N7885A

Service difficulty reports · 180

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N7885A' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2023030698679Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL156. MARKED<[01] UPDATE PARTIAL STEPS 1-3;[02] SRM 53-00-03-2R-1 REPAIR 1 IS APPLICABLE TO THIS A/C AND REPIR.;[03] PERFORMED CUT OUT ON S-25R FCB; REMOVED DAMAGE PART FROM BS 500D+10 TO BS 540 IAW SRFeb 3, 2023 · N7885A · Boeing 73776N · Fuselage Main, Longeron/StringerSDR SWAA2023030698687Panel · crackedCRACKED PLEXIGLAS ON RH EMERGENCY EXIT DOOR ACTUATOR CORRECTION TO FAULT DESCRIPTION: CRACKED PLEXIGLASS GUARD OVER R/H EMERGENCY EXIT COUNTERBALANCE ASSEMBLY<[01] REMOVED SIDEWALL PANEL 232 YJW FOR ACCESS IAW AMM 25-21-46-000-801;[02] REMOVED AND REPLACED R/HFeb 3, 2023 · N7885A · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2023030698111Tie Down · corrodedCORROSION ON AFT CARGO BAY TIE DOWN AT BS 787+4 LBL 17.<[01] VERIFIED APPLICABILITY PER REF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2;[02] REMOVED CORROSION AT DISCREPANCY AREA L=5 W=1.ONE LIP WAS REMOVED ON CARGO BAY TIE DOWN .THEREFORE FOUND TO BE OUT OF LIMITFeb 2, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697701Support · crackedCRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 1.<[01] REMOVED PASSENGER CABIN FLOOR SUPPORT PANEL BREAK AT BS 540 FROM BL0-RBL24 IAW SRM 51-40-02;[02] LOCATED AND DRILLED PASSENGER CABIN FLOOR SUPPORT PANEL BREAK AT BS 540 FROM BL0-RBL24 IAW SRM 51-40-0Feb 1, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697700Support · crackedCRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 1.<[01] REMOVED PASSENGER CABIN FLOOR SUPPORT PANEL BREAK AT BS 540 FROM BL0-LBL24 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW PASSENGER CABIN FLOOR SUPPORT PANEL BREAK AT BS 540 FROM BL0-LBL24 IAW SRM 51-Feb 1, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697204Bracket · crackedCRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL 12.<[01] REMOVED ON AFT CARGO BAY WATYER SERVICE BRACKET AT BS 907+12 RBL 12 IAW SRM 51-40-02;[02] CRACKED ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL 12 P/N 147A7221-32 WITH NEXT DIMENSJan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697208Rail · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 7 BS 767+6.<[01] VERIFIED APPLICABILITY PER REF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION ON DISCREPANCY AREA L=2 W= .7 ;THE LOST MATERIAL IS MORE THAN 50% THEREFORE FOUND TO BE OUT OF LIMITS PER REJan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697207Rail · carbonedCORROSION ON AFT CARGO BAY RAIL AT LBL 3 BS 767+6.<[01] VERIFIED APPLICABILITY PER REF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION ON DISCREPANCY AREA L=2 W= .7 ;THE LOST MATERIAL IS MORE THAN 50% THEREFORE FOUND TO BE OUT OF LIMITS PER REJan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697209Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727A+6; BS 727B+14; BS 727D+8; BS 727D+14; BS 727E+6; BS 747+7.<[01] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE;[02] PARTIAL STEP 1 TO 6;[03Jan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697210Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 747+10; BS 747+18; BS 767+3; BS 767+4; BS 767+7; BS 767+13; BS 767+10.<[01] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE[17] INSTALLED FLOOR TJan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030697212Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A; BS 727C+6; BS 727D+10; BS 727D+14; BS 727D+18; BS 727E+6; BS 727E+10; BS 727E+14.<[01] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE;[14]Jan 31, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030696879Support · crackedFLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTACH GUSSET CRACKED BS261 S-10L WL255. MARKED<[01] FLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTACH SUPPORT CLIP CRACKED AT STR 10L BS 261 WL 255 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM Jan 30, 2023 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2023030207954Panel · exposedPANEL 192AR OUTER SKIN PREVIOUS REPAIR HAS EXPOSED FIBERS.<[01] IDENTIFIED PANEL 192AR IAW SRM 53-40-70-OI-1 PARA FIGURE 2; ITEM 2; TABLE 2.<BR>FOUND DAMAGE TO BE OUT ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A.(6)<BR>WILL PERFORM REPAIRS IAW SRM 51-70-05-Jan 26, 2023 · N7885A · Boeing 73776N · Fuselage Main, Attach FittingsSDR SWAA2023030694479Skin · cracked#1 SLAT SKIN CRACK AT ACTUATOR ATTACH POINT; LOWER SKIN RIVET. (RIVET MARKED)<[01] #1 SLAT SKIN CRACK AT ACTUATOR ATTACH POINT; LOWER SKIN RIVET WILL BE REPAIRED ON FAULT TTG8Q00HCWD0;[02] VERIFIED CORRECTIVE ACTION 1.Jan 23, 2023 · N7885A · Boeing 73776N · Wing StructureSDR SWAA2023030694473Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 3RD VERTICAL STIFFENER IS CRACKED. MARKED<[01] REMOVED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10 PER REF SRM 51-40-02;[08] FABRICATED REPAIR PARTS PER REJan 23, 2023 · N7885A · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2023030694474Barrier · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] VERIFIED APLICABILITY BY SRM 57-10-10-2R-5 REP 5;[02] TRIMED OUT UPPER ATTACH ANGLE AT VAPOR BARRIER BS 663 WL 160 RBL 15 PER SRM 57-10-10-2R-5 REPAIR 5;[03] PERFORM AN OPEN HOLE IJan 23, 2023 · N7885A · Boeing 73776N · Wing Main, Frame StructureSDR SWAA2023030694475Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 160.<[01] VERIFIED APLICABILITY BY SRM 57-10-10-2R-5 REPAIR 5;[02] TRIMED OUT UPPER ATTACH ANGLE AT VAPOR BARRIER BS 663 WL 160 LBL 15 PER SRM 57-10-10-2R-5 REPAIR 5;[03] PERFORM AN OPEN HOLJan 23, 2023 · N7885A · Boeing 73776N · Wing Main, Frame StructureSDR SWAA2023030694129Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 9.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).<BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-04Jan 22, 2023 · N7885A · Boeing 73776N · Trailing Edge FlapsSDR SWAA2023030694122Fairing · pulled#8 FLAP TRACK FAIRING 644BB FASTENERS FOR AFT SEAL RETAINER HAVE PULLED FASTENERS (MARKED)<[01] PART/MATERIAL IDENTIFIED PER SRM 57-53-70-0I-1 FIGURE. 4 TABLE 3 ITEM 3.<BR>PULLED FASTENER HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-53-70-1A-1. PARA 4 Jan 22, 2023 · N7885A · Boeing 73776N · Trailing Edge FlapsSDR SWAA2023030694126Flange · broken#1 ENGINE PYLON OUTBOARD AFT FIRE SEAL CLIP HORIZONTAL FLANGE IS BROKEN<[01] REMOVED #1 ENGINE PYLON O/B AFT FIRE SEAL CLIP AND FIRE SEAL BRACKET COMMON TO THE CLIP IAW SRM 51-40-02-0G-0.;[02] CERTIFIED ACTION 1;[03] UPDATED PARTS REMOVED / INSTALLED;[04] INSTJan 22, 2023 · N7885A · Boeing 73776N · Nacelle/Pylon Miscellaneous StructureSDR SWAA2023030693637Skin · crackedCRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED<[01] NDI VERIFY CRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS AND MARK ENDS PER SRM 51-10-02-0G-0;[10] FABJan 20, 2023 · N7885A · Boeing 73776N · Leading Edge DevicesSDR SWAA2023030693633Spar · corrodedCORROSION ON RIGHT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IFSS119. MARKED<[01] VERIFIED APLICABILITY SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3;[02] REMOVED CORROSION ON R/H WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING JUMPER PER SRM 57-20-10-1A-3Jan 20, 2023 · N7885A · Boeing 73776N · Wing Miscellaneous StructureSDR SWAA2022121380913Scuff Plate · crackedSUPPLEMENTAL INFORMATION: AFT CARGO DOOR CENTER SCUFF PLATE CRACKED<[01] PERFORMED HFEC PER 737 NDT PART 6 51-00-00 PROCEDURE 23 OF UNDERLYING STRUCTURE AT THE DAMAGED AREA. NO CRACKS OR OTHER DAMAGED NOTED. REF SRM 53-60-15-1A-3.;[02] R&R AFT CARGO DOOR CENTEDec 13, 2022 · N7885A · Boeing 73776N · Fuselage Main, FrameSDR SWAA2022121380907Attach Bracket · crackedFWD RH ATTACH BRACKET FOR PANEL 192F CRACKED / [01] R&R FWD RH ATTACH BRACKET FOR PANEL 192F PER AMM 53-12-12.;[02] R&R FWD RH ATTACH BRACKET FOR PANEL 192F PER AMM 51-40-02.;[03] R&R FWD RH ATTACH BRACKET FOR PANEL 192F PER SRM 51-40-02;[04] REMOVED AND REPLADec 13, 2022 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2022121380900Bracket · crackedWTB PANEL 191AR AFT ATTACH BRACKET CRACKED / [01] REMOVED AND REPLACED WTB 191AR ATTACH BRACKET PER SRM 51-40-02Dec 13, 2022 · N7885A · Boeing 73776N · Fuselage Main, Attach FittingsSDR SWAA2022121380910Girt Bar · out of adjustR1 DOOR SLIDE GIRT BAR TO LONG, NEEDS TO BE REINSTALLED ON PACK. ADJUSTED THE R1GIRT BAR IAW MT725-61-06.Dec 13, 2022 · N7885A · Boeing 73776N · Emergency EquipmentSDR SWAA2022121380909Girt Bar · out of adjustL1 DOOR SLIDE GIRT BAR TO LONG. NEEDS REINSTALLED IN PACK. UNLATCHED AND REINSTALLED GIRT BAR ON THE L1 SLIDE COVER IAW AMM 25-66-01-400-801 & MT725-61-06. OPS CHECKED GOOD.Dec 13, 2022 · N7885A · Boeing 73776N · Emergency EquipmentSDR SWAA2022121380908Collar · brokenL1 DOOR SLIDE GIRT BAR AFT COLLAR BROKEN. REMOVED AND REPLACED THE RELEASE STOP ASSEMBLY ON THE L1 DOOR GIRT BAR IAW AMM 25-66-01-000-803/804.Dec 13, 2022 · N7885A · Boeing 73776N · Emergency EquipmentSDR SWAA2022103166408Plate · crackedFORWARD SERVICE DOOR LIGHT ON DURING ROLLOUT. HANDLE CAME UP SLIGHTLY TWICE. ON SECOND TIME IT TRIGGERED LIGHT. / [01] FOUND THE AFT MIDDLE STOP BEARING PLATE OF THE FWD SERVICE DOOR CRACKED AND HALF MISSING. REPLACED THE BEARING PLATE IAW AMM 52-41-01. OPS CHOct 30, 2022 · N7885A · Boeing 73776N · Galley DoorsSDR SWAA2022081742748Plate · out of positionFORWARD ENTRY DOO GIRT BAR;BASE PLATE MISSING SCREW.BASE PLATE IS NOT FLUSH TO FLOOR. / [01] INSTALLED HARDWARE AMM 53-21-00.Aug 16, 2022 · N7885A · Boeing 73776N · Passenger/Crew DoorsSDR SWAA2022060613908Counter · smokeFIRST OFFICER YOKE TRIP COUNTER STARTED SMOKING ON TAXI. SMOKE WENT OUT AFTER ABOUT ONE MINUTE. / [01] COMPLIED WITH SP3A CAPPED AND STOWED WIRE # L729 PER REQUEST #644. OK TO CONTINUE PER MEL 33-1-01. SP1 C/W. AUTHORIZATION #68924.;[02] R&R?ED F/O?S TRIP COUNMay 31, 2022 · N7885A · Boeing 73776N · Flight Compartment LightingSDR SWAA2022052611643Light · inoperativeEXTERIOR EMERGENCY LIGHT BEHIND RT FLAP INOP. / [01] RELAMPED RT WING EXTERIOR EMERGENCY LIGHT BEHIND FLAP PER AMM 33-51-04. OPS CHECK GOOD.May 26, 2022 · N7885A · Boeing 73776N · Emergency LightingSDR SWAA2022051206173Light · inoperativeLEFT HAND OVERWING EXIT LIGHT INOP / [01] RELAMPED OVERWING EXIT LIGHT PER AMM 33-21-00May 10, 2022 · N7885A · Boeing 73776N · Emergency LightingSDR SWAA2022011360061Panel · looseR/H OWING EMER EXIT ACCESS PANEL LOOSE ; / [01] TIGHTEN PANEL ON R/H OVERWING EMERGENCY EXIT PER AMM 52-22-00.Jan 9, 2022 · N7885A · Boeing 73776N · Emergency ExitsSDR SWAA2021100826541Girt Bar · displacedCREW REPORTS FWD SERVICE DOOR SLIDE GIRT BAR DISPLACED. ; CREW REPORTS FWD SERVICE DOOR SLIDE GIRT AR DISPLACED. / [01] RESECURED GIRT BAR IAW SIP. AIRCRAFT OK FOR SERVICEOct 5, 2021 · N7885A · Boeing 73776N · Escape SlideSDR SWAA2021100524325Lens · missingFWD GALLEY 'EXIT LIGHT' LENS MISSING. ; / [01] FOUND AND REINSTALLED EXIT LIGHT LENS AT FWD. GALLEY (G1) IAW BOEING 737-700 AMM 33-51-01-960-802-NG.; [02] VERIFIED STEP 1.Sep 29, 2021 · N7885A · Boeing 73776N · Emergency LightingSDR SWAA2021100522656None · crackedLH AND RH OVERWING EXIT GRIP ASSY PN- 65C35987-5 CRACKED / [01] REMOVED AND REPLACED LH AND RH OVERWING EXIT GRIP ASSY AS PER SOPM 20-50-01; [02] CERTIFIED; [03] VERIFIED STEP 1/2Sep 24, 2021 · N7885A · Boeing 73776N · Passenger Compartment EquipmentSDR SWAA2021100518395Rib · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 4 HAS A CRACK. ; / [01] REMOVED CRACKED RIB P/N 186A1304-1 PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED RIB REMOVAL; [03] LOCATED AND DRILLED NEW RIB P/N 186A1304-1 PER B737-700 SRM 51-10-02-0G-0.; [04] VERIFIED DRILLISep 15, 2021 · N7885A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2021100518396None · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 5 HAS A CRACK. ; / [01] REMOVED RIB #5 AT LH HORIZONTAL STAB L/E ACCESS PANEL AS PER B737-700 SRM 51-40-02 -0G-0; [02] REMOVED RIB CRACKED P/N 186A1305-1 AT LH HORIZONTAL STAB PANEL AS PER B737-700 SRM 51-40-02-0G-0; [03Sep 15, 2021 · N7885A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2021100517048Skin · delaminatedL1 DOOR UPPER AFT CORNER SKIN LIFTED ; / [01] REMOVED 1 EA FASTENER ON L1 DOOR AFT CORNER OUTER SKIN FOR REWORK AND NDT PER B-737-7 SRM 51-40-02-0G-0; [02] VERIFIED REMOVAL.; [03] REWORKED AND STRAIGHTENED AFT CORNER SKIN PER BAC5300-2 STEP 8.2.1; [04] VERIFIESep 12, 2021 · N7885A · Boeing 73776N · Passenger/Crew DoorsSDR SWAA2021100515051None · corrodedREF TTG8Q0068VX9 CABIN FLOOR SUPPORT BEAM TOP CAP HAS LIGHT CORROSION AROUND NUT PLATE HOLES AT BS 986.5 32' RIGHT OF CENTER LINE- COMPLIANCE FINDING WRONG ATA AND MEASUREMENTS CORRECTION ; REF TTG8Q0068VX9 CAIN FLOOR SPPORT EAM TOP CAP HAS LIGHT CORROSION AROSep 6, 2021 · N7885A · Boeing 73776N · Fuselage Main, StructureSDR SWAA2021100512758Seat Track · crackedCRACK NOTED ON LBL24.75 POSITION 'B' HOLE ; CRACK NOTED ON SEAT TRACK BS 727B LBL24.75 POSITION 'B' HOLE; CRACK LENGTH 0.030' / [01] ACCOMPLISHED FIRST OVERSIZE CLEANUP REAM TO FASTENER HOLE TO A MINIMUM OF 0.016' AS PER REFERENCE NDT PART 6; 51-00-00; PROCEDUAug 28, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100512760Seat Track · crackedCRACK NOTED ON SEAT TRACK BS 727B LBL45.5 POSITION 'B' HOLE; CRACK LENGTH 0.030' ; CRACK NOTED ON SEAT TRACK BS 727B LBL 45.5 POSITION 'B' HOLE; CRACK LENGTH 0.030' / [01] ACCOMPLISHED FIRST OVERSIZE CLEANUP REAM TO FASTENER HOLE TO A MINIMUM OF 0.016' AS PER Aug 28, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100512753Splice Strap · corrodedCORROSION FOUND AT AFT CARGO FLOOR BOARD SPLICE STRAP AT STA 767 + 5. ; / [01] REMOVED CORROSION AT AFT CARGO FLOOR BOARD SPLICE STRAP STA 767.5 AS PER REF B737 SRM 51-10-02-0G-0.; [02] VERIFIED. REMOVED CORROSION AT AFT CARGO FLOOR BOARD SPLICE STRAP STA 767.Aug 27, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100510843None · looseL1 DOOR ESCAPE SLIDE GIRT BAR AFT CLIP IS NOT SECURED. MOUNTED ON THE ESCAPE SLIDE CONTAINER. ; / [01] RESECURED GIRT BAR AFT CLIP;MOUNTED ON THE ESCAPE SLIDE CONTAINER;AT L1 DOOR.PER B 737-700 SRM 51-40-02-OG-0.; [02] VERIFIED RESECURED GIRT BAR AFT CLIP;MOUNAug 23, 2021 · N7885A · Boeing 73776N · Escape SlideSDR SWAA2021100510838None · crackedRH Z CHANNEL BETWEEN STA 500 AND STA 500A HAS CRACKED ; / [01] REPLACED FWD CARGO R/H Z CHANNEL BETWEEN STA 500 THRU 500A REF.B737-700 SRM 51-40-02-0G-0. CHANNEL WILL BE INSTALLED ON FWD CARGO MOC. CARD #TTG8Q004GCN6; [02] VERIFIED NEW PART AND TTG8Q004GCN6 FOAug 23, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100510833Scuff Plate · crackedAFT CARGO COMP. AFT CORNER SCUFF PLATE CRACKED ; / [01] LOCATED AND DRILL NEW AFT CARGO AFT SCUFF PLATE AS PER REF B737-700 SRM 51-41-05-0G-0; [02] REMOVED AFT CARGO AFT CORNER SCUFF PLATE AS PER REF B737-700 AMM 53-11-02-020-801; [03] VERIFIED STEPS #1 AND #2Aug 23, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100510835None · corrodedRH Z CHANNEL SUPPORT STA 495 TO STA 500A HAS SPOTS OF CORROSION. ; / [01] FWD CARGO R/H SIDE Z CHANNEL (SHIELD ASSY) WAS REPLACED ON FAULT #TTG8Q0068W71; [02] VERIFIED Z CHANNEL REPLACEMENTAug 23, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100509605None · crackedFWD CARGO R/H SIDE STA 500D S-19R GUSSET BRACKET CRACK. ; / [01] REMOVED GUSSET BRACKET AT STA 500D STR 19R AS PER B737-700 SRM 51-10-02-0G-0.; [02] LOCATED AND DRILLED NEW BRACKET AS PER B737-700 SRM 51-40-05-0G-0.; [03] VERIFIED STEP #2; [04] VERIFIED STEP #Aug 21, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021100509608None · crackedFWD CARGO L/H SIDE STA 500D S-19L GUSSET BRACKET CRACK. ; / [01] REMOVED CRACKED GUSSET AS PER B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW GUSSET AS PER B737-700 SRM 51-40-05-0G-0.; [03] VERIFIED DRILLING.<BR>OK TO TREAT AND PRIME HOLES.; [04] APAug 21, 2021 · N7885A · Boeing 73776N · Fuselage Miscellaneous Structure
Back to N7885A