# Service difficulty reports: N752AT, cancelled May 9, 2017

A list on [N752AT, cancelled May 9, 2017](https://openairdocs.org/deregistered/N752AT-2017-05-09.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 3 · 121 reports

- [SDR DALA2016031702172](https://openairdocs.org/sdr/DALA2016031702172.md): Wire · disconnected · Mar 15, 2016 · N752AT · Boeing 757212 · Light System Wiring
  > ROW 23 DEF MOUNT EMERGENCY LIGHT INOPERATIVE. T/S IAW FIM 33-51-813-802 FOUND WIRE UNPINNED. REPINNED WIRE, CKS GOOD.
- [SDR DALA2016030101839](https://openairdocs.org/sdr/DALA2016030101839.md): Skin · damaged · Feb 25, 2016 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > SKIN AT BS 1482 ON S7L LIGHTNING STRIKE DAMAGE.: BLENDED OUT DAMAGE, BEYOND LIMITS IAW SRM 53-00-01 CUTOUT DAMAGE, 1" HOLE IAW SRM 53-00-01, REPAIR 13, 672231 HFEC INSPECTED CUTOUT IAW NDT PART 6 51-00-01. NO CRACKS FOUND QC2084. REPAIR IS IN ZONE B THICKN
- [SDR DALA2016012500578](https://openairdocs.org/sdr/DALA2016012500578.md): Light · inoperative · Jan 24, 2016 · N752AT · Boeing 757212 · Emergency Lighting
  > ROW 37, RT EMERGENCY ESCAPE INOPERATIVE. REPLACED THE LIGHT ASSY, OPS OK.
- [SDR DALA2015103006608](https://openairdocs.org/sdr/DALA2015103006608.md): Door Frame · contaminated · Oct 29, 2015 · N752AT · Boeing 757212 · Service Doors
  > R3 DOOR HAS TROUBLE ARMING, TWO CONSECUTIVE FLIGHTS CAUSING DELAYS. CLEANED AND LUBED DOOR, FOUND DEBRI IN DOOR FRAME, DOOR OPS NORMAL IAW AMM 52-11.
- [SDR DALA2015100205938](https://openairdocs.org/sdr/DALA2015100205938.md): Skin · dented · Sep 13, 2015 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND DENT ON RK FWD FUSELAGE. BS 215. 7 O'CLOCK POSITION. 15" AFT OF RADOME BULKHEAD. REF ERA 539404-14, REV ORIG FOR REPAIR.
- [SDR DALA2015060103558](https://openairdocs.org/sdr/DALA2015060103558.md): Connector · disconnected · May 30, 2015 · N752AT · Boeing 757212 · Light System Wiring
  > IN-SEAT ESCAPE PATH LIGHT AT ROW 27R INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT 27F. RECONNECTED, OPS OK.
- [SDR DALA2015040702642](https://openairdocs.org/sdr/DALA2015040702642.md): Wire Harness · disconnected · Apr 5, 2015 · N752AT · Boeing 757212 · Light System Wiring
  > 23D IN SEAT EMERGENCY LIGHT INOPERATIVE. FOUND HARNESS DISCONNECTED UNDER SEAT. RECONNECTED HARNESS, OPS OK.
- [SDR DALA2014102305722](https://openairdocs.org/sdr/DALA2014102305722.md): Skin · damaged · Oct 22, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED BS 1621, S26R. REPAIRED IAW ER/A 519947-14AD, REV A.
- [SDR DALA2014102305721](https://openairdocs.org/sdr/DALA2014102305721.md): Skin · corroded · Oct 22, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > DURING A SERVICE CHECK, CORROSION WAS FOUND ON SKIN BS 1680-1700 STRINGERS 26-29R UNDER THE LAV SERVICE PAN, REPAIRED IAW ER/A 519950-14AD, REV A.
- [SDR DALA2014090304888](https://openairdocs.org/sdr/DALA2014090304888.md): Connector · disconnected · Sep 2, 2014 · N752AT · Boeing 757212 · Light System Wiring
  > ON SERVICE CHECK FOUND ROW 20DEF EMERGENCY LIGHT INOPERATIVE. FOUND ELECTRIC CONNECTOR DISCONNECTED, RECONNECTED AND OPS CHECKED GOOD.
- [SDR DALA2014090204861](https://openairdocs.org/sdr/DALA2014090204861.md): Shuttle Valve · failed · Sep 1, 2014 · N752AT · Boeing 757212 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF AT ROTATION, SEVERAL UPPER EICAS AMBER ANNUCIATORS ILLUMINATED BRIELY AND THEN WENT OUT WHEN THE GEAR HANDLE WAS RAISED IT WOULD NOT GO PAST OFF POSITION INTIALLY, BUT THEN WENT UP AND GEAR RETRACTED NORMALLY. FOUND RT GEAR TRUCK POSITIONER SH
- [SDR DALA2014090204862](https://openairdocs.org/sdr/DALA2014090204862.md): Strut · low pressure · Aug 31, 2014 · N752AT · Boeing 757212 · Nose/Tail Landing Gear Strut/Axle
  > CAPTAIN COULD NOT GET THE GEAR HANDLE TO COME TO FULL UP POSITION, WITH GEAR AMBE LIGHTS ON, ACFT DIVERTED. PERFORMED QRH PROCEDURES, OVERRIDE BUTTON WAS UNSUCCESSFUL, LOWERED GEAR HANDLE AND GOT 3 GREEN LIGHTS. ON ARRIVAL PERFORMED PSEU BITE WITH "NOSE GEAR
- [SDR DALA2014082004612](https://openairdocs.org/sdr/DALA2014082004612.md): Light · inoperative · Aug 20, 2014 · N752AT · Boeing 757212 · Emergency Lighting
  > SEAT 20F, INSEAT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA14031746904](https://openairdocs.org/sdr/DALA14031746904.md): Skin · damaged · May 22, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN STR 18L DAMAGED AT BS 1380, C/W ERA 526120-14, REV ORIG.
- [SDR DALA14031696904](https://openairdocs.org/sdr/DALA14031696904.md): Skin · dented · May 22, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1382 BELOW STRINGER 19L. COMPLIED WITH ERA 526120-14, REV ORIGINAL.
- [SDR DALA14031766904](https://openairdocs.org/sdr/DALA14031766904.md): Skin · dented · May 20, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > DENT AND TOOL DAMAGE FOUND ON SKIN.
- [SDR DALA14030886904](https://openairdocs.org/sdr/DALA14030886904.md): Skin · corroded · May 16, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > SKIN FOUND CORRODED BS 440 STRINGER 24L. REPAIRED IAW ERA 525750-14 REV O
- [SDR DALA14030866904](https://openairdocs.org/sdr/DALA14030866904.md): Keelbeam · corroded · May 16, 2014 · N752AT · Boeing 757212 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM RT WHEEL WELL JUST AFT OF A/C LEVELING PLACARD. REPAIRED IAW ERA 525717-14 REV O
- [SDR DALA14031446904](https://openairdocs.org/sdr/DALA14031446904.md): Skin · corroded · May 15, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON THE BUTT SPLICE PLATE AT APPROX BS 440, STRINGER 24L. REPAIRED IAW ER/A 525750-14 SECTION II.
- [SDR DALA14030856904](https://openairdocs.org/sdr/DALA14030856904.md): Sealant · loose · May 13, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > SEALANT BLOWN OUT AND POWDER FALLING OUT FROM BETWEEN SKINS 13L AND 14L. REMOVED LOOSE SEALANT AND CLEANED AREA IAW ERA 525753-14
- [SDR DALA2015102806559](https://openairdocs.org/sdr/DALA2015102806559.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 1051 AND S6L HAD A LIGHTNING STRIKE.
- [SDR DALA2015102806558](https://openairdocs.org/sdr/DALA2015102806558.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN HAD LIGHTNING STRIKE DAMAGE AT BS 1030 TWO INCHES UP FROM S6L.
- [SDR DALA14027346904](https://openairdocs.org/sdr/DALA14027346904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 977, S6L LIGHTNING BURNED. REMOVED FASTENER CLEANED AREA INSPECTED WITH 10X MAGNIFICATION. REMOVED, TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026066904](https://openairdocs.org/sdr/DALA14026066904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 1004, STRINGER 6L HAS A LIGHTNING BURN. REMOVED FASTENER CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026056904](https://openairdocs.org/sdr/DALA14026056904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 1130, STRINGER 7L HAS A LIGHTNING STRIKE, REMOVED FASTENER, CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01 FIG 201.
- [SDR DALA14026046904](https://openairdocs.org/sdr/DALA14026046904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1086, SIX INCHES DOWN FROM STRINGER 6L HAS LIGHTNING STRIKE DAMAGE. DRILLED OUT DAMAGE INSPECTED WITH 10X. TREATED PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026036904](https://openairdocs.org/sdr/DALA14026036904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1160, FOUR INCHES DOWN STRINGER 7L LIGHTNING STRIKE DAMAGE, REMOVED FASTENER, CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026026904](https://openairdocs.org/sdr/DALA14026026904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1337, TWO INCHES DOWN FROM STRINGER 6L, LIGHTNING STRIKE DAMAGE DRILLED OUT DAMAGE INSPECTED WITH 10X. TREATED, PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026016904](https://openairdocs.org/sdr/DALA14026016904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 1705 AND S8L BURNED. R & R BLIND FASTENER IAW SRM 53-00-01, SECTION 2, PARA 4.
- [SDR DALA14026006904](https://openairdocs.org/sdr/DALA14026006904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 525, S11L, LIGHTNING STRIKE, R & R FASTENER WITH A BLIND FASTENER IAW 757-200, SRM 53-00-01, SECTION 2, PARA 4.
- [SDR DALA14025996904](https://openairdocs.org/sdr/DALA14025996904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 952 S6L, LIGHTNING DAMAGE. REMOVED FASTENER, CLEANED AREA, INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED. INSTALLED BLIND FASTENER IAW SRM 53-00-01, FIG 201.
- [SDR DALA14025986904](https://openairdocs.org/sdr/DALA14025986904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 886 AND S56L IS BURNED. REMOVED FASTENER, CLEANED AREA, INSPECTED, WITH 10X DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND FASTENER IAW SRM 53-00-01, FIG 201.
- [SDR DALA14025976904](https://openairdocs.org/sdr/DALA14025976904.md): Skin · damaged · Apr 24, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FASTENER AT BS 500 S11L BURNED. R & R WITH BLIND FASTENER IAW SRM 53-00-01, SECTION 2, PARA 4.
- [SDR DALA14026166904](https://openairdocs.org/sdr/DALA14026166904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1374, FOUR INCHES DOWN FROM STRINGER 6L HAS LIGHTNING DAMAGE. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026156904](https://openairdocs.org/sdr/DALA14026156904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1516, JUST BELOW STRINGER 7L HAS A LIGHTNING STRIKE. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION, TREATED, PAINTED AND INSTALLED BLIND RIVET IAW 53-00-01, FIG 201.
- [SDR DALA14026146904](https://openairdocs.org/sdr/DALA14026146904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1550 ABOUT FIVE INCHES DOWN FROM STRINGER 7L HAS A LIGHTNING STRIKE. DRILL OUT DAMAGE AREA.159 IAW SRM 53-00-01, FIG 201, SECTION I. PERFORMED HFEC IAW NDT 51-00-16, NO DEFECTS FOUND. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00
- [SDR DALA14026136904](https://openairdocs.org/sdr/DALA14026136904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1585, THREE INCHES DOWN FROM STRINGER 7L HAS A LIGHTENING STRIKE. DRILLED OUT DAMAGE AREA.159 IAW SRM 53-00-01, FIG 201, SECTION I, PERFORMED BHEC IAW NDT 51-00-16. NO DEFECTS FOUND. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00
- [SDR DALA14026126904](https://openairdocs.org/sdr/DALA14026126904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > STATIC DISCHARGE ON SKIN AT BS 1195 AND 2.5 INCHES ABOVE STRINGER 9L. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026116904](https://openairdocs.org/sdr/DALA14026116904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > STATIC DISCHARGE ON SKIN AT BS 1225, THREE INCHES BELOW STRINGER 9L. DRILLED OUT DAMAGE INSPECTED WITH 10X MAGINIFCATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026106904](https://openairdocs.org/sdr/DALA14026106904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > STATIC DISCHARGE ON SKIN AT BS 1233, FIVE INCHES BELOW STRINGER 9L. DRILLED OUT DAMAGE, INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026096904](https://openairdocs.org/sdr/DALA14026096904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > STATIC DISCHARGE ON FASTENER AT BS 1259 AND FIVE INCHES BELOW STRINGER 9L DRILLED OUT DAMAGE, INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA14026086904](https://openairdocs.org/sdr/DALA14026086904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1482 STRINGER 7L HAS LIGHTNING STRIKE DAMAGE. BLENDED OUT DAMAGE. FOUND BEYOND LIMITS IAW SRM 53-00-01, CUT OUT DAMAGE, ONE INCH HOLE IAW SRM 53-00-01, REPAIR 13. HFEC INSPECTED CUTOUT IAW NDT PART 6 51-00-01, NO CRACKS FOUND. FABRICATED D
- [SDR DALA14026076904](https://openairdocs.org/sdr/DALA14026076904.md): Skin · damaged · Apr 23, 2014 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > ACFT SKIN AT BS 1405 AND FOUR INCHES DOWN FROM STRINGER 6L HAS LIGHTNING DAMAGE. DRILLED OUT DAMAGE. INSPECTED WITH 10X MAGIFICATION. TREATED AND PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.
- [SDR DALA13056546904](https://openairdocs.org/sdr/DALA13056546904.md): Skin · bulged · Oct 29, 2013 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > SKIN BS 1620 S26R BULGED AND HAS POPPED RIVET HEADS. REPAIRED IAW PRI 519947-14, REV 3. COMPLETED THROUGH STEP (11).
- [SDR DALA13056406904](https://openairdocs.org/sdr/DALA13056406904.md): Skin · corroded · Oct 29, 2013 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > SKIN AT AFT LAVATORY SERVICING PANEL IS CORRODED. REMOVED CORROSION IAW PRI 519950-14 AND IAW SRM 53-00-01. CORROSION FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW PRI 519950-14 AD C/W ON ERA 519950-14AD, REV O, 28OCT13 D.
- [SDR DALA13056396904](https://openairdocs.org/sdr/DALA13056396904.md): Skin · cracked · Oct 29, 2013 · N752AT · Boeing 757212 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED DURING HFEC INSPECTION IAW PRI 519950-14 REV O STEP 4 AT BS 1700 BETWEEN STRINGERS 29 & 30R APPROXIMATELY LENGTH 1 INCH. REMOVED SKIN AND REPAIRED IAW PRI 519950-14AD REV 4 C/W ERA 519950-14 AD.
- [SDR DALA13056386904](https://openairdocs.org/sdr/DALA13056386904.md): Frame · corroded · Oct 29, 2013 · N752AT · Boeing 757212 · Fuselage Main, Frame
  > TWO FRAME ANGLES CORRODED AT BS 1700 BETWEEN STRINGERS 29 & 30R. REMOVED FRAME ANGLES AND REPLACED.
- [SDR DALA1318116904](https://openairdocs.org/sdr/DALA1318116904.md): Lamp · inoperative · Sep 3, 2013 · N752AT · Boeing 757212 · Emergency Lighting
  > DURING DRC, FOUND EMERGENCY PATH LIGHT SEAT 36D, INOPERATIVE. R & R LAMP ASSY. OPS CHECKED NORMAL.
- [SDR DALA1311256904](https://openairdocs.org/sdr/DALA1311256904.md): Frame · cracked · Apr 27, 2013 · N752AT · Boeing 757212 · Fuselage Main, Frame
  > WHILE PERFORMED EDDY CURRENT INSPECTION OF CARGO DOOR, FRAMES IAW OPN 50321AD. FOUND BS 1440 FRAME WEB CRACKED AT STOP FITTING NR 6 AND ADJACENT FASTENER. CUT AND REMOVED DAMAGED SECTION OF WEB AND INSPECTED, NO DISCREPANCIES. INSURANCE CUT MADE FABRICATED
- [SDR DALA14028766904](https://openairdocs.org/sdr/DALA14028766904.md): Threshold · cracked · Dec 18, 2012 · N752AT · Boeing 757212 · Fuselage Miscellaneous Structure
  > R1 CORNER CAP FWD CRACKED. REMOVED DAMAGED PART IAW ERA 06-489867-14MA, REV F, SECTION 3. THRESHOLD REPAIRED IAW ERA 06-489867-14, REV F. INSTALLED IAW ERA 06-489867-14 MA, REV F, SECTION 3.

Next page: https://openairdocs.org/deregistered/N752AT-2017-05-09/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 = 'N752AT' AND deregistration_id = 'N752AT-2017-05-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N752AT-2017-05-09/reports

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