N682UP, cancelled Sep 22, 2011

Service difficulty reports · 527

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 = 'N682UP' AND deregistration_id = 'N682UP-2011-09-22'
  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 UPS07449766Pressure Panel · crackedINSPECTION TYPE:C ULTRASONIC INSP FOUND CRACK INDICATION AT BS 333 TO BS 334 BL 0 LEFT SIDE 1 INCH APPROX IN - LENGTH (CRACK LENGTH 0.68"). A REPAIR DOUBLER ADDED ON NOSE WHEEL WELL TOP PANEL UPPER SURFACE AT BTN BS 320 - BS 340 BL 0 IAW SRM 53-10-04 FIG 119 May 7, 2007 · N682UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS07449231Skin · crackedINSPECTION TYPE:C BS 460 STR 15R FOUND ONE EA FASTENER HOLE CRACKED AT SKIN BOND DOUBLER & STRAP. FX BS 460 STR 15R SKIN BOND DOUBLER & STRAP REPAIRED AS PER HX RS R53-11-35754 & UPS EO B747-5310-26195.Feb 19, 2007 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448221Battery Pack · inoperativeDURING ARRIVAL SERVICE CK, FOUND A/C EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK. REMOVED AND REPLACED MAIN ENTRY DOOR AFT LIGHT REF M/M CHAP 33-51-04 PG 205. OPS CK'D EMERGENCY LIGHT CKS OK.Oct 10, 2006 · N682UP · Boeing 747121 · Emergency LightingSDR UPS06448176Battery Pack · inoperativeEMERGENCY EXIT LIGHTS AT CREW SERVICE DOOR AND CABIN OVERHEAD INOP. CREW SVC DOOR SILL EMERG LT PWR PACK AND CABIN OVERHEAD CEILING EMERGENCY LT PWR PACK REPLACED. EMERGENCY LT SYSTEM, OPS CK NORMAL.Oct 3, 2006 · N682UP · Boeing 747121 · Emergency LightingSDR UPS06448034Floorbeam · damagedINSPECTION TYPE-C U/D RT BS 360 UPR DECK FLOORBEAM UPR CHORD AND FRAME ATTACHMENT AREA 1EA FASTENER HOLE FOUND OVAL AT UPR CHORD. U/D RT BS360 UPPER DECK FLOORBEAM UPPER CHORD REPAIRED AT LBL11 TO RT MOST OB AREA IAW SRM 53-10-07 FIG23.Sep 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448141Skin · corrodedINSPECTION TYPE:C M/D WING CTR SECTION UPPER SKIN CORROSION REVEAL AFTER PAINT STRIPPED AT ITEM 8,10,18A,18B,18D AND 19 PER BOEING ATTACHMENT. M/D WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35608 AND R57-14-35609 AND ENGINEERING FILE Sep 4, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06447870Skin · dentedINSPECTION TYPE-C FX UPPER FUSELAGE EXTERNAL SKIN SURFACE FOUND DENT MARK AT STA135 TO STA138 STR9L TO STR14L. DENT 0.060 INCH X 1 INCH X 1INCH. FX BS135 TO BS138 BETWEEN STR9L TO STR14L AREA SKIN FLUSH REPAIRED IAW SRM 53-30-03 FIG 4 SUBSEQUENT INSPECTIONS AAug 28, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448071Tear Strap · crackedINSPECTION TYPE:C M/D LT BS840 STR 10L SKIN AREA 1 FWD HOLE (JUST BELOW STR10L) FOUND CRACK AT TEAR STRAP APPROX 0.030" RUNNING FWD UPPER. M/D LT BS 840 STR 10L TEAR STRAP REPAIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448009Doubler · crackedM/D LT BS 840 TENSION TIE TO FRAME CONNECTION FOUND WEB DOUBLER 3 ADDITIONAL HOLES CRACKED, CRACK LENGTH 3/8". M/D LT BS 840 TENSION TIE TO FRAME ATTACHED DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 BETWEEN STR 9L TO STR 12L AREA.Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06447981Stringer · crackedLT BS 840 STR 11L STRINGER LWR HORIZ FLANGE CRACK AT AFT HOLE APPROX 0.030" RUNNING I/B. BS 830-850 STR11L REPAIRED AS PER SRM 53-10-03 FIG 4.Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS06447846Stringer · crackedMAIN E/E COMPT LT STRINGER S8L FOUND CRACKED AT STA 420 TO STA 440. CRACK LENGTH 2". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.Aug 23, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS06448146Skin · corrodedINSPECTION TYPE:C M/D CENTER SECTION UPPER SURFACE FOUND CORROSION AT BS 1180 RBL 98. CORROSION BLEND OUT 0.050" BY 2" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35603 AND UPS ENGINEERING FILE NUMBER 747-57-20115.Aug 21, 2006 · N682UP · Boeing 747121 · Wing, Plate/SkinSDR UPS06447982Hinge Fitting · crackedRHW NR 11 SPOILER PANEL ACTUATOR HINGE FITTING AFT LOWER FLANGE I/B RADIUS, FOUND 1/8" CRACK. STOP HOLE DRILLED AS PER UPS EO# B747-5740-0511-B ITEM 8.2 (6)Aug 21, 2006 · N682UP · Boeing 747121 · SpoilersSDR UPS06448051Intercostal · crackedINSPECTION TYPE:C WING CENTER SECTION BS 1230 RBL 11 INTERCOSTAL FOUND CRACK, CRACK LENGTH 3/8". WING CENTER SECTION BS 1230 RBL 11" INTERCOSTAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 20, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06448130Floorbeam · damagedINSPECTION TYPE:C RT BS 340 UPPER DECK FLOORBEAM UPPER TEE O/B HOLE FOUND OVAL AT FRAME WEB. U/D RT BS 340 FLOORBEAM UPPER TEE ATTACHED FRAME OVAL HOLE OVERSIZED TO 1/4" AND REPAIRED AS PER RS R53-12-35567 (REFER NRC6234 FOR WORKING DETAIL) CONTINUED INSPECTIAug 19, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448127Frame · damagedINSPECTION TYPE:C BS 340 RT FRAME WEB BETWEEN S11R AND S13A FASTENER HOLE IN POOR CONDITION AFTER SPLICE REMOVED. BS 340 RT FRAME POOR CONDITION HOLES AT THE EDGE OF THE FRAME CUTOUT AREA TRIMMED OFF AND FRAME REPAIRED AS PER RS R53-12-35567. CONTINUE INSPECAug 19, 2006 · N682UP · Boeing 747121 · Fuselage Main, FrameSDR UPS06447966Fitting · brokenR1 DOOR FWD LOWER STOP FTG BROKEN. R1 DOOR FWD LOWER STOP FTG REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Aug 18, 2006 · N682UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS06447842Tension Tie · crackedINSPECTION TYPE:C M/D BS 820 TO BS 840 TENSION TIE AT S10L ATT HORIZ SHEAR WEB FOUND CRACK, CRACK LENGHT 1". M/D BS 820 TO BS 840 TENSION TIE AT STR 10L ATTACH HORIZ SHEAR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 18, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447840Tension Tie · crackedINSPECTION TYPE:C M/D - BS 820-840 TENSION TIE AT S10R AT HORIZ SHEAR WEB FOUND CRACK CRACK LENGTH 3/4". BS820-840 TENSION TIE AT STR 10R AREA AT HORIZ SHEAR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 18, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06448166Skin · corrodedBS 1126-1130 LBL103-107 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.074" BY 4" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35586 AND UPS ENGINEERING FILE NUMBER 747-57-20114.Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448165Skin · corrodedINSPECTION TYPE:C M/D BS1140 LBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1" BY 3" EXCEED SRM LIMIT. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 ORIGINAL THICKNESS .0445" BLEND OUT DEPTH 0.028Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448151Web · corrodedINSPECTION TYPE:C M/D BS1160-1178 LBL11 WEB O/B FACE LWR AREA FOUND CORRODED. CORROSION BLEND OUT 0.020" X 3/4" BY 5" EXCEED SRM LIMIT. M/D BS 1140-1200 LBL11 WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06448143Skin · corrodedBS 1182-1186 RBL 67-70 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.047" BY 2.5" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35616 AND UPS ENGINEERING FILE NUMBER 747-57-20123.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448142Skin · corrodedINSPECTION TYPE:C M/D BS1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.182" BY 2" BY 6" EXCEED SRM LIMIT. BS 1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE SKIN REPAIRED AS PER RS R57-14-35607 AND UPS EO B747-5730-Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448140Skin · corrodedINSPECTION TYPE:C M/D BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043" BY 3" BY 4" EXCEED SRM LIMIT. BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35581 AND UPAug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448137Skin · corrodedBS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.079" BY 4" BY 6" EXCEED SRM LIMIT. BS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35590 AND UPS ENGINEERING FILE NUMBAug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448134Skin · corrodedBS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.063" BY 2" BY 2" EXCEED SRM LIMIT. BS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-2010Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448133Skin · corrodedBS 1080 LBL93 TO 96 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.073" BY 4" BY 4" EXCEED SRM LIMIT. BS 1080 LBL 93 TO 96 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35579 AND UPS ENGINEERING FILE NUMBER 747Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448126Skin · corrodedINSPECTION TYPE:C BS 1208-1210 LBL26-28 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.056" BY 3" BY 3" EXCEED SRM LIMIT. BS 1208-1210 LBL 26-28 WING CTR SECTION UPPER SURFACE CORROSION AREA REPAIRED AS PER RS R57-14-35594 FIG 4 AND UPAug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448117Panel · crackedFOUND L3 DOOR FWD CUTOUT LOWER REVEAL PANEL CRACK, CRACK LENGTH 0.375". REVEAL PANEL REPAIRED ASP ER RS R53-42-35595 AND UPS ENGINEERING FILE NUMBER 747-53-20336.Aug 17, 2006 · N682UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS06448114Skin · corrodedBS 1240 LBL49-53 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.161" BY 4" BY 7" EXCEED SRM LIMIT. BS 1240 LBL49-53 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-201Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06448113Skin · corrodedFOUND BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.120" BY 5" BY 5" EXCEED SRM LIMIT. BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35591 AND UPS ENGINEERING FILE NUMBER 747-57Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Plate/SkinSDR UPS06448111Skin · corrodedBS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.064" BY 4" BY 6" EXCEED SRM LIMIT. BS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35593 AND UPS ENGINEERING FILE NUMBER 7Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448110Skin · corrodedBS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.085" BY 2" BY 5" EXCEED SRM LIMIT. BS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35604 AND UPS ENGINEERING FILE NUMBERAug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448109Skin · corrodedBS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.045" BY 3" BY 4" EXCEED SRM LIMIT. BS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-20108Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448107Skin · corrodedBS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.034' BY 1.5" BY 10" EXCEED SRM LIMIT. BS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 7 AND UPS ENGINEERING FILE NUMBER 7Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448106Skin · corrodedBS 1185-1187 LBL31-33 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.056" BY 2" BY 3" EXCEED SRM LIMIT. BS 1185-1187 LBL31-33 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 3 AND UPS ENGINEERING FILE NUMBEAug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448104Skin · corrodedBS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.037" BY 3" BY 3" EXCEED SRM LIMIT. BS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35576 AND UPS ENGINEERING FILE NUMBER 747-57-2009Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448103Skin · corrodedBS 1193 LBL100 TO 103 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 2" BY 3" EXCEED SRM LIMIT. BS 1193 LBL100 TO 103 WING CTR SECTION UPPER SKIN REPAIRED AS PER RS R57-14-35597 AND UPS ENGINEERING FILE NUMBER 747-57-20104.Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448101Skin · corrodedINSPECTION TYPE:C M/D BS1235-1238 RBL57-59 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.071" BY 2" BY 4" EXCEED SRM LIMIT. M/D BS 1235-1238 RBL57-59 WING CTR SECTION UPPER CORRODED AREA REPAIRED AS PER RS R57-14-35587 AND UPS ENGINEERAug 17, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448085Fitting · delaminatedINSPECTION TYPE:C EMP LT BS2598 B/H FRAME SUPPORT UNDER STAB HINGE SUPPORT FTG FOUND 1 HOLE WITH DELAMINATION AT FWD BACK UP FTG. HOLE REPAIRED AS PER RS R53-83-35558 AND UPS ENGINEERING FILE NUMBER 747-55-20003.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS06448054Floorbeam · corrodedBS 1020 LBL 13-26 FLOORBEAM UPPER SURFACE FOUND CORROSION BLEND OUT 0.031" BY 1" BY 10". BS 1020 L11"-L33" FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06448003Intercostal · crackedBS 1220 LBL110 FLOOR INTERCOSTAL WEB CRACK AT LWR AREA, CRACK LENGTH 3/8". M/D BS 1220 LBL 110 FLOOR INTERCOSTAL WEB REPAIRED AT LOWER AREA AS PER SRM 51-40-02 FIG 1.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447976Floorbeam · corrodedBS 760 LBL83-90 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.050" BY 1.5" BY 7" EXCEED SRM LIMIT. BS760 LBL65 TO LT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447968Floorbeam · corrodedBS 980 LBL 60 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.068" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 980 LBL 20" TO LBL 70" FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447963Reveal · crackedR5 DOOR FWD CUTOUT UPPER REVEAL CRACKED, CRACK LENGTH 1/2". R5 DOOR FWD CUTOUT UPPER REVEAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447922Fitting · corrodedBS 842 LBL27-30 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.016" BY 1/2" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447921Fitting · corrodedM/D BS860 LBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.026" BY 1/2" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447920Fitting · corrodedM/D BS 978 RBL28 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.027" BY 0.5" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447919Fitting · corrodedM/D BS980 RBL83 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
Back to N682UP, cancelled Sep 22, 2011