# Service difficulty reports: N207AU, cancelled Feb 3, 2000

A list on [N207AU, cancelled Feb 3, 2000](https://openairdocs.org/deregistered/N207AU-2000-02-03.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 · 79 reports

- [SDR F3LA99102](https://openairdocs.org/sdr/F3LA99102.md): Fairing · cracked · Jul 10, 1999 · N207AU · Boeing 737201 · Nacelle/Pylon Structure
  > DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
- [SDR F3LA99101](https://openairdocs.org/sdr/F3LA99101.md): Fairing · cracked · Jul 10, 1999 · N207AU · Boeing 737201 · Nacelle/Pylon Structure
  > DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
- [SDR F3LA99100](https://openairdocs.org/sdr/F3LA99100.md): Wire Harness · damaged · Jul 8, 1999 · N207AU · Boeing 737201 · Electrical Power System Wiring
  > DURNG C-CHECK INSPECTION, REPORTED DAMAGED WIRING IN THE VERTICAL STABILIZER. CAUSE OF DAMAGE APPEARS TO BE SKYDROL HYDRAULIC FLUID. THE DAMAGE BEGAN APPROX 8 INCHES FROM RUDDER PCU ELECTRICAL CONNECTORS D-289 AND D-291 AND CONTINUED FOR APPROX 5 FEET, AFFEC
- [SDR F3LA99099](https://openairdocs.org/sdr/F3LA99099.md): Rib · cracked · Jun 30, 1999 · N207AU · Boeing 737201 · Engine Thrust Reverser
  > DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER AFT END. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
- [SDR F3LA99098](https://openairdocs.org/sdr/F3LA99098.md): Rib · cracked · Jun 30, 1999 · N207AU · Boeing 737201 · Engine Thrust Reverser
  > DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER LOWER SIDE. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
- [SDR F3LA99097](https://openairdocs.org/sdr/F3LA99097.md): Chord · cracked · Jun 30, 1999 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > DEN - DURING C-CHECK INSPECTION, REPORTED THREE CRACKS FOUND IN PRESSURE DECK COMPRESSION CHORD AT STATION 663.75, RBL 25 AND LBL 25. MAINTENANCE FABRICATED AND REPLACED RIB PER EA 51-737-003 AND SRM 51=40-3. (M)
- [SDR F3LA99096](https://openairdocs.org/sdr/F3LA99096.md): Igv · cracked · Jun 30, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor Section
  > DEN - DURING C-CHECK INSPECTION REPORTED, NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE, 10 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, PAGES 901 AND 9
- [SDR F3LA99095](https://openairdocs.org/sdr/F3LA99095.md): Igv · cracked · Jun 30, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor Section
  > DEN - DURING C-CHECK, INSPECTION REPORTED NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE AT 2 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, REPAIR NR 14,
- [SDR F3LA99090](https://openairdocs.org/sdr/F3LA99090.md): Shear Tie · cracked · Jun 29, 1999 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > DEN - DURING C-CHECK INSPECTION REPORTED, CRACK IN SHEAR TIE, LAST RIVET TO EDGE OF TIE, AT BS 294.5 ABOVE STRINGER 13L. MAINTENANCE REPAIRED CRACKED AT SHEAR TIE PER SRM 53-10-4, FIG 8. (M)
- [SDR F3LA99088](https://openairdocs.org/sdr/F3LA99088.md): Angle · cracked · Jun 29, 1999 · N207AU · Boeing 737201 · Engine Cowling System
  > DEN - DURING C-CHECK, INSPECTION REPORTED CRACK AT NR 2 ENGINE NOSE COWL FAIRING (SUGAR SCOOP) SEAL RETAINER INNER ANGLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. (M)
- [SDR F3LA99087](https://openairdocs.org/sdr/F3LA99087.md): Skin · cracked · Jun 28, 1999 · N207AU · Boeing 737201 · Nacelle/Pylon, Plate/Skin
  > DEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3. (M)
- [SDR F3LA99094](https://openairdocs.org/sdr/F3LA99094.md): Exhaust Case · cracked · Jun 25, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/Nozzle
  > DEN - DURING C-CHECK INSPECTION, REPORTED NR 2 ENGIEN EXHAUST CASE CRACKED AT 3 O'CLOCK STRUT, TOP SIDE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54 PAGE 204 AND BAC 5975. (M)
- [SDR F3LA99086](https://openairdocs.org/sdr/F3LA99086.md): Stringer · cracked · Jun 25, 1999 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > DEN - DURING C-CHECK, INSPECTION REPORTED STRINGER 7R CRACKED ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 360. MAINTENANCE REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED STRINGER PER SRM 51-10-2, 51-30-2 AND 51-20-01. (M)
- [SDR F3LA99093](https://openairdocs.org/sdr/F3LA99093.md): Exhaust Case · cracked · Jun 23, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/Nozzle
  > DEN - DURNG C-CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE STRUT CRACKED AT 9 O'CLOCK POSITION AT ROOT. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC5975. (M)
- [SDR F3LA99092](https://openairdocs.org/sdr/F3LA99092.md): Exhaust Case · cracked · Jun 23, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/Nozzle
  > DEN - DURING C-CHECK INSPECTION, REPORTED A 3 INCH CRACK IN THE NR 2 ENGINE EXHAUST CASE UNDER 3 O'CLOCK POSITION STRUT, EXTENDING TOWARD CENTER OF CASE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC 5975. (M)
- [SDR F3LA99091](https://openairdocs.org/sdr/F3LA99091.md): Igv · cracked · Jun 22, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor Section
  > DEN - DURING C-CHECK INSPECTION REPORTED NR 2 ENGINE INLET GUIDE VANE CRACKED AND STOP DRILLED AT 2 O'CLOCK POSITION, AFT WELD. MAINTENANCE WELDED CRACK IAW P/W E/M 72-23-04, REPAIR 14, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4 AND STRESS RELIEVED IAW P/W E/M
- [SDR F3LA99085](https://openairdocs.org/sdr/F3LA99085.md): Fitting · cracked · Jun 18, 1999 · N207AU · Boeing 737201 · Passenger/Crew Doors
  > DEN - DURING C-4 CHECK INSPECTION, REPORTED LEFT UPPER FORWARD STOP FITTING ON AFT AIRSTAIR DOOR CRACKED. MAINTENANCE INSTALLED REPLACEMENT FITTING PER SRM 51-30-2. (M)
- [SDR F3LA98172](https://openairdocs.org/sdr/F3LA98172.md): Wire · loose · Oct 14, 1998 · N207AU · Boeing 737201 · Light System Wiring
  > PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA98167](https://openairdocs.org/sdr/F3LA98167.md): Actuator · failed · Oct 11, 1998 · N207AU · Boeing 737201 · Drag Control Actuator
  > DEN - UPON ARRIVAL, FLT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE DURING LANDING. MAINTENANCE REPLACED NR 5 GROUND SPOILER OUTBOARD ACTUATOR, SERVICED HYDRAULIC SYSTEM. PERFORMED LEAK CHECK AND CHECKED OK. (M)
- [SDR F3LA98165](https://openairdocs.org/sdr/F3LA98165.md): Gasper Fan · malfunctioned · Sep 16, 1998 · N207AU · Boeing 737201 · Air Distribution Fan
  > PIH - EN ROUTE TO SEA, FLT CREW REPORTED A STRONG ELECTRICAL ODOR IN AFT PASSENGER CABIN. AIRCRAFT WAS DIVERTED TO POCATELLO AND LANDED WITHOUT INCIDENT. MAINTENANCE DETECTED ODOR COMING FROM AIR VENTS WITH GASPER FAN 'ON'. INSPECTED AIR CONDITIONING DISTRI
- [SDR F3LA98032](https://openairdocs.org/sdr/F3LA98032.md): Skin · corroded · Apr 18, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK, INSPECTION REPORTED BULGING SKIN AT AFT CORNER OF CUTOUT AT BS 294.5 WL 148, RBL 24. MAINTENANCE REMOVED CORRODED AREAS. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-1, 51-30-2 AND ER 96-0315. (M)
- [SDR F3LA98030](https://openairdocs.org/sdr/F3LA98030.md): Skin · cracked · Apr 17, 1998 · N207AU · Boeing 737201 · Cargo/Baggage Doors
  > PAE - DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LOWER CORNER OF AFT CARGO DOOR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1, FIGURE 2, SRM 51-10-6, SRM 51-30-2 AND ER 98-0291. (M)
- [SDR F3LA98029](https://openairdocs.org/sdr/F3LA98029.md): Skin · corroded · Apr 17, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK, INSPECTION REPORTED SKIN PILLOWING AT BS 415-430, STRINGER 18R TO 19R. MAINTENANCE REMOVED A 13 INCH BY 20 INCH CORRODED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, AND 53-30-3. (M)
- [SDR F3LA98031](https://openairdocs.org/sdr/F3LA98031.md): Lights · inoperative · Apr 16, 1998 · N207AU · Boeing 737201 · Emergency Lighting
  > DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA98028](https://openairdocs.org/sdr/F3LA98028.md): Skin · corroded · Apr 15, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK, INSPECTION REPORTED BULGE IN SKIN AT BS 1018 BETWEEN STRINGER 27-R AND 28-R. MAINTENANCE REMOVED DAMAGED AREA (7.1 INCH BY 2 INCH). FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3, PAGE 97, SRM 53-30-3, FIGURE 128, SRM 51-30-2, AN
- [SDR F3LA98027](https://openairdocs.org/sdr/F3LA98027.md): Stringer · corroded · Apr 14, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-R, BS 360-540. MAINTENANCE REMOVED CORRODED AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3, FIGURE 16, AND SRM 51-30-2. (M)
- [SDR F3LA98026](https://openairdocs.org/sdr/F3LA98026.md): Stringer · corroded · Apr 10, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 14-R, BS 440-500, AND CRACK IN STRINGER 14-R, BS 440-448. MAINTENANCE REPAIRED CORRODED AREAS, PER SRM 51-30-2, 53-30-1,53-30-3 AND 51-40-2. FABRICATED REPLACEMENT PARTS AND REPAIRED CRACK PER S
- [SDR F3LA98025](https://openairdocs.org/sdr/F3LA98025.md): Stringer · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK, INSPECTION REPORTED STRINGER 16-R CRACKED AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE REMOVED A 1 INCH BY 1.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, AND ER 98-0277. (M)
- [SDR F3LA98024](https://openairdocs.org/sdr/F3LA98024.md): Stringer · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK INSPECTION, FOUND STRINGER 16L CRACKED AT BS 500B PLUS 19 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, SRM 51-10-1 AND ER 98-0277. (M)
- [SDR F3LA98022](https://openairdocs.org/sdr/F3LA98022.md): Frame · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Frame
  > PAE - DURING C-CHECK INSPECTION REPORTED, FRAME CRACKED AT BS 360 BETWEEN STRINGER 20R AND 21R. MAINTENANCE REMOVED A 1. INCH BY 3.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1 AND 51-40-3. (M)
- [SDR F3LA98021](https://openairdocs.org/sdr/F3LA98021.md): Skin · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK INSPECTION REPORTED, CRACK AT BS 950 BELOW STRINGER 14R AT EDGE OF SKIN LAP. MAINTENANCE REMOVED A 1 INCH BY 3 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)
- [SDR F3LA98019](https://openairdocs.org/sdr/F3LA98019.md): Stringer · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN STRINGER 16R AT BS 500B PLUS 16 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0275. (M)
- [SDR F3LA98018](https://openairdocs.org/sdr/F3LA98018.md): Stringer · cracked · Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK INSPECTION REPORTED, CRACK IN STRINGER 16L AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0277. (M)
- [SDR F3LA98015](https://openairdocs.org/sdr/F3LA98015.md): Skin · delaminated · Apr 7, 1998 · N207AU · Boeing 737201 · Leading Edge Devices
  > PAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FROM OUTBOARD LOWER SURFACE, 13 INCHES OF DELAMINATED SKIN FROM OUTBOARD UPPER SURFACE AND 15 INCHES
- [SDR F3LA98010](https://openairdocs.org/sdr/F3LA98010.md): Frame · cracked · Apr 7, 1998 · N207AU · Boeing 737201 · Fuselage Main, Frame
  > DURING C-CHECK, MAINTENANCE REPORTED FRAME CRACKED AT STA 7472, STR 9L. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3. (X)
- [SDR F3LA98023](https://openairdocs.org/sdr/F3LA98023.md): Stringer · corroded · Apr 6, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-L, BS 450-459. MAINTENANCE REMOVED A 3 INCH BY 2.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, PAGES 3 AND 4, SRM 53-30-3, FIGURE 16, SRM 53-30-3, PAGES 51-53, AND SR
- [SDR F3LA98020](https://openairdocs.org/sdr/F3LA98020.md): Skin · corroded · Apr 6, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON STRINGER 4L SKIN LAP AT BS 500A PLUS 10 INCHES. MAINTENANCE REMOVED A 1.2 INCH BY 2 INCH CORRODED AREA, FABIRCATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)
- [SDR F3LA98011](https://openairdocs.org/sdr/F3LA98011.md): Floorbeam · corroded · Apr 3, 1998 · N207AU · Boeing 737201 · Fuselage Main, Floor Beam
  > DURING C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD BS 328 FLOORBEAM, LBL 30-4, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF BS 328 BEAM UPPER CHORD FROM LBL 28 TO LBL 65. FABRICATED REPAIR PARTS AND INSTALLED WET WITH FASTENERS PER SRM 53-10-9,
- [SDR 97ZZZX3892](https://openairdocs.org/sdr/97ZZZX3892.md): Battery Pack · failed · Aug 24, 1997 · N207AU · Boeing 737201 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY.
- [SDR F3LA97141](https://openairdocs.org/sdr/F3LA97141.md): Pressure Web · cracked · Jul 30, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EIGHT.5 INCH CRACKS IN LEFT PRESSURE WEB AT STATION 259 AND TWO.5 INCH CRACKS IN RIGHT PRESSURE WEB AT STATION 259 FORWARD OF DOOR IDLER FITTING. MAINTENANCE TRIMMED OUT CRACKS. FABRICATED FILLER AND INSTALL
- [SDR F3LA97136](https://openairdocs.org/sdr/F3LA97136.md): Battery Pack · discharged · Jul 12, 1997 · N207AU · Boeing 737201 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 11 INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHECKED OKAY. (X)
- [SDR F3LA97128](https://openairdocs.org/sdr/F3LA97128.md): Light · malfunctioned · Jun 2, 1997 · N207AU · Boeing 737201 · Emergency Lighting
  > UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD GALLEY DOOR EMERGENCY LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)
- [SDR F3LA97027](https://openairdocs.org/sdr/F3LA97027.md): Slide · low pressure · Jan 29, 1997 · N207AU · Boeing 737201 · Escape Slide
  > DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSRUE LOW. REPLACED ESCAPE SLIDE. (M)
- [SDR F3LA97019](https://openairdocs.org/sdr/F3LA97019.md): Doubler · corroded · Jan 22, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF NR 2 DME ANTENNA FOR BS 520 FRAME REMOVAL FOUND CORROSION ON NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0 WL 148.5. REMOVED CORROSION FROM AROUND NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0, WL 148.5 AREA FOUND TO BE OUT OF LIMITS. (
- [SDR 97ZZZM203](https://openairdocs.org/sdr/97ZZZM203.md): Doubler · corroded · Jan 22, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - UPON REMOVAL OF NR 1 ADF ANTENNA FOR BS 520 FRAME REMOVAL, FOUND CORROSION ON NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. REMOVED CORROSION FROM AROUND NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. AREA FOUND TO BE OUT OF
- [SDR F3LA97017](https://openairdocs.org/sdr/F3LA97017.md): Nose Chord · corroded · Jan 21, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON RIGHT LOWER NOSE CHORD HORIZONTAL FLANGE BS 237 TO 250 RBL 18, WL 164. REMOVED RT LOWER NOSE CHORD DUE TO CORROSION WAS BEYOND LIMITS IN A ONE INCH AREA IAW SRM 53-10-1. INSTALLED NEW NOSE CHORD WITH A SPLICE IAW SRM 51-40-3, 53-10-2, 51-3
- [SDR F3LA97015](https://openairdocs.org/sdr/F3LA97015.md): Delta Beam · cracked · Jan 15, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CRACK ON PREVIOUS REPAIR BEHIND RAM AIR DUCT RIGHT SIDE AT BS 574-579, RBL 40, WL 152 ON DELTA BEAM. REMOVED 2 INCH CRACK BY REMOVING DAMAGE AREA, REPAIRED LOWER DELTA BEAM WEB, RT SIDE BS 574-579, RBL 40, WL 152 IAW SRM 53-10-6 FIG 1 WITH PART FA
- [SDR F3LA97014](https://openairdocs.org/sdr/F3LA97014.md): Skin · gouged · Jan 15, 1997 · N207AU · Boeing 737201 · Nacelle/Pylon Structure
  > PAE - WHILE WORKING ENGINE NR 195 FOUND RT LOWER RAM AIR INTAKE SKIN GOUGED AT BS 500B PLUS 7 STRINGER 24 RT. REMOVED DAMAGED WEB AT BS 500B PLUS7, STRINGER 24 RT FABRICATED WEB FROM MATERIAL 2024-T3,.040 INCH PER SRM 51-20-01. ALODINED, PRIMED AND INSTALLE
- [SDR F3LA97013](https://openairdocs.org/sdr/F3LA97013.md): Frame · damaged · Jan 15, 1997 · N207AU · Boeing 737201 · Fuselage Main, Frame
  > FOUND CORROSION ON THE FORWARD SIDE OF THE 520 FRAME IN THE FORWARD CARGO BAY BS 520 LBL 18 TO RBL 14, WL 149. REMOVED DAMAGED FRAME, STRINGER CLIPS, STRINGER 26 LT (30 INCH) AND DAMAGED INTERCOSTALS AS WELL AS FLOOR TO SIDEWALL SUPPORT PLATES. FABRICATED NE
- [SDR F3LA97012](https://openairdocs.org/sdr/F3LA97012.md): Web · corroded · Jan 11, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CORROSION IN NOSE WHEEL WELL UPPER HORIZONTAL WEB AROUND RT ACCESS PANEL CUTOUT BS 236 TO 252, LBL 2 TO 16, WL 190. FOUND CORROSION ON NOSE WHEEL WELL UPPER HORIZ WEB AND STIFFENERS TO BE OUT OF LIMITS, FABRICATED DOUBLERS FROM.080 7075 T6. INST

Next page: https://openairdocs.org/deregistered/N207AU-2000-02-03/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 = 'N207AU' AND deregistration_id = 'N207AU-2000-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N207AU-2000-02-03/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.