# Service difficulty reports: Boeing 727-2D4

A list on [Boeing 727-2D4](https://openairdocs.org/model/boeing-727-2d4.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 279 reports

- [SDR FDEA201212144302](https://openairdocs.org/sdr/FDEA201212144302.md): Window · cracked · Dec 14, 2012 · N287FE · Boeing 7272D4 · Flight Compartment Windows
  > DURING CRUISE, FL320, PILOTS L1 WINDOW OUTER FRAME CRACKED. MUTIPLE BROWN MARKS ALONG TOP WITH DELAMINATION. COMPLIED WITH QRH, TURNED OFF L1 WINDOW HEAT. INSPECTED WINDOW AND FOUND GLASS PANELS TO BE OK. THE INNER VINYL PANEL IS SEPARATED. 1 "CRACK" STA
- [SDR FDEA201208313201](https://openairdocs.org/sdr/FDEA201208313201.md): Slide · damaged · Aug 31, 2012 · N288FE · Boeing 7272D4 · Escape Slide
  > INDIVIDUAL EXPULTED THE EVACUATION SLIDE. R & R L1 DOOR ESCAPE SLIDE IAW MM 25-60-015-2.
- [SDR FDEA201207292814](https://openairdocs.org/sdr/FDEA201207292814.md): Battery Pack · discharged · Jul 29, 2012 · N288FE · Boeing 7272D4 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS ARMED AND ACFT POWER OFF. BOTH COCKPIT AND ENTRY EMERGENCY LIGHTS, AND EXTERIOR DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERIES IAW MM 33-50-001-0. REPLACED EXTERIOR DOOR SLIDE POWER SUPPLY IAW 33-50-051-2. ALL LIGHTS OPS CHECKED NOR
- [SDR FDEA201203030767](https://openairdocs.org/sdr/FDEA201203030767.md): Slide · dislodged · Mar 3, 2012 · N288FE · Boeing 7272D4 · Escape Slide
  > ESCAPE SLIDE FELL OUT OF CONTAINER. REINSTALLED DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-60-015-2. ACFT OK FOR SERVICE.
- [SDR FDEA201112305461](https://openairdocs.org/sdr/FDEA201112305461.md): Slide · low pressure · Dec 30, 2011 · N287FE · Boeing 7272D4 · Escape Slide
  > ON INBOUND WALK AROUND, FOUND ESCAPE SLIDE PRESSURE GAUGE READING BELOW LIMITS. R & R ESCAPE SLIDE IAW 25-60-015-2. ACFT OK FOR CONT SERVICE.
- [SDR FDEA201112105237](https://openairdocs.org/sdr/FDEA201112105237.md): Indicator · failed · Dec 10, 2011 · N287FE · Boeing 7272D4 · Airspeed/Mach Indicator
  > CAPT AIRSPEED INDICATOR FAILED ON TAKE OFF. PULLED AND RESET CIRCUIT BREAKER, INDICATOR NORMAL. PERFORMED TEST ON DADC-1 AIR SPEED INDICATOR FAILS TEST. R & R CAPT'S AIRSPEED INDICATOR IAW MM 34-12-021-4. OPS CHECKED IAW MM 34-12-000-5-2, 8A. OPS CHECKED NOR
- [SDR FDEA201110224623](https://openairdocs.org/sdr/FDEA201110224623.md): Battery Pack · inoperative · Oct 22, 2011 · N287FE · Boeing 7272D4 · Emergency Lighting
  > FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK REF AMM 33-50-051-2.
- [SDR FDEA201110194595](https://openairdocs.org/sdr/FDEA201110194595.md): Battery Pack · inoperative · Oct 19, 2011 · N287FE · Boeing 7272D4 · Emergency Lighting
  > FORWARD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK. OPS CHECKED NORMAL IAW MM 33-50-051-2.
- [SDR FDEA201109284194](https://openairdocs.org/sdr/FDEA201109284194.md): Skin · misrepaired · Sep 28, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR UPPER HINGE MISREPAIRED. FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER, AND INSTALLED IAW EA 7-5330-152453.
- [SDR FDEA201109214017](https://openairdocs.org/sdr/FDEA201109214017.md): Web · cracked · Sep 21, 2011 · N288FE · Boeing 7272D4 · Cargo/Baggage Doors
  > CARGO DOOR INNER WEB IS CRACKED AT LIGHTING HOLE NEAR LEADING EDGE. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV103. FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 52-30-1 FIG 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND EA 7-5230-152450.
- [SDR FDEA201109183952](https://openairdocs.org/sdr/FDEA201109183952.md): Skin · gouged · Sep 18, 2011 · N288FE · Boeing 7272D4 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP INBD FAIRING AREA HAS A GOUGE ON L/E SKIN. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 57-10-4 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1 AND EA 7-5750-
- [SDR FDEA201109163900](https://openairdocs.org/sdr/FDEA201109163900.md): Skin · gouged · Sep 16, 2011 · N288FE · Boeing 7272D4 · Trailing Edge Flaps
  > RIGHT WING I/B FOREFLAP O/B L/E GOUGED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-4 FIG 1 REV 103
- [SDR FDEA201109103815](https://openairdocs.org/sdr/FDEA201109103815.md): Shear Tie · corroded · Sep 10, 2011 · N288FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 51-20-1 FIG 7 AND DWG 65-56129 INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.
- [SDR FDEA201109083748](https://openairdocs.org/sdr/FDEA201109083748.md): Shear Tie · damaged · Sep 8, 2011 · N288FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > IMPROPER SPACING BETWEEN FASTENERS IN SHEAR TIE AT BS 950A, FORWARD AND AFT, BETWEEN STR 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2 LOCATED,DRILLED AND DEBURRED NEW SHEAR TIE IAW SRM 51-30-5 INSTALLED SHEAR TIE IAW SRM 51-30-2
- [SDR FDEA201109073745](https://openairdocs.org/sdr/FDEA201109073745.md): Vertical Beam · damaged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > 1183 BULKHEAD HAS INSUFFICIENT FASTENER SPACING ON VERTICAL BEAM, LBL 17.8. TRIMMED DAMAGED AREA AT STA 1183 BULKHEAD 3EA AND AFT FLANGE VERTICAL BEAM LBL 17.8, FABRICATED DOUBLER REPAIR, FILLERS, TEE SECTION, SPLICE REPAIRS AND INSTALLED DOUBLER REPAIR,
- [SDR FDEA201109073746](https://openairdocs.org/sdr/FDEA201109073746.md): Skin · gouged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN BS 720C, STR 28L IS GOUGED. REPAIRED.
- [SDR FDEA201109073760](https://openairdocs.org/sdr/FDEA201109073760.md): Skin · damaged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN, BS 464 ABOVE STR 26L HAS A DRILL START. ACCOMPLISHED REPAIR ON NR N00405.
- [SDR FDEA201109073759](https://openairdocs.org/sdr/FDEA201109073759.md): Skin · misrepaired · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN MISREPAIRED AT BS 460, STR 24 TO 26L. CUT OUT DAMAGED SKIN, DOUBLER, AND TRIPLER. FABRICATED STRUCTURAL FILLER, DOUBLER, TRIPLER, AND FILLERS. INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 1B.
- [SDR FDEA201109073744](https://openairdocs.org/sdr/FDEA201109073744.md): Skin · gouged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > BS 720 BELOW S28L SKIN IS GOUGED ABOVE LT RAM AIR DUCT. CUT OUT GOUGED AREA OF SKIN IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 REV 103.
- [SDR FDEA201108173309](https://openairdocs.org/sdr/FDEA201108173309.md): Control Cable · broken · Aug 17, 2011 · N287FE · Boeing 7272D4 · Trailing Edge Flap Actuator
  > ON CLIMBOUT THRU 20K NOTICED OCCASIONAL VIBRATION IN THE CONTROL COLUMN SPOILERS WERE SLIGHTLY DEPLOYED. NUMEROUS RESETS WITH THE SPOILER HANDLE. SLIGHTLY DEPLOYING SPOILERS DID NOT HELP. ON BLOCK IN DISCOVERED LT INBD FLAP OUTER CABLE BROKEN, ALONG WITH A
- [SDR FDEA201106102198](https://openairdocs.org/sdr/FDEA201106102198.md): Skin · misrepaired · Jun 10, 2011 · N287FE · Boeing 7272D4 · Cargo/Baggage Doors
  > C2 DOOR EXTERIOR SKIN AFT LOWER EDGE HAS FASTENERS WITH IMPROPER SPACING. REMOVED EXISTING REPAIR ANGLE IAW SRM 51-30-2. FABRICATED REPAIR ANGLE, FILLER, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW EA 7-5230-136769.
- [SDR FDEA201106092171](https://openairdocs.org/sdr/FDEA201106092171.md): Skin · gouged · Jun 9, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED DAMAGED UPPER INNER SKIN SECTION, FABRICATED & INSTALLED NEW INNER SKIN IAW SRM 51-30-2, SRM 51-10-2 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201106092170](https://openairdocs.org/sdr/FDEA201106092170.md): Web · cracked · Jun 9, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Structure
  > AFT AIRSTAIRS LT LOWER TORQUE BOX UPPER WEB IS PUNCTURED AND CRACKED AT BS 1225, (BELOW BAZOOKA VALVE STAND-OFF) CUTOUT DAMAGE ON LT LWR TORQUE BOX UPPER WEB IAW SRM REV 103, 51-40-2 FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51
- [SDR FDEA201106062131](https://openairdocs.org/sdr/FDEA201106062131.md): Frame · corroded · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > CORROSION FWD SIDE STA 1166 FRAME STR 21L. REMOVED DAMAGED FRAME SECTION, FABRICATED NEW FRAME SECTION & 2 EA. SPLICES, INSTALLED NEW FRAME IAW SRM 51-30-2, SRM 53-10-2 FIG 5, SRM 51-20-1, SRM 51-10-2 & SRM 51-40-3 FIG 1 AND DWG 65-16549.
- [SDR FDEA201106062133](https://openairdocs.org/sdr/FDEA201106062133.md): Tripler · corroded · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INNER SKIN TRIPLER STA. 1164 STR 21L REMOVED DAMAGED INNER SKIN TRIPLER, FABRICATED & INSTALLED NEW TRIPLER AT BS 1164 IAW SRM 51-10-2, SRM 51-30-2 & DWG 65-25607.
- [SDR FDEA201106062134](https://openairdocs.org/sdr/FDEA201106062134.md): Tee Fitting · damaged · Jun 6, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > C2 DOOR CUTOUT LOWER SECTION, INNER CHORD HAS DOUBLE DRILLED HOLES AND HOLES WITH INSUFFICIENT SPACING AT RBL 21 BETWEEN BS 980- BS 990. REMOVED C2 DOOR CUTOUT FITTING AND TRANSITION FITTING FOR ACCESS AND REMOVED TEE FROM STA 950D TO 1010 IAW SRM 51-30-2.
- [SDR FDEA201106042112](https://openairdocs.org/sdr/FDEA201106042112.md): Skin · dented · Jun 4, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > LT SIDE OF FUSELAGE HAS A DENT AT BS 1260 BETWEEN STRINGER 21L AND 22L. CUTOUT DAMAGE AREA ON LT SIDE OF FUSELAGE BS 1260 BETWEEN STR 21L AND 22L IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3.063 IAW SRM 53-30-3. INSTALLED DOUBLER IAW SRM 53-30-3, FIG 1.
- [SDR FDEA201106012080](https://openairdocs.org/sdr/FDEA201106012080.md): Skin · gouged · Jun 1, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > INNER SURROUND SKIN GOUGED STA 620, STR 16L. REMOVED MCD INNER SURROUND SKIN LOWER SECTION, FABRICATED & INSTALLED NEW INNER LOWER SKIN IAW SRM 51-30-2, SRM 51-10-2 & DWG 53FX1535 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201105312034](https://openairdocs.org/sdr/FDEA201105312034.md): Stringer · corroded · May 31, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27R AT BS 720F. CUTOUT DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND SPLICE REPAIR IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.
- [SDR FDEA201105282014](https://openairdocs.org/sdr/FDEA201105282014.md): Structure · cracked · May 28, 2011 · N287FE · Boeing 7272D4 · Trailing Edge Flaps
  > LEFT I/B FLAP, AFT FLAP I/B TRACK CUTOUT CRACKED. REMOVED MID FLAP LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD IAW SRM 57-50-2 FIG 5 AND 51-30-5. INSTALLED I/B LT MID FLAP CHORD IAW SRM 51-30-2, REV 103
- [SDR FDEA201105241956](https://openairdocs.org/sdr/FDEA201105241956.md): Skin · corroded · May 24, 2011 · N287FE · Boeing 7272D4 · Rudder, Plate/Skin
  > UPPER RUDDER RT SIDE HAS SMALL AREA OF CORROSION ON EXTERIOR SKIN AT TOP OF RUDDER. REMOVED CORROSION ON RH SIDE OF UPPER RUDDER IAW SRM REV 103, 51-10- 6. FABRICATED DOUBLER IAW SRM 55-20-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-20 AND 55-20-3 FIG 1 AND EA
- [SDR FDEA201105241954](https://openairdocs.org/sdr/FDEA201105241954.md): Bulkhead · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > RT WW BS 870, BULKHEAD IS CRACKED BELOW LOAD CONTROL VALVE, (NDT VERIFIED). CUT OUT DAMAGE ON BULKHEAD BELOW LOAD CONTROL VALVE IAW SRM REV 103, 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-9 FIG 5. INSTALLED DOUBLERS IAW SRM 53-10-9 FIG 5.
- [SDR FDEA201105241938](https://openairdocs.org/sdr/FDEA201105241938.md): Frame · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FWD CARGO COMPT LOWER STUB FRAME EXTENSION BETWEEN STR 21L-22L AT BS 600 IS CRACKED AT THE LOWER END, IN THE UPPER RADIUS. REMOVED LOWER STUB FRAME AT BS 600, STRINGER 21L-22L IAW B727 SRM 51-30-2. FABRICATED STUB FRAME IAW DRAWING 53FX1350 REV A. INSTALL
- [SDR FDEA201105241939](https://openairdocs.org/sdr/FDEA201105241939.md): Frame · cracked · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FWD CARGO COMPT. LOWER STUB FRAME EXTENSION BTWN STR 21L-22L AT BS 560 IS CRACKED AT THE LOWER END, IN THE RADIUS. (NDT VERIFIED) REMOVED LOWER STUB FRAME EXTENSION IAW SRM 51-30-2, FABRICATED NEW STUB FRAME IAW DWG 53FX1350, HEAT TREATED STUB FRAME TO -T6 C
- [SDR FDEA201105241953](https://openairdocs.org/sdr/FDEA201105241953.md): Shear Tie · corroded · May 24, 2011 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 700 (AFT SIDE) BETWEEN STRINGER 28L AND 27L.
- [SDR FDEA201105231937](https://openairdocs.org/sdr/FDEA201105231937.md): Web · cracked · May 23, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA RT TORQUE BOX UPPER LIGHTENING HOLE AT BS 1320 HAS A SMALL CRACK AT EDGE. CUT OUT DAMAGED AREA IAW B727 SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2 REV 103.
- [SDR FDEA201105231934](https://openairdocs.org/sdr/FDEA201105231934.md): Skin · gouged · May 23, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 10L. REMOVED DAMAGED MCD INNER SKIN (UPPER AFT) SPLICE, FABRICATED NEW, AND INSTALLED IAW SRM 51-30-2 & SRM 53-10-2 FIG 3A.
- [SDR FDEA201105221927](https://openairdocs.org/sdr/FDEA201105221927.md): Bulkhead · misinstalled · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > BS 1183 PRESSURE BULKHEAD - LBL 17.8 VERT BEAM HAS SEVERAL FASTENERS WITH INSUFFICIENT SPACING. TRIMMED OFF AFT FLANGE AND LOWER END OF 65-16350-299 BEAM, REMOVED EXISTING 65- 16350-284 STRAP. TRIMMED OUT BULKHEAD WEB (3 PLACES) MAINTAINING 0.5" TRIM RADI
- [SDR FDEA201105221928](https://openairdocs.org/sdr/FDEA201105221928.md): Stringer · corroded · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R IS CORRODED AT BS 990. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1 FIG 1 AND STRINGER DRAWING 65-58387, TREATED AND PRIMED IAW SRM 51-10-2
- [SDR FDEA201105221926](https://openairdocs.org/sdr/FDEA201105221926.md): Shear Tie · corroded · May 22, 2011 · N287FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > SHEAR TIE IS CORRODED ON LWR FWD FLANGE AT BS970 BTWN STR 29L - 28L.
- [SDR FDEA201105211924](https://openairdocs.org/sdr/FDEA201105211924.md): Frame · misrepaired · May 21, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Frame
  > FRAME BS 1090 HAS IMPROPER REPAIR BTWN STR 27L - 28L. REMOVED REPAIR FROM BS 1090 FRAME BETWEEN STR 27L- 28L IAW SRM REV 103, 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3, FIG 1 AND 53-10-2, FIG 5 INSTALLED DOUBLER IAW SRM 51-40-3, FIG. 1.
- [SDR FDEA201105191884](https://openairdocs.org/sdr/FDEA201105191884.md): Door Frame · damaged · May 19, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Structure
  > C-1 DOOR CUTOUT, FWD FRAME BS 560, WEB AND OUTER ANGLE HAVE DRILL DAMAGE AT STR 22R, IN TWO PLACES. REMOVED DAMAGED FRAME WEB, FABRICATED & INSTALLED NEW WEB IAW DWG 65-56100, CUTOUT BS 560 CHORD, FABRICATED REPAIR PARTS & INSTALLED REPAIR IAW EA 7-5310-151200
- [SDR FDEA201105181942](https://openairdocs.org/sdr/FDEA201105181942.md): Web · cracked · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, RT LOWER TORQUE BOX INBD WEB HAS A CRACK AT EDGE OF UPPER ROW RIVET. CUT OUT DAMAGED AREA IAW SRM REV 103 51-10-1. FABRICATED FILLER & DOUBLER IAW SRM 53-10-2 & 51-40-2 FIG 1. INSTALLED FILLER & DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105181940](https://openairdocs.org/sdr/FDEA201105181940.md): Web · cracked · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, RT LWR TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE AT BS 1223, 7 INCHES. CUT OUT DAMAGED AREA IAW SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105181941](https://openairdocs.org/sdr/FDEA201105181941.md): Web · punctured · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LT LOWER TORQUE BOX UPPER WEB HAS PUNCTURE HOLE AT STAND-OFF BRACKET. CUT OUT DAMAGE IAW SRM REV 103 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201105182015](https://openairdocs.org/sdr/FDEA201105182015.md): Stringer · corroded · May 18, 2011 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L IS CORRODED WITH EXFOLIATION BETWEEN BS 970-990. REMOVED SECTION OF STRINGER 27L BETWEEN BS 970 AND 990 IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER SECTION IAW SRM 53-10-3 FIG 1. INSTALLED FILLER AND REPAIR SECTION IAW SRM 53-10-3 F
- [SDR FDEA201103010804](https://openairdocs.org/sdr/FDEA201103010804.md): Switch · failed · Mar 1, 2011 · N288FE · Boeing 7272D4 · Leading Edge Slat Control System
  > AFTER TAKEOFF LEADING EDGE FLAPS FAILED TO INDICATE RETRACTED. FE PANEL SHOWED NR 2 LED NOT RETRACTED. FOUND SWITCH S203 FROZEN AND VERY HARD TO MOVE. REPLACE SWITCH 203 REF WDM27-81-02 AND MM 27-82-001-4. OPS CHECK NORMAL ACFT OK FOR SERVICE.
- [SDR FDEA201008293174](https://openairdocs.org/sdr/FDEA201008293174.md): Light · failed · Aug 29, 2010 · N288FE · Boeing 7272D4 · Emergency Lighting
  > DURING MAINT PRE-DEPARTURE CHECKS OF EMERGENCY EXIT LIGHTING, NOTED THAT EXIT LIGHT OVER L1 DOOR IS DIM AND FLICKERING. REMOVED COVER AND SWITCHED LIGHT "ON" IT IS BRIGHT & STEADY. REMOVED LIGHT AND AGAIN, BRIGHT AND STEADY ON BATTERY PACK. WHEN INSTALLED IN
- [SDR FDEA201008173014](https://openairdocs.org/sdr/FDEA201008173014.md): Gyro · failed · Aug 17, 2010 · N288FE · Boeing 7272D4 · Attitude Gyro and Indicating System
  > DURING FLT, HSI SHOWS HDG FLAG RAN QRH HSI WORKS WHEN SWITCHED TO BOTH ON 2. DIVERTED TO ALTERNATE STA R & R NR 1 DG IAW M/M 34-21-071-4-0. OPS CHECK NORMAL, OK FOR SVC. ACFT IS NOT CAT II IAW GMM 6-5-400, CAT II CHECK.
- [SDR FDEA201007142508](https://openairdocs.org/sdr/FDEA201007142508.md): Element · inoperative · Jul 14, 2010 · N287FE · Boeing 7272D4 · Overheat Detection
  > AT FL 350 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH EMERGENCY PROCEDURE WHICH REQUIRES TURNING OFF RT PACK, WITH ONLY THE LT PACK ON ACFT WOULD NOT MAINTAIN CABIN ALTITUDE. WE HAD TO DECEND TO 11,000 FT TO GET CABIN ALT TO 9,500 FT. R & R R

Next page: https://openairdocs.org/model/boeing-727-2d4/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 aircraft_model_key = '7272D4'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2d4/reports

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