N817FD, cancelled Mar 2, 2024

Service difficulty reports · 66

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N817FD' AND deregistration_id = 'N817FD-2024-03-02'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201405211117Fitting · damagedLEFT RIB 5 FWD LUG BORE OUT OF ROUND REPAIRED LT RIB 5 FWD LUG BORE OUT OF ROUND IAW DWG R57249389 & COMPLIED WITH EA 6-5710-T0308275.May 21, 2014 · N817FD · Airbus A310304 · Wing Miscellaneous StructureSDR FDEA201401030015Switch · malfunctionedLEFT CABIN DOOR SHOWED UNLOCKED AT FL 240. LEVELED OFF, PERFORMED QRH & PUSHED ON THE HANDLE. DOOR SHOWED LOCKED. CONTINUED TO CLIMB & DOOR SHOWED UNLOCKED AT FL 340, FINAL ALTITUDE WAS TO BE FL 400, RETURNED TO DEPARTURE. REMOVED AND REPLACED DOOR WARNINJan 3, 2014 · N817FD · Airbus A310304 · Door Warning SystemSDR FDEA201312122966Hinge Fitting · nickedNOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.Dec 12, 2013 · N817FD · Airbus A310304 · Fuselage, Door HingeSDR FDEA201304240855Wire Harness · failedAFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 BOGIES IN POSITION IAW MM 32-11-43-04.Apr 24, 2013 · N817FD · Airbus A310304 · Landing Gear System WiringSDR FDEA201203160978Shear Plate · corrodedFWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.Mar 16, 2012 · N817FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR FDEA201202160591Computer · malfunctionedAPPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURNED TO 6.42. TROUBLESHOOTING VERIFIED FUEL LEVEL IN RT OTBD TANK ON RT NR 2 & NR 3 MAGNETIC LEVELFeb 16, 2012 · N817FD · Airbus A310304 · Fuel Quantity IndicatorSDR FDEA201107032558Floorbeam · damagedBULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.Jul 3, 2011 · N817FD · Airbus A310304 · Fuselage Main, Floor BeamSDR FDEA201107012531Stringer · gougedAFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51-21-10, PG 2, SRM 51-40-44, PG 1 AND SRM 51-75-10, PG 204.Jul 1, 2011 · N817FD · Airbus A310304 · Fuselage Main, Longeron/StringerSDR FDEA201107012532Seal · crackedMETALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.Jul 1, 2011 · N817FD · Airbus A310304 · Fuel StorageSDR FDEA201106142246Web · damagedAFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21Jun 14, 2011 · N817FD · Airbus A310304 · Fuselage Miscellaneous StructureSDR FDEA201106122211Seat Track · crackedSEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 LT SEAT TRACK SECTION AT FR 19 IAW SRM 51-72-10.Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106122212Seat Track · corrodedMDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. REPAIRED NR 6 SEAT TRACK AT FR 19 IAW EA 6-5310-145630.Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106122210Seat Track · corrodedRIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMITS IAW SRM 53-10-16. REPAIRED IAW EA 6-5310-145630.Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106122213Floorbeam · corrodedMDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED TEE FWD OF SEAT TRACK NR 3 AT FR 12A IAW SRM 51-72- 10.Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage Main, Floor BeamSDR FDEA201106102204Seat Track · damagedSEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT FR 54.3 IAW SRM 51-72-10.Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage Main, FrameSDR FDEA201106102201Seat Track · damagedMDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 5R SECTION AT FR 54.2 INCLUDING 17 INCHES AFT OF FR 54.2.Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106102203Seat Track · damaged2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT FR 54.2Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage Main, FrameSDR FDEA201106102202Seat Track · damagedSEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 IAW SRM 51-72-10.Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106052123Fitting · corrodedNR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTING IAW S/B 54-20-20 PAR. B(6) REINSTALLED NR 2 PYLON IAW AMM 54-50-00-4 COMPLIED WITH FEDEX EA 6Jun 5, 2011 · N817FD · Airbus A310304 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201106052121Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTINGS IAW S/B 54-2020 PARA B(6). REINSTALLED NR 1 PYLON IAW AMM 54-50-00-4. COMPLIED WITH EA-5450-Jun 5, 2011 · N817FD · Airbus A310304 · Nacelle/Pylon, Main FrameSDR FDEA201106012083Seat Track · misinstalledMAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 EACH RIVETS AND INSTALLED 20 EACH LOCK FASTENERS ON TOP FLANGE OF SEATTRACK REPAIR BETWEEN FRAMES Jun 1, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002090367Bellcrank · dirtyLT MAIN GEAR DOOR WOULD NOT CLOSE ON T/O. RETURNED TO DEPARTURE. OPS CHECKED LT MLG DOOR IAW MM 32-12-11-5. OPS CHECKS NORMAL. DURING TROUBLESHOOTING, WERE ABLE TO DUPLICATE THIS PROBLEM BY OPERATING DOOR WITH GROUND CONTROL HANDLE, AFTER DISASSEMBLING, CLFeb 9, 2010 · N817FD · Airbus A310304 · Landing Gear Door Retract SectionSDR FDEA200907012422Idg · underservicedON T/O ROLL AT APPROX 80 KNOTS RECEIVED ECAM ALERT, NR 1 IDG OIL PRESS W/ GEN 1 FAULT. RTO AND RETURNED TO BLOCKS. GEN 1 FAULT CLEARED BUT IDG NR1 FAULT KEPT FLICKERING. SERVICED NR 1 ENG IDG IAW AMM 12-13-24-0. RAN NR 1 ENG IAW JRH CHAP 5. NO LEAKS NOTED, Jul 1, 2009 · N817FD · Airbus A310304 · Alternator-Generator DriveSDR FDEA200812065096Bushing · damagedMAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FABRICATED REPLACEMENT REPAIR BUSHING AND INSTALLED IAW FEDEX EA 6-5310-99725A, RELEASE DATE 07/20/06.Dec 6, 2008 · N817FD · Airbus A310304 · Fuselage, Landing Gear Attach FittingsSDR 08FDEA04961Seat Track · damagedMAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-21.Nov 22, 2008 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01724Transmitter · inoperativeON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN HYD PUMPS. FAULTS ON OVERHEAD WERE AS FOLLOWS: GREEN SYS SERVO (GREEN PUMPS OFF), SLAT SYS 1 AND 2, SPOILER NR 5. DID GO AROUND FOUND RT MMay 1, 2008 · N817FD · Airbus A310304 · Hydraulic Indicating SystemSDR 08FDEA00192Hydraulic System · lowREJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE.Jan 18, 2008 · N817FD · Airbus A310304 · Hydraulic System, MainSDR 07FDEA00151Slide · lowR1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25-61-22-4-01 AND A310 - 300 AMM 52-10-00-3.Jan 22, 2007 · N817FD · Airbus A310304 · Escape SlideSDR 06FDEA03588Fitting · corrodedCOMPLY WITH AGING 9-AGING-INSP, FOUND CORROSION AND WEAR LOCATED IN RT FITTING BETWEEN FS 16A/ FS 17 IN HOLE AT ATTACHMENT FITTING OF AFT DOOR.Oct 4, 2006 · N817FD · Airbus A310304 · Fuselage Main, Attach FittingsSDR 06FDEA03400Skin · damagedRT MLG-STRUT DOOR W/SKIN SURFACE DAMAGED AND REPAIR AT LOWER AREA THE STRUT DOOR WAS REPAIRED PER FEDEX EA 6-5280-99721 EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".Sep 22, 2006 · N817FD · Airbus A310304 · Landing Gear DoorsSDR 06FDEA03054Skin · damagedFOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO ANAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03053Skin · damagedFOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTBD LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR W/W DOOR PER SRM 52-81-12. REPAIR EVALUATED PER GMM Aug 22, 2006 · N817FD · Airbus A310304 · Landing Gear DoorsSDR 06FDEA03052Skin · damagedFOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-2Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/SkinSDR 06FDEA03051Skin · damagedFOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-21-12 FIG 204. Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/SkinSDR 06FDEA03050Skin · damagedFOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR, DISCREPANCY REPORT 43000001-391Aug 22, 2006 · N817FD · Airbus A310304 · Leading Edge DevicesSDR 06FDEA03049Skin · damagedFOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS REF : RAS /DA/BRE/1642/97, REPAIR EVALUATEAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03048Skin · damagedFOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03047Skin · damagedFOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03046Skin · damagedFOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZAug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge FlapsSDR 06FDEA03045Structure · unknownFOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OUTB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THIS REPAIR WAS REMOVED AND REPLACED A NEW TRAILING EDGE PAug 22, 2006 · N817FD · Airbus A310304 · Wing Miscellaneous StructureSDR 06FDEA03044Door · misrepairedFOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA, REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03043Door · misrepairedFOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN EXISTING SRM REPAIR . NEW REPAIR ACCOMPLISHEDAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03042Door · misrepairedFOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR . NEW REPAIR ACAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03041Door · misrepairedFOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FR 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03040Door · misrepairedFOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIRAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03039Skin · damagedPREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA EXISTING REPAIR COVERED BY RAS REF:RAS/DAHAM/4014519/2001. REPAIR EVALUATED PER GMM 6-2-100Aug 22, 2006 · N817FD · Airbus A310304 · Cargo/Baggage DoorsSDR 06FDEA3035None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT AFT COMP´T DOOR FRAME BETWEEN FS 63/64 AND STRINGER BETWEEN 40/44 RT. REPAIR REQUIRES EVALUATION Aug 22, 2006 · N817FD · Airbus A310203 · Standard Practices/StructuresSDR 06FDEA3036None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 64/67 AND BETWEEN STRG 33/40 RT . REPAIR REQUIRES EVALUATION FORAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3037None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 66/68 AND BETWEEN STRG 48/54 RT . REPAIR REQUIRES EVALUATION FORAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3038None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT FS4715/4760, FS 89/90, STRG 33/38 NEXT TO APU INLET. REPAIR REQUIRED EVALUATION FOR MAJOR/ MINOR DAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/Structures
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