# Service difficulty reports: N749FD

A list on [N749FD](https://openairdocs.org/aircraft/N749FD.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 4 · 180 reports

- [SDR FDEA202608071109](https://openairdocs.org/sdr/FDEA202608071109.md): Skin · corroded · Aug 7, 2026 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > AVIONICS COMPARTMENT FR 18 - 19, STRINGERS 50L - 51L INNER SKIN CORRODED. REPAIRED THE CORRODED SKIN AT AVIONICS COMPARTMENT FR18 - FR19, S50L - S51L. THIS IS CATEGORY B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE ASSESSMENT(DT) APPROVAL. SOLUTION LIFE OR
- [SDR FDEA202607301137](https://openairdocs.org/sdr/FDEA202607301137.md): Fitting · none · Jul 30, 2026 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > CARGO DOOR, HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF TH
- [SDR FDEA202607221060](https://openairdocs.org/sdr/FDEA202607221060.md): Skin · punctured · Jul 22, 2026 · N749FD · Airbus A300B4622R · Leading Edge Devices
  > LH WING SLAT #2 LOWER SKIN BETWEEN INBOARD RIB AND RIB 2 FOUND PUNCTURE. COMPLIED WITH EA 6-5750-T0388161 P1. LH WING SLAT #2 LOWER SKIN PUNCTURED AREA BETWEEN INBOARD RIB AND RIB 2. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57
- [SDR FDEA202504110588](https://openairdocs.org/sdr/FDEA202504110588.md): Harness · inoperative · Apr 11, 2025 · N749FD · Airbus A300B4622R · Emergency Equipment
  > FO LEFT SHOULDER HARNESS WON T RELEASE LEFT SHOULDER HARNESS INERTIAL REEL DOES NOT MOVE EVEN WITH THE LOCK RELEASED. ORDER SEAT AS REQUIRED REMOVED AND REPLACED FIRST OFFICER SEAT SAFETY HARNESS PER AMM 25-11-63-04-01. OPS CHECK OK
- [SDR FDEA202504010547](https://openairdocs.org/sdr/FDEA202504010547.md): Hydraulic System · faulted · Apr 1, 2025 · N749FD · Airbus A300B4622R · Hydraulic System, Main
  > HYD GREEN RSVR LO LEVEL. COMPLIED WITH QRH AND ECAM. LANDED UNEVENTFULLY. ***EMERGENCY DECLARED*** MX PERFORMED A DVI OF THE THE A/C NO LEAKS NOTED. MX SPOKE WITH THE FLIGHT CREW AT 32,000 FT THE GOT A LOW LEVEL ON THEIR GREEN HYD SYSTEM AND THEY PERFORM
- [SDR FDEA202503170450](https://openairdocs.org/sdr/FDEA202503170450.md): Slide · malfunctioned · Mar 17, 2025 · N749FD · Airbus A300B4622R · Emergency Equipment
  > RIGHT SIDE SLIDE WILL NOT ARM. AMM: 52-73-00-05-01 RESET ASPSU AND C/W ADJ/TEST IAW A300-600 AMM CH. REF. LISTED ABOVE. ALL DOOR INDICATIONS AND WARNINGS OPS CK NORMAL. A/C OK FOR SERVICE.
- [SDR FDEA202503040328](https://openairdocs.org/sdr/FDEA202503040328.md): Lug · corroded · Mar 4, 2025 · N749FD · Airbus A300B4622R · Wing, Attach Fittings
  > RIGHT HAND WING AFT PINTLE FWD LUG HAS EVIDENCE OF CORROSION BETWEEN BUSHINGS "D" AND "E". ACCOMPLISHED REPAIR ON EA # 6-5710-T0306535 B PART 2 "WINGS - BASIC WING STRUCTURE - R/H RIB 5 LUG HAS CORROSION" STEPS 1 - 9.
- [SDR FDEA202503040327](https://openairdocs.org/sdr/FDEA202503040327.md): Lug · corroded · Mar 4, 2025 · N749FD · Airbus A300B4622R · Wing, Attach Fittings
  > LEFT HAND WING AFT PINTLE FWD LUG HAS EVIDENCE OF CORROSION BETWEEN BUSHINGS "D" AND "E". ACCOMPLISHED REPAIR ON STEPS 1-9 OF EA # 6-5710-T0382242 " WINGS - BASIC WING STRUCTURE - L/H MLG RIB 5, FWD LUG - CORROSION". MAJOR REPAIR.
- [SDR FDEA202409051245](https://openairdocs.org/sdr/FDEA202409051245.md): Hydraulic Line · leaking · Sep 5, 2024 · N749FD · Airbus A300B4622R · Hydraulic System, Main
  > AFTER DEPARTING KSDF LEFT ECAM DISPLAYED GREEN HYD SYS LO PR. AFTER RUNNING STEPS ON ECAM AND FOLLOWED QRH WHICH LED TO GRAVITY EXTENSION OF THE LANDING GEAR BECAUSE THERE WAS NO GREEN HYDRAULIC FLUID.
- [SDR FDEA202402220246](https://openairdocs.org/sdr/FDEA202402220246.md): Angle · bent · Feb 22, 2024 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FUSELAGE AFT TAIL SECTION FR86 TO FR87 FOUND 2EA ANGLES DEFORMED. DEFORMED ANGLES REMOVED AND REPLACED NEW ONE INSTALLED WITH RIVETS.(2EA) I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.6, PAGE.7B-23. REPAIR CLASSIFIED AS MINOR PER GMM
- [SDR FDEA202401300354](https://openairdocs.org/sdr/FDEA202401300354.md): Skin · cracked · Jan 30, 2024 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > 1EA CRACK INDICATION WAS FOUND AT R/H FR54, STR44 FASENTER HOLE. ACCOMPLISHED THE TRIM-OUT REPAIR AND REINFORCED WITH SHIM & EXTERNAL DOUBLER AT FR54 S-44R, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5330- T0378095 P1, SEQ NO:974, TITL
- [SDR FDEA202401270301](https://openairdocs.org/sdr/FDEA202401270301.md): Fitting · cracked · Jan 27, 2024 · N749FD · Airbus A300B4622R · Wing Main, Frame Structure
  > 1EA CRACK(7MM) WAS FOUND AT LH WING FR40 LOWER OUTBOARD RADIUS AREA. ACCOMPLISHED TRIM OUT INSTALLED WITH FILLER & COVER PLATE I.A.W EO:E6-5710- E0333574 I P23, SEQ NO:955 & EA:T6-5710-T0378152 P1, SEQ NO:965, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 (AT
- [SDR FDEA202401250302](https://openairdocs.org/sdr/FDEA202401250302.md): Skin · damaged · Jan 25, 2024 · N749FD · Airbus A300B4622R · Cargo/Baggage Doors
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FWD CARGO DOOR INNER SKIN AT FR21, BEAM1 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202401250125](https://openairdocs.org/sdr/FDEA202401250125.md): None · none · Jan 25, 2024 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 3", T/E-39" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEN
- [SDR FDEA202401250124](https://openairdocs.org/sdr/FDEA202401250124.md): None · none · Jan 25, 2024 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 3",T/E-20" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202401240306](https://openairdocs.org/sdr/FDEA202401240306.md): Frame · cracked · Jan 24, 2024 · N749FD · Airbus A300B4622R · Fuselage Main, Frame
  > 1EA CRACK WAS FOUND AT THE RIVET HEAD OF THE SEAL RETAINER RUN OUT HOLE AT FRAME 73A RH. ACCOMPLISHED THE SPLICE REPAIR AT RH DOOR FRAME FR73A I.A.W FEDEX EA NO:T6-5310- T0377912 P1, SEQ NO:971, TITLE:FUSELAGE-MAINFRAME-E0 6-5310-E0327267(SB A300-53-6175)
- [SDR FDEA202401230277](https://openairdocs.org/sdr/FDEA202401230277.md): Web · cracked · Jan 23, 2024 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT WAS FOUND WEB CRACK AT FR21,S-44L-2" REPLACED THE CRACK WEB WITH NEW ONE AT FR21, S-44L-2" I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 6, PAGE7B-23, REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.
- [SDR FDEA202401230218](https://openairdocs.org/sdr/FDEA202401230218.md): Panel · deformed · Jan 23, 2024 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > AFT CGO DOOR CUTOUT UPR FWD CORNER FOUND PANEL DEFORM FR59A~FR61, STR 28R. REPLACED THE PLATE WITH NEW PART. IAW A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B ~ PAGE.23
- [SDR FDEA202401230217](https://openairdocs.org/sdr/FDEA202401230217.md): Floorbeam · cracked · Jan 23, 2024 · N749FD · Airbus A300B4622R · Fuselage Main, Floor Beam
  > FLOOR STRUCTURE CROSS BEAM SUPPORT ANGLE CRACK AT FWD E/E COMPARTMENT FR10, PLUSY953MM POS REPLACED THE ANGLE WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2.
- [SDR FDEA202401230137](https://openairdocs.org/sdr/FDEA202401230137.md): Floorbeam · none · Jan 23, 2024 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPT FLOOR CROSSBEAM BTW -Y140 ~ -Y805, FR63 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING RE
- [SDR FDEA202401220212](https://openairdocs.org/sdr/FDEA202401220212.md): Bracket · corroded · Jan 22, 2024 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > AFT CGO COMPT FWD PARTITION LINING SUPPORT FOUND CORROSION AT FR 54 UNDER FLOOR STRUCTURE Y450~Y-450 CORROSION BRACKET REPLACED NEW PART, INSTALLED WITH RIVETS. I.A.W A300-600 SRM 51-72- 10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B-23, AS PER GMM 6-2-10
- [SDR FDEA202401200123](https://openairdocs.org/sdr/FDEA202401200123.md): None · none · Jan 20, 2024 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR86~87,STGR 43~45L COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202311071840](https://openairdocs.org/sdr/FDEA202311071840.md): Unknown · unknown · Nov 7, 2023 · N749FD · Airbus A300* · Standard Practices/Structures
  > PDIS 749 05-50 7037 07NOV23 MEM MULTIPLE BIRD STRIKES AT LIFTOFF. ***EMERGENCY DECLARED**** FACT 07NOV23 19:05 MEM AMM: 05-51-14-00 PERFORMED BIRD STRIKE INSPECTION REF. AMM 05-51-14-00,CLEANED BLOOD STAIN ON NOSE RADOME AND BOTH ENGINES,
- [SDR FDEA202206011354](https://openairdocs.org/sdr/FDEA202206011354.md): Tachometer · unknown · Jun 1, 2022 · N749FD · Airbus A300* · Brake
  > PDIS 749 32-42 5282 01JUN22 MEM FACT U ON LANDING, LEFT LANDING GEAR TRUCK BRAKE TEMP IMMEDIATELY EXCEEDED 300 DEGREES ON WHEELS 2, 5, AND 6. TEMPS ON 2 AND 5 REACHED 700 DEGREES ON TAXI IN WITH FANS RUNNING. WHEEL 1 BRAKE NEVER EXCEEDED 50
- [SDR FDEA202108142016](https://openairdocs.org/sdr/FDEA202108142016.md): Fire Loop · faulted · Aug 14, 2021 · N749FD · Airbus A300B4622R · Fire Detection
  > NO. 2 ENGINE LOOP B FAULTED IN FLIGHT MEL 14AUG21 23:34 ANC U RELEASED FOR SERVICE PER MEL: 26-12-01-01-A CATEGORY: C EXPIRATION: 24AUG21 "MEL 26-12-01-01-A: ENG 2 LOOP B - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST OF ENG FIRE WARNING SYSTEM
- [SDR FDEA202108091997](https://openairdocs.org/sdr/FDEA202108091997.md): Skin · chafed · Aug 9, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > RH FWD PAX DOOR UPR CUTOUT SKIN FOUND CHAFE MARKS REPAIRED THE CHAFE MARKS AT RH FWD PAX DOOR UPR CUTOUT SKIN (FAIL SAFE RING) PER EA 6-5310-T0363353 A P1. TITLE: FUSELAGE MAINFRAME - RH FWD CREW/COURIER DOOR FAIL SAFE RING CHAFE/WEAR DAMAGE - BLEND REPAIR
- [SDR FDEA202108011910](https://openairdocs.org/sdr/FDEA202108011910.md): Fitting · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Wing, Attach Fittings
  > JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTEN
- [SDR FDEA202108011908](https://openairdocs.org/sdr/FDEA202108011908.md): Frame · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Frame
  > FUSELAGE - MAIN FRAME - LH GANTRY 5 RH SIDE LWR FLANGE AT FR52.A FOUND CRACK SIGNAL REPAIRED THE CRACKED MAINFRAME LH #5 GANTRY RH SIDE LWR FLANGE AT FR52.A PER EO: 6-5310-7-5021 E PT8 & AIRBUS DWG: R53810583 ISSUE:D. THIS IS CATEGORY A REPAIR. MAJOR MAJ
- [SDR FDEA202108011911](https://openairdocs.org/sdr/FDEA202108011911.md): Fitting · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR42 RH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR42 RH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTE
- [SDR FDEA202108011909](https://openairdocs.org/sdr/FDEA202108011909.md): Fitting · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 RH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 RH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTEN
- [SDR FDEA202108011907](https://openairdocs.org/sdr/FDEA202108011907.md): Structure · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Structure
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "E" HOLE FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE FASTENER "E" HOLE CRACK P
- [SDR FDEA202108011905](https://openairdocs.org/sdr/FDEA202108011905.md): Web · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, LOWER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND LOWER CRACKED FASTENER HOLE PER EA 6-57
- [SDR FDEA202108011904](https://openairdocs.org/sdr/FDEA202108011904.md): Skin · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, MIDDLE FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND MIDDLE CRACKED FASTENER HOLE PER EA 6-
- [SDR FDEA202108011903](https://openairdocs.org/sdr/FDEA202108011903.md): Skin · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, UPPER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND UPPER CRACKED FASTENER HOLE PER EA 6-5
- [SDR FDEA202108011906](https://openairdocs.org/sdr/FDEA202108011906.md): Beam · cracked · Aug 1, 2021 · N749FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT CARGO - FR61 DOOR SILL BEAM FLAG CRACK WAS DEVEALED BY HFEC INSPECTION REPAIRED THE AFT CARGO FR61 CRACKED DOOR SILL BEAM FLAG PER EA 6-5320-T0363121 P1. TITLE: FUSELAGE - AUXILIARY STRUCTURE - SILL BEAM FLAG CRACK AT FR61 - REPAIR *THIS EA DEVIATES FR
- [SDR FDEA202107201819](https://openairdocs.org/sdr/FDEA202107201819.md): Seat Track · gouged · Jul 20, 2021 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FR74-FR75 -Y1137.1 SEAT TRACK FOUND GOUGE MARKS REPAIRED THE MAIN DECK FR74-FR75 -Y1137.1 SEAT TRACK PER A300-600 SRM53-10-16-201 FIG.208 SHEET 1. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202107201818](https://openairdocs.org/sdr/FDEA202107201818.md): Seat Track · gouged · Jul 20, 2021 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FR60-FR61 Y1456 SEAT TRACK FOUND GOUGE MARKS REPAIRED THE MAIN DECK FR60-FR61 Y1456 SEAT TRACK PER A300-600 SRM53-10-16-201 FIG.208 SHEET 1. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202010112461](https://openairdocs.org/sdr/FDEA202010112461.md): Smoke Detector · false activation · Oct 11, 2020 · N749FD · Airbus A300B4622R · Smoke Detection
  > PDIS 749 26-12 3604 10OCT20 MEM FACT U. PASSING FL 200 ON CLIMB OUT, GOT MAIN DECK AFT SMOKE WARNING. WARNING STOPPED AFTER A FEW MINUTES. RETURNED TO MEM, NO EXTERIOR INDICATIONS ON GROUND FROM RESCUE ON SEAN. SHGN 10OCT20 23:39 MEM U. UPON INSPECTION, N
- [SDR FDEA202009182249](https://openairdocs.org/sdr/FDEA202009182249.md): Hydraulic System · malfunctioned · Sep 18, 2020 · N749FD · Airbus A300B4622R · Hydraulic System, Main
  > PDIS 749 29-30 3529 18SEP20 MEM OPEN U. DURING TAKEOFF ROLL AT 50KTS, ECAM ALERT "HYD YELLOW PUMP LO PR" AND "YELLOW SYS LO PR" REJECTED TAKEOFF. CLEARING RWY NOTICED HYD YELLOW FLUID LEVEL ABOUT 4 NEEDLE WIDTHS BELOW TOPHAT. DID FLT CONT CHECK AND YELLOW
- [SDR FDEA201905171089](https://openairdocs.org/sdr/FDEA201905171089.md): Skin · cracked · May 17, 2019 · N749FD · Airbus A300B4622R · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN AT THE BOTH SIDE OF ACTUATOR ATTACH LUG FITTING CRACKED COMPLIED WITH EA # 6-5230-T0346774 P1, EA TITLE: DOORS - CARGO DOOR/HYD SYS - FWD CARGO DOOR INNER SKIN CRACKED AT FR22A. REPAIRED THE FWD CARGO DOOR INNER SKIN AT THE BOTH SIDE
- [SDR FDEA201905071011](https://openairdocs.org/sdr/FDEA201905071011.md): Floor Support · corroded · May 7, 2019 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FR11-FR15A Y953 FLOOR SUPPORT CORRODED REPLACED THE HEAVILY CORRODED FLOOR SUPPORT ON MAIN DECK FR11-FR15A Y953 PER SRM 51-40-21. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201905010974](https://openairdocs.org/sdr/FDEA201905010974.md): Skin · corroded · May 1, 2019 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN EXTERIOR SURFACE CORRODED, BTW FR0 AND FR1, STR 25L AND STR 26L REPAIRED THE CORRODED FUSELAGE SKIN BTW FR0 AND FR1, STR 25L AND STR 26L PER SRM 53-11-12-201 FIG201. THIS IS A CATEGORY "B" REPAIR, MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 5
- [SDR FDEA201904280951](https://openairdocs.org/sdr/FDEA201904280951.md): Beam · unknown · Apr 29, 2019 · N749FD · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON AFT CARGO COMPARTMENT CROSSBEAM AT FR60 BETWEEN -Y805 AND -Y1470 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON AFT CARGO COMPARTMENT CROSSBEAM AT FR60 BETWEEN -Y805 AND -Y1470 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH CURR
- [SDR FDEA201904280952](https://openairdocs.org/sdr/FDEA201904280952.md): Doubler · corroded · Apr 28, 2019 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR11A AND FR13 BELOW TOILET SERVICE DOOR REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR11A AND FR13 BELOW TOILET SERVICE DOOR FOUND IN CONFORMITY WITH RAS/AS/128/2003 ISSUE A AND FOUN
- [SDR FDEA201904280945](https://openairdocs.org/sdr/FDEA201904280945.md): Doubler · worn · Apr 28, 2019 · N749FD · Airbus A300B4622R · Trailing Edge Flaps
  > EXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH TD FOK/1
- [SDR FDEA201901250196](https://openairdocs.org/sdr/FDEA201901250196.md): Pressure Switch · failed · Jan 25, 2019 · N749FD · Airbus A300B4622R · Hydraulic Pressure Sensor
  > FOLLOWING T/O KMEM ECAM: (GREEN SYS LO PR) CONFERRED WITH DISPATCH / MAINT DECISION TO RETURN KMEM. FOLLOWED ECAM AND QRH PROCEDURES. GREEN HYD LVL IN GREEN BAND/PRESS ON ECAM 3100 PSI. CAPT CONFIRMED L/G WAS MANUALLY EXTENDED PER QRH. RESTORED LANDING GEAR TO
- [SDR FDEA201707292080](https://openairdocs.org/sdr/FDEA201707292080.md): Windshield · failed · Jul 29, 2017 · N749FD · Airbus A300B4622R · Flight Compartment Windows
  > FIRST OFFICER`S WINDSCREEN SHATTERED AFTER WINDOW HEAT FAULT. NO CRACKS INSIDE PANE. REMOVED AND REPLACED THE WINDSCREEN IAW AMM 56-11-11-04 AND PERFORMED ADJUSTMENT AND TEST IAW AMM 30-42-00-05. OK FOR SERVICE.
- [SDR FDEA201706141663](https://openairdocs.org/sdr/FDEA201706141663.md): Processor · failed · Jun 14, 2017 · N749FD · Airbus A300B4622R · Speed-Attitude Correction System
  > DURING CLIMB OUT NR 1 PITCH TRIM CLICKED OFF, NO RESET, NR 2 PITCH TRIM RETURNED TO DEPARTURE. REMOVED AND REPLACED THE PROXIMITY DETECTOR PROCESSING UNIT IAW AMM 32-31-71-04. OPS CHECKED GOOD. REPLACED THE NLG RELAYS 96GB AND 141GB IAW ESPM FOR FLAGGED FAU
- [SDR FDEA201702180587](https://openairdocs.org/sdr/FDEA201702180587.md): Indicator · malfunctioned · Feb 18, 2017 · N749FD · Airbus A300B4622R · Fuel Indicating System
  > DUE TO QRH PROCEDURES LEAVING CROSSFEED OPEN WITH LOW FUEL INDICATIONS, LANDED OUT OF TANK LIMITS. LEFT TANK, 7.8 RT TANK 4.6. IAW MOCC AND ENGN STICK FUEL QTY IN TANKS BOTH OUTER TANKS READING PER INDICATION L/H OUTER 7.5 AND STICK READING WAS 30 ON ST
- [SDR FDEA201702090475](https://openairdocs.org/sdr/FDEA201702090475.md): Fire Loop · malfunctioned · Feb 9, 2017 · N749FD · Airbus A300B4622R · Fire Detection
  > INFLIGHT WHEN LEVELING AT FLIGHT 330, LOOP A LIGHT ILLUMINATED ON NR 2 ENGINE. FOLLOWED QRH. PERFORMED BITE CHECK OF NR 2 ENGINE FIRE DETECTION CONTROL UNIT IAW MM 26-12-00-05-01, NO FAULTS, OPENED THE NR 2 ENG AND CHECKED RESISTENCE OF A LOOP RESPONDE

Next page: https://openairdocs.org/aircraft/N749FD/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 = 'N749FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N749FD/reports

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