# Service difficulty reports: N169AW, cancelled May 31, 2002 A list on [N169AW, cancelled May 31, 2002](https://openairdocs.org/deregistered/N169AW-2002-05-31.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 · 62 reports - [SDR AWXA0001727](https://openairdocs.org/sdr/AWXA0001727.md): Actuator · failed · May 14, 2001 · N169AW · Boeing 73733A · Leading Edge Slat Actuator > PHX - AIR TURNBACK, AFTER TAKEOFF THE FLAPS WERE RETRACTED BUT L/E FLAPS TRANSIT LIGHT ON FORWARD PANEL AND NR 1 SLAT INDICATOR ON THE OVERHEAD PANEL REMAINED ILLUMINATED. FLAPS WERE CYCLED BACK TO 1 & THEN UP SEVERAL TIMES. PILOT VISUALLY CONFIRMED THAT NR - [SDR AWXA0001691](https://openairdocs.org/sdr/AWXA0001691.md): Floorbeam · corroded · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > THREE SPOTS OF CORROSION ON UPPER FLANGE OF FLOORBEAM BS 294 RBL 28-31. REMOVED CORRODED SECTION; FORMED AND INSTALLED SECTION OF UPPER T-CHORD IAW B737 SRM 51-20-01 PG 1 AND 51-40-05 PG 3 AND 53-10-08 PG 12 AND 53-00-51 PG 207 AND 51-10-02 PG 2. - [SDR AWXA0001692](https://openairdocs.org/sdr/AWXA0001692.md): Bulkhead · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > BS 178 BLKHD WEB RBL 5 WL 200 HAS A.60 INCH CRACK EMANATING FROM BENEATH THE STRAP. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED, INSTALLED REPAIR DOUBLER AND FILLER IAW B737 SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001690](https://openairdocs.org/sdr/AWXA0001690.md): Structure · cracked · May 1, 2001 · N169AW · Boeing 73733A · Cargo/Baggage Doors > FS 837 AFT CARGO DOOR, CRACK AT LWR CROSS BEAM, LOWER TEE, VERT LEG, 3RD HI-LOK FROM END BEAM. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR FILLERS, DOUBLERS AND STRAPS IAW AWA EO 52-33-01 REV D PG 1-15. - [SDR AWXA0001689](https://openairdocs.org/sdr/AWXA0001689.md): Stiffener · corroded · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > FS 294 TEE CAP STIFFENER CORRODED RBL 28-43. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW TEE CAP STIFFENER IAW B737-300 SRM 51-40-02 PG 1-10. - [SDR AWXA0001688](https://openairdocs.org/sdr/AWXA0001688.md): Web · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > FS 178 COCKPIT FLOOR WEB CRACKED AT RBL 23 WL 207. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW WEB SECTION IAW B737-300 SRM 51-40-02 PG 1-6 & 51-10-02 PG 15. - [SDR AWXA0001687](https://openairdocs.org/sdr/AWXA0001687.md): Stiffener · corroded · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > FS 1153 TORQUE BOX LEFT LWR O/B EDGE OF STIFFENER. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-70-13 FIG 1 PG 1. - [SDR AWXA0001686](https://openairdocs.org/sdr/AWXA0001686.md): Bulkhead · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD CRACKED 2 PLACES LBL 4 & 1.2, RBL 8 WL 187-188. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001685](https://openairdocs.org/sdr/AWXA0001685.md): Skin · cracked · May 1, 2001 · N169AW · Boeing 73733A · Cargo/Baggage Doors > AFT CARGO COMPT UPPER LINER SKIN CRACKED AT CENTER LIGHTENING HOLE. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-40-02 PG 3. - [SDR AWXA0001684](https://openairdocs.org/sdr/AWXA0001684.md): Bulkhead · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD CRACK AT WL 202.5 RBL 4.8. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001683](https://openairdocs.org/sdr/AWXA0001683.md): Bulkhead · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD CRACKED AT WL 234.1 RBL 7.8-9.7. CUT OUT DAMAGED AREA, LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 265-269. - [SDR AWXA0001682](https://openairdocs.org/sdr/AWXA0001682.md): Frame · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Frame > FS 178 BLKHD CRACK AT WL 187-230 CENTER OF RADIUS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-10-02 PG 15 & 51-40-02 PG 1, 10. - [SDR AWXA0001681](https://openairdocs.org/sdr/AWXA0001681.md): Skin · corroded · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Plate/Skin > BLIND RIVET REPAIR FORWARD OF AFT PRESSURE BLKHD BS 1012 STR 23L WL 182. REMOVED DOUBLER REPAIR WITH BLIND FASTENERS; FORMED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-20-01, 53-00-01 FIG 202 PG 204. - [SDR AWXA0001680](https://openairdocs.org/sdr/AWXA0001680.md): Bulkhead · cracked · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD CRACK AT WL 202.4 LBL 4.5. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001679](https://openairdocs.org/sdr/AWXA0001679.md): Floorbeam · corroded · May 1, 2001 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > CORROSION ON AFT CORNER OF TRACK SECTION AND UPPER FLANGE OF FLOORBEAM AT BS 294 RBL 12-14; CORROSION REMOVAL OUT OF LIMITS. REMOVED FLOORBEAM T-CAP SECTION; LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW T-CAP UPPER CORD IAW B737 SRM 51-40-05 PG 7 AND 5 - [SDR AWXA0001650](https://openairdocs.org/sdr/AWXA0001650.md): Bulkhead · cracked · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD HAS 1 INCH CRACK AT WL 197-198 LBL 4.8. CUT OUT DAMAGED WEB; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001654](https://openairdocs.org/sdr/AWXA0001654.md): Bulkhead · cracked · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178.5 BLKHD CRACK AT WL 188 LBL 5.7. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW AWA ER 03-5313-01109-TB1. - [SDR AWXA0001653](https://openairdocs.org/sdr/AWXA0001653.md): Bulkhead · cracked · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD HAS 1 INCH CRACK AT WL 206 RBL.6-1.8. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001652](https://openairdocs.org/sdr/AWXA0001652.md): Bulkhead · cracked · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 BLKHD HAS 1.5 INCH CRACK AT WL 200.3 LBL 5. CUT OUT DAMAGD AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 TR 53-15 PG 1-11. - [SDR AWXA0001651](https://openairdocs.org/sdr/AWXA0001651.md): Web · punctured · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > PUNCTURE IN VERT WEB RBL 44 FS 311.CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-11 PG 1 AND 51-20-01 PG 1 AND 51-40-02 PG 3 & 4. - [SDR AWXA0001649](https://openairdocs.org/sdr/AWXA0001649.md): Bulkhead · canning · Apr 26, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > FS 178 OIL CANNING AT WL 188-207 LBL 5 TO RBL 5. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 1-11. - [SDR AWXA0001644](https://openairdocs.org/sdr/AWXA0001644.md): Bulkhead · cracked · Apr 24, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > HFEC INDICATES.5 INCH CRACK EMANATING FROM BENEATH STRAP IN WEB BS 178 BLKHD RBL 6.8 WL 212.5 CONFIRMED 10X VISUAL. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08. - [SDR AWXA0001629](https://openairdocs.org/sdr/AWXA0001629.md): Bulkhead · cracked · Apr 24, 2001 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > HFEC INDICATES CRACK AT FASTENER HOLE LBL 10 WL 234.1 BS 179 BLKHD WEB FORWARD SIDE. CUT OUT DAMAGED SKIN AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08. - [SDR AWXA0001628](https://openairdocs.org/sdr/AWXA0001628.md): Pressure Panel · cracked · Apr 24, 2001 · N169AW · Boeing 73733A · Fuselage Main, Structure > LEFT MLG W/W PRESSURE WEB CRACKED AT BS 663 APPROX BL 32. REMOVED UPPER ATTACH CHANNEL; TRIMMED OUT DAMAGED PORTION OF WEB; FABBED REPAIR -1 DOUBLER, -2 FILLER AND -3 STIFFENER; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR AND THE UPPER ATTACH CHANNEL IA - [SDR AWXA0001168](https://openairdocs.org/sdr/AWXA0001168.md): Wire · broken · Jan 2, 2001 · N169AW · Boeing 73733A · Light System Wiring > EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B FAILED TO ILLUMINATE DURING TEST. FOUND BROKEN WIRE AT SEAT 2B; SPLICED THE WIRE AND LIGHT OPS CHECKED GOOD - [SDR AWXA0000243](https://openairdocs.org/sdr/AWXA0000243.md): Frame · corroded · Apr 6, 2000 · N169AW · Boeing 73733A · Fuselage Main, Frame > C-CHECK, LEVEL 1 CORROSION AFT PRESS BULKHEAD CHORD AT RBL 2 IN BILGE AREA. REMOVED DAMAGED CHORD SEGMENT AND REPAIRED IAW ER 03-5312-00075-022 AND 737 SRM 53-80-08 FIG 206. - [SDR AWXA0000242](https://openairdocs.org/sdr/AWXA0000242.md): Stiffener · corroded · Apr 6, 2000 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > C-CHECK, LEVEL 1 CORROSION FS 1016 AFT PRESS BULKHEAD BELOW FLOOR ON STIFFENER AT CENTERLINE RT SIDE. REMOVED DAMAGED AREA, FABRICATED STIFFENER AND FILLER FROM SHT 2024 T3.040 QQA250/5, TREATED, PRIMED, AND INSTALLED IAW 737 SRMS 51-70-11 FIG 1, 51-20-01, A - [SDR AWXA0000241](https://openairdocs.org/sdr/AWXA0000241.md): Bulkhead · corroded · Apr 6, 2000 · N169AW · Boeing 73733A · Fuselage Main, Bulkhead > C-CHECK, LEVEL 1 CORROSION AFT PRESSURE BULKHEAD BELOW BL 0 TO RBL 3. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS FROM 2024 T3.032 IAW 737 SRM 53-80-08 FIG 201. INSTALLED PARTS IAW 737 SRM 53-80-08. - [SDR AWXA0000240](https://openairdocs.org/sdr/AWXA0000240.md): Skin · delaminated · Apr 5, 2000 · N169AW · Boeing 73733A · Trailing Edge Flaps > C-CHECK, LT WING I/B MID FLAP HAS AREA OF DELAMINATION 36 INCHES I/B FROM O/B END AND 2.5 INCHES UP FROM T/E UPPER AND LOWER SURFACE. REMOVED DELAMINATED SECTION, POTTED CORE DAMAGE AND FABRICATED DOUBLER IAW 737 SRM 57-53-00 AND 51-70-10 BONDED USING HOT BON - [SDR AWXA0000239](https://openairdocs.org/sdr/AWXA0000239.md): Floorbeam · cracked · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, REPAIR DOUBLER ON AFT FACE OF FLOORBEAM AT BS 520 LBL 45.5 CRACKED IN RADIUS.5 INCH. REMOVED DAMAGED DOUBLER AND REPAIRED IAW AWA EO 53-14-12. - [SDR AWXA0000238](https://openairdocs.org/sdr/AWXA0000238.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, FLOOR SUPPORT AT FS 950 LBL 50 - LBL 20 CORRODED AT FASTENER HOLES. REMOVED AND REPLACED DAMAGED PARTS IAW 737 SRM 51-40-02, FABRICATED SUPPORT FROM BAC 1506-43 7050 T76511, SHIM 7075T6.080 IAW 737 SRM 51-40-02, TREATED AND PRIMED IAW 737 SRM 53-60- - [SDR AWXA0000237](https://openairdocs.org/sdr/AWXA0000237.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, TOP SURFACE OF FLOOR SUPPORT BEAM FROM FS 1016 LBL 5 TO FS 986 LBL 20 HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW 737 SRM 51-40-02, FABRICATED REPAIR PARTS IAW 737 SRM 51-20-02 FROM 2024T3.063 7075T6.125, TREATED AND PRIMED IAW - [SDR AWXA0000236](https://openairdocs.org/sdr/AWXA0000236.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, STA 1016 FLOORBEAM UPPER T FLANGE CORRODED AT LBL 5. CUT OUT DAMAGED AREA IAW 737 SRM 53-00-5, FABRICATED REPAIR SECTION FROM (BAC 1505-100617 7075T73), TREATED AND PRIMED IAW 737 SRM 51-20-01, INSTALLED IAW 737 SRM 51-40-02, PARTS ALODINED AND PRIME - [SDR AWXA0000235](https://openairdocs.org/sdr/AWXA0000235.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, FS 967 RBL 44 UPPER T-CAP CORRODED. CUT OUT DAMAGED AREA 737 SRM 53-30-51, FABRICATED REPAIR PARTS IAW 737 SRM 53-30-51, INSTALLED PARTS IAW 737 SRM 53-30-51 FIG 202, MAT''L USED ANGLE, BAC 1490-2887 7075T6 FILLER.125 7075 T6. - [SDR AWXA0000234](https://openairdocs.org/sdr/AWXA0000234.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, FLOORBEAM AT BS 967 RBL 6 CORRODED. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS IAW 737 SRM 53-00-51, TREATED AND PRIMED IAW 737 SRM 51-20-02, INSTALLED REPAIR PARTS IAW 737 SRM 51-40-02, MAT USED: SUPPORT ANGLE BAC 1505-100617, STRAPS.063 Q - [SDR AWXA0000233](https://openairdocs.org/sdr/AWXA0000233.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, FLOORBEAM FS 1006 CORRODED AT FASTENER HOLE RBL 12. REMOVED DAMAGED AREA IAW 737 SRM 53-00-51 FIG 202, FABRICATED REPAIR STRAP FROM.125 7075 T6, ALODINED AND PRIMED STRAP, INSTALLED STRAP IAW 737 SRM 53-00-51 FIG 202. - [SDR AWXA0000232](https://openairdocs.org/sdr/AWXA0000232.md): Threshold · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > C-CHECK, L-2 DOOR MOP SILL ANGLE HAS EXFOLIATING INTERGRANULAR CORROSION AT DOOR THRESHOLD AREA. REMOVED AND REPLACED L-2 MOPSILL IAW 737 SRM 51-40-02 AND SRM 51-20-02 (NEW PART). - [SDR AWXA0000231](https://openairdocs.org/sdr/AWXA0000231.md): Skin · cracked · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Plate/Skin > C-CHECK, L-1 DOOR LOWER HINGE CUTOUT IN FUSELAGE SKIN HAS VISUAL INDICATION OF CRACK. HFEC INSP IAW 737 NTM PT 6, STOP DRILLED.25 INCH CRACK IAW 737 SRM 53-10-01, FABRICATED REINFORCING PLATE DOUBLER FROM SHT 301 1/2H.063, INSTALLED IAW 737 SRM 51-40-21 AND - [SDR AWXA0000230](https://openairdocs.org/sdr/AWXA0000230.md): Floorbeam · corroded · Apr 5, 2000 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > C-CHECK, FLOORBEAM AT 986.5 TOP T-ANGLE CORRODED FROM RBL 20 TO LBL 20 (PREVIOUS REPAIR). REMOVED DAMAGED SECTION IAW 737 SRM 53-00-51, FABRICATED PART AND INSTALLED IAW 737 SRM 53-00-51 AND 51-40-02, ALODINED AND PRIMED PARTS IAW 737 SRM 51-10-02, MAT USED: - [SDR AWXA9800187](https://openairdocs.org/sdr/AWXA9800187.md): Fuse · blown · Aug 5, 1998 · N169AW · Boeing 73733A · Emergency Lighting > SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP AT ROWS 19 THROUGH 23 LEFT. FOUND BLOWN FUSE ON BATTERY CHARGER. REPLACED FUSE, CORRECTED SHORTING CONDITION. OPS CK GOOD. - [SDR AWXA9800137](https://openairdocs.org/sdr/AWXA9800137.md): Indicator · malfunctioned · May 28, 1998 · N169AW · Boeing 73733A · Trailing Flap Position Indicating System > FLAPS DID NOT DEPLOY WITH PRIMARY CONTROL, ALTERNATE OK. REMOVED AND REPLACED FLAP POSITION INDICATOR PER 27-58-41, OPS GOOD ON GROUND AT THIS TIME. - [SDR AWXA9800030](https://openairdocs.org/sdr/AWXA9800030.md): Skin · cracked · Jan 6, 1998 · N169AW · Boeing 73733A · Fuselage Main, Plate/Skin > DURING SCHEDULED C-13 INSPECTION, FOUND CRACK ON EXTERNAL SKIN AT FWD GALLEY DOOR THRESHOLD AFT LOWER CORNER. SKIN CRACK IN EXTERNAL SKIN AT LOWER AFT CORNER OF FWD GALLEY DOOR CUTOUT. STOP DRILLED, FABRICATED DOUBLER AND TRIPLER PARTS AND INSTALLED DOUBLER - [SDR AWXA9800029](https://openairdocs.org/sdr/AWXA9800029.md): Stringer · corroded · Dec 23, 1997 · N169AW · Boeing 73733A · Fuselage Main, Longeron/Stringer > DURING SCHEDULED C-13 INSPECTION, FOUND CORROSION ON STR 27 LT, BS 947 - 954. REPAIRED STRINGER 27 LT, BS 947-954 IAW, SRM 53-00-03 AND 51-40-2. - [SDR AWXA9600741](https://openairdocs.org/sdr/AWXA9600741.md): Wire · broken · Dec 12, 1996 · N169AW · Boeing 73733A · Light System Wiring > DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 3 EMERGENCY LIGHT INOP. FOUND BROKEN WIRE. REPLACED SPLICE, OPS CHECK GOOD. - [SDR AWXA9600753](https://openairdocs.org/sdr/AWXA9600753.md): Seat Track · corroded · Dec 9, 1996 · N169AW · Boeing 73733A · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 25, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 25, WL 208 IN ACCORDANCE WITH SRM 53-00-52. - [SDR AWXA9600756](https://openairdocs.org/sdr/AWXA9600756.md): Carriage · corroded · Dec 5, 1996 · N169AW · Boeing 73733A · Trailing Edge Flaps > DURING ROUTINE MAINTENANCE CHECK, FOUND R/W OUTBOARD MID FLAP INBOARD CARRIAGE SPINDAL CORRODED. REMOVED AND REPLACED R/W O/B MID FLAP I/B CARRIAGE PER MM 27-51-44. - [SDR AWXA9600754](https://openairdocs.org/sdr/AWXA9600754.md): Seat Track · corroded · Dec 4, 1996 · N169AW · Boeing 73733A · Fuselage, Seat/Cargo Attach Fittings > DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 45, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 45, WL 258 IN ACCORDANCE WITH SRM 53-00-52. - [SDR AWXA9600757](https://openairdocs.org/sdr/AWXA9600757.md): Floorbeam · corroded · Dec 3, 1996 · N169AW · Boeing 73733A · Fuselage Main, Floor Beam > DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 294.5, WL 208, RBL 14 TO LBL 2. REPAIRED FLOORBEAM UPPER CHORD IAW, SRM 53-10-51. - [SDR AWXA9600755](https://openairdocs.org/sdr/AWXA9600755.md): Mopsill · corroded · Dec 3, 1996 · N169AW · Boeing 73733A · Fuselage Miscellaneous Structure > DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON RT MOPSILL AT BS 284 TO 332, RBL 62, WL 208. REMOVED AND REPLACED MOPSILL AT BS 284 TO 332, WL 208, RBL 62, IAW, SRM 51-40-2. - [SDR AWXA960491](https://openairdocs.org/sdr/AWXA960491.md): Pin · unseated · Jul 16, 1996 · N169AW · Boeing 73733A · Emergency Lighting > PHX - FLT 2475 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT 3-L INOPERATIVE. RESEATED PIN IN CONNECTOR UNDER SEAT 3A. OPERATONS CHECK GOOD. (X) Next page: https://openairdocs.org/deregistered/N169AW-2002-05-31/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 = 'N169AW' AND deregistration_id = 'N169AW-2002-05-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N169AW-2002-05-31/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.