JASC 5312

Service difficulty reports · 20,045

Reports filed under 5312 · Fuselage Main, Bulkhead, 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 jasc_code = '5312'
  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 SWAA2020091114582Bulkhead Web · crackedRT MLG WHEEL WELL VAPOR WEB CRACKED 5' LONG. REPAIRED VAPOR WEB CRACK IN RT MLG WHEEL WELL BEHIND HYD SYSTEM 'B' RETURN FILTER, PER APB SRM 57-10-10 2.C.(4)(B) ALLOWABLE DAMAGE 2. REINSPECT EVERY 1200 CYCLES OR MORE FREQUENTLY. MAKE SURE CRACK HAS NOT GROWNSep 7, 2020 · N8602F · Boeing 7378H4SDR SCNA20201007070Support · corrodedCORROSION FOUND ON AFT CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT STA 947 RBL 9.5 TO LBL 21 WL 157. CORROSION ON AFT CARGO AFT LOWER BULKHEAD SUPPORT OUT OF LIMITS, IAW SRM 51-10-02. REMOVED AND REPLACED AFT CARGO AFT LOWER BULKHEAD SUPPORT WITH NESep 6, 2020 · N801SY · Boeing 7378Q8SDR SWAA2020090914257Bulkhead Web · crackedRT WW VAPOR BARRIER HAS 9' CRACK BEHIND HYD SERVICE HAND PUMP BETWEEN RBL 45.64 AND RBL 54.21. APPLIED INTERIM REPAIR, IAW SRM 57-10-10-1A-2 PAR 2.C. (4) (A) AND APB 737-700 SRM SUPPLEMENT 57-10-10 ALLOWABLE DAMAGE 2.Sep 5, 2020 · N269WN · Boeing 7377H4SDR SCNA20200929052Bulkhead Web · damagedTOOL MARK FOUND C/T AFT PRESSURE WEB AT W/L 207 RT WEB JUST BELOW THE PRESSURE WEB. REMOVED .006" MATERIAL FROM .040" NOMINAL .034" REMAINING, IAW B737 SRM 53-80-08 ALLOWABLE DAMAGE. FOUND TO BE OUT OF LIMITS.Sep 4, 2020 · N819SY · Boeing 73786NSDR DALA2020090842977Bulkhead Web · canningDURING INSPECTION FOUND OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 3RH AND 5 RH AT AFT ACC COMPARTMENT. OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 3RH AND 5 RH AT AFT ACC COMPARTMENT WAS REPAIRED PERMANENT REPAIR) PER ER/A 587646-14AD REV. ORSep 4, 2020 · N382DA · Boeing 737832SDR DALA2020090842976Bulkhead Web · canningDURING INSPECTION FOUND OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 11LH AND 13 LH AT AFT ACC COMPARTMENT. OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 11LH AND 13 LH AT AFT ACC COMPARTMENT WAS REPAIRED PER ER/A 587646-14AD.Sep 4, 2020 · N382DA · Boeing 737832SDR DALA2020090842975Bulkhead Web · canningDURING INSPECTION FOUND OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 11RH AND 13 RH AT AFT ACC COMPARTMENT. OIL CAN CONDITION ON AFT PRESSURE BULKHEAD BTW STGR 11RH AND 13 RH AT AFT ACC COMPARTMENT WAS REPAIRED PER ER/A 587646-14AD. REV. ORIGINAL SECTIOSep 4, 2020 · N382DA · Boeing 737832SDR SCNA20201007062Bulkhead Web · crackedLT LOWER 663 VAPOR BARRIER CRACKED BY THE EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER. REPAIRED CRACKS BY EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER ON LT LOWER 663 VAPOR BARRIER, PER SRM 57-10-10-2R-2 PARA 1 NOTSep 3, 2020 · N801SY · Boeing 7378Q8SDR SWAA2020092814047Bulkhead Web · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 18 WL 154. REMOVED BS 663 LOWER COMPOSITE BULKHEAD, IAW SRM 51-40-02-0G-0. FABRICATED LT VAPOR BARRIER PR BOE DWG 111A1151-3, REFER TO ATS BUILD SHEET 752673. ATS LOCATED AND DRILLED, IAW SRM 51-40-05 AND INSep 3, 2020 · N744SW · Boeing 7377H4SDR REXA2020091600645Bulkhead Web · chafedFOUND CHAFES IN RPB FORWARD FACE AT LBL 36.20, LBL 18.00, RBL 18.00, RBL 27.50 AND RBL 36.20 AT WL 105. CHAFES ARE 0.200"L X 0.200"W X 0.003" DEEP. REPAIRED CHAFES ON LBL 36.2, LBL 18, RBL 18, RBL 27.50 & RBL 36.20, IAW REO 601R-53-61-2155 REV A & REO 601R-Sep 3, 2020 · N8891A · Cndair CL6002B19SDR REXA2020091600644Bulkhead Web · crackedCONTINUATION FROM JOB 8789185 OP 39. FOUND RPB HAS 2 LOCATIONS WITH MULTIPLE INDICATIONS NOTED. AT LBL 9 WL 120 2:L 80% FSH AND AT RBL 27.50 WL 136.5 2.5"L 90% FSH BOTH AREAS FAILED NDT INSPECTION. REPAIRED RPB INDICATIONS AT LB 9 WL 120 & RBL 27.50 WL 136.Sep 3, 2020 · N8891A · Cndair CL6002B19SDR SWAA2020090413713Bulkhead Web · crackedRT WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING INBOARD + UP FROM RBL 45.64 1.0 INCH LONG + 16.0 INCHES FROM BOTTOM. ACCOMPLISHED INTERIM SEAL IAW SRM 57-10-10-1A-2. REPETITIVE ACTION REQUIRED, MAKE SURE TAPE IS IN SATISFACTORY CONDITION AT EACH 600 FLIGHTSep 3, 2020 · N8326F · Boeing 7378H4SDR SWAA2020090413714Bulkhead Web · crackedRT WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING OUTBOARD + DOWN FROM RBL 45.64 3.5 INCHES LONG + 7.5 INCHES FROM BOTTOM. ACCOMPLISHED SEAL REPAIR IAW SRM 57-10-10-1A-2. REPETITIVE ACTION REQUIRED. MAKE SURE TAPE IS IN SATISFACTORY CONDITION AT EACH 600 FLSep 3, 2020 · N8326F · Boeing 7378H4SDR SWIA202055499Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYINSep 2, 2020 · N701BR · Cndair CL6002B19SDR SWIA202053607Bulkhead · corrodedFS 280.00 RT BULKHEAD AFT SIDE LOWER OUTBOARD CORNER, FLOOR LEVEL, WEB IS CORRODED, MARKED. C-CHECK RO 10/22/2020. REMOVED CORRODED FS 280 RT WEB AND REPLACED WITH NEW REFERENCING DWG CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-3Sep 2, 2020 · N753EV · Cndair CL6002C10SDR SWAA2020090413392Bulkhead Web · crackedCENTER WING SECTION REAR SPAR VAPOR BARRIER HAS VERTICAL CRACK APPROX 10 INCHES IN LENGTH LOCATED BETWEEN LBL 45.64 AND LBL 31.83 MOD. CENTER WING SECTION REAR SPAR VAPOR BARRIER HAS VERTICAL CRACK MEASURING 10 INCHES IN LENGTH BETWEEN LBL 45.64 AND LBL 31.83Sep 2, 2020 · N7748A · Boeing 7377BDSDR SWIA202053086Pressure Blkhd · corroded621 PRESS BULKHEAD FWD SIDE AT INTERSECTION OF PLANES FOR STGR 11L AND LBL 43. BLIND RIVET INSTALLED WITHOUT HOLE HAVING BEEN DRILLED THRU DOUBLER ON BACKSIDE, AS A RESULT, DOUBLER IS NOW BROKEN, CRACKED, AND DEFORMED. BOTH SIDES OF BULKHEAD HAVE BEEN MARKEDSep 1, 2020 · N464SW · Cndair CL6002B19SDR DALA2020090532964Bulkhead Web · canningDURING HCK AT QRO, WHILE PERFORMING THE INSPECTIONS REQUIRED PER WC 5312-01166-0101, AREAS WITH OIL CAN CONDITION WERE FOUND ON AFT PRESSURE BULKHEAD (APB) AT BS 1016 AT THREE WEBS PN 148A2281-1, PN 148A2281-3 AND PN 148A2281-7. DAMAGE REPAIRED PER ERA 587646-Sep 1, 2020 · N382DA · Boeing 737832SDR SWAA2020090413178Bulkhead Web · crackedDURING INSPECTION OF THE CENTER WING REAR SPAR VAPOR WEB FOUND CRACK RUNNING VERTICALLY APPROX 7.75 INCHES IN LENGTH AT LBL 45 LEFT WHEEL WELL, REF SRM 57-10-10 FOR ALLOWABLE LIMITS. MOD / PERFORMED INTERIM REPAIR OF CENTER WING REAR SPAR VAPOR WEB @ LBL 45 RSep 1, 2020 · N279WN · Boeing 7377H4SDR SWAA2020090413179Bulkhead Web · crackedDURING INSPECTION OF THE CENTER REAR SPAR VAPOR BARRIER WEB FOUND APPROXIMATELY 3.75 INCH VERTICAL HAIR LINE CRACK BETWEEN RBL 40-43 RT WHEEL WELL REF SRM 57-10-10 FOR ALLOWABLE LIMITS. MOD/PERFORMED INTERIM REPAIR OF CENTER REAR SPAR VAPOR WEB @ RBL 40-43, RSep 1, 2020 · N279WN · Boeing 7377H4SDR SWAA2020090413756Bulkhead Web · crackedSTA 663 LBL 45 VERTICAL WEB REPAIR, REF SRM 57-10-10-2R-3 ALT 2 TABLE 205 FOR REPEAT INSPECTIONS. REPAIRED STA 663 VERTICAL PRESSURE DECK WEB AT LBL 45 IAW SRM 57-10-10-2R-3 ALTERNATIVE 2 AND AAR EA 200470 IR AND SWA EA 20-157-01561 REV IR.Sep 1, 2020 · N442WN · Boeing 7377H4SDR DALA2020102903519Bulkhead · crackedDURING INSPECTION FOUND CRACK ON SKIN LT FWD BULKHEAD WALL LOWER STATION 662 AT WHEEL WELL AREA. CRACK OF 9.5" ON SKIN LT FWD BULKHEAD WALL LOWER STATION 662 AT WHEEL WELL AREA WAS REPAIRED, PER B737-800 SRM 57-10-10-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 PAR 2.Aug 31, 2020 · N382DA · Boeing 737832SDR HNAA2020092400258Guide · damagedPILOT'S BULKHEAD UPPER OUTBOARD GUIDE PIN HOLE ELONGATED. COMPLETE: REMOVED PILOTS OUTBOARD GUIDE PIN DOUBLER. FABRICATED REPAIR PARTS; ONE DOUBLER AND SACRIFICAL PLATE. ACCOMPLISHED REPAIR ON PILOTS OUTBOARD GUIDE PIN HOLE, IAW EMB 145 SRM 53-21-02 ITEM 4 Aug 30, 2020 · N690AE · Emb EMB145LRSDR SWAA2020092213372Bulkhead · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 14 WL 154. REPAIRED CRACK AT BS 663 LOWER COMPOSITE BULKHEAD AT LBL 14 WL 154, IAW SRM 51-70-04-2R-10.Aug 28, 2020 · N709SW · Boeing 7377H4SDR SWIA202054252Bulkhead Web · out of toleranceCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC-COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL Aug 27, 2020 · N441SW · Cndair CL6002B19SDR SWIA202053240Bulkhead Web · damagedFOUND RPB WEB HAS 3 AREAS WITH MULTIPLE INDICATIONS NOTED 1) LINTEL AREA .250 LONG 100%FSH 2) B 0.0 WL 129 2.7 INCHES LONG 50%FSH AND 3) RBL 18.00 WL 130 1.7 INCHES LONG 60% FSH ALL 3 AREAS FAILED NDT INSPECTION. C-CHECK RO 10/13/2020. REPAIRED LINTEL IAW BOAug 27, 2020 · N221PS · Cndair CL6002B19SDR SWIA202053902Bulkhead Web · damagedEVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL 5378), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON RT 9G BULKHEAD AFT WALLAug 26, 2020 · N926EV · Cndair CL6002B19SDR SWIA202053901Bulkhead Web · damagedEVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL 5378), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON CENTER 9G BULKHEAD Aug 26, 2020 · N926EV · Cndair CL6002B19SDR SWIA202053900Bulkhead Web · damagedEVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS (REFERENCE RIL), REPAIR IF NEEDED IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 11/11/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE AROUND POTTED INSERTS ON LT 9G BULKHEAD AFT WALL. REAug 26, 2020 · N926EV · Cndair CL6002B19SDR SWIA202053256Isolator · crackedFS 621 BULKHEAD LBL 18 TOP ISOLATER IS CRACKED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED ISOLATER AT FS 621 BULKHEAD LBL 18 TOP, IAW CRJ 200 SRM.Aug 26, 2020 · N221PS · Cndair CL6002B19SDR SWIA202053009Bulkhead · damaged9 G BULKHEAD AFT FACE HAS DAMAGE AT ALL POTTED INSERTS. C-CHECK RO 10/1/2020. COMPLIED WITH THE FOLLOWING MHIRJ EO'S IN REPAIR OF TOOLING DAMAGE ON THE 9G BULKHEAD. LT BULKHEAD, CENTER BULKHEAD, RT BULKHEAD. REPAIR WORK INSTRUCTIONS "A" NOT REQUIRED. REPAAug 26, 2020 · N920EV · Cndair CL6002B19SDR SWAA2020092212029Pressure Blkhd · corrodedCORROSION ON INNER SURFACE OF BS 1016 PRESSURE DOME ON FWD SIDE RBL 2 TO LBL 1 WL 191. EVALUATED CORROSION ON INNER SURFCE OF BS 1016 PRESSURE DOME FWD SIDE. RBL 2-LBL 1 FOUND TO BE OUT OF LIMITS. REPAIRED BS 1016 PRESSURE BLKHD WEB, PER ER 20-03169 REV A EAug 26, 2020 · N709SW · Boeing 7377H4SDR SWAA2020100210767Bulkhead Web · crackedCRACK INDUCTION FOUND AT HORIZONTAL PRESSURE WEB AT STA 663 + 1''; RBL 41. APPROXIMATE LENGTH OF CRACK: 0.591''. ACCOMPLISHED REPAIR AT HORIZONTAL PRESSURE DECK WEB ON RT BETWEEN STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60, REF B737-700 SRM 53-40-51-2R-2 FIAug 24, 2020 · N560WN · Boeing 737790SDR SWAA2020092210881Bulkhead · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 14 WL 154. REMOVED CRACKED BS 663 LOWER COMPOSITE BULKHEAD LBL 6-LBL 70 WL 154. INSTALLED REPAIRED BULKHEAD, PER SRM 51-40-02-0G-0 DWG 111A1000 DWG 111A1001 DWG 144A7100.Aug 24, 2020 · N709SW · Boeing 7377H4SDR SWAA2020082711846Bulkhead Web · crackedVAPOR BARRIER HAS 8' CRACK BETWEEN R/H WHEEL WELL & R/H PACK BAY. CRACK LOCATED JUST FWD OF 'B' SYSTEM RETURN FILTER REPETITIVE ACTION REQUIRED: DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAug 24, 2020 · N8306H · Boeing 7378H4SDR SWAA2020082710922Bulkhead Web · crackedVAPOR BARRIER HAS 8' CRACK BETWEEN R/H WHEEL WELL & R/H PACK BAY. CRACK LOCATED JUST FWD OF 'B' SYSTEM RETURN FILTER REPETITIVE ACTION REQUIRED: DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAug 24, 2020 · N8306H · Boeing 7378H4SDR SWAA2020082710921Bulkhead Web · crackedREAR SPAR VAPOR BARRIER IN WHEEL WELL RIGHT SIDE HAS CRACK BETWEEN RBL 31.83 AND 40.00 7.75 INCHES. REPETITIVE ACTION REQUIRED: STOP DRILLED AND TAPED CRACK PER SRM 57-10-10-1A-2 REQUIRES REINSPECT EVERY 1200 FLIGHT CYCLES.Aug 24, 2020 · N8306H · Boeing 7378H4SDR SWAA2020082711847Bulkhead Web · crackedREAR SPAR VAPOR BARRIER IN WHEEL WELL RIGHT SIDE HAS CRACK BETWEEN RBL 31.83 AND 40.00 7.75 INCHES. REPETITIVE ACTION REQUIRED: STOP DRILLED AND TAPED CRACK PER SRM 57-10-10-1A-2 REQUIRES REINSPECT EVERY 1200 FLIGHT CYCLES.Aug 24, 2020 · N8306H · Boeing 7378H4SDR SWAA2021081210761Nut Plate · bentSTA. 178 PRESSURE BULKHEAD FWD SIDE - LOWER TWO RADOME ATTACHMENT FITTING NUT PLATES HAVE BENT OR BROKEN NUT TABS. [DOT 124-062] / REMOVED AND REPLACED NUT PLATES AT STA 178 PRESSURE BULKHEAD FWD SIDE LOWER IAW B-737-700 SRM 51-40-02-0G-0Aug 23, 2020 · N560WN · Boeing 737790SDR AALA2020082439030Bulkhead Web · crackedAIRCRAFT WAS NOT GROUNDED: RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER PREVIOUS REPAIR RE-CRACKED AT BS 663 AND THE 4TH BAY OUT-BOARD. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9.Aug 22, 2020 · N901NN · Boeing 737823SDR SWIA2020091152479Stiffener · shearedRT WHEEL WELL FR 56 AFT PRESSURE BULKHEAD VERTICAL STIFFENER HAS SHEARED RIVET HEAD. C-CHECK RO 9/8/2020. REMOVED AND REPLACED RIVET (1) EA ON RT WHEEL WELL FR 56 AFT PRESSURE BULKHEAD VERTICAL STIFFENER AND RESTORED SURFACE PROTECTION RIVET HEAD, REF SRM.Aug 21, 2020 · N142SY · Emb ERJ170200LRSDR SWAA2020082009937Bulkhead · crackedFOUND CRACK IN L/H WHEEL WELL VAPOR BARRIER 6 INCHES LONG JUST BELOW 'A' HYDRAULIC PUMP PRESSURE MODULE. ACCOMPLISHED INTERIM REPAIR IAW SRM. 57-10-10 1A-2 PERFORM VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURAug 19, 2020 · N8301J · Boeing 7378H4SDR SWIA202052632Bulkhead Web · corrodedRT FS 280.00 LOWER WEB IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED RT FS 280 LOWER WEB AND RT FS 280 BUTTSTRAP, REFERENCE CRJ700 SRM. COMPLIED WITH TASK CARD.Aug 17, 2020 · N784SK · Cndair CL6002C10SDR SWIA202052630Bulkhead Web · corrodedLT FS 280.00 LOWER WEB IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED LT FS 280 LOWER WEB AND LT FS 280 BUTTSTRAP, REFERENCE CRJ700 SRM. COMPLIED WITH TASK CARD.Aug 17, 2020 · N784SK · Cndair CL6002C10SDR SWAA2021082308836Stanchion · corrodedAFT CARGO BAY AFT BULKHEAD INBOARD VERTICAL STANCHION IS CORRODED AT LOWER END-PART # 149A8118-8 STA 947.50; WL 180; LBL 8. / REMOVED AND INSTALLED NEW ACB AFT BULKHEAD I/B VERTICAL STANCHION IAW SRM 51-10-02; SRM 51-40-02 AND AMM 38-11-01 AT STA 947.50; WL180Aug 16, 2020 · N484WN · Boeing 7377H4SDR SWIA2020091652539Bulkhead · crackedFS 202.75 CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH IT. C-CHECK RO 9/12/2020. REPAIRED THE FS 202.75 BULKHEAD BETWEEN LBL 22 & LBL 30 AT PARKING BRAKE CABLE PASS THRU, REF MHIRJ REO. ALL CHECKS GOOD, SEE CONTINUATION CARD FOR DETAILS.Aug 14, 2020 · N916EV · Cndair CL6002B19SDR SWAA2020090908913Bulkhead Web · crackedLT WHEEL WELL STA 663 LBL 37' 2.5' FROM TOP HAS .250' CRACK EMITTING FROM FASTENER, MARKED LOCATION. REPAIRED DEFECT AT LT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB STA 663 LBL 37' 2.5' FROM TOP, IAW B737-700 SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 1. THIS IAug 14, 2020 · N745SW · Boeing 7377H4SDR AALA2020082099021Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT BS 663 BETWEEN RBL 24 AND RBL 40. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9 REPAIR 9 AND SRM 57-10-10-2R-2.Aug 14, 2020 · N807NN · Boeing 737823SDR AALA2020082099020Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT BS 663 BETWEEN LBL 30 AND LBL 35. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9 REPAIR 9 AND SRM 57-10-10-2R-2.Aug 14, 2020 · N807NN · Boeing 737823SDR SWIA202053244Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. (J)(2) MODIFYING THE Aug 12, 2020 · N221PS · Cndair CL6002B19
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