# Service difficulty reports: N933UP, cancelled Aug 24, 2007

A list on [N933UP, cancelled Aug 24, 2007](https://openairdocs.org/deregistered/N933UP-2007-08-24.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 4 · 157 reports

- [SDR UPS02238717](https://openairdocs.org/sdr/UPS02238717.md): Battery · discharged · Jul 1, 2002 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A EXIT LIGHT ABOVE COCKPIT ENTRANCE DOOR DOES NOT TEST. CABIN DOOR ENTRANCE LIGHT CHECKS OK BUT CHARGE STAT US IS IN-DOUBT. R/R EMERGENCY EXIT LIGHT BATTERIES IN COCKPIT ENTRANCE DOOR AND CABIN DOOR, REF UPS 727 M/M CHAP 33-50-67 OPS CHECKE
- [SDR UPS02238567](https://openairdocs.org/sdr/UPS02238567.md): Battery · discharged · Jun 7, 2002 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS GOOD.
- [SDR UPS02237797](https://openairdocs.org/sdr/UPS02237797.md): Angle · bulged · Feb 7, 2002 · N933UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C LT AFT NOSE W/W DOOR CUTOUT HAS BULGE FASTENERS PULLING OFF BS 320 TO BS 350. REPLACED LEFT LOWER CHORD ANGLE AT NWW AREA IAW B727 SRM 51-30-2.
- [SDR UPS02237796](https://openairdocs.org/sdr/UPS02237796.md): Skin · cracked · Feb 7, 2002 · N933UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C LT FUSELAGE SKIN HAS CRACK STARTING AT FASTENER CUT OUT BS 254 STR 10L CRACK DOES NOT NEED STOP DRILL IT RUNS FROM FASTENER HOLE TO EDGE OF SKIN, INSTALLED DOUBLER REPAIR AT LT FUSELAGE. BS 254 STR 10L AS PER B727 SRM 53-30-3 MATERIAL USE
- [SDR UPS02237795](https://openairdocs.org/sdr/UPS02237795.md): Skin · bulged · Feb 7, 2002 · N933UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C UPPER FUSELAGE SKIN HAS BULGE AT BUTT JOINT BS 521 STR 3L - 4R.
- [SDR UPS02237794](https://openairdocs.org/sdr/UPS02237794.md): Skin · canning · Feb 7, 2002 · N933UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C RT FWD FUSELAGE SKIN HAS OIL CAN, PREVIOUSLY REWORKED BS 340 STR 19R.
- [SDR UPS02237493](https://openairdocs.org/sdr/UPS02237493.md): Battery · discharged · Jan 22, 2002 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:IN EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKS NORMAL.
- [SDR UPS01237360](https://openairdocs.org/sdr/UPS01237360.md): Light · inoperative · Dec 10, 2001 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0067, S/N OFF 42-11, S/N O N 27025. OPS CHECKS GOOD
- [SDR UPS01235463](https://openairdocs.org/sdr/UPS01235463.md): Windshield · failed · Mar 28, 2001 · N933UP · Boeing 72725C · Flight Compartment Windows
  > FIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOOD
- [SDR UPS01234968](https://openairdocs.org/sdr/UPS01234968.md): Fire Loop · inoperative · Feb 13, 2001 · N933UP · Boeing 72725C · Fire Detection
  > INSPECTION TYPE:IN ENG NR 3 A-LOOP WILL NOT TEST. *S/D* FOUND CONNECTOR D354J CONTAMINATED WITH DIRT AND MOISTURE. CLEANED SAME THOROUGHLY. TESTED NORMAL. M209166 CLEARED.
- [SDR UPS00234506](https://openairdocs.org/sdr/UPS00234506.md): Structure · cracked · Nov 22, 2000 · N933UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:PRE NR 4 LEADING EDGE SLAT CRACKED. AWAITING LOG PAGE ENTRY.
- [SDR UPS00233587](https://openairdocs.org/sdr/UPS00233587.md): Flap Track · corroded · Aug 16, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B HAVE LIGHT SURFACE RUST (CORROSION C57-581-06.00-03). REMOVED CORROSION FROM NR 1 FLAP TRACK FWD ATTACH LUG FACES I/B AND O/B AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20235.
- [SDR UPS00233586](https://openairdocs.org/sdr/UPS00233586.md): Flap Track · corroded · Aug 16, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK AFT CENTER MOUNT HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF NR 20232.
- [SDR UPS00233585](https://openairdocs.org/sdr/UPS00233585.md): Flap Track · corroded · Aug 16, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION (SDN C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE. REMOVED CORROSION ON NR 7 FLAP TRACK FWD ATTACH POINT I/B FLANGE AROUND BUSHING HOLE AND REPAIRED PER FAA FORM 8130-3 SYSTEM TRACKING REF
- [SDR UPS00233609](https://openairdocs.org/sdr/UPS00233609.md): Web · corroded · Jul 31, 2000 · N933UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI, CORROSION ON UPPER SURFACE OF SHEAR WEB AT BS 640, WL 208 LBL 63. SHEAR WEB REPLACED AT STA 630 - 660, LBL 45-LBL 62, WL 208 PER ER NR 00-0952.
- [SDR UPS00233568](https://openairdocs.org/sdr/UPS00233568.md): Fitting · cracked · Jul 29, 2000 · N933UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI, STRINGER FITTING IS CRACKED AT BS 365 STR 26L. REMOVED AND REPLACED STRINGER FITTING.
- [SDR UPS00233588](https://openairdocs.org/sdr/UPS00233588.md): Fitting · cracked · Jul 27, 2000 · N933UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:SI, NR 1 K-FLAP O/B ATTACH LUG FITTING ON K-FLAP UPPER O/B SIDE IS CRACKED. REMOVED AND INSTALLED NEW K-FLAP ASSY PER MM 27-81-01.
- [SDR UPS00233540](https://openairdocs.org/sdr/UPS00233540.md): Skin · corroded · Jul 27, 2000 · N933UP · Boeing 72725C · Rudder, Spar/Rib
  > INSPECTION TYPE:C, CORROSION ON LWR RUDDER RT SKIN AT STA 120.6 IN BELOW FRONT SPAR. REPAIRED PER SRM 55-20-3 PG 1 STEP 3 & 4 AND SRM 51-40-5 PG 20 & 22 STEP 13 A-I.
- [SDR UPS00233612](https://openairdocs.org/sdr/UPS00233612.md): Stringer · cracked · Jul 26, 2000 · N933UP · Boeing 72725C · Wing, Longeron/Stringer
  > INSPECTION TYPE:SI, RIGHT WING UPPER STR 17 OUTSIDE OF RIB AT WS 304 IS CRACKED. REMOVED CRACK STRINGER SECTION. FABRICATED AND INSTALLED NEW SECTION, ALL WORK DONE IAW SRM 57-10-4, 51-20-1, 51-30-2.
- [SDR UPS00233611](https://openairdocs.org/sdr/UPS00233611.md): Flap Track · corroded · Jul 26, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, NR 5 FLAP TRACK IS RUSTED AT MAIN LANDING GEAR DOOR FWD FITTING ATTACH BOLTS. REMOVED AND REPLACED FLAP TRACK PER TC 57-581-04-4D.
- [SDR UPS00233558](https://openairdocs.org/sdr/UPS00233558.md): Carriage · corroded · Jul 26, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION (SDN C57-581-04.00-04) IN BORE OF SPINDLE FOR NR 6 FLAP CARRIAGE. REMOVED AND REPLACED NR 6 FLAP CARRIAGE PER MM 25-51-03.
- [SDR UPS00233513](https://openairdocs.org/sdr/UPS00233513.md): Mount · corroded · Jul 26, 2000 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AFT ATTACH MOUNT BLOCK OUT OF LIMITS IAW SRM 51-30-2. REMOVED AND REPLACED MOUNT BLOCK IAW SRM 51-30-5.
- [SDR UPS00233512](https://openairdocs.org/sdr/UPS00233512.md): Fitting · corroded · Jul 26, 2000 · N933UP · Boeing 72725C · Wing, Attach Fittings
  > INSPECTION TYPE:SI, NR 6 FLAP TRACK SPOILER BEAM MOUNT FITTINGS CORRODED OUT OF LIMITS IAW SRM 51-30-2 ON RT WING. FOUND WHILE WORKING NRC 178771. REMOVED CORRODED MOUNT FITTINGS AND REPLACED WITH NEW PART IAW SRM 51-30-2.
- [SDR UPS00233557](https://openairdocs.org/sdr/UPS00233557.md): Fitting · corroded · Jul 25, 2000 · N933UP · Boeing 72725C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:SI, MAIN DECK FLOOR WEB FITTING CORRODED (C53-224-01.00-03) BETWEEN LEFT CREASE BEAM AND DITCHING PAN, FWD OF BS 1183 BULKHEAD BS 1180 LBL 65, WL 208. REMOVED AND REPLACED FLOOR WEB FITTING IAW SRM 51-30-05, 53-10-01, 51-10-06.
- [SDR UPS00233556](https://openairdocs.org/sdr/UPS00233556.md): Floorbeam · corroded · Jul 25, 2000 · N933UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) FWD CARGO BAY BS 660 FLOORBEAM FWD SIDE UPPER FLANGE LOWER SURFACE AT LBL 45 TO LBL 50. REMOVED CORROSION IN DESCREPANT AREA AT LBL 45 IN A 2.4 X 1.0 X.030 ORIGINAL THICKNESS.240 OUT OF LIMITS. REMOVED UPPER
- [SDR UPS00233555](https://openairdocs.org/sdr/UPS00233555.md): Floorbeam · corroded · Jul 25, 2000 · N933UP · Boeing 72725C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY STA 540 FLOORBEAM FWD SIDE, UPPER FLANGE, LWR SURFACE AT LBL 45. REMOVED CORROSION ON UPPER CHORD LOWER FLANGE IN AN AREA OF 1.0 X 2.0. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 5. CUT OFF T
- [SDR UPS00233610](https://openairdocs.org/sdr/UPS00233610.md): Drum · corroded · Jul 23, 2000 · N933UP · Boeing 72725C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:SI, RT MLG MANUAL EXTENSION CABLE DRUM IS CORRODED. REMOVED AND REPLACED PER MM 32-34-01.
- [SDR UPS99228760](https://openairdocs.org/sdr/UPS99228760.md): Spar Chord · corroded · Feb 17, 1999 · N933UP · Boeing 72725C · Wing Spar
  > INSPECTION TYPE-C,CORROSION (C57-581-03.00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.
- [SDR UPS99228742](https://openairdocs.org/sdr/UPS99228742.md): Chord · corrosion · Feb 17, 1999 · N933UP · Boeing 72725C · Wing Spar
  > INSPECTION TYPE:C CORROSION (C57-581-03-00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIRED IAW ERO 99-5030.
- [SDR UPS99228633](https://openairdocs.org/sdr/UPS99228633.md): Seat Track · cracked · Feb 2, 1999 · N933UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C WHILE ACCESSING OVERWING FRAMES FOUND SEAT TRACK AT STA 760 RBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED SEAT TRACK FROM BS 760 TO BS 848 PER 727 SRM 53-10-5 AND 51-30-2.
- [SDR UPS99228558](https://openairdocs.org/sdr/UPS99228558.md): Skin · corroded · Jan 27, 1999 · N933UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLAP PER MM 27-81-01 AND ADJUST/TEST PER 727 MM 27-81-00.
- [SDR UPS99228530](https://openairdocs.org/sdr/UPS99228530.md): Skin · corroded · Jan 25, 1999 · N933UP · Boeing 72725C · Elevator, Plate/Skin
  > INSPECTION TYPE-C,CORROSION RT ELEVATOR AROUND BASE OF O/B STATIC WICK. REPLACED SKIN PER SRM 51-30-2 AND SRM 55-20-3.
- [SDR UPS99228559](https://openairdocs.org/sdr/UPS99228559.md): Foreflap · corroded · Jan 15, 1999 · N933UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE-C, LEFT WING O/B FOREFLAP HAS.25 X 3.5 AREA OF DELAMINATION. TAP TESTED, FOUND ADDITIONAL DELAMINATION. FOUND CORRSION ON SPAR. REPLACED O/B FOREFLAP.
- [SDR UPS99228674](https://openairdocs.org/sdr/UPS99228674.md): S Duct · cracked · Jan 14, 1999 · N933UP · Boeing 72725C · Nacelle/Pylon Structure
  > INSPECTION TYPE:C NR 2 ENGINE S DUCT HAS 5 INCH CRACK IN THE CENTER SECTION 4 RIBS FWD OF THE PRODUCTION BREAK, LT SIDE APPRX 8:00 POSITION. REMOVED DAMAGED AREA AND PERFORMED A FILLER AND DOUBLER REPAIR PER SRM 54-10-3, SRM 51-40-2 AND MM 51-20-151.
- [SDR UPS99228538](https://openairdocs.org/sdr/UPS99228538.md): Skin · corroded · Jan 13, 1999 · N933UP · Boeing 72725C · Elevator, Plate/Skin
  > INSPECTION TYPE-C, CORROSION (C55-300-10.00-01) ON LT ELEVATOR AROUND I/B STATIC WICK BASE. REMOVED CORROSION OUT OF LIMITS, REPLACED SKIN PANEL. ALL WORK DONE PER SRM 55-20-1, 55-20-2 AND MM 23-61-00.
- [SDR UPS98226858](https://openairdocs.org/sdr/UPS98226858.md): Control Valve · failed · Jun 10, 1998 · N933UP · Boeing 72725C · Air Distribution System
  > INSPECTION TYPE N/A, LEFT PACK TRIPPED OFF LIGHT ON LANDING ROLLOUT. LEFT PACK SWITCH DID NOT TURN OFF, WHITE SMOKE ENTERED COCKPIT. LOST CONTROL OF PACK EVEN WITH SWITCH OFF. LEFT PACK VLV STUCK OPEN, CYCLED VLV TO CLOSED POSITION AND ITEM DEFERRED PER MEL
- [SDR UPS98226177](https://openairdocs.org/sdr/UPS98226177.md): Battery Pack · discharged · Mar 25, 1998 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, COCKPIT EMERGENCY EXIT LIGHT INOP. FOUND BOTH BATTERIES TO BE DEAD AND OUT OF DATE. REMOVED AND REPLACED TWO BATTERIES PER MM33-50-10. SYSTEM GROUND CHECKS GOOD.
- [SDR UPS98226176](https://openairdocs.org/sdr/UPS98226176.md): Light · inoperative · Mar 25, 1998 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY.
- [SDR UPS97225318](https://openairdocs.org/sdr/UPS97225318.md): Light · inoperative · Dec 1, 1997 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY LIGHT WOULD NOT TEST, BATTERIES OK. REPLACED LIGHT ASSY.
- [SDR UPS97225089](https://openairdocs.org/sdr/UPS97225089.md): Line · cracked · Nov 14, 1997 · N933UP · Boeing 72725C · Hydraulic System, Main
  > INSPECTION TYPE-N/A, ON GEAR RETRACTION RIGHT MAIN GEAR DID NOT RETRACT, A HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. A PRESSURE WAS ZERO AND QUANTITY WAS ZERO. EXTENDED GEAR MANUALLY IN ACCORDANCE WITH AOM. FOUND RT MLG HYDRAULIC DOOR UP LINE CRACKE
- [SDR UPS97224364](https://openairdocs.org/sdr/UPS97224364.md): Skin · delaminated · Sep 4, 1997 · N933UP · Boeing 72725C · Spoilers
  > INSPECTION TYPE-C, NR 7 SPOILER HAS A 4 BY 5 AREA OF DELAMINATION ON LOWER SURFACE O/B FWD CORNER. REPAIRED DELAMINATION IAW SRM 57-50-06 FIG 5.
- [SDR UPS97224403](https://openairdocs.org/sdr/UPS97224403.md): Seat Track · cracked · Sep 3, 1997 · N933UP · Boeing 72725C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C SEAT TRACK CRACKED AT BS 660 LBL 65. REMOVED AND REPLACED SEAT TRACK AT BS 660 LBL 65.
- [SDR UPS97224365](https://openairdocs.org/sdr/UPS97224365.md): Skin · corroded · Sep 3, 1997 · N933UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE-C, NR 4 K-FLAP O/B BONDING JUMPER HOLE HAS CORROSION AROUND OLD BONDING JUMPER LOCATION. CORROSION REWORK OUT OF LIMITS IAW UPS EO B727-5740-3980 (SRM ADDENDOM) REPAIRED NR 4 K-FLAP AT OLD BONDING JUMPER LOCATION IAW SRM 57-50-3.
- [SDR UPS97224367](https://openairdocs.org/sdr/UPS97224367.md): Frame · cracked · Sep 2, 1997 · N933UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND LT 930 FRAME CRACKED AT WL 228. REPAIRED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.
- [SDR UPS97224366](https://openairdocs.org/sdr/UPS97224366.md): Rib · cracked · Sep 2, 1997 · N933UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE-C, NR 5 K-FLAP I/B LOWER BONDING JUMPER ON K-FLAP HAS CRACK EMANATING FROM HOLE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON NR 5 K-FLAP I/B RIB AT BONDING JUMPER PER SRM 57-50-3.
- [SDR UPS97224368](https://openairdocs.org/sdr/UPS97224368.md): Frame · cracked · Sep 1, 1997 · N933UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE-C, WHILE WORKING EO B727-5310-5596A (940 FRAME INSP) FOUND RT 930 FRAME CRACKED AT WL 228. REPAIRED CRACKED FRAME IAW EO B727-5310-2580 AND BOEING DRAWING 65C10084.
- [SDR UPS97224405](https://openairdocs.org/sdr/UPS97224405.md): Fitting · corroded · Aug 29, 1997 · N933UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON UNDERSIDE OF HORIZONTAL FLANGE OF BS 740 BODY FITTING LBL 65 WL 207. BODY FITTING REPAIRED IN ACCORDANCE WITH BFG ER 97-2479 AND UPS ENGINEERING FILE DOCUMENT 727-53-1959.
- [SDR UPS97222567](https://openairdocs.org/sdr/UPS97222567.md): Battery · discharged · Apr 11, 1997 · N933UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE P/F, EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AT COCKPIT DOOR. REPLACED BATTERIES ON EMERGENCY BAT PACK LIGHT (S/N 39810).
- [SDR UPS96205974](https://openairdocs.org/sdr/UPS96205974.md): Support Fitting · misdrilled · Apr 12, 1996 · N933UP · Boeing 72725C · Fuselage, Landing Gear Attach Fittings
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. REMOVED DAMAGED AREA AND REPAIRED PER EO 727-53-1754.
- [SDR UPS96205973](https://openairdocs.org/sdr/UPS96205973.md): Bullnose · corroded · Apr 11, 1996 · N933UP · Boeing 72725C · Leading Edge Devices
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW MM 27-81-0 AND OHM 57-51-01.

Next page: https://openairdocs.org/deregistered/N933UP-2007-08-24/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 = 'N933UP' AND deregistration_id = 'N933UP-2007-08-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N933UP-2007-08-24/reports

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