# Service difficulty reports: N7884G, cancelled Oct 30, 2024 A list on [N7884G, cancelled Oct 30, 2024](https://openairdocs.org/deregistered/N7884G-2024-10-30.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 · 193 reports - [SDR SWAA2024053091430](https://openairdocs.org/sdr/SWAA2024053091430.md): Lamp · inoperative · May 30, 2024 · N7884G · Boeing 73776N · Emergency Lighting > L/H LOWER CENTER SLIDE LIGHT INOP.<[01] REMOVED AND REPLACED LAMP PER AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2024042979451](https://openairdocs.org/sdr/SWAA2024042979451.md): Handle · damaged · Apr 26, 2024 · N7884G · Boeing 73776N · Service Doors > FWD SERVICE DOOR HANDLE HAS ELONGATED ATTACHMENT HOLES<[01] 01 - REMOVED AND REPLACED PER [AMM 52-41-31-400-802-NG (GALLEY SERVICE DOOR LINING INSTALLATION - PERMANENT)];[02] C/W INSPECTION - [SDR SWAA2024020247449](https://openairdocs.org/sdr/SWAA2024020247449.md): Battery Pack · inoperative · Feb 1, 2024 · N7884G · Boeing 73776N · Emergency Lighting > R1 SLIDE EMERGENCY LIGHT INOP<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06 - [SDR SWAA2023080886946](https://openairdocs.org/sdr/SWAA2023080886946.md): Oil Cooler · leaking · Aug 8, 2023 · N7884G · Boeing 73776N · APU Oil System > APU AUTO SHUTDOWN EN ROUTE<[01] FOUND OIL LEAK AT APU OIL COOLER; R&R APU OIL COOLER IAW AMM 49-91-41; OPS CHECK GOOD - [SDR SWAA2023061659896](https://openairdocs.org/sdr/SWAA2023061659896.md): Slide · out of tolerance · Jun 15, 2023 · N7884G · Boeing 73776N · Escape Slide > FWD SERVICE DOOR SLIDE GAUGE NEEDLE IN RED BAND.<[01] REMOVED SLIDE PER MT 725-61-06.;[02] INSTALLED FWD SERVICE SLIDE PER MT 725-61-06. CKS OK. - [SDR SWAA2023050945955](https://openairdocs.org/sdr/SWAA2023050945955.md): Ballast · inoperative · May 5, 2023 · N7884G · Boeing 73776N · Emergency Lighting > CAPTS SIDE EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED L/H OVERWING EMERGENCY EXIT WINDOW LIGHT BALLAST PER AMM 33-21-00. OPS CHK GOOD. - [SDR SWAA2023011329907](https://openairdocs.org/sdr/SWAA2023011329907.md): Lamp · inoperative · Jan 11, 2023 · N7884G · Boeing 73776N · Emergency Lighting > OVERHEAD FWD COVE LIGHT F/O INOP OVERHEAD FWD COVE LIGHT F/O INOPCENTER ISLE CEILING NEAR ROW 1 DEF OVERHEAD BIN. RELAMPED RECESSED CEILING LIGHT PER AMM 33-22-00 - [SDR SWAA2022101459871](https://openairdocs.org/sdr/SWAA2022101459871.md): None · inoperative · Oct 14, 2022 · N7884G · Boeing 73776N · Emergency Lighting > BOTH OUTSIDE EMERGENCY LIGHTS AFT OF THE WING INOP / [01] REPLACED M1670 BATTERY PACK PER AMM 33-51-06. OPS GOOD. - [SDR SWAA2022081841328](https://openairdocs.org/sdr/SWAA2022081841328.md): Battery Pack · inoperative · Aug 12, 2022 · N7884G · Boeing 73776N · Emergency Lighting > EMERGENCY LIGHTS AT OVERHEAD BIN LOCATION 6ABC;9ABC;14ABC;13DEF;11DEF;8DEF AND R/H OVERWING EXIT DOOR INTERIOR AND EXTERIOR INOP / [01] REMOVED AND REPLACED BATTERIES PACKS M1669 AND M2335 PER AMM 33-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1. - [SDR SWAA2022081839480](https://openairdocs.org/sdr/SWAA2022081839480.md): Intercostal · cracked · Aug 7, 2022 · N7884G · Boeing 73776N · Fuselage Miscellaneous Structure > FOUND AT FWD CARGO STA 520 STR 25 RT. SIDE INTERCOSTAL CRACKED / [01] REMOVED INTERCOSTAL FOR CRACK AT FWD CARGO STA 520 STR 25 RT 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] FABRICATED INTERCOSTAL AS PER BOEING DRAWING # 143A9803-58; MATERIAL USED 7075-0.032' PO - [SDR SWAA2022081836020](https://openairdocs.org/sdr/SWAA2022081836020.md): Gusset · cracked · Jul 28, 2022 · N7884G · Boeing 73776N · Fuselage Main, Plate/Skin > AFT OF FWD CARGO COMPARTMENT R/H SIDE WALL GUSSET CRACKED @ S-19R STA 500D MKD DOT / [01] REMOVED GUSSET AT AFT OF FWD CARGO RH SIDE WALL FOR CRACK S-19R STA 500D SRM 51-40-02-0G-0;[02] RECEIVED NEW PARTS PO#1774766 LOCATED NEW PART AND DRILLED NEW HOLES SRM 5 - [SDR SWAA2022081836021](https://openairdocs.org/sdr/SWAA2022081836021.md): Scuff Plate · cracked · Jul 28, 2022 · N7884G · Boeing 73776N · Fuselage Miscellaneous Structure > FOUND AFT CARGO COMPT; FWD CORNER SCUFF PLATE CRACKED AT MULTIPLE SPOTS. / [01] LOCATED AND OPENED NEW FASTENER HOLES AT NEW AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE AS PER B737-7 SRM 51-40-05-0G-0.;[02] SCUFF PLATE FWD CORNER WILL BE INSTALLED AT CARD TTG - [SDR SWAA2022081835252](https://openairdocs.org/sdr/SWAA2022081835252.md): Doubler · cracked · Jul 27, 2022 · N7884G · Boeing 73776N · Fuselage Main, Plate/Skin > EXTERNAL POWER RECEPTACLE CUTOUT; FWD; LOWER INNER DOUBLER CRACKED. / [01] REMOVE EPR DOOR FOR INNER DOUBLER REPLACE ACCESS REF USED SRM 53-10-15-2R-4 STEP4.A(1);[[17] PERFORMED HFEC AT CUT OUT AS PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS
[NORTEC 60 - [SDR SWAA2022082235747](https://openairdocs.org/sdr/SWAA2022082235747.md): Fitting · eroded · Jul 25, 2022 · N7884G · Boeing 73776N · Wing, Attach Fittings > L/W REAR SPAR LOWER FIXED T/E STIFFENER LOWER FITTING HAS DRILLED HOLE @ ORSS 261 O/B OF FLAP TRACK NO-3 MKD DOT / [01] MEASURED DAMAGED AREA AT L/H WING REAR SPAR LOWER AREA OF STIFFNER ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2; HOLE DIAMETER=.215' DEPTH=.0 - [SDR SWAA2022082235236](https://openairdocs.org/sdr/SWAA2022082235236.md): Fitting · loose · Jul 25, 2022 · N7884G · Boeing 73776N · Wing, Attach Fittings > L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL FITTING LOCATION ' A ' HAS PLAY / [01] RESECURED FASTENERS AT RT WING DEFLECTION CONTROL RIB AS PER B737-7 SRM 57-51-02-2R-4 FIG 202 DETAIL A-A;[02] VERIFIED STEP 1 - [SDR SWAA2022082235235](https://openairdocs.org/sdr/SWAA2022082235235.md): Fitting · loose · Jul 25, 2022 · N7884G · Boeing 73776N · Wing, Attach Fittings > R/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL FITTING LOCATION ' A ' HAS PLAY / [01] RESECURED FASTENERS AT RT WING DEFLECTION CONTROL RIB AS PER B737-7 SRM 57=51-02-2R-4; FIG. 202 DETAIL A-A;[02] VERIFIED STEP 1 - [SDR SWAA2022081933747](https://openairdocs.org/sdr/SWAA2022081933747.md): Fitting · cracked · Jul 25, 2022 · N7884G · Boeing 73776N · Trailing Edge Flaps > R/W RAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED @ FASTENER TAIL INB. MKD DOT / [01] REMOVEDND REPLACED BULB SEAL FITTING AT R/W REAR SPART T/E DEFLECTION CONTROL RIB PANEL VERTICAL. REF. SRM. 51-40-02-0G-0-A00279.;[02] CORRECTI - [SDR SWAA2022081935746](https://openairdocs.org/sdr/SWAA2022081935746.md): Fitting · damaged · Jul 25, 2022 · N7884G · Boeing 73776N · Trailing Edge Flaps > R/W REAR SPAR FIXED T/E LOWER STIFFENER FITTING LOWER SURFACE DRILLED HOLE @ ORSS 261 MKD DOT / [01] MEASURED DAMAGED HOLE AT RT WING REAR SPAR FIXED T/E LOWER STIFFNER ATREA ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2;DEPTH =.044' WITDTH =.210';CALIPER B/C 159 - [SDR SWAA2022081933746](https://openairdocs.org/sdr/SWAA2022081933746.md): Fitting · cracked · Jul 25, 2022 · N7884G · Boeing 73776N · Trailing Edge Flaps > R/W REAR SPAR LOWER T/E WIGGLE FITTING CRACKED;SHEARED FASTENERS O/B FLAP TRACK NO-6 / [01] REMOVED AND REPLACED WIGGLE PLATE AT L\H WING T/E O/B OF FLAP TRACK #6 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 - [SDR SWAA2022081933748](https://openairdocs.org/sdr/SWAA2022081933748.md): Support Angle · cracked · Jul 25, 2022 · N7884G · Boeing 73776N · Trailing Edge Flaps > L/W REAR SPAR T/E LOWER SUPPORT ANGLE CRACKED @ INB END BELOW SPOILER NO-5 MKD DOT / [01] REMOVED SUPPORT ANGLE AT LW REAR SPAR T/E FOR CRACK SRM 51-40-02-0G-0;[02] RECEIVED NEW ANGLE PP#115A3758-9 LOCATED NEW ANGLE AND DRILLED NEW HOLES SRM 51-40-05-0G-0;[03] - [SDR SWAA2022081933751](https://openairdocs.org/sdr/SWAA2022081933751.md): Plate · cracked · Jul 25, 2022 · N7884G · Boeing 73776N · Trailing Edge Flaps > L/W REAR SPAR FIXED T/E LOWER WIGGLE FITTING SHEARED FASTENERS POSSIBLE CRACKED O/B OF FLAP TRACK NO-3 MKD DOT / [01] REMOVED AND REPLACED WIGGLE PLATE AT L/W REAR SPAR O/B OF OF FLAP TRACK #3 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 - [SDR SWAA2022081933564](https://openairdocs.org/sdr/SWAA2022081933564.md): Support Angle · corroded · Jul 25, 2022 · N7884G · Boeing 73776N · Wing Miscellaneous Structure > CORROSION ** L/W REAR SPAR LOWER T/E SUPPORT ANGLE BELOW SPOILER PANEL NO- 5 MKD DOT / [01] REF TASK CARD: TTG8Q00DRWEU FOR ANGLE REPLACEMENT.;[02] VERIFIED STEP #1 - [SDR SWAA2022072732833](https://openairdocs.org/sdr/SWAA2022072732833.md): Battery Pack · inoperative · Jul 23, 2022 · N7884G · Boeing 73776N · Emergency Lighting > MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. - [SDR SWAA2022072734894](https://openairdocs.org/sdr/SWAA2022072734894.md): Battery Pack · inoperative · Jul 23, 2022 · N7884G · Boeing 73776N · Emergency Lighting > MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. - [SDR SWAA2022072734895](https://openairdocs.org/sdr/SWAA2022072734895.md): Power Supply · inoperative · Jul 23, 2022 · N7884G · Boeing 73776N · Emergency Lighting > MULTIPLE EMERGENCY EXIT LIGHTS INOP. / [01] R+R LH FWD BATTERY PACK AND RH AFT BATTERY PACK/POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. - [SDR SWAA2022071828019](https://openairdocs.org/sdr/SWAA2022071828019.md): Support Rod · broken · Jul 12, 2022 · N7884G · Boeing 73776N · Nacelle/Pylon Miscellaneous Structure > #1 ENGINE O/B FAN COWL AFT SUPPORT ROD IS BROKEN. / [01] REMOVED AND REPLACED #1 ENG O/B FAN COWL AFT SUPPORT ROD SWIVEL BASE BRACKET IN REF TO CMM 71-13-30. OPS TEST NORMAL AT THIS TIME - [SDR SWAA2022060915514](https://openairdocs.org/sdr/SWAA2022060915514.md): Light · inoperative · Jun 6, 2022 · N7884G · Boeing 73776N · Emergency Lighting > EXTERIOR EMERGENCY LIGHT BY R2 DOOR INOP / [01] RELAMPED EXTERIOR EMERGENCY LIGHT BY R2 DOOR IAW AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2022052611429](https://openairdocs.org/sdr/SWAA2022052611429.md): Lens · failed · May 25, 2022 · N7884G · Boeing 73776N · Emergency Lighting > AFT EMERGENCY LIGHT LENS FELL OFF / [01] REPLACED AFT EMERGENCY LIGHT LENS PER AMM 33-51-14. OPS CHK GOOD. - [SDR SWAA2021121452102](https://openairdocs.org/sdr/SWAA2021121452102.md): Panel · elongated · Dec 10, 2021 · N7884G · Boeing 737 · Aerodynamic Fairings > SUPPLEMENTAL INFORMATION: PNL 193D HAS (1) HOLE ELONGATED; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21 - [SDR SWAA2021121452101](https://openairdocs.org/sdr/SWAA2021121452101.md): Panel · delaminated · Dec 10, 2021 · N7884G · Boeing 737 · Aerodynamic Fairings > SUPPLEMENTAL INFORMATION: PNL 194E HAS (4) EACH HOLES DELAMINATED; / [01] INSTALLED NEW PANEL IAW AMM 53-51-21 - [SDR SWAA2021121452100](https://openairdocs.org/sdr/SWAA2021121452100.md): Panel · delaminated · Dec 10, 2021 · N7884G · Boeing 737 · Aerodynamic Fairings > SUPPLEMENTAL INFORMATION: PNL 193D HAS (4) EACH HOLE DELAMINATED; / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21 - [SDR SWAA2021041964313](https://openairdocs.org/sdr/SWAA2021041964313.md): Lens · missing · Apr 14, 2021 · N7884G · Boeing 73776N · Emergency Lighting > EMERGENCY EXIT LENS ON RT OVERWING EXIT DOOR MISSING / REPLACED EMERGENCY EXIT LENS ON RT OVERWING IAW AMM 33-51-01 - [SDR SWAA2021030151050](https://openairdocs.org/sdr/SWAA2021030151050.md): Battery Pack · inoperative · Feb 24, 2021 · N7884G · Boeing 73776N · Emergency Lighting > FOUND MULTIPLE LH EMER EXIT LIGHTS INOP AT LH OVER WING EXIT / REMOVED & REPLACED LH EMER EXIT ROW EMERGENCY BATTERY PACK & CHARGER ASSY PER AMM 33-51-06. OP CHECK GOOD - [SDR SWAA2021030152193](https://openairdocs.org/sdr/SWAA2021030152193.md): Charger · inoperative · Feb 24, 2021 · N7884G · Boeing 73776N · Emergency Lighting > FOUND MULTIPLE LH EMER EXIT LIGHTS INOP AT LH OVER WING EXIT / REMOVED & REPLACED LH EMER EXIT ROW EMERGENCY BATTERY PACK & CHARGER ASSY PER AMM 33-51-06. OP CHECK GOOD - [SDR SWAA2020090312092](https://openairdocs.org/sdr/SWAA2020090312092.md): Connector · disconnected · Aug 27, 2020 · N7884G · Boeing 73776N · Light System Wiring > RIGHT OVERWING EMERGENCY EXIT LOCATOR SIGN IS INOPERATIVE. TROUBLESHOT RIGHT OVERWING EMERGENCY LIGHT, FOUND RIGHT OVERWING SIGN DISCONNECTED. RECONNECTED RIGHT OVERWING EMERGENCY LIGHT PER WDM 33-51-13. PERFORMED GOOD OPERATIONS TEST PER AMM 33-51-01-960-801 - [SDR SWAA2020090310575](https://openairdocs.org/sdr/SWAA2020090310575.md): Battery Pack · inoperative · Aug 23, 2020 · N7884G · Boeing 73776N · Emergency Lighting > ALL EMERGENCY LIGHTS ATTACHED TO M1673 DO NOT ILLUMINATE. REPLACED M1673 BATTERY PACK AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805. - [SDR SWAA2020090310574](https://openairdocs.org/sdr/SWAA2020090310574.md): Battery Pack · inoperative · Aug 23, 2020 · N7884G · Boeing 73776N · Emergency Lighting > ALL EMERGENCY LIGHTS CONNECTED TO M1674 DO NOT ILLUMINATE. REPLACED M1674 BATTERY PACK AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805. - [SDR SWAA2020090310572](https://openairdocs.org/sdr/SWAA2020090310572.md): Wire · broken · Aug 22, 2020 · N7884G · Boeing 73776N · Emergency Lighting > FOUND L1 DOOR EMERGENCY ESCAPE SIGN LIGHT WIRE W4142-0152 BROKEN AT GROUND BLOCK. RETERMINATED W4142-0152 INTO GD3782 PER SWPM 20-90-15 & WDM 33-51-21. PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-01-960-801 STEP 2.B.(2). - [SDR SWAA2021062409936](https://openairdocs.org/sdr/SWAA2021062409936.md): Scuff Plate · cracked · Aug 19, 2020 · N7884G · Boeing 73776N · Fuselage Miscellaneous Structure > FORWARD CARGO BAY AFT SCUFF PLATE IS CRACKED / RECEIVED NEW FORWARD CARGO BAY AFT SCUFF PLATE; LOCATED AND DRILLED FORWARD CARGO BAY AFT SCUFF PLATE PER SOPM# 51-40-05-0G-0 TO BE INSTALLED ON CUSTOMER CARD# 753-140-00-01Y. 57609U 25AUG20 - [SDR SWAA2021062409935](https://openairdocs.org/sdr/SWAA2021062409935.md): Scuff Plate · cracked · Aug 19, 2020 · N7884G · Boeing 73776N · Fuselage Miscellaneous Structure > FORWARD CARGO BAY FWD SCUFF PLATE IS CRACKED / LOCATED AND DRILLED FORWARD CARGO BAY; FWD SCUFF PLATE IAW SRM 51-60-05-0G-0; IFG 9; SRM 51-40-08-0G-0; FIG; PG4 AND COUNTERSICKED; INSTALLATION OF FORWARD CARGO BAY; FWD SCUFT PLATE WILL BE PREFORMED ON TASKCARD# - [SDR SWAA2020090409581](https://openairdocs.org/sdr/SWAA2020090409581.md): Skin · dented · Aug 11, 2020 · N7884G · Boeing 73776N · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS A DENT LOCATED AT BS1016+10'; 2' ABOVE S-7L. DAMAGE WAS REPAIRED PER REF B787 SRM 53-80-01-2R-5 REPAIR 5. - [SDR SWAA2020090409346](https://openairdocs.org/sdr/SWAA2020090409346.md): Skin · dented · Aug 10, 2020 · N7884G · Boeing 73776N · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENT AT BS440+13'; 1' ABOVE S-7L. DENT MEASURES AT L=2'; W=1.5'; Y=.040'; W/Y=37.5. REPAIRED AT FUSELAGE SKIN DENT AT BS 440+13'; 1' ABOVE S-7L IAW SRM 53-00-01-2R-3 REPAIR 3 CATEGORY B. - [SDR SWAA2020090307581](https://openairdocs.org/sdr/SWAA2020090307581.md): Skin · damaged · Aug 10, 2020 · N7884G · Boeing 73776N · Trailing Edge Flaps > LT INBOARD AFT FLAP HAS SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E. LT INBOARD AFT FLAP SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E WAS REPAIRED IAW SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0. - [SDR SWAA2020090307708](https://openairdocs.org/sdr/SWAA2020090307708.md): Screw · missing · Aug 10, 2020 · N7884G · Boeing 73776N · Emergency Lighting > LEFT HAND OVERWING EMERGENCY EXIT FLOOD LIGHT LENS IS MISSING A SCREW; LOCATED ON EXTERIOR OF FUSELAGE JUST AFT OF LEFT HAND EMERGENCY EXIT. LEFT HAND OVER WING EMERGENCY EXIT FLOOD LIGHT LENS MISSING SCREW WILL BE INSTALLED ON DEFECT NUMBER U178904. - [SDR SWAA2020090412601](https://openairdocs.org/sdr/SWAA2020090412601.md): Skin · dented · Aug 8, 2020 · N7884G · Boeing 73776N · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS MULTIPLE DENTS ON PREVIOUS REPAIR DOUBLER; BS 312 BETWEEN STR 20R-23R. REMOVED DENTED REPAIR DOUBLER; BS 312 BETWEEN STR 20R-23R AND REPLACED REPAIR PER SRM 53-00-01-2R-36 REPAIR 36. - [SDR SWAA2020090437304](https://openairdocs.org/sdr/SWAA2020090437304.md): Shear Tie · corroded · Aug 7, 2020 · N7884G · Boeing 73776N · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT BS 360 BETWEEN STRINGER 25 AND 26 LT. CORROSION ON SHEAR TIE AT BS 360 BETWEEN STR25L-26L FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C. REMOVED AND REPLACED BS - [SDR SWAA2021042907303](https://openairdocs.org/sdr/SWAA2021042907303.md): Stringer Clip · chafed · Aug 5, 2020 · N7884G · Boeing 73776N · Fuselage Main, Attach Fittings > CHAFING ON STRINGER CLIP BS259 S-16L WL216. MARKED / REMOVED AND REPLACED STR CLIP STA.259 STR 16L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20 - [SDR SWAA2021042907302](https://openairdocs.org/sdr/SWAA2021042907302.md): Stringer Clip · chafed · Aug 5, 2020 · N7884G · Boeing 73776N · Fuselage Main, Attach Fittings > CHAFING ON STRINGER CLIP BS259 S-12L WL243. MARKED / REMOVED AND REPLACED STR.CLIP STA.259 STR 12L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20 - [SDR SWAA2021042907301](https://openairdocs.org/sdr/SWAA2021042907301.md): Stringer Clip · chafed · Aug 5, 2020 · N7884G · Boeing 73776N · Fuselage Main, Attach Fittings > CHAFING ON STRINGER CLIP BS259 S-10L WL253. MARKED / REMOVED AND REPLACED STR CLIP STA.259 STR 10L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20 - [SDR SWAA2021042907299](https://openairdocs.org/sdr/SWAA2021042907299.md): Stringer Clip · chafed · Aug 5, 2020 · N7884G · Boeing 73776N · Fuselage Main, Attach Fittings > CHAFING ON STRINGER CLIP BS259 S-6L WL273. MARKED / REMOVED AND REPLACED STR. CLIP STA. 259 STR 6L PER SRM 51-40-02; SRM 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG.141A0720. 91195U 8-16-20 Next page: https://openairdocs.org/deregistered/N7884G-2024-10-30/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 = 'N7884G' AND deregistration_id = 'N7884G-2024-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N7884G-2024-10-30/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, except the copies of manufacturers’ service documents, which belong to their rights holders.