# Service difficulty reports: N264US, cancelled Oct 7, 2008

A list on [N264US, cancelled Oct 7, 2008](https://openairdocs.org/deregistered/N264US-2008-10-07.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 · 54 reports

- [SDR GAIA00646](https://openairdocs.org/sdr/GAIA00646.md): Clip · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, FOUND VARIOUS STRINGER CLIPS CRACKED AT BS 580 THROUGH 720E. CORRECTIVE ACTION: ACCOMPLISHED STRINGER CLIP REPLACEMENTS IAW B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00645](https://openairdocs.org/sdr/GAIA00645.md): Skin · damaged · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY:DURING A ROUTINE MAINTENANCE CHECK, REPLACE TEMPORARY REPAIR AT BS 430, IN BETWEEN S23L AND S24L WITH PERMANENT REPAIR.CORRECTIVE ACTION: ACCOMPLISHED FUSELAGE SKIN REPAIR AT BS 430, S23L AND S24L IAW B727 SRM 53-30-3, FIGURE 3. THE A/C WAS RETURNE
- [SDR GAIA00644](https://openairdocs.org/sdr/GAIA00644.md): Floorbeam · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Floor Beam
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A FLOORBEAM WEB WAS DISCOVERED TO BE CRACKED AT BS 294.5, LBL 36. CORRECTIVE ACTION: ACCOMPLISHED BS 294.5, LBL 36, FLOOR BEAM WEB REPAIR IAW BOEING S/B 727-53-0112. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00643](https://openairdocs.org/sdr/GAIA00643.md): Angle · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY:DURING A ROUTINE MAINTENANCE CHECK, BS1342 CHORD VERTICAL ATTACH ANGLE CRACKED HORIZONTALLY THROUGH RADIUS AT WL 265, LBL 15. CORRECTIVE ACTION: ACCOMPLISHED BS1342 CHORD VERTICAL ATTACH ANGLE WELDING REPAIR IAW AVITAS ENGINEERING REPAIR ORDER FA
- [SDR GAIA00642](https://openairdocs.org/sdr/GAIA00642.md): Skin · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK AT, FUSELAGE SKIN WAS DISCOVERED TO HAVE A CRACK AT FASTENERS AT BS 1342, WL265, LBL 55. CORRECTIVE ACTION: ACCOMPLISHED FUSELAGE SKIN REPAIR AT BS1342, LBL 55, AT WL265 IAW B727 SRM 51-10-1 AND 51-30-2. THE AIRCR
- [SDR GAIA00641](https://openairdocs.org/sdr/GAIA00641.md): Skin · worn · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, FUSELAGE SKIN WAS DISCOVERED LOOSE FASTENERS AND SOME FASTENERS HAD PULLED THROUGH, AT BS 1214, BL O TO LBL 4.5 CORRECTIVE ACTION: ACCOMPLISHED FUSELAGE SKIN REPAIR AT BA 1214, BL O TO LBL 17, AT WL 170 IAW B727
- [SDR GAIA00640](https://openairdocs.org/sdr/GAIA00640.md): Skin · corroded · Oct 6, 2000 · N264US · Boeing 727251 · Cargo/Baggage Doors
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, BULGING SKIN WAS DISCOVERED NR 3 CARGO DOOR AREA. CORRECTIVE ACTION: REMOVED AND REPLACED NR 3 CARGO DOOR SKIN IAW B727 SRM 52-30-01, FIGURE 6. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00639](https://openairdocs.org/sdr/GAIA00639.md): Skin · corroded · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, BULGING SKIN WAS DISCOVERED ON SKIN LAP BS 320 TO 330, STRINGER S19L. CORRECTIVE ACTION: ACCOMPLISHED FUSELAGE SKIN REPAIR AT BS 320 TO 330. S19L IAW B727 SRM 53-30-3, FIGURE 5 AND AVITAS ENGINEERING ORDER FAS
- [SDR GAIA00638](https://openairdocs.org/sdr/GAIA00638.md): Beam · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED ON VERTICAL BEAM AT BS 1183. CORRECTIVE ACTION: ACCOMPLISHED BS1183 VERTICAL BEAM REPAIR, RBL 26.8 AND INSTALLED KIT IAW BOEING DRAWING 65C33556. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00637](https://openairdocs.org/sdr/GAIA00637.md): Skin · gouged · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, A GOUGE WAS DISCOVERED AT THE AFT CARGO DOOR FRAME, BS 990. CORRECTIVE ACTION: ACCOMPLISHED TWO EACH BLEND OUTS AT BS990, AFT CUT OUT SHIN IAW AVITAS ENGINEERING REPAIR ORDER FASI_001RO-2, ISSUED 8110-3 OCTOBER 2
- [SDR GAIA00636](https://openairdocs.org/sdr/GAIA00636.md): Pressure Panel · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED ON A DOUBLER IN THE VERTICAL WEB OF THE NOSE WHEEL WELL AT DOUBLER AT BS 232, LBL 23.5, WL180. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL WELL VERTICAL WEB REPAIR BS232, RBL 23.5, WL 180 IA
- [SDR GAIA00635](https://openairdocs.org/sdr/GAIA00635.md): Pressure Panel · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED IN THE VERTICAL WEB OF THE NOSE WHEEL WEB AT DOUBLER AT BS 246, LBL 23.5, WL 170. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL WELL VERTICAL WEB REPAIR BS 246, RBL 23.5, WL 170 IAW B727 SRM
- [SDR GAIA00634](https://openairdocs.org/sdr/GAIA00634.md): Pressure Panel · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK AT, A CRACK WAS DISCOVERED IN THE VERTICAL WEB OF THE NOSE WHEEL WELL AT BS253, RBL 23.5, WL185. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL VERTICAL WEB REPAIR BS253, RBL 23.5, WL 185 IAW B727 SRM 53-10-9. THE A
- [SDR GAIA00633](https://openairdocs.org/sdr/GAIA00633.md): Bulkhead · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED AROUND A RIVET ONE FOOT BELOW RADAR DISH MOUNT, BS178. CORRECTIVE ACTION: ACCOMPLISHED BS 178 WEB REPAIR IAW B727 S/B 727-53-098. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00632](https://openairdocs.org/sdr/GAIA00632.md): Angle · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED EMANATING FROM FASTENER AT THE AFT LEFT HAND EMERGENCY ESCAPE HATCH., BS840, STRINGER 17L. CORRECTIVE ACTION: ACCOMPLISHED BS178 BS840 FRAME ATTACH ANGLE REPAIR AT S17L, IAW B727 SRM 53-1
- [SDR GAIA00631](https://openairdocs.org/sdr/GAIA00631.md): Stiffener · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED AT THE END OF STIFFENER ONE FOOT BELOW RADAR MOUNT AT BS 178. CORRECTIVE ACTION: ACCOMPLISHED BS178 LOWER HORIZONTAL STIFFENER REPAIR IAW B727 SRM 53-10-2, FIGURE 1. THE AIRCRAFT WAS RETU
- [SDR GAIA00630](https://openairdocs.org/sdr/GAIA00630.md): Bulkhead · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Bulkhead
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED AT THE PRESSURE BULKHEAD AFT OF 940 BEAM AT RBL 50. CORRECTIVE ACTION: ACCOMPLISHED BS940 PRESSURE BULKHEAD REPAIR IAW BOEING DRAWING 65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00629](https://openairdocs.org/sdr/GAIA00629.md): Stiffener · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, A CRACK WAS DISCOVERED AT THE END OF STIFFENER ONE FOOT BELOW MOUNT FOR RADAR DISH AT BS178.CORRECTIVE ACTION: ACCOMPLISHED BS178 UPPER HORIZONTAL STIFFENER REPAIR IAW B727
- [SDR GAIA00628](https://openairdocs.org/sdr/GAIA00628.md): Stiffener · corroded · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, INNER GRANULAR CORROSION WAS DISCOVERED ON LOWER RIGHT STIFFENER ON BULKHEAD WEB FOR NOSE RADOME, BS 178. CORRECTIVE ACTION: ACCOMPLISHED BS178 LOWER RIGHT STIFFENER REPLA
- [SDR GAIA00627](https://openairdocs.org/sdr/GAIA00627.md): Plate · cracked · Oct 6, 2000 · N264US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, A CRACK WAS DISCOVERED AT FASTENERS AT NOSE WHEEL WELL UPPER DECK. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL WELL UPPER DECK REPAIR IAW B727 SRM 51-40-2, FIGURE 1. THE AI
- [SDR GAIA00383](https://openairdocs.org/sdr/GAIA00383.md): Battery Pack · inoperative · Jul 3, 2000 · N264US · Boeing 727251 · Emergency Lighting
  > FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE, FOUND DURING PREFLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM OPS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00280](https://openairdocs.org/sdr/GAIA00280.md): Warning Light · illuminated · May 22, 2000 · N264US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 2031 - MHR-IND - AFTER TAKEOFF, THE GEAR WAS RETRACTED NORMALLY, AND ALL LIGHTS EXTINGUISHED WITH THE GEAR IN THE UP POSITION. PLACED THE GEAR HANDLE TO THE OFF POSITION AND THE RED DOORS LIGHT ILLUMINATED. RECYCLED THE HANDLE TO THE UP POSITION AND RECY
- [SDR GAIA00118](https://openairdocs.org/sdr/GAIA00118.md): Frame · cracked · Mar 27, 2000 · N264US · Boeing 727251 · Fuselage Main, Frame
  > DURING ROUTINE MAINTENANCE AT DFW, FOUND BS 520 FRAME CRACKED JUST ABOVE THE FLOOR LINE. REPAIRED IAW FRAME IAW BOEING SRM 53-40-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00119](https://openairdocs.org/sdr/GAIA00119.md): Frame · cracked · Mar 27, 2000 · N264US · Boeing 727251 · Fuselage Main, Frame
  > DURING ROUTINE MAINTENANCE AT DFW, FOUND BS 540 FRAME CRACKED JUST ABOVE THE FLOOR LINE. REPAIRED FRAME IAW BOEING SRM 53-10-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00120](https://openairdocs.org/sdr/GAIA00120.md): Frame · cracked · Mar 27, 2000 · N264US · Boeing 727251 · Fuselage Main, Frame
  > DURING ROUTINE MAINTENANCE AT DFW, FOUND BS 580 FRAME CRACKED JUST ABOVE THE FLOOR LINE. REPAIRED FRAME IAW BOEING SRM 53-10-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00121](https://openairdocs.org/sdr/GAIA00121.md): Frame · cracked · Mar 27, 2000 · N264US · Boeing 727251 · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION AT DFW, FOUND BS 600 FRAME CRACKED JUST ABOVE THE FLOOR LINE. REPAIRED FRAME IAW BOEING SRM 53-10-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00122](https://openairdocs.org/sdr/GAIA00122.md): Frame · cracked · Mar 27, 2000 · N264US · Boeing 727251 · Fuselage Main, Frame
  > DURING ROUTINE MAINTENANCE AT DFW, FOUND BS 1160 FRAME DAMAGED JUST ABOVE THE FLOORLINE. REPAIRED FRAME IAW BOEING SRM 53-40-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA0091](https://openairdocs.org/sdr/GAIA0091.md): Switch · loose · Feb 21, 2000 · N264US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 1849 - FWA-SEA - AFTER TAKEOFF FLIGHT, THE DOOR WARNING LIGHT ON BOTH THE FORWARD PANEL AND FE ANNUNCIATOR PANEL ILLUMINATED. SLOWED AIRCRAFT TO 230 KNOTS, CYCLED GEAR AND WHICH RESULTED IN THE SAME INDICATIONS. THE AIRCRAFT CONTINUED ON TO SEA AND LANDE
- [SDR GAIA0089](https://openairdocs.org/sdr/GAIA0089.md): Apu · inoperative · Jan 2, 2000 · N264US · Boeing 727251 · Fire Detection
  > DURING CRUISE FROM MCI TO ELP, FLIGHT 1712, ENCOUNTERED AN APU FIRE WARNING LIGHT AND FIRE WARNING BELL. ALL EMERGENCY CHECKLISTS WERE COMPLIED WITH, ALONG WITH PULLING OF THE APU TIRE HANDLE AND DISCHARGING THE APU FIRE BOTTLE. SLOWED THE AIRCRAFT TO 270 KN
- [SDR GAIA99132](https://openairdocs.org/sdr/GAIA99132.md): Batteries · discharged · Sep 7, 1999 · N264US · Boeing 727251 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE INTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE FORWARD ENTRANCE DOOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (
- [SDR GAIA9893](https://openairdocs.org/sdr/GAIA9893.md): Sensor · out of adjust · Oct 22, 1998 · N264US · Boeing 727251 · Landing Gear Position and Warning
  > TOL - ON TAKEOFF, RETRACTED LANDING GEAR. ONCE GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR LIGHT REMAINED ILLUMINATED. RECYCLED GEAR. RIGHT MAIN GEAR LIGHT REMAINED ON. ALL INDICATIONS ON FE PANEL OK. LIGHT EXTINGUISHED AT 17,000 FT. ALL INDICATIONS OK.
- [SDR GAIA9881](https://openairdocs.org/sdr/GAIA9881.md): Link · loose · Aug 11, 1998 · N264US · Boeing 727251 · Landing Gear Retraction/Extension System
  > EN ROUTE FROM OKC TO ICT, DURING CLIMB-OUT, THE NOSE LANDING GEAR WOULD NOT RETRCT. CYCLED GEAR WITHOUT SUCCESS. CONTINUED EN ROUTE TO ICT AND LANDED WITHOUT DIFFICULTIES. INSPECTED NOSE LANDING GEAR AND FOUND THE DOWN LOCK ACTUATOR LINK DISCONNECTED. INST
- [SDR GAIA9840](https://openairdocs.org/sdr/GAIA9840.md): Stringer · corroded · Apr 22, 1998 · N264US · Boeing 727251 · Fuselage Main, Longeron/Stringer
  > DURNG A ZERO LIGHT 'C' INSPECTION, FOUND STRINGER 27L AT THE TIE END HAD CORROSION AT STATION 740. REMOVED TIE END, CLEANED CORROSION AND FOUND TO BE WITHIN LIMITS. REMOVED AND REPLACED 30 INCHES OF STRINGER IAW SRM 53-10-3 AT 27L, STATION 740. (M)
- [SDR GAIA9825](https://openairdocs.org/sdr/GAIA9825.md): Linkage · out of adjust · Feb 27, 1998 · N264US · Boeing 727251 · Landing Gear Door Retract Section
  > TOL - AFTER DEPARTING, FLIGHT CREW IDENTIFIED THE 'NOSE GEAR DOOR LIGHT ON' AFTER GEAR RETRACTION. AIRCRAFT MADE AN UNEVENTFUL RETURN TO TOL. ADJUSTED AND TESTED NOSE GEAR DOOR LINKAGE IAW B-727 MM 32-22-01. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR GAIA9724](https://openairdocs.org/sdr/GAIA9724.md): Frame · cracked · Mar 14, 1997 · N264US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING C-CHECK INSPECTION, FOUND RIGHT BODY STATION FRAME AT WL 208 CRACKED. FRAME REPAIRED ON AERO CORP EO 97-444. (M)
- [SDR GAIA9723](https://openairdocs.org/sdr/GAIA9723.md): Flap Track · corroded · Jan 29, 1997 · N264US · Boeing 727251 · Trailing Edge Flaps
  > DURING C-CHECK INSPECTION, FOUND NR 5 FLAP TRACK INBOARD ATTACH HOLE CORRODED. FLAP TRACK REPAIRED ON AERO CORP EO 97-448. (M)
- [SDR GAIA9725](https://openairdocs.org/sdr/GAIA9725.md): Floorbeam · corroded · Jan 1, 1997 · N264US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING C-CHECK INSPECTION, FOUND FLOORBEAM WEB AT STATION 1110 CORRODED. FLOORBEAM REPAIRED ON AERO CORP EO 96-413. (M)
- [SDR IXKA9600081](https://openairdocs.org/sdr/IXKA9600081.md): Indicator · inoperative · Sep 22, 1996 · N264US · Boeing 727251 · Trailing Flap Position Indicating System
  > FLT 78 - MDW-ATL - AFTER TAKEOFF UPON FLAP RETRACTION, INBOARD FLAPS WOULD NOT INDICATE LESS THAN 5 DEGREES. AIR TURN BACK TO MDW. REMOVED AND REPLACED FLAP POSITION INBOARD INDICATOR. OPS CHECK OK AS PER 27-52-00. (M)
- [SDR IXKA9600080](https://openairdocs.org/sdr/IXKA9600080.md): Connector · damaged · Sep 21, 1996 · N264US · Boeing 727251 · Trailing Edge Flap Control System
  > ATL - FLT 84 - AFTER TAKEOFF, ATL-TPA, RETURNED TO ATL WHEN INBOARD TRAILING EDGE FLAPS DID NOT RETRACT. STOPPED AT 5 DEGREES. ALL LE DEVICES RETRACTED. CHECKED AND FOUND RIGHT INBOARD FLAP TRANSMITTER, P/N 9660022001, ELECTRICAL CONNECTOR DAMAGED. REPLACE
- [SDR IXKA9600073](https://openairdocs.org/sdr/IXKA9600073.md): Control Vlv · out of adjust · Aug 30, 1996 · N264US · Boeing 727251 · Leading Edge Slat Control System
  > FLT 25 - EWR-ATL - AFTER TAKEOFF, NR 2, 3, 6 AND 7 LE DEVICES WOULD NOT RETRACT WHEN FLAP SELECTED UP. RETURNED AND LANDED AT EWR. RERIGGED LEADING EDGE SLAT CONTROL VALVE PER MM 27-81-81, OPS CHECK OK. (M)
- [SDR IXKA9600063](https://openairdocs.org/sdr/IXKA9600063.md): Seal · leaking · Jul 28, 1996 · N264US · Boeing 727251 · Nose/Tail Landing Gear Strut/Axle
  > FLT 32 - MDW - AIR TURN BACK - UNABLE TO GET NOSE DOOR LIGHT TO GO OUT ON RETRACTION. BOTH RED LIGHT AND AMBER LIGHTS ON. FOUND NOSE GEAR METERING PIN ORIFICE SEALS BAD, STRUT FLAT, TIRES HANGING UP ON DOORS. REMOVED AND REPLACED SEALS IAW 32-21-01 SWUNG NO
- [SDR 96ZZZM1269](https://openairdocs.org/sdr/96ZZZM1269.md): Seal · leaking · Jul 28, 1996 · N264US · Boeing 727251 · Nose/Tail Landing Gear Strut/Axle
  > FLT 32 - MDW - AIR TURN BACK - UNABLE TO GET NOSE DOOR LIGHT TO GO OUT ON RETRACTION. BOTH RED LIGHT AND AMBER LIGHT ON. FOUND NOSE GEAR METERING PIN ORIFICE SEALS BAD, STRUT FLAT, TIRES HANGING UP ON DOORS. REMOVED AND REPLACED SEALS IAW 32-21-01 SWUNG NOS
- [SDR IXKA9600039](https://openairdocs.org/sdr/IXKA9600039.md): Fuel Pump · failed · Jun 17, 1996 · N264US · Boeing 727251 · Engine Fuel Pump
  > FLT 81 - TPA-ATL - AFTER GEAR RETRACTION, NR 1 ENGINE SHUT DOWN. RETURNED TO TPA. FOUND FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL AS PER MM 73-11-01 PG 401-408 AND MM 73-21-2, PAGE 401-405. INSPECTED, RAN ENGINE AND OPS CHECK
- [SDR IXKA9600008](https://openairdocs.org/sdr/IXKA9600008.md): Switch · out of adjust · Feb 29, 1996 · N264US · Boeing 727251 · Door Warning System
  > EWR/ATL - FLT 25 - AT EWR, AFT CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED CARGO DOOR SWITCH PER MM 52-70-01. OPS CHECK OK. (X)
- [SDR IXKA950035](https://openairdocs.org/sdr/IXKA950035.md): Pack · malfunctioned · Dec 16, 1995 · N264US · Boeing 727251 · Cabin Cooling System
  > FLT 72 - AT 1.5 EPR, TAKEOFF ROLL AUTO PRESSURE GREEN LIGHT ILLUMINATED. APPROXIMATELY SEVERAL SECONDS LATER, BOTH PACKS TRIPPED OFF, TEMPS AND PRESSURE NORMAL. DID NOT RETARD THROTTLES UNTIL ABORT WAS INITATED. RAN AIRCRAFT AT HIGH POWER, SYSTEM CHECKS NOR
- [SDR IXKA9500025](https://openairdocs.org/sdr/IXKA9500025.md): Plug · damaged · Aug 29, 1995 · N264US · Boeing 727251 · Fire Detection
  > ON DESCENT INTO EWR, NR 2 ENGINE FIRE HANDLE INDICATED A FIRE WARNING. BOTH BOTTLE DISCHARGED, LIGHT REMAINED ON. LANDED AT EWR WITHOUT INCIDENT. FOUND NR 2 ENGINE FIRE SENSE PLUG (D1490) MISSING INSULATION IN PLUG. SYSTEM CHECKED NORMAL AS PER MM 26-11-00
- [SDR IXKA9500024](https://openairdocs.org/sdr/IXKA9500024.md): Act Fitting · sheared · Aug 5, 1995 · N264US · Boeing 727251 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, FLT NR 58, ATL TO PBI, UNABLE TO RAISE NOSE LANDING GEAR. RETURNED TO ATLANTA. UPON INSPECTION OF NOSE WHEEL WELL, FOUND NOSE LANDING ACTUATOR FITTING SHEARED. REMOVED AND REPLACED NLG LOCK ACTUATOR FITTING AND REMOVED AND REPLACED NOSE GEAR
- [SDR IXKA9500023](https://openairdocs.org/sdr/IXKA9500023.md): Hydraulic Pump · failed · Jul 26, 1995 · N264US · Boeing 727251 · Hydraulic Pump (Electric/Engine), Main
  > TPA/ATL - FLT 59 - IN-FLIGHT, LOST A-HYDRAULIC FLUID. AIRCRAFT RETURNED TO TPA. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND FILTERS. OPS CHECK AND RAN NR 1 ENGINE, CHECK OK PER MM 29-11-33. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP AND
- [SDR IXKA9500019](https://openairdocs.org/sdr/IXKA9500019.md): Wire · broken · Jun 12, 1995 · N264US · Boeing 727251 · Air Conditioning System Wiring
  > EWR/TPA - FLT 39, AFTER TAKEOFF, UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO EWR. FOUND LT FLOW CONTROL VALVE FAILED IN CLOSED POSITION DUE TO 3 BROKEN WIRES. REPAIRED WIRES AND C/P REPINNED. PRESSURE CHECKED PER MM 21-00-01 AND MM 21-31-00. OPS C
- [SDR IXKA9500017](https://openairdocs.org/sdr/IXKA9500017.md): Wire · broken · Apr 28, 1995 · N264US · Boeing 727251 · AC Generation System
  > MCO - FLT NR 74, AFTER TAKEOFF, NR 1 GEN UNDEREXCITED, ISOLATED GEN LEFT FWD BOOST PUMP CIRCUIT BREAKER POP IN NR 2 TANK, RESET, FORWARD RT BOOST PUMP CIRCUIT BREAKER POPPED, LEFT NR 2 CIRCUIT BREAKER POPPED AGAIN, NR 1 CIRCUIT BREAKER LEFT TANK BOOST PUMP POP

Next page: https://openairdocs.org/deregistered/N264US-2008-10-07/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 = 'N264US' AND deregistration_id = 'N264US-2008-10-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N264US-2008-10-07/reports

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