# Service difficulty reports: N742FD

A list on [N742FD](https://openairdocs.org/aircraft/N742FD.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 · 203 reports

- [SDR FDEA202502180243](https://openairdocs.org/sdr/FDEA202502180243.md): Sliding Window · leaking · Feb 18, 2025 · N742FD · Airbus A300B4622R · Flight Compartment Windows
  > AFTER TAKEOFF HAD SEVERE LOUD WIND NOISE INCREASING WITH AIRSPEED COMING FROM CAPT S SIDE WINDOW. WINDOW APPEARED TO BE CLOSED AND LOCKED. RETURNED TO LRD TO INVESTIGATE. NO EMERGENCY DECLARED. WHEN AIRCRAFT ARRIVED AT GATE NOTED CAPT SLIDING WI
- [SDR FDEA202502140233](https://openairdocs.org/sdr/FDEA202502140233.md): Bottle · low pressure · Feb 14, 2025 · N742FD · Airbus A300B4622R · Emergency Equipment
  > LEFT DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L1 EMERGENCY OPERATION CYLINDER TO THE PRESSURE INDICATED ON THE PLACARD.
- [SDR FDEA202412101785](https://openairdocs.org/sdr/FDEA202412101785.md): Battery · failed · Dec 10, 2024 · N742FD · Airbus A300B4622R · Emergency Lighting
  > BOTH DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY ON PASSENGER COMPARTMENT EMERGENCY LIGHT PSU PER AMM 33-51-14-04. OPS CHECKED GOOD.
- [SDR FDEA202411271787](https://openairdocs.org/sdr/FDEA202411271787.md): Battery Pack · inoperative · Nov 27, 2024 · N742FD · Airbus A300B4622R · Emergency Lighting
  > BOTH DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY.
- [SDR FDEA202409201333](https://openairdocs.org/sdr/FDEA202409201333.md): Engine · power loss · Sep 20, 2024 · N742FD · Airbus A300B4622R · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH 14,000 FT #2 ENGINE STARTED TO ROLL BACK. WE LEVELED OFF THEN GOT #2 ENG OIL LO PRESS ECAM FOLLOWED BY #2 ENG FAIL ECAM. PERFORMED ECAM AND QRH DECLARED EMERGENCY AND DIVERTED BACK TO MEM. EMERGENCY DECLARED. PER P/PLANT ENGR DAVE, #2 E
- [SDR FDEA202406200825](https://openairdocs.org/sdr/FDEA202406200825.md): Hydraulic Line · leaking · Jun 20, 2024 · N742FD · Airbus A300B4622R · Hydraulic System, Main
  > LOST GREEN HYDRAULIC QUANTITY ON APPROACH. PERFORMED EMERGENCY GEAR EXTENSION. FOUND HYD FLEX LINE P/N AE705437-1 LEAKING BEHIND B NUT AT L/H MLG DUAL CONNECTING BLOCK MANIFOLD. REPLACED FLEX LINE WITH TEMP FLEX LINE.
- [SDR FDEA202405300752](https://openairdocs.org/sdr/FDEA202405300752.md): Line · leaking · May 30, 2024 · N742FD · Airbus A300B4622R · Fuel Controlling System
  > DURING CRUISE, NR 2 ENGINE BECAME UNRESPONSIVE. IT WOULD NOT GET ABOVE 57N1, EPR.996, EGT 338, N2 80.8 AT FULL THROTTLE. RAN QRH LACK OF THROTTLE RESPONSE IN FLT, DECLARED EMERGENCY. ON LANDING, RECEIVED ECAM FADEC MINOR FAULT. TROUBLESHOT REF TSM. FOUND
- [SDR FDEA202402170253](https://openairdocs.org/sdr/FDEA202402170253.md): Girt Bar · fod · Feb 17, 2024 · N742FD · Airbus A300B4622R · Emergency Equipment
  > R1 DOOR SLIDE WILL NOT INDICATE ARMED. CLEANED DEBRIS FROM R1 DOOR GIRT BAR FITTINGS. R1 DOOR SLIDE INDICATION OPS CKS GOOD PER ABOVE LISTED REF. MEL CLEARED
- [SDR FDEA202401280122](https://openairdocs.org/sdr/FDEA202401280122.md): Fan · failed · Jan 28, 2024 · N742FD · Airbus A300B4622R · Landing Gear Brake System
  > ON POSTFLIGHT FOUND #8 BRAKE FAN SHROUD, AND GUARD MISSING. SHROUD, AND GUARD ARE ABOUT 12 INCHES IN DIAMETER. REF IPC 32-48-16-01C ITEMS 30,100 AND 110. AND ITEM 130 HAS ONE MOUNT BOLT NUTPLATE/HELICOIL MISSING. R & R NR 4 BRAKE FAN INCLUDING ALL OF THE
- [SDR FDEA202401240106](https://openairdocs.org/sdr/FDEA202401240106.md): Brake · damaged · Jan 24, 2024 · N742FD · Airbus A300B4622R · Landing Gear Brake System
  > ON TAXI OUT OF KMEM, SET PARKING BRAKE AND NOTICED LEFT AND RIGHT BRAKE PRESSURE INDICATORS SHOWING 0 PSI. AIRCRAFT STARTED TO ROLL FORWARD. APPLIED TOE BRAKES AND BRAKE PRESSURE BEGAN TO RISE TO APPROXIMATELY 500 PSI ON BOTH SIDES OF BRAKE PRESSURE INDIC
- [SDR FDEA202303180466](https://openairdocs.org/sdr/FDEA202303180466.md): Sensor · failed · Mar 18, 2023 · N742FD · Airbus A300B4622R · Aircraft Fuel System
  > AT FL350, RT INNER TANK FAULT ECAM. COMPLIED WITH ECAM AND QRH. 120# FUEL IN CTR TANK, INNER AND TRIM SHOWED 0. RIGHT OUTER TANK STARTED TO DECREASE THROUGHOUT THE DESCENT GREATER THAN THE LEFT OUTER. DECLARED EMERGENCY AS IMBALANCE REACHED 800#. AT LAN
- [SDR FDEA202301040024](https://openairdocs.org/sdr/FDEA202301040024.md): Unknown · smoke · Jan 4, 2023 · N742FD · Airbus A300B4622R · Standard Practices/Structures
  > CREW REPORTS MEM TOWER CONTACTED FLT 0700 OTBD AT800' DURING CLIMBOUT OF POSSIBLE SMOKE COMING FROM THE FUSELAGE TAIL AREA. AMM 05-50-00-02 PERFORMED GVI OF ENTIRE AIRCRAFT WITH ATTENTION TO TAIL AREA. NO VISIBLE SIGNS OF LEAKS OR SOOT. NO ABNORMAL FLIGHT
- [SDR FDEA202209172350](https://openairdocs.org/sdr/FDEA202209172350.md): None · none · Sep 17, 2022 · N742FD · Airbus A300* · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT: EXISTING UPR FLANGE REPAIR FOUND ON FWD CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 35, BTW Y140~Y805. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF E
- [SDR FDEA202209132342](https://openairdocs.org/sdr/FDEA202209132342.md): None · none · Sep 13, 2022 · N742FD · Airbus A300* · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 58, BTW Y805~Y1470. COMPLIED WITH ATTACH MENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTI
- [SDR FDEA202209132341](https://openairdocs.org/sdr/FDEA202209132341.md): None · none · Sep 13, 2022 · N742FD · Airbus A300* · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPARTMENT FLOOR CROSSBEAM AT FR 59, BTW Y805~Y1470. COMPLIED WITH ATTACH MENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTI
- [SDR FDEA202209122559](https://openairdocs.org/sdr/FDEA202209122559.md): None · cracked · Sep 12, 2022 · N742FD · Airbus A300* · Wing Main, Frame Structure
  > 1EA CRACK INDICATION WAS FOUND AT R/H SIDE HOLE W OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REAMED THE HOLE AND INSTALLED NEW FASTENER I.A.W EA NO:6-5710-T0370695 P1, SEQ NO:990, TITLE:WING- BASIC WING STRUCTURE- RH ATTACHMENT HOLES OF INTER
- [SDR FDEA202209102379](https://openairdocs.org/sdr/FDEA202209102379.md): Adapter · gouged · Sep 10, 2022 · N742FD · Airbus A300B4622R · Fuselage Main, Structure
  > AFT MAIN DECK CARGO COMPT FOUND CROSSBEAM FITTED WITH CLS ADAPTER GOT 2EA GOUGED MARKS AT FR63/BETWEEN -Y1456 AND -Y1959 DAMAGED CROSSBEAM REPALCED NEW PART, INSTALLED WITH FASTENERS I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7,PAGE
- [SDR FDEA202209092553](https://openairdocs.org/sdr/FDEA202209092553.md): Seat Track · corroded · Sep 9, 2022 · N742FD · Airbus A300* · Fuselage Main, Structure
  > MDCC SEAT TRACK SURFACE CORRODED AT FR18 8"~FR18 14", -Y450. REMOVED EXISTING REPAIR (REF TO PREVIOUS REPAIR ASSESSMENT DATA N00562 FOR AGING AIRCRAFT ASSESSMENT INFORMATION), INSTALLED NEW FABRICATED SEAT TRACK WITH SPLICES, THIS IS CAT.B REPAIR I.A.W A30
- [SDR FDEA202209092528](https://openairdocs.org/sdr/FDEA202209092528.md): Seat Track · none · Sep 9, 2022 · N742FD · Airbus A300* · Fuselage Main, Structure
  > MDCC SEAT TRACK SURFACE CORRODED AT FR18 10"~FR18 15",-Y953 REPLACED THE SEAT TRACK WITH FABRICATED PART I.A.W A300-600 SRM 53-12-16-001, PAGE.9/10, FIG.1(SHEET-4) & GMM 07-0-1001 & 51-40-21-001, PARA.6&7, PAGE.7B-50.
- [SDR FDEA202209082451](https://openairdocs.org/sdr/FDEA202209082451.md): Floor Support · corroded · Sep 8, 2022 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > N00455 AFT CGO COMP'T LH FLOOR BEAM CORROSION BTW FR60-FR61 POSITION. CUT OUT AND REPAIR WITH SPLICE, THIS IS CATE.A REPAIR I.A.W A300-600 SRM 53-10-15-201, PARA.9, PAGE237-240, FIG.207.
- [SDR FDEA202209032525](https://openairdocs.org/sdr/FDEA202209032525.md): Elevator · delaminated · Sep 3, 2022 · N742FD · Airbus A300* · Elevator Structure
  > 1EA WATER TRAPPED AREA WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL NO.14 SCREW AREA.(7"X4") REPAIRED THE DAMAGE AREA WITH CORE AND PLIES. THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-21-12-201-2 PARA.5J, PAGE266-271, FIG.212(SHEET-3) & SRI:55-21-12-201, II
- [SDR FDEA202209012552](https://openairdocs.org/sdr/FDEA202209012552.md): Seat Track · corroded · Sep 1, 2022 · N742FD · Airbus A300* · Fuselage Floor Panel
  > MDCC SEAT TRACK SURFACE CORRODED AT FR18 11"~FR18 13", Y450. CUT OUT THE DAMAGE AREA AND INSTALLED NEW FABRICATE SEAT TRACK WITH SPLICES, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 53-12-16-201, PARA.5.A., PAGE.201-207, FIG.201(SHEET.1-2) & SRI:53-12-16-201,
- [SDR FDEA202009052125](https://openairdocs.org/sdr/FDEA202009052125.md): Actuator · loose · Sep 5, 2020 · N742FD · Airbus A300B4622R · Landing Gear Door Retract Section
  > PDIS 742 32-30 3672 05SEP20 MKE OPEN U. SELECTED GEAR UP. RECEIVED ECAM "L/G DOOR NOT CLOSED" "MX SPD 270KT" "GEAR DO NOT CYCLE" FOLLOWED QRH PROCEDURE AND RETURNED TO KMKE. WHEN GEAR HANDLE WAS SELECTED BACK TO NEUTRAL FOR RETURN WE HAD EXCESSIVE NOISE &
- [SDR FDEA2020090852125](https://openairdocs.org/sdr/FDEA2020090852125.md): Warning Message · false activation · Sep 5, 2020 · N742FD · Airbus A300B4622R · Landing Gear Door Retract Section
  > SELECTED GEAR UP, RCVD ECAM L/G DOOR NOT CLOSED, MX SPD 270KT, GEAR DO NOT CYCLE, FOLLOWED QRH PROCEDURE AND RETURNED TO KMKE. WHEN GR HANDLE WAS SELECTED BACK TO NEUTRAL FOR RETURN WE HAD EXCESSIVE NOISE & VIBRATION COMING FROM NLG AREA. EMERGENCY WAS DECLA
- [SDR FDEA202007231625](https://openairdocs.org/sdr/FDEA202007231625.md): Skin · gouged · Jul 23, 2020 · N742FD · Airbus A300B4622R · Trailing Edge Flaps
  > LEFT WING INBD FLAP UPPER SURFACE, OTBD SIDE HAD A DEEP GOUGE. COMPLIED WITH EA:6-5752-123008 B P3. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA2020072391579](https://openairdocs.org/sdr/FDEA2020072391579.md): Fitting · cracked · Jul 19, 2020 · N742FD · Airbus A300B4622R · Wing Spar
  > NDT INSP - LH CENTER WING BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "C" FOUND C CRACK SIGNAL. LH CENTER WING BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "C" FOUND C CRACK SIGNAL. COMPLY WITH EA: 6-5710-T0355124 P1. TITE: WINGS - BASIC WING STRUCTURE - CRACK
- [SDR FDEA2020072391578](https://openairdocs.org/sdr/FDEA2020072391578.md): Fitting · cracked · Jul 19, 2020 · N742FD · Airbus A300B4622R · Wing Spar
  > NDT INSP - RH CENTER WING BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "F" FOUND C CRACK SIGNAL. RH CENTER WING BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "F" FOUND C CRACK SIGNAL. COMPLY WITH EA: 6-5710-T0355124 P1. TITE: WINGS - BASIC WING STRUCTURE - CRACK
- [SDR FDEA2020040870705](https://openairdocs.org/sdr/FDEA2020040870705.md): Line · leaking · Apr 7, 2020 · N742FD · Airbus A300B4622R · Landing Gear Brake System
  > PDIS 742 32-43 3053 07APR20 EWR OPEN U LOGPAGES:3269955 AFTER LANDING AT KEWR 04R AND EXTENDED TAXI RECEIVED HOT BRAKE WARNING. SELECTED BRAKE FAN ON AND NOTICED #8 BRAKE HEATING THRU 300 DEGREES. AS WE TURNED INTO SPOT THE TEMP CONTINUED T
- [SDR FDEA2019062421400](https://openairdocs.org/sdr/FDEA2019062421400.md): Floor Panel · delaminated · Jun 22, 2019 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152FF DELAMINATED FABRICATED FLOOR PANEL ON VT MAE TRAVELER T19/1424969 IAW A300 SRZ-25-005 AND SRM 53-10-33-04B CLASSIFIED AS A CAT "A" MAJOR REPAIR
- [SDR FDEA201812113490](https://openairdocs.org/sdr/FDEA201812113490.md): Autothrottle Sys · malfunctioned · Dec 11, 2018 · N742FD · Airbus A300B4622R · Auto Throttle System
  > ON TAKEOFF ROLL, WHEN TOGA WAS SELECTED, ENGINE NR 1 FAILED TO ACCELERATE PAST 1.2 EPR. CREW DISCONTINUED TAKE OFF AT 50 KNOTS. MOC DETERMINED IT WAS AN AUTOTHROTTLES PROBLEM. CREW CONTINUED FLIGHT ON MEL 22-30-01-C AUTOTHROTTLE SYSTEM INOP. ALL ENGINE IND
- [SDR FDEA201803170725](https://openairdocs.org/sdr/FDEA201803170725.md): Web · cracked · Mar 17, 2018 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > CRACKS ON FLOOR STRUCTURE WEB AND ANGLE IN FWD CARGO COMPT FR 38.0, Y 1470, UNDER FLOOR LEVEL. REMOVED CRACKED FLOOR WEB AT FR 38, Y1470 IAW SRM 51-40-21. FABRICATED NEW WEB ON T18/1327198. INSTALLED NEW WEB IAW SRM 51-40-21 AT FR 38 Y1470. MAJOR REPAIR.
- [SDR FDEA201803160721](https://openairdocs.org/sdr/FDEA201803160721.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152GF HAS DAMAGED. REPLACED PANEL 152GF IAW SRZ 25-005 REV M ON T18/1326798. MAJOR REPAIR.
- [SDR FDEA201803160720](https://openairdocs.org/sdr/FDEA201803160720.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO PANEL 151CF HAS DAMAGED. REPLACED PANEL 151CF IAW SRZ 25-005 REV M ON T18/1326797. MAJOR REPAIR.
- [SDR FDEA201803160719](https://openairdocs.org/sdr/FDEA201803160719.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 162DF HAS DELAMINATED. REPLACED PANEL 162DF IAW SRZ 25-005 REV M ON T18/1326793. MAJOR REPAIR.
- [SDR FDEA201803160718](https://openairdocs.org/sdr/FDEA201803160718.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132JG HAS DAMAGED. REPLACED PANEL 132JG IAW SRZ 25-005 REV M ON T18/1327145. MAJOR REPAIR.
- [SDR FDEA201803160717](https://openairdocs.org/sdr/FDEA201803160717.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131RF HAS DAMAGED. REPLACED PANEL 131RF IAW SRZ 25-005 REV M ON T18/1327194. MAJOR REPAIR.
- [SDR FDEA201803160716](https://openairdocs.org/sdr/FDEA201803160716.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131YF HAS DAMAGED. REPLACED PANEL 131YF IAW SRZ 25-005 ON T18/1327143. MAJOR REPAIR.
- [SDR FDEA201803160715](https://openairdocs.org/sdr/FDEA201803160715.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152JF HAS DAMAGED. REPLACED PANEL 152JF IAW SRZ 25-005 REV M ON T18/1326800. MAJOR REPAIR.
- [SDR FDEA201803160714](https://openairdocs.org/sdr/FDEA201803160714.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO PANEL 152CF HAS DAMAGED. REPLACED PANEL 152CF IAW SRZ 25-005 REV M ON T18/1326842. MAJOR REPAIR.
- [SDR FDEA201803160713](https://openairdocs.org/sdr/FDEA201803160713.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 162CF HAS DELAMINATED. REPLACED PANEL 162CF IAW SRZ 25-005 REV M ON T18/1326796. MAJOR REPAIR.
- [SDR FDEA201803160712](https://openairdocs.org/sdr/FDEA201803160712.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > BULK CARGO FLOOR PANEL 162EF HAS DELAMINATED. REPLACED PANEL 162EF IAW SRZ 25-005 REV M ON T18/1328794. MAJOR REPAIR.
- [SDR FDEA201803160711](https://openairdocs.org/sdr/FDEA201803160711.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151EF HAS DAMAGED. REPLACED PANEL151EF IAW SRZ 25-005 ON T18/1327141. MAJOR REPAIR.
- [SDR FDEA201803160710](https://openairdocs.org/sdr/FDEA201803160710.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 152BF HAS DAMAGED. REPLACED PANEL 152BF IAW SRZ 25-005 REV M ON T18/1327142. MAJOR REPAIR.
- [SDR FDEA201803160709](https://openairdocs.org/sdr/FDEA201803160709.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132HG HAS DAMAGED. REPLACED PANEL 132HG IAW SRZ 25-005 REV M ON T18/1327144. MAJOR REPAIR.
- [SDR FDEA201803160708](https://openairdocs.org/sdr/FDEA201803160708.md): Floor Panel · damaged · Mar 16, 2018 · N742FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132QF HAS DAMAGED. REPLACED PANEL 132QF IAW SRZ 25-005 REV M ON T18/1327191. MAJOR REPAIR.
- [SDR FDEA201803100643](https://openairdocs.org/sdr/FDEA201803100643.md): Seat Track · gouged · Mar 10, 2018 · N742FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK SEAT TRACK CROWN FR 54.3 Y450 HAS GOUGE IN LUG. BLENDED & CHECKED LIMITS, OUT OF TOLERANCE IAW SRM 53-10-16. REMOVED SEAT TRACK IAW SRM 51-42-21. FABRICATED REPAIR SECTION AND TWO DOUBLERS IAW SRM 51-27-11. INSTALLED REPAIR SECTION IAW SRM 5
- [SDR FDEA201803100642](https://openairdocs.org/sdr/FDEA201803100642.md): Seat Track · gouged · Mar 10, 2018 · N742FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED ON THE MAIN CABIN SEAT TRACK BETWEEN FRAMES 48- 49, -Y450, BLENDED THE GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED & REPLACED THE SEAT TRACK IAW SRM 51-40-21 & DWG NR A53832211. MAJOR REPAIR.
- [SDR FDEA201803100641](https://openairdocs.org/sdr/FDEA201803100641.md): Floor Support · corroded · Mar 10, 2018 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK LAV FLOOR SUPPORT HAS CORROSION FROM FR-11 TO 14, Y953. CLEANED AREA IAW AMM 12-21-12. UPON INVESTIGATION FOUND SUPP EXFOLIATED OUT OF LIMITS. REMOVED FLOOR SUPP Y953 FR 11 TO 15A IAW SRM 51-40-21. FABBED FLOOR SUPP NEW ON T18/132802, IAW SRM 53-12-1
- [SDR FDEA201803100640](https://openairdocs.org/sdr/FDEA201803100640.md): Floor Support · corroded · Mar 10, 2018 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK LAV FLOOR O/B SUPPORT HAS CORROSION FROM FR- 11 TO 14, LBL- 62". CLEANED AREA IAW AMM 12-21-12. UPON INVESTIGATION FOUND FLOOR SUPPORT EXFOLIATED OUT LIMIT. REMOVED FLOOR SUPPORT BETWEEN FR 11 TO FR 18 LBL Y1416 IAW SRM 51-40-21. REPAIRED FLOOR SUPP
- [SDR FDEA201803100638](https://openairdocs.org/sdr/FDEA201803100638.md): Web · cracked · Mar 10, 2018 · N742FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR STRUCTURE WEB IN FWD CARGO COMPT AT FR 37, -Y1470, UNDER FLOOR LEVEL. REMOVED WEB IN FWD CARGO COMPT AT FR-37 -Y1470 IAW SRM 51-40-21, FABRICATED WEB ON T18/1327252, INSTALLED WEB IAW SRM 51-40-21. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N742FD/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 = 'N742FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N742FD/reports

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