# Service difficulty reports: N785AT, cancelled Jan 27, 2011

A list on [N785AT, cancelled Jan 27, 2011](https://openairdocs.org/deregistered/N785AT-2011-01-27.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 · 67 reports

- [SDR DHL2008785001](https://openairdocs.org/sdr/DHL2008785001.md): Skin · damaged · Apr 11, 2008 · N785AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > MULTIPLE LIGHTNING STRIKES FOUND DURING SERVICE CHECK. CUT OUT LIGHTNING STRIKE DAMAGE AT BS 435 TO 440, STR 25R, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A, 53-30-2 FIG 2, AND 51-30-2.
- [SDR DHL2008011702](https://openairdocs.org/sdr/DHL2008011702.md): Pressure Panel · delaminated · Jan 17, 2008 · N785AT · Boeing 727214 · Fuselage Main, Bulkhead
  > 15 BY 12 AREA DELAMINATED ON PANEL NR 3455 JUST FWD OF MLG WHEEL WELL AT STA 840.
- [SDR DHL2007785021](https://openairdocs.org/sdr/DHL2007785021.md): Stringer · corroded · Nov 7, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > AFT BAG PIT HAS CORROSION WITH EXFOLIATION ON STRINGER 30 RT BS 1172. REMOVED INTERCOSTAL AND FITTING IAW B-727 SRM 51-30-2, CUT OUT DAMAGED STRINGER 30 SECTION, FABRICATED STRINGER REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 5. FABRICATE
- [SDR DHL2007785044](https://openairdocs.org/sdr/DHL2007785044.md): Shear Tie · corroded · Nov 6, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION BETWEEN STRINGER 30 AND STRINGER 29R SHEAR TIE BS 1166. REMOVED CORROSION FROM SHEAR TIE IAW B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. CUT OUT SHEAR TIE IAW B-727 SRM 51-10-2. FAB
- [SDR DHL2007785020](https://openairdocs.org/sdr/DHL2007785020.md): Shear Tie · corroded · Nov 6, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION AT LEFT STRINGER 29L BS 1166 SHEAR TIE ATTEND. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. CUT OUT SHEAR TIE IAW B-727 SRM 51-10-1 AND 53-10-4 FIGURE 11. FABRI
- [SDR DHL2007785019](https://openairdocs.org/sdr/DHL2007785019.md): Shear Tie · corroded · Nov 6, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION BEHIND SHEAR TIE BS 1166 LEFT SIDE STRINGER 30. REMOVED CORROSION AT BS 1166 SHEAR TIE STRINGER 30 IAW B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED AREA IAW B-727 SRM 53-10-4 FIGURE 11. F
- [SDR DHL2007785017](https://openairdocs.org/sdr/DHL2007785017.md): Angle · gouged · Nov 6, 2007 · N785AT · Boeing 727214 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FRAME AT BS 1050 HAS A GOUGE ABOVE STRINGER 27R. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE IAW B-727 SRM 53-10-2 FIGURE 5 AND SRM 51-40-3 FIGURE 1. HEAT TREATED ANGLE TO T6 CONDITION IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A.
- [SDR DHL2007785042](https://openairdocs.org/sdr/DHL2007785042.md): Attach Fitting · corroded · Nov 5, 2007 · N785AT · Boeing 727214 · Fuselage Main, Attach Fittings
  > CORROSION WITH EXFOLIATION AT BS 1183, STRINGER 17R ATTACHED FITTING. REMOVED ATTACH FITTING AT STRINGER 17R BS 1183 IAW B-727 SRM 51-30-2. FABRICATED NEW ATTACH FITTING IAW BOEING DRAWING NR 65-24276 AND J C NR EC-00596-001. TREATED AND PRIMED NEW FITTING
- [SDR DHL2007785041](https://openairdocs.org/sdr/DHL2007785041.md): Shear Tie · corroded · Nov 5, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION AT STRINGER 25R, BS 1166 SHEAR TIE AFT END. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1. REMOVED SHEAR TIE IAW B-727 SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW B-727 SRM 53-10-2 FIGURE 5 AND
- [SDR DHL2007785032](https://openairdocs.org/sdr/DHL2007785032.md): Stringer · cracked · Nov 5, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > AFT PIT TAIL PIECE OF STRINGER 25R BS 1180 AT SHEAR TIE CRACKED AND EXFOLIATED. REMOVED STRINGER FITTING AT BS 1183 STRINGER 25R IAW B-727 SRM 51-30-2. CUT OUT STRINGER SECTION AT BS 1160 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW STRINGER SECTION AND R
- [SDR DHL2007785029](https://openairdocs.org/sdr/DHL2007785029.md): Skin · dented · Nov 5, 2007 · N785AT · Boeing 727214 · Leading Edge Devices
  > PROTRUDING DENT ON NR 7 SLAT INBOARD UPPER SURFACE WING STATION 601. EVALUATED DENT AND FOUND OUT OF LIMITS IAW B-727 SRM 57-50-1 FIGURE 2. REMOVED NR 7 SLAT ACCESS PANELS IAW B-727 SRM 51-30-2, CUT OUT DAMAGED AREA AND COVE SKIN IAW B-727 SRM 51-10-1. FABR
- [SDR DHL2007785046](https://openairdocs.org/sdr/DHL2007785046.md): Frame · corroded · Nov 4, 2007 · N785AT · Boeing 727214 · Fuselage Main, Frame
  > SURFACE CORROSION AT BS 1090 ABOVE STRINGER 28R. CUT OUT DAMAGED AREA AT BS 1090 ABOVE STRINGER 28R IAW B-727 SRM 51-40-3 FIGURE 1. FABRICATED NEW FRAME DOUBLER IAW B-727 SRM 53-10-2 FIGURE 5, SRM 51-30-1 FIGURE 3 AND SRM 51-40-2 FIGURE 1. HEAT TREATED MATE
- [SDR DHL2007785016](https://openairdocs.org/sdr/DHL2007785016.md): Frame · dented · Nov 4, 2007 · N785AT · Boeing 727214 · Fuselage Main, Frame
  > DENT AT BS 1030 FRAME, JUST OUTBOARD OF STRINGER 27R. REMOVED FASTENERS FROM BS 1030 IAW B-727 SRM 51-30-2, CUT OUT DAMAGED AREAS AND FABRICATED REPAIR ANGLE DOUBLER IAW B-727 SRM 51-40-3 FIGURE 1 AND SRM 53-10-2 FIGURE 5. HEAT TREATED REPAIR ANGLE TO T6 CON
- [SDR DHL2007785031](https://openairdocs.org/sdr/DHL2007785031.md): Rib · cracked · Nov 2, 2007 · N785AT · Boeing 727214 · Leading Edge Devices
  > NR 7 SLAT INBOARD RIB AND OUTBOARD RIB FOR SLAT INBOARD TRACK ARE CRACKED. REMOVED 2 EACH DAMAGED RIBS FROM NR 7 SLAT IAW B-727 SRM 51-30-2. FABRICATED NEW RIBS IAW B-727 SRM 57-50-2 FIGURE 2 AND 51-20-1. HEAT TREATED NEW RIBS IAW FAS ENGINEERING REPORT NR
- [SDR DHL2007785034](https://openairdocs.org/sdr/DHL2007785034.md): Intercostal · damaged · Nov 2, 2007 · N785AT · Boeing 727214 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT INTERCOSTAL AT STRINGER 28R BETWEEN BS 540 AND BS 560 HAS ELONGATED HOLES AT BOTTOM. REMOVED INTERCOSTAL FROM BS 540 TO BS 560 STRINGER 28R IAW B-727 SRM 51-30-2. FABRICATED NEW INTERCOSTA IAW B-727 SRM 53-10-2 FIGURE 3 AND 51-20-1.
- [SDR DHL2007785048](https://openairdocs.org/sdr/DHL2007785048.md): Stringer · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STRINGER 28R BS 560. REMOVED INTERCOSTALS FROM BS 540 TO BS 580 STRINGER 28R FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF STRINGER DIMENSION 17.75" IAW B-727 SRM 53-10-13 FIGURE 1. FABRICATED NEW STRINGER SECTION IAW B-727
- [SDR DHL2007785033](https://openairdocs.org/sdr/DHL2007785033.md): Angle · cracked · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS CUT OUT AREA, LOWER SPLICE ANGLE AT BS 1217 RBL 10 IS CRACKED. REMOVED CRACKED SPLICE ANGLE IAW B-727 SRM 51-30-2, FABRICATED NEW ANGLE IAW B-727 SRM 53-10-2 FIGURE 2, 51-10-3, AND 51-20-1. TREATED AND PRIMED NEW SPLICE ANGLE IAW B-727 SRM 51-1
- [SDR DHL2007785025](https://openairdocs.org/sdr/DHL2007785025.md): Skin · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > FORWARD PIT SKIN CORRODED AT ANTENNA CUT OUT BS 510 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS AND ANTENNA RING IAW B-727 SRM 51-30-2, REMOVED CORROSION FROM SKIN IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-30-1 FIGURE 1. REMOV
- [SDR DHL2007785018](https://openairdocs.org/sdr/DHL2007785018.md): Shear Tie · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION AT SHEAR TIE, BS 950B LEFT SIDE OF STRINGER 30. REMOVED FASTENERS AT BS 950B LEFT SIDE OF STRINGER 30 IAW B-727 SRM 51-30-2. REMOVED CORROSION AT FRAME SHEAR TIE IAW B-727 SRM 51-10-6. CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FI
- [SDR DHL2007785014](https://openairdocs.org/sdr/DHL2007785014.md): Stringer · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > INTERGRANULAR CORROSION NOTED ON STRINGER 26R AT BS 720E + 19". CUT OUT DAMAGED SECTION IAW B-727 SRM 53-10-2 FIGURE 1. FABRICATED REPAIR FILLER. FABRICATED REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PA
- [SDR 2007785014](https://openairdocs.org/sdr/2007785014.md): Stringer · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > INTERGRANULAR CORROSION NOTED ON STRINGER 26R AT BS 720E + 19". CUT OUT DAMAGED SECTION IAW B-727 SRM 53-10-2 FIGURE 1. FABRICATED REPAIR FILLER. FABRICATED REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND SRM 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PA
- [SDR DHL2007785010](https://openairdocs.org/sdr/DHL2007785010.md): Stringer · corroded · Nov 1, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > SLIGHT BULGING ON INBOARD SIDE OF STRINGER 27R BS 560 TO BS 567. CUT OUT DAMAGED SECTION OF STRINGER APPROXIMATE DIMENSION 18" LONG IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED REPAIR STRINGER. FABRICATED REPAIR SPLICES IAW B-727 SRM 51-10-3 FIGURE 1 AND SRM
- [SDR DHL2007785045](https://openairdocs.org/sdr/DHL2007785045.md): Angle · corroded · Oct 31, 2007 · N785AT · Boeing 727214 · Fuselage Miscellaneous Structure
  > LEFT WHEEL WELL APU SCREEN FORWARD VERTICAL ANGLE HAS CORROSION BS 910. REMOVED NUT PLATES TO GAIN ACCESS IAW B-727 SRM 51-30-2, REMOVED CORROSION IAW B-727 SRM 51-10-6. FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED ANGLE (BEAM) AND ATTACHED A
- [SDR DHL2007785039](https://openairdocs.org/sdr/DHL2007785039.md): Stringer Splice · corroded · Oct 31, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > SURFACE CORROSION AT STRINGER 28R CHANNEL, FORWARD AND AFT SPLICES BETWEEN BS 1000 TO BS 1015. REMOVED STRINGER SPLICE IAW B-727 SRM 51-30-2, FABRICATED NEW STRINGER SPLICE IAW B-727 SRM 53-10-2 FIGURE 9, 51-30-5 AND 51-20-1. TREATED AND PRIMED NEW SPLICE IA
- [SDR DHL2007785040](https://openairdocs.org/sdr/DHL2007785040.md): Beam · corroded · Oct 30, 2007 · N785AT · Boeing 727214 · Fuselage Main, Structure
  > SURFACE CORROSION AT BS 1183 LOWER HORIZONTAL "I" BEAM INBOARD SIDE JUST AFT OF OUT FLOW VALVE, STRINGER 26R. REMOVED CORROSION IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1, REMOVED BEAM IAW B-727 SRM 51-30-2, FABRICATED
- [SDR DHL2007785027](https://openairdocs.org/sdr/DHL2007785027.md): Rib · cracked · Oct 29, 2007 · N785AT · Boeing 727214 · Leading Edge Devices
  > CRACK INDICATION ON RIGHT WING NR 5 SLAT OUTBOARD AND INBOARD ACTUATOR ROD END MOUNT BRACKET, PREVIOUSLY REPAIRED. REMOVED SLAT ACCESS PANELS TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CRACKED RIBS IAW B-727 SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW
- [SDR DHL2007785022](https://openairdocs.org/sdr/DHL2007785022.md): Shear Tie · corroded · Oct 29, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION AT BS 1130 LEFT OF STRINGER 29L. REMOVED FASTENERS FOR CORROSION REMOVAL AT BS 1130 BETWEEN STRINGER 29L AND 28L AT SHEAR TIE AREA IAW B-727 SRM 51-30-2. REMOVED CORROSION AT FRAME, WITHIN LIMIT IAW B-727 SRM 53-10-1 FIGURE 1, 53-10-2, AND
- [SDR DHL2007785043](https://openairdocs.org/sdr/DHL2007785043.md): Shear Tie · corroded · Oct 27, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION AT RIGHT STRINGER 27L BS 1166 SHEAR TIE AFT SIDE. REMOVED CORROSION AT BS 1166 STRINGER 27L IAW B-727 SRM 51-10-6 FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED PREVIOUS SHEAR TIE IAW B-727 SRM 51-30-2. FABRICATED NE
- [SDR DHL2007785015](https://openairdocs.org/sdr/DHL2007785015.md): Stringer · corroded · Oct 27, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53-10-3 FIGURE 1. FABR
- [SDR DHL200785015](https://openairdocs.org/sdr/DHL200785015.md): Stringer · corroded · Oct 27, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53-10-3 FIGURE 1, FABRIC
- [SDR 2007785015](https://openairdocs.org/sdr/2007785015.md): Stringer · corroded · Oct 27, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FORWARD PIT BS 720F TO BS 740 STRINGER 27R SHOWS CORROSION. REMOVED CORROSION AT BS 720F TO BS 740 STRINGER 27R IAW B-727 SRM 51-10-6, CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. CUT OUT DAMAGED STRINGER IAW B-727 SRM 53-10-3 FIGURE 1. FABR
- [SDR DHL2007785026](https://openairdocs.org/sdr/DHL2007785026.md): Skin · punctured · Oct 26, 2007 · N785AT · Boeing 727214 · Elevator, Plate/Skin
  > RIGHT ELEVATOR LOWER SKIN PUNCTURED AT ELEVATOR STATION 35.55. REMOVED FASTENERS AT RIGHT ELEVATOR LOWER SKIN STATION 35.55 IAW B-727 SRM 51-30-2, CUT OUT SKIN DAMAGED IAW B-727 SRM 55-20-3 FIG 4. FABRICATED REPAIR DOUBLER IAW B-727 SRM 55-20-3 FIGURE 4. IN
- [SDR DHL2007785035](https://openairdocs.org/sdr/DHL2007785035.md): Stringer · cracked · Oct 24, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FOUND CRACK IN TWO PLACES AT STRINGER 28R BETWEEN BS 480 TO BS 520. CUT OUT STRINGER 28R SECTION AND FABRICATED NEW STRINGER SECTION AND REPAIR SPLICE IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2
- [SDR DHL2007785037](https://openairdocs.org/sdr/DHL2007785037.md): Trunnion · corroded · Oct 23, 2007 · N785AT · Boeing 727214 · Fuselage, Landing Gear Attach Fittings
  > LT NLG TRUNNION AND LOWER CAP BORE HAS PITTING CORROSION. CLEANED LT NLG TRUNNION AS REQUIRED IAW B-727 MM 12-40-0. CORROSION FOUND, REQUIRES REPAIR IAW B-727 SRM 53-40-1 FIGURE 2. REAMED LT NLG TRUNNION IAW B-727 SRM 53-40-1 FIGURE 2, TRUNNION REWORKED WI
- [SDR DHL2007785036](https://openairdocs.org/sdr/DHL2007785036.md): Trunnion · corroded · Oct 23, 2007 · N785AT · Boeing 727214 · Fuselage, Landing Gear Attach Fittings
  > RT NLG TRUNNION AND LOWER CAP BORE HAS PITTING CORROSION. CLEANED RT NLG TRUNNION IAW BSOPM 20-30-05 AFTER FURTHER EVALUATION FOUND CORROSION ON SUPPORT LOWER CAP IAW B-727 SRM 51-10-6 PARA 3A. REWORKED RT TRUNNION IAW B-727 SRM 53-40-1 FIGURE 2. TRUNNION R
- [SDR DHL2007785013](https://openairdocs.org/sdr/DHL2007785013.md): Shear Tie · cracked · Oct 23, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > FORWARD PIT RIGHT BS 720 BETWEEN STRINGER 27R AND 28R FRAME CRACKED AT BOTTOM FLANGE. FABRICATED FRAME SHEAR TIE REPAIR FROM 7075-T6.063" PO NR 9005685 APPROXIMATE DIMENSION 4.375" BY 5.875" IAW B-727 SRM 53-10-4 FIGURE 12 AND SRM 53-10-2 FIGURE 3. CUT OUT
- [SDR DHL2007785012](https://openairdocs.org/sdr/DHL2007785012.md): Stringer · damaged · Oct 23, 2007 · N785AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > MISDRILLED HOLE IN STRINGER 28R BS 695. REMOVED FASTENERS AT BS 695 STRINGER 28R, CUT OUT DAMAGED AREA IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED FILLER. FABRICATED SPLICES 2 EACH IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED NEW
- [SDR DHL2007785028](https://openairdocs.org/sdr/DHL2007785028.md): Structure · cracked · Oct 19, 2007 · N785AT · Boeing 727214 · Leading Edge Devices
  > NR 4 KRUEGER FLAP LOWER INBOARD END CRACKED WING STATION 131. CUT OUT CRACKED AREA, FABRICATED REPAIR PLATE, REPAIR FILLER AND REPAIR ANGLE IAW B-727 SRM 57-50-3 FIGURE 3. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT NR 4 KRU
- [SDR DHL2007785047](https://openairdocs.org/sdr/DHL2007785047.md): Angle · corroded · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Miscellaneous Structure
  > FOUND SURFACE CORROSION ON FORWARD PIT FUSELAGE SKIN AT BASE OF INTERCOSTAL BS 480-500 STRINGER 28R. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. REMOVED INTERCOSTAL ANGLE IAW B-727 SRM 51-30-2. FABRICATED NEW
- [SDR DHL2007785038](https://openairdocs.org/sdr/DHL2007785038.md): Shear Tie · corroded · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > CORROSION WITH SOME EXFOLIATION ON SHEAR TIE BS 500 BETWEEN STRINGER 28R AND STRINGER 28L. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-40-1 FIGURE 1 AND 53-10-2 FIGURE 3. CUT OUT SHEAR TIE IAW B-727 SRM 51-10-1. FABRICATED
- [SDR DHL2007785008](https://openairdocs.org/sdr/DHL2007785008.md): Shear Tie · corroded · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCESS IAW B-727 SRM 51-30-2, REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIE
- [SDR DHL2007785007](https://openairdocs.org/sdr/DHL2007785007.md): Shear Tie · corroded · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIE
- [SDR DHL2007785011](https://openairdocs.org/sdr/DHL2007785011.md): Frame · gouged · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Main, Frame
  > C-1 DOOR CUT OUT AFT FRAME BS 620, WEB HAS DEEP GOUGE ON THE FORWARD SURFACE BETWEEN STRINGER 26R AND 27R. BLEND OUT AREA IAW B-727 SRM 51-10-1. OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 3. REMOVED FASTENERS FROM AREA IAW B-727 SRM 51-
- [SDR DHL2007785009](https://openairdocs.org/sdr/DHL2007785009.md): Shear Tie · corroded · Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting Structure
  > SURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIE
- [SDR DHL2007785049](https://openairdocs.org/sdr/DHL2007785049.md): Seat Track · corroded · Oct 16, 2007 · N785AT · Boeing 727214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACKS LBL 45 BS 480-BS 690 HAVE LIGHT CORROSION. REMOVED CABIN FLOOR PANELS BETWEEN BS 480 AND 700 LBL 22 LBL65-LBL22 FOR ACCESS IAW B-727 MM 53-30-11. REMOVED SEAT TRACK OUT OF LIMITS FROM BS 480 TO 700 LBL45 IAW B-727 SRM 51-30-2. FABRICA
- [SDR DHL2007785024](https://openairdocs.org/sdr/DHL2007785024.md): Skin · damaged · Oct 15, 2007 · N785AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE UPPER SKIN HAS LIGHTNING STRIKE AT BS 700 + 8" STRINGER 9R. BLEND OUT DAMAGE IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-1 FIGURE 1 AND 2. CUT OUT DAMAGED AREA (DIMENSION.875" DIAMETER) AND FABRICATED REPAIR DOUBLER FROM 2024-T3 0.063" PO NR 900
- [SDR DHL2007785030](https://openairdocs.org/sdr/DHL2007785030.md): Skin · bulged · Oct 12, 2007 · N785AT · Boeing 727214 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER RIGHT SIDE ABOVE UPPER RUDDER HAS BULGING SKIN (FIN WL 168 AT FIN STA 305). CUT OUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 55-30-3 FIGURE 6 AND 55-30-2 FIGURE 1. TREATED AND PRIMED PARTS IAW B-727 SRM 51
- [SDR DHL2007785023](https://openairdocs.org/sdr/DHL2007785023.md): Skin · damaged · Oct 11, 2007 · N785AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > SCRATCH ON UPPER FUSELAGE SKIN BS 1090 STRINGER 4R TO STRINGER 5R. BLENDED OUT DAMAGE AREA IAW B-727 SRM 51-10-4. FOUND OUT OF LIMITS IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-1 FIGURE 1 AND 2. DISPLACED GILLINER CABIN LINER FOR ACCESS BETWEEN BS 1030 AND BS
- [SDR DHL2007785006](https://openairdocs.org/sdr/DHL2007785006.md): Radome · cracked · Aug 25, 2007 · N785AT · Boeing 727214 · Aerodynamic Fairings
  > AT COMPLETION OF PUSH BACK, GROUND CREW UNABLE TO REMOVE TOW BAR. WHEN TOW BAR RELEASED, WITH PARKING BRAKE SET, ACFT MOVED FORWARD. VISIBLE DAMAGE NOTED TO RADOME ASSY.
- [SDR DHL2007785005](https://openairdocs.org/sdr/DHL2007785005.md): Support Fitting · cracked · Jun 27, 2007 · N785AT · Boeing 727214 · Wing, Attach Fittings
  > NR 8 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED. REMOVED FITTING AND REPLACED WITH NEW FITTING PER B727 SRM 51-30-2 FIG 1, FIG 15, AND B727 MM 27-61-91.

Next page: https://openairdocs.org/deregistered/N785AT-2011-01-27/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 = 'N785AT' AND deregistration_id = 'N785AT-2011-01-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N785AT-2011-01-27/reports

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