N440UP

Service difficulty reports · 229

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 = 'N440UP' 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 IPXA11564379Frame · damagedINSPECTION TYPE:C1, UPPER LOBE LT FRAME, BS 1320, STR 15-16L, INBD FLANGE HAS 1 SCREW STRIKE DAMAGE, MARKED. REPAIRED IAW ER 11-01045, DATED 20, JAN 11.Jan 3, 2011 · N440UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA11564361Frame · gougedINSPECTION TYPE:C1, UPPER LOBE RT FRAME BS 480, 2" BELOW STR 15R, INBD FLANGE HAS IEA SCREW STRIKE DAMAGE. REPAIRED IAW EO B757-5310-41112-A/ATS ER 11-01049.Jan 3, 2011 · N440UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11564359Frame · gougedINSPECTION TYPE:C1, UPPER LOBE LT FRAME, BS 1280, STR 15L-16L FLANGE HAS 1 EA SCREW STRIKE DAMAGE. REPAIRED IAW EO B757-5310-41126-A.Jan 3, 2011 · N440UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11564341Panel · chafedINSPECTION TYPE:C1, PYLON PANEL 433FL IS CHAFED ON INNER SURFACE. R & R IAW EO B757-5450-22203-C.Jan 3, 2011 · N440UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA11564315Frame · damagedINSPECTION TYPE:C1, CUT-OUT AFT FRAME, BS 620 INBD FLANGE BETWEEN STR 8L-9L HAS 1EA SCREW STRIKE DAMAGE (MARKED). R & R STRAP IAW 51-40-02-0G, SOPM 20-44-04, AMM51-21-00 AND AMM51-21-10-7.Jan 3, 2011 · N440UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11564457Support · crackedINSPECTION TYPE:C1, TAIL COMPARTMENT, APU FIRE BOTTLE MOUNTING SUPPORT TRAY CRACKED AT SEVERAL HOLES. REPLACED IAW SRM & DWG.Jan 2, 2011 · N440UP · Boeing 75724APF · Fire Bottle, FixedSDR IPXA1564273Support · corrodedINSPECTION TYPE:C1, CORROSION AFT CARGO COMPARTMENT ON FLOOR TO SIDEWALL SUPPORT AT BS 1529-1620, LBL 17. R & R SIDE PANEL IAW SRM 51-40-02-0G.Jan 2, 2011 · N440UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA1564207Support · corrodedINSPECTION TYPE:C1, APU DOOR HSG CUTOUT FWD EDGE HAS CORROSION AT SEVERAL HOLES. REPLACED PARTS IAW SRM 51-40-02-0G AND DWG 148N3105.Jan 2, 2011 · N440UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA1564205Support · corrodedINSPECTION TYPE:C1, APU DOOR HSG CUT-OUT FWD EDGE HAS CORROSION AT SEVERAL HOLES. REPLACED PARTS IAW SRM 51-40-02-0G AND DWG 148N3105.Jan 2, 2011 · N440UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA1564204Strap · corrodedINSPECTION TYPE:C1, APU DOOR HSG CUT-OUT FWD EDGE HAS CORROSION AT SEVERAL HOLES. REPLACED PARTS IAW SRM 51-40-02-0G AND DWG 148N3105.Jan 2, 2011 · N440UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA1564201Angle · corrodedINSPECTION TYPE:C1, APU DOOR HSG CUT-OUT FWD EDGE HAS CORROSION SEVERAL HOLES. REPLACED PARTS IAW SRM 51-40-02-0G AND DWG 148N3105.Jan 2, 2011 · N440UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA1564200Angle · corrodedINSPECTION TYPE:C1, APU DOOR HOUSING CUT-OUT FWD EDGE HAS CORROSION AT SEVERAL HOLES. REPLACED PARTS IAW SRM 51-40-02-0G AND DWGS 148N3105.Jan 2, 2011 · N440UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA11564463Web · corrodedINSPECTION TYPE:C1, CORROSION ON FLIGHT COMPARTMENT FLOOR AT NUTPLATES FOR FO'S OTBD AFT SEAT TRACK (MARKED). REPAIRED IAW ER 11-01040.Dec 31, 2010 · N440UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA11564372Floor Skin · corrodedINSPECTION TYPE:C1, CORROSION ON FLIGHT COMPARTMENT AT CTR NUTPLATES FOR CAPTAINS OTBD AFT SEAT TRACK. REPAIRED IAW EO B757-5310-41108-A AND ATS ER 11-01038.Dec 31, 2010 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA11564370Floor Skin · corrodedINSPECTION TYPE:C1, CORROSION ON FLIGHT COMPARTMENT AT FWD END OF CAPTAINS INBD FWD SEAT TRACK. REPAIRED IAW EO B757-5310-41108-A AND ATS ER 11-01038.Dec 31, 2010 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA11564369Floor Skin · corrodedINSPECTION TYPE:C1, CORROSION ON FLIGHT COMPARTMENT FLOOR AT AFT END OF CAPTAINS INBD AFT SEAT TRACK. REPAIRED IAW EO B757-5310-41108-A AND ATS ER11-01038.Dec 31, 2010 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA11564367Web · corrodedINSPECTION TYPE:C1, CORROSION ON FLIGHT DECK COMPARTMENT FLOOR AT AFT END OF CAPTAINS OTBD AFT SEAT TRACK. REPAIRED IAW EO B757-5310-41108-A AND ATS ER11-01038.Dec 31, 2010 · N440UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR UPS09554658Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1280, STR 26L. TRIMMED THE DAMAGE AREA, DIM ARE: L=0.50" W=1.40" IAW EA 757-5362-27- A1821 PRELIMINARY 1 STEP1. HFEC ON CUTOUT IAW NTM 757-51-00-19 PT6, NO DEFECTS FOUND. ENLARGED THE CUTOUT BY 0.04 AS AN INSURANCE CUT FINAJan 31, 2009 · N440UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554731Wedge · dentedINSPECTION TYPE:C RT WING NR 9 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY, 9.5 INCHES FROM I/B END, 8.4 INCHES FROM T/E, .50 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554701Skin · dentedINSPECTION TYPE:C LT WING-35 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-15.25 INCH FROM INBD END, 5.6 INCH FROM T/E, 2.0 INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG203 FIG 201. CLEANED/PREP FORJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554700Wedge · dentedINSPECTION TYPE:C- LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 71.75 INCH FROM INBD END, 4.5 INCH FROM T/E, 1.8 INCH DIA. REMOVED TOPCOAT PREP FOR BOND OF DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203 FIG 201. CLEANEDJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554699Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 69.0 INCHES FROM OTBD END, 1.6 INCH FROM T/E, 1.7 INCH DIA. REMOVED TOPCOAT TO PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG 203 FIG 201. CLEANED/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554698Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENT INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E,(C) PAGE 203M FIG 201. CLEANED AND PREP FOR BOND IAW SRM 57-43-02/51-70-10 REPAIR NR 2, (C) PG 203 FIG 201. FABRJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554697Skin · dentedINSPECTION TYPE:C LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-16.25 INCH FROM OTBD END, 2.8 INCH FROM T/E 1.5 INCH DIAMETER. REMOVED TOPCOAT FOR BOND OF DOUBLER IAW SRM 57-43-02/57-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554696Skin · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-58.0 INCH FROM OTBD END, 4.8 INCH FROM T/E 1.5 INCH DIA. EVAL DENT DUE TO HAIL DAMAGE IAW SRM 57-43-03-A1 FIG 101 SHT 4. REMOVED SURF FINISH PREP FOR BOND IAW SRM 57-43Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554695Wedge · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 1 WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-36.5 INCHES FROM OTBD END,1.45 INCH FROM T/E .050 INCH DIA. REMOVED SUR FINISH AND PREP FOR BOND IAW SRM 57-43-02 REP 1 FIG 201/SRM 51-70 10 REP NR 2, E(C) PJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554694Wedge · dentedINSPECTION TYPE:C LT WING, NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 73 INCHES FROM OTBD END, 1.7 INCH FROM T/E. REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED AND PREPPED FOR Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554693Wedge · dentedINSPECTION TYPE:C LT WING NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 6.5 INCHES FROM OTBD END, 6.3 INCHES FROM T/E (MARKED AS GROUP 1). REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10, REP NR 2, E(C) PG 203, FIG 20Jan 29, 2009 · N440UP · Boeing 75724APF · Wing Main, Frame StructureSDR UPS09554691Wedge · dentedINSPECTION TYPE:C LT WING-NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-97.5 INCH FROM OTBD END, 2.1 INCH FROM T/E (MARKED GRP 3). REMOVED TOPCOAT TO PREPARE FOR BOND OF DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10 PRE NR 2,E, (C)PG203, FIG201. Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554673Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E EDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 57.1 INCH FROM INBD END, 8.3 INCH FROM T/E, .70 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201 SRM 51-70-1Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554672Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 19.9 INCH FROM OTBD END, 6.4 INCH FROM T/E, 1.8 INCH DIA (MARKED GROUP 3). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 2Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554665Wedge · dentedINSPECTION TYPE:C RT WING NR 10 SLAT T/E WEDGE HAS 2 (EA) DENTS OUT OF LIMITS DUE TO PROXIMITY 36.75 INCHES FROM T/E, 2.0 INCHES DIA (MARKED GROUP 2). REMOVED SURFACE FINISH FAB AND BONDED 1(EA) DOUBLER IAW SRM 57-43-02 & SRM 51-70-10-R2 FIG 201.Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554664Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 8.25A INCHES FROM T/E .60 DIA (MARKED GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-53-02 REPAIR 1 FIG 201 Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554663Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 36.5 INCHES FROM O/B END, 1.2 INCH FROM T/E, .65 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIGJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554662Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1(EA) DENT OUT OF LIMITS DUE TO PROXIMITY 100.26 INCHES FROM O/B END, 1.6 INCH FROM T/E, .50 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02, REPAIR 1 FIJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554661Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1EA DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 4.55 FROM T/E IN A 1.7 DIA (MARKED AS GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR 1 FIG 201 PJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554531Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1060-1100 RBL 25, EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1060-1100 RBL 25 PER SAMPLE IAW EO B757-5520-9692-F. MATERIAL P/N A402H-48X144. MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALJan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554479Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1020-1055 LBL 24-45 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1020-1055 LBL 24-45, PER SAMPLE IAW EO B757-5320-9692-F, MATERIAL A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALLJan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554474Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1020-1055 LBL 24-45 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1020-1055 LBL 24-45, PER SAMPLE IAW EO B757-5320-9692-F, MATERIAL A402H-48X144 MATERIAL BATCH 0001333 438.Jan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554684Structure · crackedINSPECTION TYPE:C NR 1 PYLON FWD AND AFT SLEEVE BOLT HOLE SHOW CRACK INDICATIONS. REMOVED BTH FWD/AFT SLEEVE BLT HOLES TO REMOVE CRACK, HOLE DIA AFTER REAM PER EO757-5410-17144 0.7815" HFEC IAW 757NTM51-00-16 PT6. NO CRACK FOUND (ROTO PROBE) REMOVED FWD/AFT Jan 22, 2009 · N440UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR UPS09554683Strut · crackedINSPECTION TYPE:C NR 2 PYLON STRUT TO UPPER LINK FITTING, 2 UPPER VERTICAL HOLES HAVE CRACK INDICATIONS (HFEC). HFEC UPPER LINK FITTING NDT51-00-16 PT6 IND CRACK IN HOLES. HFEC UP LNK STRUT HOLES IAW NDT51-00-17 PT6 IND NO CRACK. REMOVED 2 DISCREP HOLES TO Jan 22, 2009 · N440UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR UPS09554681Bulkhead · crackedINSPECTION TYPE:C NR 2 PYLON MID BULKHEAD TO STRUT TO UPPER LINK FITTING 2 HOLES HAVE CRACK INDICATIONS (HFEC) (LOCATIONS MARKED NO DOT). HFEC SOTO PROBE IAW NTM 757-51-00-16 PT6 AND 17 IND CRACK BOTH FWD AND AFT SLEEVE BOLT HOLE INBD AND OTBD LOC. NO CRACK Jan 22, 2009 · N440UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/FirewallSDR UPS09554660Fitting · damagedINSPECTION TYPE:C "04" ITEM, NR 2 PYLON 1EA COMMON TO THE OUTBOARD BATHTUB FITTING AND THE OUTBOARD LOWER CHORD WAS REAMED OVERSIZE (MECH REQ). REAMED UP ELONGATED HOLE COMMON TO BATHTUB FITTING AND O/B LWR CHORD UNTIL TRUE AND ROUND IAW EA 757-5450-27-A1829.Jan 17, 2009 · N440UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR UPS09554617Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1100-1200 RBL 35, EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PANEL STA 1100-1200 RBL 35 PER SAMPLE IAW EO B757-5320-9692-F. MATERIAL P/N A402H-48X144 BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALL ON A/C.Jan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554530Floor Panel · puncturedINSPECTION TYPE:C MAIN DECK FLOOR PUNCTURED AT STA 460, LBL 34. FABRICATED NEW MAIN DECK FLOOR PANEL STA 460, LBL 34 PER SAMPLE IAW EO B757-5320-9692-F. MATERIAL P/N A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALL ON A/C.Jan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554528Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 900-1200 LBL 24-45 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 900-1020 LBL 24-45, PER SAMPLE IAW EO B757-5320-9692-F MATERIAL P/N A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALJan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554526Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1100-1200, RBL 25 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1150-1200, RBL 25, PER SAMPLE IAW EO B757-5320-9696-F MATERIAL P/N A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALL Jan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554525Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 100-1200-BL 0 - LBL 24 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PANEL STA 1100-1200 BL 0 - LBL 24, PER SAMPLE IAW EO B757-5320-9694-F. MATERIAL P/N A402H. MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TJan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554524Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1020-1055 LBL 48-60 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1020-1055 LBL 48-60 PER SAMPLE IAW EO B757-5320-9692-F MATERIAL P/N A402H-48X144. MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INJan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554488Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1100-1200 LBL 48-60 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1100-1200 LBL 48-60, PER SAMPLE IAW B757-5320-9792-F. MATERIAL P/N A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTAJan 9, 2009 · N440UP · Boeing 75724APF · Fuselage Floor Panel
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