# Service difficulty reports: N208AU, cancelled Jul 20, 2000

A list on [N208AU, cancelled Jul 20, 2000](https://openairdocs.org/deregistered/N208AU-2000-07-20.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 · 98 reports

- [SDR P2EA99348](https://openairdocs.org/sdr/P2EA99348.md): Skin · delaminated · Dec 3, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - LEFT WING OUTBOARD FLIPPER FLAPPER DELAMINATED. DEFECT SIZE, LENGTH 9 INCH, WIDTH 7.25 INCH. REPAIRED FLIPPER FLAPPER PER COOPESA EO COO-CMP-3-57-711-99, DATED DECEMBER 7, 1999. (M)
- [SDR P2EA99344](https://openairdocs.org/sdr/P2EA99344.md): Frame · cracked · Dec 3, 1999 · N208AU · Boeing 737222 · Fuselage Main, Frame
  > SJO - C-CHECK, FRAME CRACKED AT BS 967, BETWEEN STRINGER 20/21LT. DEFECT SIZE, LENGTH 3.5 INCH, WIDTH.16 INCH, DEPTH.63 INCH. REPAIRED FUSELAGE SECTION AT BS 967, BETWEEN STRINGER 19 AND 21 LEFT PER SRM 51-40-3. (M)
- [SDR P2EA99337](https://openairdocs.org/sdr/P2EA99337.md): Seat Track · corroded · Dec 1, 1999 · N208AU · Boeing 737222 · Fuselage, Seat/Cargo Attach Fittings
  > SJO - C-CHECK, SEAT TRACK CORRODED FROM BS 360 TO BS 380, LBL 35 INCHES. DEFECT SIZE, LENGTH 8 INCHES, WIDTH 2.25 INCHES, DEPTH.200 INCHES. REPAIRED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 53-10-5, FIG 2. (M)
- [SDR P2EA99356](https://openairdocs.org/sdr/P2EA99356.md): Skin · disbonded · Nov 30, 1999 · N208AU · Boeing 737222 · Ailerons
  > SJO - DURING C-CHECK, RIGHT AILERON INBOARD TRAILING EDGE DISBONDED AT REAR SPAR AREA. REPAIRED RIGHT AILERON PER SRM 51-40-6, PAR 5. (M)
- [SDR P2EA99347](https://openairdocs.org/sdr/P2EA99347.md): Frame · cracked · Nov 30, 1999 · N208AU · Boeing 737222 · Cargo/Baggage Doors
  > SJO - FORWARD CARGO DOOR FRAME CRACKED AT AFT FRAME, DEFECT SIZE, LENGTH.750 INCH. REPAIRED FORWARD CARGO DOOR BETWEEN BEAM NR 1 AND BEAM NR 3 PER SRM 51-40-3 FIG 1. (M)
- [SDR P2EA99346](https://openairdocs.org/sdr/P2EA99346.md): Rib · cracked · Nov 30, 1999 · N208AU · Boeing 737222 · Wing Spar
  > SJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH.32 INCH. REPLACED RIB AT SS 356 OUTBOARD TRACK PER SRM 51-30-2. (M)
- [SDR P2EA99338](https://openairdocs.org/sdr/P2EA99338.md): Floorbeam · corroded · Nov 30, 1999 · N208AU · Boeing 737222 · Fuselage Main, Floor Beam
  > SJO - C-CHECK, FLOORBEAM UPPER CHORD CORRODED AT BS 344, WL 208, BETWEEN LBL 32 AND BL 0. DEFECT SIZE, LENGTH 15 INCHES, WIDTH 1.5 INCH, DEPTH.050 INCH. REPAIRED FLOORBEAM AT BS 344, BETWEEN RBL 9 INCHES AND LBL 40 INCHES PER SRM 53-10-2, FIG 7. (M)
- [SDR P2EA99334](https://openairdocs.org/sdr/P2EA99334.md): Intercostal · cracked · Nov 30, 1999 · N208AU · Boeing 737222 · Service Doors
  > SJO - FORWARD SERVICE DOOR INTERCOSTAL CRACKED AT BEAM 3. ANGLE REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2 PAGE 8. (M)
- [SDR P2EA99341](https://openairdocs.org/sdr/P2EA99341.md): Skin · cracked · Nov 29, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - C-CHECK, FUSELAGE SKIN CRACK FROM BS 764 TO BS 767 BETWEEN STRINGER 18 AND 19 LEFT. DEFECT SIZE, LENGTH 3 INCH, WIDTH.032 INCH, DEPTH.028 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 759.5 TO BS 771, BETWEEN STRINGER 18 LT AND 20 LT PER COOPESA EO CO
- [SDR P2EA99339](https://openairdocs.org/sdr/P2EA99339.md): Skin · scratched · Nov 29, 1999 · N208AU · Boeing 737222 · Electrical/Electronic Compartment Doors
  > SJO - C-CHECK, E/E DOOR WITH DEEP SCRATCHES AND MISSING MATERIAL. DEFECT SIZE, LENGTH 1.125 INCH, WIDTH.250 INCH, DEPTH.040 INCH. REPLACED DOOR SKIN PER SRM 51-10-1 PAGE 5 AND PER SRM 51-30-2. (M)
- [SDR P2EA99309](https://openairdocs.org/sdr/P2EA99309.md): Detent Arm · out of adjust · Oct 31, 1999 · N208AU · Boeing 737222 · Leading Edge Slat Control System
  > MDW - FLT 277 - FLAPS 1 THROUGH 25 SELECTED, NR 6 LEADING EDGE SLAT EXTENDS CROOKED. FLAPS 30 THROUGH 40 SELECTED, NR 6 LEADING EDGE SLAT GOES TO FULL EXTEND. ADJUSTED DETENT ARMS ON NR 6 L/E SLAT PER MM 27-81-0A. OPS CHECKS NORMAL. (X)
- [SDR P2EA99216](https://openairdocs.org/sdr/P2EA99216.md): Mechanism · out of adjust · Jun 29, 1999 · N208AU · Boeing 737222 · Leading Edge Slat Control System
  > MDW - FLT 586 - NR 6 LEADING EDGE SLAT WOULD NOT EXTEND IN FLIGHT UNTIL FLAPS 30 POSITION WAS SELECTED. ADJUSTED TENSION ON NR 6 SLAT DETENT ARMS PER MM 27-81-0. SLATS OPERATE NORMALLY. (X)
- [SDR P2EA99199](https://openairdocs.org/sdr/P2EA99199.md): Connector · loose · Jun 1, 1999 · N208AU · Boeing 737222 · AC Generation System
  > DEN - FLT 305 - EMERGENCY DECLARED (APU PREVIOUSLY DEFERRED) LANDING UNEVENTFUL AT SCHEDULED DESTINATION. LEFT ENGINE DRIVEN GENERATOR DROPPED OFF LINE IN FLIGHT AND WOULD NOT RESET. SWAPPED APU GCU WITH NR 1 ENGINE GCU. RAN NR 1 ENGINE. GENERATOR OPS CHEC
- [SDR P2EA99127](https://openairdocs.org/sdr/P2EA99127.md): Keel Beam · corroded · Mar 13, 1999 · N208AU · Boeing 737222 · Fuselage Main, Keel
  > SJO - DURING Q-CHECK, A SECTION OF THE KEEL BEAM AT BS 630, RBL 5 WAS FOUND WITH CORROSION. THE AREA WAS REPAIRED AS PER COOPESA EO C00-3-53-176-99 AND BOEING FAX NR COO-SJO-0384RR. (M)
- [SDR P2EA99091](https://openairdocs.org/sdr/P2EA99091.md): Bolt · worn · Mar 1, 1999 · N208AU · Boeing 737222 · Engine Mount Section
  > SJO - DURING Q-CHECK, THE NR 2 ENGINE, AFT MOUNT ATTACH BOLT, WAS FOUND WITH WEAR. NR 2 ENGINE AFT MOUNT ATTACH BOLT REPLACED IAW MM 71-21-11. (M)
- [SDR P2EA99083](https://openairdocs.org/sdr/P2EA99083.md): Skin · damaged · Feb 26, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, A SKIN REPAIR AT BS 500A, STRINGER 26R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3, FIGURE 16. (M)
- [SDR P2EA99101](https://openairdocs.org/sdr/P2EA99101.md): Panel · delaminated · Feb 25, 1999 · N208AU · Boeing 737222 · Wing, Plate/Skin
  > SJO - DURING Q-CHECK, THE RIGHT WING FIXED TRAILING EDGE PANEL, P/N 65-70947-24 WAS FOUND DELAMINATED. THE PANEL WAS REPAIRED IW EO NR COO-CMP-3-57-159-99. (M)
- [SDR P2EA99100](https://openairdocs.org/sdr/P2EA99100.md): Skin · delaminated · Feb 25, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, THE LEFT WING NR 2 TRAILING EDGE SLAT WAS FOUND WITH DELAMINATION. THE SLAT WAS REPAIRED IAW EO NR COO-CMP-3-57-149-99. (M)
- [SDR P2EA99111](https://openairdocs.org/sdr/P2EA99111.md): Skin · delaminated · Feb 24, 1999 · N208AU · Boeing 737222 · Ailerons
  > SJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M)
- [SDR P2EA99097](https://openairdocs.org/sdr/P2EA99097.md): Skin · delaminated · Feb 24, 1999 · N208AU · Boeing 737222 · Spoilers
  > SJO - DURING Q-CHECK, FLIGHT SPOILER NR 3 WAS FOUND WITH DELAMINATION. FLIGHT SPOILER REPAIRED AS PER COOPESA EO NR COO-CMP-3-57-150-00. (M)
- [SDR P2EA99092](https://openairdocs.org/sdr/P2EA99092.md): Bolts · worn · Feb 24, 1999 · N208AU · Boeing 737222 · Engine Mount Section
  > SJO - DURING Q-CHECK, NR 2 ENGINE, FORWARD MOUNT THRUST LINKS ATTACH BOLTS FOUND WITH WEAR. REPLACED ATTACH BOLTS AS PER MM 71-20-11. (M)
- [SDR P2EA99089](https://openairdocs.org/sdr/P2EA99089.md): Bolt · worn · Feb 24, 1999 · N208AU · Boeing 737222 · Engine Mount Section
  > SJO - DURING Q-CHECK, ENGINE NR 1 FORWARD MOUNT THRUST LINK ATTACH BOLTS FOUND WITH WEAR. BOLTS REPLACED AS PER MM 71-20-11. (M)
- [SDR P2EA99118](https://openairdocs.org/sdr/P2EA99118.md): Mechanism · corroded · Feb 23, 1999 · N208AU · Boeing 737222 · Service Doors
  > SJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. REWORKED BEARING BORE AND MOUNTING HOLES AS PER OHM 52-46-05. (M)
- [SDR P2EA99117](https://openairdocs.org/sdr/P2EA99117.md): Bearing · corroded · Feb 23, 1999 · N208AU · Boeing 737222 · Service Doors
  > SJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER OHM 52-46-06. (M)
- [SDR P2EA99106](https://openairdocs.org/sdr/P2EA99106.md): Skin · delaminated · Feb 23, 1999 · N208AU · Boeing 737222 · Ailerons
  > SJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M)
- [SDR P2EA99084](https://openairdocs.org/sdr/P2EA99084.md): Bulkhead Chord · cracked · Feb 23, 1999 · N208AU · Boeing 737222 · Fuselage Main, Bulkhead
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE BS 178 PRESSURE BULKHEAD, FORWARD SIDE, LOWER HORIZONTAL CHORD. CRACK WAS REPAIRED IAW SRM 51-40-4 FIGURE 1. (M)
- [SDR P2EA99126](https://openairdocs.org/sdr/P2EA99126.md): Support · worn · Feb 22, 1999 · N208AU · Boeing 737222 · Engine Thrust Reverser
  > SJO - DURING Q-CHECK, THE NR 1 ENGINE THRUST REVERSER, RIGHT ACTUATOR SUPPORT WAS WORN TO LIMITS. THE ACTUATOR SUPPORT WAS REPLACED IAW SRM 51-10-1. (M)
- [SDR P2EA99107](https://openairdocs.org/sdr/P2EA99107.md): Skin · cracked · Feb 22, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, LFEC DETECTED A CRACK IN A FASTENER HOLE AT BS 492.4, BETWEEN STRINGERS 23 AND 24 RIGHT. THE AREA WAS REPAIRED AS PER COOPESA EO NR COO-2-53-157-99 AND BOEING FAX NR COO-SJO-99-0319. (M)
- [SDR P2EA99125](https://openairdocs.org/sdr/P2EA99125.md): Firewall · worn · Feb 21, 1999 · N208AU · Boeing 737222 · Nacelle/Pylon, Bulkhead/Firewall
  > SJO - DURING Q-CHECK, THE NR 2 ENGINE PYLON FORWARD FIREWALL WAS FOUND WORN. THE FIREWALL PANEL WAS REPAIRED AS PER COOPESA EO NR 3-54-189-99 AND BOEING FAX COO-SJO-99-0389. (M)
- [SDR P2EA99124](https://openairdocs.org/sdr/P2EA99124.md): Intercostal · corroded · Feb 21, 1999 · N208AU · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, A STIFFENER AND INTERCOSTAL IN THE E/E COMPARTMENT BETWEEN BS 294.5 AND BS 312 AT STRINGER WERE FOUND WITH CORROSION. THE INTERCOSTAL AND STIFFENER WERE REPLACED AS PER SRM 51-30-2. (M)
- [SDR P2EA99099](https://openairdocs.org/sdr/P2EA99099.md): Bulkhead Web · cracked · Feb 21, 1999 · N208AU · Boeing 737222 · Fuselage Main, Bulkhead
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE WEB OF THE PRESSURE BULKHEAD AT BS 294.5 BETWEEN STRINGER 27 AND 28 RT IN THE E/E COMPARTMENT. WEB SECTION WAS REPAIRED IAW EO NR COO-3-53-146-99 AND BOEING FAX NR COO-SJO-99-0293. (M)
- [SDR P2EA99085](https://openairdocs.org/sdr/P2EA99085.md): Rib · cracked · Feb 21, 1999 · N208AU · Boeing 737222 · Wing, Rib/Bulkhead
  > SJO - DURING Q-CHECK, A RIB WAS FOUND CRACKED IN THE RIGHT WING INTERNAL AREA AT WS 505 UPPER FLANGE. THE CRACK WAS REPAIRED IAW SRM 57-10-7 FIG 1. (M)
- [SDR P2EA99123](https://openairdocs.org/sdr/P2EA99123.md): Frame · cracked · Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, Frame
  > SJO - DURING Q-CHECK, THE BS 685 RIGHT FRAME FITTING WAS FOUND CRACKED. THE CRACK WAS REPAIRED AS PER BOEING FAX NR COO-SJO-99-0388RR AND COOPESA EO NR COO-3-53-155-99. (M)
- [SDR P2EA99119](https://openairdocs.org/sdr/P2EA99119.md): Skin · cracked · Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, THE L1 DOOR CUT OUT LOWER AFT CORNER OUTER SKIN WAS FOUND CRACKED. THE SKIN WAS REPAIRED FROM BS 322 TO 355 IAW SB 53-1083 REV 3, PART IV AND DRAWING NR 65C27253. (M)
- [SDR P2EA99098](https://openairdocs.org/sdr/P2EA99098.md): Floorbeam · cracked · Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, Floor Beam
  > SJO - DURING Q-CHECK, THE UPPER FLANGE OF THE FLOORBEAM AT BS 668.75, LBL 25 WAS FOUND CRACKED. REPAIRED FLOORBEAM AS PER COOPESA EO NR COO-3-53-154-99 AND BOEING FAX NR COO-SJO-98-0993RR. (M)
- [SDR P2EA99122](https://openairdocs.org/sdr/P2EA99122.md): Skin · corroded · Feb 19, 1999 · N208AU · Boeing 737222 · Wing, Plate/Skin
  > SJO - DURING Q-CHECK, THE RIGHT WING OUTBOARD MID-FLAP SKIN AT WS 497 WAS BULGED. REPAIRED SKIN AS PER BOEING FAX COO-SJO-99-0330RR. (M)
- [SDR P2EA99116](https://openairdocs.org/sdr/P2EA99116.md): Mechanism · corroded · Feb 19, 1999 · N208AU · Boeing 737222 · Passenger/Crew Doors
  > SJO - DURING Q-CHECK, THE L2 DOOR HANDLE MECHANISM HOUSING HAD CORROSION AT LOWER TORQUE TUBE BEARING HOLE. THE HOLE AND BUSHING WERE REWORKED IAW OHM 52-16-03. (M)
- [SDR P2EA99115](https://openairdocs.org/sdr/P2EA99115.md): Skin · cracked · Feb 19, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, INBOARD MID FLAP LE SKIN AT INBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX COO-SJO-99-0279RR. (M)
- [SDR P2EA99114](https://openairdocs.org/sdr/P2EA99114.md): Skin · cracked · Feb 19, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, OUTBOARD MIDFLAP LE SKIN AT OUTBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX NR COO-SJO-99-0279RR. (M)
- [SDR P2EA99105](https://openairdocs.org/sdr/P2EA99105.md): Skin · worn · Feb 19, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, THE SKIN ON THE LEADING EDGE OF THE RIGHT WING OUTBOARD FOREFLAP WAS FOUND WITH WEAR. THE SKIN WAS REPAIRED FROM WSL 498 TO 505 AS PER SRM 57-50-40- FIG 1. (M)
- [SDR P2EA99104](https://openairdocs.org/sdr/P2EA99104.md): Rib · cracked · Feb 19, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, LEFT WING OUTBOARD MID FLAP INTERNAL LE RIB AT WBL 298 WAS FOUND CRACKED. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA99103](https://openairdocs.org/sdr/P2EA99103.md): Rib · cracked · Feb 19, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, THE LEFT INBOARD MID FLAP STRUCTURE, FOREFLAP CENTER TRACK SUPPORT FITTING RIB (INBOARD) WAS CRACKED AT TWO PLACES. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA99093](https://openairdocs.org/sdr/P2EA99093.md): Stringer · corroded · Feb 19, 1999 · N208AU · Boeing 737222 · Fuselage Main, Longeron/Stringer
  > SJO - DURING Q-CHECK, A REPAIR LOCATED AT BS 767, STRINGER 9L WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 6. (M)
- [SDR P2EA99080](https://openairdocs.org/sdr/P2EA99080.md): Skin · damaged · Feb 19, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 727A, STRINGER 8R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND A PERMANENT REPAIR WAS INSTALLED AS PER SRM 53-30-3 FIGURE 6. (M)
- [SDR P2EA99895](https://openairdocs.org/sdr/P2EA99895.md): Cargo Track · corroded · Feb 18, 1999 · N208AU · Boeing 737222 · Fuselage, Seat/Cargo Attach Fittings
  > SJO - DURING Q-CHECK, THE FORWARD CARGO COMPARTMENT CARGO TRACK AT BS 468, RBL 14, WAS FOUND WITH CORROSION. THE TRACK WAS REPAIRED AS PER SRM 53-10-5 FIG 5. (M)
- [SDR P2EA99121](https://openairdocs.org/sdr/P2EA99121.md): Splice · cracked · Feb 18, 1999 · N208AU · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, THE STRINGER SPLICE AT BS 359, STRINGER 14L WAS FOUND CRACKED. THE STRINGER SPLICE WAS REPLACED AS PER SRM 51-10-1 PAGE 5. (M)
- [SDR P2EA99112](https://openairdocs.org/sdr/P2EA99112.md): Stringer · corroded · Feb 18, 1999 · N208AU · Boeing 737222 · Fuselage Main, Longeron/Stringer
  > SJO - DURING Q-CHECK, TO VERIFY SRM COMPLIANCE, A REPAIR AT BS 1016 STRINGER 18L WAS REMOVED FOR INVESTIGATION. THE AREA WAS CLEANED, INSPECTED, AND REPAIRED AS PER COOPESA EO NR COO-3-53-152-99. (M)
- [SDR P2EA99110](https://openairdocs.org/sdr/P2EA99110.md): Web · cracked · Feb 18, 1999 · N208AU · Boeing 737222 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE NLG WHEEL WELL UPPER WEB AT BS 278, RBL 10. THE UPPER WEB WAS REPAIRED IAW COOPESA EO NR COO-SJO-99-0267. (M)
- [SDR P2EA99109](https://openairdocs.org/sdr/P2EA99109.md): Skin · cracked · Feb 18, 1999 · N208AU · Boeing 737222 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE RIGHT WING INBOARD MIDFLAP, LE SKIN AT WBL 87.75. CRACK REPAIRED IAW BOEING FAX COO-SJO-99-0280. (M)
- [SDR P2EA99102](https://openairdocs.org/sdr/P2EA99102.md): Rib · cracked · Feb 18, 1999 · N208AU · Boeing 737222 · Wing, Rib/Bulkhead
  > SJO - DURING Q-CHECK, RIGHT WING, UPPER CHANNEL OF THE LE RIB AT WS 213 WAS FOUND CRACKED. THE CHANNEL WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M)

Next page: https://openairdocs.org/deregistered/N208AU-2000-07-20/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 = 'N208AU' AND deregistration_id = 'N208AU-2000-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N208AU-2000-07-20/reports

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