# Service difficulty reports: N246LV

A list on [N246LV](https://openairdocs.org/aircraft/N246LV.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 · 322 reports

- [SDR SWAA2026081857572](https://openairdocs.org/sdr/SWAA2026081857572.md): Vapor Barrier · cracked · Aug 7, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK FOUND IN BS 639 L/H STUB BEAM STRAPS AFT FASTENER HOLE DURING NDI INSPECTION, ENGINEERING REQUIRED CRACK FOUND IN BS 639 L/H STUB BEAM STRAPS AFT FASTENER HOLE DURING NDI INSPECTION ENGINEERING REQUIRED L/H VAPOR BARRIER C/W STA.578-STA.616 VERIFIED STEP
- [SDR SWAA2026070216974](https://openairdocs.org/sdr/SWAA2026070216974.md): Cable · disconnected · Jun 28, 2026 · N246LV · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 15C, EMERGENCY EXIT ROW WILL NOT STAY UPRIGHT. SEAT SECURED UPRIGHT POSITION OK TO CONTINUE PER MEL 25-6-01 SP1B AUTH 326674. RECONNECTED RECLINE CABLE FOR SEAT 15C IAW CMM 25-21-42. OPS CHECK GOOD.
- [SDR SWAA2026030973597](https://openairdocs.org/sdr/SWAA2026030973597.md): Stiffener · cracked · Feb 24, 2026 · N246LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB RIB NR 4, HSS 120, STIFFENER NR 4 LOWER RADIUS CRACKED. REPAIRED IAW SRM 55-10-09-2R-4, REPAIR 4 ON THE LT HORIZONTAL STAB RIB NR 4, STIFFENER NR 4.
- [SDR SWAA2026031172744](https://openairdocs.org/sdr/SWAA2026031172744.md): Floor Panel · pulled · Feb 20, 2026 · N246LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026031072038](https://openairdocs.org/sdr/SWAA2026031072038.md): Megaphone · damaged · Feb 19, 2026 · N246LV · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE HANDLE FASTENER STRIPPED. TASK CARD COMPLETED, REPLACED AFT MEGAPHONE IAW AMM USE OF STANDARD INDUSTRY PRACTICES OPS CHECK GOOD.
- [SDR SWAA2026031072301](https://openairdocs.org/sdr/SWAA2026031072301.md): Light · damaged · Feb 19, 2026 · N246LV · Boeing 7377H4 · Emergency Lighting
  > G1 EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED G1 EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802..
- [SDR SWAA2026031072039](https://openairdocs.org/sdr/SWAA2026031072039.md): Bracket · cracked · Feb 19, 2026 · N246LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > PANEL 551GB INBD BRACKET CRACKED. THE BRACKET WAS REMOVED FROM PANEL 551GB IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026030972037](https://openairdocs.org/sdr/SWAA2026030972037.md): Diffuser · missing · Feb 18, 2026 · N246LV · Boeing 7377H4 · Emergency Lighting
  > CEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IS MISSING DIFFUSER ATTACH CLIP. REMOVED AND REPLACED CEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IAW AMM 33-51-01-960-802.
- [SDR SWAA2026031171727](https://openairdocs.org/sdr/SWAA2026031171727.md): Light · broken · Feb 17, 2026 · N246LV · Boeing 7377H4 · Emergency Lighting
  > LAVATORY A, CENTER FWD LOWER CEILING EXIT LIGHT ASSY HAS BROKEN TABS. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-51-01-960-802 STEP 3. C. (6).
- [SDR SWAA2026031069610](https://openairdocs.org/sdr/SWAA2026031069610.md): Stringer Clip · cracked · Feb 11, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP 2L AT BS 686. FABRICATED AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 144A1106, REV A.
- [SDR SWAA2026031069611](https://openairdocs.org/sdr/SWAA2026031069611.md): Stringer Clip · cracked · Feb 11, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP, BS 706, S6L.. FABRICATED AND INSTALLED A NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 144A1107, REV A.
- [SDR SWAA2026030969606](https://openairdocs.org/sdr/SWAA2026030969606.md): Stiffener · cracked · Feb 11, 2026 · N246LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB RIB #4 (STAB STA 120) STIFFENER #2 LOWER RADIUS IS CRACKED.<[01] REPAIRED IAW SRM 55-10-09-2R-5 REPAIR 5<BR>L/H H. STAB RIB #4 STIFFENER #2;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2026031068185](https://openairdocs.org/sdr/SWAA2026031068185.md): Cover · cracked · Feb 6, 2026 · N246LV · Boeing 7377H4 · Elevator Structure
  > RIGHT ELEVATOR LOWER INBD HINGE COVER PANEL 344GB CRACKED. NEW PANEL 344GB WILL BE IMSTALLED ON TTG8Q01A3LE5 IAW AMM 20-50-11-910-801.
- [SDR SWAA2026031168018](https://openairdocs.org/sdr/SWAA2026031168018.md): Shield · corroded · Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED FWD CARGO FWD SHIELD, BS 420+1 - 420+19, RBL 22, WL 156 HAD MULTIPLE AREAS AROUND NUT PLATE HOLES. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02, & DWG 143A0080, REV-
- [SDR SWAA2026031068180](https://openairdocs.org/sdr/SWAA2026031068180.md): Scuff Plate · cracked · Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFF PLATE CRACKED ON THE AFT EDGE. REMOVED THE COATINGS AND UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). WELDED THE DAMAGED AREA OF SCUFF PLATE IAW SRM 53-10-15-2R-2, STEP 4.B.(4). THE SCUFF
- [SDR SWAA2026030968179](https://openairdocs.org/sdr/SWAA2026030968179.md): Stringer · corroded · Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL153 APROX. REPAIRED PER EA 26-153-00361. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.
- [SDR SWAA2026030968017](https://openairdocs.org/sdr/SWAA2026030968017.md): Shield · corroded · Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 TO BS 794, RBL 22, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02, DWG 146A0081, REV-.
- [SDR SWAA2026031067601](https://openairdocs.org/sdr/SWAA2026031067601.md): Seat Track · corroded · Feb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK, LBL 45, BS 480+11 TOP, BS 500+6 TOP, BS 500B WELL, 500D+15 TOP, & 500D+15 WELL, WL 208. THE SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01A8V2U.
- [SDR SWAA2026031067602](https://openairdocs.org/sdr/SWAA2026031067602.md): Seat Track · corroded · Feb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 25, BS 500+7 TOP, BS 500B+2 TOP, BS 500A+18 TOP, BS 500C+11 TOP, BS 500D+15, WELL, WL 208. THE SEAT TRACK TO BE REPLACED ON CCN TTG8Q01A8V2T.
- [SDR SWAA2026031067808](https://openairdocs.org/sdr/SWAA2026031067808.md): Seat Track · corroded · Feb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PAX CABIN SEAT TRACK, RBL 25, BS 578+16 TOP, BS 663+18 WELL, BS 683+3 TOP, BS 708+8 WELL, BS 727A+8 TOP, WL 208. REMOVED CORROSION ON SEAT TRACK IAW SRM 51-10-02-0G-0. TREAT AND PRIME WILL BE COMPLETED ON CARD: TTG8Q01A8V4N
- [SDR SWAA2026031167430](https://openairdocs.org/sdr/SWAA2026031167430.md): Scuff Plate · cracked · Feb 3, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026031067085](https://openairdocs.org/sdr/SWAA2026031067085.md): Doubler · corroded · Feb 3, 2026 · N246LV · Boeing 7377H4 · Fluid Service Doors
  > LAV SERVICE DOOR HAS CORROSION ON EXTERIOR SURFACE ON PREVIOUS REPAIR DOUBLER. REMOVED AND REPLACED LAV SERVICE DOOR IAW AMM 52-49-07-000-801; AMM 52-49-07-400-801. BOND CHECK GOOD. BONDING METER: ATS312 11/2026. OPS CHECK GOOD.
- [SDR SWAA2026031067429](https://openairdocs.org/sdr/SWAA2026031067429.md): Scuff Plate · cracked · Feb 3, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.
- [SDR SWAA2026031067437](https://openairdocs.org/sdr/SWAA2026031067437.md): Bear Strap · cracked · Feb 3, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK NOTED ON R1 DOOR BEAR STRAP AROUND FASTENER, L: 0.3, BS 291.5+4, BETWEEN S8R - 9R, WL 265. REPAIRED IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.
- [SDR SWAA2026031067041](https://openairdocs.org/sdr/SWAA2026031067041.md): Doubler · cracked · Feb 2, 2026 · N246LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EGPR SURROUND DOUBLER IS CRACKED BS 233, WL 175, 8 INCHES ABOVE S24R. CRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-5. TRIMMED OUT THE DAMAGED AREA OF THE EGPR SURROUND DOUBLER IAW SRM 53-10-15-2R-4, REPAIR 4, PARA 4(C). FABRICATED REPAIR PARTS IA
- [SDR SWAA2026030967042](https://openairdocs.org/sdr/SWAA2026030967042.md): Battery Pack · no test · Feb 2, 2026 · N246LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M1670 FAILS CAPACITANCE TEST. REMOVED, REPLACED, AND PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK M1670 IAW AMM 33-51-06-960-805.
- [SDR SWAA2026030967046](https://openairdocs.org/sdr/SWAA2026030967046.md): Battery Pack · failed · Feb 2, 2026 · N246LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M1669 FAILS CAPACITANCE TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669, OPS CHECK PERFORMED, GOOD FOR SERVICE IAW AMM 33-51-06-960-805.
- [SDR SWAA2026010859138](https://openairdocs.org/sdr/SWAA2026010859138.md): Engine · damaged · Jan 6, 2026 · N246LV · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > AFTER TAKE OFF AT ABOUT 800 FEET BIRD STRIKE NR 1 ENGINE SMELLED IN THE CABIN / FLIGHT DECK. NR 1 ENGINE 100 DEGREES HOTTER, REF LOG PAGE 2953324 FOR ACCOMPLISHMENT OF BIRD STRIKE CONDITIONAL INSPECTION. PERFORMED MT 772-00-00, BIRD STRIKE VISUAL INSPECTION
- [SDR SWAA2026010557431](https://openairdocs.org/sdr/SWAA2026010557431.md): Slide · dislodged · Jan 1, 2026 · N246LV · Boeing 7377H4 · Escape Slide
  > R2 DOOR SLIDE FELL OUT OF BOX. REPACKED AFT SERVICE DOOR SLIDE IAW MT 725-61-06. AC OK FOR SERVICE
- [SDR SWAA2025120442190](https://openairdocs.org/sdr/SWAA2025120442190.md): Fastener · missing · Dec 3, 2025 · N246LV · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR SLIDE COMPARTMENT GIRT BAR RETAINER MISSING FASTNER. INSTALLED THE FASTENER IAW SRM 51-40-02
- [SDR SWAA2025112639309](https://openairdocs.org/sdr/SWAA2025112639309.md): Girt Bar · detached · Nov 23, 2025 · N246LV · Boeing 7377H4 · Escape Slide
  > BRACKET FOR GIRT BAR DETACHED FROM EMERGENCY SLIDE COVER. PERFORMED MX TASK 725-61-06 REM/INST AND PERFORMED EA M-23-125-01839 AND INSTALLED THREADED FASTNER/NUT.
- [SDR SWAA2025092216225](https://openairdocs.org/sdr/SWAA2025092216225.md): Spring · unsecure · Sep 19, 2025 · N246LV · Boeing 7377H4 · Emergency Lighting
  > AFT F/A EMERGENCY EXIT LIGHT SWITCH COVER SPRING INOPERATIVE. SECURED AFT F/A EMERGENCY EXIT LIGHT SWITCH COVER SPRING IAW AMM SIP.
- [SDR SWAA2025070788513](https://openairdocs.org/sdr/SWAA2025070788513.md): Circuit Breaker · tripped · Jul 5, 2025 · N246LV · Boeing 7377H4 · Light System Wiring
  > CIRCUIT BREAKER P18-3 B10 FOUND POPPED ON PREFLIGHT LIGHTING EMERGENCY CHGR<[01] PERFORMED FILM 33-50 TASK 801 RESET C/B & EMERGENCY LIGHTS OPS CHECK OK @ THIS TIME
- [SDR SWAA2025060678633](https://openairdocs.org/sdr/SWAA2025060678633.md): Apu · failed · Jun 5, 2025 · N246LV · Boeing 7377H4 · APU Core Engine
  > DRIVE #2 LIGHT CAME ON DURING LANDING MX VERIFIED APU OIL QTY IS FULL 22-APR-2025 14:21 UTC FAULT: FLIGHT CREW REPORTS #2 ENG DRIVE LIGHT TEMPORARILY ILLUMINATED THEN EXTINGUISHED AFTER LANDING. ACTION: INSPECTED #2 ENG DIG FOUND LOW ON OIL. SERVICED IDG. REF
- [SDR SWAA2025052273416](https://openairdocs.org/sdr/SWAA2025052273416.md): Bracket · bent · May 20, 2025 · N246LV · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY DOOR GIRT BAR BRACKET (ON DOOR) BENT <[01]. ADJUSTED GIRT BAR HOLD BRACKET PER S.I.P.
- [SDR SWAA2024072515996](https://openairdocs.org/sdr/SWAA2024072515996.md): Isolator · broken · Jul 24, 2024 · N246LV · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR SLIDE AFT TOP ISOLATOR BRACKET IS BROKEN.<[01] R&R FWD SERVICE DOOR SLIDE AFT TOP ISOLATOR IAW SRM 51-40-02;
- [SDR SWAA2024062104244](https://openairdocs.org/sdr/SWAA2024062104244.md): Lamp · burned out · Jun 20, 2024 · N246LV · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY CEILING LIGHT BURNED OUT<[01] RELAMPED FWD GALLEY CEILING LT (SERV. DOOR SIDE) PER AMM 33-26-02.
- [SDR SWAA2024041875954](https://openairdocs.org/sdr/SWAA2024041875954.md): Girt Bar · loose · Apr 17, 2024 · N246LV · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR IS LOOSE IN ITS HOLDER<[01] 04 - REPAIRED PER [AMM 25-66-00-201-NG (DOOR-MOUNTED ESCAPE SYSTEM - MAINTENANCE PRACTICES - PERMANENT)] TIGHTENED FWD SERVICE GIRT BAR RETENTION HOOK IAW AMM 25-66-00.
- [SDR SWAA2024041875908](https://openairdocs.org/sdr/SWAA2024041875908.md): Lamp · inoperative · Apr 17, 2024 · N246LV · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR EMERGENCY DOOR LIGHT BY THE L2 DOOR IS INOP. RELAMPED EXTERIOR EMERGENCY DOOR LIGHT BY THE L2 DOOR. OPS CHECK IS GOOD. REF. AMM 33-51-03
- [SDR SWAA2024031354985](https://openairdocs.org/sdr/SWAA2024031354985.md): Panel · cracked · Feb 23, 2024 · N246LV · Boeing 7377H4 · Passenger/Crew Doors
  > CRACK ENTRY DOOR SUPPORT ANGLE PANEL AT AFT GALLEY AREA (1 EA) 2024 123501<[01] REPLACED DOOR SUPPORT ANGLE PANEL AT AFT GALLEY AREA (1 EA) I.A.W B737-700 SRM 51-10-02 ITEM9.;[02] REPLACED DOOR SUPPORT ANGLE PANEL AT AFT GALLEY AREA (1 EA) I.A.W B737-700 SRM 5
- [SDR SWAA2024031255489](https://openairdocs.org/sdr/SWAA2024031255489.md): Light · deteriorated · Feb 23, 2024 · N246LV · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2024-123518<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-400-802
- [SDR SWAA2024031454029](https://openairdocs.org/sdr/SWAA2024031454029.md): Angle · cracked · Feb 20, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS867 AND STR26L AFT CARGO COMPARTMENT 2024-123445<[01] REPLACED ANGLE AND FASTENERS LOCATED BS867 AND STR26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV-.;[02] CORRECTED STEP 1<BR>RE
- [SDR SWAA2024031454031](https://openairdocs.org/sdr/SWAA2024031454031.md): Intercostal · corroded · Feb 20, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 WL156 AND RBL 21.83 AFT CARGO COMPARTMENT 2024-123447<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 767 TO BS 794.3 WL 156 AND RBL 21.83 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02
- [SDR SWAA2024031454032](https://openairdocs.org/sdr/SWAA2024031454032.md): Angle · corroded · Feb 20, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ANGLE LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21.83 AFT CARGO COMPARTMENT 2024-123448<[01] REPLACED ANGLE LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21.83 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. DWG: 146A8123 SHEET:
- [SDR SWAA2024031254028](https://openairdocs.org/sdr/SWAA2024031254028.md): Support · corroded · Feb 20, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS787 LBL 21.83 WL 156.5 AFT CARGO COMPARTMENT 2024-123450<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 130060401; DUE DATE: 20-MAR-24;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727+4? TO BS787 LBL 21.83 WL
- [SDR SWAA2024031453829](https://openairdocs.org/sdr/SWAA2024031453829.md): Angle · cracked · Feb 19, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR25R TO STR27R AFT POSITIO AT AFT CARGO COMPARTMENT 2024-123422<[01] REPLACED ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;
- [SDR SWAA2024031453828](https://openairdocs.org/sdr/SWAA2024031453828.md): Angle · cracked · Feb 19, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BTW BS907 TO BS 927 AND BTW STR25R TO STR 27R FWD POSITION AT AFT CARGO COMPARTMENT 2024-123420<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS 927 AND BTW STR25R TO STR 27R FWD POSITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9
- [SDR SWAA2024031453831](https://openairdocs.org/sdr/SWAA2024031453831.md): Support · cracked · Feb 19, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-123424<[01] REPLACED ANGLE - SUPPORT LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT; IAW BOEING 737-700 SRM 51-10-02 ITEM 9; BOEING 737-700 SRM 51-40-02 AND BOEIN
- [SDR SWAA2024031453729](https://openairdocs.org/sdr/SWAA2024031453729.md): Angle · cracked · Feb 19, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE BS 663.75 AND RBL 9 WL 173.5 AT CENTER WING BOX 2024-123402<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25;[02] REPLACED ANGLE BS 663.75 AND BETWEEN RBL5 TO RBL70 WL 173.5 AT CENTER WING BOX IAW B737-700
- [SDR SWAA2024031453733](https://openairdocs.org/sdr/SWAA2024031453733.md): Bracket · cracked · Feb 19, 2024 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT LT AIR CONDITIONING BAY 2024-123405<[01] REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT LT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G-0.;[02] COMPLETED JOB

Next page: https://openairdocs.org/aircraft/N246LV/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 = 'N246LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N246LV/reports

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