# Service difficulty reports: Boeing 727-212

A list on [Boeing 727-212](https://openairdocs.org/model/boeing-727-212.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 405 reports

- [SDR I5PA2016022642502](https://openairdocs.org/sdr/I5PA2016022642502.md): Drag Brace · cracked · Feb 26, 2016 · N86425 · Boeing 727212 · Landing Gear Retraction/Extension System
  > AFTER FURTHER ASSESSMENT, WE IDENTIFIED THE PROBLEM THAT CAUSED THE AIRCRAFT'S NLG ASSEMBLY NOT TO EXTEND. WE FOUND THAT THE NOSE GEAR DRAG BRACE CTR LOCK ARM SPLINE HAD CRACKED, WHICH DID NOT ALLOW THE SYS TO UNLOCK NORMALLY OR MANUALLY FOR THE NOSE GEAR TO
- [SDR I5PA2015102631902](https://openairdocs.org/sdr/I5PA2015102631902.md): Line · unknown · Oct 25, 2015 · N319NE · Boeing 727212 · Turbine Engine Oil System
  > NUMBER 3 ENG EXPERIENCED OIL LOSS. OIL PRESS AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOOTING IN PROGRESS. ENG HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL. FOUND OIL SUP
- [SDR I5PA2015102631901](https://openairdocs.org/sdr/I5PA2015102631901.md): Engine · leaking · Oct 25, 2015 · N319NE · Boeing 727212 · Turbine Engine Oil System
  > NR 3 ENG EXPERIENCED OIL LOSS. OIL PRESSURE AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOT NR ENG OIL LOSS, ENG INITIALLY HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL FOR TR
- [SDR PCSA2014122201](https://openairdocs.org/sdr/PCSA2014122201.md): Engine · making metal · Dec 20, 2014 · N598AJ · Boeing 727212 · Engine (Turbine/Turboprop)
  > ENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.
- [SDR 3FMR20140903001](https://openairdocs.org/sdr/3FMR20140903001.md): Skin · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF AD 85-24-02, CORROSION WAS FOUND IN LOWER SKIN BS 870, RBL 3 - 8, WATERLINE 160.8.
- [SDR 3FMR20140903006](https://openairdocs.org/sdr/3FMR20140903006.md): Skin · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF AD 82-24-02, CORROSION WAS FOUND IN THE LT AIR CONDITIONING PLENUM AREA ON THE LOWER SURFACE SKIN AT BS 826 - 848 AT LBL 32, W/L 160.8. FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJ-N598AJ - 04/ 14.
- [SDR 3FMR20140903004](https://openairdocs.org/sdr/3FMR20140903004.md): Structure · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Wing Main, Frame Structure
  > DURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE LT FRONT SPAR LOWER ANGLE AT WS 383 - 465. FOUND TO BE OUT OF SRM LIMITS. REPAIRED.
- [SDR 3FMR20140903005](https://openairdocs.org/sdr/3FMR20140903005.md): Spar Cap · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Horizontal Stabilizer, Spar/Rib
  > CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER. CORROSION IS LOCATED AT HORIZONTAL STAB STATION 78.13. FOUND TO BE OUT OF MFG SRM LIMITS. REPAIRED IAW DWG 55-14215-1A.
- [SDR 3FMR20140903003](https://openairdocs.org/sdr/3FMR20140903003.md): Skin · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Wing Structure
  > RIGHT WING LOWER SKIN WAS FOUND CORRODED AROUND FRONT SPAR ATTACH FASTENERS LOCATED AT WING STA 509 - 519. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJN598AJ 3/14.
- [SDR 3FMR20140903002](https://openairdocs.org/sdr/3FMR20140903002.md): Spar · corroded · Sep 3, 2014 · N598AJ · Boeing 727212 · Wing Spar
  > DURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE RIGHT HAND WING, FRONT SPAR, LOWER CHORD AT WING STATION 509 TO 519. CORROSION WAS FOUND OUTSIDE OF MANUFACTURER SRM LIMITATIONS. A DESIGNATED ENGINEERING REPRESENTATIVE REPAIR HAS BEEN SOUGHT.
- [SDR I5PA201405010002](https://openairdocs.org/sdr/I5PA201405010002.md): Gearbox · leaking · Apr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory Drive
  > AT APPROX 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY, FOLLOWED BY LOW OIL PRESS, HIGH ENG EMP AT FL 330. DECLARED AN EMER AT 0738Z & AIR RETURNED BACK SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEARBOX IAW AMM 72-63-00. INSPECTE
- [SDR I5PA201405010001](https://openairdocs.org/sdr/I5PA201405010001.md): Gearbox · unknown · Apr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory Drive
  > AT APPROXIMATELY 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY FOLLOWED BY LOW OIL PRESS, HIGH ENG TEMP AT FL 330. THEY DECLARED AN EMERGENCY AT 0738Z & AIR RETURNED BACK TO HNL STATION SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEA
- [SDR I5PA2013101600053](https://openairdocs.org/sdr/I5PA2013101600053.md): Frame · corroded · Oct 16, 2013 · N86425 · Boeing 727212 · Fuselage Main, Frame
  > CORROSION WAS FOUND AT BS 720D FRAME BETWEEN S25-26R. CORROSION REMOVED IAW SRM 53-10-1, FIG 1.
- [SDR FY4Y2013101600005](https://openairdocs.org/sdr/FY4Y2013101600005.md): Skin · corroded · Oct 14, 2013 · N86425 · Boeing 727212 · Fuselage Main, Plate/Skin
  > DURING 7C CHECK & CPCP INSPECTION, INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON CENTER WING LOWER SURFACE BETWEEN STRINGER 4C & 5C, WING LBL 24 TO LBL 28, AFTER BLEND OUT OF CORROSION, FOUND OUT OF LIMITS IAW SRM 57-30-1, TABLE 1.
- [SDR FY4Y201310160001](https://openairdocs.org/sdr/FY4Y201310160001.md): Skin · corroded · Oct 14, 2013 · N86425 · Boeing 727212 · Fuselage Main, Plate/Skin
  > DURING CPCP INSPECTION, INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON FUSELAGE EXTERNAL SURFACE OF BS 640 TO 660, FOUND OUT OF LIMITS IAW SRM 53-30-1, FIG 2.
- [SDR PCSA2013092501](https://openairdocs.org/sdr/PCSA2013092501.md): Duct · ruptured · Sep 23, 2013 · N598AJ · Boeing 727212 · Pneumatic Distribution System
  > LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND DUCT RUPTURED
- [SDR FY4Y201307180003](https://openairdocs.org/sdr/FY4Y201307180003.md): Bulkhead · corroded · Jul 17, 2013 · N319NE · Boeing 727212 · Fuselage Main, Bulkhead
  > 8C CHECK. DURING CPCP INSPECTION, CORROSION WAS FOUND. THE CORROSION DAMAGE THROUGH THE PART ON THE NOSE WHEEL WELL BS 294.5 BULKHEAD WEB.
- [SDR FY4Y20130718197](https://openairdocs.org/sdr/FY4Y20130718197.md): Frame · corroded · Jul 17, 2013 · N319NE · Boeing 727212 · Fuselage Main, Frame
  > 8C CHECK. DURING CPCP INSPECTION, PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON LOWER ANGLE OF BS 950 CANTED BULKHEAD BETWEEN S22-23L. BLENDED OUT CORROSION, PENETRATION DEPTH WAS OVER LIMITS IAW SRM 53-10-1, FIG 1.
- [SDR FY4Y20130718002](https://openairdocs.org/sdr/FY4Y20130718002.md): Skin · corroded · Jul 16, 2013 · N319NE · Boeing 727212 · Fuselage Main, Plate/Skin
  > 8C CHECKK. DURING PERFORMED CPCP INSPECTION, CORROSION WAS FOUND ON THE UPPER SKIN UPPER SURFACE OF THE WING CENTER SECTION, AT BS 783.95, BETWEEN RBL 63.0 AND RBL 65.5. CORROSION BLENDED OUT. THE DAMAGE CONDITION HAD EXCEEDED THE ALLOWABLE LIMITATION IAW
- [SDR PCSA2013051001](https://openairdocs.org/sdr/PCSA2013051001.md): Fuel Control · faulty · May 6, 2013 · N598AJ · Boeing 727212 · Fuel Control/Turbine Engines
  > ENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE NR 2 FUEL PUMP AND FUEL CONTROL UNIT REPLACED AND TESTED PER THE B727 AMM AND THE AIRCRAFT RETURN
- [SDR R5KB2013013150501](https://openairdocs.org/sdr/R5KB2013013150501.md): Mount · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Engine Mount Section
  > NR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.
- [SDR R5KB46252](https://openairdocs.org/sdr/R5KB46252.md): Pin · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Wing, Attach Fittings
  > RIGHT WING AFT BOTTLE PIN CUP HAS EVIDENCE OF CORROSION UNDER PIN CUP.
- [SDR R5KB2013013150398](https://openairdocs.org/sdr/R5KB2013013150398.md): Seat Track · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT BUTTLINE 55 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN STA 991 TO 1030.
- [SDR R5KB2013013150353](https://openairdocs.org/sdr/R5KB2013013150353.md): Seat Track · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT BUTTLINE 56, STA 344 SEAT TRACK CORRODED.
- [SDR R5KB2013013150349](https://openairdocs.org/sdr/R5KB2013013150349.md): Seat Track · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BETWEEN STA 800 TO 815, LEFT BUTTLINE 25.
- [SDR R5KB2013013150258](https://openairdocs.org/sdr/R5KB2013013150258.md): Stringer · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Main, Longeron/Stringer
  > EVIDENCE OF CORROSION BETWEEN STA 950E AND 950E, STRINGER 15L.
- [SDR R5KB2013013146411](https://openairdocs.org/sdr/R5KB2013013146411.md): Intercostal · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED AT STA 1060 STRINGER 20 LEFT.
- [SDR R5KB2013013150363](https://openairdocs.org/sdr/R5KB2013013150363.md): Floorbeam · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Main, Floor Beam
  > TOP CORD OF FLOORBEAM CORRODED ON FLOORBEAM AT STA 1110, LEFT BUTTLINE 24 TO 52.
- [SDR R5KB2013013150432](https://openairdocs.org/sdr/R5KB2013013150432.md): Support · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SUPPORT CORRODED AT LEFT BUTTLINE 45.5, STA 1090 TO 1110.
- [SDR R5KB2013013150369](https://openairdocs.org/sdr/R5KB2013013150369.md): Web · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > CORROSION AROUND PINS IN FLOOR WEB AT STA 1146 BETWEEN RIGHT BUTTLINE 54 AND 58.
- [SDR R5KB2013013150368](https://openairdocs.org/sdr/R5KB2013013150368.md): Web · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > CORROSION AROUND EDGE OF WALL AND FLOOR WEB AT STA 1148, RIGHT BUTTLINE 63.
- [SDR R5KB46410](https://openairdocs.org/sdr/R5KB46410.md): Intercostal · corroded · Jan 31, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STA 1060, LEFT BUTTLINE 26 AREA OF CORROSION.
- [SDR R5KB2013012850324](https://openairdocs.org/sdr/R5KB2013012850324.md): Web · cracked · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > FLOOR TO SKIN WEB CRACKED,.25' AT EDGE OF LIGHTENING HOLE AT STA 490, RIGHT BUTTLINE 72.
- [SDR R5KB2013012850439](https://openairdocs.org/sdr/R5KB2013012850439.md): Floorbeam · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 1110 LEFT BUTTLINE 1 TO RIGHT BUTTLINE 12.
- [SDR R5KB2013012846287](https://openairdocs.org/sdr/R5KB2013012846287.md): Skin · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder, Plate/Skin
  > CORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.
- [SDR R5KB2012012846190](https://openairdocs.org/sdr/R5KB2012012846190.md): Skin · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder, Plate/Skin
  > CORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.
- [SDR R5KB2013012846405](https://openairdocs.org/sdr/R5KB2013012846405.md): Shear Tie · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 29 AND 30 LEFT.
- [SDR R5KB2013012846406](https://openairdocs.org/sdr/R5KB2013012846406.md): Shear Tie · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT STA 1110, BETWEEN STR 28 AND 29 LEFT.
- [SDR R5KB2013012850560](https://openairdocs.org/sdr/R5KB2013012850560.md): Panel · delaminated · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder, Plate/Skin
  > LEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.
- [SDR R5KB2013012850553](https://openairdocs.org/sdr/R5KB2013012850553.md): Web · cracked · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Miscellaneous Structure
  > SUPPORT WEB CRACKED LEFT BUTTLINE 25 FROM STA 1130 TO 1110.
- [SDR R5KB2013012846189](https://openairdocs.org/sdr/R5KB2013012846189.md): Structure · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder Miscellaneous Structure
  > CORROSION ON LEFT SIDE OF UPPER RUDDER BETWEEN STA 212 AND 220.
- [SDR R5KB2013012850361](https://openairdocs.org/sdr/R5KB2013012850361.md): Floorbeam · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 1110 LEFT BUTTLINE 12 TO LEFT BUTTLINE 24 TOP AND BOTTTOM.
- [SDR R5KB2013012846194](https://openairdocs.org/sdr/R5KB2013012846194.md): Skin · damaged · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder, Plate/Skin
  > UPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.
- [SDR R5KB2013012846281](https://openairdocs.org/sdr/R5KB2013012846281.md): Skin · damaged · Jan 28, 2013 · N727NK · Boeing 727212 · Rudder, Plate/Skin
  > SKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.
- [SDR R5KB2013012846403](https://openairdocs.org/sdr/R5KB2013012846403.md): Shear Tie · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.
- [SDR R5KB2013012850568](https://openairdocs.org/sdr/R5KB2013012850568.md): Frame · damaged · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Main, Frame
  > FRAME DAMAGED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.
- [SDR R5KB2013012846170](https://openairdocs.org/sdr/R5KB2013012846170.md): Structure · cracked · Jan 28, 2013 · N727NK · Boeing 727212 · Nacelle/Pylon Miscellaneous Structure
  > CRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.
- [SDR R5KB2013012846396](https://openairdocs.org/sdr/R5KB2013012846396.md): Frame · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Main, Frame
  > FRAME AT STA 1148 CORRODED AT STR 26R.
- [SDR R5KB2013012846404](https://openairdocs.org/sdr/R5KB2013012846404.md): Shear Tie · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT STATION 1130 BETWEEN STR 27 AND 28 LEFT.
- [SDR R5KB2013012846435](https://openairdocs.org/sdr/R5KB2013012846435.md): Shear Tie · corroded · Jan 28, 2013 · N727NK · Boeing 727212 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED STA 1166 BETWEEN STR 29 AND 30 LEFT.

Next page: https://openairdocs.org/model/boeing-727-212/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 = '727212'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-212/reports

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