N669FE

Service difficulty reports · 320

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 = 'N669FE' AND registry_match = 'registration'
  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 FDEA200903040844Floor Panel · damagedMAIN CABIN FLOOR PANEL 241 RJ IS BROKEN. FABRICATED NEW FLOORBOARD 241RJ IAW DWG SRZ-25-005 REV G.Mar 4, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020792Floor Panel · brokenFWD PIT FLOOR PANEL 131 SG IS BROKEN. FABRICATED NEW PANEL IAW DWG. SRZ-25-005 REV. G. REF. DWG. SRZ-25-005 REV. G. PANEL PART MARKED IAW GMM 7-0-1001 PANEL.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020796Floor Panel · crackedFWD PIT FLOOR PANEL 131 NG IS CRACKED. FABRICATED FLOOR PANEL IAW DRAWING SRZ 25-005, REV "G", PO 626008.1. MARKED FLOOR PANEL IAW GMM 7-0-1001. APPLIED FOAM TAPE TO THE FLOOR PANEL REF DRAWING SRZ 25-005, REV "G".Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020794Floor Panel · crackedFWD PIT FLOOR PANEL 131 QG IS BROKEN. FABRICATED FLOOR PANEL 131 QG IAW DWG SRZ 25-005, REV "G". FLOOR PANEL MARKED IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020795Floor Panel · brokenFWD PIT FLOOR PANEL 131 LG IS BROKEN. FABRICATED FLOORBOARD IAW DWG. SRZ-25-005 REV.G. PART MARKED IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020793Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL; 152 XF HAS A DAMAGED AND TORN FACE. MATERIAL ID N407 FLOORBOARD MATERIAL REF DWG SRZ 25-005, REV "G" ; PO NR 626008.1. FABRICATED FLOOR PANEL 152 XF REF DWG SRZ 25-005, REV "G". MARKED FLOOR PANEL 152 XF IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020791Floor Panel · crackedAFT PIT FLOOR PANEL 151 UF IS CRACKED. MATERIAL ID N407 FLOORBOARD MATERIAL REF DWG SRZ 25-005, REV "G"; PO NR 626008.1. FABRICATED FLOOR PANEL 151 UF REF DWG SRZ 25-005, REV "G". MARKED FLOOR PANEL 151 UF IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020790Floor Panel · crackedAFT PIT FLOOR PANEL 151 XF IS CRACKED. MATERIAL ID N407 FLOORBOARD MATERIAL REF DWG SRZ 25-005, REV "G"; PO NR 626008.1. FABRICATED FLOOR PANEL 151 XF REF DWG SRZ 25-005, REV "G". MARKED FLOOR PANEL 152 UF IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200903020789Floor Panel · crackedAFT PIT FLOOR PANEL 152 UF IS BROKEN. MATERIAL ID N407 FLOORBOARD MATERIAL REF DWG SRZ 25-005, REV "G"; PO NR 626008.1. FABRICATED FLOOR PANEL 152 UF REF DWG SRZ 25-005, REV "G". MARKED FLOOR PANEL 152 UF IAW GMM 7-0-1001.Mar 2, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902270754Adapter · wornMAIN CABIN FLOOR STRUCTURE SEAT TRACK HAS WEAR AND BARE METAL AT FRAME 22; RBL 21 - RBL 36. ADAPTER TRACK WEAR OUT OF LIMITS IAW A300-600 SRM 53-10-15; FIG 107. REMOVED ADAPTER TRACK IN REF TO A300-600 SRM 51-40-21; PARA 7. RECEIVED NEW ADAPTER P/N A53781Feb 27, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902270752Floor Panel · brokenMAIN CABIN FLOOR PANEL 251 XG IS BROKEN. FABRICATED NEW FLOOR PANEL251XG IAW DWG SRZ-25-005 REV G.Feb 27, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902270751Floor Panel · brokenMAIN CABIN FLOOR PANEL 251 UH IS BROKEN. FABRICATED NEW FLOORBOARD 251UH IAW DWG SRZ-25-005 REV G.Feb 27, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902260736Floor Panel · crackedMAIN CABIN FLOOR PANEL 261 AH IS CRACKED AT FRAME 80, LBL 90. FABRICATED NEW FLOORBOARD IAW STANDARD REPAIR DRAWING FOR FLOOR PANEL REPLACEMENT FX SRZ 25-005, REV "G". PART MARKED FLOORBOARD IAW FEDEX GMM 7-0-1000.Feb 26, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902260735Floor Panel · damagedMAIN DECK FLOOR PANEL 252 AH IS CRACKED FROM FRAME 65 - FRAME 69, RBL 65 - RBL 70. FABRICATED NEW FLOORBOARD 252AH IAW STANDARD REPAIR DWG. SRZ-25-005 REV. G. PART MARKED NEW FLOORBOARD 252AH IAW GMM 7-0-1000. APPLIED ANTI-SKID COATING IAW DWG SRZ-25-005 RFeb 26, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902260734Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 VF HAS HEAVY IMPACT DAMAGE FROM FRAME 62 - FRAME 65. FABRICATED NEW FLOOR PANEL IAW STANDARD REPAIR DWG. (SDR) SRZ-25-005 REV. G MATERIAL I.D. IS A402H IAW DWG. SRZ-25-005 REV. G. PART MARKED NEW FLOOR PANEL IAW GMM 7-0-1000. APPLIFeb 26, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902260733Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 UH HAS HEAVY IMPACT DAMAGE FROM FRAME 60 - FRAME 62. FABRICATED NEW FLOOR PANEL IAW STANDARD REPAIR DWG. (SDR) SRZ-25-005 REV. G MATERIAL I.D. IS A402H IAW DWG SRZ-25-005 REV. G. PART MARKED NEW FLOOR PANEL IAW GMM 7-0-1000. APPLIEFeb 26, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902260732Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 PH HAS HEAVY IMPACT DAMAGE FROM FRAME 58 - FRAME 60. FABRICATED NEW FLOOR PANEL IAW STANDARD REPAIR DWG. (SDR) SRZ-25-005 REV. G MATERIAL I.D. IS A402H IAW DWG. SRZ-25-005 REV. G. PART MARKED NEW FLOOR PANEL IAW GMM 7-0-1000. APPFeb 26, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902250722Seat Track · wornMAIN CABIN FLOOR STRUCTURE, SEAT TRACK HAS BARE METAL AT FRAME 32, RBL 27 - RBL 36. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM A300-600 SRM 53-10-15, FIG 107. UT GAUGE USED T8225R. REMOVED AND REPLACED ADAPTER PO 3 649102.1.Feb 25, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902240701Seat Track · corrodedMAIN SEAT TRACK IS CORRODED IN SEVERAL PLACES FROM FRAME 63 TO FRAME 69, BL 0. REMOVED & REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-10-16 FIG 201.Feb 24, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902240700Seat Track · corrodedMAIN CABIN SEAT TRACK FLANGE IS CORRODED AT FRAME 16A, RBL 36. REMOVED CORROSION FROM THE TRACK & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED CORRODED SEAT TRACK IAW SRM 51-72-10. LOCATED & DRILLED NEW SEAT TRACK IAW DWG A53612500 & SRM 51-40-21.Feb 24, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902240699Skin · chafedTHE SKIN ABOVE THE L-1 DOOR CORNERS ARE CHAFED AT FRAME 14C - FRAME 15C. ACCOMPLISHED E.A. 6-5310-127928. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 51-31-20; FIG 35 & SRM 53-10- 15; FIG 107.Feb 24, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200902240698Skin · chafedTHE SKIN ABOVE THE R-1 DOOR IS CHAFED AT FRAME 14 - FRAME 15C. ACCOMPLISHED EA 6-5310-127928.Feb 24, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200902230871Floorbeam · gougedMAIN CABIN FLOOR SUPPORT FITTING GOUGED FR48 LBL 17.5 FABRICATED 1 EA SUPPORT BRACKET IAW AIRBUS DWG A53812968 REV A AND SRM 51-21-10. DRILLED UP SUPPORT BRACKET IAW AIRBUS DWG A53812968 REV A. TOP COATED IAW SRM 51-23-10. PART MARKED SUPPORT BRACKET IAW GFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200902230658Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 24, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. ADAPTER FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED ADAPTER IAW SRM 51-40-21. RECEIVED NEW ADAPTER. LOCATED, DRILLED, COUNTERSUNK AND DEBURRED IAW DWG AFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA200902230654Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 29, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. BLENDED OUT. ORIGINAL THICKNESS 0.472. MATERIAL LOSS 0.035. MATERIAL REMAINING 0.447 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED AND REPLACED ADAPTER PFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200902230652Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 31, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. REMOVED WEAR MARKS. ORIGINAL THICKNESS 0.472. REMAINING THICKNESS 0.440. REMOVED 0.032 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED CLS ADAPTER IAW SRFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA200902230669Adapter · wornMAIN CABIN FRAME 30, LBL 69, SEAT TRACK ADAPTER IS WORN. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 51-31-20; FIG 35 & SRM 53-10- 15; FIG 107. REMOVED ADAPTER IAW SRM 51-40-21. RECEIVED NEW ADAPTER. LOCATED & DRILLED PART IAW DWG A53781936. INSTALFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230668Floorbeam · corrodedMAIN CABIN FRAME 32, LBL 67 IS CRACKED. BLENDED CRACKED FLOORBEAM IAW SRM 53-10-15 FIG 212. CRACK STILL PRESENT AFTER ACCOMPLISHING HFEC OF AREA IAW NTM 51-10-08. CUT OUT DAMAGE IAW SRM 53-10-15 FIG 212. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 53-10-15 FFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA200902230667Frame · crackedMAIN CABIN FRAME 31, LBL 67 IS CRACKED. NDT VERIFIED CRACK IAW PT 6 51-10-08. CUT OUT CRACK NDT VERIFYED NO CRACK NOTED. FABBED REPAIR PARTS. INSTALLED REPAIR IAW SRM 53-10-15.Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA200902230664Seat Track · wornMAIN CABIN FRAME 27, LBL 69, SEAT TRACK ADAPTER IS WORN. REMOVED CLS ADAPTER IAW SRM 51-40-21. LOCATED & DRILLED NEW ADAPTER IAW DWG 13A53781908. INSTALLED NEW ADAPTER IAW SRM 51-40-21. PAINTED NEW ADAPTER IAW SRM 51-75-10.Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230663Adapter · wornMAIN CABIN FRAME 27, LBL 69, SEAT TRACK ADAPTER IS WORN. REMOVED CLS ADAPTER IAW SRM 51-40-21. LOCATED & DRILLED NEW ADAPTER IAW DWG 13A53781908. INSTALLED NEW ADAPTER IAW SRM 51-40-21. PAINTED NEW ADAPTER IAW SRM 51-75-10.Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230662Adapter · wornMAIN CABIN FRAME 26, LBL 69, SEAT TRACK ADAPTER IS WORN. REMOVED ADAPTER IAW SRM 51-40-21; PARA A. ADAPTER FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15; FIG 101. LOCATED & DRILLED ADAPTER IAW DWG 10A53781935. INSTALLED IAW SRM 51-40-21; PARA A & DWG 10A5Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230661Adapter · wornMAIN CABIN FRAME 25, LBL 69, SEAT TRACK ADAPTER IS WORN. ADAPTER FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. REMOVED ADAPTER IAW SRM 51-40-21. RECEIVED NEW ADAPTER. LOCATED, DRILLED, COUNTERSUNK & DEBURRED IAW DWG A537819352. PRIMED ADAPTER IAW SRM 51Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230660Floorbeam · crackedMAIN CABIN FLOOR STRUCTURE, FWD SIDE OF FRAME 27 IS CRACKED 1 INCH BELOW FLOOR LEVEL AT RBL 27. BLENDED CRACKED FLOORBEAM IAW SRM 53-10-15 FIG 212. CRACK STILL PRESENT AFTER ACCOMPLISHING HFEC OF AREA IAW NTM 51-10-08. CUT OUT DAMAGE IAW SRM 53-10-15 FIG 21Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200902230659Floorbeam · crackedMAIN CABIN FLOOR STRUCTURE, FWD SIDE OF FRAME 28 IS CRACKED 1 INCH BELOW FLOOR LEVEL AT RBL 27. BLENDED CRACKED FLOORBEAM IAW SRM 53-10-15 FIG 212. CRACK STILL PRESENT AFTER ACCOMPLISHING HFEC OF AREA IAW NTM 51-10-08. CUT OUT DAMAGE IAW SRM 53-10-15 FIG 21Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200902230657Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 23, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. NEW ADAPTER, LOCATED & DRILLED ADAPTER PLATE IAW DWG 10A53781937, REV "A". INSTALLED NEW ADAPTER PLATE IAW SRM 51-40-21.Feb 23, 2009 · N669FE · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230656Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 25, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. SEAT TRACK ADAPTER FOUND TO OUT OF LIMITS IAW SRM 53-10-15. REMOVED ADAPTER IAW SRM 51-40-21. LOCATED & DRILLED HOLES IAW DWG 10A53781935; REV "B". INSTALLED AFeb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200902230655Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 28; RBL 27 - RBL 36 HAS WEAR AND BARE METAL. CLEANED UP WEAR AREA OF ADAPTER AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG 107. LOCATED AND DRILLED ADAPTER PLATE IAW DWG A53781937. INSTALLED IAW SRM 51Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230653Adapter · wornMAIN CABIN STRUCTURE, SEAT TRACK ADAPTERS AT FRAME 30, RBL 27 - RBL 36 HAS WEAR AND BARE METAL. REMOVED WEAR MARKS. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. RECEIVED NEW ADAPTER. LOCATED & DRILLED IAW DWG A53781937. INSTALLED ADAPTER IAW DWG A53781937 Feb 23, 2009 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200902190590Floorbeam · crackedAFT CARGO COMPARTMENT MAIN FLOOR ATTACH ANGLE AT FRAME 60 - FRAME 60, RBL 60 - 80. REMOVED ATTACH ANGLE IAW A300-600 SRM 51-40-21. RECEIVED NEW ANGLE P/N A5327541120300, PO NR 648839.1. LOCATED AND DRILLED IAW A300-600 SRM 51-40-44, PARA 2. INSTALLED IAW AFeb 19, 2009 · N669FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200902190592Floor Support · crackedMAIN CABIN FLOOR SUPPORT FITTING IS CRACKED AT FRAME 48, RBL 55. REMOVED CRACKED FLOOR FITTING IN REF TO SRM 51-40-21. DRILLED NEW SUPPORT FITTING IN REF TO SRM 51-40-44 & DWG A53812080. INSTALLED NEW SUPPORT FITTING IN REF TO SRM 51-40-21 & A53812080.Feb 19, 2009 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200902190591Floor Support · crackedMAIN CABIN FLOOR SUPPORT FITTING IS CRACKED AT FRAME 48, LBL 55. REMOVED CRACKED TRACK LINK IAW SRM 51-40-21. LOCATED, DRILLED AND INSTALLED IAW DWG A53812080.Feb 19, 2009 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200902190586Floor Panel · puncturedBULK CARGO COMPARTMENT FLOOR PANEL 161 HF BOTTOM SKIN IS PUNCTURED. REPAIRED PUNCTURES (2EA) ONFLOOR PNL. 161HF REF. SRM 53-10-20 PARA. 10.Feb 19, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200902190583Floor Panel · corrodedBULK CARGO COMPARTMENT FLOOR PANEL 161 BF BOTTOM SKIN IS DELAMINATED. FABRICATED BOARD IAW DWG. SRZ-25-011 REV.C. FLOORBOARD PART MARKED PER GMM 7-0-1001. NON SKID TAPE APPLIED IAW DWG. SRZ-25-011 REV.BFeb 19, 2009 · N669FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00325Module · failedAFTER POWER TO FLEX AROUND 40K HAD TO ABORT TAKEOFF DUE TO YELLOW HYD LOW AER ECAM, AFTER ABORT, ALL RESET TRIED AGAIN SAME OUTCOME ABORTED T/O AROUND 52K. REMOVED AND REPLACED YELLOW SYSTEM RESERVOIR CHECK VALVE. REMOVED AND REPLACED DIODE MODULE 35VD. ALLJan 30, 2008 · N669FE · Airbus A300F4605R · Hydraulic System, MainSDR 07FDEA01757Access Panel · damagedON TAKEOFF WHEN LANDING GEAR WAS RETRACTED THE LEFT MAIN GEAR DOOR AMBER LIGHT STAYED ILLUMINATED ON BOTH THE OVERHEAD AND FORWARD PANEL. DROPPED LEFT GEAR DOOR AND DISCOVERED INNER ACCESS PANEL TO LEFT PACK LAYING ON GEAR DOOR. (SMASHED) UNABLE TO REINSTALMay 10, 2007 · N669FE · Airbus A300F4605R · DoorsSDR 07FDEA01096Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED FROM FRAME 38.2 TO 40 RBL 77 REMOVED AND REPLACED SEAT TRACK ASSY IAW A300-600 SRM 51-40-21 PARA 6 AND A300-600 SRM 41-40-21 PARA 7, MINOR REPAIR PO 565247.1.Mar 22, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01066Frame · gougedRT SIDE INSIDE FUSE FR47 BETWEEN STR 12R AND 13R GOUGED FRAME COMPLIED WITH FEDEX EA NR 6-5310-105186 TITLE FUSELAGE MINOR NICKS IN FRAME 47 STRINGER 12L-13L AND 12R-13R REPAIR, BLENDED 2 AREAS WITH A MAXIMUM DEPTH OF .077 ON THE INBD CORNER AS NOTED IN FIGUMar 21, 2007 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR 07FDEA01065Frame · gougedLT SIDE INSIDE FUSE, FS 47, BETWEEN STR 12L AND 13L GOUGED FRAME. COMPLIED WITH FEDEX EA NR 6-5310-105186 TITLE FUSELAGE, MINOR NICKS IN FRAME 47 STRINGER 12L-13L AND 12R - 13R REPAIR, BLENDED 2 AREAS WITH A MAXIMUM DEPTH OF .077 ON THE INBD CORNER AS NOTEDMar 21, 2007 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR 07FDEA01063Frame · gougedUPPER FUSELAGE FRAME 28 GOUGED 3 EACH PLACES BETWEEN STR 9L AND STR 7L COMPLIED WITH FEDEX EA 6-5310-105185 TITLE FUSELAGE - MINOR NICKS IN FRAME 28 STRINGER 7L TO 9L REPAIR. BLENDED 3 AREAS WITH A MAXIMUM DEPTH OF .063 ON THE INBOARD CORNER AS NOTED IN FIGURMar 21, 2007 · N669FE · Airbus A300F4605R · Fuselage Main, Frame
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