# Service difficulty reports: N805EA, cancelled Nov 8, 2006

A list on [N805EA, cancelled Nov 8, 2006](https://openairdocs.org/deregistered/N805EA-2006-11-08.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DL72S030340](https://openairdocs.org/sdr/DL72S030340.md): Spar · cracked · Apr 4, 2003 · N805EA · Boeing 727225A · Wing Spar
  > THE LOWER STRUCTURE AND WEB OF THE LT WING AUX SPAR BEAM WERE FOUND CRACKED NEAR THE NR 7 INBD SPOILER ACTUATOR SUPPORT FITTING. THE LOWER STRUCTURE WAS CUT AND THE CRACKED SECTION REMOVED. A NEW SECTION WAS SPLICED IN WITH STEEL REPAIR ANGLES. THE WEB WA
- [SDR DL72S030208](https://openairdocs.org/sdr/DL72S030208.md): Indicator · malfunctioned · Mar 3, 2003 · N805EA · Boeing 727225A · Attitude Gyro and Indicating System
  > CAPTS ATTITUDE INDICATOR INTERMITTENT. ROLLS TO 45/90 DEGS WITH AFF FAIL FLAG AND A COMPARITOR ROLL LIGHT. REPLACED CAPTS ADI AND VG PER M/M. SYS CHECKS NORMAL.
- [SDR DL72S021413](https://openairdocs.org/sdr/DL72S021413.md): Angle · cracked · Dec 5, 2002 · N805EA · Boeing 727225A · Wing Structure
  > NO. 12 SPOILER ACTUATOR ATTACH BRACKET CRACKED OUT BOARD ENDREPLACED ATTACH ANGLE
- [SDR DL72S021136](https://openairdocs.org/sdr/DL72S021136.md): Battery · discharged · Sep 25, 2002 · N805EA · Boeing 727225A · Emergency Lighting
  > FWD GALLEY DOOR EMERGENCY EXIT LIGHT INOP. WILL NOT TEST, REPLACED BATTERIES AND BULBS OPERATIONAL CHECKS NORMAL.
- [SDR DL72S020920](https://openairdocs.org/sdr/DL72S020920.md): Fuel Control · malfunctioned · Aug 7, 2002 · N805EA · Boeing 727225A · Fuel Control/Turbine Engines
  > ON CLIMBOUT AUS NUMBER 3 ENGINE SLOWLY ROLLED BACK TO IDLE. ENGINE SHUTDOWN ON FINAL DFW. REPLACED FUEL PUMP AND FUEL CONTROL RIGGED AND TRIMMED ENGINE, ALL OPS CHECK NORMAL.
- [SDR DL72S020459](https://openairdocs.org/sdr/DL72S020459.md): Rib · cracked · Apr 19, 2002 · N805EA · Boeing 727225A · Leading Edge Devices
  > L/E NOSE RIB ON NR 5 SLAT I/B SIDE OF ACTUATOR ROD END IS CRACKED. REPAIRED PER M/M 57-54-000-8 AND ERA 382989-14.
- [SDR DL72S011506](https://openairdocs.org/sdr/DL72S011506.md): Switch · contaminated · Sep 8, 2001 · N805EA · Boeing 727225A · Landing Gear Position and Warning
  > NOSE GEAR RED UNSAFE LIGHT ILLUM IN FLT ON GEAR EXTENSION RED AND GREEN NOSE GEAR IND LIGHT ILLUM. MTC FOUND THE NOSE GEAR RED LIGHT ILLUM AT THE GATE CLEANED THE CANNON PLUG FOR THE NOSE GEAR LOCK SWITCH AND OPS CHECK NORMAL PER THE MTC M
- [SDR DL72S011500](https://openairdocs.org/sdr/DL72S011500.md): Stringer · cracked · Sep 6, 2001 · N805EA · Boeing 727225A · Empennage Structure
  > VERT STAB STRINGER 6R CRACKED AT STA 6.372 REPAIRED PER MM 55-30-000-8 FIG 803
- [SDR DL72S011499](https://openairdocs.org/sdr/DL72S011499.md): Stringer · cracked · Sep 6, 2001 · N805EA · Boeing 727225A · Empennage Structure
  > VERT STAB STR 6R CRACKED @ STA 6.372 REPAIRED PER M/M 55-30-000-8 FIG 803
- [SDR DL72S011419](https://openairdocs.org/sdr/DL72S011419.md): Light · inoperative · Aug 27, 2001 · N805EA · Boeing 727225A · Emergency Lighting
  > PAX SEAT 15 & 29 EMERGENCY LIGHTS INOP. RE-ATTACHED CONNECTOR AT SEAT ROW 15 AND RELAMPED SEAT ROW 29.
- [SDR DL72S011022](https://openairdocs.org/sdr/DL72S011022.md): Actuator · bypassing · Jun 20, 2001 · N805EA · Boeing 727225A · Landing Gear Retraction/Extension System
  > ON GEAR EXTENSION MAIN GEAR EXTENDED NORMALLY NOSE GEAR DID NOT. FOUND LOCK ACTUATOR BYPASSING INTERNALLY. REPLACED SAME.
- [SDR DL72S010915](https://openairdocs.org/sdr/DL72S010915.md): Actuator · leaking · Jun 5, 2001 · N805EA · Boeing 727225A · Landing Gear Door Actuator
  > COMPLETE LOSS OF A SYSTEM HYD UPON GEAR RETRACTION. FOUND RT GEAR DOOR ACTUATOR LEAKING. REPLACED SAME PER M/M.
- [SDR DL72S010621](https://openairdocs.org/sdr/DL72S010621.md): Connector · inoperative · Apr 15, 2001 · N805EA · Boeing 727225A · Emergency Lighting
  > RED EMERGENCY LIGHT INOPERATIVE INBD SIDE OF FWD COAT CLOSET. FOUND WIRE PULLED FRM CONNECTOR. REPAIRED CONNECTOR
- [SDR DL72S010167](https://openairdocs.org/sdr/DL72S010167.md): Angle · cracked · Jan 29, 2001 · N805EA · Boeing 727225A · Leading Edge Devices
  > FOUND ON C1 LETTER CK, TWO.25 INCH CRACKS IN THE NUMBER 6 SLAT LOWER COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-000-8.
- [SDR DL72S001183](https://openairdocs.org/sdr/DL72S001183.md): Fuel Heater · failed · Jun 19, 2000 · N805EA · Boeing 727225A · Fuel Heater
  > NEAR TOP OF CLIMB FL330 NR 1 OIL TEMP WAS 140 DEG CELSIUS. REMAINED IN YELLOW FOR 15 MIN. PERFORMED POM. REPLACED NR 1 FUEL HEAT VALVE, CKS GOOD.
- [SDR DL72S001173](https://openairdocs.org/sdr/DL72S001173.md): Actuator · failed · Jun 16, 2000 · N805EA · Boeing 727225A · Landing Gear Door Actuator
  > THE RIGHT MAIN LANDING GEAR WOULD NOT EXTEND NORMALLY. CHECKLIST PROCEDURES FOLLOWED, GEAR WAS MANUALLY EXTENDED (IE CRANKED DOWN). NORMAL INDICATIONS APPEARED AFTER MANUAL EXTENSION. LANDING UNEVENTFUL. INSTALLED 3000 PSI GAUGE TO UPLINE OF GEAR ACTUATOR
- [SDR DL72S000935](https://openairdocs.org/sdr/DL72S000935.md): Frame · corroded · May 8, 2000 · N805EA · Boeing 727225A · Wing Spar
  > THE VERTICAL LEG OF THE LOWER CHORD OF THE FRONT SPAR ON THE LT WING WAS FOUND CORRODED AT FSS 402. THE CHORD PLATE WAS ALSO FOUND WITH CORROSION DAMAGE ON ITS LOWER SURFACE IN THE SAME AREA. DAMAGE WILL BE REPAIRED BY NESTED ANGLES AND A STRAP. ER/A 3343
- [SDR DL72S000719](https://openairdocs.org/sdr/DL72S000719.md): Sequence Valve · chafed · Apr 15, 2000 · N805EA · Boeing 727225A · Hydraulic System, Main
  > AFTER T/O LOST A SYS HYD FLUID. AIR TURNBACK TO ABQ. FOUND LINE IN RT MAIN GEAR FROM SEQUENCE VALVE CHAFED THROUGH. MTC REPLACING SAME.
- [SDR DL72S992607](https://openairdocs.org/sdr/DL72S992607.md): Seal · leaking · Nov 25, 1999 · N805EA · Boeing 727225 · Passenger/Crew Doors
  > AIRCRAFT WOULD NOT HOLD SCHEDULED CABIN PRESSURE WITH SINGLE PACK OPS AT FL 210. CABIN WAS 8000 FT, CLIMBING 500-700 FEET PER MIN. DESCENDED TO 15,000 TO HOLD LEVEL AT 8000 FEET CABIN PRESSURE. PRESSURIZED ACFT. FOUND AIR LEAKS AT L-1 AND R-1 DOOR SCUFF PL
- [SDR DL72S992582](https://openairdocs.org/sdr/DL72S992582.md): Angle · cracked · Nov 22, 1999 · N805EA · Boeing 727225 · Leading Edge Devices
  > LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14.
- [SDR DL72S992579](https://openairdocs.org/sdr/DL72S992579.md): Angle · cracked · Nov 22, 1999 · N805EA · Boeing 727225 · Leading Edge Devices
  > COVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0.
- [SDR DL72S992578](https://openairdocs.org/sdr/DL72S992578.md): Angle · cracked · Nov 22, 1999 · N805EA · Boeing 727225 · Leading Edge Devices
  > COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.
- [SDR DL72S991772](https://openairdocs.org/sdr/DL72S991772.md): Connector · loose · Aug 9, 1999 · N805EA · Boeing 727225A · Emergency Lighting
  > FIRST CLASS CABIN EMERGENCY LIGHTS WON'T TEST. RESEATED PIN AT QUICK DISCONNECT AT SEAT 4AB. SYSTEM CHECKS NORMAL.
- [SDR DL72S991600](https://openairdocs.org/sdr/DL72S991600.md): Skin · damaged · Jun 24, 1999 · N805EA · Boeing 727225 · Cargo/Baggage Doors
  > ON SHOP VISIT, DAMAGE WAS FOUND TO THE TOP HALF OF THE C1 DOOR, OUTER SKIN. THE SKIN WAS TRIMMED BETWEEN THE NR 3 AND NR 4 STOP BEAMS AND REMOVED TO THE UPPER EDGE. A NEW SECTION WAS FABRICATED AND SPLICE INSTALLED. THE SPLICE CONSISTED OF AN EXTERNAL DOUBL
- [SDR DL72S991335](https://openairdocs.org/sdr/DL72S991335.md): Wire · broken · Jun 13, 1999 · N805EA · Boeing 727225A · Light System Wiring
  > EMERGENCY LIGHT AT SEAT 26D INOP. FOUND BROKEN WIRE AT CONNECTOR. SPLICED WIRE, OPS CHECK GOOD.
- [SDR DL72S991212](https://openairdocs.org/sdr/DL72S991212.md): Valve · inoperative · May 31, 1999 · N805EA · Boeing 727225A · Aircraft Fuel Distribution System
  > WHILE DEPARTING ATL, CENTER FUEL GAUAGE WAS READING 2500 LBS LOWER, WHILE RT WING GAUGE WAS READING HIGHER BY THE SAME. TWO UNITS TRIM REQUIRED FOR LEVEL FLT. AFTER RETURNING TO GATE, FOUND NR 3 TANK VALVE SWITCH IN THEOPEN POSITION DUE TO A BROKEN GUARD COV
- [SDR DL72S991019](https://openairdocs.org/sdr/DL72S991019.md): Ballast · failed · May 9, 1999 · N805EA · Boeing 727225 · Passenger Compartment Lighting
  > AFT CABIN AISLE FLUORESCENT LIGHTING (OVERHEAD) WAS SMOKING AND HAD ELECTRICAL SMELL WITH SPARKING. UPON INSPECTION CEILING RAFTER C/B WAS POPPED. REPLACED LIGHT BALLAST.
- [SDR DL72S991013](https://openairdocs.org/sdr/DL72S991013.md): Battery Pack · discharged · May 8, 1999 · N805EA · Boeing 727225 · Emergency Lighting
  > FWD F/C EMER EXIT LIGHT STROBES INOP DURING TEST. REPLACED BATTERY PACK.
- [SDR DL72S981932](https://openairdocs.org/sdr/DL72S981932.md): Web · cracked · Sep 17, 1998 · N805EA · Boeing 727225 · Fuselage Miscellaneous Structure
  > FOUND ON A1 LETTER CK, RT VERTICAL WEB IN LOWER TORQUE BOX AREA CRACKED STA 1223 AND 1233 AT LIGHTENING HOLES. REPAIRED PER MM 53-11-0.
- [SDR DL72S981931](https://openairdocs.org/sdr/DL72S981931.md): Angle · cracked · Sep 17, 1998 · N805EA · Boeing 727225 · Leading Edge Slat Actuator
  > FOUND ON A1 LETTER CK, NR 3 SLAT I/B ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72S980611](https://openairdocs.org/sdr/DL72S980611.md): Light · inoperative · Mar 19, 1998 · N805EA · Boeing 727225 · Emergency Lighting
  > AFT AIRSTAIR EMERG LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY PACK.
- [SDR DL72S980363](https://openairdocs.org/sdr/DL72S980363.md): Stringer · corroded · Feb 10, 1998 · N805EA · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > FUSELAGE/STRINGER 29R/FS 950D PLUS 10, FS 1007. SPLICE REPAIR A SECTION OF STRINGER 29R NEAR FS 950D PLUS 10 WAS FOUND BADLY CORRODED. THE STRINGER WAS CUT AT STATION 950D PLUS 10 AND THE AFT END REMOVED. A NEW SECTION WAS SPLICED IN PER ER/A 363641-14, REV
- [SDR DL72S980326](https://openairdocs.org/sdr/DL72S980326.md): Skin · torn · Feb 4, 1998 · N805EA · Boeing 727225 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING MODIFICATIONS AROUND THE AFT LAV SERVICE PANEL CUTOUT IN THE SKIN, THE BONDED INTERNAL DOUBLER WAS TORN IN SEVERAL LOCATIONS. THE SKIN AND BONDED DOUBLER WERE CUTOUT AND REMOVED BETWEEN FS 1158 AND 1183 AND BETWEEN STR 20L AND 23L. A NEW
- [SDR DL72S980278](https://openairdocs.org/sdr/DL72S980278.md): Skin · corroded · Feb 2, 1998 · N805EA · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND CORRODED BETWEEN STA 480 AND 500 AND BETWEEN S28L AND BL 0. THE CORROSION WAS TRIMMED AWAY WITH A 9 BY 20 CUTOUT. REPAIRED PER ERA 363693-14.
- [SDR DL72S980203](https://openairdocs.org/sdr/DL72S980203.md): Skin · corroded · Jan 20, 1998 · N805EA · Boeing 727225 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN BETWEEN STA 490 TO 520 WAS FOUND CORRODED AT STRINGER 27R. THE DAMAGED SKIN WAS CUTOUT AND A DOUBLER AND STRUCTURAL FILLER WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 363702-14, REV B.
- [SDR DL72S980205](https://openairdocs.org/sdr/DL72S980205.md): Beam · corroded · Jan 19, 1998 · N805EA · Boeing 727225 · Wing, Landing Gear Attach Fittings
  > TYPICAL CORROSION WAS FOUND IN MANY OF THE HOLE BORES OF THE LT AND RT MAIN LANDING GEAR SUPPORT BEAMS AT THE SKIN PANEL ATTACH LOCATIONS. SURFACE CORROSION WAS ALSO FOUND ON THE BEAMS. THE SURFACE WAS MACHINED TO REMOVE CORROSION AND THE HOLE BORES WERE OV
- [SDR DL72S980144](https://openairdocs.org/sdr/DL72S980144.md): Skin · corroded · Jan 18, 1998 · N805EA · Boeing 727225 · Wing, Plate/Skin
  > CORROSION WAS FOUND DURING 4-37113-3 IN THE CENTER WING LWR SKIN. DAMAGE LOCATED BETWEEN S3C AND S7C FROM RBL 15 TO RBL 32 ON THE LWR SURFACE. REPAIRED PER ERA 331186-14AD.
- [SDR DL72S980106](https://openairdocs.org/sdr/DL72S980106.md): Angle · cracked · Dec 9, 1997 · N805EA · Boeing 727225 · Trailing Edge Flaps
  > NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.
- [SDR DL72S980105](https://openairdocs.org/sdr/DL72S980105.md): Angle · cracked · Dec 9, 1997 · N805EA · Boeing 727225 · Trailing Edge Flaps
  > NR 3 MIDFLAP WAS FOUND WITH A CRACKED LOWER AFT SPAR RAIL. DURING SHOP INSPECTION, THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.
- [SDR DL72S980104](https://openairdocs.org/sdr/DL72S980104.md): Angle · cracked · Dec 9, 1997 · N805EA · Boeing 727225 · Trailing Edge Flaps
  > NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER SPAR ANGLE DURING SHOP INSPECTION. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.
- [SDR DL72S972668](https://openairdocs.org/sdr/DL72S972668.md): Skin · torn · Dec 8, 1997 · N805EA · Boeing 727225 · Trailing Edge Flaps
  > .625 INCH LONG CRACK, CONE SKIN 31 FROM I/B END OF FLAP, ALSO COVE SKIN TORN 32 FROM O/B END OF FLAP. BOTH AREAS REPAIRED PER MM 57-52-FIG 809.
- [SDR 96ZZZM871](https://openairdocs.org/sdr/96ZZZM871.md): Engine · failed · Apr 21, 1996 · N805EA · Boeing 727225 · Engine (Turbine/Turboprop)
  > ON TAKEOFF NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND SHUT ENGINE DOWN FOR PRECAUTION. WHEN AIRCR
- [SDR 96ZZZM1261](https://openairdocs.org/sdr/96ZZZM1261.md): Bearing · failure · Apr 21, 1996 · N805EA · Boeing 727225 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND PILOT MENTIONED HE SHUT ENGINE DOWN FOR PRE
- [SDR 95ZZZM700](https://openairdocs.org/sdr/95ZZZM700.md): Squat Switch · malfunctioned · Nov 2, 1995 · N805EA · Boeing 727225 · Landing Gear Position and Warning
  > FLT KIC019 - AKL-SYD - ON LANDING, BOTH RIGHT MAIN TIRES BLEW CAUSING GEAR DOOR AND FLAP TRACK DAMAGE. FOUND NOSE GEAR SQUAT SWITCH (S480) OUT OF RIG. RIGGED SWITCH PER MM 32. REPLACED NR 4 BRAKE ANTI-SKID VALVE (LOOSE SOLENOID). REPLACED RIGHT BRAKE CONTR

## 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 = 'N805EA' AND deregistration_id = 'N805EA-2006-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N805EA-2006-11-08/reports

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