# Service difficulty reports: N210UP, cancelled Aug 9, 2002

A list on [N210UP, cancelled Aug 9, 2002](https://openairdocs.org/deregistered/N210UP-2002-08-09.md).

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

- [SDR UPS01235925](https://openairdocs.org/sdr/UPS01235925.md): Stringer · corroded · May 1, 2001 · N210UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, FUSELAGE SKIN AT BS 1010 S29 HAS BULGE AT RIVET HEAD. REMOVED FASTENERS FOR ACCESS INSPECTED AREA. FOUND CORROSION BEYOND LIMITS PER SRM PER 51-30-2. CLEANED AREA AND REPLACED STRINGER AS PER SRM 53-10-3 FIG 1.
- [SDR UPS01235924](https://openairdocs.org/sdr/UPS01235924.md): Skin · corroded · May 1, 2001 · N210UP · Boeing 727247 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, FUSE SKIN BS 1010, S-28R HAS BULGE AT RIVET. CORROSION FOUND BEYOND LIMITS. REMOVED CORROSION IAW SRM 53-30-3, CUT OUT AREA AND INSTALLED DOUBLER IAW SRM 53-30-3.
- [SDR UPS01235091](https://openairdocs.org/sdr/UPS01235091.md): Regulator · inoperative · Feb 27, 2001 · N210UP · Boeing 727247 · Crew Oxygen System
  > INSPECTION TYPE:N/A, O2 REGULATOR AT F/O POSITION WILL NOT INDICATE FLOW DURING MASK TEST. *S/D* REMOVED AND REPLACED F/O''S REGULATOR O2, OPS CHECKED AND LEAK CHECKED GOOD.
- [SDR UPS01234826](https://openairdocs.org/sdr/UPS01234826.md): Battery Pack · discharged · Feb 1, 2001 · N210UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE:IN, COCKPIT EMER EXIT LIGHT WILL NOT COME ON DURING TEST. REMOVED AND REPLACED BATTER PACK, OPS CHECK GOOD.
- [SDR UPS01234828](https://openairdocs.org/sdr/UPS01234828.md): Light · inoperative · Jan 31, 2001 · N210UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE:IN, BATTERIES REMOVED FROM EMERGENCY EXIT LIGHT. REPLACED COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD.
- [SDR UPS01234822](https://openairdocs.org/sdr/UPS01234822.md): Battery Pack · inoperative · Jan 31, 2001 · N210UP · Boeing 727247 · Emergency Lighting
  > INSPECTION TYPE:PFLT, EMERGENCY EXIT LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK.
- [SDR UPS00233774](https://openairdocs.org/sdr/UPS00233774.md): Downlock Switch · out of adj · Sep 19, 2000 · N210UP · Boeing 727247 · Landing Gear Position and Warning
  > INSPECTION TYPE:N/A, AIR TURNBACK TO MIA DUE TO NOSE GEAR UNLOCKED LIGHT ILLUM. UPON GEAR RETRACT (GREEN LIGHT ALSO REMAINED ILLUM THE WHOLE TIME). FOUND NOSE LANDING GEAR DOWN AND LOCK SW OUT OF ADJUSTMENT. ADJUSTED THE SAME PER B727 MM 32-60-00, OPS CKD GO
- [SDR UPS00231515](https://openairdocs.org/sdr/UPS00231515.md): Stringer · cracked · Feb 3, 2000 · N210UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, STR 1 BS 620, HOLE CRACKED AT REMOVED STRINGER CLIP LOCATION. REPAIRED STRINGER PER SRM.
- [SDR UPS00231387](https://openairdocs.org/sdr/UPS00231387.md): Frame · corroded · Jan 16, 2000 · N210UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE:C, WHILE WORKING NRC 051193, FOUND CORROSION ON FRAME BS 600, RBL 8 WL 153. REPAIRED FRAMED PER SRM 53-10-2, 53-10-4, 51-30-2, MM 51-20-131.
- [SDR UPS00231380](https://openairdocs.org/sdr/UPS00231380.md): Stringer Clip · cracked · Jan 14, 2000 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C STRINGER CLIP CRACKED AT BS 660 STR5L AND STR 7L. REPLACED STRINGER CLIPS IAW SRM 51-30-2.
- [SDR UPS00231390](https://openairdocs.org/sdr/UPS00231390.md): Stringer · corroded · Jan 13, 2000 · N210UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON STR28R BS 565 WL 148 RBL 8. REPAIRED STRINGER IAW SRM'S 53-10-3, 51-30-05, 51-30-2, MM 51-20-151 AND SRM 51-20-4.
- [SDR UPS00231389](https://openairdocs.org/sdr/UPS00231389.md): Web · corroded · Jan 13, 2000 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION (C53-113-01.00-01), WEB BS560-580 WL 148 RBL 8. REPAIRED PER SRM'S 51-10-3, 51-30-5, 51-30-6, 51-20-4, 51-30-2.
- [SDR UPS00231388](https://openairdocs.org/sdr/UPS00231388.md): Skin · corroded · Jan 13, 2000 · N210UP · Boeing 727247 · Leading Edge Devices
  > INSPECTION TYPE:C, WHILE WORKING NRC 051378 (WINGS 75), FOUND CORROSION TO BE OUT OF LIMITS ON NR 3 K-FLAP. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.
- [SDR UPS00231386](https://openairdocs.org/sdr/UPS00231386.md): Skin · cracked · Jan 12, 2000 · N210UP · Boeing 727247 · Leading Edge Devices
  > INSPECTION TYPE:C, NR 4 SLAT UPPER SURFACE SKIN IS CRACKED AT O/B GUIDEHOOK UPPER FASTENER. REPAIRED PER SRM 57-50-3 FIG 10.
- [SDR UPS99229684](https://openairdocs.org/sdr/UPS99229684.md): Light · inoperative · May 27, 1999 · N210UP · Boeing 727247 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD PER MM 33-50-01, P/N ON AND OFF 10-0067-9 S/N OFF 28158 S/N ON 28163.
- [SDR UPS99229683](https://openairdocs.org/sdr/UPS99229683.md): Light · inoperative · May 27, 1999 · N210UP · Boeing 727247 · Emergency Lighting
  > MAIN ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, P/N ON AND OFF 10-00 67-9 S/N OFF 5200 S/N ON 27025. OPS CHECK GOOD PER MM 33-50-01.
- [SDR UPS98227538](https://openairdocs.org/sdr/UPS98227538.md): Floorbeam · corrosion · Aug 26, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON LOWER CHORD OF BS 1130 FLOORBEAM BETWEEN LBL 2 AND RBL 51 WL 201. REPAIRED CORROSION WITH NEW PART IAW ENGINEERING REPAIR NR 98-2760.
- [SDR UPS98227535](https://openairdocs.org/sdr/UPS98227535.md): Floorbeam · corroded · Aug 26, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-04.00-01) ON MAIN DECK FLOORBEAM UPPER CHORD TOP FLANGE BS 1130, RBL 22, WL 208 AT SMALL DRILLED HOLE (NR 40 BIT). REPAIRED PER ENGINEERING REPAIR NR 98-2760.
- [SDR UPS98227534](https://openairdocs.org/sdr/UPS98227534.md): Floorbeam · corroded · Aug 26, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-04.00-01) ON MAIN DECK FLOORBEAM UPPER CHORD AT BS 1130, RBL 18, WL 208 UNDER SHEAR WEB. REPAIRED IAW ENGINEERING REPAIR NR 98-2760.
- [SDR UPS98227588](https://openairdocs.org/sdr/UPS98227588.md): Fitting · corroded · Aug 24, 1998 · N210UP · Boeing 727247 · Spoilers
  > INSPECTION TYPE-SI, NR 11 SPOILER FITTING CORRODED AT MOUNT HOLE. REPLACED PER SRM 51-30-2.
- [SDR UPS98227587](https://openairdocs.org/sdr/UPS98227587.md): Stringer · corroded · Aug 24, 1998 · N210UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-SI, CORROSION (C53-111-01-3D) ON STRINGER BS 1016 WL 150 RBL 28. STRINGER REPAIRED BS 1006 TO BS 1016 PER 727 SRM 53-10-3 AND 51-30-2.
- [SDR UPS98227567](https://openairdocs.org/sdr/UPS98227567.md): Seat Track · corrosion · Aug 24, 1998 · N210UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION BETWEEN SEAT TRACK AND EXPANSION LINK FLANGES BS 850 LBL 45 WO L208. REPLACED SEAT TRACK ON EXPANSION LINK PER 727 SRM 51-30-2, 51-20-151 51-30-5, 51-10-1.
- [SDR UPS98227569](https://openairdocs.org/sdr/UPS98227569.md): Seat Track · corrosion · Aug 20, 1998 · N210UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SI CORROSION ON SEAT TRACK UPPER AND LOWER FLANGES STA 1070-1130 RBL 45 WL 208. REMOVED CORRODED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-2, 53-10-5.
- [SDR UPS98227568](https://openairdocs.org/sdr/UPS98227568.md): Frame · corrosion · Aug 19, 1998 · N210UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE:SI CORROSION (C53-111-03.00-01) ON FRAME WEB AT BS 294.5 WL 167-169 RBL 35-40 FABRICATED NEW WEB AND INSTALLED WORK DONE IAW SRM 53-10-1, 51-40-2 51-10-2, AND 51-30-2.
- [SDR UPS98227540](https://openairdocs.org/sdr/UPS98227540.md): Seat Track · corrosion · Aug 19, 1998 · N210UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION ON EXPANSION LINK UPPER SEAT TRACK O/B FLANGE UNDER STRAP AFT OF BS 740 LBL 45 WL 208. REMOVED CORRODED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 51-30-2.
- [SDR UPS98227539](https://openairdocs.org/sdr/UPS98227539.md): Fitting · corroded · Aug 19, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION ON LONGITUDINAL BEAM AT I/B FLOOR SUPPORT FITTING ATTACH POINT BS 850 LBL 45 WL 208. REMOVED CORRODED PART, INSTALLED NEW PART IAW SRM 51-30-2, 51-30-5.
- [SDR UPS98227479](https://openairdocs.org/sdr/UPS98227479.md): Support · corroded · Aug 17, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION ON (C53-224-01.05-01) FLOOR SUPPORT BS 312 TO 322 LBL 30 WL 208. REPLACED FLOOR SUPPORT PER 727 SRM 51-20-4 AND 51-30-2.
- [SDR UPS98227478](https://openairdocs.org/sdr/UPS98227478.md): Clip · corroded · Aug 17, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, FWD BAY STR 23L, BS 540 HAS A CRACKED AND CORRODED STRINGER CLIP. REPLACED STRINGER CLIP PER 727 SRM 51-30-2.
- [SDR UPS98227477](https://openairdocs.org/sdr/UPS98227477.md): Support · corroded · Aug 17, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOOR SUPPORT BS 344 LBL 30 WL 208. REPLACED FLOOR SUPPORT PER 727 SRM 51-30-2 AND 51-20-4.
- [SDR UPS98227474](https://openairdocs.org/sdr/UPS98227474.md): Floorbeam · corroded · Aug 17, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) FLOORBEAM BS 720D LBL 5 TO 25 WL 208. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-10-02, 53-10-8, 51-40-02, 51-30-02.
- [SDR UPS98227476](https://openairdocs.org/sdr/UPS98227476.md): Seat Track · corroded · Aug 16, 1998 · N210UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 655 TO 668, LBL 45, WL 208. REMOVED CORROSION FROM SEAT TRACK BS 668 TO 655, FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK BS 480 TO 685, ALL WORK PERFORMED IAW SRM 51-10-06, 53-10-01, 51-30-02, 53-10-05.
- [SDR UPS98227431](https://openairdocs.org/sdr/UPS98227431.md): Crease Beam · corroded · Aug 14, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SI CORROSION (C53-224-01.00-01), ON CREASE BEAM AT BS 418 RBL 60 WL 208. REPLACED CREASE BEAM PER 727 SRM 51-30-2.
- [SDR UPS98227430](https://openairdocs.org/sdr/UPS98227430.md): Floorbeam · corroded · Aug 13, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI CORROSION (C53-224-01.05-01), ON FLOORBEAM BS 344 LBL 60 RBL 5 WL 208. REMOVED CORROSION FOUND OUT OF LIMITS REPAIRED IAW SRM 53-10-01, 53-10-08, 51-30-02, 51-20-31.
- [SDR UPS98227429](https://openairdocs.org/sdr/UPS98227429.md): Floorbeam · corroded · Aug 13, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) FLOOR BEAM BS 680 WL 208 LBL 2-15. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED PER 51-10-6, 53-10-1, 51-30-02, 53-10-08, 51-10-02, 51-20-15 SRM.
- [SDR UPS98227472](https://openairdocs.org/sdr/UPS98227472.md): Floorbeam · corroded · Aug 11, 1998 · N210UP · Boeing 727247 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 312 LBL 3 TO 25 WL 208. REMOVED OUT OF LIMITS CORRODED FLOORBEAM, FABRICATED NEW FLOORBEAM AND REPAIR PARTS IAW SRM 53-10-8, 51-30-2, INSTALLED PARTS IAW SRM 51-30-2.
- [SDR UPS98227432](https://openairdocs.org/sdr/UPS98227432.md): Frame · corroded · Aug 11, 1998 · N210UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE:SI WHILE WORKING CUST CARD 816656 (INTERIOR 105), FOUND CORROSION ON FRAME AT BS 377 RBL 60 WL 209. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS AS PER SRM 51-40-3.
- [SDR UPS98227536](https://openairdocs.org/sdr/UPS98227536.md): Seat Track · corroded · Aug 6, 1998 · N210UP · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION BETWEEN SEAT TRACK AND EXPANSION LINK FLANGES AT BS 850 RBL 25 WL 208. REPLACED SEAT TRACK AND EXPANSION LINK AS PER SRM 51-30-5.
- [SDR UPS98227473](https://openairdocs.org/sdr/UPS98227473.md): Keel Beam · corroded · Aug 4, 1998 · N210UP · Boeing 727247 · Fuselage Main, Keel
  > INSPECTION TYPE-SI, SEVERAL RIVETS SHOW SIGNS OF CORROSION EMANATING FROM FASTENER HOLES, THIRD HOLE AFT ON KEEL BEAM, LOWER FWD CHORD, (MARKED) (C53-123-01.03-01) STA 750 BL 0. LOWER CHORD FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW LO
- [SDR UPS98227475](https://openairdocs.org/sdr/UPS98227475.md): Crease Beam · corroded · Jul 31, 1998 · N210UP · Boeing 727247 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-06-1B) ON MOP SILL OUTER FLANGE AT LEFT HAND AFT SERVICE DOOR CUTOUT BS 1048 TO 1058 LBL 66 WL 209. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW CREASE BEAM PER SRM 51-30-5, MM 51-20-21, AND SRM 51
- [SDR UPS97222069](https://openairdocs.org/sdr/UPS97222069.md): Stringer · corroded · Feb 15, 1997 · N210UP · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C, WHILE WORKING FUSELAGE 36 FOUND CORRODED STRINGER 26R BS 1146 TO 1183 FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-10-03. REPAIRED STRINGER PER SRM 51-10-1, 51-10-2, 51-30-2, 53-10-3.
- [SDR UPS97222070](https://openairdocs.org/sdr/UPS97222070.md): Frame · corroded · Feb 7, 1997 · N210UP · Boeing 727247 · Fuselage Main, Frame
  > INSPECTION TYPE-C, CORROSION ON FRAME OUT OF LIMITS STA 950B LBL 9 WL 138. FABRICATED AND INSTALLED NEW ANGLE AND DOUBLERS ALL IAW SRM 53-10-2, 51-30-3.
- [SDR UPS97221923](https://openairdocs.org/sdr/UPS97221923.md): Hinge Lug · cracked · Feb 1, 1997 · N210UP · Boeing 727247 · Leading Edge Devices
  > NR 1 KREUGER FLAP HAS CRACK ON CENTER HINGE LUG AT BOTTOM BOLT HOLE. REPLACED NR 1 KREUGER FLAP IAW MM 27-81-01. SYS OP/C NORMAL. LANDING LIGHT OP/C NORMAL.
- [SDR UPS205568](https://openairdocs.org/sdr/UPS205568.md): Support · cracked · Feb 24, 1996 · N210UP · Boeing 727247 · Passenger/Crew Doors
  > CREW REPORTED, AFTER TAKEOFF LOUD AIR LEAK COMING FROM FWD ENT DOOR. FOUND CRACK AROUND A LIGHTENING HOLE SUPPORT AREA FOR TORQUE TUBE LATCH ARM FWD UPPER CORNER OF DOOR. NO TYPICAL SRM REPAIR ADDRESSING EITHER REPLACING THE DOOR OR AN EO FOR REPAIR.
- [SDR UPS805130](https://openairdocs.org/sdr/UPS805130.md): Eel · inoperative · Dec 6, 1995 · N210UP · Boeing 727247 · Emergency Lighting
  > WHILE ON GROUND IN YHM, MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT L1 CABIN ENTRY DOOR DOES NOT TEST. EMERGENCY EXIT LIGHT ASSY REMOVED AND REPLACED AS PER M/M 33-50-01, OPS CHK GOOD.
- [SDR UPS204934](https://openairdocs.org/sdr/UPS204934.md): Eel Assy · malfunctioned · Nov 4, 1995 · N210UP · Boeing 727247 · Emergency Lighting
  > CREW REPORTED, EMERGENCY EXIT LIGHTS VERY DIM. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD.
- [SDR UPS204919](https://openairdocs.org/sdr/UPS204919.md): Battery · discharged · Oct 30, 1995 · N210UP · Boeing 727247 · Emergency Lighting
  > WHILE ON THE GROUND, MAINTENANCE FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES ON THE COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-101. PERFORMED ADJ/TEST IAW MM 33-50-01 GRD, OPS CK'D GOOD.
- [SDR UPS204027](https://openairdocs.org/sdr/UPS204027.md): Fitting · cracked · Aug 7, 1995 · N210UP · Boeing 727247 · Wing Miscellaneous Structure
  > WHILE IN FOR C-CHECK, MAINTENANCE FOUND LOWER IB T/E SUPPORT BEAM FOR NR 8 SPOILER SUPPORT FITTING IS CRACKED AND HAS SEVERAL LOOSE FASTENERS. REMOVED CRACKED SUPPORT FITTING, FABRICATED REPAIR PARTS IAW B 727-5710-7222-A.
- [SDR UPS204026](https://openairdocs.org/sdr/UPS204026.md): Rib · cracked · Aug 7, 1995 · N210UP · Boeing 727247 · Leading Edge Devices
  > WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 SLAT RIB STRUCTURE BUILD UP FOR ACTUATOR ROD END MOUNT IS CRACKED. REMOVED DAMAGED SLAT AND REPLACED WITH SERVICEABLE SLAT PER MM 27-81-11.
- [SDR UPS204025](https://openairdocs.org/sdr/UPS204025.md): Rib · cracked · Aug 7, 1995 · N210UP · Boeing 727247 · Trailing Edge Flaps
  > WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT O/B FOREFLAP CENTER LINK TO TRACK ATTACH BOLT IS CHAFING ON MIDFLAP CUTOUT RIB. FOUND CHAFED AREA TO HAVE CRACK REMOVED AND REPLACED RIB PER SRM 51-30-2.
- [SDR UPS202159](https://openairdocs.org/sdr/UPS202159.md): Eel · inoperative · Feb 1, 1995 · N210UP · Boeing 727247 · Emergency Lighting
  > MAINTENANCE REPORTED EXIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.

## 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 = 'N210UP' AND deregistration_id = 'N210UP-2002-08-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N210UP-2002-08-09/reports

---
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