airbus A300B4622R · Spoilers
  > RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: 50MM*15MM, DEPTH: 1.80MM COMPLIED WITH EA 6-5750-T0384249 REPAIRED RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE DELAMINATED SKIN. TITLE: WING - FLIGHT SURFACES - RH #3 SPOI
- [SDR FDEA202507201360](https://openairdocs.org/sdr/FDEA202507201360.md): Web · cracked · Jul 20, 2025 · N748FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPARTMENT - UNDER FLOOR FR47 WEB CRACKED BETWEEN Y0 AND -Y450 REPAIRED THE MAIN DECK CARGO COMPARTMENT UNDER FLOOR FR47 CRACKED WEB BETWEEN Y0 AND -Y450 PER A300-600 SRM 53-15-15-201 PARA.5A. THIS IS A CAT B REPAIR. THE FIRST INSPECTION W
- [SDR FDEA202507181362](https://openairdocs.org/sdr/FDEA202507181362.md): Door Frame · cracked · Jul 18, 2025 · N748FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > RIGHT FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPAIRED THE RH FWD PAX DOOR FRAME FR14C CRACKED SEGMENT PER SRM 51-40-21 AND DWG F52181297 ISSUE: K AND DWG F52181299 ISSUE: G. THIS IS A CAT A REPAIR AND RSC TRACKING EA 6-5210-T0384405 WAS ISSU
- [SDR FDEA202507131361](https://openairdocs.org/sdr/FDEA202507131361.md): Fitting · damaged · Jul 13, 2025 · N748FD · Airbus A300B4622R · Cargo/Baggage Doors
  > CARGO DOOR / HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE M
- [SDR FDEA202502140226](https://openairdocs.org/sdr/FDEA202502140226.md): Outflow Valve · failed · Feb 14, 2025 · N748FD · Airbus A300B4622R · Pressure Regulator/Outflow Valve
  > NUMBER 1 OUTFLOW VALVE DEFERRED. AFTER TO #2 OUTFLOW STUCK FULL OPEN. COMPLIED WITH QRH REQUIRED MANUAL CONTROL TO OPEN ON TAXI IN. REMOVED AND REPALACED THE FWD OUTFLAW VALVE ASSY (202HM) I.A.W AMM 21-31-12-04 OPS CHECK PER AMM 21-31-00-5 OPS CHECK PASS
- [SDR FDEA202501220120](https://openairdocs.org/sdr/FDEA202501220120.md): Electronic Unit · failed · Jan 22, 2025 · N748FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > IN SYS 1 LANDING GEAR POSITION DETECTOR, TOOK OFF AND ATTEMPTED TO RAISE GEAR. UNABLE. WENT TO SYSTEM 2, GEAR CAME UP, BUT WE GOT MULTIPLE FAILURES. PITCH TRIM 1, ATS, CAPT PITOT OVERHEAT, FO PITOT OVERHEAT, STBY PITOT OVERHEAT, CAPT TAT HEAT FAILURE, CAB
- [SDR FDEA202410211569](https://openairdocs.org/sdr/FDEA202410211569.md): Power Supply · failed · Oct 21, 2024 · N748FD · Airbus A300B4622R · Emergency Lighting
  > ON MX PREFLIGHT: JUMPSEAT AREA EMERGENCY LIGHTS INOP. REPLACED EMERG. SUPPLY BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202407311071](https://openairdocs.org/sdr/FDEA202407311071.md): Warning Light · inoperative · Jul 31, 2024 · N748FD · Airbus A300B4622R · Emergency Equipment
  > ON POSTFLIGHT, R1 DOOR ESCAPE SLIDE RELEASE WARNING LIGHT INOP, BUZZER OPERATES NORMALLY. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CAT C EXP: AUG24 - R1__ CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP." R1 DOOR BUZZER OPERATES NORMAL,
- [SDR FDEA202407100980](https://openairdocs.org/sdr/FDEA202407100980.md): Hydraulic System · low · Jul 10, 2024 · N748FD · Airbus A300B4622R · Hydraulic System, Main
  > REJECTED TAKE OFF AT 40KTS FOR BLUE HYDRAULIC LOW ECAM CAUTION.
- [SDR FDEA202401230128](https://openairdocs.org/sdr/FDEA202401230128.md): Selector · inoperative · Jan 23, 2024 · N748FD · Airbus A300B4622R · Landing Gear Brake System
  > PERFORMED CAT III AUTOLAND WITH LOW BRAKES. DURING ROLLOUT PHASE, AIRCRAFT PULLED TO THE RIGHT WHEN AUTO BRAKES APPLIED. REQUIRED TO DISCONNECT AUTOPILOT AND RECENTER AIRCRAFT. WHEEL ECAM PAGE SHOWED RIGHT MAIN GEAR TEMPERATURE BETWEEN 450-500 DEGREES DEGRE
- [SDR FDEA202304200865](https://openairdocs.org/sdr/FDEA202304200865.md): Skin · dented · Apr 20, 2023 · N748FD · Airbus A300* · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FOUND 1EA DENT AT FR99 PLUS 5",S-4L PLUS 5" REPAIRED THE DAMAGE AREA WITH DOUBLER, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 53-19-12- 201, PARA.5, FIG.201, PAGE.204~208 "MAJOR REPAIR"
- [SDR FDEA202304200794](https://openairdocs.org/sdr/FDEA202304200794.md): Skin · delaminated · Apr 20, 2023 · N748FD · Airbus A300* · Elevator Structure
  > 1EA WATER TRAPPED AREA(140MM X 180MM) WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL T/E NO.26 SCREW. ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-21-12-201- 2, PARA.5F(REPAIR NO.6) PAGE.239-243, FIG.209(SHEET1-2) & SRI:55-21-
- [SDR FDEA202201080025](https://openairdocs.org/sdr/FDEA202201080025.md): Warning Message · false activation · Jan 8, 2022 · N748FD · Airbus A300B4622R · Drag Control System
  > ON FINAL APPROACH ON RW 27, KMEM AT 3000 FT, GOT A SPOILER FAULT WITH #7 SPOILER SHOWING UP. DID ECAM & QRH PROCEDURE AND COULD NOT GET IT TO GO DOWN. DECLARED AN EMERGENCY AND LANDED ON RW 36C, BRAKES WERE NOT SHOWING HOT. TAXIED BACK TO THE RAMP. S
- [SDR FDEA202112283154](https://openairdocs.org/sdr/FDEA202112283154.md): Sensor · faulted · Dec 28, 2021 · N748FD · Airbus A300B4622R · Engine Oil Temperature
  > HI ENG OIL TEMP #1, GOT INITIAL ADVISORY AT CRUISE LEVELOFF 35,000; 168C. FOLLOWED QRH ADVISORY WHICH LED TO ENG OIL HI TEMP QRH PROCEDURE. TEMPERATURE PEAKED AT 176C, SHOWED 36C TO 40C HOTTER THAN #2 ENG DURING DESCENT AT FLIGHT IDLE. EMERGENCY DECLARED,
- [SDR FDEA202107051678](https://openairdocs.org/sdr/FDEA202107051678.md): Spar · damaged · Jul 5, 2021 · N748FD · Airbus A300B4622R · Wing Spar
  > DURING THE EO NO: E 6-5710-E0342809 B P3 PARA. 5, FOUND THE HOLE "I" HAD BEEN ENLARGE ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE I REPAIR I.A.W. A300-600 EA NO: T6-5710-T0362021 P1, SEQ NO: 001077
- [SDR FDEA202107021649](https://openairdocs.org/sdr/FDEA202107021649.md): Frame · cracked · Jul 2, 2021 · N748FD · Airbus A300B4622R · Fuselage Main, Frame
  > DURING EA NO: T 6-5710-T0307375 P2, FOUND HOLE "S" DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENERS HOLES CRACK REPAIR I.A.W. A300-600 EA NO: T6-5710- T0307375 A P3, SEQ NO: 001079.
- [SDR FDEA202106171559](https://openairdocs.org/sdr/FDEA202106171559.md): Panel · cracked · Jun 17, 2021 · N748FD · Airbus A300B4622R · Nacelle/Pylon, Attach Fittings
  > PFM E.O. NACELLES /PYLONS INSP FOUND NO.2 PYLON O/B SIDE PNL AT RIB 8 HAS CRACK ALONG FRONT SCREW HOLE IAW WORK CARD SEQ 000960 INSPECTION OF PYLON SIDE PANELS AT RIB 8 AIRBUS SBA300-54- 6015 R03 & A310-54-2018 R03 E.O. 6-5450-7-5003 H PT4 SUBSTEP A. THRU
- [SDR FDEA202106121517](https://openairdocs.org/sdr/FDEA202106121517.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #232RG FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121516](https://openairdocs.org/sdr/FDEA202106121516.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #232CF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121515](https://openairdocs.org/sdr/FDEA202106121515.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #241PH FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121514](https://openairdocs.org/sdr/FDEA202106121514.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #262XF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121513](https://openairdocs.org/sdr/FDEA202106121513.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #152GF FLOOR PANEL OF LOWER AFT CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121512](https://openairdocs.org/sdr/FDEA202106121512.md): Floor Panel · broken · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #132RF FLOOR PANEL OF LOWER FWD CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.
- [SDR FDEA202106121511](https://openairdocs.org/sdr/FDEA202106121511.md): Floor Panel · damaged · Jun 12, 2021 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE #162HF FLOOR PANEL WAS FOUND SOFTEN & SERIOUS DAMAGED OVER HALF AREA FABRICATED THE FLOOR PNL I.A.W. FEDEX DWG. SRZ-25-005, REV. R AND SRZ25-011, REV. E.
- [SDR FDEA202106071453](https://openairdocs.org/sdr/FDEA202106071453.md): Seat Track · gouged · Jun 7, 2021 · N748FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK CROWN AREA GOT A GOUGE AT FR 59,-Y450 PERFORM CUT OUT DAMAGE TRACK ( LENGTH 30.6") & REINFORCED REPAIR PART AND SPLICE U- SECTION WORK INSTUCTION I.A.W A300-600 SRM SUPPLEMENT 53-10-16-201, PARA 5 FG 202, P. 209-214
- [SDR FDEA202106071451](https://openairdocs.org/sdr/FDEA202106071451.md): Seat Track · gouged · Jun 7, 2021 · N748FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK CROWN FOUND GOUGE BTWN FR26 16" AND FR26 18". ACCOMPLISHED THE FLOOR SEAT TRACK REPAIR I.A.W. A300-600 SRM 53-10-16-201, PARA. 10, FIG. 208 (SHEET 1) P. 243-248.
- [SDR FDEA202106071454](https://openairdocs.org/sdr/FDEA202106071454.md): Skin · delaminated · Jun 7, 2021 · N748FD · Airbus A300B4622R · Spoilers
  > 2EA DELAMINATIONS WERE FOUND. AREA 1 (80CM2) NEAR O/B HINGE ARM OF RH SPOILER 4. AREA 2 (82CM2) NEAR I/B HINGE ARM OF RH SPOILER 4. ACCOMPLISHED THE WORK: WING - FLIGHT SURFACES - RH 4# SPOILER LOWER SKKIN DELAMINATION NEAR CENTER HINGE ARM REPAIR I.A.W.
- [SDR FDEA202106071452](https://openairdocs.org/sdr/FDEA202106071452.md): Seat Track · gouged · Jun 7, 2021 · N748FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > M/D Y1456 SEAT TRACK CROWN GOUGE AT FR66 12.5" ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W. A300-600 SRM SUPPLEMENT 53-10-16-201, PARA. 5, FIG. 202, P. 209-214.
- [SDR FDEA202106021432](https://openairdocs.org/sdr/FDEA202106021432.md): Skin · dented · Jun 2, 2021 · N748FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING O/B FLAP L/E NOSE GOT A DENT AT RIB17 5". ACCOMPLISHED THE DENTED AREA REPAIR I.A.W. A300-600 SRM 57-50-00-201, PARA. 4H, P. 230- 234, FIG. 208. THIS IS CAT. B REPAIR I.A.W. A300-600 SRM 57-50-00-201, P. 202 AND SRI 57-50-00-201 IIR 57-50- 00-2- 00
- [SDR FDEA201906291441](https://openairdocs.org/sdr/FDEA201906291441.md): Power Supply · inoperative · Jun 29, 2019 · N748FD · Airbus A300B4622R · Door Warning System
  > MDIS 748 52-70 3083 29JUN19 MEM FACT U WHILE TROUBLESHOOTING R1 DOOR, PERFOMED BITE TEST OF ASPSU REF AMM 52-73-00-05-01 AND FOUND TEST TO BE FAILING. SHOWS BAT 1 AND BAT 2 FAILURE. REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: POS: ON
- [SDR FDEA201906161314](https://openairdocs.org/sdr/FDEA201906161314.md): Switch · chafed · Jun 16, 2019 · N748FD · Airbus A300F4622R · Service Doors
  > RT SIDE ENTRY DOOR, IN FLIGHT, MAKING LOUD SQUEAL AND HAS A FLASHING RED LIGHT. INDICATIONS WERE NORMAL WHEN ARMED ON THE GRD. COCKPIT INDICATIONS NORMAL. DURING FLIGHT. CORRECTED ITSELF AFTER LANDING WITH NO PRESSURIZATION IN CABIN AREA. TROUBLESHOT REF
- [SDR FDEA201905291181](https://openairdocs.org/sdr/FDEA201905291181.md): Limit Switch · out of adjust · May 29, 2019 · N748FD · Airbus A300B4622R · Door Warning System
  > AFTER FLIGHT, JUMPSEATER REPORTED THAT RIGHT CREW ENTERY DOOR (R1) WAS BEEPING AND PRESSURE LIGHT WAS ON ABOVE 10,000 FEET. THERE WERE NO INDICATIONS IN THE COCKPIT. ADJUST R1 DOOR LIMIT SWITCH 10WN REF. MM 52-73-13-05-01 FIGURE 501. OPS CHECKED GOOD, RETURN
- [SDR FDEA2019042520880](https://openairdocs.org/sdr/FDEA2019042520880.md): Floor Panel · delaminated · Apr 22, 2019 · N748FD · Airbus A300B4622R · Fuselage Floor Panel
  > FLOOR PANEL P/N A5398408500600 IS CRUSHED ON THE INBOARD SIDE OF TOP PANEL AND MISSING A SECTION OF PANEL. FABRICATED NEW FLOOR PANEL PER DWG SRZ-25-005 REV P
- [SDR FDEA2019041630791](https://openairdocs.org/sdr/FDEA2019041630791.md): Indicator · malfunctioned · Apr 13, 2019 · N748FD · Airbus A300B4622R · Airspeed/Mach Indicator
  > REJECTED TAKE-OFF TO STAGNATED AIRSPEED @ 100 KIAS BOTH CAPT AND F\O AIRSPEED INDICATORS. PERFORMED RTO CHECK LIST. NO BRAKE FANS INSTALLED ON THIS AIRCRAFT, TAXI BACK TO GATE 823 WITH HOT BRAKES, MOST TEMPS ON BRAKES WERE ABOVE 440 ON RIGHT ECAM. TR
- [SDR FDEA201903130586](https://openairdocs.org/sdr/FDEA201903130586.md): Selector Valve · inoperative · Mar 13, 2019 · N748FD · Airbus A300B4622R · Landing Gear Selector
  > ON GEAR EXTENSION GEAR DID NOT COME DOWN RECYCLEED GEAR 3 REDS PROC "MAIN GEAR EXT"ACCOMPLISHED PER QRH. POS DET 1& 2. GOT TOWED TO RAMP. HYD SYST NORMAL IN FLIGHT AFTER BLOCK IN GREEN SYST OFF SCALE HIGH. RESET MANUAL GEAR EXTENSION TO NORMAL POSITION IAW AMM
- [SDR FDEA201811103179](https://openairdocs.org/sdr/FDEA201811103179.md): Restrictor Valve · dirty · Nov 10, 2018 · N748FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR TOOK AN EXTRA 20 SECONDS TO COME DOWN WE ALMOST HAD TO GO AROUND. REMOVED AND CHECKED LEFT MAIN GEAR VALVE AND GEAR DOOR RESTRICTOR VALVES. FOUND DIRT IN GEAR RESTRICTOR VALVE. REPLACED GEAR RESTRICTOR PER AMM 32-31-57-04 AND GEAR DOOR RESTRICTO

Next page: https://openairdocs.org/aircraft/N748FD/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 = 'N748FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N748FD/reports

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