# Service difficulty reports: N7854B

A list on [N7854B](https://openairdocs.org/aircraft/N7854B.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 · 204 reports

- [SDR SWAA2026061612709](https://openairdocs.org/sdr/SWAA2026061612709.md): Lamp · inoperative · Jun 16, 2026 · N7854B · Boeing 73771B · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS R2 EXTERIOR EMERGENCY EXIT LIGHT IAW AMM 33-51-01.
- [SDR SWAA2025050666893](https://openairdocs.org/sdr/SWAA2025050666893.md): Light · inoperative · May 3, 2025 · N7854B · Boeing 73771B · Emergency Lighting
  > EMERGENCY EXIT WALL LIGHT AFT OF RH EMERGENCY DOOR IS INOP<[01] R/R EMERG EXIT WALL LIGHT ASSY AFT OF RH EMERG DOOR PER AMM 33-51-01. OPS CHECKS GOOD.
- [SDR SWAA2025042125630](https://openairdocs.org/sdr/SWAA2025042125630.md): Handle · loose · Apr 17, 2025 · N7854B · Boeing 73771B · Service Doors
  > FWD GALLEY SERVICE DOOR R1 INTERIOR HANDLE LOOSE.<[01] RE-SECURED FWD GALLEY SERVICE DOOR INTERIOR HANDLE REF AMM 20-50-11.
- [SDR SWAA2025021094295](https://openairdocs.org/sdr/SWAA2025021094295.md): Lamp · inoperative · Feb 8, 2025 · N7854B · Boeing 73771B · Emergency Lighting
  > AFT R/H SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED AFT R/H SERVICE DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2024122680428](https://openairdocs.org/sdr/SWAA2024122680428.md): Light · inoperative · Dec 23, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR IAW AMM 33-51-04; OPS CHECK GOOD.
- [SDR SWAA2024120272936](https://openairdocs.org/sdr/SWAA2024120272936.md): Handle · broken · Nov 30, 2024 · N7854B · Boeing 73771B · Passenger/Crew Doors
  > AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] REPLACED ASSIT HANDLE FROM AFT LAV; AFT LAV ASSIT HANDLE NOW MISSING; OK TO CONTINUE PER MEL 25-10-01 SP1B;[02] INSTALLED AFT LAV HANDLE WHICH WAS REMOVED TO COMPLY WITH MEL 25-10-01 IAW CMM 25-42-60. MEL CLEARED.
- [SDR SWAA2024112670546](https://openairdocs.org/sdr/SWAA2024112670546.md): Isolation Mount · cracked · Nov 22, 2024 · N7854B · Boeing 73771B · Escape Slide
  > AFT ENTRY DOOR FWD SLIDE MOUNT UPPER ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT UPPER ISOLATOR IAW SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024112670547](https://openairdocs.org/sdr/SWAA2024112670547.md): Light · inoperative · Nov 22, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > L/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-01;[02] 02 - INSPECTED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2024102250556](https://openairdocs.org/sdr/SWAA2024102250556.md): Retainer · loose · Oct 19, 2024 · N7854B · Boeing 73771B · Emergency Equipment
  > CUSTOMER REQUEST MAIN ENTRY DOOR SLIDE BAR LOOSE DURING THE DOOR OPERATION (2 TIMES). 2024-573003<[01] PERFORMED AJUST GIRB BAR RETAINER CLIP IN FWD ENTRY DOOR I.AW B737-700 AMM 25-66-01-200-802 STEP 3.B(1)(F) ITEM 4)B);[02] CORRECTED STEP 1 <BR>PERFORMED AJUS
- [SDR SWAA2024102339868](https://openairdocs.org/sdr/SWAA2024102339868.md): Stringer · cracked · Sep 21, 2024 · N7854B · Boeing 73771B · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 15-L LOCATED BETWEEN STA 294.5 AND STA 303.9 AT FWD PASSENGER COMPARTMENT 2024-572947<[01] TOOL USED ON STEP 2 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 20
- [SDR SWAA2024102339513](https://openairdocs.org/sdr/SWAA2024102339513.md): Floorbeam · cracked · Sep 19, 2024 · N7854B · Boeing 73771B · Fuselage Main, Floor Beam
  > AAI REPORT: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 LBL 24.75 2024-572931<[01] REPLACED PANEL BREAK FLOOR STRUCTURE AT STA 540; BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9;SRM 51-40-02-0G-0 DWG
- [SDR SWAA2024102339515](https://openairdocs.org/sdr/SWAA2024102339515.md): Floorbeam · cracked · Sep 19, 2024 · N7854B · Boeing 73771B · Fuselage Main, Floor Beam
  > AAI REPORT: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 RBL 24.75 2024-572932<[01] INSTALLED NEW PANEL BREAK AND PLATE AND FASTENERS FLOOR STRUCTURE AT STA 540; BL 0 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 DWG 14
- [SDR SWAA2024102339202](https://openairdocs.org/sdr/SWAA2024102339202.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO 400 BL0 2024-572914<[01] REPLACED ANGLE LOC. FLOOR STRUCTURE BTW BS 380 UP TO 400 BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 92 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[0
- [SDR SWAA2024102339204](https://openairdocs.org/sdr/SWAA2024102339204.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO BS 400 RBL 10 2024-572916<[01] REPLACED ANGLE LOCATED BTW BS 380 UP TO BS 400 RBL 10 IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV.A<BR>SEE INDIVIDUAL SING-OFF BELLOW;[02] CERTIFIED CORRECTI
- [SDR SWAA2024102339203](https://openairdocs.org/sdr/SWAA2024102339203.md): Angle · cracked · Sep 18, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BTW BS 380 UP TO BS 400 LBL 13 2024-572915<[01] REPLACED ANGLE AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 38 REV- SEE INDIVID
- [SDR SWAA2024102338582](https://openairdocs.org/sdr/SWAA2024102338582.md): Support Angle · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-572892<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV.?<BR>M
- [SDR SWAA2024102338579](https://openairdocs.org/sdr/SWAA2024102338579.md): Support Bracket · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 727 AT LEVEL STR 27R ON FWD PARTITION AT AFT CARGO COMPARTMENT 2024-572887<[01] REPLACED SUPPORT BRACKET LOCATED BS 727 AT LEVEL STR 27R ON FWD PARTITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-0
- [SDR SWAA2024102238577](https://openairdocs.org/sdr/SWAA2024102238577.md): Support · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572885<[01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG#146A7500; SHEET:85;
- [SDR SWAA2024102238580](https://openairdocs.org/sdr/SWAA2024102238580.md): Shield · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 787 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572888<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TE
- [SDR SWAA2024102238581](https://openairdocs.org/sdr/SWAA2024102238581.md): Angle · corroded · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT 2024-572890<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-10-02
- [SDR SWAA2024102238583](https://openairdocs.org/sdr/SWAA2024102238583.md): Web · cracked · Sep 17, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24.75 AT AFT CARGO COMPARTMENT 2024-572893<[01] REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24.75 AT AFT CARGO COMPARTMENT I.A.W DWG 149A8100 SHEET: 1 REV: - AND B737-700 SRM 51-40-02-0G
- [SDR SWAA2024102338079](https://openairdocs.org/sdr/SWAA2024102338079.md): Scuff Plate · cracked · Sep 16, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2024-572857<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: A23046084; DUE DATE 23-MAY-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:1753759; DUE DATE: 07/DEC/24;[03] REPAIRED F
- [SDR SWAA2024102338334](https://openairdocs.org/sdr/SWAA2024102338334.md): Support Bracket · cracked · Sep 16, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-572867<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W DWG 146A7901 SHEET: 66 REV: A AND B737-700 SRM 51-40-02-0G-0; B737-700 SRM 51
- [SDR SWAA2024102338332](https://openairdocs.org/sdr/SWAA2024102338332.md): Angle · cracked · Sep 16, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CRACK ON ANGLE OF ACCESS PANEL 551FB AT LT WING 2024-572864<[01] REPLACED ANGLE OF ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2710 SHEET 8 REV A MEASURE OF CRACK IS L=1.500' TOOL USED CALIPER P/N: 500-196-30 S/N: A23325478 DUE DATE
- [SDR SWAA2024102338078](https://openairdocs.org/sdr/SWAA2024102338078.md): Plate · cracked · Sep 15, 2024 · N7854B · Boeing 73771B · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING 2024-572854<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING I.A.W DWG 115A3712 SHEET: 7 REV: A; DWG 115A3700 SHEET: 41 REV: - AND B737-700 SRM 51-10-02
- [SDR SWAA2024102338077](https://openairdocs.org/sdr/SWAA2024102338077.md): Web · cracked · Sep 15, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CRACK ON WEB LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2024-572852<[01] REPLACED WEB LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0; 51-102G-0 ITEM 9 AND DWG 115A2512 SHEET 14 REV A SEE IN
- [SDR SWAA2024102337956](https://openairdocs.org/sdr/SWAA2024102337956.md): Frame Splice · corroded · Sep 15, 2024 · N7854B · Boeing 73771B · Fuselage Main, Frame
  > CORROSION FRAME STA 500A AND BTW S-25R TO S-26R AND WL 154.0 AT FWD CARGO COMPARTMENT 2024-572841 CORROSION ON SPLICE STA 500A AND BTW S-25R TO S-26R AND WL 154.0 AT FWD CARGO COMPARTMENT.<[01] REPLACED SPLICE AND FASTENERS LOC. FRAME STA 500A AND BTW S-25R TO
- [SDR SWAA2024102337845](https://openairdocs.org/sdr/SWAA2024102337845.md): Seat Track · cracked · Sep 14, 2024 · N7854B · Boeing 73771B · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON CAPTAIN AND F/O SEAT TRACK INBOARD SIDE AT CONTROL CABIN (2EA) 2024-572805<[01] REPLACED ON CAPTAIN AND F/O SEAT TRACK INBOARD SIDE AT CONTROL CABIN (2EA) IAW B737-700 AMM 25-11-11-400-801.;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2024102348913](https://openairdocs.org/sdr/SWAA2024102348913.md): Battery Pack · inoperative · Sep 14, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > INOP BATTERY PACK LOCATED BTW BS 500C AND 500D S-16 AND S-17 LH SIDE ON PASSENGER CABIN 2024-572766<[01] REPLACED BATTERY PACK LOCATED BTW BS 500C AND 500D S-16 AND S-17 LH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS OK.;[02] REPL
- [SDR SWAA2024102348911](https://openairdocs.org/sdr/SWAA2024102348911.md): Battery Pack · inoperative · Sep 14, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > INOP BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN 2024-572769<[01] REPLACED BATTERY PACK LOCATED BTW BS 597 UP TO BS 616 AND S-16 TO S-17 RH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS O
- [SDR SWAA2024102348912](https://openairdocs.org/sdr/SWAA2024102348912.md): Battery Pack · inoperative · Sep 14, 2024 · N7854B · Boeing 73771B · Emergency Lighting
  > INOP BATTERY PACK LOCATED BTW BS 727C UP TO BS 727D S-16 TO S17 LH SIDE ON PASSENGER CABIN 2024-572770<[01] REPLACED BATTERY PACK LOCATED BTW BS 727C UP TO BS 727D S-16 TO S17 LH SIDE ON PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.<BR><BR>TEST IS OK.;[02
- [SDR SWAA2024102337559](https://openairdocs.org/sdr/SWAA2024102337559.md): Skin · cracked · Sep 14, 2024 · N7854B · Boeing 73771B · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-572755<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D;
- [SDR SWAA2024102337747](https://openairdocs.org/sdr/SWAA2024102337747.md): Plate · cracked · Sep 14, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING 2024-572793<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEMP 9.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS
- [SDR SWAA2024102337746](https://openairdocs.org/sdr/SWAA2024102337746.md): Support Angle · cracked · Sep 14, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATE ORSS 270 INTERNAL CAVITY TRAILING EDGE AT LT WING 2024-572791<[01] REPLACED SUPPORT ANGLE LOCATE ORSS 270 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW B737-700 SRM 51-10-02. ITEM 9; SRM 51-40-02 <BR>MEASURE OF CRACK: L= 0.900. T
- [SDR SWAA2024102337742](https://openairdocs.org/sdr/SWAA2024102337742.md): Access Panel · damaged · Sep 14, 2024 · N7854B · Boeing 73771B · Wing, Plate/Skin
  > ELONGATE HOLES ON ACCESS PANEL 561BB AT LEFT WING 2024-572792<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:A21042057 DUE DATE: 17-APR-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 03-APR-25;[03] STEP 12 TOOL USED ULTRASONIC FLAW DETECT
- [SDR SWAA2024102337743](https://openairdocs.org/sdr/SWAA2024102337743.md): Support Bracket · cracked · Sep 14, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOCATED AT LEVEL ORSS 269 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT RT WING 2024-572785<[01] REPLACED SUPPORT BRACKET LOCATED AT LEVEL ORSS 269 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 5
- [SDR SWAA2024102337744](https://openairdocs.org/sdr/SWAA2024102337744.md): Retainer · corroded · Sep 14, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CORROSION ON NUTPLATE RETAINER INTERNAL CAVITY LEADING EDGE LOCATED ORSS 449 AT LT WING 2024-572786<[01] REPLACED NUTPLATE RETAINER ( GANG CHANNEL) INTERNAL CAVITY LEADING EDGE LOCATED ORSS 449 AT LT AND PERFORMED GENERAL VISUAL INSPECTION ON ADJACENT AREA AND
- [SDR SWAA2024102337745](https://openairdocs.org/sdr/SWAA2024102337745.md): Retainer · corroded · Sep 14, 2024 · N7854B · Boeing 73771B · Wing Miscellaneous Structure
  > CORROSION ON NUTPLATE RETAINER INTERNAL CAVITY LEADING EDGE LOCATED ORSS 570 AT LT WING 2024-572787<[01] REPLACED NUTPLATE RETAINER ( GANG CHANNEL) INTERNAL CAVITY LEADING EDGE LOCATED ORSS 570 AT LT AND PERFORMED GENERAL VISUAL INSPECTION ON ADJACENT AREA AND
- [SDR SWAA2024102337551](https://openairdocs.org/sdr/SWAA2024102337551.md): Intercostal · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK INTERCOSTAL WEB LOCATED BETWEEN STA 294.5 AND STA 303.9 AND S-15L AT FWD PASSENGER COMPARTMENT 2024-572737<[01] REPLACED INTERCOSTAL WEB LOCATED BETWEEN STA 294.5 AND STA 303.9 AND S-15L AT FWD PASSENGER COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0
- [SDR SWAA2024102337535](https://openairdocs.org/sdr/SWAA2024102337535.md): Floor Support · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 AT FWD GALLEY AREA 2024-572718<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AN
- [SDR SWAA2024102337529](https://openairdocs.org/sdr/SWAA2024102337529.md): Floorbeam · corroded · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE BEAM BS 986.5 BETWEEN RBL 29 TO RBL 43 AT AFT GALLEY AREA 2024-572703 CORROSION FLOOR STRUCTURE BEAM BS 986.5 BETWEEN RBL 40 TO RBL 43 APPROX. AT AFT GALLEY AREA<[01] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON S
- [SDR SWAA2024102337536](https://openairdocs.org/sdr/SWAA2024102337536.md): Floor Support · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND LBL 12 AT FWD GALLEY AREA 2024-572719<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH
- [SDR SWAA2024102337547](https://openairdocs.org/sdr/SWAA2024102337547.md): Floor Support · corroded · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE INNER CHORD AT RBL 50 AND BTW STA 947.5 AND STA 986.6 AND WL 210 AFT GALLEY AREA. 2024-572733<[01] TOOL USED STEP 5: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221859911; DUE DATE: 17 NOV 24.;[02] EVALUATED CORROSION FLOOR STRUCTURE I
- [SDR SWAA2024102337549](https://openairdocs.org/sdr/SWAA2024102337549.md): Frame · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Main, Frame
  > CRACK FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN 2024-572738<[01] PERFORMED TRIM OUT ON FRAME BS 312 LOCATED BETWEEN STRINGER 5L TO STRINGER 6L AT PASSENGER CABIN I.A.W EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERF
- [SDR SWAA2024102337550](https://openairdocs.org/sdr/SWAA2024102337550.md): Tie Clip · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP LOCATED AT STA 277 AND S-10R AT PASSENGER CABIN 2024-572739<[01] REPLACED TIE CLIP LOCATED AT STA 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DRAWING 141A1110 SHEET: 18 REV: -; DRA
- [SDR SWAA2024102337543](https://openairdocs.org/sdr/SWAA2024102337543.md): Slat Track · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Leading Edge Devices
  > CRACK SLAT 2 I/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING 2024-572734<[01] REPLACED SUPPORT ANGLE LOCATED SLAT 2 I/B AUXILIARY TRACK I/B AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND MEASURES OF CRACK IS:2.000 INCHES TOOL USED: CALIPER P/N: 500-196-30 S/N:
- [SDR SWAA2024102237532](https://openairdocs.org/sdr/SWAA2024102237532.md): Floor Support · cracked · Sep 13, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND BL 0 AT FWD GALLEY AREA 2024-572721<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG
- [SDR SWAA2024102336380](https://openairdocs.org/sdr/SWAA2024102336380.md): Strap · corroded · Sep 11, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT STRAP LOCATED ON BS 787 AND STRINGER 26R AFT CARGO COMPARTMENT 2024-572513<[01] REPLACED SUPPORT STRAP LOCATED ON BS 787 AND STRINGER 26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02. MEASURES OF CORROSION ARE: L: 1.1200 IN W: 0.4785 IN
- [SDR SWAA2024102336851](https://openairdocs.org/sdr/SWAA2024102336851.md): Scuff Plate · cracked · Sep 11, 2024 · N7854B · Boeing 73771B · Fuselage Miscellaneous Structure
  > CRACK SCUFF PLATE ON SERVICE DOOR AT FWD GALLEY AREA 2024-572624<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:A23046084;DUE DATE:23-MAY-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1753759; DUE DATE 17-DEC-24 WAS USED ON STEP 4;[03] REPAIRED SCUFF PLATE ON SERVIC
- [SDR SWAA2024102336846](https://openairdocs.org/sdr/SWAA2024102336846.md): Vapor Barrier · cracked · Sep 11, 2024 · N7854B · Boeing 73771B · Fuselage Main, Bulkhead
  > (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED AT BS 663.75 BETWEEN LBL 31.83 TO LBL 5.64 2024-572609 (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED AT BS 663.75 BETWEEN LBL 31.83 TO LBL 5.64 LH SIDE WHEEL WELL COMPARTMENT<[01] TOOL USED HOT BONDER P/N:

Next page: https://openairdocs.org/aircraft/N7854B/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 = 'N7854B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7854B/reports

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