# Service difficulty reports: N460AT, cancelled Jul 6, 2000

A list on [N460AT, cancelled Jul 6, 2000](https://openairdocs.org/deregistered/N460AT-2000-07-06.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 · 88 reports

- [SDR AT9900611](https://openairdocs.org/sdr/AT9900611.md): Connector · loose · Aug 27, 1999 · N460AT · Boeing 737214 · Emergency Lighting
  > ONCE IN FLIGHT, EMERGENCY EXIT LIGHTS AND AISLE PATH LIGHTING CAME ON IN FLIGHT WITH SWITCH IN ARMED POSITION. CYCLED AIRCRAFT POWER, TESTED OK. INSPECTED AND FOUND LOOSE CONNECTION ON THE AFT SWITCH, SECURED AND CLEANED CONNECTOR AND TESTED GOOD.
- [SDR AT9900538](https://openairdocs.org/sdr/AT9900538.md): Battery Pack · discharged · Jul 28, 1999 · N460AT · Boeing 737214 · Emergency Lighting
  > R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT (SLIDE) WILL NOT ILLUMINATE. REMOVED AND REPLACED R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT BATTERY PACK IAW B737 MM 33-51-71.
- [SDR AT9900121](https://openairdocs.org/sdr/AT9900121.md): Skin · misrepaired · Jan 21, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THREE EXISTING REPAIRS RIGHT FORWARD FUSELAGE AT COCKPIT NOT REPAIRED IAW SB 737-53-111. CUT OUT EXISTING REPAIRS, FABRICATED AND INSTALLED DOUBLERS, SPLICE PLATES, AND FILLER IAW SB737-53-111 AND BOEING DRAWING 6
- [SDR AT9900056](https://openairdocs.org/sdr/AT9900056.md): Skin · misrepaired · Jan 20, 1999 · N460AT · Boeing 737214 · Horizontal Stabilizer, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HORIZONTAL STABILIZER STA 166 SKIN REPAIR HAS NO EDGE DISTANCE ON FILLER. REMOVED EXISTING REPAIR AND FABRICATED DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR PARTS PER B737 SRM 51-30-2 A
- [SDR AT9900039](https://openairdocs.org/sdr/AT9900039.md): Skin · cracked · Jan 17, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAINS FWD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SCREW. FABRICATED DOUBLER FROM 2024-T3.0125 THOUSANDS IAW B737 SRM 51-30-8. INSTALLED REPAIRED IAW B737 SRM 53-30-3 AND AIRTRAN RES NR 9938.
- [SDR AT99000039](https://openairdocs.org/sdr/AT99000039.md): Skin · cracked · Jan 17, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAIN'S FORWARD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SCREW. FABRICATED DOUBLER FROM 2024-T3.0125 THOUSANDS IAW B737 SRM 51-30-8. INSTALLED REPAIRED IAW B737 SRM 53-30-3 AND AIRTRAN RES NR 9938
- [SDR AT9900186](https://openairdocs.org/sdr/AT9900186.md): Angle · corroded · Jan 16, 1999 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE LAVATORY WALL HAT SECTION AT BS 300 LBL 35-50 HEAVY EXFOLIATION. MECHANICALLY REMOVED CORROSION, REMOVED HAT SECTION AND L ANGLE AND FABRICATED NEW REPLACEMENT SECTIONS, HEAT TREATED, PRIMED, AND INSTALLED
- [SDR AT9900124](https://openairdocs.org/sdr/AT9900124.md): Structure · corroded · Jan 15, 1999 · N460AT · Boeing 737214 · Fuselage Main, Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLIGHT DECK FLOOR BULGING AND RIVETS PULLING THROUGH. ALSO, THE NOSE WHEEL WELL AT STA 243, STRINGER 28R FRAME HAS EXFOLIATION AND THE E/E COMPARTMENT AT STA 351 STRINGER 23L WEB WITH CORROSION. REMOVED CORRO
- [SDR AT9900122](https://openairdocs.org/sdr/AT9900122.md): Structure · corroded · Jan 14, 1999 · N460AT · Boeing 737214 · Fuselage Main, Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL AREAS CORRODED. THE FORWARD CARGO DOOR FRAME AT STRINGER 25R, INTERCOASTAL FRAME AT STA 500 TO 520 RBL 25 IN THE FORWARD PIT, THE AFT CARGO AFT BULKHEAD UPPER SUPPORT STA 947 FROM L-25L TO L-25R, AND THE F
- [SDR AT9900040](https://openairdocs.org/sdr/AT9900040.md): Skin · damaged · Jan 14, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. STA 847 STR 22R HAS RIPPED SKIN. FABRICATED DOUBLER AND INSTALLED REPAIR IAW B737 SRM'S 53-30-3, 51-30-2, AND AIRTRAN RES NR 9937. (X)
- [SDR AT9900120](https://openairdocs.org/sdr/AT9900120.md): Door · corroded · Jan 11, 1999 · N460AT · Boeing 737214 · Air Conditioning Doors
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT TURBO FAN EXHAUST LOUVER DOOR HAS CORROSION AND PULLING THRU FASTENERS AT STA 685. REMOVED AND REPLACED RIGHT EXHAUST MODULATION ASSEMBLY IAW B737 MM 21-52-91. COMPLIED WITH RES NR 99335 AND INSTALLED B
- [SDR AT9900118](https://openairdocs.org/sdr/AT9900118.md): Skin · damaged · Jan 11, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND RIGHT SIDE FUSELAGE SKIN HAS A PREVIOUS.5 BY.75 CUT OUT, WITH FILLER INSTALLED AT FORWARD LOWER CORNER OF FORWARD GALLEY SERVICE R-1 DOOR. REMOVED FORWARD COVER PLATE TO FACILITATE REPAIR. FABRICATED NEW DOUBLER
- [SDR AT9900185](https://openairdocs.org/sdr/AT9900185.md): Angle · corroded · Jan 10, 1999 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AND A CRACK ABOVE SIDE WALL AND FLOOR ATTACHMENT AT BS 420-440. MECHANICALLY CLEAN CORROSION, FABRICATED ANGLE SUPPORT REPAIR, HEAT TREATED, DRILLED, DEBURRED, PRIMED AND INSTALLED IAW B737 SRM 51-40-3,
- [SDR AT9900123](https://openairdocs.org/sdr/AT9900123.md): Seat Track · cracked · Jan 10, 1999 · N460AT · Boeing 737214 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT DIFFERENT LOCATIONS. FIRST, THE LAVATORY WALL HAT SECTION AT STA 300 L-35 TO 50, SECONDLY THE SEAT TRACK IN THE CABIN AT STA 328 TO 344 BL 24 TO 75R, AND THE SIDE WALL IS CRACKED AND CORRODED AT STA 4
- [SDR AT9900117](https://openairdocs.org/sdr/AT9900117.md): Panel · damage · Jan 5, 1999 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PANEL 6403R HAS LEADING EDGE SCREW HOLE DAMAGE FROM WIND EROSION. PANEL HAS 15 PERCENT FLAME SPRAY MISSING. CLEANED PANEL AND REMOVED PAINT. APPLIED FIBERGLASS OVERLAY AND ASTRO STRIKE AND SEALED IAW B737 SRM 51-
- [SDR AT9900119](https://openairdocs.org/sdr/AT9900119.md): Stringer · cracked · Jan 4, 1999 · N460AT · Boeing 737214 · Wing, Longeron/Stringer
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING UPPER STRINGER NR 13 HAS 3 CRACK AT RIB AT WBL 135.00. REMOVED TEMPORARY REPAIR, FABRICATED NEW REPAIR PARTS, HEAT TREATED, PRIMED, PAINTED AND INSTALLED IAW B737 SRM 57-10-4 FIG 3, 57-40-4 FIG 3, 51-10-
- [SDR VJ9800381R1](https://openairdocs.org/sdr/VJ9800381R1.md): Brake · fire · Sep 11, 1998 · N460AT · Boeing 737214 · Landing Gear Brake System
  > NR 3 BRAKE CAUGHT ON FIRE AFTER HIGH SPEED TAXI TEST WAS PERFORMED; TEST COMMENCED AT 100 KNOTS AND AT 80 KNTS LOST PRESSURE AND WENT TO STOP ON RIGHT BRAKES. ATC ALERTED FLIGHT CREW FIRE WAS EMINATING FROM THE RIGHT WHEEL WELL AREA. BROUGHT THE AIRCRAFT TO
- [SDR VJ9800316](https://openairdocs.org/sdr/VJ9800316.md): Power Supply · inoperative · Sep 1, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.
- [SDR VJ0900298](https://openairdocs.org/sdr/VJ0900298.md): Battery Charger · inoperative · Aug 26, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHTS INOP. REPLACED THE LIGHT BATTERY CHARGER ASSY.
- [SDR VJ9800296](https://openairdocs.org/sdr/VJ9800296.md): Battery Pack · discharged · Aug 23, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > RT FUSELAGE EXTERNAL OVERWING EMERGENCY LIGHT FOUND INOPERATIVE DURING LAYOVER CHECK. REPLACED BATTERY PACK.
- [SDR VJ9800227](https://openairdocs.org/sdr/VJ9800227.md): Battery Pack · discharged · Jul 16, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK INOP. REPLACED BATTERY PACK.
- [SDR VJ9800198](https://openairdocs.org/sdr/VJ9800198.md): Gearbox · leaking · Jun 19, 1998 · N460AT · Boeing 737214 · Turbine Engine Accessory Drive
  > ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND OIL QTY WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. FOUND THAT THE NR 2 ENGINE HAD A BANJO FITTING BROKEN FROM THE GEARBOX LOSING OIL. REMOVED THE GEARBOX. THE HELICOIL WAS PULLED OUT OF THE G
- [SDR VJ9800197](https://openairdocs.org/sdr/VJ9800197.md): Light · inoperative · Jun 18, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT INOP AT L-2 DOOR DURING THE LAYOVER CHECK. REPLACED THE LIGHT ASSY.
- [SDR VJ9800009](https://openairdocs.org/sdr/VJ9800009.md): Switch · failed · Feb 9, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > EMERGENCY EXIT LIGHT WILL NOT ARM, ON FLIGHT CREW PRE FLIGHT. REMOVED AND REPLACED MICRO SWITCH IAW MM 33-51-121; OPS CHECKED GOOD.
- [SDR 98ZZZM160](https://openairdocs.org/sdr/98ZZZM160.md): Lamp · missing · Jan 6, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (M)
- [SDR 98ZZZM159](https://openairdocs.org/sdr/98ZZZM159.md): Lens · missing · Jan 6, 1998 · N460AT · Boeing 737214 · Emergency Lighting
  > DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (M)
- [SDR ZZDA5324297](https://openairdocs.org/sdr/ZZDA5324297.md): Angle · cracked · Nov 3, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND CRACK AT AFT CARGO COMPARTMENT OF APPROXIMATELY 1 INCH IN STRINGER TO FRAME REINFORCEMENT ANGLE AT STA 907, RIGHT, STR 26 UNDER TRANSITION PANEL. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-30-2. BLENDED OUT CRACK
- [SDR ZZDA3325297](https://openairdocs.org/sdr/ZZDA3325297.md): Lamp · inoperative · Oct 31, 1997 · N460AT · Boeing 737214 · Emergency Lighting
  > DURING LAYOVER CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT INOPERABLE, ROW 15. RELAMPED ROW 15 FLOOR TRACK EMERGENCY LAMP IAW MM 33-51-00. OPS CHECK GOOD. (X)
- [SDR ZZDA3325097](https://openairdocs.org/sdr/ZZDA3325097.md): Power Supply · fire · Oct 31, 1997 · N460AT · Boeing 737214 · Emergency Lighting
  > RIGHT OVERWING EXTERIOR LIGHT INOPERABLE. INSPECTED POWER SUPPLY ASSY. REMOVED C/P, CHECKED CIRCUIT BOARD. INSTALLED IN RT POWER SUPPLY AND OPS CHECKED GOOD. LT BATTERY PACK INSTALLED IN RT POWER SUPPLY LIGHT STAYS ON, EVEN IN ARM. UPON REINSTALLING, RT B
- [SDR ZZDA5721197](https://openairdocs.org/sdr/ZZDA5721197.md): Skin · dented · Oct 10, 1997 · N460AT · Boeing 737214 · Trailing Edge Flaps
  > DURING C-CHECK AT AERO CORP, FOUND RIGHT WING INBOARD FLAP L/E HAS 1.0 INCH BY 2.0 INCH DENT AT WBL 80.0 OUT OF LIMITS. CUT OUT DENT AREA IAW B 737 57-50-4 FIG 3. FABRICATED FILLERS AND DOUBLER IAW B 737 SRM 57-50-4 FIG 3. ALODINED AND PRIMED IAW B 737 SRM
- [SDR ZZDA5322197](https://openairdocs.org/sdr/ZZDA5322197.md): Skin · corroded · Sep 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT AERO CORP, AT AFT CARGO PIT FROM STA 727B TO STA 767, FOUND CORROSION AROUND NUTPLATES (30 EACH) AT UNDERSIDE OF THE LT TRANSITION PANEL TO BE BEYOND LIMITS. REMOVED THE TRANSITION PANEL FROM BS 727 - BS 767, REMOVED CORROSION STA 745 AND ST
- [SDR ZZDA5326897](https://openairdocs.org/sdr/ZZDA5326897.md): Skin · misdrilled · Sep 19, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT AERO CORP, FOUND BELLY SKIN HAS DOUBLER DRILLED HOLES AT STA 328 BETWEEN STR 25 - STR 26. FABRICATED DOUBLER FROM 2024 T3.050 INCH 12 INCHES BY 16 INCHES IAW B 737 SRM 53-30-3. INSTALLED IAW B 737 SRM 53-30-3, FIG 1. (X)
- [SDR ZZDA5327097](https://openairdocs.org/sdr/ZZDA5327097.md): Support · corroded · Sep 14, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND CABIN BS 344 - BS 380 RBL 15 FLOOR SUPPORT UPPER SURFACE CORRODED BS 350 - BS 354. FABRICATED SUPPORT FROM 7075 T6.060 INCH 15 INCHES BY 2 INCHES AND FILLER FROM 7075 T6.100 INCH 12 INCHES BY 2 INCHES IAW B 737 SRM 51-40-4
- [SDR ZZDA5321697](https://openairdocs.org/sdr/ZZDA5321697.md): Support · corroded · Sep 12, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND FORWARD CABIN CORRODED ON FLOOR SUPPORTS WL 208.1 FROM STA 251.6 TO STA 328 BL AND BL 12R. REMOVED THE CORRODED FLOOR SUPPORTS, CORRODED BEYOND LIMITS IAW B 737 SRM 53-10-1 FIG 1. REMOVED FWD LAVATORY VANITY, COCKPIT DOOR,
- [SDR ZZDA5327697](https://openairdocs.org/sdr/ZZDA5327697.md): Seat Track · broken off · Sep 10, 1997 · N460AT · Boeing 737214 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK AT AERO CORP, LT INBD SEAT TRACK LUGS AT STATIONS 480-520, AND STATIONS 540-597 ARE BROKEN OFF. FABRICATED SEAT TRACKS FROM BAC 1500-841 44.50 INCHES AND BAC 1520 792 77.5 INCHES BY 3.5 INCHES IAW B 737 SRM 53-10-5, FIG 1. INSTALLED IAW B 737 S
- [SDR ZZDA5322097](https://openairdocs.org/sdr/ZZDA5322097.md): Skin · cracked · Sep 9, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT AERO CORP, FOUND 5 EACH FASTENERS WITH CRACK INDICATIONS W/HFEC RT SECTION 41 SKIN. REMOVED COCKPIT SIDE PANELS AND INSULATION FOR ACCESS. REMOVED CRACKED AREAS AND HFEC INSPECTED FOR VERIFICATION OF REMOVAL IAW SRM 51-00-00 PART 6 FIG 23.
- [SDR ZZDA5323197](https://openairdocs.org/sdr/ZZDA5323197.md): Seat Track · corroded · Sep 5, 1997 · N460AT · Boeing 737214 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK AT AERO CORP, FOUND OUTBOARD SEAT TRACK HAS CORROSION OUT OF LIMITS FROM BS 360 TO BS 480. REMOVED SEAT TRACK AND REPLACED WITH NEW TRACK (1A-24092-1) BAC 1520-792 7178T6 EXTRUSION STA 360 - STA 480, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRI
- [SDR ZZDA5321997](https://openairdocs.org/sdr/ZZDA5321997.md): Chord · corroded · Sep 5, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND T-CHORD FROM BS 324 - BS 360 STR 28R CORRODED BEYOND LIMITS. FABRICATED ANGLE REPAIR FROM 301 1/2 CRES STAINLESS STEEL.050 INCH IAW RES 04403 AND NEW BRACKET FROM 7075 T6.003 INCH. DIMENSIONS: ANGLES 11.6250 INCHES BY 1
- [SDR ZZDA5321897](https://openairdocs.org/sdr/ZZDA5321897.md): Chord · corroded · Sep 5, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND T-CHORD HAS HEAVY CORROSION FROM STA 360 - STA 294.5, STR 28L. FOUND TO BE BEYOND LIMITS. REMOVED DAMAGED T-CHORD FROM STA 294.5 - STA 360 IAW BAC 737 SRM 51-30-2. REPLACED DAMAGED T-CHORD WITH A NEW SECTION OF T-CHORD IAW
- [SDR ZZDA5326797](https://openairdocs.org/sdr/ZZDA5326797.md): Skin · corroded · Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOVED AND REPLACED SKINS AT STA 259.5 - STA 360, BL ZERO, STR 24L AND 24R IAW B 737 SRM 51-30-2 AND BA
- [SDR ZZDA5323497](https://openairdocs.org/sdr/ZZDA5323497.md): Support · corroded · Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY LONGITUDINAL FLOOR SUPPORT AT BS LBL 14 HAS CORROSION. BLENDED CORROSION MATERIAL LOSS 50 PERCENT BEYOND LIMITS IAW B 737 SRM 53-10-1 AND FORMED NEW SUPPORT, DRILLED, DEBURRED, TREATED, PRIMED, AND PAINTED IAW B
- [SDR ZZDA5321597](https://openairdocs.org/sdr/ZZDA5321597.md): Floorbeam · corroded · Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor Beam
  > DURING C-CHECK AT AERO CORP, AFT LAVATORY FLOOR BEAM UPPER CHORD BS 1006 HAS CORROSION AT LBL 9. FABRICATED DOUBLER FROM 7075 T6.071 INCH 10.50 INCHES, 1.0625 INCH, AND 10.0625 INCHES BY 1.0625 INCHES. FABRICATED FILLER FROM BAC 1505-100817, 44 INCHES BY 3
- [SDR AADA5323597](https://openairdocs.org/sdr/AADA5323597.md): Support · corroded · Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY FLOOR SUPPORT BEAM BS 986.5 - BS 1016 LBL 20 DIAGONALLY TO LBL 4 CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT FROM STA 986.5 - STA 1016. CORROSION REMOVAL BEYOND LIMITS PER 737 MM 51-10-6 AND MM 51-10-2. FABR
- [SDR 98ZZZX108](https://openairdocs.org/sdr/98ZZZX108.md): Skin · corroded · Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOVED AND REPLACED SKINS AT STA 259.5 - STA 360, BL ZERO, STR 24L AND 24R IAW B 373 SRM 51-30-2 AND BA
- [SDR ZZDA5317997](https://openairdocs.org/sdr/ZZDA5317997.md): Skin · corroded · Sep 2, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, LT FS 967 FOUND CORROSION UNDER FASTENER HEAD AT STR 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. FABRICATED FILLER FROM 2024 T3.071 INCH 1.1250 INCHES BY 1 INCH. FABRICATED REPAIR DOUBLER FROM 2024 T3.090 INCH 11.50 INCHES BY 6 INCHES. INSTAL
- [SDR 97ZZZM1052](https://openairdocs.org/sdr/97ZZZM1052.md): Skin · corroded · Sep 2, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, LEFT FUSELAGE STATION 967 CORROSION UNDER FASTENER HEAD AT STRINGER 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. (M)
- [SDR ZZDA5322997](https://openairdocs.org/sdr/ZZDA5322997.md): Floor Beam · corroded · Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor Beam
  > DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR SUPPORT AT LBL 12 IAW B 737 51-30-2 AND FABRICATED NEW FLOOR SUPPORT FROM 60-8004 15 INCHES BY 2 INCHES IAW B 737 SRM 51-30-2.
- [SDR ZZDA5322897](https://openairdocs.org/sdr/ZZDA5322897.md): Floor Beam · corroded · Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor Beam
  > DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM BS 328 HAS CORROSION ON UPPER CHORD FROM RBL 48 TO LBL 12, FOUND TO BE BEYOND LIMITS. REMOVED CORROSION ON FLOOR BEAM PER 737 SRM 51-20-6. REMOVED OVER 20 PERCENT MATERIAL LOSS, OUT OF LIMITS PER
- [SDR ZZDA5322797](https://openairdocs.org/sdr/ZZDA5322797.md): Floor Beam · corroded · Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM BS 294 HAS CORROSION ON UPPER CHORD FROM RBL 12 TO RBL 50. REMOVED CORROSION FROM THE UPPER CHORD FLOOR BEAM IAW B737 SRM 51-10-1. MATERIAL LOSS MORE THAN 50 PERCENT OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW UPPER CHORD AND 10
- [SDR ZZDA5321797](https://openairdocs.org/sdr/ZZDA5321797.md): Floor Beam · corroded · Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor Beam
  > DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR BEAM AT LBL 12 IAW B 737 SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT IAW B 737 SRM 53-40-4. TREATED AND PRIMED IAW B 737 SRM 51

Next page: https://openairdocs.org/deregistered/N460AT-2000-07-06/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 = 'N460AT' AND deregistration_id = 'N460AT-2000-07-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N460AT-2000-07-06/reports

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