# Service difficulty reports: N185FE, cancelled May 23, 2007

A list on [N185FE, cancelled May 23, 2007](https://openairdocs.org/deregistered/N185FE-2007-05-23.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 · 114 reports

- [SDR 06FDEA2569](https://openairdocs.org/sdr/06FDEA2569.md): Blade · damaged · Jul 15, 2006 · N185FE · Boeing 727100 · Engine (Turbine/Turboprop)
  > AS POWER WAS ADVANCED TO MAX POWER FOR T/O, THERE WAS A LOUD BANG AND THUMP IN THE THROTTLE QUADRANT, FOLLOWED BY THE SOUND OF A CABLE UNWINDING. T/O WAS DISCONTINUED AND AIRCRAFT RETURNED TO MX. AFTER DEBRIEFING FLIGHT CREW PROCEEDED TO INSPECT NR 2 ENGINE
- [SDR 06FDEA1659](https://openairdocs.org/sdr/06FDEA1659.md): Attach Fitting · damaged · May 1, 2006 · N185FE · Boeing 72722 · Wing, Landing Gear Attach Fittings
  > FORWARD TRUNNION ATTACH FTG OVERSIZE HOLE REWORK. COMPLIED WITH EA 7-5710-7-92417 WINGS MAIN FRAME MLG TRUNNION ATT FITTING OVERSIZE HOLE REWORK RII:573074.
- [SDR 06FDEA1658](https://openairdocs.org/sdr/06FDEA1658.md): None · none · May 1, 2006 · N185FE · Boeing 72722 · Standard Practices/Structures
  > TRUNNION ATTACH FITTING MODIFICATION. COMPLIED WITH EO 7-5710-7-2314D PT5 WINGS MLG TRUNNION ATTACH FITTING.
- [SDR 06FDEA1657](https://openairdocs.org/sdr/06FDEA1657.md): Attach Fitting · cracked · May 1, 2006 · N185FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EO 7-5710-7-2314D PT6 EOCN D1 WINGS - MLG TRUNNION ATTACH FITTING MODIFICATION BOEING S/B 72 7-57AD132 R3 AD 2004-18-08. COMPLIED WITH EO 7-5710-7-2314D PT6 RII:536327.
- [SDR 06FDEA0308](https://openairdocs.org/sdr/06FDEA0308.md): Lamp · inoperative · Jan 21, 2006 · N185FE · Boeing 727100 · Landing Gear Position and Warning
  > LT MLG GREEN LIGHT DID NOT ILLUMINATE FOR LANDING. CREW REPORTED GEAR WAS DOWN BY VISUAL INSPECTION UPON ARRIVAL RE-LAMPED LEFT MAIN GEAR GREEN LIGHT OPS CHECK GOOD IAW MMSP.
- [SDR 05FDEA01270](https://openairdocs.org/sdr/05FDEA01270.md): Wire · broken · May 13, 2005 · N185FE · Boeing 72722 · Landing Gear System Wiring
  > EXTENDING GEAR, DID NOT GET RIGHT MAIN GEAR GREEN LIGHT. TAIL SKID LIGHT ON S/O PANEL WAS ALSO ILLUMINATED. CHECKLIST LEAD US TO TEST GREEN LIGHT, LIGHT WAS WORKING. CB PRESS TO TEST AND LIGHTS WERE RESET PER CHECKLIST. VERIFIED RIGHT MAIN DOWN WITH MANUAL
- [SDR 05FDEA00093](https://openairdocs.org/sdr/05FDEA00093.md): Fairing · missing · Jan 14, 2005 · N185FE · Boeing 727100 · Aerodynamic Fairings
  > ON ARRIVAL FOUND AFT CARGO DOOR MOVABLE FAIRING MISSING FROM AIRCRAFT. INSTALLED AFT CARGO DOOR MOVABLE FAIRING PER 727-100 MM 52-33-00-4. OPS CHECK GOOD.
- [SDR 04FDEA03199](https://openairdocs.org/sdr/04FDEA03199.md): Control Unit · malfunctioned · Nov 24, 2004 · N185FE · Boeing 72722 · Smoke Detection
  > LOWER AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. RAN QRH. DISCHARGED BOTTLE-1, LANDED IN LCK IN 20 MIN. SECOND BOTTLE DID NOT AUTO-FIRE AS PER 25 MIN REQUIREMENT. CFR CREWS DETERMINED NO FIRE PRESENT. FOUND ALL TEST LIGHTS ON AFT LOWER CARGO COMPART
- [SDR 04FDEA02265](https://openairdocs.org/sdr/04FDEA02265.md): Skin · corroded · Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN AT AFT CARGO DOOR AFT CUTOUT LOWER CORNER. REPAIRED INNER SKIN AT AFT CARGO DOOR AFT CUT OUT LOWER CORNER PER FED EX E.A. 7-5310-55341.
- [SDR 04FDEA02264](https://openairdocs.org/sdr/04FDEA02264.md): Door Frame · corroded · Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Structure
  > CORROSION AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD CONTINUING UNDER FILLER. REPAIRED AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD PER FED EX E.A. 7-5310- 55341.
- [SDR 04FDEA02263](https://openairdocs.org/sdr/04FDEA02263.md): Stringer · corroded · Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > CORROSION ON UPPER SURFACE OF STRINGER 7L STA 876. CORROSION DAMAGE ON UPPER SURFACE OF STRINGER 7L, STA 876 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED DAMAGED STRINGER SECTION BS 870 - 890+10, STR 7L PER SRM 51-10-5 AND 51-30-2. FA
- [SDR 04FDEA02266](https://openairdocs.org/sdr/04FDEA02266.md): Skin · cracked · Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT EDGE OF LAP JOINT BS 1064 RBL 26 STR 26R.
- [SDR 04FDEA02180](https://openairdocs.org/sdr/04FDEA02180.md): Skin · dented · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN BS 320-330 AND 2 INCHES ABOVE STR 21R. REPAIRED THE FUSELAGE SKIN AT BS 320 TO 330 2 INCHES ABOVE STR 21R PER EA 7-5330- 70671
- [SDR 04FDEA02191](https://openairdocs.org/sdr/04FDEA02191.md): Stringer · cracked · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > WHILE WORKING CARD N00533, FOUND CRACKED STRINGER AT BS 1114 STR 25 RT. *S/D* REPAIRED STRINGER 25 RT AT BS 1107-1115 PER SRM 53-10-3 FIG 1.
- [SDR 04FDEA02190](https://openairdocs.org/sdr/04FDEA02190.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND SEAT TRACK LINK AFT ATTACH BOLT BS 870 LBL 25 WL 205. *S/D* CORROSION ON AROUND SEAT TRACK LINK ATTACH BOLT AT BS 870 LBL 25 WL 205 WAS FOUND TO BE IN LIMITS. CORROSION ON LINK AT BS 870 LBL 25 WL 208 WAS OUT OF LIMITS. REMOVED & REPLACED
- [SDR 04FDEA02189](https://openairdocs.org/sdr/04FDEA02189.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 870-950, RBL 45, WL 208. CORROSION ON SEAT TRACK AT BS 870-950 RBL 45 WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-5.
- [SDR 04FDEA02188](https://openairdocs.org/sdr/04FDEA02188.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 760-840 RBL 22 WL 208. REMOVED AND REPLACED LONGITUDAL BEAM STA 760-848 RBL 22, WL 208 IAW SRM 51-30-02, 51-30-5.
- [SDR 04FDEA02187](https://openairdocs.org/sdr/04FDEA02187.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 760-840 LBL 25 WL 208 AT FASTENER HOLES. REMOVED CORROSION ON SEAT TRACK FROM BS 760-840 LBL 25 WL 208 FOUND SEAT TRACK TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW LONGITUDAL BEAM AND INSTALLED IAW SRM 51-30-2.
- [SDR 04FDEA02186](https://openairdocs.org/sdr/04FDEA02186.md): Seat Track · damaged · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED.040, 1 INCH X 1 INCH FROM.080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRACK, INSTALLED NEW SEA
- [SDR 04FDEA02185](https://openairdocs.org/sdr/04FDEA02185.md): Angle · dented · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. *S/D* FOUND J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. REMOVED, FABRICATED AND INSTALLED NEW J-ANGLE IAW SRM 53-10-1 PG 2 FIG 1 SHEET 2, SRM 51-30-2.
- [SDR 04FDEA02184](https://openairdocs.org/sdr/04FDEA02184.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 RBL 48 WL 205. *S/D* CORROSION ON LINK AT BS 742 WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK LINK AND FWD ATTACH BOLT AT BS 742 RBL 48 WL 205 PER SRM 51-30-2, 53-10-1 & 53-10-5 & AT BS 740-760 R
- [SDR 04FDEA02183](https://openairdocs.org/sdr/04FDEA02183.md): Seat Track · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 LBL 25 WL 205. *S/D* REMOVED AND REPLACED SEAT TRACK LINK BS 740 TO BS 760, LBL 25, IWL 205 IAW SRM 51-30-2.
- [SDR 04FDEA02182](https://openairdocs.org/sdr/04FDEA02182.md): Stringer · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > CORROSION WHILE WORKING CARD N00233 FOUND CORROSION ON STRINGER 26 LEFT LBL 20 BS 1135. CORROSION ON STA 26 LEFT BS 1135 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED STR 26 LEFT BS 1120-1140 AND INSTALLED NEW STRINGER & REPAIR SPLICE PER SRM 53-10-
- [SDR 04FDEA02181](https://openairdocs.org/sdr/04FDEA02181.md): Floorbeam · corroded · Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM BS 344, BS LBL 60 - RBL 12, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM SECTION AT BS 344 LBL 7 TO LBL 65 WL 208 PER SRM 53-10-8.
- [SDR 04FDEA02142](https://openairdocs.org/sdr/04FDEA02142.md): Fitting · cracked · Jul 20, 2004 · N185FE · Boeing 727100 · Fuselage Main, Attach Fittings
  > CRACKED STR FITTING AT BS 874 STR 9R. REMOVED AND REPLACED STRINGER 9R FITTING AT BS 874 IAW BOEING 727 SRM 51-30-5, BOEING 727 SRM 51-30-2.
- [SDR 04FDEA02143](https://openairdocs.org/sdr/04FDEA02143.md): Stringer · damaged · Jul 20, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442 STR 5L. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-10-3, 51-30-2, 51-10-2 AND 51-10-6. INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2.
- [SDR 04FDEA02138](https://openairdocs.org/sdr/04FDEA02138.md): Frame · damaged · Jul 19, 2004 · N185FE · Boeing 727100 · Fuselage Main, Frame
  > DAMAGE AT REPAIR DOUBLER AT BS 930, 3 INCHES ABOVE STR 14 LT, AFT SIDE OF FRAME. REMOVED AND REPLACED REPAIR DOUBLER AT BS 930, 3 ABOVE STR 14 LT PER SRM 51-30-2, 53-10-3.
- [SDR 04FDEA02096](https://openairdocs.org/sdr/04FDEA02096.md): Skin · corroded · Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > (C54-451-01, 2) EXTERNAL FUSELAGE SKIN PILLOWED & EMINATING POWDER AT BUTT JOINTS BS 1363-1379, 6 INCHES OVER NR 2 ENGINE CUTOUT, RT SIDE. REMOVED DAMAGE SKIN PANEL AT BS 1363 TO 1379 AND FABRICATED NEW PANEL. ALODINE, PRIMED AND PAINTED NEW PANEL. INSTALL
- [SDR 04FDEA02095](https://openairdocs.org/sdr/04FDEA02095.md): Stringer · cracked · Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT, STR 21 LT BS 488 IS CRACKED. REMOVED DAMAGE PORTION OF STR 21 LT, BS 488. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-3 FIG 1.
- [SDR 04FDEA02094](https://openairdocs.org/sdr/04FDEA02094.md): Floorbeam · corroded · Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION 870 FLOORBEAM UPPER SECTION RBL 20 & RBL 26 WL 208. REMOVED CORROSION ON 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208. FOUND 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208 TO BE IN LIMITS IAW SRM 53-10-1, FIG 8.
- [SDR 04FDEA02093](https://openairdocs.org/sdr/04FDEA02093.md): Floor Panel · corroded · Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Floor Panel
  > CORROSION ON FLOOR WEB BS 620, LBL 48-55, WL 208, AND ELONGATED FASTENER HOLES. COMPLIED WITH FED EX E.A. 7-5310-70670 ON THE 620 FLOORBEAM LBL 48-55 WL 208.
- [SDR 04FDEA02092](https://openairdocs.org/sdr/04FDEA02092.md): Stringer · damaged · Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442, STR 6L. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 6L BS 442 I.A.W. BOEING 727 SRM 53-10-3 FIG 3.
- [SDR 04FDEA02089](https://openairdocs.org/sdr/04FDEA02089.md): Floorbeam · corroded · Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM LWR FWD AT BS 1050 LBL 1 TO 22 WL 201. REMOVED DAMAGE ON FLOORBEAM LWR FWD AT BS 1050, LBL 1-22. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-8, 51-10-1.
- [SDR 04FDEA02088](https://openairdocs.org/sdr/04FDEA02088.md): Floorbeam · corroded · Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM FASTENER HOLES BS 1110 LBL 21 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD SECTION AT BS 1110 LBL 20-22.5 WL 208 PER SRM 53-10-8
- [SDR 04FDEA02087](https://openairdocs.org/sdr/04FDEA02087.md): Crease Beam · corroded · Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Structure
  > CORROSION ON CREASE BEAM BS 1080 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1080, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED CREASE BEAM. INSTALLED NEW CREASE BEAM IAW 51-30-2, 51- 20-4.
- [SDR 04FDEA02085](https://openairdocs.org/sdr/04FDEA02085.md): Crease Beam · corroded · Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Structure
  > CORROSION ON CREASE BEAM BS 1010 - 1050 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1010 TO BS 1050, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVE DAMAGED CREASE BEAM, INSTALLED NEW CREASE BEAM IAW SRM 51-30- 2, 51-20-4.
- [SDR 04FDEA02090](https://openairdocs.org/sdr/04FDEA02090.md): Floorbeam · corroded · Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION ON LOWER FLOORBEAM FASTENERS BS 1110 RBL 1-12 WL 201. REMOVED CORROSION ON FLOORBEAM LWR CHORD BS 1110 RBL 6 WL 201, 2 X 1 MAXIUMUN MATERIAL LOSS.036 ORIGINAL THICKNESS.125 OUT OF LIMMITS PER SRM 51-10-6, 53-10-2 CUT OUT DAMAGE LWR FLANGE BS 1110 A
- [SDR 04FDEA02078](https://openairdocs.org/sdr/04FDEA02078.md): Beam · corroded · Jul 14, 2004 · N185FE · Boeing 727100 · Horizontal Stabilizer Structure
  > CORROSION ON RT HORIZONTAL STAB UPPER T/E BEAM UPPER SURFACE, ABOVE NR 7 HINGE. REMOVED AND REPLACED RT HORIZONTAL STAB UPR T/E BEAM IAW SRM 51-10-2, 51-30-2, 51- 30-5, 51-30-8 AND SOPM 20-50-01 AND EA 7-5510-72372.
- [SDR 04FDEA02077](https://openairdocs.org/sdr/04FDEA02077.md): Stringer · corroded · Jul 14, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 23R BS 740. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-10-3. FABRICATED REPAIR PER SRM 53-10-3 FIG. 1. INSTALLED REPAIR ONS TR 23R BS 740 PER SRM 53-10-3 AND SRM 53-30-2.
- [SDR 03FDEA00942](https://openairdocs.org/sdr/03FDEA00942.md): Flap · malfunctioned · Jun 21, 2003 · N185FE · Boeing 727100 · Leading Edge Slat Control System
  > NR 4 LEADING EDGE FLAP WOULD NOT RETRACT WHEN WE MOVED FROM FLAP 5 TO 2 WHILE INFLIGHT. INSTALLED JUMPER CABLE ON NR 4 L/E FLAP. UPON INSP FOUND NR 4 LE FLAP LIGHT ON AT S/O'S. PANEL WHEN NR 4 LE FLAP FULLY RETRACTED. INSTALLED ADAPTER CABLE ON NR 4 LE FL
- [SDR 01FDEA00583](https://openairdocs.org/sdr/01FDEA00583.md): Actuator · inoperative · Jul 19, 2001 · N185FE · Boeing 72722 · Leading Edge Slat Control System
  > 01-243 AFT DEPART WHEN FLAPS WERE RETRACTED TO 2 DEG #5 SLAT W/N RETRACT. R&R ACTUATOR PER 27-81-032-4. LEAK OPS CK GOOD.
- [SDR 00FDEA00181](https://openairdocs.org/sdr/00FDEA00181.md): Switch · bent · Mar 28, 2000 · N185FE · Boeing 72722 · Leading Edge Slat Control System
  > NR 5 LEAD EDGE FLAP SHOW INTRANSIT ABOUT 5 MIN AFT T/O. DID RED TABS, EXT TO 5 DEG AND BACK TO 0 AND LIGHT WENT OUT. REMOVED AND REPLACED MICRO SWITCH PER MM 27-81.
- [SDR 99FDEA00417](https://openairdocs.org/sdr/99FDEA00417.md): Switch · malfunction · Oct 8, 1999 · N185FE · Boeing 72722 · Landing Gear Position and Warning
  > 99-248 REPEAT, LEFT MAIN GEAR IND GREEN LIGHT MALFUNCTION. SUSPECT DOWN LOCK SWITCH. REPLACED DOWNLOCK SWITCH PER 727 MM 32-61-021-4. PERF ADJUST AND TEST PER MM 32-61-021-5, OPER CK GOOD. OK FOR SERV.
- [SDR 99FDEA00416](https://openairdocs.org/sdr/99FDEA00416.md): Connector · dirty · Oct 8, 1999 · N185FE · Boeing 72722 · Landing Gear Position and Warning
  > 99-247 - LEFT MAIN GEAR NOT DOWN AND LOCKED WITH HANDLE DOWN. NEGATIVE G PER RED TABS LOCK DOWN GEAR. CLEANED CANNON PLUG ON DOWN LOCK SWITCH LEFT GEAR. OPER CK GOOD PER GENERAL MM.
- [SDR 99FDEA00414](https://openairdocs.org/sdr/99FDEA00414.md): Frame · corroded · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Frame
  > NR 991, CORROSION ON BELTFRAME EXTRUSION BS 333 AT LT SKATE ANGLE. CUT OUT DAMAGE AND INSTALLED REPAIR PER DRAWING 65C 15724.
- [SDR 99FDEA00413](https://openairdocs.org/sdr/99FDEA00413.md): Bulkhead · corroded · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Bulkhead
  > NR 991 - CORROSION ON BULKHEAD BS 348 IN NOSE W/W IN AREA OF DRAG BRACE FITTING. REMOVED AND REPLACED PER EA 7-5310-45369 DATED AUG 16, 1999.
- [SDR 99FDEA00411](https://openairdocs.org/sdr/99FDEA00411.md): Frame · cracked · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Frame
  > NR 544, BS 804, STR 5R FRAME HAS VISUAL IND OF CRACK AT STR ATTACH RIVETS. CONFIRMED CRACK WITH DYE PENATRANT. REMOVED (CUTOUT) DAMAGED AREA. INSTALL REPAIR ANGLE PER SRM 53-10-4.
- [SDR 99FDEA00408](https://openairdocs.org/sdr/99FDEA00408.md): Stringer · damaged · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > NR 522, STR 4L DAMAGED O/B SIDE BS 680 4 GOUGES IN 3 SECTION, 1 GOUGE THROUGH STR. REPAIR STR PER SRM 53-10-3 FIG 3.
- [SDR 99FDEA00406](https://openairdocs.org/sdr/99FDEA00406.md): Bulkhead · cracked · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Bulkhead
  > NR 379, CRACK IN 1183 BULKHEAD LT DOOR FRAME WEB AT WL 263. INSTALLED NEW BEAM SECTION AND SPLICED PER EA 7532045307 DATED 7/16/99 AND SB 727-53-210.
- [SDR 99FDEA00405](https://openairdocs.org/sdr/99FDEA00405.md): Frame · cracked · Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Frame
  > NR 543, CRACK IN BELLFRAME BS 822 AT STR 5R. CUT OUT CRACKED AREA AND INSTALL.090 DOUBLER ALL PER 53-10-4 FIG 2.

Next page: https://openairdocs.org/deregistered/N185FE-2007-05-23/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 = 'N185FE' AND deregistration_id = 'N185FE-2007-05-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N185FE-2007-05-23/reports

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