# Service difficulty reports: N216WR A list on [N216WR](https://openairdocs.org/aircraft/N216WR.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 7 · 301 reports - [SDR SWAA2026090819670](https://openairdocs.org/sdr/SWAA2026090819670.md): Light · contaminated · Sep 4, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > CABIN SEAT ROW 1ABC PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R & R THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15. - [SDR SWAA2026070216762](https://openairdocs.org/sdr/SWAA2026070216762.md): Lamp · inoperative · Jun 28, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > RIGHT FO SIDE EXIT LIGHT INOPERATIVE. RELAMPED RIGHT SIDE OVER WING EMERGENCY EXIT WINDOW LIGHT IAW AMM 33-51-04 - [SDR SWAA2026051296950](https://openairdocs.org/sdr/SWAA2026051296950.md): Battery Pack · inoperative · May 9, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > RIGHT AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED RIGHT AFTER BATTERY PACK ON EMERGENCY LIGHTS PER AMM 33-51-06 OPS CHECK GOOD AT THIS TIME - [SDR SWAA2026050594499](https://openairdocs.org/sdr/SWAA2026050594499.md): Battery Pack · inoperative · May 1, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > LEFT FORWARD EMERGENCY LIGHTS NOT CHARGING. REMOVED AND REPLACED CHARGER AND BATTERY PACK IAW M/M 33-51-06. - [SDR SWAA2026041387346](https://openairdocs.org/sdr/SWAA2026041387346.md): Support Bracket · cracked · Apr 8, 2026 · N216WR · Boeing 7377H4 · Wing Miscellaneous Structure > R/H WING UPPER TRAILING PANEL SUPPORT BRACKET CRACKED BETWEEN #7 GROUND SPOILER AND DEFLECTION RIB (SEE ATTACHED PICS)<[01] R&R R/H WING UPPER TRAILING PANEL SUPPORT BRACKET BETWEEN #7 GROUND SPOILER AND DEFLECTION RIB IN REF WITH SRM 51-40-02;[02] R&R R/H WIN - [SDR SWAA2026041087348](https://openairdocs.org/sdr/SWAA2026041087348.md): Cover · missing · Apr 8, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > RH OVERWING EMERGENCY LIGHT FLOOR COVER MISSING<[01] INSTALLED RH OVERWING FLOOR LIGHT COVER PER AMM 33-51-01 - [SDR SWAA2026040987557](https://openairdocs.org/sdr/SWAA2026040987557.md): Girt Bar · out of adjust · Apr 8, 2026 · N216WR · Boeing 7377H4 · Passenger/Crew Doors > AFT PASSENGER DOOR GIRT CONTACTING DOOR JAM WHILE CLOSING DOOR<[01] SECURED AFT PASSENGER DOOR GIRT PER AMM 25-66-01 - [SDR SWAA2026032682416](https://openairdocs.org/sdr/SWAA2026032682416.md): Cover · missing · Mar 23, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > ROW 1; ABOVE SEAT C; LIGHT COVER MISSING.<[01] REINSTALLED MISSING ROW 1CBA EMERGENCY AREA LIGHT COVER IAW AMM 33-51-03. - [SDR SWAA2026021971479](https://openairdocs.org/sdr/SWAA2026021971479.md): Lens · missing · Feb 17, 2026 · N216WR · Boeing 7377H4 · Emergency Lighting > ROW 22 DEF BULL NOSE EMERGENCY LIGHT LENS MISSING. INSTALLED THE LENS IAW AMM 33-51-03. - [SDR SWAA2025122254060](https://openairdocs.org/sdr/SWAA2025122254060.md): Slide · dislodged · Dec 19, 2025 · N216WR · Boeing 7377H4 · Escape Slide > R 2 DOOR EVAC. SLIDE FELL OUT OF HOLDER.<[01] REINSTALLED R2 ESCAPE SLIDE PER MT 725-61-06. OK FOR SERVICE. - [SDR SWAA2025071791668](https://openairdocs.org/sdr/SWAA2025071791668.md): Isolation Mount · broken · Jul 16, 2025 · N216WR · Boeing 7377H4 · Emergency Equipment > AFT ENTRY DOOR FORWARD SLIDE ATTACH BRACKET HAS TWO BROKEN MOUNT ISOLATORS. R & R IAW SRM 51-40-02. - [SDR SWAA2025062384193](https://openairdocs.org/sdr/SWAA2025062384193.md): Girt Bar · out of adjust · Jun 20, 2025 · N216WR · Boeing 7377H4 · Emergency Equipment > FWD ENTRY GIRT BAR IS OUT OF ALIGNMENT. <[01] REPOSITIONED THE FWD ENTRY GIRT BAR AS REQUIRED. REF. AMM 25-66-01. OPS CHECK GOOD. - [SDR SWAA2025040821715](https://openairdocs.org/sdr/SWAA2025040821715.md): Fuse · inoperative · Apr 5, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] SLAVED IN NEW LAMP AND BATTERY PACK. NO HELP. OK TO CONTINUE PER MEL 33-14-01. SP.1 AUTH #245726;[02] REPLACED FUSE IN AFT POWER SUPPLY REF AMM 33-51-06 OPS CHECK GOOD THIS CLEARS MEL. - [SDR SWAA2025032408168](https://openairdocs.org/sdr/SWAA2025032408168.md): Sign · out of adjust · Mar 20, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > FWD SERVICE DOOR EXIT LIGHT COVER FELL OFF <[01]. R&R?D FWD SERVICE OVER DOOR EMERGENCY EXIT SIGN ASSY. IAW MM 33-51-01. OPS CK?D OK. - [SDR SWAA2025031798935](https://openairdocs.org/sdr/SWAA2025031798935.md): Threshold · corroded · Feb 23, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON THRESHOLD PLATE AT COCKPIT 2025-112784<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00YW6S7;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00YW6S7 - [SDR SWAA2025031498524](https://openairdocs.org/sdr/SWAA2025031498524.md): Plate · corroded · Feb 23, 2025 · N216WR · Boeing 7377H4 · Flight Compartment Equipment > CORROSION ON THRESHOLD PLATE AT COCKPIT 2025-112784 <[01]. REPLACED THRESHOLD PLATE AT COCKPIT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9.; [02] REPLACED THRESHOLD PLATE AT COCKPIT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9. - [SDR SWAA2025031295686](https://openairdocs.org/sdr/SWAA2025031295686.md): Strip · deteriorated · Feb 13, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > DETERIORATED PHOTOLUMINESCENT STRIP LH (5EA) AND RH (5EA) AT FWD GALLEY AREA 2025-113163 <[01]. REPLACED PHOTOLUMINESCENT STRIP LH (5EA) AND RH (5EA) AT FWD GALLEY AREA IAW B737-700 AMM-33-51-15-400-802 AND DWG-33500007 REV 2.; [02] CORRECTED STEP 1. REPLACE - [SDR SWAA2025031395328](https://openairdocs.org/sdr/SWAA2025031395328.md): Support Angle · cracked · Feb 12, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT LOCATED BS807 LBL47 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON ANGLE - SUPPORT LOCATED BETWEEN BS787+15 TO BS 807+5, LBL47 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0 FIGURE 201 SHEET 2. TASK CARD COMPLETE. - [SDR SWAA2025031494855](https://openairdocs.org/sdr/SWAA2025031494855.md): Frame · cracked · Feb 10, 2025 · N216WR · Boeing 7377H4 · Fuselage Main, Frame > CRACK WEB FRAME LOCATED BS 259 AND BTW STR 8R TO STR 9R AT PASSENGER CABIN 2025-113077 <[01]. PERFORMED PERMANENT REPAIR LOCATED BS259 AND BTW STR6R TO STR11R AT PASSENGER CABIN. IAW B737-700 EA 25-153-00402-WIP1. SEE INDIVIDUAL SIGN OFFS BELOW.; [02] PERFORM - [SDR SWAA2025031794500](https://openairdocs.org/sdr/SWAA2025031794500.md): Stringer · cracked · Feb 9, 2025 · N216WR · Boeing 7377H4 · Wing, Longeron/Stringer > CRACK ON STRINGER 8 INTERNAL AREA FUEL TANK LOCATED BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AT RT WING 2025-113037<[01] PERFORMED PERMANENT REPAIR ON LOCATED STRINGER 8 INTERNAL AREA FUEL TANK LOCATED BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AT RT - [SDR SWAA2025031794502](https://openairdocs.org/sdr/SWAA2025031794502.md): Stringer · cracked · Feb 9, 2025 · N216WR · Boeing 7377H4 · Wing, Longeron/Stringer > CRACK ON STRINGER 9 INTERNAL AREA FUEL TANK LOCATED BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AT RT WING 2025-113040<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPAIRED UPPER STRINGER U9 BTW RIB 2 - [SDR SWAA2025031494503](https://openairdocs.org/sdr/SWAA2025031494503.md): Panel · cracked · Feb 9, 2025 · N216WR · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-113042 <[01]. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 186A3101 SHEET 2 REV B; [02] CERTIFIED WORK PERFORMED. - [SDR SWAA2025031494560](https://openairdocs.org/sdr/SWAA2025031494560.md): Support Angle · cracked · Feb 9, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR27L AT AFT CARGO COMPARTMENT 2025-113049 <[01]. REPLACED ANGLE-SUPPORT LOCATED BS 867 AT LEVEL STRINGER 27L AT AFT CARGO COMPARTMENT; IAW BOEING 737-700 SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV-. CRACK LENGTH - [SDR SWAA2025031294436](https://openairdocs.org/sdr/SWAA2025031294436.md): Battery Pack · inoperative · Feb 9, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > INOP BATTERY PACK ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY 2025-113017 <[01]. REPLACED BATTERY PACK ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY IAW B737-700 AMM 33-51-06-960-805 SEE INDIVIDUALS SIGN OFF BELOW. TEST IS OK.; [02] REPLACED BATTERY - [SDR SWAA2025031294437](https://openairdocs.org/sdr/SWAA2025031294437.md): Battery Pack · inoperative · Feb 9, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > INOP BATTERY PACK ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY 1EA 2025-113018 <[01]. REPLACED BATTERY PACK ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY IAW B737-700 AMM 33-51-06-960-805 SEE INDIVIDUALS SIGN OFF BELOW. TEST IS OK; [02] REPLACED BATT - [SDR SWAA2025031294438](https://openairdocs.org/sdr/SWAA2025031294438.md): Power Supply · inoperative · Feb 9, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > INOP EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY 1EA 2025-113019 <[01]. REPLACED EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL LH SIDE AT AFT AREA GALLEY IAW B737-700 AMM 33-51-06-960-806. SEE INDIVIDUALS SIGN OFF BELOW. TEST IS O - [SDR SWAA2025031294439](https://openairdocs.org/sdr/SWAA2025031294439.md): Power Supply · inoperative · Feb 9, 2025 · N216WR · Boeing 7377H4 · Emergency Lighting > INOP EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY 1EA 2025-113020 <[01]. REPLACED EMERGENCY POWER SUPPLY ON LOWER CEILING PANEL RH SIDE AT AFT AREA GALLEY IAW B737-700 AMM 33-51-06-960-806 SEE INDIVUALS SIGN OFF BELOW. TEST IS OK; - [SDR SWAA2025031794432](https://openairdocs.org/sdr/SWAA2025031794432.md): Stringer · cracked · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2025-113006<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26;[02] TOOL US - [SDR SWAA2025031794433](https://openairdocs.org/sdr/SWAA2025031794433.md): Stringer · corroded · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CORROSION STRINGER 26L LOCATED BS540 WL156.5 AT FWD CARGO COMPARTMENT 2025-113004<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130066401 AND DUE DATE: 21-OCT-25.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 2 - [SDR SWAA2025031794270](https://openairdocs.org/sdr/SWAA2025031794270.md): Panel · cracked · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Floor Panel > CRACK LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN 2025-112959. - [SDR SWAA2025031494434](https://openairdocs.org/sdr/SWAA2025031494434.md): Support Angle · cracked · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR28R FWD CARGO COMPARTMENT 2025-113009 <[01]. REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS500D AT LEVEL STR28R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143 - [SDR SWAA2025031494271](https://openairdocs.org/sdr/SWAA2025031494271.md): Shield · corroded · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON SHIELD LOCATED BTW BS492.4 TO BS500A AT LEVEL STR26R WL156.5 AT FWD CARGO COMPARTMENT 2025-112979 <[01]. REPLACED SHIELD AND FASTENERS LOCATED BTW BS492.4 TO BS500A AT LEVEL STR26R WL156.5 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM - [SDR SWAA2025031494272](https://openairdocs.org/sdr/SWAA2025031494272.md): Pressure Deck · cracked · Feb 8, 2025 · N216WR · Boeing 7377H4 · Fuselage Main, Structure > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA. 663 TO STA. 675 RBL 42. CRACK LENGTH 0.625 IN. PASSENGER CABIN 2025-112981 <[01]. TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 240525411; DUE DATE: 13-NOV -25.; [02] TOOL USED: EDD - [SDR SWAA2025031794244](https://openairdocs.org/sdr/SWAA2025031794244.md): Support Bracket · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT BRACKET BS 663.75 AND RBL 54 AT LOWER FUSELAGE 2025-112923<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26;[02] TOOLS USED: POWER PACK: P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 17-JUN-25; THER - [SDR SWAA2025031794245](https://openairdocs.org/sdr/SWAA2025031794245.md): Intercostal · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14R AT PASSENGER CABIN 2025-112924<[01] REPLACED WEB INTERCOSTAL
LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14R
AT PASSENGER CABIN.
IAW:
B737-700 SRM 51-40-02
DWG: 144A7500 SHEET: 6 - [SDR SWAA2025031794115](https://openairdocs.org/sdr/SWAA2025031794115.md): Support Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK ON SUPPORT ANGLE LOCATED AT LEVEL STR 17R BTW BS 291.5 TO 294.5 AT PASSENGER CABIN 2025-112898 <[01]. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT LEVEL STR 17R BTW BS 291.5 TO 294.5 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8310 - [SDR SWAA2025031794123](https://openairdocs.org/sdr/SWAA2025031794123.md): Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Leading Edge Devices > CRACK SLAT 8 ANGLE ON INBOARD AUXILIARY TRACK AT RT WING 2025-112907 <[01]. REPLACED ANGLE LOCATED ON SLAT 8 INBOARD AUXILIARY TRACK AT RT WING.
IAW B737-700 SRM 51-10-02 ITEM 9 B737-700 SRM 51-40-02 AND DWG: 114A5010 SHEET: 6 REV: D. TOOL USED: CALIPER: - [SDR SWAA2025031494113](https://openairdocs.org/sdr/SWAA2025031494113.md): Panel · delaminated · Feb 7, 2025 · N216WR · Boeing 7377H4 · Horizontal Stabilizer Structure > DELAMINATE ON ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZER 2025-112894 <[01]. TOOL USED P/N: EPOCH 600; S/N: 120357005; CAL DUE: 10-JUN-25.;[02] REPAIRED ACCESS PANEL 333CB AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUA - [SDR SWAA2025031494114](https://openairdocs.org/sdr/SWAA2025031494114.md): Support Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK SEAL - PLATE ACCESS PANEL 333AB SUPPORT ANGLE LT HORIZONTAL STAB 2025-112897 <[01]. REPLACED PLATE ACCESS PANEL 333AB SUPPORT ANGLE LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 186A3101 SHEET 16 REV C; [02] CERTIFIED WO - [SDR SWAA2025031494120](https://openairdocs.org/sdr/SWAA2025031494120.md): Support Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK SEAL - PLATE ACCESS PANEL 343AB SUPPORT ANGLE RT HORIZONTAL STAB 2025-112899 <[01]. REPLACED PLATE ACCESS PANEL 343AB SUPPORT ANGLE RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [02] REPLACED PLATE ACCESS PANEL 343AB SUPPORT ANGL - [SDR SWAA2025031494241](https://openairdocs.org/sdr/SWAA2025031494241.md): Rail · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Leading Edge Devices > CRACK O/B FIXED LEADING EDGE RAIL NUT PLATE OFSS 449 AT RT WING 2025-112911<[01]. REPLACED O/B FIXED LEADING EDGE RAIL NUT PLATE (GANG CHANNEL) OFSS 449 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG# 112A4402; SHEET 13; REV-. MEASURE OF CRACK IS: 0.250 INCH TO - [SDR SWAA2025031494118](https://openairdocs.org/sdr/SWAA2025031494118.md): Support Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE WING BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE 2025-112895 <[01]. REPLACED SUPPORT ANGLE LOC. WING BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 - [SDR SWAA2025031494252](https://openairdocs.org/sdr/SWAA2025031494252.md): Girt Bar · deteriorated · Feb 7, 2025 · N216WR · Boeing 7377H4 · Emergency Equipment > DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT ENTRY DOOR AT AFT GALLEY AREA 2025-112910 <[01]. REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 PARAGRAPH 3D; 3E TEST IS OK.; - [SDR SWAA2025031494253](https://openairdocs.org/sdr/SWAA2025031494253.md): Girt Bar · deteriorated · Feb 7, 2025 · N216WR · Boeing 7377H4 · Emergency Equipment > DETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT SERVICE DOOR AT AFT GALLEY AREA 2025-112909 <[01]. REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.; [02] REPLACED GIRT BAR F - [SDR SWAA2025031494247](https://openairdocs.org/sdr/SWAA2025031494247.md): Intercostal · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON INTERCOSTAL LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14L AT PASSENGER CABIN 2025- 112927 <[01]. REPLACED WEB INTERCOSTAL LOCATED BTW BS 685 TO BS 707 AT LEVEL STR 14L AT PASSENGER CABIN. IAW: B737-700 SRM 51-40-02 DWG: 144A7500 SHEET: 6 REV: A. SEE - [SDR SWAA2025031494122](https://openairdocs.org/sdr/SWAA2025031494122.md): Support Angle · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA 2025-112904 <[01]. REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A1311 SHEET 1 REV; [02] CORRECT - [SDR SWAA2025031494248](https://openairdocs.org/sdr/SWAA2025031494248.md): Support Bracket · cracked · Feb 7, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2025-112932 <[01]. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 146A7901; SHEET: 66; R - [SDR SWAA2025031793990](https://openairdocs.org/sdr/SWAA2025031793990.md): Scuff Plate · cracked · Feb 6, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2025-112830<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04/MAR/25.;[02] EQUIPMENT P/N XRP-3000; S/N 1859843; DUE DATE 10-MAR-25 WAS USED ON STEP 4;[03] REPAIRED FWD CORNER SCUF - [SDR SWAA2025031793770](https://openairdocs.org/sdr/SWAA2025031793770.md): Intercostal · cracked · Feb 6, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO LBL24.75 AT PASSENGER CABIN 2025-112771<[01] REPLACED INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG: 14 - [SDR SWAA2025031793763](https://openairdocs.org/sdr/SWAA2025031793763.md): Intercostal · cracked · Feb 6, 2025 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED AT BS540 BTW BL0 TO RBL24.75 AT PASSENGER CABIN. 2025-112772 CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO RBL24.75 AT PASSENGER CABIN<[01] REPLACED INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED AT Next page: https://openairdocs.org/aircraft/N216WR/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 = 'N216WR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N216WR/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.