# Service difficulty reports: N726FD

A list on [N726FD](https://openairdocs.org/aircraft/N726FD.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 · 237 reports

- [SDR FDEA202308021855](https://openairdocs.org/sdr/FDEA202308021855.md): Trunnion · unknown · Aug 2, 2023 · N726FD · Airbus A300* · Fuselage, Landing Gear Attach Fittings
  > RIB 5 FWD GEAR TRUNION PINTLE HAS HEAVY PITTINGIN BETWEEN BEARING HALFSAT 2:00 TO 3:00 OCLOCK POSITIONS. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425
- [SDR FDEA202307051147](https://openairdocs.org/sdr/FDEA202307051147.md): Frame · cracked · Jul 5, 2023 · N726FD · Airbus A300* · Fuselage Main, Frame
  > FUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24L - S25L REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24L - S25L PER FEDEX EA: #: 6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH&RH DOOR FRA
- [SDR FDEA202307051146](https://openairdocs.org/sdr/FDEA202307051146.md): Frame · cracked · Jul 5, 2023 · N726FD · Airbus A300* · Fuselage Main, Frame
  > FUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24R - S25R REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24R - S25R PER FEDEX EA:#:6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH &RH DOOR FR
- [SDR FDEA202307031142](https://openairdocs.org/sdr/FDEA202307031142.md): Spoiler · delaminated · Jul 3, 2023 · N726FD · Airbus A300* · Spoilers
  > RH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1): 50MM*20MM, DEPTH: 1.60MM (2): 10MM*15MM DEPTH:2.3MM PERFORMED THE REPAIR ON RH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARM
- [SDR FDEA202307031141](https://openairdocs.org/sdr/FDEA202307031141.md): Spoiler · delaminated · Jul 3, 2023 · N726FD · Airbus A300* · Spoilers
  > RH WING #3 SPOILER INBD HINGE ARM INBD SURFACE FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.70MM PERFORMED THE REPAIR ON RH WING #3 SPOILER INBD HINGE ARM INBD SURFACE PER FEDEX EA # 6-5750-T0374955 TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HIN
- [SDR FDEA202204251049](https://openairdocs.org/sdr/FDEA202204251049.md): Angle · damaged · Apr 25, 2022 · N726FD · Airbus A300* · Wing Main, Frame Structure
  > (6-5710-T0307446 B PT4) R/H REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLES "A" HAS REJECTABLE INDICATION NOTED AT BOTTOM LAYERS. REPAIRED FASTENER HOLE "A" PER EA 6-5710-T0307446 C PT8 WINGS - BASIC WING STRUCTURE - AD 201
- [SDR FDEA202204251048](https://openairdocs.org/sdr/FDEA202204251048.md): Angle · cracked · Apr 25, 2022 · N726FD · Airbus A300* · Wing Main, Frame Structure
  > (6-5710-T0307446 B PT4) L/H REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLE "G" HAS CRACK INDICATION NOTED AT 12:0'CLOCK BOTTOM LAYERS. REPAIRED FASTENER HOLE "G" PER EA T-6-5710-T0307446 C PT8 WINGS - BASIC WING STRUCTURE - A
- [SDR FDEA202204221029](https://openairdocs.org/sdr/FDEA202204221029.md): None · none · Apr 22, 2022 · N726FD · Airbus A300* · Fuselage Main, Structure
  > ENTERED FOR TRAINING PURPOSES ONLY NO ACTION REQUIRED.
- [SDR FDEA202204221028](https://openairdocs.org/sdr/FDEA202204221028.md): Joint · damaged · Apr 22, 2022 · N726FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > FWD CARGO FRAME 40 LH HAS FASTENERS WITH DAMAGED INDICATIONS HOLES A, B, AND C. COMPLIED WITH EA 6-5710-127939 PT8: WINGS - BASIC WING STRUCTURE - ALI WORKCARD 5710390-00-11 REPAIRED CRACKED HOLES IN CTR WING JOINT - FR 40 LH / RH. MAJOR REPAIR
- [SDR FDEA202108242081](https://openairdocs.org/sdr/FDEA202108242081.md): Switch · failed · Aug 24, 2021 · N726FD · Airbus A300B4622R · Hydraulic System, Main
  > RECEIVED 4 TRANSIENT ECAM GREEN HYD PR LO INDICATION DURING TAXI, WHICH ALSO CAUSED AN AUTO-BRAKE SYSTEM TO FAILURE. ANALOG AND ECAM GREEN HYD PRESSURE AND QUANTITY BOTH SHOWED GOOD WHILE ECAM MESSAGE WAS DISPLAYED. HAD TO ABORT T/O DUE TO SECOND INDIC
- [SDR FDEA202101270199](https://openairdocs.org/sdr/FDEA202101270199.md): Damper · no test · Jan 27, 2021 · N726FD · Airbus A300B4622R · Galley Doors
  > DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA (1 EA). REPLACED PASSENGER CREW DOOR 831 DOOR DAMPER, IAW A300-600 AMM 52-10-14-04-01 AND A300-600 AMM 52-10-14-05-01. PERFORMED FUNCTIONAL TEST, IAW A300-600 AMM 52-10-11-05-0
- [SDR FDEA202101160135](https://openairdocs.org/sdr/FDEA202101160135.md): Floor Panel · cracked · Jan 16, 2021 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 131CG IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131CG IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.
- [SDR FDEA202101160134](https://openairdocs.org/sdr/FDEA202101160134.md): Floor Panel · cracked · Jan 16, 2021 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 131AG IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131AG IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.
- [SDR FDEA202101160133](https://openairdocs.org/sdr/FDEA202101160133.md): Floor Panel · cracked · Jan 16, 2021 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 131UF IN FWD CARGO COMPARTMENT (1 EA) REPLACED FLOOR PANEL 131UF IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.
- [SDR FDEA202101110159](https://openairdocs.org/sdr/FDEA202101110159.md): Floor Panel · cracked · Jan 11, 2021 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 232TG IN MAIN DECK CARGO COMPARTMENT IN PASSENGER CABIN. REPAIRED FLOOR PANEL 232TG IN MAIN DECK CARGO COMPARTMENT IN PASSENGER CABIN, AS PER A300-600 SRM 53-10-20 PB201 PARA 9C (3)(B). TOOL USED CALIPER P/N 500-197-30 SN A18135103 DUE DATE
- [SDR FDEA202012310308](https://openairdocs.org/sdr/FDEA202012310308.md): Frame · cracked · Dec 31, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION AREA OPEN FASTENER HOLES LOWER POSITION RH SIDE, CRACK DIRECTION IS 6 O CLOCK IN FWD CARGO COMPARTMENT (1EA) PERFORMED REAPIR ON FRAME 40 TO CENTER WING JOINT AT UP
- [SDR FDEA202012310182](https://openairdocs.org/sdr/FDEA202012310182.md): Frame · cracked · Dec 31, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 13 OPEN FASTENER HOLE AT LEVEL OF STR 9 RT SIDE, CRACK DIRECTION IS 9 O`CLOCK AT FWD GALLEY AREA (1 EA). REPLACED STRINGER SECTION LOCATED ON FR 13 AT LEVEL STR 9 RT SIDE, IAW A300-600 SRM 51-40-20-001 AND DRAWING #A53610301 ISSUE K
- [SDR FDEA202012300439](https://openairdocs.org/sdr/FDEA202012300439.md): Pressure Deck · corroded · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Structure
  > CORROSION INTERNAL STRUCTURE FWD FACE PRESSURE DECK AT LEVEL FR 39 LOWER AREA IN FWD CARGO COMPARTMENT PERFORMED REPAIR ON PRESSURE BULKHEAD FR39 BTW STR 53LH TO STR 55LH IAW EA# 6- 5314-T0359508 TITLE: FUSELAGE CENTER SECTION-FR39 BULKHEAD BTW S-53LH TO S-
- [SDR FDEA202012300229](https://openairdocs.org/sdr/FDEA202012300229.md): Seat Track · corroded · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK Y953 BETWEEN FR 18 TO FR 19 IN PASSENGER CABIN (MAIN DECK). REPLACED SEAT TRACK Y953 BETWEEN FR 15 TO FR 19 IN PASESENGER CABIN (MAIN DECK), IAW A300-600 SRM 51-40-20 AND DWG NR A53781051 ISSUE A SHEET 3 AND DWG A53612502 ISSUE F SHEET 1.
- [SDR FDEA202012300205](https://openairdocs.org/sdr/FDEA202012300205.md): Floor Support · corroded · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y1213 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y1456 IN PASSENGER CABIN (MAIN DECK), IAW A300-600 DWG 53612310 ISSUE A AND A300-600 SRM 51-72-10.
- [SDR FDEA202012300184](https://openairdocs.org/sdr/FDEA202012300184.md): Floor Support · corroded · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y180 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE Y953 LOCATED BETWEEN FR 11 AND FR 15 IN (MAIN DECK), IAW A300-600 SRM 51-72-10 AND DRAWING A53612519 ISSUE AN.
- [SDR FDEA202012300181](https://openairdocs.org/sdr/FDEA202012300181.md): Frame · cracked · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 13 OPEN FASTENER HOLE AT LEVEL OF STR 9 LT SIDE, CRACK DIRECTION IS 3 O`CLOCK AT FWD GALLEY AREA (1 EA). REPLACED STRINGER SECTION LOCATED ON FR 13 AT LEVEL STR 9 LT SIDE, IAW A300-600 SRM 51-40-20-001 AND DWG #A53610301 ISSUE K SHEE
- [SDR FDEA202012300014](https://openairdocs.org/sdr/FDEA202012300014.md): Floor Support · corroded · Dec 30, 2020 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 13 Y730 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 13 Y730 IN PASSENGER CABIN (MAIN DECK), IAW A300-600 SRM 51-72-10 AND DWG A53612214 SHEET 01 ISSUE M.
- [SDR FDEA202012290324](https://openairdocs.org/sdr/FDEA202012290324.md): Crossbeam · cracked · Dec 29, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Structure
  > CRACK FRAME 15A CROSS BEAM AT ATTACHMENT FITTING OF RACK 107VU IN FWD AVIONIC COMPARTMENT PERFORMED REPAIR ON FRAME 15A CROSSBEAM ATTACHMENT FITTING OF RACK 107VU IN FWD AVIONIC COMPARTMENT IAW EA # 6-5310-T0358885 P1 EA TITLE: FUSELAGE-MAINFRAME - AD 20
- [SDR FDEA202012280444](https://openairdocs.org/sdr/FDEA202012280444.md): Frame · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44LT (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44LT (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMEN
- [SDR FDEA202012280443](https://openairdocs.org/sdr/FDEA202012280443.md): Frame · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 54 STGR 36 LH (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA)(CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC ON FRAME 54, STGR 36LH (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT IAW EA 6-5316-T0359314. TITLE: FUSELA
- [SDR FDEA202012280327](https://openairdocs.org/sdr/FDEA202012280327.md): Door · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Cargo/Baggage Doors
  > CRACK ON FORWARD WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A, ON AFT CARGO COMPARTMENT DOOR PERFORMED REPAIR ON FWD WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A ON AFT CARGO COMPARTMENT DOOR IAW EA# 6-5230-T0359408. TITLE: DOORS-CARGO DOOR /HYD SYS-AFT CARGO
- [SDR FDEA202012280447](https://openairdocs.org/sdr/FDEA202012280447.md): Skin · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC. ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCHES UPPER) OPEN HOLE IN AFT CARGO COMPA
- [SDR FDEA202012280328](https://openairdocs.org/sdr/FDEA202012280328.md): Web · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Cargo/Baggage Doors
  > CRACK ON AFT WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A, ON AFT CARGO COMPARTMENT DOOR PERFORMED REPAIR ON AFT WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A ON AFT CARGO COMPARTMENT DOOR IAW EA 6-5230-T0359408. TITLE: DOORS-CARGO DOOR/ HYD SYS-AFT CARGO DOOR
- [SDR FDEA202012280137](https://openairdocs.org/sdr/FDEA202012280137.md): Floor Panel · cracked · Dec 28, 2020 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 131TF IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131TF ON FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.
- [SDR FDEA202012260278](https://openairdocs.org/sdr/FDEA202012260278.md): Skin Panel · dented · Dec 26, 2020 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > DENT EXTERNAL SKIN FR 66 TO FR 67 AND STR 52R TO STR 54R AT LOWER FUSELAGE PERFORMED PERMANENT REPAIR ON DENTS LOC EXTERNAL SKIN FR66 TO FR67 AND STR 52R TO STR 54R AT LOWER FUSELAGE. IAW EA 6-5317-103271 A. TITLE: FUSELAGE - FUSELAGE AFT INTERMEDIATE SECT
- [SDR FDEA202012053040](https://openairdocs.org/sdr/FDEA202012053040.md): None · failed · Dec 5, 2020 · N726FD · Airbus A300B4622R · Engine (Turbine/Turboprop)
  > CLIMBING THRU 14000 ON DEPARTURE OUT OF KORF #2 ENGINE SLEZED EPR ROLLED BACK TO 0, NI INDICATED 13.5 % N2 WAS 0,EGT SPIKED TO 790 DEG, LOW OIL PRESS LIGHT ILLIMINATED. DIVIERTED TO KRIC AFTER DECLIARING EMERGENCY. #2 ENGINE REPLACEMENT.
- [SDR FDEA202011142842](https://openairdocs.org/sdr/FDEA202011142842.md): Sensing Element · failed · Nov 14, 2020 · N726FD · Airbus A300B4622R · Overheat Detection
  > DURNING CLIMBOUT ENGINE NO 1 BLEED LEAK, DIVERTED INTO TPA BECAUSE WE LOST PRESSURIZATION DUE TO DEFERRED NO 2 PACK, DECLARED EMERGENCY. FACT 15NOV20 16:06 TPA. R & R MANIFOLD OVERHEAT SENSING ELEMENT ON LT WING PYLON I/R/T MM 36-22-12-04, REMOVAL P/N 35518-
- [SDR FDEA201901180171](https://openairdocs.org/sdr/FDEA201901180171.md): Sensor · faulty · Jan 18, 2019 · N726FD · Airbus A300B4622R · Fuel Quantity Sensor
  > PDIS 726 28-20 3775 18JAN19 MEM OPEN U LOGPAGES:2958677 OPERATING IN MANUEL FUEL FEED PER THE MEL, CENTER TANK PUMPS OFF, ECAM MEMO PAGE SHOWED CTR TANK FEEDING. ON SCHEMATIC PAGE, CENTER TANK RIGHT PUMP DISPLAY SHOWS ON BUT FAULTED. (OF NOTE, DURING
- [SDR FDEA201812023414](https://openairdocs.org/sdr/FDEA201812023414.md): Proximity Sensor · failed · Dec 2, 2018 · N726FD · Airbus A300B4622R · Landing Gear Position and Warning
  > PER CREW VERBAL, GEAR WOULD NOT RETRACT IN POS DET SYS NR 1, (SYS 2 IS ON MEL). SWITCHED TO POS DET SYS NR 2 AND IT WORKED. COMPLETED INSTALL OF 8GB, AND 12GA BOGIE BEAM SENSOR INCLUDING DIMENSION CHECKS ON RT MAIN GEAR. STILL REQUIRES OPS CHECK. REMOVED AND R
- [SDR FDEA201811233357](https://openairdocs.org/sdr/FDEA201811233357.md): Proximity Sensor · inoperative · Nov 23, 2018 · N726FD · Airbus A300B4622R · Landing Gear Position and Warning
  > DURING TAKEOFF KMDT LANDING GEAR POSITION DET, SYS2 GEAR HANDLE CAME UP TO NORMAL POSITION, SELECTED SYS 1, WOULD NOT MOVE TO UP WENT BACK TO SYSTEM 2, GEAR HANDLE CAME UP NORMAL. REMOVED REPLACED ELECTRONIC PROXIMITY UNIT IAW MM 32-31-71-04. PERFORMED NORMAL
- [SDR FDEA201811223361](https://openairdocs.org/sdr/FDEA201811223361.md): Electronic Unit · failed · Nov 22, 2018 · N726FD · Airbus A300B4622R · Landing Gear Position and Warning
  > DURING TAKEOFF KMDT LANDING GEAR POSITION DET, SYS 2 GEAR HANDLE CAME UP TO NORMAL POSITION, SELECTED SYS 1, WOULD NOT MOVE TO UP WENT BACK TO SYSTEM 2, GEAR HANDLE CAME UP NORMAL. REMOVED REPLACED ELECTRONIC PROXIMITY UNIT IAW MM 32-31-71-04. PERFORMED NORM
- [SDR FDEA201807181771](https://openairdocs.org/sdr/FDEA201807181771.md): Duct · contaminated · Jul 18, 2018 · N726FD · Airbus A300B4622R · Air Distribution System
  > J/S REPORTED AN OILY ODOR IN COURIER COMP. WITH VISIBLE OILY SMOKE. THE FIRST OFFICER STATED THAT JUMPSEATERS NOTIFIED THE CREW THAT OILY SMOKE WAS COMING UP THROUGH THE FLOOR VENTS. F/O VERIFIED THAT IT WAS NOT CONDENSATION & WAS OILY SMOKE. NO SMOKE OR ODO
- [SDR FDEA201807161717](https://openairdocs.org/sdr/FDEA201807161717.md): Rib · cracked · Jul 16, 2018 · N726FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/Rib
  > RT PYLON RIB 19 HAS CRACK JUST AFT OF AFT PYLON MOUNT. COMPLIED WITH EA 6-5480-T0340823 P1 NACELLES/PYLON FILLETS/FAIRINGS-RW-HW PYLON, AFT FAIRING, RIB 19 CRACKED SRM REPAIR W/MINOR DEVIATIONS, REPAIR IS CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA2018071641712](https://openairdocs.org/sdr/FDEA2018071641712.md): Skin · damaged · Jul 14, 2018 · N726FD · Airbus A300B4622R · Trailing Edge Flaps
  > RT WING CENTER FLAP APPROX 16" FROM INBD END AND 19" FROM LEADING EDGE, LOWER SURFACE SKIN PREVIOUS REPAIR DEBONDED / CRACKS. REPLACED STRINGER SECTION, REPAIR ANGLE, PACKING PLATE, PACKING STRIPS, AND INSTALLED REPAIR FLAP SKIN DOUBLER IAW SRM 57-50-00-201 FI
- [SDR FDEA201807031619](https://openairdocs.org/sdr/FDEA201807031619.md): Floor Panel · cracked · Jul 2, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241WH HAS CRACK. FABRICATED FLOOR PANEL 241WH ON T18/1351638 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241WH INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807031618](https://openairdocs.org/sdr/FDEA201807031618.md): Floor Panel · cracked · Jul 2, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 214QH HAS CRACK. FABRICATED FLOOR PANEL 241QH ON T18/1350937 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241QH INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807031617](https://openairdocs.org/sdr/FDEA201807031617.md): Floor Panel · cracked · Jul 2, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241RJ HAS CRACK. FABRICATED FLOOR PANEL 241RJ ON T18/1350935 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241RJ INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807011613](https://openairdocs.org/sdr/FDEA201807011613.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241TH HAS EDGE CRACK. FABRICATED FLOOR PANEL 241TH ON T18/1351637 IAW DWG SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201807031616](https://openairdocs.org/sdr/FDEA201807031616.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251WH HAS CRACK. FABRICATED FLOOR PANEL 251WH ON T18/1351014 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251WH INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807031615](https://openairdocs.org/sdr/FDEA201807031615.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251GF HAS CRACK. FABRICATED FLOOR PANEL 251GF ON T18/1350940 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251GF INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807031614](https://openairdocs.org/sdr/FDEA201807031614.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251PH HAS CRACK. FABRICATED FLOOR PANEL 251PH ON T18/1351013 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251PH INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.
- [SDR FDEA201807031612](https://openairdocs.org/sdr/FDEA201807031612.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 242XH HAS CRACK. FABRICATED FLOOR PANEL 242XH ON T18/1350938 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201807031611](https://openairdocs.org/sdr/FDEA201807031611.md): Floor Panel · punctured · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241DF HAS VARIOUS PUNCTURES. FABRICATED FLOOR PANEL 241DF ON T18/1350934 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201807031610](https://openairdocs.org/sdr/FDEA201807031610.md): Floor Panel · cracked · Jul 1, 2018 · N726FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 242EF HAS CRACK. FABRICATED FLOOR PANEL 242EF ON T18/1350939 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N726FD/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 = 'N726FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N726FD/reports

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