# Service difficulty reports: N195FE, cancelled Oct 15, 2002

A list on [N195FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N195FE-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.

- [SDR 00FDEA00138](https://openairdocs.org/sdr/00FDEA00138.md): Clamp · loose · Mar 7, 2000 · N195FE · Boeing 72722 · Pneumatic Distribution System
  > NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. RETIGHTEN CLAMP IN THE PNEU DUCT PER MM 36-00-002-4 CK. LEAK CHECK GOOD, OK TO CONTINUE.
- [SDR 98FDEA00498](https://openairdocs.org/sdr/98FDEA00498.md): Clamp · loose · Aug 11, 1998 · N195FE · Boeing 72722 · Pneumatic Distribution System
  > 98-0199 - DURING CLIMB-OUT PASSING 10K FT, ENG 3 STRUT LGT ILLUM. RT PACK WAS TURNED OFF AND ENG 3 BLEED CLOSED. WHILE REFERENCING RED TABS, LGT EXT LGT TESTED OK. RED TABS COMPLETE. FOUND NR 3 ENG BLEED VLV IN 3 STRUT WITH LOOSE CLAMPS. AIR LEAK. RESECU
- [SDR 96FDEA01330](https://openairdocs.org/sdr/96FDEA01330.md): Overheat Light · illuminated · Aug 6, 1996 · N195FE · Boeing 72722 · Overheat Detection
  > AFTER T/O ON CLIMBOUT, ENG NR 1 STRUT OVERHEAT LITE ON. RAN CHKLST. ENG AT IDLE FOR 3 MIN LITE REMAINED ON. SHUTDOWN ENG PER CHKLST. AFTER 5 MIN LITE STILL ON. PULLED FIRE HANDLE AS PRECAUT. 2 MIN LATER LITE OFF. WINDMILL 20 MIN OIL PRESS 43. REMD PNLS T
- [SDR 96FDEA01309](https://openairdocs.org/sdr/96FDEA01309.md): Light · inoperative · Aug 2, 1996 · N195FE · Boeing 72722 · Emergency Lighting
  > NRO774 AND 046, EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. *S/D* REPLACED FWD ENTRY LIGHT ASSEMBLY, FUNCTIONAL TEST CHECKS OK IAW FEDEX MM 33-50-101.
- [SDR 96FDEA01304](https://openairdocs.org/sdr/96FDEA01304.md): Light · inoperative · Aug 1, 1996 · N195FE · Boeing 72722 · Emergency Lighting
  > LP 558749 045C. EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. REPLACED FORWARD ENTRY LIGHT ASSEMBLY. FUNCTIONAL TEST CHECKS GOOD IAW FEDEX MM 33-50-101. (BS 328, WL 200 LBL 65.)
- [SDR 96FDEA01301](https://openairdocs.org/sdr/96FDEA01301.md): Skin · cracked · Jul 30, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR0171 009. BS 520, STR 25, RBL 30, THERE IS A CRACK IN SKIN. ****S/D**** MECHANICALLY REMOVED CRACK IN SKIN LOCATED AT BS 520, STR 25R, RBL 30. REPAIRED SKIN PER FEDEX EA 7-5310-29202.
- [SDR 96FDEA01300](https://openairdocs.org/sdr/96FDEA01300.md): Skin · lightning strike · Jul 30, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0100 044. BS 360 - 440, WL 160, STR 24-26R, THERE ARE SEVERAL LIGHTNING STRIKES (MARKED). ****S/D**** REPAIRED LIGHTNING STRIKES PER FEDEX SRM 53-30-3, FIG 20 AT BS 360 - 440, WL 160, STR 24-26R.
- [SDR 96FDEA01293](https://openairdocs.org/sdr/96FDEA01293.md): Chord · corrosion · Jul 29, 1996 · N195FE · Boeing 72722 · Wing Miscellaneous Structure
  > NR 0231 042. CORROSION C53-132-02(1) ON STA 870, UPPER CHORD LBL 58-60, 46, 36-38, 26-28, 17-19, RBL 55, 45, 10, 0 WL 172. REMOVED AND REPLACED 870 UPPER CHORD LBL 70 - RBL 70, WL 172 PER FEDEX EA 7-5710-29709.
- [SDR 96FDEA01290](https://openairdocs.org/sdr/96FDEA01290.md): Frame · cracked · Jul 26, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0370 039. BS 913, WL 194, STR 18A FRAME IS CRACKED IN MAIN WHEELWELL. REPAIRED CRACKED FRAME BS 13, WL 194, STR 18A IAW FEDEX EA 7-5310-29295A.
- [SDR 96FDEA01286](https://openairdocs.org/sdr/96FDEA01286.md): Longeron · cracked · Jul 24, 1996 · N195FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > NR 0729 038. WHILE WORKING NR 0312, DISCOVERED CRACK IN FORWARD MOST FASTENER HOLE OF LONGERON AT BS 1110, STR 27R. ***S/D**** COMING.
- [SDR 96FDEA01294](https://openairdocs.org/sdr/96FDEA01294.md): Frame · cracked · Jul 22, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0757 041. CRACK ON INBOARD FLANGE OF FRAME AT BS 480 STR 26R RBL 24. REMOVED DAMAGE IN FRAME AT BS 480, STR 26R RBL 24. FABRICATED REPAIR PART, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PART PER FEDEX SRM 51-40-3.
- [SDR 96FDEA01276](https://openairdocs.org/sdr/96FDEA01276.md): Frame · cracked · Jul 21, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: (NR 0316)(036) CRACK IN FRAME AT BS 1070, LBL 37, WL 153 ABOVE STR 25L. CORRECTIVE ACTION: *****S/D **** COMING.
- [SDR 96FDEA01275](https://openairdocs.org/sdr/96FDEA01275.md): Frame · cracked · Jul 21, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0321, 037 CORROSION (C53-113-01) AND CRACK AT PREVIOUS REPAIR FRAME AT BS 1057.5 RBL. *S/D* REMOVED AND REPLACED 1057.6 MAIN FRAME RT SIDE, PER FEDEX SRM 53-10-2 AND BOEING DRAWING 65-20728.
- [SDR 96FDEA01260](https://openairdocs.org/sdr/96FDEA01260.md): Floor Beam · corrosion · Jul 16, 1996 · N195FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DISCREPANCY: NR 0259(033) CORROSION (C53-111-01) AROUND NUTPLATES AROUND EXISTING FLOOR BEAM REPAIR STA 600 RBL 1, 5, 8, 12, 15, 19, 24, WL 198 (FWD BAY). CORRECTIVE ACTION: *****S/D******** COMING.
- [SDR 96FDEA01259](https://openairdocs.org/sdr/96FDEA01259.md): Gusset · cracked · Jul 16, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0340 (032) FRAME GUSSET IS CRACKED AT BS 825, LBL 67, WL 197. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET AT BS 25, LBL 67, WL 197.
- [SDR 96FDEA01256](https://openairdocs.org/sdr/96FDEA01256.md): Shear Tie · corroded · Jul 15, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0225 (031) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25 LT FWD BAY. CORRECTIVE ACTION: *****S/D*****.
- [SDR 96FDEA01255](https://openairdocs.org/sdr/96FDEA01255.md): Shear Tie · corroded · Jul 15, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0225 (030) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25, LT FORWARD BAY. CORRECTIVE ACTION: REPAIRED SHEAR TIE, STA 540 LT BETWEEN STR 24-25 LT PER SRM 53-10-4.
- [SDR 96FDEA01254](https://openairdocs.org/sdr/96FDEA01254.md): Floorbeam · gouge · Jul 15, 1996 · N195FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DISCREPANCY: NR 0245 (029) FOUND GOUGES IN FLOORBEAM, STR 680 RBL 25, LBL 25 WL 198 (FORWARD BAY). CORRECTIVE ACTION: BLENDED GOUGES, ONE WAS OUT OF LIMITS IN FLOOR BEAM STA 600 RBL 4.75 WL 198 PER FEDEX SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED REPAI
- [SDR 96FDEA01253](https://openairdocs.org/sdr/96FDEA01253.md): Stringer · corroded · Jul 15, 1996 · N195FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: NR 0222 (028) CORROSION (C53-111-01 (2) ON STR FLANGE, STR 23 RT, STA 489 RT, FORWARD BAY. CORRECTIVE ACTION: REPAIRED STR AT BS 489, STR 23R PER FEDEX SRM 53-10-3, FIG 2.
- [SDR 96FDEA01261](https://openairdocs.org/sdr/96FDEA01261.md): Stringer · cracked · Jul 11, 1996 · N195FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: NR 0725 (034) WHILE WORKING NR 0722, FOUND CRACK UNDERNEATH FASTENER AT BS 540, STRINGER 24 LT. REPAIRED CRACK UNDERNEATH FASTENER AT BS 540, STR 24L PER FEDEX SRM 53-10-3.
- [SDR 96FDEA01248](https://openairdocs.org/sdr/96FDEA01248.md): Frame · corrosion · Jul 11, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: NR 0235 (027) CORROSION ON C-CHANNEL, STATION 532, RBL 26, WL 155. CORRECTIVE ACTION: REPAIRED DENT IN FRAME BS 540 BETWEEN STR 23 AND STR 24L, SRM 51-40-3.
- [SDR 96FDEA01295](https://openairdocs.org/sdr/96FDEA01295.md): Gate Beam · cracked · Jul 10, 1996 · N195FE · Boeing 72722 · Passenger/Crew Doors
  > NR 0143 040. FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED 2 EACH PLACES ADJACENT TO LOWER FORWARD STOP PIN FITTING. REMOVED AND REPLACED LOWER GATE BEAM PER FEDEX SRM 51-10-1.
- [SDR 96FDEA01229](https://openairdocs.org/sdr/96FDEA01229.md): Frame · corroded · Jul 9, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: NR 0581(021) CORROSION (C53-221-01) ON FRAME BS 251.6, WL 223, LBL 48. CORRECTIVE ACTION *****S/D***** REPAIRED FRAME STA 251.6, WL 223, LBL 48 IAW SRM 51-40-2.
- [SDR 96FDEA01228](https://openairdocs.org/sdr/96FDEA01228.md): Skin · oil canned · Jul 9, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0177, 020, OIL CANNED SKIN AT 1243 TO 1253 STR 22 TO 23 LT. *S/D* REPAIRED PER SRM 53-30-3 FIG 1.
- [SDR 96FDEA01246](https://openairdocs.org/sdr/96FDEA01246.md): Frame · dented · Jul 8, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: NR 0235 (025) FOUND DENT IN FRAME STA 540 BETWEEN STRINGERS 23 TO 24 LT FORWARD BAY. CORRECTIVE ACTION: REPAIRED DENT IN FRAME STA 540 BETWEN STR 23 - STR 24L, FWD BAY PER FEDEX SRM 51-40-3.
- [SDR 96FDEA01217](https://openairdocs.org/sdr/96FDEA01217.md): Bonding Jumper · corroded · Jul 8, 1996 · N195FE · Boeing 72722 · Leading Edge Devices
  > DISCREPANCY: NR 0551 (015) CORROSION (C57-562-01) NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER ATTACH POINT. CORRECTIVE ACTION: CORRODED AREA FOUND TO BE OUT OF LIMITS PER FEDEX DWG R 27-57-010. REPAIRED NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMP
- [SDR 96FDEA01216](https://openairdocs.org/sdr/96FDEA01216.md): Frame · corroded · Jul 8, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: NR 0579 (014) CORROSION (C53-221-01) ON FRAME BS 227.8 WL 226 AND 233 RBL 41-43 5. CORRECTIVE ACTION: **S/D** REPAIRED FRAME BS 227.8 W/L 226 AND 283 RBL 41 - 43.5 PER SRM 51-40-2.
- [SDR 96FDEA01211](https://openairdocs.org/sdr/96FDEA01211.md): Frame · corroded · Jul 8, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > DISCREPANCY: NR 0255 (011) CORROSION (C53-111-01) ON WEB/FRAME, BS 572, RBL 24-26 WL 157 FORWARD BAY. CORRECTIVE ACTION: REPAIRED WEB/FRAME BS 572, RBL 24-26, WL 157 IAW FEDEX EA 7-5310-29271.
- [SDR 96FDEA01210](https://openairdocs.org/sdr/96FDEA01210.md): Floor Beam · corroded · Jul 8, 1996 · N195FE · Boeing 72722 · Fuselage Main, Floor Beam
  > NR 0719, 010, CORROSION (C53-111-01) ON FLOOR BEAM STA 660 RBL 24 WL 198. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8.
- [SDR 96FDEA01243](https://openairdocs.org/sdr/96FDEA01243.md): Tripler · corroded · Jul 7, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0717 024, BS 1110 TO 1130, STR 26R, WL 152. SKIN IS BULGED. *S/D* OPENED SKIN LAP REMOVED THE CORROSION BY BLENDING.002 FROM AN AREA OF 6 BY 12 ON THE SKIN. REMOVED THE TRIPLER REINSTALLED FASTENERS, AREA IS WITHIN LIMITS AS PER SRM 53-30-1.
- [SDR 96FDEA01242](https://openairdocs.org/sdr/96FDEA01242.md): Chord · corroded · Jul 7, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0622 023 CORROSION ON UPPER CHORD BS 344, RBL 7 TO LBL 55, WL 208. ***S/D *** REMOVED AND REPLACED UPPER CHORD OF FLOOR AT STATION 344, RBL 65 TO LBL 65 IAW FED EX SRM 27-53-007.
- [SDR 96FDEA01241](https://openairdocs.org/sdr/96FDEA01241.md): Bulkhead Web · cracked · Jul 7, 1996 · N195FE · Boeing 72722 · Fuselage Main, Bulkhead
  > DISCREPANCY: NR 0711. FOUND CRACK ON WHEELWELL BULKHEAD STA 870, WL 190, LBL 50 (CENTER TANK). CORRECTIVE ACTION: REPAIRED PER SRM 53-10-9, FIG 4.
- [SDR 96FDEA01226](https://openairdocs.org/sdr/96FDEA01226.md): Bonding Jumper · corroded · Jul 7, 1996 · N195FE · Boeing 72722 · Leading Edge Devices
  > NR 0552, 018, CORROSION (C57-562-01) NR 3 K-FLAP TO BULLNOSE O/B BONDING JUMPER, UPPER LOWER ATTACH POINTS. *S/D* REPLACED NR 3 K-FLAP BULLNOSE, REPAIRED K-FLAP RIB AT O/B BONDING JUMPER UPPER ATTACH POINT IAW MM 27-81-1, SRM 57-50-3.
- [SDR 96FDEA01219](https://openairdocs.org/sdr/96FDEA01219.md): Bonding Jumper · corroded · Jul 7, 1996 · N195FE · Boeing 72722 · Leading Edge Devices
  > NR 0547, 007, CORROSION (C57-562-01) AT BOTH ATTACH POINTS ON THE O/B BONDING JUMPER ON THE NR 5 K-FLAP BULLNOSE. *S/D* REPAIRED UPPER ATTACH POINT PER FEDEX SRM 57-50-3 FIG 3, LOWER ATTACH POINT WITHIN LIMITS AFTER CORROSION REMOVAL PER FEDEX DWG R 27-57-01
- [SDR 96FDEA01273](https://openairdocs.org/sdr/96FDEA01273.md): Floorbeam · corroded · Jul 6, 1996 · N195FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DISCREPANCY: (NR 0743 (035) WHILE WORKING 0251, FOUND CORROSION ON FLOORBEAM LOWER CHORD BS 540 LBL 14 TO RBL 23 WL 200. CORRECTIVE ACTION: REPAIRED FLOORBEAM LOWER CHORD BS 540 LBL 14 - RBL 23 WL 200 PER FEDEX SRM 53-10-8.
- [SDR 96FDEA01227](https://openairdocs.org/sdr/96FDEA01227.md): Upper Lug · corroded · Jul 4, 1996 · N195FE · Boeing 72722 · Leading Edge Devices
  > NR 0549, 019, CORROSION (C57-562-01) ON THE O/B UPPER LUG O/B HINGE NR 4 K-FLAP. *S/D* REMOVED AND REPLACED K-FLAP PER MM 27-81-1.
- [SDR 96FDEA01215](https://openairdocs.org/sdr/96FDEA01215.md): Stringer · corroded · Jul 4, 1996 · N195FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: NR 00250 (013) CORROSION (C53-111-01) ON STR 27L CHANNEL STR 536-546 LT FORWARD BAY. CORRECTIVE ACTION: **S/D** REMOVED CORRODED SECTION OF STR FROM BS 530-550 STR 27L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 1.
- [SDR 96FDEA01218](https://openairdocs.org/sdr/96FDEA01218.md): Te Skin · disbonded · Jul 2, 1996 · N195FE · Boeing 72722 · Ailerons
  > NR 0464, 016, RIGHT WING O/B AILERON IS DELAMINATED AT O/B TRAILING EDGE. *S/D* REPAIRED O/B AILERON AT O/B TRAILING EDGE IAW FEDEX SRM 51-40-06.
- [SDR 96FDEA01204](https://openairdocs.org/sdr/96FDEA01204.md): Skin · corroded · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DISCREPANCY: NR 0205 (005). CORROSION (53-100-01). BS 1080 STR 26R, RBL 30 ON EXTERIOR SKIN AT LAP RBL 13, WL 208. REPAIRED DAMAGED AREA BS 1060 - 1080, STR 26R, RBL 30 ON EXTERIOR SKIN IAW FEDEX EA 7-5330-29612.
- [SDR 96FDEA01203](https://openairdocs.org/sdr/96FDEA01203.md): Intercostal · corroded · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 0572, 006, CORROSION (53-221-01) ON INTERCOSTAL BS 268 TO 277 RBL 13 WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL BS 268 TO 277 RBL 13 WL 208, DUE TO CORROSION BEING OUT OF LIMITS IAW FED-EX SRM 53-10-1.
- [SDR 96FDEA01202](https://openairdocs.org/sdr/96FDEA01202.md): Skin Panel · gouged · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > NR 0110, 004, BS 380 PLUS 15 WL 160, STR 23 TO 24R THERE IS A SHARP PROTRUDING DENTS IN SKIN. *S/D* REPAIRED DENT AT BS 380 PLUS 15 BETWEEN STR 23 AND 24 RIGHT PER SRM 53-30-3 FIG 3.
- [SDR 96FDEA01201](https://openairdocs.org/sdr/96FDEA01201.md): Clip · corrosion · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0274 (003) GOUGE IN STRING CLIP BS 910 STR 11 RT. ***S/D*** REMOVED STR CLIP AT BS 910, STR 11 RT, AND FOUND GOUGE TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED WITH NEW STRINGER CLIP.
- [SDR 96FDEA01200](https://openairdocs.org/sdr/96FDEA01200.md): Floor Beam · corroded · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Main, Floor Beam
  > DISCREPANCY: NR 0301 (002) CORROSION (53-113-01-27) ON LOWER FLANGE OF FLOORBEAM, BS 1110, BBL 50 TO LBL 30 AT THE NUTPLATE HOLES. ***S/D*** REMOVED CORROSION AND REPAIRED LOWER FLANGE OF FLOOR BEAM AT BS 1110, RBL 50 TO LBL 30, REFERENCE SRM 53-10-8, FIG
- [SDR 96FDEA01199](https://openairdocs.org/sdr/96FDEA01199.md): Frame · corroded · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Main, Frame
  > NR 0256, 001, CORROSION (C53-111-01) ON FRAME STR 580 BETWEEN STR 22 TO 25 LT FWD BAY 8. *S/D* CORROSION ON FRAME BS 580, BETWEEN STR 22 TO 25 LT IS OUT OF LIMITS PER SRM 53-10-01. REPAIRED FRAME PER SRM 51-40-3, ALODINED AND PRIMED ALL BARE METAL.
- [SDR 96FDEA01194](https://openairdocs.org/sdr/96FDEA01194.md): Intercostal · corroded · Jul 2, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0563 (007) CORROSION (C53-221-01) ON INTERCOSTAL BS 277-295, LBL 13 WL 208 ***S/D*** REMOVED AND REPLACED UPPER CHORD OF INTERCOSTAL, FLOOR SUPPORT BS 277 TO 295, LBL 13, WL 208. CORROSION FOUND TO BE OUT OF LIMITS.
- [SDR 96FDEA01214](https://openairdocs.org/sdr/96FDEA01214.md): Web · corroded · Jul 1, 1996 · N195FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NR 0574 (012) CORROSION (C53-221-01) ON UNDERSIDE OF HORIZONTAL WEB AND L-ANGLES BS 224-259, LBL 42-54, WL 224-236 CORRECTIVE ACTION: REPAIRED HORIZONTAL WEB BS 237 TO 259, LBL 42-54, WL 224-232, AND REPLACED L-ANGLES IAW SRM 51-40-2, DUE TO CO
- [SDR 96FDEA00720](https://openairdocs.org/sdr/96FDEA00720.md): Hydraulic Module · leaking · Mar 30, 1996 · N195FE · Boeing 72722 · Hydraulic System, Main
  > MAIN GEAR AND USED ALT FLAP EXT IN FLT AND BOTH A-SYS LOW PRESS LIGHT CAME ON, FOLLOWED BY OVERHEAT TO SYS. OVERHEAT LIGHT WENT OUT, BUT HAD A-SYS PRESS WITH GOOD A-SYS QTY. RED TAB PROCEDURE AND EWR MX SUGGESTIONS, DID NOT REGAIN A-SYS PRESS. NOTE - IN RIC
- [SDR 95FDEA01292](https://openairdocs.org/sdr/95FDEA01292.md): Chord · corrosion · Sep 12, 1995 · N195FE · Boeing 72722 · Wing Miscellaneous Structure
  > NR 0232 043. CORROSION C53-132-2(1) ON STA 870 LOWER CHORD LBL 70, 38-41, RBL 20, WL 156. REMOVED AND REPLACED BS 870 LOWER CHORD, LBL 70, WL 156 PER FEDEX EA 7-5710-29709.
- [SDR 95FDEA00314](https://openairdocs.org/sdr/95FDEA00314.md): Sliding Window · came open · Mar 18, 1995 · N195FE · Boeing 72722 · Flight Compartment Windows
  > ON ROTATION L/H SLIDING WINDOW CAME OPEN. TESTED CAPTS L2 WINDOW (SLIDING WINDOW) PER 727 MM 56-12-11 PG 505 PARA A, NO DEFECT NOTED. INSPECTED ENGINE INLETS AND EXHAUSTS, NO DEFECTS NOTED.

## 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 = 'N195FE' AND deregistration_id = 'N195FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N195FE-2002-10-15/reports

---
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