# Service difficulty reports: N185AW, cancelled Mar 28, 2003

A list on [N185AW, cancelled Mar 28, 2003](https://openairdocs.org/deregistered/N185AW-2003-03-28.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 · 118 reports

- [SDR AWXA200200009](https://openairdocs.org/sdr/AWXA200200009.md): Light · inoperative · Jan 7, 2002 · N185AW · Boeing 737277 · Emergency Lighting
  > PHX - EEL - C - DURING INSPECTION EMERGENCY LIGHT AT ROW 13 LT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.
- [SDR AWXA0002209](https://openairdocs.org/sdr/AWXA0002209.md): Actuator · failed · Aug 27, 2001 · N185AW · Boeing 737277 · Leading Edge Slat Actuator
  > LAX - AIR TURNBACK - FLT 115 - DURING DEPARTURE CLIMB THE NR 6 LEADING EDGE SLAT WAS EXTENDED WITH FLAPS SELECTED UP. THE AIRCRAFT ENCOUNTERED A ROLL TO THE LEFT, MAX SPEED WAS 250 KTS. THE AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING. IN LAX MAI
- [SDR AWXA0001922](https://openairdocs.org/sdr/AWXA0001922.md): Skin · corroded · Jul 5, 2001 · N185AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > D: Phx- during routine maitenance the lower lobe skin was found to have corrosion at BS727-727A between STR 27L and Str 27R.C: Repaired per SRM 53-10-01, 51-10-6 and AWA E.R. 15-5331-01179-JL2
- [SDR AWXA0001435](https://openairdocs.org/sdr/AWXA0001435.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AT FS 1153 RIGHT SIDE 12 INCHES ABOVE THE HORIZONTAL STABILIZER. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-30-03 FIG 2.
- [SDR AWXA0001449](https://openairdocs.org/sdr/AWXA0001449.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN RT BS 747 STR 17R. REPLACED FUSELAGE SKIN RT SIDE BS 727-817 STR 14R - 20R IAW AWA ER 15-5330-01045-JS1 AND SRM 51-30-02 PG 2 AND 51-30-01 PG 2&3.
- [SDR AWXA0001448](https://openairdocs.org/sdr/AWXA0001448.md): Stringer · damaged · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES THRU SKIN AND STRINGER AT FS 790 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049-DL1 AND SRM 53-10-03 FIG 1 AND 53-30-03 FIG 10.
- [SDR AWXA0001447](https://openairdocs.org/sdr/AWXA0001447.md): Stringer · damaged · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES THRU SKIN AND STRINGER AT FS 760 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049 DL2 AND SRM 53-10-03 FIG 1 AND 53-30-03 FIG 10.
- [SDR AWXA0001446](https://openairdocs.org/sdr/AWXA0001446.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > R2 SERVICE DOOR UPPER HINGE LWR AFT CORNER OF CUTOUT HAS A.125 INCH CRACK. REMOVED FASTENERS, ROUTED OUT CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-02 AND 51-30-02.
- [SDR AWXA0001445](https://openairdocs.org/sdr/AWXA0001445.md): Floorbeam · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 520 LBL 44 HAS A 3 INCH CRACK IN UPPER RADIUS AND HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING DOUBLERS AND REPAIRED IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 5.
- [SDR AWXA0001444](https://openairdocs.org/sdr/AWXA0001444.md): Floorbeam · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 520 LBL 24 HAS A 3 INCH CRACK IN UPPER RADIUS THAT HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING DOUBLERS AND INSTALLED REPAIR IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 2 & 5.
- [SDR AWXA0001443](https://openairdocs.org/sdr/AWXA0001443.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN CRACKED IN RADIUS AT L2 DOOR UPPER HINGE CUTOUT. INSTALLED SKIN REPAIR IAW SRM 53-30-03 AND 51-10-02.
- [SDR AWXA0001442](https://openairdocs.org/sdr/AWXA0001442.md): Tie Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 597 STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001441](https://openairdocs.org/sdr/AWXA0001441.md): Tie Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 727B STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001440](https://openairdocs.org/sdr/AWXA0001440.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 727A STR 6L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001439](https://openairdocs.org/sdr/AWXA0001439.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 727A 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001438](https://openairdocs.org/sdr/AWXA0001438.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 727B STR 4R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001437](https://openairdocs.org/sdr/AWXA0001437.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 787 STR 2R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001436](https://openairdocs.org/sdr/AWXA0001436.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CABIN STR CLIP AT FS 787 STR 5R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.
- [SDR AWXA0001434](https://openairdocs.org/sdr/AWXA0001434.md): Angle · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > NR 2 VHF ANTENNA SUPPORT ANGLE IS CRACKED OUT OF FASTENER HOLE ON RT SIDE AT FS 500 TO 500A BETWEEN STR 28L AND 28R. REMOVED CRACKED ANGLE AND SUPPORTING STRUCTURE; INSTALLED NEW SUPPORTS, CLIPS, ANGLE, FITTING AND DOUBLER IAW AWA EO 53-33-02 AND DWG 65C27810
- [SDR AWXA0001433](https://openairdocs.org/sdr/AWXA0001433.md): Web · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Cargo/Baggage Doors
  > AFT CARGO DOOR INTERNAL WEB IS CRACKED AT ATTACH POINT TO LWR CROSS BEAM, LOCATED IN CENTER OF DOOR BELOW HANDLE MECHANISM. INSTALLED FILLER AND DOUBLER IAW SRM 51-10-03, 52-30-01, 51-10-01, 51-30-02 AND 51-40-03.
- [SDR AWXA0001432](https://openairdocs.org/sdr/AWXA0001432.md): Stringer Clip · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > STRINGER CLIP AT FS 807, STRINGER 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-01 PG 5.
- [SDR AWXA0001431](https://openairdocs.org/sdr/AWXA0001431.md): Skin · buckled · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > KEEL BEAM SKIN PANEL BETWEEN GEAR WELLS BUCKLED AND HAS LOOSE RIVETS. REMOVED AND REPLACED KEEL BEAM SKIN PANEL IAW ER 15-5331-01040-JS2.
- [SDR AWXA0001430](https://openairdocs.org/sdr/AWXA0001430.md): Door Frame · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Structure
  > CRACK IN L2 DOOR JAMB FWD UPPER WEB AT BS 947. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 51-40-03.
- [SDR AWXA0001429](https://openairdocs.org/sdr/AWXA0001429.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER SKIN HAS A 1 INCH CRACK AT LIGHTENING HOLE BELOW HANDLE MECHANISM. STOP DRILLED CRACK; FABED, DRILLED, TREATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, 51-10-01, 51-30-01.
- [SDR AWXA0001428](https://openairdocs.org/sdr/AWXA0001428.md): Web · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > FLOOR WEB ON AFT SIDE OF FS 178 BLKHD SIDE CHORD AREA CRACKED. REPAIRED FLOOR WEB IAW SRM 53-20-04 PG 1-7, SRM 51-30-01 PG 2, 3, 5, 32, SRM 51-10-03 PG 1-10, SRM 51-10-01 PG 20-24 AND B737-200 MM 51-21-41 PG 702-706.
- [SDR AWXA0001427](https://openairdocs.org/sdr/AWXA0001427.md): Web · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > FLOOR WEB ON AFT SIDE OF BS 178 BLKHD SIDE CHORD AREA AT WL 207 CRACKED. REPLACED FLOOR WEB IAW SRM 51-20-4 PG 1-7, SRM 51-30-5 PG 32, 2, 3, 5, SRM 51-40-03 PG 1-10, SRM 51-10-01 PG 20-24 AND MM 51-21-41 PG 702-706.
- [SDR AWXA0001426](https://openairdocs.org/sdr/AWXA0001426.md): Bulkhead · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Bulkhead
  > FS 178 BLKHD HAS 3 CRACKS IN WEB MEASURING 1.3, 0.2, AND 0.3 INCH. REPAIRED WEB IAW SRM 53-10-02 PG 3, 5, 8-10, 53-10-11 PG 1-8, 53-30-02 PG 2, 3, 5, 32, 51-20-04 PG 1-7 AND B737-200 MM 51-21-40 PG 702-706.
- [SDR AWXA0001425](https://openairdocs.org/sdr/AWXA0001425.md): Skin · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Passenger/Crew Doors
  > FWD ENTRY DOOR INNER SKIN CRACKED AT UPPER FWD ACCESS OPENING. FABED REPAIR DOUBLER AND INSTALLED IAW B737-200 SRM 51-40-02.
- [SDR AWXA0001424](https://openairdocs.org/sdr/AWXA0001424.md): Bulkhead · cracked · Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Bulkhead
  > FS 178 BLKHD HAS A CRACK IN WEB EMINATING FROM FASTENER HOLE. CUT OUT DAMAGED AREA; HFEC CONFIRMS NO CRACKS ON EDGE OF CUTOUT. FABED, DRILLED AND INSTALLED FILLER AND DOUBLER IAW B737-200 SRM 53-30-02.
- [SDR AWXA0001230](https://openairdocs.org/sdr/AWXA0001230.md): Bearing · worn · Jan 11, 2001 · N185AW · Boeing 737277 · Elevator Control System
  > ON LANDING FLARE IN SFO THE ELEVATOR CONTROL WAS STIFF. PERFORMED OPERATIONAL AND VISUAL INSPECTION OF ELEV CONTROL SYSTEM, NO DEFECTS NOTED. DUE TO PRIOR REPORT OF STIFF ELEV; BOEING WAS CONSULTED; PER THEIR RECOMMENDATION THE ELEV TORQUE TUBE BEARINGS WERE
- [SDR AWXA0001116](https://openairdocs.org/sdr/AWXA0001116.md): Wire · chafed · Dec 18, 2000 · N185AW · Boeing 737277 · Engine Starting System Wiring
  > D: PHX - AIR TURNBACK - NR 1 START VALVE LIGHT ILLUMINATED IN FLIGHT AT 250 KTS. 18000 FEET; WENT THROUGH QRH AND SHUTDOWN THE ENGINE; START VALVE OPEN LIGHT EXTINGUISHED WHEN THE ENGINE WAS SHUT DOWN. REMOVED AND REPLACED THE START VALVE; DURING START VALVE R
- [SDR AWXA0000150](https://openairdocs.org/sdr/AWXA0000150.md): Support Bracket · cracked · Mar 22, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN SKIN SUPPORT BRACKET CRACKED 1.5 IN AT STR 13R BETWEEN FS 277 - 294.5. REMOVED BRACKET IAW 737 SRM 51-30-2, FABRICATED REPLACEMENT IAW 737 SRM 51-20-1 FIG 7 FROM (.050 7075 T6 R698980), INSTALLED PART IAW 737 SRM 51-30-02.
- [SDR AWXA0000149](https://openairdocs.org/sdr/AWXA0000149.md): Flap Track · corroded · Mar 22, 2000 · N185AW · Boeing 737277 · Trailing Edge Flaps
  > C-CHECK CORROSION LEVEL 2, SURFACE CORROSION ON AFT MOUNT PAD ON LT WING NR 1 FLAP TRACK. REMOVED AND REPLACED LT WING NR 1 FLAP TRACK PER TASK CARD R3L27002.
- [SDR AWXA0000148](https://openairdocs.org/sdr/AWXA0000148.md): Flap Track · corroded · Mar 22, 2000 · N185AW · Boeing 737277 · Trailing Edge Flaps
  > C-CHECK CORROSION LEVEL 2, SMALL AREA OF SURFACE CORROSION AT I/B FWD MOUNT LOBE ON LT WING NR 2 FLAP TRACK. REMOVED AND REPLACED LT WING NR 2 FLAP TRACK PER TASK CARD R3L27003.
- [SDR AWXA0000076](https://openairdocs.org/sdr/AWXA0000076.md): Skin · cracked · Feb 10, 2000 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 770 STR 17L. REMOVED TEMP REPAIR IAW 737 SRM 53-30-3 FIG 6, HFEC IAW 737NTM PT6 AND IG 23, NO CRACK NOTED. FABRICATED REPAIR DOUBLER IAW 737 SRM 51-10-2 FRM (.090 2024T3 R 710338). INSTALLED REPAIR DOUBLER AND COUNTERSINK WASH
- [SDR AWXA0000075](https://openairdocs.org/sdr/AWXA0000075.md): Frame · cracked · Feb 10, 2000 · N185AW · Boeing 737277 · Cargo/Baggage Doors
  > AFT CARGO DOOR T-CHORD AND LOWER BEAM ARE CRACKED. REMOVED DAMAGED T CHORD AND BEAM IAW 737 SRM 51-30-2. FABRICATED REPLACEMENT PARTS FRM (BAC 1505 10057TMS60-10058 2024 T3511 R7377114), ALODINED AND PRIMED IAW 737 SRM 51-10-2. INSTALLED PARTS IAW 737 SRM 5
- [SDR AWXA0000074](https://openairdocs.org/sdr/AWXA0000074.md): Web · cracked · Feb 9, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > CRACK IN LT OUTBD FLOOR LEVEL WEB AT STA 618 LT, LBL 75 (UNDER EMER EXIT). REMOVED WEB IAW 737 SRM 51-30-2, FABRICATED REPLACEMENT WEB IAW SRM 737 53-10-2 FIG 13 AND DWG 65-47973 FRM (7075 T6.032 R672714). TREATED AND PRIMED IAW 737 SRM 51-10-2. INSTALLED
- [SDR AWXA0000073](https://openairdocs.org/sdr/AWXA0000073.md): Shear Tie · cracked · Feb 9, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > SHEAR TIE AT FS 639 STR 4R CRACKED. REMOVED AND REPLACED SHEAR TIE IAW 737 SRM 51-30-02.
- [SDR AWXA0000072](https://openairdocs.org/sdr/AWXA0000072.md): Tie Clip · cracked · Feb 9, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > HORIZONTAL STAB BOX INTERIOR STA 1121 STR 2R FRAME TO STR TIE CLIPIS CRACKED. REMOVED TIE CLIP IAW 737 SRM 51-30-2. FABRICATED TIE CLIP PER DWG 69-40367 AND 737 SRM 53-10-4 FIG 6. TREATED AND PRIMED CLIP IAW 737 SRM 51-10-2. INSTALLED CLIP IAW 737 SRM 51-3
- [SDR AWXA0000071](https://openairdocs.org/sdr/AWXA0000071.md): Tie Clip · cracked · Feb 8, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK CRACK, NR 527831, STRINGER CLIP FS 277 STR 15R CRACKED. REMOVED STRINGER CLIP IAW 737 SRM 51-30-2. FABRICATED REPAIR PART FRM (7075T6.040 R699649), ALONDINED AND PRIMED IAW 51-10-6. INSTALLED CLIPS IAW 737 S
- [SDR AWXA0000070](https://openairdocs.org/sdr/AWXA0000070.md): Stringer · cracked · Feb 8, 2000 · N185AW · Boeing 737277 · Fuselage Main, Longeron/Stringer
  > C-CHECK, L-1 DOOR FUSELAGE INTERIOR DOOR CUT-OUT, AFT SIDE OF STR 14L STA 344 CRACKED. REMOVED AND REPLACED CRACKED STRINGER SPLICE AT STA 344 STR 14L AFT OF L-1 DOOR IAW 737 SRM 51-30-2 (NEW PART).
- [SDR AWXA0000069](https://openairdocs.org/sdr/AWXA0000069.md): Skin · delaminated · Feb 8, 2000 · N185AW · Boeing 737277 · Cargo/Baggage Doors
  > C-CHECK, FWD CARGO DOOR EXT SKIN DELAMINATED APPROX 4 AREA. REMOVED FWD CARGO DOOR, REMOVED DAMAGE SKIN IAW 737 SRM 52-30-1,FABRICATED REPLACEMENT SKIN IAW 737 SRM 52-30-1 FRM (.071 2024 T3QQA 250/5). TREATED AND PRIMED SKIN IAW 737 SRM 51-10-6, INSTALLED S
- [SDR AWXA0000068](https://openairdocs.org/sdr/AWXA0000068.md): Angle · corroded · Feb 8, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, FWD CABIN, R-1 DOOR CUSP ANGLE CORRODED FS 312. REMOVED R-1 DOOR CUSP ANGLE, FAB'D REPAIR PARTS FRM (7075-0R710361.080 HEATED TO T6) IAW 737 SRM 53-10-2. TREATED AND PRIMED IAW 737 SRM 51-10-2, INSTALLED REPLACEMENT PARTS IAW 737 SRM 53-10-2.
- [SDR AWXA0000067](https://openairdocs.org/sdr/AWXA0000067.md): Shear Tie · gouged · Feb 8, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, HORIZONTAL STAB BOX INT, FS 1121, BTW STR 2 R AND STR 3 R, FRAME SHEAR TIE HAD GOUGES IN RADIUS. REMOVED DAMAGE SHEAR TIE IAW 737 SRM 51-30-2, FAB'D REPLACEMENT SHEAR TIE FRM (7075T6 QQA 250/13 R 676547.040) IAW 737 SRM 53-10-4 FIG 6, TREATED AND PR
- [SDR AWXA0000064](https://openairdocs.org/sdr/AWXA0000064.md): Tie Clip · cracked · Feb 7, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, HORIZONTAL STAB BOX INT FS 1138 STR 2L FRAME TO STR TIE CLIP BENT/CRACKED. REMOVED CRACKED TIE CLIP IAW 737 SRM 51-30-2, FABRICATED REPLACEMENT CLIP, FRM (7075T6.032 R 672714) IAW 737 SRM 53-10-4, ALODINED AND PRIMED IAW 737 SRM 51-20-2, INSTALLED
- [SDR AWXA0000063](https://openairdocs.org/sdr/AWXA0000063.md): Floorbeam · corroded · Feb 7, 2000 · N185AW · Boeing 737277 · Fuselage Main, Floor Beam
  > C-CHECK, CORROSION LEVEL 1. FWD CABIN FS 312, LBL 24 TO RBL 28 FLOORBEAM UPPER T WEB CORRODED. REMOVED CORRODED T CAP IAW 737 SRM 51-30-2, FABRICATED REPLACEMENT PARTS IAW 737 SRM 53-10-2 FRM (BAC 1505-100617-7075-T6 QQA 200/11 R696033 AND BHC 506-43-70T7 AM
- [SDR AWXA0000062](https://openairdocs.org/sdr/AWXA0000062.md): Bracket · cracked · Feb 4, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN FLOORBEAM SUPPORT BRACKET AT FS 639 BL 0 TO LBL 48 WAS CRACKED AT LOWER END. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2 (NEW PART).
- [SDR AWXA0000061](https://openairdocs.org/sdr/AWXA0000061.md): Angle · cracked · Feb 4, 2000 · N185AW · Boeing 737277 · Wing Miscellaneous Structure
  > C-CHECK, PANEL SUPPORT ANGLE CRACKED PAST STOP DRILL, ON LT WING UPPER SURFACE UNDER PANEL 6301 UPPER FWD PYLON PANEL. REMOVED DAMAGED ANGLE IAW 737 SRM 51-30-2, FABRICATED NEW REPAIR ANGLE FRM (2024-0.063 R700214) IAW 737 SRM 51-20-1, H/T TO 2024-T4 ALODINE
- [SDR AWXA0000060](https://openairdocs.org/sdr/AWXA0000060.md): Channel · corroded · Feb 4, 2000 · N185AW · Boeing 737277 · Fuselage Miscellaneous Structure
  > C-CHECK, CORROSION -- LEVEL NOT DETERMINED. R-2 DOOR FRAME STRUCTURE CORRODED AT LOWER AFT CORNER STA 840-847. REMOVED DAMAGED DOOR FRAME ANGLE IAW 737 SRM 51-40-2, FABRICATED REPAIR ANGLE IAW 737 SRM 51-20-1, FLAT PATTERN LAYOUT FRM (7075-0 BAC 1510-434 R
- [SDR AWXA0000059](https://openairdocs.org/sdr/AWXA0000059.md): Skin · cracked · Feb 4, 2000 · N185AW · Boeing 737277 · Fuselage Main, Plate/Skin
  > C-CHECK, L-1 DOOR UPPER HINGE CUTOUT HAD.3/4 CRACK ON EXT FUSELAGE. REMOVED DAMAGED AREA IAW 737 SRM 53-30-3 FIG 21 SHT 3, HEEC IAW 737 NTM PT 6 51-00-00. NO CRACKS NOTED, FABRICATED DOUBLER AND FILLER IAW 53-30-3 FRM (2024 T3.036) BOND CLAD, INSTALLED CO

Next page: https://openairdocs.org/deregistered/N185AW-2003-03-28/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 = 'N185AW' AND deregistration_id = 'N185AW-2003-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N185AW-2003-03-28/reports

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