# Service difficulty reports: N934UP, cancelled May 10, 2007

A list on [N934UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N934UP-2007-05-10.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 2 · 60 reports

- [SDR UPS03240694](https://openairdocs.org/sdr/UPS03240694.md): Light · intermittent · May 14, 2003 · N934UP · Boeing 72721C · Emergency Lighting
  > MAIN ENTRY DOOR EMERG LT INTERMITTENT. R/R LT ASSY & BATTERIES. OPS CK OK IAW MM 33-50-67. LT ASSY P/N ON/OFF 10-0067-9/10-0067-7. S/N ON/OFF S106/7432.
- [SDR UPS03240693](https://openairdocs.org/sdr/UPS03240693.md): Battery · inoperative · May 14, 2003 · N934UP · Boeing 72721C · Emergency Lighting
  > COCKPIT DOOR EMERG LT INOPERATIVE. R/R BATTERIES P/N S106. IAW MM 3307. OPS CK OKAY.
- [SDR UPS03240053](https://openairdocs.org/sdr/UPS03240053.md): Panel · cracked · Jan 14, 2003 · N934UP · Boeing 72721C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL STA 245 LT SIDE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS03240055](https://openairdocs.org/sdr/UPS03240055.md): Spar · cracked · Jan 10, 2003 · N934UP · Boeing 72721C · Elevator, Spar/Rib
  > INSPECTION TYPE: C, DURING REPLACEMENT OF RT O/B RIB FOR ELEVATOR STA 209.5 LWR REAR SPAR FOUND TO BE CRACKED BETWEEN TWO FASTENERS AT O/B EDGE OF SPAR. REPAIRED IAW SRM 55-10-5 FIG 1.
- [SDR UPS03240050](https://openairdocs.org/sdr/UPS03240050.md): Bracket · cracked · Jan 8, 2003 · N934UP · Boeing 72721C · Elevator Control System
  > INSPECTION TYPE:C ON REMOVAL OF L/H ELEVATOR PCU BRACKET ON FRONT SPAR OF ELEVATOR FOU ND TO BE CRACKED POSITION SENSOR BRACKET ON L/H ELEV. FRONT SPAR REPLACED IAW MM 27-3 0-01 PG 410 STEP 4J
- [SDR UPS03240057](https://openairdocs.org/sdr/UPS03240057.md): Door · cracked · Jan 7, 2003 · N934UP · Boeing 72721C · Landing Gear Doors
  > INSPECTION TYPE:C WING LANDING GEAR DOOR R/H SIDE CRACK FOUND ON INSIDE OF DOOR REAR S PAR OF DOOR 19TH UP FROM BOTTOM OF DOOR CRACK IS ALONG BETWEEN 2 RIV ET HOLES REPAIR CARRIED OUT IAW SRM 51-40-2
- [SDR UPS03240056](https://openairdocs.org/sdr/UPS03240056.md): Fitting · cracked · Jan 7, 2003 · N934UP · Boeing 72721C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, CRACK INDICATION IN ONE HOLE BS 870 LT HOLE LOCATED 2ND FASTENER ROW FROM FWD EDGE OF FITTING TOP FASTENER HOLE OF LWR FITTING. REPAIRED IAW UPS EO B727-5310-3057-H.
- [SDR UPS03240049](https://openairdocs.org/sdr/UPS03240049.md): Bracket · broken · Jan 7, 2003 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C FLAT BRACKET BROKEN ON FUSELAGE SKIN AT BS 740 AT INTERSECTION WITH STR. 17R NEW PLATE FABRICATED IAW SRM 51-20-01 FIG 7 INSTALLED IAW SRM 51-30-02
- [SDR UPS03240066](https://openairdocs.org/sdr/UPS03240066.md): Elevator · cracked · Jan 6, 2003 · N934UP · Boeing 72721C · Elevator Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON LH ELEVATOR REAR SPAR @ 2 ND HINGE FROM O/B @ TOP I /B CORNER DUE TO UNAVAILABILITY OF REAR SPAR REPLACEMENT KIT. REPLACED L/H ELE VATOR IAW MM 27-30-01
- [SDR UPS03240065](https://openairdocs.org/sdr/UPS03240065.md): Fitting · cracked · Jan 6, 2003 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK INDICATION IN 2 HOLES BS 950 L/H HOLES LOCATED ON ROWS 2ND FRO M FWD EDGE OF FITTING AND 2ND HOLES FROM BOTTOM OF SPLICE PLATE JUST BELOW STR. 6 L/H BS 950 BULKHEAD FITTING REPLACED IAW EO B727-5310-3012 & DRAWING 65C18332 AND 2MI
- [SDR UPS03240048](https://openairdocs.org/sdr/UPS03240048.md): Skin · corroded · Jan 6, 2003 · N934UP · Boeing 72721C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, POPPED RIVET HEAD AT BS 1180 STR 7L DUE TO CORROSION. ALSO FURTHER SIGNS OF CORROSION ON STR 7L BETWEEN 1180 & 1150. LFEC INSP PERFORMED AT 1180 STR 7L, 10-15 PERCENT MATERIAL LOSS EVIDENT. CORRODED SKIN REMOVED APPROX 10 INCHES X 5 INCH
- [SDR UPS03240064](https://openairdocs.org/sdr/UPS03240064.md): Frame · cracked · Jan 4, 2003 · N934UP · Boeing 72721C · Horizontal Stabilizer, Spar/Rib
  > INSPECTION TYPE: C, SUSPECT CRACK ON LT HORIZONTAL STAB UPPER FRAME JUST I/B OF ELEVATOR RIB STA 173.21. REPAIR CARRIED OUT IAW SMRO EO 2003-001-004 UPS ENGINEERING FILE 727-55-20029.
- [SDR UPS01236766](https://openairdocs.org/sdr/UPS01236766.md): Light · defective · Aug 30, 2001 · N934UP · Boeing 72721C · Emergency Lighting
  > INSPECTION TYPE:PFLT EXIT LIGHTS STAY ON IN ARMED POSITION. REPLACED LIGHT ASSEMBLY
- [SDR UPS01236257](https://openairdocs.org/sdr/UPS01236257.md): Frame · cracked · Jun 28, 2001 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK INDICATION AT FRAME, FUSELAGE BS913.5 RIGHT SIDE. CRACK CONFIRMED BY NDT INSP. PART 6 51-00-00 STOP DRILL CRACK AT FRAME AT BS 913.5 B727-51-10-01 INSTALLED KIT REPAIR AS PER EO B727- 5310-1896-B APPENDIX C AT FRAM FUSELAGE BS 913
- [SDR UPS01236261](https://openairdocs.org/sdr/UPS01236261.md): Bulkhead · cracked · Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C, RT WHEEL WELL FWD LOWER FRAME SHOWS CRACK DAMAGE AT BS 870 RBL 4.5. REMOVED FASTENERS AT DAMAGED AREA SRM 51-30-2, CUTOUT WEB DAMAGED AREA APPROX 1 X 1.5 INCH SRM 51-40-2 AT BS 870 RBL 4.5 HFEC INSP CUT OUT IAW M/M 51-00-00 PART 6 FIG 4. I
- [SDR UPS01236260](https://openairdocs.org/sdr/UPS01236260.md): Bulkhead · cracked · Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C RIGHT WHEEL WELL STA 870 BULKHEAD CRACK AT APU VALVE CUT OUT RBL4.5 STOP DRILL CRACK ON RH W/W STA 870 AT APU VALVE CUT OUT RBL45 STOP DRILL 1/4" SIVE AND NDT INSPECTION ACCOMPISHED HFEC AS PER PART6-51- 00-00 FIG4 INSTALL 3 DOUBLER REPA
- [SDR UPS01236259](https://openairdocs.org/sdr/UPS01236259.md): Frame · cracked · Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, Frame
  > INSPECTION TYPE:C, LEFT WW FRAME 930 HAS PREVIOUS REPAIR WITH STOP HOLE, BUT IS CONTINUING UPWARDS AFTER STOP HOLE FRAME BELOW FLOOR BS 930. PERFORMED HFEC INSP ON I/B FLANGE AS PER NDT MANUAL PART 6-51-00-01 FIG 4. CRACK AT 1/4 BOLTS HOLE APPROX.5 INCH DOW
- [SDR UPS01236258](https://openairdocs.org/sdr/UPS01236258.md): Web · cracked · Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C NOSE LANDING GEAR BAY RH SIDE WALL AT BS 266 HAS A CRACK INDICATION. REMOVED ACCESS PANEL #3125 AS PER SRMB727-51-30-2 CUT OUT DAMAGE AREA AS PER B727-51-40-2 APPROX 3.5"X1" ACCOMLPISHED NDT INSPECTION AND INSTALLED DOUBLER REPAIR AS PER
- [SDR UPS01236256](https://openairdocs.org/sdr/UPS01236256.md): Web · cracked · Jun 20, 2001 · N934UP · Boeing 72721C · Fuselage Main, Structure
  > INSPECTION TYPE:C NOSE LANDING GEAR BAY LH SIDE AT BS 259 SIDE WALL HAS A CRACK INICATION. REMOVED ACCESS PANEL #3124 AND LOWER WEB TO GAIN ACCESS TO DAMAGE AREA, CUT OUT DAMAGE AREA APPROX 5"X1" AT NOSE LANDING GEAR BS259 AS PER B727 SRM51-40-2 ACCOMPLISH
- [SDR UPS00234570](https://openairdocs.org/sdr/UPS00234570.md): Landing Gear · faulty · Dec 27, 2000 · N934UP · Boeing 72721C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A NOSE GEAR DID NOT EXTEND ON FIRST TRY. RECYCLED & NOSEGEAR EXTENDED. JACKED AIRCRAFT, HEATED NOSE WHEEL AREA TO REMOVE ICE. GREASED TRUNI ON, OVERCENTER KNUCKLE, GEAR DOORS. CYCLED GEAR SEVERAL TIMES.
- [SDR UPS00232190](https://openairdocs.org/sdr/UPS00232190.md): Line · cracked · Apr 3, 2000 · N934UP · Boeing 72721C · Hydraulic System, Main
  > AIR TURN BACK ON DELIVERY FLIGHT FROM C CHECK AT SNN. CREW EXPERIENCED TOTAL LOSS OF B SYSTEM HYD PRESS. PRESS LINE FROM NR 1 B PUMP TO B SYS PRESS MODULE FOUND FRACTURED AT SLEEVE PRESS LINE CANIBALIZED FROM A/C N912UP TO REPLACE FRACTURED PIPE LINE. HYD S
- [SDR UPS00232144](https://openairdocs.org/sdr/UPS00232144.md): Support Bracket · cracked · Mar 21, 2000 · N934UP · Boeing 72721C · Engine Thrust Reverser
  > INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED AS PER MM 78-30-00
- [SDR UPS00232142](https://openairdocs.org/sdr/UPS00232142.md): Support Bracket · cracked · Mar 20, 2000 · N934UP · Boeing 72721C · Wing Miscellaneous Structure
  > INSPECTION TYPE: C, LT WING, FIXED TE SUPPORT BRACKET CRACKED, AREA BELOW 37 SPOILER I/B HINGE. REPLACED BRACKET IAW SRM 51-30-02
- [SDR UPS99228741](https://openairdocs.org/sdr/UPS99228741.md): Battery Pack · discharged · Feb 17, 1999 · N934UP · Boeing 72721C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FWD ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL PER MM 33-50-01. A/C OK FOR SERVICE.
- [SDR UPS98227730](https://openairdocs.org/sdr/UPS98227730.md): Skin · damaged · Sep 11, 1998 · N934UP · Boeing 72721C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:D WHILE REPLACEING BS 740 LT FITTING SEVERAL HOLES ON FUSELAGE SKIN COMMON TO FITTING FOUND DAMAGED. CARRIED OUT SKIN SPLICE REPAIR IAW EO 98-27-002 ENGINEERING FILE NR 5330-2071.
- [SDR UPS98227780](https://openairdocs.org/sdr/UPS98227780.md): Balance Panel · corroded · Sep 10, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer Structure
  > INSPECTION TYPE-D, CORROSION ON NR 3 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.
- [SDR UPS98227777](https://openairdocs.org/sdr/UPS98227777.md): Balance Panel · corroded · Sep 10, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer Structure
  > INSPECTION TYPE-D, CORROSION ON NR 5 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21.
- [SDR UPS98227732](https://openairdocs.org/sdr/UPS98227732.md): Rib · corroded · Sep 10, 1998 · N934UP · Boeing 72721C · Vertical Stabilizer, Spar/Rib
  > INSPECTION TYPE:D TENSION TIE RIB FWD AND AFT VERTICAL HOLES ARE PITTED. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NO 727-55-0374.
- [SDR UPS98227731](https://openairdocs.org/sdr/UPS98227731.md): Rib · corroded · Sep 10, 1998 · N934UP · Boeing 72721C · Vertical Stabilizer, Spar/Rib
  > INSPECTION TYPE:D TENSION TIE RIB ATTACH FITTINGS FWD AND AFT VERTICAL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NR 727-55-0374.
- [SDR UPS98227779](https://openairdocs.org/sdr/UPS98227779.md): Balance Panel · cracked · Sep 8, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer Structure
  > INSPECTION TYPE-D, RT STAB NR 4 BALANCE PANEL CRACKED. BALANCE PANEL REPLACED IAW MM 27-30-21.
- [SDR UPS98227778](https://openairdocs.org/sdr/UPS98227778.md): Balance Panel · corroded · Sep 8, 1998 · N934UP · Boeing 72721C · Horizontal Stabilizer Structure
  > INSPECTION TYPE-D, RT STAB, LIGHT SURFACE CORROSION ON NR 5 BALANCE PANEL. BALANCE PANEL REPLACED IAW MM 27-30-21.
- [SDR UPS98227729](https://openairdocs.org/sdr/UPS98227729.md): Panel · corroded · Sep 3, 1998 · N934UP · Boeing 72721C · Wing, Plate/Skin
  > INSPECTION TYPE:D LT WING BOLT ON FUEL TANK ACCESS PANELS ARE CORRODED PANELS NR 15 - NR 19. REPLACED PANELS IAW 28-12-11.
- [SDR UPS98227728](https://openairdocs.org/sdr/UPS98227728.md): Panel · corroded · Sep 3, 1998 · N934UP · Boeing 72721C · Wing, Plate/Skin
  > INSPECTION TYPE:D NR 1 FUEL TANK ACCESS PANEL CORRODED (FRONT SPAR) LT WING. REPLACED PANEL IAW 28-11-10.
- [SDR UPS98227725](https://openairdocs.org/sdr/UPS98227725.md): Bracket · cracked · Sep 2, 1998 · N934UP · Boeing 72721C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:D FRAME BS 488 OUTER CHORD ATTACH BRACKET CRACKED AT MAIN CARGO SUPPORT FITTING (FWD SIDE OF FRAME). CARRIED OUT REPAIR IAW SRM 53-10-4 FIG 11.
- [SDR UPS98227724](https://openairdocs.org/sdr/UPS98227724.md): Bracket · cracked · Sep 1, 1998 · N934UP · Boeing 72721C · Trailing Edge Flaps
  > INSPECTION TYPE:D LT OUTBD FLAP OUTBD SUPPORT RAMP STAY ROD REAR SPAR ATTACH BRACKET SUSPECT CRACKED. REPLACED SUPPORT BRACKET IAW SRM 51-30-2.
- [SDR UPS98227723](https://openairdocs.org/sdr/UPS98227723.md): Web · cracked · Sep 1, 1998 · N934UP · Boeing 72721C · Ailerons
  > INSPECTION TYPE:D LT OUTBD AILERON FIXED WEIGHT BAY, INBOARD WEB IS CRACKED. REPAIRED IAW SRM 51-30-02.
- [SDR UPS98227722](https://openairdocs.org/sdr/UPS98227722.md): Casting · corroded · Sep 1, 1998 · N934UP · Boeing 72721C · Spoilers
  > INSPECTION TYPE:D ON FURTHER INVESTIGATION OF NR 6 SPOILER LINKAGE SUPPORT CASTING MIGRATED REWORK SLEEVE REMOVED AND CORROSION FOUND IN REWORKED AREA. REPLACED SUPPORT CASTING IAW DRAWING NR 65-16216.
- [SDR UPS98227721](https://openairdocs.org/sdr/UPS98227721.md): Rib · cracked · Sep 1, 1998 · N934UP · Boeing 72721C · Leading Edge Devices
  > INSPECTION TYPE:D CRACK AT NR 6 SLAT I/B TRACK O/B RIB. REPAIRED RIB IAW SRM 51-40-2.
- [SDR UPS98226343](https://openairdocs.org/sdr/UPS98226343.md): Bulb · failed · Apr 9, 1998 · N934UP · Boeing 72721C · Emergency Lighting
  > CABIN ENTRY DOOR EMERGENCY EXIT 1 LIGHT INOP. RELAMPED, GROUND CHECKS OK.
- [SDR UPS97224438](https://openairdocs.org/sdr/UPS97224438.md): Hose · leaking · Sep 16, 1997 · N934UP · Boeing 72721C · Hydraulic System, Main
  > INSPECTION TYPE-N/A, LOSS OF HYDRAULIC SYSTEM 'B' FLUID AT 15,000 FT BOTH 1 AND 2 'B' PUMPS LOW PRESS LIGHTS CAME ON, QTY INDICATION 0. DECLARED EMERGENCY, COMPLIED WITH CHECKLISTS, LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 'B' PUMP PRESSURE LINE CHAFED TH
- [SDR UPS97224319](https://openairdocs.org/sdr/UPS97224319.md): Actuator · leaked · Aug 29, 1997 · N934UP · Boeing 72721C · Leading Edge Slat Actuator
  > INSPECTION TYPE-N/A, LOSS OF HYDS, GEAR EXTENDED MANUALLY. FOUND LEAK AT NR 5 LE SLAT ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW MM 27-81-3 2, SERVICED HYDS, RAN ENGINES, CYCLED ALL FLT CONTROLS, CKD FOR LEAKS, OK FOR SERVICE.
- [SDR UPS205333](https://openairdocs.org/sdr/UPS205333.md): Mid Spar · chafed · Jan 25, 1996 · N934UP · Boeing 72721C · Vertical Stabilizer
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRED PER UPS EO 727-55-0309.
- [SDR UPS205319](https://openairdocs.org/sdr/UPS205319.md): Wedge · corroded · Jan 24, 1996 · N934UP · Boeing 72721C · Trailing Edge Flaps
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2.
- [SDR UPS205332](https://openairdocs.org/sdr/UPS205332.md): Rib · cracked · Jan 23, 1996 · N934UP · Boeing 72721C · Horizontal Stabilizer, Spar/Rib
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT END. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2.
- [SDR UPS205331](https://openairdocs.org/sdr/UPS205331.md): Slat · cracked · Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge Devices
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW MM 27-81-11.
- [SDR UPS205330](https://openairdocs.org/sdr/UPS205330.md): Bonding Jumper · corrosion · Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge Devices
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00.
- [SDR UPS205329](https://openairdocs.org/sdr/UPS205329.md): Angle · cracked · Jan 23, 1996 · N934UP · Boeing 72721C · Leading Edge Devices
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51-30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1.
- [SDR UPS205327](https://openairdocs.org/sdr/UPS205327.md): Rod End · corroded · Jan 23, 1996 · N934UP · Boeing 72721C · Aileron Control System
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILERON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00.
- [SDR UPS205326](https://openairdocs.org/sdr/UPS205326.md): Hinge Tab · corroded · Jan 23, 1996 · N934UP · Boeing 72721C · Aileron Tab Control System
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0.
- [SDR UPS205328](https://openairdocs.org/sdr/UPS205328.md): Hinge Fitting · corroded · Jan 22, 1996 · N934UP · Boeing 72721C · Aileron Control System
  > WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND REPLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-

Next page: https://openairdocs.org/deregistered/N934UP-2007-05-10/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 = 'N934UP' AND deregistration_id = 'N934UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N934UP-2007-05-10/reports

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