# Service difficulty reports: N214AU, cancelled Jul 20, 2000

A list on [N214AU, cancelled Jul 20, 2000](https://openairdocs.org/deregistered/N214AU-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 · 57 reports

- [SDR F3LA99129](https://openairdocs.org/sdr/F3LA99129.md): Heat Duct · cracked · Oct 13, 1999 · N214AU · Boeing 737201 · Engine Anti-Icing System
  > MLI - DURING CLIMB-OUT FROM MDW, FLIGHT CREW REPORTED THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT WAS DIVERTED TO MOLINE, IL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CRACKED FUEL HEAT DUCT AND CHECKED OK. (M)
- [SDR F3LA99113](https://openairdocs.org/sdr/F3LA99113.md): Wire · broken · Aug 12, 1999 · N214AU · Boeing 737201 · Light System Wiring
  > DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN GROUND WIRE AFT OF BATTERY PACK CONNECTION. TC: 90,747. (X)
- [SDR F3LA99112](https://openairdocs.org/sdr/F3LA99112.md): Wire · broken · Aug 11, 1999 · N214AU · Boeing 737201 · Light System Wiring
  > DEN - FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE AT D9022P AND CHECKED OKAY. TC: 90,745. (X)
- [SDR F3LA99111](https://openairdocs.org/sdr/F3LA99111.md): Battery Pack · discharged · Aug 10, 1999 · N214AU · Boeing 737201 · Emergency Lighting
  > DEN - FLT 317 - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS FLICKERED IN-FLIGHT. MAINTENANCE RECHARGED BATTERY PACKS AND OPERATIONAL CHECKED OKAY. PART TC: 90,740. (X)
- [SDR F3LA99110](https://openairdocs.org/sdr/F3LA99110.md): Battery Charger · failed · Aug 9, 1999 · N214AU · Boeing 737201 · Emergency Lighting
  > DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING DID NOT EXTINGUISH WHEN TESTED. MAINTENANCE REPLACED AFT SEAT BATTERY CHARGING UNIT. TC: 9,073. (X)
- [SDR F3LA99080](https://openairdocs.org/sdr/F3LA99080.md): Bearing · out of limits · Jun 16, 1999 · N214AU · Boeing 737201 · Main Landing Gear Attach Section
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN RIGHT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT.057. MAINTENANCE REPLACED RIGHT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7007. (M)
- [SDR F3LA99078](https://openairdocs.org/sdr/F3LA99078.md): Bearing · out of limits · Jun 16, 1999 · N214AU · Boeing 737201 · Main Landing Gear Attach Section
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN LEFT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT.052. MAINTENANCE REPLACED LEFT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7006. (M)
- [SDR F3LA99028](https://openairdocs.org/sdr/F3LA99028.md): Battery Pack · discharged · Apr 4, 1999 · N214AU · Boeing 737201 · Emergency Lighting
  > DEN - UPON WALK AROUND MAINTENANRE REPORTED EMERGENCY LIGHT ACTIVATION CABLE LOOSE AT SLIDE COVER ON L1 DOOR, EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK. SECURED CABLE ASSY AND CHECKED OK. (M)
- [SDR F3LA99020](https://openairdocs.org/sdr/F3LA99020.md): Wire · broken · Feb 22, 1999 · N214AU · Boeing 737201 · Light System Wiring
  > PHX - DURING C-CHECK INSPECTION, REPORTED CABIN EMERGENCY LIGHTING AND FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT OVERWING BATTERY PCK PER WDM 33-51-01. (M)
- [SDR F3LA99019](https://openairdocs.org/sdr/F3LA99019.md): Wire · broken · Feb 22, 1999 · N214AU · Boeing 737201 · Light System Wiring
  > PHX - DURING C-CHECK INSPECTION, REPORTED BROKEN WIRE IN L1 DOOR EXIT LIGHT. MAINTENANCE REPAIRED BROKEN WIRE PER SPWM 20-30-12. (M)
- [SDR F3LA99016](https://openairdocs.org/sdr/F3LA99016.md): Bracket · cracked · Feb 22, 1999 · N214AU · Boeing 737201 · Pneumatic Distribution System
  > PHX - DURING C-CHECK INSPECTION, REPORTED FASTENER MISSING AND CRACKED MOUNT FLANGE ON 8TH STAGE BLEED DUCT. MAINTENANCE INSTALLED FASTENER AND REPAIRED BRACKET/FLANGE PER 727 OHM 36-10-3, PAGE 5. (M)
- [SDR F3LA99010](https://openairdocs.org/sdr/F3LA99010.md): Frame · cracked · Feb 22, 1999 · N214AU · Boeing 737201 · Fuselage Main, Frame
  > PHX - DURING C-CHECK INSPECTION, REPORTED A 4 INCH CRACK IN FRAME AT BS 380, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-4, FIG 1. (M)
- [SDR F3LA99009](https://openairdocs.org/sdr/F3LA99009.md): Skin · cracked · Feb 22, 1999 · N214AU · Boeing 737201 · Wing, Plate/Skin
  > PHX - DURING C-CHECK INSPECTION, REPORTED DENT AND CRACK ON RIGHT WING OUTBOARD SIDE OF PYLON, FLAP SIDE LOAD ROLLER AND CORROSION UNDER FLAP ROLLER WEAR STRIP. MAINTENANCE REMOVED DAMAGED SECTION. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-3 AN
- [SDR F3LA99007](https://openairdocs.org/sdr/F3LA99007.md): Bulkhead Frame · cracked · Feb 22, 1999 · N214AU · Boeing 737201 · Fuselage Main, Bulkhead
  > PHX - DURING C-CHECK INSPECTION, REPORTED FORWARD CARGO RIGHT FORWARD BULKHEAD FRAME CRACKED. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-3, FIG 1. (M)
- [SDR F3LA99022](https://openairdocs.org/sdr/F3LA99022.md): Fitting · broken · Feb 21, 1999 · N214AU · Boeing 737201 · Ailerons
  > PHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED ATTACH ANGLE AND REPAIRED PER SRM 51-30-2, 51-20-3, AND 51-20-1 AND 51-40-4. (M)
- [SDR F3LA99018](https://openairdocs.org/sdr/F3LA99018.md): Stiffeners · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Engine Thrust Reverser
  > PHX - DURING C-CHECK INSPECTION, REPORTED WEB STIFFENERS ON FORWARD EDGE OF NR 2 ENGINE THRUST REVERSER COWL CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, FIG 1. (M)
- [SDR F3LA99017](https://openairdocs.org/sdr/F3LA99017.md): Housing · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Turbine Section
  > PHX - DURING C-CHECK INSPECTION, REPORTED 9 INCH CRACK ON NR 6 TURBINE BEARING EXHAUST CASE HOUSING BETWEEN 9-12 O'CLOCK POSITION ON NR 1 ENIGNE. MAINTENANCE REPAIRED PER JT8D MM 72-54, PARAGRAPH 4. (M)
- [SDR F3LA99015](https://openairdocs.org/sdr/F3LA99015.md): Skin · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Trailing Edge Flaps
  > PHX - DURING C-CHECK INSPECTION REPORTED A 1.25 INCH CRACK ON LEFT WING TRAILING EDGE INBOARD MIDFLAP INBOARD EDGE FLAP REAR SPAR T-CHORD. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-4, FIG 1 51-40-3 AND 51-30-02.
- [SDR F3LA99014](https://openairdocs.org/sdr/F3LA99014.md): Door · bent · Feb 21, 1999 · N214AU · Boeing 737201 · Landing Gear Doors
  > PHX - DURING C-CHECK INSPECTION, REPORTED LEFT MAIN GEAR AFT OUTER CORNER OF INBOARD DOOR BENT AND BULGING. MAINTENANCE REMOVED FASTENERS, CLEANED AREA, RESEALED AND INSTALLED NEW FASTENERS PER SRM 51-20-4 AND 51-30-2. (M)
- [SDR F3LA99013](https://openairdocs.org/sdr/F3LA99013.md): Rib · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Fuselage Main, Frame
  > PHX - DURING C-CHECK INSPECTION, RERPORTED CRACK ON FORWARD SIDE OF RIB AT BS 505. MAINTENANCE REPLACED RIB PER SRM 51-10-1, PAGE 5, AND 51-30-2. (M)
- [SDR F3LA99012](https://openairdocs.org/sdr/F3LA99012.md): Skin · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Wing, Plate/Skin
  > PHX - DURING C-CHECK INSPECTION, REPORTED A.125 INCH CRACK ON RIGHT WING UPPER WING SKIN AT NR 5 SPOILER CENTER HINGE. MAINTENANCE REPAIRED PER SRM 57-30-1, FIG 4, DETAIL 7. (M)
- [SDR F3LA99011](https://openairdocs.org/sdr/F3LA99011.md): Wedge · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Trailing Edge Flaps
  > PHX - DURING C-CHECK INSPECTION, REPORTED 1 INCH BY 1.5 INCH CRACK IN LEFT WING TRAILING EDGE FLAP WEDGE. MAINTENANCE REPAIRED PER SRM 57-50-1, FIG 16, DETAIL 15. (M)
- [SDR F3LA99006](https://openairdocs.org/sdr/F3LA99006.md): Frame · cracked · Feb 21, 1999 · N214AU · Boeing 737201 · Fuselage Main, Frame
  > PHX - DURING C-CHECK INSPECTION, REPORTED A 4.5 INCH CRACK IN FRAME AT BS 360, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-40-3, AND 53-10-4. (M)
- [SDR F3LA99008](https://openairdocs.org/sdr/F3LA99008.md): Skin · cracked · Feb 20, 1999 · N214AU · Boeing 737201 · Wing, Plate/Skin
  > PHX - DURING C-CHECK INSPECTION, REPORTED A.5 INCH CRACK IN LEFT WING UPPER SKIN AT WBL 157. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER/TRIPLER AND REPAIRED PER EO B737-5723-0001 AND DRAWING 65C30113. (M)
- [SDR F3LA99021](https://openairdocs.org/sdr/F3LA99021.md): Battery Pack · discharged · Feb 9, 1999 · N214AU · Boeing 737201 · Emergency Lighting
  > PHX - DURING C-CHECK INSPECTION, REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RECHARGED BATTERY PACK PER MM 33-51-11. (M)
- [SDR F3LA98144](https://openairdocs.org/sdr/F3LA98144.md): Battery Pack · discharged · Jul 28, 1998 · N214AU · Boeing 737201 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY. (X)
- [SDR F3LA98037](https://openairdocs.org/sdr/F3LA98037.md): Wire · failed · Apr 30, 1998 · N214AU · Boeing 737201 · Light System Wiring
  > ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT WAS 1 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA97170](https://openairdocs.org/sdr/F3LA97170.md): Connector · failed · Dec 25, 1997 · N214AU · Boeing 737201 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED CANNON PLUG WIRE CONNECTING PIN AND CHECKED OK. (M)
- [SDR F3LA97167](https://openairdocs.org/sdr/F3LA97167.md): Skin · cracked · Dec 2, 1997 · N214AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - CRACK IN UPPER AFT CORNER OF L-3 WINDOW CUTOUT. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-30-3. (M)
- [SDR F3LA97166](https://openairdocs.org/sdr/F3LA97166.md): Bulkhead · cracked · Dec 2, 1997 · N214AU · Boeing 737201 · Fuselage Main, Bulkhead
  > PAE - RIGHT BS 727 BULKHEAD LOWER CHORD DISCOVERED CRACKED DURING ACCOMPLISHMENT OF FRONTIER ENGINEERING ORDER NR 53-10-737-004. REMOVED AND REPLACED LOWER SECTION OF CHORD IAW EO NR 53-10-737-001. (M)
- [SDR F3LA97165](https://openairdocs.org/sdr/F3LA97165.md): Skin · corroded · Dec 2, 1997 · N214AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - CORROSION ON INNER DOUBLER ON BACK SIDE OF FORWARD LAV SERVICING PAN AT STATION 270. CORROSION OUT OF LIMITS IAW SRM 51-10-6, 53-10-1. REMOVED AND REPLACED IAW PAN DOUBLER IAW SRM 51-30-2. (M)
- [SDR F3LA97164](https://openairdocs.org/sdr/F3LA97164.md): Skin · corroded · Dec 2, 1997 · N214AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PILLOWING SKIN BETWEEN RIVETS AT BS 416, STRINGER 221. REMOVED FASTENERS AND DISCOVERED CORROSION BETWEEN SKIN AND STRINGER, CORROSION ON SKIN OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGED SECTION OF SKIN AND ACCOMPLISHED EXTERNAL SKIN REPAIR IAW SRM 53-30-
- [SDR F3LA96051](https://openairdocs.org/sdr/F3LA96051.md): Stringer · corroded · Oct 21, 1996 · N214AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - FOUND CORROSION AROUND FASTENERS IN STRINGER 27R, BS 947-967 WL 173. REMOVED DAMAGED SECTION OF STRINGER 27R, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-3. (M)
- [SDR F3LA96050](https://openairdocs.org/sdr/F3LA96050.md): Bulkhead Web · cracked · Oct 18, 1996 · N214AU · Boeing 737201 · Fuselage Main, Bulkhead
  > PAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS REPLACED IAW BOEING SRM AND BOEING DRAWING NR 65-16300. REPLACEMENT ACCOMPLISHED ON TRAMCO MWO FUSELAGE 212. (M)
- [SDR F3LA96049](https://openairdocs.org/sdr/F3LA96049.md): Bulkhead Web · cracked · Oct 18, 1996 · N214AU · Boeing 737201 · Fuselage Main, Bulkhead
  > PAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES BELOW PRESSURE DECK IAW EWO 96-0606. LEAK CHECKED ALL ITEMS. REMOVED FOR ACCESS, NO LEAKS FOUND.
- [SDR F3LA96048](https://openairdocs.org/sdr/F3LA96048.md): Chord · cracked · Oct 17, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CRACK INDICATIONS IN LT BS 727, STRINGER 18A OUTBOARD CHORD FORWARD AND AFT OF BOTH FASTENER HOLES. ACCESSED REPAIR AREA. FOUND CRACKS CONTAINED IN FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PARTS FOR INTERIM REPAIR PER SB 737-53A1166. RE-
- [SDR F3LA96046](https://openairdocs.org/sdr/F3LA96046.md): Floorbeam · cracked · Oct 17, 1996 · N214AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS BS 520 WL 207.75, RBL 25 AND RBL 46. REPAIRED FLOORBEAM CRACK AT BS 520, WL 207.75, RBL 25 AND RBL 46 IAW EWO 396-0643. (M)
- [SDR F3LA96045](https://openairdocs.org/sdr/F3LA96045.md): Floorbeam · cracked · Oct 17, 1996 · N214AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS AT BS 520, WL 207.75, LBL 25 - LBL 47. REPAIRED CRACKS IN FLOORBEAM AT BS 520, WL 207.75, LBL 25, LBL 45 AND LBL 47 PER EWO NR 96-0643. (M)
- [SDR F3LA96044](https://openairdocs.org/sdr/F3LA96044.md): Chord · cracked · Oct 16, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - HFEC INSPECTION OF THE BS 178 LT SIDE CHORD AT WL 194-196 SHOWS A CRACK INDICATION. CUT OUT DAMAGED AREA OF CHORD. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER TRAMCO EWO NR 96-0619. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 276. (M)
- [SDR F3LA96040](https://openairdocs.org/sdr/F3LA96040.md): Keelbeam · cracked · Oct 16, 1996 · N214AU · Boeing 737201 · Fuselage Main, Keel
  > PAE - FOUND CRACK IN THE AFT END OF RT KEELBEAM BS 814-818, STRINGER 27 RT. REPAIRED CRACK IAW TRAMCO EWO 96-0613. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 255. (M)
- [SDR F3LA96047](https://openairdocs.org/sdr/F3LA96047.md): Stiffener · cracked · Oct 15, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CRACK EMANATING FROM FASTENER HOLE AT BS 540, WL 203.5, LBL 26 ON VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER AND INSTALLED PER SRM 57-10-02, SRM 51-30-02. WORK DOCUMENTED ON TRAMCO MWO INTERIOR 174. (M)
- [SDR F3LA96042](https://openairdocs.org/sdr/F3LA96042.md): Chord · cracked · Oct 15, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > HFEC INSPECTION EXHIBITS CRACK APPROX 1.5 INCH LONG IN RADIUS OF BS 540 CHORD BETWEEN STRINGER 21R AND STRINGER 22R, CRACK IS ON SPLICE PLATE. ACCESSED AREA, REMOVED DAMAGED SPLICE PLATE. FABRICATED NEW SPLICE PLATE PER TRAMCO EO NR 96-0629. INSTALLED NEW S
- [SDR F3LA96041](https://openairdocs.org/sdr/F3LA96041.md): Door Frame · cracked · Oct 15, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - HFEC INSPECTION OF THE FORWARD CARGO DOOR FRAME, REVEALED A CRACK INDICATION AT STRINGER 23R ON THE FORWARD SIDE OF THE FRAME AT THE LOWEST OUTBOARD CORNER OF THE DOOR STOP FITTING. ACCESSED INDICATED AREA AND FOUND NUMEROUS GOUGES LOCATED BENEATH DOOR
- [SDR F3LA96038](https://openairdocs.org/sdr/F3LA96038.md): Frame · corroded · Oct 15, 1996 · N214AU · Boeing 737201 · Fuselage Main, Frame
  > PAE - FOUND CORROSION (C53-208-01) ON AFT SIDE OF FRAME BS 520 RBL 7, WL 150. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FRAME PER SRM 51-40-3. (M)
- [SDR F3LA96039](https://openairdocs.org/sdr/F3LA96039.md): Frame · cracked · Oct 14, 1996 · N214AU · Boeing 737201 · Fuselage Main, Frame
  > PAE - FOUND CRACK IN FRAME WEB AT UPPER CORNER OF STRINGER CUTOUT BS 294.5, STRINGER 18R. FOUND CRACK CONTAINED IN FASTENER HOLE. REPAIRED PER SRM 51-40-02 AND TRAMCO ER100396MW3. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 233. (M)
- [SDR F3LA96037](https://openairdocs.org/sdr/F3LA96037.md): Shear Tie · corroded · Oct 14, 1996 · N214AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-10-4, FIG 8. DURING REPAIR, FOUND DAMAGE TO BONDED DOUBLER BENEATH SHEAR TIE. CUT OUT DAMAGED DOUBLE
- [SDR F3LA96036](https://openairdocs.org/sdr/F3LA96036.md): Floorbeam · corroded · Oct 12, 1996 · N214AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND CORROSION ON UNDERSIDE OF CARGO FLOORBEAM BS 500, RBL 18, WL 156. REMOVED CORROSION ON UNDERSIDE OF FLOORBEAM AND REPAIRED IAW SRM 53-10-1, 51-40-3 REF WORK ORDER FUSELAGE 262. (M)
- [SDR F3LA96035](https://openairdocs.org/sdr/F3LA96035.md): Stringer · cracked · Oct 12, 1996 · N214AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - FOUND CRACK IN STRINGER 10 LEFT, BS 296, WL 256. REMOVED DAMAGED SECTION OF STRINGER 10L BS 296, WL 256. REPAIRED STRINGER IAW SRM 53-10-3 FIGURE 3 RED WORK ORDER INTERIOR 154. (M)
- [SDR F3LA96034](https://openairdocs.org/sdr/F3LA96034.md): Intercostal · cracked · Oct 12, 1996 · N214AU · Boeing 737201 · Cargo/Baggage Doors
  > PAE - FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS ARE CRACKED ON THE AFT OTBOARD FLANGE. REMOVED AND REPLACED FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS IAW SRM 51-10-1, 51-10-2, 51-30-2, REF WORK ORDER D
- [SDR F3LA96033](https://openairdocs.org/sdr/F3LA96033.md): Stringer · cracked · Oct 12, 1996 · N214AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > FOUND CRACK IN STRINGER 14R AT BS 277. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC INTERIOR 178. (M)

Next page: https://openairdocs.org/deregistered/N214AU-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 = 'N214AU' AND deregistration_id = 'N214AU-2000-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N214AU-2000-07-20/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.