# Service difficulty reports: N555LV

A list on [N555LV](https://openairdocs.org/aircraft/N555LV.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 5 · 243 reports

- [SDR SWAA2026090714145](https://openairdocs.org/sdr/SWAA2026090714145.md): Battery Pack · no test · Sep 1, 2026 · N555LV · Boeing 7377BD · Emergency Lighting
  > LEFT FWD EMERGENCY LIGHTS BATTERY PACK FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026071315514](https://openairdocs.org/sdr/SWAA2026071315514.md): Support · cracked · Jun 24, 2026 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ZEE, BS 500A, S26L, WL152.5 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON SUPPORT SEE SECTION IAW SRM 51-10-02-0G-0, SRM 53-00-53-2R-6, REPAIR 6, AND DRAWING 43A7500, SHEET 71, REV-.
- [SDR SWAA2026071315516](https://openairdocs.org/sdr/SWAA2026071315516.md): Shield · corroded · Jun 24, 2026 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB, BETWEEN BS 492.5 - 500A, WL 152.5, S26R IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G-0 AND DWG 143A0080, SHEET 41, REV-.
- [SDR SWAA2026071015718](https://openairdocs.org/sdr/SWAA2026071015718.md): Support Bracket · cracked · Jun 24, 2026 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET ON FLOOR STRUCTURE LOCATED BS400 AT LEVEL STR26R AT FWD CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS ON FLOOR STRUCTURE LOCATED BS400 AT LEVEL STR26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 1
- [SDR SWAA2026071417058](https://openairdocs.org/sdr/SWAA2026071417058.md): Strap · no discrepancy · Jun 23, 2026 · N555LV · Boeing 7377BD · Fuselage Structure (General)
  > BS 328 FRAME STRAP CONFIGURATION LOCATED ON S20R TO S22R DOES NOT MATCH WITH FIGURE 15. IAW EA 26-153-01702; THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026071315092](https://openairdocs.org/sdr/SWAA2026071315092.md): Support Angle · cracked · Jun 23, 2026 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500D, STR 28L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0 DWG 143A7902 SHEET 126 REV:A.
- [SDR SWAA2026071314601](https://openairdocs.org/sdr/SWAA2026071314601.md): Access Panel · cracked · Jun 21, 2026 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > CRACKED BLADE, ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED BLADE, ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02.
- [SDR SWAA2026071314221](https://openairdocs.org/sdr/SWAA2026071314221.md): Angle · cracked · Jun 20, 2026 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, LOCATED BS400 AT LEVEL S26L AT FWD CARGO BAY. REPLACED THE ANGLE AND LOCATED BS400 AT LEVEL STR26L AT FWD CARGO BAY IAW 51-40-02 AND DWG 143A7505, SHEET 117, REV-.
- [SDR SWAA2026071014117](https://openairdocs.org/sdr/SWAA2026071014117.md): Battery Pack · inoperative · Jun 20, 2026 · N555LV · Boeing 7377BD · Emergency Lighting
  > INOPERATIVE BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE POSITION. REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE POSITIO IAW AMM 33-51-06-960-805. TESTED OK.
- [SDR SWAA2026071013227](https://openairdocs.org/sdr/SWAA2026071013227.md): Access Panel · elongated · Jun 17, 2026 · N555LV · Boeing 7377BD · Wing Miscellaneous Structure
  > ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026061511236](https://openairdocs.org/sdr/SWAA2026061511236.md): Lamp · inoperative · Jun 11, 2026 · N555LV · Boeing 7377BD · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT OVERWING EMERGENCY EXIT LAMP IAW AMM 33-51-04. NO FIX, REMOVED AND REPLACED POWER SUPPLY, BATTERY PACK AND POWER SUPPLY FUSES IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026061512471](https://openairdocs.org/sdr/SWAA2026061512471.md): Battery Pack · inoperative · Jun 11, 2026 · N555LV · Boeing 7377BD · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT OVERWING EMERGENCY EXIT LAMP IAW AMM 33-51-04. NO FIX, REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AND POWER SUPPLY FUSES IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026061512472](https://openairdocs.org/sdr/SWAA2026061512472.md): Fuse · inoperative · Jun 11, 2026 · N555LV · Boeing 7377BD · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT OVERWING EMERGENCY EXIT LAMP IAW AMM 33-51-04. NO FIX., REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AND POWER SUPPLY FUSES IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025072493866](https://openairdocs.org/sdr/SWAA2025072493866.md): Battery · inoperative · Jul 22, 2025 · N555LV · Boeing 7377BD · Emergency Equipment
  > FWD CABIN EMERGENCY FLASHLIGHTS REQ NEW BATTERYS. REMOVED AND REPLACED THE BATTERIES IAW AMM 25-64-00-900-806-NG.
- [SDR SWAA2025072193239](https://openairdocs.org/sdr/SWAA2025072193239.md): Engine · power loss · Jul 20, 2025 · N555LV · Boeing 7377BD · Engine (Turbine/Turboprop)
  > CLIMBING THROUGH 10000 FEET HEARD LOUD BANGS; AIRCRAFT SHOOK; OBSERVED N1 REDUCED TO APPROX 60% N1. REDUCED POWER AND ENGINE INDICATIONS RETURNED TO NORMAL. DID NOT DECLARE EMERGENCY. ENGINE NUMBER 1. REMOVED AND REPLACED #1 ENGINE PER [AMM 71-00-02-401-NG/
- [SDR SWAA2025051969844](https://openairdocs.org/sdr/SWAA2025051969844.md): Battery Pack · inoperative · May 11, 2025 · N555LV · Boeing 7377BD · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1674 INOP<[01] REMOVED; REPLACED WITH SERVICABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY BATTERY PACK M1674 IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025030300814](https://openairdocs.org/sdr/SWAA2025030300814.md): Slide · out of adjust · Feb 28, 2025 · N555LV · Boeing 7377BD · Escape Slide
  > AFT ENTRY SLIDE FELL OUT OF CONTAINER <[01]. REPACKEDAFT ENTRY SLIDE REF AMM 25-66-01. & MT 725-61-06AE.
- [SDR SWAA2024121777679](https://openairdocs.org/sdr/SWAA2024121777679.md): Guide Plate · sheared · Dec 15, 2024 · N555LV · Boeing 7377BD · Passenger/Crew Doors
  > L1 DOOR WILL NOT OPEN<[01] FOUND GUIDE PLATES PIN SCREW SHEARED. R&R GUIDE PLATES PIN AND SCREW IAW AMM 52-11-21.
- [SDR SWAA2024101046412](https://openairdocs.org/sdr/SWAA2024101046412.md): Table · broken · Oct 7, 2024 · N555LV · Boeing 7377BD · Passenger Compartment Equipment
  > TRAY TABLE BROKEN ROW 12F<[01] RESECURED TRAY TABLE ARM SCREW AS PER CMM 25-23-46
- [SDR SWAA2024092039310](https://openairdocs.org/sdr/SWAA2024092039310.md): Slide · dislodged · Sep 19, 2024 · N555LV · Boeing 7377BD · Escape Slide
  > CUSTOMER WALK: R1 SLIDE GUSSET OUT OF SLIDE COVER.<[01] FAULT ACCOMPLISHED ON TTG8Q00VYUCB;[02] FINAL INSPECTION; VERIFIED STEP #1.
- [SDR SWAA2024092037795](https://openairdocs.org/sdr/SWAA2024092037795.md): Skin · damaged · Sep 11, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > ACCOMPLISH REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 120.3 AFT POSITION<[01] ACCOMPLISHED REPAIR AT L/H HORIZONTAL STAB LOWER SKIN AFT POSITION STA 120.3 PER 737-700 SRM 55-10-01-2R REPAIR 11; 24-155-02458-WIP1 (COMPONENT - AAR (MIA) - HORIZONTAL STAB (LH)
- [SDR SWAA2024092037796](https://openairdocs.org/sdr/SWAA2024092037796.md): Skin · damaged · Sep 11, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > ACCOMPLISH REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 120.3 FWD POSITION<[01] ACCOMPLISHED REPAIR AT L/H HORIZONTAL STAB LOWER SKIN FWD POSITION STA 120.3 PER 737-700 SRM 55-10-01-2R REPAIR 11; 24-155-02458-WIP1 (COMPONENT - AAR (MIA) - HORIZONTAL STAB (LH)
- [SDR SWAA2024092036747](https://openairdocs.org/sdr/SWAA2024092036747.md): Skin · damaged · Sep 11, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 15 AFT OF FWD EDGE OF SKIN I/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 15 AFT OF FWD EDGE OF SKIN I
- [SDR SWAA2024092036745](https://openairdocs.org/sdr/SWAA2024092036745.md): Skin · damaged · Sep 11, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 2 FWD OF AFT EDGE OF SKIN O/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 2 FWD OF AFT EDGE OF SKIN O/B
- [SDR SWAA2024092036746](https://openairdocs.org/sdr/SWAA2024092036746.md): Skin · damaged · Sep 11, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 10 FWD OF AFT EDGE OF SKIN O/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 10 FWD OF AFT EDGE OF SKIN O
- [SDR SWAA2024092036062](https://openairdocs.org/sdr/SWAA2024092036062.md): Battery Pack · inoperative · Sep 10, 2024 · N555LV · Boeing 7377BD · Emergency Lighting
  > PAX EMERGENCY LIGHTS FWD ENTRY AND MID CABIN L/H & R/H INOP<[01] REMOVED AND REPLACED PAX EMERGENCY LIGHT BATTERY PACK M1670; M1672 & M1673 I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK NORMAL;[02] VERIFIED STEP 1
- [SDR SWAA2024092034973](https://openairdocs.org/sdr/SWAA2024092034973.md): Door · corroded · Sep 7, 2024 · N555LV · Boeing 7377BD · Fluid Service Doors
  > POTABLE WATER SERVICE DOOR PANEL 146AR STOP PADS HAS CORROSION<[01] RESTORED STOP PADS AT POTABLE WATER SERVICE DOOR PANEL 146AR BACK TO A SERVICABLE CONDITION AS PER SOPM 20-30-03; SRM 51-10-02-0G-0; AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.;[02] FINAL I
- [SDR SWAA2024092034462](https://openairdocs.org/sdr/SWAA2024092034462.md): Skin · damaged · Sep 5, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB UPPER SKIN AT #4 RIB INSTALLATION AREA HAS ELONGATED HOLES<[01] REMOVED DAMAGED AT L/H HORIZONTAL STAB UPPER SKIN AT#4 RIB AREA AS PER SRM 51-10-02-0G-0 AND SRM 55-10-01-2R-3. FABRICATED REPAIR PARTS DOUBLER AND FILLER AT LT HORIZONTAL STAB
- [SDR SWAA2024092034463](https://openairdocs.org/sdr/SWAA2024092034463.md): Skin · damaged · Sep 5, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA HAS ELONGATED HOLES<[01] FAULT ACCOMPLISHED ON ASSIGNED EA 24-155-02458-WIP1 [TTG8Q00VP5ED];[02] CORRECTION TO STEP 1 EA #: FAULT ACCOMPLISHED ON ASSIGNED EA 24-155-02458-WIP1 [TTG8Q00VSG87].;[03] VERIF
- [SDR SWAA2024092032788](https://openairdocs.org/sdr/SWAA2024092032788.md): Skin · damaged · Sep 1, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB UPPER AND LOWER SKIN AT RIB #4 INSTALLATION AREA WITH MULTIPLE ATTACHING HOLES ELONGATED.<[01] REPAIR OF L/HORIZONTAL STAB UPPER SKIN AT #4 RIB INSTALLATION AREA WILL BE ACCOMPLISHED ON CUSTOMER CARD [TTG8Q00VP5EB];[02] REPAIR OF L/HORIZONTA
- [SDR SWAA2024092332503](https://openairdocs.org/sdr/SWAA2024092332503.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACKS FOUND AT HOLES OF LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 AT FASTENER HOLES LOCATED 8';11';15'; 34.5' AND LOWER O/B FLANGE- 34'; FROM FRONT SPAR. CRACKS FOUND AT HOLES OF LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 AT FASTENER HOLES LOCATED
- [SDR SWAA2024092332783](https://openairdocs.org/sdr/SWAA2024092332783.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND AT LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 FASTENER HOLE LOCATED 8' FROM FRONT SPAR<[01] LEFT HORIZONTAL STAB #4 RIB ASSY WAS REPLACED ON TASKCARD TTG8Q00VKHWU.;[02] VERIFIED STEP 1.
- [SDR SWAA2024092332785](https://openairdocs.org/sdr/SWAA2024092332785.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND AT LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 FASTENER HOLE LOCATED 11' FROM FRONT SPAR<[01] LEFT HORIZONTAL STAB #4 RIB ASSY WAS REPLACED ON TASKCARD TTG8Q00VKHWU.;[02] VERIFIED STEP 1.
- [SDR SWAA2024092332786](https://openairdocs.org/sdr/SWAA2024092332786.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND AT LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 FASTENER HOLE LOCATED 15' FROM FRONT SPAR<[01] LEFT HORIZONTAL STAB #4 RIB ASSY WAS REPLACED ON TASKCARD TTG8Q00VKHWU.;[02] VERIFIED STEP 1.
- [SDR SWAA2024092332787](https://openairdocs.org/sdr/SWAA2024092332787.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND AT LOWER I/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 FASTENER HOLE LOCATED 34.5' FROM FRONT SPAR<[01] LEFT HORIZONTAL STAB #4 RIB ASSY WAS REPLACED ON TASKCARD TTG8Q00VKHWU.;[02] VERIFIED STEP 1.
- [SDR SWAA2024092332784](https://openairdocs.org/sdr/SWAA2024092332784.md): Rib · cracked · Aug 30, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK FOUND AT LOWER O/B FLANGE OF LEFT HORIZONTAL STAB RIB #4 FASTENER HOLE LOCATED 34' FROM FRONT SPAR<[01] LEFT HORIZONTAL STAB #4 RIB ASSY WAS REPLACED ON TASKCARD TTG8Q00VKHWU.;[02] VERIFIED STEP 1.
- [SDR SWAA2024092331974](https://openairdocs.org/sdr/SWAA2024092331974.md): Stub Frame · cracked · Aug 29, 2024 · N555LV · Boeing 7377BD · Fuselage Main, Structure
  > TYPICAL CRACK FOUND AT R1 DOOR STUB FRAME JUST ABOVE SEAL DEPRESSOR. CRACK LENGTH: 0.781'.<[01] REMOVED AND REPLACED STUB FRAME AT R1 DOOR SURROUND STRUCTURE SRM 51-40-02-0G-0 AND DWG:141A8370;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.
- [SDR SWAA2024092331723](https://openairdocs.org/sdr/SWAA2024092331723.md): Support Angle · cracked · Aug 28, 2024 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKS FOUND AT FASTENER HOLES #2 AND #16 (I/B TO O/B) AT R/H VAPOR BARRIER UPPER SUPPORT ANGLE.<[01] REMOVED AND REPLACED R/H VAPOR BARRIER UPPER SUPPORT ANGLE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#111A1000 AND DWG#111A4000<BR>FASTENERS COMMON TO RH V
- [SDR SWAA2024092331725](https://openairdocs.org/sdr/SWAA2024092331725.md): Support Angle · cracked · Aug 28, 2024 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKS FOUND AT OPEN FASTENER HOLES #2 AND #44 ( I/B TO O/B) AT L/H VAPOR BARRIER UPPER SUPPORT ANGLE.<[01] REMOVED AND REPLACED L/H VAPOR BARRIER UPPER SUPPORT ANGLE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#111A1000 AND DWG#111A4000<BR>FASTENERS COMMON T
- [SDR SWAA2024092331502](https://openairdocs.org/sdr/SWAA2024092331502.md): Drip Tray · cracked · Aug 28, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer Miscellaneous Structure
  > FWD CONTROL MECHANISM DRIP SHIELD CRACKED<[01] RECEIVED NEW STABILIZER FORWARD CONTROL MECHANISM DRIP SHIELD. TO BE INSTALLED ON ITEM#TTG8Q004CX35;[02] VERIFIED STEP 1 NEW STABILIZER FORWARD CONTROL MECHANISM DRIP SHIELD. TO BE INSTALLED ON ITEM#TTG8Q004CX35
- [SDR SWAA2024092031727](https://openairdocs.org/sdr/SWAA2024092031727.md): Floor Support · corroded · Aug 28, 2024 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION MULTIPLE SPOTS AT AFT CARGO FLOOR STRUCTURE RT Z CHANNEL FWD BULKHEAD TO STA 727D.<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS FOUND OUT OF LIMITS ON OLD AFT CARGO RIGHT Z CHANNEL. REMOVED; LOCATED AND DRILLED; TREATED A
- [SDR SWAA2024092031728](https://openairdocs.org/sdr/SWAA2024092031728.md): Floor Support · corroded · Aug 28, 2024 · N555LV · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION MULTIPLE SPOTS AT AFT CARGO FLOOR STRUCTURE RT Z CHANNEL FROM STA 727D TO STA 767.<[01] RIGHT Z CHANNEL FOUND OUT OF LIMITS; TO BE REPLACED ON TASKCARD TTG8Q00VJ8P9. CORRECTION TO STEP 1: REMOVED CORROSION FROM AFT CARGO RT 'Z' CHANNEL FROM STA 727D
- [SDR SWAA2024092330921](https://openairdocs.org/sdr/SWAA2024092330921.md): Attach Angle · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CENTER WING REAR SPAR VAPOR WEB LOWER ATTACHMENT ANGLE STA 663 RBL 8; CRACK NOTED.<[01] RH CENTER WING REAR SPAR VAPOR WEB LOWER ATTACHMENT ANGLE STA 663 REPLACED.<BR>WORK ACCOMPLISHED ON TASKCARD#TTG8Q00VHYVM;[02] TTG8Q00VHYVM;[03] CORRECTION TO STEP 2: VERIF
- [SDR SWAA2024092330922](https://openairdocs.org/sdr/SWAA2024092330922.md): Angle · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Fuselage Main, Bulkhead
  > CENTER WING REAR SPAR VAPOR WEB LOWER ATTACHMENT ANGLE STA 663 LBL 8; CRACK NOTED.<[01] LH CENTER WING REAR SPAR VAPOR WEB LOWER ATTACHMENT ANGLE STA 663 REPLACED.<BR>WORK ACCOMPLISHED ON TASKCARD#TTG8Q00VJ02Y;[02] VERIFIED STEP 1
- [SDR SWAA2024092330916](https://openairdocs.org/sdr/SWAA2024092330916.md): Rib · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER INSPAR RIB ASSY. #4 (STB STA 120.30); STIFFENER #2 CRACK NOTED AT LOWER AREA.<[01] ASSEMBLY/REPLACEMENT OF NEW RIB #4 AT LEFT HORIZONTAL STABILIZER STA 120.3 ACCOMPLISHED ON TASKS [TTG8Q00VKHWU] [TTG8Q00VGLVC].;[02] VERIFIED STEP 1.
- [SDR SWAA2024092330917](https://openairdocs.org/sdr/SWAA2024092330917.md): Rib · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER INSPAR RIB ASSY. #4 (STB STA 120.30); STIFFENER #3 CRACK NOTED AT LOWER AREA.<[01] REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER IN SPAR RIB #4 ACCOMPLISHED ON [TTG8Q00VKHWU] INSTALLATION ACCOMPLISHED ON [TTG8Q00VGLVC].;[02] VERIFIED
- [SDR SWAA2024092330419](https://openairdocs.org/sdr/SWAA2024092330419.md): Bracket · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Wing Miscellaneous Structure
  > LH WING REAR SPAR ATTACH BRACKET (LOCATED FWD OF DOOR 551DB FWD OB CORNER) CRACKED.<[01] REMOVED AND REPLACED LH WING REAR SPAR ATTACH BRACKET (LOCATED FWD OF DOOR 551DB FWD OB CORNER PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
- [SDR SWAA2024092030914](https://openairdocs.org/sdr/SWAA2024092030914.md): Vapor Barrier · delaminated · Aug 26, 2024 · N555LV · Boeing 7377BD · Fuselage Main, Bulkhead
  > ACCOMPLISH REPAIR OF L/H VAPOR BARRIER AS REQUIRED<[01] REPAIRED BOTH SIDE OF L/H VAPOR BARRIER PER B737 SRM 51-70-04-2R-10 PARAGRAPH 4.F; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N.2. MATERIALS USED RESIN EY3804 P/O#2080789; CLOTH P/O#1690463. TOOLS USED TEMP CONTR
- [SDR SWAA2024092030915](https://openairdocs.org/sdr/SWAA2024092030915.md): Vapor Barrier · delaminated · Aug 26, 2024 · N555LV · Boeing 7377BD · Fuselage Main, Bulkhead
  > ACCOMPLISH REPAIR OF R/H VAPOR BARRIER AS REQUIRED<[01] REPAIRED BOTH SIZE OF R/H VAPOR BARRIER PER B737 SRM 51-70-04-2R-10 PARAGRAPH 4.F; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N.2. MATERIALS USED RESIN EY3804 P/O#2080789; CLOTH P/O#1690463. TOOLS USED TEMP CONTR
- [SDR SWAA2024092030923](https://openairdocs.org/sdr/SWAA2024092030923.md): Rib · cracked · Aug 26, 2024 · N555LV · Boeing 7377BD · Wing, Rib/Bulkhead
  > RT WING TE DEFLECTION CONTROL RIB CRACKED AT PANEL/SERRATED PLATE ATTACHED AREA.<[01] ACCOMPLISHED REPAIR OF R/W T/E DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3.;[02] VERIFIED REPAIR OF R/W T/E DEFLECTION CONTROL RIB UPPER TAB;[03] REJECT....T/C TTG

Next page: https://openairdocs.org/aircraft/N555LV/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 = 'N555LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N555LV/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.