# Service difficulty reports: N727FD

A list on [N727FD](https://openairdocs.org/aircraft/N727FD.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 · 185 reports

- [SDR FDEA202503080494](https://openairdocs.org/sdr/FDEA202503080494.md): Rib · damaged · Mar 8, 2025 · N727FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING I/B FLAP INTERNAL STRUCTURE WAS FOUND 1EA FASTENER HOLE ENLARGED AT RIB25A RS PLUS 5" FABRICATED WEB AND INSTALLED WITH FASTENERS AT LH I/B FLAP RIB25A RS PLUS 5" I.A.W AIRBUS DRAWING NO:A57960114 REV E SHEET 1 & A300-600 SRM 51-40-21-001, PARA7 P
- [SDR FDEA202503080444](https://openairdocs.org/sdr/FDEA202503080444.md): Plate · loose · Mar 8, 2025 · N727FD · Airbus A300F4622R · Wing Main, Frame Structure
  > LH WING I/B FLAP INTERNAL STRUCTURE WAS FOUND 1EA FASTENER HOLE ENLARGED AT RIB25A RS PLUS 5" FABRICATED WEB AND INSTALLED WITH FASTENERS AT LH I/B FLAP RIB25A RS PLUS 5" I.A.W AIRBUS DRAWING NO:A57960114 REV E SHEET 1 & A300-600 SRM 51-40-21-001, PARA7 P
- [SDR FDEA202503060447](https://openairdocs.org/sdr/FDEA202503060447.md): Rib · damaged · Mar 6, 2025 · N727FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > FOUND DAMAGE AT R5 SPOILER ACTUATOR OUTBOARD JACK RIB LOWER HOLE ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH WING #5 JACK RIB ABX184.625 I.A.W FEDEX EA NO: T6-5740-T0382580 P1, SEQ NO:1188, TITLE: WING-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX
- [SDR FDEA202503050359](https://openairdocs.org/sdr/FDEA202503050359.md): Floor Support · corroded · Mar 5, 2025 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT CORROSION AT FR12A PLUS 13", Y730 REPLACED THE CORRODED SUPPORT WITH NEW PART AT MAIN DECK FLOOR SUPPORT FR12A PLUS 13", Y730. I.A.W A300-600 SRM 51-72-10-001, PAGE.2& 51-40-21-001, PARA.6, PAGE.7B~23. THIS REPAIR IS CLASSIFIED AS M
- [SDR FDEA202503040488](https://openairdocs.org/sdr/FDEA202503040488.md): Fitting · not reported · Mar 4, 2025 · N727FD · Airbus A300B4622R · Cargo/Baggage Doors
  > REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO: E6-5230- E0378588B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN1- LONGN3 I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:1088, TITLE: DOORS-
- [SDR FDEA202503040487](https://openairdocs.org/sdr/FDEA202503040487.md): Fitting · not entered · Mar 4, 2025 · N727FD · Airbus A300B4622R · Cargo/Baggage Doors
  > REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO: E6-5230- E0378588B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN1- LONGN3 I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:1088, TITLE: DOORS
- [SDR FDEA202503020463](https://openairdocs.org/sdr/FDEA202503020463.md): Plate · cracked · Mar 2, 2025 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > PLATE CRACK FOUND AT FR22 STRG40 SIDE LEFT IN FWD CARGO COMPARTMENT REPLACED THE CRACKED PLATE WITH NEW PART AT FWD CARGO COMPARTMENT FR22, S-40L. I.A.W SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~PAGE.23. THIS REPAIR IS CLASSIFIED AS MINOR
- [SDR FDEA202503020451](https://openairdocs.org/sdr/FDEA202503020451.md): Flap · cracked · Mar 2, 2025 · N727FD · Airbus A300B4622R · Trailing Edge Flaps
  > 2EA CRACKS (5MM & 22MM) WERE FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RH WING CENTER FLAP RIB26, S-2.7~R/S AND EXTERNAL PLATE AT RH WING CENTER FLAP RIB26~27, S-2
- [SDR FDEA202503010486](https://openairdocs.org/sdr/FDEA202503010486.md): Skin · corroded · Mar 1, 2025 · N727FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING O/B FLAP UPPER SKIN GOT CORROSION AT STATIC DISCHARGER RETAINER CONTACT SURFACE. PERFORMED CUT OUT DAMAGED AREA AND INSTALLED REPAIR PATCH AT LH WING OUTER FLAP UPPER SKIN UNDERNEATH STATIC DISCHARGER I.A.W FEDEX EA NO:T6-5750-T0382504 P1, SEQ NO
- [SDR FDEA202501020003](https://openairdocs.org/sdr/FDEA202501020003.md): Pbe · expired · Jan 2, 2025 · N727FD · Airbus A300B4622R · Emergency Equipment
  > DURING POST-FLIGHT INSPECTION, FOUND PBE IN COAT CLOSET WITH EXPIRED SHELF LIFE DATE. AMM: 35-31-12-04. REMOVED AND REPLACED PBE REF AMM 35-31-12-04
- [SDR FDEA202211052846](https://openairdocs.org/sdr/FDEA202211052846.md): Floor Panel · delaminated · Nov 5, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AT THE TIME OF AGING AIRCRAFT INSPECTION,FOUND A FLOOR PANEL SHOWS SIGNS OF DELAMINATION BETWEEN FRAMES 54.1 AND 55 LHY805-1570 IN THE AFT CARGO COMPARTMENT. FABRICATED AND REPLACED THE FLOOR PANEL WITH RAW MATERIAL IAW FEDEX DRAWING NO:SRZ-25-005 REV.R.
- [SDR FDEA202211052845](https://openairdocs.org/sdr/FDEA202211052845.md): Floor Panel · damaged · Nov 5, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AT THE TIME OF AGING AIRCRAFT INSPECTION,FOUND A FLOOR PANEL HAS SEVERAL DAMAGES AT THE FRAME 67 AREA IN THE AFT CARGO COMPARTMENT. FABRICATED AND REPLACED THE FLOOR PANEL WITH RAW MATERIAL IAW FEDEX DRAWING NO:SRZ-25-005 REV.R AND SRZ-25-011 REV.D.
- [SDR FDEA202210282778](https://openairdocs.org/sdr/FDEA202210282778.md): Floor Panel · damaged · Oct 28, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE Z240 FLOOR PANEL #242EJ WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W. FEDEX DRAWING NO. SRZ-25-005.
- [SDR FDEA202210282777](https://openairdocs.org/sdr/FDEA202210282777.md): Floor Panel · damaged · Oct 28, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE Z240 FLOOR PANEL #241PH WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W. FEDEX DRAWING NO. SRZ-25-005.
- [SDR FDEA202210282776](https://openairdocs.org/sdr/FDEA202210282776.md): Floor Panel · damaged · Oct 28, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE Z240 FLOOR PANEL #241QH WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W. FEDEX DRAWING NO. SRZ-25-005.
- [SDR FDEA202210282775](https://openairdocs.org/sdr/FDEA202210282775.md): Floor Panel · damaged · Oct 28, 2022 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > THE Z240 FLOOR PANEL #242TG WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W. FEDEX DRAWING NO. SRZ-25-005.
- [SDR FDEA202210262736](https://openairdocs.org/sdr/FDEA202210262736.md): None · none · Oct 26, 2022 · N727FD · Airbus A300B4605R · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON O/B SIDE AT RIB 8A POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETE
- [SDR FDEA202210262735](https://openairdocs.org/sdr/FDEA202210262735.md): None · none · Oct 26, 2022 · N727FD · Airbus A300B4605R · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON I/B SIDE AT RIB 8A POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETE
- [SDR FDEA202210242753](https://openairdocs.org/sdr/FDEA202210242753.md): None · none · Oct 24, 2022 · N727FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR24L~26L,FR72~73. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600 SRM 5
- [SDR FDEA202210242734](https://openairdocs.org/sdr/FDEA202210242734.md): None · none · Oct 24, 2022 · N727FD · Airbus A300B4622R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR26R~29R,FR77~78. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERMINED
- [SDR FDEA202202120282](https://openairdocs.org/sdr/FDEA202202120282.md): Actuator · failed · Feb 12, 2022 · N727FD · Airbus A300B4622R · Leading Edge Slat Actuator
  > HYD GREEN RSVR LO LEVEL ECAM W/ ASSOCIATED GREEN HYD QUANTITY IN YELLOW ABOVE THE RED DOT THEN BELOW THE RED DOT. CROSS CHECKED ECAM HYD PAGE AND INDICATION CORRELATED W/GAUGE. FOLLOWED QRH PROCEDURE W/NEGRES. REMOVED R/H KRUEGER FLAP ACTUATOR PER A30
- [SDR FDEA202109272420](https://openairdocs.org/sdr/FDEA202109272420.md): Damper · failed · Sep 27, 2021 · N727FD · Airbus A300* · Landing Gear Retraction/Extension System
  > PDIS 727 32-30 6830 27SEP21 BFM OPEN U ON TAKEOFF GEAR WOULD NOT RETRACT WITH SYSTEM 1 OR SYSTEM 2. QHR COMPLETED. REMOVED AND REPLACED LT AND RT PITCH DAMPERS IAW AMM 32-11-15-04. ACCOMPLISHED 10 GEAR RETRACTION AND EXTENSION CHECKS NO DEF
- [SDR FDEA202104291069](https://openairdocs.org/sdr/FDEA202104291069.md): Smoke Warning · false activation · Apr 29, 2021 · N727FD · Airbus A300B4622R · Smoke Detection
  > ON TAXI OUT GOT AVIONICS SMOKE WARNING. SNIFFER DID NOT CONFIRM PRESENCE OF SMOKE. TROUBLE SHOT IN REF TO TSM 26-15 COULD NOT DUPLICATE, SYSTEM CHECKS OK.
- [SDR FDEA202104291068](https://openairdocs.org/sdr/FDEA202104291068.md): Clamp · loose · Apr 29, 2021 · N727FD · Airbus A300B4622R · Detection System
  > SNIFFER HOSE DETACHED FROM SNIFFER WHILE TROUBLESHOOTING AVIONICS SMOKE. HOSE RETRACTED INTO AVIONICS BAY. RETRACTED HOSE FROM CAVITY AND RECONNECTED CLAMP AND SECURED REF. A300-600 AMM 20-21-12. (IPC 26-15-01-01A)
- [SDR FDEA202007241643](https://openairdocs.org/sdr/FDEA202007241643.md): Floor Panel · worn · Jul 24, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > WHILE GIVING OK TO INSTALL FOUND PANEL 147EF FLUID SOAKED AND SOFT. FABRICATED NEW FLOOR PANEL 147EF FROM 5065-400001EB-G BATCH # 0003635145 PER SRZ 25-005 REV R. MAJOR REPAIR.
- [SDR FDEA202007171571](https://openairdocs.org/sdr/FDEA202007171571.md): Window Frame · chafed · Jul 17, 2020 · N727FD · Airbus A300B4622R · Fuselage Main, Structure
  > RIGHT FLIGHT DECK SLIDING WINDOW, INSPECTION OF PREVIOUS DAMAGE & REWORK IAW EA 6- 5300-167476 INDICATES ADDITIONAL DAMAGE EXISTS. REPAIR ACCOMPLISHED ON EA 6-5300-167476-A PART 3. CAT "B" REPAIR. MAJOR REPAIR.
- [SDR FDEA202007161553](https://openairdocs.org/sdr/FDEA202007161553.md): Mount · corroded · Jul 16, 2020 · N727FD · Airbus A300B4622R · Engine Mount Section
  > LEFT PYLON, NR 1 - 4 FWD ENG MOUNT BOLT HOLES WERE CORRODED AND PITTED. REPAIRED THE ENG MOUNT BOLT HOLES IAW EA 6-5454 -T0354758, P1, STEPS 1 - 8. ACCOMPLISHED FINAL EA 6-5450-T0354758 P1. MAJOR REPAIR.
- [SDR FDEA2020070631441](https://openairdocs.org/sdr/FDEA2020070631441.md): Floor Panel · cracked · Jul 3, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131JG HAS CRACK. FABRICATED FLOOR PANEL 131JG ON TD/000389 IAW SRZ 25-005 REV R, CLASSSIFED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA2020070211420](https://openairdocs.org/sdr/FDEA2020070211420.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132YF HAS CRACK. FABRICATED FLOOR PANEL 132YF ON TD/000369 IAW SRZ-25-005 REV R. CLASSIFIED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211422](https://openairdocs.org/sdr/FDEA2020070211422.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132ZF HAS CRACK. FABRICATED FLOOR PANEL 132ZF ON TD/000368 IAW SRZ-25-005 REV R. CLASSIFIED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211421](https://openairdocs.org/sdr/FDEA2020070211421.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO 131JG COVER PANEL HAS CRACK. FABRICATED FLOOR PANEL 131JG COVER PANEL ON TD/000390 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211418](https://openairdocs.org/sdr/FDEA2020070211418.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131YF HAS CRACK. FABRICATED FLOOR PANEL 131YF ON TD/000370 IAW SRZ-25-005 REV R. CLASSIFIED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211417](https://openairdocs.org/sdr/FDEA2020070211417.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 162DF HAS CRACK AND DELAMINATED. FABRICATED FLOOR PANEL 162DF ON TD/000359 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211415](https://openairdocs.org/sdr/FDEA2020070211415.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152LF HAS CRACK. FABRICATED FLOOR PANEL 152LF ON TD/000360 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020070211414](https://openairdocs.org/sdr/FDEA2020070211414.md): Floor Panel · cracked · Jul 1, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151HF HAS CRACK AND DELAMINATED EDGE. FABRICATED FLOOR PANEL 151HF ON TD/000353 IAW SRZ-25-005 REV R. CLASSFIED AS CAT "A" MAJOR REPAIR.
- [SDR FDEA2020062541341](https://openairdocs.org/sdr/FDEA2020062541341.md): Floor Panel · cracked · Jun 24, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131MG HAS CRACK. REMOVED AND REPLACED FLOOR PANEL 131MG IAW DWG A53272573. PART FABBED ON TD/000383. MAJOR REPIAR.
- [SDR FDEA2020062541340](https://openairdocs.org/sdr/FDEA2020062541340.md): Floor Panel · cracked · Jun 24, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131GG HAS CRACK. FABRICATED FLOOR PANEL 131GG ON TD/000384 IAW DWG A53272573. MAJOR REPAIR.
- [SDR FDEA2020062541339](https://openairdocs.org/sdr/FDEA2020062541339.md): Floor Panel · cracked · Jun 24, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131DG HAS CRACK. REMOVED AND REPLACED FLOOR PANEL 131DG IAW DWG A53272573. PART FABBED ON TD/000382. MAJOR REPAIR.
- [SDR FDEA202006231319](https://openairdocs.org/sdr/FDEA202006231319.md): Floor Panel · cracked · Jun 23, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 232BH HAS CRACK. FABRICATED FLOOR PANEL 232BH ON TD/000363 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.
- [SDR FDEA202006231318](https://openairdocs.org/sdr/FDEA202006231318.md): Floor Panel · cracked · Jun 23, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FLOOR PANEL 232HG MAIN CARGO DECK HAS CRACK. FABRICATED FLOOR PANEL 232HG ON TD/000361 IAW DWG SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.
- [SDR FDEA202006231317](https://openairdocs.org/sdr/FDEA202006231317.md): Floor Panel · cracked · Jun 23, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 231EF HAS CRACK. FABRICATED FLOOR PANEL ON TD/000362 IAW DWG SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.
- [SDR FDEA2020071721306](https://openairdocs.org/sdr/FDEA2020071721306.md): Floor Panel · cracked · Jun 22, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151ZF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRM53-10-20, & DWG A2547838. RESTORED FINISH IAW SRM 51-75-10. CLASSIFIED AS CAT AN -A- REPAIR. MAJOR REPAIR.
- [SDR FDEA2020071021306](https://openairdocs.org/sdr/FDEA2020071021306.md): Floor Panel · cracked · Jun 22, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151ZF HAS CRACK. FABRICATED A NEW FLOOR PANEL. RESTORED FINISH IAW SRM 51-75-10. FABRICATED THE NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A25472838. CLASSIFIED AS CAT A REPAIR. MAJOR REPAIR.
- [SDR FDEA2020062321307](https://openairdocs.org/sdr/FDEA2020062321307.md): Floor Panel · cracked · Jun 22, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241LH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV R. CLASSIFIED AS CAT "A" REPAIR. FLOOR PANEL 241LH INSTALLED ON 240-FL-FIT 000079. MAJOR REPAIR.
- [SDR FDEA2020062321306](https://openairdocs.org/sdr/FDEA2020062321306.md): Floor Panel · cracked · Jun 22, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151ZF HAS CRACK. FABRICATED FLOOR PANEL 131ZF ON TD/000371. RESTORED FINISH IAW SRM 51-75-10. FAB FLOOR PANEL IAW SRM 53-10-20 & DWG A25472838. CLASSIFIED AS CAT "A" REPAIR. MAJOR REPAIR
- [SDR FDEA2020062301297](https://openairdocs.org/sdr/FDEA2020062301297.md): Floor Panel · cracked · Jun 20, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131TF HAS CRACK. FABRICATED FLOOR PANEL IAW DWG A53272573. CLASSIFIED AS CAT "A" REPAIR. MAJOR REPAIR
- [SDR FDEA202006191288](https://openairdocs.org/sdr/FDEA202006191288.md): Floor Panel · gouged · Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222NF GOUGED. FABRICATED COURIER FLOOR PANEL 222NF ON VT MAE TRAVELER # TD/000305. CAT "A" MAJOR REPAIR IAW SRZ-25-005 REV "R"
- [SDR FDEA202006191287](https://openairdocs.org/sdr/FDEA202006191287.md): Floor Panel · gouged · Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222QF GOUGED. FABRICATED COURIER FLOOR PANEL 222QF ON VT MAE TRAVELER # TD/000306. CAT "A" MAJOR REPAIR IAW SRZ-25-005 REV "R"
- [SDR FDEA202006191293](https://openairdocs.org/sdr/FDEA202006191293.md): Floor Panel · cracked · Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131HG HAS CRACK. FABRICATED FLOOR PANEL 131HG ON TD/000322 IAW SRZ-25-005 REV R. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 131HG INSTALLED ON 130-FL-FIT CARD 000061.
- [SDR FDEA202006191292](https://openairdocs.org/sdr/FDEA202006191292.md): Floor Panel · cracked · Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 242MH HAS CRACK. FABRICATED FLOOR PANEL 242MH ON VT MAE TRAVELER TD/000322 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 242MH INSTALLED ON 240-FL-FIT CARD 000079

Next page: https://openairdocs.org/aircraft/N727FD/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 = 'N727FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N727FD/reports

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