# Service difficulty reports: Boeing 727-214

A list on [Boeing 727-214](https://openairdocs.org/model/boeing-727-214.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 296 reports

- [SDR DHLA200800133](https://openairdocs.org/sdr/DHLA200800133.md): Skin · damaged · Dec 4, 2008 · N786AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > ACFT SKIN DAMAGE 2 IN HOLE LOWER RT SIDE BELOW PITOT TUBE. ACFT DAMAGED BY CARGO CONTAINER. INSTALLED REPAIR IAW SRM 53-30-3 AT STA 212 RT STR 25R.
- [SDR DHL2008F00002](https://openairdocs.org/sdr/DHL2008F00002.md): Structure · cracked · Jul 9, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > L/E SLAT HAS 2 SMALL CRACKS AT IB SLAT TRACK ATTACH POINT. CRACKS WERE BURNISHED OUT WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01. (K)
- [SDR DHLA200800048](https://openairdocs.org/sdr/DHLA200800048.md): Light · inoperative · May 13, 2008 · N788AT · Boeing 727214 · Emergency Lighting
  > FLT NR 177, FORWARD ENTRY DOOR EMERGENCY LIGHT INOP DURING STBY PWR CHECK. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-50-01. OPS CHECK NORMAL. AIRCRAFT WAS GROUNDED.
- [SDR DHL2008788003](https://openairdocs.org/sdr/DHL2008788003.md): Structure · cracked · May 2, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > NR 3 L/E K-FLAP HAS SMALL CRACK ON THE BOTTOM I/B CORNER. REPAIRED SMALL CRACK PER SRM 51-40-0.
- [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 DHL2008788001](https://openairdocs.org/sdr/DHL2008788001.md): Skin · gouged · Mar 25, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > NR 3 K-FLAP HAS SMALL GOUGE ON LOWER I/B EDGE. DEFECT WAS BLENDED IAW B727SRM 57-50-1 DETAIL 4 GOUGE REMOVED, MINIMAL MATERIAL LOSS.
- [SDR DHLA200800029](https://openairdocs.org/sdr/DHLA200800029.md): Light · defective · Mar 11, 2008 · N786AT · Boeing 727214 · Emergency Lighting
  > FWD ENTRY L1 DOOR EMERGENCY LIGHT ASSY "ON" IN ARM POSITION, WOULD NOT TURN OFF. REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHT ASSY IAW MM 33-50-101. OPS CKS NORMAL PER MM 33-50-01. AIRCRAFT WAS GROUNDED.
- [SDR DHLA200800020](https://openairdocs.org/sdr/DHLA200800020.md): Light · inoperative · Mar 3, 2008 · N786AT · Boeing 727214 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT ASSY INOP, BATTERIES OK. REMOVED AND REPLACED PER B727 MM 33-50-101 AND OPS CKS GOOD. AIRCRAFT WAS GROUNDED.
- [SDR DHLA200800011](https://openairdocs.org/sdr/DHLA200800011.md): Switch · lack of lube · Jan 30, 2008 · N788AT · Boeing 727214 · Door Warning System
  > FLT 194, FWD ENTRY DOOR LIGHT DOES NOT ILLUMINATE WITH DOOR OPEN TEST. TRANSFERED TO DMI 31565 IAW MEL 52-4 CAT C PLACARD INSTALLED. CLEANED AND LUBED L1 DOOR WARNING SWITCH, OPS CHK GOOD IAW MM 52-11-01. DMI 31565 CLEARED PLACARDS REMOVED. ACFT GROUNDED.
- [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 DHLA200700055](https://openairdocs.org/sdr/DHLA200700055.md): Torque Box · cracked · Nov 6, 2007 · N788AT · Boeing 727214 · Fuselage Main, Structure
  > DURING AN"A" CHECK, TORQUE BOX AREA, LIGHTING HOLES AT STA 1223 LT AND RT HAVE SMALL CRACKS 2 AFT AIR STAIR AREA (PREVIOUSLY REJECTED ON NR 138359). CUT OUT DAMAGED AREA AT TORQUE BOX AREA LIGHTING HOLES/H DIMENSION CUTOUT 3/4" BY 1/4" IAW B727 SRM 53-10-1 FI
- [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

Next page: https://openairdocs.org/model/boeing-727-214/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 aircraft_model_key = '727214'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-214/reports

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