# Service difficulty reports: N946UP, cancelled May 10, 2007

A list on [N946UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N946UP-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 5 · 215 reports

- [SDR UPS04243509](https://openairdocs.org/sdr/UPS04243509.md): Switch · will not test · Nov 18, 2004 · N946UP · Boeing 72725C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WON'T TEST. FOUND 2 SCREWS LOOSE ON EMERGENCY LIGHT SWITCH. TIGHTENED SCREWS, CKS OK PER MM 33-50-01.
- [SDR UPS04243508](https://openairdocs.org/sdr/UPS04243508.md): Light · inoperative · Nov 18, 2004 · N946UP · Boeing 72725C · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT WILL NOT CK ON PREFLT. RESET RELAY R-70 CKS OK.
- [SDR UPS03241048](https://openairdocs.org/sdr/UPS03241048.md): Frame · corroded · Jul 24, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, DURING INSPECTION OF SKIN CHANGE AREA FRAME AT BS 303 FOUND DAMAGED BETWEEN S10L AND S9L. CLEANED UP DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PART IAW SRM 51-40-4. INSTALLED REPAIR PART IAW SRM 51-40-4.
- [SDR UPS03241060](https://openairdocs.org/sdr/UPS03241060.md): Hinge Fitting · cracked · Jul 22, 2003 · N946UP · Boeing 72725C · Passenger/Crew Doors
  > INSPECTION TYPE:C, DURING NDT OF ALL FASTENER HOLES COMMON TO SKIN CHANGE AT FWD ENTRY DOORWAY, CRACK FOUND IN FWD ENTRY DOOR UPPER HINGE LOWER FITTING. FITTING REPLACED IAW DRG 65-17684.
- [SDR UPS03241069](https://openairdocs.org/sdr/UPS03241069.md): Skin · delaminated · Jul 17, 2003 · N946UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:C 2 AREAS OF DELAM FOUND DURING SURFACE CORROSION REMOVAL ON LEFT I/B MIDFLAP AFT UPPER SKIN. NOTE THAT DURING REPAIR 2 AREAS OF DISBOND OCCURRED ON LOWER SURFACE. REPAIRS CARRIED OUT IAW SRM 51-40-20.
- [SDR UPS03241063](https://openairdocs.org/sdr/UPS03241063.md): Panel · cracked · Jul 17, 2003 · N946UP · Boeing 72725C · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE: C, VERTICAL FIN LEADING EDGE LOWER PANEL 9501, MATING STRAP HAS A CRACK IN THE OUTER SKIN. CRACK STOP DRILLED IAW SRM 51-10-01, REPAIR DOUBLER FABRICATED IAW SRM 51-20-01, FIG 7. REPAIR DOUBLER INSTALLED IAW SRM 51-30-02.
- [SDR UPS03241062](https://openairdocs.org/sdr/UPS03241062.md): Fastener · cracked · Jul 17, 2003 · N946UP · Boeing 72725C · Fasteners
  > INSPECTION TYPE: C, FOLLOWING HFEC INSPECTION AROUND FASTENER HOLES IN O/B FLANGES OF VERTICAL FIN FRONT SPAR FORGING, 2 CRACKS FOUND COMING FROM FASTENER HOLES ON LEFT SIDE. CRACKS STOP DRILLED IAW DRG 65-81528. REFERENCE SMRO EO 2003-041-001 FOR REWORK. R
- [SDR UPS03241008](https://openairdocs.org/sdr/UPS03241008.md): Skin · cracked · Jul 17, 2003 · N946UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE: C, SMALL CRACK 1 INCH IN LENGHT ON TAI SKIN OF NR 4 KREUGER FLAP, JUST I/B OF ACTUATOR ROD END ATTACH POINT ON FLAP. RECTIFICATION CARRIED OUT IAW UPS EO B727-5750-3082.
- [SDR UPS03241068](https://openairdocs.org/sdr/UPS03241068.md): Support Fitting · cracked · Jul 16, 2003 · N946UP · Boeing 72725C · Spoilers
  > INSPECTION TYPE:C NR 11 SPOILER SUPPORT FITTING IS CRACKED. FITTING REPLACED IAW UPS EO B727-5750-5182.
- [SDR UPS03240995](https://openairdocs.org/sdr/UPS03240995.md): Skin · cracked · Jul 16, 2003 · N946UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE: C, NR 3 SLAT OUTER SKIN CRACKED ADJACENT TO I/B HOOK ATTACH POINT. HFEC INSP CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT CRACK CONFIRMED & END MARKED. REPAIR CARRIED OUT IAW SRM 51-10-1, 57-50-3 & 51-30-3.
- [SDR UPS03241007](https://openairdocs.org/sdr/UPS03241007.md): Stringer · damaged · Jul 15, 2003 · N946UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, HOLE IN FLANGE OF STRINGER B-HYD SYS COMPARTMENT O/B OF HYD RESERVOIR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 2, DAMAGED REMOVED IAW SRM 51-10-06. CUT LINE TO BE NDT'D HFEC INSP CARRIED OUT AROUND CUT LINE ON THE ABOVE AREA IAW B727 NDTM
- [SDR UPS03241070](https://openairdocs.org/sdr/UPS03241070.md): Panel · debonded · Jul 14, 2003 · N946UP · Boeing 72725C · Spoilers
  > INSPECTION TYPE:C NR 3 SPOILER PANEL LOWER SURFACE DISBOND AT ACTUATOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-40-05.
- [SDR UPS03241067](https://openairdocs.org/sdr/UPS03241067.md): Skin · corroded · Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C EVIDENCE OF CORROSION AT LAP JOINT BS 820 TO BS 870, S-4R REPAIR CARRIED OUT IAW UPS EO B727-5330-0509.
- [SDR UPS03241066](https://openairdocs.org/sdr/UPS03241066.md): Skin · cracked · Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, EVIDENCE OF CRACK AROUND FASTENER AT MID GALLEY DOOR CUTOUT BS 640, S-8L. REPAIR CARRIED OUT IAW SMRO EO 2003-041-004. REFERENCE UPS EO B727- 5330-19065.
- [SDR UPS03241065](https://openairdocs.org/sdr/UPS03241065.md): Skin · debonded · Jul 14, 2003 · N946UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE: C, LEFT O/B AFT FLAP - DISBOND AT UPPER SURFACE 5 TO 20 INCHES FROM O/B END. REPAIR CARRIED OUT IAW SRM 51-40-20.
- [SDR UPS03241064](https://openairdocs.org/sdr/UPS03241064.md): Tab · contaminated · Jul 14, 2003 · N946UP · Boeing 72725C · Elevator, Tab Structure
  > INSPECTION TYPE: C, FOLLOWING X-RAY INSPECTION OF RT ELEVATOR TAB, WATER INGRESS FOUND ON RT ELEVATOR TAB AT APPROX ELEV STA 95 TO ELEV STA 105. REPAIR CARRIED OUT IAW SRM 51-40-05.
- [SDR UPS03241061](https://openairdocs.org/sdr/UPS03241061.md): Pressure Panel · cracked · Jul 14, 2003 · N946UP · Boeing 72725C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C NLG WHEEL WELL RT CEILING PRESSURE PANEL HAS A CRACK FROM OUTBOARD EDGE OF PANEL TO BOLT HOLE. PANEL REPAIRED IAW 2003-041-005. REFERENCE UPS ENGINEERING FILE NR 727-53-20125.
- [SDR UPS03241050](https://openairdocs.org/sdr/UPS03241050.md): Skin · cracked · Jul 14, 2003 · N946UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE: C, LEFT I/B MIDFLAP LWR SURFACE 2 CRACKS AT FWD I/B & O/B CORNERS OF SKIN CUTOUT FOR I/B AFT FLAP ACTUATING ROD. CRACK STOP DRILLED TO.250 INCH IAW SRM 51-10-1. REPAIR CARRIED OUT IAW MRO EO 2003-041-002. UPS FILE NR 727-27-20007.
- [SDR UPS03241049](https://openairdocs.org/sdr/UPS03241049.md): Frame · cracked · Jul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE: C, FRAME CRACKED AT BS 1070 AND ATTACH POINT FOR AFT LWR CARGO DOOR. CRACKED FRAME AT BS 1070 REMOVED AND NEW FRAME INSTALLED IAW DRAWING NR65-18622.
- [SDR UPS03241010](https://openairdocs.org/sdr/UPS03241010.md): Fairing · cracked · Jul 11, 2003 · N946UP · Boeing 72725C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENG NR 3 THRUST REV O/B FAIRING IS CRACKED NEAR FWD SUPPORT BRACKET UPPER EXISTING DOUBLER AT CRACK LOCATION REMOVED IAW SRM 51-30-02. CRACKS TOP DRILLED IAW SRM 78-30-01 0.025 HOLE. HFEC INSP CARRIED ON STOP DRILL IAW B727 NDTM PT 6 51-00-
- [SDR UPS03241006](https://openairdocs.org/sdr/UPS03241006.md): Skin · lightning strike · Jul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, LIGHTNING STRIKE DAMAGE AT BS 590 S25R. FASTENER REMOVED AND AREA CLEANED IAW SRM 51-30-02. HFEC INSP CARRIED OUT ON DAMAGED AREA IAW B727 NDTM PT 6 FIG 4. RESULT CRACK FOUND AS MARKED ON A/C & ENDS OF CRACK MARKED. REPAIR CARRIED OUT
- [SDR UPS03241005](https://openairdocs.org/sdr/UPS03241005.md): Doubler · corroded · Jul 11, 2003 · N946UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE: C, CORROSION ON DELTA BEAM LT WEB DOUBLER AT BS 740. REMOVED CORRODED DOUBLER IAW SRM 51-30-02. REMOVED CORROSION FOUND ON DELTA BEAM WEB & FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01 & 53-1 0-2. FABRICATED REPAIR PARTS IAW SRM 53-10-2. CA
- [SDR UPS03241071](https://openairdocs.org/sdr/UPS03241071.md): Skin · cracked · Jul 10, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SKIN CRACKS FROM FASTENER HOLES BS 255 (AFT OF NR 3 RT WINDOW CUTOUT) BETWEEN S-10R AND S-9R. REPAIR CARRIED OUT IAW SRM 53-30-03, FIGURE 29.
- [SDR UPS03241009](https://openairdocs.org/sdr/UPS03241009.md): Angle · corroded · Jul 10, 2003 · N946UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SURFACE CORROSION ON ANGLE IN LT MLG WHEEL WELL AT BS 935 FWD OF 940 FITTING AT STR 19. REMOVED ANGLE IAW SRM 51-30-02. ANGLE FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. FABRICATED ANGLE IAW DRAWING 65-22419 & SRM 51-20-01 & 51-40-3. I
- [SDR UPS03240994](https://openairdocs.org/sdr/UPS03240994.md): Support Bracket · cracked · Jul 10, 2003 · N946UP · Boeing 72725C · Engine Thrust Reverser
  > INSPECTION TYPE: C, ENG NR 3 THRUST REVERSER OUTER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-01.
- [SDR UPS03241072](https://openairdocs.org/sdr/UPS03241072.md): Skin · corroded · Jul 9, 2003 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SKIN CRACK FOUND AT FWD CORNER CUTOUT OF FWD ENTRY DOOR S-7L. NOTE: WHEN NDT WAS CARRIED OUT IN REPAIR AREA, IT WAS FOUND THAT THERE WAS CORROSION BETWEEN THE SKIN AND BONDED DOUBLER IN THE AREA SURROUNDING THE FWD ENTRY DOOR SKIN PANEL P/N
- [SDR UPS02238974](https://openairdocs.org/sdr/UPS02238974.md): Latch · out of adjust · Aug 3, 2002 · N946UP · Boeing 72725C · Passenger/Crew Doors
  > INSPECTION TYPE:N/A, ENTRY DOOR HANDLE UNLATCHED ON LANDING FOUND DOOR ENTRYWAY PARTIALLY OPENED. ALSO ACFT SUFFICIENT TO MAINTAIN PRESSURIZATION IN AUTO/MAN. PERFORMED FWD ENTRY DOOR ADJ FOR SOFT UNLATCHING PER MM 52-11-00.
- [SDR UPS01237093](https://openairdocs.org/sdr/UPS01237093.md): Stringer · cracked · Oct 18, 2001 · N946UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:N/A STRINGER 20R CRACKED AT FRAME 294 FWD OF LAV WASTE CHUTE STRINGER REPAIRED AS PER SRM 53-10-03. STATION 319 TO 284.5 REPAIRED
- [SDR UPS01237036](https://openairdocs.org/sdr/UPS01237036.md): Lap Joint · corroded · Sep 23, 2001 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:IN CORROSION AT CREW OXYGEN SERVICE PORT LAP SEAM, STRINGER 19R, STATION 360 TO 344 HAS CORROSION AT LAP SEAM. REMOVED FASTENERS HS 86801 10501 / REMOVED CORROSION HS 86801. VERIFIED REMOVAL OF CORROSION. REINSTALLED FASTENERS AS PER EO B727-
- [SDR UPS01235481](https://openairdocs.org/sdr/UPS01235481.md): Smoke Detector · inoperative · Apr 1, 2001 · N946UP · Boeing 72725C · Smoke Detection
  > MAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED AND DISPATCHED AIRCRAFT
- [SDR UPS01235063](https://openairdocs.org/sdr/UPS01235063.md): Battery · discharged · Feb 23, 2001 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, ROW 2 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 2 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
- [SDR UPS01235061](https://openairdocs.org/sdr/UPS01235061.md): Plate · inoperative · Feb 23, 2001 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, FWD L1 EMERGENCY EXIT ID AND PLATE IS INOPERATIVE DUE TO EMERGENCY LIGHT TEST INOP ON FWD L1 DOOR. REMOVED AND REPLACED BASE EXIT ID AND PLATE ON L1 DOOR.
- [SDR UPS01235060](https://openairdocs.org/sdr/UPS01235060.md): Transmitter · inoperative · Feb 23, 2001 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, FWD L1 DOOR EMERGENCY BATTERY LIGHT DOES NOT TEST ON GROUND. REMOVED AND REPLACED TRANSMITTER, OPS CK GOOD.
- [SDR UPS01235059](https://openairdocs.org/sdr/UPS01235059.md): Battery · discharged · Feb 23, 2001 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, ON EMERGENCY EXIT LIGHT TEST THE FOLLOWING LIGHTS FAILED MED EXIT MARKERS, RT GALLEY EXIT MARKER AND 2 GALLEY EXIT LOCATORS. REPLACED EMERGENCY EXIT BATTERIES PACKS, TESTED OK.
- [SDR UPS01234573](https://openairdocs.org/sdr/UPS01234573.md): Connector · loose · Dec 29, 2000 · N946UP · Boeing 72725C · Elevator Control System
  > INSPECTION TYPE:N/A PILOT REPORT-STAB TRIM AND STICK SHAKER ON APPROACH CLEANED AND LUBED JACK SCREW. R/R CONNECTOR ON CAPT STICK SHAKER
- [SDR UPS00233738](https://openairdocs.org/sdr/UPS00233738.md): Fitting · cracked · Aug 23, 2000 · N946UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE:C, CRACKED MAIN CARGO DOOR LATCH SUPPORT FITTING, BS 580 CRACK LOCATED A T-UPPER INBOARD FLANGE. INSTALLED SUPPORT FITTING REPAIR KIT IAW UPS EO B727-5310-0437I APPX 8.6 & 8.7.
- [SDR UPS00233734](https://openairdocs.org/sdr/UPS00233734.md): Spar · corroded · Aug 19, 2000 · N946UP · Boeing 72725C · Wing Spar
  > INSPECTION TYPE:C, OPEN AREA AT LOWER CHORD, AFT SPAR ON CENTER TANK OUTBOARD END, LEFT SIDE INSPECTION FOR SUSCEPTIBLE CORROSION. ACCOMPLISHED REPAIR OF WING CENTER SECTION REAR SPAR LOWER CHORD AT BBL 41.82 IAW UPS EO B727-5710-13234-A AND BOEING TELEX PRO-
- [SDR UPS00233737](https://openairdocs.org/sdr/UPS00233737.md): Spar · corroded · Aug 15, 2000 · N946UP · Boeing 72725C · Wing Spar
  > INSPECTION TYPE:C, CORROSION ON CENTER TANK, AFT SPAR, UPPER CHORD, OUTBOARD END, LEFT SIDE. ACCOMPLISHED WING CENTER SECTION REAR SPAR UPPER CHORD CORROSION REP AIR BETWEEN LBL 39.07 & LBL 70 IAW UPS EO B727-5710-13233-A, AVITAS EINGINEERING REPAIR ORDER AVH
- [SDR UPS00233707](https://openairdocs.org/sdr/UPS00233707.md): Web · cracked · Aug 12, 2000 · N946UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL RIGHT SIDE VERTICAL WEB IS CRACKED AT BS 267, 5 INCHES DOWN FROM CEILING. STOP DRILLED CRACK AND INSTALLED WEB REPAIR IAW SRM 51-40-2 FIG 1.
- [SDR UPS00233736](https://openairdocs.org/sdr/UPS00233736.md): Bulkhead · cracked · Aug 9, 2000 · N946UP · Boeing 72725C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C, FORWARD PRESSURE BULKHEAD BS 178 FORWARD FACE BL 0 & WL 190 APPROXIMATELY HAS CRACK RUNNING FROM FASTENER. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR IAW UPS EO B727-5310-4290-B APPX B.
- [SDR UPS00233735](https://openairdocs.org/sdr/UPS00233735.md): Skin · corroded · Aug 8, 2000 · N946UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, FUSELAGE SKIN BULGE AT STRINGER 10 LEFT BS 349 - 360. ACCOMPLISHED SKIN CORROSION REPAIR FROM STA 344 - 360, STR 10 - 9 LEFT IAW UPS EO B727-5330-13232A, BOEING TELEX UPS-MIA-00-00016H, AND AVI TAS ENGINEERING REPAIR ORDER AVHM-149RO-1.
- [SDR UPS00232739](https://openairdocs.org/sdr/UPS00232739.md): Controller · malfunctioned · May 29, 2000 · N946UP · Boeing 72725C · Detection System
  > INSPECTION TYPE:N/A, WHEEL WELL FIRE INDICATION APPROX 6000 WITHIN 15 MILES OF SDF. ALSO, BELL CUTOUT DID NOT WORK PROPERLY, HAD TO HOLD BELL CUTOUT SWITCH IN. INSPECTED LOOPS, REMOVED AND REPLACED WHEEL WELL CONTROL UNIT. SYS OPS GOOD ON GROUND.
- [SDR UPS00232236](https://openairdocs.org/sdr/UPS00232236.md): Battery · inoperative · Apr 7, 2000 · N946UP · Boeing 72725C · Emergency Lighting
  > ALL EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED 7 EACH EMERGENCY EXIT LIGHT BATTERIES. REMOVED AND REPLACED REMOTE POWER ASSY. OPS CHECK GOOD.
- [SDR UPS00231451](https://openairdocs.org/sdr/UPS00231451.md): Battery Pack · discharged · Jan 28, 2000 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A LH AFT OVERWG DOOR EMERG. LIGHT INOP REMOVED AND REPLACED BATT PACK OPS CHECK GOOD
- [SDR UPS00231392](https://openairdocs.org/sdr/UPS00231392.md): Light · inttermittent · Jan 23, 2000 · N946UP · Boeing 72725C · Emergency Lighting
  > GREEN EXIT LIGHT AT FLOOR LEVEL AT FWD ENTRY DOOR BLINKS CONTINUOUSLY IN FLIGHT AND ON GROUND. RESET LIGHT ASSY, OPS CHECK GOOD.
- [SDR UPS00231332](https://openairdocs.org/sdr/UPS00231332.md): Battery Pack · discharged · Jan 14, 2000 · N946UP · Boeing 72725C · Emergency Lighting
  > EMERGENCY LIGHT EXIT MARKER AT GALLEY DOOR FLOOR LEVEL FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.
- [SDR UPS00231330](https://openairdocs.org/sdr/UPS00231330.md): Battery Pack · discharged · Jan 14, 2000 · N946UP · Boeing 72725C · Emergency Lighting
  > ROW 19 EMERGENCY LIGHT FAILED TEST. REPLACED BATTERY. OPS CHECKS GOOD.
- [SDR UPS99231159](https://openairdocs.org/sdr/UPS99231159.md): Light · inoperative · Nov 30, 1999 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF FWD RT OVERWING EMERGENCY EXIT INOP, LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY AND BATTERY PACK, OPS CHECK GOOD. LIGHT ASSY (P/N 96-3-1032-2), BATTERY PACK (P/N 96-2-1015).
- [SDR UPS99231158](https://openairdocs.org/sdr/UPS99231158.md): Battery Pack · discharged · Nov 30, 1999 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF LT AFT OVERWING EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY PACK AT LT AFT OVERWING EXIT, OPS CHECKS GOOD.
- [SDR UPS99231157](https://openairdocs.org/sdr/UPS99231157.md): Batter Pack · discharged · Nov 30, 1999 · N946UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AFT OF LT FWD OVERWING EXIT WAS DIM. REMOVED AND REPLACED BATTERY PACK.

Next page: https://openairdocs.org/deregistered/N946UP-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 = 'N946UP' AND deregistration_id = 'N946UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N946UP-2007-05-10/reports

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