# Service difficulty reports: N154FE, cancelled Oct 15, 2002

A list on [N154FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N154FE-2002-10-15.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 00FDEA00363](https://openairdocs.org/sdr/00FDEA00363.md): Actuator · leaking · Jun 1, 2000 · N154FE · Boeing 72725 · Leading Edge Slat Actuator
  > LOST A SYS QUANTITY ON LAND GEAR RETRACTION, LOST ALL A PRESSURE SHORTLY AFTER, COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 6 LEAD EDGE FLAP ACTUATOR PER 727-100 MM 27-81-22. NO LEAK, RE-SAFETY ALL SWITCHES IN COCKPIT WITH BREAK-AWAY WIRE.
- [SDR 99FDEA00502](https://openairdocs.org/sdr/99FDEA00502.md): Control Valve · failed · Dec 17, 1999 · N154FE · Boeing 72725 · Trailing Edge Flap Control System
  > 99-285 - ON FLAP RETRACT UP TO FLAPS 2, BOTH INBD AND OTBD NEEDLES STUCK BETWEEN 2 AND 5. ALL LED'S IND EXT. REMOVED AND REPLACED O/B FLAP CONTROL VALVE PER MM 27-51-00. LUBED I/B FLAP CONTROL DRUM RIGGED CK GOOD PER 27-51-00-5.
- [SDR 98FDEA00587](https://openairdocs.org/sdr/98FDEA00587.md): Light · inoperative · Sep 22, 1998 · N154FE · Boeing 72725 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT FELL DOWN DURING T/O ROLL. REINSTALLED COCKPIT EMERGENCY EXIT LIGHT, OPER CKS GOOD PER FEDEX M/M 33-50-00.
- [SDR 98ZZZX4546](https://openairdocs.org/sdr/98ZZZX4546.md): Fitting · damaged · Sep 21, 1998 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF A REPEAT INSPECTION PER SB 737-53-194, HOLE NR 1 WAS FOUND ELONGATED. LOCATED AT STA 870 STR 9 AT THE TERMINAL FITTING. LT HAND SIDE. REPAIRED PER: DALFORT AEROSPACE, L.P. XEA X1-53-692 DATED 9-14-98, BOEING SB 727-53-194, BOEING D
- [SDR 98FDEA00582](https://openairdocs.org/sdr/98FDEA00582.md): Fitting · damaged · Sep 17, 1998 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > DAL - NR 375 - DURING ACCOMPLISHMENT OF REPEAT INSPECTION PER BOEING SB 727-53-194, HOLE NR 1 WAS FOUND ELONGATED. LOCATED AT BS 870 IN THE TERMINAL FITTING, LEFT SIDE. (X)
- [SDR 98FDEA00252](https://openairdocs.org/sdr/98FDEA00252.md): Engine · failed · Apr 4, 1998 · N154FE · Boeing 72725 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE OIL PRESSURE EXCEEDED RED RADIAL DURING DEPARTURE AT ALL POWER SETTINGS ABOVE IDLE. OIL TEMPERATURE 118C, PRESS 60 PSI PRESS 52 PSI AT IDLE. FOUND BREATHER PRESSURE AT 5.6 PSI OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE FOR HIGH BREATHER PRE
- [SDR 98FDEA00016](https://openairdocs.org/sdr/98FDEA00016.md): Wire · loose · Jan 8, 1998 · N154FE · Boeing 72725 · Door System Wiring
  > WHEN PASSING THROUGH FLIGHT LEVEL 270, MAIN CARGO DOOR LIGHT ILLUMINATED WITH NO LOSS OF PRESSURIZATION. DESCENDED TO 10,000, DEPRESSURIZED AIRCRAFT. LIGHT STAYED ON UNTIL LANDED. REPRESSURIZED AFTER LANDING, NO LIGHT ON. FOUND LOOSE WIRE ON NORMALLY CLOSE
- [SDR 96FDEA1015](https://openairdocs.org/sdr/96FDEA1015.md): Air Distr · odor · May 22, 1996 · N154FE · Boeing 72725 · Air Distribution System
  > STRONG ACRID ODOR IN COCKPIT AT FLIGHT LEVEL 330. PACK TEMPERATURES NORMAL, NOTHING ABNORMAL INDICATED AND DETECTION SYSTEM TESTED NORMAL. SUSPECT EITHER ELECTRICAL MALFUNCTION OR TOILET CHEMICAL MIXING CAUSED TOXIC FUMES. NO VISIBLE SMOKE. AIRCRAFT RELEAS
- [SDR 96FDEA00849](https://openairdocs.org/sdr/96FDEA00849.md): Bolt · missing · Apr 25, 1996 · N154FE · Boeing 72725 · Power Lever
  > AFTER T/O, NR 3 ENG THROTTLE DID NOT AFFECT ENGINE PRODUCTION, APPEARS AS IF THROTTLE LINKAGE DISCONNECTED. SHUT ENGINE DOWN USING NORMAL PROCEDURES. FOUND A BOLT HAD FALLEN OUT OF LINKAGE ON NR 3 ENGINE. REINSTALLED COTTER PIN AND CHECKED RIG WHICH WAS GOO
- [SDR 96FDEA00785](https://openairdocs.org/sdr/96FDEA00785.md): Beam · corroded · Apr 15, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR0470, FOUND CORROSION ON 740 BEAM UPPER SEAT AT LBL 25.
- [SDR 96FDEA00784](https://openairdocs.org/sdr/96FDEA00784.md): Skin · corroded · Apr 15, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION BETWEEN SKIN AND WINDOW CUTOUT DOUBLER BETWEEN STR 10 TO 11R STA 1083. REMOVED WINDOW FRAME, FOUND CORROSION TO BE OUT OF LIMITS ON FRAME AT 2 AREAS OF OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLES ON OUTER SKIN AND REPLACED FRAME IAW FEDEX E
- [SDR 96FDEA00783](https://openairdocs.org/sdr/96FDEA00783.md): Chord · cracked · Apr 15, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CRACK IN REINFORCEMENT CHORD ON UPPER FUEL CELL SKIN BS 745 WL 204.5 RBL 45.5. REMOVED DAMAGED CHORD BS 745 TO 783 RBL 45 WL 204. FABRICATED NEW CHORD AND INSTALLED IAW FEDEX EA 7-5710-28237.
- [SDR 96FDEA00762](https://openairdocs.org/sdr/96FDEA00762.md): Skin · corroded · Apr 12, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN SURFACE IS BULGING AND HAS TWO SKIN PLUGS MISDRILLED AT BS 330 - 334 AT LOWER LT NOSE CHORD STR 27L. REMOVED SKIN IN AREA OF REPAIR PLUGGED HOLES AND FABRICATED REPAIR FILLER AND DOUBLER. INSTALLED REPAIR PARTS PER FEDEX EA 7-5330-28230.
- [SDR 96FDEA00750](https://openairdocs.org/sdr/96FDEA00750.md): Bulkhead · corroded · Apr 8, 1996 · N154FE · Boeing 72725 · Fuselage Main, Bulkhead
  > CORROSION (C53-100-01, 4) ON FWD SIDE OF 178 BULKHEAD, RBL 21-26 WL 218. CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.
- [SDR 96FDEA00751](https://openairdocs.org/sdr/96FDEA00751.md): Side Frame · cracked · Apr 6, 1996 · N154FE · Boeing 72725 · Passenger/Crew Doors
  > FWD ENTRY DOOR, FWD SIDE FRAME IS CRACKED IN RADIUS ON LOWER EDGE, ADJACENT TO THE LOWER FWD STOP PIN FITTING. REMOVED FWD ENTRY DOOR CRACKED FWD SIDE FRAME, INSTALLED ONE EACH FWD SIDE FRAME IAW FEDEX 727 SRM 51-30-2 MM 52-11-01.
- [SDR 96FDEA00742](https://openairdocs.org/sdr/96FDEA00742.md): Skin · gouged · Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > WHILE WORKING NR0152, FOUND THE FUSELAGE SKIN TO BE GOUGED AT BS 307 RBL 63 WL 249, ADJACENT TO THE FORWARD ENTRY DOOR FUSELAGE TORQUE TUBE. REMOVED DAMAGED AREA, REPAIRED SKIN IAW FEDEX SRM 53-30-3.
- [SDR 96FDEA00741](https://openairdocs.org/sdr/96FDEA00741.md): Floor Beam · corroded · Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOOR BEAM AROUND FASTENER HOLES BS 1110, RBL 10 TO 60 WL 208. REMOVED CORROSION FROM FLOOR BEAM, FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR BS 1110, RBL 10 TO 60 WL 208, IAW FEDEX SRM
- [SDR 96FDEA00740](https://openairdocs.org/sdr/96FDEA00740.md): Floor Beam · corroded · Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON FLOOR BEAM BS 344 LBL 45 AND RBL 37 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 45 AND RBL 37 WL 208, PER FEDEX SRM 27-53-007.
- [SDR 96FDEA00739](https://openairdocs.org/sdr/96FDEA00739.md): Floor Beam · corroded · Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON FLOOR BEAM BS 380, LBL 28 TO 34 AND LBL 55 WL 208. REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR PER FEDEX SRM 53-10-8.
- [SDR 96FDEA00738](https://openairdocs.org/sdr/96FDEA00738.md): Stringer · corroded · Apr 5, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-113-01, 2) FOUND WHILE WORKING NR0602 STA 1055 STRINGER 28R IN STRINGER. FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA, REPAIRED STR 28R IAW FEDEX SRM 53-10-3.
- [SDR 96FDEA00760](https://openairdocs.org/sdr/96FDEA00760.md): Skin · corrosion · Apr 4, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION (C53-132-02(1)). ON UPPER FUEL CELL AT BS 870, WL 190, RBL 44, RUNNING ORDER CAP. REMOVED CORROSION ON UPPER FUEL CELL SKIN AT BS 870, WL 190, RBL 44, AND REPAIRED DAMAGED SKIN PER FEDEX EA 7-5710-28189.
- [SDR 96FDEA00729](https://openairdocs.org/sdr/96FDEA00729.md): Stringer · corroded · Apr 1, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > NR 0623, 042 CORROSION (C53-113-01, -2) FOUND WHILE WORKING NR0602 STA 1055 STR 28R IN STRINGER. *S/D* FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA REPAIRED STR 28R IAW FEDEX SRM 53-10-3.
- [SDR 96FDEA00728](https://openairdocs.org/sdr/96FDEA00728.md): Stringer · corroded · Mar 29, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > NR 0624 AND 043, CORROSION FOUND ON END OF STR SECTION STR 28R BS 1059.
- [SDR 96FDEA00723](https://openairdocs.org/sdr/96FDEA00723.md): Bracket · corroded · Mar 28, 1996 · N154FE · Boeing 72725 · Wing Miscellaneous Structure
  > LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING IS CORRODED AROUND MAIN PULLEY BOLT HOLE AND TWO OTHER AREAS ON CASTING WBL 410. REMOVED CORRODED LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING AND INSTALLED NEW CASTING IAW FEDEX MM 27-10-0,
- [SDR 96FDEA00722](https://openairdocs.org/sdr/96FDEA00722.md): Frame · corroded · Mar 28, 1996 · N154FE · Boeing 72725 · Fuselage Main, Frame
  > WHILE WORKING ON NR 0412, FOUND CORROSION (7-5310-3364 PT 6) ON WINDOW FRAME AT BS 970 TO 990 ABOVE STR 11R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED WINDOW FRAME AND INSTALLED NEW WINDOW FRAME AT BS 970 TO 990 STR 11R IAW SRM 53-10-1.
- [SDR 96FDEA00700](https://openairdocs.org/sdr/96FDEA00700.md): Hinge Fitting · cracked · Mar 25, 1996 · N154FE · Boeing 72725 · Ailerons
  > NR0348 AND 030, RT WING O/B AILERON NR 3 HINGE FITTING IS CRACKED.
- [SDR 96FDEA00699](https://openairdocs.org/sdr/96FDEA00699.md): Doubler · corroded · Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0611 AND 033, WHILE WORKING NR0602, FOUND DOUBLER TO HAVE CORROSION FROM BS 1050 TO 1125 FRONT STRINGER 26 TO 27R.
- [SDR 96FDEA00698](https://openairdocs.org/sdr/96FDEA00698.md): Beam · corroded · Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0486 AND 034, CORROSION (C53-224-01) ON LONGITUDINAL BEAM AND BARE METAL AROUND NUT CLIP HOLES LOWER SURFACE BS 780 TO 848 LBL 25.
- [SDR 96FDEA00697](https://openairdocs.org/sdr/96FDEA00697.md): Stringer · damage · Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > NR0604 AND 036, WHILE WORKING NR0156, FOUND MECH DAMAGE ON STR 24 AT STA 482.
- [SDR 96FDEA00696](https://openairdocs.org/sdr/96FDEA00696.md): Skin · corroded · Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION C53-113-01(2). FOUND WHILE WORKING NR 0240 FWD AND AFT CORNERS OF DOOR THRESHOLD STA (1107) TO 1060, WL 160, RBL 37. *****S/D**** REPLACED BARE STRAP LOWER HALF IAW EA 7-5310-28087.
- [SDR 96FDEA00694](https://openairdocs.org/sdr/96FDEA00694.md): Skin · corroded · Mar 25, 1996 · N154FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > WHILE WORKING NR0602, FOUND SKIN AND BONDED DOUBLER TO HAVE CORROSION ON MATING SURFACES AT BS 1110 TO 1128 FROM STR 25 TO 26R. REMOVED CORROSION FROM BLER AND TRIPLER. DAMAGE ON TRIPLER WAS OUT OF LIMITS. FABRICATED NEW TRIPLER, ALODINED AND PRIMED TRIPLER
- [SDR 96FDEA00693](https://openairdocs.org/sdr/96FDEA00693.md): Floor Beam · corroded · Mar 25, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON FLOOR BEAM BS 360 LBL 12 RBL 5 AND 48 WL 208. REPAIRED FLOOR BEAM BS 360 LBL 12 AND RBL 5 WL 208. FOUND FLOOR BEAM BS 360 RBL 48 TO BE WITHIN SERVICEABLE LIMITS. CLEANED AND TREATED BS 360 RBL 48 WL 208 PER FEDEX SRM 51-10-6. REPA
- [SDR 96FDEA00692](https://openairdocs.org/sdr/96FDEA00692.md): Stringer Clip · gouged · Mar 22, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > MECH DAMAGE TO STR CLIP BS 1148 STR 16R. REMOVED DAMAGED STR CLIP AND INSTALL NEW STR CLIP AT BS 1148 STR 16R.
- [SDR 96FDEA00666](https://openairdocs.org/sdr/96FDEA00666.md): Threshold · corroded · Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION (C53-113-01, 2) ON DOOR THRESHOLD STIFFENER BS 1057.5 TO 1110 WL 164 RBL 35. INSTALLED NEW DOOR THRESHOLD STIFFENER.
- [SDR 96FDEA00636](https://openairdocs.org/sdr/96FDEA00636.md): Clip · cracked · Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP BS 420 STR 4L. REMOVED CRACKED STR CLIP, DRILLED NEW STR CLIP AND INSTALLED AT BS 420 STR 4L.
- [SDR 96FDEA00635](https://openairdocs.org/sdr/96FDEA00635.md): Stringer · damaged · Mar 20, 1996 · N154FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > MECH DAMAGE ON STR 23L AT STA 482. REMOVED DAMAGED STR BS 482 STR 23L AND INSTALLED REPAIR PER FEDEX SRM 53-10-3.
- [SDR 96FDEA00578](https://openairdocs.org/sdr/96FDEA00578.md): Bulkhead Web · corrosion · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Bulkhead
  > NR0079 AND 006, CORROSION (C53-100-0164) ON FWD SIDE OF 178 BULKHEAD RBL 21 TO 26 WL 218. *S/D* CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.
- [SDR 96FDEA00577](https://openairdocs.org/sdr/96FDEA00577.md): Skin · creased · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0098 AND 007, CREASE IN SKIN BS 1108 WL 208 LBL 60. REMOVED DAMAGE IN SKIN BS 1108 WL 208 LBL 60 FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 53-30-3.
- [SDR 96FDEA00576](https://openairdocs.org/sdr/96FDEA00576.md): Frame · damaged · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Frame
  > NR0168 AND 008, DAMAGED FRAME BS 1130 RBL 50 WL 188 UNDER FLANGE.
- [SDR 96FDEA00574](https://openairdocs.org/sdr/96FDEA00574.md): Shear Tie · corrosion · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0235 AND 010, CORROSION (C53-113-01, 2) ON SHEAR TIE BS 990 WL 158 STR 29R. REMOVED DAMAGED SHEAR TIE BS 990 WL 158 STR 29R AND INSTALLED REPAIR PER FEDEX SRM 53-10-4.
- [SDR 96FDEA00573](https://openairdocs.org/sdr/96FDEA00573.md): Frame · corrosion · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Frame
  > NR0451 AND 011, CORROSION ON FRAME BS 700 WL 155 RBL TO LBL 11.
- [SDR 96FDEA00572](https://openairdocs.org/sdr/96FDEA00572.md): Frame · corrosion · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Frame
  > NR0452 AND 012, CORROSION ON FRAME BS 700 WL 149 RBL 4.
- [SDR 96FDEA00571](https://openairdocs.org/sdr/96FDEA00571.md): Floor Beam · corroded · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0474 AND 013, CORROSION (C53-224-01) AND OR BARE METAL AROUND ALL NUT CLIP HOLES LOWER SURFACE BS 760 TO 848 RBL 25 WL 208 ON LONGITUDINAL FLOOR BEAM. CORROSION DAMAGE ON LONGITUDINAL FLOOR BEAM WAS FOUND OUT OF LIMITS. REMOVED DAMAGED BEAM AND INSTALLED
- [SDR 96FDEA00570](https://openairdocs.org/sdr/96FDEA00570.md): Te Wedge · delamination · Mar 18, 1996 · N154FE · Boeing 72725 · Trailing Edge Flaps
  > NR0480 AND 014, RT WING O/B MIDFLAP TRAILING EDGE WEDGE HAS A DISBOND 88 FROM I/B END ON UPPER SKIN.
- [SDR 96FDEA00569](https://openairdocs.org/sdr/96FDEA00569.md): Floor Beam · corrosion · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01) ON FLOOR BEAM BS 480 LBL 39 WL 208. PERFORMED FLOOR BEAM REPAIR AT BS 480 LBL 39 WL 208 IAW 53-10-8 FEDEX 727 SRM AND ENGINEERING REQUEST.
- [SDR 96FDEA00568](https://openairdocs.org/sdr/96FDEA00568.md): Floor Beam · corroded · Mar 18, 1996 · N154FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0542 AND 016, CORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOORBEAM AROUND NUTPLATE AND FASTENER HOLES, BS 1030 RBL 48 TO 60 WL 208.
- [SDR 96FDEA00575](https://openairdocs.org/sdr/96FDEA00575.md): Forging · corroded · Mar 17, 1996 · N154FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > (NR 0230 AND NR 009). CORROSION (C53-111-01 (3)) ON THE BS 950 FORGING WL 208, RBL 50. **** S/D **** REMOVED CORROSION ON THE BS 950 FORGING, WL 280, RBL 50. BLENDED DAMAGED AREA, CLEANED, TREATED AND RE-INSTALLED FASTENERS PER FEDEX EA 7-5310-28062.
- [SDR 96FDEA00567](https://openairdocs.org/sdr/96FDEA00567.md): Skin · damaged · Mar 15, 1996 · N154FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0097 AND 001, LIGHTNING STRIKE ON FASTENER HEAD BS 316 LBL 55 WL 178.
- [SDR 96FDEA00566](https://openairdocs.org/sdr/96FDEA00566.md): Hinge Fitting · corroded · Mar 15, 1996 · N154FE · Boeing 72725 · Ailerons
  > NR0196 AND 002, LEFT O/B AILERON NR 1 HINGE FITTING IS CORRODED ON LOWER SURFACE.
- [SDR 96FDEA00565](https://openairdocs.org/sdr/96FDEA00565.md): Skin · delaminated · Mar 15, 1996 · N154FE · Boeing 72725 · Trailing Edge Flaps
  > NR0248 AND 003, RT WING O/B TRAILING EDGE AFT FLAP IS DELAMINATED APPROX 96 INCHES FROM I/B EDGE.

Next page: https://openairdocs.org/deregistered/N154FE-2002-10-15/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 = 'N154FE' AND deregistration_id = 'N154FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N154FE-2002-10-15/reports

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