# Service difficulty reports: N252US, cancelled Sep 22, 2011

A list on [N252US, cancelled Sep 22, 2011](https://openairdocs.org/deregistered/N252US-2011-09-22.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 · 98 reports

- [SDR GAIA06035ST](https://openairdocs.org/sdr/GAIA06035ST.md): Skin · damaged · Dec 13, 2006 · N252US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING WALKAROUND, A HOLE WAS FOUND ON THE LT FUSELAGE SKIN BETWEEN BS 360 AND BS 380. FURTHER INSPECTION FOUND THAT STRINGER 24 WAS ALSO DAMAGED. PERFORMED REPAIRS IAW 53-30-3, FIG 1 AND 53-30-3, FIG 3A, DETAIL 1 IN THE SRM AND EA B7-53-032. AIRCRAFT RETUR
- [SDR GAIA06012](https://openairdocs.org/sdr/GAIA06012.md): Skin · cracked · Mar 23, 2006 · N252US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING INSPECTION A CRACK WAS FOUND ON THE SKIN BY THE LOWER AFT CORNER OF THE R-2 DOOR CUT OUT. REPAIRED THE SKIN IAW SB. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA06011](https://openairdocs.org/sdr/GAIA06011.md): Attach Fitting · cracked · Mar 23, 2006 · N252US · Boeing 727251 · Wing, Landing Gear Attach Fittings
  > DURING INSPECTION A CRACK WAS FOUND ON THE RT MLG FORWARD TRUNNION ATTACH FITTING. REMOVED AND REPLACED THE TRUNNION ATTACH FITTING IAW SB AC RETURNED TO SERVICE. (K)
- [SDR GAIA06008](https://openairdocs.org/sdr/GAIA06008.md): Switch · intermittent · Feb 24, 2006 · N252US · Boeing 727251 · Landing Gear Position and Warning
  > ON APPROACH TO LANDING, AT GEAR EXTENSION THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED GREEN NOSE GEAR LIGHT NOT ILLUMINATED. EVENTUALLY THE RED LIGHT WENT OUT AND THE GREEN LIGHT CAME ON. AN UNEVENTFUL LANDING WAS MADE. LUBRICATED NOSE LANDING GEAR, CLEANED
- [SDR GAIA06007](https://openairdocs.org/sdr/GAIA06007.md): Accessory Unit · intermittent · Feb 24, 2006 · N252US · Boeing 727251 · Landing Gear Retraction/Extension System
  > ON APPROACH TO LANDING, AT GEAR EXTENSION THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED GREEN NOSE GEAR LIGHT NOT ILLUMINATED. SECONDARY VIEW PORT INDICATED GEAR DOWN. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW MM. NO
- [SDR GAIA06006](https://openairdocs.org/sdr/GAIA06006.md): Switch · intermittent · Feb 23, 2006 · N252US · Boeing 727251 · Landing Gear Position and Warning
  > ON APPROACH TO LANDING, AT GEAR EXTENSION THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED GREEN NOSE GEAR LIGHT NOT ILLUMINATED. SECONDARY VIEW PORT INDICATED GEAR DOWN. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NOSE GEAR DOWN AND LOCK SWITCH IAW MM.
- [SDR GAIA0521OP](https://openairdocs.org/sdr/GAIA0521OP.md): Coalescer Bag · dirty · Jun 23, 2005 · N252US · Boeing 727251 · Humidity Control System
  > DURING CLIMB OUT, FUEL ODOR, LANDING WAS MADE WITHOUT INCIDENT. CHECKED AFT SPAR ENGINE FUEL FEED LINE SHROUDS, NO LEAKS NOTED. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS, RAN BOTH PACKS, NO FUEL ODOR NOTED. OPS AND LEAK CHECKED OK. AIRCRAFT WAS RETURN
- [SDR GAIA04176OP](https://openairdocs.org/sdr/GAIA04176OP.md): Gcu · malfunctioned · Dec 7, 2004 · N252US · Boeing 727251 · AC Regulator
  > DURING APPROACH, LOST ALL (REMAINING, NR 2 AND NR 3) GENERATORS IN FLIGHT DURING APPROACH. RESET NR 2 GEN. NO VOLTAGE OR FREQS. ON NR 3, UNABLE TO RESET. FAULT PANEL INDICATED NR 3 SYSTEM UNDER VOLTAGE. LANDING WAS MADE WITHOUT INCIDENT. SWAPPED NR 3 GCU
- [SDR GAIA04091OP](https://openairdocs.org/sdr/GAIA04091OP.md): Accessory Unit · inoperative · Aug 31, 2004 · N252US · Boeing 727251 · Landing Gear Retraction/Extension System
  > FLT 713 - SJU-MIA - DURING CRUISE, RIGHT MAIN GEAR RED LIGHT ILLUMINATED IN FLIGHT. FLIGHT CONTINUED TO SJU WHERE A LANDING WAS MADE WITHOUT INCIDENT. TROUBLE SHOT PER MM 32-61-01 AND FOUND LANDING GEAR ACCY UNIT TO BE AT FAULT. REMOVED AND REPLACED SAME PE
- [SDR GAIA04069OP](https://openairdocs.org/sdr/GAIA04069OP.md): Clamp · loose · Apr 20, 2004 · N252US · Boeing 727251 · Pneumatic Distribution System
  > NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON JUST AFTER TAKE-OFF. CREW RETURNED AIRCRAFT TO DEPARTURE AERODROME (FWA) WHERE AN UNEVENTFUL LANDING WAS MADE. DUPLICATED PROBLEM DURING GROUND ENGINE RUN. TIGHTENED SEVERAL CLAMPS ON BLEED LINES AND (B) NUT ON SENSE
- [SDR GAIA04050OP](https://openairdocs.org/sdr/GAIA04050OP.md): Connector · dirty · Mar 17, 2004 · N252US · Boeing 727251 · Flight Control System Wiring
  > AFTER TAKEOFF, THE NR 3 LEADING EDGE DEVICE DID NOT RETRACT ON FLAP RETRACTION. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. CLEANED CONNECTOR ON NR 3 LEADING EDGE DEVICE ACTUATOR. RAN FLAPS SYSTEM, OPS CHECKED NORMAL. THE AIRCRAFT WAS
- [SDR GAIA03021OP](https://openairdocs.org/sdr/GAIA03021OP.md): Pump · failed · Jun 25, 2003 · N252US · Boeing 727251 · Engine Fuel Pump
  > DURING CLIMB-OUT FROM EWR AT 6500 FEET, THE NR 3 ENGINE QUIT. THE AIRCRAFT RETURNED TO EWR. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND THE DRIVE SHAFT SHEARD ON THE ENGINE DRIVEN FUEL PUMP. THE FUEL PUMP AND FUEL CONTROL WERE REPLACED. OPERATIONALLY
- [SDR GAIA03018OP](https://openairdocs.org/sdr/GAIA03018OP.md): Odor · detected · Jun 11, 2003 · N252US · Boeing 727251 · Air Distribution System
  > DURING FLIGHT AND TAXI IN, CREW NOTICED A UNIDENTIFIABLE ODOR IN THE COCKPIT. FUEL LEAKS WERE REPAIRED AT LT WING TO BODY BOLT AND AT BOTH LT AND RT FORWARD TRUNNION FITTINGS. REMOVED AND REPLACED BOTH WATER SEPARATOR SOCKS. INSPECTED ENTIRE AIRCRAFT, RAN E
- [SDR GAIA03017OP](https://openairdocs.org/sdr/GAIA03017OP.md): Coalescer Bag · contaminated · Jun 10, 2003 · N252US · Boeing 727251 · Humidity Control System
  > DURING CLIMB-OUT, CREW NOTICED A STRONG, SMOKEY SOLVENT ODOR COMING FROM AIR VENTS. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED BOTH WATER SEPARATOR SOCKS. INSPECTED ENTIRE AIRCRAFT, RAN ENGINES, AND PRESSURIZED AIRCRAFT TO 5 PSI DIFFERENTIAL PRESSU
- [SDR GAIA03016OP](https://openairdocs.org/sdr/GAIA03016OP.md): Line · leaking · May 16, 2003 · N252US · Boeing 727251 · Engine Bleed Air System
  > RIGHT STRUT OVERHEAT LIGHT CAME ON IN FLIGHT. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED 13TH STAGE MOD VALVE SENSE LINE ON NR 3 ENGINE. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02154OP](https://openairdocs.org/sdr/GAIA02154OP.md): Hinge · cracked · Nov 7, 2002 · N252US · Boeing 727251 · Fuselage, Door Hinge
  > DURING ROUTINE INSPECTION OF THE MAIN CARGO DOOR HINGE, A CRACK WAS INDICATED ON THE FORWARD END OF BOTH HALVES, FUSELAGE/DOOR. ALSO, AT THE AFT END OF FUSELAGE HALF. NON DESTRUCTIVE INSPECTION CONFIRMED FINDING. REMOVED AND REPLACED HINGE IAW SB AEIO1-01 R
- [SDR GAIA02099OP](https://openairdocs.org/sdr/GAIA02099OP.md): Light · inoperative · Aug 28, 2002 · N252US · Boeing 727251 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE CABIN EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02033OP](https://openairdocs.org/sdr/GAIA02033OP.md): Transmitter · inoperative · Apr 11, 2002 · N252US · Boeing 727251 · Trailing Flap Position Indicating System
  > FLT 2863 - BWI-FWA - ON APPROACH, THE AIRCRAFT HAD THE OUTBOARD FLAPS ASYMMETRY BETWEEN ZERO AND TWO DEGREES FLAPS. THE CREW USED THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT FWA UNEVENTFUL. REMOVED AND REPLACED LEFT AND RIGHT O
- [SDR GAIA02032OP](https://openairdocs.org/sdr/GAIA02032OP.md): Connector · dirty · Apr 10, 2002 · N252US · Boeing 727251 · Trailing Edge Flap Control System
  > FLT 713 - HSV-FWA - ON APPROACH, THE AIRCRAFT HAD OUTBOARD SPLIT FLAP INDICATION. THE CREW USED THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT HSV UNEVENTFUL. CLEANED THE CONNECTOR PLUG AT THE OUTBOARD FLAP TRANSMITTERS. CYCLED T
- [SDR GAIA02030BOP](https://openairdocs.org/sdr/GAIA02030BOP.md): Engine · failed · Apr 4, 2002 · N252US · Boeing 727251 · Engine (Turbine/Turboprop)
  > FLT 734 - FWA-DFW - ON CLIMB AT FL270, THE FLIGHT CREW HEARD THE NR 1 ENGINE MAKE A GRINDING NOISE. THE OIL TEMP INCREASED TO 120 AND THERE WAS A SHARP JUMP IN EPR. OIL PRESSURE DECREASED AND THE NR 1 ENGINE WAS SHUTDOWN. THE CREW DECLARED AN EMERGENCY AND
- [SDR GAIA02021OP](https://openairdocs.org/sdr/GAIA02021OP.md): Transmitter · damaged · Feb 28, 2002 · N252US · Boeing 727251 · Trailing Flap Position Indicating System
  > FLT 715 - ELP-FWA - ON DESCENT, THE AIRCRAFT HAD OUTBOARD SPLIT FLAP IINDICATION. THE CERW USED THE ALTERNATE FLAP SYSTEM TO LOWER THE FLAPS TO THEIR DESIRED SETTINGS PER THE CHECKLIST. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED IN FWA UNEVENTFUL
- [SDR GAIA02019OP](https://openairdocs.org/sdr/GAIA02019OP.md): Indicator · stuck · Feb 23, 2002 · N252US · Boeing 727251 · Trailing Flap Position Indicating System
  > FLT 1801 - FWA-MCO - ON APPROACH TO MCO, THE OUTBOARD FLAPS ASYMMENTRIED LESS THAN 2 DEGREES. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED AT MCO WITHOUT FURTHER DIFFICULTIES. FOUND THE OUTBOARD FLAP POSITION INDICATOR STICKING. REMOVED AND REPLAC
- [SDR GAIA01311OP](https://openairdocs.org/sdr/GAIA01311OP.md): Light · disconnected · Oct 3, 2001 · N252US · Boeing 727251 · Emergency Lighting
  > FLT 1713 - HSV-FWA - DURING CRUISE, THE COCKPIT EMERGENCY EXIT LIGHT BECAME DISCONNECTED FROM IT FIXED MOUNT. THE AIRCRAFT CONTINUED ITS FLIGHT TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REINSTALLED THE COCKPIT EMERGENCY EXIT LIGHT. IT WAS FOUND TO
- [SDR GAIA01299OP](https://openairdocs.org/sdr/GAIA01299OP.md): Control Handle · stiff · Aug 21, 2001 · N252US · Boeing 727251 · Landing Gear Selector
  > FLT 2019 - PHX-MHR - ON TAKEOFF, THE GEAR RETRACTED NORMAL, THE GEAR HANDLE WAS ABOUT TWO INCHES SHORT OF BEING IN THE FULL UP POSITION. RETURNED THE GEAR HANDLE TO OFF POSITION AND WAS DIFFICULT TO MOVE. RECYCLED THE HANDLE TO UP AND THE HANDLE MOVED ALL THE
- [SDR GAIA01187ST](https://openairdocs.org/sdr/GAIA01187ST.md): Seat Track · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT SEAT TRACK BS 720C LBL 45.50 HAS ELONGATED LOCK HOLES. ACCOMPLISHED SEAT TRACK REPAIR BS 690-740 LBL 45.50 IAW B727 SRM 53-10-5 FIG 1. (M)
- [SDR GAIA01188ST](https://openairdocs.org/sdr/GAIA01188ST.md): Frame · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 360 FRAME INBOARD FLANGE CHORD CRACKED IN THE RADIUS AT STRINGER 9L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 360 STRINGER 9L IAW B727 SRM 53-10-4 FIG 2. (M)
- [SDR GAIA01189ST](https://openairdocs.org/sdr/GAIA01189ST.md): Web · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 178 B/H WEB IS CRACKED AT FASTENER LOCATION WL 198 RBL 3 AND WL 201 STIFFENERS ARE CRACKED AT RBL 8. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 198 RBL 3 IAW B727 SRM 53-10-9 FIG 4 AND RE
- [SDR GAIA01190ST](https://openairdocs.org/sdr/GAIA01190ST.md): Seat Track · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 700 RBL 45.50 SEAT TRACK HAS ELONGATED LOCK HOLES. ACCOMPLISHED BS 690-740 RBL 45.50 SEAT TRACK REPAIR IAW B727 SRM 53-10-5 FIG 1. (M)
- [SDR GAIA01191ST](https://openairdocs.org/sdr/GAIA01191ST.md): Stiffener · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT HORIZONTAL STIFFENER EXFOLIATED ON TOP OF NOSE WHEEL WELL BS 302 RBL 12-LBL 12 WL 181. ACCOMPLISHED HORIZONTAL STIFFENER REPLACEMENT BS 302 WL 181 LBL 12 - RBL 12 IAW B727 SRM 53-10-2 FIG 2 AND 51-
- [SDR GAIA01192ST](https://openairdocs.org/sdr/GAIA01192ST.md): Frame · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON LEFT 1070 FRAME INBOARD CHORD AT STRINGER 10L. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1070 STRINGER 10L IAW B727 SRM 53-10-4 FIG 2. (M)
- [SDR GAIA01193ST](https://openairdocs.org/sdr/GAIA01193ST.md): Web · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT VENTRAL STAIRS TORQUE BOX AT BS 1323 AFT LIGHTING HOLE HAS A CRACK ON LOWER HOLE EDGE. ACCOMPLISHED AFT AIRSTAIR LEFT LOWER TORQUE BOX WEB REPAIR BS 1323 IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA01194ST](https://openairdocs.org/sdr/GAIA01194ST.md): Web · chafed · Jun 11, 2001 · N252US · Boeing 727251 · Empennage Structure
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TOP TRAILING EDGE OF LOWER RUDDER HAS METAL CHAFED THROUGH TOP. ACCOMPLISHED LOWER RUDDER CLOSE OUT WEB REPAIR IAW B727 SRM 55-30-1 AND 51-30-2. (M)
- [SDR GAIA01195ST](https://openairdocs.org/sdr/GAIA01195ST.md): Skin · deformed · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT DEFORMED FUSELAGE SKIN BS 215-227 STRINGER 25-26R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 215-227 STRINGER 25-26R IAW B727 SRM 53-30-3 FIG 3A. (M)
- [SDR GAIA01196ST](https://openairdocs.org/sdr/GAIA01196ST.md): Frame · dented · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT BS 1166 FRAME DENTED AT WL 212. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1166 LEFT WL 212 IAW B727 SRM 53-10-4 FIG 2. (M)
- [SDR GAIA01197ST](https://openairdocs.org/sdr/GAIA01197ST.md): Frame · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT RIGHT BS 1166 FRAME FAIL/SAFE CHORD CRACKED AT STRINGER 9R. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1166 RIGHT STRINGER 9R IAW B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA01198ST](https://openairdocs.org/sdr/GAIA01198ST.md): Frame · dented · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT LEFT BS 1166 FRAME DENTED AT WL 212. ACCOMPLISHED FUSELAGE FRAME REPAIR BS 1166 LEFT WL 212 IAW B727 SRM 53-10-4 FIG 2. (M)
- [SDR GAIA01199ST](https://openairdocs.org/sdr/GAIA01199ST.md): Web · dented · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT SHEAR WEB DENTED AT BS 1153 LBL 25 WL 208. ACCOMPLISHED SHEAR WEB REPAIR BS 1153 LBL 25 WL 208 IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA01200ST](https://openairdocs.org/sdr/GAIA01200ST.md): Skin · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Passenger/Crew Doors
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT L1 DOOR SKIN CRACKED AT LOWER HINGE CUT OUT. ACCOMPLISHED L1 DOOR EXTERNAL SKIN REPAIR IAW B727 SRM 52-03-00 FIG 3. (M)
- [SDR GAIA01201ST](https://openairdocs.org/sdr/GAIA01201ST.md): Stiffener · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT BS 1183 AFT BULKHEAD UPPER RIGHT SIDE STIFFENER IS CORRODED. ACCOMPLISHED 1183 BULKHEAD STIFFENER REPAIR IAW B727 SRM 51-40-4. (M)
- [SDR GAIA01202ST](https://openairdocs.org/sdr/GAIA01202ST.md): Stringer · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT CORROSION ON SKIN LAP BS 440 STRINGER 26L. ACCOMPLISHED STRINGER REPAIR BS 440 STRINGER 26L IAW B727 SRM 53-10-3 FIG 1. (M)
- [SDR GAIA01203ST](https://openairdocs.org/sdr/GAIA01203ST.md): Skin · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Electrical/Electronic Compartment Doors
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT CORROSION ON THE MAIN ELECTRONIC COMPARTMENT DOOR SKIN BS 420-440 STRINGER 28L-28R. ACCOMPLISHED E/E DOOR EXTERNAL SKIN REPLACEMENT IAW B727 SRM 52-40-1 FIG 2 AND 51-30-2. (M)
- [SDR GAIA01204ST](https://openairdocs.org/sdr/GAIA01204ST.md): Bulkhead · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TWO CRACKS IN BS 178 B/H WEB AT FASTENER LOCATIONS WL 235 LBL 10-12. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 235 LBL 10-12 IAW B727 SRM 53-10-9 FIG 4. (M)
- [SDR GAIA01205ST](https://openairdocs.org/sdr/GAIA01205ST.md): Bulkhead · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TWO CRACKS IN BS 178 B/H WEB AT FASTENER LOCATIONS WL 235 RBL 10-12. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 235 RBL 10-12 IAW B727 SRM 53-10-9 FIG 4. (M)
- [SDR GAIA01206ST](https://openairdocs.org/sdr/GAIA01206ST.md): Skin · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A CRACK IN FUSELAGE SKIN BS 300 STRINGER 17R AT FASTENER VERIFIED BY HFEC. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 300 STRINGER 17R IAW B727 SRM 53-30-3 FIG 3. (M)
- [SDR GAIA01207ST](https://openairdocs.org/sdr/GAIA01207ST.md): Pressure Panel · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A CRACK IN THE UPPER SKIN IN THE NOSE WHEEL WELL BS 287-292 BBL 0 WL 200. ACCOMPLISHED NOSE WHEEL WELL UPPER SKIN REPAIR BS 287-292 BBL 0 WL 200 IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA01208ST](https://openairdocs.org/sdr/GAIA01208ST.md): Skin · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Elevator, Plate/Skin
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE LEFT ELEVATOR INBOARD TRAILING EDGE STATIC DISCHARGER CORROSION BETWEEN BASE AND ELEVATOR SKIN. ACCOMPLISHED LEFT ELEVATOR UPPER SKIN REPAIR ELEVATOR STATION 209.96 IAW B727 SRM 55-20-3 FIG 3. (M)
- [SDR GAIA01209ST](https://openairdocs.org/sdr/GAIA01209ST.md): Skin · bulged · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT BULGING SKIN ALONG LAP SEAM BS 1130-1148 STRINGER 3-4L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1130-1148 STRINGER 3-4L IAW B727 SRM 53-30-3 FIG 1. (M)
- [SDR GAIA01210ST](https://openairdocs.org/sdr/GAIA01210ST.md): Skin · gouged · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT A GOUGE ON FUSELAGE SKIN BS 630 STRINGER 15-16R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 630 STRINGER 15-16R IAW B727 SRM 53-30-3 FIG 3. (M)
- [SDR GAIA01211ST](https://openairdocs.org/sdr/GAIA01211ST.md): Stiffener · corroded · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT HORIZONTAL STIFFENER AT BS 309 LBL 12 - RBL 12 WL 181 ON TOP OF NOSE WHEEL WELL IS EXFOLIATED. ACCOMPLISHED HORIZONTAL STIFFENER REPLACEMENT BS 309 LBL 12 TO RBL 12 WL 181 IAW B727 SRM 53-10-2 FIG
- [SDR GAIA01212ST](https://openairdocs.org/sdr/GAIA01212ST.md): Stringer · cracked · Jun 11, 2001 · N252US · Boeing 727251 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT STRINGER 15L IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR BS 720B PLUS 15 STRINGER 15L IAW B727 SRM 53-10-3 FIG 5. (M)

Next page: https://openairdocs.org/deregistered/N252US-2011-09-22/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 = 'N252US' AND deregistration_id = 'N252US-2011-09-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N252US-2011-09-22/reports

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