# Service difficulty reports: N7828A

A list on [N7828A](https://openairdocs.org/aircraft/N7828A.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 · 208 reports

- [SDR SWAA2026083132559](https://openairdocs.org/sdr/SWAA2026083132559.md): Slide · out of position · Aug 27, 2026 · N7828A · Boeing 7377CT · Escape Slide
  > CABIN - AFT GALLEY SERVICE DOOR R2 SLIDE GIRT HANGS LOW. REPACKED CABIN AFT GALLEY SERVICE DOOR R2 SLIDE GIRT REF AMM 25-66-01.
- [SDR SWAA2026083122879](https://openairdocs.org/sdr/SWAA2026083122879.md): Panel · cracked · Aug 27, 2026 · N7828A · Boeing 7377CT · Service Doors
  > CABIN - AFT GALLEY SERVICE DOOR R2 LOWER PANEL 844DZ AFT MOUNTING BRACKET CRACKED. R/R AFT GALLEY SERVICE DOOR R2 LOWER PAN ASSY REF AMM 52-41-31.
- [SDR SWAA2026081050870](https://openairdocs.org/sdr/SWAA2026081050870.md): Light · detached · Aug 6, 2026 · N7828A · Boeing 7377CT · Emergency Lighting
  > RT OVERWING AND FWD SERVICE DOOR INDICATOR LIGHTS FELL FROM OVERHEAD PANEL ON TAKEOFF RESECURED RT OVERWING AND FWD SERVICE INDICATOR LIGHTS IAW SIP. OPS CHECK GOOD.
- [SDR SWAA2026070617710](https://openairdocs.org/sdr/SWAA2026070617710.md): Light · broken · Jul 1, 2026 · N7828A · Boeing 7377CT · Emergency Lighting
  > OVERWING EXIT KORRY LIGHT BROKEN. REINSTALLED IAW SIP.
- [SDR SWAA2025062383727](https://openairdocs.org/sdr/SWAA2025062383727.md): Cabin Air Sys · odor · Jun 19, 2025 · N7828A · Boeing 7377CT · Air Distribution System
  > FORWARD FLIGHT ATTENDANTS REPORTED A EXHAUST SMELL ON A CLIMBOUT. NO ABNORMAL SMELLS OR INDICATION ON THE COCKPIT OR AFT SECTION OF THE AIRPLANE <[01]. C/W CONDITIONAL INSPECTION PER MM 05-51-56. R&R BOTH PACKS COALESCER BAGS PER MM 21-51-05. R&R RECIRCULAT
- [SDR SWAA2025043021762](https://openairdocs.org/sdr/SWAA2025043021762.md): Stringer Splice · corroded · Apr 4, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 142811019 DUE DATE: 29-JAN-26.;[02
- [SDR SWAA2025043021682](https://openairdocs.org/sdr/SWAA2025043021682.md): Plate · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INC
- [SDR SWAA2025043021684](https://openairdocs.org/sdr/SWAA2025043021684.md): Plate · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.780
- [SDR SWAA2025043021685](https://openairdocs.org/sdr/SWAA2025043021685.md): Angle · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -
- [SDR SWAA2025043055843](https://openairdocs.org/sdr/SWAA2025043055843.md): Plate · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING 2025-238300<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 215 AT LT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A2001 SHEET:30 REV:A. MEASURE CRACK IS 0.322 INC
- [SDR SWAA2025043055845](https://openairdocs.org/sdr/SWAA2025043055845.md): Plate · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2025-238301<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.780
- [SDR SWAA2025043055846](https://openairdocs.org/sdr/SWAA2025043055846.md): Angle · cracked · Apr 4, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING 2025-238302<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A930 SHEET 8 REV -
- [SDR SWAA2025042955847](https://openairdocs.org/sdr/SWAA2025042955847.md): Stringer Splice · corroded · Apr 4, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER SPLICE 28L STA360 AT EQUIPMENT ELECTRONIC COMP 2025-238305<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 142811019 DUE DATE: 29-JAN-26.;[02
- [SDR SWAA2025043055842](https://openairdocs.org/sdr/SWAA2025043055842.md): Plate · cracked · Apr 3, 2025 · N7828A · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING 2025-238292<[01] REPLACED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS261 AT LT WING IAW. B737-700 SRM 51-40-02-0G AND DWG. 115A2001 SHEET 29 REV - MEASURE CRACK IS L=0.932 IN
- [SDR SWAA2025042955841](https://openairdocs.org/sdr/SWAA2025042955841.md): Frame · cracked · Apr 3, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSENGER CABIN 2025-238282<[01] PERFORMED REPAIR ON FRAME LOCATED BS 727D BTW STR 8R TO STR 9R AT PASSENGER CABIN IAW EA 1-A53-12114 SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED RII
- [SDR SWAA2025043020500](https://openairdocs.org/sdr/SWAA2025043020500.md): Pressure Web · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-238167<[01] TOOL USED ON STEP 6 AND STEP 7:EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; D
- [SDR SWAA2025043020347](https://openairdocs.org/sdr/SWAA2025043020347.md): Threshold · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 16 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED THRESHOLD SHEET AF
- [SDR SWAA2025043020771](https://openairdocs.org/sdr/SWAA2025043020771.md): Floorbeam · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Floor Beam
  > CRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEEN LBL 0 AND LBL 24.75 AT CENTER PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND D
- [SDR SWAA2025043020501](https://openairdocs.org/sdr/SWAA2025043020501.md): Access Panel · delaminated · Apr 1, 2025 · N7828A · Boeing 7377CT · Aerodynamic Fairings
  > DELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 F
- [SDR SWAA2025043020348](https://openairdocs.org/sdr/SWAA2025043020348.md): Scuff Plate · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:1753759; DUE DATE: 30/JUN/25;[03] REPAIRED THE FWD
- [SDR SWAA2025043055801](https://openairdocs.org/sdr/SWAA2025043055801.md): Threshold · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ON THRESHOLD SHEET AFT CARGO COMPARTMENT 2025-238163<[01] REPLACED THRESHOLD SHEET AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 16 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED THRESHOLD SHEET AF
- [SDR SWAA2025043055802](https://openairdocs.org/sdr/SWAA2025043055802.md): Scuff Plate · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2025-238162<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N:1753759; DUE DATE: 30/JUN/25;[03] REPAIRED THE FWD
- [SDR SWAA2025043055807](https://openairdocs.org/sdr/SWAA2025043055807.md): Floorbeam · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Floor Beam
  > CRACK ON BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL 1 AT PASSENGER CABIN 2025-238184<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BETWEEN LBL 0 AND LBL 24.75 AT CENTER PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND D
- [SDR SWAA2025043055804](https://openairdocs.org/sdr/SWAA2025043055804.md): Access Panel · delaminated · Apr 1, 2025 · N7828A · Boeing 7377CT · Aerodynamic Fairings
  > DELAMINATED ACCESS PANEL 193B BODY FAIRING AT LOWER FUSELAGE 2025-238170<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-41435; DUE DATE: 11/APR/25.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 F
- [SDR SWAA2025042955803](https://openairdocs.org/sdr/SWAA2025042955803.md): Pressure Web · cracked · Apr 1, 2025 · N7828A · Boeing 7377CT · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO BS 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 IN. APPROX 2025-238167<[01] TOOL USED ON STEP 6 AND STEP 7:EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; D
- [SDR SWAA2025043020344](https://openairdocs.org/sdr/SWAA2025043020344.md): Access Panel · cracked · Mar 31, 2025 · N7828A · Boeing 7377CT · Aerodynamic Fairings
  > CRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE:
- [SDR SWAA2025043055798](https://openairdocs.org/sdr/SWAA2025043055798.md): Access Panel · cracked · Mar 31, 2025 · N7828A · Boeing 7377CT · Wing, Plate/Skin
  > CRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE:
- [SDR SWAA2025043055740](https://openairdocs.org/sdr/SWAA2025043055740.md): Nut · deteriorated · Mar 29, 2025 · N7828A · Boeing 7377CT · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-237983<[01] REPLACED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW SOPM 20-50-01 REV NO. 38;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2025043055745](https://openairdocs.org/sdr/SWAA2025043055745.md): Doubler · corroded · Mar 29, 2025 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > DOUBLER BTW BS 400 TO BS 420 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR. 2025-237993<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28-MAY-25;[02] PERFORMED REPAIR CATEGORY B IAW EA 25-153-00902. SEE INDIVIDU
- [SDR SWAA2025031704784](https://openairdocs.org/sdr/SWAA2025031704784.md): Battery Pack · failed · Mar 13, 2025 · N7828A · Boeing 7377CT · Emergency Lighting
  > R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. <[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025031704783](https://openairdocs.org/sdr/SWAA2025031704783.md): Battery Pack · failed · Mar 13, 2025 · N7828A · Boeing 7377CT · Emergency Lighting
  > L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. <[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025020693656](https://openairdocs.org/sdr/SWAA2025020693656.md): Light · inoperative · Feb 6, 2025 · N7828A · Boeing 7377CT · Emergency Lighting
  > R1 DOOR OUTER EMERGENCY LIGHT INOP<[01] REPLACED R1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2024110857259](https://openairdocs.org/sdr/SWAA2024110857259.md): Pump · leaking · Nov 6, 2024 · N7828A · Boeing 7377CT · Hydraulic Pump (Electric/Engine), Main
  > HYD SYS B QTY WENT TO 0; FOLLOWED BY ENG HYD LOW PRESS LIGHT.<[01] FOUND B ENGINE DRIVEN HYDRAULIC PUMP LEAKING AT PRESSURE FITTING. DUE TO POSSIBILITY DAMAGE FROM PUMP CAVITATION; REMOVED PUMP AND PRESSURE LINE PER AMM 29-11-11.;[02] INSTALLED B ENGINE HYDRAU
- [SDR SWAA2024100744537](https://openairdocs.org/sdr/SWAA2024100744537.md): Light · missing · Oct 2, 2024 · N7828A · Boeing 7377CT · Emergency Lighting
  > EMERGENCY EXIT OVERHEAD LIGHT MISSING<[01] RELAMPED PER [AMM 33-18-00-960-801-NG (INDICATOR LIGHT - LAMP REPLACEMENT - PERMANENT)]
- [SDR SWAA2024061300962](https://openairdocs.org/sdr/SWAA2024061300962.md): Battery Pack · no test · Jun 13, 2024 · N7828A · Boeing 7377CT · Emergency Lighting
  > EMX BATTERY PACK M01668 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01668 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024061300960](https://openairdocs.org/sdr/SWAA2024061300960.md): Battery Pack · no test · Jun 13, 2024 · N7828A · Boeing 7377CT · Emergency Lighting
  > EMX BATTERY PACK M01669 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01669 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024061300966](https://openairdocs.org/sdr/SWAA2024061300966.md): Skin · cracked · Jun 13, 2024 · N7828A · Boeing 7377CT · Leading Edge Devices
  > LEFT WING #2 SLAT LOWER SKIN HAS A CRACK APPROXIMATELY.3 LONG EXTENDING FROM A FASTENER BELOW ACTUATOR ATTACH POINT. REMOVED AND REPLACED #2 SLAT IAW AMM OPS CHECK GOOD. REMOVED AND REPLACED #2 SLAT IAW AMM 27-81-21 OPS CHECK GOOD.
- [SDR SWAA2023080786040](https://openairdocs.org/sdr/SWAA2023080786040.md): Lens · obstructed · Aug 5, 2023 · N7828A · Boeing 7377CT · Emergency Lighting
  > R WING ESCAPE LOWER EMER LIGHT LENS PAINTED OVER<[01] REMOVED PAINT FROM LENS PER SIP
- [SDR SWAA2023062167907](https://openairdocs.org/sdr/SWAA2023062167907.md): Battery Pack · inoperative · Jun 21, 2023 · N7828A · Boeing 7377CT · Emergency Lighting
  > L/H FWD EMERGENCY LIGHTING BATTERY PACK ONLY LAST 45 SECONDS BEFORE LIGHTS GO OUT.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.
- [SDR SWAA2023050527306](https://openairdocs.org/sdr/SWAA2023050527306.md): Rib · cracked · Apr 13, 2023 · N7828A · Boeing 7377CT · Horizontal Stabilizer, Spar/Rib
  > CRACK ACCESS PANEL 341B RIB LE STA 105.26 AT RH HORIZONTAL STABILIZER 2023-212862<[01] REPLACED RIB LOCATED STA 105.26 AT RH HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DRAWING 186A1304 SHEET 1 REV: -;[02] REPLACED RIB LOCATED STA
- [SDR SWAA2023050524476](https://openairdocs.org/sdr/SWAA2023050524476.md): Support · cracked · Apr 6, 2023 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW BS 727E PLUS 12INCH TO BS 847 LBL 52 AT AFT CARGO COMPARTMENT 2023-212858<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BTW BS 727E PLUS 12INCH TO BS 847 LBL 52 AT AFT CARGO COMPARTMENT IAW B737 - 700 SRM 51-40-02; SRM 5
- [SDR SWAA2023050523372](https://openairdocs.org/sdr/SWAA2023050523372.md): Angle · cracked · Apr 3, 2023 · N7828A · Boeing 7377CT · Wing Spar
  > CRACK FRONT SPAR ANGLE LOCATED FUEL BOOST PUMP IFSS 120 AT RT WING 2023-212848<[01] REPLACED FRONT SPAR ANGLE LOCATED FUEL BOOST PUMP IFSS 120 AT RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWINGS 116A3001 SHEET 11 REV -; 112A2004 SHEET 5 REV -. SEE INDI
- [SDR SWAA2023050522952](https://openairdocs.org/sdr/SWAA2023050522952.md): Battery Pack · faulty · Apr 2, 2023 · N7828A · Boeing 7377CT · Emergency Lighting
  > DOES NOT PASS THE OPERATIONAL TEST ON BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL AFT GALLEY AREA 2023-212845<[01] REPLACED BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL AFT GALLEY AREA IAW BOEING 737-700 AMM 33-51-06-960-805 AND PERFORMED OP
- [SDR SWAA2023050522482](https://openairdocs.org/sdr/SWAA2023050522482.md): Bracket · cracked · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2023-212795<[01] REPLACED SUPPORT BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT.IAW B737 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET 6 REV: - SEE
- [SDR SWAA2023050522488](https://openairdocs.org/sdr/SWAA2023050522488.md): Frame · cracked · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Main, Frame
  > CRACK FRAME ON BS 907 AND BETWEEN STR25R TO STR26R AFT CARGO COMPARTMENT 2023-212796<[01] REPLACED FRAME ON BS 907 AND BETWEEN STR24R TO STR24L AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG# 147A1007; SHEET 42; REV.D. SEE INDIVIDUAL SIGN OFF B
- [SDR SWAA2023050522481](https://openairdocs.org/sdr/SWAA2023050522481.md): Support · cracked · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT (2 EA) 2023-212794<[01] REPLACED ANGLE - SUPPORT AND FASTENERS LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT (2 EA) IAW B737-700 SRM 51-
- [SDR SWAA2023050522479](https://openairdocs.org/sdr/SWAA2023050522479.md): Tie · cracked · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACK TIE CLIP BS 277 STR 10R AT PASSENGER CABIN 2023-212776<[01] REPLACED TIE CLIP BS 277 STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A1110 SHEET 17 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED AS RII <BR>REPL
- [SDR SWAA2023050522253](https://openairdocs.org/sdr/SWAA2023050522253.md): Keelbeam · broken · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Main, Keel
  > BROKEN HANDLE CENTRE TANK SUMP DRAIN (KEEL BEAM) AT LOWER FUSELAGE 2023-212770<[01] REPLACED SUMP DRAIN VALVE(KEEL BEAM) AT LOWER FUSELAGE IAW B737-700 AMM 28-11-41-000-801 AMM 28-11-41-400-801 SEE INDIVIDUAL SIGN BELOW;[02] REPLACED SUMP DRAIN VALVE(KEEL BEAM
- [SDR SWAA2023050522487](https://openairdocs.org/sdr/SWAA2023050522487.md): Support · corroded · Mar 30, 2023 · N7828A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT TEE LOCATED BS794 BETWEEN STR25R TO STR26R AND WL157 AT AFT CARGO COMPARTMENT 2023-212787<[01] REPLACED SUPPORT TEE LOCATED BS794 BETWEEN STR25R TO STR26R AND WL157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND D
- [SDR SWAA2023050521717](https://openairdocs.org/sdr/SWAA2023050521717.md): Stringer · cracked · Mar 28, 2023 · N7828A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 23R AT BS540 FWD CARGO COMPARTMENT 2023-212749<[01] UT EQUIPMENT P/N: 45MG; S/N: 221859911; DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GO

Next page: https://openairdocs.org/aircraft/N7828A/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 = 'N7828A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7828A/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.