# Service difficulty reports: N468FE, cancelled Dec 18, 2013

A list on [N468FE, cancelled Dec 18, 2013](https://openairdocs.org/deregistered/N468FE-2013-12-18.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 · 106 reports

- [SDR FDEA201207112551](https://openairdocs.org/sdr/FDEA201207112551.md): Smoke Detector · faulted · Jul 11, 2012 · N468FE · Boeing 727225 · Smoke Detection
  > LOWER AFT CARGO COMPARTMENT SMOKE DETECTOR FAULTS ON THE "B" LOOP. RELEASED FOR SERVICE IAW MEL: 26-19-D, CATEGORY: C EXPIRATION: 21JUL12 "MEL 26-19-D: B LOOP IN THE AFT LOWER CARGO COMPARTMENT - INOP." BITE TEST OF THE AFT CEU FAULTS DETECTOR - "1B". R &
- [SDR FDEA201112055151](https://openairdocs.org/sdr/FDEA201112055151.md): Sense Line · dirty · Dec 5, 2011 · N468FE · Boeing 727225 · Engine Pressure Ratio (EPR)
  > REJECTED TAKE OFF DUE LOW NR 2 EPR INDICATION. REJECTED TAKE OFF AT 80 KTS AND APPLIED BRAKES AT 60KTS, NO BRAKE COOLING REQUIRED. ON SUBSEQUENT TAKE OFF NORMAL EPR WAS OBTAINED, BUT IT REQUIRED ALMOST FULL THROTTLE THROW ON NR 2 (LARGE SPLIT). OPENED NR 2
- [SDR FDEA201109103817](https://openairdocs.org/sdr/FDEA201109103817.md): Engine · overtemp · Sep 10, 2011 · N468FE · Boeing 727225 · Engine (Turbine/Turboprop)
  > NR 3 ENGINE OVERTEMP. R & R NR 3 ENGINE IAW WORKCARD 70T0001-03,70T003-03 AND 70T0301-03, OPS CHECKED GOOD.
- [SDR FDEA201109103816](https://openairdocs.org/sdr/FDEA201109103816.md): Engine · overtemp · Sep 10, 2011 · N468FE · Boeing 727225 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE OVERTEMP. R & R NR 2 ENGINE IAW WORKCARD 70T0002, 70T0301-02, AND 70T0003-02, OPS CHECKED GOOD.
- [SDR FDEA201108193384](https://openairdocs.org/sdr/FDEA201108193384.md): Engine · damaged · Aug 19, 2011 · N468FE · Boeing 72725F · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, RECEIVED A RED WINDSHEAR WARNING LIGHT PERFORMED WINDSHEAR ESCAPE MANUVER W/FIREWALL POWER, APPROX 1 MIN. INSPECTED ALL EXHAUST AREAS FOR DAMAGE DUE TO OVERTEMP CONDITION. NO DAMAGE FOUND. R & R ENGINE. OPS CHECKED GOOD.
- [SDR FDEA201104211591](https://openairdocs.org/sdr/FDEA201104211591.md): Skin · misrepaired · Apr 21, 2011 · N468FE · Boeing 727225 · Cargo/Baggage Doors
  > MCD EXTERNAL SKIN DOUBLER TO EXTERNAL SKIN STA 560 STR 10L. REMOVED REPAIR AT MCD EXTERNAL SKIN STA 560 STR 10L IAW SRM 51-30-2. FABRICATED DOUBLER AND FILLER, AND INSTALLED FILLER AND DOUBLER REPAIR PER EA 7-5230-136752.
- [SDR FDEA201104081410](https://openairdocs.org/sdr/FDEA201104081410.md): Stringer · corroded · Apr 8, 2011 · N468FE · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STA 1010, STR 27L CORROSION AROUND RIVET TAIL. REMOVED AND REPLACED PRODUCTION SPLICE STRINGER 27L STA 1010 IAW B727 SRM 51-30-2 REV 103
- [SDR FDEA201104051319](https://openairdocs.org/sdr/FDEA201104051319.md): Skin · damaged · Apr 5, 2011 · N468FE · Boeing 727225 · Cargo/Baggage Doors
  > C-1 DOOR FWD LOWER OUTER SKIN IS OIL CANNED AT BS 560 3" CUT OUT DAMAGED AREA OF SKIN ( DIM 2" X 1 13/16") IAW SRM 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 51-30-2 REV 103 AND EA
- [SDR FDEA201104051380](https://openairdocs.org/sdr/FDEA201104051380.md): Stringer · cracked · Apr 5, 2011 · N468FE · Boeing 727225 · Wing, Longeron/Stringer
  > RT WING STA 686.5 STR 9 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT RT WING STA 686.5 STR 9.
- [SDR FDEA201104041379](https://openairdocs.org/sdr/FDEA201104041379.md): Stringer · cracked · Apr 4, 2011 · N468FE · Boeing 727225 · Wing, Longeron/Stringer
  > LT WING, STA 686.5 STR 14 IS CRACKED. CUT ACCESS HOLE IN LT WING STR 14 VENT BOX, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 686.5 STR 14.
- [SDR FDEA201104041378](https://openairdocs.org/sdr/FDEA201104041378.md): Stringer · cracked · Apr 4, 2011 · N468FE · Boeing 727225 · Wing, Longeron/Stringer
  > LT WING STA 629.0, STR 8 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 629.0 STR 8.
- [SDR FDEA201104011279](https://openairdocs.org/sdr/FDEA201104011279.md): Angle · chafed · Apr 1, 2011 · N468FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > HEADER BEAM, LOWER ANGLE STRAP CHAFED BS 640.
- [SDR FDEA201103301253](https://openairdocs.org/sdr/FDEA201103301253.md): Skin · gouged · Mar 30, 2011 · N468FE · Boeing 727225 · Trailing Edge Flaps
  > LEFT WING, INBD FLAP, FORE FLAP HAS AREA AT MOST OUTBD L/E GOUGED. REMOVED PREVIOUS REPAIR FROM LT INBD FOREFLAP IAW SRM REV 103, 51-30-2. FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 4 AND 57-50-2, FIG 3 INSTALLED DOUBLER IAW SRM 51-30-2 AND 57-50-4, FIG 4
- [SDR FDEA201103301254](https://openairdocs.org/sdr/FDEA201103301254.md): Frame · bent · Mar 30, 2011 · N468FE · Boeing 727225 · Fuselage Main, Frame
  > AFT CARGO STATION 1050 AT STRINGER 28R, FRAME BENT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3 FIG 1.
- [SDR FDEA201103301246](https://openairdocs.org/sdr/FDEA201103301246.md): Frame · damaged · Mar 30, 2011 · N468FE · Boeing 727225 · Fuselage Main, Frame
  > BS 783 FRAME HAS DOUBLE DRILLED HOLE AT FLANGE 3" ABOVE STRINGER 17R. REMOVED DAMAGED HOLE AND INSTALLED FASTENER IAW EO 7-5310-7-3367 PT 4 AND SRM 51-30-2.
- [SDR FDEA201103301247](https://openairdocs.org/sdr/FDEA201103301247.md): Skin · damaged · Mar 30, 2011 · N468FE · Boeing 727225 · Nacelle/Pylon, Plate/Skin
  > NR 3 ENGINE NOSE COWL O/B T/E SKIN DAMAGED AT 4:30 POAITION. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-30-2, 54-30-3 FIG 8.
- [SDR FDEA201103291468](https://openairdocs.org/sdr/FDEA201103291468.md): Beam · damaged · Mar 29, 2011 · N468FE · Boeing 727225 · Fuselage Main, Structure
  > BS 1183 BULKHEAD LBL 20 BEAM AND WEB HAVE CLOSE ON CENTER SPACING BETWEEN FASTENERS. ACCOMPLISHED EA 7-5310-123586.
- [SDR FDEA201103191080](https://openairdocs.org/sdr/FDEA201103191080.md): Actuator · malfunctioned · Mar 19, 2011 · N468FE · Boeing 727225 · Leading Edge Slat Control System
  > DURING CLIMBOUT NR 4 LT L/E SLAT DID NOT RETRACT. RAN QRH. RETURNED TO DEPARTURE. JUMPER INSTALLED ON NR 4 SLAT ACTUATOR. DO TO IND OF EXTEND POSITION. MM 27-82-000-1-0, INSTALLED NR 4 L/E SLAT EXTEND SWITCH JUMPER. SYS GROUND CHECKS NORMAL. JUMPER IN
- [SDR FDEA200811194925](https://openairdocs.org/sdr/FDEA200811194925.md): Actuator · failed · Nov 19, 2008 · N468FE · Boeing 727225 · Leading Edge Slat Actuator
  > NR 7 LEADING EDGE DEVICE FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG. RAN QRH LED DID NOT RETRACT FLIGHT CONTROL INPUTS INDICATE THE LEADING EDGE DEVICE WAS ACTUALLY EXTENDED. R & R NR 7 SLAT ACTUATOR IAW MM 27-81-032-4. OPS CK AND L
- [SDR 08FDEA04925](https://openairdocs.org/sdr/08FDEA04925.md): Actuator · failed · Nov 19, 2008 · N468FE · Boeing 727225 · Leading Edge Slat Actuator
  > NR 7 LED FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG, RAN QRH LED DID NOT RETRACT FLIGHT CONTROLS INPUTS INDICATE THE LED WAS ACTUALLY EXTENDED. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER M/M 27-81-032-4. OPS CKS AND LEAK CKS NML.
- [SDR 08FDEA04322](https://openairdocs.org/sdr/08FDEA04322.md): Seat Track · corroded · Oct 13, 2008 · N468FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 950 LBL 24. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED, DRILLED, AND DEBURRED SEAT TRACK IAW SRM 53-10-5 AND 51-30-5 AND 51-30-8. TREATED & PRIMED TRACK & REPAIR PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK & REPAI
- [SDR 08FDEA04321](https://openairdocs.org/sdr/08FDEA04321.md): Seat Track · corroded · Oct 13, 2008 · N468FE · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK STA. 950 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK AND 2 SPLICE ANGLES IAW SRM 53-10-5 FIG 1 AND 51-30-8. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED TRACK & REPAIR PARTS IAW SRM 53-10-5 & 51-30-5, AND
- [SDR 08FDEA04298](https://openairdocs.org/sdr/08FDEA04298.md): Skin · dented · Oct 10, 2008 · N468FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > SKIN DENTES AND HOLES BS 620 TO 635 S25R.
- [SDR 08FDEA04295](https://openairdocs.org/sdr/08FDEA04295.md): Seat Track · misaligned · Oct 9, 2008 · N468FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > STA 720F LBL 45 HAS HOLE FOR FLOORBOARD DRILLED ON EXISTING SEAT TRACK SPLICE ON A FASTENER. REMOVED SEAT TRACK AND SPLICE BS 720F - 750 LBL 45 IAW SRM 51-30-2. LOCATED, DRILLED, DEBURRED NEW SEAT TRACK SECTION IAW SRM 53-10-5. FABRICATED SPLICE ANGLE IAW SR
- [SDR 08FDEA02300](https://openairdocs.org/sdr/08FDEA02300.md): Cabin Pressure · malfunctioned · Jun 18, 2008 · N468FE · Boeing 727225 · Cabin Pressure Control System
  > FL270 AND.80 MACH, UPON COMP OF THROTTLE ALIGN CK AND RECYCLING OF NR 1 AND NR 2 ENG BLEED S CABIN PRESS BEGAN TO CLIMB AT 500-1000' FPM. COULD NOT STOP CLIMB AND APPROACHING 10K CAB PRESS WE WERE FORCED TO DESCEND TO 10K' AND DIVERT INTO DSM. IAW QRH ATTEM
- [SDR 08FDEA00427](https://openairdocs.org/sdr/08FDEA00427.md): Support · corroded · Feb 14, 2008 · N468FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > LOWER AFT CARGO PIT, LT SIDE EDGE SUPPORT FROM FS 950F TO FS 1030 HAS AREAS OF SURFACE CORROSION AS MARKED REMOVED CORROSION. ORIGINAL THICKNESS.056",.017 INCH REMAINING,.036 INCH MAT REMOVED. OUT OF LIMITS. REPAIR DOUBLER FABRICATED, TREATED AND PRIMED
- [SDR 06FDEA1687](https://openairdocs.org/sdr/06FDEA1687.md): Skin · chafed · May 3, 2006 · N468FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND RIGHT HAND LOWER FUSELAGE OUTER SKIN HAVE MULTIPLE CHAFED DAMAGE APPROX BETWEEN STA 1100 TO STA 1175, AREA BETWEEN STA 1100 TO STA 1110 AND STA 1175 FOUND OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 1 AND REINSTALLED ALL R
- [SDR 06FDEA1611](https://openairdocs.org/sdr/06FDEA1611.md): Skin · damaged · Apr 26, 2006 · N468FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND LOWER CARGO COMPARTMENT EXTERIOR SKIN SURFACE IS DAMAGED BETWEEN STA 1050 TO STA 1070, STR 25R. REMOVED DAMAGE PARTS IAW SRM 53-30-3, FABRICATED REPAIR PARTS IAW SRM 53-30-2 FIG 4 AND INSTALLED DOUBLER REPAIR PARTS IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3
- [SDR 06FDEA1610](https://openairdocs.org/sdr/06FDEA1610.md): Repair · unknown · Apr 26, 2006 · N468FE · Boeing 727200 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-30-3 FIG 5 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSH
- [SDR 06FDEA1567](https://openairdocs.org/sdr/06FDEA1567.md): Repair · misinstalled · Apr 22, 2006 · N468FE · Boeing 727200 · Standard Practices/Structures
  > FUSELAGE SKIN REPAIR AT FS 1140 & STR 19L DOES NOT COMPLY WITH SRM REPAIR. REMOVED AND REPLACED EXISTING REPAIR DOUBLERS IAW SRM 53-30-3 FIG 5.
- [SDR 06FDEA1530](https://openairdocs.org/sdr/06FDEA1530.md): Repair · unknown · Apr 19, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT STA 720E (WING ROOT) AND STR 19L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE MAJOR, AND WAS ACCOMPLISHED USING FAA APPROVED DATA.
- [SDR 06FDEA1529](https://openairdocs.org/sdr/06FDEA1529.md): Repair · unknown · Apr 19, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT 720D AND STR 25L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.
- [SDR 06FDEA1528](https://openairdocs.org/sdr/06FDEA1528.md): Repair · unknown · Apr 19, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND REPAIR LOCATED AT STN 1150 STR 21R REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CLASSIFIED AS MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.
- [SDR 06FDEA1443](https://openairdocs.org/sdr/06FDEA1443.md): Repair · unknown · Apr 13, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1090 STR 26L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA1441](https://openairdocs.org/sdr/06FDEA1441.md): Repair · unknown · Apr 13, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1100 STR 23R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS C
- [SDR 06FDEA1442](https://openairdocs.org/sdr/06FDEA1442.md): Repair · unknown · Apr 13, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. REPAIR IS CLASSIFED AS MAJOR PER
- [SDR 06FDEA1440](https://openairdocs.org/sdr/06FDEA1440.md): Repair · unknown · Apr 13, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS
- [SDR 06FDEA1439](https://openairdocs.org/sdr/06FDEA1439.md): Repair · unknown · Apr 13, 2006 · N468FE · Boeing 727225 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 415 STR 17R WAS ACCOMPLISHED IAW EO 7- 5313-7-2304 PT2 SECT A, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTING OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP,
- [SDR 06FDEA1398](https://openairdocs.org/sdr/06FDEA1398.md): Skin · dented · Apr 12, 2006 · N468FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FORWARD LEFT FUSELAGE HAS DENT OUTER SKIN APPROX STA 196 STR 25L.
- [SDR 03FDEA01747](https://openairdocs.org/sdr/03FDEA01747.md): Bolt · missing · Oct 15, 2003 · N468FE · Boeing 727200 · Trailing Edge Flaps
  > AFTER SEVERAL SUCCESSFUL FLAP RETRACTION CYCLES, OUTBOARD FLAPS STOPPED AT 5 DEG & STAYED THERE WHILE FLAPS 2 WERE COMMANDED, ALTERNATE FLAP SELECTION WAS UNABLE TO MOVE THEM FURTHER UP OR DOWN. USE OF NORMAL HYD MOTOR WAS ABLE TO DRIVE OUTBOARDS DOWN. BUT
- [SDR 03FDEA01706](https://openairdocs.org/sdr/03FDEA01706.md): Floorbeam · corroded · Oct 7, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01(3)) ON BS 1148 FLOORBEAM LOWER CHORD BL 0, WL 200. *S/D* CORROSION ON FLOORBEAM AT BS 1148 LOWER CHORD BL 0 WL 200 WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER FED EX EA 7-5310-55019.
- [SDR 03FDEA01707](https://openairdocs.org/sdr/03FDEA01707.md): Skin · gouged · Oct 7, 2003 · N468FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN GOUGE STRINGER 19R LAP BS 720D 14. REPAIRED RT FUSELAGE SKIN GOUGE PER SRM 53-30-3, AND SR DRAWING SR 27-57-056.
- [SDR 03FDEA01682](https://openairdocs.org/sdr/03FDEA01682.md): Vent · cracked · Oct 2, 2003 · N468FE · Boeing 727200 · Wing Miscellaneous Structure
  > LT WING FWD VENT BOX TAB CRACKED AT STA. 656.60. REPAIRED IAW EA 7-5710-55011.
- [SDR 03FDEA01683](https://openairdocs.org/sdr/03FDEA01683.md): Stringer · cracked · Oct 2, 2003 · N468FE · Boeing 727200 · Wing, Longeron/Stringer
  > N01203 LT WING STA 656.5, STRINGER 12 UPPER TAB CRACKED (VENT BOX) REPAIRED IAW EA 7-5710-55011.
- [SDR 03FDEA01684](https://openairdocs.org/sdr/03FDEA01684.md): Stringer · cracked · Oct 2, 2003 · N468FE · Boeing 727200 · Wing, Longeron/Stringer
  > LT WING STR 10 UPPER CRACKED AT TAB WING STA 656.50 ** SD ** COMING
- [SDR 03FDEA01668](https://openairdocs.org/sdr/03FDEA01668.md): Frame · cracked · Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Frame
  > RT 930 FRAME CRACKED AT LWR SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 RT, PER SRM 53-10-4, EA 7-5310-55032.
- [SDR 03FDEA01665](https://openairdocs.org/sdr/03FDEA01665.md): Frame · cracked · Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Frame
  > LT 930 FRAME CRACKED AT LOWER SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 LT, PER SRM 53-10-4, EA 7-5310-55032.
- [SDR 03FDEA01669](https://openairdocs.org/sdr/03FDEA01669.md): Frame · damaged · Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Frame
  > N01698, BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L, REPAIR AND FASTENERS NOT INSTALLED WITH SEALANT, MECHANICAL DAMAGE ON FAIL SAFE CHORD AT TOP HORZ FASTENER, LARGE GAP BETWEEN DOUBLER AND FRAME, 1 FASTENER TO SHORT WITH GAPPED COLLAR, 1 FASTENER WITH
- [SDR 03FDEA01666](https://openairdocs.org/sdr/03FDEA01666.md): Structure · gouged · Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Structure
  > NLG WHEEL WELL HAS NUMEROUS GOUGES AROUND RT AFT PRESSURE PANEL CUTOUT. REPAIRED AS PER SRM 51-40-2.
- [SDR 03FDEA01667](https://openairdocs.org/sdr/03FDEA01667.md): Floorbeam · corroded · Oct 1, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor Beam
  > N01643, CORROSION ON UPPER SURFACE OF LOWER SECTION OF FLOORBEAM BS 1070 LBL 7 WL 200. ** SD ** COMING

Next page: https://openairdocs.org/deregistered/N468FE-2013-12-18/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 = 'N468FE' AND deregistration_id = 'N468FE-2013-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N468FE-2013-12-18/reports

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