# Service difficulty reports: N462AT, cancelled Jun 13, 2006

A list on [N462AT, cancelled Jun 13, 2006](https://openairdocs.org/deregistered/N462AT-2006-06-13.md).

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

- [SDR AT9900634](https://openairdocs.org/sdr/AT9900634.md): Oil Line · broken · Sep 3, 1999 · N462AT · Boeing 737297 · Turbine Engine Oil System
  > NR 2 ENGINE OIL PSI AND QUANTITY WENT TO ZERO, SHUT DOWN ENGINE IN-FLIGHTAND DIVERTED TO JAN. LANDED AIRCRAFT WITHIN THIRTY MINUTES OF INCIDENT. FOUND BROKEN OIL LINE AT ENGINE MAIN OIL SCREEN, REPLACED OIL LINE.
- [SDR AT9900601R1](https://openairdocs.org/sdr/AT9900601R1.md): Tire · blown · Aug 18, 1999 · N462AT · Boeing 737297 · Tire
  > NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 AND NR 4 TIRE AND BRAKE, NR 1 AND NR 2 ENGINE HYDRAULIC PUMP DUE TO SYSTEM FAILURE. REPLACED HYDRAULIC TEE FITTING, SUPPLY B SYSTEM TUBE ASSEMBL
- [SDR AT9900601](https://openairdocs.org/sdr/AT9900601.md): Tire · failed · Aug 18, 1999 · N462AT · Boeing 737297 · Tire
  > NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 TIRE AND A REVISION NR AT9900601R1 WILL FOLLOW AFTER AIRCRAFT WILL COME BACK FOR SERVICE.
- [SDR AT9900575](https://openairdocs.org/sdr/AT9900575.md): Fitting · damaged · Aug 13, 1999 · N462AT · Boeing 737297 · Engine Oil Pressure
  > AT ALTITUDE NR 1 ENGINE OIL QUANTITY WENT TO ZERO AND OIL PRESSURE DROPPED INTO THE AMBER BAND. SHUT DOWN THE ENGINE AND RETURNED. OIL PRESSURE REMAINED AT 35 PSI FOR 40 MIN WINDMILL. INSPECTED, FOUND FITTING UNSECURED. THREAD DAMAGED. REPAIRED GEARBOX, I
- [SDR ATT9900539](https://openairdocs.org/sdr/ATT9900539.md): Pump · leaking · Jul 28, 1999 · N462AT · Boeing 737297 · Turbine Engine Oil System
  > NR 1 ENGINE LOST ALL OIL QUANTITY. ENGINE WAS SHUT DOWN ON SHORT FINAL WITH OIL PRESSURE GOING TOWARDS ZERO. OIL TEMPERATURE OK. INSPECTION FOUND OIL PUDDLING AROUND NR 6 BEARING AREA AND IN TAILPIPE. REMOVED AND REPLACED NR 6 GARLOCK SEAL AND NR 6 BEARING
- [SDR AT9900493](https://openairdocs.org/sdr/AT9900493.md): Fuse · failed · Jul 13, 1999 · N462AT · Boeing 737297 · Emergency Lighting
  > DURING LAYOVER, FOUND AN EMERGENCY PATH LIGHTING SEGMENT OUT. REPLACED BATTERY CHARGER FOR BLOWN FUSE (F2), OPS CHECK NORMAL IAW MM 33-51-00.
- [SDR AT9900492](https://openairdocs.org/sdr/AT9900492.md): Battery Charger · defective · Jul 9, 1999 · N462AT · Boeing 737297 · Emergency Lighting
  > EMERGENCY EVACUATION LIGHTS INOPERATIVE IN FORWARD SECTION OF AIRCRAFT. REMOVED AND REPLACED FORWARD BATTERY PACK CHARGER IAW MM 33-51-51.
- [SDR VJ9800364](https://openairdocs.org/sdr/VJ9800364.md): Intercoastal · corroded · Aug 7, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > FUSELAGE INTERIOR BETWEEN BS 312 AND 294.5, INTERCOSTAL AT RBL 24 IS CORRODED ON TOP. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1 AND 51-10-6. REMOVED INTERCOSTAL AND FABRICATED REPAIR FROM 7075 T6.080 17 BY 2 1/1 BY 1. DRILLED, DEBURRED, TREATED AND P
- [SDR VJ9800363](https://openairdocs.org/sdr/VJ9800363.md): Floorbeam · corroded · Aug 7, 1998 · N462AT · Boeing 737297 · Fuselage Main, Floor Beam
  > FUSELAGE INTERIOR, FLOORBEAM AT BS 294.5 IS CORRODED ON TOP AT RBL 12. REMOVED CORROSION.024 TO.041 MATERIAL LOSS OUT OF LIMITS. GAUGE NR A-0358 IAW SRM 51-10-6 AND 53-10-1. REMOVED STIFFENERS AND UPPER CHORD FROM RL 26 TO LBL 20 NECESSARY TO INSTALL CHOR
- [SDR VJ9800360](https://openairdocs.org/sdr/VJ9800360.md): Angle · corroded · Aug 7, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > AFT CARGO STRINGER 27R AT STA 962 AT FASTENER HOLE CORRODED. MAT LOSS IN THE BASE OF STRINGER AT STA 951-967 (27R) OUT OF LIMITS IAW SRM 53-10-1. CUT OUT CORRODED SECTION STRINGER IAW SRM 53-10-3. FORMED 1 V CHANNEL AND 2 ANGLE REPAIR 7075-0 HEAT TREATED BA
- [SDR VJ9800367](https://openairdocs.org/sdr/VJ9800367.md): Skin · corroded · Aug 6, 1998 · N462AT · Boeing 737297 · Fuselage Main, Plate/Skin
  > CORROSION ON SIDE MOUNT AREA FOR EYE BROW WINDOW NR 5. REMOVED CORROSION OUT OF LIMITS, FABRICATED REPAIR DOUBLER FROM 2024 T-3.063 ABD STRAP REPAIR FROM 7075 T-6.032 IAW TSR NR B737-53-009, B737 --56-002 AND DWG B737-980006. TREATED AND PRIMED IAW SRM 51-
- [SDR VJ9800356](https://openairdocs.org/sdr/VJ9800356.md): Floorbeam · corroded · Aug 6, 1998 · N462AT · Boeing 737297 · Fuselage Main, Floor Beam
  > EXFOLIATED CORROSION ON BS 328 FLOORBEAM CAP UNDER TAPERED SHIN RBL 54. REMOVED CORROSION IAW SRM 51-10-6. MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED T CHORD STA 328 LBL 15 RBL 65 IAW SRM 51-30-2 AND 53-10-9. FABRICATED REPAIR SECTION AND REPAIR ANGLES IAW
- [SDR VJ9800359](https://openairdocs.org/sdr/VJ9800359.md): Angle · corroded · Aug 5, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > L-1 DOOR FWD GIRT BAR ATTACH BRACKET BLOCK CORRODED ON BS 312 FLOORBEAM. REMOVED CORRODED ATTACH BRACKET IAW SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR ANGLE FROM 7075-0.070 IAW SRM 51-40-3. DRILLED, TRIMMED, AND COUTER SUNK
- [SDR VJ9800358](https://openairdocs.org/sdr/VJ9800358.md): Angle · corroded · Aug 4, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > FILLER STRIPS ON TOP SIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD CORRODED BS 312-344. REMOVED CORROSION ON THRESHOLD, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01 AND 51-10-6. REMOVED ANGLE AND FORMED REPAIR ANGLE FROM 7075-0-.080. HEAT TREATED TO T6 IAW SRM 51-
- [SDR VJ9800357](https://openairdocs.org/sdr/VJ9800357.md): Angle · corroded · Aug 4, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > EXFOLIATED CORROSION AROUND NUT PLATE ON UNDERSIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD, BS 326. REMOVED SUPPORT ANGLE AND REMOVED CORROSION, LOSS FOUND TO BE OUT OF LIMITS IAW B737 SRM 51-10-6, AND 53-10-1. FABRICATED REPAIR ANGLE FROM LS 980-2. TRIMMED, DR
- [SDR VJ9800350](https://openairdocs.org/sdr/VJ9800350.md): Angle · corroded · Aug 4, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > L-1 DOOR SILL LOWER SUPPORT ANGLE BETWEEN STA 328-312 HAS 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE AND CLEANED CORROSION, MATERIAL LOSS 100 PERCENT OUT OF LIMITS IAW 737 SRM 53-10-1, 51-10-6. FABRICATED REPAIR ANGLE LS980-2. DRILLED, TRIMMED, DEBURR
- [SDR VJ9800351](https://openairdocs.org/sdr/VJ9800351.md): Angle · corroded · Aug 2, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > AFT ALV AT STA 296 BUTT LINE LBL35 ON REMOVAL OF SUPPORT ANGLE, LOWER SUPPORT U CHANNEL HAS CORROSION BEYOND LIMITS. REMOVED LOWER CHANNEL SUPPORT IAW B 737 SRM 51-30-2. FABRICATED REPAIR SUPPORT CHANNEL IAW 737 SRM 51-40-4. TREATED AND PRIMED IAW 737 SRM 5
- [SDR VJ9800361](https://openairdocs.org/sdr/VJ9800361.md): Angle · corroded · Aug 1, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > AFT TOILET FLOOR SUPPORT AT BL 12 L BS 1016 IS CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-30-1. REMOVED CORROSION IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. FABRICATED ANGLE REPAIR FROM 7075-0.100 IAW SRM 51-40-3. DRILLED, TRIMMED, AND DEBURRED ANGLE RE
- [SDR VJ9800365](https://openairdocs.org/sdr/VJ9800365.md): Stringer · corroded · Jul 31, 1998 · N462AT · Boeing 737297 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 27L FROM APPROX 986-1010 HAS NUMBEROUS SURFACE CORROSION ON THE CHANNEL AND ON LT SIDE AND ON THE BELLY SKIN. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1 FROM 2 PLACES AT STR 27L STA 986-1006. REMOVED CORROSION WITHIN LIMITS FROM STA 9
- [SDR VJ9800355](https://openairdocs.org/sdr/VJ9800355.md): Angle · corroded · Jul 31, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FWD LAV AFT WALL ATTACH ANGLE BS 300 LB 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED ATTACH ANGLE IAW SRM 51-30-2. FABRICATED REPAIR ANGLE IAW SRM 51-40-3. TREATED AND PRIMED IAW 51-10-2 AND MM 51-21-51. INST
- [SDR VJ9800353](https://openairdocs.org/sdr/VJ9800353.md): Floorbeam · corroded · Jul 31, 1998 · N462AT · Boeing 737297 · Fuselage Main, Floor Beam
  > AFT CARGO AREA AROUND STA 1006-1016 UNDER LT AFT LAV CORROSION BETWEEN THE FLOORBEAMS AND FLOOR BOARDS. REMOVED CORRODED AREA STA 1006-1016 WITHIN LIMITS. REMOVED CORROSION OUT OF LIMITS AT STA 1006 IAW SRM 53-10-1 FIG 1. FABRICATED ANGLES FROM 7075 -0.080
- [SDR VJ9800354](https://openairdocs.org/sdr/VJ9800354.md): Angle · corroded · Jul 30, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > AFT TOILET FWD WALL TIE DOWN ANGLE IS CORRODED. REMOVED CORROSION OUT OF LIMTS, MAT LOSS.045 IAW SRM 53-10-1. REMOVED BRACKET TO FABRICATE NEW ANGLE IAW SRM 51-40-3. FABBED REPAIR ANGLE (BRACKET) AND PRIMED IAW SRM 51-40-3, 51-10-2, MM 51-21-51. INSTALLED
- [SDR VJ9800352](https://openairdocs.org/sdr/VJ9800352.md): Angle · corroded · Jul 29, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FWD AFT LAV AFT WALL ATTACH ANGLE, AT BS 300, LOWER HAT SUPPORT HAS IG CORROSION. REMOVED HAT SUPPORT FOUND CORROSION BEYOND LIMTS IAW SRM 53-10-1 MADE REPAIR EXTRUDED PART OUT OF BAC-1510-335 IAW SRM 51-40-4. ALODINED IAE STM 51-10-2, PRIMED
- [SDR VJ9800362](https://openairdocs.org/sdr/VJ9800362.md): Support · corroded · Jul 28, 1998 · N462AT · Boeing 737297 · Fuselage Miscellaneous Structure
  > AFT TOILET UNDER FLOOR SUPPORT AT BL0 BS 1016 IS CORRODED. REMOVED CORROSION IAW SRM 51-10-2. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 AND 51-10-1. REPAIRED EXTRUDED SECTION IAW SRM 51-40-4 FROM 7075 T6 511. INSTALLED FLOOR SUPPORT REPAIR IA
- [SDR VJ9800366](https://openairdocs.org/sdr/VJ9800366.md): Panel · corroded · Jul 27, 1998 · N462AT · Boeing 737297 · Fuselage Main, Plate/Skin
  > FWD CARGO PTI, STA 492.4 TO 520 RT SIDE TRANSITION PANEL HAS CORROSION OVER TOP OF STRINGER 26 RT. REMOVED CORROSION OUT OF LIMITS. FABRICATED TRANSITIONS PANEL FROM 2024 T3.040, TREATED AND PRIMED AND INSTALLED IAW SRM 51-10-2, 51-20-11, AND 51-40-2.
- [SDR VJ9800041](https://openairdocs.org/sdr/VJ9800041.md): Battery · discharged · Mar 12, 1998 · N462AT · Boeing 737297 · Emergency Lighting
  > BOTH EMERGENCY EXIT LIGHTS AT AFT ENTRY SERVICE DOOR INOP. REPLACED BATTERY PACK.
- [SDR ZZDA3324697](https://openairdocs.org/sdr/ZZDA3324697.md): Lamp · failed · Oct 28, 1997 · N462AT · Boeing 737297 · Emergency Lighting
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND BOTH AFT EXTERIOR EMERGENCY LIGHTS INOPERABLE. RELAMPED BOTH EXTERIOR EMERGENCY LIGHTS. OPS CHECKED GOOD. (X)
- [SDR 97ZZZM1053](https://openairdocs.org/sdr/97ZZZM1053.md): Power Supply · inoperative · Aug 29, 1997 · N462AT · Boeing 737297 · Emergency Lighting
  > POST FLT INSPECTION, RIGHT FUSELAGE FWD EMERGENCY EXTERIOR LIGHT ASSY CORRODED. REPAIRED BARE WIRE AND REPLACED BATTERY PACK IN FWD CARGO PIT. REPLACED REFLECTOR ON R1 LIGHT. BOTH FWD EMERGENCY LIGHTS (EXTERIOR) OPS CHECK NORMAL.
- [SDR 97ZZZM1054](https://openairdocs.org/sdr/97ZZZM1054.md): Wire · broken · Jul 23, 1997 · N462AT · Boeing 737297 · Light System Wiring
  > DURING POST FLIGHT, FOUND ROW 19 EMERGENCY EXIT FLOOR LIGHT INOP. REPAIRED BROKEN WIRE AT ROW 19 EMERGENCY LIGHT SOCKET.
- [SDR 97ZZZM928](https://openairdocs.org/sdr/97ZZZM928.md): Light · inoperative · Jul 19, 1997 · N462AT · Boeing 737297 · Emergency Lighting
  > DURNIG A LAYOVER SERVICE, TWO E-PATH FLOOR LIGHTS WERE NOTICED INOP. THE TWO E-PATH FLOOR LIGHTS WERE REPLACED. THE SYSTEM WAS TESTED NORMAL. (M)
- [SDR ZZDA5311197](https://openairdocs.org/sdr/ZZDA5311197.md): Stringer · damaged · May 28, 1997 · N462AT · Boeing 737297 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND REPAIR AT STR 2L AND STR 3L AT STA 578 TO STA 597 NEEDS REPLACEMENT. FABRICATED DOUBLER FROM 2024 T3.080 INCH, 10.5 INCHES BY 8 INCHES IAW B737 SRM 51-30-3. INSTALLED IAW B737 SRM 51-30-3 AND SRM 51-30-2. (X)
- [SDR ZZDA5711397](https://openairdocs.org/sdr/ZZDA5711397.md): Skin · corroded · May 27, 1997 · N462AT · Boeing 737297 · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND CORROSION AROUND SCREW HOLES IN LEFT MAIN GEAR SUPPORT STRUCTURE. REMOVED CORROSION AROUND SCREW HOLES AND OVERSIZED 14 EACH HOLES TO.25 INCH IAW AERO CORP E.O. 97-580 AND RES 04452. MATERIAL LOSS LESS THAN.005 INCH. INSTALLED PANEL
- [SDR ZZDA5311497](https://openairdocs.org/sdr/ZZDA5311497.md): Skin · cracked · May 27, 1997 · N462AT · Boeing 737297 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND STR 19R AT BS 312.3 LOWER ROW OF FASTENERS OF SKIN LAP SHOW CRACK INDICATIONS. FABRICATED FILLER AND DOUBLER FROM 2024 T3.080 INCH, 2 INCHES B6 8.4 INCHES BY 8.2 INCHES IAW B737 SRM 53-30-3. INSTALLED IAW B737 SRM 53-30-3 AND SRM 51-30
- [SDR ZZDA5311297](https://openairdocs.org/sdr/ZZDA5311297.md): Floor Beam · corroded · May 27, 1997 · N462AT · Boeing 737297 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM AT FASTENER HOLE AT STA 986.5. FABRICATED DOUBLER FROM 7075 T6.071 INCH, 11 INCHES BY 2.5 INCHES. FABRICATED DOUBLER FROM 7075 T6.090 INCH, 9.25 INCHES BY 2.5 INCHES IAW B737 SRM 53-10-9. INSTALLED DOUBLER IAW
- [SDR ZZDA5310997](https://openairdocs.org/sdr/ZZDA5310997.md): Seat Track · corroded · May 27, 1997 · N462AT · Boeing 737297 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, FOUND EXFOLIATION CORROSION IN INBOARD SEAT TRACK AT STA 344. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 13.75 INCHES BY 3.5 INCHES IAW B737 SRM 53-10-5. INSTALLED IAW B737 SRM 53-10-5. (X)
- [SDR ZZDA5310897](https://openairdocs.org/sdr/ZZDA5310897.md): Seat Track · corroded · May 27, 1997 · N462AT · Boeing 737297 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, FOUND CORROSION IN RIGHT OUTBOARD SEAT TRACK AT STA 344. FABRICATED NEW FLOOR TRACK SECTION FROM BAC 1520-792 34 INCHES BY 3.25 INCHES IAW B737 SRM 53-10-5. INSTALLED IAW B737 SRM 51-30-3. (X)
- [SDR 96ZZZM1418](https://openairdocs.org/sdr/96ZZZM1418.md): Wheel Assy · failed · Jul 12, 1996 · N462AT · Boeing 737297 · Wheel/Ski/Float
  > AFTER LANDING, DURING TAXI TO GATE, THE NR 4 MLG WHEEL ASSY FAILED CAUSING THE NR 4 HUB CAP TO IMPACT THE NR 2 ENG INBOARD COWLING DAMAGING THE FORWARD AND AFT SECTIONS. UPON OPENING UP NR 2 ENGINE COWL INVESTIGATION REVEALED AFT FIREWALL AND TAILPIPE DAMAGE.
- [SDR 95ZZZM315](https://openairdocs.org/sdr/95ZZZM315.md): Harness · failed · Jul 28, 1995 · N462AT · Boeing 737297 · Fuel System Wiring
  > ON APPROACH TO CVG THE CREW OF FLIGHT 700 OBSERVED THE NR 1 FUEL QUANTITY SYSTEM GIVING AN ERRATIC INDICATION. THE CAPTAIN DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED THE ERRATIC INDICATION WAS CAUSED BY CONDENSATION BUILDUP ON
- [SDR 95ZZZM1](https://openairdocs.org/sdr/95ZZZM1.md): Skin · delaminated · Apr 19, 1995 · N462AT · Boeing 737297 · Leading Edge Devices
  > ON 4-18-95, THE PILOT IN COMMAND OF A/C FOUND NR 6 LE SLAT DELAMINATED DURING PREFLIGHT AT CVG. MAINTENANCE CONTROL CONTACTED AN EMERGENCY MAINTENANCE CREW TO EVALUATE THE DAMAGE. PER BOEING SPECS, THE AIRCRAFT WAS FERRIED TO MCO FOR MAINTENANCE. THE NR 6 L

## 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 = 'N462AT' AND deregistration_id = 'N462AT-2006-06-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N462AT-2006-06-13/reports

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