# Service difficulty reports: N212UP, cancelled Dec 4, 2003

A list on [N212UP, cancelled Dec 4, 2003](https://openairdocs.org/deregistered/N212UP-2003-12-04.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR UPS01236763](https://openairdocs.org/sdr/UPS01236763.md): Support Bracket · cracked · Aug 31, 2001 · N212UP · Boeing 727247 · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:PFLT NOSE GEAR LOCK ACTUATOR SUPPORT BRACKET IS CRACKED. SUPPORT BRACKET IS LOCATED ON AFT BULKHEAD WALL. REMOVED NOSE GEAR LOCK ACTUATOR SUPPORT BRACKET. DRILLED UP NEW SUPPORT BRACKET AS REQUIRED. INSTALLED BRACKET IAW 727 SRM 51-30-02
- [SDR UPS01235459](https://openairdocs.org/sdr/UPS01235459.md): Shear Tie · corroded · Mar 6, 2001 · N212UP · Boeing 727247 · Fuselage Main, Structure
  > INSPECTION TYPE:C. DISCOVERED SHEAR TIE AT BS 1148 LBL 10 WL 150 TO BE CORRODED SHEAR TIE FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-1 REMOVED OLD SHEAR TIE AND INSTALLED NEW SHEAR TIE PER SRM 51-30-2 AND 51-10-2
- [SDR UPS01235240](https://openairdocs.org/sdr/UPS01235240.md): Seat Track · corroded · Feb 22, 2001 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SEAT TRACK FLANGE CORRODED AT LBL 45, STA 520-529, WL 208. FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 480--BS 530 PER SRM 53-10-05 FIG 1 AND SRM 51-30-2.
- [SDR UPS00233514](https://openairdocs.org/sdr/UPS00233514.md): Connector · loose · Aug 2, 2000 · N212UP · Boeing 727247 · Drag Control Actuator
  > INSPECTION TYPE:N/A, DURING CLIMB AT FL 180 ORANGE LED LIGHT CAME ON NR 4 LED WAS OUT. SELECTED FLAP 2 DEGREE, NO GREEN LIGHT. RETRACTED FLAPS AND LIGHT EXTINGUISHED. SHORTLY THEREAFTER AMBER LIGHT ILLUM, 4-5 MIN LATER LIGHT EXTINGUISHED. AFTER CREW DEBRIE
- [SDR UPS00233471](https://openairdocs.org/sdr/UPS00233471.md): Window · stuck · Aug 1, 2000 · N212UP · Boeing 727247 · Flight Compartment Windows
  > INSPECTION TYPE:N/A, CREW PREFLIGHT - CAPTS SLIDING WINDOW STICKING. RIGGED WINDOW AND OPS NORMAL.
- [SDR UPS99231183](https://openairdocs.org/sdr/UPS99231183.md): Battery · discharged · Dec 6, 1999 · N212UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHT AT MAIN ENTRY DOOR INOP. REPLACED BATTERIES, OPS CK GOOD.
- [SDR UPS99230817](https://openairdocs.org/sdr/UPS99230817.md): Stringer · corroded · Sep 30, 1999 · N212UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C CORROSION STR 26R CORRODED BS 720F PLUS 16 740-4. REPAIRED STR 26R SRM 53-10-3, SPLICED IN NEW SECTION FROM BS 720F PLUS 5 TO BS 720F PLUS 16, AFTER BLENDING CORROSION OUT OF LIMITS.
- [SDR UPS99230816](https://openairdocs.org/sdr/UPS99230816.md): Stringer · corroded · Sep 30, 1999 · N212UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C CORROSION ON KEEL BEAM STRINGER 29L BS 950E PLUS 12 TO 950E PLUS 15 LBL 7 WL 138 (C53-113-01.06-02). REPAIRED PER ER NR 99-6148 AND 727 SRM.
- [SDR UPS99230819](https://openairdocs.org/sdr/UPS99230819.md): Seat Track · corroded · Sep 29, 1999 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C WHILE WORKING CARD 006467 UPON REMOVAL OF FLOOR PANEL BS 870-950, RBL 45-RBL 65, FOUND SEAT TRACK AT BS 900, RBL 47, WL 208 OUTBOARD FLANGE CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK IAW 51-30-02.
- [SDR UPS99230818](https://openairdocs.org/sdr/UPS99230818.md): Clip · corroded · Sep 29, 1999 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD CARGO COMPARTMENT STR CLIP BS 720F, STR 27R, RBL 15 IS CORRODED. REMOVED AND REPLACED CORRODED STR CLIP BS 720F STR 27R, RBL 15 IAW 51-30-02, 51-30-05.
- [SDR UPS99229634](https://openairdocs.org/sdr/UPS99229634.md): Door · cracked · May 17, 1999 · N212UP · Boeing 727247 · Landing Gear Doors
  > INSPECTION TYPE:N/A, RIGHT WING GEAR FLYING DOOR, FWD AND AFT OF HINGE PANEL AREA, SKIN CRACKED UNDER AND BEYOND DOUBLER. REMOVED EXISTING DOUBLER, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 52-80-2 FIG 2.
- [SDR UPS99228327](https://openairdocs.org/sdr/UPS99228327.md): Light · inop · Jan 6, 1999 · N212UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE:N/A E/E/L INOP BY CREW ENTRY DOOR R/R FWD E/E/L WITH ROBBED PART FROM A/C 910 OPS CHECK GOOD. S/N ON 2841-8 S/N OFF 6508
- [SDR UPS98227149](https://openairdocs.org/sdr/UPS98227149.md): Light · inoperative · Jul 14, 1998 · N212UP · Boeing 727247 · Landing Gear Steering System
  > INSPECTION TYPE-N/A, EMERGENCY LIGHT AT COCKPIT DOOR FAILURE. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKED OK PER MM 33-50-01.
- [SDR UPS98226017](https://openairdocs.org/sdr/UPS98226017.md): Seat Track · corrosion · Mar 4, 1998 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION (C53-224-01.05-03) ON SEAT TRACK FLANGE STA 1130-1175, LBL 45, WL 208. REMOVED OUT OF LIMITS SEAT TRACK FABRICATED AND INSTALLED NEW SEAT TRACK AND REPAIR PARTS IAW SRM 53-10-5, 51-30-2.
- [SDR UPS98226023](https://openairdocs.org/sdr/UPS98226023.md): Carriage · corroded · Mar 3, 1998 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE:SI CORROSION (C57-581-04.00-03) NR 1 FLAP CARRIAGE HAS CORROSION INSIDE OF SPINDLE CORRODED CARRIAGE WAS REMOVED SENT TO OUTSIDE VENDOR FOR REPAIR DETERMINED TO BE SERVICABLE AND REINSTALLED ON A/C IAW SRM 27-51-13.
- [SDR UPS98226020](https://openairdocs.org/sdr/UPS98226020.md): Flap Track · corroded · Mar 2, 1998 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 2 T/E FLAP TRACK CENTER AFT ATTACH MOUNT BOLT HOLE CORRODED. REMOVED CORRODED MOUNT ROUTED TO MACHINE SHOP FOR REWORK PER ER NR 98-2214, REINSTALL AFTER REWORK.
- [SDR UPS98226019](https://openairdocs.org/sdr/UPS98226019.md): Fitting · fretted · Mar 2, 1998 · N212UP · Boeing 727247 · Wing, Control Surface Attach Fittings
  > INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 4 T/E FLAP TRACK FWD ATTACH FITTING FRETTED ON INBOARD SIDE OF TRACK ATTACH POINT. REMOVED FITTING AND ROUTED TO MACHINE SHOP. FITTING REWORKED PER ER NO 98-2216.
- [SDR UPS98226018](https://openairdocs.org/sdr/UPS98226018.md): Track · corrosion · Mar 2, 1998 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 1 T/E FLAP TRACK FORWARD ATTACH FITTING ON O/B SIDE OF TRACK ATTACH FLANGE AROUND BUSHING FITTING REWORKED PER ER 98-2225.
- [SDR UPS98225871](https://openairdocs.org/sdr/UPS98225871.md): Track · corroded · Feb 19, 1998 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-SI, CORROSION (C57-581-06.00-04) NR 6 T/E FLAP TRACK SPOILER BEAM MOUNT PAD CORRODED. REMOVED CORRODED FLAP TRACK AND INSTALLED SERVICABLE FLAP TRACK IAW MM 27-51-31, REF TC NR C57-581-04-4D.
- [SDR UPS98226021](https://openairdocs.org/sdr/UPS98226021.md): Seat Track · corroded · Feb 18, 1998 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION (4-25-02) ON MAIN DECK SEAT TRACK FLANGE FASTENER HOLES, AS MARKED AT BS 595-BS 684 RBL 23, WL 208. REMOVED OUT OF LIMITS SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK AND REPAIR PARTS IAW SRM 51-10-2,
- [SDR UPS98225872](https://openairdocs.org/sdr/UPS98225872.md): Floorbeam · corroded · Feb 11, 1998 · N212UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM FASTENER HOLE BS 380, LBL 50, WL 208. MECHANICALLY REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-2, 53-10-6. REPAIRED FLOORBEAM PER SRM 53-10-8.
- [SDR UPS98226022](https://openairdocs.org/sdr/UPS98226022.md): Seat Track · corroded · Feb 10, 1998 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION (C53-224-01.00-03) ON SEAT TRACK UPPER FLANGE BS 1125-BS 1130,, LBL 55, WL 208. REMOVE CORROSION AND OUT OF LIMITS IAW SRM 53-10-1. REPLACED TRACK IAW SRM 51-30-2, SRM 51-10-1, 51-10-1, 51-10-6 AND MM 51-20-151.
- [SDR UPS98225873](https://openairdocs.org/sdr/UPS98225873.md): Intercostal · corroded · Feb 10, 1998 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-02) ON INTERCOSTAL RBL 27, BS 546, WL 147 FWD CARGO BAY. CORROSION FOUND TO BE OUT LIMITS PER SRM 53-10-1. FABRICATED PART PER SRM 51-10-3 AND INSTALLED PER SRM 51-30-2, SRM 51-40-2 AND SRM 51-10-2.
- [SDR UPS97222842](https://openairdocs.org/sdr/UPS97222842.md): Tr Link Assy · sheared bolts · May 3, 1997 · N212UP · Boeing 727247 · Engine Thrust Reverser
  > INSPECTION TYPE-N/A, ENCOUNTERED HEAVY AIRCRAFT VIBRATION THROUGH ENTIRE FLIGHT FROM DTW TO PHL. HEAVY LEFT WING WAS CORRECTED BY ROLL INPUT AND RUDDER INPUT. NR 1 ENGINE SEEMED TO HAVE LARGE PART OF PROBLEM. FOUND LOWER BUCKET OF NR 1 ENG T/R FREEWHEELING.
- [SDR UPS96221741](https://openairdocs.org/sdr/UPS96221741.md): Light · inoperative · Dec 10, 1996 · N212UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE-N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK GOOD (P/N 10-0067-9) (S/N 19703) ON, S/N 18001) OFF.
- [SDR UPS96220969](https://openairdocs.org/sdr/UPS96220969.md): Skin · delaminated · Aug 25, 1996 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 AREAS OF DISBOND UPPER SURFACE. REPAIRED PER SRM 51-40-6.
- [SDR UPS96220968](https://openairdocs.org/sdr/UPS96220968.md): Skin · delaminated · Aug 25, 1996 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > INSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 INCH AREA OF DISBOND, LOWER SURFACE. REPAIRED PER SRM 51-40-6.
- [SDR UPS96220967](https://openairdocs.org/sdr/UPS96220967.md): Shear Tie · corroded · Aug 25, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1166 BETWEEN STR 28 AND 29 LT. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE AT STA 1166 IAW SRM 51-30-1.
- [SDR UPS96220974](https://openairdocs.org/sdr/UPS96220974.md): Shear Tie · corroded · Aug 23, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01. 02-02) ON SHEAR TIE STA 1130 BETWEEN STR 28 TO 29 RT. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED. ALL WORK DONE IAW SRM 53-10-1, 53-10-4, 51-30-2, 51-10-02.
- [SDR UPS96220972](https://openairdocs.org/sdr/UPS96220972.md): Blkhd Stiffener · corrosion · Aug 23, 1996 · N212UP · Boeing 727247 · Fuselage Main, Bulkhead
  > INSPECTION TYPE-C, 740 BULKHEAD VERTICAL STIFFENER HAS CORROSION ON BOTTOM AROUND FASTENERS, RBL 25 WL 146. REMOVED CORROSION AND FOUND OUT OF LIMITS. STIFFENER WAS REMOVED AND INSTALLED NEW STIFFENER. ALL WORK ACCOMPLISHED PER SRM 53-10-11, 51-30-5, 51-20-
- [SDR UPS96220976](https://openairdocs.org/sdr/UPS96220976.md): Shear Tie · corrosion · Aug 22, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, SHEAR TIE IS CORRODED AND FOUND OUT LIMITS. WHILE REMOVING SHEAR TIE FOUND FRAME SPLICE PLATE TO BE CRACKED. RECEIVED AND INSTALLED NEW SHEAR TIE AND FABRICATED NEW FRAME SPLICE PLATE AND INSTALLED. ALL WORK ACCOMPLISHED PER SRM 51-10-6,
- [SDR UPS96220975](https://openairdocs.org/sdr/UPS96220975.md): Support · cracked · Aug 22, 1996 · N212UP · Boeing 727247 · Leading Edge Devices
  > INSPECTION TYPE-C, NR 2 SLAT I/B TRACK SUPPORT, O/B RIB IS CRACKED. REMOVED AND REPLACED NR 2 SLAT ASSY PER M/M 27-81-11.
- [SDR UPS96220973](https://openairdocs.org/sdr/UPS96220973.md): Shear Tie · corroded · Aug 22, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C530113-01.00-01) CORROSION ON SHEAR TIE AND WEB STA 600, LBL 19 TO 22 WL 146. CORROSION REMOVAL OUT OF LIMITS ON SHEAR TIE, WEB WAS WITHIN LIMITS. FABRICATED NEW SHEAR TIE AND INSTALLED. FOUND CRACKED SKIN UNDER SHEAR TIE, REM
- [SDR UPS96221031](https://openairdocs.org/sdr/UPS96221031.md): Stringer · corroded · Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8, WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 INCH BY 1 INCH AREA, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.
- [SDR UPS96220979](https://openairdocs.org/sdr/UPS96220979.md): Stringer · corroded · Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8 WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 BY 1 AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.
- [SDR UPS96220977](https://openairdocs.org/sdr/UPS96220977.md): Shear Tie · corroded · Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1070 BETWEEN STR 29 TO 30 LT. CORROSION FOUND OUT OF LIMITS, DUPLICATE WRITE-UP OF NRC 584267, ALL WORK TO BE ACCOMPLISHED ON NRC 584267.
- [SDR UPS96220990](https://openairdocs.org/sdr/UPS96220990.md): Stiffener · corroded · Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01.00-02) ON SHEAR TIE STA 969.5 WL 149 LBL 2, LBL 10 AREA MARKED. REMOVED CORROSION AND FOUND STIFFENER OUT OF LIMITS, SHEAR TIE CORROSION WAS WITH IN LIMITS. REMOVED AND REPLACED STIFFENER. ALL WORK IAW SRM 51-10-6, 5
- [SDR UPS96220980](https://openairdocs.org/sdr/UPS96220980.md): Support · corroded · Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) AROUND BOTTOM OF NUTPLATES STA 520 TO 540. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, FLOOR SUPPORT WILL BE REPLACED ON NRC 584590.
- [SDR UPS96220978](https://openairdocs.org/sdr/UPS96220978.md): Clip · corroded · Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON STRINGER CLIP STA 1040, STR 29 RT. STRINGER CLIP CORRODED OUT OF LIMITS. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-10-1, 51-19-6 AND 53-10-1.
- [SDR UPS96220971](https://openairdocs.org/sdr/UPS96220971.md): Frame · corroded · Aug 16, 1996 · N212UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE-C, CORROSION ON STIFFENER AND FRAME BS 990 WL 139 LBL 7 TO 13. REMOVED CORRODED AREA OF FRAME AND REPAIRED PER SRM 53-10-04.
- [SDR UPS96220970](https://openairdocs.org/sdr/UPS96220970.md): Shear Tie · corroded · Aug 16, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION SHEAR TIE BS 950A BETWEEN STR 28 TO 29 RT. REMOVED SHEAR TIE AND REPLACED PER SRM.
- [SDR UPS96221007](https://openairdocs.org/sdr/UPS96221007.md): Fitting · corroded · Aug 15, 1996 · N212UP · Boeing 727247 · Aileron Tabs
  > INSPECTION TYPE: C. LT INBOARD TAB FITTINGS CORRODED AILERON SIDE. REMOVED AND REPLACED LT INBOARD TAB FITTINGS AILERON SIDE PER SRM 51-30-2.
- [SDR UPS205015](https://openairdocs.org/sdr/UPS205015.md): Battery · missing · Nov 11, 1995 · N212UP · Boeing 72722C · Emergency Lighting
  > WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT IN FLIGHT DECK INOP. BATTERIES ROBBED FOR A/C 212 FROM 929. REMOVED AND REPLACED 2 BATTERIES, OPS GOOD.
- [SDR UPS504885](https://openairdocs.org/sdr/UPS504885.md): Battery · discharged · Oct 26, 1995 · N212UP · Boeing 72730C · Emergency Lighting
  > WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-101. OPS CHECKED GOOD PER MM 33-50-101.
- [SDR UPS203280](https://openairdocs.org/sdr/UPS203280.md): Switch · inop · May 19, 1995 · N212UP · Boeing 727247 · Landing Gear Position and Warning
  > WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON LT WING, I/B MID FLAP, LWR T/E CHORD AT THE I/B AFT FLAP, I/B TRACK CUTOUT, I/B AFT FLAP ACTUATING MECHANISM CUTOUT AND THE AFT FLAP I/B CENTER TRACK CUTOUT. REPLACED CHORD PER SRM 51-30-2, 51-40-4, OHM20-50-01.
- [SDR UPS203279](https://openairdocs.org/sdr/UPS203279.md): Rib · cracked · May 19, 1995 · N212UP · Boeing 727247 · Leading Edge Devices
  > WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT ACTUATOR ROD END SUPPORT RIBS, I/B AND O/B SIDES IN SLAT COVES. INSTALLED REPAIR PER SRM 51-30-2, MM27-80-00, OHM 20-50-01.
- [SDR UPS203267](https://openairdocs.org/sdr/UPS203267.md): Te Wedge · corroded · May 17, 1995 · N212UP · Boeing 727247 · Trailing Edge Flaps
  > WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON T/E WEDGE, LT WING I/B IN FLAP. INSTALLED REPAIR PER SRM 51-30-2.
- [SDR UPS203266](https://openairdocs.org/sdr/UPS203266.md): Attach Rib · cracked · May 17, 1995 · N212UP · Boeing 727247 · Leading Edge Devices
  > WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT ACTUATOR ATTACH RIB, O/B SIDE. REPLACED RIB PER SRM 51-30-2, MM 27-81-32.
- [SDR UPS203265](https://openairdocs.org/sdr/UPS203265.md): Skin · corroded · May 17, 1995 · N212UP · Boeing 727247 · Leading Edge Devices
  > WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP, JUST ABOVE THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR B727-57-1361.

## 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 = 'N212UP' AND deregistration_id = 'N212UP-2003-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N212UP-2003-12-04/reports

---
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