# Service difficulty reports: N915UP, cancelled Aug 23, 2006

A list on [N915UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N915UP-2006-08-23.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 3 · 114 reports

- [SDR UPS01236444](https://openairdocs.org/sdr/UPS01236444.md): Fitting · corroded · Jul 30, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:IN FRAME FOOT ANGLE AT FS 351 BETWEEN STRINGERS 24R AND 25R IS SEVERELY CORRODED. THIS IS UNDER FLOOR PANEL ON RT SIDE OF NLG WW ENCLOSURE ON THE INSIDE. R&R FRAME FOOT ASSY PER SRM 51-30-02.
- [SDR UPS01236434](https://openairdocs.org/sdr/UPS01236434.md): Angle · cracked · Jul 27, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A FRAME ANGLE CRACKED STA 351 JUST AFT OF O/B AFT CORNER OF ACCESS PANEL BEHIND NLG RT SIDE CUTOUT DAMAGED ANGLE PER SRM 51-10-01 PERFORMED HFEC INSPECTION OF CUTOUT AREA NO CRACKS NOTED REPAIRED PER B727 5330 15208.
- [SDR UPS01236400](https://openairdocs.org/sdr/UPS01236400.md): Skin · corroded · Jul 20, 2001 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A CORROSION AFT OF NLG WW, BELLY SKIN. REMOVED CORROSION AT BS 340 TO BS 360 BETWEEN STR 26 AND 27 RT PER SRM 51-10-01. INSTALLED LT AND RT INTERNAL DOUBLER SPLICES AND T ANGLES, INSTALLED NEW FUSELAGE SKIN IAW 727 SRM 51-30.
- [SDR UPS01235828](https://openairdocs.org/sdr/UPS01235828.md): Actuator · malfunctioned · May 8, 2001 · N915UP · Boeing 72727C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A LT MLG WOULD NOT RETRACT AFTER LANDING GEAR RETRACTION THE RED DOORS WARNING LIGHT AND LEFT GEAR UNLOCKED RED LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE WAS PUT IN OFF POSITION THE LEFT GEAR GREEN LIGHT WAS ILLUMINATED. REMOVED AND REPLAC
- [SDR UPS00234540](https://openairdocs.org/sdr/UPS00234540.md): Web · cracked · Nov 21, 2000 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A 1 INCH CRACK AT BOLT HOLE, WEB AREA 24 INCHES AFT OF BULKHEAD NOSE W/W 3 INCHES UP FROM DOOR OPENING LT SIDE REPAIR CRACKED WEB PER B727 SRM 51-40-2 SHEET 6
- [SDR UPS00234445](https://openairdocs.org/sdr/UPS00234445.md): Battery · discharged · Nov 12, 2000 · N915UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:C, FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.
- [SDR UPS00234444](https://openairdocs.org/sdr/UPS00234444.md): Battery · discharged · Nov 12, 2000 · N915UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:C, COCKPIT EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.
- [SDR UPS00233798](https://openairdocs.org/sdr/UPS00233798.md): Skin · damaged · Sep 16, 2000 · N915UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 171.5 ABOVE NR 3 LEADING EDGE FLAP DAMAGED. INSTALLED SKIN REPAIR FROM WS 171.5 TO 160.0, DOUBLER MATERIAL USED, 2024-T3, 0.080, 8 X 7 INCHES. ANGLE REPAIR INSTALLED MATERIAL USED 7075-T6, 20 TRACK PART NUMBER
- [SDR UPS00233797](https://openairdocs.org/sdr/UPS00233797.md): Skin · damaged · Sep 16, 2000 · N915UP · Boeing 72727C · Trailing Edge Flaps
  > INSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 251 ABOVE NR 2 LEADING EDGE FLAP IS DAMAGED. INSTALLED DOUBLER REPAIR, MATERIAL 2024-T3,0. 080, 9 X 7 INCHES, FILLER 2024-T3, 0.080, 3.35 X 3.125 INCHES, HEAT SHIELD MATERIAL USED, 2024-T3 0.016, 9.5 X 10.5 INCH
- [SDR UPS00231267](https://openairdocs.org/sdr/UPS00231267.md): Skin · corroded · Jan 11, 2000 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FUSELAGE COMPLY WITH D185003 CORROSION AT STA 118 3 LEFT SIDE. CUT OUT DAMAGED SECTION AT STR 9 LT BS1181 TO 1175 PER SRM 51-10-1. PERFORMED HFEC INSP OF CUTOUT PER NDT PART 6 51-10-1 FIG 4 AND NO CRACKS NOTED. COMPLETED REPAIR PER SRM 51
- [SDR UPS99229224](https://openairdocs.org/sdr/UPS99229224.md): Fitting · corroded · Apr 2, 1999 · N915UP · Boeing 72727C · Ailerons
  > INSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51-30-2.
- [SDR UPS99229210](https://openairdocs.org/sdr/UPS99229210.md): Fitting · corroded · Apr 2, 1999 · N915UP · Boeing 72727C · Ailerons
  > INSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTING PER SRM 51-30-2.
- [SDR UPS99229209](https://openairdocs.org/sdr/UPS99229209.md): Rib · cracked · Apr 2, 1999 · N915UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 3 SLAT OUTBOARD ACTUATOR RIB IS CRACKED. REMOVED 2 EA RIBS O/B ACTUATOR RIB AND NEXT ONE O/B FOR ACCESS, DRILLED NEW RIB AND INSTALLED, INSTALLED ACCESSED RIB IAW SRM 51-30-02, 51-30-05, 51-10-01.
- [SDR UPS99229213](https://openairdocs.org/sdr/UPS99229213.md): Skin · corroded · Mar 24, 1999 · N915UP · Boeing 72727C · Fuel Storage
  > INSPECTION TYPE:C WHILE WORKING NRC 923405, FOUND CENTER FUEL CELL UPPER SKIN CORRODED UNDER SEAL RETAINER RBL 50-65. REPAIRED PER ER 99-5206.
- [SDR UPS99229215](https://openairdocs.org/sdr/UPS99229215.md): Chord · corroded · Mar 21, 1999 · N915UP · Boeing 72727C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON WING CENTER SECTION AFT LOWER CHORD RBL 42-48 AND AFT UPPER CHORD RBL 38-42. REPLACED UPPER AND LOWER CHORD PER SRM 51-30-2 AND ER 99-5195.
- [SDR UPS99229212](https://openairdocs.org/sdr/UPS99229212.md): Fitting · corroded · Mar 19, 1999 · N915UP · Boeing 72727C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C, LEFT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-02.
- [SDR UPS99229211](https://openairdocs.org/sdr/UPS99229211.md): Fitting · corroded · Mar 19, 1999 · N915UP · Boeing 72727C · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C, RT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED FITTING PER SRM 51-30-02.
- [SDR UPS99229214](https://openairdocs.org/sdr/UPS99229214.md): Link · corroded · Mar 5, 1999 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION EMANATING FROM AROUND AFT BUSHING LBL 24 EXPANSION LINK BS 868 WL 205. REMOVED EXPANSION LINK FROM AIRCRAFT, REMOVED CORROSION FROM AROUND BUSHING HOLES AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW EXPANSION LINK AND INSTALLED IA
- [SDR UPS97224560](https://openairdocs.org/sdr/UPS97224560.md): Spoiler · delaminated · Sep 29, 1997 · N915UP · Boeing 72727C · Spoilers
  > INSPECTION TYPE-C, NR 12 SPOILER HAS A 3 X 3 AREA OF DELAMINATION ON UPPER SURFACE 8 FROM FWD EDGE ON O/B END. REPAIRED NR 12 SPOLER UPPER SURFACE IAW SRM 57-50-06.
- [SDR UPS97224559](https://openairdocs.org/sdr/UPS97224559.md): Seat Track · corroded · Sep 29, 1997 · N915UP · Boeing 72727C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C, CORROSION ON SEAT TRACK AND AROUND FASTENERS STA 850 TO 870 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. ALSO, FOUND ATTACHING EXPANSION LINK CORRODED OUT OF LIMITS. REPLACED TRACK LINK AND EXPANSION LINK (P/N 65-34144-2
- [SDR UPS97224564](https://openairdocs.org/sdr/UPS97224564.md): Stiffener · corroded · Sep 22, 1997 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-111-03.00-01) ON NOSE WHEEL WELL UPPER SKIN BS 313 RBL 11 WL 181. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-11-1. REPLACED STIFFENER AND REPAIRED PER SRM 51-30-2, 51-40-2, 51-10-2 AND MM 51-20-151.
- [SDR UPS97224563](https://openairdocs.org/sdr/UPS97224563.md): Floorbeam · corroded · Sep 22, 1997 · N915UP · Boeing 72727C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C, WHILE ACCESSING FOR INTERIOR 81 CUSTOMER NR 740183 DISCOVERED FLOORBEAM UPPER CHORD TO BE CORRODED LBL 16 RBL 16 WL 208 BS 344. REMOVED CORROSION ON FLOORBEAM FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED BEAM PER SRM 53-10-01.
- [SDR UPS97224562](https://openairdocs.org/sdr/UPS97224562.md): Skin · corroded · Sep 22, 1997 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, CORROSION (C53-100-01.00-4) EXTERNAL SKIN PILLOWED WITH DISHED RIVET HEADS AND LIGHTNING STRIKE STR 19R STA 664 TO 682 WL 199. REMOVED CORROSION ON SKIN, FOUND TO BE OUT OF LIMITS PER SRM 53-30-01. LIGHTNING STRIKE FOUND TO BE OUT OF LIMIT
- [SDR UPS97224561](https://openairdocs.org/sdr/UPS97224561.md): Seat Track · corroded · Sep 22, 1997 · N915UP · Boeing 72727C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C, CORROSION ON SEAT TRACK AND AROUND FASTENERS BS 850 TO 870 LBL 25 WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED SEAT TRACK PER SRM 51-30-02.
- [SDR UPS97224468](https://openairdocs.org/sdr/UPS97224468.md): Beam · cracked · Sep 17, 1997 · N915UP · Boeing 72727C · Passenger/Crew Doors
  > INSPECTION TYPE-C, FWD ENTRY DOOR UPPER GATE BEAM CRACKED IN RADIUS OF OUTER ANGLE. REMOVED AND REPLACED FWD ENTRY DOOR UPPER GATE BEAM IAW SRM 51-30-2, 51-20-4, 51-10-1 AND MM 51-20-151.
- [SDR UPS97224474](https://openairdocs.org/sdr/UPS97224474.md): Skin · cracked · Sep 16, 1997 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, POSSIBLE CRACK STA 219 UPPER AFT CORNER OF B2 WINDOW. REPAIRED PER UPS EO B727-5310-0012K.
- [SDR UPS97224473](https://openairdocs.org/sdr/UPS97224473.md): Skin · corroded · Sep 16, 1997 · N915UP · Boeing 72727C · Elevator, Plate/Skin
  > INSPECTION TYPE-C, CORROSION NOTED ON RT ELEVATOR 2ND O/B STATIC WICK BASE. CORROSION OUT OF LIMITS IAW SRM 55-20-1. REPAIRED ELEVATOR (RT) IAW 55-20-3 SRM 51-80-7 SRM.
- [SDR UPS97224472](https://openairdocs.org/sdr/UPS97224472.md): Skin · corroded · Sep 16, 1997 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, CORROSION (C53-111-03.00-01) FOUND ON UPPER SKIN OF NLG DOGHOUSE BS 304 RBL 6 TO 13 WL 181. REWORK UPPER SKIN OF DOGHOUSE BS 304 OUT OF LIMITS IAW 53-10-1. REPAIRED UPPER SKIN IAW SRM 53-30-4, 51-40-2, 51-30-2, 51-20-4 51-10-2 AND MM 51-20
- [SDR UPS97224471](https://openairdocs.org/sdr/UPS97224471.md): Spoiler · delaminated · Sep 16, 1997 · N915UP · Boeing 72727C · Spoilers
  > INSPECTION TYPE-C, NR 12 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED NR 12 SPOILER IAW MM 27-61-01.
- [SDR UPS97224470](https://openairdocs.org/sdr/UPS97224470.md): Spoiler · delaminated · Sep 16, 1997 · N915UP · Boeing 72727C · Spoilers
  > INSPECTION TYPE-C, NR 14 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED NR 14 SPOILER IAW MM 27-61-01.
- [SDR UPS97224469](https://openairdocs.org/sdr/UPS97224469.md): Spoiler · delaminated · Sep 16, 1997 · N915UP · Boeing 72727C · Spoilers
  > INSPECTION TYPE-C, NR 13 SPOILER HAS DELAMINATION AROUND ACTUATOR FITTING ON UPPER AND LOWER SURFACE. REMOVED NR 13 SPOILER AND REPLACED IAW MM 27-61-01.
- [SDR UPS97224467](https://openairdocs.org/sdr/UPS97224467.md): Chord · corroded · Sep 16, 1997 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 736862 FOUND CORROSION ON RT UPPER NLG CHORD BS 294 TO 315 RBL 11 WL 181. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED THE NLG RT UPPER CHORD AND REPLACED IAW SRM 51-20-1, 51-30-2, 51-10-2, 51-20-4 AN
- [SDR UPS97224477](https://openairdocs.org/sdr/UPS97224477.md): Rib · corroded · Sep 15, 1997 · N915UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE-C, CORROSION AT THE O/B LOWER BONDING JUMPER ON THE NR 3 K-FLAP RIB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER EO 5740-3980. REPAIRED PER SRM 57-50-03.
- [SDR UPS97224476](https://openairdocs.org/sdr/UPS97224476.md): Rib · corroded · Sep 15, 1997 · N915UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE-C, CORROSION AT THE I/B LOWER BONDING JUMPER ON NR 3 K-FLAP RIB. REMOVED CORROSION PER EO B727-5740-3980, FOUND TO BE OUT OF LIMITS PER EO B727-5740-3980. REPAIRED PER SRM 57-50-3.
- [SDR UPS97224475](https://openairdocs.org/sdr/UPS97224475.md): Skin · cracked · Sep 15, 1997 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, POSSIBLE CRACK STA 219 UPPER AFT CORNER OF R2 WINDOW. REPAIRED PER UPS EO B727-5310-0012K.
- [SDR UPS96206006](https://openairdocs.org/sdr/UPS96206006.md): Frame · misdrilled · Apr 16, 1996 · N915UP · Boeing 72727C · Fuselage Main, Frame
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2.
- [SDR UPS96206005](https://openairdocs.org/sdr/UPS96206005.md): Frame · misdrilled · Apr 16, 1996 · N915UP · Boeing 72727C · Fuselage Main, Frame
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2.
- [SDR UPS96206004](https://openairdocs.org/sdr/UPS96206004.md): Frame · misdrilled · Apr 16, 1996 · N915UP · Boeing 72727C · Fuselage Main, Frame
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHEET 1.
- [SDR UPS96206003](https://openairdocs.org/sdr/UPS96206003.md): Frame · misdrilled · Apr 16, 1996 · N915UP · Boeing 72727C · Fuselage Main, Frame
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36279 AND SRM 51-30-2.
- [SDR UPS96206002](https://openairdocs.org/sdr/UPS96206002.md): Frame · misdrilled · Apr 16, 1996 · N915UP · Boeing 72727C · Fuselage Main, Frame
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME 825.95 HAS HOLE DRILLED IN FASTENER STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHT 1.
- [SDR UPS96206007](https://openairdocs.org/sdr/UPS96206007.md): Fitting · corroded · Apr 12, 1996 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 870 RT TERMINAL SEVERLY CORRODED ON VAPOR SEAL ATTACH FLANGE WL 190 RBL 65 TO 71. CUT OUT AND BLENDED CORROSION PER SRM 51-10-6, PERFORMED HFEC INSPECTION FOR CRACKS AND CORROSION PER NDT MANUAL A, 6 51-00-00 FIG
- [SDR UPS96205999](https://openairdocs.org/sdr/UPS96205999.md): Seat Track · worn · Apr 11, 1996 · N915UP · Boeing 72727C · Fuselage, Seat/Cargo Attach Fittings
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 500 BL 0 SEAT TRACK IS WORN BEYOND LIMITS. FAB AND INSTALLED SEAT TRACK PER SRM 51-10-2.
- [SDR UPS96205998](https://openairdocs.org/sdr/UPS96205998.md): Floor Beam · unplugged hole · Apr 10, 1996 · N915UP · Boeing 72727C · Fuselage Main, Floor Beam
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FASTENER HOLE UNPLUGGED FS 1166 RBL 45 FLOOR BEAM SUPPORT CHANNEL. INSTALLED FREEZE PLUG, FAB AND INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2.
- [SDR UPS96205996](https://openairdocs.org/sdr/UPS96205996.md): Floor Beam · corrosion · Apr 10, 1996 · N915UP · Boeing 72727C · Fuselage Main, Floor Beam
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 360 WL 208, FLOOR BEAM UPPER FLANGE AFTER NUTPLATE AND CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE BEYOND LIMITS FROM RBL 4.45 TO RBL 10.45 AT THE AREAS TO BE WITHIN LIMITS PER SRM 53-10-1. REPAIRED AREA.
- [SDR UPS96205993](https://openairdocs.org/sdr/UPS96205993.md): Floor Beam · corroded · Apr 8, 1996 · N915UP · Boeing 72727C · Fuselage Main, Floor Beam
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE CORROSION WAS FOUND TO BE BEYOND LIMITS PER SRM 53-10-1, AT STA 560 WL 208 FROM LBL 50 TO LBL 60. REMOVED AND REPLACED FLOOR BEAM UPPER FLANGE PER SRM 53-10-8 FIG 5.
- [SDR UPS96205995](https://openairdocs.org/sdr/UPS96205995.md): Bracket · cracked · Apr 4, 1996 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CABIN FLOOR BEAM SUPPORT BRACKET IS CRACKED AT THE UPPER EDGE TWO PLACES, BS 1130 AND RBL 44. REMOVED AND FABRICATED PART PER DRW 65-45373, ALODINED AND PRIMED PER SRM 51-10-2, AND INSTALLED PER SRM 51-10-1 AND
- [SDR UPS96206001](https://openairdocs.org/sdr/UPS96206001.md): Stringer · corrosion · Apr 3, 1996 · N915UP · Boeing 72727C · Fuselage Main, Longeron/Stringer
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT EXTERNAL FUEL TANK AT WS 224 TO 230 STR 1 REQUIRES REPAIR DUE TO CORROSION BEYOND LIMITS. SPLICED STR 1 AT STA 209 TO TERMINATING END, FUEL LEAK CHECK GOOD IAW MM 28-00-00.
- [SDR UPS96205951](https://openairdocs.org/sdr/UPS96205951.md): Angle · cracked · Apr 3, 1996 · N915UP · Boeing 72727C · Wing Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING AT ACCESS PANEL JUST I/B OF NR 4 K-FLAP I/B END BULKHEAD ANGLE AT LOWER END HAS NUMEROUS CRACKS AT FASTENERS. REMOVED CRACKED CHORD, FABRICATED CHORD PER SRM 57-20-2, ALODINED AND PRIMED PER SRM 51-10-2 AND I
- [SDR UPS96205949](https://openairdocs.org/sdr/UPS96205949.md): Angle · cracked · Apr 2, 1996 · N915UP · Boeing 72727C · Aerodynamic Fairings
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FAIRING SUPPORT ANGLE HAS CRACK AT GROUND. REMOVED FASTENER AND TERMINATED CRACK AT RIVET HOLE. INSTALLED DOUBLER PER SRM 53-50-1 AND 51-40-3.
- [SDR UPS96206000](https://openairdocs.org/sdr/UPS96206000.md): Floor Beam · corrosion · Mar 30, 1996 · N915UP · Boeing 72727C · Fuselage Main, Floor Beam
  > WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE AFTER CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE BEYOND LIMITS. REMOVED DAMAGED SECTION OF FLOOR BEAM FAB AND INSTALLED PER SRM 53-10-8 FIG F, STA 680 RBL 26 TO 44 RBL 60 WL 208.

Next page: https://openairdocs.org/deregistered/N915UP-2006-08-23/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 = 'N915UP' AND deregistration_id = 'N915UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N915UP-2006-08-23/reports

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