# Service difficulty reports: N522UP, cancelled Jul 19, 2010

A list on [N522UP, cancelled Jul 19, 2010](https://openairdocs.org/deregistered/N522UP-2010-07-19.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 7 · 320 reports

- [SDR UPS08452007](https://openairdocs.org/sdr/UPS08452007.md): Coalescer Bag · odor · Apr 10, 2008 · N522UP · Boeing 747212B · Humidity Control System
  > CLIMBING THROUGH FL 220 A VIBRATION WAS FELT ACCOMPANIED BY A BURNING ODOR. SECURED NR 3 PACK AND VIBRATION AND ODOR WENT AWAY. ON NR 3 PACK REPLACED COALESCER BAG AND RETAINING RING MM 21-51-05 LP 935157/1. REPLACED COMP DISCH TEMP BULB MM 21-51-02 LP 93515
- [SDR UPS07450487](https://openairdocs.org/sdr/UPS07450487.md): Battery Pack · loose · Aug 23, 2007 · N522UP · Boeing 747200 · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY -EXIT- SIGN AT CREW SERVICE DOOR INOP. FOUND BATTERY PACK LOOSE. SECURED, OPERATIONAL NORMAL PER AMM 33-51-02.
- [SDR UPS07450267](https://openairdocs.org/sdr/UPS07450267.md): Support · cracked · Jul 14, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D BS 930-940 LBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 3/8". M/D BS 920-940 LBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450266](https://openairdocs.org/sdr/UPS07450266.md): Support · cracked · Jul 14, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D BS920-940 RBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 5/16". M/D BS 920-940 RBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450277](https://openairdocs.org/sdr/UPS07450277.md): Floorbeam · corroded · Jul 10, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C AFT CARGO COMPT CARGO FLOORBEAM UPPER TEE FOUND CORROSION AT STA 1920 CARGO NET ATT HOOK RBL4 TO LBL4. CORROSION BLEND OUT 0.045" BY 1.5" BY 2". AFT CARGO COMPT BS 1920 LBL 42 TO RBL 42 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SR
- [SDR UPS07450271](https://openairdocs.org/sdr/UPS07450271.md): Sill · cracked · Jul 9, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D L1 DOOR SILL FOUND CRACK, CRACK LENGTH 1" APPROX. M/D L1 DOOR SILL AT BS 434 TO BS 440 WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07450289](https://openairdocs.org/sdr/UPS07450289.md): Door Frame · cracked · Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED INNER CHORD AREA S23L - 26L FOUND TOTAL HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME,STRAP, INNER CHORD OR REVEAL) (CRACK LENGTH 0.050" & THROUGH THICKNESS) M/D BS2231 FRAME ATTACH REVEAL REPAIRED
- [SDR UPS07450288](https://openairdocs.org/sdr/UPS07450288.md): Frame · cracked · Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Main, Frame
  > INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED, RT BS 2231 FRAME INNER CHORD AREA S23R-26R FOUND TOTAL 4 HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME STRAP, INNER CHORD) (CRACK LENGTH 0.040",1/16", THROUGH THICKNESS). M/DECK BS 2231 FRAME ATTACH
- [SDR UPS07450263](https://openairdocs.org/sdr/UPS07450263.md): Shear Tie · corroded · Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C AFT OF BULK CARGO COMPT SKIN ATT ANGLE FOUND BULGE AT STA 2200 BTN S42L AND S37L. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS. AFT OF BULK CARGO COMPT BS 2200 STR 37L TO STR 42L FRAME ATTACH SUPPORT ANGLE REPLACED AND INSTALLED
- [SDR UPS07450249](https://openairdocs.org/sdr/UPS07450249.md): Sill · cracked · Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D RT BS434 TO BS 440 FLOOR SILL WEB CORROSION CRACK REVEALED, CRACK LENGTH 1" APPROX. M/D BS 434 TO BS 440 DOOR 1R SILL WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07450268](https://openairdocs.org/sdr/UPS07450268.md): Reveal · cracked · Jul 7, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FOUND CRACK AS MARKED, CRACK LENGTH 1/2" APPROX. M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FTG REPLACED AN INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450265](https://openairdocs.org/sdr/UPS07450265.md): Reveal · cracked · Jul 7, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG FOUND CRACK, CRACK LENGTH 3/4" APPROX. M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450319](https://openairdocs.org/sdr/UPS07450319.md): Skin · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NR 3R MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED. NR 3R MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5310-24674 APP N.
- [SDR UPS07450306](https://openairdocs.org/sdr/UPS07450306.md): Skin · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NR 3L MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/16" TO 5/8" RESP. NR 3L MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP M.
- [SDR UPS07450280](https://openairdocs.org/sdr/UPS07450280.md): Bear Strap · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NR 3R MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/8" TO 2". NR 3R MED CUTOUT AFT UPPER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX P & L.
- [SDR UPS07450273](https://openairdocs.org/sdr/UPS07450273.md): Frame · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Frame
  > INSPECTION TYPE:C M/D RT BS 2231 FRAME INNER CHORD S23R-25R FOUND 2 HOLES CRACK AT FRAME STRAP, CRACK LENGTH 1/16" AND 0.040". M/D BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BEN STR 22R TO STR26R AREA REPAIRED AS PER SRM 53-10-04 FIG 115. CONTINUE INSP RE
- [SDR UPS07450264](https://openairdocs.org/sdr/UPS07450264.md): Skin · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NR 3L MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE FOUND CRACKED, CRACK LENGTH 1/8" APPROX. NR 3L MED CUTOUT AFT UPPER CORNER AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP I AND O.
- [SDR UPS07450254](https://openairdocs.org/sdr/UPS07450254.md): Stringer Clip · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA 1760, CRACK LENGTH 5/16". AFT CARGO COMPT BS 1760 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450253](https://openairdocs.org/sdr/UPS07450253.md): Intercostal · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LT FUSELAGE SKIN AREA AT BS 340-350 STR 5A 1 FASTENER HOLE FOUND CRACKED AT INTERCOSTAL. (1ST LAYER FROM I/B) RUNNING DOWNWARD APP 0.030" IN LENGTH (REFER SKETCH FOR DETAIL). LT FUSELAGE SKIN BS 340-360 STR 5A ATTACHED INTERCOSTAL REPLACED A
- [SDR UPS07450250](https://openairdocs.org/sdr/UPS07450250.md): Frame · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Frame
  > INSPECTION TYPE:C M/D LT BS2231 FRAME INNER CHORD S24L-25L FOUND 1 HOLE CRACK AT FRAME STRAP RUNNING FWD APPROX 1/8". M/D BS2231 FRAME ATTACH INNER CHORD AND STRAP REPAIRED BTN STR22L TO 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSPECTION ARE REQ AS PE
- [SDR UPS07450248](https://openairdocs.org/sdr/UPS07450248.md): Intercostal · cracked · Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C NWW TOP PANEL LBL20 INTERCOSTAL FOUND CRACK AT 1 FASTENER LOCATION AT BS290 AS MARKED, CRACK LENGTH 1/2". NWW TOP PANEL AT BS 290 LBL20 INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.
- [SDR UPS07450318](https://openairdocs.org/sdr/UPS07450318.md): Stringer Splice · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C FWD CARGO COMPT S31R STRINGER SPLICE FOUND CRACKED AT STA738. CRACK LENGTH 1/4". FWD CARGO COMPT BS 738 STR 31R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.
- [SDR UPS07450317](https://openairdocs.org/sdr/UPS07450317.md): Stiffener · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Wing Miscellaneous Structure
  > INSPECTION TYPE:C RT W/G W/W STIFFENER APPEAR CORRODED AT STA1241 RBL 63. RT W/G W/W AT BS 1241 RBL63 VERTICAL STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-10 PG 9 AN 51-30-02.
- [SDR UPS07450308](https://openairdocs.org/sdr/UPS07450308.md): Stringer Clip · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C FWD CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA780, CRACK LENGTH 1/4". FWD CARGO COMPT BS 780 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 3 AND 51-30-02.
- [SDR UPS07450301](https://openairdocs.org/sdr/UPS07450301.md): Floorbeam · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C M/D BS2340 LBL40-59 FLOORBEAM UPPER CHORD FOUND SEVERAL AREAS OF CORROSION. CORROSION BLEND OUT 0.040" BY 1" BY 3" EXCEED SRM LIMIT. M/D BS 2340 LBL 25 TO LT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.
- [SDR UPS07450293](https://openairdocs.org/sdr/UPS07450293.md): Support · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Wing Main, Frame Structure
  > INSPECTION TYPE:C RT WING WS500 L/E MOST FWD INTERIOR LOWER SUPPORT CHORD BULGED AS MARK. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS EXCEED SRM LIMIT. RHW WS 492 TO WS 508 L/E MOST FWD INTERIOR LOWER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UPS07450290](https://openairdocs.org/sdr/UPS07450290.md): Skin · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822, CRACK LENGTH 0.030" AND 0.090"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822. CONTINUE INSPECTION ARE REQUIRED AS PER H
- [SDR UPS07450281](https://openairdocs.org/sdr/UPS07450281.md): Support Angle · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD CARGO COMPT STA 1000 BULKHEAD 1 SUPPORT ANGLE FOUND CRACKED AT LBL 100 WL 155, CRACK LENGTH 1/2". FWD CARGO COMPT BS 1000 BULKHEAD AT LBL 100 WL 155 SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450279](https://openairdocs.org/sdr/UPS07450279.md): Stiffener · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C RT W/G W/W STIFFENER CORROSION AT STA 1241 RBL 85, CORROSION BLEND OUT 0.105" BY 2" BY 4" EXCEED SRM 57-10-01 FIG 1 LIMITS. RT W/G W/W AT BS 1241 RBL 85" VERT STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450278](https://openairdocs.org/sdr/UPS07450278.md): Shear Tie · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Wing Main, Frame Structure
  > INSPECTION TYPE:C RT W/G REAR SPAR WS 375 UPPER FIXED PANEL SUPPORT APPEARED CORRODED. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS 2" BY 3/4" EXCEED SRM LIMIT. RT W/G REAR SPAR WS375 UPPER FIXED PANEL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.
- [SDR UPS07450276](https://openairdocs.org/sdr/UPS07450276.md): Floor Support · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C M/D STA2300-2320 LBL34 FLOOR SUPPORT FOUND SEVERAL CORROSION. CORROSION BLEND OUT 0.023" BY 1" BY 4" EXCEED SRM LIMIT. M/D BS 2300-2320 LBL34 FLOOR SUPPORT REPLACED AND INSTALED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450275](https://openairdocs.org/sdr/UPS07450275.md): Floorbeam · corroded · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C M/D BS 2360 LBL 55 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 1" BY 2" EXCEED SRM LIMIT. M/D BS 2360 LBL25 TO LT MOST O/B AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.
- [SDR UPS07450274](https://openairdocs.org/sdr/UPS07450274.md): Crease Beam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C RT FX CROWN BS980-1000 UPPER CREASE BEAM FWD RADIUS FOUND CRACK APPROX 1" LONG. FX CROWN BS 980-1000 RT UPPER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450272](https://openairdocs.org/sdr/UPS07450272.md): Floorbeam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C M/D BS 2300 LBL50 FLOORBEAMS WEB REAR SIDE STIFFENER FOUND CRACKED AS MARKED, CRACK LENGTH 3/8". M/D BS 2300 LBL50 FLOORBEAM WEB REAR SIDE STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450261](https://openairdocs.org/sdr/UPS07450261.md): Crease Beam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C RT FX CROWN BS960-980 LOWER CREASE BEAM FWD FLANGE FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450260](https://openairdocs.org/sdr/UPS07450260.md): Crease Beam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C FX CROWN BS 940-960 LOWER CREASE BEAM FWD FLANGE RADIUS FOUND CRACK APPROX 3/8" LONG. FX CROWN BS 940-960 LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450259](https://openairdocs.org/sdr/UPS07450259.md): Crease Beam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C LT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS960-980 LT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450258](https://openairdocs.org/sdr/UPS07450258.md): Crease Beam · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C RT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450257](https://openairdocs.org/sdr/UPS07450257.md): Stringer Clip · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA1680, CRACK LENGTH 3/8". AFT CARGO COMPT BS 1680 STR33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450255](https://openairdocs.org/sdr/UPS07450255.md): Panel Support · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO COMPT SLOPE PANEL LT SIDE UPPER SUPPORT FOUND CRACKED AT STA 1540, CRACK LENGTH 1/2". AFT CARGO COMPT BS 1530 TO BS 1550 LT SIDE SLOPE PANEL UPPER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.
- [SDR UPS07450252](https://openairdocs.org/sdr/UPS07450252.md): Stringer · cracked · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C FWD CARGO COMPT S30L STRINGER FOUND DAMAGED AT STA 550, CRACK LENGTH 7/16". FWD CARGO COMPT BS 550 STR 30L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 2 SHEET 4 TABLE 3. UPS MPI NR P109
- [SDR UPS07450251](https://openairdocs.org/sdr/UPS07450251.md): Door Frame · chafed · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Structure
  > INSPECTION TYPE:C APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FLANGE LWR SURFACE FOUND CHAFED MARKED. APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
- [SDR UPS07450245](https://openairdocs.org/sdr/UPS07450245.md): Stringer · deformed · Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C FWD CARGO COMPT S38L STRINGER FOUND DEFORM AT STA 485, FWD CARGO COMPT BS 484 TO BS 496 STR38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.
- [SDR UPS07450174](https://openairdocs.org/sdr/UPS07450174.md): Skin · chipped · Jul 5, 2007 · N522UP · Boeing 747200 · Engine Thrust Reverser
  > INSPECTION TYPE:C NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE CHIPPED AT 5 O`CLOCK POSITION. CRACK LENGTH.1875 INCH. NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE AT 5 O`CLOCK POS REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07450320](https://openairdocs.org/sdr/UPS07450320.md): Skin · cracked · Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C U/D FX SKIN AT BS340-350 S5-5A FOUND CRACKS AT 3 FASTENER HOLES, CRACK LENGTH 1/16, 1/2 AND 9/16". FX BS 340 TO 350 STR5L SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127807 REV A REPEAT I
- [SDR UPS07450315](https://openairdocs.org/sdr/UPS07450315.md): Skin · cracked · Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C U/D FX SKIN AT BS 340 S5-5A FOUND CRACK AT 1 FASTENER HOLE CRACK LENGTH 1/16". FX BS 340 BETWEEN STR 5R TO 5 AR SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127808 REV A REPEAT INSP IS REQ
- [SDR UPS07450270](https://openairdocs.org/sdr/UPS07450270.md): Panel · bulged · Jul 4, 2007 · N522UP · Boeing 747212B · Wing, Plate/Skin
  > INSPECTION TYPE:C LWS 888 L/E LOWER FIXED PANEL FWD BULGED AS MARKED. CORROSION BLEND OUT 0.040" BY 1" BY 2". LHW L/E WS888 LOWER FIXED PANEL FWD SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.
- [SDR UPS07450269](https://openairdocs.org/sdr/UPS07450269.md): Floorbeam · cracked · Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C M/D STA2280 LBL39 FLOORBEAMS WEB REAR SIDE FOUND SEVERAL CRACKS, CRACK LENGTH 1/4". M/D BS 2280 LBL 39 FLOORBEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS07450256](https://openairdocs.org/sdr/UPS07450256.md): Support · cracked · Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO COMPT DIVIDER SUPPORT HOOK AREA FOUND CRACKED AT STA 1920 LBL 4 TO RBL 4 FLOOR AREA, CRACK LENGTH 2". AFT CARGO COMPT DIVIDER SUPPORT AT BS 1920 LBL 42 TO RBL 42 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.
- [SDR UPS07450246](https://openairdocs.org/sdr/UPS07450246.md): Skin · dented · Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C EMP LT TAIL CONE SKIN FOUND DENT MARK AT STA 2725 BTN S0L AND S1L. EMP LT TAIL CONE SKIN AT BS2725 BTN STR 0 AND STR 1L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Next page: https://openairdocs.org/deregistered/N522UP-2010-07-19/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 = 'N522UP' AND deregistration_id = 'N522UP-2010-07-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N522UP-2010-07-19/reports

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