# Service difficulty reports: N7857B

A list on [N7857B](https://openairdocs.org/aircraft/N7857B.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 4 · 190 reports

- [SDR SWAA2026092899589](https://openairdocs.org/sdr/SWAA2026092899589.md): Engine · power loss · Sep 22, 2026 · N7857B · Boeing 73779P · Engine (Turbine/Turboprop)
  > NR 2 ENGINE SLOW TO SPOOL ON SETTING TO POWER PERFORMED TEST 8, ACCELERATION CHECK IAW AMM 71-00-00 AND VERIFIED THAT THE NR 2 ENGINE WOULD MAKE TAKEOFF POWER IAW AMM 71-00-00 AND ALL CHECKED GOOD.
- [SDR SWAA2026081711566](https://openairdocs.org/sdr/SWAA2026081711566.md): Link · worn · Aug 13, 2026 · N7857B · Boeing 73779P · Trailing Edge Flaps
  > LEFT WING NR 2 FLAP SUPPORT FAIRING HAD PLAY. R & R LT FLAP FAIRING SUPPORT LINK AT NR 2 IAW AMM 27-51-28.
- [SDR SWAA2026081307051](https://openairdocs.org/sdr/SWAA2026081307051.md): Control Rod · loose · Aug 9, 2026 · N7857B · Boeing 73779P · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE IS LOOSE. FOUND FORWARD ENTRY DOOR HAVING SOFT UNLATCHING & LOWER CONTROL ROD JAM NUT LOOSE. READJUSTED LOWER CONTROL ROD ON FWD ENTRY DOOR IN REF 52-11-00. OPS CHECK GOOD & NO OTHER DEFECTS NOTED
- [SDR SWAA2026050494234](https://openairdocs.org/sdr/SWAA2026050494234.md): Flashlight · inoperative · Apr 29, 2026 · N7857B · Boeing 73779P · Emergency Equipment
  > AFT F/A FLASHLIGHT RED LIGHT NOT FLASHING. REMOVED AND REPLACED IAW AMM 25-64-00-201-NG.
- [SDR SWAA2026012964857](https://openairdocs.org/sdr/SWAA2026012964857.md): Battery Pack · corroded · Jan 27, 2026 · N7857B · Boeing 73779P · Emergency Equipment
  > AFT GALLEY MEGAPHONE BATTERY PACK CORRODED. REPLACED AFT GALLEY MEGAPHONE IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2026012964862](https://openairdocs.org/sdr/SWAA2026012964862.md): Lamp · inoperative · Jan 27, 2026 · N7857B · Boeing 73779P · Emergency Lighting
  > RIGHT EMERGENCY LIGHT FWD OF AFT CARGO DOOR, INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-03. OPS CHECKED GOOD.
- [SDR SWAA202601015715](https://openairdocs.org/sdr/SWAA202601015715.md): Data Plate · detached · Jan 1, 2026 · N7857B · Boeing 73779P · Engine (Turbine/Turboprop)
  > ENGINE DATA PLATE, DETACHES FROM THE ENGINE FAN FRAME. THIS ALL EA PROVIDES TEMPORARY RELIEF AND INITIATES EA M-20-172-00810-TLD TO AUTHORIZE A 45-DAY DEFERRAL OF REINSTALLATION OF DATA PLATE OR THE BRACKET AND DATA PLATE ASSEMBLY.
- [SDR SWAA2026F00001](https://openairdocs.org/sdr/SWAA2026F00001.md): Data Plate · loose · Jan 1, 2026 · N7857B · Boeing 73779P · Engine (Turbine/Turboprop)
  > ENGINE DATA PLATE (P/N'S 649-804-020-0, 649-804-023-0, 649-804-024-0, 649-804-027-0), DETACHES FROM THE ENGINE FAN FRAME. THIS ALL EA PROVIDES TEMPORARY RELIEF AND INITIATES EA M-20-172-00810-TLD TO AUTHORIZE A 45-DAY DEFERRAL OF REINSTALLATION OF DATA PLATE O
- [SDR SWAA2026010157157](https://openairdocs.org/sdr/SWAA2026010157157.md): Data Plate · detached · Dec 27, 2025 · N7857B · Boeing 73779P · Engine (Turbine/Turboprop)
  > ENGINE DATA PLATE (P/N'S 649-804-020-0, 649-804-023-0, 649-804-024-0, 649-804-027-0), DETACHES FROM THE ENGINE FAN FRAME. <THIS ALL EA PROVIDES TEMPORARY RELIEF AND INITIATES EA M-20-172-00810-TLD TO AUTHORIZE A 45-DAY DEFERRAL OF REINSTALLATION OF DATA PLATE
- [SDR SWAA2025120139743](https://openairdocs.org/sdr/SWAA2025120139743.md): Counterweight · corroded · Nov 26, 2025 · N7857B · Boeing 73779P · Rudder Control System
  > THE RUDDER COUNTER BALANCE WEIGHT CORRODED AND MISSING PAINT. REPLACED THE RUDDER COUNTER BALANCE WEIGHT IAW CMM 55-40-09.
- [SDR SWAA2025120139731](https://openairdocs.org/sdr/SWAA2025120139731.md): Lamp · inoperative · Nov 26, 2025 · N7857B · Boeing 73779P · Emergency Lighting
  > PASSENGER CABIN LT EMERGENCY EXIT DOOR LIGHT IS INOPERATIVE. REPLACED THE LAMPS IN THE EXIT LIGHT IAW AMM 33-21-00.
- [SDR SWAA2025120139741](https://openairdocs.org/sdr/SWAA2025120139741.md): Attach Bolt · cracked · Nov 26, 2025 · N7857B · Boeing 73779P · Leading Edge Slat Actuator
  > RIGHT WING NR 8 SLAT ACTUATOR, ONE FASTENER CRACKED AT ATTACHMENT POINT. REMOVED AND REPLACED THE RT WING NR 8 SLAT AND OPS CHECKED GOOD IAW AMM 27-81-21.
- [SDR SWAA2025120139744](https://openairdocs.org/sdr/SWAA2025120139744.md): Cover · cracked · Nov 26, 2025 · N7857B · Boeing 73779P · Passenger/Crew Doors
  > FWD ENTRY DOOR LINER HANDLE COVER IS CRACKED. R & R FWD ENTRY DOOR LINER HANDLE COVER IAW AMM 52-11-31.
- [SDR SWAA2025111133110](https://openairdocs.org/sdr/SWAA2025111133110.md): Starter · faulted · Nov 7, 2025 · N7857B · Boeing 73779P · Engine Starter
  > DURING NR 2 ENGINE START. THE ENGINE WOULD NOT ACCELERATE BEYOND 8 PERCENT. R & R THE NR 2 ENG STARTER AIR TURBINE IAW AMM 80-11-01. OPS CHECKED IAW AMM 71-00-00-800-811-F00, OPS CHECKED GOOD.
- [SDR SWAA2025061179863](https://openairdocs.org/sdr/SWAA2025061179863.md): Cover · broken · Jun 9, 2025 · N7857B · Boeing 73779P · Emergency Lighting
  > COVER FOR THE EXIT ROW LIGHT ON THE BULKHEAD OF THE FOS EXIT ROW BROKE OFF.<[01] INSTALLED/SECURED EMERGENCY EXIT LIGHT COVER @RH OVER WING EXIT IAW AMM 33-51-03
- [SDR SWAA2025033119087](https://openairdocs.org/sdr/SWAA2025033119087.md): Plate · cracked · Mar 28, 2025 · N7857B · Boeing 73779P · Wing Main, Frame Structure
  > LT WING; UPPER WING FIXED T/E PANEL STRUCTURE THAT SERRATED PLATE ATTES TO IS CRACKED; PANEL JUST O/B OF 551CT<[01] REPAIRED LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR.;[02]
- [SDR SWAA2025030495136](https://openairdocs.org/sdr/SWAA2025030495136.md): Web · cracked · Feb 11, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS400 TO BS420AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93419<[01] REPLACED WEB LOCATED BTW BS400 TO BS420AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET:2 REV.B.<BR>
- [SDR SWAA2025030494420](https://openairdocs.org/sdr/SWAA2025030494420.md): Skin Panel · delaminated · Feb 8, 2025 · N7857B · Boeing 73779P · Wing, Plate/Skin
  > DELAMINATED FIXED TRAILING EDGE SKIN PANEL UPPER SURFACE AT LH WING 2025-93409<[01] TOOLS USED= CALIPER P/N: 500-197-30; S/N: B20189571; DUE DATE: 06-JUN-25;[02] TOOL USED= SCALE P/N: CR5200; S/N: 8342514625; DUE DATE: 24-FEB-25;[03] TOOL USED= HOT BONDER P/N:
- [SDR SWAA2025030494107](https://openairdocs.org/sdr/SWAA2025030494107.md): Web · cracked · Feb 7, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS440 TO BS460 AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93402<[01] REPLACED WEB LOCATED BTW BS440 TO BS460 AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 3 REV A.<B
- [SDR SWAA2025030494106](https://openairdocs.org/sdr/SWAA2025030494106.md): Web · cracked · Feb 7, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS500 TO BS500A AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93403<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS500 TO BS500A AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505
- [SDR SWAA2025030492777](https://openairdocs.org/sdr/SWAA2025030492777.md): Support · corroded · Feb 3, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS747 RBL22 WL156.5 AFT CARGO COMPARTMENT 2025-93368<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS727 TO BS767 RBL22 WL156.5 AFT
- [SDR SWAA2025030492776](https://openairdocs.org/sdr/SWAA2025030492776.md): Support · corroded · Feb 3, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS807 LBL22 WL156.5 AFT CARGO COMPARTMENT 2025-93369<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS 847 LBL22 WL156.5 AFT CARGO COMPART
- [SDR SWAA2025030492778](https://openairdocs.org/sdr/SWAA2025030492778.md): Angle · cracked · Feb 3, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT 2025-93374<[01] NSTALLED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL
- [SDR SWAA2025030492781](https://openairdocs.org/sdr/SWAA2025030492781.md): Rib · cracked · Feb 3, 2025 · N7857B · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER 2025-93380<[01] REPLACED CHORD OF THE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02;DWG 186A1303 SHEET 1 REV - AND DWG 186A1001 SH
- [SDR SWAA2025030492782](https://openairdocs.org/sdr/SWAA2025030492782.md): Rib · cracked · Feb 3, 2025 · N7857B · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-93381<[01] REPLACED CHORD OF THE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02; DWG 186A1304 SHEET 1 REV - AND DWG 186A1001
- [SDR SWAA2025030492415](https://openairdocs.org/sdr/SWAA2025030492415.md): Support Angle · cracked · Feb 2, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW BS807 TO BS827 AND LBL53 UPPER AREA AT AFT CARGO COMPARTMENT 2025-93367 <[01]. REPLACED ANGLE - SUPPORT LOCATED BTW BS727E TO BS847 AND LBL53 UPPER AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02;
- [SDR SWAA2025030492154](https://openairdocs.org/sdr/SWAA2025030492154.md): Stringer · cracked · Feb 1, 2025 · N7857B · Boeing 73779P · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2025-93339<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130066401 AND DUE DATE: 21-OCT-25.;[02] TOOL USED STEP 6: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28 MAY 25.
- [SDR SWAA2025030491885](https://openairdocs.org/sdr/SWAA2025030491885.md): Support · corroded · Jan 31, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS500 TO BS500D LBL21 AND WL156 FWD CARGO COMPARTMENT 2025-93324<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3.;[02] INSTALLED SUPPORT ZEE LOCATED BTW TO BS400 TO BS 500D LBL 21 WL156 FWD CA
- [SDR SWAA2025030491882](https://openairdocs.org/sdr/SWAA2025030491882.md): Floorbeam · cracked · Jan 31, 2025 · N7857B · Boeing 73779P · Fuselage Main, Floor Beam
  > CRACK PLATE LOCATED BS 540 AT LEVEL BL 0 AT PASSENGER CABIN 2025-93320<[01] REPLACED BREAK ASSY AND FASTENERS LOCATED BS 540 AT LEVEL BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A. SEE INDIV
- [SDR SWAA2025030491881](https://openairdocs.org/sdr/SWAA2025030491881.md): Angle · cracked · Jan 31, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS 500B AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT 2025-93321<[01] REPLACED ANGLE CLIP AND FASTENERS LOCATED BS 500B AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 143A
- [SDR SWAA2025030491883](https://openairdocs.org/sdr/SWAA2025030491883.md): Angle · cracked · Jan 31, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS 500C AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT 2025-93322 <[01]. REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV B. SEE
- [SDR SWAA2025030491884](https://openairdocs.org/sdr/SWAA2025030491884.md): Intercostal · corroded · Jan 31, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BS 492.4 TO BS 500A AT LEVEL STR26R FWD CARGO COMPARTMENT 2025-93323 <[01]. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS 492.4 TO BS 500A AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02
- [SDR SWAA2025030491037](https://openairdocs.org/sdr/SWAA2025030491037.md): Access Panel · cracked · Jan 29, 2025 · N7857B · Boeing 73779P · Fuselage Main, Plate/Skin
  > CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-93279<[01] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[02] TASK COMPLETED
- [SDR SWAA2025030491266](https://openairdocs.org/sdr/SWAA2025030491266.md): Skin · debonded · Jan 29, 2025 · N7857B · Boeing 73779P · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT RT WING 2025-93281<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189443; DUE DATE: 06/MAR/25.;[02] TOOL USED ON STEP 4 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[03] T
- [SDR SWAA2025030490323](https://openairdocs.org/sdr/SWAA2025030490323.md): Battery Pack · inoperative · Jan 27, 2025 · N7857B · Boeing 73779P · Emergency Lighting
  > INOP BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING RT SIDE AT AFT GALLEY AREA 2025-93185<[01] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING RT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CERTIFIED WORK PERFO
- [SDR SWAA2025030490322](https://openairdocs.org/sdr/SWAA2025030490322.md): Battery Pack · inoperative · Jan 27, 2025 · N7857B · Boeing 73779P · Emergency Lighting
  > INOP BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING LT SIDE AT AFT GALLEY AREA 2025-93184<[01] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING LT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CERTIFIED WORK PERFO
- [SDR SWAA2025030489878](https://openairdocs.org/sdr/SWAA2025030489878.md): Nut · deteriorated · Jan 27, 2025 · N7857B · Boeing 73779P · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-93122<[01] REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3G. ITEM
- [SDR SWAA2025030490085](https://openairdocs.org/sdr/SWAA2025030490085.md): Indicator · deteriorated · Jan 27, 2025 · N7857B · Boeing 73779P · Emergency Lighting
  > DETERIORATED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN 2025-93166 <[01]. INSTALLED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [0
- [SDR SWAA2025030489875](https://openairdocs.org/sdr/SWAA2025030489875.md): Scuff Plate · cracked · Jan 26, 2025 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-93118 <[01]. TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: B23399190; DUE DATE: 04 / MAR / 25.; [02] TOOL USED IN STEP 4: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1753759 DUE DATE: 30-JUN-25;[03]
- [SDR SWAA2024101045795](https://openairdocs.org/sdr/SWAA2024101045795.md): Girt Bar · out of adjust · Oct 6, 2024 · N7857B · Boeing 73779P · Emergency Equipment
  > FA REPORTS FWD ENTRY GIRT BAR OUT OF ADJUSTMENT<[01] ADJ FWD EXIT DOOR EVAC SLIDE GIRT BAR BRACKET PER AMM 25-66-00
- [SDR SWAA2024070807958](https://openairdocs.org/sdr/SWAA2024070807958.md): Light · contaminated · Jul 2, 2024 · N7857B · Boeing 73779P · Emergency Lighting
  > ROW 1 AISLE PHOTOLUMINESCENT STRIPS MOISTURE PRESENT.<[01] R&R ROW 1 AISLE PHOTOLUMINESCENT FLOOR STRIPS IAW AMM 25-00-00.
- [SDR SWAA2024050983328](https://openairdocs.org/sdr/SWAA2024050983328.md): Shutoff Valve · failed · May 7, 2024 · N7857B · Boeing 73779P · Fuel Selector/Shut-Off Valve
  > LEFT WING SHUT OFF VALVE INOP<[01] CLEANED AND RESET S/O VLV OVERIDE SW AND FUELING VALVES OPS NORMAL IAW AMM 28-21-51. A/C O K FOR SERVICE.
- [SDR SWAA2023050544157](https://openairdocs.org/sdr/SWAA2023050544157.md): Flap · debonded · May 2, 2023 · N7857B · Boeing 73779P · Trailing Edge Flap Control System
  > LT WING O/B AFT FLAP I/B END UPPER SURFACE REPAIR DISBONDED AND MISSING<[01] REMOVED AND REPLACED AFT FLAP WITH NEW WORK PERFORMED IAW AMM 27-51-22;[02] ENTERED IN ERROR <BR>REMOVED AND REPLACED L/H AFT FLAP WITH NEW WORK PERFORMED IAW AMM 27-51-22
- [SDR SWAA2023032312723](https://openairdocs.org/sdr/SWAA2023032312723.md): Angle · cracked · Mar 5, 2023 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT 2023-116991<[01] REPLACED ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 146A8120 SHEET 31 REV- AND D
- [SDR SWAA2023032304774](https://openairdocs.org/sdr/SWAA2023032304774.md): Angle · cracked · Feb 18, 2023 · N7857B · Boeing 73779P · Fuselage Main, Plate/Skin
  > CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN 2023-116966<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEE
- [SDR SWAA2023032304775](https://openairdocs.org/sdr/SWAA2023032304775.md): Angle · cracked · Feb 18, 2023 · N7857B · Boeing 73779P · Fuselage Main, Plate/Skin
  > CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN 2023-116968<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. SEE
- [SDR SWAA2023032304777](https://openairdocs.org/sdr/SWAA2023032304777.md): Angle · cracked · Feb 18, 2023 · N7857B · Boeing 73779P · Fuselage Main, Plate/Skin
  > CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN 2023-116967<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG
- [SDR SWAA2023032304399](https://openairdocs.org/sdr/SWAA2023032304399.md): Angle · cracked · Feb 17, 2023 · N7857B · Boeing 73779P · Fuselage Main, Plate/Skin
  > CRACK ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT 2023-116961<[01] REPLACED ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG143A1220 SHEET 30
- [SDR SWAA2023032304394](https://openairdocs.org/sdr/SWAA2023032304394.md): Intercostal · corroded · Feb 17, 2023 · N7857B · Boeing 73779P · Fuselage Main, Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS792AT LEVEL STR26R AND WL 154 AFT CARGO COMPARTMENT 2023-116957<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS792AT LEVEL STR26R AND WL 154 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND
- [SDR SWAA2023032304395](https://openairdocs.org/sdr/SWAA2023032304395.md): Support Angle · corroded · Feb 17, 2023 · N7857B · Boeing 73779P · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN STR27L TO STR25R AND WL 162 AT AFT CARGO COMPARTMENT 2023-116959<[01] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN STR27L TO STR25R AND WL 162 AT AFT CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM

Next page: https://openairdocs.org/aircraft/N7857B/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 = 'N7857B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7857B/reports

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