# Service difficulty reports: N929UP, cancelled Aug 23, 2006

A list on [N929UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N929UP-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 4 · 163 reports

- [SDR UPS03240133](https://openairdocs.org/sdr/UPS03240133.md): Skin · cracked · Jan 20, 2003 · N929UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SP CRACK FOUND ON FUSELAGE ABOVE # 1 ENGINE STATION 1183 STRINGER 4L-8L REMOVED PREVIOUS REPAIR DOUBLER AND DAMAGED AREA I.A.W. SRM.53-30-3 FIG. 26 & 24, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I.A.W. SRM. 53-30-3 FIG. 26 & 24 AT
- [SDR UPS01236772](https://openairdocs.org/sdr/UPS01236772.md): Light · will not test · Sep 5, 2001 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AT COCKPIT DOOR WILL NOT TEST. R&R LIGHT ASSY WITH NEW BATTERIES, OPS CHECK K PER MM 33-50-01.
- [SDR UPS01236729](https://openairdocs.org/sdr/UPS01236729.md): Light · defective · Aug 29, 2001 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:IN COCKPIT EMERGENCY LIGHT ILLUMINATED DURING FLIGHT THEN FELL OUT OF ITS CONTAINER. UNABLE TO REINSTALL. REINSTALLED EMERGENCY EXIT LIGHT ASSY TEST OK LENS SECURED.
- [SDR UPS01235445](https://openairdocs.org/sdr/UPS01235445.md): Girt Bar · inoperative · Mar 21, 2001 · N929UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE: PREFLT, ESCAPE SLIDE GIRT BAR STOW HOOKS DO NOT HOLD BAR IN PLACE WHEN SLIDE IS DISENGAGED. REMOVED MAIN ENTRY DOOR SLIDE COVER FOR REPAIR. INSTALLED MAIN ENTRY DOOR EVACUATION SLIDE AND COVER IAW B727 MM 25-60-03.
- [SDR UPS01235325](https://openairdocs.org/sdr/UPS01235325.md): Slide · out of position · Mar 21, 2001 · N929UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE IN ESCAPE SLIDE FELL OUT. RE-PACKED EMERGENCY ESCAPE SLIDE.
- [SDR UPS01234910](https://openairdocs.org/sdr/UPS01234910.md): Battery · discharged · Feb 7, 2001 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS FOUND INOP, PRE-FLT. FOUND BATTERIES WEAK, INSTALLED NEW BATTERIES. OPS CKS NORMAL.
- [SDR UPS01234820](https://openairdocs.org/sdr/UPS01234820.md): Light · malfunctioned · Jan 30, 2001 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:IN, COCKPIT DOOR EMERGENCY LIGHT VERY DIM. OPS CHECK COCKPIT EMERGENCY LIGHTS WITH BOTH THE SWITCH AT THE ASSY AND THE EMERGENCY LIGHT ARM/DISARM ON THE P4. NO DEFECTS NOTED.
- [SDR UPS01234786](https://openairdocs.org/sdr/UPS01234786.md): Light · inoperative · Jan 21, 2001 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:IN, NEITHER EMERGENCY ENT LIGHT WORKING. RESET SWITCH, OPS CHECK IAW MM 33-50-01. OPS CHECK NORMAL.
- [SDR UPS01234726](https://openairdocs.org/sdr/UPS01234726.md): Angle · cracked · Jan 2, 2001 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CK FWD LAV FLOOR INTERCOSTAL ANGLE HAS 2 CRACKS AT STA 320 RIGHT SIDE 20 INCHES FROM RIGHT HAND WALL. INSTALLED DOUBLER REPAIR, ACCOMPLISHED IN ACCORDANCE WITH SRM 51-40-2. REPLACED UPPER ANGLE IN ACCORDANCE WITH SRM 52-30-2.
- [SDR UPS01234728](https://openairdocs.org/sdr/UPS01234728.md): Structure · cracked · Dec 31, 2000 · N929UP · Boeing 72722C · Wing Miscellaneous Structure
  > INSPECTION TYPE:C CK RIGHT WING L/E CAVITY AT STA 330.6, EXISTING REPAIR ANGLE IS CRACKED. REMOVED AND REPLACED REPAIR ANGLE IN ACCORDANCE WITH SRM 51-30-2.
- [SDR UPS00234108](https://openairdocs.org/sdr/UPS00234108.md): Light · inoperative · Oct 12, 2000 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULBS, OPS OK. A/C OK FOR SERVICE.
- [SDR UPS00233409](https://openairdocs.org/sdr/UPS00233409.md): Light · inoperative · Jul 21, 2000 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT ABOVE CABIN ENTRANCE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD.
- [SDR UPS00231344](https://openairdocs.org/sdr/UPS00231344.md): Skin · delaminated · Jan 17, 2000 · N929UP · Boeing 72722C · Nose/Tail Landing Gear
  > NLG RT FIXED STRUT DOOR DELAMINATED AT LEADING EDGE. AREA OF DELAMINATION APROX.375 SQ INCH ON LEADING EDGE OF DOOR. REPAIRED PER SRM 51-40-09 PG 25 ITEM TRANSFERRED TO DMI LOG D185351.
- [SDR UPS00231343](https://openairdocs.org/sdr/UPS00231343.md): Floor Pan · cracked · Jan 17, 2000 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > CRACK AT RT MLG FLOOR PAN STA 910. TRANSFERRED TO DMI D185355 AIRCRAFT TO FERRY TO MIA FOR REPAIR.
- [SDR UPS00231342](https://openairdocs.org/sdr/UPS00231342.md): Web · cracked · Jan 17, 2000 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > CRACK AT RT MLG WEB BS STA 910. TRANSFER TO DMI D185355 AC TO FERRY TO MIA FOR REPAIR. ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPLISHED AND A/C IS IN SAFE OPERATING CONDITION FOR FERRY.
- [SDR UPS99230982](https://openairdocs.org/sdr/UPS99230982.md): Flap Track · cracked · Oct 23, 1999 · N929UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:N/A LH INBD FLAP OUTBD TRACK CRACKED ***MRR FILED AS OPEN***
- [SDR UPS99230015](https://openairdocs.org/sdr/UPS99230015.md): Support · corroded · Jun 28, 1999 · N929UP · Boeing 72722C · Aileron Control System
  > INSPECTION TYPE:C CORROSION UNDER AFT AILERON LOCKOUT GEARBOX ATTACH BOLT (NUTSIDE) ON L/W O/B AILERON LOCKOUT FITTING. REPLACED AILERON LOCKOUT FITTING (SUPPORT) PER ER NR 99-5678.
- [SDR UPS99229986](https://openairdocs.org/sdr/UPS99229986.md): Seat Track · corroded · Jun 25, 1999 · N929UP · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SEAT TRACK FROM BS 590 TO 605 RBL 25 WL 208 HAS CORROSION IN CHANNEL. AFTER THE CORROSION REMOVAL PROCESS, FOUND THE AREA TO GO BEYOND ALLOWABLE LIMITS.
- [SDR UPS99229982](https://openairdocs.org/sdr/UPS99229982.md): Skin · corroded · Jun 24, 1999 · N929UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION (C53-113-01.01-01) ON SKIN BS 687 TO 694 LBL 25 JUST ABOVE STR 26 LT SIDE. AFTER REMOVAL OF CORROSION, FOUND THE SKIN TO GO BEYOND ALLOWABLE DAMAGE. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTAL
- [SDR UPS99229985](https://openairdocs.org/sdr/UPS99229985.md): Skin · cracked · Jun 21, 1999 · N929UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CRACK INDICATED NOTED AROUND 2 FASTENER HEADS AT LT BS 243.7, WL 198.5 AND WL 200. AREAS MARKED IN RED. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-3, SRM 51-30-02 AND MM 51-20-151.
- [SDR UPS99230014](https://openairdocs.org/sdr/UPS99230014.md): Skin · cracked · Jun 19, 1999 · N929UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CRACK INDICATION NOTED AROUND TWO FASTENER HEADS AT RT BS 235.8 WL 228 AND 229, MARKED IN RED. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER AND INSTALLED. WORK DONE IAW 53-30-03, 51-10-2, AND 51-30-2
- [SDR UPS99229984](https://openairdocs.org/sdr/UPS99229984.md): Skin · cracked · Jun 19, 1999 · N929UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CRACK INDICATION NOTED AT BS 243.7 WL 229 AROUND FASTENER HEAD MARKED IN RED (RIGHT HAND SIDE. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-03, 51-30-02 AND MM 51-20-151.
- [SDR UPS99229983](https://openairdocs.org/sdr/UPS99229983.md): Chord · corrosion · Jun 18, 1999 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NOSE MID CHORD BS 349, LBL 15, WL 169. REMOVED CHORD, INSTALLED NEW CHORD. REPLACED WEB WITH FABRICATED WEB, WORK DONE IAW SRM 51-30-2, 53-10-2.
- [SDR UPS00231393](https://openairdocs.org/sdr/UPS00231393.md): Frame · cracked · Jan 18, 1999 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > BS 930 FRAME INBOARD AND OUTBOARD FLANGE CRACKED, FROM STRINGER 18A TO MAIN LANDING GEAR PRESSURE DECK. REPLACED BS930 FITTING, RIGHT SIDE IN ACCORDANCE WITH BOEING DRAWING 65-16336.
- [SDR UPS98226478](https://openairdocs.org/sdr/UPS98226478.md): Battery · discharged · Apr 23, 1998 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS LIGHTS, COCKPIT FWD ENTRY DOOR INOP. REMOVED AND REPLACED BOTH SETS OF BATTERIES OUT OF THE EMERGENCY EXIT LIGHT UNITS PER MM 25-60-00, OPS CHECK NORMAL AT THIS TIME.
- [SDR UPS98226476](https://openairdocs.org/sdr/UPS98226476.md): Light · inoperative · Apr 23, 1998 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE STAIR TO COCKPIT INOP (UPPER DECK). REMOVED AND REPLACED COCKPIT STAIR EMERGENCY LIGHT, OPS CHECK GOOD (P/N 51356B37) ON, (S/N 18149) ON, (S/N 33648) OFF.
- [SDR UPS96221745](https://openairdocs.org/sdr/UPS96221745.md): Slat Actuator · inoperative · Dec 12, 1996 · N929UP · Boeing 72722C · Leading Edge Slat Actuator
  > INSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32, SLAT OPS CHKS NORMAL ON GROUND (P/N 141095-9-2) (S/N 3997L) OFF, (S/N 01405BDJLMN) ON.
- [SDR UPS96221470](https://openairdocs.org/sdr/UPS96221470.md): Batteries · discharged · Oct 25, 1996 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES.
- [SDR UPS96221055](https://openairdocs.org/sdr/UPS96221055.md): Batteries · discharged · Sep 5, 1996 · N929UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE N/A EMERGENCY LIGHT INOP. REPLACED BATTERIES.
- [SDR UPS96220572](https://openairdocs.org/sdr/UPS96220572.md): Frame · cracked · Jun 29, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE SI, RT 870 FORGING SPLICE AT STR 9 HAS 5 CRACKED HOLES AND ONE 2 TO 3 INCH CRACK IN RADIUS OF AFT FLANGE. REPAIRED BS 870 FORGING BY REMOVING DAMAGED SECTION AND SPLICING A NEW SECTION IN PLACE IAW B727-5310-3057 AND B727-5310-8080A.
- [SDR UPS96220571](https://openairdocs.org/sdr/UPS96220571.md): Frame · cracked · Jun 29, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE SI, LT 870 FORGING STR 9 HAS ONE CRACKED HOLE AND CRACK IN RADIUS ON FWD FLANGE. INSTALLED EXTERNAL DOUBLERS AND REPAIRED IAW EO B727-5310-3057E AND EO B727-5310-8080A.
- [SDR UPS96220576](https://openairdocs.org/sdr/UPS96220576.md): Floor · corroded · Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Floor Panel
  > INSPECTION TYPE SI, CORROSION ON FLOOR STA 209 TO 231 LBL 6 TO 18 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED FLOOR PANEL PER SRM 51-40-2, 51-10-2 MM 51-20-151, SRM 51-30-02.
- [SDR UPS96220575](https://openairdocs.org/sdr/UPS96220575.md): Floor Beam · corroded · Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE SI, CORROSION ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE AT NUTCLIP HOLES STA 680 WL 207.5 LBL 5, 29, 33, 35 RBL 4, 37, 59, 60, AREAS MARKED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2363.
- [SDR UPS96220574](https://openairdocs.org/sdr/UPS96220574.md): Floor Beam · corroded · Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE SI, DOUBLE HOLES IN LOWER FLANGE OF THE 1110 FLOOR BEAM LBL 19 RBL 45 WL 201. DURING REMOVAL OF CEILING SUPPORT FOUND FLOOR BEAM TO BE CORRODED OUT OF LIMITS PER SRM 53-10-01. REPAIRED PER EO 96-2357.
- [SDR UPS96220573](https://openairdocs.org/sdr/UPS96220573.md): Floor Beam · corroded · Jun 28, 1996 · N929UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE SI, CORROSION AT NUTPLATES IN FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 640 WL 207.5 LBL 38 AREAS MARKED. FOUND FLOOR BEAM AT BS 640 LBL 38 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 640 LBL 38 PER UPS EO 727-53-1780.
- [SDR UPS96220535](https://openairdocs.org/sdr/UPS96220535.md): Frame · corroded · Jun 27, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT BS 304 WL 175 LBL 44. CLEANED AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER EO 96-2371.
- [SDR UPS96220539](https://openairdocs.org/sdr/UPS96220539.md): Expansion Link · corroded · Jun 26, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 LBL 25 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED EXPANSION LINK PER SRM 51-10-1, 51-30-2.
- [SDR UPS96220538](https://openairdocs.org/sdr/UPS96220538.md): Expanson Link · corroded · Jun 26, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPLACED EXPANSION LINK PER SRM 51-10-1, 51-30-5, 51-30-8, 51-30-2, 51-20-4.
- [SDR UPS96220529](https://openairdocs.org/sdr/UPS96220529.md): Web · corroded · Jun 21, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CRACK ON FLOOR WEB STA 480 WL 208 LBL 55 AREA MARKED. WHILE WORKING CRACK FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-1. REPAIRED PER SRM 51-40-2, 51-10-2 AND M/M 51-21-151.
- [SDR UPS96220527](https://openairdocs.org/sdr/UPS96220527.md): Support · corroded · Jun 21, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON COCKPIT ENTRY SUPPORT STA 304 WL 208 LBL 4,9 RBL 3,8 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FARICATED REPLACEMENT SUPPORT PER SRM 51-20-1, 51-30-8 AND 51-30-5. REPLACED FLOOR SUPPORT AT BS 304 LBL 1
- [SDR UPS96220525](https://openairdocs.org/sdr/UPS96220525.md): Stiffener · corroded · Jun 21, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 25 WL 208 IN CENTER CHANNEL AT FWD END. FOUND EXPANSION LINK TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED EXPANSION LINK AT BS 740 TO 760 RBL 25 WL 208 PER SRM 51-10-1, 51-30-4,
- [SDR UPS96220547](https://openairdocs.org/sdr/UPS96220547.md): Channel · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON HAT CHANNEL FROM BS 300 TO 342, RBL 12, WL 208. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-30-2, 53-10-1, 51-40-4.
- [SDR UPS96220546](https://openairdocs.org/sdr/UPS96220546.md): Spar · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Wing Spar
  > INSPECTION TYPE SI, CORROSION R/W UPPER REAR SPAR CHORD AT WBL 86 JUST ABOVE NR 3 ENGINE FUEL SHUTOFF VALVE. REPAIRED UPPER REAR SPAR CHORD IAW SB 727-57-0145, SRM 57-10-6 AND BOEING DRAWING 65-C19647.
- [SDR UPS96220545](https://openairdocs.org/sdr/UPS96220545.md): Frame · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE SI, CORROSION ON FRAME CHORD STA 312, RBL 43, WL 178. REMOVED AND REPLACED CHORD IAW SRM 53-10-1, 51-40-3, 51-30-2.
- [SDR UPS96220544](https://openairdocs.org/sdr/UPS96220544.md): Frame · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE SI, CORROSION ON BS 351 WEB AT RBL 37 AND 47, WL 168 BELOW DOGHOUSE FLOOR. REMOVED DAMAGED WEB SECTION AND INSTALLED NEW SECTION IAW SRM 51-40-2. ALSO, REPLACED CORRODED SHEAR TIE AT STR 24R DUE TO CORROSION OUT OF LIMITS.
- [SDR UPS96220543](https://openairdocs.org/sdr/UPS96220543.md): Stiffener · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON DOGHOUSE FLOOR SUPPORT AT BS 351, RBL 20 AND RBL 30, WL 170. REMOVED AND REPLACED STIFFENER/FLOOR SUPPORT IAW SRM 51-30-2, 53-10-1, 51-30-5.
- [SDR UPS96220542](https://openairdocs.org/sdr/UPS96220542.md): Crease Beam · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORRROSION ON STA 1176 CREASE BEAM FROM LBL 25 TO 55 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED CREASE BEAM CHORD AND REPLACED PER SRM 51-30-2.
- [SDR UPS96220541](https://openairdocs.org/sdr/UPS96220541.md): Rib · cracked · Jun 20, 1996 · N929UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE SI, NR 8 SLAT I/B TRACK SUPPORT STRUCTURE O/B RIB IS CRACKED IN 2 PLACES. REMOVED AND REPLACED NR 8 SLAT I/B TRACK SUPPORT FITTINGS AND WEBS PER SRM 51-30-2.
- [SDR UPS96220540](https://openairdocs.org/sdr/UPS96220540.md): Intercostal · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON BOTTOM OF INTERCOSTAL STA 219.8 TO STA 227 LBL 42 WL 227. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-10-2, 51-30-2, 51-20-4.
- [SDR UPS96220534](https://openairdocs.org/sdr/UPS96220534.md): Floor Support · corroded · Jun 20, 1996 · N929UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE SI, CORROSION ON LAV FLOOR SUPPORT STA 315 WL 208 RBL 17, 20, 24, 27, 30, 39 AREAS MARKED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2, 53-10-1, 51-30-5.

Next page: https://openairdocs.org/deregistered/N929UP-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 = 'N929UP' AND deregistration_id = 'N929UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N929UP-2006-08-23/reports

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