# Service difficulty reports: N315NE, cancelled Feb 29, 2008

A list on [N315NE, cancelled Feb 29, 2008](https://openairdocs.org/deregistered/N315NE-2008-02-29.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 3 · 102 reports

- [SDR EISA20010101](https://openairdocs.org/sdr/EISA20010101.md): Crease Beam · cracked · Jun 17, 2001 · N315NE · Boeing 727223 · Fuselage Main, Structure
  > LT FUSELAGE CREASE BEAM WEB IS CRACKED AT BS 1090 FLOOR LEVEL. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED WEB AND FILLER ANGLE. REPAIRS IAW B727 SRM 51-30-2, 51-10-1, 51-40-2, 51-10-2 AND MM 51-22-11.
- [SDR EISA20010100](https://openairdocs.org/sdr/EISA20010100.md): Floorbeam · corroded · Jun 17, 2001 · N315NE · Boeing 727223 · Fuselage Main, Floor Beam
  > AFT PIT-CABIN FLOORBEAM BS 1110 RBL 22 AFT SIDE EXFOLIATED AT NUT CLIP. CUT OUT CORRODED SECTION OF THE UPPER FLANGE OF FLOORBEAM, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIRS IAW B727 SRM 53-10-8 FIG 1.
- [SDR EISA20010099](https://openairdocs.org/sdr/EISA20010099.md): Floorbeam · cracked · Jun 16, 2001 · N315NE · Boeing 727223 · Fuselage Main, Floor Beam
  > FLOORBEAM IS CRACKED IN THE RT MID CABIN AT BS 848, UNDER THE O/B, RT SEAT TRACK APPROX 10 INCHES LONG IN LENGTH. REMOVED CRACKED SECTION. FABRICATED AND INSTALLED A NEW WEB, WEB SPLICE AND T-CAP REPAIRS IAW B727 SRM 51-40-2 FIG 1 & 51-30-2.
- [SDR EISA20010070](https://openairdocs.org/sdr/EISA20010070.md): Flap · delaminated · Mar 12, 2001 · N315NE · Boeing 727223 · Trailing Edge Flaps
  > DURING ROUTINE B-CHECK INSPECTION, FOUND RT INBOARD LOWER FLAP HAS DELAMINATED AREA. BONDED FIBERGLASS OVERLAYS TO REPAIR DOUBLER AND FILLER, ALODINED, SEALED AND PRIMED IAW SRM 51-40-5, 51-40-2, 57-50-1 AND M/M 51-20-151.
- [SDR EISA20010031](https://openairdocs.org/sdr/EISA20010031.md): Connector · loose · Feb 24, 2001 · N315NE · Boeing 727223 · Leading Edge Slat Actuator
  > NR 8 LEADING EDGE SLAT HAD BOTH AMBER LIGHTS ON IN AGREEMENT, PILOT STATED THAT HE COULD FEEL VIBRATION. THE AIRCRAFT OVERFLEW DFW TO IND. INSPECTED NR 8 ACTUATOR AND FOUND LOOSE CONNECTOR. TIGHTENED CONNECTOR ON ACTUATOR, OPS CHECK GOOD.
- [SDR EISA20000195](https://openairdocs.org/sdr/EISA20000195.md): Cylinder · intermittent · Oct 29, 2000 · N315NE · Boeing 727223 · Landing Gear Retraction/Extension System
  > PERFORMED MANUAL NOSE GEAR EXTENSION INTO (JFK). REMOVED AND REPLACED NOSE GEAR TRANSFER CYLINDER AND REDUCER VALVE.
- [SDR EISA20000147](https://openairdocs.org/sdr/EISA20000147.md): Coupler · inoperative · Sep 12, 2000 · N315NE · Boeing 727223 · Gust Lock Damper System
  > ON TAKEOFF UPPER YAW DAMPER INOP. AIR TURNBACK TO (IND). REMOVED AND REPLACED YAW DAMPER COUPLER. OPS CHECK NORMAL.
- [SDR EISA20000131](https://openairdocs.org/sdr/EISA20000131.md): Flow Valve · inoperative · Aug 27, 2000 · N315NE · Boeing 727223 · Cabin Cooling System
  > UNABLE TO MAINTAIN CABIN PRESSURE. LEFT PACK APPEARS TO BE INOP, RETURNED TO IND. REMOVED AND REPLACED NEW FLOW CONTROL VALVE, OPS CHECK NORMAL, PER M/M 36-10.
- [SDR EISA2000029](https://openairdocs.org/sdr/EISA2000029.md): Rivet · sheared · Mar 7, 2000 · N315NE · Boeing 727223 · Nose/Tail Landing Gear Strut/Axle
  > TAILSKID LIGHT REMAINED ON AFTER GEAR UP. REPLACED SHEARED RIVETS IN ENERGY ABSORBER IAW 32-71-71. ADJUSTED SWITCH IAW 3271-91. (M)
- [SDR EISA99179](https://openairdocs.org/sdr/EISA99179.md): Skin · corroded · Oct 7, 1999 · N315NE · Boeing 727223 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE OF AT WS 491.5 TO 505 BETWEEN STRINGER 5 AND 6. REMOVED CORROSION PER SRM 51-10-6. FABRICATED AND INSTALLED DOUBLER PER FLIGHT VEHICLES CONSULTING INC EO NR 5
- [SDR EISA99178](https://openairdocs.org/sdr/EISA99178.md): Skin · corroded · Oct 7, 1999 · N315NE · Boeing 727223 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON LOWER SURFACE OF RIGHT WING AT WS 460 BETWEEN STRINGER 8 AND 9. REMOVED CORROSION PER SRM 51-10-6. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER PER FLIGHT VEH
- [SDR EISA99204](https://openairdocs.org/sdr/EISA99204.md): Fitting · misdrilled · Oct 5, 1999 · N315NE · Boeing 727223 · Vertical Stabilizer
  > DURING REPLACEMENT OF VERTICAL FIN FRONT SPAR UPPER RIGHT TERMINAL FITTING AND SUBSEQUENT REMOVAL OF PREVIOUS REPAIR FOUND MIS-DRILLED HOLES IN LEFT HAND TERMINAL FITTING. REMOVED AND REPLACED LEFT TERMINAL FITTING PER SB 55-0060 AND BAC DRAWING 65-89361. (M
- [SDR EISA99203](https://openairdocs.org/sdr/EISA99203.md): Skin · corroded · Oct 5, 1999 · N315NE · Boeing 727223 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE FROM WS 460 TO 650 AROUND FASTENERS. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS PER SRM 57-30-1, FABRICATED AND INSTALLED DOUBLER PER FLIGHT VEHICLES CONSULT
- [SDR EISA99205](https://openairdocs.org/sdr/EISA99205.md): Fitting · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Vertical Stabilizer
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND 1 INCH CRACK IN VERTICAL FIN SPAR TERMINAL FITTING RIGHT SIDE. REMOVED DAMAGED FITTING REPLACED WITH NEW FITTING PER SB 55-0060 AND BAC BLUEPRINT 65-89361. (M)
- [SDR EISA99202](https://openairdocs.org/sdr/EISA99202.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 348, STRINGER 25R. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99201](https://openairdocs.org/sdr/EISA99201.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 277, STRINGER 25R. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99200](https://openairdocs.org/sdr/EISA99200.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 400 STRINGER 26L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99199](https://openairdocs.org/sdr/EISA99199.md): Skin · delaminated · Sep 14, 1999 · N315NE · Boeing 727223 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND DELAMINATION AT TRAILING EDGE OF RIGHT INBOARD AFT FLAP. REMOVED DAMAGED AREA. INSTALLED NEW HONEYCOMB CORE PER SRM 51-40-6 AND FIBERGLASS OVERLAY PER SRM 51-40-6. PRIMED AND PAINTED PER MM 51-20-15
- [SDR EISA99198](https://openairdocs.org/sdr/EISA99198.md): Skin · delaminated · Sep 14, 1999 · N315NE · Boeing 727223 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND RIGHT INBOARD MID FLAP DELAMINATED AT TRAILING EDGE AT WBL 200. REMOVED DAMAGED SKIN PER SRM 51-40-6. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. (M)
- [SDR EISA99197](https://openairdocs.org/sdr/EISA99197.md): Skin · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CRACK AT INBOARD OF RIGHT INBOARD FOREFLAP. REMOVED DAMAGED AREA, REPAIRED INBOARD TIP WITH POTTING COMPOUND PER SRM 51-40-6. (M)
- [SDR EISA99196](https://openairdocs.org/sdr/EISA99196.md): Skin · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 800 RBL 18. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS PER SRM 57-10-1. FABRICATED REPAIR DOUBLER PER SRM 57-30-3. TREATED AND PRIMED REPAIR PARTS
- [SDR EISA99195](https://openairdocs.org/sdr/EISA99195.md): Support · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION AT FS 805 WING CENTER FUEL TANK ABOVE AFT END OF RIGHT HEAT EXCHANGER ON STRUCTURE SUPPORT OUTBOARD SURFACE. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICATED DOUBLER PER SRM 51-40
- [SDR EISA99194](https://openairdocs.org/sdr/EISA99194.md): Skin · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 805, LBL 18. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS PER SRM 57-10-1. FABRICATED REPAIR PER SRM 57-30-3, TREATED AND PRIMED PER SRM 51-10-2 AND
- [SDR EISA99193](https://openairdocs.org/sdr/EISA99193.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 23L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99192](https://openairdocs.org/sdr/EISA99192.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 22L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99191](https://openairdocs.org/sdr/EISA99191.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Emergency Lighting
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 20L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99190](https://openairdocs.org/sdr/EISA99190.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 19L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99189](https://openairdocs.org/sdr/EISA99189.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 500 STRINGER 19R. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99188](https://openairdocs.org/sdr/EISA99188.md): Tie Clip · cracked · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CLIP CRACKED AT FS 700 STRINGER 20L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M)
- [SDR EISA99187](https://openairdocs.org/sdr/EISA99187.md): Seat Track · gouged · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 5 SEAT TRACK GOUGED FROM FS 720D TO 720E. DAMAGE OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 222136-1-1 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2.
- [SDR EISA99186](https://openairdocs.org/sdr/EISA99186.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARAD FOUND NR 4 SEAT TRACK CORRODED AT FS 640. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 222136-1-1 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INST
- [SDR EISA99185](https://openairdocs.org/sdr/EISA99185.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED AT FS 1110. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520 -792 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INST
- [SDR EISA99184](https://openairdocs.org/sdr/EISA99184.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 1070. MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALL
- [SDR EISA99183](https://openairdocs.org/sdr/EISA99183.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 870. REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INS
- [SDR EISA99182](https://openairdocs.org/sdr/EISA99182.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK, LBL 24, CORRODED FROM FS 760 TO 850. MATERIAL LOSS OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2.
- [SDR EISA99181](https://openairdocs.org/sdr/EISA99181.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 720C. CORROSION OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SRM 53-10-05. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 460 T
- [SDR EISA99180](https://openairdocs.org/sdr/EISA99180.md): Seat Track · corroded · Sep 14, 1999 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED FROM FS 460 TO 690 LBL 42. CORROSION OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SRM 53-10-05. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW TR
- [SDR EISA98173](https://openairdocs.org/sdr/EISA98173.md): Line · failed · Jul 8, 1998 · N315NE · Boeing 727223 · Pneumatic Distribution System
  > AFTER DEPARTURE FROM LAX, PASSING 4500 FT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, PERFORMED CHECKLIST LIGHT EXTINGUISHED. FOUND LEAKING SENSE LINE AT 13TH STAGE MODULATION VALVE. REPLACED LINE, OPS CHECK GOOD PER MM 36-10-00, 36-12-00, NO OTHER LEAKS NOTED.
- [SDR EISA98172](https://openairdocs.org/sdr/EISA98172.md): Clamp · failed · Jul 7, 1998 · N315NE · Boeing 727223 · Pneumatic Distribution System
  > ON CLIMB-OUT OF PDX AT APPROXIMATELY 4500 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RETURNED TO NORMAL. R
- [SDR EISA98171](https://openairdocs.org/sdr/EISA98171.md): Clamp · loose · Jul 7, 1998 · N315NE · Boeing 727223 · Pneumatic Distribution System
  > AFTER TAKEOFF FROM LAX WHILE CLIMBING THROUGH 5000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RETURNED T
- [SDR EISA98170](https://openairdocs.org/sdr/EISA98170.md): Clamp · loose · Jul 7, 1998 · N315NE · Boeing 727223 · Pneumatic Distribution System
  > AFTER TAKEOFF FROM MCI WHILE CLIMBING THROUGH 3200 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLT, EVEN AFTER NR 1 THROTTLE RETURNED TO NO
- [SDR EISA98169](https://openairdocs.org/sdr/EISA98169.md): Clamp · loose · Jul 7, 1998 · N315NE · Boeing 727223 · Engine Start Valves/Controls
  > AFTER TAKEOFF FROM IND WHILE CLIMBING THROUGH APPROXIMATELY 5000 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMALS ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES COOLING PERIOD, LIGHT REMAINED OFF FOR REMAINDER OF FLIGHT
- [SDR EISA98149](https://openairdocs.org/sdr/EISA98149.md): Clamp · loose · Jul 1, 1998 · N315NE · Boeing 727223 · Pneumatic Distribution System
  > DFW - DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, REDUCED POWER, CLOSED NR 1 ENGINE BLEED PER ABNORMAL CHECKLIST, LIGHT EXTINGUISHED. TIGHTENED CLAMP TO DUCT. START LEAK TEST, OK FOR SERVICE IAW MM 26-14. (M)
- [SDR EISA98165](https://openairdocs.org/sdr/EISA98165.md): Skin · delamintated · Jun 28, 1998 · N315NE · Boeing 727223 · Rudder, Tab Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER TAB DELAMINATED AT TRAILING EDGE LOWER CORNER. REPAIRED DELAMINATION PER SRM 51-40-6. (M)
- [SDR EISA98164](https://openairdocs.org/sdr/EISA98164.md): Frame · cracked · Jun 28, 1998 · N315NE · Boeing 727223 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF CPCP CARD C53-224-05, FOUND CRACK IN FUSELAGE FRAME AT FS 500 WL 214. REMOVED DAMAGED AREA. FABRICATED REPAIR PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2. (M)
- [SDR EISA98162](https://openairdocs.org/sdr/EISA98162.md): Seat Track · corroded · Jun 28, 1998 · N315NE · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK AT FS 848-870. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK FROM FS 848.95 TO FS 870. (M)
- [SDR EISA98161](https://openairdocs.org/sdr/EISA98161.md): Fitting · cracked · Jun 28, 1998 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING REPLACEMENT OF LEFT MAIN LANDING GEAR, FOUND FORWARD TRUNNION BEARING ATTACH FITTING CRACKED AT LOWER INBOARD BUSHING HOLE. REMOVED DAMAGED FITTING. INSTALLED NEW FITTING PER SRM 51-10-1 AND 51-30-1. (M)
- [SDR EISA98160](https://openairdocs.org/sdr/EISA98160.md): Stringer · cracked · Jun 28, 1998 · N315NE · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND STRINGER 24L CRACKED JUST FORWARD OF FS 950A. REMOVED DAMAGED AREA. FABRICATED REPAIR PER SRM 53-10-3 AND INSTALLED PER SRM 53-10-03. (M)
- [SDR EISA98159](https://openairdocs.org/sdr/EISA98159.md): Bracket · corroded · Jun 28, 1998 · N315NE · Boeing 727223 · Cargo/Baggage Doors
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FORWARD CARGO DOOR LOWER AFT CORNER, ANGLE BRACKET EXFOLIATED. REMOVED BRACKET. FABRICATED AND INSTALLED NEW BRACKET PER SRM 53-10-02. (M)
- [SDR EISA98158](https://openairdocs.org/sdr/EISA98158.md): Web · cracked · Jun 28, 1998 · N315NE · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF CPCP WORK CARD, C3-224-08, FOUND CRACK INSIDE FS 1183 WALL AT LBL 50 EXTENDING FROM LIGHTENING HOLE IN WEB. REMOVED DAMAGED AREA IN WEB. FABRICATED REPAIR PER SRM 51-40-2 AND INSTALLED REPAIR PER SRM 57-30-02. TT: 72,562.53 HOURS.

Next page: https://openairdocs.org/deregistered/N315NE-2008-02-29/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 = 'N315NE' AND deregistration_id = 'N315NE-2008-02-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N315NE-2008-02-29/reports

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