# Service difficulty reports: N968WN

A list on [N968WN](https://openairdocs.org/aircraft/N968WN.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 4 · 157 reports

- [SDR SWAA2026091818638](https://openairdocs.org/sdr/SWAA2026091818638.md): Cover · out of adjust · Sep 14, 2026 · N968WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVER WING EXIT SIGN COVER OUT OF ADJUST. REPLACED OVER WING EMERGENCY EXIT LIGHT COVER PER AMM 33-51-03.
- [SDR SWAA2025111936308](https://openairdocs.org/sdr/SWAA2025111936308.md): Girt Bar · unpacked · Nov 18, 2025 · N968WN · Boeing 7377H4 · Emergency Equipment
  > R1 DOOR ESCAPE SLIDE GIRT UNPACKED. REPACKED R1 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01.
- [SDR SWAA2025111936314](https://openairdocs.org/sdr/SWAA2025111936314.md): Girt Bar · unpacked · Nov 18, 2025 · N968WN · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE GIRT, REPACK REQUIRED. REPACKED L1 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01.
- [SDR SWAA2025102225613](https://openairdocs.org/sdr/SWAA2025102225613.md): Handle · loose · Oct 18, 2025 · N968WN · Boeing 7377H4 · Passenger/Crew Doors
  > ASSIST HANDLE AFT OF L1 DOOR IS LOOSE. TIGHTEN ASSIST HANDLE AFT OF L1 DOOR PER AMM 25-21-31-420-802.
- [SDR SWAA2025102225160](https://openairdocs.org/sdr/SWAA2025102225160.md): Lamp · inoperative · Oct 17, 2025 · N968WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN ON FWD LAV HAS ONE LAMP INOPERATIVE. REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF THE EMERGENCY EXIT SIGN ON FWD LAV IAW AMM 33-51-01-960-801<BR><BR>COMPLETED TASK CARD.
- [SDR SWAA2025102224366](https://openairdocs.org/sdr/SWAA2025102224366.md): Support · cracked · Oct 14, 2025 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > DURING OK TO CLOSE FOUND CRACK ON RH WING TO BODY FAIRING SUPPORT AROUND THE FASTENER. REMOVED DAMAGED RIB/FAIRING SUPPORT AND INSTALLED NEW RIB/FAIRING SUPPORT PER DWGS 149A7101; 116A31100; 116A3010 AND SRM 51-40-02-0G-0.
- [SDR SWAA2025102222524](https://openairdocs.org/sdr/SWAA2025102222524.md): Plate · cracked · Oct 7, 2025 · N968WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING T/E WIGGLE PLATE JUST I/B OF THE #8 FLAP TRACK CRACKED. UPON FURTHER INVESTIGATION; SUSPECTED CRACK ON RIGHT WING T/E WIGGLE PLATE OF # 8 FLAP TRACK WAS LIMITED TO SURFACE FINISH (PRIMER) ONLY. REPRIMED AREA IAW AMM 51-21-99-300-801.
- [SDR SWAA2025102222525](https://openairdocs.org/sdr/SWAA2025102222525.md): Plate · cracked · Oct 7, 2025 · N968WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IAW SRM 51-40-02 AIPC 57-50-00-22A.
- [SDR SWAA2025102221733](https://openairdocs.org/sdr/SWAA2025102221733.md): Stub Frame · cracked · Oct 5, 2025 · N968WN · Boeing 7377H4 · Fuselage Main, Frame
  > 2 EA CRACKS FOUND ON FSD STUB FRAME ABOVE SEAL DEPRESSOR WL 206 + 57.5 L 1' W.01'; WL 206 + 58.5 L.06' W.01'. REMOVED AND REPLACED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV D.
- [SDR SWAA2025061179782](https://openairdocs.org/sdr/SWAA2025061179782.md): Sign · missing · Jun 9, 2025 · N968WN · Boeing 7377H4 · Emergency Lighting
  > MID CABIN OVERHEAD EXIT LIGHT COVER MISSING<[01] R&R CABIN OVHD EMERGENCY EXIT SIGN ASSY PER AMM 33-51-01.
- [SDR SWAA2025060275749](https://openairdocs.org/sdr/SWAA2025060275749.md): Vapor Barrier · cracked · May 28, 2025 · N968WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > A/C HAS FIBER VAPOR BARRIER CRACK BETWEEN RBL 31.83 & RBL 40 APPRX 11.5 IN LENGTH AND 11 FROM BOTTOM OF VAPOR BARRIER. ZONE 1 <[01]. PERFORMED STOP DRILL OF CRACKED AREA AND APPLIED SPEED TAPE. REF SRM. 57-10-10-1A-2 STEP 2(C)(4). DO A VISUAL INSPECTION OF TH
- [SDR SWAA2025032408349](https://openairdocs.org/sdr/SWAA2025032408349.md): Light · missing · Mar 21, 2025 · N968WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTS: BLUE FLOOR ILLUMINATION PROXIMITY PHOTOLUMINESCENT STRIP MOST AFT. LEFT SIDE IS MISSING<[01] REPLACED STRIP. ALL GOOD. REF AMM 33-51-15.
- [SDR SWAA2025010382399](https://openairdocs.org/sdr/SWAA2025010382399.md): Handle · loose · Jan 1, 2025 · N968WN · Boeing 7377H4 · Galley Doors
  > AFT SERVICE DOOR HANDLE AIRCRAFT RIGHT LOOSE<[01] INSTALLED NEW DOOR ASSIST HANDLE LOWER BASE ON DOOR PER M/M 52-13-31.OPS NORMAL.
- [SDR SWAA2024102149158](https://openairdocs.org/sdr/SWAA2024102149158.md): Seal · cracked · Oct 16, 2024 · N968WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL STABILIZER FWD UPPER SLIDER SEAL CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL FWD UPPER SLIDER SEAL IAW AMM 53-31-31.
- [SDR SWAA2024082127253](https://openairdocs.org/sdr/SWAA2024082127253.md): Megaphone · damaged · Aug 18, 2024 · N968WN · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY MEGAPHONE MISSING ATTACHMENT BOLT<[01] REMOVED AND REPLACED FWD GALLEY MEGAPHONE PER AMM 25-64-00
- [SDR SWAA2023112824322](https://openairdocs.org/sdr/SWAA2023112824322.md): Handle · loose · Nov 24, 2023 · N968WN · Boeing 7377H4 · Passenger/Crew Doors
  > R2/L2 ENTRY DOORS ASSIST HANDLES LOOSE 2023-661655<[01] TIGHTENED R2/L2 ENTRY DOORS ASSIST HANDLES I.A.W. SOPM 20-50-01 REV 38;[02] TASK CARD COMPLETED
- [SDR SWAA2023112825527](https://openairdocs.org/sdr/SWAA2023112825527.md): Handle · loose · Nov 24, 2023 · N968WN · Boeing 7377H4 · Passenger/Crew Doors
  > R2/L2 ENTRY DOORS ASSIST HANDLES LOOSE 2023-661655<[01] TIGHTENED R2/L2 ENTRY DOORS ASSIST HANDLES I.A.W. SOPM 20-50-01 REV 38;[02] TASK CARD COMPLETED
- [SDR SWAA2023112818814](https://openairdocs.org/sdr/SWAA2023112818814.md): Access Panel · damaged · Nov 6, 2023 · N968WN · Boeing 7377H4 · Trailing Edge Flaps
  > ELONGATED HOLE FITTING ACCESS PANEL 551GB TRAILING EDGE AT LT WING 2023-661623<[01] REMOVED AND REPLACED FITTING ON TRAILING EDGE ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] COMPLETED
- [SDR SWAA2023112817339](https://openairdocs.org/sdr/SWAA2023112817339.md): Angle · cracked · Nov 2, 2023 · N968WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION RT WING 2023-661609<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION RT WING IAW. B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG: 115A2000 SHEET: 22 REV: A TOOL USED: DIGITAL CALIPER
- [SDR SWAA2023112816905](https://openairdocs.org/sdr/SWAA2023112816905.md): Angle · cracked · Nov 1, 2023 · N968WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING 2023-661597<[01] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307
- [SDR SWAA2023112816457](https://openairdocs.org/sdr/SWAA2023112816457.md): Web · cracked · Oct 31, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCTED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156 AFT CARGO COMPARTMENT 2023-661594<[01] REPLACED WEB - INTERCOSTAL LOCTED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02
- [SDR SWAA2023112815984](https://openairdocs.org/sdr/SWAA2023112815984.md): Support Angle · broken · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BROKEN BODY STATION 663.75 SUPPORT ANGLE LOCATED AT RBL 25.00 AT MAIN WHEEL WELL COMPARTME 2023-661580<[01] REPLACED SUPPORT ANGLE LOCATED ON BODY STATION 663.75 & RBL 25.0 AT MAIN WHEEL WELL COMPARTMENT. IAW B737-700 SRM 51-10-02.;[02] CORRECTED STEP 1.<BR>RE
- [SDR SWAA2023112816268](https://openairdocs.org/sdr/SWAA2023112816268.md): Doubler · corroded · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 727B AND 727C; STR 1 AND STR 2R AT UPPER FUSELAGE 2023-661591<[01] REPLACED FASTENERS EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 727B AND 727C; STR 1 AND STR 2R AT UPPER FUSELAGE IAW B737-700 SRM 51-40-02 AND DR
- [SDR SWAA2023112816269](https://openairdocs.org/sdr/SWAA2023112816269.md): Doubler · corroded · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 747 AND BS 767; STR 1 AND STR 2R AT UPPER FUSELAGE 2023-661592<[01] REPLACED FASTENERS EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 747 AND BS 767; STR 1 AND STR 2R AT UPPER FUSELAGE IAW B737-700 SRM 51-40-02 AND
- [SDR SWAA2023112816128](https://openairdocs.org/sdr/SWAA2023112816128.md): Support Angle · cracked · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT BS 867 BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT 2023-661583<[01] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9.;
- [SDR SWAA2023112816270](https://openairdocs.org/sdr/SWAA2023112816270.md): Support · corroded · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BETWEEN BS 727C TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT 2023-661590<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 232019809; DUE DATE: 22-SEP-24.;[02] EVALUATED DAMAGE ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 767 RBL 21 & WL
- [SDR SWAA2023112816127](https://openairdocs.org/sdr/SWAA2023112816127.md): Bracket · cracked · Oct 30, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2023-661586<[01] REPLACED BRACKET LOCATED BS 947.5 & STRINGER 26L AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 & DWG 149A8103 SHEET 7; REV A.;[02] CORRECTED STEP 1.<BR>REPLACED BRACKET LOC
- [SDR SWAA2023112716126](https://openairdocs.org/sdr/SWAA2023112716126.md): Light · deteriorated · Oct 30, 2023 · N968WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5EA) 2023-661585<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOO
- [SDR SWAA2023112815980](https://openairdocs.org/sdr/SWAA2023112815980.md): Support Angle · cracked · Oct 29, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN 2023-661573<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND B737-700 DWG:153A5400 SHEET 122 REV:-SEE INDIVIDUAL SIGN
- [SDR SWAA2023112815810](https://openairdocs.org/sdr/SWAA2023112815810.md): Angle · cracked · Oct 28, 2023 · N968WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE INBOARD AUXILIARY SLAT TRACK ON SLAT1 AT LT WING 2023-661534<[01] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307;
- [SDR SWAA2023112815259](https://openairdocs.org/sdr/SWAA2023112815259.md): Stringer · corroded · Oct 27, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-661505<[01] TOOL USED:ULTRASONIC EQUIPMENT P/N 45MG S/N 221860711 DUE DATE: 07-NOV-23.;[02] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[03] TOOL USED TEMPERATURE CONTROL
- [SDR SWAA2023112815260](https://openairdocs.org/sdr/SWAA2023112815260.md): Stringer · corroded · Oct 27, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-661506<[01] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[02] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLL
- [SDR SWAA2023112815262](https://openairdocs.org/sdr/SWAA2023112815262.md): Rib · cracked · Oct 27, 2023 · N968WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER 2023-661510<[01] REPLACED LEADING EDGE RIB (CHORD) LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-10-02 ITEM 9 AND DWG# 186A1001 REV-; DWG# 186A1305 REV-. SEE INDIVIDUAL
- [SDR SWAA2023112815265](https://openairdocs.org/sdr/SWAA2023112815265.md): Support Angle · cracked · Oct 27, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R PASSENGER CABIN 2023-661511<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 3R PASSENGER CABIN SUPPORT ANGLE MUST BE REPLACED IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 146A7901 SHEET: 66
- [SDR SWAA2023112815147](https://openairdocs.org/sdr/SWAA2023112815147.md): Plate · corroded · Oct 26, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE LOCATED FLOOR STRUCTURE BS 1016 PLUS 13 INCHES AT AFT GALLEY AREA 2023-661470<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 221861811; DUE DATE: 08-NOV-23;[02] EVALUATED PLATE LOCATED FLOOR STRUCTURE BS 1016 PLUS 13 INCHES AT AFT
- [SDR SWAA2023112815146](https://openairdocs.org/sdr/SWAA2023112815146.md): Stringer Clip · broken · Oct 26, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > BROKEN STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE 2023-661469<[01] REPLACED STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE I.A.W SOPM 20-50-01 REV. 38;[02] REPLACED STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE I.A.W SOPM 20-50-01 REV
- [SDR SWAA2023112715150](https://openairdocs.org/sdr/SWAA2023112715150.md): Fitting · deteriorated · Oct 26, 2023 · N968WN · Boeing 7377H4 · Escape Slide
  > DETERIORATED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SERVICE AT AFT GAL LEY AREA 2023-661394<[01] REPLACED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SERVICE AT AFT GALLEY AREA I.A.W. B737-700 AMM 25-66-02-201;[02] REPLACED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SE
- [SDR SWAA2023112814759](https://openairdocs.org/sdr/SWAA2023112814759.md): Fitting · elongated · Oct 25, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > ELONGATED HOLE ON FITTING LOCATED BS 1016 UPPER AREA AT AFT GALLEY AREA 2023-661434<[01] REPLACED FITTING LOCATED BS 1016 UPPER AREA AT AFT GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9. AND DWG 148A2230 SHEET: 8 REV: C. SEE INDIVIDUALS SIGN-OFF BELOW;[02] RE
- [SDR SWAA2023112814930](https://openairdocs.org/sdr/SWAA2023112814930.md): Skin · corroded · Oct 25, 2023 · N968WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > CORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 1 2023-661449<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130063701 AND DUE DATE: 24-JUL-24.;[02] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[03] REPAIRED INLET COWL LIP-SKI
- [SDR SWAA2023112814931](https://openairdocs.org/sdr/SWAA2023112814931.md): Skin · corroded · Oct 25, 2023 · N968WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > CORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 2 2023-661450<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. PN: 45MG; SN: 232019809; DUE DATE: 22-SEP-24;[02] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130063701; CAL DUE DATE: 24-JUL-24;[03] REPAIRE
- [SDR SWAA2023112814461](https://openairdocs.org/sdr/SWAA2023112814461.md): Floorbeam · corroded · Oct 24, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2023-661415<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130060401 DUE DATE: 20-MAR-24;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 200053402 AND DUE DATE: 24-
- [SDR SWAA2023112814460](https://openairdocs.org/sdr/SWAA2023112814460.md): Support Bracket · cracked · Oct 24, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET ASSY LOCATED BTW BS 540 TO BS 559 RT SIDE AT AIR CONDITIONING BAY 2023-661413<[01] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS559 RT SIDE AT AIR CONDITIONING BAY IAW SRM B737-700 51-10-02-0G ITEM 9 AND SRM B737-700 51-40-02-0G-0
- [SDR SWAA2023112814465](https://openairdocs.org/sdr/SWAA2023112814465.md): Scuff Plate · elongated · Oct 24, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-661417<[01] REPLACED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1.<BR>REPLACED SCUFF PLATE AFT CORNER AT AFT
- [SDR SWAA2023112814002](https://openairdocs.org/sdr/SWAA2023112814002.md): Battery Pack · inoperative · Oct 24, 2023 · N968WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK ON FWD PASSENGER CABIN (2 EA) AFT PASSENGER CABIN (2 EA) AND OVER-WING ESCAPE HATCH (1 EA) 2023-661407<[01] REPLACED BATTERY PACK ON FWD PASSENGER CABIN (2 EA) AFT PASSENGER CABIN (2 EA) AND OVER-WING ESCAPE HATCH LT (1 EA) I.A.W B737-700 AMM
- [SDR SWAA2023112714303](https://openairdocs.org/sdr/SWAA2023112714303.md): Stringer · cracked · Oct 24, 2023 · N968WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-661411<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV - SEE INDIVIDUA
- [SDR SWAA2023112725257](https://openairdocs.org/sdr/SWAA2023112725257.md): Tie Clip · cracked · Oct 24, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-661411<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV - SEE INDIVIDUA
- [SDR SWAA2023112813851](https://openairdocs.org/sdr/SWAA2023112813851.md): Support Angle · cracked · Oct 23, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 0 AT PASSENGER CABIN 2023-661370<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02] REPL
- [SDR SWAA2023112813852](https://openairdocs.org/sdr/SWAA2023112813852.md): Support Angle · cracked · Oct 23, 2023 · N968WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2023-661371<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02]
- [SDR SWAA2023112813681](https://openairdocs.org/sdr/SWAA2023112813681.md): Battery Pack · inoperative · Oct 23, 2023 · N968WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK LOCATED BS 603 WL 212 RBL 67 AT PASSENGER CABIN 2023-661361<[01] REPLACED BATTERY PACK LOCATED BS 603 WL 212 RBL 67 AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED BATTERY PACK LOCATED BS
- [SDR SWAA2023112713850](https://openairdocs.org/sdr/SWAA2023112713850.md): Access Panel · cracked · Oct 23, 2023 · N968WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER 2023-661369<[01] TOOL USED CALIPER P/N: 500-197-30; S/N 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED HOT BONDER P/N HCS9200B; S/N 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N CL5000; S/N AE-40875

Next page: https://openairdocs.org/aircraft/N968WN/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 = 'N968WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N968WN/reports

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