# Service difficulty reports: N311EA, cancelled Feb 23, 2004

A list on [N311EA, cancelled Feb 23, 2004](https://openairdocs.org/deregistered/N311EA-2004-02-23.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 · 58 reports

- [SDR WRNA200300011](https://openairdocs.org/sdr/WRNA200300011.md): Pressure Switch · leaking · May 21, 2003 · N311EA · Lkheed 10113851 · Turbine Section
  > DURING CLIMB/CRUISE FULL FIRE INDICATION ON ENG NR 3, LOOP A&B ON, FIRE HANDLE ON, FIRE BELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATIONS OFF IMMEDIATELY AFTER ENGINE SHUTDOWN. FIRE BOTTLE NOT FIRED. APPROX 8800 GALS. OF FUEL DUMPED. A/C RETURNED TO FIELD, LANDED
- [SDR WRNA200300010](https://openairdocs.org/sdr/WRNA200300010.md): Fire Loop · false activation · May 21, 2003 · N311EA · Lkheed 10113851 · Fire Detection
  > AFTER TAKE OFF AND DURING CLIMB OUT A FULL FIRE INDICATION ON NR 3 ENGINE. LOOP A & B ON, FIRE HANDLE ON, FIREBELL ON. ENGINE WAS SHUTDOWN, FIRE INDICATION OFF IMMEDIATLY AFTER ENGINE SHUTDOWN. FIRE BOTTLES NOT FIRED. FUEL DUMPED (APPROX. 8800 GALLONS) AIRCRAF
- [SDR WRNA200200007](https://openairdocs.org/sdr/WRNA200200007.md): Fire Loop · shorted · Oct 22, 2002 · N311EA · Lkheed 10113851 · Fire Detection
  > Enroute to BDL @ approx. 270fl, A&B fire loop on #1 engine came on. Engine fire lights came on and fire bell. Bell silenced, #1 engine shutdown per procedures. Alt fire bottle discharged, light remained in handle, Main bottle discharged light remained on. Fuel
- [SDR WRNA200200006](https://openairdocs.org/sdr/WRNA200200006.md): Duct · detached · Oct 18, 2002 · N311EA · Lkheed 10113851 · Cabin Pressure Control System
  > Aircraft at F/L 280 outflow valves full closed cabin climbing at 2,000 ft/min. Manual and stby control no help. Aircraft returned to departing airport. Fuel dumped (42K lbs.) to make max landing wt. Aircraft landed normal.Corrective Action: Mx found duct out o
- [SDR WRNA200200004](https://openairdocs.org/sdr/WRNA200200004.md): Computer · unserviceable · Aug 22, 2002 · N311EA · Lkheed 10113851 · Flight Controller
  > During Climb to cruise altitude Both Mach Feel Fail Lights came on. Fuel dump procedures carried out for Max landing wt (26K lbs dumped). Aircraft landed normal and returned to base.Corrective Action: Removed and replaced Trim Augmentation Computer. Op's check
- [SDR WRNA00023](https://openairdocs.org/sdr/WRNA00023.md): Cover · out of position · Nov 13, 2001 · N311EA · Lkheed 10113851 · Humidity Control System
  > AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED, CLAMP SECURED AND TORQUED IAM MM 21-51-07
- [SDR WRNA200100018](https://openairdocs.org/sdr/WRNA200100018.md): Cover · separated · Nov 13, 2001 · N311EA · Lkheed 10113851 · Humidity Control System
  > AT 27,000 FEET NR 2 PACK WATER SEPARATOR COVER BLEW OFF. CREW UNABLE TO MAINTAIN PRESSURIZATION ON NR 3 PACK ONLY. AIRCRAFT RETURNED TO BQN. FUEL DUMPED. AIRCRAFT LANDING NORMAL. WATER SEPARATOR COVER REINSTALLED AND CLAMP SECURED AND TORQUED IAM MM 21-51
- [SDR 20010529SG003](https://openairdocs.org/sdr/20010529SG003.md): Engine · vibration · Apr 23, 2001 · N311EA · Lkheed 10113851 · Engine (Turbine/Turboprop)
  > ENGINE SHUTDOWN FOR HIGH VIBRATION INDICATION AT FL350. IN CRUISE INDICATION 3 AND AMBER LIGHT. BOTH A AND B PICKUPS. LOW SELECTION INDICATES THIS PROBLEM. TEST CARRIED OUT IAW 71-00-00 TEST 16. ALL TRIM WEIGHTS REMOVED. EPR 1.53=1.3 UNITS 90 PERCENT N1=
- [SDR WRN2001F00000](https://openairdocs.org/sdr/WRN2001F00000.md): Turbine Blades · failed · Apr 22, 2001 · N311EA · Lkheed 10113851 · Turbine Section
  > INSPECTION REVEALED IP TURBINE BLADE FAILURE. REMOVED AND REPLACED ENGINE IAW TRADEWINDS CARD L2-130-A01 AND FORMS TWM-7103B AND TWM-7103BB. AIRCRAFT RUN AND LEAK CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 2001F00004](https://openairdocs.org/sdr/2001F00004.md): O-Ring · pinched · Apr 14, 2001 · N311EA · Lkheed 10113851 · Turbine Engine Oil System
  > NR 3 ENGINE OIL QUANTITY DROPPED TO 1 QUART, OIL PRESSURE FLUCTUATED BUT DID NOT DROP BELOW 35 PSI. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGED (PINCHED) O-RING AT NR 3 ENGINE OIL PRESSURE FILTER BOWL CAP. REMOVED AND REPLACED O-RING IAW MM 72-01-00. R
- [SDR WRN2001F00001](https://openairdocs.org/sdr/WRN2001F00001.md): Compressor · stalled · Apr 12, 2001 · N311EA · Lkheed 10113851 · Turbine Engine Compressor Section
  > ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR ENGINE CHANGE AT MAIN
- [SDR 20010509SG004](https://openairdocs.org/sdr/20010509SG004.md): Compressor · stalled · Apr 12, 2001 · N311EA · Lkheed 10113851 · Turbine Engine Compressor Section
  > ON TAKEOFF ROLL AT 125 KNOTS, NR 1 ENGINE HAD COMPRESSOR STALL. VIBRATION INDICATOR AT 2 UNITS WITH CAUTION LIGHT ON. AIRCRAFT RETURNED TO GATE. PREPARATION FOR TWO ENGINE FERRY BEING ACCOMPLISHED IAW LOCKHEED MM AND TRADEWINDS GMM FOR ENGINE CHANGE AT MX B
- [SDR 20000516AP005](https://openairdocs.org/sdr/20000516AP005.md): Card · malfunctioned · Mar 30, 2000 · N311EA · Lkheed 10113851 · Lighting System
  > NR 2 ENGINE FILTER PRESSURE LIGHT, ALSO ENGINE VIB FILTER PRESSURE LIGHT CAME ON DURING CRUISE. NR 2 ENGINE SHUTDOWN. A/C CAME IN WITH NORMAL APPROACH AND LANDING. REMOVED AND REPLACED PRESSURE FILTER AND FINE SCAVENGE FILTER IAW 72-01-00. LEAK CHECKS GOOD
- [SDR 20000615AP019](https://openairdocs.org/sdr/20000615AP019.md): Doubler · corroded · Jan 9, 2000 · N311EA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING INSPECTION OF FESC, CORROSION FOUND BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV VENTILATION DUCT. REMOVED AND REPLACED CORRODED DOUBLER. CLEANED AND PAINTED AREA. DWG NR 1548569. (M)
- [SDR 20000405AP001](https://openairdocs.org/sdr/20000405AP001.md): Doubler · corroded · Jan 9, 2000 · N311EA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING INSPECTION OF FESC, FOUND CORROSION BETWEEN FS 315 AND 297 FORWARD OF NOSE WHEEL AREA, SURROUNDING FORWARD LAV. VENTILATION DUCT REMOVED AND REPLACED CORRODED DOUBLER. CLEANED AND PAINTED AREA. (M)
- [SDR 2000ZZZM250](https://openairdocs.org/sdr/2000ZZZM250.md): Oil Pump · failed · Oct 19, 1999 · N311EA · Lkheed 10113851 · Turbine Engine Oil System
  > NR 2 ENGINE RAPID LOSS OF OIL QTY ENGIEN RAN APPROXIMATELY 2 MINUTES PRIOR TO SHUTDOWN WINDMILLED WITH NO OIL QTY 23 MINUTES OIL PRESSURE NR 2 LIGHT ON. RETURNED TO BQN, LANDING NORMAL. REMOVED AND REPLACED PRIMARY OIL PUMP ASSEMBLY IAW MM 72-63-03. RUN AND
- [SDR 98ZZZM404](https://openairdocs.org/sdr/98ZZZM404.md): Hyd Line · leaking · Mar 18, 1998 · N311EA · Lkheed 10113851 · Hydraulic System, Main
  > SYSTEM 'C' HYD RSVR QTY LOW AND DECREASING. SWITCHING PUMP OFF DID NOT STOP FLUID LOSS. REF MANUAL GEAR EXTENSION, ATM TURNED OFF FLUID LOSS STOPPED AT AROUND THREE-EIGHTHS TANK QTY. AIRCRAFT LANDING NORMAL. FOUND PIN HOLE LEAK IN HYD C-CHECK SYSTEM RETURN
- [SDR 98ZZZM193](https://openairdocs.org/sdr/98ZZZM193.md): Actuator · failed · Jan 16, 1998 · N311EA · Lkheed 10113851 · Leading Edge Slat Actuator
  > AFTER TAKEOFF DURING FLAP RETRACTION FLAP/SLAT LOCK LIGHT ON, L/E TRANS LIGHT REMAINED ON. GREEN SLAT LIGHTS ON LEFT WING. NO LIGHTS ON RT WING. AIRCRAFT RETURNED TO BASE. LANDING NORMAL. REMOVED AND REPLACED NR 7 SLAT ACT IAW 27-81-21. REMOVED AND REPLA
- [SDR 97ZZZX3958](https://openairdocs.org/sdr/97ZZZX3958.md): Tire · failed · Aug 22, 1997 · N311EA · Lkheed 10113851 · Tire
  > ON TAKEOFF ROLL, NR 6 TIRE BLEW. TIRE RUBBER DAMAGED HYDRAULIC LINE AND T/E WING PANEL. ACFT DUMPED FUEL AND RETURNED TO BASE. LANDING NORMAL. NR 5 AND NR 6 TIRES REPLACED. PANEL P/N 1529072-191 LOCATION NR 541BB WAS REPLACED PER SRM 57-34-00, NOTE 12. P
- [SDR 97ZZZX3800](https://openairdocs.org/sdr/97ZZZX3800.md): Rudder Stud · sheared · Aug 4, 1997 · N311EA · Lkheed 10113851 · Rudder Control System
  > BQN - DURING TAXI, CREW NOTICED A BINDING WITHIN THE RUDDER PEDALS FOLLOWED BY A 'POP' SOUND FROM UNDERNEATH COCKPIT FLOOR. AIRCRAFT RETURNED TO GATE. BQN MAINTENANCE FOUND A RUDDER LINKAGE STUD SHEARED ON THE RIGHT HAND SIDE. REMOVED AND REPLACED STUD AND
- [SDR 97ZZZX3393](https://openairdocs.org/sdr/97ZZZX3393.md): Brace Assy · cracked · Jul 14, 1997 · N311EA · Lkheed 10113851 · Main Landing Gear Attach Section
  > RIGHT MLG DOWNLOCK JURY BRACE FOUND CRACKED UPON MAINTENANCE WALK-AROUND. REMOVED AND REPLACED DOWNLOCK JURY BRACE IAW 32-11-14. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR 97ZZZM707](https://openairdocs.org/sdr/97ZZZM707.md): Actuator · failed · Jun 2, 1997 · N311EA · Lkheed 10113851 · Landing Gear Door Actuator
  > AFTER TAKEOFF, LEFT GEAR INTRANS DOOR, F/E LEFT GEAR OR DOOR LIGHTS ON GEAR RETRACTED. AIRCRAFT DUMPED FUEL AND RETURNED TO BQN WITH A NORMAL LANDING. WHEN AIRCRAFT RETURNED TO GATE, MAINTENANCE NOTED LEFT GEAR DOOR OPEN. MX TROUBLESHOT AND FOUND MLG DOOR A
- [SDR 97ZZZM674](https://openairdocs.org/sdr/97ZZZM674.md): Water Separator · failed duct · May 23, 1997 · N311EA · Lkheed 10113851 · Humidity Control System
  > APPROX 20 MINUTES AFTER TAKEOFF, LOST CONTROL OF CABIN PRESSURE DUE TO LEAK AT 28,000 FEET. A LOUD NOISE OCCURRED AT THE SAME TIME. RETURNED TO GSO, LANDING NORMAL. INSPECTION FOUND NR 2 WATER SEPARATOR HAD BLOWN DUCT. REMOVED AND REPLACED WATER SEPARATOR
- [SDR 97ZZZM570](https://openairdocs.org/sdr/97ZZZM570.md): Panels · missing · Apr 9, 1997 · N311EA · Lkheed 10113851 · Aerodynamic Fairings
  > AFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVIC
- [SDR 97ZZZM569](https://openairdocs.org/sdr/97ZZZM569.md): Panels · missing · Apr 9, 1997 · N311EA · Lkheed 10113851 · Aerodynamic Fairings
  > AFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVIC
- [SDR 97ZZZM571](https://openairdocs.org/sdr/97ZZZM571.md): Actuator · failed · Apr 8, 1997 · N311EA · Lkheed 10113851 · Landing Gear Door Actuator
  > ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT ON, WITH RED DOOR AND RED INTRANSIT LIGHT ON. FUEL JETTISON FROM 76,000 LBS TO 30,000 LBS. AIRCRAFT LANDED NORMALLY. RIGHT DOOR ACTUATOR REMOVED AND REPLACED IAW 32-33-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SE
- [SDR 96ZZZX5798](https://openairdocs.org/sdr/96ZZZX5798.md): Line · cracked · Oct 30, 1996 · N311EA · Lkheed 10113851 · Hydraulic System, Main
  > A-HYD SYS RAPIDLY DEPLETED AT 33,000 FEET. SYS SHUTDOWN IAW FLIGHT MANUAL. AIRCRAFT LANDED NORMALLY. FOUND HYD LINE IN NR 1 PYLON AREA LEAKING. REPAIRED LINE IAW REV MM ATA 20. AIRCRAFT RETURNED TO SERVICE.
- [SDR 96ZZZX5797](https://openairdocs.org/sdr/96ZZZX5797.md): Pdu Motor · cracked · Oct 29, 1996 · N311EA · Lkheed 10113851 · Leading Edge Slat Actuator
  > A-HYD RESERVOIR QTY LOW AND LOW QTY LIGHT ON. TURNED OFF HYD PUMP - LEAK STOPPED. AIRCRAFT LANDED NORMAL. FOUND SLAT A-SYS PDU HYD MOTOR HOUSING CRACKED. REMOVED AND REPLACED MOTOR IAW MM 27-80-10. AIRCRAFT RETURNED TO SERVICE.
- [SDR 96ZZZM1536](https://openairdocs.org/sdr/96ZZZM1536.md): Lock Actuator · failed · Oct 18, 1996 · N311EA · Lkheed 10113851 · Landing Gear Door Retract Section
  > MAIN GEAR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT. LANDING NORMAL. REMOVED AND REPLACED MAIN GEAR DOOR LOCK ACTUATOR IAW 32-33-08 OF THE MM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 96ZZZM371](https://openairdocs.org/sdr/96ZZZM371.md): Prox Logic Box · malfunctioned · Feb 20, 1996 · N311EA · Lkheed 10113851 · Landing Gear Position and Warning
  > NOSE GEAR OR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB, RETURNED TO AIRPORT. LANDING WAS NORMAL. ADJUSTED NOSE GEAR UPLOCK SENSOR IAW 32-61-04. REMOVED AND REPLACED PROX LOGIC BOX IAW 31-22-01. INSTALLED PROX LOGIC CARD IAW 31-22-02, CARRIED
- [SDR DLSP96004](https://openairdocs.org/sdr/DLSP96004.md): Skin · cracked · Feb 16, 1996 · N311EA · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN WAS FOUND WITH AN APPROXIMATE 1 INCH LONG CRACK RUNNING HORIZONTALLY FROM THE FORWARD EDGE OF THE SKIN AT FS 1363 LOCATED MIDWAY BETWEEN STR 18 AND STR 19. THE CRACK IS SIMILAR TO THOSE ADDRESSED IN
- [SDR DLSP96003](https://openairdocs.org/sdr/DLSP96003.md): Angle · oversize holes · Feb 16, 1996 · N311EA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > ATL - DURING CONTRACT MAINTENANCE AT DALA, C/W AD 94-05-01, REPLACEMENT OF FUSELAGE LT AND RT WING TO FUSELAGE AT TACH UPPER ROOT JOINT FAIL-SAFE ANGLE, SEVERAL HOLES WERE FOUND OVERSIZED AND OUT-OF-ROUND. REAMED HOLES TO A ROUND CONDITION PER DL ERA 273277-1
- [SDR DLSP96002](https://openairdocs.org/sdr/DLSP96002.md): Skin · cracked · Feb 16, 1996 · N311EA · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > ATL - DURING CONTRACT MAINTENANCE WITH DALA, FOUND FUSELAGE SKIN AT FS 1363 CRACKED IN THE TYPICAL MANNER DEPICTED IN THE L1011 SRM 53-11-00, FIGURE 826, REPAIR. THE SUBJECT CRACK IS APPROXIMATELY 12 INCHES IN LENGTH AND HAD BEEN PREVIOUSLY REPAIRED PER SRM 5
- [SDR DLSP96001](https://openairdocs.org/sdr/DLSP96001.md): Skin · cracked · Feb 16, 1996 · N311EA · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN AT FS 1363 IS CRACKED IN THE TYPICAL MANNER DEPICTED IN SRM 53-11-00, FIGURE 826, REPAIR. THE CRACK IS APPROXIMATELY 2.25 INCHES LONG, LOCATED BETWEEN STR 21 AND STR 22. THE SUBJECT CRACK WAS PREVI
- [SDR 96ZZZM283](https://openairdocs.org/sdr/96ZZZM283.md): Press Ctlr · failed · Feb 4, 1996 · N311EA · Lkheed 10113851 · Cabin Pressure Controller
  > AIRCRAFT DEPARTED BQN EN ROUTE TO GSO, CREW EXPERIENCED DIFFICULTY WITH CABIN PRESSURIZATION. C/B 3X14 PULLED AND RESET TO NO AVAIL. AIRCRAFT RETURNED TO BQN. LANDING NORMAL. AFT OUTFLOW VALVE OK IN ALL MODES, FORWARD VALVE INOP IN ALL MODES. T/S PER 21-5
- [SDR 95ZZZM520](https://openairdocs.org/sdr/95ZZZM520.md): Angle · cracked · Sep 12, 1995 · N311EA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING NORMAL SERVICING OF ATM, MAINTENANCE NOTICED A CRACK LOCATED AT FS 1363 WL 147 (APPROXIMATELY) ON THE RIGHT SIDE. ANGLE 1561639-101 REPAIRED IAW SRM 53-11-00 FIG 822. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 95ZZZM506](https://openairdocs.org/sdr/95ZZZM506.md): Pin · cracked · Sep 2, 1995 · N311EA · Lkheed 10113851 · Landing Gear Retraction/Extension System
  > WHILE PERFORMING ROUTINE MAINTENANCE, MECHANIC FOUND LEFT MLG RETRACT ACTUATOR PIN CRACKED AT AFT HOUSING. MLG PIN WAS REMOVED AND REPLACED IAW 32-11-27. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR 95ZZZX4103](https://openairdocs.org/sdr/95ZZZX4103.md): Bulkhead · cracked · Jul 8, 1995 · N311EA · Lkheed 10113851 · Fuselage Main, Bulkhead
  > ACCOMPLISHED AD 95-12-24. DISCOVERED CRACKS ON RIGHT LOWER OUTBOARD SECTION OF FS 1363 BULKHEAD BY VISUAL INSPECTION. PERFORMED BOLT HOLE EDDY CURRENT INSPECTION IAW SB 093-53-268. TWO CRACKS WERE FOUND ON THE BULKHEAD CAP AT BL 42.5. LOCKHEED NOTIFIED AND
- [SDR 95ZZZW622](https://openairdocs.org/sdr/95ZZZW622.md): Spar Web · cracked · Apr 18, 1995 · N311EA · Lkheed 10113851 · Wing Spar
  > WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W)
- [SDR 95ZZZW621](https://openairdocs.org/sdr/95ZZZW621.md): Spar Web · cracked · Apr 18, 1995 · N311EA · Lkheed 10113851 · Wing Spar
  > WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W)
- [SDR DALR950002](https://openairdocs.org/sdr/DALR950002.md): Fitting · cracked · Apr 17, 1995 · N311EA · Lkheed 10113851 · Fuselage, Landing Gear Attach Fittings
  > ATL - DURING LETTER CHECK AT DALR, THE NLG SHOCK STRUT SUPPORT FITTING ON THE RBL 22 BULKHEAD WAS FOUND CRACKED NEAR FS 449. CRACKS WERE REPAIRED PER DER APPROVED DATA, EL ERA 270628-14. TT, 38155 HRS. CYCLES, 18905. (X)
- [SDR DALR950006](https://openairdocs.org/sdr/DALR950006.md): Fitting · corroded · Apr 6, 1995 · N311EA · Lkheed 10113851 · Wing Miscellaneous Structure
  > ATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVESIZED TO CLEAN UP CORROSION PER DL ERA 270605-14. TT 38155 HRS. CYCLES, 18905. (X)
- [SDR DALR950013](https://openairdocs.org/sdr/DALR950013.md): Wing Skin · cracked · Apr 5, 1995 · N311EA · Lkheed 10113851 · Wing, Plate/Skin
  > ATL - DURING LETTER CHECK, COMPLYING WITH AD 94-05-01 AND AD 93-17-01. AT THE REPLACEMENT OF THE LEFT WING INBOARD REAR SPAR SECTION, A CRACK WAS FOUND IN THE UPPER WING SKIN AT APPROXIMATELY IWS 332 AT A FASTENER HOLE. THE HOLE WAS OVERSIZED TO REMOVE THE C
- [SDR DALR950005](https://openairdocs.org/sdr/DALR950005.md): Spar Cap · cracked · Apr 3, 1995 · N311EA · Lkheed 10113851 · Wing Spar
  > ATL - DURING LETTER CHECK AT DALR. THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP WAS FOUND WITH A CRACK IN ITS LEFT SIDE OUTBOARD END. THIS CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPISHED PER DL ERA 270580-14. TT, 38155
- [SDR DALR950004](https://openairdocs.org/sdr/DALR950004.md): Spar Cap · cracked · Apr 3, 1995 · N311EA · Lkheed 10113851 · Wing Spar
  > ATL - DURING LETTER CHECK AT DALR, WING CENTER SECTION FS 1043 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLIHSED PER DL ERA 270578-14. TT, 38155 HRS. CY
- [SDR DALR950003](https://openairdocs.org/sdr/DALR950003.md): Spar Cap · cracked · Apr 3, 1995 · N311EA · Lkheed 10113851 · Wing Spar
  > ATL - DURING LETER CHECK AT DALR. THE WING CENTER SECTION INTERMEDIATE SPAR UPPER CAP AT FS 1103 WAS FOUND CRACKED AT THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLISHED PER DL ERA 270579-14. TT, 3
- [SDR DALR950001](https://openairdocs.org/sdr/DALR950001.md): Fitting · corroded · Apr 3, 1995 · N311EA · Lkheed 10113851 · Wing, Landing Gear Attach Fittings
  > ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10 DURING THE REPLACEMENT OF THE INBOARD LEFT AND RIGHT REAR SPAR WEB AND REWORK OF THE UPPER 1.1250 INCH (2 TOTAL) AND INBOARD.6250 INCH (4 TOTAL) HOLES AT THE MLG BACKUP FITTING IWS
- [SDR DALR950008](https://openairdocs.org/sdr/DALR950008.md): Skin · cracked · Mar 31, 1995 · N311EA · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > ATL - DURING LETTER CHECK A DALR. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER RIGHT SIDE OF THE FS 983 PRESSURE BULKHEAD UNDER THE FUSELAGE-TO-WING BOX LONGERON. THE SKIN WAS FOUND WITH A 1.5 INCH LONG CRACK IN THE SECOND FASTENER ROW FORWARD OF THE BUL
- [SDR DALR950010](https://openairdocs.org/sdr/DALR950010.md): Doubler · cracked · Mar 30, 1995 · N311EA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 FUSELAGE NLG WHEELWELL MOD. FS 328 PER DL EO.7-53207-3AD. AN ADDITIONAL CRACK WAS FOUND THAT WAS BEYOND THE SCOPE OF THE E.O. THE CRACK LIES IN THE SKIN DOUBLER AT THE FORWARD LEFT CORNER OF THE
- [SDR DALR950009](https://openairdocs.org/sdr/DALR950009.md): Longeron · corroded · Mar 30, 1995 · N311EA · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > ATL - DURING LETTER CHECK AT DALR. CONSIDERABLE CORROSION WAS FOUND AT FS 328 ON THE VERTICAL FLANGE OF THE LBL 22 NLG WHEELWELL SIDEWALL LOWER LONGERON. A NEW SECTION OF LONGERON WAS SPLICED IN PER DL ERA 270527-14. TT, 38155 HRS. CYCLES, 18905. (X)

Next page: https://openairdocs.org/deregistered/N311EA-2004-02-23/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 = 'N311EA' AND deregistration_id = 'N311EA-2004-02-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N311EA-2004-02-23/reports

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