# Service difficulty reports: N214UP, cancelled May 6, 2003

A list on [N214UP, cancelled May 6, 2003](https://openairdocs.org/deregistered/N214UP-2003-05-06.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 2 · 91 reports

- [SDR UPS01237375](https://openairdocs.org/sdr/UPS01237375.md): Battery · discharged · Dec 20, 2001 · N214UP · Boeing 7272A1 · Emergency Lighting
  > INSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD.
- [SDR UPS01237193](https://openairdocs.org/sdr/UPS01237193.md): Bulkhead · corroded · Oct 30, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, Bulkhead
  > INSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT STANDING ON AIRSTAIRS JUST O/B OF NR 2 ENGINE GENERATOR FEEDER CABLES NUMEROUS FASTENERS ARE CORRODED AS IS A STIFFENER. CLEANED AND TREATED
- [SDR UPS01236767](https://openairdocs.org/sdr/UPS01236767.md): Window · cracked · Sep 5, 2001 · N214UP · Boeing 7272A1 · Flight Compartment Windows
  > INSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11.
- [SDR UPS01236152](https://openairdocs.org/sdr/UPS01236152.md): Battery · discharged · Jun 19, 2001 · N214UP · Boeing 7272A1 · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES.
- [SDR UPS01235403](https://openairdocs.org/sdr/UPS01235403.md): Terminal · damaged · Mar 23, 2001 · N214UP · Boeing 7272A1 · Door Warning System
  > AMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED PER MEL 52-4 AND COMPLIED WITH DMP VERIFYING THAT MAIN CARGO DOOR CLOSED AND LOCKED PRIOR TO DEPARTURE. ITEM DEFERRED M211761 PLACARD INSTLD
- [SDR UPS01235239](https://openairdocs.org/sdr/UPS01235239.md): Skin · cracked · Feb 15, 2001 · N214UP · Boeing 7272A1 · Trailing Edge Flaps
  > INSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. REPAIRED PER SRM 57-50-4.
- [SDR UPS01235023](https://openairdocs.org/sdr/UPS01235023.md): Stringer · corroded · Jan 10, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1.0 X.5 X.020 INCH FROM ORIG THICKNESS OF.090 INCH OUT OF LIMITS PER SRM 53-10-1, SRM 53-10-2 SRM 5
- [SDR UPS01235022](https://openairdocs.org/sdr/UPS01235022.md): Shear Tie · corroded · Jan 7, 2001 · N214UP · Boeing 7272A1 · Fuselage Main, Structure
  > INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-151.
- [SDR UPS99230991](https://openairdocs.org/sdr/UPS99230991.md): Battery Pack · discharged · Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency Lighting
  > INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS99230990](https://openairdocs.org/sdr/UPS99230990.md): Battery Pack · discharged · Oct 26, 1999 · N214UP · Boeing 7272A1 · Emergency Lighting
  > INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS99230241](https://openairdocs.org/sdr/UPS99230241.md): Skin · corroded · Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148 AND REPAIRED IAW ER NR 99-5802 AND SRM 53-30-03 FIG 3A.
- [SDR UPS99230239](https://openairdocs.org/sdr/UPS99230239.md): Keel Beam · corroded · Jul 28, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Keel
  > INSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WITH NEW SEGMENT IAW ER 99-5790.
- [SDR UPS99230240](https://openairdocs.org/sdr/UPS99230240.md): Stringer · corroded · Jul 27, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1153 AND REPLACED WITH NEW STRINGER IAW SRM 51-40-03, 51-10-1, 51-30-02, DRW NR 65-16349.
- [SDR UPS99230238](https://openairdocs.org/sdr/UPS99230238.md): Clip · corroded · Jul 26, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519). REMOVED CORRODED T-CLIP AND REPLACED WITH NEW T-CLIP IAW 51-10-1 AND 51-30-02.
- [SDR UPS99230172](https://openairdocs.org/sdr/UPS99230172.md): Shear Tie · corroded · Jul 25, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. REPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148 PER SRM 53-10-1, 51-30-2, 53-10-4, 51-10-2.
- [SDR UPS99230171](https://openairdocs.org/sdr/UPS99230171.md): Shear Tie · corroded · Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND REPAIRED IAW SRM 53-10-04 FIG 15.
- [SDR UPS99230170](https://openairdocs.org/sdr/UPS99230170.md): Seat Track · corroded · Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 960.
- [SDR UPS99230156](https://openairdocs.org/sdr/UPS99230156.md): Crease Beam · cracked · Jul 23, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, WL 209, LBL 64 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF CREASE BEAM FROM BS 1157 TO BS 1177, FABRICATED NEW CREASE BEAM, REPAI
- [SDR UPS99230157](https://openairdocs.org/sdr/UPS99230157.md): Splice · corroded · Jul 22, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 148. REMOVED AND REPLACED STR SPLICE BS 1000 STR 29R, RBL 6, WL148, WITH NEW STR SPLICE.
- [SDR UPS99230178](https://openairdocs.org/sdr/UPS99230178.md): Crease Beam · corroded · Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLISHED ON NRC 973389 DO TO OTHER DEFECTS REPAIR WILL COVER FROM 1138-1176.*
- [SDR UPS99230177](https://openairdocs.org/sdr/UPS99230177.md): Crease Beam · corroded · Jul 12, 1999 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLISHED ON NRC 973397, WHICH ENCOMPASS THIS AREA. REPAIR GOES FROM BS 1159-1176.
- [SDR UPS99230112](https://openairdocs.org/sdr/UPS99230112.md): Frame · cracked · Jul 6, 1999 · N214UP · Boeing 7272A1 · Fuselage Main, Frame
  > INSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCESSED AREA AT 1183 FRAME AND REPAIRED FRAME IAW SB B727-53-0210.
- [SDR UPS99229972](https://openairdocs.org/sdr/UPS99229972.md): Window · shattered · Jun 25, 1999 · N214UP · Boeing 7272A1 · Flight Compartment Windows
  > INSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-71762-39) (S/N 1429) OFF. (P/N 5-71762-39) (S/N 84-H -3-5-116) ON. HEAT CONTROL (P/N 1231-2) (S/N 9
- [SDR UPS98225724](https://openairdocs.org/sdr/UPS98225724.md): Skin · corroded · Feb 5, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 14L AND 16L. CORROSION OUT OF LIMITS IAW SRM 53-30-3. REPAIRED SKIN AROUND PERIF OF LT SIDELIGHT I
- [SDR UPS98225711](https://openairdocs.org/sdr/UPS98225711.md): Rib · corroded · Feb 2, 1998 · N214UP · Boeing 7272A1 · Vertical Stabilizer, Spar/Rib
  > INSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2.
- [SDR UPS98225664](https://openairdocs.org/sdr/UPS98225664.md): Bottle Pin · corroded · Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing, Fuselage Attach Fittings
  > INSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLACED ON AOG (BOEING)
- [SDR UPS98225663](https://openairdocs.org/sdr/UPS98225663.md): Rear Spar · cracked · Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing Spar
  > INSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314.
- [SDR UPS98225709](https://openairdocs.org/sdr/UPS98225709.md): Support · corroded · Jan 22, 1998 · N214UP · Boeing 7272A1 · Trailing Edge Flaps
  > INSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIRES REPLACEMENT I/B AND O/B AT RADIUS BLOCKS. REPLACED NR 7 FLAP TRACK FITTING IAW SRM 51-10-1 WILL
- [SDR UPS98225710](https://openairdocs.org/sdr/UPS98225710.md): Support · corroded · Jan 18, 1998 · N214UP · Boeing 7272A1 · Trailing Edge Flaps
  > INSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND REPLACED NR 4 FLAP TRACK FWD FITTING IAW MM 32-11-51.
- [SDR UPS98225496](https://openairdocs.org/sdr/UPS98225496.md): Sill · cracked · Jan 16, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2.
- [SDR UPS98225497](https://openairdocs.org/sdr/UPS98225497.md): Beam · corroded · Jan 15, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONGITUDINAL BEAM IAW SRM 51-10-1, 51-30-2.
- [SDR UPS98225495](https://openairdocs.org/sdr/UPS98225495.md): Stringer · cracked · Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.
- [SDR UPS98225478](https://openairdocs.org/sdr/UPS98225478.md): Skin · corroded · Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1090 STR 28R IAW SRM 53-30-3.
- [SDR UPS98225477](https://openairdocs.org/sdr/UPS98225477.md): Chord · corroded · Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED FLOORBEAM PER SRM 53-10-8.
- [SDR UPS98225473](https://openairdocs.org/sdr/UPS98225473.md): Angle · corroded · Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON LWR SUPPORT ANGLE IAW 51-10-06, 53-10-1. REMOVED AND REPLACED ANGLE IA
- [SDR UPS98225472](https://openairdocs.org/sdr/UPS98225472.md): Seat Track · corroded · Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 720D TO BS 720F LBL 25 IAW SRM 53-10-5.
- [SDR UPS98225470](https://openairdocs.org/sdr/UPS98225470.md): Frame · cracked · Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Frame
  > INSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 IAW UPS EO B727-5310-5474.
- [SDR UPS98225469](https://openairdocs.org/sdr/UPS98225469.md): Seat Track · corroded · Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25. CORROSION REWORK OUT OF LIMTS IAW SRM 53-10-1. MECHANICAL DAMAGE WITHIN LIMITS IAW SRM 53-10-1. SEAT TRACK WAS REMOVED AND REPLACED IAW
- [SDR UPS98225468](https://openairdocs.org/sdr/UPS98225468.md): Floorbeam · corroded · Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED 950 FLOORBEAM RBL 25 TO 65 IAW TRAMCO/BFG EWO 98-2012 (UPS FILE 727-53-1983).
- [SDR UPS98225467](https://openairdocs.org/sdr/UPS98225467.md): Lug · corroded · Jan 12, 1998 · N214UP · Boeing 7272A1 · Leading Edge Devices
  > INSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.
- [SDR UPS98225466](https://openairdocs.org/sdr/UPS98225466.md): Floorbeam · corroded · Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8.
- [SDR UPS98225465](https://openairdocs.org/sdr/UPS98225465.md): Seat Track · corroded · Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SEAT TRACK, FABRICATED, INSTALLED REPAIR SEAT TRACK IAW SRM 53-10-5.
- [SDR UPS98225464](https://openairdocs.org/sdr/UPS98225464.md): Seat Track · corroded · Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-05, 51-30-08, MM 51-20-31, OHM 20-50-01
- [SDR UPS98225463](https://openairdocs.org/sdr/UPS98225463.md): Link · corroded · Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED LINK PER SRM 51-20-1, 51-10-1, 51-30-2.
- [SDR UPS98225404](https://openairdocs.org/sdr/UPS98225404.md): Frame · corroded · Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Frame
  > INSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
- [SDR UPS98225403](https://openairdocs.org/sdr/UPS98225403.md): Floorbeam · corroded · Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 200. REMOVED DAMAGED SECTION AND REPAIRED LOWER FLANGE IAW SRM 53-10-8.
- [SDR UPS98225462](https://openairdocs.org/sdr/UPS98225462.md): Floorbeam · corroded · Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.
- [SDR UPS98225461](https://openairdocs.org/sdr/UPS98225461.md): Floorbeam · corroded · Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS PER SRM 53-10-8.
- [SDR UPS98225460](https://openairdocs.org/sdr/UPS98225460.md): Seat Track · dented · Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUND TO BE WITHIN LIMITS AFTER CLEAN UP. HOWEVER, DENTS WERE FOUND ON BS 490 AND BS 571 WHICH WERE OUT OF LIMITS. SEAT TRACK WAS REPLACED FRO
- [SDR UPS98225397](https://openairdocs.org/sdr/UPS98225397.md): Floorbeam · corroded · Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor Beam
  > INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER ANGLE AND FILLER IAW SRM 53-10-8.

Next page: https://openairdocs.org/deregistered/N214UP-2003-05-06/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 = 'N214UP' AND deregistration_id = 'N214UP-2003-05-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N214UP-2003-05-06/reports

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