# Service difficulty reports: N682UP, cancelled Sep 22, 2011

A list on [N682UP, cancelled Sep 22, 2011](https://openairdocs.org/deregistered/N682UP-2011-09-22.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 11 · 527 reports

- [SDR UPS07449766](https://openairdocs.org/sdr/UPS07449766.md): Pressure Panel · cracked · May 7, 2007 · N682UP · Boeing 747121 · Fuselage Main, Bulkhead
  > INSPECTION 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
- [SDR UPS07449231](https://openairdocs.org/sdr/UPS07449231.md): Skin · cracked · Feb 19, 2007 · N682UP · Boeing 747121 · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR UPS06448221](https://openairdocs.org/sdr/UPS06448221.md): Battery Pack · inoperative · Oct 10, 2006 · N682UP · Boeing 747121 · Emergency Lighting
  > DURING 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.
- [SDR UPS06448176](https://openairdocs.org/sdr/UPS06448176.md): Battery Pack · inoperative · Oct 3, 2006 · N682UP · Boeing 747121 · Emergency Lighting
  > EMERGENCY 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.
- [SDR UPS06448034](https://openairdocs.org/sdr/UPS06448034.md): Floorbeam · damaged · Sep 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS06448141](https://openairdocs.org/sdr/UPS06448141.md): Skin · corroded · Sep 4, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > INSPECTION 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
- [SDR UPS06447870](https://openairdocs.org/sdr/UPS06447870.md): Skin · dented · Aug 28, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/Skin
  > INSPECTION 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 A
- [SDR UPS06448071](https://openairdocs.org/sdr/UPS06448071.md): Tear Strap · cracked · Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR UPS06448009](https://openairdocs.org/sdr/UPS06448009.md): Doubler · cracked · Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, Structure
  > M/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.
- [SDR UPS06447981](https://openairdocs.org/sdr/UPS06447981.md): Stringer · cracked · Aug 24, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/Stringer
  > LT 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.
- [SDR UPS06447846](https://openairdocs.org/sdr/UPS06447846.md): Stringer · cracked · Aug 23, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/Stringer
  > MAIN 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.
- [SDR UPS06448146](https://openairdocs.org/sdr/UPS06448146.md): Skin · corroded · Aug 21, 2006 · N682UP · Boeing 747121 · Wing, Plate/Skin
  > INSPECTION 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.
- [SDR UPS06447982](https://openairdocs.org/sdr/UPS06447982.md): Hinge Fitting · cracked · Aug 21, 2006 · N682UP · Boeing 747121 · Spoilers
  > RHW 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)
- [SDR UPS06448051](https://openairdocs.org/sdr/UPS06448051.md): Intercostal · cracked · Aug 20, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06448130](https://openairdocs.org/sdr/UPS06448130.md): Floorbeam · damaged · Aug 19, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
  > INSPECTION 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 INSPECTI
- [SDR UPS06448127](https://openairdocs.org/sdr/UPS06448127.md): Frame · damaged · Aug 19, 2006 · N682UP · Boeing 747121 · Fuselage Main, Frame
  > INSPECTION 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 INSPEC
- [SDR UPS06447966](https://openairdocs.org/sdr/UPS06447966.md): Fitting · broken · Aug 18, 2006 · N682UP · Boeing 747121 · Passenger/Crew Doors
  > R1 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.
- [SDR UPS06447842](https://openairdocs.org/sdr/UPS06447842.md): Tension Tie · cracked · Aug 18, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06447840](https://openairdocs.org/sdr/UPS06447840.md): Tension Tie · cracked · Aug 18, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06448166](https://openairdocs.org/sdr/UPS06448166.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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.
- [SDR UPS06448165](https://openairdocs.org/sdr/UPS06448165.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > INSPECTION 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 0.028
- [SDR UPS06448151](https://openairdocs.org/sdr/UPS06448151.md): Web · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS06448143](https://openairdocs.org/sdr/UPS06448143.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/Skin
  > BS 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.
- [SDR UPS06448142](https://openairdocs.org/sdr/UPS06448142.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > INSPECTION 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-
- [SDR UPS06448140](https://openairdocs.org/sdr/UPS06448140.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > INSPECTION 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 UP
- [SDR UPS06448137](https://openairdocs.org/sdr/UPS06448137.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 NUMB
- [SDR UPS06448134](https://openairdocs.org/sdr/UPS06448134.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 747-57-2010
- [SDR UPS06448133](https://openairdocs.org/sdr/UPS06448133.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 747
- [SDR UPS06448126](https://openairdocs.org/sdr/UPS06448126.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/Skin
  > INSPECTION 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 UP
- [SDR UPS06448117](https://openairdocs.org/sdr/UPS06448117.md): Panel · cracked · Aug 17, 2006 · N682UP · Boeing 747121 · Passenger/Crew Doors
  > FOUND 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.
- [SDR UPS06448114](https://openairdocs.org/sdr/UPS06448114.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/Skin
  > BS 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 747-57-201
- [SDR UPS06448113](https://openairdocs.org/sdr/UPS06448113.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Plate/Skin
  > FOUND 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 747-57
- [SDR UPS06448111](https://openairdocs.org/sdr/UPS06448111.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 7
- [SDR UPS06448110](https://openairdocs.org/sdr/UPS06448110.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 NUMBER
- [SDR UPS06448109](https://openairdocs.org/sdr/UPS06448109.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 747-57-20108
- [SDR UPS06448107](https://openairdocs.org/sdr/UPS06448107.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 7
- [SDR UPS06448106](https://openairdocs.org/sdr/UPS06448106.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 NUMBE
- [SDR UPS06448104](https://openairdocs.org/sdr/UPS06448104.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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 747-57-2009
- [SDR UPS06448103](https://openairdocs.org/sdr/UPS06448103.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > BS 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.
- [SDR UPS06448101](https://openairdocs.org/sdr/UPS06448101.md): Skin · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Wing, Center Box
  > INSPECTION 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 ENGINEER
- [SDR UPS06448085](https://openairdocs.org/sdr/UPS06448085.md): Fitting · delaminated · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS06448054](https://openairdocs.org/sdr/UPS06448054.md): Floorbeam · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
  > BS 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.
- [SDR UPS06448003](https://openairdocs.org/sdr/UPS06448003.md): Intercostal · cracked · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > BS 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.
- [SDR UPS06447976](https://openairdocs.org/sdr/UPS06447976.md): Floorbeam · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
  > BS 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.
- [SDR UPS06447968](https://openairdocs.org/sdr/UPS06447968.md): Floorbeam · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
  > BS 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.
- [SDR UPS06447963](https://openairdocs.org/sdr/UPS06447963.md): Reveal · cracked · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous Structure
  > R5 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.
- [SDR UPS06447922](https://openairdocs.org/sdr/UPS06447922.md): Fitting · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
  > BS 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.
- [SDR UPS06447921](https://openairdocs.org/sdr/UPS06447921.md): Fitting · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
  > M/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.
- [SDR UPS06447920](https://openairdocs.org/sdr/UPS06447920.md): Fitting · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
  > M/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.
- [SDR UPS06447919](https://openairdocs.org/sdr/UPS06447919.md): Fitting · corroded · Aug 17, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach Fittings
  > M/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.

Next page: https://openairdocs.org/deregistered/N682UP-2011-09-22/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 = 'N682UP' AND deregistration_id = 'N682UP-2011-09-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N682UP-2011-09-22/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.