# Service difficulty reports: N716FD, cancelled Jun 27, 2024

A list on [N716FD, cancelled Jun 27, 2024](https://openairdocs.org/deregistered/N716FD-2024-06-27.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 3 · 110 reports

- [SDR FDEA201403120490](https://openairdocs.org/sdr/FDEA201403120490.md): Smoke Detector · false indication · Mar 12, 2014 · N716FD · Airbus A300B4622 · Fire Detection
  > RECEIVED AVIONICS SMOKE WARNING AT CRUISE ALTITUDE. AFTER INITIAL STEADY WARNING THE WARNING BECAME INTERMITTENT. NO SIGN OF SMOKE THROUGH THE SNIFFER.
- [SDR FDEA201402270411](https://openairdocs.org/sdr/FDEA201402270411.md): Panel · cracked · Feb 27, 2014 · N716FD · Airbus A300B4622 · Wing, Center Box
  > RIGHT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE INTERNAL FITTING ONLY STEP BY STEP 0.4 MM PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402270410](https://openairdocs.org/sdr/FDEA201402270410.md): Panel · cracked · Feb 27, 2014 · N716FD · Airbus A300B4622 · Wing, Center Box
  > LEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE CRACKED LAYERS FROM INTERNAL TO EXTERNAL PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402270409](https://openairdocs.org/sdr/FDEA201402270409.md): Panel · cracked · Feb 27, 2014 · N716FD · Airbus A300B4622 · Wing, Center Box
  > LEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE PICK-UP ANGLE AND LOWER KEEL BEAM ONLY STEP BY STEP 0.4MM PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 P1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402270408](https://openairdocs.org/sdr/FDEA201402270408.md): Structure · cracked · Feb 27, 2014 · N716FD · Airbus A300B4622 · Wing, Center Box
  > CENTER WING BOX REAR SPAR & BOTTOM PANEL CRACKED. REPAIRED IAW EA6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402270407](https://openairdocs.org/sdr/FDEA201402270407.md): Frame · cracked · Feb 27, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Frame
  > LEFT WING CTR WING BOX REAR SPAR & BOTTOM PANEL CRACKED. REPAIRED IAW EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100
- [SDR FDEA201402240393](https://openairdocs.org/sdr/FDEA201402240393.md): Skin · worn · Feb 24, 2014 · N716FD · Airbus A300B4622 · Wing, Plate/Skin
  > RIGHT WING, RIBS 7 - 8 LOWER SKIN WORN. REPAIRED IAW EA 6-5730-T0305940 PART1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240392](https://openairdocs.org/sdr/FDEA201402240392.md): Skin · worn · Feb 24, 2014 · N716FD · Airbus A300B4622 · Wing, Plate/Skin
  > LEFT WING RIB 7 - 8 LOWER SKIN WORN. REPAIRED IAW DWG R57150532 AND INSTALLED BUSHINGS IAW DWG R57150532. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240390](https://openairdocs.org/sdr/FDEA201402240390.md): Skin · cracked · Feb 24, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > NOSE LANDING GEAR WW RT AFT LOWER CUTOUT SKIN ONE EACH HOLE FOUND CRACKED. REPAIRED IAW EA 6-5330-T0305901 PART1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402240389](https://openairdocs.org/sdr/FDEA201402240389.md): Frame · cracked · Feb 24, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Frame
  > JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING, FOUND FRAME 43 CRACKED. REPAIRED IAW EA 6-5710-T0305954 PART 1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201402240388](https://openairdocs.org/sdr/FDEA201402240388.md): Frame · cracked · Feb 24, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Frame
  > JUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING, FOUND FRAME 42 CRACKED. REPAIRED IAW EA6-5710-T0305954 PART 1. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402240387](https://openairdocs.org/sdr/FDEA201402240387.md): Frame · cracked · Feb 24, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Frame
  > JUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING, FOUND FRAME 41 CRACKED. REPAIRED EA 6-5710-T0305954. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402210380](https://openairdocs.org/sdr/FDEA201402210380.md): Frame · cracked · Feb 21, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Frame
  > MAIN DECK CARGO FRAME 52 FOUND CRACKED FROM FASTERNER HOLE AT STRINGER 27L. REAMED THROUGH ALL LAYERS TO REMOVE CRACK AND COMPLIED WITH EA 6-5310-T0305807 PT1. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201402170343](https://openairdocs.org/sdr/FDEA201402170343.md): Door Frame · corroded · Feb 17, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Structure
  > AFT CARGO DOOR FWD CUTOUT FRAME CORRODED AT FR 59A BETWEEN STRINGER 42R - STRINGER 43R. REMOVED CORROSION IAW A300-600 SRM51-74-10 & REPAIR IAW EA6-5310-T0305876. TITLE FUSELAGE MAIN FRAME. CORROSION ON FRAME 59A AT STRINGER 42R - 44R.
- [SDR FDEA201402140318](https://openairdocs.org/sdr/FDEA201402140318.md): Skin · cracked · Feb 14, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > SKIN, FRAME 54, STRINGER 36 & 44, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5330-T0305912A PT1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201402140317](https://openairdocs.org/sdr/FDEA201402140317.md): Skin · cracked · Feb 14, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > SKIN AT FRAME 54, STRINGER 36 & 44, SHOWS A CRACK SIGNAL AT BUTT JOINT. REPAIRED IAW EA 6-5330-T0305912A PT1. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201402130313](https://openairdocs.org/sdr/FDEA201402130313.md): Skin · dented · Feb 13, 2014 · N716FD · Airbus A300B4622 · Trailing Edge Flaps
  > LEFT WING OTBD SIDE CENTER FLAP LOWER SKIN FOUND A DENTED BETWEEN RIB 9 - 10. FABRICATED REPAIR DOUBLER IAW SRM 57-50-00/201 FIG205 AND INSTALLED IAW SRM 57-50-00/201 FIG 205.
- [SDR FDEA201402030238](https://openairdocs.org/sdr/FDEA201402030238.md): Support Angle · gouged · Feb 3, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FRAME 60 CROSS FLOOR BEAM LOWER SUPPORT ANGLE WITH TWO EACH DEEP GOUGES AT ABOUT Y 1470 LOCATION. REMOVED THE DAMAGE ANGLE PER A300-600 SRM51-40-21. MADE THE PART PER ATTACHED ADFS(DWG:A53973318) INSTALLED THE NEW PART PER A300-600 SRM
- [SDR FDEA201402030242](https://openairdocs.org/sdr/FDEA201402030242.md): Support Fitting · cracked · Feb 3, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FRAME 63 CROSS FLOOR BEAM LOWER SUPPORT FITTING WITH A CRACK AT ABOUT Y 1470, LOCATION CRACK LENGTH 0.35 INCHES. REMOVED THE DAMAGED FITTING PER A300-600SRM51-40-21. INSTALLED THE FITTING PER A300-600 SRM51-40-21.
- [SDR FDEA201402030240](https://openairdocs.org/sdr/FDEA201402030240.md): Support Fitting · cracked · Feb 3, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FRAME 60 CROSS FLOOR BEAM LOWER SUPPORT FITTING WITH A CRACK AT ABOUT Y 1470, LOCATION CRACK LENGTH 0.3 INCHES. REMOVED THE DAMAGED FITTING PER A300-600 SRM51-40-21. INSTALLED THE FITTING PER A300-600SRM51-40-21.
- [SDR FDEA201402020233](https://openairdocs.org/sdr/FDEA201402020233.md): Stringer · corroded · Feb 2, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FRAME 60 - 61, STRINGER 46R, STRINGER CORRODED. REPLACED THE CORRODED STRINGER WITH A NEW ONE PER A300-600 SRM51-40-21 AT AFT CARGO FR58-FR65, S-46R LOCATION.
- [SDR FDEA201402020234](https://openairdocs.org/sdr/FDEA201402020234.md): Stringer · cracked · Feb 2, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STRINGER 47RT, STRINGER CRACK AT FRAME 59 LOCATION. REPAIRED THE DAMAGED STRINGER PER A300-600 SRM53-10-14 PARA 4 A FIG201 AT AFT CARGO COMPT AT FR59 STGR 47R.
- [SDR FDEA201402020236](https://openairdocs.org/sdr/FDEA201402020236.md): Fitting · cracked · Feb 2, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FRAME 63A LOWER FRAME FITTING CRACK BETWEEN STRINGER 44R - STRINGER 46R. REMOVED THE DAMAGED FITTING PER A300-600SRM51-40-21. INSTALLED THE FITTING PER A300-600SRM51-40-21.
- [SDR FDEA201402020235](https://openairdocs.org/sdr/FDEA201402020235.md): Support Beam · cracked · Feb 2, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT Y 525 LONGITUDINAL SUPPORT BEAM FOUND CRACK BETWEEN FRAME 65 - FRAME 66. REMOVED THE CRACK SUPPORT BEAM PER A300-600 SRM51-40-21. INSTALLED THE NEW SUPPORT BEAM PER A300-600 SRM51-40-21.
- [SDR FDEA201401290214](https://openairdocs.org/sdr/FDEA201401290214.md): Skin · corroded · Jan 29, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > FORWARD CARGO BAY DOOR CUTOUT FITTING CORRODED BETWEEN FRAMES 23 - 24, STRINGERS 49R - 54L. CORROSION REMOVED AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-13-12-201 PARA 6B(6) & PARA6B(4).
- [SDR FDEA201401270203](https://openairdocs.org/sdr/FDEA201401270203.md): Roller Track · cracked · Jan 27, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Structure
  > AFT CARGO BAY DOOR SILL AREA ROLLER TRACK LOWER SURFACE FOUND CRACKED AT FRAME 63A. CRACK LENGTH 1.5 INCHES. REPLACED IAW SRM 51-40-21 & DWG A25772929. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201401240189](https://openairdocs.org/sdr/FDEA201401240189.md): Floor Support · corroded · Jan 24, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO FLOOR SUPPORT CORRODED BETWEEN FRAMES 13 - 13A,Y D TO E. REMOVED FLOOR SUPPORT IAW SRM 51-40-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21
- [SDR FDEA201401210148](https://openairdocs.org/sdr/FDEA201401210148.md): Floorbeam · corroded · Jan 21, 2014 · N716FD · Airbus A300B4622 · Fuselage Main, Floor Beam
  > BULK CARGO BAY FRAME 66 FLOORBEAM CORRODED. REMOVED FLOORBEAM IAW SRM 51-40-21. INSTALLED NEW FLOORBEAM IAW SRM 51-72-10. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201401170125](https://openairdocs.org/sdr/FDEA201401170125.md): Sill · corroded · Jan 17, 2014 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW SRM 53-17-18/201 2.
- [SDR FDEA201201110100](https://openairdocs.org/sdr/FDEA201201110100.md): Battery · inoperative · Jan 11, 2012 · N716FD · Airbus A300B4622 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS, TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW MM 33-51-14-04-09. OP'S CHECKED SERVICEABLE.
- [SDR FDEA201112065175](https://openairdocs.org/sdr/FDEA201112065175.md): Cylinder · failed · Dec 6, 2011 · N716FD · Airbus A300B4622 · Landing Gear Door Retract Section
  > AFTER TAKE-OFF, DURING GEAR RETRACTION, AMBER LIGHT DOOR OPEN ON FORWARD PANEL AND UPPER PANEL, VIBRATIONS AFTER LEVEL-OFF AT FL330, AND LOWER ALTITUDES UNTIL LANDING GEAR WAS EXTENDED FOR LANDING, DOOR AMBER LIGHT CONTINUED ILLUMINATION DURING ENTIRE SEQUE
- [SDR FDEA201112065172](https://openairdocs.org/sdr/FDEA201112065172.md): Warning Light · false activation · Dec 6, 2011 · N716FD · Airbus A300B4622 · Landing Gear Position and Warning
  > AFTER TAKEOFF AND DURING GEAR RETRACTION, AN AMBER NOSE DOOR LIGHT ILLUMINATED ON FORWARD PANEL AND OVERHEAD PANEL. LIGHTS WENT OUT ON TAXI IN. TROUBLESHOT IAW TSM 32-30-00 FIG 102. INSPECTED SEQUENCE VALVE, NO DEFECTS NOTED. INSPECTED SWITCHES TO BOTH SYS
- [SDR FDEA201107012530](https://openairdocs.org/sdr/FDEA201107012530.md): Skin · damaged · Jul 1, 2011 · N716FD · Airbus A300B4622 · Nacelle/Pylon, Plate/Skin
  > UPON REMOVAL OF SKIRT ANGLE ON NR 2 PYLON INBD SIDE, 2 EA DOUBLE DRILLED HOLES, 1 HOLE WITHIN.1 OF ANOTHER HOLE. REPAIRED HOLES IAW TD 70548824/012/2011, ISSUE A.
- [SDR FDEA201106222385](https://openairdocs.org/sdr/FDEA201106222385.md): Roller Track · corroded · Jun 22, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > L1 ROLLER TRAY IN FWD CARGO COMPT BETWEEN FRAMES 29 AND 30 HAS 2 EA AREAS OF CORROSION ON OTBD FLANGE BLENDED CORROSION IAW SRM 517-74-10 AND FOUND CORROSION TO BE OUT OF LIMITS IAW 53-10-15, PG 108. REPAIR ROLLER TRACK IAW SRM 53-10-15, FIG 202.
- [SDR FDEA201106172324](https://openairdocs.org/sdr/FDEA201106172324.md): Skin · misrepaired · Jun 17, 2011 · N716FD · Airbus A300B4622 · Trailing Edge Flaps
  > FLUSH REPAIR LOCATED ON LT WING CENTER FLAP UPPER T/E SKIN BETWEEN RIBS 22 TO 24 & AFT OF REAR SPAR IS NOT A VALID REPAIR. REMOVED FLUSH REPAIR AND REPAIRED SKIN WITH AN EXTERNAL DOUBLER PER EA 6-5750-145623.
- [SDR FDEA201106172319](https://openairdocs.org/sdr/FDEA201106172319.md): Skin · gouged · Jun 17, 2011 · N716FD · Airbus A300B4622 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB L/E PANEL 341CB HAS SEVERAL SMALL GOUGES AND NICKS ON L/E FROM INBD TO OTBD END. SMOOTHED AND BLENDED 4 AREAS OF L/E AREA. NR 1 AND 4 ARE WITHIN LIMITS AND NR 2 AND 3 ARE OUT OF LIMITS IAW SRM 51-10-00 TABLE 1. FABRICATED AND INSTALLED REPAI
- [SDR FDEA201106162294](https://openairdocs.org/sdr/FDEA201106162294.md): Roller Track · corroded · Jun 16, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > CARGO ROLLER TRAY IN FWD CARGO COMPT. LT CENTER CORRODED AT FRAMES 23 AND 18 AFTER CORROSION REMOVAL, ROLLER TRAY FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, PG 108. REPAIRED ROLLER TRAY IAW SRM 53-10-15, FIG 202.
- [SDR FDEA201106112208](https://openairdocs.org/sdr/FDEA201106112208.md): Skin · corroded · Jun 11, 2011 · N716FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > 8 SQ IN OF FUSELAGE INTERNAL SKIN CORROSION ON FWD CARGO AFT BILGE BETWEEN STR 55 AND STR 54R FWD OF FR 38.2. REMOVED CORROSION IAW SRM 51-74-10. FOUND AREA OUT OF LIMITS IAW SRM 53-14-12 FIG. 101. REPAIRED MANHOLE INTEGRAL PLATE IAW SRM 53-14-12 FIG. 208 W
- [SDR FDEA201106092176](https://openairdocs.org/sdr/FDEA201106092176.md): Roller Track · corroded · Jun 9, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > ROLLER TRAY 2L INBD FLANGE HAS CORROSION BETWEEN FRAMES 34 AND 35 IN FWD CARGO COMPT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF ROLLER TRACK IN FWD LOWER CARGO COMPARTMENT, ROLLER TRAY 2 LT BETWEEN FR 34 AND FR 35 AND INSTALLED CARGO COMPARTMENT
- [SDR FDEA201106092177](https://openairdocs.org/sdr/FDEA201106092177.md): Roller Track · corroded · Jun 9, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > ROLLER TRACK 2R BETWEEN FRAMES 29 AND 30 CORRODED IN FWD CARGO COMPT. AFTER REMOVAL OF LEVEL 1 CORROSION, TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 PG 107. REPAIRED ROLLER TRACK IAW SRM 53-10-15 FIG 203. REPROTECTED IAW A300-600 SRM 51-75-10.
- [SDR FDEA201106092179](https://openairdocs.org/sdr/FDEA201106092179.md): Roller Track · damaged · Jun 9, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT. ROLLER TRAY R1 HAS DOUBLE DRILLED HOLE BETWEEN FRAME 35 AND 36 REMOVED AND REPLACED ROLLER TRACK SECTION IAW SRM 53-10-15 PG 211/212.
- [SDR FDEA201106082159](https://openairdocs.org/sdr/FDEA201106082159.md): Floor Support · corroded · Jun 8, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF ROLLER TRAY ON N01207 IN FWD CARGO COMPT BETWEEN FR 35 AND 36, FOUND CORROSION ON TOP OF FLOOR SUPPORT AT FRAME 35. REPAIRED FLOOR SUPPORT AT FRAME 35 IAW SRM 53-10-15, FIG 207.
- [SDR FDEA201106062135](https://openairdocs.org/sdr/FDEA201106062135.md): Frame · corroded · Jun 6, 2011 · N716FD · Airbus A300B4622 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD BOTTOM FWD SIDE AT FR 80/82 CIRCUMFERENTIAL STRAP CORRODED 7 IN LENGTH X 4 IN WIDTH BETWEEN STR 54R TO 56R. REMOVED CIRCUMFERENTIAL STRAP STRINGER 51R TO 54L IAW SRM 51-40-21. VERIFIED NO FURTHER CORROSION DAMAGE FOUND. INSTALLED NE
- [SDR FDEA201105191879](https://openairdocs.org/sdr/FDEA201105191879.md): Roller Track · misrepaired · May 19, 2011 · N716FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > EXISTING ROLLER TRACK REPAIR HAS INCORRECT ANGLES SHAPE AND THICKNESS AND MS20470D6 RIVETS INSTALLED FROM BOTTOM SURFACE UP AND NO COUNTERSUNK RIVETS AT OUTER FLANGES AFT CARGO ROLLER TRACK LT NR 3 Y1470 BETWEEN FR 55 TO FR 56 EXISTING REPAIR REMOVED AND
- [SDR FDEA201105191881](https://openairdocs.org/sdr/FDEA201105191881.md): Stringer · misrepaired · May 19, 2011 · N716FD · Airbus A300B4622 · Fuselage Main, Longeron/Stringer
  > STRINGER 53L BETWEEN FRAMES 63 TO 64 EXISTING REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED EXISTING REPAIR SPLICE ON STRINGER 53LT BETWEEN FRAMES 63 TO 64 AND REMOVED AND REPLACED FWD STRINGER SECTION BETWEEN FRAME 62 TO
- [SDR FDEA201105191880](https://openairdocs.org/sdr/FDEA201105191880.md): Stringer · misinstalled · May 19, 2011 · N716FD · Airbus A300B4622 · Fuselage Main, Longeron/Stringer
  > STRINGER 52L BETWEEN FRAMES 63 TO 64 REPAIR SPLICE ANGLE HAS INCORRECT MATERIAL THICKNESS INSTALLED REMOVED AND REPLACED REPAIR SPLICE ANGLE ON STRINGER 52L/H BETWEEN FRAMES 63 TO 64 PER A300-600 SRM 53-10-14 FIG 201 PAGES 203 TO 206.
- [SDR FDEA201105181872](https://openairdocs.org/sdr/FDEA201105181872.md): Stringer Splice · failed · May 18, 2011 · N716FD · Airbus A300B4622 · Fuselage Main, Longeron/Stringer
  > STRINGER 44 RT SPLICE ANGLE BETWEEN FRAMES 38.2 TO 39 HAS INCORRECT THICKNESS INSTALLED REMOVED AND REPLACED STRINGER 44RH SPLICE ANGLE BETWEEN FRAME 38.2 TO 39 WITH CORRECT REPAIR MATERIAL PER A300-600 SRM 53-10-14 FIG 201 PAGES 203 TO 206
- [SDR FDEA201105171857](https://openairdocs.org/sdr/FDEA201105171857.md): Seat Track · misrepaired · May 17, 2011 · N716FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR LOCATED INCORRECTLY BETWEEN FRAMES 60 AND 61 OTBD SIDE AT SEAT TRACK 2R -Y450. REMOVED AND REPLACED SEAT TRACK 2R -Y450 FROM FRAME 58 TO 62 WITH NEW SECTION AND SPLICES PER A300-600 SRM 53-10-16 FIG 208 SHEET 1 PAGES 243 TO 248
- [SDR FDEA201105121832](https://openairdocs.org/sdr/FDEA201105121832.md): Skin · punctured · May 12, 2011 · N716FD · Airbus A300B4622 · Elevator, Plate/Skin
  > LT ELEVATOR UPPER SURFACE AT STA 253/ RIB NR 8 UPPER SKIN HAS A HOLE PUNCTURE APPROX 0.25 IN. LONG THROUGH INTO HONEYCOMB. REPAIRED LT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, PARA I, PAGES 248 THRU 252.
- [SDR FDEA201009163501](https://openairdocs.org/sdr/FDEA201009163501.md): Engine · failed · Sep 16, 2010 · N716FD · Airbus A300B4622 · Turbine Engine Reduction Gear
  > NR 2 ENG CATASTROPHIC FAILURE. (DURING CRUISE, ECON, COST INDEX 55) MC1 U IAW POWERPLANT ENGINEER THIS ENGINE IS APPROVED FOR ENGINE CHANGE. NR 2 ENGINE CHANGED REF WC 64T0711-2. ITEM CLOSED.

Next page: https://openairdocs.org/deregistered/N716FD-2024-06-27/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 = 'N716FD' AND deregistration_id = 'N716FD-2024-06-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N716FD-2024-06-27/reports

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