# Service difficulty reports: Airbus A300 B4-622

A list on [Airbus A300 B4-622](https://openairdocs.org/model/airbus-a300-b4-622.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 528 reports

- [SDR FDEA202408161136](https://openairdocs.org/sdr/FDEA202408161136.md): Rib · cracked · Aug 16, 2024 · N730FD · Airbus A300B4622 · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WING - FLIGHT SURFACES
- [SDR FDEA201811140159](https://openairdocs.org/sdr/FDEA201811140159.md): Not Reported · malfunctioned · Nov 14, 2018 · N719FD · Airbus A300B4622 · Landing Gear System
  > DURING OPS TEST FOR GEAR HANDLE R/R, NLG RETRACTED AND AIRCRAFT CAME TO REST ON FUSELAGE. ALL REPAIRS ACCOMPLISHED UNDER WORK ORDER 73414 AND EA 6-0550-T0343547 PART1-14, INADVERTENT NLG RETRACTION- INSPECTION AND REPAIR REQUIREMENTS.
- [SDR FDEA201810162902](https://openairdocs.org/sdr/FDEA201810162902.md): Rib · cracked · Oct 16, 2018 · N717FD · Airbus A300B4622 · Trailing Edge Flaps
  > X-RAY INSPECTED, LT WING CENTER FLAP RIB 27 POSN FOUND CRACKED. PER SRM 57-50-00-201 PARA 4A FIG 201 REPAIRED THE CRACKED RIB. AND PER SRM 57-50-00-201 PARA 4E FIG 205 MAKE THE SKIN REPAIR DOUBLER & WET INSTALL THE REPAIR DOUBLER. THIS REPAIR IS CAT A MAJOR RE
- [SDR FDEA201810152884](https://openairdocs.org/sdr/FDEA201810152884.md): Stringer · cracked · Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/Stringer
  > NDT INSPECTED, RT WING LOWER SKIN RIB18, STRINGER 11 WEB POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201810152883](https://openairdocs.org/sdr/FDEA201810152883.md): Stringer · cracked · Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/Stringer
  > NDT INSPECTED, RT WING UPPER SKIN RIB18, STRINGER 11 POSN FOUND CRACKED. COMPLIED WITH EA 6-5720-T0342825. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201810152882](https://openairdocs.org/sdr/FDEA201810152882.md): Stringer · cracked · Oct 15, 2018 · N717FD · Airbus A300B4622 · Wing, Longeron/Stringer
  > LT WING FUEL TANK RIB18 STRINGER WEB NDT INSPECT FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5720-T0343001. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA2018102612756](https://openairdocs.org/sdr/FDEA2018102612756.md): Doubler · chafed · Oct 1, 2018 · N717FD · Airbus A300B4622 · Trailing Edge Flaps
  > EXISTING REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR ON RT INBD FLAP UPPER SKIN BTW NOSE RIB27 AND RIB3 WAS EVALUATED AND FOUND CHAFING DAMAGE ON REPAIR DOUBLER PER EA: 6-5750-124214. REWORK THE REP
- [SDR FDEA201809252674](https://openairdocs.org/sdr/FDEA201809252674.md): Fitting · cracked · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > FUSELAGE CENTER WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE "M" FOUND CRACK SIGNAL. PER EA 6-5710-167809 B PT2 REPAIR THE CRACKED "M" HOLE. THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201809252678](https://openairdocs.org/sdr/FDEA201809252678.md): Web · cracked · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201809252677](https://openairdocs.org/sdr/FDEA201809252677.md): Web · cracked · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y0 AND Y-450 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201809252676](https://openairdocs.org/sdr/FDEA201809252676.md): Web · cracked · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > TOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. TOP OF THE CENTER FUEL TANK - UNDER MDCC FLOOR FR47, B/W Y1456 AND Y953 FOUND 1EA WEB CRACKED. REPAIR THE CRACKED WEB PER SRM 53-15-15-201 PARA.5.A FIG201. THIS IS B
- [SDR FDEA201809252675](https://openairdocs.org/sdr/FDEA201809252675.md): Web · cracked · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > TOP OF THE CENTER FUEL TANK UNDER MDCC FLOOR FR47, B/W Y-1456 AND Y-953 FOUND 1EA WEB CRACKED. REPLACED THE CRACKED WEB PER SRM 51-40-21. THIS IS A CATEGORY REPAIR. MINOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201809252673](https://openairdocs.org/sdr/FDEA201809252673.md): Crossbeam · unknown · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Main, Structure
  > EXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR35 Y-140 - Y-1470 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAI
- [SDR FDEA201809252671](https://openairdocs.org/sdr/FDEA201809252671.md): Crossbeam · unknown · Sep 25, 2018 · N717FD · Airbus A300B4622 · Fuselage Main, Structure
  > EXISTING REPAIR ON FWD CARGO FLOOR CROSSBEAM AT FR27 Y-140 - Y-805 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53- 10-15 FIG207,EO:6-5100-7-5000 D07 PT1 WAS COMPLETED,TITLE:STRUCTURES-REPAIR
- [SDR FDEA201808182126](https://openairdocs.org/sdr/FDEA201808182126.md): Outflow Valve · malfunctioned · Aug 18, 2018 · N719FD · Airbus A300B4622 · Cabin Pressure Control System
  > HAD TO BE AT 21000 FEET TO HOLD CABIN PRESSURE OF 10000 FEET WITH OVERBOARD VALVE OPEN. ON INBOUND, FOUND OVERBOARD EXHAUST VALVE FULLY OPENED, NOT PARTIALLY OPENED IAW MEL 21-23-06 FIG 21-23-06 B, CAUSING ELBOW DUCT ABOVE OVERBOARD EXHAUST VALVE TO COLLAPSE
- [SDR FDEA201807101661](https://openairdocs.org/sdr/FDEA201807101661.md): Limiter · malfunctioned · Jul 10, 2018 · N717FD · Airbus A300B4622 · Leading Edge Slat Control System
  > SLATS STUCK LESS THAN 15 DEGREES ON RETRACTION. SLATS SYS 1 AND 2 FAULT LIGHTS ILLUMINATED. FOLLOWED ECAM AND QRH. SFP1 SLAT POSITION REMAINED STUCK. ARRIVED AT THE GATE THE FLAPS AND SLATS WERE FULLY RETRACTED, CREW DEBRIEF STATED THAT THE SLATS RESET AFTER
- [SDR FDEA201806301609](https://openairdocs.org/sdr/FDEA201806301609.md): Computer · failed · Jun 30, 2018 · N717FD · Airbus A300B4622 · Leading Edge Slat Control System
  > SLATS SYS 1/2 FAULTS AND SLATS STUCK BETWEEN 0 AND 15 DURING RETRACTION AFTER TAKEOFF. CYCLED SLAT/FLAP HANDLE PER QRH. SLATS WENT BACK TO 15 BUT STUCK AGAIN DURING RETRACTION. RETURNED TO AIRPORT AND SLATS AND FLAPS EXTENDED NORMALLY FOR APPROACH. SLATS RETRA
- [SDR FDEA201806191541](https://openairdocs.org/sdr/FDEA201806191541.md): Pitot Tube · failed · Jun 19, 2018 · N717FD · Airbus A300B4622 · Pitot/Static System
  > DURING T/O ROLL, FO'S PFD DID NOT DISPLAY ANY AIRSPEED. REJECTED T/O AT 65 KIAS. REMOVED AND REPLACED F/O'S PITOT TUBE REF 34-11-15-04, OPS CHECK GOOD. INSPECTED OLD PITOT TUBE ASSY AND FOUND INSECT IN TUBE. A/C OK FOR CONTINUED SERVICE.
- [SDR FDEA201806191540](https://openairdocs.org/sdr/FDEA201806191540.md): Adc · failed · Jun 19, 2018 · N717FD · Airbus A300B4622 · Air Data Computer
  > DURING T/O ROLL, NO AIRSPEED WAS INDICATED ON THE F/O'S PFD. REJECTED T/O AT 70 KTS. PERFORMED LEAK TEST, HELD 350 KTS FOR OVER 20 MINUTES. REMOVED AND REPLACED NR 2 ADC, OPS CHECK GOOD. A/C OK FOR CONTINUED SERVICE.
- [SDR FDEA201806161508](https://openairdocs.org/sdr/FDEA201806161508.md): Battery · failed · Jun 16, 2018 · N741FD · Airbus A300B4622 · Door Warning System
  > RT SIDE SLIDE DID NOT ARM ON FIRST TRY. OPENED DOOR AND CLOSED IT AND THEN IT ARMED. R1 DOOR ESCAPE SLIDE ARMED NORMALLY ON ARRIVAL, BITE TEST OF ASPSU FAILS NR 1 BATTERY. R&R NR 1 BATTERY PER AMM 52-73-18-04-0. DOOR SLIDE OPS CHECK GOOD PER AMM 52-73-00-05-
- [SDR FDEA201803150699](https://openairdocs.org/sdr/FDEA201803150699.md): Flap System · malfunctioned · Mar 15, 2018 · N717FD · Airbus A300B4622 · Trailing Edge Flap Control System
  > ON APPROACH, SLATS EXTENDED AND INDICATED NORMALLY. AT FLAPS 15 AND FLAPS 20 COULD FEEL A PITCH CHANGE, BUT STILL NO INDICATOR MOVEMENT. CYCLED THE FLAP HANDLE AND COULD FEEL PITCH CHANGE BUT STILL NO INDICATION. PERFORMED A GO AROUND AND INDICATOR BEGAN TO
- [SDR FDEA201802210458](https://openairdocs.org/sdr/FDEA201802210458.md): Actuator · failed · Feb 21, 2018 · N719FD · Airbus A300B4622 · Landing Gear Actuator
  > DURING LANDING GEAR EXTENSION, SYS 1 SELECTED, ALL AMBER DOOR LIGHTS ILLUMINATED, MAIN GEAR GREENS ON, NOSE GEAR RED UNLOCK REMAIN, LIGHT ON BOTH SYS 1 & 2. IAW QRH MANUAL GEAR EXTENSION, VISUAL CHECKED IN E & E CONFIRMED NOSE GEAR DOWN, STILL UNSAFE IND
- [SDR FDEA201802100334](https://openairdocs.org/sdr/FDEA201802100334.md): Proximity Sensor · failed · Feb 10, 2018 · N719FD · Airbus A300B4622 · Landing Gear Position and Warning
  > DURING GEAR EXTENSION, THE NOSE GEAR WAS RED, UNLOCKED ON BOTH NR 1 & 2 SYSTEMS, NO AMBER GEAR DOOR LIGHTS, WITH THE RED NOSE GEAR LIGHT ON. GOOD GREEN HYDRAULICS, CYCLED THE GEAR AND STILL RED UNLOCKED ON NOSE. ABOUT SIX MINUTES AFTER EXTENSION NOSE G
- [SDR FDEA201712223429](https://openairdocs.org/sdr/FDEA201712223429.md): Smoke Detector · false activation · Dec 22, 2017 · N719FD · Airbus A300B4622 · Smoke Detection
  > AVIONICS SMOKE LIGHT ILLUMINATED. ECAM SHOWED AVIONICS SMOKE PROCEDURE. NO SMOKE OBSERVED. RETURNED TO DEPARTURE. AVIONICS SMOKE LIGHT HAD EXTINGUISHED ON TAXI IN, PREFORMED ADJ/TEST AVIONICS COMPARTMENT SMOKE DETECTION SYSTEM IAW MM 26-15-00-05. NO DISCR
- [SDR FDEA201710112900](https://openairdocs.org/sdr/FDEA201710112900.md): Floorbeam · corroded · Oct 11, 2017 · N719FD · Airbus A300B4622 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOORBEAM FRAME 58, -Y1470 FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-15, FIG 208. MAJOR REPAIR.
- [SDR FDEA201709282781](https://openairdocs.org/sdr/FDEA201709282781.md): Rudder · delaminated · Sep 28, 2017 · N717FD · Airbus A300B4622 · Elevator Structure
  > RUDDER THERMOGRAPH FAILS STEP 10 EA 6-5540-A0319362 A PT2 PREVIOUS REPAIR. REPAIRED RIGHT HAND PREVOUS REPAIR AREA BETWEEN NR 3 AND NR 4 SCREW ON TRAILING EDGE FROM BOTTOM IAW SRM 55-41-12-201 PARA 31 FIG 222, EA 6-5540-T0335547, AND TD/7037 1608/807/2017A. M
- [SDR FDEA201709282779](https://openairdocs.org/sdr/FDEA201709282779.md): Skin · dented · Sep 28, 2017 · N717FD · Airbus A300B4622 · Rudder, Plate/Skin
  > RUDDER OUTER LEFT SKIN APPROX 4.5FT FROM BOTTOM OF RUDDER AND APPROX 3 FT FROM THE LEADING EDGE SPAR THERE IS A DENT " BY 0.025". REPAIRED SKIN IAW SRM 55-41-12 PARA 30 FIG 219-220, AND COMPLIED WITH EA 6-5540-T0335649 CLASSIFIED AS A CAT "B" MAJOR REPAIR.
- [SDR FDEA201709272755](https://openairdocs.org/sdr/FDEA201709272755.md): Web · cracked · Sep 27, 2017 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > FWD PIT FR38-38.1 LT O/B WEB UNDER ROLLER TRAY CRACKED. REMOVED AND REPLACED NEW SHEAR PLATE (WEB) IAW SRM 51-40-21, CLASSIFIED AS MAJOR REPAIR.
- [SDR FDEA201709272754](https://openairdocs.org/sdr/FDEA201709272754.md): Floor Panel · cracked · Sep 27, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO COMPT FLOOR PANEL 152DF BROKEN/DELAM. FABRICATED NEW FLOOR PANEL 152DF ON T17/1299063 PER SRZ 25-005, CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA201709272753](https://openairdocs.org/sdr/FDEA201709272753.md): Floor Panel · corroded · Sep 27, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > DURING OK TO CLOSE FOUND FLOOR PANEL 162HF CORRODED. FABRICATED NEW FLOOR PANEL 162HF ON T17/1298516 PER SRZ 25-005. CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA201709272752](https://openairdocs.org/sdr/FDEA201709272752.md): Floor Panel · damaged · Sep 27, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO-COMPT FLOOR PANEL 152HF BROKEN/DELAM. FABRICATED NEW FLOOR PANEL 152HF ON T17/1299865 PER SRZ 25-005, CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA201709232698](https://openairdocs.org/sdr/FDEA201709232698.md): Floor Support · corroded · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR SUPPORT FRAME 55, Y0, UNDER LOADING TRAY CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-10-15.
- [SDR FDEA201709232697](https://openairdocs.org/sdr/FDEA201709232697.md): Floor Support · corroded · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR SUPPORT FRAME 57.1, Y 0, UNDER LOADING TRAY CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-10-15. CLASSIFED AS A MAJOR REPAIR.
- [SDR FDEA201709232696](https://openairdocs.org/sdr/FDEA201709232696.md): Floor Panel · damaged · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131HG DELAMINATED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232695](https://openairdocs.org/sdr/FDEA201709232695.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 161CF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232694](https://openairdocs.org/sdr/FDEA201709232694.md): Floor Panel · damaged · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 161HF CORNER DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232693](https://openairdocs.org/sdr/FDEA201709232693.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 161GF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232692](https://openairdocs.org/sdr/FDEA201709232692.md): Floor Panel · delaminated · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152BD DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232691](https://openairdocs.org/sdr/FDEA201709232691.md): Floor Panel · cracked · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152GF CORNER CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232690](https://openairdocs.org/sdr/FDEA201709232690.md): Floor Panel · delaminated · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151FF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232689](https://openairdocs.org/sdr/FDEA201709232689.md): Floor Panel · delaminated · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152FF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232688](https://openairdocs.org/sdr/FDEA201709232688.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151JF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232687](https://openairdocs.org/sdr/FDEA201709232687.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152AF PUNCTURED ON UPPER SKIN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232686](https://openairdocs.org/sdr/FDEA201709232686.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151CF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232685](https://openairdocs.org/sdr/FDEA201709232685.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151LF PUNCTURED ON UPPER SKIN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232684](https://openairdocs.org/sdr/FDEA201709232684.md): Floor Panel · cracked · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151BF CRACKED ON EDGE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232683](https://openairdocs.org/sdr/FDEA201709232683.md): Floor Panel · broken · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152LF HAD A BROKEN CORNER. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201709232682](https://openairdocs.org/sdr/FDEA201709232682.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152JF PUNCTURED. FABRICATED A NEW FOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.
- [SDR FDEA201709232681](https://openairdocs.org/sdr/FDEA201709232681.md): Floor Panel · punctured · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152RF FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, MAJOR REPAIR.
- [SDR FDEA201709232679](https://openairdocs.org/sdr/FDEA201709232679.md): Floor Panel · damaged · Sep 23, 2017 · N719FD · Airbus A300B4622 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152KF FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Next page: https://openairdocs.org/model/airbus-a300-b4-622/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 aircraft_model_key = 'A300B4622'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a300-b4-622/reports

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